Pitts S-2S

Aviat Aircraft Inc.

фотография с сайта www.aviataircraft.com

specifications 
 
Engine make/model:  Lycoming AEIO-540, 260 Hp
Horsepower @ RPM @ altitude: 185@2550@SL
Horsepower for takeoff: 260
TBO hours: 1200
Fuel type: 100LL
Propeller make/type: Hartzell, constant speed, composite three-blade
Landing gear type: Fixed/Conv.
Max ramp weight (lbs): 1700
Gross weight (lbs): 1700
Max landing weight (lbs): 1700
Empty weight (lbs): 1155
Useful Load (lbs): Normal 545 (aerobatic 470)
Payload (full fuel) (lbs): 371
Usable fuel (gals): 28 (23 aerobatic)
Oil capacity (qts): 12
Wingspan:  20 ft.
Overall length:  17 ft. 9 in.
Height: 6 ft. 5 in.
Wing area (sq. ft.): 127.5
Wing loading (lbs/sq. ft.): 13.3 (12.7 aerobatic)
Power loading (lbs/hp): 6.59 (6.25 aerobatic)
Wheel base: 163 in.
Wheel track: 603/4 in.
Wheel size (in): 500X5
Cabin seats: 2
Cabin width: 2 ft. 4 in.
Cabin length: 6 ft. 11 in.
Baggage capacity (lbs): 20
performance 
Cruise speed (knots): 
 
75% power: 157
65% power: 150
55% power: 147
Max range (with reserve) (nm): 
75% power: 246
65% power: 274
55% power: 300
Fuel consumption (gph):  
75% power: 13.май
65% power: 12
55% power: 11
Estimated endurance 56
(65% power w/1 hr reserve) (hrs)  
Best rate of climb (fpm): 2900
Service ceiling (ft.) N/A
Takeoff ground roll (ft.): 554
Takeoff over 50-ft obstacle (ft.):  860
Landing ground roll (ft.): 750
Landing over 50-ft obstacle (ft.): 1200 factory specifications only

Сайт разработчика: www.aviataircraft.com