EASA Part 66 Module 14 UPDATED Actual Exam Questions and CORRECT Answers
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EASA Part 66 Module 14
Institution
EASA Part 66 Module 14
EASA Part 66 Module 14 UPDATED
Actual Exam Questions and CORRECT
Answers
From where is manifold pressure taken on a supercharged engine?
a) Between the carburetor and the supercharger
b) Between the supercharger and the throttle
c)Between the carburetor and the induction ports - CORRECT ANS...
EASA Part 66 Module 14 UPDATED
Actual Exam Questions and CORRECT
Answers
From where is manifold pressure taken on a supercharged engine?
a) Between the carburetor and the supercharger
b) Between the supercharger and the throttle
c)Between the carburetor and the induction ports - CORRECT ANSWER✔✔- c)Between the
carburetor and the induction ports
On a gas turbine engine, what is the fan driven by?
a) HP turbine
b) LP turbine
c) IP turbine - CORRECT ANSWER✔✔- b) LP turbine
What is an engine stage?
a) One rotor plus one stator
b) One IGV and one rotor
c) One compressor rotor and one nozzle guide vane - CORRECT ANSWER✔✔- a) One
rotor plus one stator
The air data input to the FADEC fails. The result will be
a) a lack of flight data
b) uncorrected data from hard wired analogue sensors is utilized
c) the FADEC reverts to the failsafe mode - CORRECT ANSWER✔✔- c) the FADEC
reverts to the failsafe mode
Torque measurement is taken from the
a) free turbine shaft
b) reduction gearbox
c) prop shaft - CORRECT ANSWER✔✔- b) reduction gearbox
,A FADEC system consists of
a) HMU, sensors and an EEC
b) HMU, ADC and sensors
c) EEC, ADC and sensors - CORRECT ANSWER✔✔- a) HMU, sensors and an EEC
What power supply is required for a thermocouple system to work?
a) Direct current
b) Alternating current
c) Neither of the above - CORRECT ANSWER✔✔- c) Neither of the above
In a 24 thermocouple system, one thermocouple goes open circuit. What error is detected at
the indicator?
a) None
b) No indication
c) Gauge freezes at last known reading - CORRECT ANSWER✔✔- a) None
In a thermocouple temperature sensing system, what is the purpose of the compensating
resistor?
a) To standardise the reading for different engine types
b) To correct for varying ambient temperatures at the cold junction
c) To correct for varying ambient temperatures at the hot junction - CORRECT
ANSWER✔✔- b) To correct for varying ambient temperatures at the cold junction
In a dive, with the throttles fixed, the EPR will
a) increase
b) decrease
c) not change - CORRECT ANSWER✔✔- c) not change
How is the N1 and N2 measured on a triple spool engine?
a) Pulse type speed probes
, b) Tachometer connected to the external gearbox
c) Tachometer connected to the internal gearbox - CORRECT ANSWER✔✔- a) Pulse type
speed probes
A twin spool engine has
a) one turbine on one shaft
b) two turbines on one shaft
c) two turbines on two shafts - CORRECT ANSWER✔✔- c) two turbines on two shafts
A free turbine aircraft engine is most likely to be used on a
a) high bypass engine
b) a direct coupled engine
c) a helicopter engine - CORRECT ANSWER✔✔- c) a helicopter engine
Propeller speed is measured from
a) a slip ring pulse probe
b) a tachometer on the LP turbine shaft
c) a pulse probe at the engine side of the reduction gear - CORRECT ANSWER✔✔- a) a slip
ring pulse probe
Propeller torque is analogous to
a) engine RPM
b) shaft horsepower
c) propeller RPM - CORRECT ANSWER✔✔- b) shaft horsepower
How is power indicated on a fixed pitch propeller?
a) RPM gauge
b) Torque gauge
c) Horsepower gauge - CORRECT ANSWER✔✔- a) RPM gauge
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