SAE AIR 1899 : 2001

Superseded

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AEROSPACE MILITARY AIRCRAFT HYDRAULIC SYSTEM CHARACTERISTICS

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Superseded date: 05-03-2023

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Published date: 03-01-2001

Publisher: SAE International

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Table of Contents - (Show below) - (Hide below)

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 - (Show below) - (Hide below)

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.

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Committee	A-6A2
Document Type	Revision
ISBN
Pages
Published
Publisher	SAE International
Status	Superseded
Superseded By	SAE AIR1899A:2001(R2023)

Standards Referenced By This Book - (Show below) - (Hide below)

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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