Maximum Cruise Speed
Takeoff Field Length
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.
With renowned durability, careful student-focused design and forgiving flying characteristics, this superior platform employs advanced diesel engine technology, allowing for improved performance, increased fuel efficiency and simplified power management.
The Turbo Skyhawk JT-A offers a proven classroom experience that instructors, students and observers have come to know and expect.
Rugged and built to take the abuse of pilots-in-training, the JT-A features three seats, large wraparound windows and soft LED lighting throughout the cabin, maintaining comfortable conditions throughout every lesson. A 12-volt power outlet keeps your mobile devices fully charged, while seatbelt airbags help keep everyone secure. Farther aft, a cargo area fully equipped with tie-down rings allows for 120 pounds (54 kilograms) of gear. Customize the cabin to your preferences with optional skylights, leather seats, an aft bench and air-conditioning.
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.
- 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
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.
Wingspan – 36 ft 1 in (11.00 M)
Length – 27 ft 2 in (8.28 M) Height – 8 ft 11 in (2.72 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)|
|Height||48 in (1.22 m)|
|Width||40 in (1.00 m)|
|Length||11 ft 10 in (3.61 m)|
|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||1,750 lb (794 kg)|
|Useful Load||802 lb (364 kg)|
|Maximum Payload||800 lb (363 kg)|
|Full Fuel Payload||503 lb (228 kg)|
|Maximum Cruise Speed||134 ktas (248 km/h)|
|Maximum Range||885 nm (1,639 km)|
|Takeoff Distance||1,615 ft (492 m)|
|Ground Roll||944 ft (288 m)|
|Landing Distance||1,335 ft (407 m)|
|Ground Roll||575 ft (175 m)|
|Maximum Climb Rate||712 fpm (217 mpm)|
|Maximum Limit Speed||163 kias (302 km/h)|
|Stall Speed||48 kcas (89 km/h)|
|Power Output||155 hp (155 hp)|
|Propeller Manufacturer||MT Propeller|
|Description||3 blade composite|
Aircraft performance is dependent on multiple variables (i.e. winds aloft, number of passengers, temperature and altitude of departure and arrival airports). The range, speed and endurance listed here represent average performance data. Contact one of our experienced Client Services Representatives who will be able to advise you on additional fuel stops or other limitations needed based on your itinerary and aircraft.