Module 11C.4–11C.6 — B3 light aeroplanes: heating and ventilation, instruments and avionics, electrical power
1,018 words · checked 2026-10-03 · Pro
B3 levels for these sub-modules
| Sub-module | B3 level |
|---|---|
| 11.4(e) Heating and ventilation (the only part of 11.4 for B3) | 1 |
| 11.5.1 Instrument systems | 2 |
| 11.5.2 Avionics systems | 1 |
| 11.6 Electrical power | 3 |
Remember B3 privileges: avionics work only where simple tests prove serviceability and no troubleshooting is needed (66.A.20) — but electrical power is level 3, so you must understand and troubleshoot the electrical system.
11.4(e) Heating and ventilation (level 1)
- Exhaust shroud (muff) heater: ram air heated around the exhaust muffler → heater valve (push-pull "CABIN HEAT") → cabin and windscreen defrost outlets; surplus dumped overboard.
- Carbon monoxide hazard: cracks in the muffler/exhaust inside the shroud let CO into the cabin; inspect exhaust systems at each scheduled inspection (and per ADs for some mufflers), fit a CO detector (spot card or electronic).
- Ventilation: fresh-air scoops/eyeball vents, opening windows, NACA inlets; cabin exhaust outlets.
- Electric heaters (ground) and combustion heaters are rare on B3 aircraft.
Key fact: The biggest maintenance risk of an exhaust-shroud cabin heater is carbon monoxide from a cracked exhaust.
11.5.1 Instrument systems (level 2)
Pitot-static
- ASI (pitot + static) with colour arcs: white (flap operating range, V_S0 to V_FE), green (normal operating, V_S1 to V_NO), yellow (caution, V_NO to V_NE), red line (V_NE). Arc positions must match the AFM — check after instrument change.
- Altimeter (static, aneroid capsules, subscale setting) and VSI (static, metered leak).
- Alternate static source in the cabin → altimeter and ASI read slightly high.
- Pitot-static leak test after disturbance; correct line routing and drains.
Gyroscopic instruments
- Attitude indicator and heading indicator — usually vacuum-driven (suction 4.5–5.5 inHg) or electric.
- Turn coordinator (electric, gyro canted about 30°) or turn-and-slip indicator (rate gyro, horizontal axis) with slip ball.
- Heading indicator drift — reset to the compass.
Compass
Direct-reading compass: deviation card after a compass swing, compensator screws; avoid steel tools/magnetic items near it; variation, turning and acceleration errors.
Stall warning and AoA
Reed horn (pneumatic) or vane switch with horn/light; AoA indicators fitted as modifications on some aircraft.
Glass cockpit and engine indications
- Light-aircraft EFIS/integrated displays with AHRS and ADC; engine monitors (EGT/CHT for each cylinder, fuel flow).
- Indications of other systems: fuel quantity, oil pressure/temperature, ammeter/voltmeter, suction, annunciators.
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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 (B3 column)
- FAA-H-8083-31B Aviation Maintenance Technician Handbook — Airframe, Ch. 9 Electrical System, Ch. 10 Instrument Systems, Ch. 16 Cabin Environmental Control
- FAA-H-8083-25C Pilot's Handbook of Aeronautical Knowledge, Ch. 7 Aircraft Systems and Ch. 8 Flight Instruments