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Elements and Performance Criteria

1. Load fueller
   • Vehicle is positioned at loading bay and all precautionary and reporting requirements are carried out
   • Vehicle is grounded and loading bay bonding lead is connected to fueller
   • Fueller is dipped and ullage is determined
   • Loading operations and quality control checks are completed
2. Conduct pre-operational checks on fueller/dispenser vehicle and equipment
   • Personal protective equipment (PPE) is selected and used in accordance with workplace procedures
3. Hazards are identified, risks are assessed and hazard management implemented
4. Pre-operational checks of fueller/dispenser vehicle and auxiliary equipment are conducted
5. Problems or defects identified during pre-operational checks are reported or rectified in accordance with workplace procedures and manufacturer requirements
6. Outcomes of pre-operational checks are reported and recorded
   • Vehicle is positioned at loading bay and all precautionary and reporting requirements are carried out
7. Vehicle is grounded and loading bay bonding lead is connected to fueller
8. Fueller is dipped and ullage is determined
9. Loading operations and quality control checks are completed
10. Position fueller/dispenser vehicle
    • Fueller/dispenser vehicle is moved to aircraft
11. Aircraft is approached following confirmation has been provided that is safe to approach the aircraft in accordance with the aircraft operator's manual suite and workplace procedures
12. Vehicle is positioned either underwing or standoff, depending on aircraft type
13. Appropriate precautions are taken to avoid risk of collision with aircraft control surfaces and engines
14. Fueller/dispenser vehicle is parked in a position that provides easiest route for evacuation in an emergency
15. Carry out refuelling operations
    • Vehicle is grounded and bonding lead is connected to aircraft
16. Pressure refuelling auxiliary equipment is positioned and hose is connected
17. Hydrant dispenser delivery hoses and couplings are connected to aircraft and intake hose is connected to inlet coupler
18. Aircraft is refuelled to required fuel quantity or tank capacity
19. Complete post-refuelling operations
    • Refuelling operations are completed
20. Fuel sample is taken from filter sump/inlet and visual check is made prior to aircraft departure
21. Hoses, couplings and auxiliary equipment are disconnected and stowed
22. Hydrant dispenser lanyard is disconnected, and pit valve dust cover and hydrant pit lid are replaced
23. Reel hoses are rewound and stowed
24. Fueller/dispenser vehicle is driven either to depot or to next aircraft in accordance with workplace procedures, regulatory requirements and local instructions
25. Complete documentation
    • Hard copy documentation and paperwork is completed as required and airline representative’s signature is obtained
26. Electronic fuel management systems are used to report, record and verify refuel operations

Range Statement

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

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