SAE ARP 1786C : 2013

Superseded

View Superseded by

WHEEL ROLL ON RIM CRITERIA FOR AIRCRAFT APPLICATIONS

Available format(s)

Hardcopy , PDF

Superseded date

08-07-2020

Language(s)

English

Published date

01-01-2013

Publisher

SAE International

1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 TEST
5 SERVICE ROLL ON RIM
6 NOTES

Specifies a recommended minimum laboratory roll performance for main landing gear aircraft wheels without tires installed and applies to both bolted and lock-ring wheel designs for FAA Part 25 and military aircraft main wheels (not required for any nose wheels or main wheels on FAA Part 23, 27 or 29 applications).

Committee	A-5A
DocumentType	Revision
Pages	3
PublisherName	SAE International
Status	Superseded
SupersededBy	SAE ARP 1786C : 2013(R2019)

SAE ARP5381:2000(S2012)	MINIMUM PERFORMANCE RECOMMENDATIONS FOR PART 23, 27 AND 29 AIRCRAFT WHEELS, BRAKES, AND WHEEL AND BRAKE ASSEMBLIES
SAE ARP 1493 : 2013	WHEEL AND BRAKE DESIGN AND TEST REQUIREMENTS FOR MILITARY AIRCRAFT