Falcon 50EX Limitations

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Author:
Pilot
ID:
185028
Filename:
Falcon 50EX Limitations
Updated:
2012-11-23 18:31:11
Tags:
Falcon DA50 DA50EX Limitations
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Falcon 50EX Limitations
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  1. VA
    210
  2. VFE Slats
    200 KIAS
  3. VFE Slats + Flaps 20°
    190 KIAS
  4. VFE Slats + Flaps 48°
    175 KIAS
  5. VLE/MME
    220 KIAS / .75 Mach
  6. VLO/MLO
    190 KIAS / .70 Mach
  7. VMCA
    82.5 KCAS
  8. VMO/MMO
    • Sea Level: 350 KIAS
    • 0' MSL to 10K': 350 - 370 KIAS
    • 10K' to 24K': 370 KIAS
    • Above 24K': .86 Mach
  9. AUTO SLAT Light On
    270 KIAS
  10. Cracked Windshield
    230 KIAS
  11. DV Window Open
    180 KIAS
  12. Either/Both Hyd Inop
    260 KIAS / .76 Mach
  13. Mach Trim Inop w/ No A/P
    .78 Mach
  14. Thrust Reverser Deployed
    230 KIAS
  15. Tire Speed
    180
  16. Turbulent Air Penetration
    280 KIAS / .76 Mach
  17. VWWO - Windshield Wiper Ops
    205 KIAS
  18. TFE 731-40-1C 
    Ground Start ITT
    991 °C
  19. TFE 731-40-1C
    Airstart Start ITT
    991 °C
  20. TFE 731-40-1C
    Takoff ITT
    1013 °C for 5 Minutes Max
  21. TFE 731-40-1C
    Max Continuous ITT
    991 °C
  22. TFE 731-40-1C
    Max Cruise ITT
    974 °C
  23. TFE 731-40-1C
    Takeoff/Max Continuous N1%
    100.1%
  24. TFE 731-40-1C
    Takeoff/Max Continuous N2%
    101.0%
  25. TFE 731-40-1C
    Transient Max Allowable N1%
    100.5% for 5 Seconds Max Allowable
  26. TFE 731-40-1C
    Transient Max Allowable N2%
    102.5% for 5 Seconds Max Allowable
  27. TFE 731-40-1C
    Max RPM in Reverse
    84.0% N1
  28. TFE 731-40-1C
    Grnd Start from 10% N2 to Lightoff
    10 Seconds Maximum
  29. TFE 731-40-1C
    Grnd Start from Lightoff to Idle
    60 Seconds Max
  30. TFE 731-40-1C
    Windmilling Airstart
    No Time Limit
  31. TFE 731-40-1C
    Start Assist Airstart from Fuel Flow N2 to 60% N2
    45 Seconds Maximum
  32. TFE 731-40-1C
    Thrust Rating
    • 3700 Lbs - Takeoff
    • 3641 Lbs - Max Continuous
  33. TFE 731-40-1C
    Oil Temperature
    • 0' MSL to FL300: 127 °C
    • Above FL300: 140 °C
    • Transient: 149 °C
    • Minimum: -40 °C
    • Min above Idle: +30 °C
  34. TFE 731-40-1C
    Oil Pressure
    • Takeoff or Max Continuous: 65-80 psi
    • Idle: 50-80 psi
    • Transient: 100 psi Max (<3 Minutes)
  35. Max Ramp Wt
    40,780 Lbs
  36. Max Toff Wt
    40,780 Lbs
  37. Max Ldg Wt
    35,715 Lbs
  38. Max Zero Fuel Wt
    25,570 Lbs
  39. Min Flight Wt
    18,959
  40. Max Baggage Weight
    2200 Lbs
  41. Max Baggage Loading
    123 Lbs/ft2
  42. Enroute Max Alt
    49,000'
  43. Max Alt w/ Slats or Flaps Extended
    20,000'
  44. Max Alt for Stby Hyd Pump Inop
    45,000'
  45. Max Gs
    • Flaps Up: +2.6 to -1
    • Flaps Down: +2 to 0
  46. Max Δ P: Overpressure Relief Valve
    9.5 psi
  47. Max Δ P: Baggage Overpressure Relief Valve
    9.7 psi
  48. Cabin Altitude Limiter
    14,500'
  49. Battery Temp
    • > 150 °F
    • or
    • > 160 °F with digital BAT TEMP indicator
  50. Gen Max Voltage
    32 V
  51. Gen Max Amp
    • Transient (1 Min Max): 350 A
    • Up to 39,000': 300 A
    • Above 39,000': 250 A
  52. Fuel Quantity HI Level Feeders
    15,514 lbs
  53. Fuel Quantity LO Level Feeders
    13,213 lbs
  54. Regulation Level for all Feeder Tanks is
    609 lbs (91 gallons)
  55. Fuel Quantity Indicator Selector switch should normally be left in the _____ position
    REAR
  56. Transfer Pumps should be switched ___ when no fuel left in wing tanks
    OFF
  57. With illumination of the ____ ____ light, stop pressure refueling
    STOP FUELING
  58. Max Feed Pressure (SPR)
    50 psi (3.5 bars)
  59. In extended cruise in cold temps, if necessary, ____ ____ or ____ ____ to raise TAT
    • Increase Mach
    • Decrease Altitude
  60. Engine Anti-Ice should be ON when total temp is below ___ °C in visible moisture
    +5 °C
  61. Engine Anti-Ice should be OFF when total temp is above ___ °C in visible moisture
    +10 °C
  62. Wing Anti-Ice must be OFF when total temp is above ___ °C in visible moisture
    +10 °C
  63. Both Pilot's & Copilot's Windsheild Heat switches should be set to the ___ ___ ___
    Same operating position
  64. Do not operate ____ Anti-Ice on the ground except for Maintenance Checks cnducted in accordance with the Maintenence Manual.
    Wing Anti-Ice
  65. Airbrake control handle should be held until proper ____ /____ is ascertained
    extension / retraction
  66. If ___ or ___ is inadvertantly exceeded, do not hesitate to use the ____
    • Vmo / Mmo
    • Airbrakes
  67. In flight, extend ____ to next detent only after cessation of movement to the ____ ____
    • Flaps
    • previous position
  68. Do not extend flaps if the ___ green light is off
    Slats
  69. CAUTION: Above ____ feet, do not establish or maintain flaps or slats extended
    20,000'
  70. Airport Pressure Altitude
    -1,000' to 14,000'
  71. Max Water depth for Takeoff
    3/4"
  72. Max Demonstrated Crosswind
    30 Kts
  73. Max Runway Slope
    +2.5% to -2.5%
  74. Limiting Tailwind Component
    10 Kts
  75. Engine Syncronizer must be OFF for ___, ___ & ___
    Takeoffs, Landings & Missed Approaches
  76. Engine Computers must be ____ for Takeoff
    Operative
  77. Engine low pressure rotor speed ___ is the thrust setting parameter
    N1
  78. Takeoff and Max Continuous thrust must be based on ___ values given in the AFM, Section V, unless ___ is limiting
    N1; ITT
  79. Min O2 below 10,000' without passengers
    650 psi
  80. Min O2; 2 Crew with 10 or less pax to FL410
    700 psi
  81. Min O2 above FL410
    Check Ops Manual
  82. APU Max EGT Rated
    680 °C
  83. APU Max EGT Allowed
    732 °C
  84. APU Max Generator Load
    300 Amp
  85. APU Max Speed Rated
    100%
  86. APU Max Speed Allowed
    110%
  87. APU approved for ____ use only
    Ground
  88. APU bleed must be ___ for Engine of Airframe Anti-Ice checks
    OFF
  89. Discontinue APU Start (Stop pushbutton) if T5 does not rise within ___ seconds.
    10
  90. Wait ___ minutes before attempting a 2nd APU start
    5

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