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Engines |
Rolls Royce
BR710A2-20 on
Corporate Care
Program |
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 Left |
Right |
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Time Since New: |
1203.34 |
1203.34 |
|
Cycles: |
553 |
553 |
|
HSI & Overhaul: |
On Condition |
On Condition |
|
|
APU |
Allied Signal
RE-220 (GX) on
MSP.Time Since
New: 511;
Cycles: 963 |
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Additional
Equipment |
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Illuminated
Ordinance Signs
Cabin/Lavatory Call
System
Manual storage -
cockpit - side
consoles
Baker Cabin
Management System
(CMS):
Function control
switch panels at
every passenger
location
IR
Receiver/Transmitter
c/w two (2)
hand-held remotes
Entertainment
System:
High quality cabin
speaker arrangement
Passenger headphone
distribution
Two (2) 21.3” LCD
video monitors
Four (4) 10.4”
plug-in video
monitors
One (1) 6.5” plug-in
video monitors
Compact Disc (CD)
and Digital Video
Disc (DVD) Player
Video Cassette
Player
(multi-standard)
Airshow 400
One (1) power
converter (3500
VA/115V/60Hz)
Ten (10) clear
leather seat with
electric inflatable
lumbar support
Three (3) places16G
divan, approved for
taxi, take-off and
landing, with
armrest end cabinet.
Two (2) slipping
places when
deployed. (RHS).
Conference Hi-Lo
Table
Exterior service
panel lights
Common panel keyed
locks
Aft equipment bay
ladder
Aft equipment bay
storage box
Cockpit and
Jump-seat
flashlights
Footrests
Additional cockpit
lights
Approach chart
holders
Entry area heated
400 Hz Service Bus –
ground power
Securaplane CAM-11
incorporating four
(4) video cameras
and CMX-01 vertical
fin camera. |
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Maintenance & Inspections |
| |
|
Engines on Corporate
Care
Jar-Op’s Compliant |
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+1.954.771.3096
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Avionics |
| |
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Honeywell Primus 2000 XP
Integrated Avionics
System
6-Tube Electronic Flight
Instrument System (EFIS)
/ Engine Instrument and
Crew Advisory System (EICAS)
using DU-870 8 by 7-inch
color displays
Dual fail-operational
(automatic switching)
auto-pilot
Triple integrated Flight
Management Systems
Triple long-range NAV
source (3 FMS’s)
Navigation Data Base
Data Loader
Global Positioning
System (GPS)
Dual full flight regime
auto-throttle
Triple IC-800 Integrated
Avionics Computers (IAC);
built in EFIS
reversionary capability
and fault warning
redundancy - combines
the functions of five
major subsystems
Triple Micro Air Data
Computers (MADC)
Triple LASEREF Inertial
Reference Systems (IRS)
Quad DA-810 Data
Acquisition Units (DAU)
Color Weather Radar -
Dual control heads
Honeywell LSZ-860
Lightning Sensor System
(LSS)
Dual Integrated
Nav./Com/Ident. Radios -
VOR/ILS/MKR, ADF,nDME,
VHF Comm, Mode 'S'
Diversity Transponder.
Compliance with European
8.33 kHz channel spacing
requirements
Honeywell RCZ-833 3rd
VHF Transceiver
Honeywell Additional
Global Positioning
System (GPS)
Central Aircraft
Information Maintenance
System (CAIMS)
Miltope PrinterTP-4840
TCAS RT-950 Traffic
Alert and Collision
Avoidance System
Dual HF Comm
Selective Calling (SELCAL)
System
Dual Radar Altimeter
Cockpit Voice Recorder (CVR)
Digital Flight Data
Recorder (DFDR)
Enhanced Ground
Proximity Warning System
(EGPWS)
406MHz Emergency Locator
Transmitter (ELT)
Sextant Head-up Display
Teledine Telelink
SATCOM
NAT-MNPS
B-RNAV
RVSM |
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Weights |
| |
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Gross Weight (Ramp):
96,250 lbs.
Max Take Off Weight:
96,000 lbs.
Fuel Capacity: 43,350
lbs.
Max Landing Weight:
78,600 lbs.
Max Zero Fuel Weight:
56,000 lbs |
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Sales@GlobalExpressJetsForSale.com |
