2012 LEONARDO AW139

2012

LEONARDO

AW139

41323

Used

IFR

Saskatoon, SK

2072

14,991 lb

150 knots

Yes

Yes

Yes

On Leonardo PBH plan

PRATT & WHITNEY

ON P&WC GOLD EAGLE SERVICE PLAN

PRATT & WHITNEY

ON P&WC GOLD EAGLE SERVICE PLAN

Approach plate chart holders with lights for pilot and co-pilot • TCAS I KTA-970 Honeywell Bendix/King • Concorde lead acid main battery • Weather radar primus 660 • Honeywell Wire strike protection system • Full icing protection system capable (currently disabled) • Air conditioning system • Super silent MGB premium upgrade • Nose landing gear doors • Fischer pilot and co-pilot adjustable seats with armrests (in lieu of standard seats) • Main rotor blades high visibility paint • Factory NVG compatibility for cockpit with NVG friendly cabin and external lights • 2nd GPS CMA-3024 (Canadian Marconi) • Slump pads (tow bar adapter included) • Rescue hoist single – Fixed provisions only • Wireless ICS Polycon System (UHF) • Spectrolab SX-16 Nightsun Search Light • Auxiliary transversal fuel tank 132 USG • Cargo hook cameras (Qty 2) • Auxiliary heavy duty battery 27 AH • Separation wall with sliding windows • Active vibration control system (AVCS) fixed provisions • Swiveling searchlights (two - belly mounted) • Enhanced ground proximity warning system (EGPWS) • Health & usage monitoring system (HUMS) • SATCOM - Iridium Skytrac • Technisonic TDFM 9100 P25 Tactical radio system – Cockpit & cabin control heads • MTOW 6800 Kg upgrade • Cabin external lights (Queensland lighting kit) • Agusta EMS provisions (Structural and Electrical) • Single and dual stretcher, with rescue basket capability • Medical floor & storage cabinet system • External cameras • Gaseous medical oxygen system with regulators • Medical vacuum system with regulators • EMS AC inverter with 110VAC receptacles • Ground auxiliary EMS battery & shore power • Engine inlet barrier filters • Separate cockpit/cabin ECS control zones with cockpit floor heat modifications • ACI cabin cocoon noise reduction wall panel system • Sagem moving map/multi-function display • ACI engine wash Kit

HONEYWELL

PRIMUS EPIC

Yes

Yes

Yes

Yes

Yes

Yes

Yes

Yes

ON HONEYWELL HAP PBH PROGRAM • 1st PFD (Pilot Primary Flight Display 8" × 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data • 2nd PFD (Co-pilot Primary Flight Display 8" × 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data • 1st MFD (Pilot Multifunction Display 8" × 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data • 2nd MFD (Co-pilot Multifunction Display 8" × 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data • One electronic standby instrument system (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data) • Two attitude and heading reference systems (AHRS) • Two air data modules (ADM) • Two flux valves • Two display controllers (DC) • Two cursor control devices (CCD) • One reversion control panel (RCP) • One display dimming control panel (DCP) • One stability augmentation system (SAS) control panel • Two remote instrument controllers (RIC) • Two modular avionic units (MAU) incorporating the following major subsystems and/or functions: • Vehicle monitoring system (VMS) dual • Monitor warning system (MWS) dual • Aural warning generator (AWG) single • Central maintenance computer (CMC) single • 4-axis dual digital automatic flight control system (DAFCS) • Provision for CVR/FDR data interface (single) • Flight director system (dual) • Pilot and co-pilot interphone control (cyclic grip and floor switches) • Left modular radio cabinet (MRC) with the following modules: • One VHF comm. • One VOR/LOC/GS/MB • Right modular radio cabinet (MRC) with the following modules: • One VHF Comm. • One Mode S diversity transponder • One VOR/LOC/GS/MB • One ADF • One DME • Two pedestal mounted multi control function display units (MCDU) • 1st radar altimeter RT-300 • 2nd radar altimeter RT-300 • Emergency locator transmitter (ELT) • One flight guidance controller • Honeywell GPS module with flight plan management system (FPMS) • Pilot and co-pilot digital audio panels with remote ICS audio port for ground operation • Dual electrical power connection for CVR/FDR • Cockpit voice recorder & flight data recorder with underwater locator beacon

Yes

Yes

Yes

Yes

Yes