SUNDAY   |   May 11, 2008   

Introducing The Cessna Skyhawk Turbo Diesel

  • Turbocharged diesel engine
  • Fully integrated G1000 with GFC 700 autopilot
  • Full Authority Digital Engine Control (FADEC)
  • Composite constant speed 3-blade propeller
  • Thielert Centurion 2.0

LEGENDARY AIRCRAFT, REVOLUTIONARY ENGINE

Solid, responsive handling. Classic, high-wing design. Fun, forgiving flight characteristics. As the best-selling aircraft in the history of aviation, the Cessna Skyhawk has a whole lot to love. Now, with the Skyhawk Turbo Diesel, you can add dramatic fuel savings to the list – pushing cost-per-flighthour down.

SKYHAWK TURBO DIESEL | Features and Benefits

PRODUCTION-FRIENDLY FULLY INTEGRATED DESIGN

  • Factory installed STC
  • Incorporated standard aircraft design changes to simply and improve STC
  • integration and installation
  • G1000 system integration – engine indication, warnings and alerts

CERTIFIED FOR OPERATION WITH JET A ONLY

  • Worldwide fuel availability
  • Lower fuel cost relative to Avgas
  • Jet A specific fuel filler neck prevents unintentional Avgas fueling

LOW DIRECT OPERATING COST (DOC)

  • Lower fuel consumption and fuel price (Jet A)
  • 2,400 hour TBR
  • Increased margins for flight training and rental operations
  • Increased range and endurance. Ideal for special missions applications

TURBOCHARGED ENGINE

  • Sustained engine performance at higher density altitudes
  • Maintains 100% power to 8,000 feet
  • Reduced noise signature

FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC)

  • Monitors and simplifies engine operation (throttle, propeller, mixture)
  • Enables single lever power control
  • Improved all-operation engine starting
  • Reduced fuel consumption
  • Electronic engine parameter data logging

CONSTANT SPEED 3-BLADE PROPELLER

  • Improved takeoff and climb performance
  • Improved ground clearance
  • RPM reduction gear drive (2,300 rpm) – reduces noise signature

WARRANTY

  • 2,400 hours or 12 years (prorated after the first two years of full coverage)

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PRELIMARY SPECIFICATIONS AND PERFORMANCE DATA

AIRCRAFT DIMENSIONS

Overall Height 8 ft 11 in
2.72 m
Overall Length 27 ft 2 in
8.28 m
Wingspan 36 ft 1 in
11.00 m
Wing Area 174 sq ft
16.20 m
Wing Loading 14.7 lb/sq ft
71.8 kg/sq m
Cabin — Height 48 in
1.22 m
Length (firewall to aft baggage bulkhead) 142 in
3.61 m
Width 40 in
1.00 m
Maximum Seating Capacity 4

POWERPLANT

Engine: Thielert Centurion 2.0 TAE 125-02-114  
Horsepower at 2,300 rpm 155 bhp  
Composite three-blade propeller    

DESIGN WEIGHTS AND CAPABILITIES

Maximum Ramp Weight 2,552 lb
1,158 kg
Standard Empty Weight 1,808 lb
820 kg
Maximum Useful Load 742 lb
336.57 kg
Fuel Capacity (usable) 44.6 U.S. gal
169 L

PERFORMANCE

Speed – Maximum at 10,000 ft 130 ktas
Cruise Speed – 85% Power at 8,000 ft 118 ktas
Cruise Range 588 nm
1,089 km
Rate of Climb at Sea Level 622 fpm
189 mpm
Service Ceiling 16,000 ft
4,877 m
Takeoff Performance (ground roll) 840 ft
256 m
Total Distance Over 50-ft Obstacle 1,755 ft
535 m
Landing Performance (ground roll) 575 ft
175 m
Total Distance Over 50-ft Obstacle 1,335 ft
407 m
     

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