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Examen 6

Andres Felipe Londono 94 questions

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Questions in this quiz (94)

  1. 1Where would a pilot find the type of engine oil a specific aircraft uses
    1. ADo not even look, call maintenance
    2. BIn the approved Airplane Operating Manual (AOM) or similar
    3. CIn the Certificate of Airworthiness (Powerplant subsection)
  2. 2If during a preflight a pilot sees that a tire is showing just a thread of canvass, he should:
    1. Aonsult with a maintenance technician
    2. BConsult the limits / tolerances in the approved AFM.
    3. CLook it up in the Maintenance section of the company’s Operations Specifications
  3. 3If at an airport JET A or Jet B type fuels are not available for your aircraft, would you:
    1. ATop it up with 100/130 LL Avgas not to exceed a 50% ratio
    2. BLook in the Flight / Maintenance Manual for alternate fuels
    3. CNot use any other fuel than JET A or Jet B
  4. 4Modern aircraft are usually pressurized in flight by using:
    1. ABleed air tapped off from usually the compressor section of the engine
    2. BAuxiliary Power Units which are installed for this purpose primarily
    3. CPressure controlled bleed air tapped off usually from the last stage turbine section of the engine
  5. 5At what Mach range does the subsonic flight range normally occur?
    1. ABelow .75 Mach.
    2. BFrom .75 to 1.20 Mach
    3. CFrom 1, 20 to 2, 50 Mach
  6. 6How should thrust reversers be applied to reduce landing distance for turbojet aircraft?
    1. AImmediatly after ground contact.
    2. BImmediatly prior to touchdown.
    3. CAfter applying maximum wheel braking.
  7. 7What characterizes a transient compressor stall?
    1. ALoud, steady roar accompanied by heavy shuddering.
    2. BSudden loss of thrust accompanied by loud whine.
    3. CIntermittent "bang", as backfires and flow reversal take place.
  8. 8What indicates that a compressor stall has developed and become steady?
    1. AStrong vibrations and loud roar.
    2. BOccasional loud "bang" and flow reversal.
    3. CComplete loss of power with severe reduction in airspeed.
  9. 9In turbine engine jargon, a Hot Start is when:
    1. AThe outside air temperature is above ISA + 45o C
    2. BThe EGT rises rapidly before the N1/N2N/3 reach sufficient speed and the engine is about to exceed limitations
    3. CTheITT/EGT rises rapidly and exceeds limitations before sufficient turbine/compresso rrotation is obtained
  10. 10Turbine engines can deliver reverse thrust by.
    1. ABringingtheenginefromforwardthrustintoamomentarystop(stationary)thenspooledupintor eversethrust.
    2. BIt is merely accelerated as the exhaust is redirected forward
    3. CStarting the engine in the opposite direction of normal forward thrust.

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Quiz on Examen 6, created by Andres Felipe Londono on 09/11/2016.
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