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la-8
INFORMATION FROM FLIGHT MANUAL FOR AMPHIBIAN AIRPLANE LA-8
Amphibian airplane LA-8 is designed for business and passenger transportation, patrolling, rendering medical aid in regions difficult of access, search and rescue, tourism and entertainment and for other operations, as well as for carrying out training flights over the earth and water surface in compliance with visual flight regulations. This airplane can take-off from and land on ground and water, paved or unpaved airfields meeting the requirements of the present Manual. In passenger option the number of seats is maximum eight, including the pilot.
Airplane LA-8 is a cantilever monoplane with upper position of the wing, conventional single-fin empennage and tricycle landing gear system, including the nose landing gear. The airplane is fitted with two power plants - two aircraft engines M-337 AK made in Czech Republic - each rated at 210 h.p.
The airplane is supposed to be used in all latitudes in Russia, in the countries of European Community, South-East Asia, the Middle East, and Latin America.
GEOMETRIC PARAMETERS
Length, m 11.10
Wing length, m * 14.0 / 15.0
The height of the parking lot, m 3.4
The maximum width of the fuselage, m 2.00
Wheel track, m 1,782
Wheelbase, m 3,432
Wing area, m * 20.2 / 22.1
DIMENSIONS OF PASSENGER (CARGO)
CAR AND COVERS
Length, m 3.45
Width, m 1.64
Height, m 1.24
Cabin volume cbm 3.7
Max. Length of cargo, m 4.43
Front upper hatch, mm 450 x 580
The rear top hatch, mm 1690 x 1290
Emergency (left, right), mm 680 x 680
PERFORMANCE DATA
Max. take-off weight, kg 2720
Max. useful payload, kg 800
Max. fuel capacity, l 1500
Technical maximum altitude, m 4500
Max. allowable operating speed, km / h 305
Max. level flight speed, km / h 275
Cruising speed (economy), km / h 235
Range, at a speed of 235 km / h
(at a commercial nagruzke800 lbs.), km / distillation 1200/4000
Time of flight at the speed of 235 km / h
(in commercial nagruzke800 kg.) h 5.6
Rate of climb, m / sec 4-6
Takeoff land / water (at max. Weight), m 350/450
Landing speed (at max. Weight), km / h 98
Max. operating load, units +3,8-1,9
* Modification - distant sea
Amphibian airplane LA-8 is designed for business and passenger transportation, patrolling, rendering medical aid in regions difficult of access, search and rescue, tourism and entertainment and for other operations, as well as for carrying out training flights over the earth and water surface in compliance with visual flight regulations. This airplane can take-off from and land on ground and water, paved or unpaved airfields meeting the requirements of the present Manual. In passenger option the number of seats is maximum eight, including the pilot.
Airplane LA-8 is a cantilever monoplane with upper position of the wing, conventional single-fin empennage and tricycle landing gear system, including the nose landing gear. The airplane is fitted with two power plants - two aircraft engines M-337 AK made in Czech Republic - each rated at 210 h.p.
The airplane is supposed to be used in all latitudes in Russia, in the countries of European Community, South-East Asia, the Middle East, and Latin America.
GEOMETRIC PARAMETERS
Length, m 11.10
Wing length, m * 14.0 / 15.0
The height of the parking lot, m 3.4
The maximum width of the fuselage, m 2.00
Wheel track, m 1,782
Wheelbase, m 3,432
Wing area, m * 20.2 / 22.1
DIMENSIONS OF PASSENGER (CARGO)
CAR AND COVERS
Length, m 3.45
Width, m 1.64
Height, m 1.24
Cabin volume cbm 3.7
Max. Length of cargo, m 4.43
Front upper hatch, mm 450 x 580
The rear top hatch, mm 1690 x 1290
Emergency (left, right), mm 680 x 680
PERFORMANCE DATA
Max. take-off weight, kg 2720
Max. useful payload, kg 800
Max. fuel capacity, l 1500
Technical maximum altitude, m 4500
Max. allowable operating speed, km / h 305
Max. level flight speed, km / h 275
Cruising speed (economy), km / h 235
Range, at a speed of 235 km / h
(at a commercial nagruzke800 lbs.), km / distillation 1200/4000
Time of flight at the speed of 235 km / h
(in commercial nagruzke800 kg.) h 5.6
Rate of climb, m / sec 4-6
Takeoff land / water (at max. Weight), m 350/450
Landing speed (at max. Weight), km / h 98
Max. operating load, units +3,8-1,9
* Modification - distant sea