CS 22.965 Fuel tank tests

• ED Decision 2003/13/RM found in: Sailplane Rule Book - Part-SAO Part-SFCL CS-22 (Nov 2022)

CS 22.965 Fuel tank tests ED Decision 2003/13/RM (a) Each fuel tank must be able to withstand the following pressures without failure or leakage: (1) for each conventional metal tank and non-metallic tank with walls not supported by the sailplane structure, a pressure of 0.25 bar; (2) for each non-metallic tank with walls supported by the sailplane structure and constructed in an acceptable manner using acceptable basic tank material, and with actual or simulated support conditions, a pressure of 0.14 bar for the first tank of a specific design.