Elements and Performance Criteria
- Manage engine failure after take-off
- Control of aeroplane is maintained during emergency response procedures
- Immediate actions are performed in accordance with pilot’s operating handbook (POH)
- Landing area within gliding distance is selected and emergency procedures performed in accordance with aircraft flight manual (AFM)/POH
- Flight profile is flown, from which a controlled landing could be achieved
- Air traffic services or other agencies capable of providing assistance are advised of situation and intentions
- Perform forced landing following engine failure
- Immediate actions are performed in accordance with POH
- Recovery plan is formulated and explained, most suitable landing area within gliding distance selected and aeroplane manoeuvred to nominated landing area
- Consideration is given to restarting engine as required, and engine is restarted as required
- Optimal gliding flight profile is selected and flown, from which a controlled landing could be achieved
- Passengers and/or flight crew members are updated on flight situation and are advised to adopt emergency positions, time permitting
- Aeroplane is landed ensuring safest outcome if engine restart is not achieved
- Conduct precautionary search and landing
- Intentions are communicated to other traffic or agencies as required
- Aeroplane is configured for inspection flight profile
- Landing area is selected and inspected for approach, landing distance, surface and obstacle clearance to ensure aeroplane can be landed safely
- Aeroplane is landed and secured and passengers managed as required
- Manage on-board abnormal and emergency situations
- Abnormal and emergency situations are correctly identified and managed in accordance with relevant emergency procedures and regulatory requirements
- Appropriate emergency procedures are followed in accordance with AFM/POH and published procedures while maintaining control of aeroplane
- Requirement for emergency evacuation of aeroplane is identified
- Emergency evacuation of aeroplane is executed as required