Archives West Finding Aid
Table of Contents
Trans World Airlines records, 1929-2006 (bulk 1944-1970)
Overview of the Collection
- Creator
- Trans World Airlines
- Title
- Trans World Airlines records
- Dates
-
1929-2006 (bulk 1944-1970) (inclusive)Date of CollectionDate of Collection
- Quantity
- 188.79 cubic ft. (288 boxes)
- Collection Number
- 02673
- Summary
- The records of Trans World Airlines, containing materials related primarily their engineering, mechanical, and technical operations, from 1929-2001.
- Repository
-
American Heritage Center, University of Wyoming
American Heritage Center
University of Wyoming
1000 E. University Ave.
Dept. 3924
Laramie, WY
82071
Telephone: 3077663756
ahcref@uwyo.edu - Access Restrictions
-
Access Restrictions
There are no access restrictions on the materials for research purposes, and the collection is open to the public.
- Languages
- English
- Sponsor
- The creation of the EAD-version of this finding aid has been made possible through a grant from the National Historic Publications and Records Commission.
Historical NoteReturn to Top
Trans World Airlines, formerly Transcontinental & Western Air, was founded in 1930 by a merger of Pittsburgh Aviation Industries, Western Express, and T.A.T.- Maddox Airlines (founded in 1929 by Charles Lindbergh). Trans World Airlines began all-air coast to coast commercial service in 1930-1931 and was built into an aviation giant by Howard Hughes. TWA merged with American Airlines in 2001.
Content DescriptionReturn to Top
The bulk of the collection's materials date from 1944-1970 and include engineering reports and aircraft data on airplanes used by Trans World Airlines. It also contains TWA aircraft blueprints, engineering orders, manuals, specifications, maintenance and service records, and subject files. Items specific to aeronautical vendors such as British Aircraft Corporation, Boeing, General Electric, and a significant amount of Lockheed files are also present.
Use of the CollectionReturn to Top
Restrictions on Use
Copyright InformationThe researcher assumes full responsibility for observing all copyright, property, and libel laws as they apply.
Preferred Citation
Preferred CitationItem Description, Box Number, Folder Number, Collection Name, Collection Number, American Heritage Center, University of Wyoming.
Administrative InformationReturn to Top
Related Materials
Related MaterialsThere are no known other archival collections created by Trans World Airlines at the date of processing.
Acquisition Information
Acquisition InformationThis material was received from TWA from 1970-1982 and Georgia State University Library, Special Collections and Archives in 2019.
Processing Note
Processing InformationThe collection was processed by Kathryn Brooks and Emily Christopherson in February 2012 and updated by Jamie Greene in February 2021.
Detailed Description of the CollectionReturn to Top
Series I. Administrative, 1929-1972Return to Top
Contains mostly memoranda, correspondence, and notes relating to TWA vendors and internal operations. Also included are publicity materials and speeches.
Container(s) | Description | Dates |
---|---|---|
Box | ||
186 | Advertising and publicity |
1967 |
186 and 287 | Advertising and publicity - Calendars |
1943-2003 |
284 | Advertising and publicity - TWA ephemera |
1956-2000 |
288 | Advertisement - TWA airplane cutout |
1980 |
288 | Advertisement - TWA Magic Carpet |
1960 |
186 | Aircraft - Advanced Technology Transport (ATT) |
1967 |
186 | Aircraft - Boeing 747 - Customer Preference Survey |
1967 |
186 | Aircraft - Boeing 747 - Leasing |
1967 |
186 | Aircraft - Boeing 747 PAA - Contract |
1966 |
186 | Aircraft - Boeing |
1966-1967 |
186 | Aircraft - Convair 880 |
1956-1961 |
186 | Aircraft - Douglas DC-10 (Airbus) |
1967 |
186 | Aircraft - Douglas |
1967 |
186 | Aircraft - Engine numbers |
1968 |
186 | Aircraft - Lockheed C-5A |
1967 |
186 | Aircraft - Lockheed |
1968-1970 |
186 | Aircraft - SST - DCA (Parmet's) |
1966-1967 |
186 | Aircraft - Supersonic |
1966 |
186 | Aircraft - Used |
1967 |
186 | Aircraft - VTOL/STOL |
1967 |
186 | Aircraft - Warranty - Claims |
1967 |
186 | Aircraft |
1967 |
284 | Annual Reports |
1941-1993 |
284 | Articles: "TWA-Death of a Legend" St. Louis Magazine |
July 28, 2006 |
Artifacts: |
||
Box | ||
286 | TWA cup and saucer |
1960 |
286 | TWA airplane model |
1996 |
Books: |
||
Box | ||
284 | Children's books for TWA |
1954 and 1969 |
284 | "Howard Hughes' Airline: An Informal History of TWA" by Robert Serling |
1983 |
284 | "Legacy of Leadership: A Pictorial History of Trans World Airlines" |
1970 |
284 | "TWA Cabin Attendants, Wings of Pride: A Pictorial History, 1935-1985" |
1985 |
284 | "TWA: Kansas City's Hometown Airline" by Julius A Karash and Rick Montgomery |
2001 |
177 | CALTEX Aviation Bulletins |
1956-1957 |
186 | Collision Avoidance - Airborne |
1966 |
186 | Douglas DC-9 (masters) |
1964 |
186 | Emergency evacuation |
1967 |
185 | Financial |
1958-1963 |
59 | Flight Operations Engine Out Ferry Policy |
1964 |
178 | Flight Safety Foundation Design Notes |
circa 1951-1956 |
284 | History of TWA |
1926-2005 |
186 | Inventions and patents |
1966 |
186 | LAC 1649A LD-138 - originals |
1955 |
285 | Management Policy and Procedure manual |
1991 |
288 | Map: Kansas City International Airport expansion (aerial view) |
November 3, 2000 |
284 | Memoranda: |
|
Box | ||
284 | Commissary instruction letter |
1941 |
284 | Hanger circulars |
1936-1941 |
284 | Maintenance service letters |
1941 |
284 | System operations circulars |
1941 |
284 | Menus - Ambassador service |
undated |
178 | News Releases, etc. |
1929, 1969 |
178 and 288 | Newspaper clippings |
1970-2001 |
186 | Noise problems |
1967-1969 |
186 | Northeast Airlines |
1967 |
285 | Pamphlets |
1980-2000 |
178 | Photographs |
1929, undated |
186 | Planning and Research - Monthly Report |
1966 |
186 | Planning and Research - Objectives |
1966 |
186 | Planning and Research - Staff Meetings |
1966 |
Posters: |
||
Box | ||
288 | Employee information and safety posters |
1990-2000 |
288 | Fuel Saver, Cargo, and Station Olympics |
1980-1990 |
288 | Red Worldwide destination posters |
1980-2000 |
288 | Trans World, Boeing 717 airplane |
1980 |
288 | TWA posters, #1-125 |
1990-2000 |
288 | TWA - Coast to Coast in 48 hours: Celebrating our Heritage |
1980 |
288 | TWA travel/destination posters (skiing the Rockies, Lisbon, Egypt, Tel Aviv, Denver, London, Paris, NYC, America |
1980-2000 |
288 | Prints: Trans World Airlines, A Half Century of Service - 1926-1976, 50th anniversary airplane set |
1976 |
Publications: |
||
Box | ||
285 | "Ambassador, Trans World Airlines Magazine" |
1976-2001 |
285 and 288 | "TWA Skyliner" |
1937-2002 |
285 | TWA Travel Tips (France, Portugal, Switzerland, Israel, Ireland) |
1965-1976 |
285 | Safety instructions (for DC9, 727, and 747 airplanes) |
1980-2001 |
178 | Speeches by M. A. Brenner |
1969-1972 |
183 | Speeches |
1966 |
183 | TWA - Continental Airlines contracts |
1967-1968 |
Video: |
||
Box | ||
286 | AA & TWA: The Next Story (VHS) |
2000 |
286 | Flying High: The TWA Story (VHS) |
undated |
286 | TWA, 75th Anniversary Airshow (VHS) |
August 16, 2000 |
Series II. Engineering, 1942-1970Return to Top
Contains records, reports, blueprints, and general documentation of TWA engineering tasks.
Container(s) | Description | Dates |
---|---|---|
Box | ||
275-278 | Blueprints |
1947-1965 |
196 | Convair/Weber Aircraft Corporation - Structural Analysis
Buffets |
1959-1976 |
88 | Cross Index |
undated |
160 | Curtiss-Wright Corporation - Field Engineering Department
Reports |
circa 1954-1959 |
280-283 | Diagrams - LAC - J13-J16, K11-K14, L11, L13 |
undated |
275-278 | Diagrams |
1947-1965 |
178 | Disassembly of B-3 Driftmeter-Gyro |
undated |
40 | Douglas - 20099 - Loading Chart, Equipment List, & Weight
Data Required for Operation of C54-DC Type Airplanes |
1946 February 11 |
40 | Douglas - 3924 - General Aerodynamic Data Concerning the
Characteristics of C-47 Type Cargo Airplanes |
1942-1943 |
40 | Douglas - C-54 Flight Crew Operating Manual |
1953-1960 |
40 | Douglas - OC-7084 - Actual Weight & Balance Model C-47B ,
Airplane no. 3601 |
1944 December 1 |
40 | Douglas - Operating Requirements, Performance, & Other Data
for Douglas DC-3 Type Airplanes |
undated |
40 | Douglas - SM 10840 - C54A & C54B General Performance
Data |
1944-1945 |
40 | Douglas - SM 13091 - Effects of Air Temperature & Runway
Slope on the Take-Off Landing, & Climb Performance of Transport
Aircraft |
1947 September 12 |
60 | Drafting |
1945-1963 |
177 | E.O. Numbers Assigned to Martin Service Bulletins & Service
Information Letters/Cross Index |
undated |
17 | Engine Overhaul Specifications BA & BD & Exhaust
System |
1956-1965 |
17 | Engine Overhaul Specifications DA & EA |
1956-1965 |
201 | Engineering Orders Index |
circa 1950-1959 |
148-156 | Engineering orders |
1952-1962 |
184 | Engineering originals/masters |
1968-1969 |
188 | Engineering originals/masters |
1943-1967 |
156-158 | Engineering reports |
1943-1951 |
98-102 | Engineering/Maintenance Liaison Records |
1950-1960 |
47 | Equip. & Furnishings |
1957-1958 |
184 | General Engineering - 2-Way Distorion Tests |
1942 |
184 | General Engineering - Effect of Aging on Burning Characteristics
of Non-Inflammable Hydraulic Fluids |
1948 |
184 | General Engineering - Flight Performance on XB-25E Plane
#42-32281 in Natural Ice During February, March and April |
1945 |
184 | General Engineering - Forecasting Principles Precipitation
Static |
undated |
184 | General Engineering - Investigation of Tail Dropping on LAC
049 |
1946 |
184 | General Engineering - Numerical Listing of Radio Stock Items
Showing Disposition of Surplus Items |
1944 |
184 | General Engineering - Originals, Vu Graphs, Charts - EAC's Paper
- Flight System |
1965 |
184 | General Engineering - Survey of System Engineering and Overhaul
Base Requirements and Airline Comparison Study |
1946 |
184 | General Engineering - Tests of Briggs Mobile Lube Oil
Clarifier |
circa 1944 |
185 | General Specification for Martin 2-0-2 Pressurized
Airliner |
1949-1950 |
185 | Glenn L. Martin Company - communications |
1951-1952 |
185 | Glenn L. Martin Company - notice of shipment |
1950-1951 |
185 | Inspections, letters, and reports |
1947-1963 |
185 | Liquidometer - communications |
1954-1961 |
178 | Numerical Index - Constellation Service Information
Letters |
1946-1948 |
53 | P/C 515-555-702 Final Repair Costs |
undated |
53 | Plane SFO 101 |
1958 |
19 | Propeller Performance Data |
1946-1957 |
18 | R2800 & BC Overhaul Specifications |
1956-1961 |
215 | Reports 1161-1313 |
1957-1970 |
211 | Reports 684-803 |
1948-1949, 1952-1965 |
212 | Reports 804-875 |
1948-1951 |
213 | Reports 876-991 |
1950-1955 |
214 | Reports 993-1159 |
1953-1966 |
161-162 | Service Bulletins - Airesearch |
1946-1959 |
162-163 | Service Bulletins - Bendix |
1949-1966 |
163 | Service Bulletins - Dynamic Air |
1951-1957 |
163-172 | Service Bulletins - Lockheed |
1945-1965 |
172-175 | Service Bulletins - Wright |
1949-1967 |
175-176 | Service Information Letters - Lockheed |
1945-1950 |
160 | Stanford Research Institute Reports |
1950-1954 |
177 | T.W.A. Compressor Amplifier |
1949-1950 |
177 | T.W.A. Engineering Reports Covering Douglas DC-3
Aircraft… |
circa 1957 |
93 | TWA Base Engineering - 3350 Engine & Power Egg Requirements
Dom. & Intl. Div. for Constellation Sched. |
1947 |
187 | TWA Base Engineering - ATA and TWA Methods of Computing Block to
Block Speeds and Resulting Differences in Payload and Direct
Costs |
1944 |
93 | TWA Base Engineering - Boeing 707 Performance Tests After
Conversion for Army Transport Service |
1942 |
94 | TWA Base Engineering - Comparison of Bendix VS Goodyear Brakes
LAC 049, 749, 749A |
1949 |
93 | TWA Base Engineering - Comparison of Costs per Standard Available
Ton-Miles Flown, TWA, American, & United Airlines First 6
Months |
1946 |
93 | TWA Base Engineering - Comparison of Performance & Economic
Characteristics of Transport A/C |
1943 |
187 | TWA Base Engineering - Comparison of Performance and Economic
Characteristics of Transport Aircraft |
1943 |
187 | TWA Base Engineering - Constellation 49 Modifications - Equipment
Additions Required for Overseas Service |
1945 |
93 | TWA Base Engineering - Constellation Model 49 Modifications &
Equipment Additions Required for Overseas Service |
1945 |
187 | TWA Base Engineering - Convair 880 Flutter Damper
Information |
1960 |
187 | TWA Base Engineering - Course Sensitivity Variations of ILS
Equipments |
1948 |
94 | TWA Base Engineering - Design, Calculations, & Substantiation
of Index Loading Form 0-818 for Constellation 49-25 A/C |
1946 |
187 | TWA Base Engineering - Determination of Cost Characteristics of
DC-3 as a Cargo Airplane |
1945 |
93 | TWA Base Engineering - Determination of Cost Characteristics of
DC3 as Cargo Airplanes |
1945 |
187 | TWA Base Engineering - Determination of Direct Cost
Characteristics of DC-8 Skybus |
1945-1946 |
187 | TWA Base Engineering - Determination of Direct Cost
Characteristics of LAC 49-46-25 and 26 with Outer Wing
Tanks |
1945-1946 |
187 | TWA Base Engineering - Determination of Direct Cost
Characteristics of LAC 49-46-25 and 26 |
1945 |
187 | TWA Base Engineering - Determination of Direct Cost
Characteristics of LAC 49-79-21 and 22 with Outer Wing
Tanks |
1946 |
93 | TWA Base Engineering - Determination of Direct Cost
Characteristics of LAC 49-79-21&-22 with Outer Wing
Tank |
1946 |
187 | TWA Base Engineering - Determination of Direct Cost
Characteristics of LAC 49-79-21 |
1945 |
187 | TWA Base Engineering - Determination of Direct Cost
Characteristics of M202 |
1945 |
187 | TWA Base Engineering - Determination of Revenue and Profit
Possibilities of Transport Aircraft |
1945 |
187 | TWA Base Engineering - Dimensional and Performance Data of
Miscellaneous Aircraft |
1944 |
187 | TWA Base Engineering - Direct Cost Calculations Convair
37 |
1944 |
187 | TWA Base Engineering - Direct Cost Calculations DC-7 |
1944 |
187 | TWA Base Engineering - Direct Cost Calculations LAC
89 |
1944 |
187 | TWA Base Engineering - Economic Analysis of Beechcraft
18-3 |
1943 |
187 | TWA Base Engineering - Economic Analysis of Boeing 307-4 at
Various Landing Weights |
1945 |
187 | TWA Base Engineering - Economic Analysis of Boeing
307B-1 |
1945 |
187 | TWA Base Engineering - Economic Analysis of Boeing
307-J |
1945 |
187 | TWA Base Engineering - Economic Analysis of Boeing
377-10 |
1945 |
187 | TWA Base Engineering - Economic Analysis of Boeing
377-2 |
1944 |
187 | TWA Base Engineering - Economic Analysis of Boeing
377-4 |
1945 |
187 | TWA Base Engineering - Economic Analysis of Convair
110 |
1945 |
187 | TWA Base Engineering - Economic Analysis of Convair 12
Passenger |
1944 |
187 | TWA Base Engineering - Economic Analysis of Convair 28 Passenger
Short-Haul Airplanes |
1944 |
187 | TWA Base Engineering - Economic Analysis of Convair Model
33 |
1944 |
187 | TWA Base Engineering - Economic Analysis of Converted
DC-54A |
1945 |
187 | TWA Base Engineering - Economic Analysis of CW 20E-2 |
1945 |
187 | TWA Base Engineering - Economic Analysis of CW
20E-2A |
1945 |
187 | TWA Base Engineering - Economic Analysis of CW Airplane 20E and
20F |
1944 |
187 | TWA Base Engineering - Economic Analysis of
CW-P-306A |
1945 |
187 | TWA Base Engineering - Economic Analysis of DC-6 |
1944 |
187 | TWA Base Engineering - Economic Analysis of
DC-6-477A |
1945 |
187 | TWA Base Engineering - Economic Analysis of
DC-6-496A |
1945 |
187 | TWA Base Engineering - Economic Analysis of Douglas
DC-4-282A |
1945 |
187 | TWA Base Engineering - Economic Analysis of Fairchild
Packet |
1945 |
187 | TWA Base Engineering - Economic Analysis of Hypothetical 400,000
lb Airplane |
1944 |
187 | TWA Base Engineering - Economic Analysis of LAC 89 |
1945 |
187 | TWA Base Engineering - Economic Analysis of LAC Model
549 |
1945 |
187 | TWA Base Engineering - Economic Analysis of Martin
202 |
1945 |
187 | TWA Base Engineering - Economic Analysis of Republic
RC-2 |
1945 |
187 | TWA Base Engineering - Effect of Utilization of Plane Upon Its
Economic Potential |
1944 |
93 | TWA Base Engineering - Effects of Block Distance & Time Lost
on Block Speed |
1943 |
187 | TWA Base Engineering - Effects of Block to Block Distance and
Time Lost on Block Speed |
1943 |
187 | TWA Base Engineering - En Route Analysis of CW
20E-2A |
1945 |
93 | TWA Base Engineering - Flight Test of Constellation 500 Air
Conditioning & Pressurizing Systems (51 Pass) |
1945 |
187 | TWA Base Engineering - Galley 3 - Stress Analysis Fittings
880 |
1962 |
187 | TWA Base Engineering - Gasoline - Monthly Aviation
Survey |
1945-1946 |
187 | TWA Base Engineering - Instrumentation on Boeing 307B-1 for
Measurement of Prop. and Cabin Pressure |
1945 |
93 | TWA Base Engineering - Interchangeability of Dynamotors for
Localizer Receivers |
1948 |
93 | TWA Base Engineering - Investigation of Hi Fuel Pressures During
Take-off on Boeing 307B-1 |
1946 |
187 | TWA Base Engineering - Investigation of USAF Jet Propulsion
Aircraft |
1945 |
187 | TWA Base Engineering - LAC and Douglas DC-4 Operating Costs and
Payloads for 2393 Mile Trip |
1944 |
187 | TWA Base Engineering - Method for Determining Earning Power of
LAC Constitution for 1500 Mile Trip |
1945 |
187 | TWA Base Engineering - MN-60A Loop Antenna Compensation
Data |
1947 |
187 | TWA Base Engineering - MN-60A Loop Antenna Compensation Data, LAC
49 Centerline Belly Mounting |
1947 |
93 | TWA Base Engineering - Modification of S345 Tone
Generator |
1948 |
93 | TWA Base Engineering - Monthly Aviation Gasoline
Survey |
1945 |
187 | TWA Base Engineering - Northrop All-Wing Transport Direct
Operating Cost Analysis |
1945 |
93 | TWA Base Engineering - Permissible Frequency Separation for
Adjacent Crystals in ARC-1 VHF Transceiver |
1948 |
187 | TWA Base Engineering - Preliminary Investigation of Allowable
Operation Weights for 307B-1 at Albuquerque, Las Vegas, Phoenix, and St.
Louis |
1944 |
94 | TWA Base Engineering - Removable Equipment for 36 Passenger
M202A |
1950 |
94 | TWA Base Engineering - Removable Equipment for 49 Passenger
749A |
1950 |
94 | TWA Base Engineering - Removable Equipment for 57 Passenger
Constellation A/C |
1950 |
94 | TWA Base Engineering - Removable Equipment for 81 Passenger
Constellation A/C |
1950 |
94 | TWA Base Engineering - Service Experience of Ball Type &
Chrome Plated Body Oil Pressure Relief Valves Installed in WAC Cyclone
G202A |
1945 |
94 | TWA Base Engineering - Service Experience With BG Spark Plugs
Type RB19R in WAC C9 & C18 Engines |
1946 |
93 | TWA Base Engineering - Service Performance of Wright A/C Engines
in TWA Operations for 1934 through 1943 |
1944 |
94 | TWA Base Engineering - Standard & Removable Equipment CAC
749-79-22 |
1949 |
187 | TWA Base Engineering - Standardized Cost Formulas |
1943 |
93 | TWA Base Engineering - Standardized Cost Formulas |
1943 |
94 | TWA Base Engineering - Summary of Stress Analysis of TWA
Constellation Lounge Seat & Installation |
1951 |
187 | TWA Base Engineering - Terrain Warning Indicator Supply Voltage
Under Typical Flight Conditions |
1948 |
187 | TWA Base Engineering - TWA Standard Aircraft Specification
Index |
1945 |
94 | TWA Base Engineering - Weight & Balance Analysis of TWA
M303 |
1946 |
94 | TWA Base Engineering - Weight & Balance Calculations for
Average TWA Constellation 25 A/C |
1947 |
187 | TWA Communications Engineering - Dual ADF and Compass Calibration
on P324 |
1947 |
187 | TWA Communications Engineering - Investigation of Aircraft Radio
Tube Failures |
1945 |
187 | TWA Communications Engineering - Investigation on DC-3 12V Power
Supply System |
1945 |
187 | TWA Communications Engineering - Modern Air Transport Cockpit
Controls |
undated |
187 | TWA Communications Engineering - Navigation Receiver
Specifications |
undated |
187 | TWA Engineering - Convair Gear Placard Speeds and their Effect on
Deceleration Performance |
1957 |
187 | TWA Engineering - Equipment Planning - Convair 880 Specification
Weight Empty |
1957-1960 |
187 | TWA Engineering - Evaluation of Boeing Master Change 26-3
Preloaded Baggage Container Installation |
1957 |
187 | TWA Engineering - Most Economical Cruising Speed and Altitude for
Operation of Boeing 707-131 |
1957 |
97 | TWA Engineering International - 749 Troubles Experienced by
PAA |
1947 |
95 | TWA Engineering International - A/A Weight Control System for TWA
Int. Div. |
1948 |
95 | TWA Engineering International - Aerologation |
1946 |
96 | TWA Engineering International - Altimeter & Rate of Climb
Errors Alternate Source LAC 049 |
1947 |
96 | TWA Engineering International - Altimeter Errors Introduced by
Reversal of Static Lines at Static Selector Valve |
1947 |
96 | TWA Engineering International - Analysis of Integral Fuel Tank
Sealing Problem |
1947 |
97 | TWA Engineering International - Analysis of Piston Failures
R-2000 Engine C-54 Series Airplane |
1948 |
96 | TWA Engineering International - Analysis of WAC BA Engine
Performance |
1947 |
95 | TWA Engineering International - C-54 High Altitude Climb &
Cruise Performance Tests |
1943 |
95 | TWA Engineering International - C-54 Induction System
Temperatures |
1945 |
95 | TWA Engineering International - Committee & Procedures
Controlling Modification of Intl. Aircraft |
1946 |
97 | TWA Engineering International - Construction & Operation of
Test Panel of Overhaul Simmonds Pacitor Components: Power Unit,
Junction, Adjustment Box & Ind. |
1948 |
97 | TWA Engineering International - Cruise & Performance Charts,
LAC 749 |
1948 |
97 | TWA Engineering International - Determination of LAC 749
Compliance with CAR Part 41.722 Airplanes with 4 or more Engines - 2
Engines Inoperative |
1948 |
97 | TWA Engineering International - Determination of Wing, Horizontal
Stabilizer & Engine Thrust Line Rigging DC-54B TWA Plane 606, 607,
608, DC-54E TWA Plane 601 |
1948 |
96 | TWA Engineering International - Determination Skymaster
Compliance with CAR Part 41.2722 Airplanes with 4 or more Engines - 2
Engines Inoperative |
1947 |
96 | TWA Engineering International - Effects of Payloads by Proposed
Regulations of Presidents Special Board of Inquiry on Air
Safety |
1947 |
95 | TWA Engineering International - Eng. Induction System Fire #3
Eng. 049 Plane 553 Reading Pa. Feb. 21, 1946 |
1946 |
95 | TWA Engineering International - Engineering Project
Committee |
1946 |
95 | TWA Engineering International - Equipment Analysis
C-69 |
1945 |
97 | TWA Engineering International - Fire Detector Test
Set |
1948 |
187 | TWA Engineering International - Gross Weight/Runway
Charts |
1949 |
95 | TWA Engineering International - Index Unit Loading Form EID-703
Analysis Computations & Instructions |
1947 |
97 | TWA Engineering International - Index Unit Loading Form EID-749
Analysis Computations & Instructions LAC 749 |
1948 |
96 | TWA Engineering International - Index Unit Loading Form EID-753
Analysis Computations & Instructions DC-54G |
1946 |
96 | TWA Engineering International - Index Unit Loading Form EID-754
Analysis Computations & Instructions DC-54B |
1947 |
96 | TWA Engineering International - Investigation Mechanical
Condition & Maint. History Plane 552 After Accident New Castle Nov.
18, 1947 |
1947 |
95 | TWA Engineering International - Investigation Mechanical
Condition of Constellation Plane 554 Washington DC March 29,
1946 |
1946 |
187 | TWA Engineering International - Investigation of Accuracy of
Pioneer Autosyn Fuel Flowmeters |
1948 |
96 | TWA Engineering International - Investigation of Circumstances
Surrounding Accident Plane 556 New Castle, Oct. 12, 1946 |
1946 |
96 | TWA Engineering International - Investigation of Engine Fire on
Plane 603 at Algiers |
1947 |
96 | TWA Engineering International - Investigation Speed-Power &
Airspeed Calibration DC-54B TWA Plane 608 |
1947 |
187 | TWA Engineering International - Overhaul of Loop
Antennas |
1948 |
96 | TWA Engineering International - Preliminary Analysis of Weight
& Balance & Payload Characteristics of Proposed C-54 Passenger
A/C |
1946 |
95 | TWA Engineering International - Range Analysis for DC-54
Transport A/C |
1943 |
95 | TWA Engineering International - Removable Equipment Constellation
049-46 |
1946 |
97 | TWA Engineering International - Removal of Induction System
Deposits - R - 2000 Engines C-53 |
1948 |
95 | TWA Engineering International - Repair of Leading Edge, Left
Outboard Wing Panel Plane 605 |
1946 |
95 | TWA Engineering International - Repair of Wing Spar & #3
Nacelle of Plane #650 |
1947 |
94 | TWA Engineering International - Report of Accident Investigation
Plane NC 86513 |
1946 July 11 |
95 | TWA Engineering International - Report on C-69 Winterization
Tests |
1945 |
97 | TWA Engineering International - Service Troubles Experienced by
EAL LAC 649 |
1948 |
96 | TWA Engineering International - Specifications for Converting
TACA C-54B A/C to TWA Passenger A/C |
1947 |
96 | TWA Engineering International - Specifications for Converting TWA
C-54 Plane 650 & 651 to Passenger Planes |
1947 |
97 | TWA Engineering International - Specifications for Overhaul of
TWA R-2000-9 & R-2000-SD1G Engines |
1948 |
95 | TWA Engineering International - Standard & Removable
Equipment C-54E-DC A/C |
1948 |
95 | TWA Engineering International - Standard & Removable
Equipment DC54B |
1948 |
96 | TWA Engineering International - Standard & Removable
Equipment DC-54G Cargo A/C |
1948 |
97 | TWA Engineering International - Test Panel for Voltage Booster
& Relays |
1948 |
97 | TWA Engineering International - Test Stand for Linear
Actuators |
1948 |
96 | TWA Engineering International - Use of Jet Assisted Take-Off
(JATO) |
1947 |
97 | TWA Engineering International - Weight & Balance Calculations
for DC 54-E TWA Plane 601 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for DC 54-E TWA Plane 602 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for DC 54-E TWA Plane 603 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for DC 54-E TWA Plane 604 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for DC 54-E TWA Plane 605 |
1948 |
96 | TWA Engineering International - Weight & Balance Calculations
for DC-54B TWA Plane 607 |
1947 |
96 | TWA Engineering International - Weight & Balance Calculations
for DC-54B TWA Plane 608 |
1947 |
96 | TWA Engineering International - Weight & Balance Calculations
for DC-54B TWA Plane 650 |
1947 |
96 | TWA Engineering International - Weight & Balance Calculations
for DC-54B TWA Plane 651 |
1947 |
97 | TWA Engineering International - Weight & Balance Calculations
for DC-54E TWA Plane 600 |
1948 |
96 | TWA Engineering International - Weight & Balance Calculations
for DC-54G TWA Plane 606 |
1947 |
96 | TWA Engineering International - Weight & Balance Calculations
for DC-54G TWA Plane 652 |
1947 |
96 | TWA Engineering International - Weight & Balance Calculations
for DC-54G TWA Plane 653 |
1947 |
97 | TWA Engineering International - Weight & Balance Calculations
for TWA LAC 749 Plane 701 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for TWA LAC 749 Plane 702 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for TWA LAC 749 Plane 703 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for TWA LAC 749 Plane 704 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for TWA LAC 749 Plane 705 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for TWA LAC 749 Plane 706 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for TWA LAC 749 Plane 707 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for TWA LAC 749 Plane 708 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for TWA LAC 749 Plane 709 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for TWA LAC 749 Plane 710 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for TWA LAC 749 Plane 711 |
1948 |
97 | TWA Engineering International - Weight & Balance Calculations
for TWA LAC 749 Plane 712 |
1948 |
97 | TWA Engineering International - Weight & Balance Information
LAC 749 |
1948 |
67 | TWA Engineering Orders 1000-1099 |
1944-1945 |
68 | TWA Engineering Orders 1100-1369 |
1944-1946 |
69 | TWA Engineering Orders 1370-1659 |
1945-1947 |
70 | TWA Engineering Orders 1660-1799 |
1945-1946 |
70 | TWA Engineering Orders 2001-2099 |
1945-1946 |
64 | TWA Engineering Orders 2-1 to 2-199 |
1946-1948 |
71 | TWA Engineering Orders 2100-2339 |
1945-1948 |
67 | TWA Engineering Orders 2-1903 to 2-3209 |
1947 |
65 | TWA Engineering Orders 2-200 to 2-299 |
1946-1949 |
66 | TWA Engineering Orders 2-300 to 2-449 |
1947-1950 |
72 | TWA Engineering Orders 2340-2649 |
1945-1951 |
67 | TWA Engineering Orders 2-450 to 2-619 |
1948-1950 |
73 | TWA Engineering Orders 2650-2869 |
1946-1949 |
74 | TWA Engineering Orders 2870-3129 |
1945-1948 |
75 | TWA Engineering Orders 3130-3369 |
1946-1948 |
76 | TWA Engineering Orders 3370-3689 |
1947-1948 |
77 | TWA Engineering Orders 3690-3919 |
1947-1954 |
78 | TWA Engineering Orders 3920-4169 |
1947-1954 |
79 | TWA Engineering Orders 4170-4439 |
1947-1952 |
80 | TWA Engineering Orders 4440-4674 |
1948-1951 |
81 | TWA Engineering Orders 4675-4869 |
1949-1955 |
82 | TWA Engineering Orders 4870-4980 |
1949-1953 |
83 | TWA Engineering Orders 4981-5049 |
1949-1954 |
84 | TWA Engineering Orders 5050-5183 |
1949-1955 |
85 | TWA Engineering Orders 5184-5234 |
1950-1955 |
86 | TWA Engineering Orders 5235-5359 |
1950-1955 |
87 | TWA Engineering Orders 5360-5469 |
1950-1955 |
88 | TWA Engineering Orders 5470-5579 |
1950-1954 |
89 | TWA Engineering Orders 5580-5729 |
1951-1954 |
90 | TWA Engineering Orders 5730-5889 |
1951-1957 |
91 | TWA Engineering Orders 5890-6039 |
1951-1956 |
92 | TWA Engineering Orders 6040-6339 |
1951-1955 |
67 | TWA Engineering Orders Index |
1945-1946 |
64 | TWA Engineering Orders Pre-Flood |
1950-1951 |
187 | TWA Operations Engineering - Airline Accidents |
1947 |
187 | TWA Operations Engineering - Analysis of Constellation Payloads
in Non-Stop Transcontinental Service |
1947 |
187 | TWA Operations Engineering - Flight Characteristics of New
Aircraft |
1947 |
187 | TWA Operations Engineering - Landing Ground Roll
Distances |
1946 |
187 | TWA Operations Engineering - Malfunctions of Airplane or
Equipment - Constellation |
1947 |
187 | TWA Operations Engineering - Method of Analyzing Constellation
Transcontinental Payloads |
1947 |
187 | TWA Operations Engineering - Method of Analyzing DC-3
Payloads |
1947 |
187 | TWA Operations Engineering - Method of Analyzing Payloads of
Boeing 307 |
1947 |
187 | TWA Operations Engineering - Routine Schedule Flight
Reports |
1947 |
178 | TWA SB |
1959 |
187 | TWA Staff Engineering - Analysis of Factors Involved in the
93,000 lb Gross Takeoff Weight Modification Constellation |
1948 |
187 | TWA Staff Engineering - Boeing 707-131 Aircraft Airport Runway
Analysis |
undated |
187 | TWA Staff Engineering - Comparative Tests of Aircraft
Wire |
1947 |
187 | TWA Staff Engineering - Comparative Tests of Electric 2 Gallon
Liquid Containers Manufactured by Landers, Frary, Clarke and Mansfield
Manufacturing Company |
1948 |
187 | TWA Staff Engineering - Comparison of Capacitor Type Liquid
Quantity Measuring Systems |
1946 |
187 | TWA Staff Engineering - Convair 340 Analysis - TWA |
undated |
187 | TWA Staff Engineering - Cruising Performance Analysis and
Preparation of Cruising Control Charts |
1946 |
187 | TWA Staff Engineering - Data Requirements for Evaluation of
Short-Haul Airplanes |
1963 |
187 | TWA Staff Engineering - Ground Test of Hydraulic Drive LAC 49
Cabin Supercharger |
1948 |
187 | TWA Staff Engineering - Hydraulic Drive LAC 49 Cabin Supercharger
Takeoff RPM Test |
1948 |
187 | TWA Staff Engineering - Investigation of Costs PB-10 Auto Pilot
Installation in Constellation 25 and 26 |
1946 |
187 | TWA Staff Engineering - Pioneer Directional Horizon Indicator
Examination |
1947 |
187 | TWA Staff Engineering - Preliminary Report Ground Test of
Hydraulic Drive LAC 49 Cabin Supercharger |
1948 |
187 | TWA Staff Engineering - Takeoff and Climb Performance Test of
M404 at a Gross Weight of 44,900 lb Under Above Standard Atmospheric
Conditions |
1952 |
187 | TWA Staff Engineering - Test Constellation Cockpit Electric Boost
Heater |
1946 |
187 | TWA Staff Engineering - Weight Report Boeing 707-131 |
1958 |
161 | Wright Cyclone C18BD Series Engines Installation Features &
Data |
1949 January |
161 | Wright Turbo-Compound Engine TC18EA Series Models 981TC18EA1,
988TC18EA1, EA2, & EA3 Installation Data |
1956 March |
Series III. Maintenance & Service records, 1944-1982Return to Top
Contains manuals, bulletins, records, and other documents related to the maintenance and service of TWA aircraft.
Container(s) | Description | Dates |
---|---|---|
Box | ||
181 | Boeing 707-331 |
1982 |
185 | Boeing 727 Masters |
1962-1964 |
274 | CJ805 - Overhaul Manual (microfilm) |
undated |
42 | Constellation 049 Maintenance Manual |
1956-1961 |
43 | Constellation 049 Maintenance Manual |
1955-1961 |
34 | Constellation 1049 Maintenance Manual Vol. 2 |
1952-1960 |
33 | Constellation 1049 Maintenance Manual Vol. I |
1952-1959 |
46 | Constellation Model 749 Maintenance Manual |
1948-1967 |
47 | Constellation Model 749 Maintenance Manual |
1952-1967 |
49 | Constellation Model 749 Maintenance |
1947-1953 |
181 | Convair 880 - Freon and Electrical Power |
1960-1969 |
200 | Convair 880 - Maintenance Significant Item Analysis |
1972 |
185 | Convair lease project |
1949 |
185 | Convair Windshields information, correspondence, and
wires |
1961-1970 |
194 | Convair Work Cards - Routine Base Overhaul |
1973 |
194 | Convair Work Cards - Station Service |
1970-1973 |
184 | Engine Overhaul Bulletins |
1956-1959 |
183 | Engineering/Maintenance Liaison Records - ADI System |
1952 |
183 | Engineering/Maintenance Liaison Records - Air
Conditioning |
1952-1960 |
183 | Engineering/Maintenance Liaison Records - Anti-Icing and
Deicing |
1954-1958 |
183 | Engineering/Maintenance Liaison Records - Cabin
Equipment |
1951-1964 |
183 | Engineering/Maintenance Liaison Records - Conversion |
1951-1958 |
183 | Engineering/Maintenance Liaison Records - Crew
Compartment |
1951-1959 |
183 | Engineering/Maintenance Liaison Records - Defogging and
Defrosting |
undated |
183 | Engineering/Maintenance Liaison Records - Electrical |
1950-1963 |
183 | Engineering/Maintenance Liaison Records - Emergency
Equipment |
1952-1959 |
183 | Engineering/Maintenance Liaison Records - EMLR Subject
Index |
1952 |
183 | Engineering/Maintenance Liaison Records - Engine and Engine
Sections |
1951-1963 |
183 | Engineering/Maintenance Liaison Records - Engines
Control |
1953-1958 |
183 | Engineering/Maintenance Liaison Records - Exterior
Markings |
1952-1961 |
183 | Engineering/Maintenance Liaison Records - Fire
Extinguishing |
1952-1960 |
183 | Engineering/Maintenance Liaison Records - Flight
Controls |
1952-1964 |
183 | Engineering/Maintenance Liaison Records - Fuel
System |
1952-1960 |
183 | Engineering/Maintenance Liaison Records - Galley |
1952-1961 |
183 | Engineering/Maintenance Liaison Records - General |
1959 |
183 | Engineering/Maintenance Liaison Records - Ground and Servicing
Equipment |
1952 |
183 | Engineering/Maintenance Liaison Records - Hydraulic |
1951-1961 |
183 | Engineering/Maintenance Liaison Records -
Instruments |
1951-1958 |
184 | Engineering/Maintenance Liaison Records - Landing
Gear |
1953-1962 |
184 | Engineering/Maintenance Liaison Records - Lining and
Soundproofing |
1953 |
184 | Engineering/Maintenance Liaison Records - Material and Process
Specification |
1953 |
184 | Engineering/Maintenance Liaison Records - Navigation
Equipment |
1953-1961 |
184 | Engineering/Maintenance Liaison Records - Oil System |
1954-1963 |
184 | Engineering/Maintenance Liaison Records - Oxygen
System |
1951-1964 |
184 | Engineering/Maintenance Liaison Records - Placards and
Markings |
1951-1958 |
184 | Engineering/Maintenance Liaison Records - Propellers and
Accessories |
1951-1958 |
184 | Engineering/Maintenance Liaison Records - Radio |
1950-1963 |
184 | Engineering/Maintenance Liaison Records - Structure -
Aileron |
1952-1959 |
184 | Engineering/Maintenance Liaison Records - Structure -
Elevator |
1954-1958 |
184 | Engineering/Maintenance Liaison Records - Structure -
Fuselage |
1950-1961 |
184 | Engineering/Maintenance Liaison Records - Structure - Horizontal
Stabilizer |
1953-1959 |
184 | Engineering/Maintenance Liaison Records - Structure - Nacelle and
Cowling |
1951-1959 |
184 | Engineering/Maintenance Liaison Records - Structure - Power
Plant |
1952-1957 |
184 | Engineering/Maintenance Liaison Records - Structure -
Rudder |
1951-1958 |
184 | Engineering/Maintenance Liaison Records - Structure - Systems
Controls |
1953-1958 |
184 | Engineering/Maintenance Liaison Records - Structure - Vertical
Stabilizer |
1959 |
184 | Engineering/Maintenance Liaison Records - Structure - Wash Water
System |
1951-1960 |
184 | Engineering/Maintenance Liaison Records - Structure - Wing Center
Section |
1951-1959 |
184 | Engineering/Maintenance Liaison Records - Structure - Wing
Flaps |
1953-1959 |
184 | Engineering/Maintenance Liaison Records - Structure - Wing
Inner |
1953-1964 |
184 | Engineering/Maintenance Liaison Records - Structure - Wing
Outer |
1950-1963 |
185 | General Dynamics - engineering letter |
1968 |
185 | General |
1958 |
184 | Index - Constellation Service Instructions, Service Information
Letters, and Service Bulletins |
circa 1951-1958 |
181 | Jetcal Analyzer - Service Manual Models BH112J and
BH112JA |
undated |
181 | Maintenance Information Letters (MIL) |
1958-1968 |
181 | Maintenance or Overhaul Time Extension documentation |
1969 |
216 | Maintenance Overhaul and work control forms and
correspondence |
1960-1962 |
217 | Maintenance Overhaul and work control forms and
correspondence |
1962-1965 |
218 | Maintenance Overhaul and work control forms and
correspondence |
1963-1973 |
285 | Metal and Machine shops |
September 22, 1966 |
39 | Model 1649 Series Maintenance Manuals |
1957-1966 |
185 | Roylyn Incorporated |
1952 |
181 | Service Analysis and Information |
1953-1957 |
190 | Service Bulletin Index - Convair 880 |
circa 1960-1973 |
210 | Service bulletins - Aerocom Airborne Communications
Equipment |
1955 |
210 | Service bulletins - Aeronautical Communications
Equipment |
1953-1967 |
210 | Service bulletins - Air Associates |
1954-1955 |
208 | Service bulletins - AiResearch |
1954-1969 |
210 | Service bulletins - Airwork |
1962 |
210 | Service bulletins - Allen Aircraft Products |
1965 |
210 | Service bulletins - Calco |
1961 |
210 | Service bulletins - Caltex |
1958 |
210 | Service bulletins - Canadian Applied Research
Limited |
1961 |
210 | Service bulletins - Cannon Electric |
1964 |
210 | Service bulletins - Champion |
1962 |
210 | Service bulletins - Cleveland Pneumatic |
1961 |
202-203 | Service bulletins - Convair 880 |
1960-1971 |
210 | Service bulletins - Cornelius Company |
1961 |
210 | Service bulletins - Dyne |
1964 |
205-206 | Service bulletins - Eclipse-Pioneer |
1945-1962 |
210 | Service bulletins - Fenske, Fedrick, and Miller |
undated |
210 | Service bulletins - Fenwal |
1968 |
210 | Service bulletins - Firewel Company |
1964 |
210 | Service bulletins - Flite Line |
1969 |
210 | Service bulletins - FMC Corporation |
1964 |
210 | Service bulletins - Foote Brothers Gear and Machine
Corporation |
1959 |
210 | Service bulletins - Ford Industries |
1970 |
207 | Service bulletins - General Electric |
1948-1956 |
210 | Service bulletins - Goodyear |
1948-1974 |
205 | Service bulletins - Hamilton Standard |
1946-1969 |
210 | Service bulletins - Hardman Tool and Engineering
Company |
1959-1964 |
210 | Service bulletins - Heli-Coil |
1954 |
210 | Service bulletins - Holley Carburetor |
1959-1967 |
210 | Service bulletins - ITT Federal |
1961-1966 |
210 | Service bulletins - Jack and Heintz |
1960-1962 |
210 | Service bulletins - Janitrol |
1949-1965 |
208 | Service bulletins - Kollsman Instruments |
1947-1968 |
210 | Service bulletins - Lear |
1955-1958 |
210 | Service bulletins - Lewis Engineering |
1959-1960 |
210 | Service bulletins - Lionel Pacific |
1962-1968 |
210 | Service bulletins - Liquidometer Corporation |
1955, 1965 |
206-207 | Service bulletins - Lockheed |
circa 1952-1959 |
210 | Service bulletins - Loud |
1962 |
210 | Service bulletins - LTV Military Equipment |
1964 |
210 | Service bulletins - Magnetic Control |
1962 |
210 | Service bulletins - Marotta Valve |
1966-1969 |
210 | Service bulletins - Mechanical Products |
1960 |
210 | Service bulletins - Minneapolis Honeywell |
1959-1964 |
210 | Service bulletins - Monarch Aircraft Sales
Incorporated |
1957 |
210 | Service bulletins - Monogram |
1962 |
210 | Service bulletins - Motor Generator Corporation |
undated |
210 | Service bulletins - Motorola |
1961 |
210 | Service bulletins - Nash |
1966 |
210 | Service bulletins - Parker Aircraft Company |
1955 |
210 | Service bulletins - Parker-Hannifin Corporation |
1964-1970 |
210 | Service bulletins - Peacock Engineering and Manufacturing
Company |
1960 |
210 | Service bulletins - Pesco Products |
1954-1965 |
204 | Service bulletins - Pratt and Whitney Aircraft |
circa 1946-1962 |
210 | Service bulletins - Resistoflex |
1957-1958 |
210 | Service bulletins - Sales |
1960 |
210 | Service bulletins - Simmonds Aerocessories
Incorporated |
1959 |
210 | Service bulletins - Solar Aircraft Company |
1958-1959 |
209 | Service bulletins - Sperry Gyroscope Company |
1944-1958 |
185 | Service bulletins - Stratotech |
1952 |
210 | Service bulletins - Thermix Corporation |
1954-1961 |
210 | Service bulletins - Thompson Products |
1949-1957 |
210 | Service bulletins - Vard |
1963-1965 |
204 | Service bulletins - Vickers Incorporated |
circa 1951-1962 |
210 | Service bulletins - Vinson |
1962 |
210 | Service bulletins - Wacline |
1963-1964 |
210 | Service bulletins - Walter Kidde and Company |
1953-1969 |
210 | Service bulletins - Wave Labs |
1965 |
210 | Service bulletins - Western Gear |
undated |
210 | Service bulletins - Winslow Aerofilter |
1957-1958 |
209 | Service bulletins - Wright Aircraft Engines (Wright Aeronautical
Corporation) |
circa 1948-1963 |
181 | Service bulletins and information |
1952-1969 |
45 | Service Data |
1949-1958 |
184 | Service Information Letters |
1949-1962 |
185 | Spare Parts and Tools Procurement Guide |
1954-1965 |
181 | Structural Inspection |
1970 |
60 | Structural Repair |
1957 August 15 |
185 | Sud-Aviation - Caravelle Specifications |
1961-1962 |
36 | Super Constellation 1049G Maintenance Manuals |
1955-1964 |
37 | Super Constellation 1049G Maintenance Manuals |
1955-1964 |
50 | Super Constellation Model 1049 Maintenance Instruc. |
1952-1953 |
185 | Technical Development Company |
1955 |
182 | Time Extensions - Base Overhaul - Boeing 331 |
1971 |
182 | Time Extensions - Base Overhaul - Convair 880 |
1973 |
182 | Time Extensions - Base Overhaul - DC-9 |
1966-1977 |
176 | Time Extensions - Base Overhaul 1049G & 1649A 5000 Hours
#2 |
1962 |
176 | Time Extensions - Base Overhaul 1049G & 1649A 5000
Hours |
1962 |
176 | Time Extensions - Base Overhaul 749/A 5000 Hours |
1962 |
176 | Time Extensions - Base Overhaul 749/A 6250 Hours |
1964-1965 |
176 | Time Extensions - Base Overhaul Constellation A/C 5500
Hours |
1963 |
182 | Time Extensions - Check C - Convair 880 |
1973 |
182 | Time Extensions - Check C - DC-9 |
1966-1972 |
182 | Time Extensions - Check C Deferred - Boeing 707-131 |
1970 |
176 | Time Extensions - Engines BD-1 2500 Hours |
1961-1962 |
176 | Time Extensions - Engines BD-1 2600 Hours |
1963 |
176 | Time Extensions - Engines BD-1 2700 Hours |
1964 |
176 | Time Extensions - Engines BD-1 2800 Hours |
1964 |
176 | Time Extensions - Engines BD-1 2900 Hours |
1965 |
176 | Time Extensions - Engines CB-1 1800 Hours |
1959 |
177 | Time Extensions - Engines TC18 2000 Hours |
1962 |
177 | Time Extensions - Propellers 43E60 749/A 3100 Hours |
1962 |
177 | Time Extensions - Propellers 43H60 1049G 2900 Hours |
1962 |
177 | Time Extensions - Propellers 43H60 1649A 2400 Hours |
1960 |
182 | Time Extensions - Reports |
1956-1970 |
182 | Time Extensions - Turbo Compressors - Boeing 707 |
1960-1965 |
182 | Time Extensions - Turbo Compressors - Convair 880 |
1972 |
182 | Time Extensions - Units - Boeing 707 |
1963 |
182 | Time Extensions - Units - Boeing 707-131 |
1962-1963 |
182 | Time Extensions - Units - Convair 880 |
1964-1965 |
182 | Time Extensions - Weight and Balance |
1967-1969 |
185 | Townsend Company |
1955-1958 |
27 | TWA Inventory Parts Catalog Repair & Return Volume IV Part
2 |
1957-1967 |
181 | TWA Maintenance Program - 10000 Hour Base Overhaul |
1969-1970 |
201 | TWA Work Cards - Convair 880 |
1972-1973 |
192 | Vendor Overhaul Manual - Convair 880 - ADC Electronics through
Avionic Products |
1960-1973 |
192 | Vendor Overhaul Manual - Convair 880 - Bendix through Custom
Components |
1959-1973 |
191 | Vendor Overhaul Manual - Convair 880 - Diehl through Gar
Precision |
circa 1958-1969 |
192 | Vendor Overhaul Manual - Convair 880 - General Electric through
Grimes |
circa 1961-1973 |
192 | Vendor Overhaul Manual - Convair 880 - Hamilton
Standard |
1961-1972 |
192 | Vendor Overhaul Manual - Convair 880 - Hartman Electrical through
Kidde |
1963-1973 |
192 | Vendor Overhaul Manual - Convair 880 - Koehler Aircraft through
Markite |
1958-1974 |
192 | Vendor Overhaul Manual - Convair 880 - Meletron through
Raychem |
1959-1973 |
192 | Vendor Overhaul Manual - Convair 880 - Redco though Superior
Electric |
1959-1973 |
192 | Vendor Overhaul Manual - Convair 880 - Talley through Vapor
Heating |
1960-1968 |
192 | Vendor Overhaul Manual - Convair 880 - Vard through
Wilcolator |
1964-1970 |
185 | Western Electric |
undated |
185 | Weston |
1953 |
185 | William R. Whittaker Company - Field Service Report |
1953-1956 |
185 | Wright Aeronautical - Numerical Index |
1951-1962 |
185 | Wright Aircraft Engines - Operation Bulletins Index |
1955 |
185 | Wright Aircraft Engines - Spare Parts and Tools
Procurement |
1955 |
20 | Wright Aircraft Engines Series C18BD Overhaul Manual |
1952 September |
23 | Wright Aircraft Engines Series TC18DA Overhaul Instructions Book
Two |
1954-1963 |
22 | Wright Aircraft Engines Series TC18DA Overhaul
Instructions |
1959 January |
24 | Wright Aircraft Engines Series TC18EA Overhaul Instructions Book
One |
1953-1960 |
31 | Wright Aircraft Engines Series TC18EA Overhaul Instructions Book
Two |
1957-1963 |
20 | Wright Aircraft Engines Series TC1EA Service Manual |
1956 March |
21 | Wright Aircraft Engines Turbo Compound Maintenance
Manual |
1963 |
54 | Wright Cyclone Engines Series 18BD Service Manual |
1946 October |
Series IV. Lockheed, 1940-1978Return to Top
Contains materials involving Lockheed aircraft, their subject files and engineering records.
Container(s) | Description | Dates |
---|---|---|
Sub-series 1. Subject files |
1944-1978 | |
Box | ||
41 | 049 CAA Approved Operating Manual |
1946-1957 |
41 | 049 Maintenance Instructions |
1946-1948 |
20 | 11560 - Constellation Model 1649 Series C.A.A. Approved
Airplane Flight Manual |
1957 |
56 | 1649 Overhaul |
1957-1958 |
263 | 300-1 Super Starlifter |
1966 |
25 | 7787 - Super Constellation Model 1049 Series C.A.A. Approved
Airplane Operating Manual |
1952-1957 |
270 | Action Item Summary Protective Finish Design
Review |
1970 |
265 | Addendum A to ER 9622 LAC 500 Aircraft
Description |
1968 |
268 | Aids/Flight Data Recorder Signals |
1969 |
263 | Aircraft Noise |
undated |
270 | Aircraft Upholstery Fabrics |
1969 |
266 | Airline Structural Design Review - Wing -
Empennage |
1969 |
273 | Airlines /LAC/RR 9th Power Plant Design Review Meeting
Record |
1970 |
273 | Airlines Meeting to Resolve Model L-1011-1 Configuration
Differences |
1970 |
268 | Airlines/LAC Pylon Design Review Meeting Record |
1969 |
26 | Airplane Flight Manual for Super Constellation Model 1649
Series |
1957-1961 |
265 | Assault STOL C-130 |
1966 |
269 | Bleed-Air Duct Overheat Detection System |
1969-1970 |
270 | Building Block Concept for Aircraft Recording
Systems |
1970 |
268 | Buyer-Furnished Equipment (BFE) On-Deck Dates for First 22
TWA L-1011 Aircraft |
1969 |
27 | C.A.A. Approved Airplane Operating Manual for the models
649-79, 749-79, & 749A-79 Constellation |
1947-1966 |
264 | C-141A Starlifter - Loading and Airport Operations Data
Book |
1966 |
265 | C5A Brochure |
undated |
265 | CAB NE Corridor VTOL Investigation |
1968 |
273 | CALAC Automatic Test Equipment Program |
circa 1969 |
264 | Cargo Loading C141A |
1967 |
263 | Change Requests Applicable to Standardization Meeting Agenda
Items |
1967 |
264 | Characteristics Summary Model GL-334-17 Super
Starlifter |
1965 |
271 | CL-1011 2 Engine Turbofan for Domestic Commercial
Operation |
1966 |
273 | Cole L-1011 Connectors |
undated |
263 | Commercial Aircraft Fleets Jet Equipped Airlines of the Free
World |
1967-1968 |
271 | Commercial Airline Systems Analysis |
1967 |
263 | Commercial Cargo Transport |
1968 |
265 | Commercial VTOL Aircraft Evolution Submitted to
CAB |
1967 |
265 | Community Noise and Pavement Data |
1966 |
264 | Comparative Evaluation-Control Modes of Operation for Landing
Gear Position Selector Valve |
1967-1968 |
264 | Comparison Isobaric and Adaptive-Isobaric Cabin Pressure
Control |
1968 |
270 | Connector, Electric Circular, Environment Resistant, High
Temperature |
1966 |
263 | Constant M Cruise Data |
1965 |
60 | Constellation Accessories Overhaul Manual |
1945-1946 |
263 | Constitution Charts and Data |
1951 |
263 | Corrosion Susceptibility of Aluminum When Coupled with
Titanium Fasteners |
1968 |
264 | Coupling Joints for L-1011 Metal Duct Systems - Study and
Evaluation |
1968 |
60 | Crew Operating Manual for the Constellation Models
649-749 |
1951 August 1 |
266 | Customer/Lockheed Hydraulic System Design Review |
1969 |
265 | Dash 8 JetStar Performance Improvements |
1967 |
267 | Detail Specification Model C-141A Cargo
Transport |
1966 |
270 | Direct Lift and Speedbrake Control System |
1970 |
263 | Direct Operating Cost Payload-Range and Weight Summary for
Different Fuel Tank Configurations |
1968 |
270 | Eastern Detail Specification |
1970 |
263 | Effect of Containerization on Air Cargo Costs |
1965 |
265 | Electric Bonding Requirements - General |
1969 |
262 | Electrical Load Analysis - Eastern Airlines |
1970 |
270 | Electroform Nickel Wash Basins in lieu of Stainless Steel
Wash Basins |
1970 |
263 | Engine and Engine Pod Equipment |
1971 |
267 | Engineering Description Series - Electrical |
1970 |
267 | Engineering Description Series - Flight Station |
1970 |
267 | Engineering Description Series - Hydraulics and Flight
Controls |
1970 |
267 | Engineering Description Series - Maintainability and
Reliability |
1970 |
267 | Engineering Description Series - Pneumatics Air Conditioning
APU |
1970 |
267 | Engineering Description Series - Propulsion |
1970 |
53 | Engineering Design Handbook |
1948-1961 |
29 | Engineering Purchasing Specification Manual |
1949-1963 |
270 | Equipment Specification - Environmental
Requirements |
1971 |
269 | Equipment Specification - Evacuation Slide
Assembly |
1969 |
264 | FAA Approved Airplane Flight Manual for Model 300-50A-01
Equipped with PW TF-33-P-7 Engines |
1967 |
267 | Feasibility Study Foster Oven |
undated |
268 | Final Report - Digital Air Data Computer Development
Progress |
1970-1971 |
269 | Flame Tests for Aircraft Interior Materials |
1969 |
270 | Flight Station Configuration and Panel Arrangement
EAL |
1972 |
270 | Food and Beverage Service Carts Design Review |
1970 |
270 | Galley Steering Committee Meeting |
1970 |
265 | General Requirements for Large Twin Engined Passenger
Transport |
1970 |
263 | Hercules Aid Freighter Terminal Operations |
1968 |
265 | Honeycomb Sandwich Structure Study for Supersonic Transport
Airframe Application |
1966 |
271 | Hydraulic System Tubing and Connection Methods
Program |
1967 |
265 | Interior and Avionics Specification for Executive Jet
Aviation JetStar 5099 |
1967 |
271 | Interior Trim Specifications |
1967-1969 |
267 | Joint Airline/LAC L-1011 Program Review |
1970 |
265 | L-100 STOL |
undated |
262 | L-1011 Addendums to LR-22641 |
1969 |
266 | L-1011 Advanced Heat Sink Brake |
1969 |
273 | L-1011 Aids Hydraulic Condition Signal List LAC Support
Option 9.7 |
1969 |
272 | L-1011 Aids/Flight Data Recorder Signals Quotation
Package |
1969 |
270 | L-1011 Aids/Flight Data Recorder Signals |
1970 |
272 | L-1011 Aids/Flight Data Recorder Signals |
1969-1970 |
264 | L-1011 Air Data Anti-Icing Heater Control and Monitoring
Study |
1968 |
266 | L-1011 Air Data System Design Review |
undated |
264 | L-1011 Aircraft Electromagnetic Compatibility Control for
Equipment Installation |
1969 |
270 | L-1011 Aircraft Engine Pneumatic Starter and Control
Valve |
1972 |
272 | L-1011 Airline Airframe Structures Design Review |
1969 |
273 | L-1011 Airline Design Review - Integrated Pneumatic
Systems |
1969 |
272 | L-1011 Airline Executive Program Review |
1969 |
272 | L-1011 Airline Steering Committee Quarterly Weight
Review |
1969 |
272 | L-1011 Airline Structural Design Review Descriptions Related
to View Charts - Wing, Empennage |
1969 |
267 | L-1011 Airlines/Lockheed/Rolls Royce Power Plant Design
Review Meeting Board |
1969-1970 |
267 | L-1011 Airplane Characteristics Summary |
1978 |
267 | L-1011 Airplane Sales, Service Life, and Spare Parts Sales
Contracts |
1968 |
266 | L-1011 Applicable Documents for Procurement of Galley
Equipment |
1968 |
263 | L-1011 APU Airline Design Review |
1970 |
271 | L-1011 APU Economic Analysis |
1967 |
266 | L-1011 APU Replacement |
undated |
273 | L-1011 APU System Design |
1971 |
270 | L-1011 Attitude and Heading Reference System General
Description for FAA |
1970 |
264 | L-1011 Automatic Flight Guidance and Control Performance
Criteria |
1968 |
267 | L-1011 Avionic Flight Control System |
1970 |
271 | L-1011 Balance Matrix Airline Quarterly Weight
Review |
1970 |
273 | L-1011 Baseline Sign System |
undated |
269 | L-1011 Bun Warmer Modular-Underfloor Galley
Specifications |
1969 |
266 | L-1011 Cabin Centerline Storage Module with
Table |
1968 |
273 | L-1011 Cabin Centerline Storage Module with
Table |
1968 |
264 | L-1011 Cabin Fire Suppressant System Study |
1968 |
269 | L-1011 Cart, Waste |
1971 |
270 | L-1011 Circuit Breaker, Remote Control General
Specification |
1968 |
268 | L-1011 Circuit Breaker, Remote Control |
1968 |
269 | L-1011 Coffeemaker - Modular Galley Service Unit
Specification |
1969 |
269 | L-1011 Cold Storage Unit - Underfloor Galley |
1969 |
264 | L-1011 Comparative Evaluation Electric Trim
Control |
1968-1969 |
269 | L-1011 Component Handling Manual |
1968 |
271 | L-1011 Component Maintainability Contract |
1968 |
271 | L-1011 Component Reliability Contract |
1968 |
269 | L-1011 Connectors, Special Purpose Electrical Miniature
Circular Environment Resisting 2000 Maximum Temperature |
1969-1970 |
270 | L-1011 Crew Seats |
1970 |
272 | L-1011 Crew Seats |
1970 |
272 | L-1011 DCS-ORIG REF/ATA INDES ATA/DCS Index |
1965, 1970 |
270 | L-1011 Description of Modular Navigation System for
Submittal |
1970 |
272 | L-1011 Design for Structural Integrity |
undated |
266 | L-1011 Design Review - Flight Engineer's System Control
Panels |
1969 |
268 | L-1011 Design Review - Interior Lighting Emergency Evacuation
Equipment |
1969 |
262 | L-1011 Digital Air Data Computer Development
Report |
1969 |
271 | L-1011 Door Seal Concepts Evaluation |
1968-1969 |
266 | L-1011 Electric Power System |
undated |
270 | L-1011 Electrical Power, Characteristics and
Utilization |
1968 |
264 | L-1011 Electromagnetic Compatibility Control for Electric
Bonding |
1968 |
264 | L-1011 Electromagnetic Compatibility Control for Wire and
Cabling Installation |
1968 |
264 | L-1011 Electromagnetic Compatibility Control
Plan |
1968 |
270 | L-1011 Electromagnetic Interference Characteristic
Requirements and Measurement for Equipment Instruments and
Subsystems |
1968 |
273 | L-1011 Elevator Drive System |
1971 |
270 | L-1011 Emergency Hydraulic Power Supply System |
1968 |
262 | L-1011 Engine Change Methods Study |
1969 |
268 | L-1011 Engine Evaluation Presentation |
1969 |
266 | L-1011 Engine Evaluation |
1968 |
268 | L-1011 Engine Evaluation |
1969 |
273 | L-1011 Environmental Control System - Integrated Pneumatic
System Design Review Meeting |
1969 |
269 | L-1011 Equipment Specification - Multiplexed Passenger
Services and Audio Entertainment System |
1969 |
269 | L-1011 Equipment Specification Drive System, Galley
Lift |
1969 |
269 | L-1011 Equipment Specification Refrigerator, Modular,
Underfloor Galley |
1969 |
269 | L-1011 Equipment Specification Weight and Balance
System |
1968-1969 |
268 | L-1011 Evaluation of General Purpose and SWAMP Area Electric
Wire Candidates |
1969 |
268 | L-1011 Evaluation of Protective Systems for Titanium and
Steel Fasteners |
1970 |
271 | L-1011 Evaluation of Support Plans for Alternate Engine
Installations |
1971 |
272 | L-1011 Exhibits to LAC/RR Airframe/Propulsion System
Agreement |
1968 |
273 | L-1011 Extended Range Comprehensive Aids/FDR Signal
List |
undated |
273 | L-1011 Family Study |
1968 |
268 | L-1011 Fault Isolation Symposium |
1970 |
262 | L-1011 Flight Guidance/Instrument Color Configuration
Matrix |
1970 |
267 | L-1011 Flight Guidance/Instrument Color Configuration
Matrix |
1970 |
262 | L-1011 Flight Instrument Failure Warning and Monitoring
System Design Concept |
1970 |
262 | L-1011 Flight Station Configuration and Panel Arrangements
for TWA |
1973 |
272 | L-1011 Flight Station Configuration Mockup
Review |
1969 |
269 | L-1011 Flight Station Seats |
1968 |
268 | L-1011 Flight Station Technical Information |
1969 |
273 | L-1011 Flight Test Program Summary |
undated |
262 | L-1011 Food and Beverage Service System
Definition |
1970 |
266 | L-1011 Fuel System |
undated |
266 | L-1011 Functional Trouble Shooting |
1968 |
273 | L-1011 Galley Lift System |
undated |
272 | L-1011 Galley Service Time and Motion Study |
1968 |
268 | L-1011 Galley Steering Committee Meeting |
1969 |
268 | L-1011 Galley System |
1969 |
270 | L-1011 General Description Extended Range
Airplane |
1969 |
271 | L-1011 General Description |
undated |
273 | L-1011 Ground Support Equipment Standardization |
1968 |
264 | L-1011 Hydraulic System Reservoir Pressurization
System |
1968 |
270 | L-1011 Hydraulic Units General Requirements |
1968 |
269 | L-1011 Icemaker and Cold Storage Unit |
1969 |
272 | L-1011 Increased Range Version |
1968 |
268 | L-1011 Industry Survey and LAC Design Concept for VHF Push
Button Tuning Control System |
1969 |
267 | L-1011 Information |
undated |
266 | L-1011 Initial Cruise Altitude Capability |
1968 |
273 | L-1011 Initial Cruise Altitude Capability |
1968 |
264 | L-1011 Integral Vacuum Cleaning System Study |
1968 |
268 | L-1011 Integrated Pneumatic System Technical
Description |
undated |
269 | L-1011 Interface Control DWG Multiplexed Passenger Service
and Entertainment System with Seat Control Units |
1971 |
272 | L-1011 Interface Control DWG Multiplexed Passenger
Service |
1970 |
271 | L-1011 Interface Document, Baggage/Cargo
Container |
1969 |
264 | L-1011 Interface Document, Container Loader |
1968 |
270 | L-1011 Joint Food Test Plan |
1969 |
272 | L-1011 Kit |
1968 |
270 | L-1011 Lighting Instrument, Integral, White |
1978 |
262 | L-1011 Lightning Protection - Radome for Submittal to
FAA |
1970 |
268 | L-1011 Lightning Protection - VOR Antenna System |
1970 |
266 | L-1011 List of Differences Between EAL/TWA |
1968 |
272 | L-1011 Lockheed/Rolls Royce Operational Support Information
Exchange System |
undated |
273 | L-1011 Lounge Study Presented to TWA |
1970 |
273 | L-1011 Maintainability and Reliability |
1971 |
266 | L-1011 Maintenance Engineering Analysis Manual of
Instructions |
1969 |
266 | L-1011 Maintenance Program Development and Structural
Sampling Charts |
undated |
268 | L-1011 Maintenance Review Board Plan |
1969 |
272 | L-1011 Major Installation Releases |
undated |
270 | L-1011 Meeting Record Airlines/LAC/RR Power Plant Design
Review |
1969 |
268 | L-1011 Minutes of Galley Steering Committee
Meeting |
1969 |
270 | L-1011 Modular Navigation System Review |
1970 |
270 | L-1011 Module, Cartridge Valve and Manifold,
Hydraulics |
1968 |
266 | L-1011 MRB Planning Meeting |
1969 |
273 | L-1011 Operations Planning Manual Including Basic Performance
CL-1011-365 RR |
1967 |
269 | L-1011 Oven-Modular, Underfloor Galley |
1969 |
270 | L-1011 Panels, Information, Integrally
Illuminated |
1968 |
269 | L-1011 Passenger Address Amplifier |
1970 |
269 | L-1011 Passenger Seating Specifications |
1969 |
271 | L-1011 Passenger Supplemental Oxygen System |
undated |
269 | L-1011 Pneumatic Ducting Equipment General
Requirements |
1968 |
272 | L-1011 Power Plant Objectives |
undated |
271 | L-1011 Pratt and Whitney Study |
1968 |
273 | L-1011 Pratt and Whitney Study |
1968 |
262 | L-1011 Preliminary List of Ground Support Equipment
(GSE) |
1970 |
269 | L-1011 Preliminary List of Ground Support Equipment
Requirements |
1971 |
270 | L-1011 Preliminary Recommended Minimum Equipment
List |
1968 |
272 | L-1011 Preliminary Specification Icemaker - Galley,
Modular |
1969 |
268 | L-1011 Progress Reports |
1971 |
264 | L-1011 QEC Transporting |
1968 |
270 | L-1011 R.B. 211 Thrust Indicating and Thrust Management
Systems |
1969 |
271 | L-1011 Rated Engine Pressure Ratio Computer System
Study |
1969 |
267 | L-1011 Reliability and Maintainability Control Program
Plan |
1967 |
273 | L-1011 Removal and Installation Concept for APU, NLG, and MLG
Engines |
undated |
266 | L-1011 Rest/Sleep Study |
undated |
268 | L-1011 Roll Stability Augmentation System Description for
Submittal to FAA |
1970 |
273 | L-1011 S-Duct |
1968 |
272 | L-1011 Selected Major Components Status Review |
1971 |
270 | L-1011 Selection of Equipment Specification, Parts,
Materials, Processes, and Standards |
1967 |
269 | L-1011 Serving Cart - Beverage Equipment
Specification |
1971 |
269 | L-1011 Serving Cart - Beverage |
1970 |
269 | L-1011 Serving Cart, Food - Coach Class
Specification |
1970 |
269 | L-1011 Serving Cart, Food - First Class
Specification |
1969 |
268 | L-1011 Specifications for Production and Acceptance - Flight
Testing |
1970-1975 |
268 | L-1011 Speed Control System Description for Submittal to
FAA |
1970 |
270 | L-1011 Standardization Criteria, Flight Station Displays and
Controls |
1968 |
272 | L-1011 Structural Compatibility of the La Guardia Runway
Extensions |
1968 |
268 | L-1011 Study - Aft Engine Installation Tail Down |
1969 |
271 | L-1011 Study and Proposal for Advanced Modular Attitude and
Navigation System |
1968 |
268 | L-1011 Study Proposal Air Canada - Extreme Temperature Ground
Handling Operations |
1967 |
268 | L-1011 Summary Report on Exterior Finish Material
Qualification Test Program |
1968 |
266 | L-1011 Supplier Data - AC Generator and Generator Control
Unit |
circa 1968 |
272 | L-1011 Supplier Data - Air Data System |
1968 |
273 | L-1011 Supplier Data - Air Turbine Motor |
1968 |
271 | L-1011 Supplier Data - Avionic Flight Control
System |
1968 |
273 | L-1011 Supplier Data - Constant Speed Drive,
Generator |
1968 |
267 | L-1011 Supplier Data - Fuel Flow Measurement
System |
1968 |
271 | L-1011 Supplier Data - Hydraulic Pump Electric Motor
Driven |
1968 |
271 | L-1011 Supplier Data - Hydraulic Pump Engine
Driven |
1968 |
271 | L-1011 Supplier Data - Main Landing Wheels and
Brakes |
1967-1968 |
270 | L-1011 Supplier Data - Specification Fire Detection System,
Power Plant and APU |
undated |
266 | L-1011 Supplier Data - Transformer-Rectifier |
1968 |
270 | L-1011 Task Descriptions for Airline Personnel Participating
in Food Service Tests |
1970 |
268 | L-1011 Technical Description of LAC Modular Navigation System
Concept |
1969 |
272 | L-1011 Terminal Junction Modules |
1969 |
266 | L-1011 Third Underfloor Galley Meeting Report |
1968 |
273 | L-1011 Tri-Jet Transport and Airports |
undated |
267 | L-1011 Tristar Advancement Program |
1978 |
268 | L-1011 Troubleshooting Symposium |
1970 |
266 | L-1011 TWA Aids Quotation Package |
1969 |
271 | L-1011 TWA Analysis of Summer 1972 Requirement |
1971 |
271 | L-1011 TWA General Description |
undated |
266 | L-1011 TWA Partial Aids - Proposed Signal
Analysis |
1969 |
266 | L-1011 TWA Partial Aids |
1969 |
272 | L-1011 TWA Photo Progress Report |
1969 |
268 | L-1011 TWA Proposal Studies Between-Seat Stowage
Compartments |
1970 |
271 | L-1011 TWA/EAL Technical Briefing |
1968 |
273 | L-1011 Two Engine Study |
1968 |
266 | L-1011 Underfloor Galley Meeting Report |
1968 |
273 | L-1011 Underfloor Galley |
undated |
262 | L-1011 Visual Aids System for TWA |
1969 |
270 | L-1011 Waste Management Study |
1970 |
270 | L-1011 Weight and Balance System Description and Flight Test
Plan |
1970 |
270 | L-1011 Weight and Balance System Design Review |
1969 |
272 | L-1011 Wire Prime Considerations |
undated |
269 | L-1011 Wiring Document Assembly and Installation Procedures
for Electrical Wiring |
1977 |
272 | L-1011 Wiring Document Assembly and Installation Procedures
for Electrical Wiring |
1970 |
268 | L-1011 Yaw Stability Augmentation System Description for
Submittal to FAA |
1970 |
268 | L-1011-1 Ground Support Equipment |
1969 |
272 | L-1011-1 Serial 1025 Domestic Route Performance |
1970 |
262 | L-1011-358-8 Basic Performance Rolls Royce RB. 211-56
Engines |
1969 |
264 | L-1011-385 Effect of Tire Pressure on Pavement
Loading |
1968 |
271 | L-1011-385-1 Component Reliability CLD-103-3A Contract with
TWA |
undated |
271 | L-1011-385-1 Growth Characteristics (with Rolls Royce or
General Electric Figures) |
undated |
264 | L-1011-385-1 Pavement Loading Report |
1968 |
264 | L-1011-385-1 Rolls Royce RB. 211-22 Engines Basic
Performance |
1968-1970 |
272 | L-1011-385-6 Basic Performance Rolls Royce R.B. 211-28
Engines |
1969 |
262 | L-1011-385-8 Basic Performance Rolls Royce RB. 211-56
Engines |
1970 |
262 | L-1011-385-8 Basic Performance Rolls Royce RB. 211-57
Engines |
1969 |
262 | L-1011-385-8 Model Specification Long Range
Airplane |
1969 |
271 | L-1011-385-8 Optional Installation Report |
1969 |
262 | L-1011-385-8.4 Optional Installation Report |
1969 |
267 | L-1011-500 Review |
1978 |
267 | L-1011-500 Technical Review - Airplane
Configuration |
undated |
262 | L-1011-8 Engine Out Performance, Rolls Royce RB.
211-56 |
1969 |
273 | L-1011-8 Extended Range Airplane Study |
1969 |
269 | L-1011Drive System, Galley Lift
Electro-mechanical |
1969 |
265 | L-500 Aircraft Description |
undated |
265 | L-500 Aircraft Performance |
1968 |
265 | L-500 Operational and Economic Summary |
1969 |
265 | L-500 |
undated |
263 | LAC 100-20 Generalized Block Fuel, Block Time, and DOC
Data |
1968 |
263 | LAC 100-20 Hercules for Domestic All-Cargo
Service |
1968 |
263 | LAC 100-20 Hercules with External Tanks Basic Performance
Data |
1968 |
263 | LAC 100-20 Hercules without External Tanks Basic Performance
Data |
1968 |
269 | LAC 1011 General Performance W JT9D |
1967 |
265 | LAC 500 Aircraft Performance LG500-114MD |
1968 |
265 | LAC 500 Airport Compatibility |
1968 |
265 | LAC 500 Basic Economics of Air Freight
Transportation |
1968 |
265 | LAC 500 Reliability Control Program Plan |
1968 |
263 | LAC and Airline Reliability and Maintainability
Program |
1968 |
263 | LAC Engineering Capability |
1968 |
264 | LAC Information on Commercial Starlifter GL-334-26A Including
Performance |
1966 |
262 | LAC L-1011 Food and Beverage Service System
Definition |
1969 |
265 | LAC Status Report - Structural Compatibility of La Guardia
Runway |
1968 |
269 | LAC TEN-ELEVEN TWA Requirements |
1967 |
272 | LAC/RR Technical Exhibits |
1971 |
265 | LG500-114ZD Basic Performance General Electric CF6-50A
Engine |
1969 |
52 | Lockheed Engineering Standards Manual Section 99 Procurement
Section |
1961-1963 |
30 | Lockheed Material Specifications |
1960-1961 |
30 | Lockheed Process Bulletin Manual |
1957-1963 |
52 | Lockheed Process Specification Manual |
1948-1964 |
263 | Lockheed/ATA Meeting - Collected Papers on Long Life Aircraft
Design |
1968 |
41 | Materials Specification Manual |
1944-1946 |
270 | Meeting Record Airlines/LAC/RR Power Plant Design
Review |
1970 |
270 | Meeting Record Engine Installation and Ground Support
Equipment Review |
1970 |
269 | MFG Facilities and MFG Plan |
1967 |
55 | Model 1649 Series Maintenance Manual |
1957-1962 |
56 | Model 1649 Series Maintenance Manual |
1957-1964 |
55 | Model 1649 Series Maintenance |
1957-1962 |
29 | Model 1649 Series Wiring Manual |
1957-1963 |
263 | Model 200 Computer-Calculated Route Performance |
1967 |
263 | Model 200 Performance Data |
1966-1967 |
263 | Model 200 Starlifter Domestic All-Cargo Service |
1966 |
264 | Model GL 334-26A Super Starlifter Preliminary TWA Route
Study |
1966 |
265 | Model LG500-114ZC Aircraft Description |
1969 |
265 | Model Specification for JetStar Specification |
1968 |
265 | Model Specification for LAC Model CL-1026-27 Compound
Helicopter Transport |
1967 |
265 | Model Specification for Model L-200 Starlifter Jet
Cargo |
1966 |
265 | Model Specification LAC 500 |
1969 |
265 | Model Specification LAC JetStar P5116 |
1968 |
263 | Model Specification Model 382E-44K-20/L-100-20 Hercules
Airfreighter |
1968 |
264 | Model Specification TWA L-1011 |
1970 |
273 | Modular Navigation System Review |
1970 |
266 | Modular Navigation System Technical Brief Avionics
Report |
1969 |
263 | Noise - Interim Review |
undated |
273 | Operational Schedule Analysis of L-1011-385-1 for
TWA |
undated |
265 | Operations Planning Report for CL-1026 Interurban Transport
CT64-630-2 Engines |
1967 |
272 | Optimum Center Engine Installation |
1967 |
273 | Optional Installations Report |
1969 |
267 | Passenger Accommodations Development Review |
1971 |
270 | Passenger Supplemental Oxygen System |
1969 |
264 | Preliminary Data Commercial C-141 Airfreighter G1
334-26 |
1965 |
268 | Preliminary List of GSE Requirements |
1970-1971 |
265 | Preliminary Market Analysis of CL-1026 Compound
Aircraft |
1967 |
271 | Preliminary Study of Spare Engine Pod |
1968 |
263 | Presentation Material - Standardization Meetings |
1967 |
269 | Procurement Policies and Procedures |
1967 |
263 | Profits at Surface Yields |
1965 |
265 | Program Report LAC Observation Flights on TWA Boeing 747
Aircraft |
1970 |
269 | Proposal for Model 209 Digital Flight Data
Recorder |
1970 |
263 | Proposal for New Guidance System for Approach and
Landing |
1969 |
272 | R.B. 211 Engine Rollover with Crane and Forklift |
1971 |
267 | Reliability and Maintainability Program |
1971 |
269 | Reliability and Maintainability Program |
1970 |
265 | Report to President's Sonic Boom Committee of National
Academy of Sciences |
1964 |
269 | Research and Development Facilities |
1967 |
272 | Rolls Royce LAC Basic Agreement for R.B. 211 Propulsion
System |
1971 |
263 | SALT - Self-Contained All-Weather Landing and
Taxing |
1969 |
53 | SDR 5001 - Instructions For Use of the LAS Model 109-C Flight
Recorder in Aircraft Accident Investigations |
1960 July 1 |
53 | SDR 5001a - Training Manual Readout & Handling of Flight
Data on the LAS Model 109-C Flight Recorder for Use in Aircraft
Accident Investigations |
1960 November 3 |
263 | Speed Trends in Air Transportation |
1969 |
271 | Standardization Meeting (AAL, Delta, EAL, TWA,
UAL) |
1967 |
264 | Standardization Meeting Agreements |
1968 |
269 | Stereophonic High Fidelity Music Tape Reproducer |
1969 |
269 | Stereophonic High Fidelity Passenger Address
Amplifier |
1969 |
269 | Stereophonic High Fidelity Passenger Address Loudspeaker
Assembly |
1969 |
268 | Study for Disinsection Requirement for International
Flight |
1969 |
25 | Super Constellation Model 1049 Series C.A.A. Approved
Airplane Flight Manual |
1955-1962 |
26 | Super Constellation Model 1049 Series C.A.A. Approved
Airplane Flight Manual |
1956-1960 |
57 | Super Constellation Model 1649A Parts |
1957-1963 |
264 | Super Starlifter |
1965 |
263 | Systems Approach to Material Selection and Design for
Structural Integrity |
1968 |
268 | Technical Proposal to Manufacture Escape Slide
Assemblies |
1969 |
269 | Thermoplastic Sheet |
1969 |
263 | Total Airline Profit and Simulation Models |
1969 |
273 | Tri-Jet Transport General Presentation |
1968 |
265 | TWA Boeing 747 Problem Analysis Report |
1970 |
270 | TWA Interior Furnishings and Structures Review |
1970 |
266 | Underfloor Galley Review |
1968 |
265 | Urban Public Resources and VTOL Terminals |
1967 |
270 | Visual Entertainment System Interface |
1972 |
266 | Weight Status Meeting and Galley Review |
1968 |
264 | Wire, Electric, Fluorocarbon/Polyimide Insulated Coated
Copper and High Strength Copper Alloy |
1970 |
264 | Wire, Electric, TFE Fluorocarbon/Liquid Polyimide Insulated
Silver Coated Copper |
1969 |
264 | Zone and Access Door and Panel Identification |
1968 |
Sub-series 2. Engineering |
1940-1963 | |
Box | ||
131 | 10034 - Installation Approval Tests WAD 975C18CB-1 Engines,
Mark 1 Afterbodies & Long-Chord Cowl Flaps |
1954 July 16 |
131 | 10054 - Speed Improvement Program Constellation, Basic Model
1049 |
1954 |
131 | 10119 - Full Scale Mockup Tests of Various Model 1049A, B,
& C Oil System Configurations |
1954 November 2 |
131 | 10183 - Cruising Control - Model 1049B, C, & E with
Hamilton Standard Propellers |
1954 |
131 | 10200 - Electrical Equipment (Worksheets) |
1955-1956 |
131 | 10294 - Evaluation of WAD Alternate Fuel Source |
1954-1955 |
131 | 10341 - Type Certificate Tests Super Constellation Model
1049G & H with Hamilton Standard 43H60/6959B-0
Propellers |
1956 |
131 | 10342 - Measurement of Windshield Deviation &
Distortion |
1955 |
131 | 10389 - Structural Design Criteria |
1955-1958 |
131 | 10391 - Empennage Loads |
1955-1957 |
132 | 10392 - Wing Loads |
1955-1957 |
132 | 10393 - Fuselage Loads |
1955-1958 |
132 | 10394 - Landing Gear & Power Plant Loads |
1955-1957 |
132 | 10438 - Basic Cruising Performance of Super Constellation
Models 1049G/H with Ham. Std. Props WAD TC18EA-3 or EA-6
Eng. |
1958 February 28 |
132 | 10438 - Basic Cruising Performance of the Model 1049G &
1049H Super Constellation with Hamilton Standard 6959
Propellers |
1956 December 1 |
132 | 10438 - Basic Cruising Performance of the Model 1049G Super
Constellation with Hamilton Standard 6959 Propellers |
1955-1956 |
133 | 10478 - Structural Capabilities |
1955 |
114 | 1049 Electrical Drawing Cross-Ref. |
1951-1952 |
133 | 10514 - Long Range Transport Airplane
Performance |
1955-1957 |
19 | 10560 - Manufacturer's Basic Model Specification for the
Serial 1649A-001 Super Constellation Passenger Airplane |
1955-1958 |
19 | 10560-4 - Manufacturer's Detail Specification for the Model
1649A Super Constellation Airplanes |
1955-1957 |
133 | 10580 - Northwest Airlines Fuel Pressure Drop-Off Inv.
Interim Report |
1955 |
133 | 10620 - Constellation Electrical Data Book |
1957 |
133 | 10620 - Electrical Equipment (Worksheets) |
1955-1956 |
134 | 10621 - Static Tests of Wing Joints & Panels |
1955-1956 |
134 | 10644 - Constellation Radio Data Book |
1956-1957 |
134 | 10665 - Fuselage, Seats, Floors, & Equipment Stress
Analysis |
1955-1956 |
134 | 10685 - Flashweld Proof Test Loads |
1956 |
11 | 1074 - Weight & Balance Report TWA A/C #810 |
1952 December 13 |
134 | 10799 - Wing Station 468.5 Upper Joint Compression
Test |
1955 August |
134 | 10807 - CAA Type Certification Tests - Mark I Afterbodies
& Long-Chord Cowl Flaps - Constellation Model 1049 |
1955 |
134 | 10821 - Model 1649A Main Landing Gear Analysis |
1955-1957 |
134 | 10822 - Model 1649A Nose Landing Gear Analysis |
1956 |
135 | 10830 - Flight Incidents which Demonstrate the Constellation
Fuselage Pressure Vessel to be Fail-Safe |
1955 September 7 |
135 | 10835 - Constellation Electrical Data Book |
1956 |
135 | 10838 - Model 1649A Static & Fatigue Tests of Riveted
Butt Joints Employing Various Types of Faying Surface
Sealants |
1954-1956 |
135 | 10870 - H.F. Flush Antenna Evaluation on R7V-2
Aircraft |
1955 November 11 |
136 | 10906 - Wing Internal Loads |
1956-1957 |
136 | 10907 - Wing Box Analysis |
1956-1957 |
136 | 10908 - Wing Components Analysis |
1956-1957 |
136 | 10909 - Interaction Curves of Stiffened Curved Panels Under
Shear & Compression |
1955-1956 |
136 | 10910 - Fuselage IBM Internal Loads |
1956 |
137 | 10911 - Fuselage Shell Analysis |
1956-1957 |
137 | 10912 - Fuselage Frame & Bulkhead Analysis |
1956-1957 |
137 | 10913 - Fuselage Miscellaneous Structures
Analysis |
1956 |
137 | 10914 - Fuselage External Loads & Section
Properties |
1956-1958 |
138 | 10915 - Control System Analysis Model 1649A |
1956-1957 |
138 | 10918 - Outboard Nacelle Analysis |
1956-1957 |
138 | 10919 - Inboard Nacelle & Engine Mount
Analysis |
1956-1957 |
138 | 10920 - Horizontal - Stabilizer Analysis |
1956-1957 |
139 | 10921 - Floor, Seats, & Equipment Stress Analysis Model
1649A |
1956-1958 |
139 | 10924 - Model 1649A Proof Test Loads |
1956 |
139 | 10959 - Constellation Radio Data Book - TWA |
1956 |
139 | 10961 - Nacelle Ring Bending Test |
1955 October 26 |
142 | 11,683 - Static Tests of the Model 1649A
Airplane |
1957 January 14 |
139 | 11104 - Super Constellation Airplane Performance |
1956 May 2 |
139 | 11110 - Fatigue Tests of model 1649 Wing Joints |
1956-1957 |
135 | 11113 - Static Tests of Fuselage Shear Panels |
1956 |
135 | 11223 - High Altitude Tests of Ceramic-Coated Cabin
Heaters |
1956 |
135 | 11312 - Wing Station 106 Leading Edge Rib Test |
1956 |
139 | 11320 - Fatigue Test of No. 473437 Aileron Control Link
Assembly |
1956 May 23 |
139 | 11325 - Static Test of Model 1649 Flap Track |
1956 |
139 | 11353 - Static Single Shear Properties of ACT-509 &
SAL-100 Lockbolt Joints |
1956 |
139 | 11354 - Aileron & Aileron Tab Static Test |
1956-1957 |
139 | 11355 - Static Test of Model 1649A Outboard Wing
Flap |
1956 |
140 | 11378 - Test Program - Model 1649A Control System
Tests |
1956 |
140 | 11380 - Tests, Fuselage-to-Wing Attachment Bolts &
Fittings |
1956 |
140 | 11381 - Vertical Surfaces |
1956 |
140 | 11410 - Review of Flight Control Booster Design |
1956-1957 |
140 | 11414 - Proposed Inspection Procedure for Cargo Aircraft
Operated at Weights Above Certified Gross Weights |
1956-1960 |
140 | 11435 - Constellation Radio Data Book |
1957 |
140 | 11457 - Model 1649-A Proof Test Loading |
1956 |
141 | 11473 - Constellation Electrical Data Book |
1957 October 7 |
141 | 11477 - Constellation Electrical Data Book |
1957 April 1 |
142 | 11535 - Constellation Electrical Data Book |
1957 April 9 |
142 | 11574 - Vibration & Slosh Test of No. 479492 Alcohol
Tank |
1956-1957 |
142 | 11586 - Substatiation of Ditching Characteristics of the
1649A Super Constellation |
1956 |
142 | 11607 - Hydraulic Reservoir Slosh & Vibration
Tests |
1956-1957 |
142 | 11625 - Investigation of Fuel Dumping & the Attendant
Fire Hazard with Constellation Type Aircraft |
1956 |
143 | 11686 - Fuselage Stress Analysis |
1956 October 1 |
143 | 11715 - Drop Tests & Inflight Brake Tests of 1649 Main
Landing Gear |
1957 |
143 | 11724 - Loading Data for C.A.A. Certification of 1649 Series
Constellation Airplanes |
1957-1958 |
143 | 11724-1 - Loading Data for C.A.A. Certification of 1649
Series Constellation Airplanes |
1957-1958 |
143 | 11724-2 - Loading Data for C.A.A. Certification of 1649
Series Constellation Airplanes |
1957-1958 |
143 | 11726 - Preliminary Flutter Analysis, Model 1649A Airplane
Final Flutter Analysis |
1957 |
143 | 11740 - Ground Vibration Tests & Justification of Flutter
Analysis, Model 1649A Airplane |
1957-1958 |
14 | 11771 - Proof Tests Main Landing Gear Bearings |
1956 October 22 |
14 | 11799 - Static Test of Main Landing Gear Doors |
1956 October 17 |
14 | 11832 - 7075-T6, X7178-T6, & Magnesium Parts |
1956 October 24 |
14 | 11837 - Fuel Dump Chute Assembly Operational
Test |
1956 November 30 |
14 | 11839 - Static & Fatigue Tests of Faying Surface Sealed
7075-T6 Clad Butt Joints Subjected to Environmental
Conditioning |
1956 November 12 |
14 | 11843 - Engine Oil Tanks Twenty-Five Hour Vibration &
Slosh Tests |
1956 October 23 |
14 | 11846 - Control System Proof & Operation
Tests |
1956 December 21 |
14 | 11866 - C.A.A. Master Equipment List 1649 Series
Airplanes |
1957 |
14 | 11876 Model 1649A Fuel System Mockup Tests Demonstrating
Compliance with Civil Air Regulation 4b & Tank Filling Rate
Requirement |
1956-1957 |
14 | 12004 - Winslow Oil Filter Test Submitted Under |
1956-1957 |
14 | 12007 - Basic Cruising Performance of the Model 1649A
Airplane with Hamilton Standard or Curtiss Propellers |
1958 January 20 |
15 | 12009 - CAA Type Certification Report - Model 1649A with WAD
988TC18EA2 Engines & Hamilton Standard 43H60/HA17A3-4
Propellers |
1957 |
15 | 12011 - CAA Type Certification Report - Model 1649A with WAD
988TC18EA-2 Engines & Hamilton Standard 43H60/6993B-4
Propellers |
1958-1959 |
15 | 12011, Supp. I - CAA Type Certificate Report - Model 1649A
with WAD 988TC18EA-2 Engines & Ham. Stand. 43H60/6993B-4
Propellers |
1959 |
15 | 12013-002 - Weight & Balance Data 1649A Plane
1002 |
1957 |
15 | 12013-003 - Weight & Balance Data 1649A Serial
1003 |
1957 |
15 | 12013-004 - Weight & Balance Data 1649A Serial
1004 |
1957 May |
15 | 12013-005 - Weight & Balance Data 1649A Serial
1005 |
1957 |
15 | 12013-006 - Weight & Balance Data 1649A Serial
1006 |
1957 |
15 | 12013-007 - Weight & Balance Data 1649A Plane
1007 |
1957 |
15 | 12013-008 - Weight & Balance Data 1649A Serial
1008 |
1957 |
15 | 12013-009 - Weight & Balance Data 1649A Serial
1009 |
1957 |
15 | 12013-010 - Weight & Balance Data 1649A Serial
1010 |
1957 |
15 | 12013-013 - Weight & Balance Data 1649A Serial
1013 |
1957 |
15 | 12013-014 - Weight & Balance Data 1649A Serial
1014 |
1957 April 14 |
15 | 12013-015 - Weight & Balance Data 1649A Serial
1015 |
1957 |
15 | 12013-016 - Weight & Balance Data 1649A Serial
1016 |
1957 |
15 | 12013-017 - Weight & Balance Data 1649A Serial
1017 |
1957 April 27 |
15 | 12013-018 - Weight & Balance Data 1649A Serial
1018 |
1957 |
15 | 12013-019 - Weight & Balance Data 1649A Serial
1019 |
1957 |
15 | 12013-021 - Weight & Balance Data 1649A Serial
1021 |
1957 |
15 | 12013-022 - Weight & Balance Data 1649A Serial
1022 |
1957 |
15 | 12013-023 - Weight & Balance Data 1649A Serial
1023 |
1957 |
15 | 12013-024 - Weight & Balance Data 1649A Serial
1024 |
1957 |
15 | 12013-025 - Weight & Balance Data 1649A Serial
1025 |
1957 |
15 | 12013-026 - Weight & Balance Data 1649A Serial
1026 |
1957 August 7 |
15 | 12013-029 - Weight & Balance Data 1649A Plane
1029 |
1957 July 9 |
15 | 12013-030 - Weight & Balance Data 1649A Plane
1030 |
1957 |
15 | 12013-035 - Weight & Balance Data 1649A Plane
1035 |
1957 August 24 |
15 | 12013-037 - Weight & Balance Data 1649A Serial
1037 |
1957 August 22 |
16 | 12025 - Flight Tests of the High Rate Discharge Fire
Extinguishing System for the Model 1649A Power Plant |
1957 January 11 |
16 | 12027 - Model 1649A High Rate of Discharge Fire Extinguishing
System Mockup Test at the Power Plant Laboratory |
1957 |
16 | 12080 - Investigation of the 1049C-Band Nose
Radome |
1957 |
16 | 12107 - Super Constellation Model 1049H Cargo Loading
Instructions |
1957 April 1 |
16 | 12277 - CAA Airplane Performance - Super Constellation Model
1049H/01 with Hamilton Standard 43H60/6959B-0 Propellers & WAS
988TC18EA-3 Engines |
1957 |
16 | 12277 Supp. I - CAA Airplane Performance - Super
Constellation Model 1049G/01 & H/01 with Ham. Std. 4360/6959B-0
Propellers & WAD 988TC18EA-3 Engines |
1958 |
16 | 12380 - CAA Certification Sperry Integrated Instrument
System |
1957 June 10 |
16 | 12385 Add. A - PB-20 Autopilot C.A.A. Certification Report
Including Throttle Control-Model 1649A Airplane |
1957 |
16 | 12406 - Cruising Control for the Model 1049G/H Super
Constellation with Hamilton Standard Propellers |
1957 August 5 |
16 | 12411 - Static Tests of Some M.L.G. Components for Increased
Gross Weight - 1649A |
1957 |
16 | 12423 - Model 1649A Cabin Heater Fire Extinguishing System
Mockup Test at the Power Plant Laboratory |
1957 July 3 |
16 | 12479 - Type Certificate Test for Ferry Operation of
Constellation Model 1649A |
1959 |
16 | 12649 - Evaluation of the Effect of the Gordon Israel Baffle
Installation on the Constellation Models 1049 &
1649A |
1957 October 24 |
16 | 12772 - Power Plant Build-Up Instructions for Super
Constellation Series Airplanes |
1958 |
16 | 12926 - Evaluation of the Effect of Fuel System Modification
on EA Series Engine Performance |
1958 March 4 |
16 | 13189 - Basic Cruising Performance of Electra Model 188A with
Aeroproducts -606 Propellers & Allison D-13 Engines |
1958-1959 |
10 | 1498 - Engine Nacelle Analysis |
1940-1952 |
11 | 2050 Appendix E - Cabin Trim Specifications for 49-46-02
Transport Airplanes for First Customer |
1940 November 9 |
11 | 2411 - Wing Test Program |
1941 October 29 |
10 | 2666 - Stub Wing Analysis |
1942 December 8 |
5 | 2711 -Landing Gear Analysis |
1941-1943 |
6 | 2712 - Control Systems Analysis |
1940-1946 |
7 | 2890 II - Horizontal Stabilizer Analysis |
1940-1943 |
7 | 2890 III - Vertical Surfaces |
1940-1943 |
6 | 2890-1 - Horizontal Stabilizer Loading |
1940-1943 |
7 | 2942 - Model 49 Vibration Tests |
1945-1951 |
8 | 4192 - Analysis of Wing Flap & Support
Structure |
1940-1943 |
8 | 4192 Appendix A - Analysis of Wing Flap & Support
Structure (2) |
1950-1951 |
8 | 4251 - Tests of Flexible Hydraulic Connectors |
1943 |
8 | 4566 - Tests of Proposed Model 49 Floor Panel |
1943-1945 |
8 | 4692 - Constellation Performance at 82,000 lbs. with Pratt
& Whitney… |
1944 |
9 | 4733-1 - Inner Wing Box Beam |
1944-1945 |
9 | 4955 - Actual Weight Report Model 49-46-10 |
1944 December 4 |
9 | 5057 - Model 49 Elevator Booster Contamination
Test |
1945 January 22 |
9 | 5096 - Faults of a Generator Feeder to a Vibrating
Plate |
1949-1950 |
13 | 516 - Weight & Balance Data Serial 049-1969 |
1953 April 20 |
9 | 5333 - Inner Wing Aft Structure Test |
1945 April 25 |
9 | 5342 - Winterization Tests of Model C-69 Rudder Control
Surface Booster |
1945 May 16 |
1 | 5530 - Manufacturer's Detail Model Specification for the
Constellation Cargo Speedpak |
1945 October 10 |
2 | 5540 - Loading Data for C.A.A. Certification of Constellation
Airplanes |
1945 October 23 |
2 | 5555-041 - Weight and Balance Data |
1954 March 29 |
2 | 5555-044 - Weight and Balance Data |
1953 March 13 |
2 | 5555-070 - Weight and Balance Data |
1953 March 21 |
2 | 5555-076 -Weight and Balance Data |
1954 January 13 |
2 | 5555-078 -Weight and Balance Data |
1954 February 20 |
2 | 5555-084 -Weight and Balance Data |
1953 February |
2 | 5555-085 -Weight and Balance Data |
1953 February 2 |
2 | 5555-087 -Weight and Balance Data |
1953 June 1 |
2 | 5555-088 -Weight and Balance Data |
1953 April 24 |
2 | 5555-634 -Weight and Balance Data |
1950 |
2 | 5555-970 -Weight and Balance Data |
1953 May 26 |
3 | 5599 - Performance of the Lockheed Constellation Model
49-51 |
1945 December 10 |
4 | 5602 - Outer Wing and Tip Analysis |
1946 July 3 |
4 | 5622 - Loading & Balance Characteristics of T.W.A.
Constellation Airplanes |
1946 January 22 |
4 | 5625 - Detail Weight & Balance Lockheed Model 49-46-25
(3) |
1946 January 29 |
4 | 5651 - Landing Gear Analysis |
1946 October 7 |
4 | 5665 - Wing Joint Analysis |
1946 July 12 |
5 | 5666 - Inner Box Beam Analysis |
1946-1947 |
103 | 5683-A - Fuselage Shell Analysis |
1946 September 3 |
103 | 5684 - Fuselage Miscellaneous Structure |
1946 October 15 |
104 | 5686 - Stub Wing Analysis |
1946 September 15 |
104 | 5725 - Results of Model C-69 Cold Weather Tests in Winter of
1945-1946 |
1946 May 2 |
104 | 5775 - Type Certificate Tests on Constellation with Two-Speed
Fuel Injection Engines |
1946 July 17 |
104 | 5775 (Appendix A) - Type Certificate Tests on Constellation
with Two-Speed Fuel Injection Engines |
1946 July 17 |
104 | 5775 (Appendix B) - Type Certificate Tests on Constellation
with Two-Speed Fuel Injection Engines |
1946 July 17 |
104 | 5819 - Cabin Smoke Tests Crash Investigation - TWA
Constellation #2040 |
1946 July 20 |
104 | 5822 - Ground Tests on 049-2021 Relative to the Crash of TWA
Constellation 2040 |
1946 July 23 |
104 | 5823 - Laboratory Tests of Generator Circuit Faults &
Loose Connections at the Fuselage Stud |
1946 July |
104 | 5825 - Smoke Pattern Tests in Connection with Investigation
of TWA Constellation 2040 Crash |
1946 July 23 |
104 | 5831 - Tests of Circuit Breakers & Fuses in the Generator
Field Circuits |
1946 July 26 |
104 | 5861 - Numerical Drawing Index |
1946 September 30 |
105 | 5867 - CAA Proving Flights on Modified
Constellation |
1946 August 29 |
105 | 5867 (Appendix I & II) - CAA Proving Flights on Modified
Constellation |
1946 August 29 |
105 | 5868 - Installation Tests of Two-Speed Fuel Injection
Engines |
1946 September 5 |
105 | 5871 - Flush Static System Airspeed Calibration Tests on the
Model 49 |
1946 September 3 |
105 | 5873 - Constellation Cruising Control (2) |
1946 December 2 |
105 | 5879 - Demonstration of Placard Dive Speed - Lockheed
Constellation Model 49-46 |
1946 September 18 |
105 | 5885 - Fuselage Analysis |
1946 November 7 |
105 | 5891 - Modification of the Model 49 Fuel Dumping
System |
1946 October 3 |
105 | 5909 - Repair Instructions for Integral Fuel & Oil Tank
Sealant Constellation & Super Airplanes |
1953 |
105 | 5913 - 49-46 Take-Off at 2600 RPM |
1946 October 30 |
106 | 5948 - Weight & Balance Data for C.A.A. Certification of
649 & 749 Constellation Airplanes |
1946 December 20 |
106 | 5950 - Substantiation Report 84500 lb. Ldg. & 102,000 lb.
T.O. |
1947 January 6 |
106 | 5967 - Effect of Simulated Air Gusts on Control Surfaces of
Constellation Airplane |
1947 January 7 |
13 | 6 7/8 - Pictorial Review of Turbine Hood Configurations for
Model 1049 A, B, & C Series Airplanes & a649A
Airplanes |
1958 March 11 |
106 | 6000 - De-icing Boot Tests on Ship 1979 |
1945 December 11 |
106 | 6015 - 649 (749) Performance Summary |
1946 January 8 |
106 | 6026 - Engine Nacelle Analysis |
1946 March 14 |
107 | 6029 - Structural Capabilities Model 749 |
1947 February 19 |
107 | 6030 - Weight & Balance Data for C.A.A. Certification of
Model 149 Constellation Airplanes |
1947 May 22 |
107 | 6056 - C.A.A. Master Equipment List |
1947 March 14 |
107 | 6108 - Limit Load Criteria PICAO |
1947-1953 |
107 | 6122 - Constellation Heating & Ventilating System
Modification |
1947 June 2 |
107 | 6128 - Tests of Model 649 Cabin Windows |
1947 May 9 |
107 | 6196 - Model 649 Cabin Supercharger & Power Plant
Installation Tests at the Power Plant Lab |
1947 October 15 |
107 | 6200 - Drop Tests of Constellation Main Landing Gear Drag
Strut Damper |
1947 August 4 |
107 | 6207 - CAA Approval Tests on Landing Gear Dampers as
Installed on Lockheed Constellation Model 649-749 |
1947 August 5 |
107 | 6208 - Model 749-79 A Civil Air Regulation Performance
Discussion |
1947 August 8 |
108 | 6237 - Range Performance & Cruise Control for Lockheed
Constellation Model 649-749 |
1947 September 10 |
108 | 6283 -Constellation Electrical Data Book |
1948 |
109 | 6290 - Constellation Radio Data Book |
1947 October 28 |
109 | 6295 - Tests of a Nesa Coated Windowshield |
1947 October 30 |
109 | 6304 - Part VI "Kaynar" Nut Conformance Tests |
1951 October 11 |
109 | 6332 - Effects of an Undercowl Induction Scoop on the WAS
749C18BD1 Engine Installation |
1947 |
109 | 6343 - Constellation Generator System Protection
Program |
1947 December 21 |
109 | 6394 - Data for Determination of Take-off Field Lengths for
Model 49 & 149 Constellations |
1948 February |
109 | 6611 - Investigation of Cabin Contamination with Carbon
Dioxide on the Constellation - Model 049 |
1948 July 16 |
109 | 6660 - Air Conditioning Performance Summary Constellation
Model 649 |
1948 September 9 |
109 | 6773 - Cabin Humidification Study for the
Constellation |
1948 December 16 |
109 | 6795 - Proposed Liquid Heating System |
1948 December 21 |
109 | 6843 - Stability Tests on Elevator Booster from TWA
Constellation No. 559 (2) |
1949 January 27 |
109 | 6899 - TWA Constellation No. 551 Elevator
Booster |
1949 February 25 |
109 | 6924 - Analysis of Braking Tests on Model 749A
(2) |
1949 March 17 |
109 | 6960 - An Operational Description of the New Generator
Prospective System for the Constellation Airplane |
1949 April 27 |
109 | 6966 - A New Generator Control System Which Provides
Protection Against Generator Overvoltage & Under Voltage &
Feeder Faults |
1949 May 5 |
110 | 7031 - 749-749A Electrical Data Book |
1949-1952 |
110 | 7039 - Model 49 Fuel Tank Dip Stick Accuracy as a Function of
Airplane Attitude |
1949 June 16 |
110 | 7057 - Radio Data Book |
1950-1952 |
110 | 7066 - Effect of Undercowl Induction Scoop on the WAC
749C18BD1 Engine Installation During Automatic Lean
Operation |
1949 October 14 |
110 | 7113 - Analysis of Service Costs-Goodrich Dual Expander Tube
Brake vs. Goodyear Single Disc Brake |
1949 August 23 |
110 | 7130 - External Antenna Elimination Program - Constellation
Airplanes - Domestic |
1949 September 8 |
111 | 7188 - Constellation Electrical Data Book for Chicago &
Southern Airlines, Inc. |
circa 1949-1951 |
111 | 7238 - Constellation Radio Data Book for Chicago &
Southern |
1950 July 12 |
111 | 7256 - Drag Evaluation & Performance Improvement Flight
Tests - Constellation Model 749A |
1949 December 30 |
111 | 7258 - Flight Tests of Jet Stack Exhaust System,
Constellation Model 749A |
1950 February 8 |
111 | 7311 - Type Certification Tests-Constellation Model 749A
Equipped with Hamilton Standard 43E60 |
1950 February 14 |
112 | 7381 - Tests of Model 049 Sierracin Windows &
Supplementary Investigations |
1950 April 5 |
143 | 7412 - Cruising Control for Model 749A-Hamilton Standard
6869A Propellers |
1950 |
143 | 7412 App. I - Cruising Control for Model 649A & 749A with
Speedpak Installed - Hamilton 6869A Props. |
1951 January 29 |
112 | 7412 App. II - Cruising Control for Model 749A - Hamilton
Standard 6869A Propellers - Three Ferry Operation |
1951 August 27 |
144 | 7477 - Basic Limit Loads |
1951 |
144 | 7478 - Fuselage & Wing Ultimate Design Loads |
1951-1953 |
144 | 7479 - Nose Landing Gear Analysis |
1951-1953 |
144 | 7484A - Stub & Inner Wing Analysis Box Beam
Surfaces |
1951 |
144 | 7484B - Wing Analysis Main Wing Ribs |
1951 April 18 |
145 | 7484C - Inner & Stub Wing Analysis Part C: Main
Beams |
1951 |
145 | 7485 - Wing External & Internal Loads |
1951 |
145 | 7486 - Wing Allowable Stresses & Miscellaneous Pressure
Calculations |
1951 August 1 |
145 | 7502 - Performance Report for Lockheed 1049-53 |
1950-1951 |
146 | 7559 - Numerical Index of Installation & Assembly
Drawings |
1950 |
146 | 7579 - Manufacturer's Detail Specification for Model 1949E
Constellation Airplanes |
1954-1956 |
19 | 7579-18 - Final Corrected Manufacturer's Detail Specification
for the 1049G Model Constellation Airplanes |
1953-1956 |
146 | 7590 - Electronic Controlled Rubber Boot De-Icer System: the
Effect of Vacuum Shutoff |
1950 |
146 | 7682 - Fuselage Nose Wheel Well & Cockpit |
1950-1951 |
146 | 7683 - Fuselage Miscellaneous Bulkheads |
1951-1957 |
147 | 7684 - Fuselage Main Frames & Tail Bulkheads |
1951 March 16 |
147 | 7685 - Fuselage Miscellaneous Structure |
1951-1953 |
147 | 7687 - Fuselage Shell Analysis (2) |
1951-1953 |
112 | 7688A - Fuselage Shell Section Properties & Internal
Loads - Part A Section Property Data |
1950 December 26 |
112 | 7688B - Fuselage Shell Section Properties & Internal
Loads - Part B Internal Loads |
1950 December 26 |
113 | 7694 - Vertical Surfaces |
1951 July 26 |
113 | 7695 - Horizontal Surfaces |
1951 July 26 |
113 | 7739 - Main Landing Gear Analysis |
1951 January 13 |
114 | 7753 - Landing Gear Analyses Models 1049A, B, C; 1249A;
137,500#/113,000# (Parts A-D) |
1952 January 14 |
114 | 7778 - Fuselage Miscellaneous Bulkheads |
1951 May 15 |
114 | 7783 - Engine Nacella Analysis |
1950 December 19 |
114 | 7798 - Flight Test Unit Airload Instructions |
1951 April 5 |
114 | 7827 - Constellation Radio Data Book for TWA Contract
LD-75 |
1952 January 30 |
114 | 7828 - Constellation Electrical Data Book Model |
1951 September 30 |
115 | 7830 - Type Certification Tests-Constellation Model749A with
Speedpak & Hamilton Standard 43E60/6869A-0
Propellers |
1951 February 16 |
115 | 7843 - Flight Test Evaluation of Hamilton Standard 43E60/6869
Propeller Feathering System |
1951 February 5 |
115 | 7844 - Cargo Loading Data Super Constellation
Airplanes |
1951 February 19 |
115 | 7848 - Cruising Control for Model 649A & 749A Equipped
with Hamilton Standard 6869A Propellers… |
1951 February 5 |
115 | 7848 App. I - Cruising Control for Model 649A & 749A
Equipped with Hamilton Standard 6869A Propellers… |
1951 March 15 |
115 | 7848 App. II - Cruising Control for Model 649A & 749A
Equipped with H.S. 6869A Propellers & a Jet Exhaust
System… |
1951 August 27 |
115 | 7898 - Floor, Seats, & Equipment of Model
1049B |
1952 January 28 |
115 | 7899 - Fuselage Shell Analysis |
1952 January 7 |
116 | 7927 - Functional Test of Landing Gear Selector
Valve |
1951 March 27 |
116 | 7946 - Engine Nacelle Analysis for Models 1049A, B, C, D,
E |
1951 December 31 |
116 | 7972 - Substatiation of Model 1049 Wing for 120,000 lbs.
Take-Off Weight |
1951 July 31 |
116 | 7974 - Flush Type V.O.R. Antenna for C121-C
Aircraft |
1952 July 30 |
116 | 7975 - Model 1049 Carburetor Air Induction System Anti-Icing
Test at the Lockheed Power Plant Laboratory |
1951 April 17 |
116 | 8017 - Type Certificate Tests of Model 049 with Jet Exhaust
Stacks |
1951 May 12 |
116 | 8045 - Development of Model 049 Jet Stack Exhaust System -
WAC 745C18BA3 Engine |
1951 June 18 |
117 | 8050 - Wing External & Internal Loads for Models 1049 B
& C |
1952 June 23 |
117 | 8051 - Wing Allowable Stresses & Misc. Pressure
Calculations for Models 1049 B & C |
1952 April 30 |
117 | 8054 - Wing Analysis of Model 1049A |
1953 April 1 |
117 | 8055 - Wing Tip & Tip Tank Analysis Model
1049A |
1953 June 10 |
118 | 8072 - Vertical Surfaces Models 1049 A, B, C |
1952 February 1 |
118 | 8073 - Horizontal Tail Surfaces Models 1049 A, B, C 1249
A |
1952 May 29 |
118 | 8077 - Tests of Model 1049 Sierracin Cabin
Windows |
1954 May 17 |
118 | 8097 - C.A.A. Master Equipment List 1049 Series Constellation
Airplanes |
1951 July 10 |
120 | 8098-### - Weight & Balance Data |
1955-1957 |
118 | 8098-015 - Weight & Balance Data |
1952 July 7 |
118 | 8098-016 - Weight & Balance Data |
1952 May 12 |
118 | 8098-017 - Weight & Balance Data |
1952 May 16 |
118 | 8098-018 - Weight & Balance Data |
1952 August 11 |
119 | 8098-019 - Weight & Balance Data |
1952 June 12 |
119 | 8098-020 - Weight & Balance Data |
1952 |
119 | 8098-021 - Weight & Balance Data |
1952 July 24 |
119 | 8098-022 - Weight & Balance Data |
1952 July 14 |
119 | 8098-023 - Weight & Balance Data |
1952 |
119 | 8098-024 - Weight & Balance Data |
1952 |
119 | 8098-582 - 8098-599 - Weight & Balance Data |
1955 |
120 | 8104 - Structural Tests of Nesa Windshield |
1951 July 9 |
121 | 8133 - Control System Analysis |
1951 July 26 |
121 | 8139 - Fuselage Nose Wheel Well, Cockpit Enclosure Misc.
Bulkheads Main Frames, & Tail Bulkheads - Model
1049 |
1953 March 1 |
121 | 8140 - Fuselage Miscellaneous Structure Model
1049C |
1953 March 1 |
121 | 8141 - Floors, Seats, & Equipment Model
1049C |
1953 March 1 |
122 | 8142 - Fuselage Shell Analysis Model 1049C (KLM) |
1953 March1 |
122 | 8159 - Loading Data for C.A.A. Certification of 1049 Series
Constellation Airplanes |
1951 August 9 |
122 | 8159-18 - Loading Data for C.A.A. Certification of 1049
Series Constellation Airplanes |
1956 May 29 |
122 | 8159-40 - Loading Data for C.A.A. Certification of 1049
Series Constellation Airplanes |
1958 March 15 |
122 | 8159-7 - Loading Data for C.A.A. Certification of 1049 Series
Constellation Airplanes |
1955 February 11 |
122 | 8162 - Radiation Patterns of VHF Antennas for KLM 1049
Constellation Aircraft |
1951 November 17 |
123 | 8281 - Wing Surfaces Analysis Model 1049 B &
C |
1952 November 7 |
123 | 8307 - Model 1049 Fuselage Pressure Test |
1951 December 4 |
123 | 8364 - Metallurgical Analysis of Corroded Aluminum Alloy
Channel |
1951 December 12 |
123 | 8379 - Wing Internal Loads, Model 1249A |
1953 October 5 |
123 | 8385 - Static Test Compound Engine Nacelle Cowling, Flaps,
& Mount |
1952 May 9 |
123 | 8389 - ADF Reversal Tests Model 1049 Airplanes |
1952 January 4 |
123 | 8400 - Passenger Door Cutout Structure Model
1049C |
1953 March 1 |
124 | 8402 - W.S. 80 Lower Surface Joint Tests |
1952 January 15 |
124 | 8416 - Tension & Compression Tests of Upper Surface
Joint, Wing Station 458 |
1952 January 22 |
124 | 8482 - Model 1049 Cruising Control with Wright 956C18CA1
Engines |
1952 March 6 |
124 | 8538 - Model 1049 Wing & Empennage Deicer System Flight
Tests |
1952 April 8 |
7 | 8581 - Sound Levels in Model 1049 No. 4002 |
1952 |
124 | 8581 - Sound Levels in Model 1049, No. 4002 |
1952-1953 |
124 | 8720 - Cruising Control for Model 1049 with Wright 975C18CB1
Engines |
1952 August 8 |
124 | 8736 - Investigation of Rust in New TWA Model 1049
Engines |
1952 August 19 |
124 | 8737 - Model 1049E Nose Wheel Well Cockpit Enclosure &
Misc. Bulkheads Stress Analysis (2) |
1954 April 14 |
124 | 8738 - Fuselage Main Frames & Tail Bulkheads Stress
Analysis for Model 1049E |
1954 January 29 |
124 | 8886 - Wing Station 458 Lower Surface Joint Test |
1953 January 14 |
124 | 8906 - Development of Protective Shields for Model 1049 Cabin
Pressure Windows |
1953 March 3 |
124 | 8941 - Berth Sound Level Measurements in TWA 1049 No.
905 |
1953 March 18 |
125 | 8964 - Fuselage Shell Analysis, Model 1049E |
1954 May 10 |
125 | 9043 - Transport Study with Twin-Spool T-34
Engines |
1953 January |
125 | 9084 - Evaluation of the X-Ray Process as a Technique for
Inspecting Constellation Blind Structures |
1953 May 4 |
125 | 9154 - Supplement A Speed Kit Operation |
1954 |
125 | 9162 - Fire Test of High Temperature Hose &
Insulations |
1953-1954 |
125 | 9234 - Honeycomb Flooring Configuration Development
Tests |
1953 January 25 |
125 | 9393 - Constellation Radio Data Book TWA |
1954 November 17 |
125 | 9397 - Speed Kit Investigation Report for Model
1049C |
1953 September 30 |
128 | 9438 - Predicted Performance of Goodyear PD494-1 Brakes on
Model 1049C Airplane |
1953 October 9 |
125 | 9465 - Constellation Functional Assembly |
1952 |
125 | 9469 - Constellation Fuselage Center Section Load
Distributions |
1953 December 22 |
126 | 9496 - Constellation Electrical Data Book |
1954-1955 |
18 | 9500-15 - Manufacturer's Detail Specification for the Model
1049G Constellation Airplane |
1955-1957 |
13 | 955 - Model 1249 Test of Manual Weld of Main Gear Cylinder
CPT Part No. 9291B-2B |
1957 October 21 |
126 | 9595 - Model 1049C Main Landing Gear Static Test |
1954 February 23 |
126 | 9636 - Cabin Floor Dynamic Test |
1954 January 12 |
127 | 9662 - Fuselage Section Properties & External &
Internal Loads, 1049E |
1954 |
126 | 9696 - Model 1049 DEGH Wing Internal Loads |
1954 May 14 |
127 | 9697 - Wing Surfaces & Beams Models 1049
DEGH |
1954-1958 |
128 | 9698 - Model 1049 DEGH Wing Rib & Flap
Analysis |
1954 May 7 |
127 | 9699 - Maintenance of Structural Strength |
1960 |
128 | 9705 - Airplane Balance & Unit Inertia Data
(2) |
1954-1958 |
128 | 9706 - Wing Unit Spanwise Airload Distributions Super
Constellation Models |
1954 April 1 |
129 | 9707 - Structural Design Criteria |
1954-1958 |
129 | 9708 - Net Wing Loads |
1954-1958 |
129 | 9709 - Net Fuselage Loads - Passenger & Cargo
Models |
1954-1958 |
129 | 9794 - Basic Cruising Performance, Lockheed Models 1049B, C,
& E, with WAD DA-1 Engines… |
1954 April 1 |
130 | 9837 - Model 1049F Fuselage Shell Section
Properties |
1954 May 21 |
130 | 9838 - Fuselage Internal Loads Model 1049F |
1954 July 30 |
130 | 9839 - Fuselage Shell Analysis Model 1049F |
1954 October 25 |
130 | 9866 - Engine Oil Consumption Experience Super Constellation
Aircraft |
1954 April 27 |
131 | 9905 - Model 1049 High Rate of Discharge Fire Extinguisher
System Mockup Tests at the Power Plant Laboratory |
1954 May 13 |
19 | A5344-11 - Manufacturer's Detail Model Specification for the
Model 749 Constellation Airplanes |
1947-1948 |
18 | A5344-20 - Manufacturer's Detail Model Specification for the
Model 749A Constellation Airplanes |
1949 September 2 |
9 | A5344-21 - Manufacturer's Detail Model Specification for the
649A Constellation Airplanes |
1949 September 9 |
13 | Charts presented during Transport Symposium |
1951 October 23 |
2 | Commercial C-69 Electrical Data Book - Part No.
P290233 |
1945 November |
2 | Commercial C-69 Electrical Data Book - Report No. 5563 Part
No. P290233 Change "B," |
1945 November |
3 | Commercial C-69 Electrical Data Book - Report No. 5563 Part
No. P290233 Change "E," |
1945 November |
3 | Constellation Electrical Data Book - Model
649-79-21 |
1946 April 1 |
12 | Control Cable Replacement Records - 049, 749, 749A, 1049,
1049G, & 1649A |
1958 |
14 | Control Cable Replacement Records - 049, 749, 749A, 1049,
1049G, & 1649A |
undated |
53 | Crack repair communications |
1954-1961 |
13 | ER 2-487 - Electrically Heated Windshield |
1951-1955 |
13 | ER 2-731 - Filters, Hydraulic, Aircraft |
1957 |
13 | ER 2-763 - Wheel & Brake Requirements |
1955 June |
103 | F5685 - Fuselage Bulkhead Analysis |
1946 October 4 |
14 | Full Scale Mockup Tests of Model 1649A Inboard & Outboard
Oil Systems |
1956-1957 |
61 | Functional Test A2500 - A2814 |
1955-1958 |
62 | Functional Test B - E |
1950-1957 |
62 | Functional Test F - H |
1950-1957 |
62 | Functional Test J - J2209 |
1946-1958 |
62 | Functional Test J2210 - J2309 |
1949-1958 |
63 | Functional Test J2310 - J2399 |
1951-1959 |
63 | Functional Test J2400 - J2449 |
1952-1959 |
63 | Functional Test J2452 - J2499 |
1954-1959 |
63 | Functional Test J2501 - J2559 |
1955-1958 |
63 | Functional Test J2560 - J2609 |
1956-1958 |
63 | Functional Test J2610 - J2835 |
1956-1958 |
61 | Functional Tests A2292 - A2499 |
1950-1958 |
61 | Functional Tests Index - A2291 |
circa 1945-1963 |
43 | Functional Tests K - K2005 |
1944-1955 |
43 | Functional Tests K2272 - K2379 |
1948-1957 |
43 | Functional Tests K2380 - K2569 |
1949-1957 |
44 | Functional Tests K2570 - K2717 |
1953-1960 |
44 | Functional Tests K2800 - M2009 |
1950-1957 |
44 | Functional Tests M2010 - N2079 |
1944-1957 |
44 | Functional Tests N2080 - N2259 |
1946-1960 |
44 | Functional Tests N2260 - P2019 |
1946-1958 |
45 | Functional Tests P2021 - P2319 |
1954-1958 |
45 | Functional Tests P2320 - P2817 |
1954-1958 |
13 | HSO-344 - Report on 1649A Autopilot/Booster Lab. & Fl.
Test Program LAC 1001 & TWA 320 |
1957 January 8 |
10 | Joint Investigation Report of Supercharger Failure Serial
#1185 |
1947 |
13 | LAC PCS-60-35 |
1960 |
13 | LAC Process Specification 1061 Repair of Aircraft
Structures |
1950-1951 |
12 | LAL 337 - Effect of Icing Conditions as Simulated by Spoilers
on 1/14 Scale 1049-G Aerodynamic Data |
1956 |
11 | LAS reports: 1119, 1120, 1121, 1122 (Ultrasonic Testing &
Inspection) |
1960 February |
13 | LASI Report 1043 - Weight & Balance Aircraft
611 |
1952 June 16 |
13 | LASI Report 1044 - Weight Report A/C 612 |
1952 June 23 |
13 | LASI Report 1051 - Supplement to be Added to Existing Weight
Report A/C # 605 |
1952 July 21 |
1 | Lockheed- Engineering Flight Test Division
Report |
1945 |
11 | MCRM 1904 - Metallurgical Analysis of Service-Failed Main
Landing Gear Outboard Actuating Arm Model 1649A |
1958 August 28 |
11 | MCRM 1909 - Metallurgical Analysis of Cracked Main Landing
Gear Outboard Actuating Arm - Model 1649A |
1958 September 23 |
11 | MCRM 1916 - Metallographic Analysis of Model 049
Service-Failed Pressure Bulkhead |
1958 November 7 |
12 | MCRM 1941 - Hydraulic Fluid Contamination Study - Model 1649
(2) |
1959 July 14 |
11 | MCRM No. 1826 - Metallurgical Examination of Service Failure
- Main Landing Gear Cap Weld - Model 1049-H |
1957 May |
11 | MCRM No. 1849 - Analysis of Causes of Cracking in a Main
Landing Gear Oleo Strut - Model 1049 |
1957 October 2 |
10 | MRM 2128 - Vacuum Pump Performance |
1941 November 5 |
7 | MRM# 3445 - Fuel Line Drain Icing Tests |
1957 February 22 |
11 | Removable Equipment Items for the Refurbished 749
Aircraft |
1955 November 23 |
13 | Report on 1649A Autopilot/Booster |
1957 January 8 |
13 | SDR 1031 - Installation of Berths in TWA 1049
Airplanes |
1951-1952 |
13 | SDR 1034 - Conversion of 60-Passenger Aircoach to
70-Passenger Version |
1952 February 23 |
11 | SDR 1082 - Specification Drinking Fountain Constellation
Sky-Tourist |
1952-1953 |
11 | SDR 1358 - Weight & Balance Calculations for TWA
Constellation 749 Aircraft |
1956 February 4 |
11 | SDR 1359 - Standard Equipment Items for the Refurbished 749
Aircraft TWA Plane 812 |
1956 February 4 |
12 | SDR 1361 - Weight & Balance Calculations for TWA
Constellation 749 Aircraft |
1956 February 18 |
12 | SDR 1362 - Standard Equipment Items for the Refurbished 749
Aircraft TWA Plane 829 Serial 2653 N 86522 |
1956 February 18 |
11 | SDR 1659 - Weight & Balance Data |
1957 November 12 |
11 | SDR 1660 - Weight & Balance Data |
1957 November 21 |
11 | SDR 1666 - Weight & Balance Data |
1957 December 3 |
11 | SDR 1669 - Weight & Balance Data |
1957 December 10 |
11 | SDR 1681 - Weight & Balance Data |
1957 December 20 |
11 | SDR 1687 - Weight & Balance Data |
1957 December 30 |
11 | SDR 1694 - Weight & Balance Data |
1958 January 9 |
11 | SDR 1697 - Weight & Balance Data |
1958 January 16 |
11 | SDR 1703 - Weight & Balance Data |
1958 January 24 |
11 | SDR 1704 - Weight & Balance Data |
1958 |
11 | SDR 1731 - Weight & Balance Data |
1958 February 10 |
11 | SDR 1743 - Weight & Balance Data |
1958 February 16 |
11 | SDR 1747 - Weight & Balance Data |
1958 February 27 |
11 | SDR 1748 - Weight & Balance Data |
1958 March 5 |
11 | SDR 1752 - Weight & Balance Data |
1958 March 13 |
7 | SDR 3025 A - Conversion of 1649A Airplane to Cargo
Configuration for Deutche Lufthansa |
1960 January 22 |
7 | SDR 3076 - Specification for Conversion of 1649A to Cargo
Configuration |
1960 February 15 |
53 | SDR 5079 - Weight Report TWA |
1960 October 13 |
106 | SDR 6016 - Stress Analysis TWA Jet Engine Cradle |
1960 December 8 |
11 | SDR/1937 - Conversion of Models 1049C, 1049E, & 1049G to
Cargo Configuration |
1959 January |
16 | SK72754 - Constellation Radio Data Book |
1954 July 29 |
11 | SLR/1010 - Super Constellation Model 1049 B for Cargo
Loadability Report |
1951 June 9 |
11 | SLR/1122 - Use of (U.S.) Cab Statistics on Operating Costs of
Civil Transport Aircraft |
1953 March 9 |
11 | SLR/1126 - Operational Performance Comparison Super
Constellation Airplanes with Turbocompound & Turboprop
Engines |
1953 January 27 |
11 | SLR/1154 - Preliminary Maintenance Cost Formulas for Turbojet
& Turboprop Engines |
1953 May 5 |
10 | SLR/1177 - Operations & Economic Analysis Cargo
Conversion Constellation Model 749A & 049D |
1954 February 23 |
10 | SLR/1200 - Method for the Estimation of Direct Operating
Costs of Aircraft |
1954 |
10 | SLR/1213 - Dimensional & Loading Data Cargo &
Passenger/Cargo Transports |
1954 April 29 |
11 | SLR/1502A - Aircraft Characteristics Super Constellation
Model 1049H/01 |
1957 February 15 |
12 | SLR/1584A - Super Constellation Model 1049H Economic Analysis
for TWA |
1957 June 18 |
12 | SLR/1584B - Super Constellation Model 1049H Route Analysis
for TWA |
1957 June 18 |
12 | SLR/1778 - The Effects of Various Operating Weight Limit
Improvements on Super Constellation Model 1049H
Operations |
1958 July 8 |
12 | SLR/1951 - Operational & Economic Analysis Super
Constellation Model 1649A Modified for Cargo |
1959 November 20 |
11 | SLR/1956 - Operational & Economic Analysis Super
Constellation Model 1049G Modified for Cargo |
1959 December 2 |
13 | SLR/667 - Airport Planning Aircraft Data for the
Constellation |
1946 April 3 |
12 | SLR/856 - Basic Data for Operations & Economic Analyses
Modelsamp; 1049G & H WAD DA-3 & EA-3 Engines |
1956-1957 |
126 | SP-9645 - Cargo Utilization System 1049-H
Constellation |
1960 April 4 |
11 | SRD 1308 - Standard & Removable Equipment for the
Convertible International/Domestic Cargo C-54 |
1955 October 12 |
11 | SRD-1336 - Standard Equipment Items for the Refurbishing 749
Aircraft TWA Plane 810 Serial 2646 |
1956 November 23 |
10 | SRM 349 - Investigation of Surface Cracking in TWA Sierracin
Cabin Windows |
1954 December 29 |
13 | SRM 372 - Investigation of Double Cabin Window Failure on a
TWA Model 1049 |
1956 January 16 |
13 | Stress Memos |
1949-1955 |
1 | Type Certificate Tests Lockheed Constellation |
1945 September 12 |
13 | W.S. 80 Joint - Investigation of Mislocation of Screw Holes
on Wing |
1952 September |
11 | Weight Study 1049E & 1049G Aircraft |
1959 June 24 |
Series V. Subject files, circa 1940-1980Return to Top
Contains reference materials from private and public companies and agencies, including manuals and reports.
Container(s) | Description | Dates |
---|---|---|
Box | ||
41 | 049 Drawing Manual |
1944-1945 |
58 | 1649A Operating Manual |
1959-1965 |
269 | Abex Corporation - Electro Hydraulic Servo Valve
Model |
undated |
219 | Abex Corporation - Electro Hydraulic Servo Valve
Model |
1968 |
269 | Abex Corporation - Engineering Design Proposal to Boeing for
Hydraulic Pump in Accordance with Specification |
1967 |
219 | ACF Industries - Preliminary Proposal for Navigation Display
System for Supersonic Transport |
1963 |
219 | Advance Data System Corporation - Technical Proposal for Marathon
Data Converter |
1962 |
219 | Aereon Corporation - Lifting Body Airship |
1967 |
219 | Aero Service - Supplement to Navigation Training Slide
Catalog |
1967-1968 |
219 | Aero Spacelines Incorporated - Preliminary Feasibility Study for
Conversion of Boeing 377 for Transporting Saturn SIVB Stafe |
1964 |
219 | Aero Spacelines Incorporated - Preliminary Report on Operators of
Boeing 377PG (Pregnant Guppy) |
1964 |
219 | Aero Spacelines Incorporated - Special Cargo Carrier Model
PG-2 |
1964 |
219 | Aeronautical Radio Incorporated - Avionics Maintenance Conference
in Miami |
1969-1970 |
219 | Aeronautical Radio Incorporated - Avionics Maintenance Conference
in Seattle |
1970 |
219 | Aeronautical Radio Incorporated - Extended Range VHF |
1964 |
219 | Aeronautical Radio Incorporated - Integral
Electronics |
1963 |
219 | Aeronautical Radio Incorporated - publication list |
1963 |
219 | Aeronautical Radio Incorporated - Story of UAL "C" Band Radar
Evaluation Program |
1954 |
219 | Aeronautical Research and Development - Hearings Before
Subcommittee on Advanced Research and Technology |
1968 |
219 | Aeronautical Research Institute of Sweden - Atmospheric
Magnification of Sonic Booms in the Oklahoma Tests |
1967 |
219 | Aeronautical Research Institute of Sweden - Menace of Sonic Boom
to Society and Civil Aviation |
1966 |
219 | Aeronautical Research Institute of Sweden - Pros and Cons of
Supersonic Aviation in Relation to Gains or Losses in Combined
Time/Comfort Consideration |
1964 |
219 | Aeronautical Research Institute of Sweden - Sonic Boom Waves in
Strong Winds |
1964 |
219 | Aerosmith Products Corporation - General Specifications Passenger
Seating "35" Series "Jet-Rest," |
undated |
219 | Aerospace Industries Association - Recommendations to FAA for
Noise Standards |
1969 |
219 | Aerospace Industries Association - Recommendations to FAA to
Improve Aircraft Safety |
1969 |
219 | Aerospace Industries Association - Transport Aircraft
Characteristics, Trends, Growth Projections |
1969 |
219 | Aerospace Industries Association of America - Aircraft Engine
Exhaust Emissions |
1968 |
220 | Aerotherm - Another New Concept |
1968 |
220 | Aerotherm - Bantam Passenger Seating Designs |
1965-1967 |
220 | Aerotherm - Bantam |
1967 |
219 | Aerotherm - Lit-Aire - Stretcher System |
undated |
219 | Aerotherm - MCR Basic Model 603G |
1961 |
219 | Aerotherm - Model 645 Deluxe Passenger Seat |
1965-1966 |
219 | Aerotherm - New Concept Tourist/Economy Passenger
Seating |
1965-1966 |
219 | Aerotherm - New Depths in First Class Seating |
1966 |
219-220 | Aerotherm - Preliminary Seating Designs for Boeing
747 |
1966 |
220 | Aerotherm - Proposal to TWA for Coach Passenger
Seats |
1970 |
220 | Aerotherm - Proposal to TWA for First Class Passenger
Seats |
1970 |
219 | Aerotherm - Safety Belt Energy Absorption |
1960 |
219 | Aerotherm - Specific Safety Harness Retracting Inertia Locking
Double |
1959 |
219 | Aerotherm - Static and Dynamic Test Report Model 643A-2 Passenger
Seat |
1962 |
219 | Aerotherm - Zephyr II - New Concept in First/Tourist/Economy
Passenger Seating |
1962 |
219 | Aerotherm - Zephyr II Design Studies - Convertible Type
Seat |
1964 |
219 | Aerotherm - Zephyr II Seats |
1966 |
220 | Agard - Application Dynamic Testing Procedures to Stability and
Control Flight Test Programs |
1958-1959 |
220 | Agard - Ceramics and Glass and Their Application in Modern
Aeronautics |
1958-1959 |
220 | Agard - Combustion Liquid Fuel |
1954 |
220 | Agard - Flight Tests with TU-104 |
1958-1959 |
220 | Agard - Measurements and Power Spectra of Runway Roughness of an
Airport |
1959-1961 |
220 | Agard - Mechano-Chemical Attack on Metals |
1957-1959 |
220 | Agard - Problem Structural Safety with Particular Reference to
Safety Requirements |
1957-1959 |
220 | Agard - Problems Associated with Measurements of Very Low
Pressures |
1958 |
220 | Agard - Runway Roughness Effects on Military
Aircraft |
1957-1959 |
220 | Agard - Shockwave Generation by Supersonic Airplanes |
1959-1961 |
220 | Agard - Transparent Materials for Aircraft |
1957 |
220 | Agard - Wind Tunnel Calibration Models |
1958-1959 |
221 | Air Canada - Aircraft Spraying Project |
1965-1968 |
221 | Air Canada - Laboratory Report - Corrosion Protection DC-8 Cargo
Compartments |
1967 |
221 | Air Canada - Mentzer Committee Recommendations for Water System
Supersonic Transport |
1968 |
221 | Air Canada - Study on Requirement for Removal of Precipitation
Accretion Prior to Takeoff |
1968 |
221 | Air Coordinating Committee - Federal Policy Regarding Development
of Commercial Transport Helicopters |
1951 |
221 | Air India - Boeing 747 Galley Requirement
Specification |
1969 |
221 | Air Land Systems Company - Digital Approach and Landing
System |
1969 |
221 | Air Transport Association of America - Achieving Better Landings
- All Weather Operations |
1969 |
221 | Air Transport Association of America - Airborne Collision
Avoidance System (CAS) - Statement of Airline Policy and Requirements
and Technical Description of System |
1971 |
221 | Air Transport Association of America - Airborne Collision
Avoidance System (CAS) |
1967-1968 |
221 | Air Transport Association of America - Airline System Economic
Impact Study |
1969 |
221 | Air Transport Association of America - Airport Surface
Conditions |
1965 |
221 | Air Transport Association of America - Design Manual on Aircraft
Fire Protection Engineering Memo |
1954-1956 |
221 | Air Transport Association of America - Design of Aircraft and
Equipment with Respect to Crash Survival |
1953 |
221 | Air Transport Association of America - Development Automated
Ultrasonic Facsimile Recording System Detection and Recording Corrosion
and Other Discontinuities in Aircraft |
1965 |
221 | Air Transport Association of America - Facts and Figures on Air
Transportation |
1960-1965 |
221 | Air Transport Association of America - Flight Test and Evaluation
of Airborne Collision Avoidance System (CAS) |
1970 |
221 | Air Transport Association of America - Legal
Considerations |
undated |
221 | Air Transport Association of America - National Air Traffic
Management System |
1969 |
221 | Air Transport Association of America - Proposed Noise
Studies |
undated |
221 | Air Transport Association of America - Radar Traffic Control
Preset Status and Future Plans |
undated |
221 | Air Transport Association of America - Safe Control of Expanding
Air Traffic |
1947 |
221 | Air Transport Association of America - Standard Method of
Estimating Comparative Direct Operating Costs of Transport
Airplanes |
undated |
221 | Air Transport Association of America - United States Airline and
Industry Forecast of Turbine Fuel Demand |
1967-1975 |
221 | Air Transport Association of America - Warm Fog Dispersal Test
Program |
1967-1968 |
221 | Air University - 999 Survived: Analysis of Survival Experiences
in the Southwest Pacific |
1953 |
221 | Air University - Airmen Against the Sea |
undated |
221 | Air University - Analysis of Survival Equipment |
1956 |
221 | Air University - Down in the North |
1953 |
221 | Air University - Jungle Survival Field Test |
1956 |
221 | Air University - Sun, Sand and Survival |
1953 |
222 | Airbus International - A300A Maintenance Objective Control During
Design |
1970 |
222 | Airbus International - A300B Analysis of Typical Maintenance
Costs and Investments |
1970 |
222 | Airbus International - A300B Design Features |
1969 |
222 | Airbus International - A300B Performance and Economics
Summary |
1970 |
222 | Airbus International - A300B Presentation |
1970 |
222 | Airbus International - A300B Route and Cost Study for
TWA |
1970 |
222 | Airbus International - A300B Support Division -
Performance |
1970 |
222 | Airbus International - Airplane Characteristics - Airport
Planning |
1970-1971 |
222 | Airbus International - Maintainability and Reliability Analysis
During Design |
1970 |
222 | Airbus International - Meeting the Challenge |
1969-1970 |
222 | Aircraft Industries Association - Aircraft Electrical
Installations Design Manual |
1950-1958 |
222 | Aircraft Industries Association - Aircraft Fire Protection Design
Manual |
1954 |
222 | Aircraft Industries Association - Aircraft Fire Protection for
Reciprocating and Gas Turbine Engine Installation Design
Manual |
1957 |
222 | Aircraft Industries Association - Aircraft Fire Protection
Report |
1947 |
222 | Aircraft Industries Association - MIL-F Fluid, Hydraulic,
Nonflammable Aircraft |
1950 |
222 | Aircraft Industries Association - NASC Ground-to-Aircraft
Servicing Connections Proposed for International
Standardization |
1947-1948 |
222 | Aircraft Industries Association - National Aircraft
Standards |
1952-1960 |
222 | Aircraft Industries Association - Oxygen Requirements for High
Altitude Transport Aircraft |
1957 |
222 | Aircraft Industries Association - Proposed MIL Specification for
Nonflammable Hydraulic Fuel |
1950 |
223 | AiResearch Manufacturing Company - Air Turbine Starter Model
ATS100-206 Specifications |
1964 |
223 | AiResearch Manufacturing Company - Air Turbine Starter Model
ATS100-239 Specifications |
1963 |
222 | AiResearch Manufacturing Company - Airline Products Facility -
Aircraft Seating |
undated |
223 | AiResearch Manufacturing Company - APU Installed Weight
Summary |
undated |
223 | AiResearch Manufacturing Company - Boeing 707 Starting System
Configuration |
1956 |
223 | AiResearch Manufacturing Company - Boeing 720 Integral Gas
Turbine Auxiliary Power System Specifications |
1962 |
223 | AiResearch Manufacturing Company - Boeing 727 Air Turbine Starter
Model ATS100-189 Specifications |
1962 |
223 | AiResearch Manufacturing Company - Boeing 727 Gas Turbine
Auxiliary Power Unit |
1963 |
223 | AiResearch Manufacturing Company - Boeing 727 Operating Costs
Parameters Short Haul Fan Jet Airplane |
undated |
223 | AiResearch Manufacturing Company - Boeing 727 Preproduction Air
Turbine Starter Model ATS100-189 Test Report |
1962 |
222 | AiResearch Manufacturing Company - Boeing 747 Auxiliary Power
Unit |
1966 |
222 | AiResearch Manufacturing Company - Boeing 747 Conceptual Studies
for Main Deck |
undated |
222 | AiResearch Manufacturing Company - Boeing 747 Electric Heater
Lower Lobe Galley Technical Proposal |
1970 |
223 | AiResearch Manufacturing Company - Boeing 747 Evaluation Study of
Environmental Control System Engine Starting |
1966 |
222 | AiResearch Manufacturing Company - Boeing 747 Gas Turbine
Auxiliary Power Unit Product Assurance Plans |
1966 |
223 | AiResearch Manufacturing Company - Boeing 747 Gas Turbine
Auxiliary Power Unit |
1966 |
223 | AiResearch Manufacturing Company - Boeing 747 Liquid Nitrogen
Refrigeration Systems for Aircraft Galleys Technical
Proposal |
1968 |
223 | AiResearch Manufacturing Company - Boeing 747 Preliminary
Proposal Air Data System |
undated |
223 | AiResearch Manufacturing Company - Capabilities for Supersonic
Transport Applications |
1961 |
223 | AiResearch Manufacturing Company - Concorde Supersonic Transport
Sliding Door Actuation System |
1970 |
222-223 | AiResearch Manufacturing Company - Concorde Thrust Reverser
Actuation System |
1970 |
223 | AiResearch Manufacturing Company - DC-9 Interim Reliability
Report - Environmental and Ice Protection Control Systems |
1967 |
223 | AiResearch Manufacturing Company - Design Data for SUD Supersonic
Transport Air Turbine Starters/Multi Purpose Starter System Electric
Power Generation Systems |
1962 |
223 | AiResearch Manufacturing Company - Economic and Operational
Evaluation of Self Contained Twin Jet Transport in Trans
Canada |
1963 |
223 | AiResearch Manufacturing Company - Final Report on Human
Tolerance to Rate of Change in Cabin Pressure |
1967 |
222 | AiResearch Manufacturing Company - Flight Test Report -
Refrigerated Air Cargo Container |
1967 |
223 | AiResearch Manufacturing Company - Galley Refrigeration Systems -
Liquid Nitrogen |
1967 |
222 | AiResearch Manufacturing Company - Galley Refrigeration Systems
Economic Evaluation Study |
1969 |
223 | AiResearch Manufacturing Company - Gas Turbine Auxiliary Power
Unit for Air Transport Industry (Model GTCP85) |
1963 |
222 | AiResearch Manufacturing Company - Gas Turbine Auxiliary Power
Unit Model Specifications |
1964 |
223 | AiResearch Manufacturing Company - Gas Turbine Compressor and
Power Unit Specification (Model GTCP85-291) |
1961 |
222 | AiResearch Manufacturing Company - General Specifications Mach
Number Meters Type 1a |
1956 |
223 | AiResearch Manufacturing Company - Integrated Secondary Power
System ADS |
1965 |
223 | AiResearch Manufacturing Company - Jumbo Transport |
undated |
222 | AiResearch Manufacturing Company - L01011 Liquid Nitrogen Galley
Refrigeration System |
1968 |
223 | AiResearch Manufacturing Company - Less-Than-Long-Range Transport
Pneumatic System Configurations |
1967 |
222 | AiResearch Manufacturing Company - Non-Destructive Radiographic
Inspection of Assembled Engine |
undated |
223 | AiResearch Manufacturing Company - Power Unit, Aircraft Auxiliary
Gas Turbine Service Type 4 Specifications |
1961 |
222 | AiResearch Manufacturing Company - Proposal to TWA for 707-331
Interiors |
undated |
222 | AiResearch Manufacturing Company - Spectrographic Oil Analysis
Program |
undated |
223 | AiResearch Manufacturing Company - Starting Systems |
1961 |
222 | AiResearch Manufacturing Company - Supersonic Transport Airframe
Systems Subcontractor Participation |
1966 |
223 | AiResearch Manufacturing Company - Supersonic Transport Design
Data Air Turbine Starters/Multi-Purpose Starter Systems Electric Power
Generation Systems |
1962 |
223 | AiResearch Manufacturing Company - T76 Turboprop
Engine |
circa 1965 |
223 | AiResearch Manufacturing Company - Technical Proposal - Combined
Jet Fuel Starter, Pneumatic Starter, Emergency Power Unit for
L-2000 |
1965 |
223 | AiResearch Manufacturing Company - Technical Proposal - Constant
Speed Drive Starter Model Designed for Installation on Rolls-Royce Spey
and Medway Engines |
1964 |
223 | AiResearch Manufacturing Company - Technical Proposal Engine
Pressure Ratio Indicating System |
1966 |
222 | AiResearch Manufacturing Company - Typical Central Air Data
Computing Systems |
1959 |
222 | Airtron Incorporated - Electrical Test Results of Double Ridge
Waveguide for Airborne Weather Penetration Radar Per ARINC
Characteristic |
1954 |
223 | All American Engineering Company - Proposal Sheaffer Spring Tail
Hook for Jets |
1960 |
223 | All American Engineering Company - Report on Evaluation Tests
Model 56C and 56D Runway Barrier Systems |
1961 |
223 | All American Engineering Company - Report on Feasibility Tests of
Aircraft-Mounted Arresting Hook |
1960 |
223 | All American Engineering Company - Runway Brakes Commercial Boost
for Airlines |
1958 |
223 | All American Engineering Company - Turbo Launch System 130,000 lb
Thrust a Boost for Commercial Aviation |
undated |
223 | Aluminum Company of America - Aluminum and Its
Alloys |
1947 |
220 | American Airlines - Description of Circuitry for Erasing Video
Signals Above Selected Threshold Level |
1949 |
220 | American Airlines - Designated Alternation Station Engineering
Evaluation, Litton LTN-51 Inertial Navigation System Final
Report |
1968 |
220 | American Airlines - Inter-Metropolitan STOL Evaluation Phase 10
Final Report |
1970 |
220 | American Airlines - NE Corridor VTOL Investigation
Docket |
1968 |
220 | American Airlines - Propulsion System Requirements for Supersonic
Transport |
1967 |
220 | American Airlines - RFC to Concorde Technical
Specification |
1967 |
220 | American Airlines - Study of Single APU vs. Dual APU vs. Ground
Support Equipment for Boeing 747 Ground Operations |
1966 |
220 | American Airlines - Turbofan Aircraft Engine Propulsion System
for Communication Subsonic Specifications |
1967 |
220 | American Airlines - Turbofan Aircraft Engine Propulsion System
for Supersonic Transport Specifications |
1967 |
224 | American Machine and Foundry Company - 463L Materials Handling
Support System |
1961 |
220 | American Machine and Foundry Company - Mechanized Air Freight
Terminal - Travis Air Force Base |
undated |
220 | American Machine and Foundry Company - Typical Airline Terminal
Study |
undated |
220 | American Machine and Foundry Company - Unifreight |
undated |
224 | American Machine and Foundry Company |
1961-1964 |
224 | American Museum of Safety - Ground Safety in Aviation
Operations |
1954 |
224 | American Petroleum Institute - Airport Fueling
Systems |
1954-1957 |
224 | American Petroleum Institute - Filtration and Dehydration of
Aviation Fuel |
1955-1957 |
224 | American Petroleum Institute - Fueling Turbine-Powered
Aircraft |
1957 |
224 | American Petroleum Institute - Storage and Handling of Jet Fuels
at Airports |
1956 |
224 | American Rocket Society - Jet Propulsion |
1954 |
224 | American Rocket Society - roster |
1953-1954 |
224 | American Society for Testing Materials - Activities of the ASTM
in the Field of Lubricants and Lubrication |
1948 |
224 | American Society for Testing Materials - Determination of Sulfur
in Petroleum Oils |
1948 |
224 | American Society for Testing Materials - Effects of Grinding
Direction and Abrasive Tumbling on Fatigue Limit of Hardened
Steel |
1958 |
224 | American Society for Testing Materials - Filtration Study to
Determine Test Methods |
1956 |
224 | American Society for Testing Materials - Methods for Reducing
Effect of Barometric Pressure in Measurement of Octane
Number |
1956 |
224 | American Society for Testing Materials - Relative
Stress-Corrosion Susceptibility of Titanium Alloys in Presence of Hot
Salt |
1964 |
224 | American Society for Testing Materials - Sampling of Liquefied
Petroleum Gases |
undated |
224 | American Society for Testing Materials -
Specifications |
1964 |
224 | American Society for Testing Materials - Volume Correction and
Specific Gravity Conversion of Liquefied Petroleum Gases |
1948 |
224 | American Society of Mechanical Engineers - ASME Role in Powered
Flight |
1954 |
224 | American Society of Mechanical Engineers - New Concept for
Passenger Handling - Airport Mobile Lounge |
1960 |
224 | American Society of Mechanical Engineers - Slotted and Recessed
Head Tapping Screws and Metallic Drive Screws |
1955-1957 |
224 | American Society of Mechanical Engineers - Sperry Engine Analyzer
- New Method of Gas Engine Supervision |
undated |
224 | American Society of Mechanical Engineers - Turbojet Engine Design
for High Speed Flight |
1950 |
185 | Another Step Forward with TWA and the DC-9 |
1965-1966 |
224 | Apco Accessory Products - Program Management and Pricing Proposal
Boeing 747 Flame Protection System Fuel Tank Vent |
1967 |
224 | Aquafine Corporation - Water Filters |
1955 |
224 | Argus - New Guidance System |
1969 |
177 | Army Air Force Contract No. W-33-038-ac-9489 Final Report
Aircraft Power Plant Fire Protection |
1948 February |
224 | Aro Equipment Corporation - 1800 Cubic Inch Survival Kit
Proposal |
undated |
224 | Aro Equipment Corporation - Gas Turbine Starting Oxygen Assist
System Proposal |
undated |
224 | Aro Equipment Corporation - Instructions for Handling
Oxygen |
undated |
224 | Aro Equipment Corporation - Liquid Oxygen System CV22
Proposal |
1957 |
224 | Aro Equipment Corporation - Proposal for Oxygen, Manifold
Regulator |
1956 |
224 | Ashland Oil Company - Reclamation of JP-6 Type Jet Fuels Which
Became Thermally Unstable During Storage |
1964 |
224 | Ashland Oil Company - Special Jet Propulsion and Missile
Fuels |
1959 |
224 | Astek Instrument Corporation - Flight Instrument and Air Data
System |
1962 |
224 | Atkins and Merrill Incorporated - L-1011 Cockpit Procedures
Trainer |
1970-1971 |
224 | Atlantic Aviation Corporation - Design Concept for L-1-11
Prototype Food Cart Tray Carrier |
1971 |
224 | Atlantic Research - 30 mm Personnel Distress Signal |
1969 |
224 | Autonetics - Compensation of Aircraft Static Pressure
Errors |
1957 |
224 | Autonetics - Inertial Guidance for Cruise Vehicles |
1964 |
224 | Autonetics - Inertial Navigation |
1958 |
224 | Autonetics - Mechanization of Supersonic Transport Inertial
Navigation Computations in an A11-DDA Computer |
1964 |
224 | Aviation Writers Association - Panel Discussion on Aviation
Safety |
1957 |
224 | Avions Marcel Dessault - Mercure - Short-Haul
Presentation |
1970 |
224 | Avions Marcel Dessault - Mercure Market Study TWA |
1970 |
224 | Avions Marcel Dessault - Mercure Short-Haul
Transport |
1970 |
224 | Avions Marcel Dessault - Mercure with JT8D-15
Engines |
1970 |
224 | Avions Marcel Dessault - Mercure |
1969 |
225 | Baldwing-Lima-Hamilton Corporation - Integral Aircraft Weighing
System |
1964 |
225 | Baldwing-Lima-Hamilton Corporation - Technical Data Compiled by
BLH on the On-Board Aircraft Weighing Systems |
1968 |
225 | Baldwing-Lima-Hamilton Corporation - Test Data on TWA 8793
(B320C) with On-Board Aircraft Weighing System |
1969 |
225 | Batelle Development Corporation - Boundary Layer
Control |
1970 |
225 | Batelle Memorial Institute - Elastomers for Fuel Systems
Containing Microorganism-Controlling Additives |
1962-1964 |
225 | Bearing Inspection Incorporated - Ball and Roller Bearings -
Greater Reliability Through Failure Analysis and Rigid
Inspection |
1962-1964 |
225 | Beech Aircraft Corporation - Effect of Jet Blast or Wake on Other
Aircraft |
1955 |
225 | Bell Aerosystems - Ground Based Tactical Landing
System |
1969 |
225 | Bell Aerosystems - Instrument Landing System |
1969 |
225 | Bell Aerosystems - Thermal Stress Determination Techniques in
Supersonic Aircraft Structures |
1962 |
228 | Bendix Corporation - Aerospace Division - Boeing 707-120B Brake
Energy Analysis |
1961 |
228 | Bendix Corporation - Aerospace Division - Boeing 727-200
Technical Proposal for Wheels and Brakes |
1966 |
228 | Bendix Corporation - Aerospace Division - Boeing 747 Main Landing
Gear Wheels/Brakes - Engineering Design Proposal |
1967 |
228 | Bendix Corporation - Aerospace Division - Boeing 747 Main Landing
Gear Wheels/Brakes - Program Management Plan |
1967 |
229 | Bendix Corporation - Avionics Division - Avionics Design
Summary |
1969 |
229 | Bendix Corporation - Avionics Division - DFA-74 ADF System
Maintenance Manual |
1970 |
228 | Bendix Corporation - Avionics Division - DFA-74 ADF
System |
undated |
228-229 | Bendix Corporation - Avionics Division - DMA-31 Digital DME
System |
1968-1969 |
229 | Bendix Corporation - Avionics Division - RDR-1F Weather Radar
System |
1969 |
228-229 | Bendix Corporation - Avionics Division - RNA-27A VHF VOR/ILS
Navigation Receiver |
1969 |
228 | Bendix Corporation - Avionics Division - RTA-42 VHF Transceiver -
Instruction Manual |
1968 |
229 | Bendix Corporation - Avionics Division - RVA-33 VOR Receiver
Design Summary |
1970 |
229 | Bendix Corporation - Eclipse-Pioneer Division - Addition of
Attitude Monitoring to 300 Series Flight Director System |
undated |
229 | Bendix Corporation - Eclipse-Pioneer Division - Analytical Study
of ILS Beam Characteristics |
1962 |
229 | Bendix Corporation - Electric Power Division - Bearing Failure
Sensing and Oil Lubrication vs. Grease Lubrication for Aircraft
Generators |
1968 |
229 | Bendix Corporation - Filter Division - Cleaner Hydraulic Systems
with Microedge Filters |
1963 |
229 | Bendix Corporation - Instrument and Life Support Division -
Boeing 747 Liquid Nitrogen Refrigeration System |
1968 |
229 | Bendix Corporation - Instrument and Life Support Division - Crew
Oxygen System Panel Mounted Regulator |
1969 |
229 | Bendix Corporation - Pioneer-Central Division - Automatic
Altitude Reporting |
1964 |
229 | Bendix Corporation - Pioneer-Central Division - Automatic
Continuous Flow Oxygen Regulator Hi Capacity for Transport
Aircraft |
1955 |
229 | Bendix Corporation - Products Division - Boeing 707 AP-143 Main
Wheel and Brake Plus Nose Wheel Equipment |
1956 |
229 | Bendix Corporation - Radio Division - 3rd Avionics Engineering
Symposium Proceedings |
1961 |
228 | Bendix Corporation - Radio Division - ADF System Test Panel -
Test Equipment - Operation and Maintenance Handbook |
1963 |
228 | Bendix Corporation - Radio Division - ADF-73 Automatic Direction
Finder System - Maintenance Instruction Manual |
1963 |
228 | Bendix Corporation - Radio Division - Air to Air Synchronization
Without Addressing for Collision Avoidance System |
1967 |
228 | Bendix Corporation - Radio Division - ALA-51 Airborne Low-Range
Radio Altimeter System - TSO Test Report |
1966 |
228 | Bendix Corporation - Radio Division - ALA-51A Radio Altimeter -
Overhaul Manual |
1966 |
228 | Bendix Corporation - Radio Division - ANA-42A VHF Airborne
Antenna for Satellite Communication - Engineering Report |
1967 |
228 | Bendix Corporation - Radio Division - CNA-24/CPA-24 Navigation
Computer - TWA Autopilot Mod |
1961 |
227 | Bendix Corporation - Radio Division - CPA-24 Navigation Computer
System - Doppler Computer Controllers - Maintenance and Overhaul
Instruction Manuals |
1966, 1970 |
227 | Bendix Corporation - Radio Division - CPA-24 Navigation Computer
System - Doppler Navigation Computers - Maintenance Instruction
Manuals |
1966, 1973 |
227 | Bendix Corporation - Radio Division - CPA-24 Navigation Computer
System - Installation Instruction Manual |
1963 |
228 | Bendix Corporation - Radio Division - CPA-24 Navigation Computer
System Use With DRA-12 Doppler Radar System |
1961 |
228 | Bendix Corporation - Radio Division - DFA-73A ADF Receiver - TSO
Test |
1962 |
229 | Bendix Corporation - Radio Division - DRA-12 Doppler Radar
Navigation System |
1967 |
227 | Bendix Corporation - Radio Division - DRA-12 Doppler Radar System
- Antennas - Overhaul Manual |
1962, 1973 |
227 | Bendix Corporation - Radio Division - DRA-12 Doppler Radar System
- Control Panel and Indicator - Maintenance Instruction
Manual |
1962 |
227 | Bendix Corporation - Radio Division - DRA-12 Doppler Radar System
- Doppler Frequency Tracker - Instruction Manual |
1967 |
227 | Bendix Corporation - Radio Division - DRA-12 Doppler Radar System
- Transmitter-Receiver - Maintenance Instruction Manual |
1961 |
228 | Bendix Corporation - Radio Division - Fail-Safe DC Comparison
Monitor for use in Low Approach Landing Systems |
1966 |
228 | Bendix Corporation - Radio Division - Frequency Diversity Time
Multiplex Technique for Increasing Capacity of a Common System
CAS |
1967 |
228 | Bendix Corporation - Radio Division - INA-51 Altimeter Indicator
- Overhaul Manual |
1967 |
228 | Bendix Corporation - Radio Division - MKA-28C, D - Marker
Receiver - Overhaul Manual |
1966, 1969 |
229 | Bendix Corporation - Radio Division - MKA-28C, D - Marker
Receiver - Technical Pamphlet |
1966 |
228 | Bendix Corporation - Radio Division - Power Allocation
Considerations for Collision Avoidance System |
1967 |
229 | Bendix Corporation - Radio Division - Proposed RF Switching and
Control Logic for VHF Satellite Communication System |
1966 |
229 | Bendix Corporation - Radio Division - RDR-1E Airborne Weather
Radar System - Overhaul Manual |
undated |
229 | Bendix Corporation - Radio Division - RDR-1F Weather Radar
System |
1958 |
228 | Bendix Corporation - Radio Division - RNA-26C VHF Navigation
Receiver - Descriptive Data |
undated |
229 | Bendix Corporation - Radio Division - RNA-26C VHF Navigation
Receiver - Localizer/Glide Slope |
1966 |
228 | Bendix Corporation - Radio Division - RNA-26C VHF Navigation
Receiver - Overhaul Manual |
1966 |
229 | Bendix Corporation - Radio Division - RNA-26C VHF Navigation
Receiver - Reliability and Maintainability |
1967 |
228 | Bendix Corporation - Radio Division - RNA-26C VHF Reliability,
Maintainability, and Fault Analysis |
1967 |
229 | Bendix Corporation - Radio Division - RNA-26CF Flight Inspection
System |
undated |
229 | Bendix Corporation - Radio Division - RTA-41A, B VHF Transceiver
- Overhaul Manual |
1965 |
228-229 | Bendix Corporation - Radio Division - RTA-42 VHF
Transceiver |
undated |
228 | Bendix Corporation - Radio Division - Use of Slant Distance
Uncorrected for Altitude in Parallel Track Navigation - Engineering
Report |
1967 |
229 | Bendix Corporation - Radio Division - VHF Aircraft Satellite
Relay - Flight Test Final Report |
1965 |
228 | Bendix Corporation - Scintilla Division - Flameout Sensor for
Automatic Relight |
1962 |
228 | Bendix Corporation - Scintilla Division - Specifications for
Automatic Ignition Actuator |
undated |
228 | Bendix Corporation - Utica Division - Air Breathing
Starter |
1963 |
225 | BOAC - Air Safety Review |
1971 |
226 | Boeing Company - 131 and 331 Operation Costs and Revenue
Potential for Various Passenger Configurations |
1956-1961 |
261 | Boeing Company - 473 Jet Transport Brochure |
undated |
226 | Boeing Company - 707 - Flight Test Evaluation of Effect of Sound
Damping Tape on Passenger Cabin Sound Levels |
1965 |
226 | Boeing Company - 707 - Investigation of Epon 933 as a Liquid Shim
Material |
1964 |
259 | Boeing Company - 707 Airplane Weight and Operational
Status |
1957 |
260 | Boeing Company - 707 and 720 Structural Improvement
Program |
1966 |
260 | Boeing Company - 707 and 727 Deceleration Data |
1962-1965 |
260 | Boeing Company - 707 and 727 Ground Clearance Angles |
1963 |
260 | Boeing Company - 707 and 727 Interiors Superjet Look for
TWA |
undated |
260 | Boeing Company - 707 and 727 New Airplane Interiors |
1971 |
258 | Boeing Company - 707 Basic Aerodynamic Drag Data |
1954 |
261 | Boeing Company - 707 Brochure |
undated |
259 | Boeing Company - 707 Estimated Noise Level Profiles |
1955 |
259 | Boeing Company - 707 Passenger Berth Mock-Up
Demonstration |
undated |
260 | Boeing Company - 707 Performance with JT3D-3 and JT3D-3(B)
Engines |
1963 |
259 | Boeing Company - 707 Radiographic Inspection Details of Aft Rib
Landing Gear Support |
undated |
261 | Boeing Company - 707 Technical Data |
1952-1955 |
258 | Boeing Company - 707-120 Noise Profile - Advanced Wet/Dry
Thrust |
1958 |
258 | Boeing Company - 707-120B Integrated Range Data |
1959 |
260 | Boeing Company - 707-120B Spec Range Curves Results of Drag
Improvement Program |
1960 |
260 | Boeing Company - 707-121B Wing Leading Edge
Modification |
undated |
258 | Boeing Company - 707-131B Retrofit Kit to Convert |
1959 |
259 | Boeing Company - 707-220 Stratoliner JT4A-3 Engines |
1955 |
258 | Boeing Company - 707-420 Intercontinental
Stratoliner |
undated |
260 | Boeing Company - 707-620/820-504 Performance Data |
1964 |
260 | Boeing Company - 720 Performance |
1960 |
226 | Boeing Company - 720-051B |
1961 |
260 | Boeing Company - 727 and 707 Superjet Look for TWA
Interiors |
undated |
226 | Boeing Company - 727 and 737 Flight Management
System |
1978 |
260 | Boeing Company - 727 ATA Conference, Engineering and
Maintenance |
1970 |
260 | Boeing Company - 727 Balance |
1959 |
260 | Boeing Company - 727 Cargo Plane |
1963 |
260 | Boeing Company - 727 Fire Detection |
1961-1962 |
260 | Boeing Company - 727 Improvement Program for TWA |
1969 |
260 | Boeing Company - 727 Landing Diagrams |
1962 |
260 | Boeing Company - 727 Miscellaneous Performance
Charts |
1966-1967 |
260 | Boeing Company - 727 Significant Service Item
Summary |
1971 |
260 | Boeing Company - 727 Stall Characteristics |
1964 |
260 | Boeing Company - 727 Stall Design Considerations |
1964 |
260 | Boeing Company - 727-100 Extended Range Study |
1967 |
226 | Boeing Company - 727-200 Community Noise Characteristics of
JT8D-7 Engines During Takeoff and Landing |
1967 |
226 | Boeing Company - 727-200 Community Noise Characteristics of
JT8D-9 (BG-5) Engines |
1968 |
226 | Boeing Company - 727-200 Effect of Installation of Acoustically
Treated JT8D-9S Installed Engine |
1968 |
261 | Boeing Company - 727-200 General Description |
1977 |
260 | Boeing Company - 727-200 Ground Handling
Characteristics |
1968 |
260 | Boeing Company - 727-200 Superjet Look for TWA
Interiors |
1969 |
260 | Boeing Company - 727-200 |
1967 |
260 | Boeing Company - 727-300 Performance Data |
1969 |
260 | Boeing Company - 727-31C/QC TWA Loadability Study |
1965 |
260 | Boeing Company - 737 Brochure |
1964 |
260 | Boeing Company - 737 Performance with JT8D-9 Engines |
1966 |
261 | Boeing Company - 737-200C Advanced for Saudi Arabian
Airlines |
undated |
261 | Boeing Company - 737-200C Study Configuration and Weight Data for
Proposed Saudi Arabian Airplane |
1969 |
261 | Boeing Company - 747 Airport Pavement Strength
Requirements |
1966 |
226 | Boeing Company - 747 and Supersonic Transport 1971-1976 Airport
Activity Report |
1966 |
226 | Boeing Company - 747 APU Noise Survey |
1970 |
261 | Boeing Company - 747 Cargo Terminal and Container
Meeting |
1966 |
261 | Boeing Company - 747 Community Noise Level |
1966 |
261 | Boeing Company - 747 Emergency Equipment and
Evacuation |
1967 |
261 | Boeing Company - 747 Flight Crew Emergency Equipment and Escape
Provisions |
undated |
261 | Boeing Company - 747 for TWA Route Study and Takeoff Gross Weight
Comparison |
1968 |
261 | Boeing Company - 747 General Description |
1967 |
226 | Boeing Company - 747 Noise Levels in Near Vicinity of Airplane
RA101 |
1969 |
261 | Boeing Company - 747 Operational and Economic
Evaluation |
1966 |
261 | Boeing Company - 747 Passenger Oxygen System |
undated |
261 | Boeing Company - 747 Potable Water System |
undated |
261 | Boeing Company - 747 Prepared for TWA - Meeting of Board of
Directors |
1966 |
261 | Boeing Company - 747 Single Deck Airplane Study |
1965 |
261 | Boeing Company - 747 Weight Summary for TWA Route Analysis and
Design Improvement Changes |
1967 |
261 | Boeing Company - 747-331B Route Analysis |
1966 |
261 | Boeing Company - 757 Airbus Presentation to TWA, WH Spannuth/NR
Parmet |
1967 |
226 | Boeing Company - 757 Program Review |
1978 |
226 | Boeing Company - 757 Rolls-Royce RB. 211-535 |
1978 |
261 | Boeing Company - 757 TWA Airbus Review |
1967 |
260 | Boeing Company - 767 Motorpump Proposal |
1979 |
261 | Boeing Company - 767 New Airplane Program Presentation to
TWA |
1969 |
261 | Boeing Company - 767 Program Review |
1978 |
259 | Boeing Company - Air Cargo by Stanley H. Brewer |
1957-1965 |
258 | Boeing Company - Air Cargo Density Study |
1970 |
261 | Boeing Company - Airport Activity Analysis and Supersonic
Transport |
1967-1976 |
259 | Boeing Company - Airport Noise Study |
1966 |
259 | Boeing Company - All-Weather Program |
1962 |
258 | Boeing Company - Analysis of TWA Cargo Systems |
1971 |
259 | Boeing Company - Cargo and Intermediate Cargo-Passenger
Configurations |
undated |
258 | Boeing Company - Charts |
undated |
258 | Boeing Company - Color and Material Proposal for
Galley |
1968 |
258 | Boeing Company - Development of Air Mobility by Helicopter from
Korea through Algeria, Vietnam, and Israel |
1968 |
226 | Boeing Company - Domestic Air Traffic Forecast
1925-1975 |
1961-1962 |
259 | Boeing Company - Domestic Air Traffic Forecast
1961-1975 |
1961-1975 |
260 | Boeing Company - Evaluation 120B Conversion Data |
1959 |
259 | Boeing Company - Feasibility Study VSTOL Concepts for Short Haul
Transport Aircraft - Technical Proposal |
1965 |
259 | Boeing Company - Field Service Cost and Flow Time Comparison of
Painted VS Scotch CAL Insignia |
1957 |
258 | Boeing Company - Fleet Plan Summary |
1971-1975 |
261 | Boeing Company - Flight Deck Review |
1978 |
258 | Boeing Company - Flight Operations Services Program |
1971 |
226 | Boeing Company - Flight Test of GE 40KVA VSCF AC Generating
System 10-61419 |
1967-1969 |
226 | Boeing Company - Floor Panel Evaluation Using the Sheep's Foot
Roller |
1966 |
226 | Boeing Company - Forecast of Free World Passenger and Air Cargo
Traffic 1965-1975 |
1959 |
261 | Boeing Company - Friction Study of Aircraft Tire Material on
Concrete |
1950 |
261 | Boeing Company - High Altitude Indoctrination Notes |
1958 |
226 | Boeing Company - Hi-Lok Seal Collars - Effects of Teflon Seal
Extrusion |
1969 |
259 | Boeing Company - Investigation Lifting Effects on Intensity of
Sonic Boom |
1960 |
261 | Boeing Company - Jet Fleet Statistics |
1978 |
261 | Boeing Company - Jet Transport of Tomorrow |
undated |
261 | Boeing Company - Jet Transports Brochure |
undated |
259 | Boeing Company - La Guardia Study |
1961 |
259 | Boeing Company - Main Landing Gear Incidents |
1959-1960 |
258 | Boeing Company - Maintainability Design Guide for Design
Engineers |
undated |
259 | Boeing Company - Material Specifications |
1951-1960 |
258 | Boeing Company - Method of Passenger Allocation in Fleet
Planning |
1964 |
260 | Boeing Company - New York Visit |
1970 |
259 | Boeing Company - Next 12 Years - Forecast and
Analysis |
1967 |
226 | Boeing Company - Operations with Supersonic
Transport |
1966 |
226 | Boeing Company - Operations with the Supersonic Transport
1975-1980 Routes, Schedules, Operations with 2707 Supersonic
Transport |
1966-1967 |
226 | Boeing Company - Pedigree of Champions: Boeing Since
1916 |
1963 |
226 | Boeing Company - Performance and Economic Analysis Model 733
Supersonic Transport |
1964 |
258 | Boeing Company - Performance, Economics, and Noise Team Meeting
Presentation Material |
1969 |
226 | Boeing Company - Pratt and Whitney JT8D-209 for the Eighties and
Beyond |
1978 |
261 | Boeing Company - Program Status |
1977 |
260 | Boeing Company - Ram and Static Air Temperature
Calibration |
1960-1961 |
258 | Boeing Company - Range and Takeoff Weight Growth
History |
1968 |
258 | Boeing Company - Results of Performance Audit |
undated |
226 | Boeing Company - Route and Economic Analysis of Advanced
Supersonic Transport for TWA |
1966 |
259 | Boeing Company - Sabena Accident Review |
1961 |
258 | Boeing Company - Seat Study |
undated |
259 | Boeing Company - Sonic Boom Study |
1966 |
259 | Boeing Company - Standards for Reliability of Cabin
Pressurization Equipment |
1958 |
258 | Boeing Company - Statement of Airport Problem by J. E.
Steiner |
1966 |
258 | Boeing Company - Study and Development of Turbofan Nacelle
Modifications to Minimize Fan-Compressor Noise Radiation |
1967 |
259 | Boeing Company - Study Development Turbofan Nacelle Modification
to Minimize Fan Compressor Noise Radiation |
1968 |
259 | Boeing Company - Summary Brewer Report on Domestic Air
Cargo |
1957 |
259 | Boeing Company - Summary of Low Temperature Fuel Tests of
Aircraft Fuel Systems |
1956 |
226 | Boeing Company - Supersonic Transport Cost Factors |
1966 |
260 | Boeing Company - Support to Airline Operations TWA
Visit |
1970 |
258 | Boeing Company - Traffic Forecast |
1966 |
261 | Boeing Company - Tri-Jet Development |
1978 |
260 | Boeing Company - TWA Presentation: Boeing Support to Airline
Operations |
1970 |
259 | Boeing Company - TWA Production Status Report |
1957-1971 |
259 | Boeing Company - U.S.-International Air Cargo Future by Stanley
H. Brewer |
1958 |
259 | Boeing Company - Under-Seat Restraint Study |
1969 |
226 | Boeing Company - Wire Comparison Study |
1964 |
225 | Bolt Beranek and Newman - Convair 880 Exterior Noise from Flight
and Ground Operations |
1959-1964 |
225 | Bolt Beranek and Newman - General Electric Caravelle Exterior
Noise from Flight and Ground Operations |
1961 |
225 | Bolt Beranek and Newman - L-1011 Hi-Fi Public Address and
Boarding Music System |
1969 |
225 | Bolt Beranek and Newman - Seats |
undated |
225 | Booz-Allen Applied Research - Supersonic Transport Development
and Production Cost Analysis Program |
1966 |
225 | Bowmar/Tic Incorporated - Galley Oven Demonstration |
1970 |
225 | BP Research Centre - Draft Tables for Calculating Aromatics,
Luminometer Number, and Smoke Point of ATK from Gravity and Aniline
Point |
1966-1967 |
230 | Bristol Siddeley - BS75 Brochure |
1960 |
230 | Bristol Siddeley - BS75 Ducted Fan Engine -
Performance |
1960 |
230 | Bristol Siddeley - BS75 for British Aircraft - Engineering and
Commercial Considerations |
1960 |
230 | Bristol Siddeley - Concorde Customer Conference - Olympus 593
Power Plant Presentation |
1965 |
230 | Bristol Siddeley - Concorde Customer Conference at Bristol,
Paris, and Toulouse |
1966 |
229 | Bristol Siddeley - Olympus 593 Control System |
1966 |
229 | Bristol Siddeley - Olympus 593 Customer Requirements
Committee |
1966 |
229 | Bristol Siddeley - Olympus 593 Engine and Exhaust
System |
1966 |
230 | Bristol Siddeley - Olympus 593 Engines in Concorde Supersonic
Transport |
1967 |
230 | Bristol Siddeley - Olympus 593 Exhaust System -
Concorde |
undated |
230 | Bristol Siddeley - Olympus 593 for Concorde |
1964-1966 |
230 | Bristol Siddeley - Olympus 593 for SUD/BAC Concorde |
1964 |
230 | Bristol Siddeley - Olympus 593 Low-Pressure Fuel
System |
1967 |
230 | Bristol Siddeley - Olympus 593 Maintenance -
Concorde |
1969 |
230 | Bristol Siddeley - Olympus 593 Performance Data |
1965 |
229 | Bristol Siddeley - Olympus 593 Power Plant
Presentation |
1965 |
229 | Bristol Siddeley - Olympus 593 Preliminary Data |
1964 |
230 | Bristol Siddeley - Olympus 593 Specification for Concorde Mark
601 Engines |
1967-1970 |
230 | Bristol Siddeley - Olympus 593 Technical Progress
Report |
1965 |
229 | Bristol Siddeley - Olympus 593 Transport Trailer |
1966 |
229 | Bristol Siddeley - Olympus 593B in Concorde - Preliminary
Analysis of Engine Change Time |
1965 |
229 | Bristol Siddeley - Olympus 593B in Concorde - Technical Notes
Following Concorde Customers Conference |
1965 |
229 | Bristol Siddeley - Propulsion Controls on the
Concorde |
1966 |
229 | Bristol Siddeley - Viper 500 Series Engines in HS 125 Aircraft -
Warranty |
1966 |
229 | Bristol Siddeley |
1960 |
234 | British Aircraft Corporation - Air Travel Market and Supersonic
Transport Fare Differential |
1966 |
233 | British Aircraft Corporation - Airport Planning Data |
1976 |
234 | British Aircraft Corporation - Analysis of Relative Merits of
Operating with 2 Reversers and a Braking Parachute Compared with 4
Thrust Reversers |
undated |
234 | British Aircraft Corporation - Appraisal of Concorde
Economics |
1966 |
232 | British Aircraft Corporation - ASC Subcommittee Environmental
Control System |
1970 |
233 | British Aircraft Corporation - ASC Subcommittee Passenger
Evacuation |
1970-1971 |
232 | British Aircraft Corporation - ASC Subcommittees - Concorde
Passenger and Cargo Accommodation |
1969 |
233 | British Aircraft Corporation - ASE Environmental Control System
Meeting in Toulouse |
1968 |
231 | British Aircraft Corporation - BAC 3-11 Aircraft Characteristics
for Airport Planning |
1969 |
231 | British Aircraft Corporation - BAC 3-11 Brochure |
1967 |
231 | British Aircraft Corporation - BAC 3-11 Engineering
Features |
1969 |
231 | British Aircraft Corporation - BAC 3-11 Performance
Data |
1969 |
231 | British Aircraft Corporation - BAC 3-11 Project
Progress |
1969 |
231 | British Aircraft Corporation - BAC 3-11 Study for
TWA |
1969 |
234 | British Aircraft Corporation - BAC/SUD Concorde - Cabin Interior
and Emergency Evacuation Philosophy |
1965 |
234 | British Aircraft Corporation - BAC/SUD Concorde Preliminary
Performance Information |
1963 |
234 | British Aircraft Corporation - BAC/SUD Concorde Progress of Major
Structural Tests |
1966 |
231 | British Aircraft Corporation - BAC/SUD Concorde Specification
Review Airline Requests for Studies |
1967 |
232 | British Aircraft Corporation - BAC/SUD Concorde Specification
Review and Standardization/PAA/Electric Power System |
undated |
231 | British Aircraft Corporation - Boeing 747 Specification for
Rumbold Consort Seat Range |
1969 |
231 | British Aircraft Corporation - Boeing 747 Specification for
Rumbold First Class Seat |
1969 |
233 | British Aircraft Corporation - Combustion Chamber
Airworthiness |
1969 |
234 | British Aircraft Corporation - Community Noise and the
Concorde |
1966 |
234 | British Aircraft Corporation - Comparison of Direct and Total
Operating Costs - Concorde vs. Boeing 707 |
1965 |
233 | British Aircraft Corporation - Concorde - Airport and Terminal
Operations |
1969 |
234 | British Aircraft Corporation - Concorde - Alternative Interior
Center Galley Rear Toilets |
1969 |
233 | British Aircraft Corporation - Concorde - ASC Meeting in
Miami |
1971 |
233 | British Aircraft Corporation - Concorde - Basic Production Flight
Deck Review with Airlines |
1967 |
234 | British Aircraft Corporation - Concorde - Cabin Decompressions
with Emergency Descent |
1965 |
232 | British Aircraft Corporation - Concorde - Characteristics for
Evaluation of Static Strength of Runways |
1967 |
234 | British Aircraft Corporation - Concorde - Characteristics of
Electrical Power Supplies for Production |
1968 |
234 | British Aircraft Corporation - Concorde - Climb Data |
1965 |
231-232 | British Aircraft Corporation - Concorde - Customer Conference -
Toulouse |
1966 |
231 | British Aircraft Corporation - Concorde - Customer Requirements
Specification |
1967 |
233 | British Aircraft Corporation - Concorde - Customer's Symposium -
BAC/SUD Meeting with Electric Specialist Group |
1967 |
234 | British Aircraft Corporation - Concorde - Customer's
Symposium |
1967 |
232 | British Aircraft Corporation - Concorde - Economic Analysis -
IATA Presentation |
1964 |
234 | British Aircraft Corporation - Concorde - Effect of Cabin
Pressurization Failure on Fuel Reserves for the North
Atlantic |
1965 |
233 | British Aircraft Corporation - Concorde - Effect of Single Class
Operation on Airline Profitability - International |
undated |
233 | British Aircraft Corporation - Concorde - Effect of Single Class
Operation on Airline Profitability - US Domestic |
undated |
234 | British Aircraft Corporation - Concorde - Effects of Engine
Failure on the North Atlantic |
1965 |
233 | British Aircraft Corporation - Concorde - Effects on Runway
Strength of a Widened Bogie Track |
1970 |
234 | British Aircraft Corporation - Concorde - Electric Cable
Identification |
1968 |
234 | British Aircraft Corporation - Concorde - Electrical Cable
Installation Practice |
1968 |
234 | British Aircraft Corporation - Concorde - Electrical Cable
Protection Practice |
1969 |
232 | British Aircraft Corporation - Concorde - Equipment Access
Through Main Cabin Floor |
undated |
234 | British Aircraft Corporation - Concorde - Estimated
Weights |
1969 |
233 | British Aircraft Corporation - Concorde - Estimated
Weights |
1971 |
234 | British Aircraft Corporation - Concorde - Estimated
WTS |
1969 |
231 | British Aircraft Corporation - Concorde - Evacuation
Exercises |
1967 |
234 | British Aircraft Corporation - Concorde - Examined for IATA
Technical Committee |
1964 |
233 | British Aircraft Corporation - Concorde - Flight Test
Program |
1968 |
233 | British Aircraft Corporation - Concorde - Flight Tests Progress
to Date |
1969 |
232 | British Aircraft Corporation - Concorde - Fuel
System |
undated |
232 | British Aircraft Corporation - Concorde - Furnishing |
1968 |
233 | British Aircraft Corporation - Concorde - Ground Air
Conditioning |
1969 |
234 | British Aircraft Corporation - Concorde - Heat Exchanger
Qualification Test Procedure |
1968 |
234 | British Aircraft Corporation - Concorde - Installation
Requirements for BFE Seats |
1971 |
232 | British Aircraft Corporation - Concorde - Interior and Furnishing
Group |
undated |
234 | British Aircraft Corporation - Concorde - Interior
Color |
1971 |
234 | British Aircraft Corporation - Concorde - Interior
Design |
1967 |
234 | British Aircraft Corporation - Concorde - Maintenance Costs
Estimate |
1965-1966 |
233 | British Aircraft Corporation - Concorde - Maintenance
Costs |
1971 |
233 | British Aircraft Corporation - Concorde - Major Structural
Tests |
1968 |
233 | British Aircraft Corporation - Concorde - Operations Group
Notes |
1971 |
234 | British Aircraft Corporation - Concorde - Pacific Network
Appraisal |
1968 |
233 | British Aircraft Corporation - Concorde - PEN Team Meeting
Working Documents |
1971 |
234 | British Aircraft Corporation - Concorde - Performance and
Operations |
1965 |
234 | British Aircraft Corporation - Concorde - Performance Initial
Introduction |
1964 |
234 | British Aircraft Corporation - Concorde -
Performance |
1964 |
234 | British Aircraft Corporation - Concorde - Power Plant Glossary of
Terms |
1967 |
232 | British Aircraft Corporation - Concorde - Power Plant Maintenance
Equipment Replacement Features and Component Location |
1966 |
233 | British Aircraft Corporation - Concorde - Presentation to Ad-Hoc
ASC Meeting |
1970 |
232 | British Aircraft Corporation - Concorde - Production Aircraft
Starting, Emergency, and Auxiliary Power Systems |
1967 |
231 | British Aircraft Corporation - Concorde - Production
Progress |
undated |
234 | British Aircraft Corporation - Concorde - Production
Progress |
1966 |
231 | British Aircraft Corporation - Concorde - Progress
Reports |
1970-1971 |
232 | British Aircraft Corporation - Concorde - Project Interiors -
Note on Galley Construction and Equipment |
1968 |
233-234 | British Aircraft Corporation - Concorde - Protection Against
Corrosion |
1969 |
231 | British Aircraft Corporation - Concorde - Report on Loading and
Unloading Trials of Underfloor Baggage Compartment |
undated |
232 | British Aircraft Corporation - Concorde - Safety
Equipment |
1968 |
234 | British Aircraft Corporation - Concorde - Specification -
Production Standard Version |
1969 |
233 | British Aircraft Corporation - Concorde - Specifications Reviewed
by American Airlines |
1966 |
231-232 | British Aircraft Corporation - Concorde - Structural
Testing |
1969 |
234 | British Aircraft Corporation - Concorde - Takeoff Climb and Noise
Abatement Techniques |
1966 |
231 | British Aircraft Corporation - Concorde - Takeoff Data and
Subsonic Cruise Specific Range |
1964 |
234 | British Aircraft Corporation - Concorde - Takeoff Performance to
S.R. 422B Requirements |
1965 |
234 | British Aircraft Corporation - Concorde - Technical Note Basic
Structural Material |
1964 |
234 | British Aircraft Corporation - Concorde - Technical Note
Navigation System |
1964 |
234 | British Aircraft Corporation - Concorde - Technical Note
Radiation and Contamination |
1964 |
232 | British Aircraft Corporation - Concorde - Testing |
1968 |
234 | British Aircraft Corporation - Concorde - Testing |
undated |
234 | British Aircraft Corporation - Concorde - Updating for
Flight |
1966 |
234 | British Aircraft Corporation - Concorde - Wind
Tunnels |
1966 |
234 | British Aircraft Corporation - Concorde Over the
Pacific |
1968 |
232 | British Aircraft Corporation - Concorde Supersonic Transport -
Detail Technical Specification for PAA |
1967 |
233 | British Aircraft Corporation - Concorde Supersonic Transport -
Flying Qualities |
1971 |
231 | British Aircraft Corporation - Concorde |
1965, 1968 |
232 | British Aircraft Corporation - Customers Symposium Preliminary
Notes on Ground Handling |
1967 |
232 | British Aircraft Corporation - Data Required from Airlines for
Maintainability and Reliability Surveillance |
undated |
234 | British Aircraft Corporation - Discussion on Subjects of Ambient
Temperature Effects on Performance Sonic Boom and Engine-Out
Procedures |
1965 |
234 | British Aircraft Corporation - Effect of Initial Subsonic Cruise
on Concorde Economics |
1965 |
234 | British Aircraft Corporation - Effect on Fuel Reserves of a
Single Engine Failure at Critical Point on LON/NY Route |
1965 |
234 | British Aircraft Corporation - Effects of Engine Failure on North
Atlantic |
1965 |
231 | British Aircraft Corporation - Engineering Computing Services
Operational Research Group |
1968 |
232 | British Aircraft Corporation - Equipment Technical
Specification |
1968 |
232 | British Aircraft Corporation - Estimate of Direct Maintenance
Costs for Prototype Concorde |
1969 |
234 | British Aircraft Corporation - Estimation of Production Aircraft
Performance |
1969 |
232 | British Aircraft Corporation - Evaluation of Low Temperature Plug
and Socket Connectors |
1968 |
234 | British Aircraft Corporation - Flight Deck Warning
System |
1970 |
232 | British Aircraft Corporation - Flying the Concorde |
undated |
234 | British Aircraft Corporation - General Description |
1964 |
234 | British Aircraft Corporation - Ground Air
Conditioning |
undated |
234 | British Aircraft Corporation - High Speed
Aerodynamics |
undated |
234 | British Aircraft Corporation - Notes on Fuel System Loading,
Usage, and Management |
1965 |
233 | British Aircraft Corporation - Operations Group
Notes |
1971 |
233 | British Aircraft Corporation - PEN Meeting in Miami |
1971 |
233 | British Aircraft Corporation - PEN Team Meeting |
1971 |
233 | British Aircraft Corporation - Profiting From Speed - New
Approach to the Integration of Supersonic Transport into Existing Fare
Structure |
undated |
231 | British Aircraft Corporation - Report on Arlington
Symposium |
1967 |
231 | British Aircraft Corporation - Rolls-Royce Olympus 593 - ASC
Sub-Committees Propulsion, Fuel, Fire Detection, Accessory
Drive |
1969 |
234 | British Aircraft Corporation - Short Commentary on Community
Noise Paper |
1965 |
234 | British Aircraft Corporation - Size of the Supersonic Transport
Market |
1965 |
234 | British Aircraft Corporation - Some Evidence and Statistics on
Present Community Noise Situation |
1965 |
232 | British Aircraft Corporation - Structural Testing |
1969 |
231 | British Aircraft Corporation - Super VC-10 Double-Deck
Performance Data |
1965 |
231 | British Aircraft Corporation - Super VC-10
Double-Deck |
1965 |
232 | British Aircraft Corporation - Supersonic Transport Climb and
Cruise Performance with Developed Engines in ISA+15c
Conditions |
1964-1965 |
232 | British Aircraft Corporation - Supersonic Transport Effect on
Takeoff Weight of Varying Holding Speeds |
1964-1965 |
232 | British Aircraft Corporation - Supersonic Transport Takeoff
Performance |
1964 |
234 | British Aircraft Corporation - System Requirement Document for
Indicators |
1966 |
234 | British Aircraft Corporation - VC-10 Brochure |
1962-1965 |
231 | British Aircraft Corporation - VC-10 Descriptive Engineering
Notes |
1964-1965 |
231 | British Aircraft Corporation - VC-10 Jet Airliner - Economics of
Passenger Appeal |
1965 |
233 | British Aircraft Corporation - Working Papers for Meetings of
Propulsion and Accessory Drive Teams |
1971 |
231 | British Aircraft Corporation - Working Papers for Meetings of
Propulsion, Fuel, Detection Team |
1971 |
225 | British Ministry of Aviation - Accidents Investigation
Branch |
1965 |
225 | British Oxygen Aviation - Liquid Nitrogen Explosion Suppression
System |
1960 |
225 | Brownline Corporation - Boeing 707 and 727 Static Test of Net
Assembly, Pallet Assembly, and Aircraft Configurations |
1966-1967 |
225 | Brownline Corporation - Boeing 727 Static Test of Uni-Pak
Container Assembly |
1966 |
225 | Brownline Corporation - Test Report of 23215-51 Net Assembly and
23219-51 Fiberglass Container |
1966 |
225 | Burndy Corporation - Boeing 747 Life Test Connector Installed on
Instrument Systems Multiplexing Box |
undated |
225 | Burndy Corporation - Qualification Cable Assemblies Passenger
Entertainment and Service |
1968 |
225 | Burns Aero Seat Company - Air Foam - Goodyear High Resolution
Cycle Compression |
1971 |
225 | Burns Aero Seat Company - Airest |
1967-1968 |
225 | Burns Aero Seat Company - Boeing 747 Lounge Proposal for
TWA |
1968 |
226 | Burns Aero Seat Company - Boeing 747 Lounge Table Delethalization
Report |
1969 |
225 | Burns Aero Seat Company - Boeing 747 Passenger Seats Overhaul
Manual with Illustrated Parts List |
1969-1970 |
226 | Burns Aero Seat Company - Boeing 747 Passenger Seats |
1967 |
225 | Burns Aero Seat Company - Boeing 747 Seat
Specifications |
1969-1970 |
226 | Burns Aero Seat Company - Boeing 747 Seating Heat Conduction
Analysis |
1969 |
226 | Burns Aero Seat Company - Boeing 747 Seating Materials
Flammability Report |
1970 |
226 | Burns Aero Seat Company - Boeing 747 Test Reports for 6-Abreast
Tourist Seating |
1970 |
226 | Burns Aero Seat Company - Facing Lounge Load
Analysis |
1969 |
225 | Burns Aero Seat Company - L-1011 First Class and Tourist Seating
TWA Proposal |
1970 |
225 | Burns Aero Seat Company - L-1011 Lounge |
1970 |
226 | Burns Aero Seat Company - Model D794 and 803 Seats Static Test
Report |
1971 |
225 | Burns Aero Seat Company - Overhaul Manual with Illustrated Parts
List Recline Lock |
1969 |
226 | Burns Aero Seat Company - Seat Specification Airest
Seat |
1964 |
226 | Burns Aero Seat Company - Static Test Report for Facing
Lounges |
1969 |
225 | Burns Aero Seat Company - Static Test Report for Model 5507
Lounge Table |
1969 |
226 | Burns Aero Seat Company - Static Test Report for
Seats |
1969 |
225 | Burns Aero Seat Company - Tightening of Seat Bottom Diaphragms on
All Airest Seats |
1968-1969 |
226 | Burns Aero Seat Company - TWA Baggage Restraint Bar
Test |
1968-1969 |
226 | Burns and Roe - Supersonic Transport/Subsonic Test Cells for
Joint Airlines Committee |
1967-1968 |
226 | Burtek Incorporated - L-1011 Cockpit Procedures Trainer Alternate
Proposal |
1970 |
237 | CAE Industries Limited - Electronics Division - CAE/CBS Visual
System for TWA - Technical Description |
1970 |
237 | CAE Industries Limited - L-1011 Cockpit Procedures Trainer for
TWA |
1970 |
237 | CAE Industries Limited - L-1011 Digital Flight Simulator for TWA
Price Proposal |
1969 |
237 | CAE Industries Limited - Suitability of SIGMA 2 |
1969 |
237 | CAE Industries Limited - Tactical Fighter/Helicopter Six Degrees
of Freedom Motion System |
1969 |
237 | Charles Butler Associates - BAC-SUD Concorde Supersonic Transport
- Proposed Interior Perspective Color Renderings |
1965 |
237 | Charles Butler Associates - BAC-SUD Concorde Supersonic Transport
Photographs Interior |
1965 |
237 | Chevron Chemical Company - Oronite High Temperature Hydraulic
Fuel M2-V Storage and Handling Manual |
1966 |
237 | Chevron Chemical Company - Oronite Hyjet III - Comparison of
Properties with Skydrol 500B |
1969 |
237 | Chevron Chemical Company - Oronite Hyjet III - New Fire-Resistant
Phosphate Ester Hydraulic Fluid |
1969 |
237 | City of Philadelphia - NE Corridor VTOL Investigation Docket
19078 |
1968 |
237 | Civil Aeronautics Administration - Air Carrier
Accidents |
1955-1962 |
237 | Civil Aeronautics Administration - Comparative Safety Statistics
in US Airline Operations |
1953 |
237 | Civil Aeronautics Administration - Comparison of Accidents in US
Scheduled Air Carrier Passenger Operations |
1953-1954 |
237 | Civil Aeronautics Administration - Determination of Some
Geometric Relationships Pertaining to Collision Paths |
1955 |
237 | Civil Aeronautics Administration - Mid-Air Collisions in US Civil
Flying |
1948-1953 |
237 | Civil Aeronautics Administration - NE Corridor Vitol
Investigation Preliminary Information Responses |
1968 |
237 | Civil Aeronautics Administration - Phenomenon of Aircraft
Aquaplaning |
1963 |
237 | Civil Aeronautics Administration - US Air Carrier and General
Aviation Accidents |
1958-1960 |
1 | Collection information (from TWA library) |
circa 1946-1961 |
237 | Collins Radio Company - 51RV-1 Typical Performance
Curves |
1962 |
237 | Collins Radio Company - 51V-3 Instruction Book |
1958 |
237 | Collins Radio Company - ADF Receiver Unit Instructions
51Y-3 |
1958 |
235 | Collins Radio Company - Aeronautical Satellite
Communication |
1967 |
235 | Collins Radio Company - Airborne Transceivers Overhaul Manual
618T |
1968 |
235 | Collins Radio Company - ALA-51A Flight Test Program |
1965 |
236 | Collins Radio Company - ATC Transponder Overhaul Manual
621A-6 |
1969 |
235 | Collins Radio Company - Central Instrument Warning System
Computer for B747 Jet (54W-3) |
1966 |
235 | Collins Radio Company - DF-206 ADF System Maintenance
Manual |
1969 |
235 | Collins Radio Company - Distance Measuring Equipment Maintenance
Manual 860E-2 |
1965 |
235 | Collins Radio Company - DME Overhaul Manual 860E-3 |
1969-1971 |
235 | Collins Radio Company - DME System Maintenance Manual
860E-3 |
1970-1971 |
237 | Collins Radio Company - Effect of Reflections on Airborne DME
Units |
1963 |
235 | Collins Radio Company - Engineering Proposal Community Navigation
and Flight Director Equipment for Supersonic Transport |
1963 |
236 | Collins Radio Company - Failure Effect Analysis for 51RV-28
VOR/ILS Receiver |
1968 |
235 | Collins Radio Company - Flight Director Control Overhaul Manual
614E |
1965 |
235 | Collins Radio Company - Flight Director Overhaul Manual
329B-7 |
1968 |
235 | Collins Radio Company - Instrument Amplifier Overhaul Manual
344C-1D |
1966 |
237 | Collins Radio Company - Marker Beacon Receiver Illustrated Parts
Catalog 51Z-3 |
1961 |
236 | Collins Radio Company - Marker Beacon Receiver Instruction Book
51Z-4 |
1967 |
237 | Collins Radio Company - Marker Beacon Receiver Maintenance Manual
51Z-3 |
1961 |
235 | Collins Radio Company - Passenger Address Amplifier Overhaul
Manual 346D |
1969 |
235 | Collins Radio Company - Product Description 618M
Transceiver |
1966 |
235 | Collins Radio Company - Signal Characteristics of a VHF
Satellite-to-Aircraft Communication Link |
1967 |
235 | Collins Radio Company - Solid State DME Product Description
860E-2 |
1963, 1966 |
235 | Collins Radio Company - Technical Standard Order Compliance Tests
for 51RV-2B VOR/ILS Navigation Receiver |
1967 |
236 | Collins Radio Company - Technical Standard Order Compliance Tests
for 618M-2B VHF Communications Transceivers |
1967 |
236 | Collins Radio Company - TSO Compliance Test for 621A-6 ATC
Transponder 599W-1 Adapter |
1969 |
237 | Collins Radio Company - Typical Performance Data 618M-1
Transceiver |
undated |
235 | Collins Radio Company - VHF Communications Transceiver
Maintenance Manual 618B |
1967 |
235 | Collins Radio Company - VHF Communications Transceiver
Maintenance Manual 618M-2B |
1967 |
58 | Connie Operating Manual |
1962-1966 |
32 | Constellation Model 049 Parts Catalog |
1950-1961 |
48 | Constellation Model 749 Parts |
1950-1966 |
184 | Constellation newsletter |
1960-1962 |
193 | Convair - Control Cable Service Parts |
1961-1962 |
197 | Convair - Drafting Room Manual |
1954 |
193 | Convair - Extruded Shapes Standards |
1957-1961 |
197 | Convair - Extruded Shapes Standards |
1954-1960 |
201 | Convair - Extruded Shapes Standards |
1957-1960 |
198 | Convair - Functional Test Instruction Manual |
1961-1962 |
199 | Convair - Manufacturing Process Specification
Manuals |
1957-1975 |
236 | Convair - Model 22 Aerodynamic Data for Link Aviation
Simulator |
1958-1962 |
190 | Convair - Operational Checkout Instructions, number
95-175. |
circa 1958-1962 |
198 | Convair - Operational Checkout Instructions, numbers
176-189 |
1960-1963 |
193 | Convair - Q-K-Y Manual |
circa 1956-1958 |
195 | Convair - Specification Control Drawings |
1958-1960 |
199-200 | Convair - Specification Control Drawings |
circa 1958-1964 |
190 | Convair - Traveler Index and Convair Travelers
Magazines |
1961-1969 |
192 | Convair 880 - Detail Model Specifications for Design of Convair
880 Turbojet Airliner for TWA |
1956-1961 |
179 | Convair 880 - Electrical Wiring Changes Made by
Northeast |
undated |
190 | Convair 880 - Engineering Repairs |
1962-1965 |
194 | Convair 880 - FAA Approved Airplane Flight Manual |
1960-1964 |
197 | Convair 880 - Flight Handbook |
1966-1974 |
196 | Convair 880 - Model 22M - Overhaul Manual, volume I, chapters
13-27 |
1961 |
194 | Convair 880 - MSG, chapters 28-30 |
circa 1971 |
190 | Convair 880 - MSG, chapters 32-38, 58 |
circa 1971 |
192 | Convair 880 - Operation Manual |
1959-1960 |
192 | Convair 880 - Overhaul Manual, chapters 1-27 |
1961-1965 |
189 | Convair 880 - Overhaul Manual, chapters 28-76 |
circa 1962-1967 |
197 | Convair 880 - Planning and Performance Manual |
1967-1973 |
201 | Convair 880 - Service Change Record and Service Change Cross
Reference |
1961 |
179 | Convair 880 - Weight and Balance Manual |
1961-1963 |
191 | Convair 880 - Wiring Diagram Manual, chapters 1-33 |
circa 1960 |
195 | Convair 880 - Wiring Diagram Manual, chapters 21-32 |
1960-1963 |
195 | Convair 880 - Wiring Diagram Manual, chapters 33-91 |
1961-1962 |
191 | Convair 880 - Wiring Diagram Manual, chapters 34-91 |
circa 1963 |
192 | Convair 880 - Wiring Diagram Manual, chapters 34-91 |
circa 1960-1964 |
196 | Convair Model 22M - Overhaul Manual, volume II, chapters
28-76 |
1961-1965 |
196 | Convair Model 30 - Overhaul Manual, chapters 13-27 |
1961-1970 |
195 | Convair Model 30 - Overhaul Manual, chapters 28-76 |
1962-1964 |
236 | Coordinating Research Council Incorporated - CRC Aircraft Engine
Exhaust Tests |
1969 |
236 | Coordinating Research Council Incorporated - Evaluation 5ML Bomb
Procedure Measuring Hi Temperature Oxidation Stability Bas Turbine
Fuels |
1969 |
236 | Coordinating Research Council Incorporated - Evaluation and
Precision of the Gas Drive Modified Standard Fuel Coker |
1970 |
236 | Crescent Dallas - Pictorial of Facilities |
undated |
236 | Crescent Dallas - Technical Proposal Boeing 747 Lower Lobe Galley
Food Service Carts |
1969 |
177 | Cruise Charts - 049 |
circa 1953-1960 |
178 | Cruise Charts - 1049 |
undated |
178 | Cruise Charts - 1649 |
circa 1957 |
177 | Cruise Charts - 749 |
circa 1951-1957 |
236 | Cryo-Jet Start Company - Ground Support Starting |
undated |
236 | Curtiss-Wright Corporation - High-Speed VTOL |
1964 |
238 | Dalto Electronics Corporation - DEC 4000 Wide Angle Visual
Simulation System |
1968 |
238 | Dalto Electronics Corporation - General Specifications for
Commercial Visual Simulation System |
1970 |
238 | Dalto Electronics Corporation - Mark III for Low Visibility
Simulator Flight Simulator/Instrument Trainer |
1961, 1964 |
238 | Dalto Electronics Corporation - Model Mark II Handbook
Description, Specification, Operation, and Maintenance |
1960 |
238 | Dalto Electronics Corporation - Revised Power Requirements
Pertaining to Visual System for TWA |
1968 |
238 | Dalto Electronics Corporation - Revision of Power Requirements
and Schedule |
1968 |
238 | Dalto Electronics Corporation - Technical Proposal for
Manufacturing Modification and Installation of Motion
System |
1970 |
238 | Dalto Electronics Corporation - Technical Specifications for Wide
Angle Direct View Visual Simulation System |
1970 |
238 | Dalto Electronics Corporation - TWA Proposal for Visual Simulator
Attachment Type V200 |
1963 |
238 | Dalto Electronics Corporation - V200 Scanalog
Specification |
1962 |
238 | Dalto Electronics Corporation |
1960 |
238 | Davis Aircraft Products Company - New Buckle
Assemblies |
undated |
238 | Dayton Aircraft Products - Protection Against Lightning
Strikes |
1958-1959 |
238 | DeHavilland Aircraft of Canada - 1st Response Requests
Information CAB NE Corridor Investigation |
1968 |
238 | DeHavilland Aircraft of Canada - 2nd Generation Jet-STOL
Transport |
1968 |
238 | DeHavilland Aircraft of Canada - Buffalo |
1965-1966 |
238 | DeHavilland Aircraft of Canada - Caribou Brochure |
1965 |
238 | DeHavilland Aircraft of Canada - DHC-4 Caribou 28,500 Lb Gross
Weight STOL Direct Operating Costs |
1966 |
238 | DeHavilland Aircraft of Canada - DHC-4 Caribou 28,500 Lb Gross
Weight STOL Performance Summary |
1961 |
238 | DeHavilland Aircraft of Canada - DHC-6 Twin Otter - Study in
Airline Service |
1966 |
238 | DeHavilland Aircraft of Canada - DHC-6 Twin Otter - Technical
Description |
1966-1967 |
238 | DeHavilland Aircraft of Canada - DHC-7 Design
Specifications |
1969 |
238 | DeHavilland Aircraft of Canada - DHC-7 Quiet STOL Airliner -
Operational Analysis for SFO Helicopter Airlines |
1969 |
238 | DeHavilland Aircraft of Canada - DHC-7 Quiet STOL Airliner -
Operational Analysis for TWA |
1969 |
238 | DeHavilland Aircraft of Canada - DHC-7 Quiet STOL Airliner -
Performance |
1969 |
238 | DeHavilland Aircraft of Canada - DHC-7 Quiet STOL
Airliner |
1968-1969 |
238 | DeHavilland Aircraft of Canada - Product Support |
1969 |
238 | DeHavilland Aircraft of Canada - Twin Otter - Commuter
Interiors |
1969 |
238 | DeHavilland Aircraft of Canada - Twin Otter Series
300 |
1968 |
238 | DeHavilland Aircraft of Canada - Twin Otter |
1966 |
238 | Delta Airlines - Preliminary Information Exchange NE Corridor
VTOL Docket 19078 |
undated |
238 | Digitran Company- Entertainment and Volume Control Switch
Technical Proposal |
circa 1965-1967 |
238 | Digitran Company- Passenger Entertainment Seat Control Units for
PAA Technical Proposal |
1968 |
238 | Diversified Avionics Incorporated - New Guidance System for
Approach and Landing |
1969 |
238 | Dorne and Margolin - DMC25 VHF Blade Antenna Technical
Data |
1967 |
238 | Dornier - Digest on VSTOL Transport Aircraft |
circa 1967 |
238 | Dornier - VSTOL Development |
circa 1970 |
240 | Douglas Aircraft Company - AAL Request for Change |
1968 |
238 | Douglas Aircraft Company - DC-10 Advanced Composite Rudder
Quarterly Technical Progress Reports |
1977-1978 |
239 | Douglas Aircraft Company - DC-10 Advanced Composite Vertical
Stabilizer Quarterly Technical Progress Reports |
1978 |
240 | Douglas Aircraft Company - DC-10 Coordination Drawing and
Specification Passenger Seats |
1970 |
240 | Douglas Aircraft Company - DC-10 Data for TWA |
1968 |
239 | Douglas Aircraft Company - DC-10 Domestic Stretch Program
Status |
1978 |
240 | Douglas Aircraft Company - DC-10 Engine Selection
Evaluation |
1968 |
240 | Douglas Aircraft Company - DC-10 Estimated Flying
Qualities |
1968 |
240 | Douglas Aircraft Company - DC-10 for TWA Supplement to
C1-807-2080 |
1970 |
239 | Douglas Aircraft Company - DC-10 International Stretch Program
Status |
1978 |
240 | Douglas Aircraft Company - DC-10 Review of Dichlorvos
Disinsection System |
1970 |
240 | Douglas Aircraft Company - DC-10 Specification Standardization
Meeting - Airline Personnel |
1967 |
240 | Douglas Aircraft Company - DC-10 Specification Standardization
Meeting - RFC Study Results |
1967-1968 |
240 | Douglas Aircraft Company - DC-10 Specification Standardization
Meeting |
1967 |
240 | Douglas Aircraft Company - DC-10 Strength Analysis Progress
Report La Guardia Runway Pier Extensions |
1968 |
240 | Douglas Aircraft Company - DC-10 Technical Summary |
1970 |
240 | Douglas Aircraft Company - DC-10D Galley
Demonstration |
1968 |
239 | Douglas Aircraft Company - DC-10D Performance Report 3 GE
CF6/36-2 Engines Data Available |
1968 |
240 | Douglas Aircraft Company - DC-10D Rolls-Royce RB211-17
Performance |
1968 |
239 | Douglas Aircraft Company - DC-8 Airplane Characteristics -
Airport Planning |
1969 |
239 | Douglas Aircraft Company - DC-8 Model 63 General Performance
Report Pratt and Whitney JT3D-7 Engines |
1969 |
239 | Douglas Aircraft Company - DC-8 Models 62F/63F Cargo
Aircraft |
1969 |
239 | Douglas Aircraft Company - DC-8-63 Loading Manual |
1968-1969 |
239 | Douglas Aircraft Company - DC-8-63F Detail Specification for 4
Engine |
1969 |
239 | Douglas Aircraft Company - DC-8-63F Detail Specifications for 4
Engine Convertible |
1969 |
239 | Douglas Aircraft Company - DC-9 Airplane Characteristics -
Airport Planning |
1968 |
239 | Douglas Aircraft Company - DC-9 Series 30 and DC-9 Series 40 for
TWA |
1969 |
239 | Douglas Aircraft Company - DC-9 Series 30 General Performance
Report Pratt and Whitney JT8D-7 Engines |
1967-1968 |
239 | Douglas Aircraft Company - DC-9 Series 40 General Performance
Report Advanced Pratt and Whitney JT8D-0 Engines |
1966 |
239 | Douglas Aircraft Company - DC-9 Series 40 General Performance
Report Pratt and Whitney JT8D-11 Engines |
1968 |
238 | Douglas Aircraft Company - DC-9 Super 80 Replacement |
1978 |
239 | Douglas Aircraft Company - DC-9 Takeoff From Wet and Slushy
Runways |
1968 |
239 | Douglas Aircraft Company - DC-9-10 Aircraft Interior Noise Levels
During Cruise |
1967 |
240 | Douglas Aircraft Company - EAL Optional Specification Change
Notices |
1968 |
239 | Douglas Aircraft Company - Series 30 General Performance Report
Pratt and Whitney JT8D-9 Engines |
1967-1968 |
240 | Douglas Aircraft Company - Summary Report Commodity
Characteristics and Module Utilization Survey for TWA |
1968 |
240 | Douglas Aircraft Company - Survey Procedure and Cargo I
Operations Report by AA Finn |
1969 |
240 | Dunlop Company - Dunlop on the Concorde |
1971 |
240 | Dynasciences - Proximity Switch - Performance and Configuration
Options |
1970 |
240 | Eastern Airlines - NE Corridor VTOL Investigation |
1968 |
240 | Eastern Airlines - Reconfiguration of Life Raft Survival
Kits |
1970 |
240 | EKCO Electronics Limited - Weather Radar Type E390/564
Airborne |
1967-1968 |
240 | Electro Development Corporation - L-1011
Transformer-Rectifier |
1962-1968 |
240 | Electro Development Corporation - L-1011 Weight and Balance
System Economic Benefits |
undated |
240 | Electro Development Corporation - Operator's Guide Weight and
Balance System |
1969 |
240 | Electronic Engineering Company - Boeing 747 Proposal Custom IFE
Passenger Control Box Designs for TWA |
1968 |
240 | Electronic Engineering Company - Test Report PCU Electromagnetic
Interference |
1970 |
240 | Electronic Engineering Company - Test Report PCU Environmental
Tests |
1970 |
240 | Electronic Engineering Company - Type 769 Airborne VHF Dual
Communication/Navigation Frequency Selector |
1964-1965 |
240 | Electronic Engineering Company of California - Passenger
Entertainment Service Controls for TWA |
1970 |
240 | Environ Laboratories Incorporated - Environmental Tests for
Litton Industries |
1969 |
241 | Esso - Conductivity Additive In Aviation Turbine
Fuel |
1961 |
240 | Esso - Fuel for Jet Transports |
1953 |
240 | Esso - Jet Fuel: What Kind? How Much Will It Cost? |
1950 |
240 | Esso - Jet Fuels: Airline Viewpoint |
1951 |
241 | Esso - New Theory For Static Relaxation From High Resistivity
Fuel |
1964 |
241 | Esso - Static Electricity Studies in an Aircraft Fuel
Tank |
1960 |
241 | Esso - Static Electricity Within Aviation Turbo-Fuel Handling
Systems |
1950, 1960 |
241 | Esso - Turbo Oil 2nd Generation Lubricant for Aircraft Gas
Turbine Engines |
1962 |
241 | Esso - Volatility Aspects of Jet Fuels |
1952 |
241 | Esso - Water Injection for Commercial Aircraft |
1947 |
241 | Esso - Weight Determinations Aircraft Fuel Load |
1951 |
243-244 | FAA - 2nd International Aviation R and D Symposium - All Weather
Systems |
1963 |
243 | FAA - Aids Program Presented at ATA E and M Meeting |
1965 |
244 | FAA - Airport Design Supplement |
1962 |
243 | FAA - Airport Paving |
1964-1967 |
243 | FAA - Airworthiness Standards: Evaluation Committee Report to the
Administrator |
1966-1967 |
242 | FAA - Airworthiness Standards: Normal Category
Rotorcraft |
1966 |
242 | FAA - Airworthiness Standards: Normal Utility and Acrobatic
Category Airplanes |
1966 |
242 | FAA - Airworthiness Standards: Transport Category
Airplanes |
1966 |
242 | FAA - Airworthiness Standards: Transport Category
Rotorcraft |
1966 |
243 | FAA - Analysis of Safety Aspects of Aircraft Landing
Operations |
1963 |
242 | FAA - Analysis of Sitting Areas and Pressures of Man |
1962 |
242 | FAA - Biochemical Effects of Lindame and Dieldrin on
Vertebrates |
1962 |
244 | FAA - Briefing for US Airlines Participating in Evaluation of
PHASE III Proposals for Supersonic Transport Development
Program |
1966 |
242 | FAA - Certification Procedures for Products and
Parts |
undated |
244 | FAA - Citizen's Guide to Aircraft Noise |
1963 |
242 | FAA - Clear Air Turbulence Radiometric Detection
Program |
1971 |
243 | FAA - Collision Avoidance Bibliography |
1968 |
244 | FAA - Control Display Pilot Factors Problems |
1963 |
244 | FAA - Control-Display Pilot Factors Program |
1963 |
244 | FAA - Crashworthiness and Passenger Evacuation Proposed Rule
Making |
1966 |
243 | FAA - Criteria for Approving Category I and II Landing Minima for
FAR 121 Operators |
1970-1971 |
242 | FAA - Definitions and Abbreviations |
1962 |
242 | FAA - Determination of Centers of Gravity of Man |
1962 |
242 | FAA - Development and Test of Explosive Exit Concept for Civil
Transport Aircraft |
1971 |
243 | FAA - Development of Techniques for Evaluating Physiological
Protective Efficiency Civil Aviation Oxygen Equipment |
1967 |
243 | FAA - Diagnostic Tests of Color Defective Vision |
1967 |
243 | FAA - Dynamic Simulation Studies of Pictorial Navigation Displays
as Aids to ATC |
1961 |
242 | FAA - Effects of Chlorinated Hydrocarbons on Substrate-Linked
Phosphorylation |
1963 |
243 | FAA - Effects of Lateral Automatic Landing Performance Overflight
Interference |
1963 |
243 | FAA - Emergency Evacuation Tests of a Crashed L-1649 |
1966-1967 |
242 | FAA - Engine Oil System as Means of Early Failure
Detection |
1965 |
242 | FAA - Evacuation Pattern Analysis of Survivable Commercial
Crashes |
1962 |
243 | FAA - Evaluation of Biocidal Turbine Fuel Additive |
1967-1968 |
243 | FAA - Evaluation of Sierra, Hanging, Quick-Don, Crew,
Pressure-Breathing, Oxygen Mask |
1966-1967 |
243 | FAA - Evaluation of Various Padding Materials for Crash
Protection |
1966-1967 |
243 | FAA - FAA/NASA Joint Technology Conference on Slush Drag and
Braking Problems |
1961 |
242 | FAA - Failure Rearward Facing Seat-Backs and Resulting Injuries
In a Survivable Accident |
1962 |
242 | FAA - Feasibility Study of a Crash-Fire Prevention System for the
Supersonic Transport |
1963 |
243 | FAA - Flaming and Self-Extinguishing Characteristics of Aircraft
Cabin Interior Materials |
1968 |
242 | FAA - Flammability and Smoke Characteristics of Aircraft Interior
Materials |
1964 |
242 | FAA - Flammability of Lip, Face, and Hair Preparations in the
Presence of 100 Percent Oxygen |
1963-1964 |
244 | FAA - Floatation Characteristics of Aircraft Passenger Seat
Cushions |
1966 |
244 | FAA - Full-Scale Dynamic Crash Test of LAC 1649 |
1965 |
243 | FAA - Functional Comparison of Basic Restraint
System |
1967-1968 |
242 | FAA - Human Survivability of Extreme Impacts in
Free-Fall |
1963 |
242 | FAA - Human Tolerances |
1962 |
242 | FAA - Improved Method for Determining the Efficiency of Crew and
Passenger Oxygen Masks |
1962-1963 |
242 | FAA - In Vivo Measurement of Total Gas Pressure in Mammalian
Tissue |
1963 |
242 | FAA - Inflight Loss of Consciousness Case Report |
1963-1964 |
243 | FAA - Investigation of Turbine Fuel Flammability Within Aircraft
Fuel Tanks |
1967-1968 |
242 | FAA - Kinematic Behavior of Human Body During
Deceleration |
1962 |
243 | FAA - Limited Survey of Commercial Jet Aircraft Altimeter System
Position Error by Pacer With Trailing Cone |
1964-1965 |
242 | FAA - Manipulation of Arousal and Its Effects on Human Vestibular
Nystagmus |
1962 |
243 | FAA - National Airport Plan |
1963-1967 |
242 | FAA - National Aviation System Planning Review
Conference |
1970 |
242 | FAA - National Plan for Navigation |
1970 |
243 | FAA - Noise Abatement Procedures |
1960 |
243 | FAA - North Atlantic Region Air Traffic Survey |
1962 |
243 | FAA - Pilot Ability to Fly Holding Patterns Utilizing Various
Navigational Techniques |
1962 |
244 | FAA - Pilot Factors Program - Supersonic Transport |
1963 |
243 | FAA - Potential of Airborne Collision Prevention
Devices |
1962 |
244 | FAA - Preliminary Data - Oklahoma City Sonic Boom
Study |
1964 |
243 | FAA - Pressure Measurement for Pressure Altimetry |
1964 |
243 | FAA - Problems in Aerial Application |
1966-1967 |
242 | FAA - Problems In Air Traffic Management: Longitudinal Prediction
of Effectiveness of Air Traffic Controllers |
1961-1962 |
243 | FAA - Project Race Report |
1963 |
243 | FAA - Proposals for Development of Commercial Supersonic
Transport |
1963 |
243 | FAA - Protective Passenger Smoke Hood |
1967 |
244 | FAA - Report to NASA on Aircraft Operating Problems |
1968 |
243 | FAA - Reports to Supersonic Transport Steering Group |
1963 |
244 | FAA - Request for Proposal for Phase III of the Supersonic
Transport Development Program |
1966 |
242 | FAA - Resume and Index of Reports of Civil Aeromedical Research
Institute |
1961-1964 |
243 | FAA - Runway Slush Effects on Takeoff of Jets |
1962 |
242 | FAA - Simulator Investigation of Supersonic Transport
Investigations of Supersonic Transport Operating Margins |
1967 |
242 | FAA - Sonotropic Effects of Commercial Aircraft on
Birds |
1962 |
244 | FAA - STAFF Study Estimated Cost of Delay at FAA Tower
Airports |
1965 |
242 | FAA - Structural Design For Fuel Containment Under Survivable
Crash Conditions |
1964 |
242 | FAA - Studies of Air Loads on Man |
1963-1964 |
243 | FAA - Study of Altitude Reporting VIA ATC Radar Beacon
System |
1960 |
244 | FAA - Supersonic Transport Boeing 707-300 Evaluation
Briefing |
1969 |
244 | FAA - Supersonic Transport Economic Model Ground
Rules |
1966 |
244 | FAA - Supersonic Transport Phase II-A Evaluation
Plan |
1964 |
243 | FAA - Supersonic Transport |
1963 |
243 | FAA - Supersonic Transports - Standards for Airworthiness
Operations and Maintenance |
1961 |
244 | FAA - System Description National Airspace System En Route Stage
A |
1965 |
244 | FAA - Technical and Economic Evaluation of Aircraft for Intercity
Short-Haul Transportation |
1966 |
242 | FAA - Technical Program Document |
1967 |
244 | FAA - Tentative Airworthiness Standards for Supersonic
Transports |
1965 |
243 | FAA - Test of Trail Cone System to Calibrate Static Ports for
Barometric Altimeters |
1964 |
242 | FAA - Toxic Hazards in Aerial Application |
1962 |
243 | FAA - Vehicular Measurements of Effective Runway
Friction |
1962 |
241 | FAA |
1945-1964 |
241 | Fairchild - F-27A Operations Planning Manual |
undated |
241 | Fairchild - F-27E Airline Configurations and
Performance |
1960 |
241 | Fairchild - F-27II |
1964 |
241 | Fairchild Hiller - Beverage Cart |
1971 |
241 | Fairchild Hiller - Cryogenic Galley Cooling System New Generation
Airline Transport Jumbo Jets |
undated |
241 | Fairchild Hiller - Food Tray Carriers |
1971 |
241 | Fairchild Hiller - L-1011 Beverage Cocktail Cart |
1969 |
241 | Fairchild Hiller - L-1011 Coach Class Food Cart |
1969 |
243 | Fairchild Hiller - L-1011 Engineering Study CO2-Freon Cooling
System in Inflight Service Carts |
1969 |
241 | Fairchild Hiller - L-1011 First Class Food Cart |
1969 |
241 | Fairchild Hiller - L-1011 Food and Beverage Service
Carts |
1970 |
241 | Fairchild Hiller - Quantas In-Flight Service Carts |
1969 |
241 | Fairchild Hiller - Specification Heli-Porter
PC-6/B-H2 |
1965-1966 |
241 | Fairchild Hiller - Strates Model TP85 Air Turbine Motor For Use
on L-1011 |
1968 |
241 | Fairchild Hiller - Waste Management for Commercial Transport
Aircraft |
1968 |
241 | Fairchild Industrial Products - Passenger Music
Reproducer |
1971 |
241 | Fenwal - Brake Temperature Monitoring System for Boeing
747 |
1967 |
241 | Fenwal - Explosion Protection System for Boeing 707 Surge
Tank |
1965 |
241 | Fenwal - Studies of Induced Current Effects Due to Simulated
Lightning Currents Near Explosion Protection System Boeing 707 Surge and
Fuel Tanks |
1967 |
242 | Fischer and Porter |
undated |
242 | Flight Equipment and Engineering - Series 900 Luxair Passenger
Seating |
1959 |
242 | Flight Safety Foundation - Bibliography of AvCIR
Reports |
1963 |
242 | Flight Safety Foundation - Criteria for Radio Guidance and Flight
Errors as Affect Safety of CAT II Landing Operations |
1967 |
242 | Flight Safety Foundation - Critical Factors in Approach and
Landing Accidents |
1960-1961 |
242 | Flight Safety Foundation - Full Scale Transport Crash Test
Program |
1964 |
242 | Flight Safety Foundation - Impact Survival in Air Transport
Accidents |
1961 |
242 | Flight Safety Foundation - Jet Accidents Relating Fire
Suppression and Passenger Evacuation - Statistical Analysis |
1967 |
242 | Flight Safety Foundation - Powers, Functions, and
Responsibilities |
1967-1968 |
242 | Flight Safety Foundation - Synthesis of Impact Acceleration
Technology for Aviation Crash Injury Prevention |
1962-1963 |
242 | Fokker - F-28 Brochure |
1964 |
242 | Fokker - F-28 Fellowship |
1965 |
242 | Fokker - F-28 Performance Information |
1964 |
242 | Fokker - Function of Air Transport in Present-Day
Europe |
1965 |
242 | Fokker - Landing Performance - Comparison Between Calculations
Results Obtained with FAA |
1964 |
242 | Fruehauf Corporation - Interline Service Container
System |
1963 |
242 | Frye Corporation - F-1 Safari Brochure |
1956 |
245 | Garbell - Drift-Down With Partial Power in Air-Carrier
Operation |
1953 |
245 | Garbell - Ground Run of Aircraft in Landing and
Takeoff |
1954 |
245 | Garbell - Initial En Route Climb of Aircraft |
1952 |
245 | Garbell - Optimum Climbing Techniques for High Performance
Aircraft |
1953 |
245 | Garbell - Visual Range in Daylight, Darkness, and
Twilight |
1952 |
245 | Garrett Corporation - Advance Report Chemically Fueled Dynamic
Emergency Power Units for Jets |
1968 |
245 | Garrett Corporation - AiResearch Cool Gas Inflation
Systems |
1968 |
245 | Garrett Corporation - AiResearch Positive Displacement Air
Motors |
undated |
245 | Garrett Corporation - Boeing 727 Operating Cost Parameters -
Short Haul Fan Jet |
undated |
245 | Garrett Corporation - Boeing 747 APU |
undated |
245 | Garrett Corporation - Boeing 747 Combination
Slide/Raft |
1967-1968 |
245 | Garrett Corporation - Emergency Transceiver System |
1970 |
245 | Garrett Corporation - Fan Reverser and Hot Stream Spoiler Control
and Actuating System |
undated |
245 | Garrett Corporation - Field Service Notes |
1970 |
245 | Garrett Corporation - Gas Turbine Presentation |
1969 |
245 | Garrett Corporation - GTCP 660 Program Review |
1969-1970 |
245 | Garrett Corporation - Integrated Pneumatic System |
1967 |
245 | Garrett Corporation - L-1011 Auxiliary Power Units |
1968 |
245 | Garrett Corporation - L-1011 Emergency Escape Slides |
1969 |
245 | Garrett Corporation - L-1011 Environmental Control System
Proposal |
1968 |
245 | Garrett Corporation - L-1011 Gas Turbine Auxiliary Power
Unit |
1967 |
245 | Garrett Corporation - L-1011 Gas Turbine Auxiliary Power
Unit |
1968 |
245 | Garrett Corporation - L-1011 Product Assurance Plan |
1968 |
245 | Garrett Corporation - L-1011 Technical and Economical
Considerations Concerning TSCP 800-2 Auxiliary Power Unit |
1968 |
245 | Garrett Corporation - Model GTCP 660-4 Modification
Plan |
1970 |
245 | Garrett Corporation - Model TSCP 800-2 Auxiliary Power
Unit |
1968 |
245 | Garrett Corporation - RESCU 99 Emergency Radio
Beacon |
1967 |
245 | General Aircraft Corporation - GAC - Detailed Type Specification
- Short Range 4 Engine Turbo-Prop Transport |
1968 |
245 | General Aircraft Corporation - GAC-100 Commercial
Transport |
1968 |
245 | General Aircraft Corporation - GAC-100 |
1967 |
245 | General American Transportation Corporation - Airworthiness
Testing Program for LD3-747 Lower Lobe Containers |
1969 |
245 | General American Transportation Corporation - Stress Analysis for
LD3-747 Lower Lobe Containers |
1969 |
246 | General Dynamics Corporation - Study: Gas Turbine Starting
Subsystem for the F111A Airplane |
1965 |
246 | General Dynamics Corporation - Terrain Avoidance Flight
Test |
1962 |
246 | General Dynamics Corporation - Terrain Avoidance
Radar |
undated |
249 | General Electric - 4th Airline Propulsion Symposium |
1970 |
248 | General Electric - 6th Annual International Aviation Maintenance
Symposium |
1970-1971 |
247 | General Electric - Agreement with CF6-36-2 Engines |
undated |
247 | General Electric - Aircraft Schedule Simulation and Maintenance
Cost Model |
1965 |
247-248 | General Electric - Airline Planning Guide: Test Facilities for
Large Advanced Turbojet Turbo-Fan Engines |
1967 |
248 | General Electric - Airline Propulsion Symposium |
1969 |
250 | General Electric - Airline Service Experience Briefing
Report |
1961 |
247 | General Electric - Airlines Symposium - DC-10
Presentations |
1968 |
249 | General Electric - Airlines Symposium - Supersonic Transport
Presentation |
1968 |
248 | General Electric - Analysis of Precipitation Static
Phenomena |
1943 |
247 | General Electric - Brochures |
undated |
247 | General Electric - CF6 Brochure |
1967 |
249 | General Electric - CF6 Brochure |
1970-1971 |
247 | General Electric - CF6 Commercial Turbofan Estimated Noise
Characteristics and Flight Noise Prediction |
1967 |
247 | General Electric - CF6 Design for Maintainability |
undated |
247 | General Electric - CF6 Engine and Thrust Reverser Support Plan
for TWA |
1968 |
247 | General Electric - CF6 Facts About Weight and Length |
1967 |
247 | General Electric - CF6 High Bypass Turbofan - Condition
Monitoring |
undated |
248 | General Electric - CF6 High Bypass Turbofan Brochure |
1971 |
247 | General Electric - CF6 High Bypass Turbofan for Commercial
Subsonic Transports |
1965 |
248 | General Electric - CF6 High Bypass Turbofan Turbine
Cooling |
1970-1971 |
249 | General Electric - CF6 High Bypass Turbofan |
1970 |
247 | General Electric - CF6 Management Presentation |
1967 |
247 | General Electric - CF6 Noise Reduction Progress |
1968 |
250 | General Electric - CF6 Program Planning Guide for
TWA |
1970 |
248 | General Electric - CF6 Series Estimated Maintenance and Man-hour
Requirements |
undated |
247 | General Electric - CF6 Story |
undated |
247 | General Electric - CF6 Support Plan for TWA |
1967 |
247 | General Electric - CF6 Turbine Temperature Approach |
undated |
247 | General Electric - CF6-22 Engine Data Study |
1967 |
247 | General Electric - CF6-30 Engine Data Study |
1967 |
247 | General Electric - CF6-32 Preliminary Engine Model
Specification |
1967 |
247 | General Electric - CF6-34 Engine Model Specification
E-2065L |
1967 |
247 | General Electric - CF6-34 Thrust Reverser, Spoiler, and Nozzle
System Technical Proposal |
1967 |
247 | General Electric - CF6-34 Warranty for TWA |
1967 |
247 | General Electric - CF6-35 Turbofan Engine |
1967 |
247 | General Electric - CF6-36-2 Growth Memorandum |
1968 |
247 | General Electric - CF6-6 High Bypass Turbofan for
L-1011 |
1970 |
248 | General Electric - CF6-6 Series Long Term Material |
1970-1971 |
247 | General Electric - CF700-1 Installation and Performance
Manual |
1959 |
247 | General Electric - CF700-1 Turbofan |
1959 |
248 | General Electric - CJ805 Classified Figures for Design Study and
Layout Quenching and Inerting System |
circa 1956-1957 |
248 | General Electric - CJ805 Experience Brochure |
1966 |
248 | General Electric - CJ805 Test Bed Procedures |
undated |
248 | General Electric - CJ805-3 Operation Hi Time - 4300 Hour Flight
Test Demonstration |
undated |
247 | General Electric - CJ810 Aft-Fan Engine Brochure |
1959 |
247 | General Electric - Combustor Maintenance Concepts for GE4
Supersonic Transport |
1967 |
249 | General Electric - Comments on Minutes of Airline Supersonic
Transport Specialist Team Review of GE4 Engine |
1966 |
247 | General Electric - Compressor Welded Rotor Program Status
Report |
1967 |
248 | General Electric - Concorde 60 KVA Variable Speed Constant
Frequency General System |
1967 |
248 | General Electric - CT58 Powered Turbocopters |
1960-1962 |
248 | General Electric - CTF39 High Bypass Turbofan |
1966 |
247 | General Electric - Development of All Weather Landing System
Reliability Analysis and Criteria |
1965 |
279 | General Electric - Diagram drawings (B&W slides) |
undated |
248 | General Electric - Domestic Air Traffic Forecast |
1963-1972 |
248 | General Electric - Effects of Improved Power Quality on
Utilization Equipment |
1969 |
249 | General Electric - Facts About Augmented Turbojet Flexibility in
Airline Use |
undated |
249 | General Electric - Facts About Engine Inlet Distortion Tolerance
and Distortion Attenuation |
1966 |
249 | General Electric - Facts About GE4 Augmenter Durability and
Simplicity |
1966 |
249 | General Electric - Facts About GE4 Turbojet Augmenter
Flameholders |
1966 |
249 | General Electric - Facts About Inlet/Engine
Compatibility |
1966 |
249 | General Electric - Facts About Overland Sonic Boom on
International Routes |
1966 |
249 | General Electric - Facts About Why General Electric Chose the
Augmented Turbojet |
undated |
248 | General Electric - Failure Analysis CJ805-3 Fuel
Heater |
1960 |
249 | General Electric - Flight Proven Approach to Supersonic Transport
GE4 |
1966 |
249 | General Electric - GE Model and Performance
Specification |
1968 |
249 | General Electric - GE4 Airline Report |
1967 |
249 | General Electric - GE4 Supersonic Transport Augmented Turbojet
Experience |
1966 |
249 | General Electric - GE4 Supersonic Transport Export Airlines
Symposium |
1967 |
249 | General Electric - GE4 Supersonic Transport J93 Development and
XB-70 Flight Test Results |
1966 |
248-249 | General Electric - GE4 Supersonic Transport Phase III Program
Development Highlights |
1970 |
249 | General Electric - GE4/J5P Installation Requirement
Specification |
1970 |
249 | General Electric - GE4/J5P Type Installation Engine
Performance |
1968 |
247 | General Electric - High Bypass Economy Through
Experience |
1968 |
247 | General Electric - Hydrocarbon Fuel Cells - Survey |
1963 |
247 | General Electric - J85 Brochure |
1960 |
247 | General Electric - L-1011 Engine Fuel Temperature Indicating
System |
1968 |
250 | General Electric - L-1011 Engine H.P. Shaft Speed Indicating
System |
1968 |
250 | General Electric - L-1011 Engine Oil Quantity Indicating
System |
1968 |
250 | General Electric - L-1011 Engine Oil Temperature Indicating
System |
1968 |
250 | General Electric - L-1011 Fuel Flow and Consumed Quantity
Indicating System |
1968 |
250 | General Electric - L-1011 Indicator, Engine Pressure
Ratio |
1968 |
250 | General Electric - L-1011 Indicator, Exhaust Gas
Temperature |
1968 |
250 | General Electric - L-1011 Indicator, L.P. Engine Shaft
Speed |
1968 |
249 | General Electric - L-500 60/80 KVA Generating System JT9D Engine
Preliminary Technical Proposal |
1968 |
248 | General Electric - Measurement of Thrust of Installed CJ805
Engine |
1957-1959 |
247 | General Electric - Measurements and Analysis of Lightning Induced
Voltages in Aircraft Electrical Circuits |
1970 |
248 | General Electric - MF239 Aft Turbofan Installation
Manual |
1960 |
248 | General Electric - MF239 Aft Turbofan Power for SOR182 Cargo
Transport |
1960 |
248 | General Electric - MF239C-3 Aft Turbofan Power for SOR182 Cargo
Transport |
1960 |
250 | General Electric - MF239C-3 Aft Turbofan Power for Support System
476L |
1961 |
247 | General Electric - New Type of Fuel Cell |
1962-1963 |
248 | General Electric - Power Plant Installation Plan |
1971 |
247 | General Electric - Precipitation Static Studies Conducted During
Series of Flights in B17 Bomber |
1960 |
249 | General Electric - Preliminary Airline Planning Guide GE4
Overhaul Facilities |
1967 |
248 | General Electric - Presentation at TWA |
1968 |
248 | General Electric - Proposal for GE Mass Flowmeter System for
Concorde |
1963-1964 |
250 | General Electric - Quarterly Progress Report |
1965-1966 |
250 | General Electric - Review of Turbofan Noise Reduction
Program |
1968 |
250 | General Electric - Review of Work at Jet Engine Noise
Control |
1961 |
248 | General Electric - Servo Temperature System for Jet Engine
Temperature Measurement |
1955 |
250 | General Electric - Summary of CF6-6D Certification Program for
FAA Final Type Board Meeting |
1970 |
250 | General Electric - Supersonic Fan Burning Engines |
1960 |
248 | General Electric - Supersonic Transport Fuels Evaluation Program
Review Presentation |
1967 |
248 | General Electric - Supersonic Transport Phase III
Program |
1969 |
248 | General Electric - Supersonic Transport Propulsion Studies
Summary Report |
1962 |
247 | General Electric - T64 Aircraft Gas Turbine |
1965 |
247 | General Electric - T64 Training Guide |
1967 |
248 | General Electric - Technical Reports |
1958-1961 |
248 | General Electric - TF39 Development Program |
1967 |
248 | General Electric - Tip Turbine Driven Cruise Fan Propulsion
System |
1962-1963 |
247 | General Electric - Variable Stator Reset Mechanism Failure
Analysis |
1961 |
248 | General Electric - Versilube F-50 for Supersonic
Transport |
1963 |
250 | General Electric - VSCF Description |
undated |
250 | General Electric - VSCF Generating System Isolated and Parallel
System Test Data |
1965 |
247 | General Electric - VSCF Progress Report and the
Future |
1969 |
189 | General Electric CJ805 - Turbojet Engine Accessories Overhaul
Manual and Illustrated Parts Catalog |
1970 |
193 | General Electric CJ805 - Turbojet Engine Installation
Manual |
1961 |
193 | General Electric CJ805 - Turbojet Engine Performance Bulletin
Manual |
1961 |
189 | General Electric CJ805 - Turbojet Engine Tools and Equipment
Manual |
1962 |
201 | General Electric CJ805-3 - Turbojet Engine Operating
Instructions |
1960 |
246 | General Precision Incorporated - Airborne Digital Computer for
Concorde Proposal |
1964 |
246 | General Precision Incorporated - Study of Turbulence
Simulation |
1967 |
246 | General Precision Systems Limited - Visual Flight Simulation
Equipment for TWA Flight Simulators |
1967 |
246 | Goodrich - Boeing 727 Prototype Brake Overheat
Detector |
1963 |
246 | Goodrich - Brake Overheat Indicator System |
1963 |
246 | Goodrich - Engineering Equipment Proposal - Design/Supply Forced
Air Cooling System for Brakes |
1961 |
59 | Ground Handling Equipment |
1954 |
246 | Grummen Aircraft - NE Corridor VTOL Investigation |
1968 |
246 | Hamilton Standard - Boeing 747 Cabin Air Conditioning and
Temperature Control Systems |
1966 |
246 | Hamilton Standard - Boeing 747 Model PS 700-1 Starter and
Valve |
1972 |
246 | Hamilton Standard - Boeing 747 Systems |
1972 |
246 | Hamilton Standard - L-1011 System Simplification |
1968 |
246 | Heath Tecna Corporation - Spacemaker I Interior Recommended
Installation Instructions |
1979 |
246 | Heath Tecna Corporation - Statement of Work for Spacemaker II
Interior Model Kits |
1980 |
246 | Honeywell - Boeing 747 Engineering Design - Fuel Quantity
Indicating System |
1967 |
246 | IITRI - Operations Research Analysis of Aircraft Noise
Abatement |
1967-1968 |
246 | Inflight Motion Pictures Incorporated - Acceleration Test
Procedures |
1981 |
246 | Inflight Motion Pictures Incorporated - Altitude Test
Procedures |
1981 |
246 | Inflight Motion Pictures Incorporated - Boeing 747 Description,
Specifications, and Terms of Inflight Motion Picture Equipment to be
Installed |
undated |
246 | Inflight Motion Pictures Incorporated - Boeing 747 Entertainment
System Installation Document |
1969 |
246 | Inflight Motion Pictures Incorporated - Boeing 747 Qualification
Test Procedure |
1969 |
246 | Inflight Motion Pictures Incorporated - Boeing 747 Summary of
Weight and Load Analysis of IMP Projection System |
1969 |
246 | Inflight Motion Pictures Incorporated - Electromagnetic
Interference and Audio and Radio Frequency Susceptibility Test
Procedures |
1981 |
246 | Inflight Motion Pictures Incorporated - Functional Test Procedure
Airborne Projection System |
1969 |
246 | Inflight Motion Pictures Incorporated - Humidity Test
Procedure |
1981 |
246 | Inflight Motion Pictures Incorporated - Installation Projection
Units |
1969 |
246 | Inflight Motion Pictures Incorporated - L-1011 Motion Picture
Entertainment System Interface Requirements |
1969 |
246 | Inflight Motion Pictures Incorporated - Load and Stress Analysis
IMP Screen Assemblies |
1969 |
246 | Inflight Motion Pictures Incorporated - Magnetic Effect and Power
Input Test Procedures |
1981 |
246 | Inflight Motion Pictures Incorporated - On Line
Instructions |
1969 |
246 | Inflight Motion Pictures Incorporated - Temperature Environment
Test Procedures |
1981 |
246 | Inflight Motion Pictures Incorporated - Vibration Test
Procedures |
1981 |
251 | Lighting and Transients Research Institute - Aircraft Antenna
System Lightning Protection |
undated |
251 | Lighting and Transients Research Institute - Aircraft Protection
from Thunderstorm Electromagnetic Effects |
1964 |
251 | Link Group, General Precision Incorporated - Boeing 747-100 FAA
Test Guide Outline |
1970 |
251 | Link Group, General Precision Incorporated - L-1011 Digital
Flight Simulator - Site Requirements Specification |
1970 |
251 | Link Group, General Precision Incorporated - L-1011 Flight
Simulator - Technical Specification for TWA |
1969-1970 |
251 | Link Group, General Precision Incorporated - L-1011 Instructor
Consoles |
1970 |
251 | Link Group, General Precision Incorporated - L-1011 TWA Flight
and Engines Performance Test Guide |
1970 |
251 | Link Group, General Precision Incorporated - Structural Analysis
of 6 Degree of Freedom Motion System - Prepared for TWA |
1970 |
251 | Link Group, General Precision Incorporated - Technical Proposal
fro Advanced Training Software for Link 707 Digital Flight
Simulator |
1967 |
251 | Litton Systems Incorporated - Pilot Considerations for
Transatlantic Flights Using Inertial Navigation |
1964 |
251 | Litton Systems Incorporated - Topics in Inertial
Navigation |
1960 |
177 | Lord - Aircraft Service & Maintenance Manual of Dynafocal
Engine Suspensions Instrument & Communication Equipment
Mountings |
circa 1943-1952 |
40 | Martin - 404 C.A.A. Approved Flight Manual |
1951-1956 |
40 | Martin - C.A.A. Approved Airplane Flight Manual 2-0-2
Airplane |
1950-1951 |
251 | Massachusetts Institute of Technology (MIT) - Analysis of VSTOL
Aircraft Configurations for Short Haul Air Transportation
Systems |
1966 |
251 | McDonnell Douglas Corporation - EROS II Airline Collision
Avoidance Purchase Agreement for TWA |
1970 |
251 | McDonnell Douglas Corporation - EROS II Airline Collision
Avoidance System |
1966 |
251 | McDonnell Douglas Corporation - EROS II Airline Collision
Avoidance Technical Proposal for TWA |
1970 |
251 | McDonnell Douglas Corporation - EROS II Collision Avoidance
System as an Aid for Landing and Ground Obstacle Avoidance |
1970 |
251 | McDonnell Douglas Corporation - Final Submittal of Written
Information - NE Corridor VTOL Investigation Docket |
1969 |
251 | McDonnell Douglas Corporation - Model 210E Commercial STOL
Transport Preliminary Performance |
1968 |
251 | McDonnell Douglas Corporation - Model 210E Commercial STOL
Transport Proposed Approach to Certification Under FAA
Regulations |
1968 |
251 | McDonnell Douglas Corporation - Model 210E Commercial STOL
Transport Summary Type Specification |
1968 |
251 | McDonnell Douglas Corporation - STOL Demonstration Program
Guidance Control Air Traffic System |
1969 |
251 | McDonnell Douglas Corporation - Study on Feasibility of VSTOL
Concepts for Short-Haul Transport Airport |
1965 |
252 | McGill University - Initiation of Showers in Cumuli by
Snow |
1953 |
252 | McGill University - Proceedings of Third Radar Weather
Conference |
1952 |
252 | McGill University - Radar Evidence of a Generating Level for
Snow |
1953 |
252 | McGill University - Turbulence in Clouds as a Factor in
Precipitation |
1953 |
252 | Midwest Research Institute - Facilities for Metallurgical
Research |
1951, 1979 |
252 | Monogram - L-1011 and Boeing 747 TWA Proposal - Beverage Cart,
Tray Module, Freezer Chest |
1971 |
252 | Monsanto - Developmental Synthetic Fluids |
undated |
252 | Monsanto - Effects Selected Strains of Microorganisms on
Composition on Fuels and Lubricants |
1963-1964 |
252 | Monsanto - Research on Mechanisms of Thermal Decomposition of
Hydrocarbons |
1962-1963 |
252 | Monsanto - Skydrol 500 Medical and Toxicological
Aspect |
1957 |
252 | Monsanto - Skydrol LD Fire Resistant Aircraft Hydraulic
Fluid |
1969 |
252 | Monsanto - Skydrol Service Manual |
undated |
189 | MSG 2 - Boeing 747 and General Electric CJ805 Power Plant
Manual |
circa 1971 |
252 | National Advisory Committee for Aeronautics - Origin and
Prevention of Crash Fires in Turbojet Aircraft |
1958 |
252 | National Aeronautics and Space Administration (NASA) - Aircraft
Operating Problems - Measurement of Altitude on SST |
1967 |
252 | National Aeronautics and Space Administration (NASA) - Conference
on Progress of NASA Research Relating to Noise Alleviation of Large
Subsonic Jets |
1968 |
252 | National Aeronautics and Space Administration (NASA) - How to Use
NASA's Information System |
1958 |
252 | National Aeronautics and Space Administration (NASA) - Jumbo Jet
and Public Safety |
1967 |
252 | National Aeronautics and Space Administration (NASA) - Theory of
Inertial Navigation - Aided System |
1969 |
252 | National Aeronautics and Space Administration (NASA) - Titanium
and Its Alloys |
1966 |
252 | National Severe Storms Laboratory - Preliminary Quantitative
Analysis of Airborne Weather Radar |
1967-1968 |
252 | National Water Lift Company - Advanced On-Board Weighing
System |
1968 |
252 | National Water Lift Company - Aircraft On-Board Weight and
Balance System |
1969 |
252 | National Water Lift Company - L-1011 On-Board Weight and Balance
System Preliminary Proposal |
1968 |
252 | New York Testing Laboratories - Report Environmental Tests 3 -
Inflight Motion Pictures Projector Systems |
1969 |
252 | New York Testing Laboratories - Report of Tests on Motion
Pictures Screen for Inflight Motion Pictures |
1969 |
252 | Nordskog Company Incorporated - Static Test Report - Nordskog
Galleys Boeing 707 |
1958 |
252 | Northrop Corporation - Laminar Flow Control Presentation for
Aeronautical Systems Division |
1962 |
252 | Office of Science and Technology - Alleviation Jet Aircraft Noise
Near Airports |
1966-1968 |
52 | Operating Instructions for Q-Meters Type 160-A & Type
170-A |
undated |
252 | Pacific Electro Dynamics - 120 Watt Passenger Address
Amplifier |
undated |
252 | Pacific Inflatables Company - 26 Man Capacity Inflatable Aviation
Life Raft |
1969 |
252 | Pacific Inflatables Company - Advanced Design Evacuation
Slide/Raft Technical Data Bulletin |
1969 |
252 | Pacific Inflatables Company - Coated Fabric |
1969-1970 |
252 | Pacific Inflatables Company - Evacuation Slide/Raft |
1970 |
252 | Pacific Inflatables Company - Slide/Raft Technical
Presentation |
undated |
252 | Pacific Inflatables Company - Stored Gas Inflation
System |
undated |
252 | Pacific Scientific Company - Performance Test Procedure for Lap
Belt Inertia Locking |
1969 |
252 | Pacific Scientific Company - Test Report 726 Tests - Retractor
Lap Belt Inertia Locking |
1970 |
252 | Philco - Navigation and Communication Satellite System
Concepts |
undated |
58 | Power Chart Manual |
1959-1967 |
181 | Publications relating to radio waves, microwaves, and electrical
technology |
1938-1959 |
252 | Puritan Compressed Gas Corporation - Crew Oxygen Mask
Assembly |
1959 |
252 | Puritan Compressed Gas Corporation - Design Proposal Passenger
Emergency Oxygen Service Unit for Convair |
1961 |
252 | Puritan Compressed Gas Corporation - Functional Test Puritan
Smoke Goggles |
1966 |
252 | Puritan Compressed Gas Corporation - Instructions for Use of
Oxygen Mask |
undated |
252 | Puritan Compressed Gas Corporation - Leak Test Report on Puritan
Sweep-On Mask |
1963 |
252 | Puritan Compressed Gas Corporation - Report Leak Test on Crew
Oxygen Mask |
1959 |
252 | Radio Corporation of America - Index to 1965 RCA Technical
Papers |
1966 |
252 | Radio Corporation of America - SECANT - Anti-Collision System for
Airplanes |
1970 |
252 | Radio Technical Commission for Aeronautics (RTCA) - Current
Status Universal Air-Ground Digital Communications System
Standards |
1968 |
252 | Radio Technical Commission for Aeronautics (RTCA) - Digital
Communications System |
1967 |
252 | Radio Technical Commission for Aeronautics (RTCA) - Environmental
Conditions and Test Procedures for Airborne Electronic
Instruments |
1967-1968 |
252 | Radio Technical Commission for Aeronautics (RTCA) - Environmental
Test Procedures Airborne Electronic Equipment |
1967 |
252 | Radio Technical Commission for Aeronautics (RTCA) - Universal
Air-Ground Digital Communications System Standards |
1964 |
252 | Raychem Corporation - Testing of Insulated Aluminum Wire for
Boeing 747 |
1968 |
252 | Redifon - Flight Simulator Compatibility Requirements for Redifon
Rigid Model Visual System |
1969 |
252 | Redifon - Flight Simulator Standards and Requirements for
Coupling Color Visual Presentation System to a Transport
Simulator |
1964 |
252 | Redifon - Flight Simulator Visual System
Specification |
1970 |
252 | Redifon - L-1011 Flight Simulator - Cost Proposal |
1969 |
252 | Redifon - L-1011 Flight Simulator Installation and Assembly
Information |
1969 |
252 | Redifon - PA Between TWA and Redifon Electronics and Redifon Air
Trainers Relating to a Visual System Complex |
1970 |
252 | Redifon - PA Between TWA and Redifon Electronics and Redifon Air
Trainers Relating to L-1011 Flight Simulator |
undated |
252 | Robbins Aviation - Oxygen Valves - Cycle Life with Various O-Ring
Compounds and Lubricants |
1960 |
252 | Robertshaw-Fulton Controls Company - Automatic Opening,
Continuous Flow Oxygen Regulator |
1961 |
252 | Robertshaw-Fulton Controls Company - Miniature Compact Crew
Oxygen System |
1963 |
252 | Robertshaw-Fulton Controls Company - Proposal to Boeing -
Miniature, Diluter-Demand Automatic-Pressure-Breathing Oxygen
Regulator |
1968 |
252 | Robertshaw-Fulton Controls Company - Puritan Mask or
Equivalent |
1967 |
252 | Robinson Technical Products - Robinson Met-L-Flex Engine Mounts
for Aircraft Jet Engines |
1963 |
252 | Rohr Corporation - Economic Impact Implementing Acoustically
Treated Nacelle and Duct Configurations Applicable to Low Bypass
Turbofan Engines |
1970 |
254 | Rolls-Royce - Atmospheric Pollution by Gas Turbine
Engines |
1967-1968 |
254 | Rolls-Royce - Contract Specification - Turbofan Spare
Engines/Exhaust Systems for L-1011 |
1968 |
254 | Rolls-Royce - Engine Presentation of Commercial
Organization |
1967 |
254 | Rolls-Royce - Engine Presentation of Engineering
Organization |
1967 |
254 | Rolls-Royce - Engine Presentation of Experimental
Organization |
1967 |
254 | Rolls-Royce - Engine Presentation of Production
Organization |
1967 |
252 | Rolls-Royce - Engine Rating, Control, and Operation |
1968 |
254 | Rolls-Royce - Geometric Tolerancing on Engineering
Drawings |
1972 |
252 | Rolls-Royce - Initial Proposal for Trend Analysis
Program |
1970 |
252 | Rolls-Royce - L-1011 Propulsion Systems |
1969 |
252 | Rolls-Royce - Maximum Parts Cost Guarantee |
1968 |
254 | Rolls-Royce - Olympus 593 Thrust Development |
1969 |
252 | Rolls-Royce - Performance Specification and Installation
Notes |
1968-1969 |
254 | Rolls-Royce - Performance Specification |
1969-1971 |
254 | Rolls-Royce - Performance Technical Report - Engine
Proposal |
1969 |
252 | Rolls-Royce - Performance, Weight, and Installation Specification
for L-1011 |
1968 |
254 | Rolls-Royce - Preliminary Contract Specification - Spare Engines
for L-1011 |
1968 |
254 | Rolls-Royce - Preliminary Contract Specification - Turbofan for
LAC 1011 |
1967 |
252 | Rolls-Royce - Preliminary Contract Specification - Turbofan Spare
Engine for LAC L-1011 |
1968 |
254 | Rolls-Royce - Propulsion System Design and Warranty
Responsibility Index |
1968 |
252 | Rolls-Royce - Propulsion System UK Service Group |
1969 |
252 | Rolls-Royce - Spare Parts Agreement Between RR and
RB211 |
1968 |
252 | Rolls-Royce - Support Engine and Support Module
Program |
1968 |
254 | Rolls-Royce - Support Proposals - Engines for U.S.
Operators |
1967-1968 |
254 | Rolls-Royce - Warranty of Civil Gas Turbine Engines and Parts -
Engines |
1967 |
254 | Rotax - High Energy Ignition Unit |
1969 |
254 | Royal Industries - Tray Module |
undated |
254 | Royal Industries - TWA Freezer Module Technical
Proposal |
undated |
254 | Saudi Arabia Airlines - Fleet Plans |
1970-1980 |
254 | Shell Oil Company - ASA-3 Additive Static Electricity Dissipater
Questions and Answers |
1961 |
254 | Shell Oil Company - ASA-3 Safety in Fuel Handling |
1964 |
254 | Shell Oil Company - Aviation Turbine Fuels and ASA-3
Additive |
1961 |
254 | Shell Oil Company - Current Status of Static Dissipater Additives
for Aviation Turbine Fuels |
1963 |
254 | Shell Oil Company - Electrostatic charging Tests on
DC-9 |
1963 |
254 | Shell Oil Company - Electrostatic Safety in Fuel
Handling |
1964 |
254 | Shell Oil Company - Static Electricity in Aircraft Fuelling Tests
at Vicker-Armstrongs |
1958 |
254 | Shell Oil Company - Static Electricity in Aircraft Fuelling Tests
on Simulated Wing Tank |
1960 |
254 | Sikorsky Aircraft - NE Corridor VTOL Investigation
Docket |
undated |
254 | Sikorsky Aircraft - VTOL IFR Flight Demonstration
NY-DCA |
undated |
254 | Sky Bar Corporation - Dispensing System |
undated |
254 | Snecma - Noise Reduction of Turbo-Jet Engines |
1970 |
255 | Society of Automotive Engineers (SAE) - Areas of Agreement
Regarding Measurement and Evaluation of Aircraft Noise
Committee |
1966 |
255 | Society of Automotive Engineers (SAE) - Development of an
Aircraft Flyover Noise Rating Scale |
1970 |
255 | Society of Automotive Engineers (SAE) - Interior Contours Main
Deck Cargo Compartment - Jet Powered Cargo Airplanes |
1966 |
183 | Society of Automotive Engineers (SAE) - Meeting |
1966 |
255 | Society of Automotive Engineers (SAE) - Proposal for
Documentation of Noise Exposure Around Airports - Cost and
Contracts |
1966 |
255 | Socony-Vacuum Oil Company - Physical Characteristics of Aircraft
Gas Turbine Fuels |
1945 |
255 | Standard Manufacturing Company - Proposed Unitized Cargo Handling
System |
1963 |
255 | Standard Oil Company - Microbiological Fuel
Contamination |
1962 |
255 | Standard Telephones and Cable - Radio Altimeters |
1963 |
255 | Stanford Research Institute - Air Cargo |
1959 |
255 | Stanford Research Institute - Precipitation Charging and
Corona-Generated Interference in Aircraft |
1961 |
255 | Stauffer Chemical Company - Aero Safe 2300 Fire Resistant
Aircraft Hydraulic Fluid |
1968 |
59 | Stores Illustrated Charges |
1956-1958 |
159 | Structural Repair Instructions for the Super Constellation models
1049C, D, E, G, H |
1960 |
159 | Structural Repair Manual for the Model 1649 Series
Airplanes |
1957-1959 |
159 | Structural Repair Manual for the Super Constellation Airplanes
Model 1049 |
1958 |
255 | Sud-Aviation - Concorde - Test Program |
1967 |
255 | Sud-Aviation - Concorde Over the Pacific |
1968 |
255 | Sud-Aviation - Concorde Pacific Network Appraisal |
1968 |
255 | Sud-Aviation - Concorde Review of Handling Characteristics in
Supersonic Flight with Aft CG Positions |
1970 |
255 | Sud-Aviation - Sonic Boom - Acceleration Effects |
1966 |
255 | Sud-Aviation - Sonic Boom Performance Comparison with Different
Flight Trajectories |
1965 |
255 | Sud-Aviation - SST Air-Conditioning System - Reliability
Analysis |
1966-1967 |
255 | Sud-Aviation - SST Aircraft - Braking System
Description |
1966 |
255 | Sud-Aviation - SST Cabin Pressure Control System Analysis of
Reliability |
1966 |
255 | Sud-Aviation - SST Concorde - Autostabilizer System - Reliability
Analysis |
1967 |
255 | Sud-Aviation - SST Concorde Autothrottle - Reliability
Analysis |
1967 |
255 | Sud-Aviation - SST Concorde Normal and Standby Braking System -
Reliability Analysis |
1967 |
255 | Sud-Aviation - SST Concorde Structural Test Program |
1965-1966 |
255 | Sud-Aviation - Tests on Air Conditioning Generation System and
Pressure Control System |
1967 |
255 | Sud-Aviation - Tires, Wheels, Brakes |
1966 |
255 | Sud-Aviation - TSS Concorde - Project Specification
Technique |
1966 |
255 | Sundstrand Engineering - 60 KW Constant Speed Drive for
Concorde |
1967 |
255 | Sundstrand Engineering - Auxiliary Hydraulic Power Supply System
Photographs |
undated |
255 | Sundstrand Engineering - CSD System for Airbus DC-10, L-1011,
757 |
undated |
255 | Sundstrand Engineering - Product Specifications for Digital
Flight Data Recorder |
1970 |
255 | Sundstrand Engineering - System Over-Running Clutch |
1969 |
49 | Super Constellation Model 1049 Crew Operating |
1951 |
35 | Super Constellation Model 1049 Parts Manual |
1952-1960 |
50 | Super Constellation Model 1049G Parts |
1956-1966 |
51 | Super Constellation Model 1049G Parts |
1958-1959 |
38 | Super Constellation Model 1049H Parts |
1957-1960 |
184 | Super Constellation Pocket Handbook |
1955 |
255 | Teledyne Company - Aircraft Escape and Rescue
Systems |
undated |
255 | Teledyne Company - Emergency Ground Egress from USAF Passenger
Carrying Aircraft |
1969 |
255 | Teledyne Company - L-1011 Parameter Tables |
1970 |
255 | Teledyne Company - Meeting |
1970 |
255 | Teledyne Company - Study of Failure in Aircraft Emergency
Evacuation Systems |
1969 |
255 | Teledyne Company - Systems for Aircraft Safety |
1970 |
255 | TIA Electric Company - Proposal for Display Case Boeing
747 |
1970 |
25 | Turbo Compound Power Recovery Turbine Service
Division |
1958-1961 |
32 | TWA Inventory Parts Catalog Vol. 2 |
1956 September |
41 | TWA Martin Operating Manual |
1953-1959 |
256 | United States Department of Health, Education, Welfare - DCA
Metropolitan Area Air Pollution Abatement Activity |
1967 |
256 | United States Department of Health, Education, Welfare - Handbook
of Sanitation of Airlines |
1964 |
256 | United States Department of the Interior - Bureau of Mines -
Function of Hydrocarbon and Nitrogen Oxides Photochemical-Smog
Formation |
1970 |
256 | United States Department of the Interior - Bureau of Mines -
Photochemical Reactivity of Diesel Exhaust |
1971 |
256 | United States Department of the Interior - Bureau of Mines -
Reactivities of Exhaust Aldehydes Investigations |
1971 |
256 | United States Department of the Interior - Mercury Contamination
in Natural Environment |
1970 |
256 | United States Department of the Navy - Naval Air Systems Interior
Communications Systems |
1970 |
256 | United States Department of the Navy - Tri-Service Coordination
of Electromagnetic Interference Standards and
Specifications |
1966 |
256 | United States Department of Transportation - Accident
Data |
1967 |
256 | United States Department of Transportation - Aircraft Accident
Report - TWA DC-9 Urbana, Ohio |
1967 |
256 | United States Department of Transportation - Aircraft Accident
Report - West Coast Airlines |
1966-1968 |
256 | United States Department of Transportation - Annual Review of
U.S. Carrier Accidents |
1966-1967 |
256 | United States Department of Transportation - Annual Review of
U.S. General Aviation Accidents |
1966-1967 |
256 | United States Department of Transportation - Briefs of Accidents
in U.S. Civil Aviation |
1967-1968 |
256 | United States Department of Transportation - Civil Air Carrier
Crash Experience - Limiting Factors in Crash Survival and
Escape |
1967-1968 |
256 | United States Department of Transportation - Design Study and
Model Structures Test Program to Improve Fuselage
Crashworthiness |
1967 |
256 | United States Department of Transportation - Investigations and
Summaries of Accidents |
1968 |
256 | United States Department of Transportation - Meeting - Operating
Problems - Accidents |
1968 |
256 | United States Department of Transportation - Ten Year Plan -
National Aviation System Plan |
1970-1980 |
256 | United States Department of Transportation - Terminal Area
Airline Delay Data |
1964-1970 |
256 | Vickers Incorporated - Auxiliary Motorpump for DC-9 |
1963 |
256 | Vickers Incorporated - Main Engine Pump for DC-9 |
1963 |
256 | Vickers Incorporated - PV3-240 Inline Pump for Boeing
747 |
1966 |
256 | Walter Kidde Company - Fuel Tank Inerting Jet
Aircraft |
1964 |
256 | Walter Kidde Company - L-1011 Fire Detection System |
1968 |
256 | Weber Aircraft - Double and Triple Coach Seats Static and Dynamic
Tests |
1962 |
256 | Weber Aircraft - Flame Resistance Characteristics of Non-Metallic
Material Used on 1047 Passenger Seats |
1971 |
256 | Weber Aircraft - L-1011 TWA Passenger Seat Development -
Coach |
1970 |
256 | Weber Aircraft - L-1011 TWA Passenger Seats Capability Profile
Proposal |
1970 |
256 | Weber Aircraft - L-1011 TWA Passenger Seats Engineering Design
Proposal |
1970 |
257 | Westinghouse Electric - Addendum to Westinghouse
Proposal |
1967 |
224 | WG Armstrong Whitworth LTD - Argosy Components Common to
Viscount, AVRO 748, Friendship, and Herald |
undated |
257 | Wiggins Oil Tool - Fatigue Testing and Comparison Testing of
Wiggins DL-100 Connectors |
1963 |
257 | Wiggins Oil Tool - Test Procedures and Results for Wiggins 3" and
4" Line Size Swaged Ferrule Wig-O-Flex Coupling |
1963 |
257 | Wilcox Electrical Company - Instruction Manual Glide Slope
Receiver |
1962-1964 |
257 | Wilcox Electrical Company - Overhaul Manual for ATC
Transponder |
1965 |
28 | Wiring Diagram Manual TWA Model 1649 Series
Airplanes |
1957-1962 |
54 | Wright Aircraft Engines Commercial Cyclone 18 Models Operating
Instructions |
1957 February |
54 | Wright Aircraft Engines Direct Injection Turbo Compound Models
Operating Instructions |
1958 September |
24 | Wright Aircraft Engines Series C18BD Parts Catalog |
1958-1965 |
23 | Wright Aircraft Engines Series TC18DA Parts Catalog |
1959-1965 |
21 | Wright Aircraft Engines Series TC18EA Parts Catalog |
1960-1965 |
54 | Wright Turbo-Compound Engine TC18EA Series…Installation
Data |
1957 October |
159 | Wright Turbo-Compound TC18DA Engine Series 972TC18DA1, DA2, &
R3350-34 Models Installation Data |
1954 January |
54 | Wright Turbo-Compound TC18DA Engine Series Models 972TC1DA1, DA2,
DA3, DA4, & Military Counterparts Installation Data
AED-20-E |
1957 March |
257 | Wright-Patterson Air Force Base - Aircraft Vibrations Due to
Brake Chatter and Squeal |
1955 |
257 | Wright-Patterson Air Force Base - Coefficient of Friction of
Aircraft Tires on Concrete Runways |
1955-1956 |
257 | Wright-Patterson Air Force Base - Community Reactions to Sonic
Booms in Oklahoma City Area |
1965 |
257 | Wright-Patterson Air Force Base - Criteria for Short Term
Exposure of Personnel to High Intensity Jet Airline Noise |
1955 |
257 | Wright-Patterson Air Force Base - Design Study of Aircraft Cargo
Handling System for High Floor Aircraft |
1959-1960 |
257 | Wright-Patterson Air Force Base - Determination of Standard
Extinguishing Agent for Airborne Fixed Systems |
1960-1961 |
257 | Wright-Patterson Air Force Base - Effect of Corrosion Inhibitors
on Fuel Behavior in Filter-Separator Life Tests |
1970 |
257 | Wright-Patterson Air Force Base - Emergency Evacuation Tests of
C-9A Aeromedical Aircraft |
1969 |
257 | Wright-Patterson Air Force Base - Engineering Study of Aircraft
Crash-Fire Prevention |
1958-1959 |
257 | Wright-Patterson Air Force Base - Examination of Methods for
Calculating Vapor Pressure of Petroleum Hydrocarbon |
1964 |
257 | Wright-Patterson Air Force Base - Factor Involved in Determining
Efficiency of Fire Extinguishing Agents |
1959 |
257 | Wright-Patterson Air Force Base - Flight Test Evaluation of
Aircraft Pressure Altimeter Installations |
1956-1957 |
257 | Wright-Patterson Air Force Base - Handbook of Liquid Oxygen
Systems |
1956-1957 |
257 | Wright-Patterson Air Force Base - Ignition Characteristics of
Fuels and Lubricants |
1963-1966 |
257 | Wright-Patterson Air Force Base - Proceedings Fatigue of Aircraft
Structures |
1959 |
257 | Wright-Patterson Air Force Base - Review of Ignition and
Flammability Properties of Lubricants |
1968 |
Names and SubjectsReturn to Top
Subject Terms
- Aeronautics, Commercial -- United States -- 20th century.
- Aerospace engineering -- United States -- 20th century.
- Airlines -- History -- United States -- 20th century.
- Airplanes -- Motors -- 20th century.
- Jet engines -- United States -- 20th century.
Corporate Names
- Lockheed Aircraft Corporation.