ChuckAnderson
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Hi Everyone!
Presented here is information on the Phoenix-Aviatekhnika LKhS-4 Light Utility Transport. This aircraft was intended for commuter, air-taxi and other local tasks throughout Russia.
(Phoenix-Aviatekhnika was a joint-stock company formed in Moscow in 1991.)
-------------------------------------------------------------------------------------------------
SOURCE
The Encyclopedia of Russian Aircraft 1875-1995
pp. 285-286
Author: Bill Gunston
Original Publishers: Osprey, Great Britain, 1995
Publishers: Motorbooks International, Osceola WI, USA 1995
Copyright Bill Gunston, 1995
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TECH DATA
Type:..........................Light Utility Transport
Accomodation:..............Four (4)
Seating:.......................Two (2) Pairs (Both pairs side-by-side), [door on each side of aircraft]
Dimensions
Wingspan:....................8.2 m (26' 10 7/8")
Length:........................5.0 m (16' 4 7/8")
Weights:......................(EMPTY); 550 kg [1,213 lbs]
(MTO/MLW); 950 kg [2,094 lbs)
Engines:......................Two (2) BA3 pusher engines, driving 1.6 m (63") pressed-metal propellers
Fuel Capacity:...............Two (2) fuselage tanks, total 100 lit [22 gal]
Performance
Cruise:.........................200 km/h (124 mph)
Climb OEI:....................102 m/min (335 ft/min
Range (Max Payload):....500 km (311 miles)
TO/Landing:.................200 m (656')
Landing Gear:...............Fixed Tricycle Gear with Leaf-spring Legs and 1.5 cm2 (22 lbs/in2 Tires for soft snow or mud
Chuck
Presented here is information on the Phoenix-Aviatekhnika LKhS-4 Light Utility Transport. This aircraft was intended for commuter, air-taxi and other local tasks throughout Russia.
(Phoenix-Aviatekhnika was a joint-stock company formed in Moscow in 1991.)
-------------------------------------------------------------------------------------------------
SOURCE
The Encyclopedia of Russian Aircraft 1875-1995
pp. 285-286
Author: Bill Gunston
Original Publishers: Osprey, Great Britain, 1995
Publishers: Motorbooks International, Osceola WI, USA 1995
Copyright Bill Gunston, 1995
-------------------------------------------------------------------------------------------------
TECH DATA
Type:..........................Light Utility Transport
Accomodation:..............Four (4)
Seating:.......................Two (2) Pairs (Both pairs side-by-side), [door on each side of aircraft]
Dimensions
Wingspan:....................8.2 m (26' 10 7/8")
Length:........................5.0 m (16' 4 7/8")
Weights:......................(EMPTY); 550 kg [1,213 lbs]
(MTO/MLW); 950 kg [2,094 lbs)
Engines:......................Two (2) BA3 pusher engines, driving 1.6 m (63") pressed-metal propellers
Fuel Capacity:...............Two (2) fuselage tanks, total 100 lit [22 gal]
Performance
Cruise:.........................200 km/h (124 mph)
Climb OEI:....................102 m/min (335 ft/min
Range (Max Payload):....500 km (311 miles)
TO/Landing:.................200 m (656')
Landing Gear:...............Fixed Tricycle Gear with Leaf-spring Legs and 1.5 cm2 (22 lbs/in2 Tires for soft snow or mud
Chuck
