SAE AIR 1899 : 2001
SAE AIR 1899 : 2001
AEROSPACE MILITARY AIRCRAFT HYDRAULIC SYSTEM CHARACTERISTICS
SAE International
Table of Contents
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
Abstract
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.
General Product Information
| Document Type | Standard |
| Status | Current |
| Publisher | SAE International |
