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Husky Pitts Eagle
Husky :
OVERVIEW - Please click here for gallery...

The new 2005 model Husky A-1B has a completely new designed aileron with enhanced performance, as well as a larger percent span flap and flap control system.

Roll rate increases 50%

Look ma... No Spades - Our new aileron has no spade. The new aileron is mass and aerodynamically balanced. The new aileron has a deeper chord and shorter span.

Stick force pressures reduced 50%
Break out stick force cut in half, from eight pounds to about four pounds

If you were flying the airplane at 1.2 Vso in a 30-degree bank to the left and rolled it to a 30-degree bank on the right, without using the rudder, you would experience the following: 

1. Two-thirds less adverse yaw – The ball will be out of the center only one half a ball. This is one-third the adverse yaw compared to being one and one half out of center with the old style aileron.
2. Stick force pressures reduced 35 percent. One - third less stick force pressure is required to input on the control stick in order to bank the airplane at low airspeeds.
3. Less rudder input required maintaining coordinated flight.
4. Reduced pilot workload.

The new larger flap is the same semi-fowler slotted flap that we have always used, but the extended flap area is increased along the span of the wing. A beefier flap hinge and flap control system was added for durability and reliability. These improvements result in:

1. A forward pointing steepened descent. The new 2005 Husky descent at gross weight with full flaps is 880 feet per minute, compared with the prior Husky A1-B at 550 feet per minute.
2. You will see shorter landing and takeoff distance as well as steeper climbs all attributed to this flap.

These changes results in a significantly reduced pilot work load while maneuvering at low airspeeds. The pilot's legs hardly have to work the rudder controls to maintain coordination. This gives the new model Husky much more capability, versatility and a very nimble and responsive feel. Once you fly Aviat's new 2005 Husky you will experience the smoothest flying Husky you've ever flown to date.

Old Flap Handle
New Flap Handle

Aviat Aircraft has developed a new flap handle that can be retrofitted to existing Huskys for easier flap operation.

Afton, WY - Aviat Aircraft has developed a new flap handle that will be standard on all future Huskys and which can be retrofitted to existing aircraft. Designed to provide three settings, 10, 20 and 30, the new handle activates the flaps with considerably shorter travel. The leverage point for deployment is always in front of the pilot. The older flap handle required pulling the lever behind the pilot's shoulder.

The new handle offers better leverage, takes less effort and is less cumbersome to operate. It takes about one hour to change out the old flap handle and install a new one. Cost for the complete retrofit kit is $532.

Aviat Aircraft manufactures the Husky, Pup, Pitts Special and kits for the Eagle. For more information on these products, call 307.885.3151.

2005 Husky MD 200 HP
Aviat has been developing and testing our most powerful Husky yet to date. The Husky MD has been flying since August 2004. The new 2005 production airplanes are fitted with the newest aireron and extending flap wing.

High Density Altitude - Made Real Easy
I can reliably say that at 10,000 feet this airplane will climb at least 300 feet per minute more that our 180 HP Husky A-1B. It cruises in the the yellow arc. The fuel burn is at least one gallon per hour less that the carbureted 180 HP. The takeoff and climb is spectacular.

Husky® is a federally registered trademark of Aviat Aircraft, Inc.®

SPECS

Husky A-1B
Engine Lycoming 0-360-A1P, 180hp
Propeller Constant Speed
Airfoil Modified Clark Y/USA 35B
Wing Span 35' 6" 10.82m
Length 22' 7" 6.9m
Wing Area 183 sq. feet
Gross Weight 2000 lbs
Gross Weight-Floats 2200 lbs
Empty Weight 1190 lbs
Useful Load 810 lbs
Useful Load-Floats 832 lbs
Cargo Capacity 10 cu. ft./50 pounds
Wing Loading 10.9 lbs/Sq. Feet
Power Loading 11.1 lbs/hp
Fuel Capacity 52 U.S. Gal (50 gal. usable)
Fuel Rating 100 Octane Avgas
Seats Two in Tandem
Husky A-1A
Engine Lycoming 0-360-A1P, 180hp
Propeller Constant Speed
Airfoil Modified Clark Y/USA 35B
Wing Span 35' 6" 10.82m
Length 22' 7" 6.9m
Wing Area 183 sq. feet
Gross Weight 1890 lbs
Gross Weight-Floats 2079 lbs
Empty Weight 1190 lbs
Useful Load 700 lbs
Useful Load-Floats 711 lbs
Cargo Capacity 10 cu. ft./50 pounds
Wing Loading 10.3 lbs/Sq. Feet
Fuel Capacity 52 U.S. Gal (50 gal. usable)

Husky Pup

Engine Lycoming 0-320-D2A, 160 hp
Propeller Sensenich fixed-pitch (74-in. dia.) 
Airfoil Modified Clark Y/USA 35B
Wing Span 35'6" 10.82m
Length 22'7" 6.9 m
Wing Area 183 sq. Feet
Gross Weight 2000 lbs.
Empty Weight 1140 lbs.
Useful Load 860 lbs.
Cargo Capacity 50 lbs.
Wing Loading 10.9 lbs. / sq. Feet
Fuel Capacity 52 gals. (50 gals. usable)
PERFORMANCE

Husky A-1B
Top Speed 145 mph  126 kts
Cruising Speed @ 75% power 140 mph 121 kts
Cruising Speed @ 55% power 130 mph 113 kts
Stall Speed with flaps (power off) 53 mph 46 kts
Stall Speed with flaps (power on) 43 mph 37 kts
Landing Speed 58 mph 50 kts
Flaps Extend Speed 80 mph 69 kts
Take-off Distance (full-flaps land) 200 feet  
Take-off Distance (floats) approx. 6 seconds 
Landing Distance (full flaps-land) 350 feet
Rate of Climb 1,500 ft/minute
Service Ceiling 20,000 feet - MSL
Fuel Consumption @ 55% power 7.7 gal./hour 29 lts./hr
Range @ 55% power 800 miles 686 nm
Husky A-1A
Top Speed 145 mph  126 kts
Cruising Speed @ 75% power 139 mph 121 kts
Cruising Speed @ 55% power 130 mph 113 kts
Stall Speed with flaps (power off) 42 mph 36 kts
Stall Speed with flaps (power on) 33 mph 29 kts
Landing Speed 48 mph 42 kts
Take-off Distance (full-flaps land) 200 feet  
Take-off Distance (floats) approx. 6 seconds 
Landing Distance (full flaps-land) 350 feet
Rate of Climb 1,500 ft/minute
Service Ceiling 20,000 feet - MSL
Fuel Consumption @ 55% power 7.7 gal./hour 29 lts./hr
Range @ 55% power 800 miles 686 nm
Notes:
1) Performance information is based on airplane flown at gross weight under standard sea level atmospheric conditions.
2) All speed indicated at airspeeds. Takeoff and landing performance is optimum. Actual performance will depend on pilot technique, operating surfaces, and other variable factors.
 
SERVICE BULLETINS

 
Service Bulletins and Letters For Husky
Service
Bulletin #
Subject
Model
Serial#
Application
18
A-1
A-1A
A-1B
All
All prior to 1467
All prior to 2096
17
A-1
1001-1329
16
All
All
15
A-1
A-1A
A-1B
1001 and Up
All
All
14
A-1
1186, 1307
13
A-1
1001-1394
12
1001-1135,
1137-1243
11
All
10
All
9
1001-1045
8
1046-1171
7
1001-1158
6
1001-1169
5
1001-1121
1123-1125
4
1086-1168
3
1001-1138
1140, 1144
1140-1141
1146-1165
2
1001-1125
1
1001-1085
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