ISO 8913:2006
Current
Current
The latest, up-to-date edition.
Aerospace Lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 400 degrees F/3 000 psi (204 degrees C/20 684 kPa) and 204 degrees C/21 000 kPa (400 degrees F/3 046 psi) Procurement specification
Available format(s)
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
Language(s)
English
Published date
30-10-2006
Important note : All end users must be registered with an Account prior to user licenses being assigned.
ISO 8913:2006 specifies requirements for lightweight polytetrafluoroethylene (PTFE) hose assemblies for use in aircraft hydraulic systems at temperatures between - 55 C and 204 C (- 65 F and 400 F), and at a nominal pressure up to 3 000 psi (20 684 kPa) or 21 000 kPa (3 046 psi). The hose assemblies are also suitable for use within the same temperature and pressure limitations in aircraft pneumatic systems where some gaseous diffusion through the wall on the PTFE liner may be tolerated.
The use of these hose assemblies in high-pressure pneumatic storage systems is not recommended. In addition, installations in which the limits specified in ISO 8913:2006 are exceeded, or in which the application is not covered specifically by ISO 8913:2006, for example for oxygen, are subject to the approval of the purchaser.
A listing of hose assembly procurement standards conforming to ISO 8913:2006 is given.
| DevelopmentNote |
Supersedes ISO/DIS 8913. (10/2006)
|
| DocumentType |
Standard
|
| Pages |
27
|
| PublisherName |
International Organization for Standardization
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| BS ISO 8913:2006 | Identical |
| SAE AIR 2000 : 2000 | AEROSPACE FLUID SYSTEM STANDARDS, METRIC, NATIONAL AND INTERNATIONAL |
| PREN 3584 : 200P2 | AEROSPACE SERIES - LIGHTWEIGHT PTFE FLEXIBLE HOSE ASSEMBLY OF A NOMINAL PRESSURE EQUAL TO 21000 KPA WITH 8 DEGREE 30 MINUTES FITTING IN TITANIUM - PRODUCT STANDARD |
| SAE AMS 5689 : 2012 | STEEL, CORROSION AND HEAT RESISTANT, WIRE 18CR - 10.5NI - 0.40TI (321) SOLUTION HEAT TREATED |
| EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
| SAE AMS5659S : 2016 | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu<br> |
| SAE AMS 5645 : 2016 | STEEL, CORROSION AND HEAT RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS, 18CR - 10NI - 0.40TI (321), SOLUTION HEAT TREATED |
| SAE AS 1912 : 2015 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, CRES REINFORCED, 400 DEGREES F, 3000 PSI, LIGHTWEIGHT, BEAM SEAL, 45 DEGREES TO 45 DEGREES |
| SAE AS 1914 : 2015 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, CRES REINFORCED, 400 DEGREES F, 3000 PSI, LIGHTWEIGHT, BEAM SEAL, 90 DEGREES TO 90 DEGREES |
| SAE AS 120 : 2012 | HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 DEGREES F, 90 DEGREES TO 90 DEGREES, FLARELESS, LIGHTWEIGHT |
| BS 2TA 12:1974 | Specification for forging stock of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm) |
| ASTM A 262 : 2015 : REDLINE | Standard Practices for Detecting Susceptibility to Intergranular Attack in Austenitic Stainless Steels |
| SAE AS 116 : 2012 | HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 DEGREES F, STRAIGHT TO 45 DEGREES, FLARELESS, LIGHTWEIGHT |
| 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 |
| SAE AS 1910 : 2015 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, CRES REINFORCED, 400 DEGREES F, 3000 PSI, LIGHTWEIGHT, BEAM SEAL, STRAIGHT TO 45 DEGREES |
| 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 |
| SAE AMS 5581 : 2010 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SEAMLESS OR WELDED TUBING, 62NI - 21.5CR - 9.0MO - 3.7CB (NB), ANNEALED |
| PREN 3120 : 200P3 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64003 - COLD WORKED AND STRESS RELIEVED - SEAMLESS TUBE FOR PRESSURE SYSTEMS - 4 MM <= D <= 51 MM - 690 MPA <= R[M] <= 1030 MPA |
| SAE AS 117 : 2012 | HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 DEGREES F, STRAIGHT TO 90 DEGREES, FLARELESS, LIGHTWEIGHT |
| ISO 2685:1998 | Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
| SAE AMS 5667 : 2015 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 72NI - 15.5CR - 0.95CB - 2.5TI - 0.70AL - 7.0FE EQUALIZED, PRECIPITATION HARDENABLE |
| 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 5743 : 2014 | STEEL, CORROSION AND HEAT-RESISTANT, BARS AND FORGINGS 15.5CR - 4.5NI - 2.9MO - 0.10N SOLUTION HEAT TREATED, SUB-ZERO COOLED, EQUALIZED, AND OVER-TEMPERED |
| SAE AMS 5697 : 2012 | STEEL, CORROSION-RESISTANT, WIRE, 19CR - 9.5NI (304), SOLUTION HEAT TREATED |
| SAE AMS 5690 : 2015 | STEEL, CORROSION AND HEAT RESISTANT, WIRE, 17CR - 12NI - 2.5MO (316), SOLUTION HEAT TREATED |
| 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 |
| PREN 3314 : 200P2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P64001 - SOLUTION TREATED AND AGED - BAR FOR MACHINING - D <= 75 MM |
| SAE AS 1055 : 2013 | FIRE TESTING OF FLEXIBLE HOSE, TUBE ASSEMBLIES, COILS, FITTINGS AND SIMILAR SYSTEM COMPONENTS |
| SAE AS 156 : 2017 | HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 DEGREES F, 45 DEGREES TO 45 DEGREES, FLARED, LIGHTWEIGHT |
| SAE AMS 5647 : 2017 | STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 19CR - 9.5NI, SOLUTION HEAT TREATED |
| ISO 8829:1990 | Aerospace Polytetrafluoroethylene (PTFE) hose assemblies Test methods |
| 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 AS 119 : 2012 | HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 DEGREES F, 45 DEGREES TO 90 DEGREES, FLARELESS, LIGHTWEIGHT |
| SAE AS 7003 : 2008 | NADCAP PROGRAM REQUIREMENTS |
| SAE AS 7112 : 1997 | NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM REQUIREMENTS FOR FLUID SYSTEM COMPONENTS |
| SAE AMS 5567 : 2015 | STEEL, CORROSION RESISTANT, SEAMLESS OR WELDED HYDRAULIC TUBING, 19CR - 10NI (304), SOLUTION HEAT TREATED |
| BS 2TA 13:1974 | Specification for forgings of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm) |
| SAE AS 115 : 2012 | HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 DEGREES F, STRAIGHT TO STRAIGHT, FLARELESS, LIGHTWEIGHT |
| BS 2TA 11:1974 | Specification for bar and section for machining of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm) |
| BS 2S 130:1976 | Specification for 18/9 chromium-nickel corrosion-resisting steel (niobium stabilized) billets, bars, forgings and parts (540 MPa: limiting ruling section 150 mm) |
| SAE AMS 5646 : 2014 | 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 |
| SAE AMS 5688 : 2012 | STEEL, CORROSION-RESISTANT, WIRE, 18CR - 9.0NI (SAE 30302), SPRING TEMPER |
| AIR 9182 : 1958 | |
| SAE AMS 4945 : 2014 | 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 |
| SAE AS 1909 : 2015 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, CRES REINFORCED, 400 DEGREES F, 3000 PSI, LIGHTWEIGH T, BEAM SEAL, STRAIGHT TO STRAIGHT |
| 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 | |
| SAE AMS 5639 : 2017 | STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, MECHANICAL TUBING, AND RINGS, 19CR - 10NI, SOLUTION HEAT TREATED |
| PREN 2530 : 2 | AEROSPACE SERIES - TITANIUM ALLOY TI-P63 - ANNEALED - 900 MPA <= R[M] <= 1160 MPA - BARS D[E] <= 150 MM |
| SAE AS 1911 : 2015 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, CRES REINFORCED, 400 DEGREES F, 3000 PSI, LIGHTWEIGHT, BEAM SEAL, STRAIGHT TO 90 DEGREES |
| SAE AS 150 : 2014 | 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:1964(S2017) | STEEL, BARS AND FORGINGS, CORROSION RESISTANT, 17CR - 7NI - 1AL |
| SAE AS 118 : 2012 | HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 DEGREES F, 45 DEGREES TO 45 DEGREES, FLARELESS, LIGHTWEIGHT |
| SAE AMS 5666H : 2016 | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, EXTRUSIONS, AND RINGS, 62NI - 21.5CR - 9.0MO - 3.65CB (NB), ANNEALED |
| SAE AS 1913 : 2015 | HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, CRES REINFORCED, 400 DEGREES F, 3000 PSI, LIGHTWEIGHT, BEAM SEAL, 45 DEGREES TO 90 DEGREES |
| ISO 8829-2:2006 | Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 2: Non-metallic braid |
| SAE AMS 5556 : 2016 | STEEL, CORROSION AND HEAT-RESISTANT, SEAMLESS OR WELDED HYDRAULIC TUBING 18CR - 11NI - 0.70CB (347) SOLUTION HEAT TREATED |
| ISO 3161:1999 | Aerospace — UNJ threads — General requirements and limit dimensions |
| SAE AMS 4928 : 2016 | 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) |
| PREN 3584 : 200P2 | AEROSPACE SERIES - LIGHTWEIGHT PTFE FLEXIBLE HOSE ASSEMBLY OF A NOMINAL PRESSURE EQUAL TO 21000 KPA WITH 8 DEGREE 30 MINUTES FITTING IN TITANIUM - PRODUCT STANDARD |
| SAE AMS 5557 : 2012 | STEEL, CORROSION AND HEAT RESISTANT, SEAMLESS OR WELDED HYDRAULIC TUBING, 18.5CR - 10.5NI - 0.40TI (SAE 30321), SOLUTION HEAT TREATED |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.