SAE ARP 1311D:2018-06-03

This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes and other landing gear systems) for all types and models of civil and military aircraft. All axles, wheel forks, links, arms, mechanical and gas/oil shock struts, downlock and uplock 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 and validated in accordance with this document. Hydraulic actuators (retraction, main and nose gear steering, positioning, damping, etc.) should also be included in this coverage. System level, non-structural components such as retraction/extension valves, controllers, secondary structure and mechanisms in the airframe (e.g., manual release mechanisms, slaved doors) as well as equipment that is located in the cockpit are not addressed in this ARP.

Author	SAE
Editor	SAE
Document type	Standard
Format	File
ICS	49.045 : Structure and structure elements
Number of pages	31
Replace	SAE ARP 1311C:2015-04-27
Set	AEROPAKS10U-10
Year	2018
Document history	SAE ARP 1311C:2015-04-27
Country	USA
Keyword	SAE 1311;SAE ARP1311D;SAE ARP1311D;SAE ARP 1311