Document ID: chunk:federal_register_of_legislation:F2025C00050:body:0:p68
Version: federal_register_of_legislation:F2025C00050
Segment Type: other
Provision Reference: 
Character Range: 230533–234197

thrust reverse, wheel brakes and other drag and braking devices (as applicable);
            4.        maintain positive control to bring the aeroplane to a safe stop;
            5.        initiate and complete engine failure procedures and checklists.
     6.               AME.6 – Manage engine failure and malfunction during approach and landing (simulated)
            1.        maintain control of aeroplane flight path;
            2.        nominate decision height for landing;
            3.         make decision to continue or abort approach and landing in a safe and timely way;
            4.        advise ATS or other agencies capable of providing assistance of situation and intentions;
            5.        establish the approach and landing configuration appropriate for the runway or landing area, and meteorological conditions, and adjust the power plant controls as required;
            6.          maintain a stabilised approach and nominated airspeed within tolerances;
            7.        achieve a smooth, positively-controlled transition from final approach to touchdown in the touchdown zone within tolerances;
            8.        maintain positive directional control and cross-wind corrections during the after-landing roll maintaining the centreline within tolerances;
            9.          use spoilers, prop reverse, thrust reversers, wheel brakes, and other drag or braking devices, as appropriate, in such a manner to bring the airplane to a safe stop after landing (as applicable).
     7.               AME.7 – Conduct go-around or missed approach with engine failure (simulated)
            1.        identify and confirm engine failure in a multi-engine aeroplane during a go-around or missed approach;
            2.        maintain control of aeroplane;
            3.         perform engine inoperative go-around safely not below the decision height.

 2.                     Range of variables
        1.        activities are performed in accordance with published procedures;
        2.        day VFR or IFR;
        3.         class-rated multi-engine aeroplane with dual controls, electronic intercom and dual control brakes;
        4.        aerodromes;
        5.        appropriate surfaces;
        6.          simulated emergencies;
        7.        simulated hazardous weather.

 3.                     Underpinning knowledge of the following:
        1.        airspeed limitations, including: VNO, VA, VX and VY, VNE, VFE, VLO, VLE, VLO2 (landing gear operations down), maximum cross-wind, turbulence penetration speed and maximum load factor;
        2.        emergency airspeeds, including: VMCA, VSSE, engine(s) inoperative climb, approach and final speed, emergency descent and best glide range speeds;
        3.         emergency procedures for: engine failure after take-off, engine fire on the ground and airborne, engine failure in the cruise, waste gate failure (if applicable) and propeller or turbine over-speed;
        4.        safety implications of asymmetric flight below VMCA;
        5.        power, flight and configuration requirements that apply to VMCA;
        6.          methods of regaining control of an aeroplane with a failed engine that is flying at a speed less than VMCA;
        7.        conditions that would increase V1 (if stated in AFM and POH);
        8.        performance the aeroplane can achieve after reaching VY or V2 during asymmetric flight;
        9.          markings on the airspeed indicator that apply to failed engine operations;
       10.          normal and cross-wind take-off and landing procedures: climb, cruise, descent procedures,