GENERAL   EQUIPMENT   INC.                    

Year

2005

Manufacturer

BELL AGUSTA AEROSPACE

Model

AB139

Price

Location

Condition

Serial Number

Registration Number

Total Time

166 Hours

Hot Section Time

170/170 SHSI

Flight Rules

IFR

Number Of Seats

12

General Information

aircraft under warranty until 9/08

Detailed Description

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.

Airframe:
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)

Engine Specs:
2 PT6C – 65 C

Prop(s):
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)

Modifications/Conversions:
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)

Avionics/Radios:
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)

Additional Equipment:
Emergency Float
Eengines inlet Particle Separator

Year Painted: 2006

Exterior:
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

Year Interior:
2006

Interior:
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

Inspection Status:
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