• DA42
  • Specs & Options
Engine Twin TAE Centurion 2.0 Turbo Diesel
Horsepower 270 hp total
Propellers MT 3-blade composite constant speed, full-feathering
Airworthiness category Normal
Length 28 ft 1 in
Height 8 ft 2in
Wing Span 44 ft
Maximum takeoff weight 3,935 lbs
Useful load 1,174 lbs
Fuel capacity, usable standard 50 US gal
Fuel capacity, usable extended 72 US gal
Fuel Jet A-1
Takeoff distance, ground roll* 1,130 ft
Takeoff distance, 50-foot obstacle 1,730 ft
Landing distance, ground roll 1,069 ft
Landing distance, 50-foot obstacle 1,877 ft
Rate of climb, sea level* 1,280 ft/min
Maximum operating altitude 18,000 ft
Maximum SE ceiling (standard day) 10,000 ft
Cruise speed at 80% 168 kts/12.5 gal/hr total
Economy at 60% 151 ktas/8.8 gal/hr total
Stall speed, full flaps gear down 56 kias
Stall speed, clean 62 kias
Maximum landing gear operating speed 194 kts
Maximum demonstrated crosswind 20 kts
Range, at 80% extended fuel 917 nm
Range, at 60% extended fuel 1,129 nm
* At 3,748 lbs takeoff weight Aircraft shown in all marketing materials, websites or brochures, may contain non-standard features, optional equipment or equipment not yet certified by a given authority, and which, if available, may be subject to additional cost. Actual weight and balance information will vary depending on options installed on aircraft. Only aircraft specific weight and balance data alone should be consulted for flight planning. Aircraft specifications, weights, equipment lists, color choices, model references and other representations made verbally or appearing on websites, in brochures or other marketing materials are for general information purposes and do not constitute an inducement to enter into, or form any part of, an agreement for the purchase and sale of aircraft. Only statements and representations set out in actual contracts entered into with Diamond Aircraft or its authorized distributors may be relied upon. Prices and specifications are subject to change without notice at any time prior to delivery.