Standard

SAE ARP1311B

Jun 2004 Withdrawn

Corrigendums and amendments are bought separately.

Language English

Services Read online + Print/Download €156.00 Read online €104.00

There are no extended editions available for this standard

There are no available corrigendum or amendments for this standard. Any future corrigendum and amendments will be added automatically for subscribers.

Abstract

This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes) for all types and models of civil and military aircraft including all aircraft with vertical landing and crash attenuation requirements. All axles, wheel forks, axle beams, links, arms, mechanical and nitrogen/oil energy absorbers, lock assemblies, braces, trunnion beams, and truck beams etc., that sustain loads originating at the ground, and that are not integral parts of the airframe structure, should be designed in accordance with this document. Hydraulic actuators (retraction, main and nose gear steering, positioning, and/or damping) should also be included in this coverage.

Document information

Standard from SAE International
Published: 24 June 2004
Withdrawn: 10 August 2011
Document type: IS
Pages
ISBN:

Publisher SAE International
Distributor SAE International

Product Relations

Replaced by: SAE ARP1311
Refers: SAE ARP4912
Replaces: SAE ARP1311A

SAE ARP1311B

Create subscription

Benefits of a subscription:

SAE ARP1311B

SAE ARP1311A

Abstract

Document information

Product Relations

Create subscription

Benefits of a subscription:

Extended editions Extended editions (0)

Version history Related corrigendum and amendments (0)

Version history History (2)

SAE ARP1311B

SAE ARP1311A

Abstract

Document information

Product Relations