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MIL-A-8865B

AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS

Organization:
AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City
Year: 1987

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.
URI: http://yse.yabesh.ir/std;query=autho1513AF679D40AC4261598F1EFDEC014A/handle/yse/190444
Subject: Aerial delivery loads
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  • AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City
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    MIL-A-8865B

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contributor authorAIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City
date accessioned2017-09-04T18:07:33Z
date available2017-09-04T18:07:33Z
date copyright05/20/1987
date issued1987
identifier otherGPCJDAAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho1513AF679D40AC4261598F1EFDEC014A/handle/yse/190444
description abstractThis 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.
languageEnglish
titleMIL-A-8865Bnum
titleAIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADSen
typestandard
page13
statusActive
treeAIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City:;1987
contenttypefulltext
subject keywordsAerial delivery loads
subject keywordsAirplane
subject keywordsControl system loads
subject keywordsCrash loads
subject keywordsExternal stores
subject keywordsFlight seats
subject keywordsFlight tests
subject keywordsFloor strength
subject keywordsFlying-boom system
subject keywordsGust
subject keywordsLitter installation loads
subject keywordsParachute brakes
subject keywordsProbe-and-drogue system
subject keywordsRefueling loads
subject keywordsRigidity
subject keywordsStrength
subject keywordsTail-to-wind loads
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