SAE AIR 5005 : 2015
Current
Current
The latest, up-to-date edition.
AEROSPACE - COMMERCIAL AIRCRAFT HYDRAULIC SYSTEMS
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
09-21-2015
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.
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 ARP 994 : 2016 | 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 ARP 4752 : 2013 | 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 AMS 5561 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, WELDED AND DRAWN OR SEAMLESS AND DRAWN TUBING, 9.0MN - 20CR - 6.5NI - 0.28N, HIGH-PRESSURE HYDRAULIC |
| SAE AMS WW T 700/4 : 2012 | TUBE, ALUMINUM ALLOY, DRAWN, SEAMLESS, 5052 |
| SAE AMS WW T 700/6C : 2001(S2015) | TUBE, ALUMINUM ALLOY, DRAWN, SEAMLESS, 6061 |
| SAE AMS 5566 : 2011 | 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 AMS 4071 : 2017 | ALUMINUM ALLOY, DRAWN, ROUND, SEAMLESS HYDRAULIC TUBING, 2.5MG - 0.25CR (5052-O), ANNEALED |
| SAE AMS 4945 : 2014 | TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3AL - 2.5V, CONTROLLED CONTRACTILE STRAIN RATIO COLD WORKED, STRESS RELIEVED |
| SAE AS 1241 : 2016 | 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 AS 1290 : 2011 | GRAPHIC SYMBOLS FOR AIRCRAFT HYDRAULIC AND PNEUMATIC SYSTEMS |
| SAE ARP 4386 : 2010 | TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION AND CONTROL TECHNOLOGIES |
| SAE AMS 4083 : 2012 | ALUMINUM ALLOY TUBING, HYDRAULIC, SEAMLESS, DRAWN, ROUND, 1.0MG - 0.60SI - 0.28CU - 0.20CR (6061-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS 4944 : 2015 | 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 AMS 4928 : 2016 | 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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