2006 Aviat Husky A-1B-200

Sunday, April 01, 2007 at 12:00 AM ET

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Key Takeaways:

The article details the specifications for the 2006 Aviat Husky A-1B-200, including its Lycoming IO-360-A1D6 engine with 350 horsepower.
It is a two-seat aircraft with a fixed tailwheel, a gross weight of 2000 lbs, a useful load of 680 lbs, and a fuel capacity of 52 gallons.
Key dimensions include a 35 ft. 6 in. wingspan and an overall length of 22 ft. 7 in.
Performance highlights include a cruise speed of 138 mph, a max range of 828 nm, a best rate of climb of 1700 fpm, and remarkably short takeoff (265 ft.) and landing (398 ft.) ground rolls.

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aviat husky

2006 Aviat Husky A-1B-200

Engine make/model:

Lycoming IO-360-A1D6

Horsepower@altitude:

350 (x2)

TBO (hrs):

200@SL

Propeller type:

MTV-15-B/205-58

Airfoil:

Modified Clark Y

Landing gear type:

Fixed tailwheel

Gross weight (lbs.):

2000

Max landing weight (lbs.):

2000

Empty weight, std. (lbs.):

1320

Useful load, std. (lbs.):

680

Fuel capacity, std. (gals.):

52

Oil capacity (qts.):

8

Baggage capacity (cu.ft./lbs.):

50

Payload, full std. fuel (lbs.):

380

Wingspan:

35 ft. 6 in.

Overall length:

22 ft. 7 in.

Height:

7 ft. 5 in.

Wing area (sq. ft.):

183

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

10.9

Power loading (lbs./hp.):

10

Seating capacity:

2

Cabin width (in.):

48

Cabin height (in.):

27

PERFORMANCE

Cruise speed (kts.):

55% power (mph/gps):

138

Max range (nm):

828

Fuel consumption (gph):

7.6

Dirty stall speed (kts.):

53

Best rate of climb, SL (fpm):

1700

Service ceiling (ft.):

20,000

Takeoff ground roll (ft.):

265

Takeoff over 50 ft. obstacle (ft.):

780

Landing ground roll (ft.):

398

Landing over 50 ft. obstacle (ft.):

1025

Source: Aviat Aircraft