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Pilot Human Factors in Stall/Spin Accidents of Supersonic Fighter AircraftA study has been made of pilot human factors related to stall/spin accidents of supersonic fighter aircraft. The military specifications for flight at high angles of attack are examined. Several pilot human factors problems related to stall/spin are discussed. These problems include (1) unsatisfactory nonvisual warning cues; (2) the inability of the pilot to quickly determine if the aircraft is spinning out of control, or to recognize the type of spin; (3) the inability of the pilot to decide on and implement the correct spin recovery technique; (4) the inability of the pilot to move, caused by high angular rotation; and (5) the tendency of pilots to wait too long in deciding to abandon the irrecoverable aircraft. Psycho-physiological phenomena influencing pilot's behavior in stall/spin situations include (1) channelization of sensory inputs, (2) limitations in precisely controlling several muscular inputs, (3) inaccurate judgment of elapsed time, and (4) disorientation of vestibulo-ocular inputs. Results are given of pilot responses to all these problems in the F14A, F16/AB, and F/A-18A aircraft. The use of departure spin resistance and automatic spin prevention systems incorporated on recent supersonic fighters are discussed. These systems should help to improve the stall/spin accident record with some compromise in maneuverability.
Document ID
19830018575
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, S. B.
(NASA Ames Research Center Moffett Field, CA, United States)
Enevoldson, E. K.
(NASA Ames Research Center Moffett Field, CA, United States)
Nguyen, L. T.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1983
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:84348
NASA-TM-84348
A-9297
Report Number: NAS 1.15:84348
Report Number: NASA-TM-84348
Report Number: A-9297
Meeting Information
Meeting: AGARD Conf. Flight Mech. Sys. Design Lessons from Operational Exper.
Location: Athens
Start Date: May 10, 1983
End Date: May 13, 1983
Accession Number
83N26846
Funding Number(s)
PROJECT: RTOP 505-34-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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