Cessna 120/140 1946-1948

SPECIFICATIONS

Engine make/model: Continental C-85-12
Horsepower for takeoff: 85
Fuel type: 80
TBO hours: 1200
Propeller make/type: Fixed
Landing gear type: Conventional
Max ramp weight (lbs): 1450
Gross weight (lbs): 1450
Max landing weight (lbs): 1450
Empty weight (lbs): 770-900
Usable fuel (gals): 22
Oil capacity (quarts): 5
Wingspan: 32 ft. 10 in.
Overall length: 21 ft. 6 in.
Wing area (sq. ft.): 167
Wing loading (lbs/sq. ft.): 9.1
Power loading (lbs/hp): 17
Wheel track: 6 ft.
Wheel size: 6 in.
Seating capacity: 2
Cabin doors: 2
Cabin width: 42 in.
Baggage capacity (lbs): 40


PERFORMANCE

Cruise speed (knots):

75% power: 94
65% power: 91
55% power: 90

Max range (with reserve) (nm):
75% power: 370
65% power: 378
55% power: 395

Fuel consumption (gph):
75% power: 4.8
65% power: 4.5
55% power: 4.2

Estimated endurance
(65% power w/1 hr reserve) (hrs) 3.8
Stall speed (flaps up) (knots): 42
Stall speed (flaps down) (knots): 39
Best rate of climb (fpm): 740
Service ceiling (ft.) 15,500
Takeoff ground roll (ft.): 773
Landing ground roll (ft.): 233

all specs are standard unless noted otherwise