| Picture |
|
| Manufacturer |
McDonnell Douglas
|
| Type |
MD600N
|
| Introduced |
5/15/1997
|
| In production? |
Yes
|
| Units produced |
0
|
| Price US $ |
1,900,000.00
|
| Overall Length |
35.9 ft
|
| Length |
29.5 ft
|
| Height |
9.3 ft
|
| Width |
4.6 ft
|
| |
|
| |
|
| Description |
The MD600N is a lightweight helicopter developed from the MD520N. Similar to its ancestor, it is equipped with a NOTAR anti-torque system (NO TAil Rotor). The main differences are the stretched fuselage to accommodate up to eight people and the longer tail boom.
|
| Advertisement |
|
| Design features |
- NOTAR anti torque device
- Larger fuselage by means of plug aft of cockpit
- Stretched tailboom
|
|
The MD600N is a lightweight helicopter developed from the MD520N. Similar to its ancestor, it is equipped with a NOTAR anti-torque system (NO TAil Rotor). The main differences are the stretched fuselage to accommodate up to eight people and the longer tail boom.
|
|
- Advertisement -
|
Design features:
- NOTAR anti torque device
- Larger fuselage by means of plug aft of cockpit
- Stretched tailboom
|
| Persons |
8
|
| Max. Range |
262 mi
|
| Cruise Speed |
154 mph
|
| Max. Speed |
155 mph
|
| Max. rate of Climb |
2100 ft/min
|
| HOGE ceiling |
6000 ft
|
| Service Ceiling |
20000 ft
|
| Gross Weight |
4100 lb
|
| Empty Weigt |
2100 lb
|
| Useful Load |
2000 lb
|
| Fuel Capacity |
114 gallons
|
| Number of Engines |
1
|
| Engine Type |
Turbine
|
| Engine Code |
Allison / Rolls-Royce 250-C47M
|
| Horse Power |
600
|
| Rotorhead |
Fully articulated six-blade system
|
| Number of rotorblades |
6
|
| Rotor Diameter |
27.5 ft
|
| Number of tail rotorblades |
0
|
| Tailrotor Diameter |
0 ft
|
|