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CS 22.1323 Air-speed indicating system
Available versions for ERULES-1963177438-5157
ED Decision 2003/13/RM
found in: Sailplane Rule Book - Part-SAO Part-SFCL CS-22 (Nov 2022)
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Sailplane Rule Boo... (Nov 2022)
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CS 22.1323 Air-speed indicating system ED Decision 2003/13/RM (a) The air-speed indicating system must be calibrated to indicate true air-speed at sea-level in standard atmosphere with a maximum pitot-static error not exceeding ± 8 km/h or ± 5% whichever is greater, throughout the following speed range 1.2 VS to VNE, and with wing-flaps neutral and air brakes closed. (b) Calibration must be made in flight. (c) The air-speed indicating system must be suitable for speeds between VS0 and at least 1.05 times VNE.