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| Aircraft Overview |
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| Aircraft Make: |
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1984 Bombardier Challenger |
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| Aircraft Model: |
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601-1A |
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| Registration: |
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N888AZ |
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| Serial Number: |
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3024 |
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| Ask Price: |
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8,995,000 |
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| Airframe Time |
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| Total Time: |
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8232 |
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| Landings: |
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5254 |
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| Left Engine |
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| Engine Model: |
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General Electric CF-34-3A |
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| Engine Program: |
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JSSI |
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| Total Time Since New: |
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7855 |
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| Time Since Overhaul: |
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2191 |
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| Cycles: |
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5839 |
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| Right Engine |
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| Engine Model: |
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General Electric CF-34-3A |
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| Engine Program: |
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JSSI |
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| Total Time Since New: |
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7967 |
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| Time Since Overhaul: |
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2294 |
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| Cycles: |
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5861 |
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| APU |
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| APU Model: |
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AlliedSignal GTCP 36-100E |
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| Total Time Since New: |
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6152 |
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| APU Engine Program: |
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MSP |
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| Avionics |
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| EFIS: |
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4 Tube Universal EFI-640 |
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| HF Comm: |
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Dual King KHF-950/SELCAL |
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| Comm: |
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Triple Collins VHF-22C w/ 8.33 |
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| Nav: |
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Dual Collins VIR32 w/ FM Immunity |
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| ADF: |
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Dual Collins ADF-60A |
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| DME: |
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Dual Collins DME-42 |
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| CVR: |
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Fairchild A100/Loral FDR new 7/01 |
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| GPS: |
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Dual UNS-1F w/ GPS and Dual Honeywell Laseref II |
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| Radar: |
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Primus 880 |
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| Satellite Weather: |
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WSI In-flight Weather |
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| Radar Alt.: |
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Single Collins ALT-55B |
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| Transponder: |
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Dual Collins TDR-94D w/ enhanced Mode S (EHS) Compliant System |
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| Collision Avoidance: |
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Collins TCAS II w/Change 7 |
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| TCAD: |
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Dual Honeywell AZ800 |
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| Additional Features |
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- Honeywell SPZ-600 IFCS Flight Director
- Cabin and Cockpit Mounted Blue Sky Phones
- Artex C-406-N Navigation interfaced 406 tri-frequency ELT
- Airshow 4000 w/ multimedia package
- Universal TAWS Class A
- Dual Universal UCDs (Universal Cockpit Displays)
- RVSM
- RNP 5 and RNP 10 compliant
- Multi-Function Display Universal MFD-640
- External Audio/Video Inputs |
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| Exterior |
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White upper exterior with a blue bottom. Accented and divided by several red stripes. Painted by Flying Colours Corp., new December 2003. |
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| Interior |
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This elegant 11 to 12 passenger interior was completely new in December 2003 by Flying Colours Corp. Nothing has been spared in the completion of this exquisite aircraft from the new forward cabin serpentine galley to the selection of the finest fabrics, leathers and woods available. It has a four place club up front with quad seating and conference table in back, opposite the 3 place couch. The cockpit has been refinished to new standards with all panels and yokes brought back to like-new condition. Cabin amenities include an Airshow 4000 with dual CD/DVD players, two (2) mounted 20” flat-screen monitors in the forward and aft bulkheads, three (3) 7” Rosen monitors position-able at any seat, microwave oven, and 12 cup coffee maker. All new December 2003. |
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| Maintenance |
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240 Month Inspection completed 7/03, 1200 Hour Inspections completed 9/06 @ 7720.3 Hours, 2400 Hour due @ 9209 Hours, 4800 Hour due @ 9434 Hours, Landing gear overhaul due 7/2013, Maintained under FAR Part 135 standards and 135 ready. In addition, the following inspections were just completed at Duncan Aviation: 100/300/600/8400 hour airframe inspections, 100/300/600 hour engine inspections, 6/12/36/48/60/96 month airframe inspections *including the CPCP (Corrosion Prevention and Control Program) checks associated with these inspections*, 60 month detailed landing gear inspection, Right engine HSI and 6000 cycle limit component replacement (done by GE), Fan disk and turbine wheel AD\'s |
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| Hard Landing Inspection |
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In 1992, there was a documented hard landing, during which time Bombardier replaced some nose structure and a right main gear axle. The aircraft flew for ten years trouble and incident free when a defect was found on the right wing by Bombardier during a scheduled gear overhaul. After some investigating and engineering recommendations, the right main landing gear attach structure and right main inboard wing spar were replaced with new. The work was done with full engineering support and was performed at Bombardier. No other indication of any other lingering issue was noted. The aircraft also went through a 6/12/24/48/60/240 month, and a 300/600/1200/7200 hour inspection at this time and all discrepancies, whether structural or cosmetic, were repaired to factory new condition. Since then, the aircraft has flown for three years and 1000 hours without any complications or faults pertaining to the repairs. There are no reduced inspection intervals associated with the repair. |
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