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AIRframeS
TTSN: 7500 hrs
Landings: 29,683
ENGINE SPECS
Engine #1 TTSN: 3014.6
Cycles: HRS 5897
Engine #2 TTSN: 2991.4
Cycles: HRS 5972
Main Gearbox TSO 264.16 HRS
Intermediate G/B TSO 0.0 HRS
Tail Rotor G/B TSO 0.0 HRS
Spindle – Red TSN 2038 HRS
Spindle – Yellow TSN 2195 HRS
Spindle – Blue TSN 0.0 HRS
Spindle – Black TSN 0.0 HRS
SYSTEMS
Hinged cockpit and cabin doors, left & right side
Improved Pilot and Copilot door lock pins
Key locks for cockpit, cabin, and baggage compartment doors
Hinged fuel filler caps with key locks
Cockpit-controlled electric locks for cabin doors
Retractable passenger boarding steps, left & right side
Heaed glass windshields
Windshield wiper and washer system
DC Electrical Power System with 2 DC Starter-generators and dual nose mounted batteries
AC electrical power system with AC Generator and dual static inverters
Manual rotor brake system
5P Bifilar vibration absorber
Forward-facing recognition lights in nose windows
Forward-facing under-fuselage recognition lights
Nose-mounted controllable searchlight
Fixed landing lights on left and right main gear struts
Pulselite System
Tel-Tail Lights on vertical stabilizer lower fairing
3-position strobe light system (Whelen)
Top and bottom anti-collision lights
INSTRUMENTS AND STABILITY SYSTEMS
Honeywell SPZ-7000 Dual Digital Automatic Flight Control System
Honeywell EDZ-705 Electronic Flight Instrument System (EFIS)
Standby Self-Contained Attitude Indicator (JET ADI-330C) with battery backup
Dual IDC encoding altimeters
Pilot-selectable alternate static source switches
Dual lighted approach plate holders
Dual overhead master switch panels
Radio master switches
AC/DC Power Management Display (Insco)
5-Function Indicator (Davtron 655-2)
Radio Altimeter (Collins ALT-55B) with digital display on EFIS
Dual C-14A compass system (Honeywell)
Standby vertical-card magnetic compass (Hamilton HI-400)
Dual digital clocks (Davtron M-877)
Roll checklist (MD-100)
Fuel flow indicators
Engine Performance Monitoring System (Howell H-598 EPAMS)
AVIonICS
Honeywell Primus II Communications and Navigation System with Dual Integrated VHF Comm. (RCZ 850) and Dual Radio Management Units (RMU- 850), Dual Integrated Nav. (RNZ-850), and Lightning Sensor (LSZ-850)
Dual Mode-S transponders, Dual DME, ADF
Third VHF communications radio for clearance delivery
Baker Cockpit Audio system with auxiliary volume controls and cabin ICS jack
Passenger Briefer and Ramp Hailer system (NAT)
Cockpit Voice Recorder
Cabin paging and chime system
Airborne Telephone System (AirCell) with handset in Cabin Credenza
Honeywell Primus 870 Weather Radar
Honeywell DataNav III Multi-Function Interface Unit with checklist
Universal UNS-1D Flight Management System with GPS/TAS
TCAS I (Bendix CAS-66A) with dual indicators
Emergency Locator Transmitter (Artex C-406-N HM)
INTERIOR & EQUIPMENT
Executive cabin interior paneling and soundproofing system with personal service units, upholstered rear bolster, overhead emergency lighting, full-length arm rests, and coat hooks
Cockpit-cabin divider bulkhead with sliding windows
Cabin refreshment credenza with two hot liquid flasks, ice drawer, refreshment and condiment storage, and AirCell handset
3-4 Place forward-facing executive divan with fold-down table and armrests
Rear divan seat bottom extension with compartments for trash, Fire Extinguisher, First Aid Kit, life vests and miscellaneous storage
2 Aft-facing single executive seats with recline and swivel
Cabin and Cockpit Air Conditioning system (Keith)
MISSION EQUIPMENT
Emergency Flotation System
Wiring provisions for Auxiliary Fuel Tank (50-Gallon)
LOOSE EQUIPMENT
Main rotor blade tie-downs (set)
Exterior covers and plugs (set)
Pitot-tube covers (2)
Landing gear pins (3)
Door lock keys