Dornier Do 27

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.

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. 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 (Air Force) and Heer (Army) ordered a total of 428 of the Do 27A and Do 27B (with dual controls).

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 as a twin-float seaplane, the Do 27S-1, and with a larger engine (254 kW/340 hp Lycoming GSO-480-B1B6) and a three-blade 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.

Variants

File:Do 27 D-ENTE.JPG

Do 27 used by Bernhard Grzimek

• Do 27A : Five-seat single-engine STOL utility transport aircraft.
• Do 27B : Dual-control version.
• Do 27H : Civil or military version, powered by a 254 kW (340 hp) 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.

Military Operators

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Specifications (Do 27Q-5)

File:Aircraft Dornier Do-27 B LH1.jpg

Luftwaffe Do 27 on display in the Deutsches Museum

Data from Macdonald Aircraft Handbook

General characteristics

• Crew: 1 or 2
• 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: 1,073 kg (2,365 lb)
• Max takeoff weight: 1,850 kg (4,080 lb)
• Powerplant: 1× Lycoming GO-480-B1A6 6-cylinder piston engine, 201 kW (270 hp)

Performance

• Never exceed speed: 333 km/h (180 kn, 207 mph)
• Maximum speed: 232 km/h (125 kn, 144 mph)
• Cruise speed: 211 km/h (114 kn, 131 mph)
• Stall speed: 74 km/h (40 kn, 46 mph)
• Range: 1,287 km (695 nmi, 800 mi)
• Service ceiling: 3,290 m (10,800 ft)

See also

Related development

• Dornier Do 25
• Dornier Do 28

Comparable aircraft

• PZL-104 Wilga
• Scottish Aviation Pioneer

Related lists

• List of military aircraft of Germany

References

Bibliography

• Donald, David (Editor) (1997). The Encyclopedia of World Aircraft. Aerospace Publishing. 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.

External links

Wikimedia Commons has media related to:

Dornier Do 27

• Welcome to Do 27
• Do 27 Alter Tiger, S/N 451

This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Dornier Do 27".