N7840A

Part: CHARGER — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,351 hrs · 40,168 cycles

AFT L2 OVERHEAD EMERGENCY EXIT LIGHT INOP.<[01] MULTIPLE AFT EMERGENCY EXIT LIGHTS INOP. TROUBLESHOT PER FIM TASK 30-50-801 AND WDM 33-51-14-5. FOUND AFT RIGHT EMERGENCY BATTERY TO BE AT FAULT.;[02] R AND R LEFT AND RIGHT BATTERY CHARGERS AND LEFT BATTERY PER MM 33-51-06. EMERGENCY LIGHTS CHECK GOOD

Part: BATTERY — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,351 hrs · 40,168 cycles

AFT L2 OVERHEAD EMERGENCY EXIT LIGHT INOP.<[01] MULTIPLE AFT EMERGENCY EXIT LIGHTS INOP. TROUBLESHOT PER FIM TASK 30-50-801 AND WDM 33-51-14-5. FOUND AFT RIGHT EMERGENCY BATTERY TO BE AT FAULT.;[02] R AND R LEFT AND RIGHT BATTERY CHARGERS AND LEFT BATTERY PER MM 33-51-06. EMERGENCY LIGHTS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,048 hrs · 39,979 cycles

EMERGENCY LIGHTS @ AISLE 9C/12C/17C/16D/19D; AFT GALLEY OVERHEAD & AFT ENTRY INOP<[01] R/R LH AISLE MID BATTERY PACK & AFT GALLEY RH BATTERY PACK IAW AMM 33-51-06 OPS CHECK GOOD

Part: BATTERY PACK — FAULTY (ZN 200 FUS TOP) · airframe 63,899 hrs · 39,880 cycles

AISLE EMERGENCY LIGHTS AT 16 AND 18 AND AFT GALLEY CEILING LIGHT AS WELL AS R2 DOOR EXTERNAL EMERGENCY LIGHTS GO OUT AFTER 5 SECONDS.<[01] REPLACED BATTERY PACK M1872. REF. AMM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,766 hrs · 39,789 cycles

EMERGENCY EXIT LIGHTS INOP OVER AFT ENTRY DOOR AND SERVICE DOOR SLIDE LIGHT<[01] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 63,613 hrs · 39,687 cycles

EMERGENCY LIGHTS FAILED CAPACITY TEST RH AFT OF OVERWING EMERGENCY DOOR<[01] R/R BATTERY PACK AT POSITION D10746 REF AMM 33-51-06;[02] BATTERY PACK AT POSITION M 10673REF AMM 33-51-06;[03] R/R BATTERY PACK AT POSITION M 10673REF AMM 33-51-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 63,613 hrs · 39,687 cycles

AFT ENT EMERGENCY DOOR SIGN LIGHTS FAILED CAPACITY CHECK<[01] R/R BATTERY PACK AT POSITION D10744 REF AMM 33-51-06;[02] R/R BATTERY PACK AT POSITION M10672 REF AMM 33-51-06

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 63,445 hrs · 39,577 cycles

MISSING LENS ON EMERGENCY LIGHT AT LOCATION 19DEF MISSING LENS ON EMERGENCY LIGHT AT LOCATION 19DEF<[01] INSTALLED EMERGENCY LIGHT LENSE AT ROW 19DEF IAW AMM 33-51-03

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,445 hrs · 39,577 cycles

AFT ENTRY DOOR; AFT SERVICE DOOR AND ROWS 19ABC;19DEF AND 24ABC EMERGENCY LIGHTS INOP AFT ENTRY DOOR AFT SERVICE DOOR AND ROWS 19ABC19DEF AND 24ABC EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK FROM POWER SUPPLY M1673 AND BATTERY PACK AND FUSES FROM POWER SUPPLY M1672 IAW AMM 33-51-06. OPS CHECK GOOD.

Part: FUSE — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,445 hrs · 39,577 cycles

AFT ENTRY DOOR; AFT SERVICE DOOR AND ROWS 19ABC;19DEF AND 24ABC EMERGENCY LIGHTS INOP AFT ENTRY DOOR AFT SERVICE DOOR AND ROWS 19ABC19DEF AND 24ABC EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK FROM POWER SUPPLY M1673 AND BATTERY PACK AND FUSES FROM POWER SUPPLY M1672 IAW AMM 33-51-06. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,256 hrs · 39,456 cycles

AFT GALLEY EMERGENCY LIGHTS INOP<[01] R&RED EMERGENCY LIGHT BATTERY PACK AT STA 952 PER AMM 33-51-06.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,507 hrs · 38,971 cycles

AFT GALLEY EMERGENCY EXIT CEILING LIGHT INOP / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK PER AMM 33-51-06. OP?S CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,177 hrs · 38,751 cycles

L/H AFT ENTRY DOOR EMERGENCY LIGHT IS INOP. / [01] REPLACED EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (R/H CABIN) · airframe 61,997 hrs · 38,633 cycles

AFT RIGHT SIDE EMERGENCY LIGHTS INOP / [01] REPLACED AFT POWER SUPPLY BATTRY PACK IAW AMM 3-51-06;OPS CECKE GOOD

Part: BATTERY PACK — INOPERATIVE · airframe 61,837 hrs · 38,524 cycles

RH AFT EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE ON TEST. AFT SERVICE DOOR IN/OUT / [01] R&R THE AFT RH EMERGENCY LIGHTS BATTERY SUPPLY IAW AMM 33-51-06. OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (AFT CABIN) · airframe 61,624 hrs · 38,383 cycles

AFT EMERG LIGHT RH INOP / [01] REPLACED RH AFT BATTERY PACK; OPTS CHECK GOOD REF AMM 33-51-06.

Part: SIGN — MISSING (R/H CABIN) · airframe 60,896 hrs · 37,881 cycles

RH EMERGENCY EXIT WIDOW LOWER EXIT SIGN MISSING DIRECTIONAL ARROW. / [01] REMOVED AND REPLACED LENS ON RH EMERGENCY EXIT SIGN PER AMM 33-51-01.;[02] INSPECTED

Part: PROXIMITY SENSOR — FAILED (#3 SLAT OB) · airframe 60,756 hrs · 37,799 cycles

AFTER TAKEOFF #3 LEADING EDGE SLAT WOULD NOT RETRACT. / [01] FLAP/SLAT ELECTRONICS UNIT BITE SHOWS F/C 27-81204 SL3 PROX OUTBOARD; #3 SLAT OUTBD. PROX. SENSOR SHOWS TARGET NEAR WHEN TARGET FAR; PERFORMED FIM 27-88 TASK 803; REPLACED #3 SLAT OUTBD. PROX. SENSOR IAW AMM 27-88-11.

Part: SIGN — MISSING (R/H OVERWING) · airframe 60,616 hrs · 37,709 cycles

EXIT SIGN AT OVERWING EMERGENCY EXIT ON F/O SIDE ;SIGN MISSING. REINSTALLED EXIT SIGN AT OVERWING EXIT F/O SIDE IAW AMM 33-51-04. OK FOR CONTINUE IN SERVICE

Part: LENS — BROKEN (CABIN) · airframe 60,283 hrs · 37,501 cycles

EXIT IDENTIFIER ON FWD LAV HAS A BROKEN LENS / [01] REMOVED AND REPLACED BROKEN EXIT IDENTIFIER LENS PER AMM 33-51-01-960-802 3.C.(5) & (9).;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED CORRECTIVE ACTION 1. WORKSCOPE COMPLETE.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 60,283 hrs · 37,501 cycles

SUPPLEMENTAL INFORMATION: FWD CARGO BAY AFT CORNER SCUFF PLATE CRACED / [01] WELDED CRACKED AREA ON FCB; AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-30-15-2R-1 PARA 4.B.(2) AND (4)<BR>WELDING MACHINE CAL ID E10583; S/N;KJ256554;[02] VERIFIED CORRECTIVE ACTION #1

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 60,283 hrs · 37,501 cycles

FWD CARGO BAY AFT CORNER SCUFF PLATE CRACED / [01] WELDED CRACKED AREA ON FCB; AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-30-15-2R-1 PARA 4.B.(2) AND (4)<BR>WELDING MACHINE CAL ID E10583; S/N;KJ256554;[02] VERIFIED CORRECTIVE ACTION #1;[03] PT INSPECTED WELDED AREA IAW SOPM 20-20-02. NO CRACKS NOTED. EQUIP USED: RADIOMETER ID: ATS2561-1;2;3;[04] SANDED WELD REPAIR SMOOTH PER SRM 53-30-15-2R-1 PARA 4.B.(5);[05] VERIFIED CORRECTIVE ACTION 4.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 60,283 hrs · 37,501 cycles

FWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED / [01] WELDED CRACKED AREA ON FCB; FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-30-15-2R-1 PARA 4.B.(2) AND (4)<BR>WELDING MACHINE CAL ID E10583; S/N;KJ256554;[02] VERIFIED CORRECTIVE ACTION #1;[03] PT INSPECTED WELDED AREA IAW SOPM 20-20-02. NO CRACKS NOTED. EQUIP USED: RADIOMETER ID: ATS2561-1;2;3;[04] SANDED WELD REPAIR SMOOTH PER SRM 53-30-15-2R-1 PARA 4.B.(5);[05] VERIFIED CORRECTIVE ACTION 4.

Part: STRIP — CRACKED (AFT CARGO) · airframe 60,283 hrs · 37,501 cycles

AFT CARGO BAY FLOOR PNL 140DF AFT CAP STRIP CRACKED BS 947 / [01] REMOVED AND REPLACED ACB AFT CAPSTRIP AT BS 947 IAW AMM 25-52-10-400-801<BR><BR>TOOL USED <BR>25 IN LBS SCREW GUN <BR>ID:ATS674<BR>S/N:UNKNOWN;[02] VERIFIED CORRECTIVE ACTION 1.

Part: BAFFLE — CRACKED (FWD CARGO) · airframe 60,283 hrs · 37,501 cycles

FWD CARGO BAY BAFFLE CRACKED BS 500 -500A LBL 24 / [01] THERE IS NO SRM ALLOWABLE DAMAGE FOR FWD CARGO BAY BAFFLE CRACKED. PART TO BE REPAIRED BY REPLACEMENT BY IAW SRM 51-10-02-0G-0 STEP 9;[02] REMOVED FCB BAFFLE BS 500 - BS 500A LBL24 IAW SRM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW FCB BAFFLE IAW SRM 51-40-05-0G-0 AND DWG 143A7505 ID:0037 REV:-<BR><BR>OK TO INSTALL NEW BAFFLE;[04] VERIFIED CORRECTIVE ACTION #3<BR>OK TO INSTALL NEW BAFFLE GIVEN;[05] INSTALLED NEW BAFFLE AT FCB BS 500 - BS 500A LBL 24 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 ID:0037 REV:-;[06] VERIFIED CORRECTIVE ACTION #5;[07] VERIFIED ALL STEPS COMPLETE

Part: ATTACH ANGLE — CRACKED (AFT CARGO) · airframe 60,283 hrs · 37,501 cycles

AFT CARGO BAY RBL 13.8 TIE DOWN TRACK ATTACH CLIP CRACKED BS 887 / [01] REMOVED AFT CARGO BAY TIE DOWN TRACK ATTACH CLIP AT BS 887; RBL 13.8 IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW CLIP IAW SRM 51-40-05 AND DWG 147A3287 REV: -;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2;[04] REQ. OK TO INSTALL NEW CLIP;[05] VERIFIED CORRECTIVE ACTION #10<BR> OK TO INSTALL NEW CLIP GIVEN;[06] INSTALLED CLIP P/N 147A7580U20 AT AFT CARGO BAY RBL 13.8 ; BS 887 IAW SRM 51-40-02-0G-0 AND DWG 147A0060 REV.- AND DWG 147A3287 REV.-;[07] VERIFIED CORRECTIVE ACTION #6;[08] VERIFIED TASK COMPLETE;[09] UPDATE CORRECTIVE ACTION #5 SHOULD STATE: VERIFIED CORRECTIVE ACTION #4;[10] CORRECTED CORRECTIVE ACTION #5

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 60,283 hrs · 37,501 cycles

CORROSION ON STIFFENER P/N 148A8640-10 BS 1124 RBL 20; APU CAVITY / [01] APPLICABILITY STATEMENT; NOT FOUND ALLOWABLE DAMAGE IN THE SRM; REPAIR BY REPLACEMENTE PART IAW SRM 51-10-02-0G-0 PARA. 9;[02] REMOVED STIFFNER IAW SRM 51-40-02-0G-0;LOCATED AND DRILLED NEW STIFFENER P/N 148A8640-10 PO # 830198 IAW SRM 51-40-05-0G-0 AND DWG 148A8650 REV.-A.OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION 1 AND 2 OK TO INSTALL;[04] INSTALLED STIFFENER P/N 148A8640-10 BS 1124 RBL 20; APU CAVITY IAW SRM 51-40-02-0G-0 AND DWG 148A8650 REV.-A;[05] VERIFIED ITEM 4 CORRECTIVE ACTION.;[06] UP DATE MEASUREMENTS;[07] VERIFIED MEASUREMENTS UPDATED.

Part: STIFFENER — CRACKED (AFT CARGO) · airframe 60,283 hrs · 37,501 cycles

CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS914 RBL11. MARKED. / [01] REMOVED SUPPORT ANGLE AT ACB BS 914 RBL 11. IAW SRM 51-40-02<BR><BR>EVALUATED CRACK ON ACB ON SUPPORT ANGLE BS 914 RBL 11 SUPPORT ANGLE DAMAGE FOUND TO BE OUT LIMITS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9.;[02] RECEIVED REPLACEMENT SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB RBL11; PO#833343/1; LOT#1481105-1. LOCATED AND DRILLED HOLES IAW SRM 51-40-05-0G-0 AND DWG 147A7221 REV:D;[03] OK TO INSTALL NEW STIFFINER.;[04] VERIFIED CORRECTIVE ACTIONS 1-3;[05] INSTALLED NEW STIFFINER IAW SRM 51-40-02 AND DWG 147A7221 REV: D.;[06] VERIFIED CORRECTIVE ACTION 5;[07] UPDATED MEASUREMENT;[08] UPDATED MEASUREMENTS AND RECEIVED REPLACEMENT SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB RBL11; PO#833343/1; LOT#1481105-1. LOCATED AND DRILLED HOLES IAW SRM 51-40-05-0G-0 AND DWG 147A7221 REV:D;[09] VERIFIED JOB COMPLETE;[10] CORRECTED MEASUREMENT SECTION.;[11] VERIFIED MEASUREMENT SECTION CORRECTED.

Part: SHIELD — CRACKED (AFT CARGO) · airframe 60,283 hrs · 37,501 cycles

CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767 - BS787 RBL22. / [01] RECEIVED NEW SHIELD ASSEMBLY ITEM: 146A8127U1ATSMRO LOT: 1473909-1. LOCATED AND DRILLED NEW SHIELD IAW SRM 51-40-02 AND DWG 146A8127 ID:0001 REV: C;[02] SRM 53-60-15-1A-1 IS APPLICABLE. NO ALLOWABLE DAMAGE. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 31-10-02-0G-0 PAR.1.9.;[03] SRM 53-60-15-1A-1 IS APPLICABLE. NO ALLOWABLE DAMAGE. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR.1.9.;[04] VERIFIED JOB COMPLETE

Part: TRACK — CRACKED (AFT CARGO) · airframe 60,283 hrs · 37,501 cycles

CRACKED TRACK AT AFT CARGO BAY BS767 LBL17. MARKED. / [01] REMOVED DAMAGED TRACK IAW SRM 51-40-02;[02] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS AIRCRAFT;[03] DAMAGE TO TRACK FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2. REPAIR BY REPLACEMENT IAW SRM 51-10-02.;[04] RECEIVED NEW TIE DOWN TRACK ASSY PN 146A7501-1 FROM STORES PO 851004. <BR>LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 146A7500.;[05] ENTERED MEASUREMENTS.;[06] OK TO INSTALL TIE DOWN TRACK ASSY.;[07] VERIFIED STEPS 1-6;[08] INSTALLED TIE DOWN TRACK ASSY AT ACB BS.727 T BS.847 IAW SRM 51-40-02 AND BOEING DWG 146A7500 REV:C;[09] STEP #1 COMPLIED;[10] INSTALLED TIE DOWN TRACK ASSY AT ACB BS.727 T BS.867 IAW SRM 51-40-02 AND BOEING DWG 146A7500 REV:C;[11] VERIFIED CORRECTIVE ACTION 8-10;[12] UPDATE PARTS;[13] VERIFIED JOB COMPLETE

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,283 hrs · 37,501 cycles

CRACKED BULKHEAD ATTACH ANGLE AT AFT CARGO BAY BS866 LBL11. MARKED. / [01] REMOVED ANGLE AT ACB BS 866 LBL 11. IAW SRM 51-40-02 <BR><BR>EVALUATED CRACK ON ACB ON ANGLE BS 914 RBL 11 SUPPORT ANGLE DAMAGE FOUND TO BE OUT LIMITS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9.;[02] RECEIVED NEW ANGLE P/N 149A8109U114 FROM TOOL ROOM AND LOCATED AND DRILLED AT BS 866 LBL11. REQUES OK TO INSTALL NEW ANGLE.;[03] RECEIVED NEW ANGLE P/N 149A8109U114 FROM TOOL ROOM AND LOCATED AND DRILLED AT BS 866 LBL11. IAW SRM 51-40-05 ; REQUES OK TO INSTALL NEW ANGLE.;[04] VERIFIED CORRECTIVE ACTIONS 1-3<BR><BR>OK TO INSTALL;[05] INSTALLED NEW ANGLE AT BS 866 LBL11. IAW SRM 51-40-02 AND DWG:149A8102 ID:0017 REV:-;[06] VERIFIED CORRECTIVE ACTION 5.;[07] VERIFIED PART REPLACED. ALL WORK ACCOMPLISHED.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 60,283 hrs · 37,501 cycles

CORROSION ON AFT SHIELD AT AFT CARGO BAY BS848 RBL20. / [01] SRM 53-60-15-1A-1 IS APPLICABLE. NO ALLOWABLE DAMAGE. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 31-10-02-0G-0 PAR.1.9. <BR><BR>RECEIVED NEW SHIELD ASSEMBLY ITEM: 7530336 PO# 821738/1. LOCATED AND DRILLED NEW SHIELD IAW SRM 51-40-02 AND DWG'S 146A8127 ID:0003 REV: C AND 146A0081 ID:0010 REV:A;[02] VERIFIED CORRECTIVE ACTION 1

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 60,283 hrs · 37,501 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A+13 - BS500B+7; BS500B+18; BS500C+4 RBL23. MARKED. / [09] REMOVED CORRODED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 400 BS 500D AND FABRICATED LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT OUT OF MATERIAL BAC 1496-444 7075 T62. APPLIED PRIMER IAW SRM 53-00-53-1A-2; SOPM 20-43-03; SRM 51-40-02; 51-40-05; DWG 143A7500 ID 17 REV A; SOPM 20-43-03;[13] CORRECTION STATEMENT OR THE FOLLOWING STEP'S 9; 10; 11 AND 12. CUSTOMER CARD TTG8Q00AJ1D0 IS FOR THE EVALUATION; REMOVAL OF CORROSION AND THE FABRICATION OF RH FLOOR TO SIDEWALL SUPPORT ONLY; BS 500A TO 500D RBL 23. FROM MATERIAL BAC 1496-444 7075 T62 LOT #1467644-1. APPLIED PRIMER IAW SRM 53-00-53-1A-2; SOPM 20-43-03; SRM 51-40-02; 51-40-05; DWG 143A7500 ID 17 REV A; SOPM 20-43-03.;[14] VERIFIED CORRECTIVE ACTION 13

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 60,283 hrs · 37,501 cycles

CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS918 RBL11. MARKED. / [01] REMOVED SUPPORT ANGLE AT ACB BS 918 RBL 11. IAW SRM 51-40-02<BR><BR>EVALUATED CRACK ON ACB ON SUPPORT ANGLE BS 918 RBL 11 SUPPORT ANGLE DAMAGE FOUND TO BE OUT LIMITS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9.;[02] RECEIVED NEW STIFFENER P/N 147A7221Y32 LOT:1473175-1; LOCATED AND DRILLED NEW STIFFENER AT ACB BS 918 REBL 11 IAW SRM 51-40-05. REQUEST OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTIONS 1; 2. <BR><BR>OK TO INSTALL;[04] INSTALLED NEW STIFFENER AT ACB BS 918 REBL 11 IAW SRM 51-40-02 AND DWG:147A7221 ID:0028 REV:-;[05] INSTALLED NEW STIFFENER AT ACB BS 918 RBL 11 IAW SRM 51-40-02 AND DWG:147A7221 ID:0028 REV:-;[06] VERIFIED CORRECTIVE ACTION 4; 5.;[07] PART REPLACED. ALL WORK ACCOMPLISHED.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 60,283 hrs · 37,501 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A+6; BS500A+10; BS500A+15; BS500B+11; BS500C+7; BS500C+11; BS420 TO BS440; BS450 - BS462 LBL23. MARKED. / [01] REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT; WITH ORIGINAL THICKNESS 0.040'<BR>BS420 TO BS440 L= 1.150' W= 0.600' D=0.006' FOUND OUT OF LIMITS.<BR>BS450 TO BS462 L= 1.00' W= 0.500' D= 0.008' FOUND OUT LIMITS.<BR>BS500A+6 L= 1.00' W= 0.600' D= 0.0025' FOUND IN LIMITS.<BR>BS500A+10 L= 0.800' W= 0.400' D= 0.003' FOUND IN LIMITS.<BR>BS500A+15 L= 1.100' W= 0.500' D= 0.008' FOUND OUT OF LIMITS.<BR>BS500B+11 L= 1.00' W= 0.500' D= 0.002' FOUND IN LIMITS.<BR>BS500C+7 L= 0.900' W= 0.400' D= 0.003' FOUND IN LIMITS.<BR>BS500C+11 L=1.00' W= 0.500' D= 0.0055' FOUND OUT OF LIMITS.INSTALLED FLOOR TO SIDEWALL SUPPORT SPLICE REPAIR LBL23 BS 480+10 AND NUTPLATES AND DOUBLERS IAW SRM 51-40-02, SRM 51-40-10, SRM 53-00-53-2R-6 SECTION 4. K,L AND DWG 143A7501 ID: 0001 REV: B.

Part: ANGLE — CORRODED (AFT FUSELAGE) · airframe 60,283 hrs · 37,501 cycles

CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS867 LBL9. / [01] ENTERED MEASUREMENTS;[02] REMOVED CORROSION IAW SRM 51-10-02. AREA MEASURES 1.00' X 0.300' X 0.003'. ORIGINAL THICKNESS:0.090'. REMAINING MATERIAL: 0.087';[03] VERIFIED CORRECTIVE ACTION 2;[04] EDIT ITEM 2. <BR>MICROMETER ID: ATS1671; SN 65093024; CAL DUE 10/2022;[05] HFEC INSPECTED BLEND AREA PER NDTM PT6 51-00-00 PROCEDURE 23; NO CRACKS NOTED; EQUIP ID ATS729;[06] UT INSPECTED BLEND AREA PER NDTM PT4 51-00-00 PROCEDURE 2; LOWEST READING WAS .087'; EQUIP ID ATS2342;[07] CORROSION REMOVAL ON AFT BULKHEAD FLOOR TO SUPPORT BS 867 LBL 9 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM;[08] VERIFIED CORRECTIVE ACTION 7;[09] AFT CARGO BAY- AFT BULKHEAD VACUUM WASTE TANK ENCLOSURE SUPPORT ANGLE REPAIRED PER ER# 22-153-00340 REV:A. <BR><BR>TASKCARD COMPLETED.;[10] COMPLETED MEASUREMENT PARAMETERS #15.;[11] VERIFIED CORRECTIVE ACTION #9 AND #10;[12] VERIFIED TASK COMPLETE

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 60,283 hrs · 37,501 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727A+15; BS727B+6; BS727B+12; BS727C+10 - BS827 LBL21. / [01] REMOVED CORROSION AFT CARGO BAY ON FLOOR SIDEWALL SUPPORT FROM BS 727+15 TO 827 ; LBL 21 ; WL 156 ; WORK AREA L 1.0' X W 1.0' X D 0.030' ; ORIGINAL MATERIAL THICKNESS 0.040'; MATERIAL REMAINING 0.010' ; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; STEP 4A; USING DIAL DEPTH GAUGE ID:ATS400;S/N: UNKNOWN; DUE 08/2022;[02] INSPECTED ACTION 1;[03] FABRICATED NEW AFT FLOOR TO SIDEWALL SUPPORT; SPLICES FROM BAC1496-377#7075T62; LOT # 1467164-1; LOCATED AND DRILL IAW SRM 51-40-05-0G-0 AND DWG 146A7502; ID:001; REV:A ; APPLIED CHEMICAL CONVERSION IAW AMM 51-21-41-370-802; OK TO APPLY PRIMER;[04] VERIFIED CORRECTIVE ACTION 3.;[05] APPLIED PRIMER NEW AFT FLOOR TO SIDEWALL SUPPORT; SPLICES IAW AMM 51-21-72-370-804; OK TO INSTALL SPLICES;[06] APPLIED PRIMER TO REPLACEMENT AFT FLOOR TO SIDEWALL SUPPORT AND SPLICE IAW AMM 51-21-72-370-804; OK TO INSTALL SPLICE AT BS 747+10';[07] VERIFIED CORRECTIVE ACTION 6. OKAY TO INSTALL SPLICE AT BS747+10.;[08] FABRICATED NEW AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT FROM BS 727 - BS 847 LBL 21 AND INSTALLED SPLICE ON FLOOR TO SIDEWALL SUPPORT AT BS 747 +10 IAW SRM 51-40-05-0G-0; DWG 146A7502 ID 1 REV:A; SRM 51-40-02-0G-0;[09] VERIFIED CORRECTIVE ACTION 8

Part: TRACK — CORRODED (AFT CARGO) · airframe 60,283 hrs · 37,501 cycles

CORROSION ON TRACK AT AFT CARGO BAY RBL13 BS847; BS843; BS812; BS818; BS802. MARKED. / [01] REMOVED CORROSION ON TRACK AT AFT CARGO BAY RBL 13 BS 802 IN AREA OF L=.25' X W=1' X D=.008 REMAINING THICKNESS .069' FROM ORIGINAL THICKNESS .070' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; SRM 51-10-02; DWG 147A7501 ID27 REV-<BR><BR>TOOL USED <BR>ATS 1672 SN65092939 CAL DUE 03/2022;[14] VERIFIED LOCATING AND DRILLIONG OF REPLACEMENT SEAT TRACK KIT PARTS. OK TO INSTALL GIVEN.<BR><BR>NOTE: SEAT TRACK REPAIR SPLICE REPAIR PARTS STILL REQUIRED TO BE FABRICATED;[15] FABRICATE SPLICE IS NOT REQUIRED; RECEIVED NEW SPLICE PART # 146A7506-20 ; LOCATED AND DRILL NEW SPLICE TRACK BETWEEN BS 747 TO BS 767 ; RBL 13; IAW SRM 53-00-53-2R-3; OK TO INSTALL;[16] VERIFIED CORRECTIVE ACTION 15. <BR>OK TO INSTALL;[17] INSTALLED NEW TRACK SPLICE BETWEEN BS 747 TO BS 767 ; RBL 13; IAW SRM 53-00-53-2R-3;[18] INSTALLED AFT CARGO TRACK BETWEEN BS 727+4 TO BS 867 ; RBL 13; WL 156; IAW SRM 51-40-02-0G-0 AND DWG 146A7500; ID: 38; REV:C;[19] VERIFIED CORRECTIVE ACTION 18;[20] VERIFIED CORRECTIVE ACTION 17;[21] INSTALLED TRACK AT AFT CARGO BAY BS 867 TO BS 887 RBL 13 IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV.-C;[22] UPDATED PART REQUIREMENTS.;[23] VERIFIED CORRECTIVE ACTIONS #21 AND #22

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 60,283 hrs · 37,501 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727A - BS767 RBL21. / [01] REMOVED CORROSION AFT CARGO BAY ON FLOOR SIDEWALL SUPPORT FROM BS 727A TO 767 ; RBL 21 ; WL 156 ; WORK AREA L 1.0' X W 1.0' X D 0.025' ; ORIGINAL MATERIAL THICKNESS 0.040'; MATERIAL REMAINING 0.015' ; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; STEP 4A; USING DIAL DEPTH GAUGE ID:ATS400;S/N: UNKNOWN; DUE 08/2022;[03] FABRICATED NEW FLOOR TO SIDEWALL SUPPORT AT ACB BS 727-767 R/H OUT OF BAC1496-377 MATERIAL LOT#1477731-1 PER DWG#146A7502 AND SRM 51-40-05. APPLIED CHEMICAL CONVERSION COATING PER AMM 51-21-41-370-802. REQUEST OK TO APPLY BMS 10-11 PRIMER.;[04] FABRICATED REPLACMENT FLOOR TO SIDEWALL SUPPORT AT ACB BS 727-767 R/H OUT OF BAC1496-377 7075-T6 MATERIAL LOT#1477731-1 PER DWG#146A7502 AND SRM 51-40-05. APPLIED CHEMICAL CONVERSION COATING PER AMM 51-21-41-370-802. REQUEST OK TO APPLY BMS 10-11 PRIMER.;[09] FABRICATED NEW FLOOR TO SIDEWALL SUPPORT AT ACB BS 727-767 R/H OUT OF BAC1496-377 MATERIAL LOT#1477731-1 APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW AMM 51-21-41-370-802. SOPM 20-41-02 SRM 51-40-02-0G-0; DWG#146A7502 REV A AND SRM 51-40-05.;[10] VERIFIED CORRECTIVE ACTION 9

Part: SUPPORT — CRACKED (L/H WING) · airframe 60,283 hrs · 37,501 cycles

BULB SEAL RETAINER SUPPORT IS CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON. PN:115A2982-9. MARKED / [01] REMOVED AND REPLACED BULB SEAL RETAINER SUPPORT AT L/W FIXED T/E PANEL JUST AFT OF THE PYLON IAW SRM 51-40-02-0G-0; PARA. 4.;[02] INSPECTION COMPLETE

Part: PLATE — CRACKED (L/H WING) · airframe 60,283 hrs · 37,501 cycles

LEFT WING T/E WIGGLE PLATE AT ORSS 261 IS CRACKED. ; / [01] REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE AT ORSS 261 IAW SRM 51-40- 02-0G-0; PARA. 4.; [02] VERIFIED JOB COMPLETE; [03] VERIFIED CORRECTIVE ACTION 1.

Part: PLATE — CRACKED (L/H WING) · airframe 60,283 hrs · 37,501 cycles

LEFT WING T/E WIGGLE PLATE AT ORSS 261 IS CRACKED. / [01] REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE AT ORSS 261 IAW SRM 51-40- 02-0G-0; PARA. 4.;[02] VERIFIED JOB COMPLETE;[03] VERIFIED CORRECTIVE ACTION 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,283 hrs · 37,501 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-25R WL156. MARKED / [01] PARTIAL ENTRY STEPS 1 TO 3;[02] VERIFIED APPLICABILITY IAW ALLOWABLE DAMAGE SRM 53-00-03-1A-1.CRACK LENGTH .500 AREA FOUND OUT OF LIMITS IAW SRM 53-00-03-1A-1 FIG. 103;[03] VERIFIED CORRECTIVE ACTION 1 AND 2.;[04] CUT OUT DAMAGE PART OF STRINGER IAW SRM 53-00-03-2R-1;[05] VERIFIED CORRECTIVE ACTION STEP 4.;[06] HFEC INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP USED: NORTEC 600 ID: ATS1465;[07] RECEIVED NEW STRINGER SECTION (1 EA ) P/N: HFAB53-STR-011 ; LOT: 1480886-1; P.O/N:854867/1<BR>FROM 7075T6 0.036' ; J CHANNEL SECTION (2 EA ) P/N:HFAB53-JC-011; LOT: 1480887-1 ;P.O/N:854865/1 FROM 7075T6 0.040' AND U CHANNEL SECTION ( 1 EA ) P/N: HFAB53-UC-011 ; LOT: 1480884-1 ; P.O/N: 854866/1 FROM 7075T6 0.040'<BR><BR>FABRICATED AND LOCATED AND DRILLED NEW STRINGER SECTION ; J CHANNEL SECTION AND U CHANNEL SECTION AT FCB STR 25 R/H BS 500D+4' TO 536 ; WL 156 IAW SRM 53-00-03-2R-1 PAR 4 STEPS D - H. AND EA 21-153-03642.;

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,283 hrs · 37,501 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-26R WL153. MARKED / [01] REMOVED PANEL 191CR TO FOM IAW AMM 53-51-21-000-803.;[02] VERIFIED APPLICABILITY IAW SRM 53-00-03-1A-1;CRAK .500 LENGHT;AREA FOUND OUT OF LIMITS IAW SRM 53-00-03-1A-1 FIG.103;[03] VERIFIED APPLICABILITY FOR STR 26 R/H IAW SRM 53-00-03-2R-1 PAR. 4 FIG 205;[04] CUT AND REMOVED DAMAGED STRINGER SECTION BETWEEN BS 500D+11' TO 536 STR 26 R/H IAW SRM 53-00-03-2R-1 PAR 4 STEP B AND 51-40-02;[05] PARTIAL ENTRY STEPS 1 TO 3;[06] VERIFIED CORRECTIVE ACTION ITEM 1 - 5.;[07] HFEC INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP USED: NORTEC 600 ID: ATS1465;[08] UPDATED STEP 4;[09] RECEIVED NEW STRINGER SECTION P/N: HFAB53-STS-011 ; PO/N: 854521/1 FROM 7075T6 0.045' AND HAT SECTION P/N:HFAB53-HS-011 ; LOT : 1480602-1; PO/N: 854526/1 ; FROM 7075T6 0.050' <BR><BR>FABRICATED AND LOCATED AND DRILLED NEW STRINGER SECTION AND HAT SECTION AT FCB STR 26R/H BS 500D+5' TO 536; WL 153 . IAW SRM 53-00-03-2R-1 PAR 4 STEPS D -H.;

Part: GUSSET — CRACKED (FWD CARGO) · airframe 60,283 hrs · 37,501 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / [01] REMOVED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET AT BS 500D; STR 19R; WL 193 IAW SRM 51-40-02-0G-0;[02] NO ALLOWABLE DAMAGE ON SRM; PART WILL TO BE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[03] LOCATED AND DRILLED NEW GUSSET AT BS 500D; STR 19R; WL 193 IAW SRM 51-40-05-0G-0 AND DWG 143A7902; ID: 21;REV:E; OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTIONS 1-3.;[05] INSTALLED NEW GUSSET AT BS 500D; STR 19R; WL 193 IAW SRM 51-40-02-0G-0 AND DWG 143A7902; ID: 21;REV:E;[06] VERIFIED CORRECTIVE ACTION 5;[07] VERIFIED ALL WORK ACCOMPLISHED.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 60,283 hrs · 37,501 cycles

CRACKED FLOOR SUPPORT AT STA 540; RBL 1; WL 207. / [01] REMOVED AND REPLACED FLOOR SUPPORT ON STA 540 RBL 1 WL 207 IAW DWG 143A0060 AND SRM 51-40-02-0G-0.;[02] VERIFIED;[03] UPDATED MEASUREMENTS;[04] VERIFIED;[05] REMOVED FLOOR PANEL 231UF FOR ACCESS IAW AMM 53-21-00-000-801.<BR>OK INSTALL;[06] VERIFIED;[07] VERIFIED CORRECTIVE ACTION 1;[08] OK TO CLOSE 231UF;[09] INSTALLED FLOOR PANEL 231UF IAW AMM 53-21-00-400-801;[10] SCREW GUN 25INCH IN TORQUE <BR>ID: PER1914<BR>S/N: ASC24111<BR>DATE:12/2021<BR>DUE:09/2022;[11] VERIFIED;[12] UPDATED PARTS;[13] VERIFIED;[14] VERIFIED CORRECTIVE ACTION 9 AND 10

Part: GUSSET — CRACKED (FWD CARGO) · airframe 60,283 hrs · 37,501 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-21L WL177. MARKED / [01] REMOVED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET AT BS 500D; STR 21L; WL 177 IAW SRM 51-40-02-0G-0;[02] NO ALLOWABLE DAMAGE ON SRM; PART WILL TO BE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[03] LOCATED AND DRILLED NEW GUSSET AT BS 500D; STR 21L; WL 177 IAW SRM 51-40-05-0G-0 AND DWG 143A7902; ID: 21;REV:E; OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTIONS 1-3;[05] INSTALLED NEW GUSSET AT BS 500D; STR 21L; WL 177 IAW SRM 51-40-02-0G-0 AND DWG 143A7902; ID: 21;REV:E;[06] VERIFIED CORRECTIVE ACTION 5.;[07] VERIFIED ALL WORK ACCOMPLISHED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,283 hrs · 37,501 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-27R WL150. MARKED / [01] APPLICABILITY STATEMENT SRM 53-00-03-2R-1 REPAIR 1 IT'S APPLICABLE FOR THIS REPAIR;[02] DAMAGE EVALUATION; FOUNT TO BE OUT OF LIMITS DIMENSION CRACK L:.500 IASW SRM 53-00-03-1A-1 STEP A(1)(A) 1) FIGURE 103 DETAIL A;[03] VERIFIED CORRECTIVE ACTION STATEMENT 1 AND 2.;[04] VERIFIED APPLICABILITY FOR STR 27 R/H IAW SRM 53-00-03-2R-1 PAR. 4 FIG 205;[05] CUT AND REMOVED DAMAGED STRINGER SECTION BETWEEN BS 500D+11' TO 536 STR 27 R/H IAW SRM 53-00-03-2R-1 PAR 4 STEP B AND 51-40-02;[06] ENTRY PARTIAL STEP 1;[07] ENTRY PARTIAL STEPS 1 AND 2;[08] VERIFIED CORRECTIVE ACTION ITEMS 4 & 5.;[09] HFEC INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP USED: NORTEC 600 ID: ATS1465;[10] UPDATED MEASUREMENTS;[11] MEASUREMENTS;[12] UPDATED MEASUREMENTS;[13] RECEIVED NEW STRINGER SECTION P/N: HFAB53-STS-011 ; PO/N: 854509/1 FROM 7075T6 0.056' AND HAT SECTION P/N:HFAB53-HS-011 ; LOT : 1480626-1; PO/N: 854510/1 ; FROM 7075T6 0.063' <BR><BR>FABRICATED AND LOCATED AND DRILLED NEW STRINGER SECTION AND HAT SECTION AT FCB STR 27R/H BS 500D+4' TO 536; WL 150 . IAW SRM 53-00-03-2R-1 PAR 4 STEPS D -H

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,283 hrs · 37,501 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-26L WL153. MARKED / [01] UP DATE PARTIAL STEP #1;[02] APPLIED PROTECTION OF THE EWIS AT WORK AREA IAW AMM20-60-07-913-801;[03] VERIFIED APPLICABILITY IAW SRM 53-00-03-1A-1;CRAK .500 LENGHT;AREA FOUND OUT OF LIMITS IAW SRM 53-00-03-1A-1 FIG.103;[04] REMOVED SHEAR TIE AT BS 520 BETW STR 26L AND 27L IAW SRM 51-40-02-0G-0 TO FOM;[05] VERIFIED CORRECTIVE ACTION 2-4;[06] VERIFIED APPLICABILITY FOR STR 26 L/H IAW SRM 53-00-03-2R-1 PAR. 4 FIG 205;[07] CUT AND REMOVED DAMAGED STRINGER SECTION BETWEEN BS 500D+11' TO 536 STR 26 L/H IAW SRM 53-00-03-2R-1 PAR 4 STEP B AND 51-40-02;[08] VERIFIED CORRECTIVE ACTION ITEMS 6 & 7.;[09] HFEC INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP USED: NORTEC 600 ID: ATS1465;[10] RECEIVED NEW STRINGER SECTION P/N: HFAB53-STS-011 ; P.O/N:854513/1 FROM 7075T6 0.045' AND HAT SECTION P/N: HFAB53-HS-011; LOT: 1480610-1 ;P.O/N: 854511/1 FROM 7075T6 0.050'<BR><BR>FABRICATED AND LOCATED AND DRILLED NEW STRINGER SECTION AND HAT SECTION AT FCB STR 26 L/H BS 500D+5 TO 536 ; WL 153 IAW SRM 53-00-03-2R-1 PAR 4 STEPS D - H.<BR><BR>APPLIED CHEMICAL CONVERSION COATING ON REPAIR PARTS. IAW SRM 53-00-03-2R-1 PAR 4 STEP I. REQUEST OK TO PRIMER.;

Part: GUSSET — CRACKED (FWD CARGO) · airframe 60,283 hrs · 37,501 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / [01] REMOVED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET AT BS 500D; STR 219L; WL 177 IAW SRM 51-40-02-0G-0;[02] NO ALLOWABLE DAMAGE ON SRM; PART WILL TO BE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[03] LOCATED AND DRILLED NEW GUSSET AT BS 500D; STR 19L; WL 193 IAW SRM 51-40-05-0G-0 AND DWG 143A7902; ID: 21;REV:E; OK TO INSTALL;[04] VERIFIED CORRECTIVE ACTION 1-3.;[05] INSTALLED NEW GUSSET AT BS 500D; STR 19L; WL 193 IAW SRM 51-40-02-0G-0 AND DWG 143A7902; ID: 21;REV:E;[06] VERIFIED CORRECTIVE ACTION 5.;[07] VERIFIED ALL WORK ACCOMPLISHED.

Part: STRAP — CORRODED (L/H WING) · airframe 60,283 hrs · 37,501 cycles

LEFT WING FWD BOOST PUMB HOUSING CORRODED AT UPPPER BONDING STRAP / [01] OPENED AND COLLARED THE NO. 1 FWD BOOST PUMP CIRCUIT BREAKER PER AMM 28-22-41-000-801 STEP 2H(4(B)) AND GAINED ACCESS TO CORROSION PER AMM 28-22-41-000-801 STEPS 4H(5; 8(UPPER STRAP ONLY);[26] REPAIRED LEFT WING CORROSION AT LEFT WING FWD BOOST PUMP HOUSING UPPER BONDING STRAP IAW SWA EA NO. 22-157-00304 REV A;

Part: STRAP — CORRODED (R/H WING) · airframe 60,283 hrs · 37,501 cycles

RIGHT WING FWD BOOST PUMP HOUSING CORRODED AT UPPER BONDING STRAP / [01] REMOVED UPPER SUPPORT ANGLE AT R/H BOOST PUMP FOR ACCESS TO FRONT SPAR WEB PER SRM57-20-10-1A-3;[24] REPAIRED CORROSION ON RIGHT WING FWD BOOST PUMP HOUSING AT UPPER BONDING STRAP IAW SWA EA NO. 22-157-00285 REV A;[25] VERIFIED CORRECTIVE ACTIONS STEP 24.;[26] UPDATED MEASUREMENT TABLE;[27] VERIFIED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,207 hrs · 37,452 cycles

EMERGENCY EXIT LIGHTS AT L1 EXTERIOR AND R1 INTERIOR ARE INOP. / [01] REMOVED AND REPLACED BATTERY PACK AT FWD LEFT LOCATION. REF AMM 33-51-06. OP CHK GOOD.

Part: SKIN — CRACKED (BS 360) · airframe 57,000 hrs · 35,569 cycles

FOUND CHEM MILL STEP CRACKED ACROSS STEP .75' LONG AT ST-10L AT STA 360 DETECTED WITH PART 6, 53-30-25. VERIFIED WITH PART 6, 53-30-09 AND PART 6, 51-00-00 PRO 23 INTERNALLY. COMPLIED WITH EA 20-153-02203 REFER TO N/R D352421 FOR LT TLD INFORMATION.

Part: SKIN — CRACKED (BS 385) · airframe 57,000 hrs · 35,569 cycles

.75' CRACK AT CHEM MILL STOP AT S-10L AT STA 385 DEFECT WITH PART 6, 53-30-25 VERIFIED WITH PART 6, 53-30-07. COMPLIED WITH EA 20-153-02203 SEE NRC NR D352428.

Part: SKIN — CRACKED (BS 385) · airframe 56,998 hrs · 35,568 cycles

.75' CRACK AT CHEM MILL STOP AT S-101 AT STA 385 DETECTED WITH PART 6; 53-30-25; VERIFIED WITH PART 6; 53-30-07 / TRANSFERED TO NR B352421

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 56,151 hrs · 35,036 cycles

FWD SERVICE DOOR SLIDE PRESSURE LOW REPLACED FWD SERVICE DOOR SLIDE IAW MT 725-61-06 RAR #51954 E41382 POS:SF P/N OFF/ON:5A3307-7 S/N OFF:BNG11726 S/N ON:BNG11050

Part: BATTERY PACK — INOPERATIVE (SLIDE LIGHT) · airframe 55,673 hrs · 34,731 cycles

RH SERVICE DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP. / BATTERY PACK M1674 REPLACED AND OPERATIONAL CHECK PERFORMED ON DEFECT NO U110075

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,673 hrs · 34,731 cycles

EMERGENCY EXIT LIGHTS IN FORWARD ENTRY DOORWAY INOP. REMOVED AND REPLACED BATTERY PACK M1674 PER MM 33-51-06-960-805 OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD PER MM 33-51-00-720-801.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 55,673 hrs · 34,731 cycles

AFT ENTRY DOOR SLIDE LIGHT IS INOP. REPLACED LAMP FOR AFT ENTRY DOOR SLIDE LIGHT AND PERFORMED GOOD OPERATIONAL TEST IAW AMM 33-51-04-960-801.

Part: WIRE — PULLED (EMERGENCY LIGHTS) · airframe 55,673 hrs · 34,731 cycles

W4142-0407-20 PULLED OUT OF GD3998 AT STA 947.5 STR 5-6L. TERMINATED W4142-0407-20 INTO GD3998 IAW WDM 33-51-11, SWPM 20-90-15. PERFORMED GOOD TEST OF EMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1672 PER AMM 33-51-00-710-801, WDM 33-51-11 AND SSM 33-51-14.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 55,673 hrs · 34,731 cycles

FORWARD ENTRY DOOR MOPSILL CRACKED COMMON BETWEEN BS. 278 TO BS. 303, FRAME LBL 60. / R&R MOPSILL PER DWG & SRM.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 55,673 hrs · 34,731 cycles

PANEL 193CL HAS DELAMINATED AREA ON EXTERNAL SURFACE / PANEL 193CL WITH A DELAMINATED AREA ON EXTERNAL SURFACE WAS REPAIRED IAW SRM 51-70-05-2R-2

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,673 hrs · 34,731 cycles

GIRT BAR FITTING SUPPORT CORRODED AT BS. 312, LBL 53 COMMON TO L/H FORWARD ENTRY MOPSILL. / R&R GIRT BAR FITTING SUPPORT IAW SRM, SOPM, & DWG.

Part: NONE — CORRODED (FSD THRESHOLD) · airframe 55,673 hrs · 34,731 cycles

***CORROSION*** ON FWD SERVICE DOOR MOPSILL R/H; STA 311-344 UPPER SURFACE; S-17R; WL 208. (MARKED) / REPAIRED CORROSION ON FWD SERVICE DOOR MOPSILL BS 311-344 STR 17R WL 208 AS PER EA #1-753-36416 REV IR AND ER #19-06425 REV IR.

Part: NONE — CRACKED (CABIN) · airframe 55,673 hrs · 34,731 cycles

CRACKED BREAK PANEL STA 540; LBL 2; WL 208. (MARKED) / REMOVED FLOOR PANEL 231UF TO FOM I.A.W. AMM 53-21-00 REMOVED CRACKED BREAK PANEL AT BS 540; LBL 2; WL 208; I.A.W. SRM 51-40-02 LOCATED AND DRILLED NEW BREAK PANEL I.A.W. SRM 51-40-05 IPC 53-31-00-05 IPC 53-21-00-09A INSTALLED BREAK PANEL I.A.W. SRM 51-40-02 IPC 53-31-00-05 REINSTALLED FLOOR PANEL 231UF I.A.W. AMM 53-21-00-400-801

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,673 hrs · 34,731 cycles

INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, LBL 44. / R&R INTERCOSTAL PER SRM AND DWG.

Part: HOOK — CORRODED (CABIN) · airframe 55,673 hrs · 34,731 cycles

R/H EMERGENCY EXIT HATCH ESCAPE HOOK HAD SURFACE CORROSION. / R&R HOOK PER AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 55,673 hrs · 34,731 cycles

R/H STABILIZER RIB AT STA. 92.7 LOWER FORWARD INBOARD FLANGE CRACKED. / REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 55,673 hrs · 34,731 cycles

L/H HORIZONTAL STABILIZER RIB AT STA. 129.50, FORWARD LOWER EDGE CRACKED. REPAIRED RIB IAW ER AND EA.

Part: STRAP — CORRODED (CABIN) · airframe 55,673 hrs · 34,731 cycles

R/H EMERGENCY EXIT HATCH ESCAPE STRAP ANCHOR HAD SURFACE CORROSION. / R&R STRAP ANCHOR PER AMM.

Part: HOOK — CORRODED (CABIN) · airframe 55,673 hrs · 34,731 cycles

L/H EMERGENCY EXIT HATCH ESCAPE STRAP ANCHOR & HOOK SURFACE CORRODED. / R&R ANCHOR AND HOOK ASSEMBLY PER AMM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 55,673 hrs · 34,731 cycles

PASSENGER CABIN SEAT TRACK CROWN CORRODED BETWEEN BS. 727B TO BS. 887, LBL 25. / R&R SEAT TRACK CROWN IAW SRM & DWG.

Part: FITTING — CRACKED (LT HORIZ STAB) · airframe 55,673 hrs · 34,731 cycles

L/H HORIZONTAL STABILIZER RIB AT STA. 129.50 FORWARD RIB TO WEB FITTING CRACKED AT FORWARD LOWER CORNER. / R&R FITTING IAW SRM AND DWG.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 55,673 hrs · 34,731 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS. 727 TO BS. 767, RBL 23. / REPAIRED SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,673 hrs · 34,731 cycles

FORWARD CARGO BAY SHIELD AFT THE DOOR HAD AREAS CORRODED BETWEEN BS. 492 TO BS. 500A, RBL 23. / R&R SHIELD IAW SRM AND DWG.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 55,673 hrs · 34,731 cycles

CABIN FLOOR PANEL 242XF IS BROKEN. / DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 242XF; REPLACED WITH NEW PANEL IAW AIPC 53-21-00-26 SHEET 001; ITEM 220. & SRM 51-10-02-0G-0 PARA 9. 57885U 12-18-19

Part: SPLICE — CORRODED (CARGO BAY) · airframe 55,673 hrs · 34,731 cycles

AFT CARGO BAY FLOOR PANEL SPLICE CORRODED AT BS. 887, BETWEEN BL 0 TO RBL 10. / R&R PANEL SPLICE IAW SRM.

Part: SUPPORT — CORRODED (BS 727D-787) · airframe 55,673 hrs · 34,731 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS. 727D TO BS. 787, LBL 23. R&R THE SUPPORT IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,673 hrs · 34,731 cycles

FLOOR BEAM CORRODED AT BS. 986, BETWEEN RBL 28 TO RBL 43. / REPAIRED FLOOR BEAM IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,673 hrs · 34,731 cycles

AFT CARGO BAY SHIELD FORWARD OF CARGO DOOR CORRODED COMMON TO NUT PLATES BETWEEN BS. 767 TO BS. 787, RBL 23. / R&R SHIELD IAW SRM & DWG.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 55,673 hrs · 34,731 cycles

LT HORIZONTAL STABILIZER NR 5 INSPAR RIB ASSEMBLY STA 129.50, NR 3 STIFFENER CRACKED AT LOWER ENDS. REPAIRED NR 3 VERTICAL STIFFENERS IAW SRM, DWG, AND AMM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 55,673 hrs · 34,731 cycles

L/H HORIZONTAL STABILIZER #5 INSPAR RIB ASSEMBLY STA. 129.50, #4 STIFFENER CRACKED AT LOWER ENDS. / REPAIRED #4 VERTICAL STIFFENERS IAW SRM, DWG, AND AMM.

Part: RETAINER — CRACKED (LEFT WING) · airframe 55,673 hrs · 34,731 cycles

LT WING UPPER T/E PANEL HORIZ. SEAL RETAINER IS CRACKED; JUST AFT OF THE #1 PYLON. / REMOVED AND REPLACED L/W UPPER T/E PANEL HORIZ SEAL RETAINER JUST AFT OF THE #1 PYLON IAW SRM 51-40-02-0G-0 PARA 4; AIPC 57-50-00-25; AND SOPM 20-50-01

Part: RETAINER — CRACKED (RIGHT WING) · airframe 55,673 hrs · 34,731 cycles

RT WING UPPER AFT T/E PANEL; JUST AFT OF #2 PYLON VERT SEAL RETAINER IS CRACKED. / REMOVED AND REPLACED R/W UPPER AFT T/E PANEL JUST AFT OF #2 PYLON SEAL RETAINER (FITTING) IAW SRM 51-40-02-0G-0 PARA 4; SOPM 20-50-01; AND AIPC 57-50-00-25.

Part: ANGLE — CRACKED (L/H WING) · airframe 55,673 hrs · 34,731 cycles

LT WING O/B ATTACH ANGLE IS CRACKED FOR THE WEB ON UPPER T/E PANEL; JUST AFT OF #1 PYLON. / REMOVED AND REPLACED L/W O/B ATTACH ANGLE FOR THE WEB ON UPPER T/E PANEL JUST AFT OF #1 PYLON IAW SRM 51-40-02-0G-0; PARA 4.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 55,673 hrs · 34,731 cycles

LT HORIZONTAL STABILIZER NR 5 INSPAR RIB ASSEMBLY STA 129.50, #2 STIFFENER CRACKED AT LOWER ENDS. REPAIRED NR 2 VERTICAL STIFFENERS IAW SRM, DWG, AND AMM.

Part: RIB — CRACKED (LEFT WING) · airframe 55,673 hrs · 34,731 cycles

LT WING DEFLECTION RIB UPPER LUG IS CRACKED FOR UPPER T/E PANEL ATTACH POINT. / REPAIRED LEFT WING DEFLECTION CONTROL RIB UPPER LUG ATTACHMENT TO UPPER T/E PANEL IAW SRM 57-51-02-2R-3; SRM 51-20-06-0G-0; SOPM 20-10-03 PARA. 7A; SRM 51-40-02-0G-0. 59796C 02JAN20

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 55,673 hrs · 34,731 cycles

RT HORIZONTAL STABILIZER NR 1 INSPAR RIB ASSEMBLY STA 92.70 NR 2 STIFFENER CRACKED. REPAIRED NR 2 STIFFENER IAW SRM AND DWG.

Part: SEAL — CRACKED (R/H VERT. STAB.) · airframe 55,673 hrs · 34,731 cycles

R/H STAB FRONT SPAR UPPER SLIDE SEAL CRACKED / REMOVED R/H STAB FRONT SPAR UPPER SLIDE SEAL IAW AMM 53-31-31-000-802 AND REPLACED IAW AMM 53-31-31-400-802. 84036U; 13JAN20.

Part: SEAL — CRACKED (L/H VERT. STAB.) · airframe 55,673 hrs · 34,731 cycles

L/H STAB FRONT SPAR UPPER SLIDE SEAL CRACKED / REMOVED L/H STAB FRONT SPAR UPPER SLIDE SEAL IAW AMM 53-31-31-000-802 AND REPLACED IAW AMM 53-31-31-400-802. 84036U; 13JAN20.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 55,673 hrs · 34,731 cycles

LOWER VAPOR BARRIER CRACKED AT BS. 663, BETWEEN RBL 15 TO RBL 25. REPAIRED VAPOR BARRIER IAW SRM.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 55,673 hrs · 34,731 cycles

L/H LOWER VAPOR BARRIER CRACKED AT BS. 663, BETWEEN LBL 45 TO LBL 55. / R&R VAPOR BARRIER IAW SRM AND DWG.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 55,673 hrs · 34,731 cycles

FORWARD SERVICE DOOR EMERGENCY LIGHT LENS BROKEN. R&R LENS IAW SOPM.

Part: RETAINER — LOOSE (L2 DOOR GIRT BAR) · airframe 55,673 hrs · 34,731 cycles

AFT ENTRY DOOR SLIDE FORWARD GIRT BAR RETAINER CLIP HAS LOOSE FASTENERS. R&R FASTENERS ON AFT ENTRY DOOR SLIDE FORWARD GIRT BAR RETAINER CLIP PER SRM 51-40-02-0G-0.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,673 hrs · 34,731 cycles

L/H WING #1 SLAT NOSE SKIN CRACKED AT ACTUATOR RIB ATTACH POINT. / REPAIRED #1 SLAT SKIN IAW SRM.

Part: PANEL — ELONGATED (LOWER EXT FUSELA) · airframe 55,456 hrs · 34,599 cycles

ALL HOLES IN LOWER FUSELAGE PANEL 193B ENLARGED. / REMOVED AND REPLACED PANEL 193B PER SRM 51-10-01; SRM 51-40-02 AND INSTALLED NEW PANEL PER AMM 53-51-21

Part: VAPOR BARRIER — CRACKED (WHEEL WELL LH) · airframe 55,285 hrs · 34,487 cycles

MLG W/W STA 663 VAPOR BARRIER HAS 10' CRACK BETWEEN LBL 46 AND LBL 54 / PERFORMED INTERIM REPAIR PER SRM 57-10-10-2R-2 REPAIR 2 PAR 1C; 2C & PAR 6. THIS IS A TIME LIMITED DEFERRAL TO DO A DETAILED VISUAL INSPECTION EVERY 3;000 FLIGHT CYCLES.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,493 hrs · 33,936 cycles

DOORWAY EMERGENCY LIGHT MODULE INOPERATIVE. R&R BATTERY PACK M1675 IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,493 hrs · 33,936 cycles

AFT OF R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,493 hrs · 33,936 cycles

R1 DOOR EMERGENCY LIGHT INOPERATIVE. / R&R BATTERY PACK M1675 IAW AMM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 54,493 hrs · 33,936 cycles

LOWER VAPOR BARRIER CRACKED AT BS. 663, LBL 46. / REPAIRED LOWER VAPOR BARRIER IAW SRM.

Part: VAPOR BARRIER — CRACKED (WHEEL WELL RH) · airframe 54,493 hrs · 33,936 cycles

R/H MAIN WHEEL WELL; LOWER VAPOR BARRIER CRACKED / APPLIED REPAIR PATCH CLOTH OVER CRACKED AREA IN R/H MAIN WHEEL WELL LOWER VAPOR BARRIER (#120) LOT# 5076276-1 IAW SRM 57-10-10-2R-2 STEPS 6(A-D) APPLIED BMS 5-95 (B 1/2 SEALANT) AT 12:45PM ON 27JUL19 56800U 27JUL19 AT RBL 16 WL 163 CRACK LENGTH OF L=5'

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,493 hrs · 33,936 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PACK PER AMM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 54,493 hrs · 33,936 cycles

RT UPPER FWD SLIDER SEAL CRACKED / R&R RT HORIZONTAL STAB. UPPER FWD SLIDER SEAL REF AMM 53-31-31.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,493 hrs · 33,936 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PACK PER AMM.

Part: PANEL — DELAMINATED (LH PYLON) · airframe 53,155 hrs · 33,078 cycles

#1 ENG STRUT AFT PYLON; I/B PANEL; 431ER; DELAMINATED; FWD; LOWER CORNER OF PANEL MEASURES 4.875' LONG; 2.25' WIDE; ZONE 1. / TRACKING 40333; CL 41339; DMA 0061216 REMOVED/REPLACED #1 ENG INBD PYLON PANEL #431 ER REF B737 AMM 54-43-01.

Part: LENS — MISSING (EXIT SIGN) · airframe 52,136 hrs · 32,413 cycles

L2 DOOR LOWER EMERGENCY EXIT/SALIDA SIGN COVER MISSING. R&R LENS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,550 hrs · 32,034 cycles

LT EMERGENCY LIGHT INOP AT M1673. R&R BATTERY IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 51,550 hrs · 32,034 cycles

LT EMERGENCY LIGHT INOP AT M2335. R&R BATTERY IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,457 hrs · 31,351 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. R&R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,457 hrs · 31,351 cycles

LT EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 6 TO ROW 24. CHARGED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (ROWS 17-23) · airframe 50,457 hrs · 31,351 cycles

LEFT EMERGENCY AISLE LIGHTS INOPERATIVE BETWEEN ROWS 17 TO 23. R & R THE LIGHT IAW AMM.

Part: CIRCUIT BREAKER — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 50,457 hrs · 31,351 cycles

AFT GALLEY CEILING EMERGENCY EXIT SIGN INOPERATIVE. RESET THE CIRCUIT BREAKER IAW AMM.

Part: CIRCUIT BREAKER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 50,457 hrs · 31,351 cycles

RIGHT OVERWING DOOR UPPER EMERGENCY EXIT LIGHT INOPERATIVE. RESET THE CIRCUIT BREAKER IAW AMM.

Part: CIRCUIT BREAKER — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 50,457 hrs · 31,351 cycles

RIGHT EMERGENCY AISLE LIGHTS INOPERATIVE BETWEEN ROWS 8 TO 19. RESET THE CIRCUIT BREAKER IAW AMM.

Part: CIRCUIT BREAKER — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 50,457 hrs · 31,351 cycles

RIGHT OVERWING DOOR EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE. RESET THE CIRCUIT BREAKER IAW AMM.

Part: CIRCUIT BREAKER — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 50,457 hrs · 31,351 cycles

RIGHT OVERWING DOOR LOWER EMERGENCY LIGHT INOPERATIVE. RESET THE CIRCUIT BREAKER IAW AMM.

Part: SPOILER — WARPED (SPOILER) · airframe 50,457 hrs · 31,351 cycles

#6 SPOILER IS WARPED / REMOVED AND INSTALLED SERVICEABLE #6 SPOILER. IAW AMM 27-62-12-000-801. AMM 27-62-12-400-801. FOUND #6 SPOILER WARPED BAD FROM STCOK. TRANSFERED TO DEFECT NO. N129069. (POS:#6; TAG NO.:360715; P/N OFF:113A4600-5; S/N OFF:025494; P/N ON:113A4600-1; S/N ON:001988)

Part: STRIP — CORRODED (BS 727E) · airframe 50,457 hrs · 31,351 cycles

CAP STRIP CORRODED AT BS 727E+12, LT SIDE. R & R THE CAP STRIP IAW SRM & DWG.

Part: RIVET — SHEARED (L1 DOOR) · airframe 50,457 hrs · 31,351 cycles

L1 DOOR ESCAPE SLIDE SHROUD AFT GIRT BAR HOOK SHEARED RIVET. R&R HOOK ASSEMBLY IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 50,457 hrs · 31,351 cycles

R1 DOOR SUB THRESHOLD WEB CRACKED AT BS 294, WL 207. R&R WEB IAW ER AND EA.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 50,457 hrs · 31,351 cycles

FORWARD CARGO SIDE SHIELD CORRODED BETWEEN BS 420 TO BS 440, RBL 22. R&R SHIELD IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 50,457 hrs · 31,351 cycles

FORWARD CARGO SIDE SHIELD CORRODED BETWEEN BS 493 TO BS 500A, RBL 22. R&R SHIELD IAW SRM AND DWG.

Part: RETAINER — CRACKED (RT WING) · airframe 50,457 hrs · 31,351 cycles

RT. WING; CRACK IN BULB SEAL RETAINER APPROX. 272 ON FIXED T/E SUPPORT. / REMOVED AND REPLACED BULB SEAL RETAINER BRACKET ON RH WING TE STRUCTURE AT APPROX 272 IAW SRM 51-40-02-00G-0 PAR 4 AND FIG 8

Part: STIFFENER — CRACKED (RT AC BAY) · airframe 50,457 hrs · 31,351 cycles

RIGHT AC BAY HORIZONTAL BRACE ON FORWARD SIDE OF 663 CRACKED ON INBOARD END. / LOCATED AND DRILLED NEW STIFFNER PART # 111A1301-6 PER SRM 51-40-05-0G-0 AND BOEING DWG # 111A1001 ID:0153 REV.B; TO BE INSTALLED ON CUSTOMER CARD # N128945 92385U 04/11/18

Part: SHIELD — CORRODED (FUSELAGE) · airframe 50,457 hrs · 31,351 cycles

AFT CARGO PIT RT FORWARD SHIELD CORRODED BETWEEN BS 767 TO BS 779, RBL 15. R&R SHIELD IAW DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 50,457 hrs · 31,351 cycles

AFT CARGO SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 21. R&R SHIELD IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 50,457 hrs · 31,351 cycles

AFT CARGO PIT RT Z CHANNEL CORRODED BETWEEN BS 867 TO BS 885. R&R ZEE CHANNEL IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 50,457 hrs · 31,351 cycles

AFT CARGO PIT RT Z CHANNEL CORRODED BETWEEN BS 727B TO BS 787. R&R Z CHANNEL IAW SRM AND DWG.

Part: RETAINER — CRACKED (LT WING) · airframe 50,457 hrs · 31,351 cycles

LT. WING; CRACK IN BULB SEAL RETAINER @APPROX. ORSS 272. / REMOVED AND REPLACED BULB SEAL RETAINER BRACKET ON LH WING TE STRUCTURE AT APPROX. ORSS 272 IAW SRM 51-40-02-0G-0 PAR 4 AND FIG 8

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 50,457 hrs · 31,351 cycles

AFT CARGO SUPPORT ZEE CORRODED BETWEEN BS 727+4 TO BS 747, LBL 21. R&R SUPPORT ZEE IAW SRM & DWG.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 50,457 hrs · 31,351 cycles

FWD ACCESS PANEL 193CR OUTER SURFACE DISBAND MARKED / REPAIRED DISBOND ON OUTER SURFACE OF FWD ACCESS PANEL 193CR PER SRM 53-40-70-2R-1 TABLE 201 AND SRM 51-70-05-2R-2

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 50,457 hrs · 31,351 cycles

CABIN FLOOR PANEL 241CF HAS DAMAGE ON FWD I/B EDGE (MARKED) / REPAIRED CABIN FLOOR PANEL 241CF I.A.W 737 SRM 53-00-50-2R-2 PARA 1; 3 TABLE 201.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 50,457 hrs · 31,351 cycles

RT WHEEL WELL LOWER VAPOR BARRIER WEB CRACKED AT BS 663.75, BETWEEN RBL 10 TO RBL 15. REPAIRED WEB IAW SRM.

Part: STUB FRAME — CRACKED (BS 294) · airframe 50,457 hrs · 31,351 cycles

R1 DOOR CRACKED STUB BEAM COMMON TO INTER STRUCTURE AFT FASTENER HOLE AT BS 294, WL 208. REPAIRED THE STUB BEAM FRAME IAW EA.

Part: FLOOR SUPPORT — CRACKED (BS 312) · airframe 50,457 hrs · 31,351 cycles

FLOOR SUPPORT CRACKED AT BS 312+5, RBL 31. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 291.5) · airframe 50,457 hrs · 31,351 cycles

FLOOR SUPPORT CRACKED AT BS 291.5+2, BL 0. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 50,457 hrs · 31,351 cycles

AFT CABIN FLOOR PANEL 241ABF HAS DAMAGE AT MIDDLE OF PANEL I/B TO O/B (MARKED) / REPAIRED AFT CABIN FLOOR PANEL 241ABF PANEL UPPER MIDDLE IAW SRM 53-00-50-2R-1

Part: GUSSET — CRACKED (BS 500D) · airframe 50,457 hrs · 31,351 cycles

FUSELAGE GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 50,457 hrs · 31,351 cycles

CABIN FLOOR PANEL 221BF HAS DAMAGE ON AFT O/B CORNER / REPAIRED CABIN FLOOR PANEL 221BF AFT O/B CORNERS IAW SRM 53-00-50-2R-6

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 50,457 hrs · 31,351 cycles

AFT CABIN FLOOR PANEL 241AEF IS DAMAGED ON AFT O/B EDGE / REPAIRED AFT CABIN FLOOR PANEL 241AEF I.A.W 737 SRM 53-00-50-2R-2 PARA 1; 3 TABLE 201

Part: GUSSET — CRACKED (FUSELAGE) · airframe 50,457 hrs · 31,351 cycles

FORWARD CARGO GUSSET CRACKED BS 500D, STR 19L. R&R GUSSET IAW SRM & DWG.

Part: PANEL — DELAMINATED (LEFT WING) · airframe 50,457 hrs · 31,351 cycles

L/H LOWER FIXED L/E WING PANEL 521DB HAS DELAMINATION ON FWD CORNERS (MARKED) / L/H LOWER FIXED L/E WING PANEL 521DB DELAMINATION ON FWD CORNERS REPAIRED IAW SRM 57-41-01-2R-1; TABLE 202 AND IAW SRM 51-70-05-2R-10 57507U 4-19-18

Part: PANEL — DELAMINATED (LEFT WING) · airframe 50,457 hrs · 31,351 cycles

L/H LOWER FIXED L/E WING PANEL 521KB HAS DELAMINATION ON FWD CORNER (MARKED) / L/H LOWER FIXED L/E WING PANEL 521KB DELAMNINATION ON FWD CORNER REPAIRED IAW SRM 57-41-01-2R-1 TABLE 202 AND IAW SRM 51-70-05-2R-10.

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 50,457 hrs · 31,351 cycles

R/H LOWER FIXED L/E WING PANEL 621DB HAS FWD CORNERS DISBONDED (MARKED) / R/H LOWER FIXED L/E WING PANEL FWD CORNERS DISBONDED MARKED REPAIRED IAW SRM 57-41-01-2R-1 TABLE 202 AND IAW SRM 51-70-05-2R-10 57517U 4-19-18

Part: BEAM — BROKEN (RIGHT WING) · airframe 50,457 hrs · 31,351 cycles

AFT. N/P ATTACH BRACKET; INBD. END ( APPROX. 3'' ) BROKEN OFF FOR PANEL 661AB. R/H TRAILING EDGE. / REMOVED BRACKET/BEAM AT WS 378-326 PNL #661AB DUE TO DAMAGE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IAW SRM 51-10-02; #9 23959R 4/9/18 REPLACED AND INSTALLED NEW BEAM P/N 115A3758-10 IAW DWG 115A3712 REV B AND SRM 51-40-02-0G-0

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 50,064 hrs · 31,092 cycles

AFT CARGO SCUFFPLATE CRACKED / REMOVED AND REPLACED SCUFF PLATE PER AMM 53-11-02.

Part: BRACKET — CRACKED (LT WING) · airframe 50,064 hrs · 31,092 cycles

LT. WING-INBD FXD T/E UPPER PANEL-SUPPORT BOTM ASSY- FWD CLIP CRACKED. / INSTALLED FWD CLIP PER SRM 51-40-02.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 48,506 hrs · 30,100 cycles

LEFT AFT EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 48,506 hrs · 30,100 cycles

LEFT FORWARD EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R & R THE BATTERY IAW AMM.

Part: STRAP — LOOSE (R1 DOOR) · airframe 46,593 hrs · 28,925 cycles

R1 DOOR SAFETY STRAP LOOSE. SECURED THE STRAP IAW SIP.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 45,512 hrs · 28,269 cycles

LEFT FORWARD WHEEL WELL BULKHEAD CRACKED. REPAIRED THE BULKHEAD IAW EA.

Part: LENS — DIRTY (EXTERIOR LIGHT) · airframe 44,310 hrs · 27,566 cycles

LEFT EMER EXIT LIGHT FOR WING FLAPS LENS DIRTY. CLEANED LENS IAW AMM.

Part: LENS — DIRTY (EXTERIOR LIGHT) · airframe 44,310 hrs · 27,566 cycles

RIGHT EMER EXIT LIGHT FOR WING FLAPS LENS DIRTY. CLEANED LENS IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 44,310 hrs · 27,566 cycles

L2 DOOR EMER EVAC SLIDE LIGHT INOPERATIVE. R & R FUSE IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 44,310 hrs · 27,566 cycles

OVERWING EMER EXIT LIGHT INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 44,310 hrs · 27,566 cycles

AFT LT OVERHEAD BIN BULLNOSE EMER LIGHT INOPERATIVE. R & R FUSE IAW AMM.

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 44,310 hrs · 27,566 cycles

LEFT WING NR 4 SPOILER UPPER SURFACE DELAMINATED. REPAIRED NR 4 SPOILER IAW SRM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 44,310 hrs · 27,566 cycles

RIGHT WING UPPER TE SURFACE PANEL, AFT SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT, ABOVE NR 2 PYLON AFT TIP. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 44,310 hrs · 27,566 cycles

LEFT WING UPPER TE SUPPORT ANGLE, CRACKED ABOVE NR 1 PYLON AFT TIP, AT TRANSVERSE WEB ATTACH POINT. R & R ANGLE IAW SRM.

Part: GIRT BAR — CORRODED (R2 DOOR) · airframe 44,310 hrs · 27,566 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR CORRODED. R & R GIRT BAR IAW AMM.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 44,310 hrs · 27,566 cycles

R1 DOOR ESCAPE SLIDE GIRT BAR RETAINING CLIPS LOOSE. R & R CLIPS IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727 - 767, STRINGER 25L. R & R SUPPORT IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

STRINGER CLIP CRACKED AT BS 948, STRINGER 18R. R & R CLIP IAW SRM & DWG.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT TO FRAME BRACKET, CORRODED AT BS 767, STRINGER 25R. R & R BRACKET IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727 - 767, STRINGER 25R. R & R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

INTERCOSTAL CRACKED ON UPPER FLANGE AT BS 353, LBL 1. REPAIRED INTERCOSTAL IAW ER & EA.

Part: STRINGER CLIP — DAMAGED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

STRINGER CLIP DAMAGED AT BS 400, STRINGER 1. R & R CLIP IAW SRM & DWG.

Part: SUPPORT FITTING — CORRODED (GIRT BAR) · airframe 44,310 hrs · 27,566 cycles

GIRT BAR SUPPORT FITTING CORRODED AT BS 344, LBL 59. R & R FITTING IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

RIGHT FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 44,310 hrs · 27,566 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB IAW SRM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 44,310 hrs · 27,566 cycles

FLIGHT DECK RT NR 1 WINDOW FRAME, CRACKED AT UPPER OTBD AREA. REPAIRED FRAME IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

LEFT NR 3 WINDOW FRAME, E - F POST CRACKED IN 2ND LOWER FASTENER HOLE. REPAIRED POST IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

RIGHT NR 3 WINDOW FRAME, E - F POST CRACKED IN 2ND LOWER FASTENER HOLE. REPAIRED FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,310 hrs · 27,566 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.