Engine

Lycoming AEIO-540, 260 hp

Recommended TBO

1,200 hr

Propeller

Hartzell 'Claw', constant speed, 78 in composite 3 blade

Length

17' 9"

Height

6' 5"

Wing Span

20'

Wing Area

127.5 sq ft

Wing Loading

13.3 lb/sq ft (normal cat) 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 (inc 5g wing tank)

29 gal (28 usable); aerobatic flight 24 gal (23 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