Maintaining fuel systems on aircraft (Aviation Maintenance) (ATA 28) Revision — Excellence, Achievement & Learning Limited Occupational Qualification
This unit identifies the training and development required in order that the apprentice can demonstrate that they are competent inbeing able to carry out maintenance activities on aircraft fuel systems, in accordance with the approved aircraft maintenance manual,approved change documentation (service bulletin) and airworthiness requirements. It covers both fixed wing and rotary winged aircraft,and covers the units and components which store and deliver fuel to the engine. It includes engine driven fuel pumps for reciprocatingengines, tanks (bladder), tanks (integral), tanks auxiliary, valves, boost pumps, fuel dump systems, fuel tank leak detection components,fuel draining, fuel tank capacitance units, float switches, float valves, temperature sensing, refuel diffuser systems, dip sticks, magneticlevel indicators, fuel tank baffling, flame arrester components and tank venting systems. The maintenance activities will include theremoval, fitting and testing of a range of fuel system components. They will be expected to use the approved procedure for correctlyisolating the system before breaking into the system circuit. They will remove the required components and fit approved replacements,as appropriate. They will then need to test and adjust the completed system to meet the aircraft maintenance manual, changedocumentation (service bulletin) and airworthiness requirements.
Exam Tips
- Always refer to the maintenance manual.
- Double-check all connections after fitting.
Common Mistakes
- Not following isolation procedures correctly.
- Using incorrect torque settings.
Key Marking Points
- Isolate the fuel system correctly before maintenance.
- Remove and fit fuel system components accurately.
- Test and adjust the system to meet specifications.
- Follow approved documentation and airworthiness requirements.