Turbine Leonardo

— Dual / Single IFR package — Pilot Flight/Navigation EFIS (2 displays)w/embedded FMS, — Synthetic Vision (SVS), HTAWS, slip indicator and bug panel (rbp) — Co-pilot flight/navigation EFIS (2 displays) w/ embedded FMS, — Synthetic Vision (SVS), HTAWS, slip indicator and bug panel (rbp) — EFIS pilot / co-pilot navigation synchronization switch (FMS data) — Electronic standby instrument system (ESIS) — Second radio management system (RMS) RTU-4210 Collins — Radio manager system (RMS) RTU-4210 Collins — VHF/am VHF-4000e (2 unit s ) — VOR/ILS Nav-4500 Collins — VOR/ILS/ADF/Nav-4000 — Collins • DME-4000 Collins • Radio altimeter ALT-4000 — Collins • Second attitude heading reference system (AHRS) — Second Air Data Unit (ADU) — Pilot GPS/SBAS CHELTON interfaced to EFIS/FMS — Co-pilot GPS/SBAS — CHELTON 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 C406-N HM Artex (w/ navigation interface module embedded) — 8.4 Cockpit central Display — Transponder (mode S) TRD-94 Collins — Attitude heading reference system (AHRS) w/ one dual AHRS control panel — Air data unit (ADU) — Digital audio control system (DACS) Cobham w/ additional cockpit panel — Magnetic sensor unit — LCD integrated display system ( IDS) — Dual gas generator speed indicator (N1%) — Dual turbine out let temperature indicator ( ̊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 i)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 ) — Out side air temperature indicator ( ̊c) — Two AC voltmeters — Two DC voltmeters

Exterior
— VIP/Corporate interior – 5 places (inc inter seat console) — All seat s crash-resistant covered with leather — 4-point Shoulder Harness with Inertia reels and Safety Belts for all seats — Super Silent Soundproofing — Intercommunication system for passengers — Headset BOSE ANR type (qty 5) — Cabin loudspeakers (qty 2) — Air conditioning ECS (Environment Control System) — Reading lights, emergency lights, floor courtesy lights — Upper and Lower Air Vents — Floor Carpeting — Seat Covers

— Emergency float s provisions (Fixed Parts Only – No Float Bags ) — 213 us gal crash-resistant fuel system ( in lieu of 152 US gal ) — Baggage compartment extension (2.3m) — Engine compartment fire extinguisher (qty 2) — Fuel Cap with Key-Lock — Pulsed Chip Detectors — Rotor Brake — Retractable/Rotating Landing Light (nose mounted) — Retractable/Rotating Landing Light (nose mounted) — Ground Equipment — Air Intake / Exhaust Covers • Tow bar and chocks — Pitot covers — Rotorcraft Flight Manual (RFM) and Technical Publications — Tie-downs