SAE AIR5005A
Current
The latest, up-to-date edition.
AEROSPACE - COMMERCIAL AIRCRAFT HYDRAULIC SYSTEMS
Hardcopy , PDF
English
21-09-2015
1. SCOPE
2. REFERENCES
3. WIDE BODY JET AIRLINERS
4. NARROW BODY JET AIRLINERS
5. TURBOPROP/COMMUTER AIRCRAFT
6. BUSINESS JET AIRCRAFT
7. NOTES
Gives information on hydraulic systems fitted to commercial aircraft.
Committee |
A-6A1
|
DocumentType |
Standard
|
Pages |
243
|
PublisherName |
SAE International
|
Status |
Current
|
Supersedes |
SAE ARP994B | DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS |
SAE AS 5586 : 2005 | GENERAL REQUIREMENTS FOR HYDRAULIC SYSTEM RESERVOIRS |
SAE AIR 5565 : 2017 | HISTORICAL DESIGN INFORMATION OF AIRCRAFT LANDING GEAR AND CONTROL ACTUATION SYSTEMS |
SAE ARP 4940 : 2014 | APPLICATION GUIDE FOR AEROSPACE HYDRAULIC MOTORS |
SAE ARP4752B | AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS |
SBAC AGS 1100 : 0 | PIPE COUPLINGS, TYPICAL JOINTS |
MIL-T-6845 Revision D:1985 | TUBING, STEEL, CORROSION-RESISTANT (304) AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION |
MIL-T-8808 Revision B:1981 | TUBING, STEEL, CORROSION RESISTANT (18.8 STABILIZED) AIRCRAFT HYDRAULIC QUALITY |
MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
SAE AMS5561G | STEEL, CORROSION AND HEAT-RESISTANT, WELDED AND DRAWN OR SEAMLESS AND DRAWN TUBING, 9.0MN - 20CR - 6.5NI - 0.28N, HIGH-PRESSURE HYDRAULIC |
SAE AMSWWT700/4A | TUBE, ALUMINUM ALLOY, DRAWN, SEAMLESS, 5052 |
SAE AMSWWT700/6C | TUBE, ALUMINUM ALLOY, DRAWN, SEAMLESS, 6061 |
SAE AMS5566M | STEEL, CORROSION RESISTANT, SEAMLESS OR WELDED HYDRAULIC TUBING, 19CR - 10NI (304) HIGH PRESSURE, COLD DRAWN |
MIL-PRF-87257 Revision C:2017 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE |
DTD 5016 : LATEST | 35-45 TON CHROMIUM NICKEL CORROSION RESISTING STEEL SOLID DRAWN CIRCULAR TUBES |
SAE AMS4071N | ALUMINUM ALLOY, DRAWN, ROUND, SEAMLESS HYDRAULIC TUBING, 2.5MG - 0.25CR (5052-O), ANNEALED |
SAE AMS4945F | TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3AL - 2.5V, CONTROLLED CONTRACTILE STRAIN RATIO COLD WORKED, STRESS RELIEVED |
SAE AS1241D | FIRE RESISTANT PHOSPHATE ESTER HYDRAULIC FLUID FOR AIRCRAFT |
MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
SAE AS1290B | GRAPHIC SYMBOLS FOR AIRCRAFT HYDRAULIC AND PNEUMATIC SYSTEMS |
SAE ARP4386C | TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES |
SAE AMS4083L | ALUMINUM ALLOY TUBING, HYDRAULIC, SEAMLESS, DRAWN, ROUND, 1.0MG - 0.60SI - 0.28CU - 0.20CR (6061-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
SAE AMS4944L | TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3.0AL - 2.5V COLD WORKED, STRESS RELIEVED |
BS 4L 56:1986 | Specification for tube of aluminium-2¼% magnesium alloy (temper designation-O) (seamless: tested hydraulically) (not exceeding 12 mm wall thickness) |
SAE AMS4928V | TITANIUM ALLOY BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL - 4V, ANNEALED |
DTD 5019 : OCT 68 | ALUMINIUM NICKEL SILICON BRASS TUBES. (SUITABLE FOR PIPE LINES AND HIGH PRESSURE HYDRAULIC SYSTEMS ESPECIALLY WHERE FLARING IS REQUIRED) |
BS T 72-T 73:1977 | Specifications for 18/10 chromium-nickel corrosion-resisting steel tube for hydraulic purposes (niobium/titanium stabilized: 550 MPa) |
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