14/30310862 DC : 0
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Status of Standard is Unknown
BS EN 4832 - AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING AND RING-LOCKED FITTING-REDUCER - INCH SERIES - TECHNICAL SPECIFICATION
Available format(s)
Hardcopy , PDF
Language(s)
English
Publisher
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Foreword
1 Scope
2 Normative references
3 Technical Requirements
4 Performances
5 Quality Assurance
6 Preparation for delivery
BS EN 4832.
| Committee |
ACE/12
|
| DocumentType |
Draft
|
| Pages |
27
|
| PublisherName |
British Standards Institution
|
| Status |
NA
|
| 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 |
| PREN 4833 : DRAFT 2017 | AEROSPACE SERIES - PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING LOCKED FITTING - FLARELESS END - INCH SERIES - EXTRA FINE THREAD PITCH |
| SAE AMS QQ A 225/9 : 2014 | ALUMINUM ALLOY 7075, BAR, ROD, WIRE, AND SPECIAL SHAPES; ROLLED, DRAWN, OR COLD FINISHED |
| SAE AMS 5737 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS AND TUBING, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1650 DEGREES F (899 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
| PREN 4835 : DRAFT 2017 | AEROSPACE SERIES - INSTALLATION AND REMOVAL REQUIREMENTS FOR RING LOCKED FITTING AND REDUCER, 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) - INCH SERIES |
| SAE AS 5620 : 2013 | TITANIUM HYDRAULIC TUBING, TI-3AL-2.5V COLD WORKED AND STRESS RELIEVED, UP TO 35000 KPA (5080 PSI), REQUIREMENTS FOR QUALIFICATION TESTING AND CONTROL |
| ISO 4287:1997 | Geometrical Product Specifications (GPS) — Surface texture: Profile method — Terms, definitions and surface texture parameters |
| SAE AMS 2488 : 2000 | ANODIC TREATMENT - TITANIUM AND TITANIUM ALLOYS SOLUTION PH 13 OR HIGHER |
| ISO 2685:1998 | Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
| EN 4315:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D ≤ 100 mm, Rm ≥ 900 MPa |
| EN 4317:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D ≤ 200 mm |
| ISO 10583:1993 | Aerospace fluid systems — Test methods for tube/fitting assemblies |
| 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 |
| ISO 6772:2012 | Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies |
| SAE AMS 4965 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS, 6.0AL 4.0V, SOLUTION HEAT TREATED AND AGED |
| 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 5734 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, AND TUBING, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1650 DEGREES F (899 DEGREES C) SOLUTION HEAT TREATED |
| SAE AS 5272 : 2016 | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING, PROCUREMENT SPECIFICATION |
| ISO 11218:2017 | Aerospace Cleanliness classification for hydraulic fluids |
| SAE AMS 5732 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING AND RINGS, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED 1800 DEGREES F (982 DEGREES C), SOLUTION AND PRECIPITATION HEAT TREATED |
| PREN 4836 : DRAFT 2017 | AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING REDUCER - FLARELESS END - INCH SERIES - EXTRA FINE THREAD PITCH |
| SAE AMS 5731 : 2012 | STEEL, CORROSION AND HEAT-RESISTANT, BARS, WIRE, FORGINGS, TUBING, AND RINGS, 15CR - 25.5NI - 1.2MO - 2.1TI - 0.006B - 0.30V, CONSUMABLE ELECTRODE MELTED, 1800 DEGREES F (982 DEGREES C) SOLUTION HEAT TREATED |
| EN 2424:2008 | Aerospace series - Marking of aerospace products |
| SAE ARP 5416 : 2013 | AIRCRAFT LIGHTNING TEST METHODS |
| ISO 7257:2016 | Aircraft Hydraulic tubing joints and fittings Rotary flexure test |
| SAE AMS 2700E : 2011 | PASSIVATION OF CORROSION RESISTANT STEELS |
| ISO 7137:1995 | Aircraft — Environmental conditions and test procedures for airborne equipment |
| SAE AS 4941 : 2015 | AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS |
| SAE ARP 5412 : 2013 | AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS |
| SAE AMS 4967 : 2014 | TITANIUM ALLOY, BARS, WIRE, FORGINGS, AND RINGS 6.0AL - 4.0V ANNEALED, HEAT TREATABLE |
| FED-STD-595 Revision C:2008 | COLORS USED IN GOVERNMENT PROCUREMENT |
| 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 |
| 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 |
| ISO 6773:1994 | Aerospace Fluid systems Thermal shock testing of piping and fittings |
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