BS 2F 67:1980
Current
The latest, up-to-date edition.
Specification for hose for aviation fuel and engine lubricating oil for aeronautical purposes
Hardcopy , PDF
English
30-09-1980
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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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