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Controlling crippled aircraft-with throttlesA multiengine crippled aircraft, with most or all of the flight control system inoperative, may use engine thrust for control. A study was conducted of the capability and techniques for emergency flight control. Included were light twin engine piston powered airplanes, an executive jet transport, commercial jet transports, and a high performance fighter. Piloted simulations of the B-720, B-747, B-727, MD-11, C-402, and F-15 airplanes were studied, and the Lear 24, PA-30, and F-15 airplanes were flight tested. All aircraft showed some control capability with throttles and could be kept under control in up-and-away flight for an extended period of time. Using piloted simulators, landings with manual throttles-only control were extremely difficult. However, there are techniques that improve the chances of making a survivable landing. In addition, augmented control systems provide major improvements in control capability and make repeatable landings possible. Control capabilities and techniques are discussed.
Document ID
19910019877
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Burcham, Frank W., Jr.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Fullerton, C. Gordon
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1991
Subject Category
Aircraft Stability And Control
Report/Patent Number
H-1747
NAS 1.15:104238
NASA-TM-104238
Report Number: H-1747
Report Number: NAS 1.15:104238
Report Number: NASA-TM-104238
Meeting Information
Meeting: International Air Safety Seminar
Location: Singapore
Country: Singapore
Start Date: November 12, 1991
End Date: November 14, 1991
Accession Number
91N29191
Funding Number(s)
PROJECT: RTOP 533-02-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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