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TR 89-D-22A (VOLUME-II) USAAVSCOM AIRCRAFT DESIGN CRASH IMPACT CONDITIONS AND HUMAN TOLERANCE - FINAL REPORT (DEC-1989)

TR 89-D-22A (VOLUME-II) USAAVSCOM AIRCRAFT DESIGN CRASH IMPACT CONDITIONS AND HUMAN TOLERANCE - FINAL REPORT (DEC-1989)., This revised edition of the Aircraft Crash Survival Design Guide (ACSDG) was prepared to assist those design engineers responsible for the incorporation of crash-worthiness inot the design of helicopters, light fixed-wing aircraft, and tilt rotor aircraft.

TR 89-D-22 Rev. A

    
 Status:
Active

 FSC Code:
 SAFT - SYSTEM SAFETY

Version:
A11-200012.00 MB TR_89-D-22A_VOL-5_DEC1990
A11-198910.86 MB TR_89-D-22A_VOL-1_DEC1990
A11-19895.77 MB TR_89-D-22A_VOL-2_DEC1990

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