Pitts S-2C

Aviat Aircraft Inc.

фотография с сайта www.aviataircraft.com

Engine  Lycoming AEIO-540, 260 hp
Recommended TBO  1,200 hr
Propeller  The Claw by Hartzell, constant speed, composite three-blade, 78 in dia
Length  17' 9"
Height  6' 5"
Wing Span  20'
Wing Area  127.5 sq ft
Wing Loading  13.3 lb/sq ft (normal category)
12.7 lb/sq ft (aerobatic)
Power Loading  6.59 lb/hp (normal category)
6.25 lb/hp (aerobatic)
Seats  2 tandem
Cabin Length  6' 11"
Cabin Width  28"
Cabin Height  47"
Empty Weight  1,155 lb
Maximum Gross Weight  1700 lb
Useful Load  545 lb (normal category)
470 lb (aerobatic)
Payload w/Full Fuel  371 lb
Fuel Capacity (w/5-gal wing tank)  29 gal (28 gal usable)
aerobatic flight, 24 gal (23 gal usable)
Aerobatic flight load limits  +6 G/-5 G
Takeoff distance ground roll  554 ft
Takeoff distance over 50-ft obstacle  860 ft
Max demonstrated crosswind component  17 kt
Rate of climb, sea level (minimum wieght)  2,900 fpm
Maximum level speed, sea level  169 kt
Cruise speed w/30 min rsv. @ 75% power  150 KTAS/ 1.6 hrs
Range w/30 min rsv. @ 75% power  284 st. miles
Fuel consumption @ 75% power  (84 pph/14gph)
Best economy  6,000 ft
Landing distance over 50-ft obstacle  1,200 ft
Landing distance, ground roll  750 ft
VX (best angle of climb)  KIAS N/A at this time
VY (best rate of climb)  KIAS 82
VA (design maneuvering)  KIAS 134
VNO (max structural cruising)  KIAS 134
VNE (never exceed)  KIAS 185
VSI (stall, clean)  KIAS 56

Сайт разработчика: www.aviataircraft.com