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Cirrus SR20 - N8139D
 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
838 lbs.

Maximum Glide
87-96

Final Approach Speed
75-80

Max. demo. X-wind
21
Airport: PAO

Tiedown: 42

Color: Wh/Grn

Hourly Rate: $224 Hobbs

Year: 2003

Equip: SR20/G

Basic Avionics
  • GPS/NAV/COM: Dual Garmin 430's & WAAS
  • PFD: Avidyne Flight Max Integra v8.0 with flight director
  • MFD: Avidyne Flight Max EX5000
  • AUDIO PANEL: Garmin GMA 340 - 4 place IC
  • TRANSPONDER: Garmin GTX 327
  • AP: Avidyne DFC90 - 2 axis with Altitude Hold (ALT), Airspeed Hold (IAS), Vertic
  • TCAS: Goodrich Skywatch
Remarks:
Propellor: 3 blade. Interior: leather. 406 mhz ELT Flivie System Compatible. High Intensity Landing Light approved for continous use. LIMITED TIME--Break-In Discount $199 3hr min cross country,select BLOCK billing program.

Specials:
c/o $214 10hr max//Promo $199 3hr min cross country

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
2162
Empty CG
141.0
MGTW
3000
MRW
3000
MLW
2900
Item Weight Arm Moment
Empty Weight
141.0
Front Passengers
143.5
Rear Passengers
180.0
Baggage
208.0
Fuel (6 lbs./gal.)
153.8
Totals
    
Takeoff C.G.   
  

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