Powerplant Physical
Engine.
. . . . . . . . . . . . Continental O-200 Empty
Weight . . . . . . . . . . . . . . . . . . . . . 817 lbs.
Rating . . . . . . . . . . . . . 100 horse power Max.
Gross Weight . . . . . . . . . . . . . . . . .1,320 lbs.
Disposition. . . . . . . . . 4-stroke, Carbureted Useful
Load . . . . . . . . . . . . . . . . . . . . . . . 504 lbs.
TBO. . . . . . . . . . . . . . . 1800 hours Fuel
Capacity with Standard Tank. . . . .14.5 gals.
(14 gals. usable)
Performance
Fuel Capacity with Optional Tank. . . . . . 29 gals.
(28.5
gals. usable)
Limit Loading . . . . . . . . . . . . . .+6, -4 g's
Baggage Capacity. . . . . . . . . . . . . . . . . . 100 lbs.
Takeoff Distance . . . . . . . . . . . 350 ft.
Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . Wood
Landing Distance. . . . . . . . . . . 410 ft.
Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21'4"
Normal Cruise . . . . . .
. . . . . . .105-115 mph Height. . . . . . . . . . . . . .
. . . . . . . . . . . . . . . 66"
Top Speed . . . . . . . . . . . . . . . . 130
mph Fuselage
Width . . . . . . . . . . . . . . . . . . . . 29"
VNE. . . . . . . . . . . . . . .
. . . . . . . 150 mph Wing
Span . . . . . . . . . . . . . . . . . . . . . . . . . 28'6"
Stall Speed . . . . . . . . . . . . . . . . 48
mph Wing Cord.
. . . . . . . . . . . . . . . . . . . . . . . . . 55"
Rate of Climb, Sea Level. . . . .1000 fpm
Seats. . . . . . . . . . . . . . . . . . . . . . . . . . . 2, Tandem
Fuel Consumption at Altitude. .6.3 gph
Warner
Aerocraft reserves the right to make price and equipment changes to standard, operational and optional equipment and to modify such
equipment
without prior notice and to do so without incurring any obligations to equip or modify models manufactured prior to or after
the effective
date of such changes.
