FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 27 > Section 1015 - Oil tank tests
section 27.1013 |
section 27.1017
Each oil tank must be designed and installed so that it can withstand, without leakage, an internal pressure of 5 p.s.i., except that each pressurized oil tank used with a turbine engine must be designed and installed so that it can withstand, without leakage, an internal pressure of 5 p.s.i., plus the maximum operating pressure of the tank.
[Amdt. 27-9, 39 FR 35462, Oct. 1, 1974]
   
Current page: FARs > Part 27 > Section 1015 - Oil tank tests
section 27.1013 |
section 27.1017
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