SAE AS1188A
Current
The latest, up-to-date edition.
Aircraft Tire Inflation-Deflation Equipment
Hardcopy , PDF
English
11-07-2014
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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.
| DocumentType |
Standard
|
| Pages |
6
|
| ProductNote |
This version is now stabilized.
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
This specification covers minimum design and test requirements for aircraft tire inflation-deflation equipment for use on all types of aircraft. It shall be the responsibility of the airframe manufacturer to determine the compatibility of the requirement with the applicable aircraft and to specify requirements in excess of these minimums as necessary.
| SAE ARP5632 | 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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