GENERAL AVIATION CRASH SURVIVABILITY
Estimates that an aircraft will be involved in an accident over a 20 year life range are as high as 60-70%. Recognition of this probability has led to crashworthiness and occupant survivability "packaging" design concepts as offering the most realistic approach to reduction of serious and fatal injuries when an accident occurs. This paper reviews and illustrates current general aviation aircraft accident experience relative to occupant impact injury and damage indexes, and provides new data relative to current-generation aircraft. Results clearly indicate that when the cabin structure remains relatively intact, the occupant is adequately restrained in an energy-absorbing seat system, the interior structures are designed to distribute loads and absorb energy, and the impact forces imposed on the occupant are within human tolerances, the occupant can survive without serious injury even when the aircraft is destroyed.
- For Meeting held February 27-March 3, 1978.
Warrendale, PA United States 15096
- Snyder, R G
- Publication Date: 1978
- Features: References;
- Pagination: 26 p.
- Society of Automotive Engineers Preprint
- Publisher: Society of Automotive Engineers (SAE)
- TRT Terms: Air transportation; Air transportation crashes; Aircraft; Aviation safety; Crashes; Crashworthiness; Crashworthiness; Fatalities; General aviation aircraft; Injuries; Manual safety belts; Occupant protection devices; Restraint systems; Seats; Survival
- Uncontrolled Terms: Aircraft safety; Occupant protection
- Old TRIS Terms: Aircraft occupant protection; Occupant restraint
- Subject Areas: Aviation; Safety and Human Factors; Vehicles and Equipment;
- Accession Number: 00188594
- Record Type: Publication
- Source Agency: Engineering Index
- Report/Paper Numbers: SAE 780017
- Files: TRIS
- Created Date: Mar 14 1979 12:00AM