cessna skyhawk turbo diesel.pdf
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8/11/2019 Cessna SKYHAWK TURBO DIESEL.pdf
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INTRODUCING THE CESSNA SKYHAWK TURBO DIESEL
8/11/2019 Cessna SKYHAWK TURBO DIESEL.pdf
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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 3-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 ........................................................................ 744 lb 337 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
Cessna Single Engine Piston Aircraft • Annex IV • 2603 South Hoover Road • Wichita, Kansas 67215
1-800- 4-CESS NA in the U.S. • +1-316-517-6056 outside the U.S. • Fax +1-316-517-2772 • SE.Cessna.com
S u r e T h i n g ®
PRODUCTION-FRIENDLY FULLY INTEGRATED DESIGN
• Factory-installed STC
• Incorporated standard aircraft design changes to simplify 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
SKYHAWK TURBO DIESEL | Features and Benefits
PRELIMINARY SPECIFICATIONS AND PERFORMANCE DATA
ISO 9001-certified • SPA07-TDMini 10/07 1M Litho in the U.S.A.