ED Decision 2005/006/R
|
Element of
System |
Strength Value
|
Remarks |
|
|
Proof |
Ultimate |
||
|
Rigid pipes and ducts Couplings Flexible hoses Return line elements |
1·5 PW 1·5 PW 2·0 PW – |
3·0 PW 3·0 PW 4·0 PW 1·5 Pf |
Pf The maximum pressure applied during failure conditions. |
|
Components other than pipes, couplings, ducts or pressure vessels |
1·5 PW |
2·0 PW |
|
|
Pressure vessels fabricated from metallic materials. (For non-metallic materials see CS 25.1436(b)(7)) Pressure vessels connected to a line source of pressure Pressure vessels not connected to a line source of pressure, e.g. emergency vessels inflated from a ground source |
3·0 PL or 1·5 PL |
4·0 PL or 2·0 PL |
The lower values are conditional upon justification by a fatigue endurance test from which a permissible fatigue life is declared, and upon the ultimate load test being made on the test specimen used for the fatigue life test. The lower values are conditional upon justification by a life endurance test of a suitably factored permissible number of inflation/deflation cycles, including temperature fluctuation results in a significant pressure variation, and upon the ultimate load test being made on the test specimen used for the life endurance test. For all pressure vessels: (1) The minimum acceptable conditions
for storage, handling and inspection are to be defined in the appropriate
manual. See CS 25.1529. (2) The proof factor is to be sustained
for at least three minutes. (3) The ultimate factor is to be
sustained for at least one minute. The factor having been achieved, the
pressure vessel may be isolated from the pressure source for the remaining
portion of the test period. |
|
2·5 PL or 1·5 PL |
3·0 PL or 2·0 PL |
||
[Amdt 25/1]
EASA CS-25 regulations define structural strength requirements for large aeroplane systems. Specifically, pressure vessels, pipes, ducts, hoses, and couplings must withstand specified proof and ultimate load factors. Metallic and non-metallic pressure vessel requirements differ, considering fatigue and life endurance testing, alongside storage, handling, and inspection protocols.
* Summary by Aviation.Bot - Always consult the original document for the most accurate information.
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