CE750 Limitations

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Author:
mbender1
ID:
58208
Filename:
CE750 Limitations
Updated:
2011-02-08 13:20:50
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CE750 Limitations
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CE750 Limitations
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  1. Max Ramp Weight
    36,000 lbs.
  2. Max Takeoff Weight
    35,700 lbs.
  3. Max Landing Weight
    31,800 lbs.
  4. Max Zero Fuel Weight
    24,400 lbs.
  5. Max Fuel Imbalance (Normal)
    400 lbs.
  6. Max Fuel Imbalance (Emergency)
    800 lbs.
  7. Tailcone Baggage Compartment
    700 lbs.
  8. Ski Compartment
    75 lbs.
  9. Vmo (below 8000 ft.)
    270 KIAS
  10. Vmo ( 8000 ft. to 30,650 ft.)
    350 KIAS
  11. Mmo (above 30,650 ft.)
    .92 Mach (indicated)
  12. Mmo (Mach Trim Inop)
    .82 Mach (indicated)
  13. Turbulent Air Penetration Speed
    300 KIAS/ .90 Mach
  14. Max Tire Groundspeed
    182 KIAS
  15. Max Slat Extended Speed
    250 KIAS
  16. Vfe 5 degrees
    250 KIAS
  17. Vfe 15 degrees
    210 KIAS
  18. Vfe FULL
    180 KIAS
  19. Vlo / Vle
    210 KIAS
  20. Max Speed Brake Extended Speed
    No Limit
  21. Min. Speed Brake Extended Speed
    Vref + 15 KIAS
  22. Min. Speed in Icing
    200 KIAS
  23. Max Operating Altitude
    FL510
  24. Max TakeOff / Landing Altitude
    14,000 ft.
  25. Max Altitude for Gear / Flap Extension
    FL180
  26. Max Temp. Takeoff & Landing
    ISA + 39* C
  27. Min. Temp. Takeoff & Landing
    -54* C
  28. Max Tailwind Component
    10 kts.
  29. Crosswind Component
    21 kts. (demonstrated)
  30. Manual Reversion
    10 kts. crosswind
  31. Slat Asymmetry
    10 kts. crosswind
  32. Main Generator Limits (up to FL410)
    400 amps
  33. Main Generator Limits (above FL410)
    300 amps
  34. APU Generator Limits (ground)
    300 amps
  35. APU Generator Limits (flight)
    200 amps
  36. Cold Soaked Battery Temp
    -20* C

    Battery should be removed and placed in a warm environment for aircraft parked at these temps.
  37. Engine Type
    Allison AE 3007C Turbofan
  38. Min. Start Duct Pressure
    25 psi (30 psi recommended)
  39. Starter Limit
    3 consecutive normal starts followed by 25 minutes of cooling
  40. Approved Oil
    Mobil Jet II
  41. Min. Oil Temp. for Start
    -40* C
  42. Max Reverse Thrust
    70% N1
  43. Fuel Type
    Jet A
  44. Min. Fuel Temp for Start
    -37* C
  45. Max Fuel Temperature
    +98.9* C
  46. Center wing transfer must be initiated prior to.....
    .....3100 lbs. per side wing fuel
  47. Simultaneous use of crossfeed and center-to-wing tank transfer is prohibited when wing fuel quantity is....
    ....2900 lbs. or less per side. Fuel lateral imbalance will result.
  48. Approved Hydraulic Fluid
    Skydrol (Purple)
  49. APU not approved for....
    ....unattended ground operation
  50. Max altitude for APU start
    31,000 ft.
  51. Max Altitude for APU operation
    31,000 ft.
  52. Max Starter Duty Cycles (APU)
    Maximun of 6 consecutive successful starts at 10 minute intervals
  53. APU compartment inspection is required after.....
    .....an automatic APU shutdown
  54. Crew O2 masks are not approved for sustained operation at a cabin altitude greater than....
    ....40,000 ft.
  55. Pax O2 masks are not approved for sustained operation at a cabin altitude greater than....
    25,000 ft.
  56. Nose Tire Inflation
    130 +/- 5 psig, unloaded.

    Unloaded weight is while the a/c is on jacks. Loaded weight will be 2 - 5 psig higher.
  57. Minimum Single Engine Enroute Climb Speed
    190 KIAS
  58. Min. Altitude for In-Flight use of Speed Brakes
    500' AGL
  59. Min. Wing Fuel per Tank for Takeoff
    500 lbs.
  60. Takeoff in High Idle is.....
    Prohibited (except for touch and go)
  61. Auto Pilot Minimum Use Height :

    Cruise:

    Precision: Cat I

    Non Precision:
    1000' AGL

    170' AGL

    400' AGL
  62. Auto Pilot coupled operation with single operational or displayed AHRS or IRS is.....
    Prohibited
  63. Auto pilot coupled ILS approached with flaps up are....
    Prohibited
  64. Normal Cabin Pressure Limitation
    9.7 psi Maximum Differential
  65. Length
    72.33'
  66. Height
    18.36'
  67. Wing Span
    63.45'
  68. Horizontal Stabalizer
    26.09'
  69. Wheel Base
    28.67'
  70. Stance
    10.55'
  71. Wing Sweep

    Horizontal Stabilizer Sweep
    40 *

    43 *
  72. Each engine produces _________ pounds of thrust at sea level?
    6442 lbs.
  73. High By Pass Ratio
    5:1
  74. Bleed Air extracted from the ____ and ____ stage of the compressor section.
    8th and the 14th
  75. Fuel Capacity
    13,000 lbs.
  76. Wing Fuel Tank Capacity
    3500 lbs.
  77. Center Tank Capacity
    6000 lbs.
  78. Fuel Burn is approx. ______for the first hour, and then approx. ______ for each hour there after.
    2500 lbs/hr

    1800 - 2000 lbs/hr

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