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Dornier 228-100 - EuroHarmony

Class 1

Dornier 228-100
Climb Chart
Climb Chart
Descent Chart
Descent Chart
Garrett engines
650 nm range
18 pax, 728 lbs cargo capacity

In the late 1970s, Dornier GmbH developed a new kind of wing subsidised by the German Government. Dornier tested it on a modified Do 28D-2 Skyservant and with Pratt Whitney Canada PT6A-110 turboprop engines. At ILA 80, Dornier presented the new aircraft in public. The prototypes were flown on 28 March 1981 and 9 May 1981 for the first time.

Over the years Dornier offered the 228 in upgraded variants and with optional equipment for special missions. In 1998 the production line was stopped for better development of the successor Fairchild-Dornier 328.

We used the Dornier 228 as a Class 1 short haul passenger plane. The detailed Gmax model was made by Björn Büchner.

General Information
Length16.56 m
Wingspan16.97 m
Height4.86 m
EngineGarrett TPE-331
Cruise Speed170 kts
Service Ceiling28,000 ft
Gross Weight6.5 t
Capacity18 pax | 728 lbs
Crew1 pilot
Price2.5M EUR
Operating Information
OEW8,243 lbs
MTOW14,550 lbs
Fuel Capacity630 gal
Fuel Weight4,156 lbs
Long Range AltitudeFL250
Long Range Speed200 kts
Max Speed234 kts
Range (MLoad...MFuel) 650... 715
Engine Thrust2 x 776 SHP
Takeoff RWY Length (Min)2,600 ft
Takeoff RWY Length (Max)3,500 ft
Landing RWY Length1,500 ft
V Rotate / Flaps111kts / 5 deg
V Approach / Flaps99kts / 30 deg
Max climb rate2000 ft/min
Max descent rate-3000 ft/min

Liveries and Downloads

MSFS 2004

Dornier 228-100MSFS 2004


Dornier 228-100MSFS X