• DA42
  • Specs & Options
AIRCRAFT ITEM INFORMATION
Engine 2x Lycoming I0-360 counter rotating engines equipped with PowerFlow tuned exhaust system
Horsepower 360 hp total
Propellers 2x Hartzell 2-blade aluminum constant speed with feathering capability
Expected availability in North America Q1 2009
Airworthiness category Normal
Length 28 ft 1 in
Height 8 ft 2 in
Wing span 44 ft
Maximum take-off weight 3,935 lbs
Useful load 1,179 lbs +/-3%
Fuel capacity, total / usable 79 gal / 76 gal
Fuel 100 LL Avgas
Take-off distance, 50-foot obstacle 1,500 ft
Landing distance, 50-foot obstacle 1,877 ft
Rate of climb, sea level 2,000 fpm
Maximum demonstrated operating altitude 18,000 ft
Maximum single-engine ceiling (standard day) 7,500 ft +
Maximum cruise speed 180+ ktas
Economy cruise speed at 55% power 140 ktas
Maximum landing gear extension speed 195 kias
Maximum demonstrated crosswind 20 kts
Range, 55% power (30 min reserve) 700 nm
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.