Airframe Landings: 197


Engines

Loc.
TSN
CSN


L
610
197


R
610
197


APU TSN: 630 Hours

The Full Fly-by-Wire (FBW) Flight Control System Features the Bombardier Vision Flight Deck:Four 14 X 11 AMLCS - LCD Adaptive Flight DisplaysThree (3) VHF Communication RadiosTwo (2) HF TransceiversOne (1) Dual SELCAL System Capable of MonitoringThree (3) VHF and Two (2) HF RadiosOne (1) Iridium Satellite COMM. SYS. with Two (2) Voice Channels and One (1) ATA ChannelOne (1) Dual Channel Interphone SystemTwo (2) Integrated Flight Information System (IFIS) with Dual File Server UnitOne (1) Head-up Display (HUD) SystemOne (1) Enhanced Vision System (EVS)One (1) Synthetic Vision System (SVS)One (1) Electronic Integrated Standby Instrument (ISI)One (1) Air Data System (ADS) Composed of Four (4) Air Data Smart Probes (ADSP)One (1) Weather RadarThree (3) Inertial Reference Systems (IRS)Two (2) GPS WAAS ReceiversTwo (2) VHF Navigation ReceiversTwo (2) ADF ReceiversTwo (2) DME TransceiversOne (1) Traffic Surveillance System and One (1)Standalone Transponder Capable of:Dual Transponder FunctionalityTCAS II Change 7.1ADS-B OutTwo (2) Radio Altimeter SystemsOne (1) Terrain Awareness and Warning Sys. (TAWS)Three (3) Flight Management Systems (FMS)Electronic Flight Instrument System (EFIS)Electronic Checklist (ECL)Dual Synchronized Digital GPS ClocksEngine Indication and Crew Awareness Sys. (EICAS)Cockpit Voice Recorder (CVR)Flight Data Recorder (FDR) with Underwater LocationEmergency Locator Transmitter (ELT)Automatic Flight Control Systems (AFCS)Flight GuidanceAutothrottleAutopilotYaw DamperAutomatic Pitch Trim

16 / 17 Passenger ConfigurationAFT Stateroom with Large Bed2 Bulkhead Mounted MonitorsVertical WeatherPredictive WindshearSurface Management System