Examen Atr-42

20 Questions
Art Quizzes & Trivia

RECURRENT EVALUATION POR ATR-42 PILOTS

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Questions and Answers
  • 1. 
    THE MASTER WARNING SYSTEM IS TYPICALLY IDENTIFIED WITH?
    • A. 

      Advisory

    • B. 

      Emergency situation

    • C. 

      Abnormal Situation

  • 2. 
    • A. 

      It provides positive power to protect critical items from power transient. It never powers the starters.

    • B. 

      During a battery start or when using the opposite GEN for a cross-start (on ground), it provides backup starter power if the MAIN BAT is weak.

    • C. 

      During a battery start only, it provides backup starter power if the MAIN BAT is week.

  • 3. 
    STBY BUS OVRD PUSH BUTTON SET ON OVRD MEANS THAT:
    • A. 

      DC STBY BUS and AC STBY BUS trough INV 1 are supplied from DC HOT MAIN BAT BUS.

    • B. 

      DC STYBY BUS AND AC STBY BUS trough INV 1 are supplied from DC HOT EMER BUS.

    • C. 

      DC STYBY BUS AND AC STBY BUS trough INV 1 are supplied from DC HOT MAIN BAT BUS.

  • 4. 
    AT TAKE OF POWER, HOW MANY ENGINES CAN ONE ELECTRIC PUMP SUPPLY?
    • A. 

      Both engines.

    • B. 

      Jet pump supply is necessary for take off.

    • C. 

      Only one

  • 5. 
    HOW ARE THE OIL PRESSURE SURGES PREVENTED DURING COLD WEATHER START?
    • A. 

      By a pressure regulating valve.

    • B. 

      By a cold relief valve that bypasses the oil back to the tank.

    • C. 

      A and B are correct

  • 6. 
    AIR CRAFT ON GROUND, PWR MGT ON T.O., APTCS PUSH BUTTON ON, ATPCS IS ARMED IF?
    • A. 

      Both PL above 65´ and both torque above 90%

    • B. 

      Both PL above 65´ and both CL on max. RPM.

    • C. 

      Both PL above 56` and both torque above 53%

  • 7. 
    WHEN THE PWR MGT IS SET IN TAKE OFF POSITION, WHAT IS INDICATED BY THE TWO AMBER TARGET BUGS ON THE TORQUE GAUGES?
    • A. 

      PWR MGT amber bugs are not indicating with PW MGT in TO position.

    • B. 

      PWR MGT amber bugs are set by FDAU (flight data acquisition unit) to the reserve take off power setting (up trim value).

    • C. 

      PWR MGT amber bugs are set by FDAU (flight data acquisition unit) to the normal take off power setting (take ff value).

  • 8. 
    • A. 

      Engine fire light on CAP and in free handle, the red light in CL

    • B. 

      Engine fire light on CAP and in free handle MASTER CAUTIONS and CRC in both loudspeakers.

    • C. 

      Engine fire light on CAP and in fire handle, MASTER WARNINGS and CRC in CM1 loudspeaker.

  • 9. 
    THE T.O. INHI FUNCTION IS CANCELLED AUTOMATICALLY WHEN:
    • A. 

      Gear is locked up

    • B. 

      The first leg of landing gear and flaps are up.

    • C. 

      Gear and flaps are up

    • D. 

      The first leg of landing gear unlocks before retraction.

  • 10. 
    • A. 

      They automatically transfer to EMER BAT

    • B. 

      The HOT MAIN BAT BUS is lost and DC ESS BAT BUS is powered by DC BUS 1.

    • C. 

      They will lose power when the battery goes below 19.5 V.

  • 11. 
    A/C ON GROUND AND ACW WXT PWR SELECTED ON, STARTING RH ENGINE AND PUTTING RH CL MAX RPM?
    • A. 

      ACW BUS 1 and ACW BUS 2 are supplied by RH ACW GEN

    • B. 

      ACW BUS 1 is still supplied by ACW EXT PWR ACW BUS 2 is supplied by ACW 2 GEN.

    • C. 

      ACW BUS 1 and ACW BUS 2 are still supplied by ACW WXT PWR

  • 12. 
    HOW IS THE LP VALVE AT THE OUTLET OF EACH TANK CONTROLLED?
    • A. 

      Electrically by the related fire handle (DC BUS 1 or 2 for the motor 1, DC EMER BUS for the motor 2).

    • B. 

      By the related CL.

    • C. 

      Mechanically by the related fire handle.

  • 13. 
    DURING START SEQUENCE, THE CROSS START SYSTEM:
    • A. 

      Makes use of the opposite DC GEN to start.

    • B. 

      Makes use of the MAIN BAT until 10% NH, THEN USES main bat AND OPPOSITE DC GEN (on ground only)

    • C. 

      Makes use of the MAIN BAT until 10% NH.

  • 14. 
    HOW IS A FAILD ENGINE DETECTED BY THE ATPCS?
    • A. 

      When one torquemeter drops below 21%

    • B. 

      When NP goes below 60% with the related power lever above flight idle.

    • C. 

      When one pressure falls below 6 psi.

  • 15. 
    • A. 

      Agent 1 DISCH on left engine + agent 2 DISCH on right engine.

    • B. 

      Agent 1 DISCH on left engine only

    • C. 

      Agent 1 DISCH on left engine + agent 1 DISCH on right engine.

  • 16. 
    SMOKE DETECTORS ARE PROVIDED?
    • A. 

      In the avionics compt. The forward and after cargo compt.

    • B. 

      In the cockpit, the cabin, the cargo compt.

    • C. 

      In the cockpit, the avionics compt, and the cargo compt.

  • 17. 
    THE CROOS-FEED BLEED VALVE OPENS AUTOMATICALLY?
    • A. 

      In flight single engine operation

    • B. 

      On ground, both engines running

    • C. 

      On ground, when BLEED AIR is supplied from a single engine.

  • 18. 
    WHAT DOES THE ¨COMPT TEMP¨ INDICATOR DISPLAY?
    • A. 

      Only the compartment temperature of the selected side.

    • B. 

      The compartment and duct temperature of the selected side.

    • C. 

      The pack and duct temperature of the selected side

  • 19. 
    IF A PACK VALVE IS CLOSED OR INOPERATIVE:
    • A. 

      The other pack, supplies both compartments via PNEUMATIC CROSSFEED.

    • B. 

      Hot air is still available from that pack via the TEMP CONTROL VALVE

    • C. 

      The other pack supplies both compartments (cockpit, cabin) through the mixing camber.

  • 20. 
    • A. 

      Both outflow valves incorporate a manometric capsule (aneroid= to hold the valve open sufficiently to prevent overpressure.

    • B. 

      Both outflow valves incorporate an electrically driven torque motor designed to fully open the valve

    • C. 

      Only the electro pneumatic valve incorporates a manometric capsule to hold the valve open sufficiently to prevent overpressure.