Contact|RisingUp Home


Federal Aviation Regulations

Sec. 27.1015 — Oil tank tests.

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]

NEXT: Sec. 27.1017 - Oil lines and fittings.
PREVIOUS: Sec. 27.1013 - Oil tanks.

Search the FARS for