2006 Bombardier Global Express XRS

Transcription

1 2006 Bombardier Global Express XRS Asking Price: Make Offer 1472 Hours as of November 5, Landings JAR OPS 1 / EASA Compliant Registration M/GYQM Engines enrolled on Corporate Care APU Enrolled on MSP

2 Floor Plan Thirteen Passengers* / Forward Galley / Forward Lavatory / Forward Crew Rest Area Forward cabin configured with a 3/place (9G), fully berthable divan (certified for in/flight use only), facing a wide single seat Monitor & Entertainment Cabinet Mid/cabin contains a Global Office Executive Work Station with a wide single seat & a 4 place conference group with a hi/low conference table. Aft cabin is fully enclosable and includes two 3/place berthable 16G divans, a 24 forward facing monitor, lavatory, wardrobe & storage cabinet. * Note: Thirteenth Seat is in the Crew Rest Area.

3 Galley A beautifully attired forward Right Hand Side Galley and a Right Hand Side Galley Annex containing: Nespresso coffee machine 10.5 touch screen LCD control monitor Lexan glassware closeout Outboard liquor storage Solid surface countertop Stainless steel sink Microwave and Hi/temp oven Storage for china, linens, cubs and saucers

4 Forward Cabin 31.5 Angle Mounted Monitor Wide Single Berthable Seat with Footrest and Electric Lumbar Side ledge pull/out table with aluminum bull nose 3/place berthable divan (in/flight use only) End Cabinets & Side ledge Storage for each side of the Divan

5 Mid / Cabin Global Office Package Executive Workstation Pop/up 18 Monitor Single Seat 4/place Fully Reclining Conference Group Electric Hi/Low Conference Table

6 Executive Workstation Global Office Package Dual Iridium Satellite Telephones Local Area Network Fax/Printer/Scanner Pull/out work surface On/board Communication Off Aircraft Connectivity Headphone Jack Switch Panel 220VAC / 50 Hz Outlet RJ/45 Jack Rich Wood Finish Miscellaneous Storage

7 Mid/Cabin Conference Seating Hi/Lo Double Pedestal Table Electrically Operated B/E Aerospace Double Seats: Fully reclining with electric lumbar support & flex wing style headrests and with Aisle Seats that Swivel

8 Enclosable Aft Cabin Two facing 3 place Berthable Divans with end Cabinets Mid/Cabin Cabinets (aluminum bull nose with flip/up lid) Two end Cabinets with Gooseneck Reading Lamps 24 semi/recessed forward facing Monitor on the aft LHS bulkhead.

9 Lavatory & Wardrobe Area Lavatory Envirovac sanitation system Large Vanity Cabinet Solid Surface Countertop Stainless Steel Sink Elegant Tap Set Concealed GFI type Outlets Miscellaneous Storage Wardrobe Area Wardrobe & Storage Cabinet Adjustable Shelving Fixed Shelving Right Side Hinged Baggage Door

10 Sink & Baggage Compartment Sink Solid Granite countertop Stainless Steel Sink Beautiful Wood Cabinetry 26 Gallon Water System Baggage Compartment Pressurized Square Feet Fold/up Hang/up Bar 2 Fold Down Shelves Miscellaneous Storage Area Plated Hardware

11 Cabin Entertainment System The Entertainment Cabinet includes: Multi/disc CD Player, Two CD / DVD / MP3 Ethernet Players, a Sony Play Station & Provisions for the Entertainment PCU. Video is via DVD Exterior Camera Views Tailwind 5000 airshow Network Passenger Information System Wiring Provisions for Direct Broadcast Television Receiver Exterior Camera Views All of the above data / images may be displayed on the following cabin monitors: Aft facing 21.3 monitor on the right hand forward cabin bulkhead. Rotating 31.5 monitor located in the left/hand forward cabin entertainment cabinet. 18 pop/up monitor, located in the right hand workstation cabinet. 24 forward facing monitor in the left/hand aft cabin bulkhead. Stereo audio is presented over the cabin speakers and through headphones. Audio source selection and audio control for the CD / DVD / MP3 Ethernet Players or the CD player may be made from: The galley touch/screen MSL PCUS The crew area in/arm touch screen Plug/in Monitors (personal audio) The entertainment PCU

12 Honeywell Primus 2000XP Integrated Avionics System: Production/Installed Avionics Six color Display Units (DU/870) 2 Primary Flight Displays (PFD), 2 Multifunction Displays (MFD), 1 EICAS and 1 System Synoptic Display: Three IC/800 Integrated Avionics Computers (IAC), each responsible for the following functions: I/O processor, ASCB controller, Electronic Display System EDS, Flight Management Computer, Autothrottle control, Flight Guidance Computer FGC. Triple long/range navigation sources: Dual integrated NZ/2000 Flight Management System with CDU/820s, One DL/900 data loader, One Lasertrack Navigation Data Unit (NDU). Triple LASERREF IV Inertial Reference System (IRS) Triple Primus II Nav/Com system with 25 KHz or 8.33 KHz channel spacing Triple AZ/840 Micro Air Data Computers (MADC) Dual Automatic Flight control System (AFCS)

13 Honeywell Primus 2000XP Con t. Artex ELT 110/406 System with Nav Interface Second Global Positioning System (GPS) (Honeywell GPS550) Thales Integrated Electronic Standby Instrument (IESI) 3 rd VHF Communication System Central aircraft Info Maintenance System (CAIMS) Airborne Data Link System (ADLS) (ACARS) EICAS System Primus 880 weather radar with dual Weather Radar Controllers Location Dual full flight regime autothrottle TCAS 2000 Traffic Alert and Collision Avoidance System with change 7 software upgrade Dual Global Positioning System (GPS) Central Aircraft Information and Maintenance System (CAIMS) Other Honeywell Systems: Enhanced Ground Proximity Warning System (EGPWS), Flight Data Recorder (FDR) [57 parameters Part 91 only for S/N 9119 and subsequent] Solid State Cockpit Voice Recorder (SSCVR) 4 channel recording with 2/hour duration. Collins Systems: Dual ALT/4000 radio altimeter systems Dual HF/9000 High Frequency (HF) communications system Coltech System: Coltech CSD/714 Selective Calling System (SELCAL) Other Avionics Systems: Thales/Sextant HUD, Bombardier BEVS Teledyne TL 806/1A Airborne Data Link System (ADLS) with weather graphics capability, Emergency Location

14 Securaplane & External Cameras Securaplane security system detects any intrusion on the interior or exterior of the aircraft It monitors as many as 64 intrusion points via motion & close proximity detectors. Any intrusion may be recorded for later review. Power communication unit provides 7 to 10 days run time. A solar panel option is provided. External Camera system is integrated with the aircraft security system and provides live outside views for display on the cabin monitors when enabled in the cockpit. The following cameras are incorporated into this system: A CAM/14 Camera unit consisting of o Four video color cameras located on the lower fuselage to provide forward, aft, right & left views. o Quad view functionality for up to 360 degrees. o Four directions, including color camera for left/right 116 degree view and color camera for the forward / aft 31 degree view. A CMZ/01 downward/looking camera, located on the belly fairing, provides: o o o o o o o State/of/the/art color zoom up to 72x zoom (18x optional + 4x digital). Automatic / manual focus control. Freeze frame. Low/light operation. Digital signal processing. Wide 48/degree field of view. Zooms in full digital telephoto mode to less than one degree. ACMX/01 vertical fin single high/resolution color camera, which provides 88 degrees field of view. ACMZ/03 glare shield camera.

15 Other Noteworthy Items 1. Full Bombardier Build & Material Specifications available upon receipt of deposit in escrow. 2. New owner may desire to consider repair of minor cracking of entryway woodwork. 3. Owner recently replaced the left in/board slat due to repair required due to an incident during cleaning of the aircraft. 4. The aircraft is privately operated and managed by a professional management company. 5. Two owner aircraft. 6. The aircraft is based in Beijing. 7. Maintenance: The aircraft will have the 1A / 1C / 2C / 4C checks, APU 500 hours inspection / due maintenance / SB Service bulletin / AD Airworthiness Directives / cleaning & servicing completed in January 2012.

16 Thank you for your time David Reynolds Manager