SAE AS 85421 : 2015
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, BEAM SEAL, 3000/4000 PSI, GENERAL SPECIFICATION FOR
Available format(s)
Hardcopy , PDF
Superseded date
04-09-2018
Superseded by
Language(s)
English
Published date
01-01-2015
Publisher
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1. SCOPE
2. REFERENCES
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Specifies the design requirements and test procedures for separable beam seal fittings which includes end fittings, fitting bodies, and boss fittings for use in aerospace fluid systems.
| Committee |
G-3
|
| DevelopmentNote |
Supersedes MIL F 85421 (B) (05/2000)
|
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| SAE AS 604 : 2012 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, HEAVYWEIGHT, HYDRAULIC |
| SAE AS 614 : 2017 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 4000 PSI, 400 DEGREES F, HEAVY DUTY, HYDRAULIC AND PNEUMATIC |
| SAE ARP 994 : 2016 | DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS |
| SAE AS 1975 : 2016 | Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems |
| SAE AS 5620 : 2017 | TITANIUM HYDRAULIC TUBING, TI-3AL-2.5V COLD WORKED AND STRESS RELIEVED, UP TO 35000 KPA (5080 PSI), REQUIREMENTS FOR QUALIFICATION TESTING AND CONTROL |
| SAE AS 1339 : 2017 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, LIGHTWEIGHT, HYDRAULIC AND PNEUMATIC |
| SAE AS 4623 : 2016 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA-ARAMID REINFORCED, 3,000 PSI, 275 DEGREES F, HEAVY DUTY, AIRCRAFT HYDRAULIC SYSTEMS |
| SAE AS 1424 : 2014 | HOSE ASSEMBLIES, METAL, MEDIUM PRESSURE, HIGH TEMPERATURE |
| SAE AS 1946 : 2015 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, UP TO 1500 PSI AND 450 DEGREES F, HYDRAULIC AND PNEUMATIC |
| SAE AMS5659S : 2016 | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu<br> |
| MIL-HDBK-505 Base Document:1998 | Definitions of Item Levels, Item Exchangeability, Models, and Related Terms |
| SAE ARP 603 : 1985 | IMPULSE TESTING OF HYDRAULIC HOSE, TUBING, AND FITTING ASSEMBLIES |
| SAE AS 1576 : 2016 | FITTINGS, WELDED, HYDRAULIC, TITANIUM, CORROSION RESISTANT STEEL AND NICKEL, 3000 PSI HYDRAULIC |
| SAE AMS 4459 : 2013 | ALUMINUM ALLOY, EXTRUSION, 2.7CU - 1.8LI - 0.7ZN - 0.3MN - 0.3MG - 0.08ZR (2099-T81), SOLUTION HEAT TREATED, STRESS RELIEVED BY STRETCHING 1 TO 3% AND AGED |
| MIL-STD-2073-1 Revision E:2008 | STANDARD PRACTICE FOR MILITARY PACKAGING |
| MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
| SAE AIR 1377B : 1980 | FIRE TEST EQUIPMENT FOR FLEXIBLE HOSE AND TUBE ASSEMBLIES |
| SAE AMS 5656F : 2015 | STEEL, CORROSION RESISTANT, BARS, WIRE, FORGINGS, EXTRUSIONS, AND RINGS, 9.0MN - 20CR - 6.5NI - 0.27N, SOLUTION HEAT TREATED |
| SAE AMS 5643 : 2016 | STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 16CR - 4.0NI - 0.30CB (NB) - 4.0CU, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE |
| 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 AS 7112/2 : 1997 | NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM REQUIREMENTS FOR FITTINGS AND OTHER MACHINED COMPONENTS |
| SAE AS 1055 : 2013 | FIRE TESTING OF FLEXIBLE HOSE, TUBE ASSEMBLIES, COILS, FITTINGS AND SIMILAR SYSTEM COMPONENTS |
| SAE ARP 1185 : 2013 | FLEXURE TESTING OF HYDRAULIC TUBING JOINTS AND FITTINGS |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| SAE AS 5440 : 2011 | HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MIL-STD-1916 Base Document:1996 | DOD PREFERRED METHODS FOR ACCEPTANCE OF PRODUCT |
| SAE AS 9100D : 2016 | QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE ORGANIZATIONS |
| SAE AMS 4965 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL 4.0V, SOLUTION HEAT TREATED AND AGED |
| SAE AS 7112 : 1997 | NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM REQUIREMENTS FOR FLUID SYSTEM COMPONENTS |
| SAE AMS 5637 : 2012 | STEEL, CORROSION RESISTANT, BARS AND WIRE 18CR - 9.0NI (SAE 30302) SOLUTION HEAT TREATED, COLD DRAWN AND STRESS RELIEVED 125 KSI (862 MPA) TENSILE STRENGTH |
| ASTM D 1974 : 1998 | Standard Practice for Methods of Closing, Sealing, and Reinforcing Fiberboard Boxes |
| SAE AS 8879 : 2004 | SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
| SAE AMS 4921 : 2016 | TITANIUM BARS, WIRE, FORGINGS, AND RINGS COMMERCIALLY PURE, 70 KSI (483 MPA) YIELD STRENGTH |
| SAE AMS 4946 : 2016 | TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC, 3AL - 2.5V, TEXTURE CONTROLLED, COLD WORKED, STRESS RELIEVED |
| SAE AS 8775 : 1998 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR |
| ASTM D 6251/D6251M : 2011 : REDLINE | Standard Specification for Wood-Cleated Panelboard Shipping Boxes |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
| MIL L 46010 : D | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING |
| SAE AMS 4928 : 2016 | TITANIUM ALLOY BARS, WIRE, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL - 4V, ANNEALED |
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