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ASA 737

Dale Elder AS 737 pilot Inglés 57 fichas

Fichas del conjunto (57)

  1. 1If not previously commanded on, "Predictive Windshear" for takeoff automatically turns on ______________________by advancing the thrust levers beyond 53 degrees
  2. 2With the TCAS pitch command on the PFD displayed , Keep the aircraft symbol____________ the area indicated by the red limitsOutside
  3. 3IMBAL (amber) alert means the main tanks differ by more than ____________1000 pounds
  4. 4Opening the Crossfeed valve inflight, ______________________allows fuel to feed from any tank to either engine
  5. 5Rotating an engine Fire Switch in one direction ____________________________________electrically fires a squib on one bottle, discharging the extinguisher
  6. 6With the OVER DET switch in the A position, ____________________________________ can initiate an overheat or fire warningonly the A detector loop
  7. 7"Reverse video" displayed on the engine Vibration readout indicates ________________________High engine vibration level
  8. 8The Thrust Mode Display indicates R-TO (green). What mode is active ?_____________________reduced takeoff thrust
  9. 9The radio Tuning Panel (RTP) displays _______ when the selected radio is not availableINOP
  10. 10Which Radio defaults to DATA on power up and at power down __________________________VHF 3
  11. 11The COWL ANTI-ICE (amber) light illuminates means ______________________________excessive pressure in the duct
  12. 12A TAI (amber) indication to the left on an N1Display Unit indicates: ______________________The Cowl Anti-Ice valve failed tp move to the position selected by the ENG ANTI-ICE switch, or is in transit.
  13. 13To manually deploy Passenger Service Unit (PSU) oxygen masks ____________________________place PASS OXYGEN Switch ON
  14. 14The ________ position on the Flight Crew mask provides continuous flow 100% oxygen at positive pressureEMER
  15. 15The _________________ pneumatically modulate(s) to control airflow into the respective Air Conditioning Pack based on air conditioning demandspack valves
  16. 16Thrust must be limited to idle with the ________________ light illuminatedDUAL BLEED
  17. 17Ground operation of the electric pump requires minimum _____________ in respective tank1675 lbs
  18. 18For ground and flight operations, the corresponding Center Tank Fuel Pump switch must be positioned OFF when the _________________ light illuminates.LOW PRESSURE
  19. 19If the Center Tank is empty, position both Center Tank FUEL PUMP switches to _________OFF
  20. 20Center Tank Fuel Pump must not be ON unless personnel are available in the Flight Deck to monitor ________________________________LOW PRESSURE lights
  21. 21For ground operation, Center Tank FUEL PUMP switches must not be positioned ON unless he Center tank fuel quantity exceeds _________________1000 lbs
    except when defueling or transferring fuel
  22. 22Main Wing Tanks must be scheduled to be full if the Center Tank contains more than _________________1000 lbs
  23. 23Random fuel imbalance must not exceed 1000 lbs for ________,______________,___________, _________Taxi, Takeoff, Flight or Landing
  24. 24Allowable lateral imbalance between Main Tanks 1 and 2 must be scheduled to be _______________Zero
  25. 25What is the minimum fuel temperature ? _________________-37 degrees unless the actual fuel freeze point is known.
  26. 26In the 700W/900ER, manually overriding the Load Alleviation System ___________________is not authorized
  27. 27Do not deploy speed brake with ___________________more than Flaps 10 extended
  28. 28In flight, do not extend the SPEED BRAKE lever _________________________beyond the FLIGHT DETENT
  29. 29Do not deploy speed brakes in flight __________________below 1000 ft AGL
  30. 30Holding in icing conditions with flaps extended is _______________________Prohibited
  31. 31What is the maximum flap extension altitude ______________________20,000 ft
  32. 32Except for engine start, The APU bleed must be closed when another source is pressurizing ___________________left bleed air duct
  33. 33APU bleed valve may be open during engine start but avoid engine power ____________________above idle
  34. 34Ensure APU BLEED air switch is closed for 2 minutes ______________ and for 1 minute _______________after start, prior to shutdown
  35. 35Maximum Operating Altitude _________________41,000 ft
  36. 36What is the maximum altitude to use the APU for Electric only ______________________41,000 ft
  37. 37What is the maximum altitude to use the APU for Bleed only ___________________17,000 ft
  38. 38What is the maximum altitude to use the APU for a Bleed and Electric load ____________________10,000 ft
  39. 39Intentional selection of reverse thrust in flight is _________________________Prohibited
  40. 40When must the Engine Start switches be in the FLT position _____________Operation in severe turbulence
  41. 41When must the Engine Start switches be in the CONT position __________________Takeoff
    Landing
    Anti-Ice Operation
    Operation in hail, sleet, or moderate to heavy rain
  42. 42What is the minimum cool-down time for shutting down the engines _________________________3 minutes
  43. 43What is the minimum warm-up time for operating the engines3 minutes
  44. 44Can you use the aileron trim with the AP engaged _________________Prohibited
  45. 45When must the AP be disengaged on an HGS AIII approach ___________________500 ft AGL
  46. 46When is the latest you would have to disengage the AP on a single channel approach _______________50 ft AGL
  47. 47What is the earliest you can engage the autopilot on takeoff ____________________1000 ft AGL
  48. 48Engine anti-ice must be ON prior to and during decent ________________________In all icing conditions, including temperatures below -40 degrees C SAT
  49. 49The engine anti-ice system must be ON during all ground and flight operations when icing conditions exist or are anticipated except ______________________during climb and cruise below
    -40 degrees C SAT
  50. 50With either one of both engine BLEED air switches ON, do not operate air condition in HIGH for _________,__________,___________takeoff
    approach
    landing
  51. 51What is the Severe Turbulence Penetration Target Speed _______________280 KIAS/.76M whichever is lower
  52. 52What is the Maximum Operating Speeds Limit __________________Observe Vmo/Mmo and Gear/Flap Placards
  53. 53What is the Minimum Takeoff and Landing Temperature _________________-54 degrees C
  54. 54What is the Maximum Takeoff and Landing Altitude _________________8,400
  55. 55What is the Maximum Operating Altitude __________________41,000
  56. 56What is the Maximum tailwind component for takeoff and landing ________________15 knots
    Does not include gusts
    steady state winds only
  57. 57—

Información

Descripción
pilot AS 737 Fichas sobre ASA 737, creado por Dale Elder el 30/05/2021.
Creado por
Dale Elder
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23
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