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Landing Gear Shock Absorption Testing of Civil Aircraft

ARP5644

Organization:
SAE - SAE International
Year: 2019

Abstract: The intent of this document is to provide recommended practices for conducting shock absorption testing of civil aircraft landing gear equipped with oleo-pneumatic shock absorbers. The primary focus is for Part 25 aircraft, but differences for Part 23, 27, and 29 aircraft are provided where appropriate.
URI: http://yse.yabesh.ir/std;query=autho1826AF679D40527369728F1ED52F014A/handle/yse/274180
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    Landing Gear Shock Absorption Testing of Civil Aircraft

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contributor authorSAE - SAE International
date accessioned2019-08-04T07:52:18Z
date available2019-08-04T07:52:18Z
date copyright4/17/2019 12:00:00 AM
date issued2019
identifier otherARP5644.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho1826AF679D40527369728F1ED52F014A/handle/yse/274180
description abstractThe intent of this document is to provide recommended practices for conducting shock absorption testing of civil aircraft landing gear equipped with oleo-pneumatic shock absorbers. The primary focus is for Part 25 aircraft, but differences for Part 23, 27, and 29 aircraft are provided where appropriate.
languageEnglish
titleLanding Gear Shock Absorption Testing of Civil Aircraften
titleARP5644num
typeStandard
treeSAE - SAE International:;2019
contenttypeFulltext
identifier DOI10.4271/ARP5644
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DSpace software copyright © 2017-2020  DuraSpace
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