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CRJ200Limitations.txt

  1. Vfe flaps 8?
    200KIAS
  2. Vfe flaps 20?
    200KIAS
  3. Vfe flaps 30?
    185KIAS
  4. Vfe flaps 45?
    170KIAS
  5. Max landing Gear Operating Speeds Vle Vloretract VloExtend?
    250KIAS 200KIAS 250KIAS
  6. Max Tire Speed gs?
    182KIAS
  7. Max Turbulent Air Penetration speed?
    280 KIAS or .75 Mach whichever is lower
  8. Stab or Mach trim Inop max speed?
    250 KIAS or .70 Mach unless autopilot engaged
  9. When operating below maneuvering speed Vref+10 bank angle is limited to _ degrees or ________?
    15 or half bank
  10. Max Windshield Wiper speed?
    220 Knots
  11. If the windshield wiper has failed in a non-parked position the airplane speed must not exceed what speed?
    220KIAS
  12. Minimum Climb Speed above 10000ft?
    not less than 250KIAS/.70 Mach unless one of the following exeptions exists 1. when mountainous terrain exists in the departure path 2. asked by ATC you may fly at Vy except in icing conditions above 1500ft 3. if restricted by an MEL (maintain the highest speed allowed by the MEL but not slower then Vx
  13. Minimum enroute cruise speed abover FL 310?
    Long Range Cruise (LRC)
  14. Minimum enroute cruise speed at or below FL310?
    two engine holding Vmd in calm air
  15. Engine Type?
    General Electric CF34-3B1
  16. Minimum oil temperature for starting?
    -40 degrees C
  17. Max continuous Oil temperature?
    +155 degrees C
  18. Max permissible oil temperature?
    +163 degrees C (15 minutes maximum)
  19. Minimum Oil Pressure steady state Idle?
    25 PSI minimum
  20. Minimum Oil Pressure takeoff power?
    45 PSI minimum
  21. Max Continuous Oil Pressure?
    115 PSI maximum
  22. Maximum oil pressure transient after cold start?
    156 PSI (130 pis at idle 10 mins maximum)
  23. Continuous ignition must be used during the following?
    takeoff and landings on contaminated runways 2. takeoffs with crosswind compontents in excess of 10knts 3.flight through moderate or heavier intensity rain 4. flight through moderate or heavier intensity turbulence 5. flight in the vicinity of thunderstorms note engine operation at or near the shaker and pusher settings is predicated on an operable auto-ignition system
  24. Engine Start Attempt?
    1st is 1min on 10 secs off 2nd is 1min on 10secs off3rd and subsequent is 1min on 5mins off
  25. Engine Dry start?
    1st is 90secs on 5mins off 2nd and subsequent is 30secs on and 5mins off
  26. Max Fuel Imbalance between left main and right main tank?
    800 pounds
  27. Take off with a fuel load in excess of ___ pounds in the center tank is not permitted unless each main wing tank is above ____ pounds?
    500 4400
  28. Take off with engine fuel temperature indications below _ degrees C is prohibited?
    5
  29. What is the minimum fuel for go-around per wing with the airplane level?
    450 pounds thiss assumes a maximum airplane climb attitude of 10 degrees nose up
  30. what is the total usable fuel?
    14518 lbs pressure refueling
  31. powered crossflow and gravity crossflow must be __ for takeoff?
    off
  32. the Hydraulic 3B pump switch must be selected __ instead of __ for all phases of flight?
    On auto
  33. What type of Oils are approved for use in the CF34-3B1?
    Type II Type I Castrol 4000
  34. What Type of APU do we have?
    Garrett GTCP-36-150RJ
  35. What is the minimum ambient temperature for starting a cold soaked APU on the ground?
    -40 degrees C
  36. The bleed air on the 10th stage valves must be ______ for takeoff and landing if the engine cowl and or wing anti ice systems have been selected __?
    Closed On
  37. Maximum differential pressure positive?
    8.7psi
  38. Maximum differential pressure negative?
    -.5psi
  39. Maximum differential pressure during taxi takeoff and landing?
    .1psi the aircraft must be completely depressurized prior to opening any doors
  40. What is the minimum AGl altitude for use of Flight Spoilers?
    1000 Ft AGL
  41. Flight spoiler use with flaps positioned greater than __ degrees is prohibited?
    30
  42. Taxi Lights must be switched OFF whenever the aircraft is stationary in excess of __ Minutes?
    10
  43. Beacon lights are used for ground recongnition purposes only and must not be used as?
    anti collision lights
  44. Thrust reversers are approved for ______ use only?
    Ground
  45. Maximum reverse thrust is not permitted at airspeeds below _____ KIAS?
    60 below 60KIAS reverse thrust must be reduced to idle
  46. Upon Departure form a wet or contaminated runway what must be done starting at 10000 ft or when SAT falls below 0 degrees C whichever occers later?
    the ailerons must be operated manually every 5000ft until the top of climb
  47. Maximum Operating Altitutde for APU?
    FL370
  48. Maximum APU start Altitude?
    FL300
  49. Maximum Altitude for using APU Bleed Air?
    15000 ft
  50. Maximum altitude for engine starts using APU bleed air?
    13000ft
  51. APU engine Start during Ground Operations?
    No bleed air extraction limitation each engine may be started using the APU as a bleed air source
  52. if both engines are to be started using the APU bleed air then the operating engine thrust must not exceed what?
    70% N2
  53. During single engine operations APU bleed air extraction for an engine start is __________?
    Not Permitted
  54. During double engine failure conditions APU bleed ari extraction for engine starts is permitted however?
    APu bleed air extraction is limited to 13000 ft and below
  55. The flight director ________ be used for takeoff?
    Will NOT
  56. Operation with the autopilot engaged is prohibited at altitudes below_____?
    600 ft AGL except when performing the following 1. for visual and non precision approaches the minumum autopilot height is 400 ft AGL 2. for precision approaches ILS
Author
erau52
ID
151720
Card Set
CRJ200Limitations.txt
Description
pncl
Updated

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