HB-XLQ - 2016 LEONARDO AW189

2016

LEONARDO

AW189

Used

HB-XLQ

IFR

LSTS

Low time machine with only 876 hours since new. Available for immediate delivery ex Switzerland. Machine fully Offshore or as utility configuration. VIP Interior and Air Conditioning could be installed.

876

18,959.75 lb

11,602.93 lb

Basic design Standard helicopter AW189: Airframe • Aluminum alloy/composite airframe structure including nose radome, cockpit, main cockpit with flat floor and luggage compartment, tail boom, vertical stabilizer, horizontal stabilizers, outer fuel tank housing • Attachments for the main gearbox and engines / APU Upper deck cowling (one slides back/one slides forward, two side cowlings for engine access that can be used as service platforms) • Step for service and access to the upper deck (left side) • Retractable three-wheel landing gear with two wheels on the nose landing gear, one-wheel and with brakes on the main landing gear with tie-down rings • Wheel brake parking electric module (WBPEM) • Two heated pitot tubes • Two heated static air intakes • Forced supply ventilation • Air heater and defroster with noise suppression • Adjustable cockpit air ducts • Cockpit instrument panel, overhead panel and console between seats • Cockpit acrylic windshields • Pilot and co-pilot windshield wipers • Overhead cockpit windows • Lower cockpit windows • Two pilot doors with emergency exit windows and a "storm window" on the pilot's side (right) • Lower window for pilot/co-pilot doors • Two handles in sliding doors for passenger access to the cabin • Eight emergency exit windows (two on each door of the passenger cabin) • Luggage compartment with 2 lockable luggage compartment doors on the left and right side Luggage compartment attachment fitting • Anti-corrosion protection

2.2. Rotors and controls • Fully articulated main rotor system (M/R) with five composite blades, five composite couplings, five elastomeric bearings and five hydraulic shock absorbers. • Fully articulated tail rotor system (T/R) with four composite blades, four elastomeric bearings and four elastomeric shock absorbers • Rotating main rotor and tail rotor actuators with elastomeric bearings • Flight controls for the pilot (collective pitch, pedals) • Flight controls for the co-pilot (collective pitch, pedals) • Control loading system • Four (4-axis autopilot) parallel trim actuators • Two dual digital linear actuators

GENERAL ELECTRIC

876

Power Unit and Fuel Systems • Two turbo-shaft engines General Electric GE ST7-2E1 with integrated particle separator • Microturbo E APU 60 auxiliary power unit (can be used as an emergency electric generator in flight) • Heated air intake anti-icing system • Three heated fuel systems and three magnetic chip detectors (one for each engine and APU) • Three complete fuel filters (one for each engine and one for APU) • Two separate dual-channel FADEC systems (one for each engine) with automatic start, auto relight, engine control functions for normal, emergency and training operations. • Engine control panel • One electronic engine control unit for APU • Group of engine compartments (engine and APU mountings, firewalls, cowlings, drains, exhaust) • Fire detection system (engines and APU) • Fire extinguishing system (one fire extinguishing bottle for each engine compartment and one separate fire extinguishing bottle for the APU compartment) • Fire alarm and extinguisher control panel • Two crashworthy fuel tanks (1,043 kg – 2,299 lb / 1,304 l – 344 US gallons) • Gravity refueling on left hand side • Two supply pumps on engines • Two booster pumps submerged in the fuel tank • Engine cross-feed fuel valves

GENERAL ELECTRIC

876

Yes

Yes

Yes

Yes

Yes

Yes

Yes

Yes

Standard Avionics Package -Cockpit display system (CDS) -Four Rockwell Collins 10 x 8'' (internal dimensions) color LCDs with LED backlighting and NVIS compatibility, two of which are normally used as primary flight displays (PFD) and two as multifunctional displays (MFD) -One integrated standby instrument system (ISIS) -Two display control panels (DCP) -Two cursor control devices (CCD) • One reversionary control panel (RCP) • One dimmable display panel (DDP) • Two master caution lights (MCL) • Two master warning lights – critical (MWL) • Two avionics ethernet full duplex switches (AFDX) • Aircraft mission and management system (AMMS) • Two aircraft mission and management computers (AMMC) • One data transfer device (DTD) • Two multi-function control and display units (MCDU) • Four-axis automatic flight control system (AFCS) – an aircraft autopilot system • One dual flight control computer (FCC) • Flight control system (FCS) control panel Navigation and radio communication equipment • Two VHF radio stations • Two NAV receivers (VOR/ ILS/MB) • One automatic direction finder (ADF) • One distance measurement equipment (DME) • One transponder with enhanced surveillance mode (S mode) • One satellite-based augmentation system (SBAS) GPS (WAAS / EGNOS / MSAS) Interphone communication system • Two audio control panels (ACP) (pilot and co-pilot stations) • One audio management unit (AMU) 5 interacting with external transmitting and receiving devices • One passenger intercom amplifier (PIA) Basic Flight Instruments • Two flux valves • Two attitude and heading reference systems (AHRS) • Two air data systems (ADS) • One radar altimeter • Two clocks • One backup magnetic compass Integrated Control System • Two helicopter control computers • Two computer control displays

Yes

Yes

Yes

Yes

- Hoist hard points and provisions - Cargo Hook provisions - Fully Offshore Equipment with Life Rafts • The luggage compartment capacity has been increased to 360 kg. • Vertical luggage net (instead of luggage compartment net) • Cargo hook (2800 kg / 6180 lbs) – hard points and preparation for installation • Autonomous emergency exit lighting system • Emergency floats • External life rafts (2x21) • Wire cutter (upper) • Stroboscopes on winglets • Auxiliary underfloor fuel tank (190 kg – 419lb / 238 l – 63 US gallons) • Auxiliary transverse fuel tank (418 kg – 922 lbs / 522 l – 138 US gallons) • Anti-corrosion protection for marine environments • Dual Hoist - preparation and hard points • Preparation for installation of a joystick to control the helicopter (within small hovering range) from the winch operator's seat • Icing sensor Mission equipment • Kit for increasing takeoff weight to 8,600 kg • Convex windows (for maximum visibility down and to the side) in the passenger cabin - Passenger cabin carpet (Baltiflex) - Windshield washer system - Luggage compartment floor carpet (Baltiflex) - The main rotor and tail rotor are painted in a bright contrasting color to enhance their visibility - Set of Tie downs and Cargo net. - Tow bar

2020

2016

16

Yes

Yes

EASA R.510

Yes