MD 600N

The NOTAR helicopter built for agility and reduced noise.

Overview

MD Helicopters United States ICAO: MD60 1995–Present Active $2.9 million

The MD 600N is a light utility helicopter that incorporates the NOTAR anti-torque system instead of a conventional tail rotor. Introduced in the 1990s, it emphasizes safety and low external noise. The aircraft is used in civil and law enforcement roles.

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Specifications

Units
Engine
Engine type
Turboshaft
Power
603 shp · 450 kW
Avionics
Garmin Avionics
Wing tips
No winglets
Seats
8
Crew
Cabin width
4 ft 0 in  ·  1.22 m
Cabin height
4 ft 0 in  ·  1.22 m
Cabin length
6 ft 7 in  ·  2.00 m
Exterior length
37 ft 1 in  ·  11.30 m
Tail height
9 ft 10 in  ·  3.00 m
Fuselage diameter
4 ft 7 in  ·  1.40 m
Wing span
27 ft 6 in  ·  8.38 m
Baggage volume
35 ft³  ·  1.0 m³
Gross weight
Empty weight
Max takeoff weight
4,500 lb  ·  2,050 kg
Max landing weight
Max payload
2,400 lb  ·  1,100 kg
Fuel capacity
120 gal · 400 L · 400 kg (Jet A)
Max cruise speed
148 kt  ·  170 mph  ·  274 km/h
Maximum speed
Cruise speed
Approach speed
Range
423 nm  ·  490 mi  ·  780 km
Fuel burn
2.33 nm/gal  ·  1.14 km/L
Ceiling
18,700 ft  ·  5,700 m
Rate of climb
2,100 ft/min  ·  11 m/s
Takeoff distance
Landing distance
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MD Helicopters MD-600N.

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Operational Context

MD 600N — light NOTAR utility helicopter

The MD 600N first flew in 1997 and entered service shortly thereafter. It builds upon earlier MD Helicopters designs while adopting the fan-driven NOTAR system for anti-torque control. The configuration reduces tail rotor hazards and improves ground safety.

A single turboshaft engine producing approximately 808 shaft horsepower powers the helicopter. Cruise speed approaches 140 knots (259 km/h). Maximum takeoff weight exceeds 4,100 pounds (1,860 kg).

The MD 600N has served in executive transport, police operations, and light utility roles. Its unique tail design distinguishes it from conventional helicopters. The aircraft continues to operate in specialized applications worldwide.