Airframe Status (As of June 6, 2008)
SERIAL NUMBER: 9058
REGISTRATION NUMBER: N79AD
DATE OF MANUFACTURE: July 2000
ENTERED INTO SERVICE: September 2001
TOTAL TIME: 1606.3
LANDINGS: 801
- 1A, 1C Inspection completed November 2007
- 4C Inspection completed September 2006
- Aircraft Maintenance Tracking Program: Flightdocs
- Airframe enrolled on the Smart Parts Program (Contract # 9058-61)
Engine Status
Left and Right Engine:
- Rolls Royce BR710A2-20
- Serial Number: 12222
- Hours: 1606.3
- Cycles: 801
- HSI and Overhaul: On Condition
Right Engine:
- Rolls Royce BR710A2-20
- Serial Number: 12223
- Hours: 1606.3
- Cycles: 801
- HSI and Overhaul: On Condition
APU: Allied Signal RE-220 (GX)
s/n P-142
1479 hrs
1807 cycles
Weights
- Gross Weight (Ramp): 96,250 lbs
- Max Take off Weight: 96,000 lbs
- Fuel Capacity: 43,350 lbs
- Max Landing Weight: 78,600 lbs
- Empty Weight: 49,462 lbs
- Basic Operating Weight: 50,300 lbs
Interior
Bombardier Completion Center, Montreal, Quebec, Canada; September 2001. Fireblocked, Eight (8) passengers, plus one jumpseat and one crew rest. Fwd cabin features four (4) executive club chairs with foldout tables. Center-Left cabin features a 3-place, 9g berthable divan opposite a two executive club chairs with foldout table. Aft left cabin features 2 executive club chairs with Conference table, opposite a 3-place, 9g berthable divan. The forward galley features a Coffee Maker and Warming oven. Fwd crew lavatory, Aft full lavatory.
Avionics
Honeywell 2000 XP Integrated Avionics System:
- Six 8"x 7" DU-870 Color EFIS displays, 2 PFD / 2 EICAS / 2 MFD
- Triple HG-2001GD03 Inertial Reference System
- Triple AZ-840 Micro Air Data Computers (MADC)
- Quad Ameteck DA-810 Data Acquisition Units (DAU)
- Triple NZ-2000 Integrated Flight Management System w/ Dual 12 Channel GPS
- Triple IC-800 Integrated Avionics Computers (IAC) with EFIS reversionary capability
- Primus 880 Color Weather Radar w/ Lightning Sensor
- TCAS 2000 Traffic Alert and Collision Avoidance System (Change 7 incorporated)
- Central Aircraft Information Maintenance System (CAIMS)
- Autothrottle System
- Full Authority Digital Engine Control System (FADEC)
- Engine Indication/Crew Alerting System (EICAS)
- Dual Primus II RM-855 Integrated NAV/COM/Ident Radios w/ VOR/ILS/MKR/ADF/DME/VHF Comm and Enhanced Mode S Diversity Transponders (Dual RCZ-833K and RNZ-851)
- 8.33kHz channel spacing and FM Immunity compliant
- 3rd VHF Comm. Installation (RCZ-833)
- Dual Collins ALT-4000 Radio Altimeters
- Dual Collins HF-9000 HF Communication System
- Single Coltech CSD-714 SELCAL
- WSI AV-200 Weather Inflight Satellite System
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Additional Equipment
- Allied Signal Mark V EGPWS
- Allied Signal SSFDR Flight Data Recorder
- Allied Signal SSCVR Cockpit Voice Recorder
- Cockpit Thermal Printer (Right Side ledge)
- Artex 406hz Emergency Location Transmitter w/ Nav Interface
- MCS-6000 SATCOM (6 channel, (5 Voice, 1 Data)
- Office in the Sky Option: (SB 700-23-003)
- MagnaStar C-2000 Airborne Telephone System
- Teledyne Datalink
- Airshow Genesys
- Audio International 10 Disc CD Changer
- Audio International DVD Player
- Audio International Video Cassette Player �� Additional Cabin Windows
- Fwd and Aft Cabin bulkhead mounted, 18" Monitors
- Securaplane Camera System
- Integrated Electronic Standby Instrument System
- Provisions for Dual CMC Electronic Flight Bags
- Head Up Display
- Fan Disk Inspection Airworthiness Directive
- Build 4 Compliant
- Cappuccino Machine
- Logo Lights
- Inside Refueling Panel
Exterior
Painted by Bombardier Completion Center, Montreal, Canada, September 2001. Overall aircraft is a split base Matterhorn White over Royal Blue with two center accent stripes of Antique Gold and Royal Blue.
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