N139WH - 2005 BELL AGUSTA AEROSPACE AB139

2005

BELL AGUSTA AEROSPACE

AB139

31031

N139WH

Used

IFR

Miscellaneous: Covers: exhaust pipes, turbine air inlets and pitot tubes Manuals: aircraft log, engines operations, flight and maintenance and overhaul, illustrated parts catalogue Tie down – assemblies: main rotor and tail rotor blades. aircraft under warranty until 9/08

166.4

Aluminum alloy Fuselage Polycarbonate Windshields Overhead cockpit windows Lower cockpit windows Cockpit ram air adjustable outlets Forced fan ventilation Bleed air heater and defroster with air noise suppression Heated Pitot tubes (2) with pitot heat failure warning (2) Heated static intakes (2) Cockpit map and data case Pilot doors (2) with push –out emergency exit window (with” storm window” on pilot side) One cockpit and one pilot can fire extinguisher Plug in sliding doors (2) for passengers cabin access Baggage compartment with 2 lockable baggage compartment doors Baggage compartment cargo tie-down fittings Wheeled retractable tricycle landing gear ( two wheels on nose gear and brakes on main landing dear) Mooring, hoisting and jacking fittings Pilot and copilot windshield wiper Tail-boom and vertical fin Maintenance steps for access to upper deck Stabilizers Steps for cockpit access Upper-deck cowlings (one front forward sliding, two side opening for engine access)

Fully articulated Main Rotor (M/R) with five composite blades, five Elastomeric bearings and five hydraulic dampers Fully articulated Tail Rotor (T/R) With four composite blades, four Elastomeric bearings and four Elastomeric dampers Three main dual servo actuators Rotating T/R flight controls Force trim system One T/R dual servo actuator Rotating M/R flight controls Dual digital 3- axis linear actuators Rotor Brake Provision for Main Rotor tracking (Magnetic pick up) Pilot fised flight controls (Cyclic, collective, anti-torque pedals)

170

SNEW

2 PT6C – 65 C

170

SNEW

New stainless steel exhaust nozzles Tail Boom attachment rework (Upgrade) Upgrade Fuel Manifold Aux Battery upgrade to 27 ah Baggage compartment upgrade/with 300kg with 300 kg FDR time delay mod Auxiliary Fuel Tank Provisions Dual Air-condition system Aux Fuel Tank TCAS I Honeywell (Bendix King KTA 970) Emergency Floats Provisions Weather radar P660 (Provisions) Emergency Floats Weather radar P660 Particle Separator Markings for High Visibility Main Rotor Blades Engine particle separator Hydraulic system noise suppression mufflers Six Tinted dual pane cabin push –out emergency exit windows (two on each passenger cabin door) Two Tinted dual pane Crew door push –out emergency exit windows 12 place aft ICS with call system interfaced to existing aircraft audio systems. Provision for 14 Bose Series X headset(s) Music system (PS Engineering PAV-80 AM/FM/CD) integrated into the existing Honeywell audio system with IPOD interface Collective Hobbs meter Edwards custom engineered sound proofing (in conjunction with Flight Environments)

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 Co-pilot Primary Flight 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 (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 Electronic Standby Instrument System (ESIS) ( attitude, airspeed, altitude, vertical speed, compass, and ILS data) One Reversion Control Panel (RCP) Two Flux valves Two Cursor Control Devices (CCDs) Two Air Data Modules (ADMs) One Display Dimming Control Panel (DCP) Two Display Controllers (DCs) One Stability augmentation System (SAS) control panel Two Remote Instrument Controllers (RICs) Pilot and copilot interphone control (cyclic grip and floor switches Pilot and copilot microphone and headset Two Modular Avionic Units (MAUs) Two Attitude and Heading Reference Systems (AHRSs) 1st. Radar Altimeter (RT-300) 2nd. Radar Altimeter system (RT-300) Left modular Radio Cabinet (MRC) with the following modules: · One VHF Comm. · One VOR/LOC/ GS/MB Left modular Radio Cabinet (MRC) with the following modules: · One VHF Comm. · One VOR/LOC/ GS/MB · One ADF · One DME Two pedestal mounted MCDUs (Multi Control Function Display Units) Pilot and copilot digital audio panels with remote ICS audio for passengers operations (Modified) Honeywell GPS module with Flight Plan Management System (FPMS) One Flight Guidance Controller Pilot clock (digital) Copilot clock (digital) One magnetic compass One Outside Air Temperature indicator Two Master Warning Lights (MWLs) Two Master Caution Lights (MCLs) Engine 1 Fire Light Engine 2 Fire Light Baggage compartment smoke detector light Autopilot standard 3 axis AFCS PA system Helicopter Emergency Exit Light System (HEELS) FLIR provision / installation Enhanced Ground Proximity Warning System (EGPWS)

Emergency Float Eengines inlet Particle Separator

2006

Custom Paint: metallic green with gold and maroon strips. Step emergency light (2) Fixed landing lights (2) Navigation Lights (3) Anti-collision light Rotating/ retracting landing light

2006

12

Twelve padded crashworthy utility passenger seats, cover with tan leather and perforated inserts 2 Custom leather and sheepskin vovering for crew seats includes matching seatbelts Custom Cabin and cockpit carpet matching throw rug for cabin with one spare for 12 and 8 seat Edwards custom covered interior panels includes: · Leather covering for lower panels · Suede type material coverings for upper and overhead panels Custom wood trim on side panels and overhead (Rosewood) Edwards custom manual limo window

Maintenance: Last Date /Hrs. C/W Date Hrs. Due 25 Hrs. 07/30/07 164.3 189.3 50 Hrs 07/30/07 164.3 214.3 100 Hrs. 03/14/07 123.2 223.2 150 Hrs. 03/14/07 123.2 273.2 300 Hrs. 03/14/07 123.2 423.2 12 Month 03/14/07 123.2 03/14/08 Aircraft is up to date thru TB 139-87