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.
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