LEONARDO AW119Ke

– Срок передачи: В течение 3 месяцев с момента поступления денежных средств.

– Место передачи: Москва

– Команда: 1-2 пилота

– Пассажиры: 6-7

– Двигатель: Pratt & Whitney PT6B-37A

– Максимальная круизная скорость: 244 км/ч

– Максимальная дальность полета: 954 км

– Запас топлива: 870 л

– Aluminum alloy and bonded panel fuselage

– Semi-monocoque aluminum alloy tail boom

– New reinforced skid type landing gear

– Two hinged jettisonable crew doors (LH & RH)

– Two sliding passenger doors (LH and RH), 1.10 m opening, with jettisonable windows

– Acrylic windshield and side windows

– Acrylic overhead windows

– Removable fiberglass tail rotor gearbox fairing

– Quick removable tail rotor drive shaft cover

– Separate baggage compartment with hinged door

– Three jacking points

– Removable fairing and cowlings, for complete accessibility to the controls and drive components

– Quick opening hinged inspection doors, to allow visual check of engine oil levels and maintenance inspection points

– Titanium main rotor hub, corrosion protected, fully articulated with four composite grips

– Four elastomeric bearings, four individually interchangeable composite material blades, swept tips, and dampers

– Steel tail rotor hub, corrosion protected, semi-rigid delta hinged type, with two composite blades, individually interchangeable

– Cyclic and collective controls powered by two hydraulic systems

– Hydraulically powered anti-torque system

– Adjustable friction devices on cyclic and collective system

– Force trim and artificial feel system

– Adjustable directional control pedals

– Flapping and droop restraint mechanism

– Pratt & Whitney Canada PT6B-37A turbo-shaft engine

– Engine mounted fuel pump and filter assembly

– Engine mounted oil pump and filter assembly

– Engine mounted fuel control and governor

– Electronic Engine Control (EEC)

– Lubrication and cooling system

– Engine oil chip detector (1)

– Engine mounted fuel heater

– Fuel system control panel

– 3-cell fuel system (605 l – 160 USG )

– Submerged fuel pumps (2 boost and 1 transfer pump)

– RH refueling point

– 917 shp for take-off and 900 shp continuous operation main transmission

– Two-stage transmission

– Transmission mounted hydraulic pumps (2) with separate reservoir

– Internal dry sump transmission lubrication with pressure and scavenge pump and oil filter

– Transmission oil chip detectors (2)

– Single stage, bevel gear T/R 90° gear box including oil level sight glass and chip detector

– Transmission cooling and lubrication system

– Transmission shafts

– 28 V DC 22 Ah nickel-cadmium battery with temperature probe

– 200 A self-cooled starter generator

– Voltage regulator

– Battery relay

– Interconnecting bus relay

– External power relay

– Distribution buses (2)

– External power receptacle

– Position lights

– 250 W landing lights (2)

– Anti-collision lights (2)

– Cockpit utility lights (2)

– Instrument lights with dimming switch

– Radio master switch

– Airspeed indicator

– Barometric encoding altimeter

– Vertical speed indicator

– Magnetic compass indicator

– Clock, 8 days and elapsed time

– Dual tachometer backup instrument

– Master warning lights

–Master caution lights

–Warning, caution and advisory messages (on IDS displays)

–Aural warning generator system

– Inter turbine gas temperature indicator (ITT°C)

– Engine torque indicator (TQ %)

– Compressor speed indicator (N1%)

– Turbine speed indicator (N2%)

– Rotor speed indicator (NR %)

– Transmission oil pressure (PSI) and temperature (°C) indicator

– Engine oil pressure (PSI) and temperature (°C) indicator

– Fuel pressure (PSI) and fuel quantity (kg) indicator

– Two hydraulic pressure system indicators (PSI)

– Outside air temperature indicator (°C)

– Two AC voltmeters (VAC)

– DC voltmeter (VDC)

– DC ammeter (Amp)

– Convertible interior (6 places) including:

–– Soundproofing

–– Painted liners

–– Seated covered with vinyl fabric

–– 3 seats, central bench aft facing with individually foldable back panel

–– 3 seats, aft bench fwd facing with individually foldable back panel

–– 3 points shoulder harness with inertia reels and back colored safety belts for all passengers seats

–– Reading lights, advisory lights

–– Rubber carpet

–– Cabin loudspeakers

–– Baggage compartment extension (2.3m)

–– Sliders on passenger doors windows

–– Dual controls

–– Cargo Hook complete provision

– Rotor Brake

– Bird resistant windshield Pilot/ CoPilot

– Windshield wipers

– Cargo Hook 1400Kg & rear view mirror

– Wire Strike protection System

– Rotor Brake

– Steps Long Boarding (LH & RH)

– 5-cell fuel system (870 l – 230USG)

– Air intake/exhaust covers

– Ground tools kit (including tow bar, ground wheels, lifting tool)

– Pitot tubes covers

– Rotorcraft Flight Manual (RFM) and technical publications

– Tie-down fitting provisions

– Two individual pilot seats, fore and aft adjustable, with lap belts and headrests

– Aluminum alloy honeycomb reinforced floor with anti-skid finishing

– Ventilation ram-air inlets

– Anti-reflection instrument panel

– Finishing in accordance with manufacturer specification (NTA 893 A)

– Primer exterior painting

– Two individual pilot seats, fore and aft adjustable, with lap belts and headrests

– Aluminum alloy honeycomb reinforced floor with anti-skid finishing

– Ventilation ram-air inlets

– Anti-reflection instrument panel

– Finishing in accordance with manufacturer specification (NTA 893 A)

– Primer exterior painting

– Standard color scheme from Company paint selection, solid color.

– ADF KR-87 Bendix/King

– Gyrocompass C14A Honeywell

– ICSpilotAG-06-1UAgusta/Gemelli

– Pilot navigation instruments (including ADI & HSI)

– Transponder BXP 6401-1

– VHF-COM/GPS Garmin 430

– VHF-COM AR 4201

– VHF FM Motorola GM 360

– ELT (C406-2HM)