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Cessna Skylane - N262CL
 Specifications may change - Pilots should always check the POH!

Exterior


Panel

Specifications

Engine
235 Horsepower

Fuel Capacity
87 gals. usable

Maximum Speed TAS
150 kts

Useful Load
1115 lbs.

Maximum Glide
76

Final Approach Speed
60-70

Max. Demo. X-wind
15

V Speeds
Vx = 65 KIAS
Vy = 80 KIAS
Va = 91-110
Vfe = 140, 120, 100 KIAS
Vs = 51 KIAS
   (max wt & most fwd CG)
Vso = 41 KIAS
   (max wt & most fwd CG)
Vne = 175 KIAS
Vno = 140 KIAS

Checkout & Currencey Requirements

Airport: PAO

Tiedown: S30

Color: Wh/Blu/Beige

Hourly Rate: $215 G1000

Year: 2004

Equip: C-182T/G

Basic Avionics
  • PANEL: Garmin G-1000 Glass Cockpit (PFD/MFD/GPS/NAV/COMM/TX)
  • AUTOPILOT: KAP 140 Dual Axis
  • AUDIO/INTERCOM: Garmin 1347 4 Place w/aux input
  • TIS: Mode S Traffic Information System
  • STORMSCOPE: BF Goodrich WX500
>>>>> Check for Avionics Manuals <<<<<
Remarks:
Flivie System Compatible. Garmin GDL 69A (Note: Full 'XM Aviator' Subscription- Satellite-based in-cockpit weather provides NEXRAD, TFRs, AIRMETs, SIGMETs, graphical and plain English METARs and National Lightning Detection Network, satellite radio). Flap Gap Seals, High Intensity Landing Light approved for continous use. Club Fuel Policy to bottom of filler neck, 32 useable gallons a side.

Specials:
$190 Mem C/O up to 5 hours

Weight and Balance
CG limits:
 
Forward 33.0 at 2250 to 
        35.5 at 2700 to 
        40.9 at 3100
    Aft 46.0

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
1995.0
Empty CG
38.3
MGTW
3100
MRW
3110
MLW
3100
Item Weight Arm Moment
Empty Weight
Front Seats
Rear Seats
Baggage
Baggage 2
Fuel (6 lbs./gal.)
Totals
    
Takeoff C.G.   
  

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