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Comparative analysis of PA-31-350 Chieftain (N44LV) accident and NASA crash test dataA full scale, controlled crash test to simulate the crash of a Piper PA-31-350 Chieftain airplane is described. Comparisons were performed between the simulated crash and the actual crash in order to assess seat and floor behavior, and to estimate the acceleration levels experienced in the craft at the time of impact. Photographs, acceleration histories, and the tested airplane crash data is used to augment the accident information to better define the crash conditions. Measured impact parameters are presented along with flight path velocity and angle in relation to the impact surface.
Document ID
19790025001
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hayduk, R. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1979
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA-TM-80102
L-13064
Accession Number
79N33172
Funding Number(s)
PROJECT: RTOP 505-02-33-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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