Document ID: chunk:federal_register_of_legislation:F2025C00050:body:0:p63
Version: federal_register_of_legislation:F2025C00050
Segment Type: other
Provision Reference: 
Character Range: 213605–216933

on aerodrome;
        8.        simulated hazardous weather;
        9.          day VFR conditions;
       10.          for landing an aeroplane in cross-wind, the cross-wind component must be:
               1.          for RPL, not more than 10 kts;
               2.         otherwise, 70% of the maximum permitted for the type of aeroplane being flown;
       11.         local area operational limitations such as noise abatement and aerodrome curfews.

 3.                     Underpinning knowledge of the following:
        1.        typical single-engine aeroplane aircraft systems;
        2.        aeroplane performance;
        3.         aeroplane limitations;
        4.        aeroplane weight and balance;
        5.        options when local conditions are not suitable for landing;
        6.          causes of loss of control of aeroplane on landing;
        7.        contents of the aircraft flight manual and pilot's operating handbook;
        8.        environmental conditions that represent VMC;
        9.          day VFR flight rules;
       10.          propeller wash, rotor wash and jet blast;
       11.         relevant sections of the AIP.

  * A5 Aeroplane advanced manoeuvres

 1.                     Unit description
This unit describes the skills and knowledge required to perform advanced manoeuvres in an aeroplane.

 1.                     Elements and performance criteria

2.1 A5.1 – Enter and recover from stall
(a) perform stalling pre-manoeuvre checks;
(b) recognise symptoms of a stall;
(c) control the aeroplane by trimming and balancing accurately for slow flight and then applying the required pitch, roll and yaw inputs to enter and recover from the following:
(i) slow flight where initial symptoms of a stall become evident;
(ii) stall, recovering without application of power;
(iii) stall, recovering with full power applied (not required for multi-engine aeroplanes);
(iv) stall under the following conditions:
(A) straight and level flight;
(B) climbing flight (not required for multi-engine aeroplanes);
(C) descending flight (not required for multi-engine aeroplanes);
(D) approach to land configuration;
(E) turning flight (not required for multi-engine aeroplanes);
(d) perform stall recovery including the following:
(i) reduce angle of attack;
(ii) prevent yaw;
(iii) use available power and height to increase the aircraft energy state;
(iv) avoid secondary stall;
(v) re-establish desired flight path and aircraft control with balanced control application;
(e) perform stall recovery in simulated partial and complete engine failure conditions;
(f) perform stall recovery at simulated low altitude.

2.2 A5.2 – Avoid spin
This element only applies to a single-engine aeroplane:

(a) perform stalling pre-manoeuvre checks;
(b) recognise wing drop at the stall;
(c) from balanced flight, recover from stall in the attitudes and configurations most likely to cause a wing drop;
(d) perform recovery where the aeroplane exhibits a tendency to drop a wing at the stall, in accordance with paragraph (d) of subclause 2.1 (5.1 – Enter and recover from stall);
(e) perform stall recovery at simulated low altitude.

2.3 A5.3 – Turn aeroplane steeply
 1.        pre-manoeuvre checks for steep turning;
 2.        steep level turn using a nominated bank angle, ending on