• Maximum Range

    963 nm

  • Maximum Cruise Speed

    134 ktas

  • Maximum Occupants


  • Useful Load

    772 lb

  • Takeoff Ground Roll

    844 ft


The new and improved Turbo Skyhawk® JT-A employs advanced diesel engine technology for improved performance, including increased fuel efficiency and simplified power management, all while accommodating growing demands and environmental regulations across the globe. Flight training may never be the same again.

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Featuring a Continental CD-155 liquid cooled in-line four-stroke 4-cylinder turbocharged engine with double overhead camshafts, direct fuel injection and common-rail technology, the Turbo Skyhawk JT-A offers lower operating costs and reliability, leading to the gateway of globally available fuel.

A single-lever power control replaces the classic throttle and mixture controls, simplifying power management



Advanced Display Technology

The Cessna Turbo Skyhawk JT-A is powered by the latest technology in integrated cockpit avionics, the Garmin G1000 NXi. With an improved graphical interface, more powerful hardware, higher resolution displays, added functionality to improve situational awareness, and optional wireless technology, managing the flight deck has never been easier.

  • Wireless database and flight plan loading

  • Enhanced HSI Functionality

  • VFR Sectionals

  • IFR High and Low Charts

  • Vertical Situation Display

  • COM Frequency Decoding
  • Standard ADS-B Out and In
  • Optional wireless data base and flight plan loading
  • Integrated VFR Sectional Charts
  • IFR High and Low Charts with Night Mode
  • Enhanced HSI features
  • COM frequency decoding
  • Vertical Situation Display
  • Selectable Visual Approaches
  • Optional Surface Watch for runway safety
  • Enhanced graphics and faster processing
  • Improved joystick with smoother panning
  • Simplified maintenance
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From manufacturing the world's most popular training airplane to a global network prepared to support you throughout the complete ownership experience, our lineup of solutions designed to move you — and your business — forward.

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27 ft 2 in (8.28 m)


8 ft 11 in (2.72 m)


36 ft 1 in (11.00 m)


Length 27 ft 2 in (8.28 m)
Height 8 ft 11 in (2.72 m)
Wingspan 36 ft 1 in (11.00 m)
Wing Area 174 sq ft (16.17 sq m)

Cabin Interior

Height 48 in (1.22 m)
Width 40 in (1.00 m)
Length 11 ft 10 in (3.61 m)
Maximum Occupants 4

Baggage Capacity

Weight 120 lb (54.4 kg)
Volume 30 cu ft (0.85 cu m)


Maximum Ramp Weight 2,552 lb (1,158 kg)
Maximum Takeoff Weight 2,550 lb (1,157 kg)
Maximum Landing Weight 2,550 lb (1,157 kg)
Usable Fuel Weight 299 lb (136 kg)
Usable Fuel Volume 45 gal (169 l)
Basic Empty Weight 1,780 lb (807 kg)
Useful Load 772 lb (350 kg)
Maximum Payload 770 lb (349 kg)
Full Fuel Payload 473 lb (215 kg)


Maximum Cruise Speed 134 ktas (248 km/h)
Maximum Range 963 nm (1,783 km)
Takeoff Distance 1,320 ft (402 m)
Ground Roll 844 ft (257 m)
Landing Distance 1,335 ft (407 m)
Ground Roll 575 ft (175 m)
Service Ceiling 18,000 ft (5,486 m)
Maximum Climb Rate 767 fpm (234 mpm)
Maximum Limit Speed 163 kias (302 km/h)
Stall Speed 48 kcas (89 km/h)


Manufacturer Continental
Model CD-155
Power Output 155 hp (155 hp)
Propeller Manufacturer MT Propeller
Description 3 blade composite