Module 15 June Session 2026 | Gas Turbine Engine

MODULE 15 JUNE 2026

  1. EGT is directly proportional to:
    A. TIT (Turbine Inlet Temperature)
    B. TOT (Turbine Outlet Temperature)
    C. CDP (Compressor Discharge Pressure)
    D. All of the above
  2. Which bearing uses a thin film of oil around the outer race to reduce vibraÆŸon?
    A. Ball Bearing
    B. Roller Bearing
    C. Slipper Bearing
    D. Hydraulic Bearing
  3. In a Fenwal fire detector system, the sensing element is:
    A. Wired in parallel
    B. Wired in series
    C. Connected through relays only
    D. Independently connected
  4. Glow-type igniter plugs are generally used in:
    A. Small engines
    B. Large engines
    C. Auxiliary engines
    D. Turbofan engines
  5. An advantage of a can-annular combusÆŸon chamber is:
    A. Greater structural integrity
    B. Larger frontal area
    C. Lower heat resistance
    D. Reduced combusÆŸon efficiency
  6. The hoƩest area in a gas turbine engine is:
    A. In and around the turbine secÆŸon
    B. Inlet secÆŸon
    C. Compressor secÆŸon
  7. Turbine shaÅŒs are commonly manufactured from:
    A. Nickel alloys
    B. Aluminium alloys
    C. Steel only
    D. Magnesium alloys
  8. Ball bearings can support:
    A. Axial loads only
    B. Radial loads only
    C. Both axial and radial loads
    D. Thrust loads only
  9. The type of oil normally used in gas turbine engines is:
    A. SyntheÆŸc oil
    B. Mineral oil
    C. Both syntheÆŸc and mineral oil
  10. A fuel control system primarily senses:
    A. Compressor discharge pressure
    B. Turbine outlet temperature
    C. Compressor inlet pressure only
  11. The funcÆŸon of an overrunning (free-wheel) clutch is:
    A. Free rotaÆŸon of the driven member
    B. Prevent rotaÆŸon in both direcÆŸons
    C. Increase shaŌ speed
    D. Reduce gearbox load
  12. Water injecÆŸon can increase engine thrust by approximately:
    A. 20%
    B. 30%
    C. 40%
    D. 50%

13.EPR is measured by:
A. Electromechanical transmiƩer
B. Mechanical transmiƩer
C. Electronic transmiƩer

  1. During engine start, the following must be monitored:
    A. EGT
    B. Oil pressure
    C. Engine speed (RPM)
    D. All of the above
  2. Propeller RPM is measured using:
    A. Tachometer
    B. Manometer
    C. EPR indicator
    D. Thermocouple
  3. Crystal-type thermocouples are used for:
    A. Temperature sensing
    B. Pressure sensing
    C. VibraÆŸon sensing
    D. Fuel flow sensing
  4. The compressor diffuser used in helicopters is generally:
    A. Convergent type
    B. Divergent type
    C. Parallel type
    D. Venturi type
  5. Low-volaÆŸlity fuel is used to:
    A. Prevent vapour lock
    B. Resist evaporaÆŸon
    C. Both A and B
    D. Increase octane raÆŸng
  6. To expel residual fuel aÅŒer a fire, the engine should be:
    A. Restarted immediately
    B. Motored
    C. Accelerated rapidly
    D. Should not restart
  7. If a fuel metering valve sÆŸcks, the effect may be:
    A. Rich mixture
    B. Lean mixture
    C. Engine malfuncÆŸon
    D. All of the above
  8. The purpose of swirl vanes is to:
    A. Provide beƩer mixing of fuel and air
    B. Increase air velocity
    C. Increase flame velocity
    D. All of the above
  9. In cold weather, fuel volaÆŸlity should be:
    A. Low
    B. High
    C. Medium
    D. Unaffected by temperature
  10. A newly stored engine should be checked:
    A. AÅŒer 24 hours with pink indicaÆŸon
    B. Within 24 hours with pink indicaÆŸon
    C. Within 24 hours with blue indicaÆŸon
    D. AÅŒer 24 hours with blue indicaÆŸon
  11. A mechanical thrust reverser operates by:
    A. Blocking the exhaust path
    B. DiverÆŸng airflow to oppose thrust
    C. Both A and B
  12. Newton’s Third Law relates to:
    A. AcceleraÆŸon and moÆŸon
    B. MoÆŸon only
    C. GravitaÆŸon only
    D. AcÆŸon and reacÆŸon forces
  13. Oil temperature indicaÆŸon is normally taken from:
    A. Inlet of the pressure pump
    B. Outlet of the pressure pump
    C. Scavenge subsystem
    D. Oil tank
  14. Factors affecÆŸng inlet condiÆŸons include:
    A. AircraŌ speed, aircraŌ aƫtude and ambient air condiƟons
    B. StagnaÆŸon density only
    C. Both A and B
    D. Compressor RPM only
  15. CharacterisÆŸcs of a bell-mouth compressor intake include:
    A. High duct efficiency
    B. Increased drag
    C. Decreased velocity
    D. All of the above
  16. MTCS discharge indicator:
    A. Red disk indicates thermal discharge
    B. Yellow disk indicates crew/system discharge
    C. Both A and B
    D. Yellow indicates normal discharge
  17. In a pressure relief valve system:
    A. The relief valve is spring-loaded to open posiÆŸon
    B. The relief valve is spring-loaded to closed posiÆŸon
    C. Both A and B
  18. An APU load compressor supplies:
    A. Electrical power only
    B. PneumaÆŸc power only
    C. Both electrical and pneumaÆŸc power
    D. Hydraulic power
  19. AÅŒer a fire has been exÆŸnguished by the engine fire exÆŸnguisher:
    A. Restart immediately
    B. Restart aÅŒer 10 minutes
    C. Do not aƩempt a restart
    D. Restart aÅŒer inspecÆŸon only
  20. If one turbine blade is damaged:
    A. N2 speed increases
    B. N2 speed decreases
    C. EGT increases
    D. Both B and C
  21. EPR is measured using:
    A. Electrical transmiƩer
    B. Electromechanical transmiƩer
    C. Both A and B
    D. PneumaƟc transmiƩer
  22. Regarding MTCS air cooling:
    A. Compressor shaÅŒs do not require cooling
    B. Bearings do not require cooling
    C. Combustor and turbine secÆŸons principally require cooling
    D. EnÆŸre engine requires equal cooling
  23. An advantage of a can-annular combusÆŸon chamber is:
    A. Greater structural stability
    B. Smaller frontal area
    C. High heat resistance
    D. All of the above
  24. The major advantage of a turboshaŌ engine is:
    A. High reliability, small size, and light weight
    B. High power output, small size, heavy weight
    C. Less power, small size, light weight
    D. Low reliability and low weight
  25. An APU can provide:
    A. Engine starÆŸng on the ground only
    B. PneumaÆŸc power only
    C. Engine starÆŸng in flight
    D. Both ground and in-flight support
  26. Why are turboshaŌ engines ideal for helicopters?
    A. Free-wheeling or overrunning clutch unit permits autorotaÆŸon during power loss
    B. Overrunning or free-wheeling Assists twin-engine transmission systems
    C. Helps in starÆŸng and single engine operaÆŸon in economy cruise mode
  27. The primary purpose of the fuel metering secÆŸon of a hydromechanical FCU is:
    A. AutomaÆŸcally stop fuel aÅŒer flameout
    B. Meter the correct amount of fuel to the combusÆŸon chamber
    C. Maintain constant pressure at all speeds
    D. All of the above
  28. A fan located ahead of the compressor:
    A. Reduces FOD suscepÆŸbility
    B. Increases compressor temperature
    C. Decreases engine efficiency
    D. None of the above
  29. Marking in combusÆŸon chambers and hot secÆŸons should be done using:
    A. Layout dye, chalk, or felt-ÆŸp marker
    B. Wax marking pencil
    C. Metal pencil or graphite pencil
    D. Centre punch
  30. Desiccant should be replaced when humidity exceeds:
    A. 20%
    B. 25%
    C. 30%
    D. 50%
  31. Turbine cooling air passing through porous holes is known as:
    A. TranspiraÆŸon cooling
    B. Film cooling
    C. Impingement cooling
    D. ConvecÆŸon cooling
  32. Fenwal fire detector systems:
    A. Can withstand one fault only
    B. ConÆŸnuous loops are connected in series
    C. Both A and B
    D. Connected in parallel
  33. For an engine stored in a shipping case, the humidity indicator should be checked:
    A. Every 10 days
    B. Every 30 days
    C. Every 90 days
    D. Every 180 days
  34. Which type of gas turbine engine consists of a fan and two independent rotaÆŸng assemblies?
    A. Dual Spool
    B. Single Spool
    C. Dual Spool with Fan
  35. If FADEC fails, the engine reverts to:
    A. EPR Mode
    B. N1 Mode
    C. Manual Fuel Mode
    D. N2 Mode
  36. Compared with a propeller engine, a forward-fan (turbofan) engine:
    A. Has less acceleraÆŸon
    B. Produces lower jet velociÆŸes
    C. Does not prevent shock waves
    D. Both A and B
  37. Turbine engine igniÆŸon systems require a large amount of energy because:
    A. IgniÆŸon is required for a longer period
    B. A high voltage is required
    C. Constant output is required
    D. None of the above
  38. TurboshaŌ engines are primarily used in:
    A. Helicopters
    B. APUs
    C. Both A and B
  39. Which of the following statements regarding wire bundles is correct (MTCS)?
    A. The minimum bend radius should not be less than 10 ÆŸmes the outside diameter of the wire
    group.
    B. Wire groups should normally not exceed ½ inch deflecƟon between support points by their own
    weight.
    C. A wire bundle should not contain more than 80 wires and should not exceed 2.5 inches in
    diameter.
    D. All of the above
  40. In an aÅŒerburner, the:
    A. Pressure increases
    B. Volume increases
    C. Pressure decreases and volume increases
    D. Temperature decreases
  41. A boroscope is:
    A. A flexible and/or rigid opÆŸcal instrument used to inspect the inside of an engine
    B. A rigid tube only
    C. A flexible hose used to inspect the outside of an engine
    D. A pressure measuring device
  42. Turbine blade shrouds are provided to:
    A. Reduce blade vibraÆŸon and ÆŸp leakage
    B. Increase blade angle at the ÆŸp
    C. Act as a diffuser
    D. Increase fuel flow
  43. Regarding aÅŒerburners:
    A. Pressure increases
    B. Velocity decreases
    C. A flame holder is required
    D. A flame holder is not required
  44. The power secƟon of a turboshaŌ engine includes:
    A. Compressor, combusÆŸon chamber, turbine and exhaust
    B. The later turbine stages and output shaŌ
    C. Compressor and accessory gearbox only
    D. ReducÆŸon gearbox only
  45. Compressor washing is performed for:
    A. EnÆŸre gas-path cleaning
    B. LubricaÆŸon of compressor blades
    C. Blade balancing
    D. VibraÆŸon reducÆŸon only
  46. Thermocouple assemblies:
    A. Consist of wires of different metals and lengths
    B. Are painted yellow
    C. Require insulaÆŸon between conductors
    D. All of the above
  47. During engine start, acceleraÆŸon temperature is excessively high. A possible cause is:
    A. Fuel control acceleraÆŸon cam incorrectly adjusted
    B. Fuel control bypass valve sÆŸcking closed
    C. Low fuel pressure
    D. Faulty thermocouple
  48. During engine start, acceleraÆŸon temperature is too low. A possible cause is:
    A. Fuel control acceleraÆŸon cam incorrectly adjusted
    B. Fuel nozzle blockage
    C. Excessive fuel flow
    D. Faulty igniter
  49. Water injecÆŸon systems:
    A. Reduce specific fuel consumpÆŸon
    B. Increase specific fuel consumpÆŸon and are therefore used only for short periods
    C. Have no effect on fuel consumpÆŸon
    D. Eliminate compressor stall
  50. Compared with gasoline, aviaÆŸon kerosene has:
    A. A lower boiling point
    B. A higher boiling point
    C. The same boiling point
    D. Extremely high volaÆŸlity
  51. A fuel flow indicator generally:
    A. Measures fuel pressure only
    B. Indicates fuel flow rate
    C. May indicate fuel quanÆŸty in gallons
    D. Both B and C
  52. Lean die-out occurs when:
    A. The fuel-air mixture becomes excessively rich
    B. The fuel-air mixture becomes excessively lean to sustain combusÆŸon
    C. Compressor speed becomes too high
    D. IgniÆŸon energy becomes excessive

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