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2008 Cessna 172S Skyhawk SP

Description:

Cessna 172S Skyhawk SP

Specification:

Powerplant Lycoming IO-360-L2A
Propeller McCauley two-blade, fixed-pitch, 76-in diameter
   
Length 26 ft 11 in
Height 8 ft 11 in
Wingspan 36 ft 1 in
Wing area 176 sq ft
Wing loading 14.5 lb/sq ft
Power loading 14.1 lb/hp
Seats 4
Cabin length 11 ft 10 in
Cabin width 3 ft 3 in
Cabin height 4 ft
Empty weight 1,600 lb
Empty weight, as tested 1,644 lb
Maximum ramp weight 2,558 lb
Useful load 958 lb
Useful load, as tested 914 lb
Payload w/full fuel 640 lb
Payload w/full fuel, as tested 596 lb
Maximum takeoff weight 2,550 lb
Maximum landing weight 2,550 lb
Fuel capacity, std 56 gal (53 gal usable)
336 lb (318 lb usable)
Oil capacity 8 qt
Baggage capacity 5.2 cu ft, 120 lb

Airframe:

  • Total Time: TBA
  • Landings: TBA

Engine:

  • Engine: Lycoming
  • Model Number : IO-360-L2A
  • Total Time : TBA
  • Cycles : TBA

Avionics/Radios:

Information is available on request.

Exterior:

Information is available on request.

Interior:

Information is available on request.

Inspection Status:

Information is available on request.

Disclaimer

The details, photographs and technical information provided are for the purpose of initial review only and will be subject to changes w.r.t. technical parameters, which may include but will not be limited to the Aircraft’s/Helicopter’s /Engine’s/Part’s condition, Airframe & component’s time, etc.
Verification of the Aircraft’s/Helicopter’s/Engine’s/Part’s actual condition shall be the sole responsibility of the Buyer/Lessee.

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