MIL-A-8865B

AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS

contributor author	AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City
date accessioned	2017-09-04T18:07:33Z
date available	2017-09-04T18:07:33Z
date copyright	05/20/1987
date issued	1987
identifier other	GPCJDAAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=autho1513AF679D40AC4261598F1EFDEC014A/handle/yse/190444
description abstract	This specification contains the strength and rigidity requirements for miscellaneous loads applicable to acquisition of airplanes. Intended Use: The requirements of this specification are intended for use in the structural design and substantiation of airplanes.
language	English
title	MIL-A-8865B	num
title	AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS	en
type	standard
page	13
status	Active
tree	AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City:;1987
contenttype	fulltext
subject keywords	Aerial delivery loads
subject keywords	Airplane
subject keywords	Control system loads
subject keywords	Crash loads
subject keywords	External stores
subject keywords	Flight seats
subject keywords	Flight tests
subject keywords	Floor strength
subject keywords	Flying-boom system
subject keywords	Gust
subject keywords	Litter installation loads
subject keywords	Parachute brakes
subject keywords	Probe-and-drogue system
subject keywords	Refueling loads
subject keywords	Rigidity
subject keywords	Strength
subject keywords	Tail-to-wind loads