Accession Number : ADA135884

Title :   Structural Response of Transport Airplanes in Crash Situations.

Descriptive Note : Final technical rept.,

Corporate Author : FEDERAL AVIATION ADMINISTRATION TECHNICAL CENTER ATLANTIC CITY NJ

Personal Author(s) : Thomson,R G ; Caiafa,C

PDF Url : ADA135884

Report Date : Nov 1983

Pagination or Media Count : 123

Abstract : This report highlights the results of contractural studies of transport accident data undertaken in a joint research program sponsored by the FAA and NASA. From these accident data studies it was concluded that the greatest potential for improved transport crashworthiness is in the reduction of fire related fatalities. Accident data pertaining to fuselage integrity, main landing gear collapse, fuel tank rupture, wing breaks, tearing of tank lower surfaces, and engine pod scrubbing are discussed. In those accidents where the energy absorbing protective capability of the fuselage structure is expended and the airplane experiences major structural damage, trauma caused fatalities are also discussed. The dynamic performance of current seat/restraint systems are examined but it is concluded that the accident data does not adequately define the relationship between occupant response and the dynamic interaction with the seat, floor and fuselage structure. (Author)

Descriptors :   *Aviation accidents, *Transport aircraft, *Structural properties, *Crashworthiness, *Accident investigations, Crashes, Structural analysis, Data acquisition, Fire hazards, Casualties, Death, Reduction, Survivability, Trauma, Fuselages, Landing gear, Collapse, Fuel tanks, Rupture, Wings, Fracture(Mechanics), Engine components, Damage, Protection, Aircraft seats

Subject Categories : Transport Aircraft
      Safety Engineering

Distribution Statement : APPROVED FOR PUBLIC RELEASE