N818TH - 1996 BOMBARDIER CHALLENGER 604

1996

BOMBARDIER

CHALLENGER 604

5315

N818TH

Used

* MONTHLY LEASE RATE: $150,000 per month (Based on a six month lease) WEIGHT: RAMP WEIGHT: 48,300 Lbs. MAX T/O WEIGHT: 48,200 Lbs. LANDING WEIGHT: 38,000 Lbs. ZERO FUEL WEIGHT: 32,000 Lbs. B.O.W.: 27,912 Lbs. FUEL CAPACITY: 20,062 Lbs. Aircraft enrolled in Smart Parts, FAA Part 135 operated, 6-Tube EFIS

5334.0

TOTAL TIME: (Times as of 11/04/2004) TTAF: 5,333.5 LANDINGS: 2,694

ENGINES: CF34-3B LEFT RIGHT TSN: 5,319.8 5,333.5 CYCLES: 2,689 2,704 SERIAL NUMBER: 872061 872047 (Engines on Condition)

AVIONICS: (Collins FCC-4000 / Pro Line 4 Avionic System) COMMUNICATIONS: (2) Dual Collins VHF-422B Comms w/ 8.33 kHz Spacing NAVIGATION: (2) Dual Collins VIR-432 Navs w/ FM Immunity AUTOPILOT / FLIGHT DIRECTOR: (2) Dual Collins FCC-4000 / Pro Line 4 Fail Operational (Automatic Switching) Autopilot System EFIS: Collins EFD-4077 6-Tube Electronic Flight Instrument System (EFIS) / Engine Instrument and Crew Advisory System (EICAS) WEATHER RADAR: Collins TWR-850 Weather Radar w/ Turbulence Detection & Dual Control Heads TRANSPONDER: (2) Dual Collins TDR-94 Mode S Transponder w/ Enhanced Surveillance Flight ID AUTOMATIC DIRECTION FINDER: Collins ADF-462 ADF RADIO ALTIMETER: Collins ALT-55B Radio Altimeter DISTANCE MEASURING EQUIPMENT: (2) Dual Collins DME-442 DME TRAFFIC ALERT & COLLISION AVOIDANCE SYSTEM: Collins TTR-920 TCAS II w/ Change 7 GLOBAL POSITIONING SYSTEM: (2) Dual Collins GPS-4000 Global Positioning System LONG RANGE NAVIGATION: (3) Triple Litton LTN-101 Inertial Reference System (IRS) FLIGHT MANAGEMENT SYSTEM: (3) Triple Collins FMS-6000 w/ Dual GPS and Data Loader AIR DATA COMPUTERS: (2) Dual Collins ADC-850 Digital Air Data Computers EGPWS: Honeywell Mark V EGPWS AFIS: Global AFIS FLIGHT DATA RECORDER: Fairchild F-800 Digital Flight Data Recorder COCKPIT VOICE RECORDER: Fairchild A100S HF: (2) Dual Collins HF-9031A High Frequency Radio w/ SELCAL EMERGENCY LOCATOR TRANSMITTER: Dorne Margoli ELT

OPTIONS & FEATURES: Pulse Landing Light System Logo Lighting Emergency Vision Assurance System (EVAS) Jumpseat Audio Panel ¡§Airshow Network¡¨ Flight Information System (Genesys) Fax/Printer/Copier 10-Disk CD Changer DVD Player VHS Video Cassette Players (multi-standard) High Temp TIA Oven Two bulkhead-mounted 18¡¨ monitors (Cabin fore and aft) Microwave Oven Krups Cappuccino/Nespresso maker Hot cup Divided Ice Drawer 4 Pull out work surfaces (Galley) Runway Advisory and Avoidance System (RAAS) Collins SAT-906 6-channel SATCOM Magnastar C-2000 Airborne Telephone System

EXTERIOR: (Completion by K-C Aviation Dallas) Two tone paint scheme, Chevron White on top with Jetglo Midnight Blue on bottom separated by an Accryglow Titanium Silver stripe.

10

INTERIOR: (Completion by K-C Aviation Dallas) The custom designed 10-passenger interior features a forward galley, aft lavatory configuration. The main passenger cabin area features a 4-club chair grouping forward and two club seats and a 4-place 9-G divan aft. All club seats and the divan are birthable. The aft lavatory features a double closet and multiple storage compartments. The interior is modern and richly appointed with light tan leather covered sculpted seats. Woodwork is a satin finished pear-wood. All main cabin and lav windows have electric window shades.

CAPABILITIES: RVSM: Yes Required Navigation Performance 5: Yes Minimum Navigation Performance Specs: Yes Required Navigation Performance 10: Yes FM Immunity: Yes 8.33 kHz Channel Spacing for Comms: Yes

MAINTENANCE: Aircraft Enrolled on Smartparts APU Enrolled in MSP Engines on Condition No Damage History Current FAR 135 Last Airframe Inspection: 96 Month (June 04) Detailed Landing Gear (June 04) SB 604-53-006 FS 409 Pressure Bulkhead Reinforcement (June 04) SB 604-27-005 Stall Computer (June 04) Last Engine Inspection: 400 Hour (June 04) NOTES: ƒô Operated and Maintained to FAR Part 135 Standards, records and maintenance history are superb.