Challenger 605
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| Производитель: | Bombardier/Challenger |
| Модель: | 605 |
| Ресурс двигателя: | 1356 часов |
- Характеристики
- Описание
- Отзывы
| Количество мест | 12 |
| Крейсерская скорость | 850 |
| Максимальная дальность полета | 7490 |
Моторы, детали:
Description General Electric CF34-3B
Serial Number(s) 950940 950938
Total Hours Since New 1,356 Hours 1,356 Hours
Total Cycles Since New 595 Cycles 596 Cycles
HSI Due/Overhaul Due On Condition
Program Coverage GE OnPoint
APU
Description Honeywell GTCP-36-150(CL)
Serial Number P-302
APU Total Time Since New 1,395 Hours
HSI Due/Overhaul Due On Condition
Serial Number(s) 950940 950938
Total Hours Since New 1,356 Hours 1,356 Hours
Total Cycles Since New 595 Cycles 596 Cycles
HSI Due/Overhaul Due On Condition
Program Coverage GE OnPoint
APU
Description Honeywell GTCP-36-150(CL)
Serial Number P-302
APU Total Time Since New 1,395 Hours
HSI Due/Overhaul Due On Condition
Авионика:
The Bombardier Challenger 605 is equipped with an integrated, Rockwell Collins Pro-Line 21 avionics suite. A general summary of this aircraft's avionics suite is as follows (Items in bold indicate optional/added equipment):
Type of Unit Quantity Description
EFIS (Electronic Flight Instrument System) Four 10"x12" Adaptive Flight Displays
ESIS (Electronic Standby Instrument System) Single Integrated Stand-by Instruments
FMS (Flight Management System Dual FMC-6000 Flight Management Systems
IRS (Inertial Reference System) Dual Honeywell Laseref V
GPS (Global Positioning System) Dual Collins GPS-4000 Navigation Units
ADC (Air Data Computer) Dual Collins ADC-850E Air Data Computers
NAV (Navigation Radio) Dual Collins NAV-4000
DME (Distance Measuring Equipment) Dual Collins DME-4000
ADF (Automatic Direction Finder) Dual Collins ADF-462
A/P (Autopilot) Dual Honeywell Autopilot system with Auto-throttle
VHF COM (Very High Freq. Communication) Dual Collins HF-4000 VHF Communication System
HF COM (High Freq. Communications) Dual Collins HF-9031A with SELCAL
SATCOM (Satellite Communications) Single ICG ICS-200 Iridium System
AFIS (Airborne Flight Information System) Single Integrated Flight Information System
RADAR Single Collins RTA-854
RADAR ALT (Radar Altimeter) Single Collins ALT-4000 Radio Altimeter
XPNDR (Transponder) Dual Collins TDR-94-D Mode S Transponders
GPWS (Ground Proximity Warning System) Single Honeywell Mark V EGPWS w /TAWS RAAS
TCAS (Traffic Collision Avoidance System) Dual Collins TTR-4000 TCAS II w/ Change 7
LSS (Lightening Detection System Single Honeywell
ELT (Emergency Locator Transmitter) Single Artex 406
CVR (Cockpit Voice Recorder Single L3 Communications CVR
FDR (Flight Data Recorder) Single L3 Communications FDR
Type of Unit Quantity Description
EFIS (Electronic Flight Instrument System) Four 10"x12" Adaptive Flight Displays
ESIS (Electronic Standby Instrument System) Single Integrated Stand-by Instruments
FMS (Flight Management System Dual FMC-6000 Flight Management Systems
IRS (Inertial Reference System) Dual Honeywell Laseref V
GPS (Global Positioning System) Dual Collins GPS-4000 Navigation Units
ADC (Air Data Computer) Dual Collins ADC-850E Air Data Computers
NAV (Navigation Radio) Dual Collins NAV-4000
DME (Distance Measuring Equipment) Dual Collins DME-4000
ADF (Automatic Direction Finder) Dual Collins ADF-462
A/P (Autopilot) Dual Honeywell Autopilot system with Auto-throttle
VHF COM (Very High Freq. Communication) Dual Collins HF-4000 VHF Communication System
HF COM (High Freq. Communications) Dual Collins HF-9031A with SELCAL
SATCOM (Satellite Communications) Single ICG ICS-200 Iridium System
AFIS (Airborne Flight Information System) Single Integrated Flight Information System
RADAR Single Collins RTA-854
RADAR ALT (Radar Altimeter) Single Collins ALT-4000 Radio Altimeter
XPNDR (Transponder) Dual Collins TDR-94-D Mode S Transponders
GPWS (Ground Proximity Warning System) Single Honeywell Mark V EGPWS w /TAWS RAAS
TCAS (Traffic Collision Avoidance System) Dual Collins TTR-4000 TCAS II w/ Change 7
LSS (Lightening Detection System Single Honeywell
ELT (Emergency Locator Transmitter) Single Artex 406
CVR (Cockpit Voice Recorder Single L3 Communications CVR
FDR (Flight Data Recorder) Single L3 Communications FDR
Оборудование:
CONNECTIVITY
Type of Unit Description
In Flight Phone ICS 200 Dual Channel Iridium Telephone
ENTERTAINMENT
Type of Unit Quantity Description
Display/TV Monitor(s) Dual 20" Monitors
Airshow System Single Airshow 410
DVD Player(s) Dual Audio International DVD Players
CD Player Single Audio International 10 Disk CD Changer
Other Notable Features 4x 110V/60Hz Power Outlets; 1x Therapeutic O2 Outlet; Dennis Tracy Audio Speakers; 10x Stereo Headsets
OTHER EQUIPMENT
Type of Unit Quantity Description
On-Board Data Loader (ODL) Single Maintenance Computer
Engine Indication and Crew Alerting System (EICAS) Single Digital control for engines
Type of Unit Description
In Flight Phone ICS 200 Dual Channel Iridium Telephone
ENTERTAINMENT
Type of Unit Quantity Description
Display/TV Monitor(s) Dual 20" Monitors
Airshow System Single Airshow 410
DVD Player(s) Dual Audio International DVD Players
CD Player Single Audio International 10 Disk CD Changer
Other Notable Features 4x 110V/60Hz Power Outlets; 1x Therapeutic O2 Outlet; Dennis Tracy Audio Speakers; 10x Stereo Headsets
OTHER EQUIPMENT
Type of Unit Quantity Description
On-Board Data Loader (ODL) Single Maintenance Computer
Engine Indication and Crew Alerting System (EICAS) Single Digital control for engines
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