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                                歐洲航空安全局認證規范定義和縮寫

                                時間:2011-10-20 00:58來源:藍天飛行翻譯 作者:航空 點擊:


                                 
                                ‘Rated 2-Minute OEI Power’ means, with respect to rotorcraft turbine engines, the approved one-engine-inoperative brake horsepower developed under static conditions at specified altitudes and temperatures within the operating limitations established for the engine, for continuation of the one-flight operation after the failure or shutdown of one engine in multi-engine rotorcraft, for up to three periods of use no longer than 2 minutes each in any one flight, and followed by mandatory inspection and prescribed maintenance action.
                                 
                                ‘Reference landing speed’ means the speed of the aeroplane, in a specified landing configuration, at the point where it descends through the landing screen height in the determination of the landing distance for manual landings.
                                 
                                ‘Reversible Pitch Propeller’ means a Propeller in which blade angle can be changed by the flight crew to produce reverse thrust.
                                [Amdt. No.:Def/1]
                                 
                                ‘Rotational Direction of Equipment’ means the direction of rotation as observed when looking at the drive face of the equipment (usually described as ‘clockwise’ or ‘anti-clockwise’).
                                 
                                ‘Rotorcraft’ means a heavier-than-air aircraft that depends principally for its support in flight on the lift generated by one or more rotors.  
                                 
                                ‘Rotorcraft-load combination’ means the combination of a rotorcraft and an external-load, including the external load attaching means. Rotorcraft-load combinations are designated as Class A, Class B, Class C and Class D as follows:
                                 
                                a. Class A rotorcraft-load combination means one in which the external load cannot move freely, cannot be jettisoned, and does not extend below the landing gear.
                                 
                                b. Class B rotorcraft-load combination means one in which the external load is jettisonable and  is lifted free of land or water during the rotorcraft operation.
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