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Cirrus SR22 - N988CD
 Specifications may change - Pilots should always check the POH!

Exterior


Panel - Left Side


Panel - Right Side


Panel - Full View

Specifications

Engine
310 Horsepower

Fuel Capacity
81 gals. useable

Maximum Speed TAS
180 kts

Useful Load
1005 lbs.

Maximum glide
88

Glide Ratio
9.6 to 1

Final Approach Speed
80-85

Max. demo. X-wind
20

Checkout & Currencey Requirements

Airport: PAO

Tiedown: 20

Color: white

Hourly Rate: $275 Hobbs

Year: 2004

Equip: SR22/G

Basic Avionics
  • GPS/NAV/COM: Dual Garmin 430W's (WAAS)
  • PFD: Avidyne Entegra Rev 7
  • MFD: Avidyne FlightMax EX5000 Rev 7
  • AUDIO PANEL: PS Engineering PMA8000B - 4 place IC
  • TRANSPONDER: Garmin GTX 327
  • AP: S-TEC 55X - 2 axis
  • TCAS: Skywatch SKY497
  • STORMSCOPE: BF Goodrich WX500
>>>>> Check for Avionics Manuals <<<<<
Remarks:
Air Conditioning. Ballistic recovery parachute system. Fuel policy to tabs: 46 useable gallons. TKS Glycol based Ice Protection System for wings, elevator and propeller. Low Vibration 6-point Engine Mount. Serial 0889. North America NavData - coast to coast and Canada/Mexico. All Cirrus must be run 75% continious power or less. 65% power is recomended cruise power setting (typical TAS 165kt at 14gph).

Specials:
$270 c/o up to 10hrs

Weight and Balance
CG limits:
 
Forward: 138@2200 
         to 139.1@2700
         to 141.4@3210
         to 143.8@3400
Aft: 148.1

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. Default fuel is set to tabs.

Empty Wt
2394
Empty CG
138.5
MGTW
3400
MRW
3400
MLW
3400
Item Weight Arm Moment
Empty Weight
Front Seats
Rear Seats
De-Ice Fluid (full)
Baggage
Fuel (6 lbs./gal.)
Totals
    
Takeoff C.G.   
  

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