Aerospace. Separable tube fittings for fluid systems, for 24° cones, for pressures up to 3 000 psi or 21 000 kPa. Procurement specification, inch/metric

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

30-11-2014

Publisher

British Standards Institution

Foreword
Introduction
1 Scope
2 Normative references
3 Classification
4 Requirements
5 Quality assurance provisions
6 Preparation for delivery
Annex A (informative) - Equivalent materials
and processes
Bibliography

Defines performance and quality requirements for the qualification and manufacture of standard 24 degrees cone fittings and manufacture of 24 degrees cone fittings to ensure reliable performance or equivalent inch-dimensioned fitting ends to ensure reliable performance in aircraft hydraulic systems.

This International Standard 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 ISO6771.

Committee	ACE/69
DevelopmentNote	Supersedes BS 3M 60(1998) and 04/30112507 DC. (05/2007)
DocumentType	Standard
Pages	32
PublisherName	British Standards Institution
Status	Current
Supersedes	BS 3M 60:1998 04/30112507 DC : DRAFT APR 2004 BS ISO 7169:2007

Standards	Relationship
ISO 7169:2014	Identical

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

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BS ISO 7169:2014

Aerospace. Separable tube fittings for fluid systems, for 24° cones, for pressures up to 3 000 psi or 21 000 kPa. Procurement specification, inch/metric

Table of Contents

Abstract

Scope

General Product Information

International Equivalents

Standards Referencing This Book

Category

Subcategory