AIRCRAFT STATUS REPORT

Transcription

1 SCHEDULED INSPECTIONS Phase A1 -A6 Airframe Inspection 300 HRS. 7,520 HRS. 0 HRS. 7,820 HRS. 264 HRS. 12 MOS 4/25/ MOS 4/26/2009 DATE 32.3 MOS Phase B1-B6 Airframe Inspection 600 HRS. 7,466 HRS. 0 HRS. 8,066 HRS. 510 HRS. *** 24 MOS 4/25/ MOS 4/26/2010 DATE 20.3 MOS PhaseC1-C6 Airframe Inspection 1,200 HRS. 7,337 HRS. 0 HRS. 8,537 HRS. 981 HRS. *** 48 MOS 4/25/ MOS 4/25/2012 DATE 3.7 MOS Phase D1-D6 Airframe Inspection 2,400 HRS. 7,325 HRS. 0 HRS. 9,725 HRS HRS. 96 MOS 6/7/ MOS 6/6/2010 DATE 19.0 MOS 3000 Landing Inspection 3,000 LND 5,904 LND 0 LND 8,904 LND 1444 LND *** Major Landing Gear Inspection 6,000 LND 5,904 LND 0 LND 11,904 LND 4444 LND 12 Year Airframe Inspection 6,000 LND 7,387 LND 0 LND 13,387 LND 5927 LND 144 MOS 1/21/ MOS 1/19/2018 DATE 72.6 MOS Hour Airframe Inspection 12,000 HRS. 0 HRS. 0 HRS. 12,000 HRS HRS. LH Engine Hot Section Inspection 1,000 HRS. 4,197 HRS. 0 HRS. 5,197 HRS. 345 HRS. LH Engine Corrosion Inspection 60 MOS 9/11/ MOS 9/10/2012 DATE 8.2 MOS LH Engine Overhaul 5,000 HRS. 0 HRS. 0 HRS. 5,000 HRS. 148 HRS. RH Engine Hot Section Inspection 1,000 HRS. 4,197 HRS. 0 HRS. 5,197 HRS. 448 HRS. RH Engine Corrosion Inspection 60 MOS 9/11/ MOS 9/10/2012 DATE 8.2 MOS RH Engine Overhaul 5,000 HRS. 0 HRS. 0 HRS. 5,000 HRS. 251 HRS. DRAG CHUTE INSP/FT N/A NOT INSTALLED 6 MOS 0 MOS 7/1/1900 DATE MOS 300 Hour Thrust Reverser Inspection 300 HRS. 7,325 HRS. 0 HRS. 7,625 HRS. 69 HRS. * C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 1 of 16

2 600 Hour Thrust Reverser Inspection 600 HRS. 7,545 HRS. 0 HRS. 8,145 HRS. 589 HRS. 300 Hour Engine Inspection, LH 300 HRS. 4,757 HRS. 0 HRS. 5,057 HRS. 205 HRS. 600 Hour Engine Inspection, LH 600 HRS. 4,757 HRS. 0 HRS. 5,357 HRS. 505 HRS. 300 Hour Engine Inspection, RH 300 HRS. 4,757 HRS. 0 HRS. 5,057 HRS. 308 HRS. 600 Hour Engine Inspection, RH 600 HRS. 4,757 HRS. 0 HRS. 5,357 HRS. 608 HRS. Lt. Fwd. & Aft. Engine Mount Isolators Insp. Rt. Fwd. & Aft. Engine Mount Isolators Insp. Lt. Engine Mount yokes. Rt. Engine Mount Yokes. During Major Engine Inspection During Major Engine Inspection During Major Engine Inspection During Major Engine Inspection Engine Yoke Assembly ,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Engine Pad Assembly ,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Engine Mounting Bolts - Forward 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Engine Mounting Bolts - Lower Rear 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Engine Mounting Bolts - Upper Rear 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Engine Mount LM-308 Top At Overhaul Engine Mount LM-308 Forward At Overhaul Engine Mount LM-308 Inboard At Overhaul Engine Oil Vent Hose At each Hot Section Engine Oil Pressure Hose At each Hot Section 12 Month RVSM Insp N/A NON RVSM AIRCRAFT 12 MOS MOS 0 MOS 12/31/1900 DATE MOS 24 Month RVSM Insp N/A NON RVSM AIRCRAFT 24 MOS MOS 0 MOS 12/31/1901 DATE MOS Left Altimeter 24 MOS 1/9/2007 MOS 0 MOS 1/9/2009 DATE 35.8 MOS *** Right Altimeter 24 MOS 1/9/2007 MOS 0 MOS 1/9/2009 DATE 35.8 MOS *** S.D.C.M. Cal. 24 MOS 1/9/2007 MOS 0 MOS 1/9/2009 DATE 35.8 MOS *** Left Static System Leak Check 24 MOS 1/9/2007 MOS 0 MOS 1/9/2009 DATE 35.8 MOS *** Right Static System Leak Check 24 MOS 1/9/2007 MOS 0 MOS 1/9/2009 DATE 35.8 MOS *** #1 Transponder 24 MOS 1/9/2007 MOS 0 MOS 1/9/2009 DATE 35.8 MOS *** #2 Transponder 24 MOS 1/9/2007 MOS 0 MOS 1/9/2009 DATE 35.8 MOS *** C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 2 of 16

3 ELT Battery Replacement 24 MOS 3/16/2009 MOS 0 MOS 3/17/2011 DATE 9.6 MOS *** ELT Operational Check (FAR (d)) 12 MOS 3/16/2009 MOS 0 MOS 3/17/2010 DATE 21.6 MOS *** CVR/FDR ULB Operational check 24 MOS 1/21/2006 MOS 0 MOS 1/22/2008 DATE 47.4 MOS *** CVR/FDR ULB Battery Replacement 72 MOS 6/7/2002 MOS 0 MOS 6/6/2008 DATE 43.0 MOS *** Lead Acid Battery Hyd Ck 100 HRS. 7,520 HRS. 0 HRS. 7,620 HRS. 64 HRS. * Lead Acid Main Batteries - Cap. Chk & Top Charge 12 MOS 3/16/2009 MOS 0 MOS 3/17/2010 DATE 21.6 MOS *** Battery Cables and Receptacles Inspection 12 MOS 3/16/2009 MOS 0 MOS 3/17/2010 DATE 21.6 MOS *** Battery Installation Inspection 6 MOS 3/16/2009 MOS 0 MOS 9/15/2009 DATE 27.6 MOS *** #1 Ni-Cad Emer. Power Supply (PS-823) Inspection 100 HRS. 7,520 HRS. 0 HRS. 7,620 HRS. 64 HRS. * #1 Ni-Cad Emer. Power Supply (PS-823) Inspection 3 MOS 3/16/2009 MOS 0 MOS 6/16/2009 DATE 30.6 MOS *** #1 Ni-Cad Emer. Power Supply (PS-823) Discharge Check 12 MOS 3/16/2009 MOS 0 MOS 3/17/2010 DATE 21.6 MOS *** #2 Ni-Cad Emer. Power Supply (PS-823) Inspection NOT INSTALLED 100 HRS. HRS. 0 HRS. HRS. HRS. #2 Ni-Cad Emer. Power Supply (PS-823) Inspection NOT INSTALLED 3 MOS MOS 0 MOS DATE MOS #2 Ni-Cad Emer. Power Supply (PS-823) Discharge Check NOT INSTALLED 12 MOS MOS 0 MOS DATE MOS Emer. Power Supply Ops. Chk. (PS PS-855) Emer. Power Supply Discharge Chk. (PS PS855) N/A This Aircraft N/A This Aircraft Interior Emer Light Power Supply Cap Ck NOT INSTALLED 6 MOS MOS 0 MOS 7/1/1900 DATE MOS Emer. Exit, Wing Light Power Supply Deep Cycle NOT INSTALLED 6 MOS MOS 0 MOS 7/1/1900 DATE MOS Emer. Power Supply - GNS Deep Cycle System Removed Accelerometer Ops. Check (AD R2) 220 HRS. 7,446 HRS. 0 HRS. 7,666 HRS. 110 HRS. Right Essential Bus Circuit Breakers N/A THIS AIRCRAFT 144 MOS MOS 0 MOS DATE MOS Right Essential Bus Circuit Breakers N/A THIS AIRCRAFT 6,000 LND LND 0 LND LND LND Left Essential Bus Circuit Breakers N/A THIS AIRCRAFT 144 MOS MOS 0 MOS DATE MOS Left Essential Bus Circuit Breakers N/A THIS AIRCRAFT 6,000 LND LND 0 LND LND LND C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 3 of 16

4 Main Bus Tie Circuit Breaker 144 MOS 1/21/2006 MOS 0 MOS 1/19/2018 DATE 72.6 MOS Main Bus Tie Circuit Breaker 6,000 LND 7,446 LND 0 LND 13,446 LND 5986 LND Yaw Servo Commutator Inspection NA By PN 1,800 HRS. Yaw Servo Bearing Replacement NA By PN 1,800 HRS. Yaw Servo 600 hour inspection NA By PN 600 HRS. Pitch Servo Commutator Inspection NA By PN 1,800 HRS. Pitch Servo Bearing Inspection NA By PN 1,800 HRS. Pitch Servo 600 Hour Inspection NA By PN 600 HRS. Roll Servo Commutator Inspection Roll Servo Bearing Inspection Roll Servo 600 Hour Inspection NA By PN NA By PN NA By PN Nose Wheel Steering Servo 1800 Hr Inspection 1,800 HRS. 7,027 HRS. 0 HRS. 8,827 HRS HRS. Nose wheel Steering Servo 600 Hour Inspection 600 HRS. 7,027 HRS. 0 HRS. 7,627 HRS. 71 HRS. * Nose Wheel Steering Actuator P/N Inspection 2,000 HRS. 6,638 HRS. 0 HRS. 8,638 HRS HRS. Horizontal Stab Actuator 600 Hour Inspection 600 HRS. 7,027 HRS. 0 HRS. 7,627 HRS. 71 HRS. * Life Vests Inspection NOT INSTALLED 60 MOS MOS 0 MOS 12/30/1904 DATE MOS Pilot's Eros Oxygen Mask Overhaul N/A THIS AIRCRAFT MOS MOS 0 MOS 1/1/1900 DATE MOS Copilot's Eros Oxygen Mask Overhaul N/A THIS AIRCRAFT MOS MOS 0 MOS 1/1/1900 DATE MOS Oxygen Bottle Hydro. Test DOT 3AA MOS 1/21/2006 MOS 0 MOS 1/21/2011 DATE 11.4 MOS *** Emergency Air Bottle (P/N ) Visual Insp. & Hydro. Test 36 MOS 6/2/2006 MOS 0 MOS 6/2/2009 DATE 31.1 MOS *** Emergency Air Bottle (P/N ) X-Ray & Hydro. Test 108 MOS 6/2/2006 MOS 0 MOS 6/1/2015 DATE 40.9 MOS Emergency Air Bottle (P/N ) X-Ray & Hydro. Test 144 MOS 1/21/2006 MOS 0 MOS 1/19/2018 DATE 72.6 MOS Emergency Air Bottle (P/N ) Replacement 180 MOS 7/1/1995 MOS 0 MOS 6/28/2010 DATE 18.2 MOS *** Emergency Air Bottle (P/N ) Visual Inspection & Hydro. Test N/A This Aircraft MOS 0 MOS DATE MOS C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 4 of 16

5 Emergency Air Bottle (P/N ) X-Ray N/A This Aircraft MOS 0 MOS DATE MOS Emergency Air Bottle (P/N ) X-Ray N/A This Aircraft MOS 0 MOS DATE MOS Emergency Air Bottle (P/N ) X-Ray N/A This Aircraft MOS 0 MOS DATE MOS Emergency Air Bottle (P/N ) Replacement N/A This Aircraft MOS 0 MOS DATE MOS Cockpit Fire Ext. Insp. 12 MOS 3/16/2009 MOS 0 MOS 3/17/2010 DATE 21.6 MOS *** Cabin Fire Ext. Insp. 12 MOS 3/16/2009 MOS 0 MOS 3/17/2010 DATE 21.6 MOS Hydro Test Cockpit Fire Ext. 144 MOS 1/30/2004 MOS 0 MOS 1/28/2016 DATE 48.8 MOS Hydro Test Cabin Fire Ext. NOT INSTALLED 144 MOS MOS 0 MOS 12/29/1911 DATE MOS Lt. Engine Fire Extinguisher Inspection 6 MOS 3/16/2009 MOS 0 MOS 9/15/2009 DATE 27.6 MOS *** Rt. Engine Fire Extinguisher Inspection 6 MOS 3/16/2009 MOS 0 MOS 9/15/2009 DATE 27.6 MOS *** Lt. Engine Fire Extinguisher Weight Check 12 MOS 3/16/2009 MOS 0 MOS 3/17/2010 DATE 21.6 MOS *** Rt. Engine Fire Extinguisher Weight Check 12 MOS 3/16/2009 MOS 0 MOS 3/17/2010 DATE 21.6 MOS *** Left Engine Fire Extinguisher Hydro Test 60 MOS 3/16/2009 MOS 0 MOS 3/16/2014 DATE 26.4 MOS Right Engine Fire Extinguisher Hydro Test 60 MOS 3/16/2009 MOS 0 MOS 3/16/2014 DATE 26.4 MOS Lt. Engine Fwd. Fire Extinguisher Catridge HTL 72 MOS 6/7/2002 MOS 0 MOS 6/6/2008 DATE 43.0 MOS *** Lt. Engine Aft Fire Extinguisher Catridge HTL 72 MOS 6/7/2002 MOS 0 MOS 6/6/2008 DATE 43.0 MOS *** Rt. Engine Fwd. Fire Extinguisher Catridge HTL 72 MOS 6/7/2002 MOS 0 MOS 6/6/2008 DATE 43.0 MOS *** Rt. Engine Aft Fire Extinguisher Catridge HTL 72 MOS 6/7/2002 MOS 0 MOS 6/6/2008 DATE 43.0 MOS *** Lower Cabin Structure & Hinge Inspection 24 MOS 3/16/ MOS 3/17/2011 DATE 9.6 MOS *** Sheet Metal Track Attach Fitting Inspection NA by SN Keel Beam Attach Bolts 144 MOS 6/7/ MOS 6/5/2014 DATE 29.0 MOS Keel Beam Attach Bolts 6,000 LND 7,325 LND 0 LND 13,325 LND 5769 LND Tip Tank Inspection 24 MOS 3/16/ MOS 3/17/2011 DATE 9.6 MOS *** Wing Tip Tank Flapper Valves 600 HRS 7,446 HRS 0 HRS 8046 HRS HRS WS 72- IB Spar 5 Wing Flapper Valves 24 MOS 3/16/ MOS 3/17/2011 DATE 9.6 MOS *** Inboard Dry Bay Inspection 24 MOS 3/16/ MOS 3/17/2011 DATE 9.6 MOS *** C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 5 of 16

6 Windshield Inspection 600 Hours After Repl. only Upper Door Handle Shaft Bolt (36" Door Only) N/A By A/C S/N Cabin Pressurization Leak Rate Test 1,200 HRS. 7,314 HRS. 0 HRS. 8,514 HRS. 958 HRS. Air Cond. Compressor Motor Brush Wear Insp. N/A - No Hour Meter Primary Aileron Contol Cables 2,400 HRS. 5,855 HRS. 0 HRS. 8,255 HRS. 699 HRS. Aileron Drive Yoke Bolts and Nuts 3,600 HRS. 5,855 HRS. 0 HRS. 9,455 HRS HRS. Aileron Center Hinge Bolts 3,600 HRS. 7,325 HRS. 0 HRS. 10,925 HRS HRS. Aileron Assembly 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Aileron Clevis Bolts 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Aileron Pulley Assemblies 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Aileron Clevis 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Aileron Yoke Assemblies 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Aileron Bearing Support Assemblies 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Aileron Hinge Bracket Assemblies 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Elevator Control System Primary Cables 2,400 HRS. 5,855 HRS. 0 HRS. 8,255 HRS. 699 HRS. Elevator Installation 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Flap Nose Roller Bushings 1,200 HRS. 7,027 HRS. 0 HRS. 8,227 HRS. 671 HRS. Outboard Flap Track Support 11,900 HRS. 0 HRS. 0 HRS. 11,900 HRS HRS. Flap Assemblies 19,300 HRS. 0 HRS. 0 HRS. 19,300 HRS HRS. Inboard Flap Hinge Fitting 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Outboard Flap Hinge Fitting 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Inboard and Outboard Flap Track Assembly 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Wing flap Sector Mount Bolts 144 MOS 1/21/2006 MOS 0 MOS 1/19/2018 DATE 72.6 MOS Wing flap Sector Mount Bolts 6,000 LND 7,446 LND 0 LND 13,446 LND 5890 LND Flap Cam Follower Bearing Inspection 1,200 HRS. 7,325 HRS. 0 HRS. 8,525 HRS. 969 HRS. Inboard Flap Nose Roller Tracks 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Outboard Flap Nose Roller Tracks 20,000 HRS. 0 HRS. 0 HRS. 20,000 HRS HRS. Flap Track Support Fittings 1,200 HRS. 7,325 HRS. 0 HRS. 8,525 HRS. 969 HRS. C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 6 of 16

7 Horizontal Stabilizer Hinge Brackets 20,000 HRS. HRS. 0 HRS. 20,000 HRS HRS. Horizontal Stabilizer Hinge Pin 20,000 HRS. HRS. 0 HRS. 20,000 HRS HRS. Horizontal Stabilizer Actuator Attach Bolts 144 MOS 1/21/2006 MOS 0 MOS 1/19/2018 DATE 72.6 MOS Horizontal Stabilizer Actuator Attach Bolts 6,000 LND 7,446 LND 0 LND 13,446 LND 5986 LND Rudder Control System Primary Cables 2,400 HRS. 5,855 HRS. 0 HRS. 8,255 HRS. 699 HRS. Rudder Installation 20,000 HRS. HRS. 0 HRS. 20,000 HRS HRS. Spoiler Actuator Bolts & Hardware (See Maint. Man.) NA BY AC SN Landing Gear Hydraulic Hoses 1,500 HRS. 7,337 HRS. 0 HRS. 8,837 HRS HRS. Landing Gear Hydraulic Hoses 60 MOS 6/3/2004 MOS 0 MOS 6/3/2009 DATE 31.1 MOS *** Lt. Engine Nacelle Fuel Hoses 2,400 HRS. 7,337 HRS. 0 HRS. 9,737 HRS HRS. Lt. Engine Nacelle Fuel Hoses 60 MOS 6/3/2004 MOS 0 MOS 6/3/2009 DATE 31.1 MOS *** Rt. Engine Nacelle Fuel Hoses 2,400 HRS. 7,337 HRS. 0 HRS. 9,737 HRS HRS. Rt. Engine Nacelle Fuel Hoses 60 MOS 6/3/2004 MOS 0 MOS 6/3/2009 DATE 31.1 MOS *** Lt. Engine Nacelle Hydraulic Hoses 2,400 HRS. 7,337 HRS. 0 HRS. 9,737 HRS HRS. Lt. Engine Nacelle Hydraulic Hoses 60 MOS 6/3/2004 MOS 0 MOS 6/3/2009 DATE 31.1 MOS *** Rt. Engine Nacelle Hydraulic Hoses 2,400 HRS. 7,337 HRS. 0 HRS. 9,737 HRS HRS. Rt. Engine Nacelle Hydraulic Hoses 60 MOS 6/3/2004 MOS 0 MOS 6/3/2009 DATE 31.1 MOS *** Airframe Pressure Fuel Hoses 144 MOS 1/21/2006 MOS 0 MOS 1/19/2018 DATE 72.6 MOS Airframe Pressure Fuel Hoses 6,000 LND 7,387 LND 0 LND 13,387 LND 5927 LND Hydraulic System Hoses (except Landing Gear & Teflon) 144 MOS 6/3/2004 MOS 0 MOS 6/1/2016 DATE 52.9 MOS Hydraulic System Hoses (except Landing Gear & Teflon) 6,000 LND 7,287 LND 0 LND 13,287 LND 5827 LND Emergency Air Hoses 144 MOS 1/21/2006 MOS 0 MOS 1/19/2018 DATE 72.6 MOS Emergency Air Hoses 6,000 LND 7,387 LND 0 LND 13,387 LND 5927 LND Left Hydraulic Brake Hoses 60 MOS 6/3/2004 MOS 0 MOS 6/3/2009 DATE 31.1 MOS *** C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 7 of 16

8 Left Hydraulic Brake Hoses 2,400 HRS. 7,337 HRS. 0 HRS. 9,737 HRS HRS. Right Hydraulic Brake Hoses 60 MOS 6/3/2004 MOS 0 MOS 6/3/2009 DATE 31.1 MOS Right Hydraulic Brake Hoses 2,400 HRS. 7,337 HRS. 0 HRS. 9,737 HRS HRS. *** Left Main Gear Strut P/N ,000 LND 0 LND 0 LND 12,000 LND 4540 LND Right Main Gear Strut P/N ,000 LND 0 LND 0 LND 12,000 LND 4540 LND Main Gear Actuator Attach Pins (P/N ) 12,000 LND 0 LND 0 LND 12,000 LND 4540 LND Main Gear Actuator Pillar Assemblies P/N & 14 18,000 LND 0 LND 0 LND 18,000 LND LND Nose Gear Strut 20,000 LND 0 LND 0 LND 20,000 LND LND Nose Gear Actuator 20,000 LND 0 LND 0 LND 20,000 LND LND Main Gear Attach Pins P/N ,000 LND 0 LND 0 LND 20,000 LND LND Main Gear Actuator Pillar Assemblies P/N ,000 LND 0 LND 0 LND 20,000 LND LND Main Gear Actuators P/N ,000 LND 0 LND 0 LND 20,000 LND LND AD Battery Change or Modification N/A by Battery Type AD R2 Spoiler Actuator Attach Bolts N/A by SB LH Wing--7/18/1972 RH Wing--7/24/1972 AD R3 Ni-Cad Battery N/A Lead Acid Batteries Installed AD R2 Lavatory Recepticles N/A Not Installed in A/C AD Landing Gear Struts PCW by SB /25/1976 1,720 HRS AD Inverter Input Power N/A by A/C S/N AD R1 Cabin door locking mechanism C/W by Installation of AMK /1/1980 3,694 HRS AD Refrigeration Cooling fan N/A by Fan P/N AD R1 Stall Warning Systems N/A by Wing Mod. AD Lithium Batteries N/A Not Installed in A/C AD SEAT BELTS N/A by Seatbelt Installed AD Cabin Main Entrance Upper Door C/W by Installation of AMK /1/ HRS AD Superceded by AD AD Superceded by AD AD EMEGENCY POWER SUPPLY N/A by M/N AD Jet Pump C/W by installation of Amk /3/ HRS AD R1 Flammable leakage in Tailcone C/W by Flight Manual Supplement 12/13/1980 AD INST OF PITCH TRIM MONITOR C/W by Installation of AMK 80-16B 11/25/1980 AD FC-110AFCS C/W by installation of AMK 80-16B 11/25/1980 C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 8 of 16

9 AD Fuel Quantity limitation C/W by Flight Manual Supplement 11/18/1985 4,760 HRS AD R3 Operational Limitations N/A by A/C S/N AD R2 Stall Warning system C/W by Operational Insp. Last Done 7446 HRS Next Due 7,666 HRS AD JET Emergency Power Supply N/A by M/N AD SWITLIK LIFE VESTS N/A Life Vests Not Installed AD Goodrich Tires N/A by Tire P/N & S/N 1/4/1984 AD Aileron Trim Tab C/W by installation of AMK 83-3 AD FLAP SYMMETRY OPS Superceded by AD /30/1990 5,451 HRS AD FUEL LEAKAGE INTO BATTERY C/W by SB /13/1985 AD COLLINS AVIONICS N/A by P/N Installed AD Scott Aviation O2 Fittings N/A by P/N Installed 12/27/1994 6,013 HRS AD R1 fuel Leakage into Battery PCW by SB 334A 9/19/1987 AD R1 Flap Operation PCW Steel Brackets Installed 4/24/1988 AD COLLINS AVIONICS N/A by M/N AD COLLINS AVIONICS N/A bym/n AD MECHANICAL PRODUCTS C/B C/W by Inspection 9/1/1995 6,110 HRS AD Failure of Drag Chute N/A Drag Chute Not Installed AD Circuit Breakers C/W by Inspection 9/1/1995 6,110 HRS AD Crew O2 Plumbing PCW by Installation of AMK /27/1993 5,855 HRS AD Pacific Scientific Company N/A effected parts not installed 12/27/1994 5,855 HRS AD Superceded by AD AD Prevent Rapid Decompression N/A by A/C S/N AD Imbalance of Fuel Loads (Par. A) Superceded by AD /7/2002 AD Imbalance of Fuel Loads (Par. B) Superceded by AD /7/2002 AD Imbalance of Fuel Loads (Par. B) Superceded by AD /7/2002 AD Puritan Bennett O2 Mask N/A Not Installed in A/C 3/2/1998 6,783 HRS AD Puritan Bennett O2 Mask N/A by P/N Installed in AC 3/2/1998 6,783 HRS AD SEAT RESTRAINTS N/A by Manufactured AD Puritan Bennett 02 Masks N/A Not Installed in A/C 12/6/1999 AD Horizontal Stab Heat Wiring C/W IAW SB 23/24/ /7/2002 7,325 HRS C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 9 of 16

10 AD MLG Tire Tread Separation N/A by S/N 8/8/2001 AD Insp for Kidde Port Halon Fire Ext. N/A Not Installed in A/C AD INSP/REPLACEMENT OF AILERON CABLES N/A per cables installed 1/21/2006 7,446 HRS AD INSP/REPLACE TIP TANK FLAPPER VALVES SB 23/24/ /21/2006 7,446 HRS AD MAIN HYD SYS ACCUMULATOR Installed Kit # /21/2006 7,446 HRS AD THRUST REVERSER ACCUMUALATOR C/W by deativation of TR's 1/21/2006 7,446 HRS ENGINE AIRWORTHINESS DIRECTIVES TITLE AD ACCESSORY DRIVE SHAFT FAILURE AD COMP. DISK FATIGUE FAILURE AD R1 1/2 STG TURBINE WHEEL REPL. AD STAGE 1 TURB. DISK FAILURE AD TURB. TORQUE RINGS & DR SHAFT AD COMBUSTION LINER CRACKS AD UNAPPROVED PARTS AD UNAPPROVED PARTS ENGINE LIFE LIMITED COMPONENTS LH ENGINE CJ SN A P/N S/N DISK AND SHAFT STAGE 1 COMPRESSOR 7,000 CYC 4,499 CYC 4,499 CYC 7,000 CYC CYC DISC, STAGE 2 COMPRESSOR 7,000 CYC 4,499 CYC 4,499 CYC 7,000 CYC CYC DISC STAGE 3 COMPRESSOR 7,000 CYC 4,499 CYC 4,499 CYC 7,000 CYC CYC DISC STAGE 4 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC DISC STAGE 5 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC DISC STAGE 6 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC DISC STAGE 7 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC DISC STAGE 8 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC AIR SEAL ROTOR STAGE I COMPRESSOR 7,000 CYC 4,499 CYC 4,499 CYC 7,000 CYC CYC C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 10 of 16

11 SPACER STAGE 2 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC SPACER STAGE 3 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC SPACER STAGE 4 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC SPACER STAGE 5 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC SPACER STAGE 6 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC SPACER STAGE 7 COMPRESSOR 6600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC SHAFT REAR COMPRESSOR CYC 4,499 CYC 4,499 CYC 13,200 CYC CYC SEAL ROT STAGE 8 COMP 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC WHEEL STAGE 1 TURBINE 10,000 CYC 4,499 CYC 4,499 CYC 10,000 CYC CYC WHEEL STAGE 2 TURBINE 10,000 CYC 4,499 CYC 4,499 CYC 10,000 CYC CYC TURBINE TORQUE RING 10,000 CYC 4,499 CYC 4,499 CYC 10,000 CYC CYC OUTER SEAL FRONT ROTATING TURBINE 10,000 CYC 4,499 CYC 4,499 CYC 10,000 CYC CYC INNER SEAL FRONT ROTATING TURBINE 10,000 HRS. 4,499 HRS. 4,499 HRS. 10,000 HRS HRS. #1 ROLLER BEARING 5,000 HRS. 5,014 HRS. 0 HRS. 10,014 HRS HRS. #2 ROLLER BEARING 5,000 HRS. 5,014 HRS. 0 HRS. 10,014 HRS HRS. #3 ROLLER BEARING 5,000 HRS. 5,014 HRS. 0 HRS. 10,014 HRS HRS. PTO BEARING ON COND 5,000 HRS. 5,014 HRS. 0 HRS. HRS. HRS. TRANSFER GEARBOX BEARING NOT APPLICABLE TO -8 ACCESSORY GEARBOX BEARING ON COND 5,000 HRS. 5,014 HRS. 0 HRS. HRS. HRS. OVERSPEED GOVERNOR 2,000 HRS. 5,014 HRS. 0 HRS. 7,014 HRS HRS. RH ENGINE SN A CJ610-6 P/N S/N DISK AND SHAFT STAGE 1 COMPRESSOR 7,000 CYC 4,499 CYC 0 CYC 11,499 CYC CYC DISC, STAGE 2 COMPRESSOR 7,000 CYC 4,499 CYC 4,499 CYC 7,000 CYC CYC DISC STAGE 3 COMPRESSOR 7,000 CYC 4,499 CYC 4,499 CYC 7,000 CYC CYC C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 11 of 16

12 DISC STAGE 4 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC DISC STAGE 5 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC DISC STAGE 6 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC DISC STAGE 7 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC DISC STAGE 8 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC AIR SEAL ROTOR STAGE I COMPRESSOR 7,000 CYC 4,499 CYC 4,499 CYC 7,000 CYC CYC SPACER STAGE 2 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC SPACER STAGE 3 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC SPACER STAGE 4 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC SPACER STAGE 5 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC SPACER STAGE 6 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC SPACER STAGE 7 COMPRESSOR 6,600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC SHAFT REAR COMPRESSOR CYC 4,499 CYC 4,499 CYC 13,200 CYC CYC SEAL ROT STAGE 8 COMP 6600 CYC 4,499 CYC 4,499 CYC 6,600 CYC CYC WHEEL STAGE 1 TURBINE 10,000 CYC 4,499 CYC 4,499 CYC 10,000 CYC CYC WHEEL STAGE 2 TURBINE 10,000 CYC 4,499 CYC 4,499 CYC 10,000 CYC CYC TURBINE TORQUE RING 10,000 CYC 4,499 CYC 4,499 CYC 10,000 CYC CYC OUTER SEAL FRONT ROTATING TURBINE 10,000 CYC 4,499 CYC 4,499 CYC 10,000 CYC CYC INNER SEAL FRONT ROTATING TURBINE 10,000 CYC 4,499 CYC 4,499 CYC 10,000 CYC CYC #1 ROLLER BEARING 5,000 HRS. 5,014 HRS. 0 HRS. 10,014 HRS HRS. #2 ROLLER BEARING 5,000 HRS. 5,014 HRS. 0 HRS. 10,014 HRS HRS. #3 ROLLER BEARING 5,000 HRS. 5,014 HRS. 0 HRS. 10,014 HRS HRS. PTO BEARING ON COND 5,000 HRS. 5,014 HRS. 0 HRS. HRS. HRS. TRANSFER GEARBOX BEARING NA 5,000 HRS. HRS. HRS. HRS. HRS. ACCESSORY GEARBOX BEARING ON COND 5,000 HRS. 5,014 HRS. 0 HRS. HRS. HRS. C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 12 of 16

13 OVERSPEED GOVERNOR 2,000 HRS. 5,014 HRS. 0 HRS. 7,014 HRS HRS. N76UM LEAR 25 SN 051 AIRCRAFT MODIFICATION SUMMARY AAK 79-2 INST OF PITOT HEAT IND SYS AAK89-4 SPOILER MODIFICATION AAK 86-2 INSTALLATION OF LANDING GEAR ACTUATOR DOWNLOCK SWITCH CONNECTORS AAK REINFORCEMENT OF LOWER CABIN DOOR JAMB AAK 89-4D INSTALLATION OF DOUBLERS AT FRAME 7 AMK 78-7 REPLACEMENT OF HYD BRAKE RETURN HOSE AMK INSTALLATION OF DIODE INSULATING COVERS AMK RELOCATION OF CABIN AIR DISTRIBUTION ORIFICE AMK REMOVAL OF CHECK VALVE FROM EMERGENCY PRESSURIZATION VALVE AMK UPPER CABIN DOOR BOLT SAFETY WIRE AMK INSTALLATION OF AILERON SCUPPER DRAIN AMK REPLACEMENT OF OXYGEN MASK REGULATOR AMK 80-1 RUDDER PEDAL REWORK AMK 80-5 REPLACE OF REFRIGERANT CONDENSER AMK INSTALLATION OF MOTIVE FLOW VALVE SHROUDS AMK INSTALLATION OF CONTROL WHEEL SWITCH AND PLACARDS AMK INSTALLATION OF AUTOPILOT TRIM TEST SWITCH AMK ADDITION OF WIRE BUNDLE INSULATING SLEEVES AMK LEAD ACID BATTERY VENT MODIFICATION AMK HORIZONTAL STAB TRIM AND AUTOPILOT IMPROVEMENT AMK REPLACEMENT OF STALL WARNING COMPUTER HARNESS AMK ENGINE THROTTLE CABLE BALL CONNECTOR AMK INSTALLATION OF HORIZONTAL STABILIZER HINGE PIN BUSHING RETAINER AMK INSTALLATION OF PITCH TRIM AND AIR IGNITION GUARD AMK REPLACEMENT OF 4 GAUGE ELECTRICAL CABLE AMK INSTALLATION OF AUTO-PILOT PITCH NOSE DOWN LIMITER AMK 82-07INSTALLATION OF FIRE WARNING LIGHT ASSEMBLIES C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 13 of 16

14 AMK REPLACEMENT OF AILERON TRIM TAB BALANCE COUNTER WEIGHT AMK AVIONICS SYSTEM LIGHT DIMMER BOX IMPROVEMENT AMK 85-1 ELECTRICAL SYS IMPROVEMENT AMK INSTALLATION OF LNDG GEAR ACT. DOWNLOCK SWITCH CONNECTER KIT. AMK REPLACEMENT OF UPPER FLAP SECTOR MOUNTING BRACKETS AMK 86-5A TAILCONE ELEC CIRCUIT PROTECTION MODIFICATION SUMMARY N76UM LEAR 25 SN 051 AMK INSTALLATION AND MODIFICATION OF THE SPOILER SYSTEM AMK 90-3B INSTALLATION OF EMER PRESS CONTROL CIRCUIT BREAKERS AMK REPLACEMENT OF THE PARALLELING CONTROL BOX AMK CREW OXYGEN AND PLUMBING AND MAP LIGHT WIRE PROTECTION SB 24/ FUEL IMBALANCE SB REPLACEMENT OF TIP TANK FLAPPER VALVES SB 24/ INSP OF CABIN PRESS OUTFLOW AND SAFETY VALVES SB REPLACEMENT OF HYD RESEVOIR SIGHT GLASS SB INSTALLATION OF CHART HOLDER ON CONTROL WHEEL ESCUTCHEON SB MODIFICATION OF MAIN ENTRANCE DOOR HOOKS SB STABILIZERS-INST OF DOWNSPRING DOOR SB INSTALLATION OF FUSELAGE PUMP BONDING WIRES SB INSP OF TIP TANK FLAPPER VALVES SB 283 P/CP CONTROL TRIM WHEEL ARMING SWITCH WIRING SB 284 REPLACEMENT OF CONDENSER FAN SB 285 SECONDARY YAW SERVO CABLE CLAMP SB 287 INCREASE ENGINE STALL MARGIN AT HIGH ALTITUDE SB 288 INSPECTION OF WING FLAP ACTUATOR SB 289 REPLACEMENT OF YAW DAMPER SERVO SECTOR BOLTS SB 290 INSTALLATION OF AIR COND SYSTEM PLACARD SB 291 INSPECTION OF AFT CABIN HONEYCOMB PANELS SB 292 MOD OF ACCESS DOOR LOCK ASSEMBLIES C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 14 of 16

15 SB 293 REWORK P/CP TRIM WHEEL SOCKETS SB 294 ADJUSTMENT AND TESTING OF STALL WARNING SYSTEM SB 295 INSP OF AILERON DRAIN HOLES SB 296 OP CK OF CABIN SAFETY VALVE SB 299 INSPECTION OF ENGINE AFT BEAM PYLON BOLTS SB 301 STALL WARN ACCEL. OPS CHECK SB 302 MOTIVE FLOW VALVE FIELD REPAIR SB 303 BATTERY VENT OBSTRUCTION SB 304 INSP. OF AIR DISTRIBUTION SLEEVES/CLAMPS IN TAILCONE SB 306 INSP OF CABIN OUTFLOW AND SAFETY VALVE SB 307 INSP OF DRAG CHUTE MACH. BOLT SB 308 INSPECTION OF DIODE SB 309 STARTER GENERATOR BRUSH WEAR SB 310 INSP OF DRAG CHUTE MECH CLEARANCE SB 311 INSP OF HORIXZ STAB HINGE PIN BUSHING MODIFICATION SUMMARY N76UM LEAR 25 SN 051 SB 313 INSPECTION OF LND GEAR AND TORQUE LINK INTERFERENCE SB 314 WASTE DISPOSAL PLACARD SB 316 INSPECTION OF #4 GAUGE WIRE CABLES SB 317 MOD OF AERONETICS RMI SB 319 APPLICATION OF FIRE PROOF PAINT SB 320 INSPECTION OF STATIC PORTS SB 321 STICK PULLER FUNCTIONAL CHECK SB 322 MOD OF AERONETICS RMI SB 323 REPLACEMENT OF STARTER GENERATORS SB 324 INSTALLATION OF CREW SEAT BELT SHOULDER HARNESS PLACARD SB327 INSP OF RUDDER PEDAL SUPPORT WELDS SB 330 INSP OF FLAP SECTOR MOUNT BRACKETS SB 333 INSP OF FLAP ATTACH FITTINGS SB 334 RELOCATION OF BATTERY VENT C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 15 of 16

16 SB 335 INSP BAGGAGE COMP STRUCTURE FOR CORROSION SB 336 SB 338 REMOVAL OF DRAG CHUTE LATCH SAFETY WIRE SB 339 INSTALLATION OF PLACARD NEXT TO BATTERY SWITCH SB 340 LNDG GEAR HYD SLE. VALVE REPLACEMENT NA SB 342 INSPECTION OF DRAG CHUTE RISER SB 343 INSP OF WIRE BUNDLES AND AILERON CABLES SB 344 INSP OF MOTIVE FLOW SHROUD VALVES SB 345 ADDITION OF ENG FIRE EXT WIRING ID SSK 922 REPLACEMENT OF NACELLE ANTI ICE HEATING ELEMENT SSK 960 REPLACEMENT OF ELEVATOR UP/DOWN SPRING DRAW BOLT SSK 993 REPLACEMENT OF LANDING GEAR WHEEL BEARINGS STC SA 1482SO WINDSHIELD DEFOGGER STC SA 1670SW KIT 369 DEE HOWARD THRUST REVERSER STC SA944NW KIT XR MOD STC SA8930SW BIZJET NACELLE HEAT BLANKETS STC ST09568SC R134A CONVERSION OF AC SYSTEM C:\Documents and Settings\Research41\Desktop\rework\Copy of N76UM SN 51 STATUS(1) 16 of 16