BS ISO 23933:2006
Current
The latest, up-to-date edition.
Aerospace series. Aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies, classification 135°C/20 684 kPa (275°F/3 000 psi) and 135°C/21 000 kPa (275°F/3 046 psi). Procurement specification
Hardcopy , PDF
English
03-16-2006
Foreword
1 Scope
2 Normative references
3 Classification
4 Requirements
4.1 Limits of application
4.2 Qualification
4.3 Materials
4.4 Construction
4.5 Inner tube requirements
4.6 Hose assembly
4.7 Fitting threads
4.8 Part numbering of interchangeable parts
4.9 Identification of products
4.10 Workmanship
4.11 Hose assembly - Test and performance requirements
5 Quality assurance
5.1 Responsibility for inspection
5.2 Classification of inspections
5.3 Qualification inspections
5.4 Quality conformance inspections
5.5 Test conditions
5.6 Inspection methods
6 Preparation for delivery
6.1 Storage and packaging
6.2 Marking
7 Ordering data
Annex A (informative) Equivalent materials
Annex B (informative) Qualification procedures and fire
resistance specifications
Bibliography
Provides requirements for aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies for use in aircraft hydraulic, oil and fuel systems at temperatures between -55 degree C and 135 degree C (-65 degree F and 275 degree F) and at a nominal pressure of 21000 kPa (210 bar) (3046 psi) or 20684 kPa (3000 psi).
Committee |
ACE/69
|
DevelopmentNote |
Supersedes 05/30128217 DC. (03/2006) Reviewed and confirmed by BSI, January 2015. (12/2014)
|
DocumentType |
Standard
|
Pages |
30
|
PublisherName |
British Standards Institution
|
Status |
Current
|
Supersedes |
This International Standard specifies requirements for aramid reinforced lightweight polytetrafluoroethylene (PTFE) hose assemblies for use in aircraft hydraulic, oil and fuel systems at temperatures between−55°C and 135°C (−65 °F and 275 °F) and at a nominal pressure of 21000kPa (210 bar) (3046 psi) or 20684kPa (3000 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 of the PTFE liner may be tolerated.
Standards | Relationship |
ISO 23933:2006 | Identical |
EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
SAE AMS 5645 : 2016 | 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) |
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 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 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 |
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 7003 : 2008 | NADCAP PROGRAM REQUIREMENTS |
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 |
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 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 |
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 AS 1241 : 2016 | FIRE RESISTANT PHOSPHATE ESTER HYDRAULIC FLUID FOR AIRCRAFT |
SAE AMS 5639 : 2017 | 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 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 |
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 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) |
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.