2010 Sikorsky S76C++

2010 Sikorsky S76C++ Serial Number: 760750 N722JE AIRCRAFT SERVICES GROUP ..' Available Immediately! EFTA01117570 EFTA01117571 or] Contact: George Reenstra Additional information available at www.vourjet.com EFTA01117572 SIKORSKY AIRCRAFT SYSTEM SPECIFICATION Air Ghislaine 2 S-76C++ Aircraft DELUXE EXECUTIVE CONFIGURATION SYS76-00121 Air Ghislaine Rev C Customer: Air Ghislaine 2 Revision: C August 3, 2009 EFTA01117573 Document Revision History REV CHANGED BY REVIEWED BY DESCRIPTION DATE - TSL MP Original Release. Prepared IAW PWA 9/19108 A TSL • Updated configuration based on adds and deletes from Contract Amendment 1 (as listed in CCD) • Reformatted and rearranged layouts and tables in second half of document. • Corrected several items in Standard Equipment section: o Engine oil, MGB oil, EFTS symbol generator, AHRS • Edited database matrix to specifically list all data transfer hardware • Edited description of 86054 • Added clarification to 90037 • Edited Database Matrix to specify ChartView region to be loaded prior to delivery 6/18/09 B C DK AMR TSL • Edited option 90025 to specify that True North sat phone system is to be used • Edited options 90036, 37 to change audio source from Com1 to Com2 • Edited nomenclature on lighting switch panels (p. 19) • Corrected option 90039 by adding fourth audio source (VHF 42) 7/20/09 Deleted 90051, customer will supply carpet 8/3/09 EFTA01117574 SIKORSKY S-76C++ AIRCRAFT STANDARD EQUIPMENT GENERAL SPECIFICATIONS PROPULSION Two Turbomeca Arriel 2S2 Engines Full Authority Digital Engine Control (FADEC) w/ Pilot and Copilot loop lights (two) Displayed on IIDS Performance Displays T5 - Power Turbine Inlet Temperature N1 - Gas Turbine w/ 30 sec. and 2 min. indication TO - Torquemeter N2/NR - Triple Tachometer O/S - Engine Overspeed, BV - Bleed Valve position, DECU readout Displayed on IIDS Engine Display Fuel Flow - digital readout Oil Temperature/Pressure Hydraulic Pressure Engine water wash w/ connections in Baggage Compartment Engine fire detection system with flame detectors and one amplifier per engine Engine fire extinguishing, two shot system (two) Dual input main gearbox - 1605 shp for takeoff Intermediate and tail gearboxes with interconnecting drive shafts Magnetic chip detectors with fuzz burn-off capability (four) EVAOR-2380-Ambe-044M4L—L-23698) Mobil 254 Synthetic Jet Oil (MIL-PRF-23699) Engine inlet barrier filters with condition monitoring display in cockpit MAIN ROTOR SYSTEM Four-blade articulated main rotor system w/ one piece aluminum hub and elastomeric bearings Main rotor blades w/ titanium spars, fiberglass skins, honeycomb cores, high visibility paint, leading edge abrasion protection, and lightning strike protection Manually actuated rotor brake system 3P Bifilar vibration suppression system Overhead lateral absorber provisions Four-blade flezbeam tail rotor w/ lightning strike and leading edge abrasion protection Oil Temperature/Pressure - display on IIDS Sight gauges for oil level in main, tail, and intermediate transmissions Provisions for track and balance w/ 5 aozel., 2 mag. sensors (RADS/AT - Chadwick 8500 - Fastrak) Free wheel units on main transmission EMOA-2880-TuFbe-04-(M16623699) BP Turbo Oil 25 Gearbox Lubricant (DOD-L-85734) FLIGHT INSTRUMENTS Airspeed - refer to Avionics Package Altimeter - refer to Avionics Package IVSI - refer to Avionics Package Pitot-Static system, dual Digital electric clock, Davtron 877 (two) Standby magnetic compass (illuminated) IIDS (Integrated Instrument Display System) - panel mounted Dual Engine Performance Display (two), Engine Display, Remote Data Acquisition Unit, Dual Temperature Probe, IIDS REV Switch/Annun. (two), Scroll Switch in Center Console, Static Port connection Master Warning/Caution Panel, mounted in low profile Glareshield, Pilot and Copilot Outside Air Temperature - mechanical, IIDS (two) CautioniWaming/Advisory - display on IIDS COCKPIT, FLIGHT & GROUND CONTROLS Primary flight - longitudinal, lateral, and directional controls provided at Pilot and Copilot stations. Conventional collective and cyclic stick controls and tail rotor pedal type controls Overhead Throttle Quadrant w/ mixed mode lights (two) Cyclic and collective stick trim controls Stick trim control panel Dual independent flight control servo systems Dual independent 3,000 psi hydraulic systems with quick disconnects for ground servicing Landing gear - fully retractable tricycle type w/ pivoting nose gear, strut remote service line and main wheel brakes, position indicators, gear up warning indicator (two). Cockpit control Pneumatic emergency landing gear extension system w/ externally visible pressure gauge Adjustable rudder pedals - fore/aft, Pilot/Copilot Search light directional control on collective Overhead master switch panels - Pilot (two), Copilot (one) Cabin dome lights master control OEI (one engine hop) training switch and light Provisions for emergency flotation system with nose float bottle access cover ELECTRICAL SYSTEM Battery - single 25.2 volt Marathon SuperPower nickel-cadmium, 44 amp-hour, located aft of Baggage Compartment Battery temperature warning system DC Generators - two 28 VDC, 200 amps each DC Generator Control Unit (GCU) - provides voltage regulation, reverse current and ground fault protection, and over-voltage protection (two) AC Generator — one 10KVA, 115VAC Three Phase AC Generator Control Unit — provides voltage regulation, load protective circuits for overvoltage, undervoltage. and overcurrent. External power supply receptacle - 28 VDC, AN type w/ reverse polarity and over-voltage protection Static Inverter - refer to Avionics Package Power Monitor, on IIDS (volts, amps, freq.) Emergency Power Supply - PS 855A (2.5 AH) Resettable type circuit breakers FUEL SYSTEM Dual fuel tanks w/ gravity fuel fillers, 281 US gallons total capacity Dual independent suction fuel systems w/ cross-feed capability Fuel quantity - displayed on IIDS w/ test and digital total of left and right tanks Capacitance type gauging probes Low level fuel warning system (two) Hinged fuel filler cap with key lock (two) EFTA01117575 SIKORSKY S-76C++ AIRCRAFT STANDARD EQUIPMENT Wiring provisions for auxiliary fuel ICE & RAIN PROTECTION Heated Glass Windshields (two) Heated pitot and static (Iwo) Engine anti-ice (Iwo) Windshield wipers, electric - two speed w/park (pilot and copilot). exposed fasteners LIGHTING Cockpit Instrument panel, pilot and copilot Non-flight instruments Glareshield Console Utility w/coil cord on controls closet (two) Cabin Exit lights, self illuminated (two) No smoking/fasten seat belt signs - see interior Emergency lights (two) w/battery pack Baggage Aft compartment (two) External Position - three Anti-collision, white strobes - three Anti-collision, red beacon - tail Fixed landing (one) - right main gear Controllable landing (Search) - nose Inspection for IGB and TGB sight gauges CABIN COMFORT SYSTEM Cockpit and cabin bleed air heating (25000 BTU) w/windshield defogging system Heater control panel Ram air ventilation system. side mounted inlets (four). cabin exhaust and valves, aft (two) Electric ventilation blower Ceiling gasper - cockpit dual air (two). cabin (refer to interior group) PAINT & CORROSION PROTECTION Refer to Paints and Finishes section Carbide black instrument panel paint finish COCKPIT/CABIN APPOINTMENTS Pilot/Copilot seats - vertically adjusting. 5 point restraintiharness, lumbar support cushion, life vest storage provisions, fabric upholstery 204 cubic foot cabin with 75 PSF floor and fittings for up to twelve (12) seats Cabin hinged entrance door w/door locks and switch, key lock and hold open device (two) Cockpit hinged entrance door w/key lock (two) and class -A* painted interior finish Common key locks - cockpit. cabin, baggage. (six): fuel filler caps (two) Door open warning panel/annunciators - CKPT (two), CABIN (two). BAGG (two) and EXT PWR Fire extinguishers (two) - cockpit. on RH side of closet: cabin, based on final interior First aid kit w/cover, on left side of controls closet Flame blocking on cabin seat cushions Flooring - 75 lb/ft2 Interior placard kit (English standard) Life vest provisions for all passenger locations Manual holder in lower aft cockpit door (two) BAGGAGE/CARGO COMPARTMENTS Separate 38 cubic foot baggage compartment with left/right doors painted inside to match Smoke detector w/cockpit indicator Lockable door w/thumb latches (two) Flooring - 75 lb/It2 Cargo tie down points Aermat floor covering Finish - textured white epoxy structure, interior of doors painted to match aircraft fuselage AVIONICS Nose mounted radome Avionics compartments. nose and tail LOOSE TOOLS & EQUIPMENT Aircraft fly-away kit containing: HEADSET/MICROPHONE EXHAUST COVER, ENGINE. LEFT EXHAUST COVER, ENGINE. RIGHT WALK-AROUND CORD, ICS. 30 FEET WALK-AROUND CORD, ICS. 6 FEET ADAPTER, ENGINE WASH TANK JUMPER ASSY. IIDS MAINTENANCE. P2294 PIN ASSY. MLG PIN ASSY. NLG SHIELD ASSY, ENGINE INLET, R/H SHIELD ASSY, ENGINE INLET, UH SHIELD ASSY, IGB INLET. R/H SHIELD ASSY. IGB INLET. UH SHIELD ASSY. AFT COWL INLET, R/H SHIELD ASSY. AFT COWL INLET, UH COVER ASSY. PITOT TUBE TIE DOWN. MAIN ROTOR BLADE COVER ASSY. ACCEL BLEED VALVE TUBE MOUNT 2 EFTA01117576 SIKORSKY S-76C++ AIRCRAFT ADDITIONAL EQUIPMENT BASELINE AVIONICS PACKAGE COMM 1 COMM 2 NAV 1 GS 1 MB 1 EHSI 1 EADI 1 AHRS 1 NAV 2 GS 2 MB 2 EHSI 2 EADI 2 AHRS 2 ADF TRANSPONDER DME AIR DATA 1 AIR DATA 2 Dual Autopilot/FD Backup Airspeed Backup Altimeter Altitude Alerter Radio Altimeter Collins VHF 22A (16w minimum) with CTL 22 (118.000 - 136.975 MHz, 4 channel preset digital display), bottom mounted VHF antenna Collins VHF 22A (16w minimum) with CTL 22 (118.000 - 136.975 MHz, 4 channel preset digital display), top mounted VHF antenna Collins VIR 32 with CTL 32 (108.00 - 117.95 MHz, 4 channel preset, digital display), DMN4-17/A - all weather blade antenna Included in No. 1 VIR 32 (40 channels), internal nose mounted antenna Included in No. 1 VIR 32 (75 MHz). with Hi-Lo Sense switch, volume control, displayed on EADI 1, bottom fuselage mounted antenna Honeywell EDZ 756 EFIS System, includes: ED 800 - Electronic 5" x 6" HSI with IVSI scale, SG 705 708 - Symbol Generator, DC 811 - Display Control Panel, RI 206 - Heading/Course (dual) Panel, Annunciator/Switch - FD CMD BARS, E.T., SG REV, ADC REV, COMP MON RESET Honeywell ED 800 - Electronic 5" x 6" ADI with airspeed and altimeter scales, Inclinometer, Baro Set Panel, Airspeed Bug Set Panel Litef LCR-100 LCR 925 - Attitude Heading Reference System. System includes: LCR 92S Fiber Optic Gyro with rate gyro output, Sikorsky Dual Compass Control Panel, Honeywell FX 220 - Flux Detector, Annunciators - AHRS/1/2. AHRS TEST Collins VIR 32, 108.00 - 117.95 MHz, Nav Diplexer Included in No. 2 VIR 32 (40 channels), GS Diplexer Included in No. 2 VIR 32 (75 MHz), with Hi-Lo Sense switch, volume control, displayed on EADI 2, marker beacon Diplexer Honeywell EDZ 756 EFIS System, includes: ED 800 - Electronic 5" x 6" HSI with IVSI scale, SG 705 708 - Symbol Generator, DC 811 - Display Control Panel, Hag and Cars control is included in EHSI 1 panel, Annunciator/Switch - FD CMD BARS, E.T., SG REV, ADC REV, COMP MON RESET Honeywell ED 800 - Electronic 5" x 6" ADI with airspeed and altimeter scales, Inclinometer. Baron Set Panel Litef LCR 92S - Attitude Heading Reference System. System includes: LCR 92S Fiber Optic Gyro with rate gyro output, Honeywell FX 220 - Flux Detector, Annunciator/Switch - AHRS TEST Collins ADF 462, 190 - 1799 KHz, and 2179 - 2185 KHz, ANT 462A - Combination Loop/Sense Antenna Collins TDR 90 - ATCRBS Transponder, - Digital Control Head, CAD 62 (-001) - Control Adapter, belly mounted L-band antenna Collins DME 42 (300 w minimum) with IND 42A, belly mounted L-band antenna. Tracks three stations simultaneously for instantaneous display selection, providing: distance and ground speed or time-to-go or station identifier (2,3, or 4 letters). DME Hold feature is incorporated in both the Nav 1 and Nav 2 controls heads, belly mounted L-band antenna Penny and Giles - Air Data Computer, w/encoding output to transponder(s) Penny and Giles - Air Data Computer, w/encoding output to transponder(s) SPZ 7600 - Dual Digital Automatic Flight Control System, includes:FZ 706 - Digital Flight Guidance Computer, two MS 700 - Mode Selector, PC 700 - Autopilot Controller, AFCS Indicator Panel, Linear Pitch Actuator (two), Linear Roll Actuator (two), Linear Yaw Servo (two), Pitch Trim Actuator, Roll Trim Actuator, Collective Trim Actuator, Pedal Damper/Trim Actuator (hydraulic). Annunciator Lights: AP 1/AP 2/CLTV/DCPL, TRIM FAIL, FD Decouple with Chime Airspeed Indicator - 3" Sensitive Altimeter (in & Mb) - 3" Honeywell AL 300 - Air Data (Altitude Preselect) Display, Annunciator - single ALT ALERT Collins ALT 55B - Receiver/Transmitter, ALI 55 - 3 inch Indicator (0 - 2500 foot), bottom fuselage mounted Antennas (two) 3 EFTA01117577 SIKORSKY S-76C++ AIRCRAFT ADDITIONAL EQUIPMENT Weather Radar Static Inverter Standby ADI Stby Power Supply ELT CVR Dual Audio ICS ICS VOX ICS Foot Switch Headsets ICS Jacks ICS Cords Passenger Briefer Cabin Paging Collective Switches Cyclic Switches Avionics Master EFIS Master Master By-Pass Cooling Fans TAWS Honeywell Primus 440, WU 440 - Transmitter/Receiver/Antenna Unit with 12 inch Antenna Radiator, Honeywell AMLCD Radar-Only Display (upgradable to display additional data) Two Marathon Model PC-251-123K 115 VAC, 250 VA lightweight Inverters (w/ integral 26 VAC transformers), Annunciators (in IIDS) - NO 1 INV FAIL, NO 2 INV FAIL BFGoodrich ADI 335D - 3-inch Stand-by Attitude Indicator providing Nay (VOR/LOC/Glideslope), DME, and FMS data. Unit is installed on the center instrument panel as a backup to the EFIS system. Features include: eight character LED display; CDINOR/Localizer and Glideslope crosspointers with appropriate validity flags; navigation modes of - en route VOR with manual OBS; OBS auto-centering and TO/FROM ambiguity indicator; precision approach ILS and back course; DME distance; groundspeed, and time- to-station; manual fast erection caging; and FMS display. Gyro is automatically tied to a dedicated power supply (30 minute minimum) during a total aircraft power loss. Upon depletion of the dedicated power supply, the ADI 335D provides approximately nine minutes of additional useful attitude information during its spin down. There is also a NAV 1/NAV 2 Annunciator/Switch that adds Nav 2 display capability into the ADI 335D indicator mounted next to the ADI 335D indicator. J.E.T. PS 855A - 2.5 AH lead acid standby power supply with Annunciator/Switch - GOOD/BATTERY TEST, EMER PWR/OFF/ARM ARTEX ELT 406-NHM with remote switch and "on" indicator, beacon transmits on 121.5, 243.0 and 406.025 MHz, two year Alkaline Battery, tail boom mounted VHF antenna Universal Navigation CVR 120: CVR Recorder with ultrasonic Underwater Locator Beacon; Control Panel with Headphone Jack, Signal Level LED Display, Pass and Fail LCD Indicators and an Erase Button. Two dB Systems 380 - Audio Selector/Amplifier/ICS Panels ICS with volume control included in dB Systems 380 Audio Panels for Cockpit, plus Cabin and Baggage Compartment maintenance jacks Cockpit ICS VOX - Voice activated keying, included in dB Systems 380 Audio Panels Sikorsky 45° pedestal mounted switch (two), permits foot keying of ICS or aircraft radios with selection on dB Systems 380 audio panels David Clark H10-26 (three) - high impedance headsets Cockpit - TJT-120 type (two), Cabin - MS connector type (one), Baggage Compartment - MS connector type (two) Cabin Maintenance - 6'; Baggage Maintenance - 30' (two); all with MS connector and push-to-talk switch Heads Up Technologies, PBS 250 Passenger Briefer w/ Takeoff, Turbulence, and Landing Briefings Page/Chime Amplifier, dB Systems 251w/ inteface to pilot and copilot audio Go Around, Trim Release, Servos 1/2 Off, Collective/Yaw Beep, Search Light Control, Engine Trim, OEI/MCP (30 sec-2 min) Push-to-talk, Trim Release, Cyclic Beep, Decouple, Floats (opt.), Cargo Hook (opt.) Sikorsky single Radio Master rocker switch in Overhead Switch Panel Sikorsky EFIS Master rocker switches in Overhead Switch Panel Sikorsky Radio Master By-Pass, EFIS By-Pass (Pilot and Copilot) CRT fans (two), Annunciator (in IIDS) - CRT FAN FAIL 1/2 Honeywell Mk XXII Enhanced Ground Proximity Warning System (EGPWS). Features include: terrain display on EHSIs; Six Modes: Mode 1 Excessive Rate of Descent, Mode 2 Excessive Terrain Closure Rate, Mode 3 Inadvertent Descent After Takeoff, Mode 4 Unsafe Terrain Clearance, Mode 5 Below Glideslope, Mode 6 Altitude Call-outs. 4 EFTA01117578 SIKORSKY 5-76C++ AIRCRAFT ADDITIONAL EQUIPMENT ADDITIONAL AVIONICS ITEMS 07025 Delete PBS 250 Passenger Briefing System, From Baseline 11002 Radio Tuning Units - RTU 4200 Dual Collins RTU 4200 radio tuning units. for use with VHF-22A Comms, VIR-32 Nays, ADF-462 and TDR 94D Transponders. System includes: two RTU 4200 - Radio Tuning Units. Features include: liquid crystal display, single control of all basic radios. Dzus mounted at the forward area of the center console. 11028 Dual - Mode S Transponders w/Diversity TDR 94D Dual Collins TDR 94D Mode S Transponders Wth aircraft address memory, exchange for standard single transponder system. The TDR-94D transponders are controlled through the RTU 4200s in the instrument panel. Includes: TDR 94 (two each) - Mode S Transponder, and three additional L-band antenna. 11037 DME, 2nd - DME 42 Second Collins DME 42 System. System includes: DME 42 - Receiver/Transmitter, IND 42A - Digital DME Indicator. L-band Antenna - bottom fuselage mounted. Features include: 252 UHF channels; 300 w minimum power; range - 0.0 - 999 nm, speed - 0 - 999 kts, time-to-go - 0 - 199 minutes, digital display with auto dimming, indicator provides simultaneous readout of distance and speed or time-to-go or station identifier (2, 3 or 4 letters); dual diagnostic code presented on indicator; built-in on/off power switch; simultaneous tracking of three (two stations with FMS) stations for instantaneous display selection. 30012 AUDIO JACKS - EMERGENCY (STD/BOSE) Emergency ICS (COMM) Panel is installed in pilots overhead that provides a direct headset connection to the No. 2 COMM radio in the event of an audio controller failure. Panel includes an -EMER/NORM" switch and both normal jack and Bose headset jack. 30020 Audio Jacks, Cockpit — Bose Installation includes: two each aircraft mounted Bose audio jacks, complete aircraft integration. Jacks are for customer furnished Bose headset operation and are in addition to standard jacks. 5 EFTA01117579 SIKORSKY 5-76C++ AIRCRAFT ADDITIONAL EQUIPMENT 30061—Cabin-ICS DELETED (Custom cabin ICS option is listed under Option 90036) 30093—Cabin-Call-System DELETED (Call function is part of ICS Option 90036) 31021 Speakers - Door, Two One speaker installed in each hinged cabin door. To be used with Cabin Paging System 32001 Cellular Phone Base and Charger (12 VDC outlet) Flush mounted in cockpit ceiling. Installation includes: flush mounting of outlet: 12 VDC voltage converter; circuit breaker: mounting hardware; aircraft wiring: and pouch to hold phone. Note: Cellular phones are not permitted to be used while airborne 32824—SatelliteCommunieations-System ;AirCell-ST-31-00 DELETED (Replaced by option 90025) 34053 NAV/LNAV Switch for ADI 335D NAV/LNAV switching adds long range navigation display capability into JET ADI 335D indicator. Includes annunciators/switch - NAV/LNAV. Features include: FMS display modes including - en route and approach, course deviation, distance to waypoint, desired track, selected course, bearing to waypoint. TO/FROM indication and waypoint passage alert. 34081 Vertical Card Standby Compass Vertical Card Magnetic Compass consisting of a 2" vertical rotating dial that is similar to an HSI type presentation. Features include: self contained and requires no external power except for internal lighting; 2" diameter with extra large numerals every 30°, with 10° bars and 5° dots; miniature airplane on the glass and heading is read at the 12 o'clock position for natural flight indication; compass card rotates and presents all quadrants in their true relation to line of flight; unit is a dry compass and utilizes eddy current damping and as such has no overshoot: 5 vdc internal lighting. Exchange for standard float/liquid type standby compass indicator. fired-to-the Collective 35055 FMS, Universal UNS-1Fw (WAAS FMS) with LPV Monitor ADDED Universal Avionics UNS 1Fw - Flight Management System. System Includes: Super FPCDU — Flat Panel Control Display Unit (6.375"h x 5.75"w x 3.617"d): Navigation Computer Unit (NCU) with internal WAAS GPS; LPV Monitor with internal WAAS GPS receiver; Configuration Module; Portable SSDTU - Solid State Data Transfer Unit; omnidirectional flat micro-strip antenna with internal pre-amp; Mode/Warning Annunciators - GPS INTEG/FMS HDG/MSG, LPV/NO LPV, LNAV/VNAV, and LOS CHG on the instrument panel; data loader jack installed on right side of cockpit console. Features Include: 5" diagonal active matrix liquid crystal color display (uses 2 character sizes for ease of data recognition) which is pilot dimmable; full alpha-numeric keyboard; holding pattern selection; ten line entry keys; multi-sensor input capable, plus uses combinations of DME/DME/DME. VOR/DME: pilot selectable Nav Auto-tune; 12 channel internal (in NCU) GPS receiver - continuously tracks up to eight satellites; map display presented on pilot and copilot EHSI's: "Direct To" key; trip planning, airport services and fuel management pages; fuel flow input from aircraft system; flight calculator; full three dimensional positioning - latitude/longitude and altitude; advisory VNAV; 3-D Approach Mode; stores — 200 flight plans of up to 98 waypoints 6 EFTA01117580 SIKORSKY S-76C++ AIRCRAFT ADDITIONAL EQUIPMENT each (3000 total), 2000 company protected routes, 100 arrivals/departures, 100 stored approaches; 100 airports, 100 runways, 100 alignment points, 25 radar waypoints, up to 200 user-created waypoints; Airwatchm restricted airspace warning system; two pages of direct to nearest airports; displays - ground speed, range, distance, bearing, desired track, drift angle, track angle, cross-track distance, vertical deviation, estimated time enroute, true airspeed, density altitude, pressure altitude and winds aloft when interfaced with standard Penny & Giles air data computer; 32 MB storage for Jeppesen worldwide or regional Data Base with updates from portable Data Transfer Unit (included) - provides plain language airport and Nav names, off-line flight planning capability (optional), clearance language format, information on all VHF Navaids, all high and low altitude intersections, all on and off-airway NDB's, all outer markers, runway thresholds, high-altitude jet routes and low altitude airways by name, SID and STAR waypoints, approach patterns, and intersections. FAA approved for GPS LPV (Localizer Performance with Vertical Guidance) approaches within the United States. 36044 LIGHTNING STRIKE SENSOR - LSZ 860 Honeywell LSZ 860 Lightning Strike Sensor System provides supplementary weather avoidance information. System includes: LP 860 - Receiver/Processor and AT 850 - Teardrop Antenna. The system is controlled through the Honeywell Multi-Function Radar Display on the instrument panel. Features include: 200 nautical mile radius detection area; three Lightning Rate Occurrence Symbols - each symbol (rate one, two and three) represents the center of an 18-mile diameter area of lightning activity for the last two minutes; Lightning Alert - places a magenta 'rate one' symbol near the outer range mark of the display, at the proper bearing, for each lightning flash; computer can track up to fifty (50) individual lightning rate symbols; Geographic Stabilization - heading and velocity inputted to keep the rate symbol over the same geographic location; 360° viewing area when radar is in standby. Control functions: OFF - removes all power from system; STBY - data is not displayed, however the Receiver/Processor is active and lightning strikes are being counted and accumulated; LX - normal working mode, lightning strikes are collected, processed and displayed; CLR/TST - erases all memory of past strikes and symbols, after 3 seconds the equipment enters the test mode. 36065 Wx Avoidance Radar - Primus 880, exchange for Primus 440 Honeywell Primus 880, Digital 5-color, fully stabilized High Power Doppler Turbulence Detection Radar System. System includes: WU 880 -Transmitter/Receiver/Antenna Unit with 12 inch Antenna Radiator and interface cables to Honeywell Multi-Function Radar Display. Features include: 10.0 KW nominal power output; X-band (9375 ± 25 MHz); 12 inch flat plate antenna; antenna horizontal scan angle - 120 degrees or 60 degrees (pilot selectable); stabilization - ± 30 degrees combined pitch, roll and tilt; antenna tilt - ± 15 degrees with digital on screen annunciation; range display selection - 2.5, 5, 10, 25, 50, 100, 200 and 300 nautical miles; Target Alert; REACT - Rain Echo Attenuation Compensation Technique alerts the crew where storms may be hidden by intervening rainfall attenuation; Turbulence detection is provided using advanced Doppler pulse pair processing techniques to detect turbulence within any storm cell - regardless of rainfall rates; self test; red "dead zone" display shows where targets will not be displayed; Mode Selections: OFF - removes system power; SBY - system energized, but no transmitter output, no display and antenna scan is stopped; WX - turns system on and selects basic weather; GMAP - Ground Map selects high sensitivity terrain mapping; FP - Flight Plan mode for stand alone navigational display, lightning strike data, etc.; TST - self test with test pattern; RCT - activates the REACT function; BRT - single turn display brightness control that adjusts the brightness of the display; GCR - selects ground clutter reduction for ranges up to 50 miles; GAIN (pulled) - rotary gain control for both weather and ground map modes, normal in position provides a calibrated gain; TGT - advise crew when a red or magenta target appears beyond the selected range for the 5 to 200 nm ranges and 7.5 degrees on each side of the 7 EFTA01117581 SIKORSKY S-76C++ AIRCRAFT ADDITIONAL EQUIPMENT aircraft heading; TRB - turbulence detection of moderate, severe and extreme areas within reflective rainfall are displayed in soft white up to 50 nm; TILT - antenna tilt adjustment; PULL AUTO - enables the Auto Tilt mode for fine tuning the tilt by ± 2 degrees; Stabilization - is disabled by pressing the TGT switch four times within three seconds; RANGE 4 - stews radar range selection up; RANGE 4 - slews radar range selection down; AZ - selects and deselects the electronic azimuth lines for display on screen; SCT - selects either full azimuth scan (120°) or sector azimuth scan (60°). 36104 Multifunction / Moving Map Display, Garmin GMX 200 The Garmin GMX 200 is a fully integrated Multi- Function Display. The system consists of a large color AMLCD display that expands a full 6.5" diagonally, 640 x 480 pixels, 65,536 different color combinations, enhanced backlighting that dramatically improves color and contrast, resulting in chart depictions and images that are brighter and more vivid in all lighting conditions. At a glance, see your aircraft's position relative to terrain, obstructions, weather, airways, navaids, restricted airspace and more, select between several charting options and easily add or remove details with the simple press of a soft key, rotary knob allows for quicker map scale changes and entry of data, front loading SD card-slot allows for expanded memory and makes loading updated charts uncomplicated. Unit is faster with 650 MHz processing speed and 256 MB memory for higher map detail. A custom map function is available which allows the user to create a display for almost any configuration required, offering extensive overlay capabilities. The GMX 200 includes high resolution terrain and hydrography data for the entire world which is prebaded for an unmatched presentation even at the lower zoom scales. The Garmin Base Map with cities, roads, rivers, and lakes has been added to further improve situational awareness. An aviation database featuring Jeppesen® NavDate" is used to draw airports, airways, navaids, airspace, and more. Map scales range from one-fourth of a mile to 2500 miles. A unique split screen function allows you to simultaneously view two charting options along with the vertical profile for the elevation of the terrain along the route of flight. The GMX 200 utilizes position information from the aircraft's FMS system for moving map features. The GMX 200 also provides for the display of charts. 36105 JeppView Option for the Garmin GMX 200 JeppView functions are based on the popular Jeppesen Electronic Airway Manual Service. Familiar Jeppesen instrument approach charts and airport-surface diagrams are viewed with the aircraft position overlaid on the GMX 200 high-resolution color display. Additionally, JeppView 8 EFTA01117582 SIKORSKY 5-76C++ AIRCRAFT ADDITIONAL EQUIPMENT displays Standard Instrument Departure and Arrival charts (SIDs and STARs). Charts are available through Jeppesen's JeppView for GMX 200 data subscription service. On departure, the GMX 200 with Chart View displays the airport surface map, including all runways and taxiways. After takeoff, the GMX 200 automatically transitions to the en-route chart, which depicts airways, airspace, terrain. navaids, rivers, lakes and highways. Within the terminal area of the destination airport, the GMX 200 transitions to the selected instrument approach plate -- complete with procedure turns and holding patterns. Once the aircraft has approached the runway and ground speed has slowed to 50 knots, the aircraft symbol is displayed on a moving map of the airport surface. 36120 Honeywell Multi Function Radar Display (MFRD) displays Radar, Flight Plan, & Checklists Exchange for: WI-880 Weather Radar Indicator (part of Option Code 36065) and LU-860 Lightning Sensor Control Panel (part of Option Code 36044) System Includes: Honeywell Multi-Function Radar Display (MFRD). Features include: The Honeywell MFRD is a multi-function display that replaces the standard radar display and has the capability to interface with various other sensor systems. The MFRD is used as a display and control for the Primus 880 Weather Radar, the LSZ-860 Lightning Strike Sensor. It will can display CAS-66A TCAS information. Flight plan information from the aircraft FMS System (UNS-1 F) can also be displayed. 37011 TCAS I System - CAS 66A Bendix-King CAS 66A - TCAS I System. System includes: TPU 66A - Processor Unit: 2 each ANT 67A - Directional Antenna, one top fuselage mounted and one bottom fuselage mounted; 2 each, antenna-to-fuselage adapter plates; installation kits: 2 each, matched sets of four custom coaxial cables for connection to the directional antennas; small access doors on left and right sides of race car. Features include: active system - which means the processor unit interrogates surrounding aircraft transponders without the need of ground based radar; displays up to 30 intruder aircraft (strapped for 12 targets with 3 ATI display and 20 targets when on a radar display); Traffic callouts: Non-Threat Traffic (relative altitude greater than ± 1200 feet or distance beyond 6 nm), Proximity Intruder Traffic u (traffic within ± 1200 feet and 5 nm), Traffic Advisory I (will display a TA when time to Closest Point of Approach is 15 to 30 seconds); crew selectable ranges of 3, 5, 10, 15. 20 and 40 nm; intruders altitudes may be displayed as absolute or relative to the aircraft; crew-selectable relative altitude; three selectable altitude display modes - normal (± 2700 ft), above (- 2700 ft to + 8700 ft), below (+ 2700 ft to - 8700 ft): fault isolation and diagnostics can be performed via RS 232 port; top and bottom directional antennas prevent blind spots caused by airframe blanking; antenna calibration performed by the Processor Unit. 37017 TCAS Control Panel - CP 66B Bendix-King CP 66B - TCAS Control Panel. Panel provides control functions of OFF-STBY- ON; flight level of ABOVE-NORM- BELOW, FAIL annunciator and "push-to-test" and -push-for-flight level". FA It TO 151 EIOCI %A< IN; 37025 TCAS I TANS! Display, Dual IVA 81D 9 EFTA01117583 SIKORSKY S-76C++ AIRCRAFT ADDITIONAL EQUIPMENT Two Honeywell IVA-81D - independent 3-ATI Traffic Advisory Indicator. Features include: color flat-panel display: UP/DN - range up/down select switches: BRT - manual display brightness control: photo cell dimming. One indicator installed on each pilot's panel. Maximum of 12 targets are displayed at any one time. PAINTS & FINISHES See Exterior Paint Rendering and Paint Scheme Drawing for Details on Paints & Finishes 50002 VIP Interior Paint Prep & Finish 50012 VIP Exterior Paint Preparation & Finish INTERIORS See Interior Specification for Details on Interior arrangement and configuration 63000 Deluxe VIP Interior Group. 63O13—Aft-Facing-Benoh--3-to-4-Piace DELETED 63038 Fwd Facing Divan, Three/Four Passenger w/ Fold Down Armrests ADDED 63071 Bulkhead Storage Compartment - Crew (Aft Facing Bench) 63085 -Cabin Coat Hooks,-Two-DELETED 63098 Acoustic Noise Reduction - Bay Blanket Kit, Lightweight 70016 Sheepskin Seating - Crew Seats 70052 Seat Belt Extension 72063 Flight Manual Storage, LH Controls Closet 76017 Cabin Door Vents, Remove 77034 Single Action Door Release 1O EFTA01117584 SIKORSKY 5-76C++ AIRCRAFT ADDITIONAL EQUIPMENT AIRCRAFT ITEMS 80001 Boarding Step, Retractable - LH Electrically operated (extend & retract) boarding step is installed on the left side of the aircraft to facilitate passenger boarding. The step reduces the vertical distance from the ramp to the cabin of the aircraft into smaller steps. The crew can retract the step or they can place the switch in the Auto position, so that when the aircraft lifts off the step(s) retract and when it touches down the step(s) extend. Installation includes: Boarding Step three position (RET-AUTO-TEST) switch, installed in the Cabin Door Lock/Boarding Step lighted panel located in the console; retractable boarding step with built-in retraction motor and accessories installed on lett side of aircraft below cabin door; step position indicator lights show when the step is either fully retracted (RET - green) or fully extended (XTND - amber) - the indicator is off during transition; micro switches in the step mechanism sense the extended and retracted positions; green BD STEP annunciator in the pilot and copilot Performance Displays of the IIDS to alert crew when the step is not fully retracted. 80002 Boarding Step, Retractable - RH Electrically operated (extend & retract) boarding step is installed on the right side of the aircraft to facilitate passenger boarding. The step reduces the vertical distance from the ramp to the cabin of the aircraft into smaller steps. The crew can retract the step or they can place the switch in the Auto position, so that when the aircraft lifts off the step(s) retract and when it touches down the step(s) extend. Installation includes: Boarding Step three position (RET-AUTO-TEST) switch, installed in the Cabin Door Lock/Boarding Step lighted panel located in the console; retractable boarding step with built-in retraction motor and accessories installed on right side of aircraft below cabin door; step position indicator lights show when the step is either fully retracted (RET - green) or fully extended (XTND - amber) - the indicator is off during transition; micro switches in the step mechanism sense the extended and retracted positions; green BD STEP annunciator in the pilot and copilot Performance Displays of the IIDS to alert crew when the step is not fully retracted. 80082 Engine Inlet Covers Storage (S-76C++) ABS type material holders attached to the inside of left and right baggage compartment doors that provide storage of the engine inlet covers. 80086 Maintenance Covers — Exterior Set of six red vinyl maintenance covers. The covers are padded and provide protection for the following areas during aircraft maintenance or storage: top of lett and right main gear doors; left and right fuselage covers for area directly above main gear doors; and left and right horizontal stabilizer (slip-on type). 80090-11orticallaylon-Access-Panels,-CSN-76-207 DELETED (This item is now part of baseline aircraft) 11 EFTA01117585 SIKORSKY S•76C++ AIRCRAFT ADDITIONAL EQUIPMENT 80092 Enhanced Door Pins Cockpit ADDED Replaces the existing uppe door pins on the pilot and copilot doors with an enhanced pin that provides a better grip. 83001 Annunciator - "FUEL X-FEED" ON FUEL X-FEED annunciator installed on center instrument panel. Annunciator is sunlight readable (blue legend color) and advises the crew that either cross-feed selector handle is locked in the cross-feed position. 83051 Hydraulic Quick Disconnect Relocation Relocate Hydraulic Quick Disconnects to baggage compartment from side of race car. Installation includes: mounting of the four fittings into the baggage compartment ceiling on each side of the aircraft; additional plumbing, clamps; and other installation hardware. 83055—Remove-LH-Accessory-Drive—CSN-76-205 DELETED (This item is now part of baseline aircraft) 83065 Pulsed Electric Engine Chip Detector System, Eaton 11(7707 This system allows the pilot two attempts to electrically discharge accumulated fuzz on the engine chip detectors. System includes: Chip Detector test switch, Chip Pulse switch, and a Zapper box. 84051 C4 Environmental System Cabin Cockpit Climate Control, C4 System, exchange for standard bleed air heating system, provides one button set-and-forget control of the cabin temperature. System includes: Master Control Panel - Sikorsky switch panel with temperature indicator, located in copilots upper overhead switch panel: Cockpit Heat Control Panel - Sikorsky switch panel with copilot two speed fan switch and both cockpit heat and windshield defroster temperature control rheostats installed in overhead above inboard copilots seat; Fan Switch Panel - Sikorsky switch panel with pilots two speed fan switch installed in overhead above inboard pilots seat: System Controller (computer): Primary and Secondary Distribution Ducts; Bleed-Air Heat Outlets - Cockpit Footwarmer (pilot and copilot bleed-air floods located between rudder pedals), Cabin Waterfall (left and right overhead waterfall panels) and Cabin Floor Floods (two forward cabin, aft facing warm air flood outlets); Variable Speed Fans (three) - pilot (two overhead Wemacs. defroster), copilot (two overhead Wemacs, defroster), cabin (eight overhead Wemacs); Cabin Temperature Sensor - one; Rosemount A9506-01-A - Outside Air Temperature Probe: Duct Temperature Sensor (two) - one in overhead duct and one in floor duct; Duct Over-temperature Sensors - seven; Bleed Air Injectors - cockpit (four), cabin (one); Outside Air Inlet - one inlet located near no 1 engine, which routes air thru air conditioner evaporator unit: NACA Exhaust Vent - two each, motor controlled vents located just forward of aft cabin bulkhead. Master Control Panel includes the following: Indicators - LCD type for cabin/set temperature (°F); LED's - AUTO (green, automatic mode is operating), AUTO FAIL (amber, controller failure or loss of power), HEAT (green, any time floor heat is being supplied), NC (blue. anytime the air conditioning compressor is operating), BV CLOSED (amber. main bleed valves are closed and bleed air is required by the automatic system), OVER TEMP (amber, over-temperature condition detected anywhere in the I2 EFTA01117586 SIKORSKY S-76C++ AIRCRAFT ADDITIONAL EQUIPMENT system); Switches - VENT (HI-AUTO-LO), BLEED AIR (ON-AUTO-OFF), CABIN HEAT (HI- AUTO-LO), A/C (ON-AUTO), AUTO TEMP (UP-TEMP-DN & ON-OFF). Features include: One button set-and-forget cabin temperature control; independent cockpit temperature controls; auto and manual modes; 50,000+ BTU engine bleed-air heating system; 21,000+ BTU vapor cycle air conditioning system; cabin temperature control range from 65°F to 85°F; temperature control from cabin available (optional). the system can be operated on the ground using a 28VDC power cart to precool the aircraft. Exchange for vent blower and controls. 85001 Annunciator - "Land LT ON" LAND LT ON annunciator (green) is activated in the pilot and copilot Performance Displays of the IIDS, in addition to wiring from the Landing Light circuit. Annunciator advises (green color legend) crew when the Landing Light switch is in the ON position. 85002 Annunciator - "Search LT ON" SEARCH LT ON annunciator (green) is activated in the pilot and copilot Performance Displays of the IIDS. in addition to wiring from the Search Light circuit. Annunciator advises (green color legend) crew when the Search Light switch is in the ON position. 85012 Gooseneck Map Lights Two Grimes flexible arm hooded floodlights with rheostat control, mounted on forward frames of pilot and copilot door frames. Features include: long flexible arm (approximately 16", 41 cm length) for direct placement of steady light, rotatable lamp hood for directional control of beam, rheostat control with positive off position, easily relampable, lusterless dull black wrinkle paint finish. 85036—Anti-Collision -Light,-Red—Bottom DELETED 85051—Landing -Light—LM-Main-Gear DELETED 85061—Reoognition-Lights—Forward-Faoing DELETED 85063—Logo-Lights DELETED 85071—Pulselight-System DELETED 85072—Putse-Landing-Lights DELETED 85073—Pulse-Recognition -Lights DELETED (All incandescent external lighting replaced by LED. Anti-collision and position lights are listed below; landing, recognition and logo lights are options 90029, 90030, and 90050) 85037 Anti-Collision LED Light, Red, Top ADDED Whelen vertical tail mounted red LED anti-collision light system. Replaces standard Grimes anti-collision light. 85039 Anti-Collision LED Light, Red, Bottom ADDED A red LED anti-collision light will be installed on the belly of the aircraft. 85040 LED Position Lights ADDED The baseline combination position/strobe lights will be replaced with Whelen combination lights in which the position lights are LEDs. 86001 Approach Plate Holder, Lighted - Pilot Red/white lighted Plexiglas approach plate/chart holder mounted on a fold- away bracket on the right side of instrument panel. Holder is mounted with the pivot side down so as to better retain the maps and charts. 86002 Approach Plate Holder, Lighted - Copilot Red/white lighted Plexiglas approach plate/chart holder mounted on a fold- away bracket on left side of instrument panel. Holder is mounted with the pivot side down so as to better retain the maps and charts. I3 EFTA01117587 SIKORSKY 5-76C++ AIRCRAFT ADDITIONAL EQUIPMENT 86016 Pencil Holder Dzus width pencil holder with narrow slot for storage of pencils, pens, and other narrow items, mounted in center console with Dzus fasteners. 86017 Console Storage Bin - Small Dzus width storage bin, for storage of miscellaneous light weight items, mounted in center console with Dzus fasteners. 86026 Sun Tint - Windshield Deep tint 3M Tµ window film installed at the top edge of the pilot and copilot glass windshields inside the aircraft. 86050 Overhead Lateral Absorber Overhead Lateral Absorber is mounted overhead in the cabin of the aircraft, which is below the main gearbox. This system absorbs lateral vibrations, making for a smoother ride. 86052 Bifilar 5P The 5P Bifilar vibration absorber consists of a four armed, cross-shaped aluminum forging. Each arm has an independent weight assembly attached through two pendulum -type pivot points. The weights are secured to the pivot pints by bolts which clamp spacers against two tapered washers. The tapered washers center the weights against the contact surfaces during rotor operation and give vertical support under static conditions. It is secured above the 3-P Bifilar on the rotor mast and is used to suppress 4/Rev in level flight and during translation. The Bifilar vibration absorber uses the concept of in-plane pendular dynamics weights which generates internal forces in opposition to the blade forces. Use of the rotating system centrifugal force field as the restoring force on the pendulum provides constant tuning throughout the rotor operating range. The 4P airframe vertical and roll vibrations are, in large part caused by the rotor 5P in-plane vibratory loads in the rotating system. The 5P Bifilar is turned to counteract and cancel the vibratory forces at their source, the main rotor, before they can reach the airframe. The 5P Bifilar also reduces the 4P airframe vibrations generated during translational lift. 86054 Track and Balance Accelerometers Installed in Fuel Cell Extension Installs cabin RH vertical and cabin LH vertical track and balance accelerometers in the fuel cell extension for measurements by the operator. Baseline aircraft has 5 accelerometers: Pilot heel vertical, pilot seat vertical, pilot seat lateral, copilot seat vertical, and tailcone 'radial'. 86060 Rotor Pedals Lube Kit Adds grease fittings to the pilot and copilot Tail Rotor Pedals providing ease of maintenance. 87001 Annunciator - "Pitot Heat" On A PITOT HEAT on annunciator (green color legend) is activated in the pilot and copilot Performance Displays of the IIDS that is tied to the No. 1 and No. 2 pitot heat current sensors. The light will illuminate when both the No. 1 and No. 2 Pitot Heat switches in the pilot's overhead switch panel are On, and electrical current is flowing to the respective pitot tubes. PLT PITOT and CPLT HEAT fail lights (amber) are standard in the Engine Display of the IIDS. 87002 Annunciator — "W/S Heat On" AWLS HEAT ON annunciator (green color legend) is activated in the pilot and copilot Performance Displays of the IIDS that is tied to the pilot and copilot windshield heat current sensors. The light will illuminate when the Pilot and/or Copilot Windshield Heat switches in the pilot's overhead 14 EFTA01117588 SIKORSKY S-76C++ AIRCRAFT ADDITIONAL EQUIPMENT switch panel are On, and electrical current is flowing to the respective windshields. MS HEAT HOT light (amber) is in the Engine Display of the IIDS. 88051 Floats Completion Sikorsky Emergency Floats system for air operations over and around water. System includes: urethane coated nylon bags (four), helium (or nitrogen) filled 300 psi float bottles (four), float bottle covers (two in cockpit) with Velcro attached access doors which contain a clear plastic sight gage window, indicator/test switch panel, OFF/ARMED switch (overhead switch panel), FLOATS firing switch on cyclic (two). annunciator - FLOATS ARMED; aircraft plumbing, and wiring. Features include: floatation bags are packed inside left and right compartments within the nose of the aircraft and on the main landing gear doors - protected from external damage; bags do not affect flight performance or cruising speed; redundant inflation and compartmentation - two spheres supply the front bags: the other two supply the rear bags; electrical power is supplied by both the DC ESS BUS and NO 2 DC PRI BUS. Upon inflation each bag reaches an operating pressure of 0.75 to 3.5 psi. 88061 Single Pilot IFR Weight and Balance for a single pilot is addressed in the design with the placement of remote boxes to eliminate or minimize ballast requirements. Cockpit instruments are laid out to ensure pilot can reach copilot's instrument adjustment knobs. 15 EFTA01117589 SIKORSKY S-76C++ AIRCRAFT ADDITIONAL EQUIPMENT CUSTOMER SPECIFIC ITEMS 90001 Cabin reading light master ON/OFF switch in the cockpit 90002 Clear Coat Exterior Paint (over metallic) 90003 Replace exterior fairing/access panel hardware with stainless steel hardware 90007 GMX-200 display to be installed on the right and the MFRD on the left 90010 Audio input jack in cockpit for iPod type device. Entertainment audio to be heard in both cockpit Bose and David Clark headsets only. No other controls, volume controlled via iPod device 90019 Do not install the 63000 magazine storage in lower cabin doors 90020 Custom upholstery/cushion fabrication requiring customer approval via pre-production prototype. Rev. A The following options are ADDED: Here to 90022 Customize ceiling reading lights. Relocate one reading light from each group to the end of outboard area of the ceiling, to be centered on outboard passenger seats. list + 90024 Relocate the reading light switches to the overhead area, adjacent to the reading lights. Relocate the dome light switches on the same panel as the relocated outboard lights, in the outboard position. Rev. B 90025 Truenorth Satellite phone system with WiFi Server to support Blackberry email. Includes cabin handset and cockpit dialer. This system provides satellite phone capability through the Iridium network, as well as connectivity for Blackberry