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Q&A Forum

1118 questions found

Module 11. Aeroplane aerodynamics, structures and systems

Compared with the flap up configuration the maximum angle of attack for the flaps down configuration is

  • unchanged.
  • larger.
  • smaller.
vmartin asking:

in Cl/aoa graphics, flaps-down line remains upwards parallel. so, why the answer is not unchanged?

Module 15. Gas turbine engine

The purpose of the rotating guide vanes on a centrifugal compressor is to

  • direct the air smoothly into the impeller.
  • provide initial diffusing of the air.
  • prevent damage by solid objects.
Jordi asking:

can someone please explain to me?

Module 15. Gas turbine engine

Acoustic linings made from composite materials are used in what section of the engine?

  • Not used to suppress noise.
  • Hot section and Cold Section.
  • Cold section only.
Jordi asking:

i dont understand

Module 15. Gas turbine engine

For fire detection and extinguishing purposes, aircraft powerplant areas are divided into fire zones based on

  • engine type and size.
  • the volume and smoothness of the airflow through engine compartments.
  • hot and cold sections of the engine.
Jordi asking:

i think this asnwer is also wrong my pdf says "The zoning layout will depend on the characteristics of the
individual engin"

Module 15. Gas turbine engine

Following the reports of a heavy landing you would

  • carry out a complete visual examination of the power plant.
  • examine the engine mountings and borescope the nozzle guide vanes and turbine.
  • examine the engine mountings and fuse pins.
Jordi asking:

why not the mountings?

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