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