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BS 2F 67:1980

Current

Current

The latest, up-to-date edition.

Specification for hose for aviation fuel and engine lubricating oil for aeronautical purposes

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

09-30-1980

US$145.86
Excluding Tax where applicable

Foreword
Specification
1. Scope
2. References
3. Construction
4. Materials
5. Dimensions
6. Freedom from defects
7. Tests on finished hose
8. Marking
9. Routine inspection and sampling
Tables
1. Bead height
2. Rubber requirements
3. Dimensions and physical properties of types 1 and
     2 hose
4. Dimensions and physical properties of type 3 hose

Gives requirements for the construction, dimensions, testing and marking of the woven fabric reinforced, woven fabric reinforced with embedded wire helix and braided textile reinforced hoses used for coupling rigid metal pipes, carrying aviation fuel or engine oil of either mineral of synthetic di-ester type, in aircraft. Suitable for use at continuous working temperatures from -40 Degrees C up to 100 Degrees C and a maximum working pressures of a quarter of the specified minimum bursting pressure.

Committee
ACE/65
DevelopmentNote
Supersedes 79/77610 DC (11/2003) Reviewed and confirmed by BSI, November 2012. (10/2012)
DocumentType
Standard
Pages
12
PublisherName
British Standards Institution
Status
Current

This British Standard specifies the requirements for the construction, dimensions, testing and marking of the following three types of hose used for coupling rigid metal pipes, carrying aviation fuel or engine oil of either mineral or synthetic di-ester type, in aircraft.

  • Type 1. Woven fabric reinforced hose.
  • Type 2. Woven fabric reinforced hose with embedded wire helix.
  • Type 3. Braided textile reinforced hose.

The hose is suitable for use at continuous working temperatures from – 40 °C up to 100 °C and at maximum working pressures of a quarter of the specified minimum bursting pressure. At higher temperatures the service life would be progressively shortened.

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