N429MC

Part: ACTUATOR — FAILED (ZONE 700) · airframe 122,091 hrs · 18,821 cycles

GEAR TILT CAUTION AND STATUS MSG'S FOR LH BODY GEAR PRIMARY AND ALT PROX SWITCH TARGET FAIL. FOUND FAILED TILT ACTUATOR. REPLACING ACTUATOR, HYDRAULIC FUSE, AND LINE TO ACTUATOR. LEAK & OPS CHECKS GOOD. NO DEFECTS NOTED IAW AMM 32-13-24,32-31-00, AND 32-13-24.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 121,994 hrs · 18,798 cycles

LEFT INBD BOTTOM ELEVATOR, FOUND DAMAGE DURING WALK AROUND. ACCOMPLISHED TEMPORARY REPAIR OF LT INBD BOTTOM ELEVATOR IAW EA-1955A032, REV 0, PART 1. TRANSFER TO NON-MEL DMI 243280 & 243280.

Part: ELEC CONNECTOR — DISCONNECTED (ZONE 400) · airframe 120,834 hrs · 18,591 cycles

ELEC DRIVE 1 ADVISARY MESSAGE. DRIVE DISCONNECTED IAW QRH. FOUND #1 ENG CONNECTOR D85125 ON FIREWALL DISCONNECT. AW0317 INTERNALLY SHORTED ON 9 WIRES. REMOVED AND REPLACED CONNECTOR D85125 IAW SWPM 20-63-13. REMOVED AND REPLACED CONNECTOR D8417J IAW SWPM 20-63-13. PERFORMED OPS & WIRING CHECKS GOOD IAW WDM 24-11-11 & FIM 24-11 TASK 820. PERFORMED ENGINE RUN AND OPS CHECK GOOD IAW 72-00-00 & 24-11-01.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 120,653 hrs · 18,547 cycles

CORROSION ON LT WING UPPER SKIN UPPER SURFACE NEAR WBL 1217.133. . REPAIRED CORROSION AREA IAW EI NR: T2025A57M-1060 REV 2. COMPLETED JOB AND CONDITION CHECK NORMAL.

Part: REPAIR — DEBONDED (ZONE 600) · airframe 120,653 hrs · 18,547 cycles

RIGHT WING INBD FORE FLAP UPPER INBD PANEL EXISTING REPAIR DOUBLER DISBOND. PERFORM PERMANENT REPAIR - UPGRADE THE EXISTING REPAIR ON TOP PANEL OF RH WING INBD FORE FLAP IAW EGAT EI NR. T2025A57M-1096 REV 1. CONDITION CHECK IS SATISFACTORY.

Part: SPAR — CORRODED (ZONE 600) · airframe 120,653 hrs · 18,547 cycles

CORROSION ON RH WING FRONT SPAR OUTBOARD LOWER CHORD AT FSSO 1509.45. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 62. BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV 62. PERFORMED NDT INSPECTION REFER TO JOB CARD NO: 044869 AND DATA SHEET NO: 11051171-1. 4. PERFORMED EI NO: T2025A57M-991 REV 1. 5. ACCOMPLISHED EI NO: T2025A57M-991 REV 3. 6. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 120,653 hrs · 18,547 cycles

FOUND THE SKIN INSIDE CORROSION AT STA 1700 - 1720, S-42L. REMOVE EXIST SKIN REPAIR DOUBLER IAW SRM 51-10-02-0G-0 REV 62. ACCOMPLISH EI NO: T2025A53M-1083 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: SKIN — DEBONDED (ZONE 500) · airframe 120,653 hrs · 18,547 cycles

SKIN, LOWER SURFACE OF L/H WING INBD AFT FLAP INBD SIDE. PERFORM PERMANENT REPAIR - UPGRADE THE EXISTING REPAIR ON LOWER PANEL OF LT WING INBD AFT FLAP IAW EGAT EI NR: T2025A57M-1065 REV 1. CONDITION CHECK IS SATISFACTORY.

Part: SKIN — DENTED (ZONE 100) · airframe 120,653 hrs · 18,547 cycles

FOUND FUSELAGE LOWER LOBE SKIN DENT AT STA 1925, S-31R ~ S-32R. ACCOMPLISHED EI NR: T2025A53M-996 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: SKIN — DENTED (ZONE 100) · airframe 120,653 hrs · 18,547 cycles

DENT - FOUND FUSELAGE LOWER LOBE SKIN DENT AT STA 1935, S-31R ~ S-32R. ACCOMPLISHED EI NO: T2025A53M-996 REV 1 AND EI ATTACHED TO W/O NO: 11010065(002). JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 120,653 hrs · 18,547 cycles

CORROSION ON R/H WING UPPER SKIN UPPER SURFACE NEAR WBL 1193. BLEND OUT THE CORROSION AREA IAW SRM 51-10-02-0G-0 REV 62. ACCOMPLISHED REPAIR AREA IAW EI NR: T2025A57M-1057 REV 2. COMPLETED JOB AND CONDITION CHECK NORMAL.

Part: ELT — NO TEST (ZONE 200) · airframe 120,653 hrs · 18,547 cycles

FOUND ELT SYSTEM OPERATIONAL TEST FAIL. REPLACED ELT TRANSMITTER IAW AMM 23-24-01-020-801 & AMM 23-24-01-420-801 REV 113. PERFORMED ELT TEST IAW AMM 23-24-01-720-801 & AMM 23-24-01-720-802, & AMM 23-24-01-720-803 REV 113. TEST RESULT WAS SATISFACTORY.

Part: REPAIR — OUT OF DATE (ZONE 100) · airframe 120,653 hrs · 18,547 cycles

UPGRADE THREE TEMPORARY FUSELAGE SKIN DOUBLER REPAIRS BETWEEN STA 1780 AND STA 1840, S-46L AND S-49L. REMOVED TIME LIMITED FUSELAGE SKIN REPAIR, TOTAL 3 AREA IAW SRM 51-40-02-0G-0 REV 62. ACCOMPLISHED EI NR T2025A53M-1055 REV 2. 3. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: BATTERY — FAULTED (ZONE 200) · airframe 120,653 hrs · 18,547 cycles

FOUND CARTRIDGE RESISTANCE OUT OF LIMIT AT L/H, R/H UPPER DECK DOOR WHEN PERFORM BATTERY AND EMERGENCY OPENING OPERATATION. REPLACED L/H & R/H UPPER DECK DOOR EMERGENCY POWER RESERVOIR IAW AMM 52-23-13-004-001 & AMM 52-23-13-404-010 AND AMM 52-23-13-406-045 REV 113. PERFORMED TEST, RESULTS WERE SATISFACTORY. JOB COMPLETED AND CONDITION CHECK NORMAL. (OFF PART: SN ALT183-3646 PN 1270154-4 & SN ALT183-3645 PN 1270156-4)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 120,395 hrs · 18,501 cycles

SEVERAL EMERGENCY LIGHTS INOPERATIVE AT EMERGENCY DOORS.(<P >REMOVED AND REPLACED EMERGENCY BATTERY PACK AT POWER SUPPLY M7030 IAW AMM 33-51-04-902-001-001. OPS CHECK GOOD PER B747AMM 33-51-04-712-006-001.</P>)

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 120,395 hrs · 18,501 cycles

SEVERAL EMERGENCY LIGHTS INOPERATIVE AT EMERGENCY DOORS.(<P >REMOVED AND REPLACED EMERGENCY BATTERY PACK AT PWR SUPPLY M312 IAW AMM 33-51-04-902-001-001. OPS CHECK GOOD PER B747 AMM 33-51-04-712-006-007.</P>)

Part: FLAP — DAMAGED (ZONE 500) · airframe 120,392 hrs · 18,500 cycles

MULTIPLE BIRD STRIKES ON APPROACH. ACCOMPLISHED BIRD STRIKE CONDITION INSPECTION IAW 05-51-14. REMOVED AND REPLACED #16 LE FLAP, #14 LE FLAP IAW AMM 27-81-81 & IPC 27-81-01-01 REV 88 & IPC 27-81-55-10 REV 88. OPS CHECK GOOD. INPECTION ON CORE OF ENGINE #2 & #3 FOUND NO UNSERVICEABLE DEFECTS NOTED IAW AMM 72-00-00 ON STGS 1 & 2 OF HPC. INPECTION ON #3 PACK INLET FOUND NO DAMAGE NOTED AND NO EVIDENCE OF DEBRIS. ACCOMPLISHED PART 1 & 3 OF EA 4457A205 ON LH INBD TE OUTBD CANOE. ACCOMPLISHED PART 1 & 3 OF EA 1957A216 ON LH OUTBD TE MID FLAP. ACCOMPLISHED PART 1 & 3 OF EA 1957A217 ON RH INBD TE FLAP. ACCOMPLISHED PART 1 & 3 EA: 1971A162 REV 0 ON #1 ENG NOSE COWL (R/R NOSE COWL PER EA 1971A162).

Part: TRANSMITTER — FAULTED (FUEL SYSTEM) · airframe 119,413 hrs · 18,351 cycles

EICAS FUEL IMBALANCE. FOLLOWED QRH 12.8 SUSPECT ENG 1 FUEL LEAK. SHUTDOWN ENGINE 1(<P>PERFORMED DVI AND WET MOTORING TO LEAK CHK PER AMM 71-00-00/201. NO LEAK NOTED. REMOVED &AMP; REPLACED #1 FUEL FLOWS TRANSMITTER PER AMM 73-31-01/401 &AMP; AIPC 78-31-01-05. AND LEAK CHK OK PER AMM 71-00-00/501.<SPAN STYLE="WHITE-SPACE: PRE;"> </SPAN></P>)

Part: ACM — ODOR (NR 3) · airframe 118,896 hrs · 18,267 cycles

STARTED ENGINE #3 USING MANUAL START PROCEDURE, CLEARED TO PUSHBACK AND THEN SMELLED SMOKE FOLLOWED BY VISUAL SMOKE. FOLLOWED FIM 21-61 TASK 924, R/R #3 PACK ACM PER AMM 21-51-04/401 AND PERFORMED OPS CHECK PER AMM 21-00-00/201. R/R ENG 3 PRSOV PER AMM 36-11-04/401 AND OPS CHECK COMPLETED PER AMM 71-00-00-705-152-J00.

Part: TIRE — FAILED (NR 5) · airframe 118,259 hrs · 18,152 cycles

#5 TIRE LOST THREAD(<P>R/R #5 MWA PER AMM 32-45-01. VERIFIED TIRE PRESSURE. VERIFIED PN PER IPC 32-45-03-02. PERFORM PART DEPARTING A/C INSPECTION PER AMM 05-51-34, FOUND DAMAGE TO THE OLEO STRUT DOOR, DAMAGE FOUND TO BE WITHIN LIMITS PER SRM 52-80-01-1A-3. TRANSFER TO NON-MEL 216047 DUE DATE 26FEB2026. 2 DENTS IN AFT MAIN LANDING GEAR DOOR SKIN WITHIN LIMITS PER SRM 52-80-01-1A-3. TRANSFER TO NON-MEL 216048 DUE DATE 26FEB2026. C/W AP 28225, NO DEFECTS NOTED.</P>)

Part: TUBE — DAMAGED (NR 1 HYD SYSTEM) · airframe 117,679 hrs · 18,050 cycles

EICAS HYD SYS 1 ON T/O ROTATION SYS 1 HYD FAILED. R & R ALL HYD DAMAGED TUBES ON LT BLG WHEEL WELL PER NRC 60, 61, 62, 66, 67, 68, 69, 70, 71, 103, 137, & 138 OF W/O 131823 FOR CORRECTIVE ACTION. OPS & LEAK CHECK NORMAL PER AMM 20-11-05.

Part: TIRE — BURST (NR 6) · airframe 117,573 hrs · 18,030 cycles

#6 MAIN TIRE DAMAGED (BURST) AT DEPARTURE. ARRIVED IN LAX(<P>R/R #5 AND #6 TIRE ASSY AND COMPLETED CH 5 INSPECTIONS IAW AMM 32-45-01 &AMP; IPC 32-45-03-02. LEAK &AMP; OPS CHK GOOD. NO DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

NO.3 ENG - LH CORE COWL INNER #2 FRAME CHAFING WORN(<P>CHAFING WORN AREA REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 114,008 hrs · 17,374 cycles

AFT CARGO LH STA 1600-1680 WALKWAY PANEL FOUND CORROSION(<P>AFT CARGO LH STA 1660-1680 WALKWAY PANEL CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02, AND CHECKED WITHIN SRM 53-00-53 ADL.1 FIG 101 LIMIT.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

LHW T/E O/B AFT FLAP UPPER SURFACE FOUND WORN (COUNT FROM O/B EDGE 4")(<P>PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 4 FIG 201</P>)

Part: FLOOR PANEL — DENTED (CARGO) · airframe 114,008 hrs · 17,374 cycles

BULK CARGO LH STA 1920-2040 FLOOR PANEL FOUND 3EA LOCATIONS DENT(<P>3EA LOCATION DENT AREA REPAIRED AS PER RI NO. RI-53-60-16251 REV A</P>)

Part: PANEL — CRACKED · airframe 114,008 hrs · 17,374 cycles

FWD CARGO RH STA 480 - STA 569 WALKWAY PANEL CRACKED(<P>CRACK AREA REPAIRED AS PER RI NO : RI-25-52-16233 REV A</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

NO.3 ENG - RH CORE COWL EXTERNAL SURFACE CRACK FOUND JUST BELOW EXHAUST LOUVER(<P>CRACK AREA REPAIRED AS PER SRM 54-41-01-2R-3 REPAIR 3 FIG 201 REV 56 DATE 20 FEB 2023</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

RHW T/E O/B FORE FLAP L/E (COUNT FROM I/B) FOUND DENT(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 114,008 hrs · 17,374 cycles

LH WLG W/W FWD BULKHEAD FOUND CORROSION (NEAR OVERRIDE JETTISON PUMP LOWER BONDING AREA)(<P>LH WLG W/W FWD BULKHEAD FOUND CORROSION (NEAR OVERRIDE JETTISON PUMP LOWER BONDING AREA) CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 AND CHECKED WITHIN SRM 57-10-10 ADL, FIG 101</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

LHW T/E I/B MID FLAP LOWER SURFACE FOUND BULGE UP (COUNT FROM LOWER EDGER 24" AND I/B EDGE 120" )(<P>PERFORMED METAL HOTBOND REPAIR AS PER RI NO: RI-57-50-16245 REV.A</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 114,008 hrs · 17,374 cycles

FWD CARGO STA 990 - 1000 STR 41L - STR 43L BILGE FUSELAGE SKIN SURFACE CORROSION(<P>FWD CARGO STA 990 - 1000 STR 41L - STR 43L BILGE FUSELAGE SKIN SURFACE CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02, AND CHECKED WITHIN SRM 53-00-01 ADL. 1 FIG 101 LIMIT</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

1EA CRACK WAS FOUND ON 1EA FASTENER HOLE AT BS 2231 S16L FRAME ON THE MOST O/B LAYER APPROX 0.040" IN DEPTH AT 3 O'CLOCK POSITION RUNNING FWD ( FRAME FWD INNER CHORD )(<P>CRACK AREA REPAIRED AS PER RI NO : RI-53-60-16252 REV A ( REPAIRED ) WAS TIME-LIMITED CATEGORY C&NBSP;</P>)

Part: BATTERY PACK — NO TEST · airframe 114,008 hrs · 17,374 cycles

EMERGENCY LT POWER SUPPLY M7050 CAPACITY CHECK FAIL(<P>POWER PACK REPLACED AND OPERATION CHECKED NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

LHW T/E I/B AFT FLAP LOWER SURFACE FOUND DELAMINATION (COUNT FROM I/B EDGE 58")(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

LHW #6 VC FLAP BULL NOSE EXT SURFACE FOUND CRACK ( COUNT FROM O/B EDGE 10" AND UPPER EDGE 8" )(<P>CRACK AREA REPAIRED AS PER SRM 57-43-02-2R-2 REPAIR 2 FIG 201</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

EMP - VERT FIN L/E FAIRING 321A FOUND DENT MARK(<P>DENT AREA REPAIRED AS PER RI NO : RI-55-30-16232 REV A</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

RHW T/E I/B MID FLAP LOWER SURFACE FOUND DENT (COUNT FROM I/B EDGE 16" AND LOWER EDGE 10")(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: FLOOR PANEL — DENTED · airframe 114,008 hrs · 17,374 cycles

BULK CARGO STA 2040-2160 CTR FLOOR PANEL FOUND 3EA DENT(<P>3EA DENT AREA REPAIRED AS PER RI NO : RI-53-60-16249 REV A</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

LHW T/E I/B MID FLAP LOWER SURFACE FOUND DENT (COUNT FROM O/B 40")(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

EMP VERT FIN L/E FAIRING 321B FOUND DENT MARK(<P>DENT MARK AREA REPAIRED AS PER RI NO : RI-55-30-16231 REV A</P>)

Part: DUCT — UNKNOWN · airframe 114,008 hrs · 17,374 cycles

NO.1 ENG LH C-DUCT FWD V BLADE UPPER AREA CRACK(<P>C-DUCT REPLACED AS PER AMM 78-31-01 REV 107 DATE : 15 MAR 2023.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

1EA CRACK FOUND ON RH STA 800 STR 17R CRACK ON 3 O/C POSITION ( VIEW LOOKING O/B ) CRACK LOCATION AT THIRD LAYER(<P>CRACK AREA REPAIRED AS PER RI NO : RI-53-20-16234 REV A ( INTERIM REPAIR )</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

NO.1 ENG LH CORE COWL INNER SURFACE NO.2 FRAME CHAFING WORN(<P>CHAFING AREA REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

RHW T/E I/B MID FLAP LOWER SURFACE FOUND DENT (COUNT FROM O/B EDGE 40" AND LOWER EDGE 10")(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: BATTERY PACK — NO TEST · airframe 114,008 hrs · 17,374 cycles

EMERGENCY LT POWER SUPPLY M7027 L/H CAPACITY CHECK FAIL(<P>POWER PACK REPLACED AND OPERATION CHECKED NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 114,008 hrs · 17,374 cycles

AFT  CARGO RH STA 1680-1780 WALKWAY PANEL FOUND CORROSION(<P>AFT CARGO RH STA 1680-1780 WALKWAY PANEL CORROSION REMOVED AND REPROTECTED IAW SRM51-10-02, AND CHECKED WITHIN SRM 53-00-53 ADL.1 FIG 101 LIMIT</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 114,008 hrs · 17,374 cycles

BULK CARGO STA 2190 STR 51L STRINGER FOUND CORROSION(<P>BULK CARGO STA 2190 STR 51L STRINGER SURFACE CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02, AND CHECKED WITHIN SRM 53-00-03 ADL.1 FIG 101 LIMIT</P>)

Part: FLOOR PANEL — PUNCTURED · airframe 114,008 hrs · 17,374 cycles

BULK CARGO STA 1920-2040 CTR FLOOR PANLE FOUND 3EA DENT AND 2EA PUNCTURE(<P>3EA DENT AND 2EA PUNCTURE AREA REPAIRED AS PER RI NO : RI-53-60-16250 REV A</P>)

Part: BATTERY PACK — NO TEST · airframe 114,008 hrs · 17,374 cycles

EMERGENCY LT POWER SUPPLY M335 CAPACITY CHECK FAIL(<P>POWER PACK REPLACED AND OPERATION CHECKED NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 114,008 hrs · 17,374 cycles

RH WLG W/W FWD BULKHEAD FOUND CORROSION ( NEAR OVERRIDE / JETTISON PUMP LOWER BONDING AREA ).(<P>RH WLG W/W FWD BULKHEAD (NEAR OVERRIDE JETTSION PUMP LOWER BONDING AREA) CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 AND CHECKED WITHIN SRM 57-10-10 ADL 2, FIG 101.</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 114,008 hrs · 17,374 cycles

FWD CARGO RH STA 880-960 WALKWAY PANEL FOUND CORROSION(<P>FWD CARGO RH STA 880-960 WALKWAY PANEL CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND CHECKED WITHIN SRM 53-00-53 ADL. 1 FIG 101 LIMIT</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

LHW O/B MID FLAP I/B L/E FAIRING I/B MOST I/B EDGE CHAFING(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5G</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

NO.3 ENG - RH CORE COWL INNER #2 FRAME CHAFING WORN(<P>FRAME CHAFING WORN AREA REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

LHW T/E O/B FORE FLAP L/E 8" COUNT FROM I/B FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: BATTERY PACK — NO TEST · airframe 114,008 hrs · 17,374 cycles

EMERGENCY LT POWER SUPPLY M312 CAPACITY CHECK FAIL(<P>POWER PACK REPLACED AND OPERATION CHECKED NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 114,008 hrs · 17,374 cycles

AFT CARGO RH STA 1500-1590 WALKWAY PANEL FOUND CORROSION(<P>AFT CARGO RH STA 1500-1590 WALKWAY PANEL CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02, AND CHECKED WITHIN SRM 53-00-53 ADL. 1 FIG 101 LIMIT</P>)

Part: FLOOR PANEL — DENTED · airframe 114,008 hrs · 17,374 cycles

BULK CARGO RH STA 1920 - 2040 FLOOR PANEL FOUND 3EA DENT AND 1EA PUNCTURE(<P>3EA DENT AND 1EA PUNCTURE AREA REPAIRED AS PER RI NO : RI-53-60-16248 REV A</P>)

Part: BATTERY PACK — NO TEST · airframe 114,008 hrs · 17,374 cycles

EMERGENCY LT POWER SUPPLY M7027 R/H CAPACITY CHECK FAIL(<P>POWER PACK REPLACED AND OPERATION CHECKED NORMAL</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,008 hrs · 17,374 cycles

EMP APU COMPT STA 2701-2709 BL0 SKIN FOUND CRACK(<P>SKIN CRACK AREA REPAIRED AS PER RI NO RI-53-81-16246 REV A</P>)

Part: NONE — NONE · airframe 112,861 hrs · 17,101 cycles

EXCESSIVE NOISE FROM R1 WINDOW SEAL LEAK (ATB)(<P>R/R R WINDSHIELD AND APPLIED SEALANT. CABIN PRESS LK NORMAL&NBSP; AS PER AMM 56-11-01..05-51-08 FIM 56-00 TASK.</P> / <P>803 ...REF LOG 1600492 M7.. EO 4430A020 PART 4 ACCOMPLISHED BY SAK MAINTENANCE</P>)

Part: PANEL — CORRODED (KEEL BEAM AREA) · airframe 107,390 hrs · 16,170 cycles

FX - KEEL BEAM #191GG PANEL FOUND CORROSION.(<P>FX - KEEL BEAM #191GG PANEL REPLACED AS PER&NBSP;<SPAN>DWG AND PL 65B11032.</SPAN></P>)

Part: POWERPACK — NO TEST (EMERGENCY LIGHTS) · airframe 107,390 hrs · 16,170 cycles

U/D LH STA 600-620 M335 EMER LIGHT POWER PACK CAPACITY CHECK FAILED.(<P>U/D LH STA 600-620 M335 EMER LIGHT POWER PACK REPLACED AND INSTALLATION TEST CARRIED OUT RESULT NORMAL IAW AMM 33-51-04 REV 101, 15 MAR 2021.</P>)

Part: POWERPACK — NO TEST (EMERGENCY LIGHT) · airframe 107,390 hrs · 16,170 cycles

U/D DOOR RHS M7027 EMER LIGHT POWER PACK CAPACITY CHECK FAILED.(<P>U/D DOOR RHS M7027 EMER LIGHT POWER PACK REPLACED AND INSTALLATION TEST CARRIED OUT RESULT NORMAL IAW AMM 33-51-04 REV 101, 15 MAR 2021.</P>)

Part: PLATE — DAMAGED (RT AILERON TE) · airframe 107,390 hrs · 16,170 cycles

RHW O/B AILERON O/B T/E AREA ATT PLATE FOUND DAMAGE.(<P>RHW O/B AILERON O/B T/E AREA ATT PLATE DAMAGED AREA REPAIRED AS PER RI-57-51-14571 REV A</P>)

Part: SKIN — DELAMINATED (RUDDER) · airframe 107,389 hrs · 16,170 cycles

EMP - LOWER RUDDER LHS T/E MOST UPPER AREA FOUND DELAMINATED(<P>DELAMINATED AREA HAVE BEEN REPAIRED WITH COMPOSITE HOT BOND REPAIR METHOD&NBSP;</P>)

Part: STRUCTURE — CORRODED (LT WING TE FLAP) · airframe 107,390 hrs · 16,170 cycles

LHW I/B MID FLAP I/B FLAP PANEL UPPER CHORD FOUND CORROSION.(<P>LHW I/B MID FLAP I/B FLAP PANEL UPPER CHORD CORROSION AREA REWORKED AS PER SRM 57-30-02-1A-1</P>)

Part: FLOORBEAM — CORRODED (BS 860 LBL 90) · airframe 107,390 hrs · 16,170 cycles

M/D STA 860 LBL 90 FLOOR BEAM SUPPORT FOUND CORROSION.(<P>M/D STA 860 LBL 90 FLOOR BEAM SUPPORT CORROSION AREA REWORKED AS PER SRM 53-00-52-1A-1.</P>)

Part: SUPPORT — CORRODED (KEEL BEAM AREA) · airframe 107,390 hrs · 16,170 cycles

FX - KEEL BEAM #191JJ PANEL FOUND CORROSION.(<P>FX - KEEL BEAM #191JJ PNL SUPPORT REPLACED AS PER DWG AND PL 69B11856-1 AND AS PER SRM 51-40-02.</P>)

Part: BATTERY — NO TEST (DOOR SLIDE) · airframe 107,390 hrs · 16,170 cycles

U/D - LH DOOR SLIDE ( M7037 ) BATTERY PACK CHECK TEST FAIL.(<P>U/D - LH DOOR SLIDE ( M7037 ) BATTERY POWER SUPPLY ASSY REPLACED AND BATTERY PACK CHECK TEST CARRIED OUT RESULT NORMAL IAW AMM 52-23-14, REV 101, DATE 15 MAR 2021.</P>)

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 107,389 hrs · 16,170 cycles

RHW I/B FORE FLAP UPPER SURFACE O/B ZONE&NBSP; FOUND DELAM(<P>DELAMINATED AREA HAVE BEEN REPAIRED WITH COMPOSITE HOT BOND REPAIR METHOD&NBSP;</P>)

Part: BATTERY — NO TEST (DOOR SLIDE) · airframe 107,390 hrs · 16,170 cycles

U/D - RH DOOR SLIDE ( M7038 ) BATTERY PACK CHECK TEST FAIL.(<P>U/D - RH DOOR SLIDE ( M7038 ) BATTERY POWER SUPPLY ASSY REPLACED AND BATTERY PACK CHECK TEST CARRIED OUT RESULT NORMAL IAW AMM 52-23-14 REV 101, DATE 15 MAR 2021.</P>)

Part: FLOORBEAM — CORRODED (BS 2220 RBL33-55) · airframe 107,390 hrs · 16,170 cycles

M/D STA 2220 RBL 33 - 55 FLOOR BEAM SUPPORT FOUND CORROSION.(<P>M/D STA 2220 RBL 33 - 55 FLOOR BEAM SUPPORT CORROSION AREA REWORKED AS PER SRM 53-00-52-1A-1.</P>)

Part: POWERPACK — NO TEST (EMERGENCY LIGHTS) · airframe 107,390 hrs · 16,170 cycles

U/D DOOR LHS M7027 EMER LIGHT POWER PACK CAPACITY CHECK FAILED.(<P>U/D DOOR LHS M7027 EMER LIGHT POWER PACK REPLACED AND INSTALLATION TEST CARRIED OUT RESULT NORMAL IAW AMM 33-51-04 REV 101, DATE 15 MAR 2021.</P>)

Part: BEAM — CRACKED (BS 1265 S5L) · airframe 107,390 hrs · 16,170 cycles

M/D STA 1265 S-5L BEAM WEB FOUND CRACK.(<P>M/D STA 1265 S-5L BEAM WEB REPLACED AND INSTALLED AS PER RI-53-00-14536 REV A.</P>)

Part: FLOORBEAM — CORRODED (BS 2260 RBL 5-11) · airframe 107,390 hrs · 16,170 cycles

M/D STA 2260 RBL 5 - RBL 11 FLOOR BEAM SUPPORT FOUND CORROSION.(<P>M/D STA 2260 RBL 5 - RBL 11 FLOOR BEAM SUPPORT CORROSION AREA REWORKED AS PER SRM 51-00-52-1A-1.</P>)

Part: POWERPACK — NO TEST (EMERGENCY LIGHTS) · airframe 107,390 hrs · 16,170 cycles

U/D RH STA 740-760 M312 EMER LIGHT POWER PACK CAPACITY CHECK FAILED.(<P>U/D RH STA 740 - 760 M312 EMER LIGHT POWER PACK REPLACED AND INSTALLATION TEST CARRIED OUT RESULT NORMAL IAW AMM 33-51-04 REV 101, DATE 15 MAR 2021.</P>)

Part: DUCT — DAMAGED (NR 3 ENGINE) · airframe 107,390 hrs · 16,170 cycles

NO.3 ENG LH C-DUCT FITTING HOLE FOUND ELONGATED REF CMM 78-32-02 REPAIR 020. THE POD SUPPORT FWD BUSHING HOLE MEASURED 1.08" DIA, WHICH HAS EXCEEDES THE MAXIMUM REPAIREABLE LIMIT 0.875" DIA.(<P>THE POD SUPPORT FTG CAN NOT REPLACED AS HAECO DOES NOT HAVE CAPABILITY&NBSP; TO DISASSEMBLE THE UPPER SIDEWALL ASSY FOR THE FITTING REPLACEMENT. THE WHOLE C-DUCT. L3 DUCT REPLACED AS PER AMM 78-31-01.</P>)

Part: FLOORBEAM — CORRODED (BS 2140 RBL70) · airframe 107,390 hrs · 16,170 cycles

M/D STA 2140 RBL 70 FLOOR BEAM SUPPORT FOUND CORROSION.(<P>M/D STA 2140 RBL 70 FLOOR BEAM SUPPORT CORROSION AREA REWORKED AS PER SRM 53-00-52-1A-1.</P>)

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 107,389 hrs · 16,170 cycles

LHW I/B FORE FLAP L/E FAIRING&NBSP; FOUND DELAM(<P>DELAMINATED AREA HAVE BEEN REPAIRED WITH COMPOSITE HOT BOND REPAIR METHOD&NBSP;</P>)

Part: FLOORBEAM — CORRODED (BS 2220 BL0-11R) · airframe 107,390 hrs · 16,170 cycles

M/D STA 2220 BL 0 - RBL 11 FLOOR BEAM SUPPORT FOUND CORROSION.(<P>M/D STA 2220 BL 0 -- RBL 11 FLOOR BEAM SUPPORT CORROSION AREA. REWORKED AS PER SRM 53-00-52-1A-1.</P>)

Part: BRACKET — CRACKED (RT FLAP TRACK) · airframe 107,390 hrs · 16,170 cycles

RHW I/B FLAP TRACK #5 FWD ATT SUPPORT FTG BRACKET FOUND CRACK.(<P>RHW I/B FLAP TRACK #5 FWD ATT SUPPORT FTG BRACKET REPLACED AS PER DWG 65B15964-253, PL AND SRM 51-40-02</P>)

Part: FAIRING — CRACKED (NR 3 ENG DUCT) · airframe 107,390 hrs · 16,170 cycles

NO.3 ENG L/H C-DUCT UPPER AFT FIXED FAIRING FOUND CRACK.(<P>#3 ENG L/H C-DUCT UPPER AFT FIXED FAIRING CRACK AREA REPAIRED AS PER CMM 78-32-02 REPAIR 007.</P>)

Part: SEAT TRACK — CORRODED (BS 2360 RBL 33) · airframe 107,390 hrs · 16,170 cycles

M/D STA 2360 RBL 33 SEAT TRACK UPPER FLANGE FOUND CORROSION.(<P>M/D STA 2360 RBL 33 SEAT TRACK UPPER FLANGE CORROSION AREA REWORKED AS PER SRM 53-00-52-1A-1.</P>)

Part: FLOORBEAM — CORRODED (BS 2200 RBL44) · airframe 107,390 hrs · 16,170 cycles

M/D STA 2200 RBL 44 FLOOR BEAM SUPPORT FOUND CORROSION.(<P>M/D STA 2200 RBL 44 FLOOR BEAM SUPPORT CORROSION AREA REWORKED AS PER SRM 53-00-52-1A-1.</P>)

Part: BEAM — CRACKED (NR 1 NACELLE) · airframe 107,390 hrs · 16,170 cycles

#1 PYLON I/B SKIRT BEAM SKIN FOUND CRACK.(<P>#1 PYLON I/B SKIRT BEAM SKIN AND SUPPORT ANGLE REPAIRED AS PER RI-54-00-14566 REV A.</P>)

Part: SKIN — GOUGED (HORIZONTAL STAB) · airframe 107,390 hrs · 16,170 cycles

LH HORI STAB STA 520 AND 560 LOWER SKIN FOUND CORROSION.(<P>LH HORI STAB STA 520 AND 560 LOWER SKIN CORROSION AREA REPAIRED AND FASTENER INSTALLED AS PER RI-55-00-14577 REV A</P>)

Part: DOOR FRAME — CRACKED (RT MLG WW) · airframe 107,390 hrs · 16,170 cycles

R/H WLG I/B W/W DOOR FWD O/B FRAME CORNER FOUND CRACK.(<P>RH WLG I/B W/W DOOR FWD O/B FRAME CORNER REPAIRED AS PER RI-52-82-14548 REV A.</P>)

Part: FAIRING — CRACKED (LT C-DUCT) · airframe 107,390 hrs · 16,170 cycles

#4 ENG LH C-DUCT UPPER AFT FIXED FAIRING FOUND CRACK.(<P>#4 ENG L/H C-DUCT UPPER AFT FIXED FAIRING CRACK AREA REPAIRED AS PER CMM 78-32-02 REPAIR 007.</P>)

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 107,390 hrs · 16,170 cycles

RH O/B ELEVATOR L/E UPPER PANEL SKIN FOUND CRACK(<P>RH O/B ELEVATOR L/E UPPER PANL SKIN REPLACED AS PER SRM 51-10-02 AND 51-40-02.</P>)

Part: SHIM — CORRODED (R4 DOOR GATE) · airframe 107,390 hrs · 16,170 cycles

M/D - #4R DOOR UPPER GATE ATT SHIM FOUND CORROSION.(<P>M/D #4R DOOR UPPER GATE ATT SHIM REPLACED AS PER DWG AND PL 65B04951-6.</P>)

Part: POWERPACK — NO TEST (EMERGENCY LIGHTS) · airframe 107,390 hrs · 16,170 cycles

U/D LH STA 540-560 M5170 EMER LIGHT POWER PACK CAPACITY CHECK FAILED.(<P>U/D LH STA 540-560 M5170 EMER LIGHT POWER PACK REPLACED AND INSTALLATION TEST CARRIED OUT RESULT NORMAL IAW AMM 33-51-04 REV 101, DATE 15 MAR 2021.</P>)

Part: PANEL — CRACKED (L5 DOOR FRAME) · airframe 107,390 hrs · 16,170 cycles

#5L DOOR FWD MID REVEAL PANEL CUTOUT FOUND CRACK.(<P>#5L DOOR FWD MID REVEAL PANEL CUTOUT CRACK AREA REPAIRED AS PER SRM 53-60-15 REPAIR 17.</P>)

Part: POWERPACK — NO TEST (EMERGENCY LIGHTS) · airframe 107,390 hrs · 16,170 cycles

U/D LH STA 740-760 M7050 EMER LIGHT POWER PACK CAPACITY CHECK FAILED.(<P>U/D LH STA 740-760 M7050 EMER LIGHT POWER PACK REPLACED AND INSTALLATION TEST CARRIED OUT RESULT NORMAL AS PER AMM 33-51-04 REV 101, DATE 15 MAR 2021.</P>)

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 107,389 hrs · 16,170 cycles

LHW O/B FORE FLAP O/B L/E FAIRING FOUND DELAM(<P>DELAMINATED AREA HAVE BEEN REPAIRED WITH COMPOSITE HOT BOND REPAIR METHOD&NBSP;</P>)

Part: FLOORBEAM — CORRODED (BS 2160 R/LBL 11) · airframe 107,390 hrs · 16,170 cycles

M/D STA 2160 LBL 11 - RBL 11 FLOOR BEAM SUPPORT FOUND CORROSION.(<P>M/D STA 2160 LBL 11 - RBL 11 FLOOR BEAM SUPPORT CORROSION AREA REWORKED AS PER SRM 53-00-52-1A-1.</P>)

Part: SKIN — DAMAGED (BS 240 S28A-30R) · airframe 107,390 hrs · 16,170 cycles

FX - STA 240 R/H S-28A TO S-30R SKIN FOUND PREVIOUS BLEND OUT AREA AT 2EA RIVET LOCATION.(<P>FX - STA 240 RH S-28A TO S-30R SKIN BLEND OUT AREA 2EA RIVET REPLACED AS PER RI-53-00-14544 REV A</P>)

Part: VALVE — DAMAGED (CABIN TEMP) · airframe 106,837 hrs · 16,087 cycles

WHILE CLIMBING THRU 15000, NOTICED COCKPIT GETTING EXTREMELY HOT. 47 DEGREES C FLIGHT DECK, 40C MAIN DECK FOUND VALVE DAMAGED. REMOVED AND REPLACED FLOW CONTROL VALVE IAW AMM 21-51-01/401. ZONE TEMP CONTROL SYSTEM OPS NORMAL REF AMM 21-61-00.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 106,484 hrs · 16,008 cycles

UPPER DECK EMERGENCY LIGHT IS INOPERABLE. REMOVED AND REPLACED U/D POWER SUPPLY UNIT. OPERATINS CHECK U/D EMERGENCY LIGHT OK, PER AMM 33-51-04.

Part: SKIN PANEL — DAMAGED (RT WING) · airframe 104,510 hrs · 15,542 cycles

FULL SPEED BRAKE PRODUCES LEFT ROLL.. REPAIRED SPOILER ACTUATOR MOUNT AT WING TRAILING EDGE. DURING REMOVAL OF NR 8 SPOILER DAMAGE WAS FOUND TO TOP SIDE OF RIGHT WING TRAILING EDGE AT BOTH SPOILER HINGE POINTS AND AT NR 8 SPOILER POWER PACK FITTING (CONT) ATTACHMENT FITTING, NO DAMAGE TO SPOILER ATTACHMENT FITTINGS WAS NOTED. DAMAGE IS RESTRICTED TO RT WING CUTOUTS AREA. RT WING T/E SKIN PANEL AT APPROXIMATE WBL 373 REPAIRED ON WING UNDER WORK ORDER 14797 FAA FORM 8130-3 ISSUED TRACKING NUMBER 5002118 DTD 24MAY20.

Part: BATTERY — NO TEST (DOOR) · airframe 103,782 hrs · 15,311 cycles

UPPER DECK - RIGHT HAND DOOR, EMERGENCY BATTERY FAILS TEST.(<P>REMOVED AND REPLACED UPPER DECK R/H DOOR, EMERGENCY BATTERY PACK PER B747-400 AMM 52-23-14-004-001. OPS CHECK GOOD PER B747-400 AMM 52-23-14-744-010.</P>)

Part: DUCT — CORRODED (AC BAY) · corrosion level 2 · airframe 102,877 hrs · 15,128 cycles

FX-# 1 AIRCON PACK RAM AIR INLET DUCT AFT OUTLET INNER DUCT CUTOUT 2 PLACES BULGE/CORROSION.(<P>FX-# 1 AIRCON PACK RAM AIR INLET DUCT AFT OUTLET INNER DUCT CUTOUT DUCT P/N: 65B07253-1 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02.<BR /></P>)

Part: BATTERY PACK — FAILED (CABIN) · airframe 102,877 hrs · 15,128 cycles

U/D STA 720-740 LT EMERGENCY LIGHT BATTERIES CAP TEST FAILED. (<P>EMERGENCY POWER PACK REPLACED AS PER AMM 33-51-04.</P>)

Part: WEB — CORRODED (FUSELAGE) · airframe 102,877 hrs · 15,128 cycles

COCKPIT-PILOT RT FORWARD PANEL SUPPORT WEB CRACKED.(<P>COCKPIT-PILOT RT FORWARD PANEL SUPPORT WEB CRACK AREAS REPAIRED IAW RI-53-00-13598 REV A.<BR /></P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 102,877 hrs · 15,128 cycles

UPPER DECK LT DOOR EMERGENCY POWER RESERVOIR BATTERY PACK CAP TEST FAILED. (<P>EMERGENCY POWER BATTERY PACK REPLACED AS PER AMM 35-51-04.</P>)

Part: FRAME — CRACKED (FUSELAGE) · airframe 102,877 hrs · 15,128 cycles

RT BS 2231 FRAME INSPECTION FOUND 1 EA HOLE CRACKED AT STR 16R THROUGH THICKNESS AT 3 O'CLOCK AND 9 O'CLOCK.(<P>CABIN-STA 2231 STR 15R TO S FRAME STRAP CRACK AREA REPAIRED IAW RI-53-00-13627 REV A.<BR /></P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 102,877 hrs · 15,128 cycles

UPPER DECK STATION 720-740 RT EMERGENCY LIGHT BATTERY CAP TEST FAILED. (<P>EMERGENCY POWER SUPPLY REPLACED AS PER AMM 33-51-04.&NBSP;</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 102,877 hrs · 15,128 cycles

UPPER DECK STATION 600-620 LT EMERGENCY LIGHT BATTERY CAP TEST FAILED. (<P>EMERGENCY POWER PACK REPLACED AS PER AMM 33-51-04.</P>)

Part: WEB — CORRODED (FUSELAGE) · airframe 102,877 hrs · 15,128 cycles

COCKPIT-PILOT LT FORWARD PANEL SUPPORT WEB CRACKED.(<P>COCKPIT-PILOT LT FORWARD PANEL SUPPORT WEB CRACK AREAS REPAIRED IAW RI-53-00-13598 REV A.<BR /></P>)

Part: BATTERY PACK — FAILED (CABIN) · airframe 102,877 hrs · 15,128 cycles

UPPER DECK L/H DOOR EMERGENCY LIGHT BATTERY CAP TEST FAILED.(<P>EMERGENCY LIGHT POWER SUPPLY BATTERY REPLACED AS PER AMM 33-51-04.</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 102,877 hrs · 15,128 cycles

UPPER DECK RT DOOR EMERGENCY LIGHT BATTERY CAP TEST FAILED. (<P>EMERGENCY LIGHT POWER SUPPLY REPLACED AS PER AMM 33-51-04.</P>)

Part: FRAME — CRACKED (FUSELAGE) · airframe 102,877 hrs · 15,128 cycles

LT BS 2231 STR 24L-STR25L FRAME INSPECTION FOUND 1 EA HOLE CRACKED.(<P>CABIN-STA 24L TO STR 26L FRAME STRAP CRACK AREA REPAIRED IAW SRM 53-60-15-2R-2 REPAIR R. THIS REPAIR IS A CATEGORY B REPAIR. REPEAT INSPECTION PER SRM 53-60-15-2R-2 REPAIR TABLE II.<BR /></P>)

Part: FRAME — CRACKED (FUSELAGE) · airframe 102,877 hrs · 15,128 cycles

RT BS 2231 STR 25R FRAME INSPECTION FOUND 2 EA HOLE CRACKED.(<P>CABIN-STA 2231 STR 24R TO STR 26R FRAME STRAP CRACK AREA REPAIRED IAW SRM 53-60-15-2R-2 REPAIR 2. THIS REPAIR IS A CATEGORY B REPAIR. REPEAT INSPECTION PER SRM 53-60-15-2R-2 REPAIR 2 TABLE II.<BR /></P>)

Part: FRAME — CRACKED (FUSELAGE) · airframe 102,877 hrs · 15,128 cycles

FUS-1 EA HOLE FOUND CRACK AT BS 2598 FRAME FWD INNER CHORD FRAME SUPPORT.(<P>FUS-STA 2598 RT UPPER CUTOUT FWD INNER SUPPORT FRAME 1 EA FASTENER CRACK AREA REPAIRED IAW RI-53-00-13619 REV A.<BR /></P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 102,877 hrs · 15,128 cycles

UPPER DECK STATION 540-560 LT EMERGENCY LIGHT CAP TEST FAILED. (<P>EMERGENCY POWER PACK REPLACED AS PER AMM 33-51-04.</P>)

Part: BATTERY PACK — DISCHARGED (EMERGENCY EXIT) · airframe 100,170 hrs · 14,568 cycles

UPPER DECK RIGHT HAND BATTERY TEST SWITCH INOP. REMOVED AND REPLACED M7037 EMERGENCY DOOR BATTERY PACK ASSY.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 98,185 hrs · 14,197 cycles

OIL ODOR FROM THE NR 1 PACK, NR 1 ENGINE OIL QTY DOWN TO 7 INFLIGHT. MX PERFORMED BOROSCOPE INSPECTION OF THE NR 1 ENGINE, OIL STAINING NOTED IN HIGH PRESSURE COMPRESSOR, NR 1 ENGINE REPLACED, PRECOOLER INSPECTED, NO FAULTS NOTED. NR 1 & 2 PACKS, & NR 3 COALESCER BAGS REPLACED.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 97,666 hrs · 14,062 cycles

EXTREME ODOR OF JET ENGINE EXHAUST IN THE COCKPIT AND UPPER DECK DURING DESCENT. PERFORMED FIM 21-00, TASK 810. FOUND RT WING GEAR DOOR RETURN HYD FITTING LEAKING. PERFORMED APU BLEED FOR OIL CONTAMINATION. PERFORMED ENGINE BLEED AIR OIL CONTAMINATION CHECK, OK. NO OCCURRENCE OF FUMES.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 96,607 hrs · 13,850 cycles

LEFT WING L/E VARIABLE CAMBER FLAP NOSE SKIN GOUGED. REPAIRED THE FLAP NOSE SKIN IAW SRM 57-43-02, REPAIR 2, SHEET 6.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 96,607 hrs · 13,850 cycles

ALL EMERGENCY LIGHTS FAILED TO STAY ON A MINIMUM OF 5 MINUTES. REMOVED AND REPLACED THE BATTERY PACKS IAW AMM 33-51-04.

Part: FLOOR SUPPORT — CRACKED (BS 2000) · airframe 96,607 hrs · 13,850 cycles

AFT CARGO BULK BAY FLOOR SUPPORT ANGLE CRACKED AT STA 2000 RBL 7.5(<P>REPAIRED IAW SRM 53-60-53, FIG 201, TABLE 1.

Part: SUPPORT — CORRODED (LT WIGN) · corrosion level 2 · airframe 96,607 hrs · 13,850 cycles

LT WING L/E BETWEEN OLES 1535 - 1617 HAS CORROSION AT LOWER WING L/E COMPARTMENT. REMOVED AND REPLACED THE SECTION OF THE LOWER L/E BEAM PANEL SUPPORT IAW SRM 57-41-13-2R-3, REPAIR 3.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 96,607 hrs · 13,850 cycles

LEFT INBD AFT FLAP DELAMINATED AT LOWER T/E SURFACE OTBD OF THE NR 4 TRACK. REMOVED AND REPLACED THE FLAP IAW AMM 27-51-03.

Part: FLAP — DAMAGED (RT WING) · airframe 96,607 hrs · 13,850 cycles

RIGHT WING NR 17 L/E VARIABLE CAMBER FLAP BULL NOSE IS DAMAGED AT OTBD END JUST ABOVE REPAIR DOUBLER. FABRICATED AND INSTALLED REPAIR DOUBLER IAW 57-43-02-2R-2, FIG 201, STEPS 4-5.

Part: SHEAR TIE — CRACKED (LT WING SKIN) · airframe 96,607 hrs · 13,850 cycles

LEFT WING TE INBD AILERON ACTUATOR COMPARTMENT HAS A CRACK ON UPPER WING SKIN ANGLE SUPPORT BRACKET ON RIB BEHIND PANEL 573AB. REPAIRED LT WING TE RIB AND SUPPORT ANGLE AT WBL 445.94 IAW EA 747-5700-28-A6834, REV IR, AND EO 4457A609, REV 0.

Part: SKIN — DENTED (VERTICAL STAB) · airframe 96,607 hrs · 13,850 cycles

VERTICAL STAB L/E SECTION 321B HAS SEVERAL DENTS. REPAIRED VERTICAL STAB L/E SECTION 321B IAW EA 747-5530-28-A6835, REV IR.

Part: SKIN — DENTED (VERTICAL STAB) · airframe 96,607 hrs · 13,850 cycles

VERTICAL STAB L/E SECTION 321E DENTED. REPAIRED THE VERTICAL STAB L/E SECTION IAW EA 747-5530-28-A6824, REV IR.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 96,607 hrs · 13,850 cycles

RT HORIZONTAL STAB L/E SECTION 341BR DENTED. REPAIRED IAW SRM 55-10-01-2R-2, REPAIR 2, FIG 201.

Part: FLAP — DAMAGED (RT WING) · airframe 96,607 hrs · 13,850 cycles

RT WING NR 18 VARIABLE CAMBER FLAP BULL NOSE IS DAMAGED AT INBD END. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 57-43-02-2R-2, FIG 201, SHEET 2, STEPS 4-5, AND SRM 57-43-02-2R-2, REPAIR 2.

Part: SKIN — DAMAGED (NR 2 NACELLE) · airframe 96,607 hrs · 13,850 cycles

NR 2 ENGINE OTBD CORE COWL OUTER SKIN FWD UPPER CORNER IS CRACKED AND BENT. REPAIRED IAW EO 1971A139.

Part: STRINGER — CRACKED (BS 480) · airframe 96,607 hrs · 13,850 cycles

CABIN UPPER DECK STRINGER 10L CRACK AROUND FASTENER LOWER SURFACE AT BS 480. REPAIRED UPPER DECK STRINGER IAW EA 747-5310-28-A6847, REV IR, AND EO 445B375, REV 0.

Part: SUPPORT BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 96,607 hrs · 13,850 cycles

LEFT WING L/E HAS CORROSION AT WS 1430 IN L/E COMPONENT. REMOVED AND REPLACED LT WING L/E SUPPORT BEAM SECTION BETWEEN WS 1336 TO WS 1430 IAW EA 747-5750-28-A6870, REV IR.

Part: SKIN — CHAFED (RT WING LOWER) · airframe 96,607 hrs · 13,850 cycles

RT WING LOWER SKIN IS CHAFED ABOVE THE NR 4 PYLON. REPEAIRED IAW EA 747-5730-28-A6833, REV IR.

Part: STRUCTURE — GOUGED (THRUST REVERSER) · airframe 96,607 hrs · 13,850 cycles

NR 4 ENGINE OTBD THRUST REVERSER GOUGED AT THE AFT SECTION. ACCOMPLISHED EO 1978A151.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 96,607 hrs · 13,850 cycles

ALL EMERGENCY LIGHT POWER PACKS REQUIRE REPLACEMENT. LIGHTS FAILED TO STAY ON A MINIMUM OF 15 MINUTES. REMOVED AND REPLACED POWER PACKS IAW AMM 33-51-04.

Part: SKIN — DENTED (VERTICAL STAB) · airframe 96,607 hrs · 13,850 cycles

VERTICAL STAB L/E PANEL 321E FOUND A FOUR INCH DENT OVER RIB. REPAIRED THE VERTICAL STAB L/E PANEL VSS 529.801 IAW EA 747-5530-28-A6853, REV IR.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 96,607 hrs · 13,850 cycles

RIGHT INBD FORE FLAP LOWER SKIN DELAMINATED JUST INBD OF THE NR 5 FLAP TRACK. REPAIRED THE FLAP LOWER SKIN IAW SRM 57-53-01-2R-1, REPAIR TABLE 1, AND SRM 51-70-07-06-0.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 96,607 hrs · 13,850 cycles

ALL EMERGENCY LIGHT POWER PACKS REQUIRE REPLACEMENT. LIGHTS FAILED TO STAY ON A MINIMUM OF 15 MINUTES. REMOVED AND REPLACED POWER PACKS IAW AMM 33-51-04.

Part: STRINGER — CRACKED (BS 480) · airframe 96,607 hrs · 13,850 cycles

CABIN UPPER DECK STRINGERS 10R CRACKED AROUND FASTENER, LOWER SURFACE AT BS 480. REPAIRED THE STRINGER IAW EA 747-5310-28-A6846, REV IR, AND EO 4453B374, REV 0.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 96,607 hrs · 13,850 cycles

ALL EMERGENCY LIGHTS FAILED TO STAY ON A MINIMUM OF 5 MINUTES. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLIES IAW AMM 33-51-04.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 96,607 hrs · 13,850 cycles

LEFT WING INBD T/E MIDFLAP CHAFED AT L/E OF FLAP. REPAIRED IAW SRM 57-53-01-2R-4, REPAIR 4.

Part: SKIN — CHAFED (LT AILERON) · airframe 96,607 hrs · 13,850 cycles

LEFT WING OTBD AILERON PANEL 591DB CHAFED WITH TWO AILERON HINGE POINTS NEAR GREASE FITTINGS. REPAIRED IAW EA 747-5730-28-A6845, REV IR.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 96,581 hrs · 13,843 cycles

DURING PUSH BACK LOST ALL HYDRAULIC QUANTITY SYSTEM 1. FOUND SUPPLY HOSE AT THE NR 1 ENGINE HYDRAULIC MANIFOLD LEAKING. REMOVED AND REPLACED THE HOSE. ALL LEAK CHECKED GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 94,320 hrs · 13,412 cycles

RUDDER RATIO MESSAGE. R & R UPPER RUDDER RATIO CHANGER (ACTUATOR) IAW AMM 27-21-12. PERF BITE TEST, ALL PASSED SATISFACTORY, OPS & INDICATIONS OF RUDDER SYSTEM SATISFACTORY.

Part: WEB — CRACKED (RT WING) · airframe 93,683 hrs · 13,280 cycles

RIGHT WING FIXED TE GROUND SPOILERS IB RIB STRUCTURE AT WBL 255.69 WEB IS CRACKED. REMOVED & REPLACED THE WEB IAW SRM 51-40-02.

Part: SUPPORT RIB — CRACKED (LT WING) · airframe 93,683 hrs · 13,280 cycles

INDICATION OF A CRACK ON THE LT WING FIXED TE GROUND SPOILERS OTBD SUPPORT RIB AT WBL 432.65. REMOVED & REPLACED IAW SRM 51-40-02.

Part: STIFFENER — CRACKED (LT WING) · airframe 93,683 hrs · 13,280 cycles

LEFT WING WBL 432.62, FIXED SUPPORT BEAM WEB STIFFNER IS CRACKED. REMOVED AND REPLACED SUPPORT BEAM WEB STIFFNER IAW SRM 51-40-02, AMM 51-20-01, AND 51-24-11.

Part: SUPPORT RIB — CHAFED (LT WING) · airframe 93,683 hrs · 13,280 cycles

LEFT WING FIXED TE GROUND SPOILER SUPPORT RIB STRUCTURE AT WBL 432.65, IB FLANGE HAS A DEEP CHAFE FROM SPOILER BULB SEAL. REPLACED IAW SRM 57-51-02 & SRM 51-40-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 91,757 hrs · 12,952 cycles

UPPER RT DOOR EXIT LIGHT DID NOT COME ON. RECHARGED EMER PACK M312 IAW CMM 25-65-02. REINSTALLED BATTERY PACK IAW AMM 33-51-04. OPERATIONS CHECKED GOOD.

Part: DOOR — FAILED (EMERGENCY EXIT) · airframe 9,578 hrs · 744 cycles

EMERGENCY DOOR OPENING DEVICE FAILED TO DEPLOY DURING CHECK. CARTRIDGE SHOWS FIRED HOWEVER PENETRATOR FAILED TO PIERCE DIAPHRAGM THUS NOT RELEASE THE CHARGE NITROGEN. AFTER INSPECTION, MANIFOLD ASSY. SHOWS PENETRATOR MADE A DENT ON RUPTURE DISC ONLY.

Part: SKIN — GOUGED (THRUST REVERSER) · airframe 89,566 hrs · 12,528 cycles

DURING MX WALKAROUND, MX FOUND TWO GOUGES ON THE NR 4 ENGINE LT THRUST REVERSER TRANSLATING COWL OUTER SKIN. PERFORMED A TIME LIMITED REPAIR.

Part: BATTERY — WEAK · airframe 88,741 hrs · 12,388 cycles

CHECK FOUND LT UPPER DOOR BATTERY NO TEST. SWAPPED BATTERY CONFIRMED WEAK. REPLACED BATTERY.

Part: STRUCTURE — CRACKED (NR 3 NACELLE) · airframe 86,708 hrs · 12,010 cycles

NR 3 NACELLE AFT END CAP CRACKED AT CTR PORTION. REPAIRED IAW EO 4471A090.

Part: TENSION TIE — CRACKED (BS 1180) · airframe 86,708 hrs · 12,010 cycles

BS 1180 RT TENSION TIE AREA FOUND CRACKED AT FRAME. REPAIRED IAW EO 4453A197 AND SB 747-53A2507 FIG 11, OVERSIZE HOLE REPAIR.

Part: CHANNEL — CRACKED (BS 1180) · airframe 86,708 hrs · 12,010 cycles

M/D STA 1180 RT TENSION TIE FWD CHANNEL CRACKED. REPAIRED IAW SRM 53-40-30-2R-1, REPAIR 1, FIG 201.

Part: FAIRING — DISTORTED (NR 4 NACELLE) · airframe 86,708 hrs · 12,010 cycles

NR 4 ENGINE RT CORE COWL AFT UPPER TITANIUM FAIRING FOUND DISTORTED AND CHAFED. (NR 4 ENG RT CORE COWL AFT UPPER TITANIUM FAIRING DAMAGED AREA REPAIRED IAW SRM 54-41-01, FIG 201, REPAIR 5.)

Part: BEAM — CRACKED (LT MLG WW) · corrosion level 2 · airframe 86,708 hrs · 12,010 cycles

LT MLG INBD WW DOOR AFT EDGE BEAM CORROSION CRACKED. LT MLG INBD WW DOOR 65B10919-35, REPLACED IAW SRM 51-10-02.

Part: SKIN — DELAMINATED (RT AILERON) · airframe 86,077 hrs · 11,895 cycles

DURING MX WALKAROUND MX FOUND DAMAGE TO THE RT INBD AILERON T/E WITH DELAMINATION DAMAGE, MEASURING 2.0" X 4.0". THE DAMAGE EXCEEDS THE LIMITS OF THE SRM 57-60-01, FIG 101 ALLOWABLE DAMAGE 1. (DISPOSITION IS TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS; DVI EVERY 1 FLIGHT CYCLE; AND PERMANENT REPAIR PRIOR TO THE ACCUMULATION OF 50 FC (FLIGHT CYCLES) AFTER PART 1.)

Part: UNKNOWN — UNKNOWN (FUEL SYSTEM) · airframe 85,592 hrs · 11,810 cycles

DURING AUTO FUELING, RED OVERFILL LIGHT ILLUMINATED AND FUEL SPILLED OUT OF LT WING. (VOLUMETRIC TOPOFF DEFERRED IAW DDPG 28-21-1-2.)

Part: BOTTLE — LOW (PAX DOOR) · airframe 85,545 hrs · 11,802 cycles

DURING DAILY CHECK, MX FOUND THE RT UPPER DECK DOOR ASSIST BOTTLE LOW (DEFERRED UPPER DECK RT DOOR).

Part: ACCESS DOOR — DAMAGED (THRUST REVERSER) · airframe 85,357 hrs · 11,766 cycles

DURING MX WALKAROUND, REVEALED NR 1 ENGINE THRUST REVERSER ACCESS DOOR WAS FOUND OPEN AND DAMAGED.

Part: SKIN — CRACKED (NACELLE) · airframe 85,297 hrs · 11,757 cycles

DURING MX WALKAROUND, MX FOUND A CRACK WHICH IS APPROX 8" LONG AND 4" WIDE ON THE NR 4 ENGINE CORE COWL SKIN. MX FOUND A 4" SECTION OF THE LT CORE COWL L/E RUB STRIP BROKEN OFF. THIS COINCIDES WITH THE 4" SCRATCH MARKINGS ACROSS THE L/E OF THE DAMAGED AREA WHICH IS AFT OF THIS RUB STRIP. THE LENGTH OF THE CRACK AND THE MISSING RUB STRIP EXCEEDS THE SRM LIMITS.

Part: SLIDE — UNWANTED DEPLOY (EMERGENCY EXIT) · airframe 6,651 hrs · 1,205 cycles

RT EMERGENCY DOOR UPPER DECK WILL NOT ARM SLIDE MANUAL TO AUTOMATIC FUNCTION. INADVERTENT SLIDE DEPLOYMENT. ITEM TRANSFERRED TO (CL1443) IAW DDG 52-23-1-3.

Part: SLIDE — OUT OF POSITION (RT EMER EXIT) · airframe 84,994 hrs · 11,696 cycles

FOUND U/D RT EMERGENCY DOOR SLIDE MODE SELECTOR LEVER CANNOT BE PUT IN AUTO MODE. SLIDE RE-POSITIONED AND OPS CHECKED OK.

Part: SKIN — CRACKED (RT NACELLE) · airframe 83,121 hrs · 11,359 cycles

ENGINE COWLING - NR 4 RT ENGINE CORE COWL OUTER SKIN - CRACK - REPAIR - DURING MX WALKAROUND, MX FOUND A CRACK ON THE NR 4 RT CORE COWL OUTER SKIN. THE CIRCUMFERENTIAL CRACK IS APPROX 1 IN LONG. THE LENGTH OF THE CRACK EXCEEDS THE SRM LIMITS. (DISPOSITION IS TO STOP DRILL THE LOWER ENDS OF THE CRACK WITH A 0.250 IN. DIAMETER HOLE; DVI EVERY 3 FLIGHT CYCLES; AND A PERMANENT REPAIR AT THE NEXT A-CHECK AFTER PART 1; EO 4471A070, SRM 51-10-02, SRM 54-41-01 FIG 101, SRM 54-41-01 FIG 201, RPR 3, DER 8110-3 FORM DTD 10APR11.)

Part: ACTUATOR — FAILED (THRUST REVERSER) · airframe 82,723 hrs · 11,293 cycles

UPON ARRIVAL, THE NR 3 RT THRUST REVERSER, MX FOUND THE T/R NOT STOWED. AFTER INSP MX FOUND THE LOWER BALLSCREW ACTUATOR AT FAULT AND FAILED, NOT ALLOWING THE THRUST REVERSER TO BE MANUALLY STOWED. (DISPOSITION IS TO PERFORM A DETAILED INSPECTION OF THE NR 3 RT THRUST REVERSER HALF REF AMM 78-31-00, REMOVAL OF THE LOWER ANGLE GEARBOX ACTUATOR, DEACTIVATION OF THE T/R IAW DDG 78-31-1, DVI EVERY FLIGHT CYCLE, AND INSTALLATION OF SERVICEABLE PARTS WITHIN 10 CALENDAR DAYS. SUBSTANTIATION IS BASED ON THE INTEGRITY OF THE CTR DRIVE UNIT (CDU), VERIFIED VIA INSPECTIONS PERFORMED, WHICH PROVIDES THE HOLDING FORCE TO PREVENT THE REVERSER FROM DEPLOYING IN FLIGHT.)

Part: BRACKET — DAMAGED (DOOR SENSOR) · airframe 82,329 hrs · 11,234 cycles

DURING WALKAROUND INSP, MX REPORTED DAMAGE TO THE LT; WLG DOOR WARNING SENSOR MOUNT BRACKET AT BS1255.750 WITH 2 EA CRACKS REF FIG 1. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS REPAIR DOUBLER (2 EA) MAKE FROM 7075-T6, 0.080 IN W/2 ROWS OF FASTENERS AROUND THE DAMAGE.

Part: PSEU — OUT OF ADJUST (MLG) · airframe 82,132 hrs · 11,189 cycles

AFTER T/O GEAR LEVER WOULD NOT MOVE UP. COMPLIED IAW QRH PROCEDURES. RAISED GEAR (REPLACED PSEU), JACKED ACFT AND TILT SENSOR ADJUSTMENTS ACCOMPLISHED. (FOUND L/B GEAR ALT SWITCH AND R/B GEAR PRIMARY SWITCHES OUT OF ADJUSTMENT). ALL OPERATIONS WERE NORMAL.

Part: SKIN — DELAMINATED (MLG DOOR) · airframe 81,743 hrs · 11,108 cycles

DURING WALKAROUND INSP, MX FOUND THE RT WING LANDING GEAR DOOR - LOWER EDGE DELAMINATION, MEASURING 2.2 IN. X 0.800 IN. (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, SCHEDULE REPEAT INSPECTIONS AT EVERY 1,000 FH (FLIGHT HOURS) AND PERMANENT REPAIR PRIOR TO THE NEXT C-CHECK AFTER PART 1 HAS BEEN ACCOMPLISHED AFTER PART 1 IAW SRM 51-70-17 OR SRM 51-70-07.)

Part: NOSE COWL — DENTED (NR 4 ENGINE) · airframe 79,951 hrs · 10,775 cycles

DURING WALK AROUND INSP, MX FOUND THE NR 4 ENGINE INLET NOSE COWL L/E DENTED AT APPROX 10 O' CLOCK POSITION MEASURING 10.0 INCHES IN LENGTH AND 0.9 INCH DEEP. AFTER DETAIL VISUAL INSP (10X MAGNIFYING GLASS) IT WAS VERIFIED THAT NO CRACK CONDITION EXISTS. (DISPOSITION WAS MADE TO PERFORM TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, INITIATE REPEAT INSPECTIONS PRIOR TO EACH FLIGHT AND SCHEDULE PERMANENT REPAIR BY REMOVING AND REPLACING THE SUBJECT DAMAGED NOSE COWL. THIS EO IS APPROVED BY DER (DERT-710167-SW) VIA FAA 8110-3 FORM ISSUED ON JULY 10, 2010.)

Part: FAILSAFE — CRACKED (BS 1200 S9L) · airframe 78,592 hrs · 10,543 cycles

DURING C-CHECK, IN MARCH 2010, A CRACK WAS FOUND IN THE 65B09631-86 BS 1200, S-9L FRAME FAILSAFE CHORD CRACK COMMON TO THE TENSION TIE. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-70-11, REPAIR 1 AND NRC 503951. THE 65B01753-369 FAILSAFE CHORD IS MADE FROM BAC1490-2632, 7075-0 SHEET 0.064 INCH THICK IAW QQ-A-200/12 HEAT TREATED TO T6 AFTER FORMING. THE REPAIR IAW SRM 51-70-12, REPAIR 1 AND HAECO NRC 503951 CONSISTS OF AN ANGLE 0.090 INCH THICK FROM 7075-T6 ALUMINUM AND INSTALLED USING BACB30MY6K4 LOCK FASTENERS. THE REPAIR IAW PART 1 AND SRM 51-70-11, REPAIR 1 IS INSTALLED ON FATIGUE CRITICAL BASELINE STRUCTURE (FCBS) AND A DAMAGE TOLERANCE EVALUATION (DTE) IS NECESSARY. A DAMAGE TOLERANCE INSP (DTI) INCLUDES AN INSP THRESHOLD, INSPECTION INTERVALS, AND INSPECTION PROCEDURES AND METHODS. IF THE DTI IS NOT AVAILABLE WHEN THE AIRPLANE RETURNS TO SERVICE, THE REPAIR IS APPROVED FOR 24 MONTHS. THIS REPAIR HAS BEEN SUBMITTED TO FOR DTI ON SR 1-1561617284. EO 4453A346 DATED 22MAR10 WAS ISSUED TO PERFORM INTERIM REPAIR.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 78,592 hrs · 10,543 cycles

RIGHT BS 1160 TENSION TIE AREA ONE FASTENER HOLE CRACKED AT ANGLE CLIP. BS 1160 TENSION TIE ANGLE CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 78,592 hrs · 10,543 cycles

LEFT SIDE BS 1160 TENSION TIE AREA FOUR FASTENER HOLES CRACKED AT FRAME WEB. BS 1160 FRAME REPAIRED AS PER EO 4453A197 PART 5 POINT 6 AND SRM 53-40-07 REPAIR 3.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 78,592 hrs · 10,543 cycles

LEFT BS 1180 TENSION TIE AREA 2 FASTENER HOLES CRACKED AT FRAME WEB. BS 1180 FRAME REPAIRED AS PER EO 4453A216 PART 7 POINT 4.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 78,592 hrs · 10,543 cycles

LEFT BS 1140 TENSION TIE AREA FOUR FASTENER HOLES CRACKED AT FRAME WEB. BS 1140 FRAME REPAIRED AS PER EO 4453A216 PART 7 POINT 2.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 78,592 hrs · 10,543 cycles

LEFT BS 1220 TENSION TIE AREA ONE FASTENER HOLE CRACKED AT FRAME. BS 1220 ENTIRE FRAME REPLACED FROM PRODUCTION SPLICE STR 4 TO STR 11.5 PRODUCTION SPLICE PER EO 4453A216 PART 7 POINT 6.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 78,592 hrs · 10,543 cycles

LEFT BS 1200 TENSION TIE AREA ONE FASTENER HOLE CRACKED AT FAILSAFE CHORD. FAILSAFE CHORD REPAIRED AS PER SRM 51-70-11 FIG 1 AND EO 4453A216.

Part: STRUCTURE — CRACKED (HORIZ STAB) · airframe 78,592 hrs · 10,543 cycles

LEFT SIDE HORIZONTAL STAB UPPER REAR SPAR AREA ONE HOLE CRACKED AT SPLICE PLATE AREA RUNNING FWD .0625 INCH. REPAIRED AS PER HX RS NUMBER R-55-12-36662 AND EO 4455A035.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 78,592 hrs · 10,543 cycles

RIGHT BS 1140 TENSION TIE AREA ONE FASTENER HOLE CRACKED AT FAILSAFE CHORD. FAILSAFE CHORD REPAIRED AS PER SRM 51-70-12-2R AND EO 4453A216.

Part: TENSION TIE — CRACKED (FUSELAGE) · airframe 78,592 hrs · 10,543 cycles

RIGHT BS 1160 TENSION TIE AREA FOUR FASTENER HOLES CRACKED AT FRAME WEB. BS 1160 TENSION TIE HOLES OVERSIZED REPAIRED AS PER EO4453A197 AND SB 747-53A2507 REV 1.

Part: FAILSAFE — CRACKED (BS 1140) · airframe 78,592 hrs · 10,543 cycles

DURING C-CHECK, IN MARCH 2010, A CRACK WAS FOUND IN THE 65B01750-806 BS 1140, S-9R FRAME FAIL-SAFE CHORD CRACK COMMON TO THE TENSION TIE. REPAIR ANGLES WERE INSTALLED IAW SRM 51-70-12, REPAIR 1 AND NRC 503241. THE 65B01750-806 FAILSAFE CHORD IS MADE FROM BAC1503-100460, 7075-0 EXTRUSION 0.072 INCH THICK PER QQ-A-200/11 HEAT TREATED TO T6 AFTER FORMING. THE REPAIR IAW SRM 51-70-12, REPAIR 1 AND NRC 503241 CONSISTS OF (2) ANGLES 0.040 INCH THICK AND 0.050 INCH THICK MADE FROM 7075-T6 ALUMINUM AND INSTALLED USING BACB30MY6K7X HI-LOKS. THE REPAIR IAW PART 1 AND SRM 51-70-12, REPAIR 1 IS INSTALLED ON FATIGUE CRITICAL BASELINE STRUCTURE (FCBS) AND A DAMAGE TOLERANCE EVALUATION (DTE) IS NECESSARY. A DAMAGE TOLERANCE INSP (DTI) INCLUDES AN INSPECTION THRESHOLD, INSP INTERVALS, AND INSP PROCEDURES AND METHODS. IF THE DTI IS NOT AVAILABLE WHEN THE AIRPLANE RETURNS TO SERVICE, THE REPAIR IS APPROVED FOR 24 MONTHS. THIS REPAIR HAS BEEN SUBMITTED TO MFG FOR DTI ON SR 1-1561617284. EO 4453A345 DATED 22MAR10 WAS ISSUED TO PERFORM INTERIM REPAIR.

Part: FAIRING — MISSING (NR 5 CANOE) · airframe 78,525 hrs · 10,525 cycles

ON WALK AROUND, FOUND NR 5 CANOE MISSING. ALSO FOUND DAMAGE TO RT FUSELAGE SKIN AND LONGERON BOX. INSTALLED NR 5 CANOE AND OPERATIONAL CHECK OK. ALSO, ACCOMPLISHED REPAIR REF EO4453A333, FUSELAGE SECTION 44-LONGERON BOX, BS 1442.41 - BS 1480 FUSELAGE SKIN DAMAGE REPAIR AND REF EO4453A334, FUSELAGE SECTION 44-LONGERON BOX- RT BS 1480, WL 92.00, LWR FAIRING CAP DENT/CRACK REPAIR. ALSO ACCOMPLISHED EO4427A040 FLIGHT CONTROL INBD AND OTBD T/E FLAP TRACK DRIVE LINK INSPECTION.

Part: SKIN — DENTED (BS 1993) · airframe 78,213 hrs · 10,472 cycles

A DENT WAS FOUND IN THE FUSELAGE SKIN AT BS 1993 BETWEEN S-41L AND S-42L. THE DENT MEASURES 3.5 INCHES LONG BY 0.5 INCHES WIDE AND 0.020 INCHES DEEP."THE DENT WAS INSPECTED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III BUT WITHIN LIMITS FOR CONTINUED OPERATION WITH A REPETITIVE DETAILED OF HFEC INSPECTION IAW SRM 53-00-01, FIG 1010, FIG 1010. A VISUAL INSPECTION WAS COMPLETED IN VCP WITH NIL FINDINGS."

Part: WEDGE — DAMAGED (RT ELEVATOR) · airframe 77,830 hrs · 10,402 cycles

THE PURPOSE OF EO 4455A032 IS TO DOCUMENT A MAJOR REPAIR. WHILE PERFORMING A-CHECK INSP, MX REPORTED DAMAGED OF THE RT INBD HORIZ STAB ELEVATOR T/E MEASURING 2.750 IN LONG AND 3.0 IN INTO THE T/E WEDGE. (PERMANENT REPAIR ACCOMPLISHED IAW THE SRM 55-20-01 FIG 201, REPAIR 1. PREPARED, CLEANED AND REPAIRED AREA OF DAMAGE ON RT ELEVATOR INBD T/E IAW SRM 55-20-01-2R-1. PREPARED, CLEANED, MASKED, PRIMED AND PAINTED AREA OF REPAIR IAW 51-20-01-06-0)

Part: SKIN — DELAMINATED (THRUST REVERSER) · airframe 77,462 hrs · 10,336 cycles

NR 4 RH T/R COWL WITH DELAMINATION DAMAGE TO THE OUTER SKIN FROM A PREVIOUS REPAIR, LOCATED AT APPROX 2:00 POSITION. DISPOSITION WAS MADE TO PERFORM A REPAIR BY FILLING THE DAMAGED AREA WITH BMS5-28 POTTING COMPOUND OR EQUIVALENT TO CONTOUR AND APPLY (2) LAYERS OF ALUMINUM FOIL TAPE (SPEED TAPE) EXTENDING MINIMUM 2 INCHES SURROUNDING DAMAGED AREA TO RESTORE OUTER SURFACE CONTOUR AND PREVENT MOISTURE/AIR INGRESS. DVI INSPECDTIONS AFTER EVERY 1 FLIGHT CYLCE UNTIL ACCOMPLISHMENT OF PERMANENT REPAIR AT THE NEXT A CHECK.

Part: STRIP — MISSING (FAN COWL) · airframe 77,377 hrs · 10,322 cycles

THE L/E STRIP ON THE NR 3 RT FAN COWL WAS FOUND WITH APPROX 20" MISSING. "DISPOSITION WAS TO APPLY 1 LAYER OF SPEED TAPE. DVI EVERY FLIGHT CYCLE AND REPLACEMENT OF THE FAN COWL AT THE NEXT "A" CHECK".

Part: FAIRING — DAMAGED (TE FLAP) · airframe 1,292 hrs · 232 cycles

NR 6 CANOE DAMAGED. PREPARED CLEANED, AND REPAIRED DAMAGE TO CANOE IAW SRM 51-70-07-06-01.

Part: DOOR — FAILED (CABIN PRESSURE) · airframe 73,998 hrs · 9,703 cycles

LOWER PRESSURE RELIEF DOOR STATUS MESSAGE DISPLAYED WITH PACK 2 MESSAGE. DEACTIVATED LOWER PRESSURE RELIEF DOOR AND PLACED ON MEL 21-32-1

Part: UNKNOWN — ODOR (COCKPIT) · airframe 73,789 hrs · 9,666 cycles

AIR TURNBACK - LLCCAFR SWITCH IN POSITION "BOTH" TEMP SELECTED FOR 7° LOWER FORWARD , AFT MAIN DECK, FWD AND AFT. THE AIR IN THE COCKPIT WAS UNCONTROLLABLE - HIGH PRESS AIR BLOWING AROUND NAV DISPLAY - SELECTED THE LLCCAFR SWITCH OFF TO CONTROL THE TEMP IN THE COCKPIT CAUSED A BURST OF MIST COMING FROM AND AROUND ALL NAV DISPLAYS & MCP PANEL. THE COCKPIT FILLED WITH A STRONG ODOR OF OVERHEAT. LOST EICAS DISPLAYS AND PFDS.

Part: SKIN — DAMAGED (CARGO DOOR)

DURING C-CHECK FORWARD CARGO DOOR EXTERNAL SURFACE SPLICE AREA FOUND 1 EA LIGHTNING STRIKE AT UPPER AFT SIDE OF MASTER LOCK HANDLE. REPAIRED AREA AS PER EO 4452A047. (S)

Part: INTERCOSTAL — CRACKED (BS 360-380)

DURING C-CHECK UPPER DECK STATION 360-380 RBL 28 INTERCOSTAL CHANNEL FOUND CRACKED. REPLACED CHANNEL AS PER SRM 51-10-02 AND INTERCOSTAL AS PER SRM 51-40-02. (S)

Part: SKIN — SCRATCHED (BS 2080 S26-27R)

DURING C-CHECK FOUND FUSELAGE SKIN WITH DEEP SCRATCH AT STATION 2080 STR 26-27R. REPAIRED AS PER SRM 53-00-01 FIGURE 201. (S)

Part: SKIN — DAMAGED (BS 520-540)

DURING C-CHECK FOUND FORWARD CARGO COMPARTMENT STATION 520-540-STR 34-35L SKIN DAMAGED. SKIN REPAIRED AS PER SRM 53-00-01 FIGURE 201. (S)

Part: SKIN — CRACKED (FUSELAGE)

DURING C-CHECK AFT CARGO DOOR CUTOUT FORWARD UPPER CORNER FOUND CRACKED AT FASTENER HOLE. REPAIRED AS PER SRM 53-60-01 FIGURE 201. (S)