• There are no items in your cart

14/30310862 DC : 0

NA
NA

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

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

View more information
US$23.96
Excluding Tax where applicable

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.