manufacturer
Leonardo
configuration
VIP
condition
Used
year
2024
time
15.5
helicopter location
United States
serial number
15016
registration number
N694SH
listing ID
HT17809
Description
Helicopter highlights include:
• Immediate availability (factory deliveries not available until late 2025)
• VIP 6 seat interior (3 fwd / 3 aft)
• Soundproofing / floor carpeting
• Air conditioning
• 230 US Gallon fuel system
• Baggage compartment extension
avionics
• Garmin G1000NXi Integrated Flight Deck system comprising:
• Two (2) GDU-1050H display units providing a Primary Flight Display (PFD) and a Multifunction Display (MFD) and integrating:
- Flight Management System (FMS)
- Synthetic Vision System (SVS)
- Helicopter Terrain Awareness and Warning System (HTAWS)
- Radio tuning controls
• Two (2) GEA-71BH Aircraft Interface Unit
• GRS-7800 AHRS
• GDC-72H Air Data Computer (ADC)
• Two GIA-64H Integrated Avionics Units (IAU) comprising: COM 1&2, NAV 1&2, GPS 1&2, Aural Alert Generator
• Transponder GTX-345R Mode-S/ADS-B dual mode 1090 Extended Squitter (ES) ADS-B Out plus 1090 and 978 ADS-B In compliant position source (WAAS/GPS)
• Airframe Hour meter
• Central Maintenance Computer (CMC) data logging Radar Altimeter GRA-55
• Digital Audio Control System (DACS) COBHAM with two (2) cockpit panels
• Magnetic Compass indicator
• L3 Avionics System EFD 750 Electronic Standby Indicator
• AC power supply system (two [2] inverters)
• AFCS 3-axis duplex SP-711 Honeywell
• Emergency Locator Transmitter
SYSTEMS DATA (on PFD/MFD)
• Inter turbine gas temperature indicator (ITT°C) (on MFD)
• Power index (on PFD)
• Engine torque indicator (TQ%) (on MFD)
• Compressor speed indicator (N1%) (on MFD)
• 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 (2) hydraulic pressure system indicators (PSI)
• Outside air temperature indicator (°C) (on PFD)
• DC voltmeter (VDC)
• DC ammeter (Amp)
CENTRAL WARNING SYSTEM (CWS)
• Master warning lights
• Master caution lights
• Warning, caution and advisory messages on PFD display
• Aural alerts
AVIONICS EQUIPMENT
1X-K-070-5CM TAS GTS 800 Garmin
ELECTRICAL SYSTEM
• 28 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
• Two (2) LED landing lights
• Two (2) anti-collision lights
• Two (2) cockpit utility lights
• Instrument lights
• Radio master switch
equipment
• Active Noise Reduction (ANR) headsets (pilot and co-pilot)
• Baggage compartment lights
• Crew open door actuators
• First aid kit
• Fuel drain electrical valves
• Portable fire extinguisher
• Quick disconnecting chip detectors
• Shoulder harness with inertial reels (pilot and co-pilot)
• Tail boom strake
• Baggage compartment extension (1.9 m): It may be affected by avionic customization
• Dual controls
• Fuel cap with key-lock
• Reinforced windshields (pilot and co-pilot)
• Rotor brake
• Sliding windows on cockpit doors
• Windshield wipers (pilot and co-pilot) with wiper switch on cyclic grips
• Hourmeter (engine run-time)
• Pulsed chip detectors: In lieu of quick disconnecting chip detectors.
UTILITY EQUIPMENT
• 1X-K-151-3CM: Air conditioning
• 1X-K-101-6CM: 230 USgal fuel system
In lieu of 160 USgal
• 1X-K-103-6CM: Baggage compartment extension (2.3 m)
MISCELLANEOUS / GROUND EQUIPMENT
• Air intake / exhaust covers
• Ground tools kit (including tow bar, ground wheels, lifting tool)
• Pitot tube cover
• Rotorcraft Flight Manual (RFM) (hard copy) and technical publications (soft copy)
• Tie-down fitting (main rotor retention straps)
interior
INTERIOR EQUIPMENT - CABIN
• 1X-A-020-3CM VIP interior - 6 places
• Soundproofing
• Leatherette covered liners
• Seats covered with leather
• 3 aft facing seats (central bench)
• 3 fwd facing seats (aft bench)
• 3-point shoulder harness with inertial reels and safety belts for all passenger seats
• Reading lights, advisory lights
• Cabin loudspeakers
• Headset Bose ANR type (Qty 6)
• Floor carpeting
INTERIOR ARRANGEMENT
• Pilot and co-pilot seats, fore and aft adjustable, with lap belts and headrests
• Aluminium alloy honeycomb reinforced floor with anti-skid finishing
• Ventilation ram air inlets
• Anti-reflection instrument panel
• Bleed air heater
• Primer finished cabin walls
exterior
• Finishing in accordance with manufacturer specification
• Primer exterior painting
FINISHING - PAINTING
• Standard painting and finishing
• Up to 4 colours from LHD selection
• 1X-K-001-8CM: Customized painting and finishing
• Customized colours
• Customized painting scheme and finishing
• Registration marks and logos (decal)
general characteristics
• Aluminium alloy and bonded panel fuselage
• Semi-monocoque aluminium alloy tail boom
• Reinforced skid type landing gear - black colour
• Two (2) hinged jettisonable crew doors (LH and RH)
• Two (2) sliding passenger doors (LH and RH), 1.10 m opening, with jettisonable windows
• Passenger short foot step (LH and RH)
• Polycarbonate windshield and side azure coloured windows
• Overhead cockpit azure coloured windows
• Lower cockpit azure coloured windows
• Removable composite tail rotor gearbox fairing
• Quick removable tail rotor drive shaft cover
• Separate baggage compartment with hinged door
• Three (3) 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
• Grounding point
engine 1
• 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
• One (1) engine oil chip detector
• Engine mounted fuel heater
• Fuel system control panel
• 3-cell crash-resistant fuel system
• Submerged fuel pumps (two [2] boost and one [1] transfer pump)
• RH refuelling point
TRANSMISSION / DRIVE SYSTEM AND HYDRAULIC SYSTEM
• 917 shp for take-off and 900 shp continuous operation main transmission
• 2-stage transmission
• Two (2) transmission mounted hydraulic pumps with separate reservoir
• Internal dry sump transmission lubrication with pressure and scavenge pump and oil filter
• Two (2) transmission oil chip detectors
• Single stage, bevel gear T/R 90° gear box including oil level sight glass and chip detector
• Transmission cooling and lubrication system
• Transmission shafts
ROTORS AND CONTROLS
• Titanium main rotor hub, corrosion protected, fully articulated with four (4) composite grips, four (4) elastomeric bearings, four (4) individually interchangeable composite material blades, swept tips, and dampers
• Steel tail rotor hub, corrosion protected, semi-rigid delta hinged type, with two (2) composite blades, individually interchangeable
• Cyclic and collective controls powered by two (2) 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
