Boarding Step, Retractable -RH
Maintenance Covers - Exterior
Annunciator - “FUEL X-FEED” ON
Hydraulic Quick Disconnect Relocation
Pulsed Electric Engine Chip Detector System, Eaton 1K7707
Air Comm Flight Deck Heater
Air conditioning System w/ Panel
Digital Cabin Air Temperature Indicator - Cockpit
Annunciator - “Land LT ON"
Annunciator - “Search LT ON"
Gooseneck Map Lights
Landing Light - LH Main Gear
Approach Plate Holder, Lighted - Pilot
Approach Plate Holder, Lighted - Copilot
Console Storage Bin-Small
Sun Tint - Windshield
Overhead Lateral Absorber
Bifilar 5PTrack and Balance Accelerometers Installed in Fuel Cell Extension
Rotor Pedals Lube Kit
Single Pilot IFR
Annunciator - “Pitot Heat” On
Annunciator - “W/S Heat On”
Fuel, Auxiliary 50 Gallon, Universal Fwd/Aft Completion
Fuel, Auxiliary 50 Gallon, Universal Fwd/Aft Provisions
Features of the S-76C++ Aircraft Code 0102:
Dynamic System - Two Turbomeca Arriel 2S2 engines, and a four blade articulated main rotor system with dual controls.
Cockpit – An Integrated Instrument Display System (IIDS), with an easy to upgrade avionics package. There is a Bleed Air Heating Defogging system and dual windshield wipers. The Pilot and Copilot equipped with a five point Restraint system.
Cabin – A large cabin that can be configured for various different missions and a 38 cubic foot baggage compartment
Other – Retractable landing gear, and 281 gallons of usable fuel
Baseline Avionics Package Includes:
Collins Proline II: Dual Collins VHF 22A Comms and VIR 32 Navs, single ADF 462 ADF, TDR 90 Transponder, DME 42 DME with IND
42A Indicator, Collins Rad ALT 1000 Radio Altimeter with Expanded Scale ALI 55A Indicator.
Honeywell EFIS/DAFCS: 4-Tube Honeywell EDZ 756 EFIS with 5" x 6" Indicators Displaying Airspeed, Altitude and Vertical Speed, Dual Litef AHRS, Dual Penny and Giles Air Data Computers, Dual Honeywell Digital SPZ 7600 Automatic Flight Control System,
Electrical: 28 Volt Electrical System with two 200 Amp Starter/Generators, 10 KVA AC Generator, Dual 375 VA Static Inverters,
Avionics and EFIS Master Switches.
Audio: Dual dB Systems Audio control panels with ICS and VOX plus three maintenance jacks, one in the cabin and two in the
baggage compartment. This also includes dual 45 pedestal mounted ICS foot switches, three David Clark Headsets, one six-foot
walk-around cord and two 30-foot walk-around cords, Cabin PA/Chime System, and a Passenger Briefing System - PBS 250.
Backup/Safety Systems: Enhanced Ground Proximity Warning System, Universal 120 CVR, 3" Backup Airspeed Indicator and
Altimeter, ADI-335D Standby Attitude Indicator with Nav1/Nav2 Select, ELT C406-N HM w/ Satellite Frequency, Electric Door
Locks – Cabin, Cabin/Cockpit and Flight Director Decouple Chime/Annunciator
Weather Related Systems: Wx Avoidance Radar - Primus 440, Windshield Washer System, Heated Glass Windshields, and Engine
Inlet Barrier Filter.