• DA42
  • Specs & Options
AIRCRAFT ITEM INFORMATION
Engine 2x Lycoming I0-360 fuel injected counter rotating engines equipped with PowerFlow tuned exhaust system
Horsepower 360 hp total
Propellers 2x MT 3-blade composite hydraulic constant speed with unfeathering accumulator
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 1,180 lbs
Fuel capacity, total / usable 79 gal / 76.4 gal
Fuel 100 LL Avgas
Take-off distance 1,590 ft
Take-off distance, 50-foot obstacle 2,450 ft
Landing ground roll 1,210 ft
Landing distance, 50-foot obstacle 2,410 ft
Rate of climb (MTOW, SL, ISA, Vy: 90kts) 1,400 fpm
Maximum demonstrated operating altitude 18,000 ft
Maximum single-engine ceiling (ROC <50 fpm) 6,400 ft
Maximum speed (Take off power, SL, ISA) 178 kts
Cruise speed at 75% power 162 ktas
Maximum Range (no reserve) 800+ 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.