Dornier Do 27
From Wikipedia, the free encyclopedia
Do 27 | |
---|---|
Do 27 in Swiss Air Force markings |
|
Type | STOL light communications aircraft |
Manufacturer | Dornier Flugzeugbau GmbH |
Maiden flight | 27 June 1955 |
Status | In civilian use |
Primary user | Luftwaffe |
Developed from | Dornier Do 25 |
The Dornier Do 27 was a German single-engine STOL-utility aircraft, manufactured by Dornier GmbH (later DASA Dornier, Fairchild-Dornier). Configuration was a classic high-wing, "tail-dragger" aircraft with fixed landing gear.
Contents |
[edit] History
The Do 27 was developed from the Do 25, an aircraft originally designed to a Spanish military requirement for a light utility aircraft.
The Do 27 seated four to six and the original prototype first flew in Spain on 27 June 1955.[1] Most production aircraft were built in Germany, the first taking flight on 17 October 1956. The remainder (50) were manufactured in Spain by Construcciones Aeronauticas (CASA) as the CASA-127.
The German Luftwaffe and German Army ordered a total of 428 of the Do 27A and Do 27B (with dual controls).[2]
A later version with the same basic specifications but equipped with wider track landing gear was known as the Do 27Q-5. The aircraft was offered on twin floats as the Do 27S-1 and with a larger engine (340 hp Lycoming Engines GSO-480-B1B6) and a three-bladed propeller as the Do 27H-2.
In addition to the military operators in Germany and Spain, a few were manufactured for other military and civilian operators.
The Do 27 was notable for being the first mass-produced aircraft in Germany after World War II. It was appreciated for its relatively wide, comfortable cabin and excellent short-field performance.
[edit] Variants
- Do 27A : Five-seat single-engine STOL utility transport aircraft.
- Do 27B : Dual-control version.
- Do 27H : Civil or military version, powered by a 340-hp (254-kW) Avco Lycoming GSO-480 piston engine.
- Do 27Q-5 : Six-seat civil version.
- Do 27Q-5(R) : Restricted category version of the Do 27Q-5.
- Do 27Q-6 : Similar to the Do 27Q-5.
- Do 27S : Floatplane version. Only one prototype was built.
- Do 27T : One prototype fitted with a Turbomeca Astazou II turboprop engine.
[edit] Military Operators
- Angola
- Belgium
- Belize
- Burundi
- Republic of the Congo
- Germany
- Guinea-Bissau
- Israel
- Nigeria
- Portugal
- Rwanda
- Spain
- Sudan
- Sweden
- Switzerland
- Turkey
[edit] Specifications (Do 27Q-5)
Data from Macdonald Aircraft Handbook [3]
General characteristics
- Crew: One or two
- Capacity: 4-6 passengers
- Length: 9.60 m (31 ft 6 in)
- Wingspan: 12 m (39 ft 5 in)
- Height: 2.80 m (9 ft 2 in)
- Wing area: 19.4 m² (208.7 ft²)
- Empty weight: 1072.8 kg (2,365 lb)
- Max takeoff weight: 1,850.6 kg (4,080 lb)
- Powerplant: 1× Lycoming GO-480-B1A6 6-cylinder piston engine, 201.3 kW (270 hp)
Performance
- Never exceed speed: 333 km/h (180 knots, 207 mph)
- Maximum speed: 232 km/h (125 knots, 144 mph)
- Cruise speed: 211 km/h (114 knots, 131 mph)
- Stall speed: 74 km/h (40 knots, 46 mph)
- Range: 1,287 km (695 nm, 800 miles)
- Service ceiling 3,292 m (10,800 ft)
[edit] See also
Related development
Comparable aircraft
Related lists
[edit] References
[edit] Notes
[edit] Bibliography
- Donald, David (Editor) (1997). The Encyclopedia of World Aircraft. Aerospace Publishing, p.341. ISBN 1-85605-375-X.
- Green, William. Macdonald Aircraft Handbook. London. Macdonald & Co. (Publishers) Ltd., 1964.
- Jackson, Paul A. German Military Aviation 1956-1976. Hinckley, Leicestershire, UK: Midland Counties Publications, 1976. ISBN 0-904597-03-2.
[edit] External links
|
|
|