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2000 Bombardier Global Express
Serial Number: 9061
Registration #: ZS-ESA
Price: US$ 46,500,000
Location: South Africa
A /C Type: Global Express
Green C of A Date: 24th August 2000
Date Entered Service: 24th March 2001
Status Date: 12th November
2008
Airframe:
TOTAL TIME: 3,239 Hrs
LANDINGS: 1,043
Engines: BR700-710A2-20
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#1 |
#2 |
| Serial Number |
12207 |
12230 |
| TTSN: |
3139.9 |
3128.8 |
APU:
Type: Allied Signal RE220GX
Serial Number:P-165
TT : 2863
Interior:
Entry Area
Forward lavatory (Magair sanitation system, vanity/storage cabinet)
Large forward galley
One fully berthable narrow executive seat in crew rest area
One pocket sliding door (crew area)
Storage cabinet with fold down table
Forward Cabin
Single sliding pocket door
Four single wide electrical executive seats with lumbar control, full recline and swivel capability
Two pull-out tables
20" monitor, bulkhead-mounted |
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Mid Cabin
Conference grouping - 2 double seats (lumbar controls, full recline and swivel inboard seat)
One single narrow executive seat in crew area (LHS ) against the work station
Manual hi-low conference table
Credenza cabinet /work station (RHS )
Entertainment cabinet
Low cabinet
One pop-up monitor
Aft Cabin
3 place 16G, fully berthable divan seat (RHS )
Two single wide executive seats (lumbar control, full recline and swivel capability)
One bi-fold table
20" monitor, bulkhead-mounted
Aft Lavatory/Storage Area
Magair sanitation system
Vanity cabinet
Wardrobe/storage compartment
Baggage Compartment
Approximately 145 cu. ft.
Aft Equipment Bay
Towbar assembly and towbar storage provisions
Ladder and ladder storage provisions
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Exterior:
The aircraft has a split paint scheme. The upper fuselage is Matterhorn white, whilst the lower section is Royal blue with red accent stripe with two further royal blue accent stripes on top. The is repeated on the tail in a reverse format.
Avionics: Honeywell Primus 2000 XP Integrated Avionics System which includes:
6 (8' x 7") DU -870 colour EFIS displays Tube Electronic Flight Instrument System (EFIS)
Crew Advisory System (EICAS)
Dual fail-operational (automatic switching) auto-pilot
Dual integrated NZ-2000 Flight Management Systems with Dual 12 Channel Global Positioning System (GPS)
Triple long-range Nav source (2x FMS and Lasertrak NDU)
Autothrottle System
Full Authority Digital Engine Control System (FADEC)
Triple LASEREF II Inertial Reference Systems (IRS)
Single Primus 880 colour weather radar dual control heads with Lighting Sensor |
Dual Primus II RM -855 Integrated Nav/Com/Txpndr Ident Radios with VOR /ILS /MKR, ADF , DME , VHF Comm, Enhanced Mode "S"
Diversity Transponder Compliant with European 8.33 kHz channel spacing and FM Immunity requirements
Central Aircraft Information Maintenance System (CAIMS)
TCAS II Traffic Alert and Collision Avoidance System (Change 7 incorporated)
Dual Collins ALT -4000 Radio Altimeter
Dual Collins HF -9000 High Frequency (HF) communications system
Coltech CSD -714 Selective Calling System (SELCAL)
Allied Signal V Enhanced Ground Proximity Warning System (EGPWS) version 7 |
Additional Features:
Allied Signal Flight Data Recorder (SSFDR) - 2 Hours
Allied Signal Solid State Cockpit Voice Recorder (SSCVR) - 4 channel recording with 2-Hour duration
Humidifier System
6 Channel MCS -6000 SATCOM , with Facsimile (5 voice and 1 data line)
MagnaStar C-2000 Airbourne Telephone System
Incorporates Build 4 Compliant
Fire blocked Seats
HUD
Thermal Printer
ARTEX 406HZ Emergency Locator Transmitter With Nav Interface
Office In The Sky (SB 700-23-003)
Teledyne Datalink
Airshow Genesys
Audio International 10 Disc CD Shuttle
Audio International DVD Player X 2
Audio International Cassette Player
Securaplane System
Head Up Displays
3RD VHF COMM
Maintenance:
Aircraft is enrolled on Smart Parts at a rate of US $ 649/Hr
Engines are covered under the Rolls Royce Power by the Hour Program at a rate of US $ 145/HR per engine
The APU is enrolled on MSP Program US $ 55.45/Hr
Rolls Royce Corporate Car Program - US $ 568/Hr (both engine)
The aircraft is maintained on CAMP program
The aircraft primary structure is covered under the warranty for 20 Years from entry into service
The last major maintenance done was the 1A, 2A, 3A, 6A completed 12/2007.
Next due is an A-Check (500hr) 23/07/2008.
Weights:
Max Take Off Weight 96 000 Lbs
Gross Weight (RAMP ) 96,250 Lbs
Fuel Capacity 43,350 Lbs
Max Landing Weight 78,600 Lbs
Empty Weight 49,462 Lbs
Basic Operating Weight 51,622 Lbs | |
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Ask for more details about the sale of this aircraft:
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The following details, identifying this aircraft, are automatically included in your inquiry. Re: 2000 Global Express For Sale Serial: 9061
Reg: ZS-ESA |
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