Patriot Air is the memeber of the company REDENLAKE LTD SA. REDENLAKE LTD SA is the official representative of the repair shop TORA KSAMC in Bolivarian Republic of Venezuela.
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Airplanes
Aircraft L410UVP / L410UVP-E
The aircraft L-410UVP/L410UVP-E assigns to passengers, mail and cargo traffics at the local airlines and it is the one of best the aircrafts in this aviation category.
The equipments of this aircraft and the aircraft performance characteristics allow to operate this aircraft in different climatic, geographic and meteorological terms as made-up as ground runaway.
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General Characteristics
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Purpose
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Passenger and cargo
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Date of manufacture
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1979-1985
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Crew
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2 (pilot, co-pilot)
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Capacity
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15 passengers
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Fixed resourse
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20000 hour 30000 landing
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TBO
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4800 hours 10 years
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Dimensions
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Wingspan
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19.48 m
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Wing area
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35.19 m2
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Length
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14.424 m
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Height
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5,83 m
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Fuselagewidth, max
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2.08 m
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Cabin length
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6.34 m
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Cabindiameter, max
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1.95 m
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Cabin height, max
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1.66 m
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Entrance door
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0.80 x 1.46 m
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Volume of passenger saloon
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17.9 m3
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Volume of baggage space
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1.370 m3
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Landing gear tread
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3.650 m
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Wheelbase
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3.666 m
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Weight
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Empty weight
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3800 kg
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Max takeoff weight
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5800 kg
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Loaded weight
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5500 kg
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Payload
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1280 kg
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Weight of fuel
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1000 kg
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Speed
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Maximum operating speed of flight
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410 km/ hour
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Cruising speed
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355 km/ hour
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Length and speed of takeoff and landing run
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Length of takeoff run
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425 m
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Length of landing run
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300 m
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Needed length of aerodrome
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800 (+ 100) m
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Takeoff speed
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145 km/hour
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Landing speed
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135 km/hour
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Distance and height of flight
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Flight distance with complete commercial payload
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400 km (3000 m, 15 passengers, 1310 kg commercial load, baggage, reserve stock in 30 min)
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Flight distance with maximal weight of fuel
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1200 km
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Height of flight (with oxygen device)
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3000 m (4200 m)
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Powerplant
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Engine
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Walter M601D(8)
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Type of engine
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Turboprop two-shaft with free turbine
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Quantity
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2
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Fuel
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Aviation kerosene Ò-1, ÒÑ-1, ÏË-6,ÐÒ or mix
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Maximal rotation frequency of turbo compressor
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37210 rpm
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Rotation frequency of propeller
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2080 rpm
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Power
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574 kW (700 hp)
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Increasing rate of pressure in the compressor
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6,55
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Max. reverse (shp/kW)
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435 / 325
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Gas generator speed (%)
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99
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Water injection
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yes
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Specific consumption of fuel:
- takeoff regime
- cruise regime
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394 g/kWhour
294 g/kWhour
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Weight
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200 kg/ each
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Dimensions
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650/590/1675 mm
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TBO
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1500 hours 2250 cycles 5 years
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Propellers
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Propeller
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V508D
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Number of blades
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3
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Propeller diameter
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basic 99 in. (2500 mm)
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Propeller type
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Tractor
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Direction of rotation
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clockwise (viewed from behind of the aircraft)
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Type of operation
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constant speed, full feathering and reversing
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Blade-pitch change operation
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Hydraulic, double acting
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Maximum horsepower rating
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up to 750SHP (560 kW)
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Maximum rated speed
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2080 RPM
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Dry, rotating prop weight
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152 lbs (69 kg) - basic version
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Propeller system accessories
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Governor, Overspeed governor, Auxiliary pump, De-icing system
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TBO
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2000 hours 6 years
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TOP positions
The aircraft L-410UVP/L410UVP-E assigns to passengers, mail and cargo traffics at the local airlines and it is the one of best the aircrafts in this aviation category.
The equipments of this aircraft and the aircraft performance characteristics allow to operate this aircraft in different climatic, geographic and meteorological terms as made-up as ground runaway.
The WALTER M601 series engines have been designed for commuter, agricultural, and trainer aircraft. The WALTER M601 engine is a free power turbine turboprop engine.
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