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Cirrus SR20 - N725SB
 Specifications may change - Pilots should always check the POH!

Exterior


Panel - Left Side


Panel - Right Side


Panel - Full View

Specifications

Engine
200 Horsepower

Fuel Capacity
56 gals. useable

Maximum Speed TAS
156 kts

Useful Load
877 lbs.

Maximum Glide
87-96

Final Approach Speed
75-80

Max. demo. X-wind
21

Checkout & Currencey Requirements

Airport: PAO

Tiedown: 22

Color: Wh/Grn

Hourly Rate: $199

Year: 2003

Equip: SR20/G

Basic Avionics
  • GPS/NAV/COM: Dual Garmin 430W WASS
  • PFD: Avidyne Flight Max Integra Rev 7 WAAS Support
  • MFD: Avidyne Flight Max EX5000 Rev 7
  • AUDIO PANEL: Garmin GMA 340 - 4 place IC
  • TRANSPONDER: Garmin GTX 327
  • AP: S-TEC 55X - 2 axis
>>>>> Check for Avionics Manuals <<<<<
Remarks:
Flivie System Compatible. SN 1363. Club Fuel Policy: to tabs 26 usable gallons. Zero fuel weight: 2900 lbs. High Intensity Landing Light approved for continous use.

Specials:
PROMO-2hr demo $399 w/Steve B. as CFI included contact front desk for details//3hrs free flt inst. w/Steve Blonstein Contact Steve steveblonstein@gmail.com or 650-799-2153

Weight and Balance
CG limits:
 
Forward: 138.7@2110
      to 141.0@2694 
      to 144.1@3000

   Rear: 144.6@2110 
      to 147.4@2570 
      to 148.1@3000

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
2123
Empty CG
142.3
MGTW
3000
MRW
3000
MLW
3000
Item Weight Arm Moment
Empty Weight
Front Seats
Rear Seats
Baggage
Fuel (6 lbs./gal.)
Totals
    
Takeoff C.G.   
  

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