Description:

Offshore configured helicopters with a 12 or 15 seat configuration in excellent condition
- 6800 MTOW
- FADEC Pratt & Whitney Engines PT6C-67C

Avionics/Radios:
1st PFD (Pilot Primary Flight Display 8" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

2nd PFD (Copilot Primary Flight Display 8" x 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" x 10" color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

2nd MFD (Copilot Multifunction Display 8" x 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 (2) Attitude and Heading Reference Systems (AHRSs)
Two (2) Air Data Modules (ADMs)
Two (2) flux valves
Two (2) Display Controllers (DCs)
Two (2) Cursor Control Devices (CCDs)
Reversion Control Panel (RCP)
Display Dimming Control Panel (DCP)
Stability Augmentation System (SAS) control panel
Two (2) Remote Instrument Controllers (RICs)
Pilot and Copilot interphone control (cyclic grip and floor switches)
Pilot and copilot headsets
Two pedestal mounted MCDUs (Multi Control Function Display Units)

Left Modular Radio Cabinet (MRC) with the following modules:
- One VHF Comm
- One VOR/LOC/GS/MB
-1st Radar Altimeter (RT - 300)
-2nd Radar Altimeter System (RT - 300)
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Two Modular Avionic Units (MAUs) 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 Digital Automatic Flight Control System - DAFCS (Basic)
- Provision for CVR/FDR data interface (single)
- Flight Director System (dual)

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

Emergency Locator Transmitter (ELT)
One Flight Guidance Controller
Honeywell GPS module with Flight Plan Management System (FPMS)
Pilot and copilot digital audio panels with remote ICS audio port for ground operation
Pilot clock (digital)
Copilot clock (digital)
Magnetic compass
Outside Air Temperature indicator
Two (2) Master Warning Lights (MWLs)
Two (2) Master Caution Lights (MCLs)
Engine 1 Fire Light
Engine 2 Fire Light
Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB)
Dual electrical power connection for CVR/FDR (FAA requirement compliant)
Baggage compartment smoke detector light
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Additional Equipment:
IFR Configured
Emergency floats provisions
Air conditioning / heating
Emergency floats removable
HEELS (Helicopter Emergency Exit Lighting System)
HUMS (Health & Usage Monitoring System) installed
Anti-collision light
Separate 4 Point Seatbelts (15 Seats)
Standard Baggage Compartment (3.4m3)
Two (2) External Emergency landing Lights on Sponsors
ADELT
Rotating and retracting Landing Light
Two (2) Fixed landing/Taxing lights on sponsors
Fifteen (15) Passenger vests
?Retractable energy absorbing Tricycle landing gear
Six(6) cabin & two (2) cockpit push-out emergency exit windows
Two (2) Life rafts - Up to 17 passengers each
Pilot & Copilot Windshield wipers
Storm Light
Two (2) Fire Extinguishers
Cockpit panel Sun-glare Shields
Overhead Cockpit windows sun-shades
ICS panel with plug for one Headset (LH side)
First Aid kit
Baggage Compartment lights (3) and smoke sensor
External Cargo Hook Provisions
Hoist Provisions
TCAS