Aircraft 2685 TT F.8L Falco
Exterior condition 9
Interior condition 9
Engine 1285 SMOH 180 hp Lycoming IO-360-BIE -
Propeller 1917 SN Hartzell
two-blade, constant-speed
Seats 2
Gross Weight, normal & utility
1880 lbs.
Maximum aerobatic weight 1650
lbs.
Useful load, normal & utility 660
lbs.
Useful load, aerobatic 430
lbs.
Payload with full fuel 420 lbs.
Wing loading 17.5 lbs/sq ft
Power loading, normal & utility
10.4 lbs/hp
Power loading, aerobatic 9.2 lbs/hp
Fuel capacity has optional inverted tank
44 U.S. gals
Baggage 90 lbs.
Rate of climb 1800 fpm
Best-rate-of-climb speed
90.5 kts
Climb gradient 758.2 ft/nm
Service ceiling 19,000 ft
Maximum speed @ sea level
191.3 kts
Never exceed speed 208.6 kts
Cruise @ 75% power @ 6,000 ft
178.4 kts
Fuel flow @ 75% power
9.6 gph
Endurance @ 75% power 3.9 hrs
Cruise @ 55% power @ 10,000 ft 158 kts
Fuel flow @ 55% power 7.5 gph
Endurance @ 55% power (economy cruise) 5.0 with 45 min. IFR reserve
Range, economy cruise 800 nm
Miles per gallon, economy cruise 24.2 smpg
Stall speed, clean
65
kts
Stall speed, flaps/gear down
53 kts
Turbulent-air penetration speed
122
kts
Take-off run to clear 50 ft obstacle 750 ft
Landing run to clear 50 ft obstacle 1,150 ft
© 2009 by Arthur L. Dominguez - All rights reserved.