Aviat Husky

The utility taildragger built for backcountry flying.

Overview

Aviat United States ICAO: HUSK 1987–Present Active $240,000

The Aviat Husky is a high-wing tailwheel aircraft introduced in the 1980s. Designed for short-field and backcountry operations, it emphasizes durability and simplicity. The aircraft remains in production.

Live Fleet Activity (HUSK)

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Specifications

Units
Engine
1 × Lycoming 0-360-A1P
Engine type
Piston
Power
180 hp · 134 kW
Avionics
VHF comm radio
Wing tips
No winglets
Seats
2
Crew
Cabin width
2 ft 0 in  ·  0.60 m
Cabin height
3 ft 11 in  ·  1.20 m
Cabin length
Exterior length
24 ft 10 in  ·  7.56 m
Tail height
11 ft 6 in  ·  3.51 m
Fuselage diameter
3 ft 3 in  ·  1.00 m
Wing span
35 ft 6 in  ·  10.82 m
Baggage volume
18 ft³  ·  0.5 m³
Gross weight
Empty weight
Max takeoff weight
2,200 lb  ·  1,000 kg
Max landing weight
Max payload
950 lb  ·  400 kg
Fuel capacity
50 gal · 200 L · 100 kg (AvGas)
Max cruise speed
120 kt  ·  138 mph  ·  222 km/h
Maximum speed
Cruise speed
Approach speed
Range
700 nm  ·  810 mi  ·  1,300 km
Fuel burn
26.00 nm/gal  ·  12.72 km/L
Ceiling
20,000 ft  ·  6,100 m
Rate of climb
1,500 ft/min  ·  8 m/s
Takeoff distance
200 ft  ·  60 m
Landing distance
350 ft  ·  110 m
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Aviat A-1B ‘Husky’

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Operational Context

Aviat Husky — light utility tailwheel aircraft

The Husky first flew in 1986 and entered service shortly thereafter. It features a fabric-covered fuselage and fixed landing gear. The aircraft is optimized for rugged terrain and remote strips.

A piston engine producing approximately 180 horsepower powers the aircraft. Cruise speed approaches 120 knots (222 km/h). Maximum takeoff weight exceeds 2,200 pounds (998 kg).

The Husky is popular among bush pilots and recreational flyers. Its STOL performance supports operations in challenging environments. Production continues in updated variants.