Specs
More Information
Year:2000
Make:BOMBARDIER
Serial Number:9061
TTAF:3120 Hrs.
Number of landings:1006
Engine(s) Manufacturer:BR700-710A2-20
Engine 1: Time since new:3120 Hrs.
Engine 2: Time since new:3120 Hrs.
Auxiliary Power Unit:RE 220GX
:: Propeller Info ::
:: Avionics :: Details:Honeywell Primus 2000 XP Integrated Avionics System which includes:
6-Tube Electronic Flight Instrument System (EFIS ) / Engine Instrument
and Crew Advisory System (EICAS ) using DU -870 8 by 7-inch colour displays
Dual fail-operational (automatic switching) auto-pilot
Dual integrated NZ-2000 Flight Management Systems
Triple long-range Nav source (2 x FMS and Lasertrak NDU )
Dual Global Positioning System (GPS )
Dual full flight regime auto-throttle
Triple LASEREF II Inertial Reference Systems (IRS)
Single Primus 880 color weather radar - dual control heads
Dual Primus II Integrated Nav/Com/Txpndr Radios - VOR /ILS /MKR, ADF
DME, VHF Comm, Mode “S” Diversity Transponder. Compliance with
European 8.33 kHz channel spacing requirements
Central Aircraft Information Maintenance System (CAIMS)
TCAS II Traffic Alert and Collision Avoidance System
Dual ALT -4000 radio altimeter systems
Dual HF -9000 High Frequency (HF ) communications system
Coltech CSD -714 Selective Calling System (SELCAL )
Enhanced Ground Proximity Warning System (EGPWS)
:: Special Features :: Details:2 hours Flight Data Recorder (FDR)
Solid State Cockpit Voice Recorder (SSCVR) – 4 channel recording with
2-hour duration
96 000 lbs MTOW
Humidifier System
6 Channel Satcom, with Facsmile
Build 4
:: Exterior :: Condition:Good
Details:
Split Base with lower Navy and Upper White with Red Accent Striping.
:: Interior :: Condition:Good
Details:Honeywell Primus 2000 XP Integrated Avionics System which includes:
6-Tube Electronic Flight Instrument System (EFIS ) / Engine Instrument
and Crew Advisory System (EICAS ) using DU -870 8 by 7-inch colour displays
Dual fail-operational (automatic switching) auto-pilot
Dual integrated NZ-2000 Flight Management Systems
Triple long-range Nav source (2 x FMS and Lasertrak NDU )
Dual Global Positioning System (GPS )
Dual full flight regime auto-throttle
Triple LASEREF II Inertial Reference Systems (IRS)
Single Primus 880 color weather radar - dual control heads
Dual Primus II Integrated Nav/Com/Txpndr Radios - VOR /ILS /MKR, ADF
DME, VHF Comm, Mode “S” Diversity Transponder. Compliance with
European 8.33 kHz channel spacing requirements
Central Aircraft Information Maintenance System (CAIMS)
TCAS II Traffic Alert and Collision Avoidance System
Dual ALT -4000 radio altimeter systems
Dual HF -9000 High Frequency (HF ) communications system
Coltech CSD -714 Selective Calling System (SELCAL )
Enhanced Ground Proximity Warning System (EGPWS)
:: Weights ::
