BACK

Edit Info

 
Contact Owner (Members Only)
Cirrus SR22 - N1403C
 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
1049 lbs.

Maximum glide
88

Glide Ratio
9.6 to 1

Final Approach Speed
80-85

Max. demo. X-wind
20

Requirements
300 hrs total time
25 hrs high performance

Airport: PAO

Tiedown: 6

Color: White/Red/Grey

Hourly Rate: $269

Year: 2003

Equip: SR22/G

Basic Avionics
  • GPS/NAV/COM: Dual Garmin 430's
  • PFD: Avidyne Flight Max Integra
  • MFD: Avidyne Flight Max EX5000
  • AUDIO PANEL: Garmin GMA 340 - 4 place IC
  • TRANSPONDER: Garmin GTX 327
  • AP: S-TEC 55X - 2 axis
  • TAS: Skywatch SKY497
  • STORMSCOPE: BF Goodrich WX5000
>>>>> Check for Avionics Manuals <<<<<
Remarks:
Ballistic recovery parachute system. Fuel policy to tabs: 46 useable gallons. Aircraft serial number 0519. TKS Glycol based Ice Protection System for wings, elevator and propeller.

Specials:
No Checkout Rate

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.

Empty Wt
2351
Empty CG
139.4
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.   
  

Entire contents © 1998, 2005 West Valley Flying Club. All rights reserved.
Reproduction in whole or in part in any form without the express written permission
of an officer of the club is strictly prohibited.