1995 Beechjet 400A. RK-104 N401ML 6,520 Hours Since New 5,064 Landings Since New. Engine Total Time: 6,520 Hours Engine Total Time: 6,520 Hours

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1 1995 Beechjet 400A SERIAL NUMBER: REGISTRATION: TOTAL TIME AIRFRAME: TOTAL CYCLES: RK-104 N401ML 6,520 Hours Since New 5,064 Landings Since New ENGINES: Model: Pratt & Whitney JT-15D-5 Left Engine S/N: PCE Right Engine S/N: PCE Engine Total Time: 6,520 Hours Engine Total Time: 6,520 Hours Engine Cycles s/n: 5,064 Cycles Engine Cycles s/n: 5,064 Cycles Time Since Overhaul: 2,920 Hours Time Since Overhaul: 2,920 Hours Time Since Hot Section: 1,120 Hours Time Since Hot Section: 1,120 Hours Time Remaining till OH: 680 Hours Time Remaining till OH: 680 Hours Overhaul and Hot Sections all done by Pratt & Whitney Factory, Fresh Borescopes and Engine 5-Point Power Assurance Runs (better than 12% margin both engines), Very Clean and in Great Condition. Full traceability and both engines fully matched. HIGHLIGHTS: Low Total Time, Excellent Maintenance and Ownership History. TCAS II, Proline IV with 4-Tube EFIS, Upgraded GPS-4000 with Upgraded FMS and EGPWS. Perfect Aircraft for Upgrade to New Garmin 5000 STC d Package. Fresh 5,000 Landing Inspection ($150k+), New Windshields 2012 ($80k+) Will be Delivered with Fresh A/B Inspections, 3/6/12/24/36 Month Inspections, Overhauled Pitch Trim Actuator ($40k), and CofA Inspections by Toledo Jet FXE. No Damage or Incident History, Enrolled on CAMP, Excellent Records, Full Traceability. Only 2 Owners Since New Provincial Government, Governor Flown 10 years East Greenway Road, Suite 201, Scottsdale, Arizona USA / Office 01- (480)

2 AVIONICS: Avionics Package: Collins FCS-850 / Pro Line 4 / 4 Tube EFIS FMS: Dual Collins FMS-850 (NPA mod) w/gps-4000, recently updated by Collins ADF: Collins ADF-462 Altimeter: Dual Collins Encoding Autopilot: Collins APS-850A Comm Radios: Dual Collins VHF-422A CVR: Fairchild CVR DME: Dual Collins DME-442 EFIS: Collins 4-tube Proline IV Flight Directors: Dual Collins FCS-850 Nav Radios: Dual Collins VIR-432 Radar Altimeter: Collins ALT-55B TCAS II: Collins TCAS-94 TCAS-II with Change 7.0 Transponders: Dual Collins TDR-94D Mode S Weather Radar: Collins RTA-854 Color EPGWS: Honeywell KGP-560 Class B TAWS ADDITIONAL EQUIPMENT: Logo Lights Thrust Reversers Freon Air EXTERIOR: Exterior done new July 2006 by DevAir in Fort Lauderdale International, Always hangared since, Overall Vestal White, Dark Blue and Light Blue Stripes in excellent condition. INTERIOR: New interior by JR Aircraft Interior Fort Lauderdale Executive Airport done August Interior consists of 7 individual executive articulating seats with a rear private belted, flushing lavatory/seat (certified 8 seats). Forward slim-line refreshment center with forward coat closet/storage area, dual mid-cabin pyramid bars, dual cabin tables, all seats done in saddle leather with light brown carpet and carpet runner. Interior is in excellent condition. No sign-off noted for fire-blocking (only needed for Part 135). MAINTENANCE/ INSPECTIONS: (see full factory inspection program following photos) The aircraft is on the standard Beechcraft Factory Phase Maintenance program and has been since delivered new. It consists of hourly and calendar inspections per the Beech Chapter 5 Maintenance Program (see program following photos). Will be delivered with a fresh A, B, 3/6/12/24/36 month inspections, 1,800 Hr. overhauled pitch trim actuator by time and AD, all new tires, batteries and exterior Teflon treatment. Enrolled on CAMP. 2,400 Hr items, A/B/C checks, horizontal tail leading edge

3 and spar web inspections were all accomplished 6,177 AFTT (343 Hrs ago), LH/RH cockpit windshields changed with new on 11/12, wing attach bolts changed to new type per SB on 6/11, On 6,433 AFTT/4,997 landings accomplished 7,400 Hr/5,000 Ldg. landing gear teardown/inspection/ndt/overhaul. Last D check accomplished 4,995 AFTT by Banyan FXE not due until 7,395 AFTT (875 Hrs remaining). Excellent records and logbook package, full traceability, all work orders and release tags since new. Both engines first hot section and second hot section and overhauls all done by Pratt & Whitney factory, matched pair, excellent condition, fresh borescope and power runs.

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11 Maintenance/ Inspections: The aircraft is on a standard Beechcraft Factory Phase Maintenance program and has been since delivered new. It consists of the following hourly and calendar inspections per the Beech Chapter 5 Maintenance Program: INSPECTION INTERVAL Inspection A Inspection B Inspection C Inspection D Lubrication Inspection A Lubrication Inspection B Lubrication Inspection C Lubrication Inspection D Autopilot Servos Emergency Light power Supply Drive Belt / Pulley Compressor / Shaft Seal Condenser Fan Condenser Coil Electrical Wiring Drive Motor / Brushes Receiver Dryer Assembly Belt Cover Lead Acid Battery Starter Generator LH Starter Generator RH Power Break Valve Filters (clean) Drive Belt / Pulley Compressor / Shaft Seal Drive Motor / Brushes Main Battery ELT Standby Power Supply Battery Capacity Test AHRS Standby Power Supply Battery Discharge Check Cockpit Portable Fire Extinguisher Cabin Portable Fire Extinguisher Recertification Transponder I / II Recertification Standby Altimeter Recertification Air Data Computer Pilot Static System Mach Overspeed Warning System Fuel Quantity Indicators CVR Underwater Locator Beacon Air Data System / Skin Waviness Pneumatic Storage Bottle 200 hours 400 hours 1200 hours 200 hours 400 hours 1200 hours 6 /48 months 3 months 200 hours / 3 months 1000 hours 1000 hours 1000 hours 1000 hours 1000 hours 1000 hours 1200 hours / 24 months 1 year 1 year 1 year 1 year 1 year 3 years

12 Oxygen Bottle Oxygen Cilinder Regulator Passenger Oxygen Control Valve Oring Engine Fire Extinguisher LH Engine Fire Extinguisher RH Engine Fire Extinguisher LH Cartridge Engine Fire Extinguisher RH Cartridge Engine Fire Extinguisher LH Engine Fire Extinguisher LH Emergency Exit Placards Door Handle Cover Emergency Exit Placards Door Handle Bleed Air Assembly Auxiliary Fuel Tank Fuselage Fuel Tank Drive Motor - Overhaul Main Landing Gear Retraction Cylinder LH Main Landing Gear Retraction Cylinder RH Nose Landing Gear Retraction Cylinder Main Landing gear Fitting Assembly Mid Fuselage Main Landing Gear Uplock Fitting Emergency Main Landing Gear Door Open Cable LH Emergency Main Landing Gear Door Open Cable RH Engine Carry Through Bracket (aft) Engine Carry Through Bracket (16ea) Pitch Trim Actuator Ribs Main Landing Gear Support Fitting Aft Fuselage Baggage Compartment, Velcro Aft Fuselage Baggage Compartment, Velcro Spark Igniters - Cleanliness, Erosion and operational test (LH/RH) Minor Inspection (LH/RH) Fuel Pump Outlet Filter (10 Micron) (LH/RH) Oil Filter Element (LH/RH) Hot Section Inspection (HSI) (LH/RH) Engine Overhaul (LH/RH) 5 years 6 years 4 years 4 years 4 years 4 years 4 years 5 years 5 years 5 years 5 years 440 hours 3000 hours 1400 hours / 1400 landings 1400 hours / 1400 landings 1400 hours / 1400 landings 7000 landings 7000 landings 200 hours 5000 hours 1800 hours 7400 hours 400 hours 2600 hours 200 hours 200 hours 200 hours 800 hours / 1 year 1800 hours 3600 hours Landing Gear Overhaul which is actually termed as a teardown/inspect/repair is due 7,400 hours or 5,000 landings whichever occurs first. (This was just accomplished on this aircraft less than 100 hours/landings ago). Installed engines are Pratt & Whitney JT15D-5 s Serial Numbers PCE LH and PCE which are 3,600 hours TBO and 1,800 hours SHS both engines are original, sequential and have matched times and were overhauled by the P&W factory in USA. Thank You and Welcome Aboard! East Greenway Road, Suite 201, Scottsdale, Arizona USA / Office 01- (480)