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CS 25.1015 Oil tank tests

Large Aeroplanes (CS-25) · CS-25 · EAR revision 26 Jan 2023

IRImplementing rule

CS 25.1015Oil tank tests

Each oil tank must be designed and installed so that –

(a)It can withstand, without failure, each vibration, inertia, and fluid load that it may be subjected to in operation; and

(b)It meets the provisions of CS 25.965, except –

(1)The test pressure –

(i)For pressurised tanks used with a turbine engine, may not be less than 34 kPa (5 psi) plus the maximum operating pressure of the tank instead of the pressure specified in CS 25.965(a); and

(ii)For all other tanks, may not be less than 34 kPa (5 psi) instead of the pressure specified in CS 25.965(a); and

(2)The test fluid must be oil at 121°C (250°F) instead of the fluid specified in CS 25.965(c).

IR · CS 25.1015 — CS-25 · ED Decision 2003/2/RM · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

All rules in SUBPART E – POWERPLANT

Consolidated from the EASA Easy Access Rules (revision 26 Jan 2023, extracted 17 Aug 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.

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