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From Wikipedia& The International Directory of Civil Aircraft

Photo by Connector

 

Specifications

ENGINE:
(2) Thielert Centurion 1.7 avtur burning turbo diesel four cylinder engines rated at 135 hp

PROPELLER:
Three blade MTV-6A-129 hydraulic constant speed props

WEIGHTS:
Empty weight: 2,270 lbs.
Max takeoff weight: 3,673 lbs.
Payload: 1,366 lbs.

Apple StoreDIMENSIONS:
Length: 27 ft 8 in
Wingspan: 44 ft 0 in
Height: 8 ft 5 in
Wing area: 177.2 ft²

PERFORMANCE FIGURES:
Cruising Speed: 180 kt
Service Ceiling: 20,000 ft
Range: 1061 nm / 1,485 with optional tanks
Initial rate of climb: 1,700 ft/min

 

 

FOR TRAINING PURPOSES ONLY

 

 


 

The Diamond DA42 Twin Star is a four seat, twin engine, propeller-driven airplane manufactured by Diamond Aircraft Industries.

The DA42 Twin Star was certified in Europe in 2004 and in the United States in 2005.

The DA42 is unusual in that it is powered by two Thielert Centurion 1.7 diesel engines. In the United States, Jet-A or Jet-A1 fuel (or premix) is used. Fuel consumption is about half that of avgas powered light twins of comparable gross weight.

The airplane is made of carbon composite material and equipped with a Garmin G1000 glass cockpit. A proof-of-concept version powered by two 180 hp Lycoming IO-360 engines also exists.

The DA42 Twin Star was the first diesel-powered aircraft to make a non-stop crossing of the North Atlantic, in 12.5 hours, with an average fuel consumption of 5.74 gallons per hour (2.87 gallons per hour per engine).

 

 

Articles:
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ILA 2006 - Diamond DA-42 Twin Star
Da42 Low pass

 

Photo by Robert Beaver


Photo by Moke Promma

 


Photo by Jerome Mervelet