05/30128217 DC : DRAFT JAN 2005
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
ISO/DIS 23933 - AEROSPACE - ARAMID REINFORCED LIGHTWEIGHT POLYTETRAFLUOROETHYLENE (PTFE) HOSE ASSEMBLIES, CLASSIFICATION 135 DEGREE C/20 684 KPA (275 DEGREE F/3 000 PSI) AND 135 DEGREE C/21 000 KPA (275 DEGREE F/3 046 PSI) - PROCUREMENT SPECIFICATION
Superseded date
16-03-2006
Superseded by
Published date
23-11-2012
Publisher
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| Committee |
ACE/69
|
| DocumentType |
Draft
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy |
| EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
| SAE AMS5645S | Steel, Corrosion and Heat Resistant, Bars, Wire, Forgings, Tubing, and Rings 18Cr - 10Ni - 0.40Ti (321) Solution Heat Treated |
| BS 2S 145:1976 | Specification for chromium-nickel-copper-molybdenum corrosion-resisting steel (precipitation hardening) billets, bars, forgings and parts (1270-1470 MPa) |
| PREN 3161 : 200P1 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 200 MM - R[M] >= 930 MPA |
| ASTM B 348 : 2013 : REDLINE | Standard Specification for Titanium and Titanium Alloy Bars and Billets |
| PREN 2539 : 200P2 | AEROSPACE SERIES - STEEL FE-PM 3801 (X5CRNICU17-4) - AIR MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - BAR - A OR D <= 200 MM - R[M] >= 965 MPA |
| MIL-T-8808 Revision B:1981 | TUBING, STEEL, CORROSION RESISTANT (18.8 STABILIZED) AIRCRAFT HYDRAULIC QUALITY |
| ISO 2685:1998 | Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
| SAE AMS5643U | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 16Cr - 4.0Ni - 0.30Cb (Nb) - 4.0Cu Solution Heat Treated, Precipitation Hardenable |
| SAE AS7112/2 | NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM REQUIREMENTS FOR FITTINGS AND OTHER MACHINED COMPONENTS |
| SAE AS1055D | Fire Testing of Flexible Hose, Tube Assemblies, Coils, Fittings, and Similar System Components |
| AIR 9160 : 1992 | CONDITIONS GENERALES DE RECETTE ET D'EMPLOI DES ACIERS CORROYES UTILISES DANS LES CONSTRUCTIONS AERONAUTIQUES |
| ISO 6772:2012 | Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies |
| SAE AS7003D | Nadcap Program Requirements |
| SAE AMS5646P | Steel, Corrosion and Heat-Resistant, Bars, Wire, Forgings, Tubing, and Rings 18Cr - 11Ni - 0.60Cb(Nb) (347) Solution Heat Treated |
| ISO 5855-3:1999 | Aerospace MJ threads Part 3: Limit dimensions for fittings for fluid systems |
| ISO 7258:1984 | Polytetrafluoroethylene (PTFE) tubing for aerospace applications Methods for the determination of the density and relative density |
| PREN 3487 : 200P2 | AEROSPACE SERIES - STEEL FE-PA3601 (X6CRNITI18-10) - AIR MELTED - SOFTENED - BAR FOR MACHINING - A OR D <= 250 MM - 500 MPA <= R[M] <= 700 MPA |
| SAE AMS4945F | Titanium Alloy Tubing, Seamless, Hydraulic 3Al - 2.5V, Controlled Contractile Strain Ratio Cold Worked, Stress Relieved |
| PREN 3162 : 200P1 | AEROSPACE SERIES - STEEL FE-PM3801 (X5CRNICU17-4) - AIR MELTED - SOLUTION TREATED AND PRECIPITATION TREATED - SHEET AND STRIP - A <= 6 MM - R[M] >= 930 MPA |
| BS 2S 129:1976 | Specification for 18/9 chromium-nickel corrosion-resisting steel (titanium stabilized) billets, bars, forgings and parts (540 MPa: limiting ruling section 150 mm) |
| AIR 9423 : 1992 | |
| ISO 9001:2015 | Quality management systems — Requirements |
| SAE AS1241D | Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft |
| SAE AMS5639J | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings 19Cr - 10Ni Solution Heat Treated |
| PREN 9133 : 200P1 | AEROSPACE SERIES - QUALITY MANAGEMENT SYSTEMS - QUALIFICATION PROCEDURE FOR AEROSPACE STANDARD PRODUCTS |
| SAE AS150E | Hose Assembly, Type Classifications of, Basic Performance and Fire Resistance |
| PREN 3311 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - ANNEALED - BAR FOR MACHINING - D <= 150 MM |
| SAE AMS5644E | Steel, Bars and Forgings, Corrosion Resistant 17Cr - 7Ni - 1Al |
| PREN 3468 : 200P1 | AEROSPACE SERIES - STEEL FE-PA13 - SOFTENED - 500 < R[M] <= 700 MPA - FORGINGS - D[E] <= 100 MM |
| ISO 8829-2:2006 | Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 2: Non-metallic braid |
| ISO 3161:1999 | Aerospace — UNJ threads — General requirements and limit dimensions |
| SAE AMS4928V | Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes 6Al - 4V Annealed |
| 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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