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BS ISO 10502:2012

Current

Current

The latest, up-to-date edition.

Aerospace. Hose assemblies in polytetrafluoroethylene (PTFE) for use up to 232 °C and 10 500 kPa. Technical specifications and requirements

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

03-31-2012

Foreword
1 Scope
2 Normative references
3 Requirements
4 Responsibility for inspection
5 Preparation for delivery
6 Ordering data
Annex A (informative) - Equivalent materials and
        components

Describes requirements for polytetrafluoroethylene (PTFE) hose assemblies for use in aircraft hydraulic, fuel and lubricating oil systems at temperatures between -55 degrees C (-67 degrees F) and 232 degrees C (450 degrees F) for Class I assemblies and between -55 degrees C (-67 degrees F) and 135 degrees C (275 degrees F) for Class II assemblies, and at nominal pressures up to 10500 kPa (1523 psi) (105 bar).

This International Standard specifies requirements for polytetrafluoroethylene (PTFE) hose assemblies for use in aircraft hydraulic, fuel and lubricating oil systems at temperatures between −55°C (−67 °F) and 232°C (450 °F) for Class I assemblies and between −55°C (−67 °F) and 135°C (275 °F) for Class II assemblies, and at nominal pressures up to 10500kPa (1523 psi) (105 bar1). The hose assemblies are also suitable for use within the same temperature and pressure limitations in aerospace pneumatic systems where some gaseous diffusion through the wall of the PTFE liner is tolerated.

This International Standard covers hose assemblies of the following classes:

  • class I: hose assemblies with fitting of corrosion-resistant steel or titanium parts [232°C (450 °F)];

  • class II: hose assemblies with fitting of corrosion-resistant steel and aluminium parts [135°C (275 °F)], DN12 and larger.

The hose assemblies specified in this International Standard are not intended for use in pneumatic storage systems. In addition, it is intended that installations in which the limits specified in this International Standard are exceeded, or in which the application is not covered specifically by this International Standard, for example for oxygen, be subject to the approval of the purchaser.

Committee
ACE/69
DevelopmentNote
Supersedes 10/30212765 DC. (03/2012)
DocumentType
Standard
Pages
28
PublisherName
British Standards Institution
Status
Current
Supersedes

Standards Relationship
ISO 10502:2012 Identical

ISO 2685:1998 Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones
ISO 6772:2012 Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies
ISO 5855-3:1999 Aerospace MJ threads Part 3: Limit dimensions for fittings for fluid systems
ISO 7258:1984 Polytetrafluoroethylene (PTFE) tubing for aerospace applications Methods for the determination of the density and relative density
ISO 8829-1:2009 Aerospace Test methods for polytetrafluoroethylene (PTFE) inner-tube hose assemblies Part 1: Metallic (stainless steel) braid

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