AVSIG: Cessna Aircraft Company Model Specs wwswsigarch.jpg (7236 bytes)

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AVSIG Discussion Sections >> Cessna

Mike OverlyAdministrator
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Reged: 04/09/01
Posts: 2608
Loc: Columbus, OH
Cessna Aircraft Company Model Specs
      07/22/07 09:34 PM

Reciprocating

Skyhawk
Single Lycoming IO-360-L2A
Horsepower: 160

Seating including pilot: 4
Useful Load: 758 lb
Cruise @ 80-percent Power: 122 kts
Cruise Range with Reserve @ 80-percent Power 580 nm
Runway Requirements/Takeoff over 50-ft Obstacle: 1685 ft
Runway Requirements/Landing over 50-ft Obstacle: 1295 ft
Climb Rate: 720 ft/min
Stall Speed w/Flaps: 47 kts


Skyhawk SP
Single Lycoming IO-360-L2A Engine
Horsepower: 180

Seating including pilot: 4
Useful Load: 837 lb
Cruise @ 75-percent Power: 124 kts
Cruise Range with Reserve @ 75-percent Power 518 nm
Runway Requirements/Takeoff over 50-ft Obstacle: 1630 ft
Runway Requirements/Landing over 50-ft Obstacle: 1335 ft
Climb Rate: 730 ft/min
Stall Speed w/Flaps: 48 kts


Skylane
Single Textron Lycoming IO-540-AB1A5 Engine
Horsepower: 230

Seating including pilot: 4
Useful Load: 1113 lb
Cruise @ 80-percent Power: 145 kts
Cruise Range with Reserve @ 80-percent Power 773 nm
Runway Requirements/Takeoff over 50-ft Obstacle: 1514 ft
Runway Requirements/Landing over 50-ft Obstacle: 1350 ft
Climb Rate: 924 ft/min
Stall Speed w/Flaps: 49 kts


Turbo Skylane
Single Textron Lycoming TI0-540-AK1A
Horsepower: 235

Seating including pilot: 4
Useful Load: 1017 lb
Cruise @ 88-percent Power: 159 kts
Cruise Range with Reserve @ 88-percent Power 615 nm
Runway Requirements/Takeoff over 50-ft Obstacle: 1385 ft
Runway Requirements/Landing over 50-ft Obstacle: 1350 ft
Climb Rate: 1040 ft/min
Stall Speed w/Flaps: 49 kts


Stationair
Single Textron Lycoming IO-540-AC1A
Horsepower: 300

Seating including pilot: 6
Useful Load: 1360 lb
Cruise @ 75-percent Power: 142 kts
Cruise Range with Reserve @ 88-percent Power 594 nm
Runway Requirements/Takeoff over 50-ft Obstacle: 1860 ft
Runway Requirements/Landing over 50-ft Obstacle: 1395 ft
Climb Rate: 988 ft/min
Stall Speed w/Flaps: 54 kts


Turbo Stationair
Single Textron Lycoming TIO-540-AJ1A
Horsepower: 310

Seating including pilot: 6
Useful Load: 1255 lb
Cruise @ 75-percent Power at 20000 ft: 164 kts
Cruise Range with Reserve @ 75-percent Power at 20000 ft:559 nm
Runway Requirements/Takeoff over 50-ft Obstacle: 1740 ft
Runway Requirements/Landing over 50-ft Obstacle: 1395 ft
Climb Rate: 1050 ft/min
Stall Speed w/Flaps: 54 kts


Recently Announced: Skycatcher
Single Continental O-200D
Projected Horsepower: 100

Projected Seating including pilot: 2
Projected Useful Load: 490 lb
Projected Cruise @ 77-percent Power: 117 kts
Projected Cruise Range with Reserve @ 77-percent Power: 390 nm
Projected Runway Requirements/Takeoff over 50-ft Obstacle: 1250 ft
Projected Runway Requirements/Landing over 50-ft Obstacle: 1040 ft
Projected Climb Rate: 890 ft/min
Projected Stall Speed w/Flaps: NA



Turboprop

Caravan
Single PT6A- 114A
Horsepower: 675

Seating including pilot: Variable personal/airline/frieght configurations
Useful Load: 4500 lb maximum
Cruise: 184 kts
Cruise Range:907 nm
Runway Requirements/Takeoff over 50-ft Obstacle: 2420 ft
Runway Requirements/Landing over 50-ft Obstacle: 1795 ft
Climb Rate: 975 ft/min
Stall Speed: 61 kts


Jet

Citation X
Range: 3070 nm
Cruise Speed: Mach 0.92
Ceiling: 51000 ft


Citation Sovereign
Range: 2664 nm
Cruise Speed: 458 ktas
Ceiling: 47000 ft


Citation XLS+
Range: 1858 nm
Cruise Speed: 440 ktas
Ceiling: 45000 ft


Citation Encore+
Range: 1762 nm
Cruise Speed: 428 ktas
Ceiling: 45000 ft


Citation CJ4
Range: 1825 nm
Cruise Speed: 435 ktas
Ceiling: 45000 ft


Citation CJ3
Range: 1875 nm
Cruise Speed: 417 ktas
Ceiling: 45000 ft


Citation CJ2+
Range: 1613 nm
Cruise Speed: 418 ktas
Ceiling: 45000


Citation CJ1+
Range: 1300 nm
Cruise Speed: 389 ktas
Ceiling: 41000 ft


Citation Mustang
Range: 1167
Cruise Speed: 340 ktas
Ceiling: 41000 ft



Data compiled by www.AVSIG.com.
Data is subject to error and omission and not for flight planning, operation, or navigation.


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