STATUS: As of January 13th, 2020:

• TOTAL TIME: 7,256 Hours
• LANDINGS: 2,023
• ENGINES: Rolls Royce BR700-710A2-20

WEIGHTS:

• MAX RAMP WEIGHT: 98,250 Lbs. MAX TAKE-OFF WEIGHT: 98,000 Lbs.
• MAX LANDING WEIGHT: 78,600 Lbs. MAX ZERO FUEL WEIGHT: 56,000 Lbs.
• EMPTY WEIGHT: 51,620 Lbs. MAX USABLE FUEL: 43,390 Lbs.

CAPABILITIES:

• ADS-B Out 
• TCAS 7.1 
• Emergency Descent Mode
• WAAS / LPV 
• RNP Capable 
• Lightning Detection
• FANS 1/A 
• MNPS 
• Auto Throttles

AVIONICS: Honeywell Primus 2000 XP Avionics Suite:

• AIR DATA COMPUTERS: Triple Honeywell AZ-840 Micro Air Data Computers
• CONTROL DISPLAY UNITS: Dual Honeywell FMS CDU 820 Control Display Units
• COCKPIT VOICE RECORDER: Honeywell SSCVR Cockpit Voice Recorder
• COMMUNICATIONS: Dual Honeywell RCZ-833M and 3rd RCZ-833 VHF Transceivers
• ELECTRONIC FLIGHT INSTRUMENT SYSTEM: Triple Honeywell IC-800 Integrated Avionics Computers (IAC) with
• six (6) 8” x 7” DU-870 color EFIS displays
• EMERGENCY LOCATOR TRANSMITTER: Artex 406 MHz ELT
• FLIGHT DATA RECORDER: Honeywell SSFDR Flight Data Recorder
• GLOBAL POSITIONING SYSTEM: Dual Honeywell Global Positioning Sensor Unit (WAAS/LPV – SB 700-34-054)
• HIGH FREQUENCY: Dual Collins HF-9031A with SELCAL
• LIGHTNING DETECTION: Honeywell LP-860 Lightning Sensor Processor
• LONG RANGE NAVIGATION: Triple Honeywell Inertial Reference Units
• NAVIGATION: Dual Honeywell RNZ-851 Integrated VHF Navigation radios with VOR/ILS/MKR/ADF/DME and FM
• Immunity
• RADIO ALTIMETERS: Dual Rockwell Collins ALT-4000 Radio Altimeters
• TERRAIN AWARENESS AND WARNING: Honeywell Mark V EGPWS
• TRANSPONDERS: Dual Honeywell RCZ-833M Transponders with ADS-B Out (SB 700-34-062)
• TRAFFIC COLLISION ALERT AVOIDANCE SYSTEM: Honeywell/ACSS TCAS 2000 with Change 7.1
• WEATHER RADAR: Honeywell Primus 880 Color Radar

ADDITIONAL ITEMS:

• Electronic Standby Instrument
• Cockpit Refuel/Defuel Panel
• Jumpseat Audio Control Panel
• 26 Gallon Forward and Aft Water Tank
• Logo Lights
• 115VAC/60Hz Electrical Outlets

Original Interior by Bombardier Tucson. (Softgoods Refurbished in March 2012 by Standard Aero). Luxurious nine-passenger executive interior features a spacious forward galley area, with an adjacent crew rest area and forward lavatory. The forward cabin consists of a four-person club seat configuration with side ledge pull-out tables on each side. The mid-cabin offers a four-person conference area with an adjustable-height table across from a three-person divan (not certified for occupancy during taxi, take-off, or landing). The aft cabin features a diagonal two-person settee (not certified for occupancy during taxi, take-off, and landing) with fold-out sleeping configuration, across from a single club seat and corner credenza. An aft lavatory with spacious wardrobe space, in-flight accessible baggage compartment, and cockpit jumpseat completes the interior.

ENTERTAINMENT:

• Baker Cabin Management System
• Airshow 400
• Kaliedescape Entertainment Movie Server
• External Camera System
• Cabin Speaker System
• Forward and Mid Cabin Bulkhead Monitor
• Aft-Cabin Pop-up Monitor
• Galley Touch Screen Monitor
• Sideledge Plug-in Monitors

COMMUNICATIONS:

• Inmarsat Swift Broadband
• CNX 200 Network Router
• ICS-200 Iridium System
• (3) Phone Handsets – (1) in the Cockpit, (2) in the Cabin

GALLEY DESCRIPTION:

• High Temp Convection Oven
• Microwave
• Food Chiller
• Coffee Maker
• Galley Touch Screen Monitor
• Generous Storage Space

LAVATORIES:

• Forward Crew Lavatory with sink
• Large Aft Lavatory with generous wardrobe

Interior Last Updated/Refurbished In 2012

Last Painted by Standard Aero in March 2012. Overall Matterhorn White with Dark Blue and Grey Striping 

Exterior Last Painted In 2012

MAINTENANCE & INSPECTIONS:

• Batch 3.3 complied with September 7 th, 2016
• Engines enrolled on Rolls Royce Corporate Care
• APU enrolled on Honeywell MSP
• Airframe enrolled on Bombardier Smart Parts
• Date of Manufacture: February 2000
• Certification Date: April 2000
• In-Service Date: December 2001
• Maintenance tracked by CAMP