SAE AS 1933 : 2013
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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AGE CONTROLS FOR HOSE CONTAINING AGE-SENSITIVE ELASTOMERIC MATERIAL
Available format(s)
Hardcopy , PDF
Superseded date
25-09-2024
Superseded by
Language(s)
English
Published date
02-01-2013
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1 SCOPE
2 REFERENCE DOCUMENTS
3 REQUIREMENTS
4 STORAGE
5 NOTES
This document establishes age limit and guidance for acceptance of hose and hose assemblies containing elastomeric materials for use in aircraft, space vehicles, missiles and component assemblies thereof at time of delivery to the contractor, procuring activity, or contracting officer.
| Committee |
G 3
|
| DevelopmentNote |
IN CONJUNCTION WITH SAE-ARP 5316 - THIS DOCUMENT SUPERSEDES MIL-STD-1523 (A)
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| DocumentType |
Standard
|
| Pages |
6
|
| PublisherName |
SAE International
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| AN 6270 : 0010 | HOSE ASSEMBLY - DETACHABLE SWIVEL FITTING, LOW PRESSURE |
| MIL-DTL-83797 Revision C:2008 | HOSE, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-DTL-8790 Revision F:2007 | Hose Assemblies, Rubber, Hydraulic, High Pressure 3,000 PSI, Operating Temperature Range -65 Degrees F to +275 Degrees F, Field Attachable |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-DTL-6000 Revision D:2007 | HOSE, RUBBER, AIRCRAFT, FUEL, OIL, COOLANT, WATER, AND ALCOHOL |
| MIL-PRF-7061 Revision E:2014 | HOSE, ELASTOMERIC, AIRCRAFT, SELF-SEALING, AROMATIC FUEL |
| MIL-PRF-26385 Revision G:2013 | HOSE, OXYGEN AND PRESSURIZATION, OZONE RESISTANT |
| MIL-DTL-83796 Revision B:2008 | HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-PRF-87961 Revision B:2013 | HOSE AND HOSE ASSEMBLIES, AIR DUCT, AIR BREATHING, OXYGEN SYSTEM |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-DTL-8788 Revision G:2015 | Hose, Rubber, Hydraulic, High Pressure 3,000 PSI, Operating Temperature Range -65 Degrees F to +160 Degrees F |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| MIL-DTL-6162 Revision C:2000 | GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-DTL-62478 Revision C:2010 | COUPLER, OPTICAL |
| MIL-STD-1587 Revision D:2017 | MATERIAL AND PROCESS REQUIREMENTS FOR AEROSPACE WEAPONS SYSTEMS |
| MIL-DTL-8795 Revision G:2014 | Hose Assemblies, Elastomeric, Hydraulic, Fuel, Coolant, and Oil Resistant, General Specification for |
| MIL-R-8931 Revision A:1994 | RESERVOIRS, AIRCRAFT AND MISSILE, HYDRAULIC SEPARATED TYPE |
| ZZ-H-617 Revision C:2002 | Hose, Rubber, Windshield Wiper |
| SAE ARP 5316 : 2014 | STORAGE OF ELASTOMER SEALS AND SEAL ASSEMBLIES WHICH INCLUDE AN ELASTOMER ELEMENT PRIOR TO HARDWARE ASSEMBLY |
| MIL-DTL-13444 Revision H:2006 | Hose and Hose Assemblies, Rubber: Fuel and Oil |
| MIL-PRF-62368 Revision C:2009 | Motor, Gearhead, 18-30 Volts, Direct Current |
| SAE AS 6399 : 1999 | HOSE, RUBBER, WIRE-WOUND, SYNTHETIC, ICE ELIMINATING SYSTEM |
| MIL-DTL-8794 Revision F:2007 | HOSE, SYNTHETIC RUBBER - HYDRAULIC FLUID, FUEL, AND OIL RESISTANT |
| MIL-DTL-5593 Revision E:2006 | HOSE, AIRCRAFT, LOW PRESSURE AIR AND VACUUM, FLEXIBLE |
| SAE AS 5316 : 2017 | STORAGE OF ELASTOMER SEALS AND SEAL ASSEMBLIES WHICH INCLUDE AN ELASTOMER ELEMENT PRIOR TO HARDWARE ASSEMBLY |
| SAE AIR 5386 : 2013 | HOSE AND HOSE ASSEMBLY SELECTION, INSTALLATION, INSPECTION AND MAINTENANCE GUIDELINES, LISTING OF |
| MIL-HDBK-695 Revision F:2017 | RUBBER PRODUCTS: RECOMMENDED SHELF LIFE |
| MIL-DTL-27516 Revision G:2011 | Hose and Hose Assembly, Nonmetallic, Suction and Discharge |
| N285.0-17/N285.6 SERIES-17 | General requirements for pressure-retaining systems and components in CANDU nuclear power plants / Material Standards for reactor components for CANDU nuclear power plants |
| MIL-DTL-26894 Revision D:1998 | Hose and Hose Assembly, Rubber, Gasoline, Refueling, Low Temperature |
| MIL-DTL-5498 Revision G:2013 | ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
| MIL-PRF-62365 Revision C:1997 | MOTOR, HYDRAULIC, CONSTANT DISPLACEMENT |
| MIL-DTL-6615 Revision G:2008 | Hose Assemblies, Rubber, Fuel and Nonpotable Water, with Reattachable Couplings, Low Temperature, General Specification for |
| MIL-DTL-28693 Revision B:2016 | Hose, Rubber, Oil and Gasoline Discharge, Smooth Bore, Lightweight Buoyant Type, Longitudinally Reinforced, 6 Inch |
| MIL-DTL-29210 Revision E:2009 | HOSE ASSEMBLY, RUBBER, METAL LINED, WIRE REINFORCED, 250 PSIG, SATURATED STEAM SERVICE |
| SAE AIR 797 : 2013 | HOSE CHARACTERISTICS AND SELECTION CHART |
| MIL-DTL-5508 Revision C:2007 | FUSES, AIRCRAFT AUTOMATIC QUANTITY-MEASURING, HYDRAULIC |
| MIL PRF 62478 : A | COUPLER, OPTICAL |
| SAE AIR 1364 : 1995 | AGE CONTROL OF AGE SENSITIVE ELASTOMERIC MATERIALS |
| MIL-DTL-13719 Revision G:2012 | HOSE AND HOSE ASSEMBLY, RUBBER, HYDRAULIC BRAKE, TYPE 1 AND TYPE 2 |
| MIL-DTL-26521 Revision L:2014 | Hose Assembly, Nonmetallic, Fuel, Collapsible, Low Temperature with Non-Reusable Couplings |
| CSA N285.2 : 0 | REQUIREMENTS FOR CLASS 1C, 2C AND 3C PRESSURE-RETAINING COMPONENTS AND SUPPORTS IN CANDU NUCLEAR POWER PLANTS |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-HDBK-695 Revision F:2017 | RUBBER PRODUCTS: RECOMMENDED SHELF LIFE |
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