Document ID: chunk:federal_register_of_legislation:F2025C00050:body:0:p162
Version: federal_register_of_legislation:F2025C00050
Segment Type: other
Provision Reference: 
Character Range: 557136–561682

task;
            8.        confirm location of ground support personnel when available;
            9.          conduct appropriate reconnaissance and pre-manoeuvre or other relevant checks prior to descending below 500 ft AGL.
     2.               LL-A.2 – Flight component
            1.        correctly performs pre-flight inspection and determine aircraft serviceability for intended flight;
            2.        initialises and checks data validity of area navigation system (if fitted);
            3.         correctly operates aircraft;
            4.        correctly performs take-off.
     3.               LL-A.3 – Aircraft handling
         1.         For this element, manoeuvres are performed at an altitude above 3,000 ft AGL for training purposes:
                1.        perform level flight, climbing and descending turns up to 60° angle of bank (45° for multi‑engine aircraft):
                       1.          visual references utilised;
                       2.         speed monitored;
                       3.       bank attitude maintained;
                       4.       pitch attitude adjusted for bank angle;
                       5.         desired altitude maintained;
                       6.       rollout and level off anticipated;
                2.        perform approach and recovery to the stall in level flight:
                       1.          recognise approach to stall conditions;
                       2.         maintain references by visual cues;
                       3.       identify the approach to stall;
                       4.       recover by AOA reduction and power application to minimise height loss;
                       5.         reconfigure aeroplane;
                3.         perform approach to the stall in turning flight and recovers:
                       1.          recognise approach to stall conditions;
                       2.         maintain references by visual cues;
                       3.       identify the approach to stall;
                       4.       recover by AOA reduction and power application to minimise height loss;
                       5.         reconfigures aeroplane;
                4.        recover from wing drop at the stall to straight and level in various configurations (limited to single‑engine aeroplanes):
                       1.          identify the approach to stall;
                       2.         recognise wing drop at the stall;
                       3.       reduce angle of attack to unstall the wing;
                       4.       prevent yaw;
                       5.         use available power and height to increase the aircraft energy state;
                       6.       avoid secondary stall;
                       7.      re-establish desired flight path and aircraft control with balanced control application;
                       8.    reconfigure aeroplane as required;
                5.        perform maximum rate turning:
                       1.          apply maximum performance turning criteria;
                       2.         maximum power applied;
                       3.       maximum bank applied for turning performance commensurate with speed;
                       4.       maximum permitted 'g' applied commensurate with speed;
                       5.         achieve turning at maximum AOA;
                       6.       ensure aeroplane does not stall or exceed permitted G limits;
                       7.      release 'g' force during roll out of turn;
                6.          perform minimum radius turning:
                       1.          apply minimum radius turning criteria;
                       2.         maximum power applied;
                       3.       height as low as safely practical;
                       4.       recognise stall warning indications (at the approach to the stall);
                       5.         ensure aeroplane does not stall;
                       6.       release 'g' force immediately prior to rolling out of the turn;
                7.        manage the energy state of the aircraft:
                       1.          identify high kinetic energy situations;
                       2.         identify low kinetic energy situations;
                       3.       identify high potential energy situations;
                       4.       identify low potential energy situations;
                8.        perform a forced landing following a simulated engine failure (single-engine