Description
HIGHLIGHTS
- Delivery time
- 5 year Leonardo warranty
- Elite completion package
- Hangared near Heathrow Int Airport, UK
ENGINES
Pratt & Whitney PW207C Turboshaft
Engine 1
S/N: PCE-BH1137
TSN: 50
Landings: 9
Engine 2
S/N: PCE-BH1139
TSN: 50
Landings: 9
Engine 1
S/N: PCE-BH1137
TSN: 50
Landings: 9
Engine 2
S/N: PCE-BH1139
TSN: 50
Landings: 9
Avionics
FLIGHT / NAVIGATION INSTRUMENTS
Pilot flight/navigation EFIS (1 display) with slip indicator and Remote Bug Panel (RBP)
Radio Management System (RMS) RTU-4210 Collins (1)
VHF/AM VHF-4000E
VOR/ILS NAV-4500 Collins
Transponder (Mode S) TDR-94 Collins
Attitude Heading Reference System (AHRS) (1) with one dual AHRS control panel
Air Data Unit (ADU) (1)
Digital Audio Control System (DACS) COBHAM with one cockpit panel
Electronic clock (1)
Magnetic compass indicator (1)
Magnetic sensor unit
Pitot tube right/left
INSTRUMENTATION (ON IDS DISPLAY)
LCD Integrated Display System (IDS)
Dual gas generator speed indicator (N1%)
Dual turbine outlet temperature indicator (TOT°C)
Dual torque meter indicator (TQ%)
Dual power turbine speed indicator (N2%)
Rotor speed indicator (NR%)
Transmission oil pressure (PSI) and temperature (°C) indicator
Two engine oil pressure (PSI) and temperature (°C) indicators
Two fuel pressure indicators (PSI)
Two fuel quantity indicators (Kg)
Two fuel flow indicators (kg/hr)
Two flight controls hydraulic system pressure indicators (PSI)
Two utility hydraulic system pressure indicator (PSI)
Outside air temperature indicators (°C)
Two AC voltmeters (VAC)
Two DC voltmeters (VDC)
Two DC ammeters (Amp)
SINGLE PILOT DUAL CONTROLS IFR AVIONIC PACKAGE
Pilot flight/navigation EFIS (2 displays) with embedded FMS, Synthetic Vision (SVS), HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and remote Bug Panel (RBP)
(*) In lieu of basic Pilot flight/navigation EFIS (1 displays) with slip indicator and Remote Bug Panel (RBP)
(**) Data services subscription for the update of the Navigation databases from Jeppesen is under Customer’s responsibility
Co-pilot flight/navigation EFIS (2 displays) with embedded FMS, Synthetic Vision (SVS), HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and remote Bug Panel (RBP)
Reversionary Control Panel (RCP)
EFIS pilot/co-pilot navigation synchronization switch (FMS data)
Electronic Standby Instrument system (ESIS)
Second Radio Management System (RMS) RTU-4210 Collins
Second VHF/AM VHF-40000E Collins
VOR/ILS/ADF NAV-4000 Collins
DME DME-4000 Collins
Radio Altimeter ALT-4000 Collins
Second Attitude Heading Reference System (AHRS)
Second Air Data Unit (ADU)
Pilot GPS/SBAS Genesys Aerosystems interfaced to EFIS/FMS
Co-pilot GPS/SBAS Genesys Aerosystems interfaced to EFIS/FMS
Digital Audio Control System (DACS) COBHAM additional cockpit panel
4-axis dual duplex digital AFCS with integrated Flight Director
Second electronic clock
Second magnetic compass indicator
ELT
Dual controls
WARNING / CAUTION ADVISORY & MAINTENANCE SYSTEM
Master warning lights (2)
Master caution lights (2)
Warning, caution and advisory message (on IDS display)
Aural warning generator system
Engine fire detection system
Exceedance recorder system (on IDS display)
Warning horn (cabin)
Pilot flight/navigation EFIS (1 display) with slip indicator and Remote Bug Panel (RBP)
Radio Management System (RMS) RTU-4210 Collins (1)
VHF/AM VHF-4000E
VOR/ILS NAV-4500 Collins
Transponder (Mode S) TDR-94 Collins
Attitude Heading Reference System (AHRS) (1) with one dual AHRS control panel
Air Data Unit (ADU) (1)
Digital Audio Control System (DACS) COBHAM with one cockpit panel
Electronic clock (1)
Magnetic compass indicator (1)
Magnetic sensor unit
Pitot tube right/left
INSTRUMENTATION (ON IDS DISPLAY)
LCD Integrated Display System (IDS)
Dual gas generator speed indicator (N1%)
Dual turbine outlet temperature indicator (TOT°C)
Dual torque meter indicator (TQ%)
Dual power turbine speed indicator (N2%)
Rotor speed indicator (NR%)
Transmission oil pressure (PSI) and temperature (°C) indicator
Two engine oil pressure (PSI) and temperature (°C) indicators
Two fuel pressure indicators (PSI)
Two fuel quantity indicators (Kg)
Two fuel flow indicators (kg/hr)
Two flight controls hydraulic system pressure indicators (PSI)
Two utility hydraulic system pressure indicator (PSI)
Outside air temperature indicators (°C)
Two AC voltmeters (VAC)
Two DC voltmeters (VDC)
Two DC ammeters (Amp)
SINGLE PILOT DUAL CONTROLS IFR AVIONIC PACKAGE
Pilot flight/navigation EFIS (2 displays) with embedded FMS, Synthetic Vision (SVS), HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and remote Bug Panel (RBP)
(*) In lieu of basic Pilot flight/navigation EFIS (1 displays) with slip indicator and Remote Bug Panel (RBP)
(**) Data services subscription for the update of the Navigation databases from Jeppesen is under Customer’s responsibility
Co-pilot flight/navigation EFIS (2 displays) with embedded FMS, Synthetic Vision (SVS), HTAWS (Helicopter Terrain Awareness and Warning System), slip indicator and remote Bug Panel (RBP)
Reversionary Control Panel (RCP)
EFIS pilot/co-pilot navigation synchronization switch (FMS data)
Electronic Standby Instrument system (ESIS)
Second Radio Management System (RMS) RTU-4210 Collins
Second VHF/AM VHF-40000E Collins
VOR/ILS/ADF NAV-4000 Collins
DME DME-4000 Collins
Radio Altimeter ALT-4000 Collins
Second Attitude Heading Reference System (AHRS)
Second Air Data Unit (ADU)
Pilot GPS/SBAS Genesys Aerosystems interfaced to EFIS/FMS
Co-pilot GPS/SBAS Genesys Aerosystems interfaced to EFIS/FMS
Digital Audio Control System (DACS) COBHAM additional cockpit panel
4-axis dual duplex digital AFCS with integrated Flight Director
Second electronic clock
Second magnetic compass indicator
ELT
Dual controls
WARNING / CAUTION ADVISORY & MAINTENANCE SYSTEM
Master warning lights (2)
Master caution lights (2)
Warning, caution and advisory message (on IDS display)
Aural warning generator system
Engine fire detection system
Exceedance recorder system (on IDS display)
Warning horn (cabin)
Additional Info
STANDARD EQUIPMENT
Active Noise Reduction (ANR) headset (pilot and co-pilot)
Baggage compartment lights
Crash-resistant co-pilot seat, fore and aft adjustable, with lap belts and headrest
Crew open door actuators
First aid kit
Fuel drain electrical valves
Internal structural provisions for utility equipment
Portable fire extinguisher
Shoulder harness with inertial reels (pilot and co-pilot)
Tail boom strake
ADDITIONAL EQUIPMENT
Airframe hourmeter
Baggage compartment extension (2.3m)
Engine compartment fire extinguishers (Qty 2)
Fuel cap with key-lock
Pulsed chip detectors (in lieu of quick disconnecting chip detectors)
Reinforced windshields
Retractable/rotating landing light (nose mounted)
Rotor brake
Windshield wipers (pilot and co-pilot) with wiper switch on cyclic grips
MISCELLANEOUS / GROUND EQUIPMENT
Air intake/exhaust covers
Ground tools kit (including tow bar, lifting tool, wheel chocks)
Pitot tubes covers
Rotorcraft Flight Manual (RFM) and technical publications
Tie-down fittings (main rotor retention straps)
CUSTOMER SELECTED EQUIPMENT
-Painting
Customized painting scheme, Premium Plus; up to 5 colours from selection, Premium finishing, Registration Marks and Logos (decal or painted)
-Utility Equipment
213 USgal crash-resistant fuel system (in lieu of 152 USG)
High-intensity white strobe lights on horizontal stabilizer
Electrically operated passenger step (LH)
-Avionic Equipment
Traffic Advisory System TAS-620 Avydine (presented on EFIS)
Weather radar RDR 2000 Bendix/King or equivalent model (presented on EFIS)
iPad certified mount with USB charger point for USB A and C in cockpit (installed by Sloane post-delivery)
8.4” cockpit central display – provision
Enhanced Vision System (EVS) Max-Viz 2300 – provision
Cockpit Voice/Flight Data Recorder (CVR/FDR) Penny & Giles - provision
Active Noise Reduction (ANR) headset (pilot and co-pilot)
Baggage compartment lights
Crash-resistant co-pilot seat, fore and aft adjustable, with lap belts and headrest
Crew open door actuators
First aid kit
Fuel drain electrical valves
Internal structural provisions for utility equipment
Portable fire extinguisher
Shoulder harness with inertial reels (pilot and co-pilot)
Tail boom strake
ADDITIONAL EQUIPMENT
Airframe hourmeter
Baggage compartment extension (2.3m)
Engine compartment fire extinguishers (Qty 2)
Fuel cap with key-lock
Pulsed chip detectors (in lieu of quick disconnecting chip detectors)
Reinforced windshields
Retractable/rotating landing light (nose mounted)
Rotor brake
Windshield wipers (pilot and co-pilot) with wiper switch on cyclic grips
MISCELLANEOUS / GROUND EQUIPMENT
Air intake/exhaust covers
Ground tools kit (including tow bar, lifting tool, wheel chocks)
Pitot tubes covers
Rotorcraft Flight Manual (RFM) and technical publications
Tie-down fittings (main rotor retention straps)
CUSTOMER SELECTED EQUIPMENT
-Painting
Customized painting scheme, Premium Plus; up to 5 colours from selection, Premium finishing, Registration Marks and Logos (decal or painted)
-Utility Equipment
213 USgal crash-resistant fuel system (in lieu of 152 USG)
High-intensity white strobe lights on horizontal stabilizer
Electrically operated passenger step (LH)
-Avionic Equipment
Traffic Advisory System TAS-620 Avydine (presented on EFIS)
Weather radar RDR 2000 Bendix/King or equivalent model (presented on EFIS)
iPad certified mount with USB charger point for USB A and C in cockpit (installed by Sloane post-delivery)
8.4” cockpit central display – provision
Enhanced Vision System (EVS) Max-Viz 2300 – provision
Cockpit Voice/Flight Data Recorder (CVR/FDR) Penny & Giles - provision
