• DA40 XLT
  • Specs & Options
DA40 XLT Specifications*
AIRCRAFT ITEM INFORMATION
Engine Lycoming IO-360-M1A
Horsepower 180 hp
Propeller Hartzell 2-blade scimitar structural composite propeller
Airworthiness category Normal and utility
Length 26 ft 5 in
Height 6 ft 6 in
Wing Span 39 ft 6 in
Maximum takeoff weight 2,645 lbs
Useful load 860 lbs (standard equipped airplane)
Fuel capacity, usable 50 gal
Fuel AVGAS 100 LL
Takeoff distance, ground roll 1,175 ft
Takeoff distance, 50-foot obstacle 1,700 ft
Landing distance, ground roll 1,155 ft
Landing distance, 50-foot obstacle 2,093 ft
Rate of climb, sea level 1,120 ft/min
Maximum operating altitude 16,400 ft
Maximum speed 157 ktas
Cruise speed at 75% 150 ktas/10 gal/hr
Stall speed, full flaps 49 kias
Maximum demonstrated crosswind 20 kts
Range, at 75% 45 minute reserve 720 nm
Range, at 55% 45 minute reserve 785 nm
* Performance specifications may vary depending on model and equipment selected 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.