Module 11A.10 — Fuel systems (ATA 28) and inerting (ATA 47)
1,103 words · checked 2026-10-03 · Pro
Levels
All parts of 11.10 are level 1 for A1 and level 3 for B1.1: system layout, tanks, supply, cross-feed/transfer, refuel/defuel, indication and warnings, dumping/venting/draining, inert gas systems (ATA 47) and longitudinal balance (CG) fuel systems.
Fuels
| Fuel | Key properties |
|---|---|
| Jet A-1 | Kerosene; freezing point −47 °C max; flash point 38 °C min; standard outside North America |
| Jet A | As Jet A-1 but freezing point −40 °C (mainly USA) |
| Jet B / JP-4 | Wide-cut (kerosene + naphtha), lower flash point, higher fire risk; cold-climate use |
| AVGAS 100LL | Piston fuel, dyed blue (see 11B/11C) |
- Additives: anti-icing (FSII), anti-static, anti-oxidant, corrosion inhibitor, biocides.
- Contamination: water (free, entrained, dissolved), solids, microbial growth (fungi/bacteria at the fuel/water interface — black sludge, corrosion of integral tanks), and mis-fuelling.
- Fuel density varies with temperature (~0.78–0.84 kg/L for Jet A-1); quantity is measured as mass.
11.10(a) System layout, tanks and supply
Tanks
| Type | Features |
|---|---|
| Integral (wet wing) | Sealed wing structure; ribs act as baffles; baffle check valves keep fuel near pumps; access panels on lower skin |
| Centre tank | In the wing centre box; on many types it is used first; heat from adjacent packs raises flammability → inerting |
| Bladder (bag) tanks | Flexible tanks in cavities (some business jets, helicopters) |
| Rigid removable | Light aircraft |
| Surge (vent) tanks | At wing tips; catch fuel from vents and return it |
| Trim tank | In the horizontal stabiliser on some long-range types — see 11.10(e) |
| Auxiliary tanks | In cargo holds on some aircraft |
Supply to engines
- Booster pumps: AC electric centrifugal pumps, two per main tank (redundancy), in canisters so they can be changed without draining; pressure switches for low-pressure warnings.
- Ejector (jet) pumps: motive flow from the booster pump or engine supply entrains fuel from tank corners/scavenge areas — no moving parts.
- Suction feed: if boost pumps fail, engine-driven pumps can suck fuel through a bypass valve — altitude limits apply (dissolved air, vapour lock).
- LP (spar) valve / fire shut-off valve: closes fuel to the engine (pulling the fire handle or engine master switch).
- Engine-driven pumps and fuel heaters/filters (see Module 15).
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Sources
- EASA Easy Access Rules for Continuing Airworthiness (Reg. (EU) No 1321/2014), rev. Sep 2025 — Part-66 Appendix I / AMC1 Module 11 syllabus
- FAA-H-8083-31B Aviation Maintenance Technician Handbook — Airframe, Ch. 14 Aircraft Fuel Systems
- FAA-H-8083-30B Aviation Maintenance Technician Handbook — General, Ch. 1 Safety, Ground Operations and Servicing (fuelling)