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AMERICAN CHAMPION SCOUT 8GCBC
SPECIFICATIONS [1]
ENGINE

    Manufacturer

Lycoming

    Model

O-360-C2A

    Rating

180 HP

    Number of Cylinders

4
PROPELLER

    Type

Fixed Pitch
WEIGHTS
    Gross Weight - (Norm. Cat.)
2,150 LBS
    Gross Weight - (Restricted Cat.)
2,600 LBS
    Empty Weight
1,315 LBS
    Useful Load
835 LBS
DIMENSIONS

    Wing Span

36.2 FT

    Length

22.8 FT

    Height

8.7 FT

    Wing Area

180 SQ.FT.
FUEL CAPACITY
    Standard Usable
35 GAL
    Optional Usable
70 GAL
OIL CAPACITY 8 QTS
PERFORMANCE [1]

    Max. Speed Level Fit

135 MPH

    Cruise Speed at 75% Power (TAS)

122 MPH

    Rate of Climb, Sea Level

1,080 FPM

    Take Off, Ground Run (Sea Level)

510 FT

    Stall Speed Full Flaps

50 MPH

    Range at 75% Power*

384 SM

    Range at 75% Power/70 Gal.*

783 SM

    Range at 55% Power/70 Gal.*

897 SM
*Includes fuel for start, taxi, takeoff, climb and descent, starting at sea level, no reserves.

[2]

Reference:
1) American Champion Aircraft Information Package, April 11, 1995.
2) Green, W., Punnett, D., The Observer's Book of Aircraft, 1975 Ed., p. 29, Frederick Warne & Co Ltd, London, 1975.
Given data is only for information. Please refer to the manufacturer for current data.

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