MD Helicopters MD 600
The MD Helicopters MD 600N is a light utility civilian helicopter designed in the United States. It is a stretched eight-seat development of the five-seat MD 520N helicopter.
MD 600N | |
---|---|
A MD 600N with NOTAR | |
Role | Light utility helicopter |
National origin | United States |
Manufacturer | McDonnell Douglas Helicopter Systems MD Helicopters |
First flight | 22 November 1994 |
Status | In service |
Primary user | United States Border Patrol |
Produced | 1995–present |
Unit cost |
US$2.9M[1] |
Developed from | MD Helicopters MD 500 |
Design and development
McDonnell Douglas Helicopter Systems (MD Helicopters since 1999) first announced it was developing a stretched MD 520N in late 1994, at that time designated the MD 630N.[2] The prototype, a modified MD 530F, had made its first flight on November 22, 1994. McDonnell Douglas gave the go-ahead for the production aircraft, redesignated the MD 600N, in March 1995.
McDonnell Douglas stretched the MD 520N fuselage by inserting a plug aft of the cockpit/cabin bulkhead and stretching the NOTAR tail boom. The larger fuselage allows for an extra (middle) row of seats. Other differences compared with the MD 520N include a new six blade main rotor (the MD 520N has a five blade unit) and an uprated Allison (now Rolls-Royce) Model 250 turboshaft.
The prototype was modified to MD 600N standard with a production standard engine and tail boom and flew in November 1995, followed the next month by the first MD 600N production prototype.[2] Certification was awarded on May 15, 1997, and deliveries began that June.
Following the 1997 Boeing/McDonnell Douglas' merger, Boeing sold the former MD civil helicopter lines to Netherlands-based RDM Holdings in early 1999.[2]
On March 8, 2017, MD Helicopters unveiled a concept variant known as the MD 6XX.[3] Unlike the MD 600, the MD 6XX utilizes a traditional tail rotor and shares its T-tail design with the smaller MD 500/530F. It is currently in development, and certification is expected to be awarded in 2020.[4]
Specifications (MD 600N)
Data from The International Directory of Civil Aircraft, 2003–2004[2]
General characteristics
- Crew: 1–2
- Capacity: 8 total
- Length: 35 ft 5 in (11.79 m)
- Rotor diameter: 27 ft 6 in (8.38 m)
- Height: 8 ft 9 in (2.65 m)
- Disc area: 594.0 sq ft (55.2 m²)
- Empty weight: 2,100 lb (952 kg)
- Max. takeoff weight: 4,100 lb (1,860 kg)
- Powerplant: 1 × Allison Model 250-C47 Turboshaft, 600 hp (447 kW)
Performance
- Maximum speed: 152 knots (175 mph, 282 km/h)
- Cruise speed: 135 knots (155 mph, 250 km/h)
- Range: 357 nmi (411 mi, 661 km)
- Service ceiling: 18,700 ft (5700 m)
- Rate of climb: 2070 ft/min (10.5 m/s)
See also
Related development
Aircraft of comparable role, configuration and era
- AgustaWestland AW119 Koala
- Bell 407
- Eurocopter AS350 Écureuil
- Eurocopter EC130
- Marenco Swisshelicopter SKYe SH09
- PZL SW-4 Puszczyk
Related lists
References
- Conklin & de Decker. "MD 600N". Business Jet Traveller.
- Frawley, Gerard: The International Directory of Civil Aircraft, 2003–2004, page 156. Aerospace Publications Pty Ltd, 2003. ISBN 1-875671-58-7.
- Johnson, Oliver. "MD unveils MD 6XX concept helicopter". Vertical Magazine. Retrieved 2019-11-21.
- Trimble, Stephen (2018-02-28). "MD Helicopters delays MD6XX certification to 2020". Flightglobal.com. Retrieved 2019-11-21.
- http://bdnews24.com/bangladesh/2013/02/12/6-injured-in-nganj-copter-crash
- "Moderno helicóptero policial fue presentado por Seguridad Pública". La Nacion. Archived from the original on 2012-12-22. Retrieved 2012-12-19.
- "MD Helicopters Proudly Presents Aircraft to Turkish National Police". helitorque.com. Retrieved 21 February 2013.
- "US Customs & Border Protection puts MD600 fleet into desert storage". helihub.com. Retrieved 24 February 2013.