SAE International Landing Gear Shock Absorption Testing of Civil Aircraft ARP5644A

Description
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.
  • Landing Gear Shock Absorption Testing of Civil Aircraft - ARP5644A - SAE International
    SAE International
Description
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.

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Landing Gear Shock Absorption Testing of Civil Aircraft - ARP5644A - SAE International
SAE International
Warrendale, PA, United States
Landing Gear Shock Absorption Testing of Civil Aircraft
ARP5644A
Landing Gear Shock Absorption Testing of Civil Aircraft ARP5644A
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.

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.

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Technical Specifications

  SAE International
Product Category Standards and Technical Documents
Product Number ARP5644A
Product Name Landing Gear Shock Absorption Testing of Civil Aircraft
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