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SAE ARP1311D

Current

Current

The latest, up-to-date edition.

Landing Gear Structures and Mechanisms

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

16-11-2023

€141.06
Excluding VAT

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.

DocumentType
Standard
Pages
31
PublisherName
SAE International
Status
Current
Supersedes

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.

SAE AS4832B Gland Design: Nominal 3/8 Inch Cross Section for Compression-Type Seals
SAE ARP4915B Disposition of Landing Gear Components Involved in Accidents/Incidents
SAE AMSQQN290D Nickel Plating (Electrodeposited)
SAE AS6053A Tests, Impact, Shock Absorber Landing Gear, Aircraft
SAE AS4716D Gland Design, O-Ring and Other Seals
SAE AMSP83461 Packing, Preformed, Petroleum Hydraulic Fluid Resistant, Improved Performance at 275°F (135°C)
SAE AS4052C Gland Design: Scraper, Landing Gear, Installation
SAE ARP5935 Use of HVOF Thermal Spray Coatings for Hard Chrome Replacement in Landing Gear Applications
SAE AS1241D Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft
SAE ARP5429 Landing Gear Fatigue Tests with Equivalent Damage Spectra
SAE AS8860 Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications
SAE AMSQQC320B Chromium Plating (Electrodeposited)
SAE ARP1595B Design and Verification of Aircraft Nose Wheel Steering Systems
SAE ARP4912C Design Recommendations for Spare Seals in Landing Gear Shock Struts
SAE ARP5936 Landing Gear Storage

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