BACK

Edit Info

 
Contact Owner (Members Only)
Bellanca - N596JR
 Specifications may change - Pilots should always check the POH!

Exterior


Panel

Specifications

Engine
115 Horsepower

Fuel Capacity
35 gal useable (6.3gph)

Maximum Speed TAS
100 kts

Useful Load
595 lbs.

Maximum glide
65 MPH

Glide Ratio
9:1

Final Approach Speed
60-75 MPH

Max. demo. X-wind
10 MPH

V Speeds
Vy 69 MPH
Vx 58 MPH
Vs 51 MPH
Vno 120 MPH
Vne 162 MPH

Requirements
Tot tailwheel time: 10hrs
Time in model:
    As required
or checkout time:
    As required
Airport: HWD
Hourly Rate: $ 96
Equip: 7ECA/G
Year: 1996
Color: Ylw/Blu
Tiedown: J38

Basic Avionics
  • NAV/COM: KLX 135A COM/GPS (GPS VFR Only)
  • INTERCOM: Flightcom 403
  • TRANSPONDER: King KT 76A
>>>>> Check for Avionics Manuals <<<<<
Remarks:
Approved for limited aerobatics - Not approved for sustained inverted flight. A letter from American Champion, dated 11/2001, authorizing the 100 lb. gross weight increase can be found in the AFM. The weight and balance was recalculated on 6/18/1998 and is current as of 2/4/2002.

Specials:
Blk 10hrs min $92

Weight and Balance
CG limits:
 
Weight          Normal    Aerobatic
1750          14.2-19.2   14.2-17.3
1325 or less  10.5-19.2   10.5-17.3

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
1154.45
Empty CG
11.44
MGTW
1750
MRW
1750
MLW
1750
Item Weight Arm Moment
Empty Weight
Front Seat
Rear Seat
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.

E