2015 LEONARDO AW139

2015

LEONARDO

AW139

Used

2015 AW139 WITH PBH ON AIRFRAME AND ENGINE

TOTAL TIME AIRCRAFT 4265 HOURS TOTAL LANDINGS 10335 CONFIGURATION OFFSHORE

2 PRATT & WHITNEY PT6C-67C TURBINE ENGINES PROVIDING EACH 1324 KW (1776 SHP - TAKE OFF POWER RATING), FULL AUTHORITY DIGITAL ENGINES CONTROL SYSTEM (NO MECHANICAL BACKUP NECESSARY). ENGINE TYPE PRATT & WHITNEY PT6C-67C LEFT 72-00 L/H: PCE-KB1606

PRATT & WHITNEY PT6C-67C RIGHT 72-00 R/H: PCE-KB1608

PHASE 7 AVIONICS 1ST PFD (PILOT PRIMARY FLIGHT DISPLAY) 8” × 10” (EXTERNAL) COLOUR 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” (EXTERNAL) COLOUR 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” (EXTERNAL) COLOUR 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” (EXTERNAL) COLOUR ACTIVE-MATRIX LIQUID CRYSTAL DISPLAY AS PART OF HONEYWELL PRIMUS EPIC SYSTEM FOR VISUALIZATION OF FLIGHT AND NAVIGATION DATA ONE ELECTRONIC STANDBY INSTRUMENT SYSTEM (ESJS) (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) DC PRIMARY POWER GENERATION: 28 V DC REGULATED VOLTAGE PROVIDED BY TWO INDEPENDENT 300 A STARTER GENERATORS: • 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) BASIC PROVISION FOR CVR/FDR DATA INTERFACE (SINGLE) • FLIGHT DIRECTOR SYSTEM (DUAL) PILOT AND CO-PILOT HEADSETS 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 WITH EXTENDED SQUITTER (ADS-B OUT 1090 MHZ) ONE VOR/LOC/GS/MB • ONEADF • ONEDME TWO PEDESTAL MOUNTED MULTIFUNCTION CONTROL DISPLAY UNITS (MCDU) 1ST RADAR ALTIMETER RT-300 2ND RADAR ALTIMETER RT-300 EMERGENCY LOCATOR TRANSMITTER (ELT) ONE FLIGHT GUIDANCE CONTROLLER TWO HONEYWELL GPS MODULES (WAAS/SBAS - WIDE AREA AUGMENTATION SYSTEM/SATELLITE BASED AUGMENTATION SYSTEM) WITH FLIGHT PLAN MANAGEMENT SYSTEM (FPMS) PILOT AND CO-PILOT DIGITAL AUDIO PANELS WITH REMOTE JCS AUDIO PORT FOR GROUND OPERATION PILOT CLOCK (DIGITAL) CO-PILOT CLOCK (DIGITAL) ONE MAGNETIC COMPASS ONE OUTSIDE AIR TEMPERATURE INDICATOR TWO MASTER WARNING LIGHTS (MWL) TWO MASTER CAUTION LIGHTS (MCL) ENGINE 1 FIRE LIGHT ENGINE 2 FIRE LIGHT BAGGAGE COMPARTMENT SMOKE DETECTOR LIGHT DUAL ELECTRICAL POWER CONNECTION FOR CVR/FDR (FAA REQUIREMENT COMPLIANT) COCKPIT VOICE RECORDER & FLIGHT DATA RECORDER (CVR/FDR) WITH UNDERWATER LOCATOR BEACON (ULB)

FORCED FAN VENTILATION BLEED AIR HEATER AND DEFROSTER WITH AIR NOISE SUPPRESSIONS COCKPIT AIR VENTILATION BAGGAGE COMPARTMENT CARGO TIE-DOWN FITTINGS FOR INCREASED LOAD CAPACITY (300 KG) ROTOR BRAKE 1ST RADAR ALTIMETER RT300 2ND RADAR ALTIMETER RT300 4-AXIS DAFCS BASIC INCORPORATED IN MAU FLIGHT DIRECTOR SYSTEM (DUAL) 2 HONEYWELL GPS MODULES (GNSS/SBAS) WITH FPMS 1 MODE-S DIVERSITY TRANSPONDER WITH EXTENED SQUITER INCORPORATED IN THE MRC CVR/FDR WITH ULB UTILITY/OFFSHORE/PASSENGER TRANSPORT CABIN BASIC ARRANGEMENT • SOUNDPROOFING • STANDARD ROOF LINERS WITH DOME LIGHTS • POLYCARBONATE PAINTED LINERS • PA SYSTEM WITH LOUDSPEAKERS ON STD ICS • FIXED STEP FOR PASSENGER CABIN ACCESS (LH AND RH) 12-SEAT OFFSHORE INTERIOR LAYOUT • 12 PADDED LIGHTWEIGHT CRASHWORTHY OFFSHORE SEAT FABRIC COVERED WITH 4 POINT SHOULDER HARNESS ECS ENVIRO ADJUSTABLE SEATS WITH ARMRESTS CO-PILOT HINGED WINDOW (STORM WINDOW) WINDSHIELD WASHING SYSTEM PILOT HEADSET HOOKS (QTY 2) CENTRAL APPROACH PLATE HOLDER WITH LIGHT AUX HEAVY DUTY BATTERY 27AH - MARATHON IMPROVED ENGINE STARTING KIT DMU EGPWS (PROVISION + REMOVABLE) HOMP (PROVISION + REMOVABLE) ADELT (2 FREQUENCY AUTOMATIC DEPLOYABLE ELT W/ GPS INTERFACE) SATCOM IRIDIUM ISAT-200 SKYTRAC TCAS II HONEYWELL TPA100B (PROVISION + REMOVABLE) HF/SSB TRANSCEIVER HONEYWELL (PROVISIONS) VHF/FM NPX-138 NAT PROVISION + REMOVABLE) WEATHER/SEARCH RADAR PRIMUS 701 (PROVISION + REMOVABLE) LOW SPEED LDG AURAL WARNING CARGO HOOK 2200 KG (PROVISION ONLY) CARGO HOOK MONITORING CAMERAS QTY 2 EMERGENCY FLOATS (PROVISION + REMOVABLE) HEELS LIFE RAFT UP TO 17 PASSENGERS EACH QTY 2 (PROVISION + REMOVABLE) RESCUE HOIST GOODRICH - SINGLE TYPE (PROVISIONS ONLY)

PILOT AND CO-PILOT CRASHWORTHY SEATS (WITH INERTIAL REELS AND SAFETY BELTS) COCKPIT DOME/STORM LIGHT COCKPIT UTILITY LIGHTS (2) 28 V DC COCKPIT/CABIN POWER OUTLET COCKPIT PANEL SUN-GLARE SHIELDS OVERHEAD COCKPIT WINDOWS SUNSHADES FLUORESCENT EMERGENCY EXIT SIGNS TWO FLASHLIGHTS FOR PILOT AND CO-PILOT MAP AND DATA CASES IN PILOT AND CO-PILOT DOORS JCS PANEL WITH PLUG FOR ONE HEADSET (LH SIDE) AIR VENTILATION SYSTEM FIRST AID KIT LIGHT OFFSHORE SOUNDPROOFING STANDARD ROOF LINERS WITH DOME LIGHTS P.A. (PASSENGER ADDRESS) SYSTEM (INCLUDING LOUDSPEAKERS) ON STANDARD ICS FIXED STEPS FOR PASSENGER CABIN ACCESS RUBBER FLOOR CARPET 12-PADDED CRASHWORTHY COMFORTABLE SEATS FABRIC COVERED (WITH INERTIAL REELS AND SAFETY BELTS) DISPOSED ON 3 ROWS