ISO 19631:2015
Current
The latest, up-to-date edition.
Aerospace series Tube fittings for fluid systems, 5 080 psi (35 000 kPa) Qualification specification
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
English
01-09-2015
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ISO 19631:2015 specifies performance and quality requirements for the qualification and manufacture of standard tube fittings to ensure reliable performance in aircraft hydraulic 5 080 psi (35 000 kPa) systems.
ISO 19631:2015 specifies baseline criteria for the design and manufacture of system fittings that are qualification tested on engines.
ISO 19631:2015 covers fittings from size ?04 to ?20 used for the following:
? separable/permanent pipe end fittings;
? permanent connection fittings;
? separable connection fittings.
ISO 19631:2015 covers fittings of the temperature types and pressure classes specified in ISO 6771.
| DevelopmentNote |
Supersedes ISO/DIS 19631. (09/2015)
|
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
International Organization for Standardization
|
| Status |
Current
|
| Standards | Relationship |
| BS ISO 19631:2015 | Identical |
| ISO 4287:1997 | Geometrical Product Specifications (GPS) — Surface texture: Profile method — Terms, definitions and surface texture parameters |
| ISO 2685:1998 | Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
| ISO 10583:1993 | Aerospace fluid systems — Test methods for tube/fitting assemblies |
| ISO 6771:2007 | Aerospace — Fluid systems and components — Pressure and temperature classifications |
| ISO 6772:2012 | Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies |
| ISO 7257:2016 | Aircraft Hydraulic tubing joints and fittings Rotary flexure test |
| ISO 7137:1995 | Aircraft — Environmental conditions and test procedures for airborne equipment |
| ISO 3161:1999 | Aerospace — UNJ threads — General requirements and limit dimensions |
| ISO 8575:2016 | Aerospace — Fluid systems — Hydraulic system tubing |
| ISO 6773:1994 | Aerospace Fluid systems Thermal shock testing of piping and fittings |
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