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SAE International - AIR5883

Landing Gear Shock Struts Bearing Selection

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Organization: SAE International
Publication Date: 3 May 2012
Status: active
description:

This document defines the criteria used for the selection of landing gear shock strut upper and lower bearings.

Document History

AIR5883
May 3, 2012
Landing Gear Shock Struts Bearing Selection
This document defines the criteria used for the selection of landing gear shock strut upper and lower bearings.

References

This document references:
AIR1494 - VERIFICATION OF LANDING GEAR DESIGN STRENGTH
Published by SAE International on February 1, 1978
A description is not available for this item.
This document references:
AIR1594 - PLAIN BEARING SELECTION FOR LANDING GEAR APPLICATIONS
Published by SAE International on March 1, 1993
This document is intended to give advisory information for the selection of plain bearings and bearing materials most suitable for aircraft landing gear applications. Information is given on bearing...
This document references:
ARP1311 - LANDING GEAR - AIRCRAFT
Published by SAE International on August 10, 2011
This ARP applies to all types and models of civil aircraft for landing gear structure and mechanism excepting wheels, tires and brakes. All axles, wheel forks, axle beams, links, arms, mechanical and...
This document references:
ARP4912 - DESIGN RECOMMENDATIONS FOR SPARE SEALS IN LANDING GEAR SHOCK STRUTS
Published by SAE International on December 1, 1996
A description is not available for this item.
This document references:
ARP5429 - Landing Gear Fatigue Tests with Equivalent Damage Spectra
Published by SAE International on June 29, 2012
This SAE Aerospace Recommended Practice (ARP) applies to fatigue testing of landing gear and landing gear components.
This document references:
AS81820 - Bearings, Plain, Self-Aligning, Self-Lubricating, Low Speed Oscillation, General Specification For
Published by SAE International on March 1, 1998
This specification covers plain spherical bearings which are self-aligning and self-lubricating by incorporating polytetrafluoroethylene (PTFE) in a liner between the ball and race (outer ring). PTFE...
This document references:
AS81820/1 - BEARING, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, LINED BORE, LOW SPEED, NARROW, GROOVED OUTER RING, -65° TO 325° F
Published by SAE International on April 1, 1998
A description is not available for this item.
This document references:
AS81934 - Bearings, Sleeve, Plain and Flanged, Self-Lubricating, General Specification For
Published by SAE International on April 1, 1998
This specification covers plain and flanged sleeve bearings which are self-lubricating by incorporating polytetrafluoroethylene (PTFE) in a liner in the bore for use in a temperature range of -65° to...
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