CS 22.221 General

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

CS 22.221 General ED Decision 2003/13/RM (a) Compliance with the following requirements must be shown in all configurations and, for a powered sailplane, with the engine idling. For sailplanes equipped to carry water ballast, the demonstrations of sub-paragraphs (b) to (g) must also be made for the most critical water ballast asymmetry that might occur due to any single malfunction or due to lateral accelerations during a spin. (b) The sailplane must be able to recover from spins of at least five turns or such lesser number at which the spin changes into a spiral dive, by applying the controls in a manner normal for recovery and without exceeding either the limiting air-speed nor the limiting positive manoeuvring load factor for the sailplane. Tests must be conducted with wing-flaps and airbrakes neutral (see [AMC 22.335](#_DxCrossRefBm2056272075)) and with: (1) controls held in the position normal for spins; (2) ailerons and rudder used in opposite directions; (3) ailerons applied in the direction of rotation. In addition and where applicable, tests must be conducted in critical combinations of airbrake extension, wing-flap deflection, waterballast including trim water-ballast and with the powerplant extended or retracted. For wing-flap positions for which a VFE limitation is established, the flap position may be adjusted during recovery after the auto-rotation has stopped. (See [AMC 22.221(b)](#_DxCrossRefBm2056272090)) (c) A sailplane, in the configurations certificated for intentional spinning, must be able to recover from any point in a spin as defined in [CS 22.221(b)](#_DxCrossRefBm2056272088) in not more than one additional turn. In those configurations not approved for intentional spinning, sub-paragraph (d) must be applied. (See [AMC 22.221(c), (d), (e) and (f)](#_DxCrossRefBm2056272089)) (d) A sailplane in the configurations not certificated for intentional spinning, must still be able to recover from a spin as defined in [CS 22.221(b)](#_DxCrossRefBm2056272088) in not more than one and a half additional turns. (e) In addition, any sailplane must be able to recover from a one turn spin in any configuration in not more than one additional turn. (f) The loss of altitude from the point at which recovery is initiated to the point at which horizontal flight is first regained must be determined in all of the above mentioned cases. (g) It must be impossible to obtain uncontrollable spins with any use of the controls.