BACK

Edit Info

 
Contact Owner (Members Only)
Cessna Skyhawk SP - N610SP
 Specifications may change - Pilots should always check the POH!

Exterior


Panel

Specifications

Engine
180 Horsepower

Fuel Capacity
53 Useable

Maximum Speed TAS
125 kts

Useful Load
854.9 lbs.

Maximum glide
68

Glide Ratio
9:1

Final Approach Speed
60-70

Max. demo. X-wind
15

V Speeds
Vx 62
Vy 74
Va 90-105
Vfe 110 & 85
Vs 53
Vso 48
Airport: SQL

Tiedown: K1

Color: White/Blue/Red

Hourly Rate: $159

Year: 2000

Equip: C-172SP/G

Basic Avionics
  • GPS: Bendix King KLN 94 (IFR approved)
  • 2 NAV/COMS: Bendix King KX 155A
  • AUDIO PANEL: Bendix King KMA 26
  • ADF: Bendix King KR 87
  • AUTOPILOT: Bendix King KAP 150
  • TRANSPONDER: Bendix King Mode C 76C
  • HSI: Bendix King KI 525A
  • STORMSCOPE: BFGoodrich WX-950
>>>>> Check for Avionics Manuals <<<<<
Remarks:
Bendix King KCS 55A slaved compass system, Club fueling policy: To bottom of filler neck (35 Useable gallons)

Weight and Balance
CG limits:
 
FWD 35.0 @ 1950 - 41.0 @ 2550
AFT 47.3

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
1695.1
Empty CG
39.76
MGTW
2550
MRW
2558
MLW
2550
Item Weight Arm Moment
Empty Weight
Front Seats
Rear Seats
Baggage
Baggage 2
Fuel (6 lbs./gal.)
Totals
    
Takeoff C.G.   
  

Entire contents © 1998, 2006 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.