N7742B

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 60,608 hrs · 33,260 cycles

AFT EMERGENCY CABIN LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE LIGHT IAW AMM 33-51-01-960-802-NG.

Part: SLIDE — DISLODGED (ZONE 800) · airframe 60,540 hrs · 33,212 cycles

UPON OPENING FWD SERVICE DOOR GIRT BAR FELL OUT PARTIALLY AND BECAME HUNG UP. SLIDE FELL OUT. INSTALLED FWD SERVICE DOOR SLIDE IAW MT 725-61-06-FS.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 59,636 hrs · 32,617 cycles

AFT ENTRY DOOR; EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. RELAMPED AFT ENTRY DOOR; EXTERIOR EMERGENCY SLIDE LIGHT REF AMM 33-51-04 - NO FIX. REQUIRES FURTHER TROUBLESHOOTING. CLEANED LAMP SOCKET AND REPLACED THE LAMP, AFT ENTRY EXTERIOR EMERGENCY SLIDE LIGHT PER AMM 33-51-04.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 59,636 hrs · 32,617 cycles

FWD ENTRY DOOR; EXTERIOR EMERGENCY SLIDE LIGHT INOPERATIVE. RELAMPED THE EXTERIOR EMERGENCY SLIDE LIGHT IAW AMM 33-51-04 - NO FIX. REQUIRES FURTHER TROUBLESHOOTING. REMOVED FWD ENTRY LIGHT ASSY FOR ACCESS IAW 33-29-00. REMOVED & REPLACED POWER PACK ASSEMBLY IAW AMM 33-51-06. LIGHT CHECK GOOD.

Part: TIRE — BLOWN (ZONE 700) · airframe 59,636 hrs · 32,617 cycles

SUSPECTED MLG TIRE BLOWN ON TAKEOFF. PERFORMED CONDITIONAL INSPECTION FOR TIRE BURST IAW AMM 05-51-54. CONFIRMED TIRE BLOWN, REF TTG8Q014SP1Z FOR FINDINGS OF CONDITIONAL INSPECTION AND WO 04719292. ALL WORK ACCOMPLISHED PER APPLICABLE AMMS. ACFT OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

ASSOCIATED EMERGENCY LIGHTS WITH M1673 BATTERY PACK ARE INOP<[01] REMOVED AND REPLACED AND PERFORMED GOOD TEST OF EMERGENCY BATTERY PACK M1673 IAW AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: FUSE — INOPERATIVE (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

RH OVERWING EXIT/ESCAPE HATCH LIGHT AND RH OVERWING SCAPE LIGHT ARE INOP L1365 OVERWING EXIT LOCATOR SIGN L751 OVERWING ESCAPE HATCH LIGHT AND L7 OVERWING SCAPE LIGHT ARE INOP.<[01] CONNECTED CONNECTORS D3668 AND D3666 AT RIGHT POSITION IAW WDM 33-51-21 AND REPLACED FUSE IN POWER SUPPLY M1669 IAW AMM 33-51-06-960-804 AND PERFORMED GOOD OPERATIONAL TEST OF RH OVERWING EXIT/ESCAPE HATCH LIGHT AND RH OVERWING SCAPE LIGHT IAW AMM 33-51-06-960-805 STEP 4.E(6).;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

ASSOCIATED EMERGENCY LIGHTS WITH M1674 BATTERY PACK ARE INOP<[01] REMOVED AND REPLACED AND PERFORMED GOOD TEST OF EMERGENCY BATTERY PACK M1674 IAW AMM 33-51-06-960-805;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

L733 AFT SCAPE SLIDE LIGHT INOP<[01] RELAMPED L733 AFT RH SLIDE LIGHT AND PERFORMED GOOD TEST PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

CRACK FOUND ON FSD STUB FRAME AT BS291.5 + 8.5; .7' ABOVE SEAL DEPRESSOR; .6' IN LENGTH MARKED LOCATION<[01] REMOVED AND REPLACED FSD UPPER STUB FRAME I.A.W SRM 51-40-02-0G-0 AND DWG 141A8370.;[02] VERIFIED CORRECTIVE ACTION #1

Part: WEB — CRACKED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

FED CUTOUT SURROUND STRUCTURE; UPPER CHORD WEB BS 312 BETWEEN S6L AND S7L HAS A CRACK (MARKED).<[01] AFTER NDI EVALUATION AT DISCREPANCY AREA; NO CRACK NOTED IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23.<BR>TOOL USED:<BR>ID ATS1465<BR>CAL. DUE 07/2025.;[02] UPPER CHORD WEB AT FED REINSPECTED AND CRACK CONFIRMED AT LOCATION STA-312 STR-5L TO 6L; REPAIR OR REPLACEMENT REQUIRED.;[03] REPAIRED DISCREPANCY AREA PER REF EA M-22-153-01244 ON CARD NBR TTG8Q00YCV3Z;[04] CORRECTIVE ACTION COMPLETED.

Part: SHIELD — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACB - CORROSION ON FWD SHIELD FLOOR STRUCTURE RBL 21.5 BS 767+3.5; BS 767+7; BS 767+11; BS 767+15.5; BS 767+19 WL 156 (MARKED)<[01] REMOVED AND REPLACED ACB FWD SHIELD IAW SRM 51-40-02 AND DWG#146A0081 ID: 0034; REV:-;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: STRAP — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACB - CORROSION ON STRAP LOWER MAIN SILL RBL 19 BS 787+3; BS 787+12; BS 807+1.5; BS 807+5; BS 807+9; BS 807+12.5; BS 827; BS 827+7; BS 827+7.25; BS 827+15 WL 156 (MARKED)<[01] REMOVED AND REPLACED STRAP LOWER MAIN SILL RBL 19 BS 775 TO BS 861 I.A.W SRM 51-40-02-0G-0 AND DWG 146A8120.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACB - CORROSION ON SIDEWALL FLOOR STRUCTURE RBL 21.5 BS 727+14.5; BS 727A+10; BS 727A+13; BS 727A+14.25; BS 727B+19; BS 727C+2; BSN 727C+6; BS 727C+14; BS 727C+17.5 WL 156 (MARKED)<[01] REMOVED AND REPLACED NEW SIDEWALL FLOOR STRUCTURE FROM BS727 TO BS767 RBL21.5 IAW SRM 51-40-02 AND DWG 146A7500 ID:0085 REV: A;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.

Part: STRAP — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACB - CORROSION ON STRAP LOWER MAIN SILL RBL 19 BS 787+3; BS 787+12; BS 807+1.5; BS 807+5; BS 807+9; BS 807+12.5; BS 827; BS 827+7; BS 827+7.25; BS 827+15 WL 156 (MARKED)<[01] OPEN FAULT HAS AN ERROR AND IS BEING CORRECTED BY RAISING A NEW FAULT<BR>TTG8Q00Y8P6H

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACB - CORROSION ON SIDEWALL FLOOR STRUCTURE RBL 21.5 BS 727D+3; BS 727D+5.5; BS 727D+10; BS 727D+13; BS 727E+1.5; BS 727E+6; BS 727E+14; BS 727E+18 WL 156 (MARKED)<[01] THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q00Y8PNX;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.;[03] VERIFIED ITEM 1 AND TASK CARD COMPLETED.

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACB - CORROSION ON RAIL FLOOR STRUCTURE BS 727D+16; BS 727E+7.5; BS 727E+9; BS 727E+12.5; BS 767+4.5; BS 787+5 LBL 8.1 WL 156 (MARKED).<[01] REMOVED AND REPLACED REPAIR PARTS ON RAIL FLOOR STRUCTURE BS767+4.5 LBL8.1 IAW SRM 53-00-53-2R-2 REPAIR 2;[02] INSTALLED REPAIR PARTS ON RAIL FLOOR STRUCTURE BS767+4.5 LBL8.1 IAW SRM 53-00-53-2R-2 REPAIR 2;[03] CLEANED AREA BETWEEN BS727D+16- BS787+5 LBL8.1 AND NO FOUND CORROSION DAMAGE. JUST PRIMER DAMAGE IAW SOPM 20-30-03.<BR>INSTALLED REPAIR PARTS ON RAIL FLOOR STRUCTURE BS767+4.5 LBL8.1 IAW SRM 53-00-53-2R-2 REPAIR 2;[04] VERIFIED CORRECTIVE ACTION 3.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACB - CORROSION ON SIDEWALL FLOOR STRUCTURE LBL 21.5 BS 747+2; 747+6; BS 747+10; BS 747+15; BS 767+3.5; BS 767+5; BS 767+9 WL 156 (MARKED)<[01] THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q00Y8LKQ;[02] ALL FLOOR TO SIDEWALL SUPPORT WILL BE REPLACED ON CARD TTG8Q00Y8LKQ.;[03] VERIFIED ITEM 2 AND TASK CARD COMPLETED.;[04] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.;[05] REMOVED AND REPLACED FROM BS727 TO BS847 LBL 21.5 ON CARD TTG8Q00Y8LKQ;[06] JOB COMPLETE.

Part: STRIP — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACB - CORROSION ON FWD CAP STRIP FLOOR BS 727+5 LBL 12; BS 727 RBL 16 WL 156 (MARKED).<[01] REPLACED NEW FWD CAP STRIP FLOOR BS 727+5 LBL 12; BS 727 RBL 16 WL 156 PER REF SRM 51-10-02 STEP 9C AND DWG NBR 453A2611;[02] VERIFIED PROCURE PART ON ITEM 1; CORRECTIVE ACTION COMPLETED.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACB - CORROSION ON SIDEWALL FLOOR STRUCTURE LBL 21.5 BS 727B+2; 727B+10; BS 727B+14; BS 727C+5; BS 727C+6; BS 727C+12 WL 156 (MARKED).<[01] VERIFIED ITEM 1 AND TASK CARD COMPLETED.;[02] REMOVED AND REPLACED ACB FLOOR TO SIDEWALL SUPPORT LBL 21.5 WL 156 IAW SRM 51-40-02 AND DWG 146A7500 ID:0085 REV: A.;[03] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACB - CORROSION ON SIDEWALL FLOOR STRUCTURE RBL 21.5 BS 747+2; BS 747+6; BS 747+10 WL 156 (MARKED)<[01] THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q00Y8PNX;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.;[03] VERIFIED ACTION ITEM 1 AND TASK CARD COMPLETED.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACB - CORROSION ON SIDEWALL FLOOR STRUCTURE LBL 21.5 BS 727D+6; 727D+9; BS 727D+15; BS 727E+6; BS 727E+9; BS 727E+13; BS 727E+17; BS 727E+19 WL 156 (MARKED)<[01] THIS DISCREPANCY WILL BE ACCOMPLISHED ON CARD TTG8Q00Y8LKQ;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.;[03] VERIFIED ITEM 1 AND TASK CARD COMPLETED.

Part: WEB — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACD CUTOUT LOWER MAIN SILL HAS MULTIPLE SPOTS OF CORROSION. (MARKED)<[01] REMOVED AND REPLACED ACB SUBTHRESHOLD WEB IAW 51-40-02-0G-0 AND DWG#146A8340;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: NUT PLATE — CRACKED (ZONE 500) · airframe 57,792 hrs · 31,530 cycles

LT WING TRAILING EDGE NUTPLATE BEAM CRACKED AT RSS 270 COMMON TO PANEL 561AB.<[01] REMOVED AND REPLACED LT WING TRAILING EDGE NUTPLATE BEAM COMMON TO PANEL 561AB IAW SRM 51-40-02 AND AIPC 57-50-00-17<BR> SCREW GUN ID PER2216 CAL DUE 11/2025;[02] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.

Part: ATTACH ANGLE — CRACKED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

CRACKED ATTACH ANGLE AT FWD CABIN BS294 RBL54 WL208. MARKED<[01] REMOVED AND REPLACED THE FWD. CABIN ATTACH ANGLE BS294 RBL54 WL208 IAW SRM 51-40-02 AND DWG # 141A8312 REV: A;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.;[03] VERIFIED ITEM 1 AND TASK CARD COMPLETED.

Part: SILL DRAIN — CORRODED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

CORR0SION ON MOP SILL STA. 308 LBL. 57 WL 208.1<[01] REPLACED MOP SILL ASSY IN FAULT TTG8Q00Y6CVD

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

FWD FLOOR PANEL 221GF FWD O/B TANG UPPER SKIN IS CRACKED.<[01] FWD FLOOR PANEL 221GF FWD O/B TANG UPPER SKIN WITH CRACK WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

FWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

FWD FLOOR PANEL 222CF UPPER SKIN HAS AREASOF PULLED STRANDS.<[01] 222CF FLOOR PANEL UPPER SURFACE DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: SUPPORT ANGLE — CORRODED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

CORROSION ON L1 I.B; THRESHOLD SUPPORT ANGLE AT STA 320 LBL57 WL 209.1<[01] REMOVED AND REPLACED ON L1 I.B SUPPORT ANGLE FROM BS312 TO BS348 LBL57 IAW SRM 51-40-02 AND DWG 141A8110 ID: 0011 REV: -;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.;[03] VERIFIED ACTION ITEM AND TASK CARD COMPLETED.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACB FWD CORNER SCUFF PLATE CRACKED<[01] APPLIED A CHEMICAL CONVERSION COATING AND PRIMER TO THE REWORKED SURFACES. IAW SRM 53-60-15-2R-1 STEP 1. B (6);[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

FWD FLOOR PANEL 231AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 231AF FLOOR PANEL UPPER SURFACE DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

CORROSION ON FLOOR SUPPORT AT FWD WET AREA BS282 LBL12 WL208.<[01] REMOVED AN REPLACED INTERCOSTAL BETWEEN BS277-BS294 LBL12 IAW B737-7 SRME 51-40-02; SRM 51-40-05 AND DWG141A5600 REV: N ID:0001 (NEW INTERCOSTAL P/N: 141A5650U3 LOT: 1591394-1)

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

ACB AFT CORNER SCUFF PLATE CRACKED<[01] APPLIED A CHEMICAL CONVERSION COATING AND PRIMER TO THE REWORKED SURFACES. IAW SRM 53-60-15-2R-1 STEP 1. B (6);[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

CRACKED INTERCOSTAL AT FWD WET AREA BS323 RBL31 WL208.<[01] REMOVED AND REPLACED THE FWD. WET AREA INTERCOSTAL BS323 RBL31 WL208; IAW SRM 51-40-02 AND DWG# 141A5410 REV: A;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.

Part: SILL DRAIN — CRACKED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

CRACKED L1 DOOR MOP SILL BS302 LBL54 WL208. MARKED<[01] REMOVED AND REPLACED L1 DOOR MOPSILL FROM BS270 TO BS360 LBL54 IAW SRM 51-40-02 AND DWG 141A8110 ID:0011 REV:-;[02] TASK CARD COMPLETED.

Part: ANGLE — CRACKED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

CRACKED INTERCOSTAL UPPER ANGLE AT AFT CABIN BS927+16 BL0 WL208. MARKED<[01] REMOVED AND REPLACED UPPER ATTACH ANGLE FROM BS927-BS947 BL0; PN#147A5430-1 IAW SRM 51-40-05 AND IAW DWG#147A5400 REV: -; 147A5400 REV: A.;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.

Part: STRAP — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

CORROSION ON TENSION STRAP AT AFT CABIN BS1018 LBL3 WL208. MARKED<[01] REMOVED AND REPLACED TENSION STRAP FROM BS1006-B1027 LBL3 IAW SRM 51-40-02 AND DWG NBR 147A5600;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.;[03] REJECTED AMT COMPLETION DUE TO MEASUREMENT FIELD: RII NEEDS TO BE CHANGED TO 'YES'.;[04] CORRECTED MEASUREMENTS;[05] CORRECTIVE ACTION COMPLETED.

Part: SHEAR WEB — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

CORROSION ON WEB AT AFT CABIN BS1016+9 BL0 WL208. MARKED<[01] REMOVED AND REPLACED L/H SHEAR WEB AT AFT CABIN BS1016-BS1027 FROM BL0-LBL38 IAW SRM 51-40-02 AND DWG NBR 147A5600;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1; CARD COMPLETE.;[03] REJECTED AMT COMPLETION FOR MEASUREMENT FIELD: RII NEED BE CHANGED TO 'YES'.;[04] CORRECTED MEASUREMENTS;[05] CORRECTIVE ACTION COMPLETED.

Part: FRAME — CRACKED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

CRACKED FRAME AT AFT PAX CABIN S-8R BS907.<[01] INSTALLED REPAIR PARTS AT BS907 BETWEEN S-7R TO S-9 IAW SRM 51-40-02-0G-0 AND EA NO 25-153-00138 REV A;[02] VERIFIED CORRECTIVE ACTION

Part: WEB — CORRODED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

CORROSION ON WEB AT AFT CABIN BS1027 LBL6 WL208. MARKED<[01] THIS CARD WILL BE ACCOMPLISHED ON CARD TTG8Q00Y5QS5;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

CORROSION ON FLOOR BEAM AT AFT CABIN BS986 RBL43 WL208. MARKED<[01] AREA REPAIRED IAW SRM 53-70-51-2R-6 ALTERNATIVE 4 FIGURE 205 SHEET1 TABLE 204. THIS REAPIR IS CATEGORY A; A PERMANENT REPAIR FOR WHICH THE INSPECTIONS GIVEN IN THE MAINTENANCE PLANNING DATA (MPD) DOCUMENTS; ARE SUFFICIENT AND NO OTHER ACTIONS ARE NECESSARY (SEE SRM 51-00-06 FOR MORE REFERENCE);[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH ASERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 242CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 232SF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH ASERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALLDAMAGE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 231XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.

Part: SHIELD — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

FWD CARGO; FWD SHIELD BS 420 TO 440 RBL 23 HAS CORROSION. (MARKED)<[01] REMOVED AND REPLACED FCB FWD SHIELD BS 420 TO BS 440 RBL 23<BR>IAW SRM 51-40-02 SRM 51-40-05 AND DWG # 143A0080 REV:-;[02] VERIFIED ITEM 1

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

FWD CARGO; ZEE SIDEPLATE BS 396 TO 500D LBL 23 HAS CORROSION (MARKED).<[01] REMOVED AND REPLACED SIDEWALL SUPPORT<BR>BS 396 TO BS 500D RBL 23 WL 156 <BR>IAW SRM 51-40-05 AND SRM 53-00-53-2R-6 AND DWG #143A7500 REV: -;[02] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.;[03] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.

Part: SHIELD — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

FWD CARGO; AFT SHIELD BS 480 TO 500A RBL 23 HAS CORROSION. (MARKED)<[01] REMOVED AND REPLACED FCB AFT SHIELD BS 492 TO BS 500A RBL 23 WL 156 IAW SRM 51-40-02 SRM 51-40-05 AND DWG # 143A0080 REV:-

Part: PLATE — CORRODED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

FWD CARGO; ZEE SIDEPLATE BS 500A TO 500D RBL 23 HAS CORROSION (MARKED).<[01] REMOVED AND REPLACED FWD CARGO ZEE SIDEPLATE BS 500A TO BS 500D RBL 23 WL 156 IAW SRM 51-40-02 AND DWG#143A7500 REV:-

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 242AF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 57,792 hrs · 31,530 cycles

CRACKED WEB VAPOR BARRIER BS 663 LBL 31.83 WL 154 (MARKED)<[01] REPAIRED CRACK DAMAGE ON VAPOR BARRIER BS 663 IAW SRM 51-70-04-2R-10.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 242DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF WITH AREAS OF PULLED STRANDS ON UPPER SURFACE WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0127;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 57,792 hrs · 31,530 cycles

PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 231ZF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH ASERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 57,585 hrs · 31,416 cycles

L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PER M/M 33-51-06.

Part: SEAL — DELAMINATED (ZN 300 STABILIZE) · airframe 57,585 hrs · 31,416 cycles

LEFT HORIZONTAL STABILIZER FORWARD LOWER SLIDER RUB STRIP DELAMINATING<[01] R/R LEFT HORIZONTAL STABILIZER FORWARD LOWER SLIDER PER AMM 53-31-31

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,227 hrs · 29,311 cycles

GEAR HANDLE WAS MOVED FROM UP TO OFF; 3 RED LIGHT AND GEAR PARTIALLY EXTENDED AT 296 KNOTS.<[01] NO PREVIOUS HISTORY. PERFORMED TEST OF LANDING GEAR POSITION INDICATING AND WARNING SYSTEM PER AMM 32-61-00. ALL INDICATIONS AND FUNCTIONS ARE NORMAL.

Part: DOUBLER — CRACKED (ZN 100 FUS LOWER) · airframe 54,035 hrs · 29,183 cycles

GPU DOOR LOWER SURROUND DOUBLER CRACK.<[01] CUT OUT DAMAGE; FAB; DRILLED UP DOUBLER AND FILLER PER SRM 53-10-15-2R-4;[02] ACCOMPLISHED HFEC OF CUT OUT AREA PER NDT PART 6; 51-00-00 PROCEDURE 23. NO DEFECTS FOUND.;[03] INSTALLED REPAIR PARTS PER SRM 53-10-15-2R-4;[04] C/W RII INSPECTIONS

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 53,876 hrs · 29,085 cycles

BS 663 RIGHT WHEEL WELL VAPOR BARRIER IS CRACKED AT RBL 31.83; CRACK MEASURES 17' LENGTH.<[01] REPAIRED DAMAGE AREA AT RIGHT WHEEL WELL VAPOR BARRIER AS PER SRM 51-70-04-2R-10.MATERIAL USED EY 3804 A/B PO#2040614 PLUS BMS9-3-120TYD CL7 PO#1690463.APPLIED TEFLON PAINT TO AFT SIDE OF RIGHT-HAND VAPOR BARRIER AS PER B 737 AMM 51-21-81-370-802 APPLIED PRIMER TO FORWARD SIDE OF VAPOR BARRIER AS PER B 737 AMM 51-21-72-370-804;[02] RII-VERIFIED REPAIR

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 53,876 hrs · 29,085 cycles

BS 663 LEFT WHEEL WELL VAPOR BARRIER IS CRACKED LBL 31.83 TO 45.84; LENGTH OF CRACK MEASURES 20.5'.<[01] REPAIRED DAMAGE AREA AT LEFT WHEEL WELL VAPOR BARRIER AS PER SRM 51-70-04-2R-10. MATERIAL USED EY 3804 A/B PO#2040614 PLUS BMS9-3-120 CL7 PO#1690463.APPLIED TOPCOAT ON LH WHEEL WELL VAPOR BARRIER REF B 737 AMM 51-21-81-370-801;[02] RII-VERIFIED REPAIR

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 53,385 hrs · 28,778 cycles

AT BS 663 RIGHT WHEEL WELL VAPOR BARRIER IS CRACKED AT RBL 31.83; CRACK MEASURES 17' LENGTH.<[01] ACCOMPLISHED EA 23-157-02635 TO NOTED AREA.;[02] VERIFIED.

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 53,385 hrs · 28,778 cycles

AT BS 663 RIGHT WHEEL WELL VAPOR BARRIER IS CRACKED AT RBL 40 AT WL 164; CRACK MEASURES 2.5' LENGTH.<[01] ACCOMPLISHED EA 23-157-02634 TO NOTED AREA.;[02] VERIFIED.

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 53,385 hrs · 28,778 cycles

AT BS 663 LEFT WHEEL WELL VAPOR BARRIER IS CRACKED LBL 31.83 TO 45.84; LENGTH OF CRACK MEASURES 20.5'.<[01] ACCOMPLISHED EA 23-157-02634 TO NOTED AREA.;[02] VERIFIED.

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 53,385 hrs · 28,778 cycles

AT BS 663 RIGHT WHEEL WELL VAPOR BARRIER IS CRACKED AT RBL 40 TO RBL 45.64; WL 169; CRACK MEASURES 12'<[01] ACCOMPLISHED EA 23-157-02634 TO NOTED AREA.;[02] VERIFIED.

Part: BRACKET — CRACKED (ZN 600 RIGHT WIN) · airframe 53,383 hrs · 28,777 cycles

-RIGHT WING TO BODY FAIRING 194AR PNL VERTICAL SUPPORT BRACKET CRACKED AT STA 500.<[01] REMOVED AND REPLACED RIGHT WING TO BODY FAIRING 194AR PNL VERTICAL SUPPORT BRACKET PER SRM 51-40-02.

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 53,383 hrs · 28,777 cycles

RIGHT HORIZONTAL STABILIZER- UPPER FORWARD SLIDER CRACKED.<[01] R&R RH HORIZONTAL UPPER FWD SLIDER REF. AMM 53-31-31.

Part: SLIDE — OUT OF ADJUST (ZN 800 DOOR) · airframe 52,048 hrs · 27,904 cycles

L1 DOOR EMERGENCY SLIDE HANGING OUT OF COMPARTMENT TSR# 2023002221<[01] ADJUSTED Z-FOLD REF MT 725-61-06 NO OTHER DEFECTS NOTED AC OK FOR SERVICE

Part: HINGE — CRACKED (AFT PAX DOOR) · airframe 51,674 hrs · 27,658 cycles

AFT ENTRY DOOR; AFT DOOR STOP HINGE; 3RD FROM THE TOP; HAS EVIDENCE OF A CRACK. AFT ENTRY DOOR AFT DOOR STOP 3RD FROM THE TOP HAS EVIDENCE OF A CRACK.<[01] PERFORMED HFEC CRACK VERIFICATION ON AFT ENTRY DOOR; AFT DOOR STOP HINGE; 3RD FROM THE TOP; IAW NDT MANUAL PART 6 51-00-00 PROCEDURE 23.;[02] R&R AFT ENTRY DOOR PER AMM 52-13-00

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,537 hrs · 27,573 cycles

L-1 DOOR EXTERIOR FUSELAGE EMERGENCY LIGHT INOP.<[01] REPLACED LAMP AT L-2 DOOR SLIDE EMERGENCY LIGHT PER AMM 33-51-04-960-801.<BR>TOOL ID 6699 CAL DUE 06/08/23<BR>AAR TAG A129955;[02] VERIFIED STEP 1

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 51,537 hrs · 27,573 cycles

SEVERAL EMERGENCY LIGHTS BY MID-CABIN SECTION FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED BATTERY AT M1669 AND M1668 I.A.W AMMM 33-51-06-960-805 SEPT 4.A TO E; AND POWER SUPPLY AT M1669 AND M1668 I.A.W AMM 33-51-06-960-806 STEP 5.A TO E; INSTALLATION TEST NORMAL;[02] VERIFIED STEP 1

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,537 hrs · 27,573 cycles

L-2 DOOR EXTERIOR FUSELAGE EMERGENCY LIGHT INOP.<[01] REPLACED LAMP AT L-1 DOOR SLIDE EMERGENCY LIGHT PER AMM 33-51-04-960-801.<BR>TOOL ID 6699 CAL DUE 06/08/23<BR>AAR TAG A129955;[02] VERIFIED STEP 1

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 51,537 hrs · 27,573 cycles

SEVERAL EMERGENCY LIGHTS BY MID-CABIN SECTION FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED BATTERY AT M1669 AND M1668 I.A.W AMMM 33-51-06-960-805 SEPT 4.A TO E; AND POWER SUPPLY AT M1669 AND M1668 I.A.W AMM 33-51-06-960-806 STEP 5.A TO E; INSTALLATION TEST NORMAL;[02] VERIFIED STEP 1

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 51,537 hrs · 27,573 cycles

RH HORIZONTAL STABILIZER RIB 5 AFT LOWER END FASTENER HOLES CRACKED IN THE MID SECTION 0.500' IN LENGTH. RH HORIONTAL STABILIER RIB 5 AFT LOWER END FASTENER HOLES CRACKED IN THE MID SECTION 0.500&#34; IN LENGTH.<[01] PERFORMED HFEC INSP ON STAB RIB 5 PER B737 NDT PART 6 51-00-00 PROC 23; 0.500' CRACK FOUND. TOOL USED NORTEC 500; B/C 19497; CAL DUE DATE 05/23;[02] REMOVED DAMAGED SECTION DUE TO CRACK AT RH HORIZ. STAB. RIB #5 AFT LOWER END SRM 51-10-02-0G-0;[03] REMOVED AFT SUPPORT ANGLE AT RH HORIZ. STAB. RIB #5 REF SRM 51-40-02-0G-0;[04] VERIFIED STEP #3;[05] PERFORMED ROTO INSP ON ALL EXISTING FASTENERS ON AFT WEB AREA REPAIR SECTION IAW B737 NDT P6 51-00-00 PROC.16; NO CRACKS NOTED<BR>TOOL USED : NORTEC 600 B/C 172389 03/23;[06] ACCOMPLISHED REPAIR AS PER EA: 22-155-03624;[07] TASK C/W;[08] TASK C/W

Part: FLOORBEAM — CORRODED (BS 986) · airframe 51,537 hrs · 27,573 cycles

CORROSION AT AFT CABIN WET AREA FLOORBEAM FWD FLANGE FASTENER HOLES BS 986.5, LBL 45. REMOVED CORROSION IAW SRM 51-40-02-0G-0, INSTALLED A REPAIR ANGLE AND STRAP IAW SRM 53-70-51-2R-6, ALTERNATIVE 4, FIGURE 205, SRM 51-40-02-0G, SRM 51-40-02-0G-0, AND SRM 51-20-05-0G-0.

Part: PANEL — CRACKED (LT WING LE) · airframe 51,537 hrs · 27,573 cycles

LEFT WING LEADING EDGE ACCESS PANEL 521MB CRACKED. PREPARED DAMAGE AREA FOR REPAIR AT LT WING LEADING EDGE PANEL 521MB IAW SRM 51-70-04-2R-6. REPAIRED THE DAMAGE AREA IAW SRM 51-70-04-2R-6. RESTORED ORIGINAL FINISHED IAW AMM 51-21-99-300-801.

Part: PANEL — CORRODED (ZN 100 FUS LOWER) · airframe 51,537 hrs · 27,573 cycles

WASTE TANK DOOR 145AL FOUND CORROSION AT BONDING JUMPER TERMINAL CONNECTION<[01] REMOVED WASTE TANK SERVICE PANEL AS PER AMM 52-49-07-000-801.;[02] VERIFIED STEP 1. OK TO INSTALL NEW WASTE TANK SERVICE PNL 145AL.;[03] INSTALLED NEW WASTE TANK SERVICE PANEL 145AL; AS PER AMM 52-49-07-400-801.;[04] APPLIED TOPCOAT AT NEW DOOR AS PER AMM 51-21-73.;[05] VERIFIED STEPS 3 AND 4

Part: RIB — CRACKED (VERTICAL STAB) · airframe 51,537 hrs · 27,573 cycles

DORSAL FIN ACCESS PANEL 321A FWD RIB #8 ASSY CRACKED P/N 174A1008-2<[01] LOCATED & DRILLED NEW RIB P/N: 174A1108-2; AS PER DWG. 174A1008 & SRM 51-40-02-0G-0.(JOB ACCOMPLISHED BY: W.C.#372).;[02] LATE ENTRY: REMOVED DAMAGE RIB #8 AT DORSAL FIN PANEL 321A; AS PER SRM 51-40-02-0G-0.;[03] VERIFIED STEPS 1 AND 2. OK TO INSTALL NEW RIB.;[04] INSTALLED NEW RIB #8 P/N: 174A1008-2 AT DORSAL FIN PANEL; 321A AS PER SRM 51-40-02-0G-0 & DWG. 174A1008.;[05] VERIFIED STEP 4

Part: ANGLE — CRACKED (BS 663) · airframe 51,537 hrs · 27,573 cycles

CRACK FOUND AT EXTERNAL LOWER RT VAPOR BARRIER WEB STA 663 OPEN HOLE LOCATION RBL 7. CRACK FOUND AT EXTERNAL UPPER RT VAPOR BARRIER WEB ATTACH ANGLE STA 663 OPEN HOLE LOCATION RBL 7.<FORMED REPLACEMENT ANGLE & SPLICE ANGLE FOR REPAIR AT VAPOR BARRIER ATTACH ANGLE; AS PER SRM. 51-10-10-2R-5 REPAIR 5; TABLE 201; FIG. 202 AND SRM.51-30-01-0G-0; REPAIR PART INSTALLATION AND STEP 18 CORRECTION FOR STEP 1.APPLIED FILLET SEALANT BMS5-95 SEALANT; AROUND THE EDGES OF THE REPAIR AS PER AMM 51-31-00-390-804.

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 51,537 hrs · 27,573 cycles

2 CRACKS FOUND AT EXTERNAL LOWER LT VAPOR BARRIER WEB STA 663 OPEN HOLE LOCATION LBL 6 AND LBL 7; MARKED. 2 CRACKS FOUND AT EXTERNAL LOWER LT VAPOR BARRIER WEB STA 663 OPEN HOLE LOCATION LBL 6 AND LBL 7 MARKED.<[01] FORMED REPLACEMENT ANGLE & SPLICE ANGLE FOR REPAIR AT LT VAPOR BARRIER ATTACH ANGLE; AS PER SRM. 57-10-10-2R-5 REPAIR 5; TABE 201; FIG. 202 AND SRM. 51-30-01-0G-0; MATERIAL USED 2024T3 ;063' & ;071' CLAD.FABRICATED FILLER AND DOUBLE REPAIR AS PER SRM 57-10-10-2R-5 REPAIR 5 TABLE 201 FIG 202.;[11] VERIFIED STEP 10 FABRICATION OF REPAIR PARTS;[12] OK TO TREAT AND PRIME REPAIR PARTS;[13] TREATED AND PRIMED AS REQUIRED AS PER SRM 51-20-01-0G-0 & AMM 51-21-72-370-803 ] INSTALLED REPAIRS PARTS REF SRM 57-10-10-2R-5 REPAIR 5 FIG 202 ;DETAIL 'B'<BR><BR>SEALANT APPLICATION :MIX TIME 14:00 APPLICATION 14:15 SQUEEZE OUT 14:30 12/13/2022 REF SOPM 20-50-19;CAP SEALED FUEL TANK FASTENERS AS PER SRM 51-80-01;[18] PERFORMED ELECT. RESISTANCE CHECK OF THE ELECT. BONDING FASTENERS: PASSED; IN REF. SWPM 20-20-00. TOOL USED: B/C: 163055ACCOMPLISHED REPAIR AS PER SRM 57-10-10-2R-5 REPAIR 5; FIG. 202. DETAIL: 'B'.;[22] ADD INF. ON STEP #10: ACCOMPLISHED ROUGHNESS TEST ON CUT OUT AREA 63 MICROINCHES RA AND REPAIR PARTS 125 MICROINCHES RA REF SRM 51-20-13-0G-0. TOOL ID# 172329

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 51,537 hrs · 27,573 cycles

AFT CARGO COMP CARGO TRACK CORROSION BETWEEN STA 787-847 RBL 14' AFT CARGO COMPARTMENT TRACK CORROSION BETWEEN STA 787 + 7 AND STA 847 - 6 RBL 13.8'<[01] FOUND EXFOLIATING CORROSION AT AFT CARGO COMPARTMENT CARGO TRACK BETWEEN STA 787 TO STA 847 RBL 14. THIS CORROSION IS OUT OF LIMITS AS PER REF 53-00-53-1A-2. PART NEEDS REPLACEMENT;[REMOVED AFT CARGO COMPARTMENT SECTION OF CARGO TRACK RBL 13.8' FROM STA 787 + 7 AND STA 847 - 6 REF SRM 51-40-02-0G-0;LOCATED AND DRILLED HOLES AT NEW AFT CARGO COMPARTMENT TRACK PN 53100007-001 BETWEEN STA 787+7' AND STA 847-6' AND RBL 13.8 REF SRM 51-40-05-0G-0;[07] LOCATED AND DRILLED HOLES AT NEW AFT CARGO COMPARTMENT TRACK PN 53100007-001 BETWEEN STA 787+7' AND STA 847-6' AND RBL 13.8 REF SRM 51-40-05-0G-0;[08] VERIFIED STEPS 1 - 4. REMOVAL OF CARGO COMPARTMENT TRACK.;[09] VERIFIED STEPS 5 - 7. LOCATING AND DRILLING OF HOLES. OK TO TREAT AND PRIME.<BR>OK TO INSTALL NUT PLATES.;[10] TREATED AND PRIMED NEW AFT CARGO COMPARTMENT TRACK PN 53100007-001 REF AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[11] INSTALLED NEW NUT PLATES AT NEW AFT CARGO COMPARTMENT TRACK PN 53100007-001 REF SRM 51-40-02-0G-0;[12] VERIFIED STEP 10 AND 11;[13] OK TO INSTALL NEW AFT CARGO TIE DOWN TRACK PN 53100007-001 BETWEEN STA 787+7' AND STA 847-6' AND RBL 13.8;[14] INSTALLED NEW AFT CARGO TIE DOWN TRACK PN 53100007-001 BETWEEN STA 787+7' AND STA 847-6' AND RBL 13.8 REF SRM 51-40-02-0G-0 AND DWG 146A7500.

Part: STRAP — CORRODED (ZN 100 FUS LOWER) · airframe 51,537 hrs · 27,573 cycles

AFT CARGO COMP STRAP UNDER FLOOR SUPPORT CORROSION STA 767+14 RBL 20'<[01] FOUND EXFOLIATING CORROSION AT AFT CARGO COMPARTMENT STRAP UNDER FLOOR SUPPORT AT STA 767+ 14 RBL 20. THIS CORROSION IS OUT OF LIMITS AS PER REF SRM 53-00-53-1A-2. PART NEEDS REPLACEMENT;[02] REMOVED STRAP AT AFT CARGO COMPARTMENT UNDER FLOOR SUPPORT STRUCTURE STA 767+14' AND RBL 20 REF SRM 51-40-02-0G-0;[03] LOCATED AND DRILLED HOLES ON NEW AFT CARGO COMPARTMENT STRAP UNDER FLOOR SUPPORT REF SRM 51-40-05;[04] VERIFIED STEP 1; 2; 3 AND OK TO INSTALL STRAP;[05] PARTIALLY INSTALLED AFT CARGO COMPARTMENT STRAP UNDER FLOOR SUPPORT AT STA 767+14 RBL 20 REF SRM 51-40-02;[06] FINALIZED INSTALLATION OF AFT CARGO COMPARTMENT STRAP UNDER FLOOR SUPPORT AT STA 767+ 14 RBL 20' REF SRM 51-40-02;[07] VERIFIED STEP 6

Part: BRACKET — CRACKED (L2 DOOR) · airframe 51,537 hrs · 27,573 cycles

L2 DOOR PANEL 834DZ FWD BRACKET CRACKED<[01] REMOVED AND REPLACED BRACKET AT L2 DOOR PANEL 834DZ REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 51,537 hrs · 27,573 cycles

MAIN CABIN BETWEEN STA 380-400 RBL 12' INTERCOSTAL CRACKED<[01] REMOVED & REPLACED INTERCOSTAL ANGLE P/N: 143A5410-170; AS PER SRM 51-40-02-0G-0 & DWG. 143A5400.;[02] VERIFIED STEP 1

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 51,537 hrs · 27,573 cycles

MAIN CABIN BETWEEN STA 380-400 LBL 14' INTERCOSTAL CRACKED<[01] REMOVED INTERCOSTAL AT MAIN CABIN BETWEEN STA 380-400 AS PER REF SRM 51-40-02;[02] VERIFIED STEP 1 OK TO INSTALL NEW INTERCOSTAL;[03] INSTALLED NEW INTERCOSTAL AT MAIN CABIN BETWEEN STA 380-400 AS PER REF SRM 51-40-02 AND DWG #143A5400;[04] CORRECTION ON STEP #3: INSTALLED NEW INTERCOSTAL AT MAIN CABIN BETWEEN STA 380-400; LBL13.24; AS PER REF SRM 51-40-02 AND DWG #143A5400;[05] VERIFIED STEP 4

Part: ANGLE — CRACKED (BS 500C S26L) · airframe 51,537 hrs · 27,573 cycles

FWD CARGO COMP STA 500C STR 26L CLIP UNDER ZEE CHANNEL CRACKED<[01] REMOVED CLIP AT FWD CARGO COMP STA 500C STR 26L AS PER REF SRM 51-40-02;[02] RREMOVED AND REPLACED 1 EA CLIP ; STA 500C STR26L SRM51-40-02 AND DWD #143A7505.;[03] VERIFIED STEPS 1 AND 2

Part: SEAL — DAMAGED (HORIZONTAL STAB) · airframe 51,537 hrs · 27,573 cycles

R/H HORIZONTAL STABILIZER CENTER BOX FWD HINGE LOWER SLIDING SEAL MISSING RUB STRIPS. REMOVED R/H HORIZONTAL STABILIZER CENTER BOX FWD HINGE LOWER SLIDING SEAL REF AMM-53-31-31-000-803;[02] VERIFIED STEP 1 REMOVAL OF LOWER SLIDING SEAL. OK TO INSTALL NEW LOWER SLIDING SEAL.. INSTALLED NEW R/H HORIZONTAL STABILIZER CENTER BOX FWD HINGE LOWER SLIDING SEAL REF AMM 53-31-31-400-803.

Part: FLOORBEAM — CORRODED (BS 986 LBL24-45) · airframe 51,537 hrs · 27,573 cycles

CORROSION AT AFT CABIN WET AREA FLOOR BEAM FWD FLANGE FASTENER HOLES STA 986.5 LBL24 TO LBL 45. REMOVED CORROSION AT AFT CABIN WET AREA FLOOR BEAM FWD FLANGE FASTENER HOLE STA 986.5 AND LBL45 REF SRM 51-40-02-0G-0.<OUT OF LIMITS REF. SRM 53-70-51-1A-1; FIGURE 103. PERFORMED HFEC INSP ON REWORKED AREA STA986.5 LBL45 IAW B737 NDT P6 51-00-00 PROC.23. NO CRACKS NOTED. TRIM OUT DAMAGED SECTION (1.250' & 0.850') AT AFT CABIN WET AREA FLOORBEAM FWD FLANGE IAW SRM 53-70-51-2R-6; FIGURE 205.

Part: FLOOR SUPPORT — CRACKED (BS 312-328 RBL30) · airframe 51,537 hrs · 27,573 cycles

MAIN CABIN FWD WET AREA BETWEEN STA 312-328 RBL 30' INTERCOSTAL CRACKED<[01] REMOVED INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN STA 312-328 RBL 30' AS PER REF SRM 51-40-02;[02] VERIFIED STEP 1 OK TO INSTALL NEW INTERCOSTAL;[03] REPLACED NEW INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN STA 312-328 RBL 30' AS PER REF SRM 51-40-02 AND DWG # 141A5400;[04] VERIFIED STEP 3

Part: FLOOR SUPPORT — CRACKED (BS 277-294 BL0) · airframe 51,537 hrs · 27,573 cycles

MAIN CABIN FWD WET AREA BETWEEN STA 277-294.5 BL 0 INTERCOSTAL CRACKED<[01] REMOVED INTERCOSTAL AT MAIN CABIN BETWEEN STA. 277 AND 294.5 BL0 WET AREA PER. REF. SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] DRILLING IN PLACE NEW INTERCOSTAL BETWEEN STA. 277-294.5 BL 0 WET AREA PER. REF. SRM 51-40-05-0G-0;[04] VERIFIED STEP 3 OK TO INSTALL NEW INTERCOSTAL;[05] INSTALLED NEW INTERCOSTAL AT STA. 277 - 294.5; BL 0; AS PER SRM 51-40-02-0G-0; & DWG. 141A5400.;[06] VERIFIED STEP 5

Part: FLOOR SUPPORT — CRACKED (BS 312-328 LBL48) · airframe 51,537 hrs · 27,573 cycles

MAIN CABIN FWD WET AREA BETWEEN STA 312-328 LBL 48' INTERCOSTAL CRACKED<[01] REMOVED INTERCOSTAL AT MAIN CABIN STA.312-328 LBL 48' PER. REF. SRM 51-40-02-0G-0;[02] DRILLING NEW INTERCOSTAL IN PLACE STA.312-348 LBL.48' PER. REF. SRM 51-40-05-0G-0;[03] VERIFIED STEP 1;[04] VERIFIED STEP 2. OK TO INSTALL INTERCOSTAL;[05] INSTALLED NEW INTERCOSTAL AT MAIN CABIN FWD. WET AREA BETWEEN STA.312-328 LBL. 48' PER REF. SRM. 51-40-02-0G-0;[06] VERIFIED STEP 5;[07] CORRECTION ON STEP #5: INSTALLED NEW INTERCOSTAL AT MAIN CABIN FWD. WET AREA BETWEEN STA.312-328 LBL. 48' PER REF. SRM. 51-40-02-0G-0 & DWG. 141A5400.;[08] VERIFIED STEP 7

Part: BRACKET — CRACKED (BS 1016 BULKHEAD) · airframe 51,537 hrs · 27,573 cycles

AFT CABIN WET AREA AFT PRESSURE BULKHEAD LT CORNER BRACKET CRACKED, BS 1016. REMOVED THE BRACKET IAW SRM 51-40-02, FABRICATED A NEW BRACKET IAW DWG 69-43232. LOCATED AND DRILLED THE BULKHEAD BRACKET IAW SRM 51-40-05. INSTALLED THE BULKHEAD BRACKET IAW SRM 51-40-02-0G-0.

Part: BRACKET — CRACKED (LT WING LE) · airframe 51,537 hrs · 27,573 cycles

LEFT WING TRAILING EDGE FIX PANEL JUST O/B OF SPOILER #6 LOWER BRACKET CRACKED<[01] REMOVED BRACKET AT LEFT WING TRAILING EDGE FIX PANEL O/B OF SPOILER #6 AS PER SRM 41-40-02-0G-0-A00729;[02] CORRECTION ON STEP #1:<BR>REMOVED BRACKET AT LEFT WING TRAILING EDGE FIX PANEL O/B OF SPOILER #6 AS PER SRM 51-40-02-0G-0-.;[03] VERIFIED STEP 2 OK TO INSTALL NEW BRACKET;[04] INSTALLED NEW BRACKET AT LEFT WING TRAILING EDGE FIX PANEL O/B OF SPOILER #6 AS PER SRM 51-40-02-0G-0-.;[05] VERIFIED STEP 4

Part: SEAT TRACK — CORRODED (BS 360 LBL 45) · airframe 51,537 hrs · 27,573 cycles

CORROSION FWD WET AREA L/H O/B SEAT TRACK CROWN LBL 45.5 STA 360+10'. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1, FIG.103, DETAIL A. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02-0G-0, AMM 51-21-72. SRM 51-40-02 & DWG. 143A5300.

Part: INTERCOSTAL — CORRODED (ZN 200 FUS TOP) · airframe 51,537 hrs · 27,573 cycles

MAIN CABIN FWD WET AREA BETWEEN STA 312-294.5 LBL 11' INTERCOSTAL UPPER SURFACE CORROSION<[01] REMOVED CORROSION AT INTERCOSTAL; BETWEEN STA. 312 - 294.5; LBL 11'; PER SRM 51-10-02.(JOB ACCOMPLISHED BY: B.M. #35723).;[02] ORIG. MAT. OF MACHINED INTERCOSTAL AT UPPER FLANGE: 0.050'; MAT. : 0.025'; REMAINING MAT.: 0.025'. FOUND OUT OF LIMITS AS PER SRM 53-10-51-1A-1. TOOL USED: WN 0004; DUE DATE: 12/16/22.;[03] FOR ACCESS FOR REMOVE INTERCOSTAL FROM STA.294.5 TO STA 312 LBL 11.16 WERE REMOVED INTERCOSTAL FROM STA.277 TO STA.294.5 AND PULLEY BRACKET FROM STA.294.5 LBL 11.16 REF.BOEING 737-700-SRM 51-40-02-0G-0;[04] REMOVED DAMAGED INTERCOSTAL & 1EA. DIAGONAL ANGLE AT BEAM STA 294.5 LBL 11 TO LBL 9;FOR ACCESS; AS PER SRM 51-40-02-0G-0.;[05] RECEIVED NEW INTERCOSTAL P/N: 141A5690U1; LOCATED & DRILLED AS PER SRM M51-40-05-0G-0 & DWG. 141A5600.;[06] OK TO INSTALL NEW RECEIVED INTERCOSTAL P/N 141A5690U1;[07] OK TO REINSTALL WHAT WAS REMOVED IN STEPS 3 AND 4 FOR ACCESS TO REMOVE INTERCOSTAL;[08] RE-INSTALLED NEW INTERCOSTAL AT LBL 11.16; STA. 312 - 294.5; AS PER SRM 51-40-02-0G-0 & DWG. 141A5600.;[09] RE-INSTALLED 1EA. DIAGONAL ANGLE AT BEAM STA 294.5 LBL 11 TO LBL 9;FOR ACCESS; AS PER SRM 51-40-02-0G-0.;[10] RE-INSTALLED INTERCOSTAL FROM STA.294.5 TO STA 312 LBL 11.16; AND PULLEY BRACKET FROM STA.294.5 LBL 11.16 REF.BOEING 737-700-SRM 51-40-02-0G-0;[11] VERIFIED STEPS 8-10;[12] VERIFIED STEPS 8-10

Part: NOT REPORTED — DAMAGED (BS 360) · airframe 51,537 hrs · 27,573 cycles

MAIN CABIN FWD WET AREA STA 360-4 LBL 61' INNER CHORD HOLE ELONGATED<[01] MEASURED DIAMETER OF ELONGATED HOLE: 0.339'.;[02] CORRECTION ON STEP #1: MEASURED DIAMETER OF ELONGATED HOLE: 0.320'.;[03] MEASURED DIMENSIONS TO 3EA. NEAREST FASTENERS: HOLE #1:(AFT O/B) 0.812'; HOLE #2: (FWD. O/B); 0.687'; HOLE #3: (FWD. I/B): 1.125'. EDGE MARGIN OF AFFECTED HOLE : 0.500'.;[04] VERIFIED STEPS 1-3;[05] REMOVED FASTENERS AND ANGLE SPLICE FOR ACCESS TO WORK AT MAIN CABIN STA.360-4 LBL 61' PER REF SRM. 51-40-02-0G-0;[06] REPAIR WAS ACCOMPLISHED ON EA: 22-153-03642.;[07] RE-INSTALLED FASTENERS AND ANGLE-SPLICE ; REMOVED ON STEP #5;AT MAIN CABIN STA.360-4 LBL 61' PER REF SRM. 51-40-02-0G-0. & DWG. 141A8110.;[08] TASK C/W;[09] VISUAL INSPECTION WAS PERFORMED OF ADJACENT STRUCTURE AND HOLES COMMON TO THE STRAP AND TAPER FILLER AT REPAIR AREA; NO FURTHER DAMAGE WAS NOTED REF SRM 51-00-06-0G-0

Part: FLOOR SUPPORT — CRACKED (BS 344-360 RBL35) · airframe 51,537 hrs · 27,573 cycles

MAIN CABIN FWD WET AREA BETWEEN BS 344-360 RBL 35 INTERCOSTAL CRACKED. REMOVED INTERCOSTAL IAW SRM 51-40-02-0G-0. LOCATED AND DRLLING A NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0. INSTALLED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, & DWG 141A5410.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 51,537 hrs · 27,573 cycles

MAIN CABIN FLOOR PANEL 221BF CRACKED<[01] RECEIVED NEW PANEL. WILL BE INSTALLED ON TTG8Q00FGHSR;[02] VERIFIED STEP 1

Part: BRACKET — CRACKED (ZN 600 RIGHT WIN) · airframe 51,537 hrs · 27,573 cycles

#2 ENGINE O/B FAN COWL CENTER UPPER BRACKET CRACKED<[01] REMOVED AND REPLACED NEW BRACKET AT #2 ENG. OB FAN COWLING CENTER UPPER POSITION PER. REF. SRM 51-40-02-0G-0;[02] CORRECTION ON STEP #1: REMOVED AND REPLACED NEW BRACKET AT #2 ENG. OB FAN COWLING CENTER UPPER POSITION PER. REF. SRM 51-40-02-0G-0 & CMM 71-13-30.

Part: SEAT TRACK — CORRODED (BS 360 LBL 25) · airframe 51,537 hrs · 27,573 cycles

CORROSION FWD WET AREA L/H I/B SEAT TRACK CROWN LBL 24.5 STA 360+10. REMOVED THE SEAT TRACK BS 360+10 - 480, LBL 24.5 IAW SRM 51-40-02-0G-0. FABRICATED A NEW SEAT SECTION IAW SRM 53-00-52-2R-4 FIGURE 202 DETAIL B-B. LOCATED AND DRILLED THE NEW SEAT TRACK IAW SRM 53-00-52-2R-4, AND SRM 51-40-05-0G-0. TREATED & PRIMED REPAIR IAW SRM 51-20-01 & AMM 51-21-72. INSTALLED THE REPAIR IAW SRM 53-00-52-2R-4 REPAIR 4. FIG.202.

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 51,537 hrs · 27,573 cycles

RIGHT HORIZONTAL STABILIZER RIB 5 STIFFENER 3 LOWER SECTION CRACKED<[01] PERFORMED HFEC INSP ON RIB # 5 STIFFENER 3 IAW B737 NDT P6 51-00-00 PROC.23; CRACK NOTED<BR>TOOL USED : NORTEC 600 B/C 166316 CALDUE: 10/23;[02] CRACK LENGTH ON STIFFENER 3 IS 0.625' PER B737 NDT PART 6 51-00-00 PROC 23; TOOL USED NORTEC 500; B/C 19497; CAL DUE DATE 05/23.;[03] PERFORMED ROTO INSP ON STIFFENER#3 LOWER CHORD EXISTING HOLES IAW B737 NDT P6 51-00-00 PROC.16; NO CRACKS<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[04] CUT OUT DAMAGE AREA FROM VERT. STIFFENER #3 OF RIB #5; LOWER SECTION AS PER SRM 55-10-09-2R-4 REPAIR 4; FIG. 202.(JOB ACCOMPLISHED BY: A.S. #22135).;[05] VERIFIED STEP 4;[06] PERFORMED HFEC INSP ON RIB # 5 STIFFENER 3 IAW B737 NDT P6 51-00-00 PROC.23; NO CRACKS.<BR>TOOL USED: NORTEC 600 B/C 166317 CALDUE: 10/23;[07] RECEIVED REPAIR KIT P/N: 55100003-01; LOCATED & DRILLED AS PER SRM 51-40-05; & 55-10-09-2R-4 REPAIR 4; FIG.202.(JOB ACCOMPLISHED BY: A.S. #22135).;[08] VERIFIED STEP 7;[09] OK TO TREAT AND PRIME REPAIR PARTS;[10] TREATED & PRIMED REPAIR PARTS AS PER SRM 51-20-01; & AMM 51-21-72-370-804.;[11] VERIFIED STEP 10. OK TO INSTALL REPAIR PARTS.;[12] INSTALLED REPAIR PARTS AT RT HORZ. STAB. RIB # 5; STIFFENER 3; AS PER SRM 55-10-09-2R-4 REPAIR 4; FIG. 202.;[13] VERIFIED STEP 12;[14] TASK C/W;[15] TASK C/W

Part: SUPPORT FRAME — CRACKED (BS 312) · airframe 51,537 hrs · 27,573 cycles

FWD CABIN WET AREA FUS.SUPPORT FRAME CRACKED @ CUTOUT FLANGE ABOVE L-1 ENTRY DOOR UPPER SILL STA 312 MKD DOT<[01] CLEANED AREA FOR NDT INSPECTION AS PER B-737-700 SOPM 20-30-03.;[02] PERFORMED HFEC INSP. AT FWD CABIN WET AREA FUS.SUPPORT FRAME CUTOUT FLANGE ABOVE L-1 ENTRY DOOR UPPER SILL STA 312 IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. NO CRACKS NOTED<BR>TOOL: NORTEC 600 B/C: 166317 DUE: 10/31/23;[03] C/W;[04] VERIFIED STEP 1. NDT VERIFIED NO CRACKS NOTED. TASK C/W

Part: BRACKET — CRACKED (RT WING LE) · airframe 51,537 hrs · 27,573 cycles

RIGHT WING TRAILING EDGE FIX PANEL JUST O/B OF SPOILER #7 LOWER BRACKET CRACKED<[01] REMOVED CRACKED LOWER ANGLE FROM RIGTH WING TRAILING EDGE FIX PANEL JUST OUT BOARD OF SPOILER #7 REF. BOEING 737-700-SRM 51-40-02-0G-0;[02] RECEIVED; LOCATED AND DRILLING; LOWER ANGLE; FOR REPLACE ON RIGTH WING TRAILING EDGE FIX PANEL JUST OUT BOARD OF SPOILER #7 P/N 115A2156U8 PO# 1799431 REF. 737-700-SRM 51-40-02-0G-0;[03] VERIFIED STEPS 1 AND 2. OK TO INSTALL NEW BRACKET.;[04] INSTALLED NEW ANGLE ON RIGHT WING TRAILING EDGE FIX PANEL JUST OUT BOAR OF SPOILER #7 REF. 737-700-SRM 51-40-02-0G-0;[05] VERIFIED STEP 4

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 51,535 hrs · 27,572 cycles

FOUND CRACKED LOWER RT VAPOR BARRIER WEB STA 663. PERFORMED VISUAL INSPECTION AND TAP TEST INSPECTION AT RT VAPOR BARRIER WEB; FOUND 3 CRACKS (9'';8'' AND 3'') IAW SRM 51-70-04-2R-10 PARAGRAPH 4 AND NDT PART 1 51-05-01 PARAGRAPH 5. REMOVED DAMAGED PLIES AND PREPARED DAMAGED AREA TO APPLY THE GLASS FABRIC REPAIR, DRILLED STOP HOLE AT THE CRACKS END, NO WATER NOTE AT REPAIR AREA IAW SRM 51-70-04-2R-10 PARAGRAPH 4 & SRM 57-10-10-2R-2 PARAGRAPH 6. APPLIED THE GLASS FABRIC REPAIR AT DAMAGED AREA ON RT VAPOR BARIER IAW SRM 51-70-04-2R-10 PARAGRAPH 4. APPLIED TEFLON PAINT ON RT VAPOR BARRIER WEB IAW AMM 51-21-81-370-802. APPLIED PRIMER AT FWD FACE OF RT VAPOR BARRIER WEB AS PER AMM 51-21-72-370-804.

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 51,535 hrs · 27,572 cycles

FOUND CRACKED LOWER LT VAPOR BARRIER WEB STA 663. PERFORMED VISUAL INSPECTION ON L\H VAPOR BARRIER AND FOUND CRACK OF 11'' IAW NTM 51-05-01 AND APPLIED STOP DRILL SIZE 0.25 DIAMETER AT THE END OF CRACK PER B737SRM57-10-10-2R-2 STEP 6.B. PREPARED DAMAGED AREA TO APPLY REPAIR AT L\W VAPOR BARRIER IAW SRM 51-70-04-2R-0. REPAIRED LT VAPOR BARRIER AT DAMAGED AREA IAW SRM 51-70-04-2R-0. APPLIED PRIMER AT FWD FACE OF WEB & PAINT AT AFT FACE OF WEB IAW AMM 51-21-72-370-804, & 51-21-81-370-801.

Part: GIRT BAR — OUT OF POSITION (DOOR SLIDE) · airframe 51,117 hrs · 27,296 cycles

AFT SERVICE SLIDE GIRT HANGS OUT / REPOSITIONED GIRT REF MM 25-66.

Part: LIGHT — MISSING (L1 DOOR) · airframe 50,695 hrs · 27,030 cycles

L1 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARROW. / [01] REMOVED AND REPLACED L1 DOOR LOWER EXIT SIGN INDICATOR LENS REF AMM 33-51-01;[02] INSPECTED

Part: LIGHT — INOPERATIVE · airframe 50,073 hrs · 26,595 cycles

EMERGENCY EXIT ROW (BOTH SIDES) CABIN LIGHTS NOT WORKING SMALL FLUORESCENT TUBES AT THE EMERGENCY EXIT DOORS / [01] OK TO CONTINUE PER MEL 33-2-03 SP1 B;[02] REPLACED THE LIGHT ASSEMBLY FUSE FOR THE L/H SIDE AND RE-LAMPED THE R/H SIDE PER AMM 33-21-00. OPS CHECKS NORMAL. MEL CLEARED.

Part: PANEL — ELONGATED (WING TO BODY) · airframe 49,784 hrs · 26,430 cycles

193B PANEL HAS NUMEROUS ELONGATED FASTENER HOLES. / [01] REPLACED 193B PANEL PER SRM 51-40-02

Part: MEGAPHONE — INOPERATIVE · airframe 49,617 hrs · 26,324 cycles

FWD MEGAPHONE INOP / [01] INSTALLED NEW BATTERY AS PER MM 25-64-00

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 49,024 hrs · 25,949 cycles

LEFT OVER WING EMERGENCY LIGHT INOP / [01] RE-LAMPED REF AMM 33-51-04 OPS CHECK GOOD

Part: PANEL — CRACKED · airframe 49,024 hrs · 25,949 cycles

194 E PANEL TRAILING EDGE HAS 3 EACH HOLES WITH CRACKS ; / [01] DRILLED; AND PREPARED NEW PANEL; [02] INSTALLED PANEL PER AMM 53-51-21

Part: PANEL — CRACKED (FUSELAGE) · airframe 49,024 hrs · 25,949 cycles

193D PANEL TRAILING EDGE HAS 3 EACH HOLES WITH CRACKS AND SERVAL COUNTERSUNK WITH EXCESSIVE WEAR ; / [01] DRILLED; TRIMMED AND PREPARED HOLE IN NEW PANEL; [02] INSTALLED PANEL 193D PER AMM 53-51-21

Part: LATCH — LOOSE (C/P EMER EXIT) · airframe 46,946 hrs · 24,733 cycles

UPPER COCKPIT DOOR EMERGENCY EXIT LATCH LOOSE ; / RESET COCKPIT DOOR EMERGENCY EXIT UPPER DOOR LATCH PER AMM 52-51-08.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,286 hrs · 24,355 cycles

CAPTAIN SIDE OVERWING EXIT LIGHT INOP / RELAMPED OPS NORMAL 33-51-21

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 45,916 hrs · 24,138 cycles

AFT GALLEY DOOR SLIDE GAUGE NEEDS ADJUSTED IN WINDOW. ADJUSTED SLIDE SO THE GAUGE IS VISIBLE, PER AMM 25-66-01.

Part: HANDLE — LOOSE (L1 DOOR ASSIST) · airframe 45,916 hrs · 24,138 cycles

FWD ENTRY DOOR INNER ASSIST HANDLE LOOSE. SECURED ASSIST HANDLE, IAW AMM 52-11-31.

Part: FLOOR PANEL — GOUGED (COCKPIT) · airframe 45,916 hrs · 24,138 cycles

FLIGHT DECK FLOOR PANEL 211AF IS GOUGED. REMOVED AND REPLACED DAMAGED FLOOR PANEL, PER SRM 51-40-02.

Part: MOUNT BRACKET — CRACKED (RT WING) · airframe 45,916 hrs · 24,138 cycles

RH WING TRAILING EDGE PANEL 651FB FWD EDGE HYDRAULIC GUIDE MOUNT BRACKET CRACKED / REMOVED AND REPLACED BRACKET PER SRM 51-40-02

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 45,916 hrs · 24,138 cycles

REFERENCE G763839: RIGHT STAB, RIB 1, STA 92.70 HAS A CRACK IN LOWER RADIUS OF VERTICAL STIFFENER NR 3. HFEC VERIFIED. REQUIRES ACCESS UPPER INSPAR SKIN OF HORIZONTAL STAB. REPAIR PER SRM. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 45,916 hrs · 24,138 cycles

CAPTAINS SEAT TRACKS ARE WORN (4 EACH). REMOVED AND REPLACED CAPTAIN'S SEAT TRACKS, PER AMM 25-11-11.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 45,916 hrs · 24,138 cycles

F/O'S SEAT TRACKS ARE WORN (4 EACH). REMOVED AND REPLACED F/O'S SEAT TRACKS, PER AMM 25-11-11.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 45,916 hrs · 24,138 cycles

RIGHT STAB RIB 1 STA 92.70 HAS A CRACK IN LOWER RADIUS OF VERTICAL STIFFENER NR 3. HFEC VERIFIED. REPAIRED RT STAB RIB 1 AT STA 92.70 NR 3 STIFFENER, PER SRM 55-10-09-2R-4.

Part: FLOORBOARD — DENTED (CABIN) · airframe 45,916 hrs · 24,138 cycles

CABIN FLOOR BOARD 241BF HAS SEVERAL DENTS AND FIBERGLASS DAMAGE. R & R CABIN FLOOR BOARD 241BF, PER AMM 53-21-00.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 45,916 hrs · 24,138 cycles

CABIN FLOOR BOARD 242AF HAS FIBERGLASS DAMAGE. R & R CABIN FLOOR BOARD 242AF, PER AMM 53-21-00.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 45,916 hrs · 24,138 cycles

CABIN FLOOR BOARD 242BF HAS FIBERGLASS DAMAGE. R & R CABIN FLOOR BOARD 242BF, PER AMM 53-21-00.

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 45,916 hrs · 24,138 cycles

COCKPIT FLOOR HAS DENT BELOW 2ND OBSERVERS SEAT. REPAIRED COCKPIT FLOOR, PER EA 1-A53-33179 SEE ALL INDIVIDUAL SIGN OFFS.

Part: PLATE — CRACKED (RT WING) · airframe 45,916 hrs · 24,138 cycles

RT WING WIGGLE PLATE CRACKED AT FWD INBD ATTACH POINT FOR LOWER T/E PANEL 651EB. / REMOVED AND REPLACED RIGHT WING WIGGLE PLATE COMMON TO LOWER T/E PANEL 651EB REF SRM 51-40-02. RESTORED FINISH REF AMM 51-21-99.

Part: BRACKET — CRACKED (RT WING) · airframe 45,916 hrs · 24,138 cycles

RT WING UNDER FWD INBD CORNER OF PANEL 651AT BRACKET CRACKED [MARKED]. / REMOVED AND REPLACED BRACKET PER SRM 51-40-02

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 44,561 hrs · 23,313 cycles

EMERGENCY LIGHT POWER SUPPLY M01672 DRAINED DURING OPS CHECK OF EMERGENCY LIGHTS. R & R'D EMERGENCY LIGHT POWER SUPPLY M01672 PER AMM 33-51-06.

Part: LENS — LOOSE (CABIN) · airframe 41,964 hrs · 21,645 cycles

LT OVERWING EXIT DOOR SIDEWALL MOUNTED EMERGENCY LIGHTED SIGN LENS LOOSE. SECURED LIGHT LENS AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 41,210 hrs · 21,168 cycles

FORWARD GALLEY EMERGENCY FLASHLIGHT STRAP BROKEN. R&R STRAP PER MM.

Part: PROBE — FAULTY (TAT) · airframe 40,474 hrs · 20,695 cycles

DECLARED EMERGENCY, ON CLIMBOUT VERTICAL NAVIGATION DISCONNECTED, UNABLE TO RECONNECT. BOTH AUTOPILOT PILOTS WOULD NOT ENGAGE. COULD NOT MODIFY THE FMG WITH ANY INPUTS. TOTAL AIR TEMP DATA WAS MISSING ON THE CENTER DISPLAY UNIT. ENGINE N1 DIGITS ALSO MISSING. NO TRUE AIR SPEED READING ON THE DISPLAY UNITS. NO AMBER CAUTION LIGHTS ILLUMINATED. NO VERTICAL MODES ON THE MLP PANEL WORKED. R&R TOTAL AIR TEMPERATURE PROBE PER AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 40,286 hrs · 20,571 cycles

R2 DOOR ESCAPE SLIDE COVER OUT OF ADJUST. REPOSITIONED SLIDE PER MT.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 40,286 hrs · 20,571 cycles

BATTERY PACK INOP AT LOCATION M1670. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 40,286 hrs · 20,571 cycles

BATTERY PACK INOP AT LOCATION M1673. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 40,286 hrs · 20,571 cycles

BATTERY PACK INOP AT LOCATION M2335. R&R BATTERY PACK PER AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 40,286 hrs · 20,571 cycles

RT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STA 120.3, ON THE LOWER END OF THE 4TH VERTICAL STIFFENER FROM THE FRONT. REPAIRED RIB PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

CABIN FLOOR PANEL SUPPORT CRACKED AT BS 540, RBL 2. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — BENT (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

AFT CARGO BAY BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT BENT BETWEEN BS 827 TO BS 847, LBL 20. R&R SUPPORT PER SRM & DWG.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 40,286 hrs · 20,571 cycles

***CORROSION*** ON ACB FLOOR PANEL 140DF / FABRICATED NEW ACB FLOOR PANEL 140DF FROM .071 2024T3; LOT# 1373736-1 PER AMM 25-52-01-201-801 AND DWG 453A2610 DUE TO NO ALLOWABLE DAMAGE GIVEN IN SRM FOR THIS PART

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 40,286 hrs · 20,571 cycles

***CORROSION*** ON ACB FLOOR PANEL 140AF / FABRICATED NEW ACB FLOOR PANEL 140AF FROM .071 2024T3; LOT# 1373736-1 PER AMM 25-52-01-201-801 AND DWG 453A2610 DUE TO NO ALLOWABLE DAMAGE LIMITS GIVEN IN SRM FOR THIS PART

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 40,286 hrs · 20,571 cycles

FCB FLOOR PANEL 120CF IS CORRODED / FABRICATED NEW FCB FLOOR PANEL 120CF FROM .071 2024T3; LOT# 1373736-1 PER AMM 25-52-01-201-801 AND DWG 453A1610 DUE TO NO ALLOWABLE DAMAGE LIMITS GIVEN IN SRM FOR THIS PART

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 40,286 hrs · 20,571 cycles

FCB FLOOR PANEL 120AF IS CORRODED AROUND EDGES / FABRICATED NEW FCB FLOOR PANEL 120AF FROM .071 202AT3; LOT# 1373736-1 PER AMM 25-52-01-201-801 AND DWG 453A1610 DUE TO NO ALLOWABLE DAMAGE LIMITS GIVEN FOR THIS PART IN SRM

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA.

Part: BEAM — CRACKED (R1 DOOR) · airframe 40,286 hrs · 20,571 cycles

R1 DOOR NR 4 LOWER BEAM CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR ANDLE BOX ASSEMBLY. R&R DOOR PER AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

AFT CARGO FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN BS 727C TO BS 798, LBL 21. R&R SUPPORT PER SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA AND ER.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 22. R&R SUPPORT PER SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 500, RBL 22. R&R WEB IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER EA & ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER EA & ER.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

SEAT TRACK CORRODED BETWEEN BS 663 TO BS 727+10, LBL 45. R&R TRACK IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

AT AFT CARGO FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 500 TO BS 500A, RBL 22. R&R SHIELD IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

CABIN FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA AND ER.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

FORWARD CARGO GUSSET PLATE CRACKED AT BS 500D, STR 19R. R&R GUSSET PLATE PER SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

AFT CARGO BAY AFT SHIELD BETWEEN BS 847 TO BS 867, RBL 20. R&R SHIELD IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

FLOOR RAIL AT AFT CARGO BAY CORRODED AT BS 767+5, RBL 3. REPAIRED FLOORBEAM PER SRM & EA.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

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

Part: SUPPORT STRAP — DAMAGED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

INTERCOSTAL SUPPORT STRAP HAD CHAFING DAMAGE AT BS 292, STR 5R. REPAIRED STRAP IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

AFT CARGO BAY FLOOR RAIL CORRODED AT BS 767+5, RBL 14. REPAIRED RAIL PER SRM & EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

CABIN FRAME HAD CHAFING DAMAGE AT BS 360, STR 8R. REPAIRED FRAME IAW SRM.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

CABIN FLOOR PANEL SUPPORT CRACKED; BS 540; LBL 1 TO LBL 23 / REMOVED CABIN FLOOR PANEL SUPPORT BS 540 LBL 1 TO LBL 23 PER SRM 51-40-02-0G-0 STEP 7 (C) 57006U 16JAN19 LEAD113 10JAN19 REPLACED FLOOR PANEL SUPPORT BS 540; LBL 1 TO LBL 23 IAW SRM 51-40-02-0G-0 AND DWG 143A0060 59205U 17JAN19

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

INTERCOSTAL CRACKED BETWEEN BS 400 TO BS 380, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

FRAME RADIUS CRACKED AT BS 313, STR 5L. REPAIRED FRAME IAW ER AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 1. R&R INTERCOSTAL PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

INTERCOSTAL CRACKED AT BS 927+6, BL 0. R&R INTERCOSTAL PER DWG AND SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 35. R&R INTERCOSTAL PER DWG AND SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 47. R&R INTERCOSTAL PER DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

R1 DOOR SCUFF PLATE INBOARD SUPPORT CORRODED BETWEEN BS 294.5 TO BS 328, RBL 60. R&R SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294.5, BL 0. R&R INTERCOSTAL PER DWG AND SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 787+7 TO BS 847, RBL 22. R&R WEB PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,286 hrs · 20,571 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 12. R&R INTERCOSTAL PER SRM AND DWG.

Part: FLOOR PANEL — BROKEN (AFT CABIN) · airframe 40,286 hrs · 20,571 cycles

AFT CABIN FLOOR PANEL 242XF BROKEN / DAMAGED FLOOR PANEL 242XF WAS REPLACED WITH A SERVICEABLE PART IAW SRM 51-10-02-0G-0 PAR. 9

Part: RETAINER — CRACKED (RIGHT WING) · airframe 40,286 hrs · 20,571 cycles

RT WING BULB SEAL RETAINER ABOVE #2 PYLON AFT TIP IS CRACKED / REMOVED AND REPLACED RT WING BULB SEAL RETAINER ABOVE #2 PYLON AFT TIP IAW SRM 51-40-02-0G-0 AND IPC 57-50-00-25 2234U 14JAN19

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 40,286 hrs · 20,571 cycles

RT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STA 120.3, LOWER END OF THE 2ND VERTICAL STIFFENER FROM THE FRONT. REPAIRED RIB IAW SRM & DWG.

Part: FLOOR PANEL — CRACKED (AFT CABIN) · airframe 40,286 hrs · 20,571 cycles

AFT CABIN FLOOR PANEL 241AEF HAS CRACK ON LOWER SKIN I/B END / AFT CABIN FLOOR PANEL 241AEF WITH CRACK ON LOWER SKIN I/B END WAS REPAIRED IAW SRM 53-00-50-2R-1; SRM 53-00-50-2R-2. AND DWG 147A5810-251. 57543U 03.JAN.19.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 40,286 hrs · 20,571 cycles

RUDDER COUNTER BALANCE WEIGHT IS CORRODED / REMOVED AND REPLACED THE RUDDER COUNTER BALANCE WEIGHT PER CMM 54-40-09 STEPS 3C(3)(A)(B)1);6)&7) AND SRM 51-60-07-0G-0 PG 6 OF 41 STEP C2)D) FOR PROPER TORQUE.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 40,286 hrs · 20,571 cycles

RT WING ATTACH ANGLE CRACKED ABOVE NR 2 PYLON AFT TIP. R&R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CRACKED (FAIRING) · airframe 40,286 hrs · 20,571 cycles

LT WING INBOARD LEADING EDGE MOST INBOARD WING TO BODY FAIRING SUPPORT ANGLE CRACKED ON THE UPPER END. R&R ANGLE IAW SRM AND DWG.

Part: RETAINER — CRACKED (LEFT WING) · airframe 40,286 hrs · 20,571 cycles

LT WING BULB SEAL RETAINER ABOVE #1 PYLON AFT TIP IS CRACKED / REMOVED AND REPLACED LT WING BULB SEAL RETAINER ABOVE #1 PYLON AFT TIP IAW SRM 51-40-02-0G-0 AND IPC 57-50-00-25 2234U 16JAN19

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 40,286 hrs · 20,571 cycles

RT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STAB STA 120.3, LOWER END OF THE 3RD VERTICAL STIFFENER FROM THE FRONT. REPAIRED RIB PER SRM.

Part: BULKHEAD — PEELING (LT MLG WW) · airframe 40,286 hrs · 20,571 cycles

LOWER COMPOSITE BULKHEAD HAD A PREVIOUS REPAIR PEELING UP AT BS 663, LBL 40. REPAIRED BULKHEAD IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 40,286 hrs · 20,571 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 41. REPAIRED WEB PER SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 40,286 hrs · 20,571 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS 665, LBL 30. REPAIRED WEB PER REF SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,984 hrs · 20,380 cycles

R2 DOOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: WINDOW — ARCED (COCKPIT) · airframe 39,969 hrs · 20,366 cycles

FIRST OFFICER'S FORWARD WINDSCREEN (R1) ARCED. R&R R1 WINDOW PER MM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 39,498 hrs · 20,067 cycles

R1 DOOR EMERGENCY EXIT SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 38,631 hrs · 19,523 cycles

L2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CASE, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,352 hrs · 19,328 cycles

LT EMERGENCY EXIT WALL LAMP INOP. R&R LAMP IAW AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 38,245 hrs · 19,259 cycles

L1 DOOR EMERGENCY EXIT SIGN COVER MISSING. R&R SIGN ASSEMBLY IAW AMM.

Part: SHIELD — BROKEN (FLASHLIGHT) · airframe 36,052 hrs · 17,869 cycles

AFT FLASHLIGHT SHIELD BROKEN. R&R SHIELD PER SIP.

Part: SIGN — BROKEN (CABIN) · airframe 35,914 hrs · 17,788 cycles

RT OVERWING EXIT SIGN BROKEN. R&R SIGN PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 34,504 hrs · 16,918 cycles

R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT & AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,928 hrs · 16,593 cycles

LEFT AFT EMERGENCY EXTERIOR LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 33,634 hrs · 16,419 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED ON VERTICAL STIFFENER HSS 120.30, SECOND RIB FROM FRONT SPAR. REPAIRED THE RIB IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 33,634 hrs · 16,419 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED ON VERTICAL STIFFENER HSS 120.30, THIRD RIB FROM FRONT SPAR. REPAIRED THE RIB IAW SRM.

Part: STRAP — CORRODED (ESCAPE HATCH) · airframe 33,634 hrs · 16,419 cycles

RIGHT EMERGENCY EXIT HATCH ESCAPE STRAP ANCHOR HOOK CORRODED. R & R STRAP IAW AMM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 33,441 hrs · 16,306 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 33,441 hrs · 16,306 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 33,363 hrs · 16,256 cycles

L1 DOOR EMERGENCY EVAC SLIDE BOTTLE PRESSURE LOW. R&R SLIDE ASSEMBLY PER MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 33,258 hrs · 16,199 cycles

R1 DOOR SLIDE ASSY OUT OF ADJUST. ADJUSTED THE SLIDE ASSY IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 26,319 hrs · 12,133 cycles

AFT CARGO COMPARTMENT RT Z ANGLE CRACKED AT BS 794.3. R & R Z ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,319 hrs · 12,133 cycles

AFT CARGO COMPARTMENT Z ANGLE CORRODED BETWEEN BS 727E TO 767, RT SIDE. R & R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,319 hrs · 12,133 cycles

AFT CARGO COMPARTMENT Z ANGLE CORRODED BETWEEN BS 727A TO 727B, LT SIDE. REPAIRED Z ANGLE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 26,319 hrs · 12,133 cycles

AFT CARGO COMPARTMENT THRESHOLD SUPPORT WEB CORRODED BETWEEN BS 847 TO 794.3, STRINGER 25R. R & R WEB IAW SRM & DWG.

Part: SIGN — BROKEN (CABIN) · airframe 26,137 hrs · 12,024 cycles

R1 DOOR EMER EXIT SIGN LIGHT BROKEN. R & R SIGN IAW MM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 23,023 hrs · 10,291 cycles

RT HORIZONTAL STABILIZER SKIN CUTOUT AT STATION 92.70 RIB 1ST & 2ND VERTICAL STIFFENERS CRACKED. REPAIRED RIB ASSEMBLY IAW SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 23,023 hrs · 10,291 cycles

AFT CARGO BAY FLOOR PANEL 140BF CORRODED AROUND THE EDGES. R & R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 23,023 hrs · 10,291 cycles

AFT CARGO BAY FLOOR PANEL 140DF CORRODED AROUND THE EDGES. R & R PANEL IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 23,023 hrs · 10,291 cycles

STRINGER CORRODED BETWEEN BS 1064 TO BS 1088, STRINGER 25R. REPAIRED STRINGER IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 23,023 hrs · 10,291 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727D TO BS 792. R & R SUPPORT IAW SRM & DRAWING.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 23,023 hrs · 10,291 cycles

AFT CARGO BAY REPAIR ANGLE CORRODED BETWEEN BS 787 TO BS 792, RBL 13.8. REPAIRED ANGLE IAW EA.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 23,023 hrs · 10,291 cycles

CABIN FLOOR PANEL NR 221BF OTBD AFT CORNER BROKEN. REPAIRED PANEL IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 23,023 hrs · 10,291 cycles

MAIN WW VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 43. R & R WEB IAW SRM.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 23,023 hrs · 10,291 cycles

FLOOR PANEL 222BF DAMAGED AT INSERT UPPER RT CORNER. REPAIRED PANEL IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,023 hrs · 10,291 cycles

EXTERNAL POWER DOOR CUTOUT AFT SIDE OF CUTOUT CRACKED. REPAIRED CUTOUT IAW EA.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 23,023 hrs · 10,291 cycles

AFT CARGO BAY FLOOR PANEL 140AF CORRODED AROUND THE EDGES. R & R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 23,023 hrs · 10,291 cycles

FWD CARGO BAY FLOOR PANEL 120CF CORRODED AROUND THE EDGES. R & R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 23,023 hrs · 10,291 cycles

FWD CARGO BAY FLOOR PANEL 120BF CORRODED. R & R PANEL IAW SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 23,023 hrs · 10,291 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MM.