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Elements and Performance Criteria

1. Operate a multi-engine aeroplane in all phases of flight
   • Normal operations of multi-engine aeroplane type on the ground and in flight are conducted in accordance with the aircraft flight manual (AFM), pilot’s operating handbook (POH) and company operating procedures
2. Asymmetric operations for all phases of flight are anticipated and contingencies are planned
3. Plan of action is self-briefed or briefed to crew members to ensure safest outcome in asymmetric operations
4. Manage engine failure/malfunction in flight
   • Control of aeroplane is maintained and/or regained during implementation of emergency response procedures
5. Failed/malfunctioning engine is identified and confirmed
6. Power set on serviceable engine/s and aeroplane configuration is adjusted to achieve desired aeroplane performance
7. Failed/malfunctioning engine is managed
8. Indicated airspeed is maintained above minimum controllable airspeed (Vmca)
9. Air traffic control (ATC) or another agency capable of assistance is advised of situation and intentions
10. Recovery or diversion to appropriate aerodrome is evaluated and conducted
11. Manage engine failure/malfunction after take-off
    • Engine failure/malfunction is managed after take-off while control of aircraft flight path is maintained
12. Initial climb not less than best engine out angle of climb speed (VX) or best engine out rate of climb speed (VY) until clear of obstacles, then VY is maintained
13. Perform rejected take-off
    • Take-off is aborted prior to speed beyond which take-off can no longer be safely aborted (V1) or at a decision point during take-off where abort procedure can be initiated and aeroplane stopped on remaining runway/stopway
14. Power is reduced smoothly and promptly
15. Spoilers, prop fine/reverse, thrust reverse, wheel brakes and other drag and braking devices are activated
16. Positive control is maintained to bring aeroplane to a safe stop
17. Engine failure procedures and/or checklists are initiated and completed
18. Manage engine failure/malfunction during approach/landing
    • Control of aeroplane flight path is maintained during implementation of emergency response procedures
19. Engine inoperative approach is performed
20. Decision is made to continue or abort approach/landing
21. Decision height for landing is nominated
22. ATC or other agency capable of providing assistance is advised of situation and intentions
23. Smooth, positively-controlled flight profile is flown, from which a controlled landing could be achieved
24. Positive directional control is maintained and cross-wind corrections are applied during after-landing roll while maintaining centreline within tolerances
25. Spoilers, prop reverse, thrust reversers, wheel brakes, and other drag or braking devices are applied to bring airplane to a safe stop after landing
26. Conduct go-around or missed approach with engine failure
    • Engine failure in a multi-engine aeroplane during a go-around or missed approach is identified and confirmed
27. Control of aeroplane flight path is maintained during implementation of emergency response procedures
28. Engine inoperative go-around is performed from decision height

Range Statement

Range is restricted to essential operating conditions and any other variables essential to the work environment.

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