AIRCRAFT TIRE INFLATION-DEFLATION EQUIPMENT

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

07-11-2014

Publisher

SAE International

1. PURPOSE
2. SCOPE
3. APPLICABLE DOCUMENTS
4. GENERAL REQUIREMENTS
5. PERFORMANCE REQUIREMENTS
6. DESIGN AND CONSTRUCTION
7. QUALIFICATION TESTS

This specification covers minimum design and test requirements for aircraft tire inflation-deflation equipment for use on all types of aircraft.

Committee	A-5A
DocumentType	Standard
Pages	6
ProductNote	This version is now stabilized.
PublisherName	SAE International
Status	Current
Supersedes	SAE AS 1188 : 1972

SAE ARP 5632 : 2016

ROTORCRAFT: APPLICATION OF EXISTING AIRCRAFT DESIGNED TIRES, WHEELS AND BRAKES

MIL-STD-704 Revision F:2004	AIRCRAFT ELECTRIC POWER CHARACTERISTICS
MIL-STD-130 Revision N:2007	IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
MIL-STD-810 Revision G:2008	ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
MIL-STD-889 Revision C:2016	DISSIMILAR METALS
MIL T 5041 : J	TIRE, PNEUMATIC, AIRCRAFT
MIL STD 839 : LATEST	PARTS WITH ESTABLISHED RELIABILITY LEVELS, SELECTION AND USE OF

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Abstract