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PC12 Test2

  1. Passenger O2 switch in AUTO permits flow when
    Cabin altitude exceeds 13,500'
  2. Probe heat switch provides how many VDC to which items?
    • 28 VDC from GEN 2 BUSS
    • Pitot Heads
    • Static Ports
    • AOA Probes
  3. Windshield elements & controller are powered by
    • LH 28 VDC GEN 2 BUSS
    • RH 28 VDC Non-ESS BUSS
  4. How many switches are used for landing gear indication and warning?
    • 6 Proximity switches
    • 2 micro switches
  5. Environmental Control System (ECS) consists of?
    • ECS consists of
    •   Air cycle system
    •   Distribution system
    •   Control system
  6. VCCS system consists of?
    • VCCS
    •   Air cycle system
    •   Distribution system
    •   Control system
  7. EIS Caution illuminates when Battery voltage is below?
    EIS Caution illuminates when BATT VDC =< 22 volts
  8. Ignition System Components are
    • Exciter
    • High Temp Cables
    • Two Spark Igniters
    • Cockpit Control Switch
  9. How many flap position sensors are there?
    5 Sensors that sense flap position
  10. AV BUS Warning illuminates when
    < 18 VDC
  11. Aircraft dimensions are
    • Wing span - 53' 3"
    • Length - 47' 3"
    • Height - 14' 0"
    • Wheel width - 14' 10"
  12. Total Fuel?

    Usable Quantity?
    • Total Fuel = 406 gal/203 gal per side
    • Usable Fuel = 402 gal/201 gal per side or 2725 lbs
  13. Turbine Oil Quantity and type
    • Turbine Oil Quantity = 14.5 qts.
    • BP 2380
  14. Not feathered stabilized propeller operation is prohibited between what RPM?
    350 - 950 RPM not feathered
  15. When is Auto-Pilot and Yaw damper off?
    Both are off during takeoff and landings.
  16. Minimum battery voltage for Battery Start
    Minimum Battery Voltage for Battery Start = 24 VDC
  17. Minimum Battery Voltage for External Start is
    Minimum battery voltage for External Start = 28 VDC
  18. When will PUSHER ICE MODE illuminate
    • Inertial Separator - OPEN
    • Prop Heat - ON
  19. VLO =
    • VLO = 177 KIAS
    • Do not retract or extend gear above this speed
  20. CAWS PROP DEICE Caution illuminates when
    PROP DE ICE system has malfunctioned
  21. CAWS Pitot 2 Caution illuminates when
    • Left pitot heat has failed.
    • (Co-pilots airspeed)
  22. CAWS PITOT 1 Caution illuminates when
    • Right side pitot heat has failed
    • (Pilot's airspeed)
  23. CAWS WSHLD HEAT Caution illuminates when
    Failure of LH or RH windshield heat when selected to ON
  24. CAWS STATIC Caution illuminates when
    LH or RH static heat malfunction
  25. CAWS INERT SEP Caution illuminates when
    Switch is set to OPEN and there is a separator malfunction
  26. CAWS DE ICE BOOTS Caution illuminates when
    • System malfunction when cycling .
    • CAWS green DE ICE BOOTS if OFF
  27. CAWS L FUEL LOW or R FUEL LOW illuminates when
    Fuel quantity is <20 gal (135 lbs) in either wing tank
  28. CAWS FUEL PRESS Caution illuminates when pressure is?
    What actions are taken?
    • Fuel system pressure is < 2 PSI
    • Power - reduce to minimum to sustain flight
    • Fuel pumps - ON
    • If FUEL PRESS light remain ON
    • Land as soon as possible
  29. CAWS 'AOA De ICE' Caution means?
    What action is taken?
    • With Probes ON
    • 1. AOA heater failure

    • 1. Check CB
    • 2. Probes switch OFF wait 3 min

    Depart icing if condition persists
  30. CAWS 'N ESSNTL BUS' caution means
    Normally indicates automatic load shedding after GEN 1 failure

    Nonessential bus voltage < 22 VDC
  31. CAWS 'ECS' caution means
    • ECS malfunction/fail or not on
    • No bleed air

    If aircraft above 10,700' O2 masks
  32. CAWS 'HYDR' caution means
    ON GROUND: 6 cycles of pump in 1 hour of flight. Requires Maintenance

    IN FLIGHT: <1800 psi or pump on for > 10 min.

    • HYDR CTL CB - PULL
    • A/S < 177 kts
  33. CAWS 'CHIP' caution means
    ON GROUND: Do Not Start

    AFTER START: Return to Parking

    • IN FLIGHT: Check & Monitor engine parameters.
    • Reduce power to minimum for safe flight
    • Land As Soon As Practical
  34. CAWS 'OIL QTY' warning light means
    Low engine oil quantity

    On ground do not start
  35. CAWS 'FLAPS' caution means
    System malfunction or with [PUSHER] on asymmetry or twist
  36. CAWS 'BAT HOT' caution means
    Battery over temp (>700 C) or sensor disconnected
  37. CAWS 'INVERTER' caution means
    Inverter output < 20 VAC
  38. CAWS 'GEN 1 OFF' caution means
    • GEN 1 is off line
    • Voltage < 20 VDC

    NON ESNTL B caution will also light
  39. CAWS 'PUSHER' caution means
    ON GROUND: Pusher test needs to be completed. If light stays on - NO FLIGHT PERMITTED

    • IN FLIGHT: Do pusher test. If light extinguishes no further action
    • Light on - A/C is not stall protected
  40. CAWS 'BUS TIE' caution means
    Bus tie relay open
  41. CAWS 'GEN 2 OFF' caution means
    • GEN 2 is off line
    • Voltage is < 20 VDC
  42. CAWS 'ENG FIRE' warning light means
    Over temp condition and/or possible engine fire
  43. CAWS 'AV BUS' warning means
    Avionics Bus 1 or 2 voltage is < 22 VDC
  44. CAWS 'ESNTL BUS' warning means
    Voltage of Battery, GEN 1 or GEN 2 is < 22 VDC
  45. CAWS 'AP TRIM' warning means
    Autopilot and/or auto trim failure
  46. CAWS 'PROP LOW P' warning means
    Propeller RPM below minimum in-flight pitch (A/C is not on the ground)
  47. CAWS 'AIR/GND' warning means
    Disparity between Left & Right AIR/GND switches, 10 sec delay
  48. CAWS 'CARGO DOOR' warning means
    Cargo door and/or handle not locked
  49. If flap asymmetry or twist is detected and flap angle is >20 what happens
    1. Stick pusher defaults to safe mode & CAWS 'PUSHER' caution light will come on 10 sec. later.

    2. Stick pusher will operate approximately 5 kts. higher airspeed
  50. If PDU motor overheats or a stalled motor condition is detected, what happens
    • Signal from PDU will open FLAP CB on BATT BUS,
    • CAWS "FLAPS" caution illuminates,
    • Reset Flap CB after 5 minutes
  51. At what speed does Stick Shaker activate?
    10 kts. above stall speed
  52. Approach speed with operational boots?
    • Speed 108 kts.
    • Flaps 150
  53. Approach speed with boot failure?
    • Speed 134 kts.
    • Flaps 00
  54. Va for following weights:
    9921
    9480
    9039
    6610
    • 9921 = 158 kts.
    • 9480 = 155 kts.
    • 9039 = 151 kts.
    • 6610 = 129 kts
  55. Speed for Vfe?
    Vfe for 150 flaps is 163 kts.

    Vfe for > 150 flaps is 130 kts.
  56. Speed for holding in icing conditions with 00 flaps?
    Holding speed for icing with 00 flaps is 170 kts.
  57. Minimum speed after boot failure is?
    Minimum speed after boot failure is 134 kts.
  58. Approach speed for:
    Flaps 150
    Pusher Ice Mode
    Approach speed is 108 kts.
Author
jaford047
ID
226700
Card Set
PC12 Test2
Description
Test 2
Updated

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