2009 Aviat Husky A-1C-200

Tuesday, August 25, 2009 at 12:00 AM ET

Verified

Edited By: Omar Filipović

Key Takeaways:

The article provides detailed specifications and performance data for the 2009 Aviat Husky A-1C-200 aircraft.
It is powered by a 200 HP Lycoming O-360-A1P engine and designed for two occupants in a tandem seating arrangement.
Key performance figures include a cruise speed of 144 mph (at 75% power) and a range of 828 statute miles (at 55% power).
The aircraft demonstrates strong Short Takeoff and Landing (STOL) capabilities with a 265 ft takeoff ground roll and a 398 ft landing ground roll, alongside a best climb rate of 1700 fpm.

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aviat

2009 AVIAT HUSKY A-1C-200

Engine make/model:

Lycoming O-360-A1P

Horsepower:

200@SL

TBO (hrs.):

2000

Propeller type:

CS Hartzell

Overall length:

22 ft. 7 in.

Overall height:

7 ft. 5 in.

Wingspan:

35 ft. 6 in.

Wing area (sq. ft.):

183

Wing loading (lbs./sq. ft.):

12

Power loading (lbs./hp):

11

Cabin width (in.):

27

Cabin height (in.):

48

Empty weight, std. (lbs.):

1320

Gross weight, std. (lbs.):

2200

Useful load, std. (lbs.):

880

Payload, full fuel (lbs.):

580

Fuel capacity (gals.):

50

Baggage capacity (lbs.):

50

Seats:

2 (tandem)

PERFORMANCE

Cruise speed, 75% power (mph.):

144

Range, 55% power (sm):

828

Best rate of climb, SL (fpm):

1700

Takeoff ground roll (ft.):

265

Takeoff over 50 ft. obstacle (ft.):

780

Landing ground roll (ft.):

398

Landing over 50 ft. obstacle (ft.):

1025

V_x (mph):

67

V_y (mph):

73

V_a (mph):

113

V_ne (mph):

153

V_so (mph):

53

Source: Aviat Aircraft

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