SAE AIR 1899 : 2001
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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AEROSPACE MILITARY AIRCRAFT HYDRAULIC SYSTEM CHARACTERISTICS
03-05-2023
01-03-2001
1 SCOPE
1.1 Purpose
1.2 Field of Application
2 APPLICABLE DOCUMENTS
2.1 SAE Publications
2.2 U.S. Government Publications
3 ATTACK AIRPLANES
3.1 Northrop Grumman A-6A
3.2 Northrop Grumman A-7E
3.3 Fairchild A-10A
3.4 Lockheed F-117A
4 FIGHTER AIRPLANES
4.1 Northrop Grumman F-5E
4.2 Northrop Grumman F-14A
4.3 Boeing F-15A
4.4 Lockheed Martin F-16A
4.5 Boeing F/A-18A
4.6 MRCA
5 BOMBERS
5.1 Boeing B-1B
5.2 Northrop Grumman B-2A
6 ANTI-SUB - FIXED WING AIRCRAFT
6.1 Lockheed Martin P-3
6.2 Lockheed Martin S-3A
7 TRANSPORT AIRPLANES
7.1 Lockheed Martin C-5A
7.2 Boeing C-17A Globemaster III
7.3 Lockheed Martin C-130
7.4 Lockheed Martin C-141B
8 HELICOPTERS
8.1 Bell 214
8.2 Sikorsky CH-53E
8.3 Sikorsky S-76
9 BOATS
9.1 M-161 Boat
Provides hydraulic system information to military vehicle system and component designers in order to assist them in future aircraft fluid power system designs. Information may be used to find similar type systems, components and materials which will in turn help solve specific problems and lower costs.
Committee |
A-6A2
|
DocumentType |
Revision
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy |
SAE ARP 4940 : 2014 | APPLICATION GUIDE FOR AEROSPACE HYDRAULIC MOTORS |
SAE ARP 1280 : 2014 | AEROSPACE - APPLICATION GUIDE FOR HYDRAULIC POWER TRANSFER UNITS |
SAE AIR 5696 : 2013 | AEROSPACE FLUID POWER - FAA REGULATORY HISTORY - TRANSPORT AIRPLANE HYDRAULIC SYSTEMS |
SAE AS 5586 : 2005 | GENERAL REQUIREMENTS FOR HYDRAULIC SYSTEM RESERVOIRS |
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