N963WN

Part: SIGN — BROKEN (ZONE 200) · airframe 42,022 hrs · 25,859 cycles

MID CABIN OVERHEAD EXIT SIGN BROKE<[01] REPLACED MID CABIN OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY PER AMM 33-51-01. OPS GOOD.

Part: ENGINE — POWER LOSS (NR 1) · airframe 42,022 hrs · 25,858 cycles

#! ENGINE ROLLED BACK DURING TAKE AT 15 INDICATED. ABORTED TAKE OFF RETURNED TO GATE<[01] C/W EEC BITE; NO FAULTS FOUND; PREFORMED POWER ASSURANCE RUN NO DEFECTS NOTED IAW FIM 73-05 TASK 808

Part: LENS — DISLODGED (ZN 200 FUS TOP) · airframe 40,569 hrs · 24,956 cycles

CREW REPORTS MID CABIN EXIT SIGN LENS DISLODGED<[01] RESECURED LENS PER AMM 33-51-01

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 40,073 hrs · 24,664 cycles

EMX BATT PACK M01674 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATT PACK M01674 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 40,073 hrs · 24,664 cycles

EMX BATT PACK M01675 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATT PACK M01675 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 40,073 hrs · 24,664 cycles

EMX BATT PACK M01673 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX BATT PACK M01673 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Part: HANDLE — LOOSE (ZN 200 FUS TOP) · airframe 38,436 hrs · 23,643 cycles

FORWARD SERVICE DOOR HANDLE LOOSE<[01] FOUND LOOSE HANDLE CAM NUT REF IPC 52-41-00-10B ITEM 40. RE TORQUED FASTENER PER AMM 20-50-11. REMOVED AND RE INSTALLED FWD SERVICE DOOR LINE PER AMM 52-41-31. OPERATIONAL TEST PER AMM 52-41-00. OPS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1670 ARE INOP<[01] REPLACED POWER SUPPLY - BATTERY PACK M1670 PER AMM 33-51-06-960-805. GOOD TEST.;[02] PARTS UPDATED.;[03] VERIFIED CORRECTIVE ACTIONS 1-2

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1672 ARE INOP<[01] REPLACED POWER SUPPLY - BATTERY PACK M1672 PER AMM 33-51-06-960-805. GOOD TEST.;[02] SIGNED FOR PART REMOVAL/INSTALLATION.;[03] VERIFIED CORRECTIVE ACTIONS 1-2.

Part: HANDLE — BROKEN (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

FWD ENTRY DOOR HANDLE COVER RETAINER IS BROKEN. R & R FWD ENTRY DOOR HANDLE COVER RETAINER PER SOPM 20-50-01.

Part: LIGHT — DAMAGED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

R/H OVERWING EMERGENCY EXIT SIGN LIGHT WIRING PINS PULLED OUT OF CONNECTOR ON SIDEWALL PANEL 232YJW<[01] CORRECTION TO TTG8Q00LUCRJ SHOULD SAY L/H OVERWING EMERGENCY EXIT LIGHT WIRING PINS PULLED OUT OF CONNECTOR ON SIDEWALL PANEL 231YJW.;[02] L/H OVERWING EMERGENCY EXIT LIGHT REPINED THE CONNECTOR ON SIDEWALL PANEL 232YJW IAW SWPM 20-64-17.;[03] VERIFIED ACTION 2 IS COMPLETE;[04] VERIFIED CORRECTIVE ACTIONS 1 & 2.

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

STOWAGE COMPARTMENT SLIDE RETAINER BELOW 1ST OBSERVERS SEAT IS BROKEN<[01] STOWAGE COMPARTMENT SLIDE RETAINER BELOW 1ST OBSERVERS SEAT WAS REPLACED IAW IPC 25-11-00-19 AND SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION 1

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

FWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] WELDED RADIUS OF FWD CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARAGRAPH 4.B. (2) AND (4)<BR>EQUIPMENT USED: WELDING MACHINE E10583; CALIBRATION DUE DATE 01/2024;[02] VERIFIED CORRECTION ACTION ITEM 1.;[03] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-RADIOMETER ID: ATS2561-1; 2; 3 CAL DUE: 08/23;[04] SANDED WELD REPAIR PER SRM 53-30-15-2R-1 PARAGRAPH 4.B.(5);[05] VERIFIED CORRECTIVE ACTION 4;[06] FWD CARGO BAY FWD CORNER SCUFF PLATE INSTALLED ON FAULT TTG8Q002QYDS;[07] VERIFIED CORRECTIVE ACTION 6

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

CRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS535 S-23R WL164. MARKED<[01] VERIFIED APPLICABILITY OF SRM 53-00-03-2R-1 REPAIR 1 - REPAIR FOR A TYPE I; TYPE II; OR TYPE IV FUSELAGE STRINGER;[02] ACCOMPLISHED CUT-OUT AND REMOVAL OF DAMAGE IAW SRM 53-00-03-2R-1 REPAIR 1 PART 4.A-B;[03] REQUEST FOR NDI HFEC INSPECTION ON REPAIR AREA IAW SRM 53-00-03-2R-1 REPAIR 1 PART 4.C;[04] HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. TOOL ATS1465 DUE 09/2023.;[05] VERIFIED CORRECTIVE ACTIONS 1 AND 2.;[06] UPDATED PARTIAL STEPS 1 AND 2;[07] FABRICATED AND DRILLED NEW STRINGER SECTION HFAB53-STR-011 CUSTOMER RO 924301-SWA-3 AND HAT SECTION HFAB53-HC-011 CUSTOMER RO NO 924301-SWA-1; APPLIED CHEMICAL CONVERSION COATING LAYER IN THE REPAIR PARTS I.A.W SRM 53-00-03-2R-1 AND SRM 51-20-01. OK TO PRIME REPAIR PARTS;

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

CRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS535 S-23L WL164. MARKED<[01] VERIFIED APPLICABILITY OF SRM 53-00-03-2R-1 REPAIR 1 - REPAIR FOR A TYPE I; TYPE II; OR TYPE IV FUSELAGE STRINGER;[02] ACCOMPLISHED CUT-OUT AND REMOVAL OF DAMAGE IAW SRM 53-00-03-2R-1 REPAIR 1 PART 4.A-B;[03] REQUEST FOR NDI HFEC INSPECTION ON REPAIR AREA IAW SRM 53-00-03-2R-1 REPAIR 1 PART 4.C;[04] HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. TOOL ATS1465 DUE 09/2023.;[05] VERIFIED CORRECTIVE ACTIONS 1 AND 2.;[06] UPDATED PARTIAL STEPS 1 AND 2;[07] RECEIVED STRINGER SECTION HFAB53-STR-011 LOT#1531111-3; HEAT TREATED AND PENETRANT INSPECTED WITH CUSTOMER RO NO 924319-SWA-3; AND HAT SECTION HFAB53-HC-011 LOT#1531115-1 WITH CUSTOMER RO NO 9243134-SWA-1;;BOTH REPAIR PARTS LOCATED AND DRILLED AT BS 500D+7 TO BS 538 STR 23L IAW SRM 53-00-03-2R-0 REPAIR-1 OK TO TREAT AND PRIME;[08] VERIFIED CORRECTIVE ACTION 7. OKAY TO TREAT AND APPLY PRIMER.;[09] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON REPAIR PARTS PER REF SRM 51-20-01 AND SOPM20-41-02 <BR><BR>OK TO INSTALL NEW SECTION AND REPAIR PART;[10] OKAY TO INSTALL NEW SECTION AND REPAIR PART.;[11] COMPLETED STEP 1 AND 2;[12] RII VERIFIED CORRECTIVE ACTION ITEM 11.;[13] 'THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 23-153-01892';[14] VERIFIED CORRECTIVE ACTION 13;[15] VERIFIED MEASUREMENT TABLE

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

CRACKED STRINGER END AT AREA AFT OF FWD CARGO BAY BS535 S-25R WL156. ACCOMPLISHED CUT-OUT AND REMOVAL OF DAMAGE IAW SRM 53-00-03-2R-1 REPAIR 1 PART 4.A-B;[03] REQUEST FOR NDI HFEC INSPECTION ON REPAIR AREA IAW SRM 53-00-03-2R-1 REPAIR 1 PART 4.C. HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. LOCATED & DRILLED ALL PARTS IAW SRM 53-00-03-2R-1 REPAIR 1 & EA 23-153-01891. CHEMICAL TREATED & PRIMED ALL REPAIR & REWORK AREA IAW SRM 51-20-01-0G-0 & SOPM 20-41-02. INSTALLED.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT STATIONS: 767+18; 787+2; 787+5; 787+6; 787+8; 787+15; LBL 22; WL 156.<[01] PARTIAL UPDATED ON STEPS 1 - 6.;[02] VERIFIED APPLICABILITY OF SRM 53-00-53-1A-2;[03] VERIFIED PARTIAL STEPS 1-6; MEASUREMENT TABLE; AND CORRECTIVE ACTION 2;[04] THIS FAULT WILL BE ACCOMPLISHED ON CARD NUMBER TTG8Q00LHMM5.<BR>COMPLETED ALL MAINTENANCE ACTIONS.;[05] VERIFIED STEPS 1-6<BR>VERIFIED CORRECTIVE ACTION 4.

Part: STRINGER CLIP — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED STRINGER CLIP AT PASSENGER CABIN BS727C S-6L. MARKED<[01] REMOVED STRINGER CLIP BS 727C; S-6L PER SRM 51-40-02.<BR><BR>ALLOWABLE DAMAGE LIMITS ENTRIES NOT FOUND IN SRM FOR THIS ITEM. STRINGER CLIP WILL BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9;[02] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02. AND DWG NBR 144A1107;[03] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02. AND DWG NBR 146A1103;[04] ITEM 3-CHANGED DWG NUMBER;[05] VERIFIED CORRECTIVE ACTION #3.<BR>VERIFIED MEASUREMENTS.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT STATIONS: 727+2; 727+6; 727C+7; 727C+11; 727C+19; 727D+3; 727D+5; 727D+6; 727D+8; 727D+10; LBL 22; WL 156.<[01] VERIFIED SRM 53-60-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.;[02] ALL STEPS COMPLETED;[03] THIS FAULT WILL BE ACCOMPLISHED ON CARD NUMBER TTG8Q00LHMM5.<BR>COMPLETED ALL MAINTENANCE ACTIONS.;[04] VERIFIED STEPS 1-10; CORRECTIVE ACTIONS 1-3<BR>VERIFIED MEASUREMENT TABLE<BR>VERIFIED SRM APPLICABILITY.

Part: WEB — CORRODED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

CORROSION ON AFT CARGO BAY DOOR CUT-OUT SUB-THRESHOLD WEB AT STA 787+16; 807+10 & +12; 827+6; & +9; WL 156; RBL 27<[01] VERIFIED SRM 53-60-15-0I-1 FOR IDENTIFICATION AND SRM 53-60-15-1A-1 FOR ALLOWABLE DAMAGE.05] LOCATED AND DRILLED NEW ACB DOOR CUT-OUT SUB-THRESHOLD WEB IAW SRM 51-40-05-0G-0 AND DWG#146A8340.;[06] VERIFIED STEP # 5;[07] OK TO ENAMEL;[08] COMPLETED STEPS 1-5; VERIFIED CORRECTIVE ACTION 7 OK TO ENAMEL;[09] APPLIED ONE COAT OF BMS10-11 TYPE II ENAMEL (P/N BAC702GL) AT SUB-THRESHOLD WEB BS 794.37- BS 847 RBL27 WL156 IAW SOPM 20-41-02.<BR>OK TO APPLICATION CIC;[10] VERIFIED CORRECTIVE ACTION 9; OK TO APPLICATION CIC;[11] APPLIED ONE LAYER OF BMS 3-23; TYPE II COMPOUND INHIBITING CORROSION BS794.367 TO BS 847 RBL 27 WL 156 I.A.W SRM 51-20-01.<BR>TIME OF APPLICATION :15-JUN-2023 21:44 UTC;[12] OK TO INSTALL;[13] VERIFIED CORRECTIVE ACTION 11 AND 12; OK TO INSTALL.;[14] INSTALLED ON AFT CARGO BAY DOOR CUT-OUT SUB-THRESHOLD WEB AT BS 794.36 TO BS 847 RBL 27 IAW SRM 51-40-02 AND DWG 146A8340;[15] VERIFIED CORRECTIVE ACTION 14<BR><BR>VERIFIED MEASUREMENT TABLE;[16] JOB COMPLETE

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

CORROSION ON AFT CARGO BAY CUT-OUT FWD SHIELD FROM STA 767+2 TO STA 767+17; RBL 21 TO RBL 23; WL 156.<[01] DAMAGE FOUND AT AFT CARGO BAY FLOOR SUPPORT FWD SHIELD BS 767 TO BS 794; RBL 22; WL 156 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT STATEMENT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARE.9C;[02] REMOVED ON AFT CARGO CUT OUT FWD SHIELD;IAW SRM 51-40-02.;[03] RECEIVED NEW ON AFT CARGO BAY CUT-OUT FWD SHIELD BS 767 TO BS 793 RBL23 P/N146A8127-12 PO#910166. LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 146A0081;[04] VERIFIED CORRECTIVE ACTION STEP #3. OK TO CONTINUE;[05] APPLIED TOP-COAT FINISH PAINT BMS10-11 TYPE2 ON NEW SHIELD IAW AMM 51-21-73-370-804;[06] UPDATE ITEM 5: TOP-COAT FINISH PAINT BMS10-11 TYPE2 APPLICATION TIME 15-JUN-2023 03:44 UTC;[07] VERIFIED STEPS #5 AND #6;[08] APPLIED CORROSION INHIBITING COMPOUND ON NEW SHIELD IAW AMM 51-21-91-620-802.<BR>15-JUN-2023 06:07 UTC;[09] VERIFIED STEP # 8;[10] OK TO INSTALL ON ACB FWD SHIELD BS 767 TO BS 793 RBL 21-23 WL 156;[11] VERIFIED CORRECTIVE ACTION 10 OK TO INSTALL;[12] INSTALLED ON AFC FWD SHIELD FROM<BR>BS 767 TO BS 793 RBL 21-23 WL 156 IAW SRM 51-40-02<BR>AND DWG 146A0081.;[13] VERIFIED CORRECTIVE ACTION 12 <BR><BR>VERIFIED MEASUREMENT TABLE

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT STATIONS: 727A+6; 727B+10; 727B+14; 727C+6; 727C+14; 727D+7; 727E+2; 727E+10; 727E+14; 727E+18; RBL 22; WL 156.<[01] PARTIALLY COMPLETED STEPS 1-10;[11] VERIFIED CORRECTED ACTION STEP 10. OK TO CONTINUE.;[12] APPLIED TOP-COAT FINISH PAINT BMS10-11 TYPE2 ON NEW FLOOR TO SIDEWALL SUPPORT IAW AMM 51-21-73-370-804; 15-JUN-2023 03:49 UTC;[13] VERIFIED STEP 12;[14] APPLIED CORROSION INHIBITING COMPOUND ON NEW FLOOR TO SIDEWALL SUPPORT IAW AMM 51-21-91-620-802.<BR>15-JUN-2023 06:07 UTC;[15] VERIFIED STEP #14;[16] OK TO INSTALL AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 767 RBL 22 WL 156;[17] INSPECTED AREA; OK TO INSTALL; STEP #16;[18] INSTALLED AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO BS 767 RBL 22 WL 156 IAW SRM 51-40-02-0G-0 AND DWG#146A7500;[19] VERIFIED STEP 18

Part: STRINGER CLIP — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED STRINGER CLIP AT PASSENGER CABIN BS706 S-4L. MARKED<[01] REMOVED STRINGER CLIP BS 706; S-4L PER SRM 51-40-02.<BR><BR>ALLOWABLE DAMAGE LIMITS ENTRIES NOT FOUND IN SRM FOR THIS ITEM. STRINGER CLIP WILL BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9;[02] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02. AND DWG NBR 144A1107;[03] VERIFIED CORRECTIVE ACTION ITEM 2.;[04] CONCUR WITH APPLICABILITY OF SRM 51-10-02-0G-0.<BR>VERIFIED MEASUREMENT TABLE COMPLETED.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT STATIONS: 727D+14; 727E+6; 727E+8; 727E+10; 727E+14; 727E+15; 727E+18; 747+2; 747+6; 747+10. CORRECTION: LBL 22 WL 156<[01] PARTIAL UPDATED ON STEPS 1 - 10;[02] VERIFIED APPLICABILITY OF SRM 53-00-53-1A-2.;[03] VERIFIED PARTIAL STEPS 1-10; CORRECTIVE ACTION 2; AND MEASUREMENT TABLE;[04] RESOLUTION OF FAULTS: TTG8Q00LHNCG; TTG8Q00LHMJV; TTG8Q00LHP1C; TTG8Q00LHP1C; TTG8Q00LHNCG; TTG8Q00LHMJV TO BE ACCOMPLISHED ON THIS FAULT.;[05] REMOVED AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 727 TO 847 I.A.W SRM 51-40-02-0G-0.;[06] FABRICATED AND DRILLED NEW AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS727-BS847 LBL22 WL 156 AND NEW SPLICE REPAIR WITH NEXT MATERIAL BAC1496-377#7075T62 LOT 1526048-1 I.A. W SRM 51-40-05-0G-0; SRM 53-00-53-2R-6 REPAIR 6 AND DWG 146A7502; APPLIED CHEMICAL CONVERSION COATING TO THE REPAIR PARTS I.A. W SRM 51-20-01. OK TO PRIME.;[07] VERIFIED CORRECTIVE ACTION 5 AND 6 OK TO PRIME<BR><BR>COMPLETED STEPS 1-10;[08] APPLIED PRIMER ON FLOOR TO SIDEWALL SUPPORT IAW SOPM 20-41-02.<BR>OK TO INSTALL SPLICE BS 747+10;[09] VERIFIED CORRECTIVE ACTION 8 OK TO INSTALL;[10] INSTALLED ON FLOOR TO SIDEWALL SUPPORT SPLICE SIDEPLATE BS747+10 IAW SRM 53-00-53-2R-6 REPAIR 6;[19] INSTALLED FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 847 LBL22 WL 156 IAW SRM 51-40-02 AND DWG 146A7502.;[20] VERIFIED STEP #19. OK FOR SERVICE

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT STATIONS: 747+14; 747+15; 747+16; 747+18; 767+3; 767+5; 767+7; 767+10; 767+14; 767+16; RBL 22; WL 156. CORRECTION: BUT LINE IS LEFT BUTT LINE 22<[01] PARTIALLY COMPLETED STEPS 1- 10;[02] REJECTION OF PARTIAL STEPS 1-10: CORROSION IS LOCATED AT LBL 22 NOT RBL 22; SEE CORRECTION IN TASK DESCRIPTION. CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL22 FROM BS 747+14 TO 767 TO BE ADDRESSED ON TTG8Q00LHN9J; AND AFT CARGO BAY CUTOUT FWD SHIELD AT RBL 22 FROM BS 767 TO 767+16 ON TTG8Q00LHMCJ;[03] PARTIALLY COMPLETED STEPS 1- 10;[04] THIS FAULT WILL BE ACCOMPLISHED ON CARD NUMBER TTG8Q00LHMM5.<BR>COMPLETED ALL MAINTENANCE ACTIONS.;[05] VERIFIED CORRECTION TO STEPS 1-10.<BR>VERIFIED MEASUREMENTS TABLE.<BR>VERIFIED CORRECTIVE ACTION 4.

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

CORROSION ON AFT CARGO BAY DOOR CUT-OUT AFT SHIELD AT STA 847+18; RBL 22; WL 156.<[01] DAMAGE FOUND AT AFT CARGO BAY FLOOR SUPPORT FWD SHIELD BS 767 TO BS 864; RBL 22; WL 156 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT STATEMENT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARE.9C;[02] REMOVED AFT CARGO CUT OUT AFT SHIELD;IAW SRM 51-40-02.;[03] RECEIVED NEW ON AFT CARGO BAY DOOR CUT-OUT SHIELD BS 847 TO BS867 RBL 22 P/N146A8127-10 PO#908098 LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG146A0081;[04] VERIFIED CORRECTIVE ACTION STEP #3. OK TO CONTINUE.;[05] APPLIED TOP-COAT FINISH PAINT BMS10-11 TYPE2 ON NEW SHIELD IAW AMM 51-21-73-370-804; 15-JUN-2023 03:47 UTC;[06] VERIFIED CORRECTIVE ACTION STEP 5;[07] APPLIED CORROSION INHIBITING COMPOUND ON NEW SHIELD IAW AMM 51-21-91-620-802.<BR>15-JUN-2023 06:07 UTC;[08] VERIFIED STEP # 7;[09] OK TO INSTALL ON ACB SHIELD BS 847 TO BS 867 RBL 22 WL 156;[10] VERIFIED CORRECTIVE ACTION 9; OK TO INSTALL;[11] INSTALLED ON ACB AFT SHIELD FROM<BR>BS 847 TO BS 867 RBL 22 WL 156 <BR>IAW SRM 51-40-02 AND DWG 146A0081.;[12] VERIFIED CORRECTIVE ACTION 11<BR><BR>VERIFIED MEASUREMENT TABLE

Part: STRINGER CLIP — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED STRINGER CLIP AT PASSENGER CABIN BS706 S-5L. MARKED<[01] REMOVED STRINGER CLIP BS 706; S-5L PER SRM 51-40-02.<BR><BR>ALLOWABLE DAMAGE LIMITS ENTRIES NOT FOUND IN SRM FOR THIS ITEM. STRINGER CLIP WILL BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9;[02] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02. AND DWG NBR 144A1107;[03] VERIFIED CORRECTIVE ACTION ITEM 2.;[04] CONCUR WITH APPLICABILITY OF SRM 51-10-02-0G-0.<BR>VERIFIED MEASUREMENT TABLE COMPLETED.

Part: STRINGER CLIP — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED STRINGER CLIP AT PASSENGER CABIN BS727C S-5R. MARKED<[01] REMOVED STRINGER CLIP BS 727C; S-5R PER SRM 51-40-02.<BR><BR>ALLOWABLE DAMAGE LIMITS ENTRIES NOT FOUND IN SRM FOR THIS ITEM. STRINGER CLIP WILL BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9;[02] REMOVED AND REPLACED STRINGER CLIP AT PASSENGER CABIN BS727C S-5R IAW SRM 51-40-02-0G-0 AND DWG#146A1103.;[03] VERIFIED CORRECTIVE ACTION #2.<BR>VERIFIED MEASUREMENTS.

Part: STRINGER CLIP — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED STRINGER CLIP AT PASSENGER CABIN BS727D S-7L. MARKED<[01] REMOVED STRINGER CLIP BS 727D; S-7L PER SRM 51-40-02.<BR><BR>ALLOWABLE DAMAGE LIMITS ENTRIES NOT FOUND IN SRM FOR THIS ITEM. STRINGER CLIP WILL BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9;[02] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02. AND DWG NBR 144A1107;[03] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02. AND DWG NBR 146A1111;[04] ITEM 3-CHANGED DWG NUMBER;[05] VERIFIED CORRECTIVE ACTION #3.<BR>VERIFIED MEASUREMENTS.

Part: STRINGER CLIP — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED STRINGER CLIP AT PASSENGER CABIN BS727B S-6L. MARKED<[01] REMOVED STRINGER CLIP BS 727B; S-6L PER SRM 51-40-02.<BR><BR>ALLOWABLE DAMAGE LIMITS ENTRIES NOT FOUND IN SRM FOR THIS ITEM. STRINGER CLIP WILL BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9;[02] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02. AND DWG NBR 144A1107;[03] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02. AND DWG NBR 146A1102;[04] ITEM 3 - CHANGED DWG NUMBER;[05] VERIFIED CORRECTIVE ACTION #3.<BR>VERIFIED MEASUREMENTS.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT STATIONS: 747+2; 747+3; 747+5; 747+10; 747+11; 747+14; 747+17; 747+18; RBL 22; WL 156<[01] PARTIALLY COMPLETED STEPS 1-8;[02] VERIFIED APPLICABILITY OF SRM 53-60-53-01-2 FOR ALLOWABLE LIMIT AND SRM 53-00-53-1A-2 FOR ALLOWABLE LIMIT;[03] VERIFIED PARTIAL STEPS 1-8;[04] CORRECTION ON CORRECTIONS ACTION 2 VERIFIED APPLICABILITY OF SRM 53-60-53-01-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE LIMIT;[05] VERIFIED CORRECTIVE ACTION 4 AND MEASUREMENT TABLE;[06] THIS FAULT WILL BE ACCOMPLISHED ON CARD#TTG8Q00LHMEV.<BR>COMPLETED ALL MAINTENANCE ACTION.;[07] VERIFIED CORRECTIVE ACTION STEP #6;[08] VERIFIED STEP ! COMPLETE.;[09] VERIFIED STEP ! COMPLETE.

Part: STRINGER CLIP — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED STRINGER CLIP AT PASSENGER CABIN BS727B S-7L. MARKED<[01] REMOVED STRINGER CLIP BS 727B; S-7L PER SRM 51-40-02.<BR><BR>ALLOWABLE DAMAGE LIMITS ENTRIES NOT FOUND IN SRM FOR THIS ITEM. STRINGER CLIP WILL BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9;[02] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02. AND DWG NBR 144A1107;[03] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02. AND DWG NBR 146A1102;[04] VERIFIED CORRECTIVE ACTION #3.<BR>VERIFIED MEASUREMENTS.

Part: STRINGER CLIP — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED STRINGER CLIP AT PASSENGER CABIN BS807 S-10R. MARKED<[01] REMOVED STRINGER CLIP BS 807; S-10R PER SRM 51-40-02.<BR><BR>ALLOWABLE DAMAGE LIMITS ENTRIES NOT FOUND IN SRM FOR THIS ITEM. STRINGER CLIP WILL BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9;[02] REMOVED AND REPLACED STRINGER CLIP AT PASSENGER CABIN BS807 S-10R IAW SRM 51-40-02-0G-0 AND DWG#146A1134.;[03] VERIFIED CORRECTIVE ACTION #2.<BR>VERIFIED MEASUREMENTS.

Part: FRAME — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

L1 DOOR CUTOUT UPPER 312 FRAME HAS A SMALL CRACK. L1 DOOR CUTOUT UPPER 312 FRAME HAS A SMALL CRACK. MARKED. BS 312 LBL 36 WL 282.1 LBL 36.<[01] REMOVED CRACK ON FRAME AT BS 312 LBL 33 WL 296 REWORKED AREA L=1.5 X W=0.040 IAW EA M-22-153-01244;[02] VERIFIED ACTION 1;[03] ALL STEPS COMPLETE;[04] COMPLETED ALL STEPS;[05] VERIFIED MEASUREMENT TABLE AND CORRECTIVE ACTION 4;[06] REPAIRED L1 DOOR CUTOUT UPPER FRAME BS 312 IAW EA: M-22-153-01244;[07] VERIFIED CORRECTIVE ACTION 6

Part: STRINGER CLIP — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

STRINGER CLIPS 5L & 6L ARE CRACKED AT BS 727D<[01] VERIFY END OF CRACK AT STRINGER CLIP BS 727D; S-5L;[02] ACCOMPLISHED HFEC SURFACE SCAN IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. NO CRACKS NOTED.<BR><BR>EQUIPMENT USED: NORTEC 600 ID: ATS1465 CAL DUE: 09/2023;[03] REMOVED STRINGER CLIP BS 727D; S-6L ONLY PER SRM 51-40-02.<BR><BR>ALLOWABLE DAMAGE LIMITS ENTRIES NOT FOUND IN SRM FOR THIS ITEM. STRINGER CLIP WILL BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9;[04] INSTALLED NEW STRINGER CLIP STR 6L PER SRM 51-40-02. AND DWG NBR 144A1107;[05] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02. AND DWG NBR 146A1111;[06] ITEM 4 CHANGED DWG NUMBER;[07] VERIFIED CORRECTIVE ACTION #1; #3; #5.;[08] VERIFIED MEASUREMENTS.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

AFT CARGO BAY FWD SCUFF PLATE IS CRACKED<[01] WELDED RADIUS OF AFT CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2) AND (4)<BR>EQUIPMENT USED: WELDING MACHINE E10583; CALIBRATION DUE DATE 01/2024;[02] VERIFIED CORRECTION ACTION ITEM 1.;[03] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-RADIOMETER ID: ATS2561-1; 2; 3 CAL DUE: 08/23;[04] SANDED WELD REPAIR AREA PER SRM 53-60-15-2R-1 PARAGRAPH 4.B (5);[05] VERIFIED CORRECTIVE ACTION 4.;[06] AFT CARGO BAY FWD SCUFF PLATE INSTALLED ON FAULT TTG8Q00LGU43;[07] VERIFIED CORRECTIVE ACTION 6

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED INTERCOSTAL AT FWD CABIN BS344+5 RBL32 WL208.<[01] REMOVED INTERCOSTAL FROM BS344-BS360 AT RBL 32 WL 208 IAW SRM 51-40-02;[02] DAMAGE FOUND AT FWD CABIN INTERCOSTAL BS344+5; RBL32; WL208; FOUND TO BE OUT OF LIMIT IAW SRM 53-1-51-1A-1 DET.4B(1A); FIG 105-N;[03] LOCATED AND DRILLED NEW INTERCOSTAL P/N 141A5410-25; LOT#1530390-1 AT BS344 TO BS 360; RBL32; WL208 IAW SRM 51-40-05-0G-0 AND DWG# 141A5400.OK TO INSTALL;[04] VERIFIED STEP #3;[05] INSTALLED INTERCOSTAL FROM BS344-BS360 AT RBL 25 WL 208 IAW SRM 51-40-02 AND IAW DGW#141A5400;[06] VERIFIED INSTALLATION AND MEASUREMENT TABLE

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED INTERCOSTAL AT FWD CABIN BS344+9 LBL11 WL208.<[01] REMOVED INTERCOSTAL FROM BS344-BS360 AT LBL 11 WL 208 IAW SRM 51-40-02;[02] DAMAGE FOUND AT FWD CABIN INTERCOSTAL BS344+9; LBL11; WL208; FOUND TO BE OUT OF LIMIT IAW SRM 53-1-51-1A-1 DET.4B(1A); FIG 105-N;[03] LOCATED AND DRILLED NEW INTERCOSTAL P/N 141A5410-148; LOT#1530397-1 AT BS344 TO BS 360; LBL11; WL208 IAW SRM 51-40-05-0G-0 AND DWG# 141A5400.OK TO INSTALL;[04] VERIFIED STEP #3;[05] INSTALLED INTERCOSTAL FROM BS344-BS360 AT LBL 11 WL 208 IAW SRM 51-40-02 AND IAW DGW#141A5400;[06] VERIFIED INSTALLATION AND MEASUREMENT TABLE

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED INTERCOSTAL AT FWD CABIN BS344+9 BL0 WL208.<[01] REMOVED INTERCOSTAL FROM BS344-BS360 AT BL0 WL 208 IAW SRM 51-40-02;[02] DAMAGE FOUND AT FWD CABIN INTERCOSTAL BS344+9; BL0; WL208; FOUND TO BE OUT OF LIMIT IAW SRM 53-1-51-1A-1 DET.4B(1A); FIG 105-N;[03] LOCATED AND DRILLED NEW INTERCOSTAL P/N 141A5410-23; LOT#1530388-1 AT BS344 TO BS 360; BL0; WL208 IAW SRM 51-40-05-0G-0 AND DWG# 141A5400.OK TO INSTALL;[04] VERIFIED STEP #3.;[05] INSTALLED INTERCOSTAL FROM BS344-BS360 AT BL 0 WL 208 IAW SRM 51-40-02 AND IAW DGW#141A5400;[06] VERIFIED INSTALLATION AND MEASUREMENT TABLE

Part: PANEL — DEBONDED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

PANEL 193D OUTER SKIN IS DISBONDED. (MARKED)<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-40-70-0I-1 FIG 2 TABLE 2 ITEM 12.<BR>FOUND DAMAGE TO 2EA AREAS TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.A(6).<BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-05-2R-2 PER SRM 53-40-70-2R-1 TABLE 201.<BR>REMOVED DAMAGED SKIN AND CORE TO 1.0' DIAMETER IN 2EA LOCATIONS; CLEANED REPAIR AREA IAW SRM 51-70-05-2R-2 PARA 4.A-C.;[02] VALIDATED APPLICABILITY OF SRM 51-70-05-2R-2.;[03] INSPECTED PANEL. OK TO CONTINUE;[04] APPLIED POTTING BMS 5-28TY7 LOT#AK2JP8360K TO OPEN CORE AND SET FOR ROOM TEMPERATURE CURE IAW SRM 51-70-05-2R-2 PARA 4.D(NOTE) AND SRM 51-70-05-2R-11 PARA 4.A-B.;[05] COMPLETED ROOM TEMPERATURE POTTING CURE; SANDED SMOOTH TO SURFACE; CLEANED REPAIR AREA; FABRICATED AND INSTALLED REPAIR PLIES USING BMS 8-79ST120 LOT#1529520-2; ADHESIVE BMS 5-129GR5 LOT#1529514-3; VACUUM BAGGED; LEAK CHECK GOOD; CURED; UNBAGGED AND LIGHTLY SANDED REPAIRS IAW SRM 51-70-05-2R-11 PARA 4.C-E AND SRM 51-70-05-2R-2 PARA 4.G-I; K.<BR><BR>REQUEST POST CURE NDI IAW SRM 51-70-05-2R-2 PARA 4.J.

Part: PANEL — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

AREA ABOVE WING BOX CENTER SECTION HAS CRACKED BREAK PANEL AT BS 540; RBL 1; WL 207<[01] REMOVED BREAK PANEL AT BS540 FROM RBL1-RBL25 IAW SRM 51-40-02;[02] LOCATED AND DRILLED NEW BREAK PANEL AT BS 540; RBL 1; WL 207 IAW SRM 51-40-05-0G-0 AND DWG 143A5240; OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION 2.<BR>OK TO INSTALL;[04] INSTALLED NEW BREAK PANEL AT BS 540; RBL 1; WL 207 IAW SRM 51-40-02-0G-0 AND DWG 143A0060; CARD IS COMPLETED;[05] VERIFIED CORRECTIVE ACTION 4;[06] VERIFIED MEASUREMENT TABLE

Part: FLOORBEAM — CORRODED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

CORROSION ON FLOOR BEAM AT FWD CABIN BS328 RBL40 WL208.<[01] VERIFIED THE APPLICABILITY OF SRM 53-10-51-0I-2 AND SRM 53-10-51-1A-1[15] FABRICATED FOR BS 328 FLOOR BEAM UPPER CHORD -1 T-CHORD FROM BAC1505-100224 7050-T76511 EXTRUSION LOT #1530415-1 ; FABRICATED -2 (2EA) ANGLES FROM BAC 1490-2811 7075-T6 CLAD FORMED ANGLE LOT #1498610-1 ; FABRICATED -3 (2EA) ANGLES FROM BAC 1490-2900 7075-T6 CLAD FORMED ANGLE LOT # 1519553-1 ; FABRICATED -4 SHIMS (9EA) FROM 7075-T6 CLAD SHEET 0.100' LOT# 1489800-1 ; AND FABRICATED -4 SHIMS FOR THE INITIAL STIFFENERS THAT IS IN-LINE WITH THE REPAIR SPLICE ANGLES AT THE FWD SIDE FROM 7075T6 CLAD 0.071' LOT #1478276-1 AND FROM 7075T6 CLAD 0.080' LOT # 1492623-1 .<BR>AND FABRICATED PARTS FOR THE MACHINED INTERCOSTAL ATTACHED TO THE FLOOR BEAM AT BL 24.82 -4 SHIMS (2EA) FROM 7075-T6 CLAD SHEET 0.020' LOT # 1516841-1 ; -5 ANGLE FROM BAC 1490-2651 7075-T6 CLAD FORMED ANGLE LOT # 1483887-1 AND FABRICATED -6 FILLER FROM 7075-T6 CLAD SHEET 0.020' LOT # 1516841-1 ; LOCATED AND DRILLED ALL REPAIR PARTS IAW SRM 53-10-51-2R-7 REPAIR 7 ; OK TO TREAT AND PRIME ALL REWORKED AREARS AND REPAIR PARTS;

Part: PANEL — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

AREA ABOVE WING BOX CENTER SECTION HAS CRACKED BREAK PANEL AT BS 540; LBL 1; WL 207<[01] REMOVED BREAK PANEL AT BS540 FROM LBL0-LBL25 IAW SRM 51-40-02;[02] LOCATED AND DRILLED NEW BREAK PANEL AT BS 540; LBL 1; WL 207 IAW SRM 51-40-05-0G-0 AND DWG 143A5240; OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION 2.<BR>OK TO INSTALL;[04] INSTALLED NEW BREAK PANEL AT BS 540; LBL 1; WL 207 IAW SRM 51-40-02-0G-0 AND DWG 143A0060; CARD IS COMPLETED;[05] VERIFIED CORRECTIVE ACTION 4;[06] VERIFIED MEASUREMENT TABLE

Part: ATTACH ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED ATTACH ANGLE AT PASSENGER CABIN BS294 RBL53 WL208.<[01] REMOVED MOPSILL SUPPORT ANGLE AT BS 294 RB53 WL 208.1 IAW SRM 51-40-02;[02] RECIVED NEW CLIP ITEM 141A8312-3 LOT 5075760-10 LOCATED AND DRILLED NEW CLIP AT BS294 RBL53 WL208 ; IAW 737-700 SRM 51-40-05-0G-0 DWG 141A8310 REV: B.-;[03] OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION 2.<BR>OK TO INSTALL;[05] INSTALLED NEW CLIP AT BS294 RBL53 WL208. IAW 737-700 SRM 51-40-02-0G-0; DWG 41A8310 REV: B.- .;[06] VERIFIED CORRECTIVE ACTION 5.

Part: CHANNEL — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED FED MOP SILL BS294+9 LBL54 WL208. MARKED<[01] REMOVED FED MOPSILL IAW SRM 51-40-02;[02] RECIVED NEW MOP SILL ITEM LOT 1530489-2 LOCATED AND DRILLED NEW MOP SILL BS 270 TO BS 360; IAW 737-700 SRM 51-40-05-0G-0 DWG 141A8110. OK TO INSTALL;[03] REJECTION OF OKAY TO INSTALL; AREA COVERED WITH FOD. STEP CREATED TO CLEAN AREA.;[04] APLICABILITY IDENTIFICATION SRM 53-10-15-0I-1 ALLOWABLE DAMAGE 53-10-15-1A-1;[05] CORECTION STEP 1;[06] VERIFIED STEP 1 COMPLETED.<BR>REJECTION CRITERIA HAS BEEN SATISFIED; OKAY TO INSTALL NEW MOP SILL GIVEN.;[07] OK TO INSTALL. REJECTION CRITERIA HAS BEEN SATISFIED;[08] INSTALLED NEW MOP SILL BS 270 TO BS 360 LBL 54 WL 208 . IAW 737-700 SRM 51-40-02-0G-0; DWG 141A8110 . ALL REQUIRED MAINTENANCE ACTIONS ARE COMPLETE=REQUEST FINAL BUYOFF;[09] INSPECTED AND VERIFIED CORRECTIVE ACTIONS. JOB COMPLETE.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED INTERCOSTAL AT FWD CABIN BS328+7 LBL46 WL208.<[01] REMOVED INTERCOSTAL FROM BS328-BS344 AT LBL 46 WL 208 IAW SRM 51-40-02;[02] DAMAGE FOUND AT FWD CABIN INTERCOSTAL BS 328+7; LBL-46; WL 208 FOUND TO BE OUT OF LIMIT IAW SRM 53-1-51-1A-1 DET.4B(1A); FIG 105-N;[03] LOCATED AND DRILLED NEW INTERCOSTAL P/N 141A5410-16 LOT#1530387-1 AT BS 328 TO BS 344 LBL 46 WL 208 IAW SRM 51-40-05-0G-0 AND DWG# 141A5400.OK TO INSTALL;[04] VERIFIED STEPS #1; #2; AND #3. OK TO INSTALL.;[05] INSTALLED NEW INTERCOSTAL AT BS 328 TO BS 344; LBL 46; WL 208 IAW SRM 51-40-02-0G-0 AND DWG# 141A5400.;[06] VERIFIED STEP #5;[07] VERIFIED STEP #5

Part: STRINGER CLIP — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

STRINGER CLIP 3L IS CRACKED AT BS 706<[01] VERIFY END OF CRACK AT STRINGER CLIP BS 706; S-3L;[02] ACCOMPLISHED HFEC SURFACE SCAN IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. NO CRACKS NOTED.<BR><BR>EQUIPMENT USED: NORTEC 600 ID: ATS1465 CAL DUE: 09/2023;[03] HFEC INSPECTED STRINGER CLIP AT BS 706; S-3L. NO CRACK NOTED AT THIS LOCATION. NO FURTHER ACTION REQUIRED;[04] PART REQUIRED NOT USED;[05] VERIFIED CORRECTIVE ACTION 3 AND 4<BR><BR>VERIFIED MEASUREMENT TABLE

Part: STRAP — CORRODED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

AFT PASSENGER FLOOR STRUCTURE TENSION STRAP HAS CORROSION AT BS 1016; LBL 3; WL 208<[01] CORROSION ON TENSION STRAP AT BS1016 LBL3 WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEMS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 PAR 9C;[02] REMOVED TENSION STRAP FROM BS1006-BS1029 LBL3 IAW SRM 51-40-02;[03] VERIFIED CORRECTIVE ACTION 1 AND 2;[04] LOCATED AND DRILLED NEW TENSION STRAP AT LBL3 FROM BS1006-BS1029; PN#147A5620-3 IAW SRM 51-40-02 AND IAW DWG#147A5600. OK TO INSTALL;[05] CORRECTIVE REFERENCE: LOCATED AND DRILLED NEW TENSION STRAP AT LBL3 FROM BS1006-BS1029; PN#147A5620-3 IAW SRM 51-40-05 AND IAW DWG#147A5600. OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION 4 AND 5;[07] INSTALLED TENSION STRAP AT LBL3 FROM BS1006-BS1029; PN#147A5620-3 IAW SRM 51-40-02 AND IAW DWG#147A5600.;[08] VERIFIED MEASUREMENT TABLE;[09] VERIFIED CORRECTIVE ACTION 7

Part: GIRT BAR — CORRODED (ZN 800 DOOR) · airframe 38,123 hrs · 23,431 cycles

CORROSION ON GIRT BAR BASE FITTING BS312 LBL54 WL208.<[01] DAMAGE FOUND ON GIRT BAR BASE FITTING BS312 LBL54 WL208 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM REMOVED AND REPLACED GIRT BAR BASE WIT A NEW P/N 141A522-2 LOT#1524839-1 IAW SRM 51-40-02-0G-0 AND DWG#141A5220.;[02] VERIFIED CORRECTIVE ACTION STEP 1;[03] VERIFIED CORRECTIVE ACTION STEP 1

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 38,123 hrs · 23,431 cycles

CRACKED INTERCOSTAL AT FWD CABIN BS275 BL0 WL208. BS- 284 BL-0<[01] REMOVED INTERCOSTAL FROM BS277-BS294 AT BL0 WL 208 IAW SRM 51-40-02;[02] DAMAGE FOUND AT FWD CABIN INTERCOSTAL BS 284; BL-0; WL 208 FOUND TO BE OUT OF LIMIT IAW SRM 53-1-51-1A-1 DET.4B(1A); FIG 105-N;[03] LOCATED AND DRILLED NEW INTERCOSTAL P/N 141A5410-3; LOT#240019 AT BS 277 TO BS 294 BL 0 WL 208 IAW SRM 51-40-05-0G-0 AND DWG# 141A5400.OK TO INSTALL;[04] VERIFIED STEPS #1; #2;AND#3. OK TO INSTALL;[05] INSTALLED NEW INTERCOSTAL AT BS 277 TO BS 294;BL 0; WL 208 IAW SRM 51-40-02-0G-0 AND DWG# 141A5400;[06] VERIFIED STEP #5;[07] VERIFIED STEP #5

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

FWD CABIN FLOOR PANEL 221CF HAS A PULLED THROUGH INSERT ON THE LEFT SIDE<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 2; TABLE 2; AND <BR>BOEING DWG DOC: 141A5810 ID: 0009. <BR><BR>DAMAGE ON LOWER SURFACE LEFT HAND SIDE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM <BR>53-00-50-1A-1 PAR. 4. ALL AREAS ON LOWER <BR>SURFACE WILL BE REPAIRED IAW SRM 53-00-50-2R-1. OK TO POT.;[09] INSTALLED REPAIR PLIES USING BMS8-201 EPOCAST 50-A (946) LOT # 1530326-1; <BR>SET UP VACUUM BAG SYSTEM WITH BLEED DOWN TEST CHECKED GOOD USING GAUGE ID: <BR>E11543 CAL/DUE: 09/2023 IAW SRM 53-00-50-2R-1 PAR. 3. K. - L. OK TO <BR>CURE.;[10] VERIFIED CORRECTIVE ACTION 9;[11] CURED REPAIR PLIES UNDER HEATLAMP MONITORED BY THERMOMETER ID: ATS2208 <BR>CAL/DUE: 10/2023 REMOVED VACUUM BAG AND SANDED REPAIR EDGES AND LOCATED <BR>ALL THROUGH INSERT LOCATIONS AND CLEANED IAW SRM 53-00-50-2R-1 PAR. 3. M. & 3. N.;[12] UPON FURTHER INSPECTION FOUND NUMBER OF REPAIR PLIES TO BE INSUFFICIENT; FABRICATED ADDITIONAL REPAIR PLIES FROM BMS9-3H2ST1581 LOT#1526805-2; OK TO INSTALL IAW SRM 53-00-50-2R-1 PARA 3K(1).

Part: FLOOR PANEL — BROKEN (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

FWD CABIN FLOOR PANEL 221BF HAS BROKEN TANG ON AFT O/B CORNER<[01] IDENTIFIED FLOOR PANEL 221BF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2. DAMAGE AT DISCREPANT LOCATION AND FOUND ADDITIONAL AREAS ON LOWER SURFACE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. ALL AREAS ON LOWER SURFACE MAY BE REPAIRED IAW SRM 53-00-50-2R-1. <BR><BR>REMOVED SEVERAL INSERTS TO FACILITATE REPAIR IAW SRM 53-00-50-2R-1 PARAGRAPH 3.B<BR><BR>REMOVED DAMAGED SKIN AT DISCREPANT AREA; AND REMOVED DAMAGE AT ADDITIONAL AREAS ON THE LOWER SURFACE. REMOVED LOOSE PIECES OF CORE AND CLEANED ALL AREAS. OKAY TO APPLY POTTING AT ALL LOCATIONS IAW SRM 53-00-50-2R-1 PARAGRAPH 3.A;C-F.;[02] VALIDATED REPAIR PER SRM 53-00-50-2R-1;[FABRICATED REPAIR PLIES USING BMS9-3 ST1581 LOT# 1526805-2. OKAY TO INSTALL PLIES AT ALL DISCREPANT LOCATIONS IAW SRM 53-00-50-2R-1 PARAGRAPH 3.H-K(1)(A).;[06] VERIFIED CORRECTIVE ACTIONS 4 AND 5<BR><BR>OK TO INSTALL REPAIR PLIES;[07] INSTALLED REPAIR PLIES USING BMS8-201 TYPE 4 LOT#1530326-1; VACUUM BAGGED; CHECKED FOR LEAKS; LEAK CHECKED GOOD USING VACUUM GAUGE ATS2441 CAL DUE DATE 08/2023 AND SET FOR CURE USING HEAT LAMPS AND THERMOMETER ATS2209 CAL DUE DATE 10/2023 IAW SRM 53-00-50-2R-1 PARA 3K(1)-L(1)-M(1).

Part: PANEL — BROKEN (ZN 300 STABILIZE) · airframe 38,123 hrs · 23,431 cycles

VERTICAL FIN - BROKEN TRAINING EDGE ON 324TL PANEL ASSY - TRAINING EDGE; BEAM SEAL; VERTICAL FIN<[01] BROKEN TRAINING EDGE ON 324TL PANEL ASSY REPLACED PER SRM 51-10-02-0G-0-A00248 STEPV9. A. (1). TO BE INSTALLED ON CARD TTG8Q00KMT4H;[02] UPDATED PARTS REQUIREMENT;[03] VERIFIED CORRECTIVE ACTION STEPS 1-2

Part: BULKHEAD — CRACKED (ZN 100 FUS LOWER) · airframe 38,123 hrs · 23,431 cycles

BS663 COMPOSITE VAPOR BARRIER BULKHEAD IS CRACKED AT WL 152; RBL 32.<[01] IDENTIFIED 663 BULKHEAD R/H VAPOR BARRIER MATERIAL IAW SRM 57-10-10-0I-2 TABLE 2 FIGURE 2 ITEM 4. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PARAGRAPH 4.D(2). DAMAGE IS REPAIRABLE IAW SRM 57-10-10-2R-2 PARAGRAPH 1.C NOTE<BR><BR>REMOVED DAMAGED AND CONTAMINATED PLIES FROM DISCREPANT LOCATION AND CLEANED AREAS IAW SRM 51-70-04-2R-10 PARAGRAPH 4.A-C.;[02] VALIDATED REPAIR PER SRM 51-70-04-2R-10;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2<BR><BR>VERIFIED MEASUREMENTS TABLE<BR><BR>VALIDATED REPAIR PER SRM 51-70-04-2R-10;[04] FABRICATED REPAIR PLIES USING BMS 9-3H2 LOT#1526805-2 IAW SRM 51-70-04-2R-10 PARA 4.D.<BR>OK TO INSTALL.;[05] INSPECTED AND VERIFIED CORRECTIVE ACTION 4. OKAY TO INSTALL REPAIR PLIES.;[06] INSTALLED REPAIR PLIES USING BMS 8-301CL1 LOT#JH2EAA8895; VACUUM BAGGED; LEAK CHECK GOOD WITH VACUUM GAUGE ID:ATS2441 CAL DUE 08/2023 IAW SRM 51-70-04-2R-10 PARA 4.D-E.;[07] INSPECTED AND VERIFIED CORRECTIVE ACTION 6.;

Part: COVER — LOOSE (ZN 200 FUS TOP) · airframe 37,433 hrs · 22,971 cycles

EMERGENCY EXIT PLASTIC COVER FELL OFF OVERWING EXIT<[01] REINSTALLED EMERGENCY EXIT SIGN COVER ON OVERWING EXIT SIGN PER MM 33-51-01

Part: SLIDE — LOW (ZN 900 LAV/GALLE) · airframe 37,194 hrs · 22,804 cycles

FWD SVC DOOR SLIDE BELOW GREEN PRESSURE LIMIT IN RED<[01] REMOVED AND REPLACED FWD SERVICE DOOR ESCAPE SLIDE REF AMM 25-66-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,948 hrs · 22,645 cycles

EXIT SIGN ASSEMBLY AT FWD ENTRY DOOR IS INOPERATIVE. REMOVED AND REPLACED FWD ENTRY DOOR LOWER EMERGENCY EXIT LIGHT ASSY IAW AMM 33-51-01.

Part: LENS — BROKEN (FWD ENTRY) · airframe 35,759 hrs · 21,839 cycles

FORWARD EXIT LIGHT COVER-TABS BROKEN-WILL STAY IN PLACE / [01] R&R?D FWD ENTRY EMER LT BASE & LENS PER SIP

Part: COVER — BROKEN (FWD ENTRY) · airframe 35,759 hrs · 21,839 cycles

FORWARD EXIT LIGHT COVER-TABS BROKEN-WILL STAY IN PLACE / [01] R&R?D FWD ENTRY EMER LT BASE & LENS PER SIP

Part: NONE — BROKEN (R2 DOOR) · airframe 35,025 hrs · 21,347 cycles

R2 DOOR ASSIST HANDLE BROKEN / [01] R&R R2 DOOR ASSIST HANDLE PER AMM 52-41-31

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,578 hrs · 19,816 cycles

AFT GALLEY RIGHT HAND SIDE L1191 EMERGENCY EXIT LOCATOR ONE LAMP INOP. ; / [01] REMOVED R/H AFT GALLEY EMERGENCY EXIT LOCATOR SIGN L1191 PER AMM 33-51-01-960-802. ROBBED SERVICEABLE PART FROM N750SA BUT DID NOT INSTALL DUE TO SCREW BROKEN OFF IN NUT PLATE; SEE FAULT TTG8Q005P7NP; [02] VERIFIED; REMOVED R/H AFT GALLEY EMERGENCY EXIT LOCATOR SIGN L1191 PER AMM 33-51-01-960-802. ROBBED SERVICEABLE PART FROM N750SA BUT DID NOT INSTALL DUE TO SCREW BROKEN OFF IN NUT PLATE; SEE FAULT TTG8Q005P7NP; [03] INSTALLED SERVICEABLE AFT GALLEY EMERGENCY EXIT LOCATOR SIGN L1191 ROBBED FROM N750SA PER AMM 33-51-01-960-802. <BR><BR>PERFORMED GOOD OPERATIONAL TEST OF NEWLY INSTALLED EMERGENCY EXIT SIGN PER AMM 33-51-00-710-801.; [04] ADDED N/A TO MEASUREMENTS.; [05] VERIFIED INSTALLATION AND GOOD FUNCTION TEST.; [06] VERIFIED INSTALLATION AND GOOD FUNCTION TEST.

Part: ANGLE — DAMAGED (AFT CARGO) · airframe 32,578 hrs · 19,816 cycles

AFT CARGO BAY FWD SHIELD ATTACH ANGLE HAS DAMAGED FASTENER HOLE BS 767 - 787, RBL 21, WL 157. LOCATED DRILLED AND INSTALLED NUT PLATES ON NEW PART IAW SRM 51-40-02 SRM 51-40-05 SRM 51-40-08 AND DWG'S 146A8123 REV:- 146A0081 REV:-. INSTALLED AFT CARGO BAY FWD SHIELD ATTACH ANGLE IAW SRM 51-40-02 AND DWG 143A8123 REV:- .

Part: VAPOR BARRIER — DAMAGED (BS 663) · airframe 32,578 hrs · 19,816 cycles

REPAIR BS 663 L/H VAPOR BARRIER LBL 31.83 WL 157 ; / [01] IDENTIFIED L/H VAPOR BARRIER<BR>IAW SRM 57-10-10-0I-2 FIGURE2; TABLE 2 ITEM 4<BR>FOUND DAMAGE TO EXCEED ALLOWABLE LIMITS<BR>IAW SRM 57-10-10-1A-2 PARA 4 D 4 (B)<BR><BR>REPAIR TO BE EFFECTED IAW SRM 51-70-04-2R-10;<BR>PER SRM 57-10-10-2R-2 PARA 1 C. NOTE<BR><BR>REMOVED DAMAGE; PREPARED AND CLEANED REPAIR AREA.<BR>IAW SRM 51-70-04-2R-10 PARA 4 A; B; & C; [02] VALIDATED APPLICABILITY OF REPAIR SRM 51-70-04-2R-10.; [03] VERIFIED DAMAGE REMOVAL AND APPLICABILITY; [04] FABRICATED REPAIR PLIES FROM BMS9-3 STYLE 1581 TYPE H2 LOT#1458851-1 IAW SRM 51-70-05-2R-10 PARA 4 STEP D. OK TO INSTALL REPAIR PLIES.; [05] VERIFIED FABRICATION OF PLIES. OK TO INSTALL; [06] INSTALLED REPAIR PLIES WITH BMS8-301 CLASS 1 LOT#JH1CAA0868; VACUUM BAGGED REPAIR PLIES; VERIFIED 5X5 WAS GOOD AND SET PLIES TO CURE USING HOTBONDER ID:ATS532 S/N: 15092117 IAW SRM 51-70-04-2R-10 PARA 4.D-F.; [07] ACTION STEP 4 SHOULD READ 'IAW SRM 51-70-04-2R-10'; [08] VERIFIED CORRECTIVE ACTION #6 AND #7; SRM 51-70-04-2R-10 IS CORRECT REFERENCE FOR ACTION STEP #4.; [09] CURED REPAIR PLIES; UN-BAGGED; LIGHTLY SANDED AND TRIMMED EDGE IAW SRM 51-70-04-2R-10 PARA 4.F.; [10] CERTIFIED CURED REPAIR PLIES; UN-BAGGED; LIGHTLY SANDED AND TRIMMED EDGE IAW SRM 51-70-04-2R-10 PARA 4.F.; [15] REPAIRED BS 663 L/H VAPOR BARRIER LBL 31.83 WL 157 IAW SRM 51-70-04-2R-10;

Part: SUPPORT — DAMAGED (BS 500A) · airframe 32,578 hrs · 19,816 cycles

FLOOR TO SIDEWALL SUPPORT ELONGATED FASTENER HOLE. ; FORWARD CARGO BAY; FLOOR TO SIDEWALL SUPPORT HAS ELONGATED FASTENER HOLE AT BS 500A+9.5; LBL20; WL156. / [01] EVALUATED ELONGATED FASTENER HOLE ON FCB FLOOR TO SIDEWALL SUPPORT L/H BS 500A+10' LBL21 WL156. DAMAGE FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS IN SRM 53-00-53-1A-2. FASTENER HOLE MEASURES 0.038' L X 0.029' W.; [02] VERIFIED OUT OF LIMITS; [03] VERIFIED OUT OF LIMITS.; [04] FABRICATED FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 400-500D LBL 20 USING BAC1498-444 7075-T62 LOT# 1459660-2 IAW SRM 51-40-05 AND BOEING DWG 143A7501. FABRICATED REPAIR SPLICE AT BS 480+10' FROM BAC1498-444 7075-T62 LOT #1459660-2 IAW SRM 53-00-53-2R-6; [05] LOCATED AND DRILLED HOLES IN FCB FLOOR TO SIDEWALL SUPPORT BS 400-500D LBL 20 IAW SRM 51-40-05-0G-0 AND DWG 143A7501 REV A; [06] OK TO APPLY CHEMICAL CONVERSION COATING AND PRIME; [07] VERIFIED; [08] VERIFIED FABRICATION; OK TO APPLY CONVERSION COATING.; [09] FABUCATED SPLICE AT BS 480 +10 IAW SRM 53-00-53-2R-6 AND APPLIED PRIMER IAW AMM 51-21-72-370-840; NSTALLED SPLICE AT BS480+10 AND APPLIED CHEMICAL CONVERSION COATING AND PRIMER. IAW SRM 53-00-53-2R-6; AMM 51-21-72-370-840; SRM 51-20-01;[VERIFIED INSTALLATION OF REPAIR SPLICE <BR><BR>IAW SRM 53-00-53-2R-6] INSTALLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 143A7500 REV : -

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 32,578 hrs · 19,816 cycles

CRACKED GUSSET - BS 500D STRINGER 19L. ; CRACKED GUSSET - BS 500D STRINGER 19L. PN # 143A9481-6. / [01] REMOVED FCB GUSSET BS 500D STR 19L PER SRM 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEW L/H GUSSET IAW SRM 51-40-02 AND DWG 143A7902 REV. 0; [03] VERIFIED ITEM 2.; [04] OK TO INSTALL NEW GUSSET.; [05] VERIFIED LOCATED AND DRILLED NEW L/H GUSSET IAW SRM 51-40-02 AND DWG 143A7902 REV. 0 OK TO INSTALL NEW GUSSET.; [06] INSTALLED NEW GUSSET IAW SRM 51-40-02 AND DWG 143A7902 REV : -; [07] UPDATE LOT# 1457201-12 FOR GUSSET PN/ 143A9481-6 - BS 500D STRINGER 19L; [08] VERIFIED - ITEM 6 AND 7.; [09] VERIFIED INSTALLATION OF BS500D STRINGER 19L GUSSET PER SRM 51-40-02; DWG 143A7902

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 32,578 hrs · 19,816 cycles

CRACKED GUSSET - BS 500D STRINGER 19R. ; CRACKED GUSSET - BS 500D STRINGER 19R. PN # 143A9481-5. / [01] REMOVED GUSSET AT FCB BS 500D STR 19R IAW SRM 51-40-02; [02] VERIFIED REMOVAL; [03] LOCATED AND DRILLED NEW R/H GUSSET IAW SRM 51-40-05 AND DWG 143A7902 OK TO INSTALL; [04] UPDATE MEASERMENT; [05] VERIFIED ITEM 3-4. LOCATED AND DRILLED NEW R/H GUSSET IAW SRM 51-40-05 AND DWG 143A7902 REV: -; OK TO INSTALL; [06] VERIFIED LOCATED AND DRILLED NEW R/H GUSSET IAW SRM 51-40-05 AND DWG 143A7902 REV: -; OK TO INSTALL; [07] INSTALLED GUSSET - BS 500D STRINGER 19R IAW SRM 51-40-02 AND DWG 143A7902 REV:-; [08] UPDATE LOT# 1457201-10 FOR GUSSET PN/ 143A9481-5 - BS 500D STRINGER 19R; [09] VERIFIED- ITEM 7 AND 8.; [10] VERIFIED INSTALLATION OF BS500D STRINGER 19R GUSSET IAW SRM 51-40-02; DWG 143A7902

Part: BULKHEAD — CRACKED (AFT CARGO) · airframe 32,578 hrs · 19,816 cycles

AFT CARGO COMPARTMENT- CRACKED FWD BULKHEAD PANEL# 142NWB. ; AFT CARGO COMPARTMENT- CRACKED FWD BULKHEAD SHROUD PANEL# 142NWB. / [01] REMOVED ACB FWD BULKHEAD PANEL 142NWB IAW AMM 25-52-18-000-801; [02] OK TO CLOSE PNL 142NWB; [03] INSTALLED FWD BLKHD LINER IAW AMM 25-52-18-401-NG; [04] REMOVED AND REQUESTING OK TO CLOSE PNL 142NWB; [05] VERIFIED; [06] VERIFIED OK TO CLOSE PANEL 142NWB.; [07] INSTALLED ACB FWD BULKHEAD PNL 142NWB IAW AMM 25-52-18-401-NG; [08] VERIFIED; [09] INSTALLED ACB FWD BULKHEAD PNL 142NWB IAW AMM 25-52-18-401-NG<BR>TOOL USED: 25IN-LBS SCREW GUN. ID:ATS2266 S/N:1703449; [10] VERIFIED; [11] VERIFIED NEW PANEL 142NWB WAS INSTALLED PER AMM 25-52-18-401-NG

Part: DOUBLER — CRACKED (BS 663 BULKHEAD) · airframe 32,578 hrs · 19,816 cycles

L/H VAPOR BARRIER DOUBLER IS CRACKED AT BS 663 LBL 25 W/L 148 / [01] FABRICATED DOUBLER FROM 2924T0 .O40 LOT #1380676-1 IAW SRM 51-30-01-0G-0 AND DWG B111A1511 REV.A; [02] VERIFIED THAT PART WAS FABRICATED DOUBLER FROM 2924T0 .O40 LOT #1380676-1 IAW SRM 51-30-01-0G-0 AND DWG B111A1511 REV.A; [03] VERIFIED THAT PART WAS FABRICATED DOUBLER FROM 2924T0 .O40 LOT #1380676-1 IAW SRM 51-30-01-0G-0 AND DWG B111A1511 REV.A; [04] HEAT TREAT DOUBLER ON CUSTOMER RO NO 828323-SWA JOB. #540630; [05] VERFIED; [06] VERIFIED CONFIRMED ON RO NO 828323-SWA JOB NO 540630 DOUBLER 2024 HEAT TREATED; NOT 2924T0 AS STATED IN ITEMS 1 ; 2 AND 3.; [07] LOCATED AND DRILLED DOUBLER IAW BOEING DWG 111A1000; DWG 144A7100; DWG 111A1001 AND SRM 51-40-05-0G-0; [08] VERIFIED LOCATION AND DRILL OF DOUBLER IAW DWG 111A1000; DWG 1447100; DWG 111A1001 AND SRM 51-40-05-0G-0; [09] VERIFIED; [10] VERIFIED LOCATION AND DRILLED; [11] APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SOPM 20-43-03 AND AMM 51-21-72-370-804; [12] VERFIED; [13] VERIFIED CONVERSION COATING AND PRIMER APPLICATION;; [14] L/H VAPOR BARRIER DOUBLER WAS INSTALLED AT BS 663 LBL 25 W/L 148 ON WORK CARD TTG8Q005H0XN; [15] L/H VAPOR BARRIER DOUBLER WAS INSTALLED AT BS 663 LBL 25 W/L 148 ON WORK CARD TTG8Q005FP1U; [16] VERIFIED; [17] VERIFIED THE L/H VAPOR BARRIER DOUBLER WAS INSTALLED AT BS 663 LBL 25 W/L 148 ON WORK CARD TTG8Q005FP1U

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 32,578 hrs · 19,816 cycles

L/H VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT BS 663 LBL 8 W/L 164 / [01] VERIFIED APPLICABILY FOR REPAIR IAW SRM 57-10-10-2R-5 REPAIR 5; [02] VERIFIED SRM 57-10-10-2R-5 REPAIR 5 IS APPLICABLE.; [03] VERIFIED SRM 57-10-10-2R-5 REPAIR 5 IS APPLICABLE.; [04] REMOVED FASTENERS AS SHOWN IN THE FIGURE 202 DETAIL B LOCATED AT B/S 663 BTW LBL 6 TO LBL 20 IAW SRM 57-10-10-2R-5 REPAIR 5; [05] PERFORMED CUT-OUT THE UPPER ATTACH ANGLE LOCATED AT B/S 663 BTW LBL 6 TO LBL 20 IAW SRM 57-10-10-2R-5 REPAIR 5 STEP 4B; [06] PERFORMED A DETAIL VISUAL INSPECTION OF THE REPAIR AREA AND THE UNDERLYNG STRUCTURE AND NOT FOUND MORE DAMAGE WITHIN THE REPAIR AREA LOCATED AT B/S 663 BTW LBL 6 TO LBL 20 IAW SRM 57-10-10-2R-5 REPAIR 5; [07] VERIFIED ITEM 4-6.; [08] INSPECTED CUTOUT AND ACCOMPLISHED DVI OF THE REPAIR AREA AND THE UNDERLYNG STRUCTURE AND NO DAMAGE WITHIN THE REPAIR AREA NOTED LOCATED AT B/S 663 BTW LBL 6 TO LBL 20 IAW SRM 57-10-10-2R-5 REPAIR 5; [09] HFEC INSPECTED INITIAL FASTENER HOLES IN THE REPAIR AREA PER NDTM PART 6; 51-00-00 PROCEDURE 16. FOUND FAULT TTG8Q005HQ86; NO OTHER CRACKS NOTED.<BR>CAL ID: ATS1465 S/N: 60004150296<BR>CAL ID: ATS1411 S/N: MM12030Z012384; [10] LOCATED AND DRILLED: REPLACEMENT ANGLE ATSHFAB-101-353 LOT. 540264 AND REPAIR SPLICE ANGLE ATSDFAB-101-355 LOT.537716 IAW SRMS 57-10-10-2R-5 AND 51-40-05;

Part: SUPPORT — CORRODED (BS 767-787) · airframe 32,578 hrs · 19,816 cycles

CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767- BS787 RBL21 WL157. ; / [01] REMOVED ACB FWD SHIELD IAW SRM 51-40-02.; [02] VERIFIED REMOVAL; [03] UPDATED MEASURMENTS; [04] LOCATED; DRILLED; AND COUNTERSANK AFT CARGO BAY FWD SHIELD BS 767-BS787 RBL21 WL157 IAW SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 146A8127 ID:0008 REV:-; [05] VERIFIED LOCATED; DRILLED; AND COUNTERSANK AFT CARGO BAY FWD SHIELD BS 767-BS787 RBL21 WL157 IAW SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 146A8127 ID:0008 REV:-; [06] FWD SHEILD IN AFT CARGO BAY BS 767-787 RBL 21 WL 157 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 ITEM 9; [07] VERIFIED NO ALLOWABLE LIMITS IN SRM PART TO BE REPLACED PER SRM 51-10-02; [08] OK TO INSTALL; [09] VERIFIED; OK TO INSTALL NEW PART; [10] INSTALLED FWD SHIELD AT AFT CARGO BAY BS767- BS787 RBL21 WL157 IAW SRM 51-40-02 AND DWG 146A0081 REV:-; [11] VERIFIED; [12] VERIFIED THE INSTALLATION OF THE FORWARD SHIELD AT AFT CARGO BAY BS767- BS787 RBL21 WL157

Part: CARGO TRACK — CORRODED (BS 727D) · airframe 32,578 hrs · 19,816 cycles

CORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS727D RBL13 WL156. ; / [01] UPDATED MEASUREMENTS; [02] REMOVED CORROSION AT ACB BS 727D RBL13. DAMAGE REMOVED : 0.05'. DAMAGE EXCEED MAXIMUM DEPTH (0.04') IN THE BOTTOM OF THE TRACK. DAMAGE FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2; [03] REMOVED AND REPLACED ACB TIEDOWN TRACK BS 727 - BS 887 RBL13 IAW CUSTOMER CARD NBR : TTG8Q005GAEJ; [04] RII INSPECTED; VERIFIED; CONFIRMED; [05] RII INSPECTED; VERIFIED; CONFIRMED JOB COMPLETE

Part: CARGO TRACK — CRACKED (AFT CARGO) · airframe 32,578 hrs · 19,816 cycles

CRACKED TRACK AT AFT CARGO BAY BS767 RBL13 WL156. ; / [01] UPDATED MEASUREMENTS; [02] CRACK LENGTH : 0.320' ORIGINAL MATERIAL LENGTH : 0.800'. DAMAGE EXCEEDS 10% OF ORIGINAL MATERIAL LENGTH. DAMAGE IS FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2; [03] REMOVED AND REPLACED ACB TIEDOWN TRACK BS 727 - BS 887 RBL13 IAW CUSTOMER CARD NBR : TTG8Q005GAEJ; [04] RII INSPECTED; VERIFIED; CONFIRMED; [05] RII INSPECTED; VERIFIED; CONFIRMED JOB COMPLETE

Part: WEB — CORRODED (BS 442) · airframe 32,578 hrs · 19,816 cycles

CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS442 RBL25 WL156. ; / [01] REMOVED SUB THRESHOLD WEB IAW 51-40-02; [02] REMOVED DAMAGE FROM SUB THRESHOLD IN A 1.2LX.9W AREA. ORIGINAL THICKNESS IS .045 IAW SRM 53-30-15-01-1 FIG 5 ITEM 3. SRM 51-10-02; SRM 53-30-15-1A-1; [03] REMOVED DAMAGE FROM SUB THRESHOLD IN A 1.2LX.9W AREA. ORIGINAL THICKNESS IS .045 AT BS442 RBL25; WL156 IAW SRM 53-30-15-01-1 FIG 5 ITEM 3. SRM 51-10-02; SRM 53-30-15-1A-1; [04] VERIFIED AND ADDED DAMAGE LOCATION; [05] VERIFIED CORROSION REMOVAL FROM SUB THRESHOLD IN A 1.2LX.9W AREA. ORIGINAL THICKNESS IS .045 AT BS442 RBL25; WL156 IAW SRM 53-30-15-01-1 FIG 5 ITEM 3. SRM 51-10-02 & SRM 53-30-15-1A-1.; [06] UPON FURTHER INVESTIGATION CORROSION FOUND TO BE OUT OF LIMITS REMAINING THICKNESS 0.037; ORIGINAL THICKNESS 0.045 IAW SRM 53-30-15-1A-1;STEP 4G(2) ;FIG 103; SRM 53-30-15-01-1;FIG 5 ID ATS400; DUE 04/2022; [12] RECEIVED REPLACEMENT FCB SUB THRESHOLD WEB; LOCATED AND DRILLED PER SRM 51-40-05;SRM 51-40-08 AND DWG 143A8330; [13] VERIFIED LOCATE AND DRILL; [14] RECEIVED REPLACEMENT FCB SUB THRESHOLD WEB; LOCATED AND DRILLED PER SRM 51-40-05;SRM 51-40-08 AND DWG 143A8330;

Part: SUPPORT — CORRODED (BS 727B-767) · airframe 32,578 hrs · 19,816 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727B - BS767 RBL20 WL156. ; / [01] REMOVED ACB FLOOR TO SIDEWALL SUPPORT R/H BS 727-767 RBL 20 IAW SRM 51-40-02; [02] VERIFIED REMOVED; [03] RECEIVED NEW ZEE ASSEMBLE LOT #1460159; [04] LOCATED AND DRILLED NEW ASSEMBLY FLOOR SUPPORT AT AFT CARGO BAY BS 727 ;RBL 20 ; WL 156 IAW SRM 51-40-05-0G-0 AND DWG 146A7500; [05] VERIFIED; [06] VERIFIED LOCATE AND DRILL UP ONLY; NO AMT UPDATES FOR CORROSION DAMAGE AND LIMITS; [07] REMOVED .009' MATERIAL FROM AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 727B - BS 767 RBL 20 WL 156 FROM ORIGINAL THICKNESS OF .040'. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [08] VERIFIED DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-00-53-1A-2; [09] OK TO INSTALL ACB FLOOR TO SIDEWALL SUPPORT BS 727-767 RBL 20 WL 156; [10] REQUEST OK TO INSTALL FLOOR TO SIDEWALL SUPPORT; [11] VERIFIED CIC'ED ON ACB FLOOR TO SIDEWALL SUPPORT BS 727-767 RBL 20 WL 156; [12] VERIFIED NO OTHER DEFECTS WITH IN WORK AREA.<BR><BR>OK TO INSTALL FLOOR TO SIDEWALL SUPPORT; [13] INSTALLED ACB FLOOR TO SIDEWALL SUPPORT BS 727-767 RBL 20 WL 156 IAW SRM 51-40-02; DWG# 146A7500 & 146A7502.; [14] VERIFIED INSTALL OF ACB R/H FLOOR TO SIDEWALL SUPPORT; [15] SIGNED FOR PART USED; [16] VERIFIED INSTALL OF ACB R/H FLOOR TO SIDEWALL SUPPORT BS 727-767 RBL 20 WL 156

Part: CARGO TRACK — CORRODED (BS 787) · airframe 32,578 hrs · 19,816 cycles

CORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS787 LBL17 WL157. / [01] FAULT RESOLVED ON TTG8Q005GC6A. PART REPLACED.; [02] VERIFIED ACB TRACK AT LBL17 WAS REPLACED ON TTG8Q005GC6A.<BR><BR>NO FURTHER ACTIONS REQUIRED.

Part: WEB — CORRODED (BS 794-847) · airframe 32,578 hrs · 19,816 cycles

CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS794 - 847 RBL26 WL157. ; / [01] REMOVED SUB THRESHOLD WEB. IAW SRM 51-40-02; [02] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS IAW SRM 53- 60- 15 -1A -1 ; REMOVED CORROSION ON SUBTHESHOLD WEB AT AFT CARGO BAY BTW B/S 794-847 IAW SRM 51- 10 -02 PARAGRAPH 15 AT SEVERAL PLACE AND EXCEEDS THE 50% OF ORIGINAL MATERIAL FOUND OUT ALLOWABLE DAMAGE LIMIST IAW SRM 53-60-15- 1A 1 FIGURE 103 DETAL 'D' . TOOL USED : S/N 643JZ DUE :04/2022; [03] UPDATED MEASUREMENTS; [04] LOCATED; DRILLED AND INSTALLED NUT PLATES ALL IAW DWG145A9340; SRM 51-40-02-0G-0; AND SRM 51-40-05-0G-0. OK TO INSTALL; [05] VERIFIED LOCATED; DRILLED AND INSTALLED NUT PLATES ALL IAW DWG145A9340; SRM 51-40-02-0G-0; AND SRM 51-40-05-0G-0. OK TO INSTALL; [06] INSTALLED REPLACEMENT ACB THRESHOLD CLOSE OUT WEB IAW DWG146A8340; AND SRM 51-40-02; [07] VERIFIED INSTALLED REPLACEMENT ACB THRESHOLD CLOSE OUT WEB IAW DWG146A8340; AND SRM 51-40-02; [08] VERIFIED INSTALLED REPLACEMENT ACB THRESHOLD CLOSE OUT WEB IAW DWG146A8340; AND SRM 51-40-02.

Part: CARGO TRACK — CORRODED (BS 787-807) · airframe 32,578 hrs · 19,816 cycles

CORROSION ON TRACK AT AFT CARGO BAY BS787-BS807 RBL13 WL157. ; / [01] UPDATED MEASUREMENTS; [02] VERIFIED; [03] REMOVED CORROSION AT BS 787 RBL13. DAMAGE REMOVED : 0.05' DAMAGE EXCEED MAXIMUM DEPTH(0.04') FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2; [04] REMOVED AND REPLACED ACB TIEDOWN TRACK BS 727 - BS 887 RBL13 IAW CUSTOMER CARD NBR : TTG8Q005GAEJ; [05] RII INSPECTED; VERIFIED; CONFIRMED; [06] RII INSPECTED; VERIFIED; CONFIRMED JOB COMPLETE

Part: CARGO TRACK — CORRODED (BS 727D) · airframe 32,578 hrs · 19,816 cycles

CORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS727D LBL17 WL156. ; / [01] FAULT RESOLVED ON TTG8Q005GC6A. PART REPLACED.; [02] VERIFIED ACB TRACK AT LBL17 WAS REPLACED ON TTG8Q005GC6A.<BR><BR>NO FURTHER ACTIONS REQUIRED.

Part: CARGO TRACK — CRACKED (BS 727E) · airframe 32,578 hrs · 19,816 cycles

CRACKED TRACK AT AFT CARGO BAY BS727E RBL13 WL156. ; / [01] REMOVED TIE DOWN TRACK RBL 13 BS 727 - BS 887 IAW SRM 51-40-02; [02] CRACK LENGTH : .250' ORIGINAL MATERIAL LENGTH : 0.800'. DAMAGE EXCEEDS 10% OF ORIGINAL MATERIAL LENGTH. DAMAGE IS FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2; [03] VERIFIED CRACK LENGTH : .250' ORIGINAL MATERIAL LENGTH : 0.800'. DAMAGE EXCEEDS 10% OF ORIGINAL MATERIAL LENGTH. DAMAGE IS FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2; [04] LOCATED AND DRILLED ACB TRACK BS 727-887; RBL 13 PER SRM 51-40-05-0G-0; DWG#146A7500.<BR><BR>LOCATED AND DRILLED TRACK SPLICE PART # 146A7506-20 B/N BS 747-767; RBL 13 PER SRM 53-00-53-2R-3.; [05] REQUEST OK TO INSTALL; [06] LOCATED AND DRILLED ACB TRACK BS 727-887; RBL 13 PER SRM 51-40-05-0G-0; DWG#146A7500; VERIFIED; AND SPLICE.; [07] INSTALLED NEW ACB TIE DOWN TRACK BS 727-BS887 RBL13 WL156 IAW SRM 51-40-02-0G-0; SRM 53-00-53-2R-4; DWG 146A7500 REV : -; AND DWG 146A0061 REV : D; [08] INSTALLED NEW ACB TIE DOWN TRACK BS 727-BS887 RBL13 WL156 IAW SRM 51-40-02-0G-0; SRM 53-00-53-2R-3; DWG 146A7500 REV : -; AND DWG 146A0061 REV : D; [09] UPDATED REFERENCE; [10] RII INSPECTED; VERIFIED; CONFIRMED; [11] RII INSPECTED; VERIFIED; CONFIRMED JOB COMPLETE

Part: CARGO TRACK — CRACKED (BS 767) · airframe 32,578 hrs · 19,816 cycles

CRACKED TRACK AT AFT CARGO BAY BS767 LBL17 WL156. ; / [01] NO LIMITS FOUNDED AT SRM FOR CRACK ON TRACK REPLACE FOR REPAIR; [02] REMOVED TRACK AT ACB BS727 TO BS 867 LBL 17 WL 156 IAW SRM 51-40-02; [03] RECEIVED PART FRON MAT. ITEM.146A7501-1 PO NUMBER 825933/1 LOCATED AND DRILLED NEW TRACK IAW SRM 51-40-05 AND DWG 146A7500 REV.0; [04] OK TO INSTALL TRACK AT FCB BS 727 TO BS 867 LBL17 WL 156; [05] VERIFIED; [06] OK TO INSTALL TRACK AT FCB BS 727 TO BS 867 LBL17 WL 156; [07] VERIFIED; [08] CORRECTION; OK TO INSTALL ACB BS 727 TO BS 867 LBL17 WL 156; [09] VERIFIED; [10] ITEM 6 CORRECTION; OK TO INSTALL ACB BS 727 TO BS 867 LBL17 WL 156; [11] INSTALLED NEW CARGO TRACK ON AFT CARGO BAY BS 727 TO BS 867;LBL 17 ; WL 156 IAW SRM 51-40-02-0G-0 AND DWG 146A7500; [12] VERIFIED INSTALL; [13] VERIFIED INSTALLATION OF ACB TRACK; BS 727 - 867; LBL 17; WL 156; PER SRM 51-40-02 AND DWG 146A7500; [14] VERIFIED ALL WORK COMPLETE THIS TASK CARD

Part: SHIELD — CORRODED (BS 500-500A) · airframe 32,578 hrs · 19,816 cycles

CORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL156. ; / [01] REMOVED FWD CARGO BAY SHIELD BS 492 - BS 500A RBL23 WL156 IAW SRM 51-40-02-0G-0; [02] THERE IS NO SRM ALLOWABLE DAMAGE FOR FWD CARGO BAY SHIELD. PART TO BE REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0; [03] THERE IS NO SRM ALLOWABLE DAMAGE FOR FWD CARGO BAY SHIELD. PART TO BE REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0; VERIFIED.; [04] LOCATED AND DRILLED FASTENER HOLES IAW SRM 51-40-08 AND DWG# 143A8126.; [05] VERIFIED LOCATE AND DRILL OF RECEIVED ATSHFAB-103-303 PART; [06] CHANGED REPAIR TYPE; [07] VERIFIED LOCATE AND DRILL OF RECEIVED ATSHFAB-103-303 PART; VERIFIED.; [08] VERIFIED; [09] OK TO INSTALL; [10] OK TO INSTALL SHIELD BS 500-500A; [11] INSTALLED FCB AFT SHIELD BS 492 - BS 500A IAW SRM 51-40-02-0G-0 AND DWG 143A0080 REV:-; [12] VERIFIED INSTALLATION OF FCB AFT SHIELD BS 492 - BS 500A IAW SRM 51-40-02-0G-0 AND DWG 143A0080; [13] UPDATED PARTS USED(NUTPLATES) PER DWG 143A0080 REV:-; [14] VERIFIED ALL STEPS COMPLETE

Part: PRESSURE DECK — CRACKED (BS 668) · airframe 32,578 hrs · 19,816 cycles

CRACK IN HORIZONTAL PRESSURE DECK BS 668; WL 202; RBL 202. BEGAN REMOVING FASTENERS IN THE REPAIR AREA IAW SRM 51-40-02. REMOVED PRESSURE SEAL AT BS 663.75-680 RBL51 IAW SRM 53-40-51-2R-2 STEP 4A(1). CUT AND REMOVED THE DAMAGED PART OF THE WEB IAW SRM 53-40-51-2R-2. PERFORMED DVI OF REPAIR IAW SRM 53-40-51-2R-2 STEP 4. D. (4) & (5). FABRICATED REPAIR DOUBLER, WEB, AND STIFFENERS.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 32,578 hrs · 19,816 cycles

FLOOR PANEL 242DF HAS PULLED FIBERS ON L/E ; / [01] DUE TO AMOUNT OF ALL DAMAGE FLOOR PANEL 242DF WITH PULLED FIBERS ON LEADING EDGE WAS REPLACED WITH A SERVICEABLE BOARD FABRICATED FROM BMS4-23 REV F TY II; LOT# 1450723-2. ALL INSERTS WERE INSTALLED USING BMS5-107 CL1 LOT# AK0DP4051K. PART MARKED PANEL IAW SRM 53-00-50-2R-0 PARA 1.A. (NOTE). AND 5.S. AND BOEING DWG# 144A5810-123.<BR><BR>THERMOMETER: ID: ATS2209 S/N: 43300739WS; [02] ADDING TO LINE 1; <BR><BR>INSERT P/N: SL5107A3-410<BR>APPLIED TAPE TO MATING SURFACE USING BMS8-283K TY1 LOT# 0NCO43865 IAW BOEING DWG 144A58810 SH.125; [03] FIXED LINE 2; <BR><BR>BOEING DWG# 144A58810 SH.123; [04] CORRECTION FOR LINES 2 & 3; DWG 114A5810; [05] CERTIFYING FABRICATION OF FLOORBOARD 242DF IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810; [06] VERIFIED FABRICATION OF FLOORBOARD 242DF IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 32,578 hrs · 19,816 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. ; / [01] BEGAN REMOVING FASTENERS IN THE REPAIR AREA IAW SRM 51-40-02; [02] FLIGHT DECK FLOOR ATDENTED AREA FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1; [03] REMOVED DAMAGED FLIGHT DECK FLOOR AT BS 270-BS 248 LBL 19-RBL 8 WL 207.54 PER SRM 51-40-02-0G-0; [04] FABRICATED REPLACEMENT FLOOR WEB .040 2024-T3 LOT #1457355-1; AND 2-EACH DOUBLERS .050 2024-T3 LOT # 1459974-1 PER SRM 51-30-01-0G-0 STEP 8; MM 51-00-51 STEP 2E AS SHOWN ON EA #1-173-34314 REV IR; [05] TREATED REPAIR PARTS REQUESTING OK TO PRIME PER EA # 1-173-34314 REV IR; [06] VERIFIED FABRICATED REPLACEMENT FLOOR WEB .040 2024-T3 LOT #1457355-1; AND 2-EACH DOUBLERS .050 2024-T3 LOT # 1459974-1 PER SRM 51-30-01-0G-0 STEP 8; MM 51-00-51 STEP 2E AS SHOWN ON EA #1-173-34314 REV IR OK TO PRIME.;

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 32,578 hrs · 19,816 cycles

CRACKED LOWER R/H COMPOSITE BULKHEAD AT BS663 RBL50 WL163. ; / [01] IDENTIFIED BS663 VAPOR BARRIER IAW SRM 57-10-10-0I-2 FIGURE 2 ITEM 4 AND TABLE 2 ITEM 4. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-10-10-1A-2 PARA 4.D.(1) AND WILL BE REPAIRED IAW SRM 51-70-04-2R-10 PER SRM 57-10-10-2R-2 PARA 1.C. VALIDATED SRM 57-10-10-2R-2 AND SRM 51-70-04-2R-10. REMOVED AN APPROXIMATE 10' LENGTH OF CRACK DAMAGE LOCATED AT RBL50; WL163 AND PREPARED DAMAGE AREA FOR REPAIR IAW SRM 51-70-04-2R-10 PARA 4.A-C.;

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 32,578 hrs · 19,816 cycles

CRACKED LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL36 WL159. ; / [01] IDENTIFIED BS663 VAPOR BARRIER IAW SRM 57-10-10-0I-2 FIGURE 2 ITEM 4 AND TABLE 2 ITEM 4. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-10-10-1A-2 PARA 4.D.(1) AND WILL BE REPAIRED IAW SRM 51-70-04-2R-10 PER SRM 57-10-10-2R-2 PARA 1.C. REMOVED MULTIPLE AREAS OF CRACK DAMAGE AND PREPARED DAMAGE AREA FOR REPAIR IAW SRM 51-70-04-2R-10 PARA 4.A-C.; [02] CERTIFIED IDENTIFICATION; ALLOWABLE DAMAGE; REPAIR AND DAMAGE REMOVAL IAW SRM 57-10-10-0I-2; SRM 57-10-10-1A-2; SRM 57-10-10-2R-2 AND SRM 51-70-04-2R-10.; [03] VALIDATED APPLICABILITY OF SRM 51-70-04-2R-10.; [04] VERIFIED CORRECTIVE ACTION STEPS 1-3; [05] FABRICATED FWD REPAIR PLIES OUT OF BMS 9-3 ST 1581 LOT#1458851-1 IAW SRM 51-70-04-2R-10 PAR 4D. OK TO INSTALL.; [06] VERIFIED FABRICATION OF FWD REPAIR PLIES IAW SRM 51-70-04-2R-10 PAR 4; OK TO INSTALL; [07] INSTALLED REPAIR PLIES USING BMS 8-301 LOT#1454403-1; VACUUM BAGGED AND CHECKED FOR LEAKS USING PRESSURE GAGE ID:ATS2587 S/N:5432766772 IAW SRM 51-70-04-2R-10 PAR 4D-E.; [08] VERIFIED INSTALLATION OF REPAIR PLIES USING; VACUUM BAGGED AND CHECKED FOR LEAKS IAW SRM 51-70-04-2R-10;

Part: BRACKET — BROKEN (L/H MLG W/W) · airframe 31,724 hrs · 19,319 cycles

LH MLG HOSE GUIDE ATTACH BRACKET (LOWER) BROKEN. / R/R L/H MLG HOSE GUIDE ATTACH BRACKET IAW SRM 51-40-02.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 31,638 hrs · 19,267 cycles

LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDER SEAL IS CRACKED. / REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDER SEAL PER AMM 53-31-31.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 31,638 hrs · 19,267 cycles

RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDER SEAL IS CRACKED. / REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDER PER AMM 53-31-31.

Part: LIGHT — INOPERATIVE (SEAT 22 DEF) · airframe 31,087 hrs · 18,913 cycles

22 DEF EMERGENCY LIGHT INOPERABLE. R & R EMERGENCY LIGHT ASSEMBLY 22 DEF, REF AMM 33-51-03. OPERATIONS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,041 hrs · 18,885 cycles

EMERGENCY (BULLNOSE) LIGHTS INOPERABLE OVER 10D AND 22D. RELAMPED PER AMM 33-51-03.

Part: ENGINE — FAILED (NR 2) · airframe 30,105 hrs · 18,299 cycles

#2 ENGINE FAILURE DURING CLIMB AFTER NOTICABLE POP AND YAW TO RIGHT SIDE. NO FIRE INDICATION NOTED. / R/R #2 ENGINE PER WI# 771-00-01 P/N OFF/ON CFM56-7B24 S/N OFF 805295 S/N ON 892568

Part: ENGINE — SHUTDOWN (RIGHT) · airframe 30,114 hrs · 18,303 cycles

F310 IND/DEN AIR RETURNED TO IND DUE TO #2 ENG IFSD (AUTO) CLIMB POWER @ 14;000FT LOUD BANG AND ENG ROLLED BACK TO ZERO CFR ROLLED /

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 30,030 hrs · 18,257 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP / RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT REF AMM 33-51-04 OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,878 hrs · 18,167 cycles

AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP RELAMPED EXTERIOR AFT SERVICE DOOR LIGHT PER AMM 33-51-04

Part: COVER — MISSING (EXIT SIGN) · airframe 16,700 hrs · 27,632 cycles

RT OVERWING EMERGENCY EXIT SIGN COVER MISSING AT SIDEWALL. R&R COVER IAW AMM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 16,700 hrs · 27,632 cycles

CABIN RT PHOTOLUMINESCENT STRIP DAMAGED BETWEEN BS. 328 TO BS. 955. R&R STRIP PER MT.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 16,700 hrs · 27,632 cycles

CABIN LT PHOTOLUMINESCENT STRIP DAMAGED BETWEEN BS. 342 TO BS. 955. R&R STRIP PER MT.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 27,632 hrs · 16,700 cycles

FORWARD RT EMERGENCY BATTERY PACK M1674 INOP. R&R BATTERY PACK PER AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

AFT GALLEY FLOOR PANEL 241YF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

AFT GALLEY FLOOR PANEL 241XF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,632 hrs · 16,700 cycles

FLOORBEAM INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, RBL 31. R&R INTERCOSTAL IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOORBOARD PANEL 242XF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOOR BOARD PANEL 241ACF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOORBOARD PANEL 242RF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 27,632 hrs · 16,700 cycles

FLOOR PANEL 222DF HAD FIBER DAMAGE THE LENGTH OF THE PANEL AND CORNER BROKEN OFF, BETWEEN BS. 270 TO BS. 420. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOOR BOARD PANEL 241ADF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOOR BOARD PANEL 241AAF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOORBOARD PANEL 221EF HAD FIBER DAMAGE THE LENGTH OF THE PANEL, BETWEEN BS. 270 TO BS. 420. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOORBOARD PANEL 241AEF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOORBOARD PANEL 242SF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOORBOARD PANEL 241ABF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 27,632 hrs · 16,700 cycles

FORWARD CARGO COMPARTMENT STRINGER GUSSET CRACKED AT BS. 500D, STR. 19L. R&R GUSSET PER SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOORBOARD PANEL 241ZF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 27,632 hrs · 16,700 cycles

FLOOR PANEL 222AF HAD FIBER DAMAGE TO UPPER SURFACE OF THE PANEL, BETWEEN BS. 270 TO BS. 420. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOORBOARD PANEL 242WF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,632 hrs · 16,700 cycles

AFT GALLEY SERVICE DOOR THRESHOLD CORRODED Z ANGLE BETWEEN BS. 965 TO BS. 986. R&R Z ANGLE PER SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOORBOARD PANEL 242TF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOORBOARD PANEL 242UF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,632 hrs · 16,700 cycles

CABIN FLOORBOARD PANEL 242VF DAMAGED, BETWEEN BS. 887 TO BS. 1016. R&R PANEL PER AMM.

Part: SUPPORT — CRACKED (RT HORIZ STAB) · airframe 27,633 hrs · 16,700 cycles

RH HORIZ STAB PANEL 343CB TE SUPPORT CRACKED (MARKED) / REMOVED AND REPLACED SUPPORT PER SRM 51-40-02 AND BOEING DWG 185A1702

Part: SUPPORT — CRACKED (LT HORIZ STAB) · airframe 27,633 hrs · 16,700 cycles

LH HORIZ STAB PANEL 333DB TE SUPPORT CRACKED (MARKED) / REMOVED AND REPLACED SUPPORT PER SRM 51-40-02 AND BOEING DWG 185A1702

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,632 hrs · 16,700 cycles

PASSENGER SEAT (1) CORRODED AT BS. 843, LBL 45. R&R #1 SEAT TRACK PR SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,632 hrs · 16,700 cycles

PASSENGER SEAT (1) CORRODED AT BS. 815, LBL 45. R&R #1 SEAT TRACK PR SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 27,604 hrs · 16,680 cycles

L2 DOOR SLIDE GIRT OUT OF ADJUSTMENT. INSTALLED L2 DOOR SLIDE PER MT AND AMM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 27,153 hrs · 16,389 cycles

RT MAIN LANDING GEAR WHEEL WELL CENTER WING REAR SPAR VAPOR WEB CRACKED, BETWEEN RBL 43.0 TO RBL 45.75. REPAIRED WEB PER SRM.

Part: WEB — DENTED (FLIGHT DECK FLOO) · airframe 26,461 hrs · 15,948 cycles

FLIGHT DECK FLOOR AT STATION 256 HAS DENT APPROX 18' X 3.5'; MAX DEPTH .070 WITH A CREASE AT FRAME AND SEVERAL GOUGES WITHIN DENT; DEEPEST MEASURING .077. NO PULLED FASTENERS OR LOOSE FASTENERS. / REPAIRED FLIGHT DECK FLOOR AT STA. 256 IAW ER 19-01963 REV. IR AND EA 1-753-34314. REV. IR

Part: BATTERY PACK — FAILED (CABIN) · airframe 26,279 hrs · 15,825 cycles

RT EMERGENCY EXIT LIGHT BATTERY PACK M1675 FAILED TEST. R&R BATTERY PACK PER AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,203 hrs · 15,110 cycles

R1 DOOR ESCAPE SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED SLIDE IAW MT.

Part: INTERCOSTAL — CRACKED (E&E BAY) · airframe 24,433 hrs · 14,607 cycles

AFT E&E COMPARTMENT; FLOORBEAM INTERCOSTAL IS CRACKED; BETWEEN STA 312 AND STA 328; AT THE UPPER CENTER FASTENER HOLE AT 45 LBL. / REMOVED AND REPLACED PER SRM 51-40-02.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 23,656 hrs · 14,118 cycles

L1 DOOR SLIDE FELL OUT OF CONTAINER. DID NOT DEPLOY, REINSTALLED THE SLIDE IAW MM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 21,855 hrs · 12,916 cycles

LT FORWARD VAPOR BARRIER MAIN WHEEL WELL CRACKED AT BS 663, LBL 30. REPAIRED BARRIER IAW EA.

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 21,022 hrs · 12,392 cycles

L MAIN WHEEL WELL STA 663 FIBER GLASS VAPOR BARRIER PANEL HAS CRACK AT LBL 36 THAT EXTEND BEYOND VERTICAL STIFFENER. / :REPAIRED PER SRM 51-70-04 REPAIR #10 AND E/A 1-757-14061.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 21,022 hrs · 12,392 cycles

AFT CARGO FLOOR PANEL 140CF PERIMETER OF PANEL AT TAPE AREA HAS CORROSION. / FABRICATED REPLACEMENT FLOOR PANEL 140CF PER BOEING DWR 453A2610.

Part: BRACKET — CRACKED (AFT CARGO BAY) · airframe 21,022 hrs · 12,392 cycles

AFT CARGO STA 947 LBL 10' AFT BULKHEAD LOWER SUPPORT BRACKET CRACKED (MARKED) / INSTALLED NEW AFT BULKHEAD LOWER SUPPORT BRACKET @ STA 947 LBL10 PER SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 21,021 hrs · 12,392 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS 773, RBL 13.5. REPAIRED SUPPORT PER EA.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 21,022 hrs · 12,392 cycles

AFT CARGO STA 727E THRU 747 RH TRANS. ANGLE HAS CORROSION IN AND AROUND NUT PLATE HOLES / REMOVED AND REPLACED R/H TRANSITION ANGLE FROM STA 727-767 PER SRM 51-40-02.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 21,022 hrs · 12,392 cycles

AFT CARGO STA 747 THRU 767 RH TRANS. ANGLE HAS CORROSION IN AND AROUND NUT PLATE HOLES / REMOVED AND REPLACED R/H TRANSITION ANGLE FROM STA 727-767 PER SRM 51-40-02.

Part: NONE — CORRODED (AFT CARGO BAY) · airframe 21,022 hrs · 12,392 cycles

AFT CARGO STA 847 THRU 869 RH TRANS. ANGLE HAS CORROSION IN AND AROUND NUT PLATE HOLES / REMOVED AND REPLACED TRANSITION ANGLE STA 847-869 PER SRM 51-10-02 SRM 51-40-02.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 21,022 hrs · 12,392 cycles

AFT CARGO STA 727D THRU 727E LH TRANS. ANGLE HAS CORROSION IN AND AROUND NUT PLATE HOLES / WP:E105618-BLACKBURN; RICHARD - 07/10/2017 01:29 COMPLETE: REMOVED L/H TRANSITION ANGLE FROM STA 727 TO 847 AND INSTALLED NEW SERVICEABLE L/H TRANSITION ANGLE FROM STA 727 TO 847 IAW SRM 51-40-02.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 21,022 hrs · 12,392 cycles

AFT CARGO STA 727B + 15' RH TRANS. ANGLE HAS CORROSION IN AND AROUND NUT PLATE HOLE / REMOVED AND REPLACED R/H TRANSITION ANGLE FROM STA 727-767 PER SRM 51-40-02.

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 21,022 hrs · 12,392 cycles

CABIN FLOOR PANEL 241AF UPPER FACE SHEET HAS PEELING FIBER DAMAGE. MRKD / REMOVED AND REPLACED CABIN FLOOR PANEL 241AF PER AMM 53-21-00. REF TASK CARD JPANEL-231-CLOSE FOR OK TO CLOSE.

Part: BRACKET — CRACKED (RT WING) · airframe 21,022 hrs · 12,392 cycles

RIGHT WING UPPER PANEL 651BT; FWD INBOARD SUPPORT BRACKET CRACKED.(MARKED) / REMOVED AND REPLACED BRACKET PER SRM 51-10-02 & 51-40-02.

Part: RIB — ELONGATED (RT WING) · airframe 21,022 hrs · 12,392 cycles

RIGHT WING UPPER SHELF PANEL AT INBOARD DEFLECTION RIB ATTACHMENT HOLES ELONGATED. / REPAIRED BEAM PER SRM 57-51-02-2R-1.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 20,025 hrs · 11,772 cycles

AFT CARGO PIT DOOR CUTOUT FORWARD THRESHOLD COVER CRACKED AT AFT EDGE. REPAIRED SCUFF PLATE IAW EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 20,025 hrs · 11,772 cycles

AFT CARGO COMPARTMENT LOWER DOOR CUTOUT SILL WEB CORRODED. R&R WEB IAW SRM & DWG.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 20,025 hrs · 11,772 cycles

AFT CARGO DOOR SKIN GOUGED AT BS 847, STRINGER 25R. REPAIRED THE SKIN IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 18,899 hrs · 11,087 cycles

FORWARD LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 16,120 hrs · 9,470 cycles

LEFT EMER LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 16,120 hrs · 9,470 cycles

RIGHT EMER LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 16,111 hrs · 9,467 cycles

FORWARD EMER EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 15,800 hrs · 9,270 cycles

L1 DOOR EXTERNAL EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 15,347 hrs · 9,004 cycles

ELECTRICAL GND POWER DOOR CUT OUT LOWER LATCH ATTACH POST CRACKED. REPAIRED CUT OUT IAW EA.

Part: WEB — CRACKED (LT MLG WW) · airframe 13,922 hrs · 8,148 cycles

CENTER WING REAR SPAR VAPOR WEB CRACKED AT STATION 727, LBL 34. REPAIRED WEB IAW EA.

Part: LIGHT — CRACKED (CABIN) · airframe 11,426 hrs · 6,686 cycles

RIGHT AFT SERVICE DOOR INTERIOR EGRESS LIGHT CRACKED. R & R LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,426 hrs · 6,686 cycles

LEFT FWD ENTRY DOOR EXTERIOR EGRESS LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 9,065 hrs · 5,361 cycles

RT AFT EMERGENCY EXIT BATTERY FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 6,921 hrs · 4,104 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF HOLDER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: LIGHT — CRACKED (CABIN) · airframe 5,324 hrs · 3,145 cycles

MID CABIN CEILING EMERGENCY EXIT LIGHT IS CRACKED AT ATTACH POINT. REMOVED AND REPLACED MID CABIN CEILING EMERGENCY EXIT LIGHT IAW M/M 33-51-01-960-802 SEC 3-C ITEM 6. FUNCTIONAL TEST WAS GOOD AS PER M/M 33-51-01-960-802 SEC 3-C ITEM 7.

Part: LENS — MISSING (CABIN) · airframe 4,885 hrs · 2,874 cycles

EMERGENCY EXIT LIGHT COVER AT OVERWING (SIDEWALL) IS MISSING (CAPT'S SIDE). REPLACED MISSING EXIT LIGHT LENS PER M/M. LIGHT OPS CHECK GOOD.

Part: COVER — CRACKED (CABIN) · airframe 3,534 hrs · 2,034 cycles

LEFT EPPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER M/M.

Part: LIGHT — CRACKED (CABIN) · airframe 2,978 hrs · 1,730 cycles

EEPLS CRACKED. REMOVED AND REPLACED EEPLS IAW M/M.