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EASA Part-66 Module 14 Cats B2 · B2L

Propulsion EASA Part-66 — Module 14 Practice Questions

Module 14 covers turbine, piston, APU and electric/hybrid propulsion, plus engine indication, propellers, starting and ignition — sat by B2 and B2L avionics candidates. Below: what's covered, exam format, and seven sample questions in the same style you'll meet on exam day.

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Every question comes with a worked, EASA-grounded explanation — understand why, don't just memorise.
660
Questions in bank
5
Syllabus sections
40 min
Exam time (B1/B2)
75 %
EASA pass mark

Syllabus at a glance

Full Module 14 syllabus
Section 14.1
Engines
  • Turbine engines: turbojet, turbofan, turboshaft, turboprop
  • Auxiliary power units (APUs) (new in 2023/989)
  • Piston engines & electric / hybrid propulsion
  • Constructional arrangement, lubrication & fuel systems
Section 14.1(e)
Engine Control
  • Full Authority Digital Engine Control (FADEC)
  • Electronic Engine Controller (EEC) & Supervisory EEC
  • Hydromechanical fuel control, metering & scheduling
  • Redundancy, fault detection & trend monitoring
Section 14.2
Engine Indication
  • EGT / ITT thermocouple circuits & cold-junction correction
  • N1 / N2 / N3 speed sensing & pulse-probe tachometry
  • EPR, oil & fuel pressure, fuel-flow transmitters
  • EICAS / ECAM electronic engine displays
Section 14.3
Propeller Systems
  • Blade element theory, blade angle & angle of attack
  • Fixed, variable & constant-speed pitch control
  • Feathering, reverse pitch & overspeed protection
  • Synchronising, synchrophasing & ice protection
Section 14.4
Starting & Ignition
  • Electric, air-turbine, hydraulic & APU starting systems
  • High-energy capacitor-discharge ignition circuits
  • Igniter plug types, construction & operation
  • Continuous ignition for adverse conditions

Three classic exam-day traps

Combustion air split: only ~25-40% is actually burned

Most candidates assume nearly all air entering the combustion section is burned. In reality, the bulk passes around the flame tube as cooling and dilution air — only a fraction enters the primary zone.

FADEC channel failover vs sensor failover

When a sensor input to one FADEC channel is lost, the active channel reads the value from the opposite channel — it does not necessarily hand control over. Confusing channel swap with data cross-feed loses marks.

Cold junction vs hot junction compensation

The compensating resistor in a thermocouple circuit corrects for ambient temperature variation at the cold (reference) junction, not the hot junction inside the gas path. Reading the question carelessly almost guarantees the wrong distractor.

What Module 14 covers — in plain English

Module 14 of the EASA Part-66 syllabus is the propulsion module for avionics-stream candidates. It covers how aircraft engines work — gas turbines, piston engines, auxiliary power units and the newer electric and hybrid architectures — but from a systems-and-indications angle rather than the deep mechanical-overhaul angle a B1 engineer would meet in Module 15 or 16. You are expected to understand engine control (FADEC, EEC, hydromechanical fuel control), the full set of engine-indication systems (EGT, N1/N2, EPR, oil and fuel parameters, vibration), propeller systems, and the starting & ignition circuits that interface with the rest of the avionics suite.

Following the 2023/989 amendment effective 12 June 2024, Module 14 was restructured from three sections into four. Auxiliary power units, piston engines and electric / hybrid propulsion are now explicitly called out under 14.1, propeller systems were promoted to their own dedicated 14.3 section, and starting & ignition became 14.4. The exam also grew from 24 questions in 30 minutes to 32 questions in 40 minutes — about 75 seconds per question — so pace matters.

Cat A, B1 and B3 candidates do not sit this module — their propulsion content lives in Modules 15 (gas turbine), 16 (piston) and 17 (propeller). Only Cat B2 and B2L (avionics) are examined on Module 14, both at the same 32-question paper length. Where a B1 engineer must be able to disassemble, inspect and re-rig the hardware, the B2 / B2L candidate is examined on how the engine interfaces with the rest of the aircraft: indication wiring, control laws, signal conditioning and the interlocks that protect the engine from a runaway start or an overspeed.

Knowledge level is 1 across the engine-architecture sub-sections 14.1 (a) through (d) — you need a working overview of how turbine, APU, piston and electric / hybrid powerplants are arranged and what their major components do — and level 2 for engine control (14.1 e), engine indication (14.2), propellers (14.3) and starting & ignition (14.4), meaning you must understand the principles and apply them, not just recognise the words. The full per-section knowledge-level breakdown and detailed bullet list are on our Module 14 syllabus page.

These samples are drawn from our live Module 14 question bank of 660 questions. The full timed practice quiz draws 32 questions per attempt (or 0 for Cat A), scored against the official EASA 75 % pass mark, with weak-area tracking across attempts.

7 free sample questions

Click "Reveal answer + explanation" after you've picked.

Take the timed practice quiz
Q1 Engines · Turbine Architecture

A free turbine aircraft engine is most likely to be used on a

  1. A high bypass engine
  2. B a direct coupled engine
  3. C a helicopter engine
Reveal answer + explanation Hide answer
Correct answer: Ca helicopter engine
In a free-turbine arrangement the power turbine is not mechanically coupled to the gas generator — ideal for driving a helicopter rotor or a turboprop reduction gearbox at a different speed from the compressor. High-bypass turbofans drive the fan directly off the LP shaft.
Q2 Engines · Combustion Section

What percentage of air passing through the combustion section is burned?

  1. A 40%
  2. B 50%
  3. C 75%
Reveal answer + explanation Hide answer
Correct answer: A40%
Only roughly the primary-zone fraction of combustion-section airflow actually mixes with fuel and burns. The remainder is secondary and dilution air, used to complete combustion, cool the flame tube walls and reduce gas temperature before the turbine inlet.
Q3 Engine Control · FADEC Redundancy

In a FADEC what is the result of Channel A failing to receive information from a sensor?

  1. A Channel B will assume control
  2. B Channel A will take the information from channel B
  3. C Channel A will take the information from the backup sensor
Reveal answer + explanation Hide answer
Correct answer: BChannel A will take the information from channel B
FADEC channels are cross-talking dual-redundant controllers. A single lost sensor input does not trigger a full channel handover — the active channel simply reads that parameter across from the opposite channel. Full handover happens only on channel-level fault.
Q4 Engine Indication · Thermocouples

In a thermocouple temperature sensing system, what is the purpose of the compensating resistor?

  1. A To standardize the reading for different engine types
  2. B To correct for varying ambient temperatures at the cold junction
  3. C To correct for varying ambient temperatures at the hot junction
Reveal answer + explanation Hide answer
Correct answer: BTo correct for varying ambient temperatures at the cold junction
A thermocouple measures the temperature difference between its hot and cold junctions. Ambient changes at the cold (reference) junction in the indicator housing would otherwise show up as false EGT swings — the compensating resistor cancels them out.
Q5 Engine Indication · Speed Sensing

How is the N1 and N2 measured on a triple spool engine?

  1. A Pulse type speed probes
  2. B Tachometer connected to the external gearbox
  3. C Tachometer connected to the internal gearbox
Reveal answer + explanation Hide answer
Correct answer: APulse type speed probes
Modern multi-spool engines use magnetic pulse-type speed probes reading off a toothed phonic wheel on each shaft. Output is a frequency proportional to RPM — converted electronically rather than via a mechanical tachometer cable, which would be impractical for inner spools.
Q6 Propeller Systems · Variable Pitch

Power is adjusted in a variable pitch turboprop aircraft by

  1. A increasing RPM
  2. B increasing fuel flow
  3. C increasing pitch
Reveal answer + explanation Hide answer
Correct answer: Bincreasing fuel flow
On a constant-speed turboprop the propeller governor holds RPM constant by adjusting blade pitch. Power is therefore commanded by fuel flow — more fuel raises turbine output, the governor increases pitch to absorb it, and torque (not RPM) rises.
Q7 Starting & Ignition · Starter Disconnect

A DC starter motor disconnects due to

  1. A current increasing switching off an overspeed relay
  2. B current decreasing switching off an overspeed relay
  3. C a centrifugal switch that acts like an overspeed relay
Reveal answer + explanation Hide answer
Correct answer: Bcurrent decreasing switching off an overspeed relay
As the engine accelerates and approaches self-sustaining speed, the back-EMF in the DC starter rises and armature current falls. The drop-out of the current-sensing (overspeed) relay then opens the starter contactor — there is no centrifugal switch on modern aircraft starters.
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Ready for the full Module 14 timed practice quiz?

Sign up, pick Module 14 from the dashboard, and take a timed exam drawn from our 660-question bank — the number of questions follows your licence category (0 for Cat A, 32 for B1/B2/B2L/B3). Your score is tracked across attempts and we surface your weakest sub-topics so revision time pays off.

Module 14 — frequently asked questions

How many questions are in the EASA Part-66 Module 14 exam?
Module 14 is not part of the Category A syllabus, so there is no Cat A paper for it — Cat A propulsion knowledge is covered elsewhere. For the categories that do sit it, the Module 14 exam has 32 multiple-choice questions. On our platform you can practise the same style of questions before exam day.
What is the pass mark for EASA Part-66 Module 14?
The pass mark for Module 14, like every EASA Part-66 module, is 75%. With 32 questions in the paper you can afford to get a limited number wrong, so accuracy across all four sections — engines, engine control, indication, propellers and starting/ignition — matters. Consistent practice on our question bank is the most reliable way to reach that threshold.
How long is the Module 14 exam?
The Module 14 exam allows 40 minutes for its 32 questions — roughly 75 seconds per question. That pace rewards candidates who recognise the underlying principle quickly rather than working each item from scratch, which is exactly what timed practice builds.
Which EASA licence categories require Module 14?
Module 14 is a restricted, avionics-stream module sat by Cats B2 · B2L only. Cat A, B1 and B3 candidates do not take it — their propulsion content is covered in Modules 15, 16 and 17 instead. The B2 / B2L focus is on how the engine interfaces with the rest of the aircraft: indication wiring, control laws and signal conditioning.
What does Module 14 cover, and what do students find hardest?
Module 14 covers engines (turbine, piston, APU and electric/hybrid propulsion, plus lubrication and fuel systems), engine control (FADEC, EEC and hydromechanical fuel metering), engine indication (EGT/ITT thermocouples, N1/N2/N3 speed sensing, EPR and EICAS/ECAM displays), propeller systems and starting & ignition. Common trip-ups include assuming nearly all combustion-section air is burned when only the primary-zone fraction actually is, confusing FADEC channel swap with sensor data cross-feed, and mixing up cold-junction versus hot-junction thermocouple compensation. Reading each stem carefully is essential, as many distractors differ by a single word.
How should I revise for Module 14?
Focus your revision on the traps that catch most candidates: the combustion air split (only a fraction of combustion-section air is burned; the rest is cooling and dilution air), FADEC data cross-feed versus full channel handover, and cold-junction versus hot-junction thermocouple compensation. Work through the four exam sections in turn and drill the indication and control topics hardest, since they carry level 2 knowledge. Practising timed sets on our Module 14 question bank trains both the recognition speed and the careful reading the paper demands.

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