Bell 407GX - Limitation

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Author:
mda
ID:
293823
Filename:
Bell 407GX - Limitation
Updated:
2015-02-26 16:00:06
Tags:
Bell 407GX Limitations
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Description:
Helicopter Bell 407GX, Limitations
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  1. Maximum continuous power
    • 93.5% Torque
    • (630 SHP)
  2. Takeoff power (5 minute limit)
    • 100% Torque
    • (674 SHP)
  3. Maximum airspeed (VNE)
    140 KIAS
  4. Maximum airspeed for Autorotation
    100 KIAS
  5. Maximum airspeed at 93.5 to 100% Torque
    100 KIAS
  6. Maximum airspeed with doors off
    (any combination removed)
    100 KIAS
  7. When takeoff landing is in shaded area of the gross weight lateral CG limits
    100 KIAS
  8. Autorotation
    Minimum rate of descent
    55 KIAS
  9. Autorotation
    Maximum glide distance
    80 KIAS
  10. Best rate of climb
    60 KIAS
  11. Hydraulic failure
    70 - 100 KIAS
  12. Maximum operating altitude
    • 20,000ft HD or
    • 20,000ft HP whichever is lower
  13. (FMS-28) 5,001lbs (2273kg) to 5,250lbs (2381kg) internal GW
    Maximum altitude for takeoff, landing and in ground effect (IGE) maneuvers
    11,000ft HD
  14. Minimum gross weight for flight
    2,650lbs (1202kg)
  15. Maximum gross weight (internal (basic aircraft)
    5,000lbs (2268kg)
  16. Maximum gross weight (internal (basic aircraft)
    5,250lbs (2381lbs)
  17. Maximum gross weight (external)
    6,000lbs (2722kg)
  18. Cargo hook rated capacity
    2,650lbs (1202kg)
  19. Maximum fuel capacity
    130 US-Gallons (492 liters)
  20. With auxiliary fuel tank installed
    149 US-Gallons (564 liters)
  21. Engine oil capacity
    6 US-Quarts (5.7 liters)
  22. Transmission oil capacity
    5 US-Quarts (4.7 liters)
  23. Tail rotor gearbox oil capacity
    0.33 US-Quarts (0.31 liters)
  24. Hydraulic oil capacity (System & Reservoir)
    1.68 US-Quarts (1.59 liters)
  25. Overall Length
    41ft 8.5in
  26. Overall Height
    10ft 3.8in
  27. Main Rotor
    Number of Blades
    4
  28. Main Rotor
    Diameter
    35ft
  29. Main Rotor
    Chord
    10.75in
  30. Main Rotor
    Twist
    -13°
  31. Engine to Main Rotor Gear Ratio
    15.23 to 1
  32. Main Rotor RPM at 100%
    413 RPM
  33. Tail Rotor
    Number of Blades
    2
  34. Tail Rotor
    Diameter
    65in
  35. Tail Rotor
    Chord
    6.40in
  36. Engine to Tail Rotor Gear Ratio
    2.53 to 1
  37. Tail Rotor RPM at 100%
    2500
  38. Passenger / Cargo Door Opening
    Height
    39in
  39. Passenger / Cargo Door Opening
    Width
    36in
  40. Litter Door
    25in
  41. Cargo Area Volume
    Main Cargo Area
    85 cubic ft
  42. Cargo Area Volume
    Baggage Compartment
    16 cubic ft

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