DA-42 Page  Interior  Panel  Engine  Propeller  Diamond Aircraft

  It offers pilot workload- reducing single-lever power controls for each engine, exceptionally low fuel consumption and all glass cockpit.
The new twin also offers familiar Diamond characteristics such as dual control sticks, all composite construction, low stall speed and unparalleled visibility.

With the landing gear retracted and at approximately 15% below maximum gross weight, the climb performance exceeded 2,000 ft/min. @ 90kts.
Cruise climb at 110 kts yielded a climb performance of 1,700 fpm.
Less than 8 minutes elapsed during continuous climb to 12,000 ft.
At this altitude, under ISA conditions, a maximum speed of just over 200 kts true airspeed was achieved.

Single engine climb rate at 12,000 ft averaged 600 ft/min.
Diamond's all new four-seat, retractable twin, powered by two Thielert Centurion 1.7 Jet A-1/diesel fuel burning engines.
The no-reserve range with standard (52 US gal) and optional long range (74 US gal) fuel tanks @75% power and 10,000 ft is 880 nm and 1251 nm respectively.
 

The theoretical maximum endurance and range at minimum power settings approach 19 hrs and 2,200 nm with the long range tank.