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MIL-T-81259B

TIE-DOWNS, AIRFRAME DESIGN, REQUIREMENTS FOR

Organization:
NAVY - AS - Naval Air Systems Command
Year: 1991

Abstract: This specification defines the design and contraction requirements for Naval Aircraft Tie-Down Fittings, Attachment Points, and the associated aircraft carry-through structures.Intended Use: This specification establishes the design and construction of aircraft tie-down fittings, attachment points, and associated aircraft carry-through structure.
URI: https://yse.yabesh.ir/std/handle/yse/36465
Subject: Aircraft Securing
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    MIL-T-81259B

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contributor authorNAVY - AS - Naval Air Systems Command
date accessioned2017-09-04T15:34:39Z
date available2017-09-04T15:34:39Z
date copyright33522
date issued1991
identifier otherONGWDAAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/36465
description abstractThis specification defines the design and contraction requirements for Naval Aircraft Tie-Down Fittings, Attachment Points, and the associated aircraft carry-through structures.Intended Use: This specification establishes the design and construction of aircraft tie-down fittings, attachment points, and associated aircraft carry-through structure.
languageEnglish
titleMIL-T-81259Bnum
titleTIE-DOWNS, AIRFRAME DESIGN, REQUIREMENTS FORen
typestandard
page16
statusActive
treeNAVY - AS - Naval Air Systems Command:;1991
contenttypefulltext
subject keywordsAircraft Securing
subject keywordsCarrier Flight Deck
subject keywordsAircraft
subject keywordsCarrier Flight Deck
subject keywordsCarrier Flight Deck
subject keywordsAircraft Mooring
subject keywordsChains
subject keywordsAircraft Mooring
subject keywordsSecuring Aircraft
subject keywordsCarrier Flight Deck
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