October 5, 2018

The Cessna Turbo Skyhawk JT-A offers better take-off performance, especially in hot and high conditions

Textron Aviation has received certification from both the FAA and the EASA (European Aviation Safety Agency) for its Cessna Turbo Skyhawk JT-A. The JT-A, which comes equipped with the next generation avionics of Garmin G1000 NXi and a Continental CD-155 engine, exceeding the initial performance objectives of Textron Aviation.

This includes a range of 963 nautical miles (an increase of 78 nm compared to the original estimated figures), a better takeoff distance of 1,320 feet and a maximum ascent speed of 767 feet per minute. According to company officials, the Turbo Skyhawk JT-A is a “factory option that includes an integrated engine, propeller and cabin upgrade package that drives Skyhawk’s standard performance.” Doug May, Vice President of Piston Aircraft of Textron Aviation noted that the Skyhawk platform represents the most successful single-engine airplane of all time and that the company is excited to further improve its capabilities with the technology of the Jet-A motorcycle group.

The Turbo Skyhawk JT-A allows operators to comply with changing environmental regulations around the world, providing solutions to increase the global reach of this platform that has already been proven. To date, the company says that more than 44,000 Skyhawks have been put into service. The 155 hp JT-A has direct fuel injection, a dual-channel FADEC powered by a single power lever, and burns Jet-A fuel. In addition to the increased range (a 50% bump over the standard Skyhawk range), the JT-A also offers a maximum cruising speed of 134 knots.

Cessna Turbo Skyhawk JT-A

Dimensions

Length 27 feet 2 inches (8.28 m)
Height 8.11 m (2.72 m)
Wingspan 36 ft 1 in (11.00 m)
Wing area 16.17 square meters (174 square feet)
 
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 lbs (54.4 kg)
Volume 30 cubic feet (0.85 m3)
 
Weights

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)
Empty basic weight 1,750 lb (794 kg)
Payload 802 lb (364 kg)
Maximum payload 800 lb (363 kg)
Total fuel payload 503 lb (228 kg)
 
Performance

Maximum cruising speed 134 ktas (248 km / h)
Maximum range 885 nm (1,639 km)
Take-off distance 492 m
Ground roll 944 feet (288 m)
Landing distance 407 m
Ground roll 575 feet (175 m)
Service Roof N / A
Maximum rate of rise 712 fpm (217 mpm)
Maximum speed limit 163 kias (302 km / h)
Parking speed 48 kcas (89 km / h)
Power plant
 
Continental Manufacturer

Model CD-155
Power 155 HP (155 HP)
Propeller Manufacturer MT Propeller
Description 3 blade composite