Dornier Do 28

· Dornier · 2 × Lycoming O-540

Airplanes

Length

11.41 m

Flat Wing Span

15.55 m

Height

3.9 m

Flat Wing Area

29 m²

Flat Wing Aspect Ratio

8.3

Max Seating

Cruise Speed

241 km/h

Max Speed

325 km/h

Max Ceiling

7680 m

Number of Engines

Aircraft Engine

First Flight

1959-04-29

Number Built

Maximum Take-Off Weight

4.015 t (paragliders: kg)

Total Fuel Capacity

893

Maximum Range

2950 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Dornier Do 28	4.015	893	2950

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Beechcraft Queen Air	Lycoming O-540	10.668	15.24	9	Compare
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Reims-Cessna F406 Caravan II		11.89	15.09	12	Compare
Britten-Norman Defender		12.2	16.15	16	Compare
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All data (26 fields)

Name: Dornier Do 28
Manufacturer: Dornier
Description: Dornier Do 28 is a type designation that comprises two different twin-engine STOL utility aircraft, manufactured by German company Dornier Flugzeugbau GmbH.
First Flight: 1959-04-29
Designer: Dornier
Type: STOL light utility aircraft
Length (m): 11.41
Height (m): 3.9
Cockpit Crew: 1
Max Seating: 12
Max Speed (km/h): 325
Cruise Speed (km/h): 241
Min Speed (km/h): 104
Max Ceiling (m): 7680
Rate of Climb (m/s): 5.334
Capacity Description: 12 or 13 passengers
Number Built: 28
Powerplant Description: 2 × Lycoming IGSO-540-A1E air-cooled flat-six engines, 283 kW (380 hp) each
Primary Users: German Air Force
Status: In civilian and military use
Wikipedia Article (URL): en.wikipedia.org/wiki/Dornier_Do_28
Flat Wing Span (m): 15.55
Flat Wing Area (m²): 29
Flat Wing Aspect Ratio: 8.3
Aircraft Engine: Lycoming O-540
Number of Engines: 2