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MIL-A-8866C

AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE

contributor authorNAVY - AS - Naval Air Systems Command
date accessioned2017-09-04T15:26:39Z
date available2017-09-04T15:26:39Z
date copyright05/20/1987
date issued1987
identifier otherNPCJDAAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/27489
description abstractThis specification defines the strength and rigidity requirements for repeated loading condition applicable to Navy procured airplanes. Intended Use: The requirements of this specification are intended for use in the structural design and substantiation of airplanes.
languageEnglish
titleMIL-A-8866Cnum
titleAIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCEen
typestandard
page15
statusActive
treeNAVY - AS - Naval Air Systems Command:;1987
contenttypefulltext
subject keywordsAirplane
subject keywordsArresting
subject keywordsCabin pressurization
subject keywordsCarrier-based airplanes
subject keywordsCatapulting
subject keywordsFatigue
subject keywordsFlight maneuver loads
subject keywordsFlight tests
subject keywordsGust loads
subject keywordsLoads
subject keywordsReliability requirements
subject keywordsRepeated loads
subject keywordsRigidity
subject keywordsService life
subject keywordsSinking speeds
subject keywordsStrength
subject keywordsTaxi ground loads
subject keywordsTrainers
subject keywordsTurbulence
subject keywordsVibration


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