ISO 7169:2014
Current
Current
The latest, up-to-date edition.
Aerospace Separable tube fittings for fluid systems, for 24 degree cones, for pressures up to 3 000 psi or 21 000 kPa Procurement specification, inch/metric
Available format(s)
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
Language(s)
English
Published date
11-13-2014
ISO 7169:2014 specifies performance and quality requirements for the qualification and manufacture of standard 24 cone fittings and manufacture of 24 cone fittings to ensure reliable performance or equivalent inch-dimensioned fitting ends to ensure reliable performance in aircraft hydraulic systems.
This International Standard specifies baseline criteria for the design and manufacture of system fittings that are qualification-tested on engines.
This International Standard covers fittings of the temperature types and pressure classes specified in ISO 6771.
| DevelopmentNote |
Supersedes 97/703624 DC. (02/2002) Supersedes AIR 8428 (06/2002) Supersedes ISO/DIS 7169. (11/2014)
|
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
International Organization for Standardization
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| BS ISO 7169:2014 | Identical |
| SAE MA 2005 : 2015 | Identical |
| BS 2M 60:1993 | Identical |
| DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
| DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| PREN 4510 : DRAFT 2017 | AEROSPACE SERIES - PIPE COUPLING, 60 DEGREES, SPHERICAL, IN TITANIUM ALLOY TI-P64001, PORT ADAPTER, STRAIGHT, DOUBLE END, WITH LOCKING RING |
| BS ISO 9538:2017 | Aerospace series. Hydraulic tubing joints and fittings. Planar flexure test |
| ISO 9538:2017 | Aerospace series — Hydraulic tubing joints and fittings — Planar flexure test |
| DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT7)SEC2/SUPP6/6(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
| BS M 55:1984 | Method for rotary flexure testing of hydraulic tubing joints and fittings for aerospace use |
| 14/30264731 DC : DRAFT JUNE 2014 | BS ISO 7257 - AIRCRAFT - HYDRAULIC TUBING JOINTS AND FITTINGS - ROTARY FLEXURE TEST |
| 16/30346081 DC : 0 | BS EN 4510 - AEROSPACE SERIES - PIPE COUPLINGS, 60 DEGREE, SPHERICAL IN TITANIUM ALLOY TIP64001 - ADAPTERS, STRAIGHT, DOUBLE END, WITH LOCKING RING |
| SAE AIR 2000 : 2000 | AEROSPACE FLUID SYSTEM STANDARDS, METRIC, NATIONAL AND INTERNATIONAL |
| BS EN 14072:2003 | Glass in furniture. Test methods |
| PREN 4834 : DRAFT 2017 | AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) PORT FOR RING LOCKED FITTING - INCH SERIES - GEOMETRIC CONFIGURATION |
| EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
| SAE AMS 2486 : 2010 | CONVERSION COATING OF TITANIUM ALLOYS FLUORIDE-PHOSPHATE TYPE |
| SAE AMS5659S : 2016 | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu<br> |
| SAE AMS QQ A 225/9 : 2014 | ALUMINUM ALLOY 7075, BAR, ROD, WIRE, AND SPECIAL SHAPES; ROLLED, DRAWN, OR COLD FINISHED |
| SAE AMS QQ P 416 : 2016 | PLATING, CADMIUM (ELECTRODEPOSITED) |
| SAE AMS 2488 : 2000 | ANODIC TREATMENT - TITANIUM AND TITANIUM ALLOYS SOLUTION PH 13 OR HIGHER |
| SAE AMS 2770 : 2015 | HEAT TREATMENT OF WROUGHT ALUMINUM ALLOY PARTS |
| ISO 10583:1993 | Aerospace fluid systems — Test methods for tube/fitting assemblies |
| ISO 6771:2007 | Aerospace Fluid systems and components Pressure and temperature classifications |
| 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 |
| ISO 6772:2012 | Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies |
| SAE AMS QQ A 367 : 2012 | ALUMINUM ALLOY FORGINGS |
| SAE AS 7003 : 2008 | NADCAP PROGRAM REQUIREMENTS |
| SAE AS 7112 : 1997 | NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM REQUIREMENTS FOR FLUID SYSTEM COMPONENTS |
| ISO 5855-3:1999 | Aerospace MJ threads Part 3: Limit dimensions for fittings for fluid systems |
| SAE AMS QQ S 763D : 2013(S2015) | STEEL, CORROSION RESISTANT, BARS, WIRE, SHAPES, AND FORGINGS |
| SAE AMS 4945 : 2014 | TITANIUM ALLOY TUBING, SEAMLESS, HYDRAULIC 3AL - 2.5V, CONTROLLED CONTRACTILE STRAIN RATIO COLD WORKED, STRESS RELIEVED |
| SAE AMS 4130 : 2014 | ALUMINUM ALLOY DIE FORGINGS, 4.4CU - 0.85SI - 0.80MN (2025-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| SAE AMS 5622 : 2013 | STEEL, CORROSION-RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS, 16CR - 4.0NI - 0.30CB - 4.0CU, SOLUTION HEAT TREATED, PRECIPITATION HARDENABLE, CONSUMABLE ELECTRODE REMELTED |
| ISO 7257:2016 | Aircraft Hydraulic tubing joints and fittings Rotary flexure test |
| ISO 9538:2017 | Aerospace series — Hydraulic tubing joints and fittings — Planar flexure test |
| ISO 8574:2004 | Aerospace Hydraulic system tubing Qualification tests for bent tubes |
| SAE AMS 4083 : 2012 | ALUMINUM ALLOY TUBING, HYDRAULIC, SEAMLESS, DRAWN, ROUND, 1.0MG - 0.60SI - 0.28CU - 0.20CR (6061-T6), SOLUTION AND PRECIPITATION HEAT TREATED |
| SAE AMS QQ A 225/6 : 1998 | ALUMINUM ALLOY, 2024, BAR, ROD, AND WIRE; ROLLED, DRAWN, OR COLD FINISHED |
| SAE AMS T 6845 : 2013 | TUBING, STEEL, CORROSION-RESISTANT (S30400), AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION |
| 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 |
| SAE AMS 4942 : 2010 | TITANIUM TUBING, SEAMLESS, ANNEALED, 40.0 KSI (275 MPA) YIELD STRENGTH |
US$150.00
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Hardcopy - English
PDF - English
PDF 3 Users - English
PDF 5 Users - English
PDF 9 Users - English
Hardcopy - English
PDF - English
PDF 3 Users - English
PDF 5 Users - English
PDF 9 Users - English
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