F-111D, DT and E Evaluation of Environmental Control, Airframe, Flight Control, and Secondary Power Subsystems. Appendix 1

• Main Author: Olson, Richard W
• Other Authors: AIR FORCE TEST CENTER EDWARDS AFB CA
• Format: Text
• Language: English
• Published: 1973
• Subjects: Bombers; Attack and Fighter Aircraft; *JET FIGHTERS; AIRFRAMES; ARCTIC REGIONS; AVIONICS; CHECKOUT PROCEDURES; COCKPITS; COLD WEATHER TESTS; COMPUTER PRINTOUTS; COOLING AND VENTILATING EQUIPMENT; DATA PROCESSING; DEICING SYSTEMS; ENVIRONMENTAL TESTS; FIGHTER BOMBERS; FLIGHT CONTROL SYSTEMS; FLIGHT TESTING; HEATING; HYDRAULIC EQUIPMENT; PERFORMANCE(ENGINEERING); TEMPERATURE; F-111D AIRCRAFT; *F-111 AIRCRAFT; Arctic
• Online Access: http://www.dtic.mil/docs/citations/ADB002373; http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADB002373

During the arctic test phase of the F-111D DT/E All-Weather Test Program, 24.0 hours of test time were accumulated in 12 test flights. Five of these flights were selected as being most representative of aircraft operation in an arctic environment. All available data obtained on these five flights are presented in this document as computer printouts. Appendix 1 to ADB002372. See also Appendix 2, ADB002374.