1995 Beechjet 400A

SERIAL NUMBER: RK-104 REGISTRATION: N401ML TOTAL TIME AIRFRAME: 6,520 Hours Since New TOTAL CYCLES: 5,064 Landings Since New

ENGINES: Model: Pratt & Whitney JT-15D-5 Left Engine S/N: PCE-10038 Right Engine S/N: PCE-10037 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.

W W W . G L O B A J E T P A R T N E R S . C O M 7905 East Greenway Road, Suite 201, Scottsdale, Arizona 85260-USA / Office 01- (480) 703-6698

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 2006. 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

and spar web inspections were all accomplished 11/2012 @ 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 4/2014 @ 6,433 AFTT/4,997 landings accomplished 7,400 Hr/5,000 Ldg. landing gear tear-down/inspection/NDT/overhaul. Last D check accomplished 7/2006 @ 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.

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 200 hours

Inspection B 400 hours

Inspection C 1200 hours

Inspection D 2400 hours

Lubrication Inspection A 200 hours

Lubrication Inspection B 400 hours

Lubrication Inspection C 1200 hours

Lubrication Inspection D 2400 hours

Autopilot Servos 6500 hours /48 months

Emergency Light power Supply 3 months

Drive Belt / Pulley 500 hours

Compressor / Shaft Seal 500 hours

Condenser Fan 500 hours

Condenser Coil 500 hours

Electrical Wiring 500 hours

Drive Motor / Brushes 500 hours

Receiver Dryer Assembly 500 hours

Belt Cover 500 hours

Lead Acid Battery 200 hours / 3 months

Starter Generator LH 1000 hours

Starter Generator RH 1000 hours

Power Break Valve Filters (clean) 1000 hours

Drive Belt / Pulley 1000 hours

Compressor / Shaft Seal 1000 hours

Drive Motor / Brushes 1000 hours

Main Battery 1200 hours / 24 months

ELT 1 year

Standby Power Supply Battery Capacity Test 1 year

AHRS Standby Power Supply Battery Discharge Check 1 year

Cockpit Portable Fire Extinguisher 1 year

Cabin Portable Fire Extinguisher 1 year

Recertification Transponder I / II 2 years

Recertification Standby Altimeter 2 years

Recertification Air Data Computer 2 years

Pilot Static System 2 years

Mach Overspeed Warning System 2 years

Fuel Quantity Indicators 2 years

CVR Underwater Locator Beacon 2 years

Air Data System / Skin Waviness 2 years

Pneumatic Storage Bottle 3 years

Oxygen Bottle 5 years

Oxygen Cilinder Regulator 6 years

Passenger Oxygen Control Valve Oring 4 years

Engine Fire Extinguisher LH 4 years

Engine Fire Extinguisher RH 4 years

Engine Fire Extinguisher LH Cartridge 4 years

Engine Fire Extinguisher RH Cartridge 4 years

Engine Fire Extinguisher LH 5 years

Engine Fire Extinguisher LH 5 years

Emergency Exit Placards Door Handle Cover 5 years

Emergency Exit Placards Door Handle 5 years

Bleed Air Assembly 440 hours

Auxiliary Fuel Tank 2400 hours

Fuselage Fuel Tank 2400 hours

Drive Motor - Overhaul 3000 hours

Main Landing Gear Retraction Cylinder LH 1400 hours / 1400 landings

Main Landing Gear Retraction Cylinder RH 1400 hours / 1400 landings

Nose Landing Gear Retraction Cylinder 1400 hours / 1400 landings

Main Landing gear Fitting Assembly 7000 landings

Mid Fuselage Main Landing Gear Uplock Fitting 7000 landings

Emergency Main Landing Gear Door Open Cable LH 2400 hours

Emergency Main Landing Gear Door Open Cable RH 2400 hours

Engine Carry Through Bracket (aft) 200 hours

Engine Carry Through Bracket (16ea) 5000 hours

Pitch Trim Actuator 1800 hours

Ribs 7400 hours

Main Landing Gear Support Fitting 2400 hours

Aft Fuselage Baggage Compartment, Velcro 400 hours

Aft Fuselage Baggage Compartment, Velcro 2600 hours

Spark Igniters - Cleanliness, Erosion and operational test (LH/RH) 200 hours

Minor Inspection (LH/RH) 200 hours

Fuel Pump Outlet Filter (10 Micron) (LH/RH) 200 hours

Oil Filter Element (LH/RH) 800 hours / 1 year

Hot Section Inspection (HSI) (LH/RH) 1800 hours

Engine Overhaul (LH/RH) 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-100387 LH and PCE-100387 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!

W W W . G L O B A J E T P A R T N E R S . C O M 7905 East Greenway Road, Suite 201, Scottsdale, Arizona 85260 -USA / Office 01- (480) 703-6698