WHEEL AND BRAKE DESIGN AND TEST REQUIREMENTS FOR MILITARY AIRCRAFT

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

11-01-2013

Publisher

SAE International

1 Scope
2 References
3 Requirements
4 Quality assurance provisions
5 Notes

Provides military aircraft wheel and hydraulically actuated brake equipment.

Committee	A-5A
DocumentType	Standard
Pages	32
ProductNote	THIS STANDARD IS NOW STABILIZED
PublisherName	SAE International
Status	Current
Supersedes	SAE ARP 1493 : 2008

SAE ARP 5146 : 2015	ASSESSMENT OF AIRCRAFT WHEEL SEALING SYSTEMS
SAE ARP 813 : 2012(R2019)	MAINTAINABILITY RECOMMENDATIONS FOR AIRCRAFT WHEEL AND HYDRAULICALLY ACTUATED BRAKE DESIGN
MIL-HDBK-516 Revision C:2014	AIRWORTHINESS CERTIFICATION CRITERIA
SAE AIR 5937 : 2012	INFORMATION ON ELECTRIC BRAKES
SAE ARP 1786C : 2013	WHEEL ROLL ON RIM CRITERIA FOR AIRCRAFT APPLICATIONS
SAE AIR 1934 : 2016	USE OF STRUCTURAL CARBON HEAT SINK BRAKES ON AIRCRAFT
SAE AS 707 : 2013	THERMAL SENSITIVE INFLATION PRESSURE RELEASE DEVICES FOR TUBELESS AIRCRAFT WHEELS
MIL-DTL-7700 Revision H:2014	FLIGHT MANUAL, PERFORMANCE DATA APPENDIX, MISSION CREW MANUAL, SUPPLEMENTAL MANUAL, AND ABBREVIATED FLIGHT CREW CHECKLIST
SAE AIR 4012 : 2012	USAF AIRCRAFT WHEELS
SAE ARP 5632 : 2016	ROTORCRAFT: APPLICATION OF EXISTING AIRCRAFT DESIGNED TIRES, WHEELS AND BRAKES