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Training aid NOVICE

Aircraft Systems Overview and Failure Symptoms

How the major aircraft systems interdepend, and what a failure in one of them looks like from the cockpit and on the ramp.

Source: AMT-SIM original training aid

ATA 24ATA 26ATA 28ATA 29ATA 31ATA 34ATA 36ATA 51

Electrical Power Distribution — Sources, Buses, Protection, Loads

Generation reaches the buses through contactors, the buses feed protected branches, and a breaker protects the wire beneath it — not the load. When unrelated systems fail together, look upstream at the common bus or source rather than at each load.

18 operable
Generator 128 V DCGenerator 228 V DCBatterystart + emergencyExternal powerground serviceGC 1contactorGC 2contactorDCdistributioncommonfeedMain DC bus28 VAvionics bus28 VEssential busbattery fedBus tiecross-connectCB 5GEN 1 fieldCB 15GEN 2 fieldCB 10FMC 1CB 7.5IRS 1Engine 1 gaugesEngine 2 gaugesNav / commavionicsFlight controlsessentialInverterDC → ACAircraft ground / bonding networkthe return path a fault current needs

Live readings

Main DC bus
28.0 V
Avionics bus
28.0 V
Essential bus
28.0 V
Bus tie
open
Engine 1 gauges
energised
Engine 2 gauges
energised
Nav / comm
energised
Flight controls
energised

Inject a fault

Operate any outlined unit. A tripped breaker or an open valve is deliberate isolation, not a defect — only the injected faults are defects.

Reference notes

Systems on an aircraft are interdependent, and that is what makes a single failure look larger than it is. Electrical generation feeds the buses, the buses power the avionics, the hydraulics and the fuel and fire systems, and the engines in turn power the generators. A single upstream failure therefore presents as many unrelated symptoms at once.

The diagnostic habit that follows from this is to look for the common cause first. Several unrelated systems losing power together points upstream to the bus, the source or the protection rather than to each individual load. A fuel quantity disagreement between the cockpit indication and the physical check points to a sensing or plumbing problem, not to a quantity error. Learn to ask what single failure would explain the largest number of symptoms.

Fuel is stored, transferred and delivered under the control of a fuel management system, and quantity indication must agree with the physical check against the uplift figures. Leaks are contained by isolating the affected tank or group, which is always the first action before any diagnosis.

Learning the symptom patterns of each system early is what makes later fault-finding fast. Work from the general to the specific: establish what has actually failed, identify the systems it affects, and only then start isolating individual components.

Books, manuals and source material

Aviation Maintenance Technician Handbook - Airframe (FAA-H-8083-31B)

Federal Aviation Administration · FAA-H-8083-31B, Airframe

Open resource

Official FAA handbook covering structures, systems, hydraulics, landing gear, electrical, fuel, fire protection, instruments and avionics.

Open source resource

Aviation Maintenance Technician Handbook - General (FAA-H-8083-30B)

Federal Aviation Administration · FAA-H-8083-30B, General

Open resource

Official FAA handbook covering mathematics, physics, materials, tools, electricity, human factors and maintenance practices.

Open source resource

A&P Technician General Textbook Reference

Jeppesen · A&P Technician General - use the learner's licensed edition and assigned chapter/pages

Use licensed copy

Course textbook reference for general knowledge topics. AMT-SIM stores citations and study links, not unauthorized textbook reproductions.

Reference this title in the licensed or school-provided copy.

Related Learning

Related Simulator Faults

These faults can be practised in the Hangar after selecting a compatible aircraft.

BUS_FAULTGEN_FAILUREFUEL_LEAKHYD_PUMP_FAILIRS_FAILOIL_LOSS

This reference is an AMT-SIM study aid. Use current approved data and instructor guidance for real maintenance.

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