CS 22.361 Engine torque

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

CS 22.361 Engine torque ED Decision 2003/13/RM (a) The engine mount and its supporting structure must be designed for the effects of: (1) the limit torque corresponding to take-off power and propeller speed, acting simultaneously with 75% of the limit loads from flight condition A of [CS 22.333(b)](#_DxCrossRefBm2056272107); (2) the limit torque corresponding to the maximum continuous power and propeller speed, acting simultaneously with the limit loads from flight condition A of [CS 22.333(b)](#_DxCrossRefBm2056272107). (b) For reciprocating engines the limit torque to be accounted for in [CS 22.361(a)](#_DxCrossRefBm2056272123) is obtained by multiplying the mean torque by one of the following factors: (1) 1.33 for engines with 5 or more cylinders; (2) 2 for engines with 4 cylinders; (3) 3 for engines with 3 cylinders; (4) 4 for engines with 2 cylinders.