Description

AIRCRAFT SPECIFICATIONS
Tail Number: N
Year 2000
Serial Number 90XX

Airframe Hours 2892
Landings 1331
Maintenance Program SmartParts

ENGINE STATUS
Left – BR7-10A2-20 - SN 12195
Time since New L 2892
Cycles Since New L 1334
Right -- BR7-10A2-20 - SN 12198
Time since New R 2892
Cycles Since New R 1331
Maintenance Program JSSI

APU STATUS
APU – RE-220(GX) – SN P-145
Total Time/Cycles Since New 2386/2838
AVIONICS ADDITIONAL EQUIPMENT & WEIGHTS
Honeywell 2000 XP Integrated Avionics System:
Office in the Sky Option: (SB 700-23-003) _7; Magnastar C-2000 Airborne Telephone System _7; Teledyne Datalink System (ACARS)
Six 8"x 7" DU-870 Color EFIS displays, 2 PFD / 2 EICAS / 2 MFD
Airshow Genesys System
Triple LASERREF III Inertial Reference System
Baker Cabin Management System
Triple AZ-840 Micro Air Data Computers (MADC)
Baker CD/DVD/VHS Entertainment system
Quad Ameteck DA-810 Data Acquisition Units (DAU)
Three 21.3 inch Video Monitors
Dual NZ-2000 Integrated FMS w/ Dual 12 Channel GPS
Securaplane Camera System w/5 External Cameras
Triple IC-800 Integrated Avionics Computers (IAC) with EFIS Reversionary capability
Integrated Electronic Standby Instrument System
Primus 880 Color Weather Radar w/ Dual Control heads
Window Frames Polished Aluminum
TCAS II Traffic Alert and Collision Avoidance System (Chg 7)
Direct TV System
Allied Signal Mark V EGPWS w/RAAS
Built-in Fax Machine
Triple Primus II RM-855 Integrated NAV/COM/ldent Radios w/ VOR/ILS/MKR/ADF/DME/VHF Comm and Enhanced Mode S Diversity Transponders (Dual RCZ-833K and RNZ-851) w/8.33kHz Channel Spacing and FM Immunity Compliant
Build 4 Compliant
3rd VHF Comm. Installation (RCZ-833)
Batch 2+ Avionics Upgrade
Dual Collins ALT-4000 Radio Altimeters
Convection Oven/Microwave
Dual Collins HF-9000 HF Communication System
Tel-Tail Lighting System
Single Coltech CSD-714 SELCAL
Inside Refuel/Defuel Panel
Full Authority Digital Engine Control System (FADEC)
Central Aircraft Information Maintenance System (CAIMS)
Dual Full Flight Regime Auto Throttle System
Engine Indication/Crew Alerting System (EICAS)
MCS-6000 SATCOM (6 channel, (5 Voice, 1 Data)
Allied Signal SSCVR Cockpit Voice Recorder
Allied Signal SSFDR Flight Data Recorder
Artex 406 Hz Emergency Location Transmitter
WEIGHTS
Gross Ramp Weight 98,250 lbs
Max Landing Weight 78,600 lbs
Max Take Off Weight 98,000 lbs
Basic Operating Weight 51,800 lbs
Basic Operating Weight 51,800 lbs
Empty Weight 50,031 lbs
Fuel Capacity 43,350 lbs

EXTERIOR
Painted by Bombardier Completion Center, Tucson, Arizona November 2001. The aircraft is a colored split base. The upper is Matterhorn white and lower is gray with center accent stripes of blue and gray.

INTERIOR
Bombardier Completion Center, Tucson, Arizona; November, 2001. Fireblocked, Twelve (12) passengers. Forward galley including one jump seat and one (1) berthable crew rest area, fwd storage and fwd crew lavatory. The fwd cabin features four (4) executive club seats with two executive foldout tables. The mid-cabin features a four (4) seat conference grouping with hi-lo manual conference table. Two (2) standard club seats with one foldout table. The aft-cabin features an entertainment cabinet with monitor and audio/visual equipment. Two (2) standard club seats with one foldout table. One diagonal two (2) place berthable divan converts to a double bed. Aft full lavatory, wardrobe compartment and baggage compartment.

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