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Cessna Skyhawk - N5346D
 Specifications may change - Pilots should always check the POH!

Exterior


Panel - Left Side


Panel - Right Side

Specifications

Engine
160 Horsepower

Fuel Capacity
50.0 gals.

Maximum Speed TAS
120 kts

Useful Load
783.25 lbs.

Maximum glide
65

Glide Ratio
9 TO 1

Final Approach Speed
55-65

Max. demo. X-wind
15
Airport: PAO

Tiedown: T-22

Color: wh/brn

Hourly Rate: $108

Year: 1979

Equip: C-172/G

Basic Avionics
  • GPS/NAV/COMM: Garmin 430
  • NAV/COM 2: King KX170B (with 2nd GS)
  • TRANSPONDER: KT 76A
  • DME: King KN 64
  • INTERCOM: Sigtronics 4-Place
  • ADF: King KR 85
  • AUDIO PANEL: KMA 20
>>>>> Check for Avionics Manuals <<<<<
Remarks:
Digital RPG/TACH. Second Turn Coordinator.

Weight and Balance
CG limits:
 
 Fwd: 35 from 0 to 1950 lbs;
      then sloping to 38.5 at 2300 lbs.
Rear: 47.3 at all wts.

Replace sample weights with your actual weights, then click on the "Calculate" button to see the new takeoff C.G.
Pilots should always calculate the W&B on the ramp prior to takeoff using the latest data from the POH, and taking into account all circumstances including the difference between takeoff and landing fuel quantity and weight.

Empty Wt
1516.75
Empty CG
38.77
MGTW
2300
MRW
2307
MLW
2300
Item Weight Arm Moment
Empty Weight
Front Seats
Rear Seats
Baggage
Fuel (6 lbs./gal.)
Totals
    
Takeoff C.G.   
  

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