DISTRIBUTION A. Approved for public release; distribution unlimited.
EN-SB-10-002, Page 1 of 11
Number: EN-SB-10-002 Rev-A
Date: 21 November 2011
Subject: Air Force Crash Load and Cargo Restraint Requirements for Fixed
Wing Aircraft
References:
1. Joint Service Specification Guide 2006, Aircraft Structures, Department of
Defense, 30 October 1998.
2. Joint Service Specification Guide 2010, Crew Systems, Department of
Defense, 30 October 1998.
3. MIL-A-8865 (ASG) “Airplane Strength and Rigidity Miscellaneous Loads,”
18 May 1960.
4. MIL-HDBK-1791, "Designing for Internal Aerial Delivery in Fixed Wing
Aircraft," 14 February 1997.
5. MIL-A-008865A “Airplane Strength and Rigidity Miscellaneous Loads,” 31
March 1971.
6. MIL-A-008865A Amendment 2 “Airplane Strength and Rigidity
Miscellaneous Loads,” 7 November 1973.
7. MIL-A-008865A Amendment 3 “Airplane Strength and Rigidity
Miscellaneous Loads,” 17 February 1977.
8. NACA TR-1133 “Mechanism of Start and Development of Aircraft Crash
Fires,” NASA Glenn Research Center, 1952.
9. “The Relationship of Injuries to Structures in Survivable Aircraft Accidents,”
Committee of Medical Research and the Committee on Aviation Medicine
of the National Research Council, 1943.
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