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    1997 MD HELICOPTERS 600N1997 MD HELICOPTERS 600N
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    1997 MD HELICOPTERS 600N

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    Aircraft Summary

    General
    Year
    1997
    Manufacturer
    MD HELICOPTERS
    Model
    600N
    Serial Number
    0013
    Condition
    Used
    FlightRules
    VFR
    Based at
    SANTA CATARINA
    Description
    General features

Crew: 1–2
Capacity: 6 total
Length: 35ft 5in. (10.80m)
Height: 8ft 9in. (2.67m)
Empty weight: 2,100 lb (953 kg)
Maximum takeoff weight: 4,100 lb (1,860 kg)
Powerplant: 1 × Allison Model 250-C47 turboshaft engine, 600 shp (450 kW)
Main rotor diameter: 27 ft 6 in. (8.38m)
Main rotor area: 594.03 square feet (55,187 m 2 )

Top speed: 152 kt (175 mph, 282 km/h)
Cruising speed: 135 kt (155 mph, 250 km/h)
Range: 357 nautical miles (411 mi, 661 km)
Service ceiling: 18,700 feet (5,700 m)
Ascent rate: 2070 ft/min (10.5 m/s)

McDonnell Douglas MD600 helicopter

• Year of manufacture: 1997
• Seats: 6 (1+5)
• Total hours: 1030hs
• Autonomy: 2h30
• Consumption: 160L/h
• Turbine: Rolls Royce C47 (same Bell 407 turbine with fadec)
• Cruising Speed: 135kt
• Air conditioning
• Six main rotor blades NOTAR technology
• Wire cut protection system
• Yaw extinguisher Stabilization boost system
• Quick Removal Door Hinges
• Particle separator engine
 

Avionics:
• Garmin GNS-430W
• Garmin AERA 660
• Garmin GTX-330
• Garmin AERA 760
• Garmin GI-106A
    Airframe
    Total Time
    1030
    Max Takeoff Weight
    4,100.6 lb
    Basic Empty Weight
    2,101.01 lb
    Max Cruise Speed
    135 knots
    Complete Logs
    Yes


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