Module 11A.6 — Electrical power (ATA 24)
1,070 words · checked 2026-10-03 · Pro
Levels
11.6 is level 1 for A1 and level 3 for B1.1 — B1.1 candidates must understand operation well enough to troubleshoot. Topics: batteries, DC and AC generation, emergency power, voltage regulation, distribution, inverters/transformers/rectifiers, circuit protection, external power.
Typical power standards (transport aeroplanes)
| Supply | Standard value |
|---|---|
| DC | 28 V DC nominal (batteries 24 V nominal) |
| AC | 115 V phase / 200 V line, 3-phase, 400 Hz constant frequency (or variable frequency about 360–800 Hz on newer types) |
| High-voltage DC (some new types) | ±270 V DC |
400 Hz allows smaller, lighter transformers and motors than 50/60 Hz.
Batteries
| Type | Cell voltage | Notes |
|---|---|---|
| Lead-acid | 2 V nominal (about 2.1 V charged) | Electrolyte sulphuric acid; state of charge by specific gravity (hydrometer; ~1.275–1.300 charged); never service in the same area/tools as NiCd |
| Nickel-cadmium (NiCd) | 1.2 V nominal | Electrolyte potassium hydroxide — specific gravity does not change with charge, so state of charge can't be read by hydrometer; electrolyte level highest when fully charged; risk of thermal runaway (high charge current, high temperature, cell imbalance) — temperature sensors and monitoring; deep-cycling restores capacity (removes "memory") |
| Lithium-ion | ~3.6–3.7 V | High energy density; requires battery management system, containment and venting because of thermal runaway risk |
- A 24 V battery = 12 lead-acid cells or 19–20 NiCd cells.
- Capacity in ampere-hours (Ah); the battery must supply essential loads for a set time after generator loss.
- Installation: secure, ventilated box (hydrogen gas from charging), sump jar with neutraliser (sodium bicarbonate solution for lead-acid spills; boric acid solution for alkaline NiCd electrolyte, per AMM), quick-disconnect connectors, correct polarity.
- Battery charging on aircraft via battery charger (constant current/constant voltage) or TRU on the DC bus.
Key fact: A NiCd battery's state of charge cannot be determined from electrolyte specific gravity; check electrolyte level only when the battery is fully charged.
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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. 9 Aircraft Electrical System
- FAA-H-8083-30B Aviation Maintenance Technician Handbook — General, Ch. 12 Fundamentals of Electricity and Electronics