cessna skyhawk turbo diesel.pdf

8/11/2019 Cessna SKYHAWK TURBO DIESEL.pdf

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INTRODUCING THE CESSNA SKYHAWK TURBO DIESEL



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.

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