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Code · CFR · Title 14 — Aeronautics and Space · Part 29 — Airworthiness Standards: Transport Category Rotorcraft · § 29.1015

§ 29.1015. Oil tank tests.

112 words·~1 min read·/us/cfr/t14/s§ 29.1015·

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Each oil tank must be designed and installed so that—
(a)It can withstand, without failure, any vibration, inertia, and fluid loads to which it may be subjected in operation; and
(b)It meets the requirements of § 29.965, except that instead of the pressure specified in § 29.965(b)—
(1)For pressurized tanks used with a turbine engine, the test pressure may not be less than 5 p.s.i. plus the maximum operating pressure of the tank; and
(2)For all other tanks, the test pressure may not be less than 5 p.s.i. [Doc. No. 5084, 29 FR 16150, Dec. 3, 1964, as amended by Amdt. 29-10, 39 FR 35462, Oct. 1, 1974]
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