N242WN

Part: MEGAPHONE — LOOSE (ZONE 200) · airframe 64,534 hrs · 38,729 cycles

FWD MEGAPHONE HANDLE LOOSE. REPLACED FWD MEGAPHONE IAW AMM 25-64-00. OPS OK.

Part: RIVET — BROKEN (GIRT BAR) · airframe 63,743 hrs · 38,185 cycles

DOOR R1 SLIDE COVER GIRT BAR HOOK HAS A BROKEN RIVET<[01] COMPLIED WITH EA M-23-125-01839

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 62,836 hrs · 37,628 cycles

RIGHT OVERWING EXIT LIGHT INOP<[01] REMOVED AND REPLACED RIGHT OVERWING EXIT LAMP PER AMM 33-51-01

Part: LENS — MISSING (ZONE 200) · airframe 61,536 hrs · 36,862 cycles

EMERGENCY OVER WING EXIT LIGHT COVER MISSING ON CO PILOT SIDE.<[01] REINSTALLED RH OVER WING EXIT EMERGENCY LIGHT LENS PER AMM 33-51-01

Part: HANDLE — LOOSE (DOOR ASSIST) · airframe 61,295 hrs · 36,708 cycles

L1 DOOR UPPER DOOR ASSIST HANDLE LOOSE<[01] TIGHTENED L1 DOOR HANDLE IAW AMM 25-21-31.

Part: HANDLE — LOOSE (DOOR ASSIST) · airframe 61,295 hrs · 36,708 cycles

R1 DOOR ASSIST HANDLE LOOSE<[01] TIGHTENED R1 DOOR ASSIST HANDLE IAW AMM 25-21-31.

Part: GIRT BAR — LOOSE (ZN 800 DOOR) · airframe 61,068 hrs · 36,564 cycles

FORWARD SERVICE DOOR SLIDE MOUNTED FORWARD GIRT BAR RETAINER CLIP FASTENERS ARE LOOSE.<[01] REMOVED AND REPLACED FASTENERS ON FWD GIRT BAR RETAINER CLIP PER SRM 51-40-02

Part: SLIDE — DISLODGED (ZONE 800) · airframe 60,486 hrs · 36,200 cycles

SLIDE FELL FROM CONTAINER. FRONT CAPTAIN SIDE SLIDE FELL FROM CONTAINER. FRONT CAPTAIN SIDE<[01] REINSTALLED FWD ENTRY SIDE PER MT 725-61-06

Part: ISOLATOR — CRACKED (ZN 800 DOOR) · airframe 60,188 hrs · 36,019 cycles

FWD GALLEY SERVICE DOOR AFT SLIDE MOUNT ISOLATOR CRACKED<[01] REMOVED AND REPLACED ISOLATOR PER SRM 51-40-02;[02] C/W INSP

Part: PANEL — CRACKED (MLG WW) · airframe 60,153 hrs · 35,997 cycles

RIGHT MLG; UPPER I/B SUPPORT PANEL CRACKED AT FWD ATTACHMENT BRACKET.<[01] REMOVED AND REPLACED BRACKET PER. SRM REF. 51-40-02.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 58,925 hrs · 35,263 cycles

BOTH FWD GALLEY EMERGENCY FLASH LIGHT BATTERIES NEED REPLACEMENT.<[01] REMOVED AND REPLACED BOTH FWD GALLEY EMERGENCY FLASHLIGHT BATTERIES REF AMM 25-64-00. NEW EXPIRATION DATE MAR 2026.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,836 hrs · 35,208 cycles

EXT. RH O/W EXIT EMERG LIGHT INOP<[01] REPLACED LAMP FOR RH OVERWING/SLIDE LIGHT AND PERFORMED GOOD TEST PER AMM 33-51-04-960-801.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,836 hrs · 35,208 cycles

EMERGENCY EXIT LOCATORS ON LEFT AND RIGHT OWE HAVE INOP BULBS FWD LOCATOR ON L/H OWE HAS 2 INOP AFT LOCATOR ON R/H OWE HAS 2 INOP<[01] RELAMPED EMERGENCY EXIT LOCATORS ON LEFT AND RIGHT OWE; PERFORMED GOOS TEST PER AMM 33-51-01-960-801; TASK CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 58,836 hrs · 35,208 cycles

ACB AFT CORNER SCUFF PLATE CRACKED<[01] SCUFF PLATE REMOVED IAW AMM 53-11-02-020-801<BR>SCUFF PLATE REPAIRED IAW BAC5975 - REF STEP 2<BR>CORNER SCUFF PLATE INSTALLED ON BAR CODE TTG8Q00RN1RP;[02] VERIFIED.

Part: BAFFLE — CRACKED (BS 460 LBL 23) · airframe 58,836 hrs · 35,208 cycles

REJECT - INTERCOSTAL CRACKED AT FASTENER ATTACHMENT WITH SIDEWALL SUPPORT FCB BS 460 LBL23 WL156. MARKED. PIC ATTACHED.<[01] REMOVED AND INSTALLED NEW BAFFLE P/N 143A7510-9 LOT#1555679-1 PO#963418/1 AT LBL 23 WL 156 BS 440- TO BS 460 IAW SRM 51-40-02 AND DWG 143A7505 REV:-;[02] VERIFIED ALL STEPS AND CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: WEB — CORRODED (BS 787-794 RBL25) · airframe 58,836 hrs · 35,208 cycles

ACB WEB(146A8322-11) HAS CORROSION AT BS 787 - BS794 RBL 25 WL 160<[01] REMOVED AND REPLACED ACB WEB(146A8322-11) AT BS 787 - BS794 RBL 25 WL 160 IAW SRM 51-40-02 AND DWG 146A8320.

Part: ANGLE — CRACKED (BS 787-794 RBL21) · airframe 58,836 hrs · 35,208 cycles

ANGLE(146A8125-52) AT BS787 - BS794 HAS CRACK AT FASTENER HOLE RBL 21 WL 157<[01] REMOVED AND REPLACED ANGLE(146A8125-52) AT BS787 - BS794 RBL 21 WL 157 IAW SRM 51-40-02-0G-0. DWG 146A0081. DWG 146A8123.;[02] VERIFIED RII CORRECTIVE ACTION ITEM 1.;[03] MEASUREMENTS TABLE OK; CARD COMPLETE.

Part: BAFFLE — CRACKED (BS 500-500A) · airframe 58,836 hrs · 35,208 cycles

FCB BAFFLE CRACKED AT FASTENER HOLE BS 500 - BS 500A LBL 25 WL 156<[01] VERIFIED INSTALLATION OF BAFFLE.;[02] REMOVED AND INSTALLED NEW BAFFLE P/N 143A7510-15 LOT#1555332-1 PO#962911/1 AT LBL 25 WL 156 BS 500 TO BS 500A IAW SRM 51-40-02;143A7510 REV:B AND DWG 143A7505 REV:-.

Part: ANGLE — CRACKED (BS 767-787) · airframe 58,836 hrs · 35,208 cycles

ANGLE(146A8125-53) AT BS767+2 - BS787 HAS CRACK AT FASTENER HOLE RBL 21 WL 157<[01] REMOVED AND REPLACED ANGLE(146A8125-53) AT BS767+2 - BS787 RBL 21 WL 157 IAW SRM 51-40-02 AND DWG 146A0081. DWG 146A8123.;[02] VERIFIED CORRECTIVE ACTION ITEM 1;MEASUREMENTS TABLE OK; CARD COMPLETE.

Part: WEB — CORRODED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

FWD CGO DOOR CUTOUT; CORROSION ON SUBTHRESHOLD BS440+31; RBL28; WL156<[01] VERIFIED STEP 1 COMPLETE.;[02] COMPLETED MEASUREMENT TABLE.;[03] REMOVED CORROSION FROM THRESHOLD WEB AND FOUND OUT OF LIMITS; IAW SRM 53-30-15-1A-1; AND INSTALLED NEW WEB P/N 143A8122-10; LOT # 1538599-1; IAW SRM 51-40-02-0G-0 AND DWG. 143A8330.;[04] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.

Part: COWL DOOR — CRACKED (NR 1 NACELLE) · airframe 58,836 hrs · 35,208 cycles

#1 ENGINE I/B FAN COWL OIL ACCESS DOOR CLOSE OUT FRAME IS CRACKED.<[01] REMOVE AND REPLACE #1 ENGINE I/B FAN COWL OIL ACCESS DOOR CLOSE OUT FRAME PER. SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE

Part: WEB — INCORRECT (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

FWD CGO DOOR CUTOUT; SUBTHRESHOLD FASTENER NOT SEATED AND WORKING OUT; BS440+30; RBL28; WL156<[01] SUB THRESHOLD WEB TO BE REPLACED ON FAULT TTG8Q00RNSDT<BR>TASK COMPLETE;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED ACB FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1. PART IS TO BE INSTALLED ON CUSTOMER CARD TTG8Q00RN1RP

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

DURING REMOVAL R/H VAPOR BARRIER FOUND CRACKED ANGLE P/N 276A9183-2 BS 663 BETWEEN RBL 45- RBL 54<[01] REMOVED AND REPLACED BRACKET P/N 276A9183-2 IAW SRM 51-40-092 AND DWG 111A1001 REV.-;[02] REMOVED AND REPLACED BRACKET P/N 276A9183-2 IAW SRM 51-40-02 AND DWG 111A1001 REV.-;[03] VERIFIED CORRECTIVE ACTION ITEM 2; MEASUREMENTS TABLE OK; CARD COMPLETE.

Part: FLOOR PANEL — TORN (NOT REPORTED) · airframe 58,836 hrs · 35,208 cycles

AFT FLOOR PANEL 242VF AFT R/H CORNER TORN<[01] AFT FLOOR PANEL 242VF WITH AFT R/H CORNER TORN WAS REPAIRED IAW SRM 53-00-50-2R-6.;[02] VERIFIED CORRECTIVE ACTION 1

Part: SKIN — CORRODED (BS 1016 CROWN) · airframe 58,836 hrs · 35,208 cycles

CORROSION ON FUSELAGE CROWN SKIN COMMON TO FASTENER LOCATIONS FROM STA 1016+2; TO STA 1016+23; BUTT LINE 8 TO 13; LEFT AND RIGHT.<[01] CERTIFIED APPLICABILITY OF SRM 53-00-01-1A-1;[02] ' AS PER EA 24-153-00521; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.';[03] VERIFIED CORRECTIVE ACTION 2

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 58,836 hrs · 35,208 cycles

MULTIPLES CRACKS ON PANEL 211A (MARKED)<[01] UPON INVESTIGATION FOUND COCKPIT PANEL 211A IS ACTUALLY 212B. FOUND ONE CRACK ON PANEL 212B; REPAIRED PANEL 212B PER CMM 25-00-66 REPAIR 3-1 PARAGRAPH 4 APPLIED FIBERGLASS AT 10:30 AM;[02] VERIFIED 24HR CURE OF FIBERGLASS REPAIR TO PANEL 212B IAW CMM 25-00-66 REPAIR 3-1 PARAGRAPH 4 AND REPLACED RIVET IN REPAIRED AREA IAW SRM 51-40-02-0G-0;[03] VERIFIED ITEMS 1 AND2

Part: SUPPORT — CORRODED (BS 460-500C) · airframe 58,836 hrs · 35,208 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS460 - BS500C LBL23 WL156.<[01] VERIFIED STEP 15 IN PARTIAL.;[02] VERIFIED STEP 16 COMPLETE.;[03] REJECT - INSTALLATION OF SIDEWALL SUPPORT; FOUND CRACK AT INTERCOSTAL FASTENER ATTACHMENT POINT; BS460; WL156; LBL23 TTG8Q00RT568;[04] 02 - INSPECTED PER [SRM 51-10-02-0G-0-A00248 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)];[05] TASK COMPLETE

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

AFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON AFT FLOOR PANEL 241ADF UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

FWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] REPAIRED AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 221CF IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 58,836 hrs · 35,208 cycles

FWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222DF WITH UPPER SKIN PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BAC DWG 141A5810 ID:185.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: PANEL — CRACKED (ZONE 100) · airframe 58,836 hrs · 35,208 cycles

MULTIPLES CRACKS ON PANEL 211B (MARKED)<[01] REMOVED AND REPLACED PANEL 211B PER SOPM 20-50-01.;[02] UPDATED MEASUREMENT TABLE.;[03] VERIFIED.

Part: FLOOR PANEL — PULLED (FWD CABIN) · airframe 58,836 hrs · 35,208 cycles

FWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222BF 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] JOB COMPLETE.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL157.<[01] REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BETWEEN BS 727+4' TO BS 767; RBL 21; WL 157 PER 51-40-02 AND DWG:146A7500.;[02] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE;

Part: SHIELD — CORRODED (BS 787 RBL 21) · airframe 58,836 hrs · 35,208 cycles

CORROSION ON FWD SHIELD AT ACB BS767 - BS787 RBL21 WL157.<[01] REMOVED AND REPLACED FWD SHIELD AT ACB BS767 - BS787 RBL21 WL157 IAW SRM 51-40-02 AND DWG 146A0081;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE

Part: SUPPORT ANGLE — CRACKED (BS 914 RBL11) · airframe 58,836 hrs · 35,208 cycles

CRACKED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS914 RBL11 WL170.<[01] REMOVED AND REPLACED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS914 WL170 IAW BOEING DWG 147A7221; SRM 51-40-05 AND SRM 51-40-02.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE

Part: FLOOR PANEL — PULLED (ZONE 100) · airframe 58,836 hrs · 35,208 cycles

FWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 221EF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — PULLED (FWD CABIN) · airframe 58,836 hrs · 35,208 cycles

FWD FLOOR PANEL 231BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FLOOR PANEL 231BF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1

Part: SUPPORT ANGLE — CRACKED (BS 918 RBL11) · airframe 58,836 hrs · 35,208 cycles

CRACKED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS918 RBL11 WL170.<[01] REMOVED AND REPLACED SUPPORT ANGLE BEHIND WATER SERVICE PANEL BS918 WL 170 IAW BOEING DWG; SRM 51-40-02 AND 51-40-05.;[02] REMOVED AND REPLACED SUPPORT ANGLE BEHIND WATER SERVICE PANEL BS918 WL 170 IAW BOEING DWG 147A7221; SRM 51-40-02 AND 51-40-05.;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENT TABLE

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS809 LBL21 WL157.<[01] REMOVED AND REPLACED SIDEWALL SUPPORT LH FROM BS 727+4 TO BS 847; LBL 21; WL 157; IAW SRM 51-40-02-0G-0 AND DWG 146A7500; ID: 0085; REV: A;[02] VERIFIED ALL STEPS; ALL STEPS AND CARD COMPLETE.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

AFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PULLED STRANDS ON AFT FLOOR PANEL 241XF UPPER SKIN HAVE BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

AFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ACF UPPER AND LOWER SKIN DAMAGED AREAS HAVE BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED REPAIR OF FLOOR PANEL 241ACF PER SRM 53-00-50-2R-1.;[03] WORKSCOPE IS COMPLETE.

Part: SHIELD — CORRODED (BS 767 RBL 23) · airframe 58,836 hrs · 35,208 cycles

CORROSION ON FWD SHIELD FWD ATTACH TAB AT ACB BS767 RBL23 WL157.<[01] REMOVED AND REPLACED FWD SHIELD FWD ATTACH TAB AT ACB BS767 RBL23 WL157 IAW SRM 51-40-02 AND DWG 146A0081;[02] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE;

Part: FLOOR PANEL — PULLED (FWD CABIN) · airframe 58,836 hrs · 35,208 cycles

FWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF 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] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (NOT REPORTED) · airframe 58,836 hrs · 35,208 cycles

FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR 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.;[02] JOB COMPLETE.

Part: NUT PLATE — CORRODED (BS 727D BL 0) · airframe 58,836 hrs · 35,208 cycles

CORROSION ON NUTPLATES AT ACB BS727D BL0 WL150.<[01] CUMPLETED STEP 1;[02] TASK CARD COMPLETED;[03] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.

Part: FLOOR SUPPORT — CRACKED (BS 344 BL 0) · airframe 58,836 hrs · 35,208 cycles

FWD WET AREA - CRACK ON INTERCOSTAL BS 344+9 BL 0 WL 208 (MARKED)<[01] UPDATED STEPS;[02] UPDATED MEASUREMENT TABLE;[03] SUMMARY; THE CRACKED INTERCOSTAL AT BS 344 BL0 WAS REMOVED AND REPLACED IAW SRM 51-10-02-0G-0 STEP 9 A (1) (2).;[04] REJECT: IMPROPERLY INSTALLATION 2E/A FASTENERS ON INTERCOSTAL STA-344 TO 360 BL-0 (MARKED WITH RED TAPE) [TTG8Q00RP6L4];[05] 2 EA IMPROPERLY INSTALLED FASTNERES REPLACED ON FAULT TTG8Q00RP6L4.;[06] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: FLOOR PANEL — PULLED (FWD CABIN) · airframe 58,836 hrs · 35,208 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] JOB COMPLETE.

Part: FLOOR SUPPORT — CRACKED (BS 277 BL0) · airframe 58,836 hrs · 35,208 cycles

FWD WET AREA - CRACK ON INTERCOSTAL BS 277+7.5 BL 0 WL 208 (MARKED<[01] UPDATED STEPS;[02] UPDATED STEP;[03] UPDATED MEASUREMENT TABLE;[04] VERIFIED STEPS 1;2;3;4; COMPLETE; STEP 5 IN PARTIAL.;[05] STEP #5 COMPLETE;[06] CUSTOMER CARD COMPLETE AND VERIFIED MEASUREMENT TABLE

Part: CARGO TRACK — CORRODED (BS 436-500 LBL18) · airframe 58,836 hrs · 35,208 cycles

CORROSION ON TRACK TIEDOWN AT FCB BS436; BS496; BS500 LBL18 WL156.<[01] REMOVED AND REPLACED TIEDOWN TRACK AT FCB BS 396 TO BS 500D LBL 18 WL 156 IAW BOEING DWG 143A7500 AND SRM 51-40-02;[02] 02 - INSPECTED PER [SRM 53-00-53-1A-2-A00028 (PERMANENT (NON-DENT DAMAGE TYPES))];[03] 02 - INSPECTED PER [SRM 53-00-53-1A-2-A00028 (PERMANENT (NON-DENT DAMAGE TYPES))] VERIFIED STEP 4

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

AFT FLOOR PANEL 241ABFF UPPER SKIN HAS AREAS OF PULLED STRANDS. PANEL SHOULD BE 241ABF<[01] AREAS OF PULLED STRANDS ON FLOOR PANEL 241ABF WERE REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>DOWNLOADED CURE SHEETS AND TAPE.;[02] VERIFIED FLOOR PANEL 241ABF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[03] WORKSCOPE IS COMPLETE

Part: INTERCOSTAL — CORRODED (BS 294) · airframe 58,836 hrs · 35,208 cycles

FWD WET AREA - CORROSION ON INTERCOSTAL LBL 11 BS 294.5+5; BS 294.5+8; BS 294.5 +14.5 WL 208 (MARKED)<[01] UPDATED STEP 1.;[02] CORRECTED MEASURMENT;[03] STEPS 4;5 COMPLETE;[04] REMOVED AND REPLACED INTERCOSTAL AT LBL 11; BS 294.5 TO BS 312 PER SRM 51-40-02-0G-0 AND BOEING DWG 141A5600.;[05] VERIFIED CORRECTIVE ACTION 4.<BR>JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1

Part: FLOOR PANEL — PULLED (CABIN) · airframe 58,836 hrs · 35,208 cycles

FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BAC DWG 141A5810 ID: 245.;[02] INFORMATION ENTERED ON ITEM 1 WAS ENTERED IN ERROR. THIS IS AN INSPECTOR BLOCK.;[03] FWD FLOOR PANEL 222CF UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BAC DWG 141A5810 ID: 245.;[04] VERIFIED FLOOR PANEL 222CF UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BAC DWG 141A5810 ID: 245

Part: FLOOR PANEL — PULLED (FWD CABIN) · airframe 58,836 hrs · 35,208 cycles

FWD FLOOR PANEL 231AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 231AF 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] JOB COMPLETE.

Part: SHIELD — CORRODED (BS 500 RBL 23) · airframe 58,836 hrs · 35,208 cycles

CORROSION ON AFT SHIELD AT FCB BS500 RBL23 WL156.<[01] REMOVED AND REPLACED FCB BAY AFT NEW SHIELD P/N 143A8126-31 LOT#1553496-2 PO#960004/2 AT BS 480+15 TO BS 500A RBL 23; WL 156 IAW SRM 51-40-02 AND DWG 143A0080 REV: -;[02] VERIFIED RII CORRECTIVE ACTION ITEM1.;[03] VERIFIED MEASUREMENTS TABLE; CARD COMPLETE.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

AFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ZF UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED REPAIR OF FLOOR PANEL 241ZF UPPER SKIN IAW SRM 53-00-50-2R-1.;[03] WORKSCOPE IS COMPLETE.

Part: FLOOR PANEL — PULLED (AFT) · airframe 58,836 hrs · 35,208 cycles

AFT FLOOR PANEL 242WF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED AFT FLOOR PANEL 242WF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 195.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 100) · airframe 58,836 hrs · 35,208 cycles

FWD FLOOR PANEL 222AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222AF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.

Part: CHANNEL — CORRODED (DOOR SILL) · airframe 58,836 hrs · 35,208 cycles

FWD WET AREA - CORROSION ON MOPSILL RBL 61 FROM BS 312+2.5 TO BS 328+14.5 WL 208 (MARKED)<[01] TASK CARD WAS CORRECTED AND WILL BE ACCOMPLISHED ON TTG8Q00RLLMU.;[02] TASK CARD WAS CORRECTED AND WILL BE ACCOMPLISHED ON TTG8Q00RLL1S;[03] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: CHANNEL — CORRODED (DOOR SILL) · airframe 58,836 hrs · 35,208 cycles

FWD WET AREA - CORROSION ON MOPSILL BS 294.5+10.5 RBL 56; BS 294.5+15 RBL 57; BS 312+3.5 RBL 57.5; BS 328+7 RBL 57.75; BS 312+10 RBL 58; BS 328+11.75 RBL 57.75; WL 208 (MARKED)<[01] UPDATED STEP 1.;[02] CORRECTED MEASUREMENT;[03] REMOVED AND REPLACED FSD MOPSILL PER SRM 51-40-02-0G-0 AND DWG#141A8310;[04] VERIFIED CORRECTION 3.<BR>JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

AFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW AFT FLOOR PANEL 241AAF IAW SRM 53-00-50-2R-0 AND BOEING DWG 147A5810 ID:0008;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

AFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242TF UPPER SKIN AREAS OF PULLED STRANDS WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED REPAIR OF FLOOR PANEL 242TF UPPER SKIN IAW SRM 53-00-50-2R-1.;[03] WORKSCOPE IS COMPLETE.

Part: WEB — CORRODED (BS 1016) · airframe 58,836 hrs · 35,208 cycles

CORROSION ON 1016 WEB AT AFT WET AREA BS1016+13 LBL7 WL208. MARKED<[01] REMOVED CORROSION ON 1016 WEB AT AFT WET AREA BS 1016+13 LBL 7; WL 208 AND REWORKED PER EA 24-153-00486.;[02] TASK CARD COMPLETE

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 58,836 hrs · 35,208 cycles

DURING HFEC INSPECTION OF LH HORIZONTAL STABILIZER LOWER SKIN (TTG8Q00BDWA5); CRACK FOUND AT STA:193.90; 18' FROM FWD EDGE; MEASURED L: 1.0' MARKED<[01] REPAIRED LH HORIZONTAL STABILIZER LOWER INSPAR SKIN AT STA 193.90 18' FROM FWD EDGE IAW SRM 55-10-01-2R-11;[02] VERIFIED TASK COMPLETED

Part: FLOORBEAM — CORRODED (BS 986) · airframe 58,836 hrs · 35,208 cycles

CORROSION ON FLOOR BEAM AT AFT WET AREA BS986 RBL43 WL208. MARKED<[01] CORROSION ON BS 986 FLOOR BEAM AT RBL 43; WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-6.;[02] CORRECTED MEASUREMENT;[03] CUSTOMER CARD COMPLETE AND VERIFIED MEASUREMENT TABLE

Part: STRAP — CORRODED (BS 1016) · airframe 58,836 hrs · 35,208 cycles

CORROSION ON TENSION STRAP AT AFT WET AREA BS1016; BS1016+11; RBL3 WL208. MARKED<[01] CORROSION ON TENSION STRAP AT AFT WET AREA BS 1016+11 RBL 3 WL 208 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED AFT WET AREA TENSION STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5730 REV: C;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE

Part: SKIN — DEBONDED (ZONE 100) · airframe 58,836 hrs · 35,208 cycles

PANEL 194CL OUTER SKIN HAS 2 TIGHTLY GROUPED DISBONDS NEAR CENTER OF PANEL. (MARKED)<[01] PANEL 194CL OUTER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 51-70-05-2R-2.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED PANEL 194CL OUTER SKIN HAS BEEN REPAIRED IAW SRM 51-70-05-2R-2.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 58,836 hrs · 35,208 cycles

CORROSION ON FLOOR BEAM AT AFT WET AREA BS986 LBL43 WL208. MARKED<[01] COMPLETED STEP 8; PARTIAL STEP 9.;[02] COMPLETED STEP 9.;[03] VERIFIED STEPS 11;13 COMPLETE.;[04] REMOVED CORROSION FROM AFT WET AREA FLOOR BEAM BS 986 LBL 43 WL 208 FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ACCOMPLISHED REPAIR OF 986 FLOOR BEAM IAW SRM 53-70-51-2R-6;[05] VERIFIED CORRECTIVE ACTION 4.<BR>JOB COMPLETE.

Part: ANGLE — CRACKED (RT WING) · airframe 58,836 hrs · 35,208 cycles

RIGHT WING FIXED T/E PANEL JUST AFT OF THE PYLON ATTACH ANGLE CRACKED JUST IB OF DEFLECTION RIB. MARKED<[01] REMOVED AND REPLACED RIGHT WING FIXED T/E ATTACH ANGLE JUST AFT OF PYLON AND I/B OF DEFLECTION RIB IAW SRM 51 -40-02-0G-0 PARA. 4.;[02] VERIFIED COMPLETE

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

FLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241EF IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241DF IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0.;[02] ADDITION TO ITEM 1: IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 SHEET:8.;[03] VERIFIED CORRECTIVE ACTION ITEMS 1 AND 2.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

FLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241FF WITH PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0013;[02] VERIFIED FLOOR PANEL 241FF WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0013

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

FLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242CF WITH PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0006;[02] JOB COMPLETE.

Part: PRESSURE DECK — CRACKED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

CRACK FOUND DURING HFEC INSPECTION OF HORIZONTAL PRESSURE DECK WEB (TTG8Q00BCA3K) AT RBL 41 BS663+2. L:0.4IN MARKED<[01] REPAIRED BEADED PRESSURE DECK BETWEEN BS 663.5 TO BS 675; RBL 30 TO RBL 60 WL 202 IAW SRM 53-40-51-2R-2 REPAIR 2. FIGURE 202.;[02] VERIFIED CORRECTIVE ACTION 1.<BR>JOB COMPLETE.

Part: PRESSURE DECK — CRACKED (BS 666, RBL 42) · airframe 58,836 hrs · 35,208 cycles

WHEEL WELL PRESSURE DECK CRACKED; BS666; RBL42; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: INLET — CRACKED (NR 2 NACELLE) · airframe 58,836 hrs · 35,208 cycles

#2 ENGINE INLET COWL OUTER LIP SKIN HAS A CRACKED RIVET HEAD AT THE 10:00 POSITION SPLICE SECOND ONE IN FROM THE AFT SIDE OF LIP SKIN.<[01] UPDATED PARTS;[02] REMOVED AND REPLACED #2 ENGINE INLET COWL IAW 71-11-01-000-802-F00 AND 71-11-01-400-802-F00 STEP 5.H.(1)(3-8) (10-13) (20-22).<BR>T/W ATS1760 DUE DATE: 09/2024; ID: PER2249 DUE DATE: 09/2024 AND BONDING METER ID: ATS1257 DUE DATE: 11/2024.;[03] VERIFIED CORRECTIVE ACTION 2;[04] PERFORMED GOOD LEAK CHECK OF THE #2 ENGINE INLET TAI DUCT PER AMM 81-11-01-400-801-F00 STEP 5H(15)-(17). ALL WORK ACCOMPLISHED.;[05] VERIFIED CORRECTIVE ACTION ITEM 4 COMPLETE.<BR>VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.

Part: PRESSURE DECK — CRACKED (BS 672 RBL41) · airframe 58,836 hrs · 35,208 cycles

WHEEL WELL PRESSURE DECK CRACKED; BS672; RBL41; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: PRESSURE DECK — CRACKED (BS 666, RBL 41) · airframe 58,836 hrs · 35,208 cycles

WHEEL WELL PRESSURE DECK CRACKED; BS666; RBL41; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: PRESSURE DECK — CRACKED (BS 665 RBL 40) · airframe 58,836 hrs · 35,208 cycles

WHEEL WELL PRESSURE DECK CRACKED; BS665; RBL40; WL200<[01] BEADED PRESSURE DECK WEB WILL BE REPAIRED WITH CUSTOMER CARD TTG8Q00RJ75C.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: PRESSURE DECK — CRACKED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

WHEEL WELL PRESSURE DECK CRACKED; BS665; LBL35; WL200<[01] PRESSURE DECK AT BS 665 LBL 35 WL 200 REPAIRED ON FAULT TTG8Q00RJ619. FAULT COMPLETE.;[02] VERIFIED RII ITEMS WERE COMPLETED ON FAULT TTG8Q00RJ619.;[03] VERIFIED COMPLETION ON FAULT TTG8Q00RJ619. CARD COMPLETE.

Part: PRESSURE DECK — CRACKED (ZN 100 FUS LOWER) · airframe 58,836 hrs · 35,208 cycles

CRACK FOUND DURING HFEC INSPECTION OF HORIZONTAL PRESSURE DECK WEB (TTG8Q00BCA3K) AT LBL 34.5 BS663+1.5. L:0.5IN MARKED<[01] REPAIRED HORIZONTAL PRESSURE DECK AT LBL 34.5 BS663+1.5 PER SRM 53-40-51-2R-2 REPAIR 2. FAULT COMPLETE.;[02] VERIFIED ALL RII STEPS ARE COMPETED.

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 58,562 hrs · 35,038 cycles

FWD CARGO FLOOR AFT OF DOOR HAS CRACK IN IT. REPLACED FWD CARGO FLOOR PANEL REF AMM 25-52-10.

Part: TAIL CONE — DELAMINATED (ZN 300 STABILIZE) · airframe 58,076 hrs · 34,712 cycles

TAIL-CONE RH SIDE HAS A DENT MEASURING 10 LONG 2 WIDE AND .106 DEEP. DENT HAS AREAS THAT ARE DELAMINATED.<[01] APPLIED SPEED TAPE TO TAIL CONE RH SIDE AND COMPLIED WITH EA - 23-153-03378.

Part: TAIL CONE — DELAMINATED (ZN 100 FUS LOWER) · airframe 58,076 hrs · 34,712 cycles

TAIL CONE RH SIDE HAS A DENT 12 FWD OF ELEVATOR INDEX PLATE MEASURING 3 LONG 3 WIDE AND .087 DEEP. DENT IS DELAMINATED. DAMAGE IS WITHIN 4 OF PREVIOUS DENT.<[01] C/W EA: 23-153-03381;[02] EDIT STEP 3 TO INDICATE 'YES'

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 58,076 hrs · 34,712 cycles

EMERGENCY LIGHT BATTERY PACKS POS M1675 AND M1674 FAILED CAPACITANCE CHECK<[01] R/R EMERGENCY LIGHT BATTERY PACKS AT POSITIONS M1675 AND M1674 REF AMM 33-51-06.

Part: HANDLE — LOOSE (ZN 200 FUS TOP) · airframe 56,981 hrs · 34,027 cycles

ALL FOUR DOOR LINER ASSIST HANDLES ARE LOOSE.<[01] RESECURED ALL FOUR DOOR LINER ASSIST HANDLE IAW AMM-25-99-99-SWA-001 PAGE 6 STEP B ITEM (C);[02] VERIFIED ITEM 1.<BR>AUDITED.

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 56,981 hrs · 34,027 cycles

DURING DVI INSPECTION FOUND L/H VAPOR BARRIER WEB CRACKED AT STA 663 WL 167 LBL47<[01] EVALUATED DAMAGE; CRACKS ARE REPAIRABLE IAW B737 SRM 57-10-10-2R-2. TAP TEST GOOD; NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 51-70-04-2R-10 PAR 4 STEPS A; B; AND C. <BR><BR>VERIFIED REPAIR MATERIAL IAW B737 SRM 51-70-04-2R-0 TABLE 203: RESIN EY3804AB (A171928); FIBERGLASS CLOTH BMS9-3 (A184337). <BR><BR>REQUIRES OKAY TO BOND.;[02] VERIFIED STEP1 AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM SRM 51-70-04-2R-10 PAR 4 STEPS D THRU G; TAP TEST GOOD; OVEN B0-06 CAL DUE 7/27/23.;[04] VERIFIED STEP 3;[05] OK TO PRIME BOTH FWD AND AFT SIDES OF VAPOR BARRIER;[06] APPLIED PRIMER ON FWD AND AFT SIDES OF VAPOR BARRIER WEB IAW B737 SRM 51-70-04-2R-10 PAR 4.P;[07] VERIFIED STEP 6<BR><BR>OK TO PAINT;[08] APPLIED PAINT ON VAPOR BARRIER WEB IAW B737 SRM 51-70-04-2R-10 PAR 4.P;[09] VERIFIED STEP 8;[10] VERIFIED ALL STEPS ARE COMPLETE;[11] AUDIT C/W

Part: BRACKET — CRACKED (ZN 600 RIGHT WIN) · airframe 56,981 hrs · 34,027 cycles

DOT A24-07 RH WING I/B L/E WING TO BODY FAIRING / L/E SUPPORT STRUCTURE ANGLE CRACKED AT FASTENER HOLE. MARKED<[01] REMOVED CRACKED ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05-0G-0 AND BOEING DWG# 116A3110 ID:0005 REV:B. WORK PERFORMED BY NATHAN JAMES #36937;[02] VERIFIED STEP 1;[03] STARTED INSTALLING NEW ANGLE IAW SRM 51-40-02-0G-0 AND BOEING DWG# 116A3110 ID:0005 REV:B. WORK PERFORMED BY NATHAN JAMES #36937;[04] FINISHED INSTALLING NEW BRACKET I.A.W SRM 51-40-02-0G-0 AND BOEING DWG# 116A3110 REV: B;[05] VERIFIED STEPS 3-4.<BR>OK TO CIC.;[06] APPLIED CIC TO NEW ANGLE BRACKET AT 2:12 PM ON 11 JULY 2023 I.A.W BOEING AMM 51-21-91-620-802;[07] VERIFIED ITEM 6<BR>AUDIT C/W

Part: FLOOR PANEL — DELAMINATED (ZN 200 FUS TOP) · airframe 56,981 hrs · 34,027 cycles

DOT A160-46; FLOOR PANEL 241BF HAS DELAMINATION<[01] WORK ACCOMPLISHED ON NON-ROUTINE TTG8Q00M1DKD

Part: FLOOR PANEL — DELAMINATED (ZN 200 FUS TOP) · airframe 56,981 hrs · 34,027 cycles

DOT A160-44; FLOOR PANEL 231ZF HAS DELAMINATION OF TOP PLYS<[01] WORK ACCOMPLISHED ON NON-ROUTINE TTG8Q00M1D0E

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 56,981 hrs · 34,027 cycles

L/H VAPOR BARRIER UPPER ANGLE IS CRACKED AT STA663 WL 167 AT LBL 10 I/B<[01] ACCOMPLISHED HFEC SURFACE AND OPEN HOLE IAW B737 NDT P6 51-00-00 P16 AND P23 TOOL 44291 DUE 03NOV23 NO CRACKS NOTED;[02] AUDIT C/W

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 56,981 hrs · 34,027 cycles

R/H VAPOR BARRIER UPPER ANGLE HAS CRACK AT STA663 WL 167 AT RBL 45<[01] RECEIVED REPAIR ANGLES FROM BACK SHOP 2024-0 .071 W/O 44942-1000-0004 AND 2024-0 .063 W/O 44942-1000-0001;[02] VERIFIED ITEM 1;[03] ACCOMPLISHED HFEC SURFACE AND OPEN HOLE IAW B737 NDT P6 51-00-00 P16 AND P23 TOOL 44291 DUE 03NOV23 NO CRACKS NOTED;[04] OK TO TREAT AND PRIME;[05] APPLIED ALODINE AND PRIMER TO REPAIR PARTS IAW SRM 51-20-01-0G-0 AMM 51-21-72-370-804;[06] STEP 5 C/W;[07] OK TO INSTALL REPAIR PARTS;[08] OK TO INSTALL REPAIR PARTS IN RII ROLE;[09] VERIFIED ITEM 1 IN RII ROLE;[10] OUT OF SEQUENCE: ACCOMPLISHED DETAILED INSPECTION OF THE REPAIR AREA AND UNDERLYING STRUCTURE NO OTHER DAMAGES FOUND IAW SRM 57-10-10-2R-5 ITEM 4;[11] INSTALLED ALL REPAIR PARTS AT STA 663 R/H IAW SRM 57-10-10-2R-5;[12] WROTE IN ERROR STEP 1<BR>SHOULD BE <BR>RECEIVED -1 AND -2 REPAIR ANGLES FROM BACK SHOP<BR>REPAIR ANGLES BEEN FABRICATED ON W/O 44942-1000-0004 AND W/O 44942-1000-0001;[13] VERIFIED ITEM 10.;[14] VERIFIED ITEMS 11;12;[15] C/W

Part: BULKHEAD WEB — CRACKED (ZN 100 FUS LOWER) · airframe 56,981 hrs · 34,027 cycles

R/H VAPOR BARRIER WEB AT STA 663 HAVE CRACK AT RBL 45 AND RBL 37<[01] EVALUATED DAMAGE; CRACK IS REPAIRABLE IAW B737 SRM 57-10-10-2R-2 REPAIR 2. NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 51-70-04-2R-10 PAR 4 STEPS A; B; AND C. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 51-70-04-2R-0 TABLE 203; RESIN EY3804 (A171928); FIBERGLASS CLOTH BMS9-3 (A184337). <BR><BR>REQUIRES OKAY TO BOND.;[02] VERIFIED STEP 1 ;OKAY TO BOND.;[03] BONDED REPAIR PLIES IAW B737 SRM 51-70-04-2R-10 PAR 4 STEPS D THRU G. TAP TEST GOOD. OVEN B0-06 CAL DUE 7/27/2023.;[04] VERIFIED STEP 3 COMPLETE.;[05] COMPLETED RII OF STEP 3.;[06] VERIFIED ALL STEPS ARE COMPLETE;[07] AUDIT C/W

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 56,635 hrs · 33,803 cycles

R1 DOOR SLIDE UNSEATED FROM HOLDER<[01] INSPECTED R1 DOOR SLIDE; RE-SECURED GIRT BAR INTO RETAINING CLIPS NO DEFECTS NOTED PER AMM 25-66-01.

Part: PANEL — ELONGATED (ZN 100 FUS LOWER) · airframe 56,252 hrs · 33,569 cycles

PANEL 193B HAS SEVERAL ELONGATED HOLES.<[01] REMOVED AND REPLACED WITH NEW PANEL PER AMM 53-51-01.;[02] INSPECTION VERIFIED CORRECTIVE ACTION STEP 1.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 54,464 hrs · 32,448 cycles

FWD ENTRY SLIDE MORE THAN ONE NEEDLE WIDTH INTO THE RED / [01] R&R FWD ENTRY SLIDE PER AMM 25-66-01

Part: SLIDE — LOW (L1 DOOR) · airframe 54,452 hrs · 32,441 cycles

FORWARD ENTRY DOOR SLIDE PRESSURE IN THE RED / [01] INSPECTED SLIDE PRESSURE IAW AMM 25-66-01; FOUND WITHIN LIMITS AT THIS TIME

Part: GIRT BAR — OUT OF POSITION (L2 DOOR) · airframe 53,344 hrs · 31,717 cycles

L2 DOOR SLIDE GIRT BAR NEEDS TO BE REPOSITIONED 2022-129940 / [01] INSTALLED CORRECTLY L2 DOOR SLIDE GIRT BAR IAW B737-700 AMM 25-66-01-000-804;[02] CORRECTED ACTION<BR>INSTALLED CORRECTLY L2 DOOR SLIDE GIRT BAR IAW B737-700 AMM 25-66-01-400-803;[03] INSTALLED CORRECTLY L2 DOOR SLIDE GIRT BAR IAW B737-700 AMM 25-66-01-400-803

Part: GUSSET — CRACKED (FWD CARGO) · airframe 53,344 hrs · 31,717 cycles

CRACK GUSSET LOCATED BS 500D; STRINGER 19L FWD CARGO COMPARTMENT 2022-129817 / [01] REPLACED GUSSET LOCATED BS 500D STRINGER 19L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7902 REV. -; SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED GUSSET LOCATED BS 500D STRINGER 19L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7902 REV. -; SEE INDIVIDUAL SIGNOFF BELOW.RII ACCOMPLISHED

Part: ANGLE — CRACKED (FWD CARGO) · airframe 53,344 hrs · 31,717 cycles

CRACK ANGLE - CLIP LOCATED BS 400; STRINGER 26L FWD CARGO COMPARTMENT 2022-129821 / [01] REPLACED ANGLE - CLIP AND FASTENERS LOCATED BS 400; STRINGER 26L FWD CARGO COMPARTMENT IAW SRM B737-700 51-40-02 AND DRAWING 143A7505 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE - CLIP AND FASTENERS LOCATED BS 400; STRINGER 26L FWD CARGO COMPARTMENT IAW SRM B737-700 51-40-02 AND DRAWING 143A7505 REV:- SEE INDIVIDUAL SIGN OFF BELOW RII

Part: SUPPORT — CRACKED (AFT CARGO) · airframe 53,344 hrs · 31,717 cycles

CRACK ANGLE SUPPORT LOCATED BS867 AND LBL 12-50 AT AFT CARGO COMPARTMENT 2022-129797 / [01] REPLACED SUPPORT LOCATED BS 867 AND LBL 12.50 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 149A8102 REV:-;SEE INDIVIDUAL SIGNOFF BELOW.;[02] CORRECTED STEP 1.<BR>REPLACED ANGLE SUPPORT LOCATED BS 867 AND LBL 12.50 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 149A8102 REV:-;SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPLACED ANGLE SUPPORT LOCATED BS 867 AND LBL 12.50 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 149A8102 REV:-;SEE INDIVIDUAL SIGNOFF BELOW.

Part: SUPPORT — CRACKED (AFT CARGO) · airframe 53,344 hrs · 31,717 cycles

CRACK ANGLE - SUPPORT LOCATED BS 947.5 AND LBL 8.10 AT AFT CARGO COMPARTMENT 2022-129812 / [01] REPLACED ANGLE-SUPPORT AND FASTENERS; AT BS947.5 AND LBL 8.10 ON AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG 149A8103 REV. ?A? SEE SIGN OFFS BELOW.;[02] REPLACED ANGLE-SUPPORT AND FASTENERS; AT BS947.5 AND LBL 8.10 ON AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG 149A8103 REV. ?A? SEE SIGN OFFS BELOW. RII

Part: GUSSET — CRACKED (FWD CARGO) · airframe 53,344 hrs · 31,717 cycles

CRACK GUSSET LOCATED BS 500D; STRINGER 19R FWD CARGO COMPARTMENT 2022-129813 / [01] REPLACED GUSSET LOCATED BS 500D STRINGER 19R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-0-02 ITEM 9 AND DRAWING 143A7902 REV -; SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED GUSSET LOCATED BS 500D STRINGER 19R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-0-02 ITEM 9 AND DRAWING 143A7902 REV -; SEE INDIVIDUAL SIGNOFF BELOW.<BR>RII ACCOMPLISHED

Part: PANEL — CRACKED (L/H WING) · airframe 53,344 hrs · 31,717 cycles

CRACK ACCESS PANEL 561BB TRAILING EDGE ARAUND HOLES LT WING 2022-129777 / [01] TOOL USED: CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 29-SEP-22.;[02] TOOL USED SCALE P/N: CL5000 S/N: AE-409558 DUE DATE: 19-MAY-22.;[03] TOOL USED HOTBONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 16-JAN-23.;[04] TOOL USED P/N FLUKE -87 S/N 193700733 DUE DATE 22SEP 22;[05] TOOL USED MULTIMETER P/N FLUKE -87 S/N 193700733 DUE DATE 22SEP 22;[06] REPAIRED ACCESS PANEL 561BB; LT WING IAW B737-700 SRM 51-70-05-2R-9 REPAIR 9. SEE INDIVIDUAL SIGN OFFS BELOW.;[07] REPAIRED ACCESS PANEL 561BB; LT WING IAW B737-700 SRM 51-70-05-2R-9 REPAIR 9. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: RIB — CRACKED (VERT. STAB.) · airframe 53,344 hrs · 31,717 cycles

CRACK ON RIB #8 ON PANEL 321A DORSAL FIN 2022-129776 / [01] REPLACED RIB #8 AND FASTENERS LOCATED ON PANEL 321A DORSAL FIN IAW B737-700 SRM 51-40-02 AND DWG 174A1008 SHEET 2 REV. C. PART NUMBER USED: 174A1108-2 P.O:2022-128747.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: PANEL — CRACKED (FUSELAGE) · airframe 53,344 hrs · 31,717 cycles

CRACK ACCESS PANEL 194DL WING TO BODY FAIRING AT FUSELAGE EXTERIOR 2022-129778 / [01] TOOL USED CALIPER P/N: 500-464 S/N: 15331926 DUE DATE: 28-SEP-22.;[02] TOOL USED: HOT BONDER P/N:HCS9200B S/N:15102320 DUE DATE: 16-JAN-23;[03] TOOL USED: SCALE P/N:1863T62 S/N:AE-40571 DUE DATE: 19-MAY-22;[04] REPAIRED ACCESS PANEL 194DL WING TO BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. SEE INDIVIDUAL SIGN OFFS BELOW.;[05] REPAIRED ACCESS PANEL 194DL WING TO BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 53,344 hrs · 31,717 cycles

CRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT 2022-129765 / [01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 2000053402; CAL DUE DATE: 23-APR-22<BR>TOOL USED PN ULTRASONIC EQUIPMENT PN: 45MG; SN: 130063701; DUE DATE: 11-MAY-22;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[03] REPAIRED STRINGER 26L LOCATED BTW BS 500D AND BS 540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1 FIGURE 206. SEE INDIVUDUAL SIGNOFF BELOW.;[04] REPAIRED STRINGER 26L LOCATED BTW BS 500D AND BS 540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1 FIGURE 206. RII ;SEE INDIVUDUAL SIGNOFF BELOW.

Part: BRACKET — CRACKED (CENTER WING BOX) · airframe 53,344 hrs · 31,717 cycles

CRACK FLOOR STRUCTURE SUPPORT BRACKET LOCATED STA. 540 AND LBL 0.07 TO LBL 24.82 AT PASSENGER CABIN 2022-129736 / [01] REPLACED FLOOR STRUCTURE SUPPORT BRACKET LOCATED STA. 540 AND LBL 0.07 TO LBL 24.82 AT PASSENGER CABIN I.A.W.B737-700 SRM 51-40-02 AND SRM 51-10-02;SEE INDIVIDUAL SING OFF BELOW.;[02] REPLACED FLOOR STRUCTURE SUPPORT BRACKET LOCATED STA. 540 AND LBL 0.07 TO LBL 24.82 AT PASSENGER CABIN I.A.W.B737-700 SRM 51-40-02 AND SRM 51-10-02;SEE INDIVIDUAL SING OFF BELOW. AS RII

Part: PANEL — ELONGATED (FUSELAGE) · airframe 53,344 hrs · 31,717 cycles

ELONGATED HOLE ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR 2022-129653 / [01] TOOL USED SCALE P/N: CL5000 S/N: AE-409558 DUE DATE: 19-MAY-22.;[02] TOOL USED HOTBONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 16-JAN-23.;[03] TOOL USED FLUKE -87 S/N 193700733 DUE DATE 22 SEP 22;[04] TOOL USED MULTIMETER P/N FLUKE -87 S/N 193700733 DUE DATE 22 SEP 22;[05] TOOL USED CALIPER PN:500-464 ; SN:15331926 DUE DATE 28/SEP/22;[06] REPAIRED ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-05-2R-9 REPAIR 9. SEE INDIVIDUAL SIGN OFFS BELOW.;[07] REPAIRED ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-05-2R-9 REPAIR 9. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: TIE DOWN — CORRODED (AFT CARGO) · airframe 53,344 hrs · 31,717 cycles

CORROSION TIE DOWN LOCATED BS 794.5 AND BS847 AT RBL25.2 AND WL163.56 AT AFT CARGO COMPARTMENT (2 EA) 2022-129594 / [01] REPLACED TIE DOWN 2 E/A LOC BS794.5 AND 847 AT RBL 25.2 WL163.56 AT AFT CARGO COMP I.A.W SRM 51-40-02 B737-700. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700;[02] REPLACED TIE DOWN 2 E/A LOC BS794.5 AND 847 AT RBL 25.2 WL163.56 AT AFT CARGO COMP I.A.W SRM 51-40-02 B737-700. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700

Part: SLAT — CRACKED (R/H WING) · airframe 53,344 hrs · 31,717 cycles

CRACK LOWER SURFACE SLAT 8 ON SLAT STATION 451.97 RT WING 2022-129548 / [01] TOOL USED : EDDY CURRENT TOOL; P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 02 JUN 22.;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 500D; SN:N500X1693P030457; DUE DATE: 02-JUN-22;[03] REPAIRED LOWER SURFACE SLAT 8 ON SLAT STATION 451.97 RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; SEE INDIVIDUAL SIGNOFF BELOW.;[04] 3. JOSUE MARTINEZ (TECHNICIAN); 22-MAR-2022 02:53 UTC <BR>REPAIRED LOWER SURFACE SLAT 8 ON SLAT STATION 451.97 RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; RII .SEE INDIVIDUAL SIGNOFF BELOW

Part: PLATE — CORRODED (AFT CARGO) · airframe 53,344 hrs · 31,717 cycles

CORROSION PLATE LOCATED 794.5 AND RBL25.2 AT WL158.1 AT AFT CARGO COMPARTMENT 2022-129593 / [01] REPLACED PLATE LOC BS 794.5 AND RBL 25.2 AT WL158.1 AT AFT CARGO COMP I.A.W SRM B737-700 51-40-02 AND SRM B737-700 51-10-02 ITEM 9;[02] REPLACED PLATE LOC BS 794.5 AND RBL 25.2 AT WL158.1 AT AFT CARGO COMP I.A.W SRM B737-700 51-40-02 AND SRM B737-700 51-10-02 ITEM 9

Part: FLOOR PANEL — ELONGATED (FUSELAGE) · airframe 53,344 hrs · 31,717 cycles

ELONGATED HOLE FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT 2022-129549 / [01] FABRICATED PANEL 120CF AT AFT CARGO COMPARTMENT I.A.W AMM 25-52-201-801 AND DRAWING# 453A1610 REV:D ; MATERIAL USED P/N:A90RG1W 0.09' P.O#2021233166;[02] FABRICATED PANEL 120CF AT AFT CARGO COMPARTMENT I.A.W AMM 25-52-201-801 AND DRAWING# 453A1610 REV:D ; MATERIAL USED P/N:A90RG1W 0.09' P.O#2021233166

Part: PANEL — CRACKED (AFT CARGO) · airframe 53,344 hrs · 31,717 cycles

CRACK BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT 2022-129552 / [01] REPLACED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 DWG #453A2510 REV.- MATERIAL CONOLITE 0.060? P/N A60SG4W P.O. 2021 214612;[02] CORRECTED STEP 1 <BR>FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 DWG #453A2510 REV.- MATERIAL CONOLITE 0.060? P/N A60SG4W P.O. 2021 214612;[03] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 DWG #453A2510 REV.- MATERIAL CONOLITE 0.060? P/N A60SG4W P.O. 2021 214612<BR>TASK COMPLETED

Part: PIN — LOOSE (L1 DOOR) · airframe 50,171 hrs · 29,886 cycles

F/A REPORTS EMERGENCY SLIDE AT L1 DOOR HAS COTTER PIN LOOSE / PERFORMED MT 725-61-06 REINSTALLED COTTER PIN

Part: ATTACH ANGLE — CRACKED (BS 867) · airframe 48,368 hrs · 28,788 cycles

AFT UPPER CABIN ; CABLE ATTACH CLIP ; AT STA 867 BETWEEN STRINGER 2R AND 3R CRACKED / REMOVED AND REPLACED CLIP AT STA 867 BETWEEN STR 2R AND 3R PER SRM 51-40-02.

Part: RETAINER — CHAFED (LT WING TE) · airframe 48,368 hrs · 28,788 cycles

L/H WING TRAILING EDGE PANEL 551GB BULB SEAL RETAINING BRACKET CHAFFED AND WORN. / REMOVED AND REPLACED L/H WING T/E PANEL 551GB BULB SEAL RETAINING BRACKET REF SOPM 20-50-01.

Part: SKIN SPLICE — CRACKED (RT HORIZ STAB) · airframe 48,368 hrs · 28,788 cycles

RT. HORIZ. STAB SKIN SPLICE (INTERNAL) SS181 HAS 5 HOLES THAT SHOWS CRACK INDICATION PER HFEC MANUAL PART 6 CH51-00-00 PROC. 16. (MARKED) / FABRICATED AND INSTALLED NEW STAB SKIN SPLICE (INTERNAL) PER EA 1-755-4672.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 48,368 hrs · 28,788 cycles

RT. HORIZ. STAB SKIN SS176 AND 2.5 INCHES FWD OF REAR SPAR HAS 1 HOLE THAT SHOWS CRACK INDICATION PER HFEC MANUAL PART 6 CH51-00-00 PROC. 16. (MARKED) / FACT AS A RESULT OF POST REPAIR INSPECTION

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 48,368 hrs · 28,788 cycles

RT. HORIZ. STAB RIB SS184.7 HAS 3 HOLES THAT SHOWS CRACK INDICATION PER HFEC MANUAL PART 6 CH51-00-00 PROC. 16. (MARKED) / REPAIRED IAW EA 1-755-4677

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 48,368 hrs · 28,788 cycles

R/H ELEVATOR UPPER SURFACE HAS MULTIPLE LARGE AREAS OF CRACKED AND BUBBLED PAINT / REMOVED AND REPLACED R/H ELEVATOR ASSY. IAW AMM 27-31-11. SEE WIPS AND SUBTASKS FOR INDIVIDUAL SIGN OFFS. TAG NO: 683848 PN ON: 183A0107-2 SN ON: 001127 PN OFF: SN OFF: 000953

Part: SKIN — DAMAGED (L2 DOOR) · airframe 48,368 hrs · 28,788 cycles

AFT ENTRY DOOR SKIN DAMAGED AROUND UPPER PLUG FOR GUIDE ARM BOLT. / REMOVED AND REPLACED AFT ENTRY DOOR AND ADJUSTED PER AMM 52-13-00. (SEE SUB TASK FOR WORK ACCOMPLISHED) TAG NO: SAM-11 PN ON: 147A6116-30 SN ON: CYC0052 PN OFF: SN OFF: 001976

Part: SKIN — DEFORMED (RT HORIZ STAB) · airframe 48,368 hrs · 28,788 cycles

R/H HORIZONTAL STABILIZER LOWER SKIN IS WAVY AT FIRST BAY O/B OF SKIN MOD DOUBLERS / FACT AS A RESULT OF POST REPAIR INSPECTION

Part: ANGLE — CORRODED (BS 747-767) · airframe 48,368 hrs · 28,788 cycles

R/H TRANSITION ANGLE FROM STA. 747-767 HAS HEAVY CORROSION THOUGHT OUT THE ANGLE THAT HAS BEEN PREVIOUSLY REWORK AND IS OUT OF LIMITS. / E104704-BLANKS; KENNETH - 03/19/2020 22:56 COMPLETE: REMOVED AND REPLACED RH TRANSITION FROM STA. 727-767 PER SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 48,368 hrs · 28,788 cycles

L/H TRANSITION ANGLE FROM STA. 747-867 HAS HEAVY CORROSION THOUGHT OUT THE ANGLE THAT HAS BEEN PREVIOUSLY REWORK AND IS OUT OF LIMITS. / INSTALLED NEW TRANSITION ANGLE FROM STOCK PER SRM 51-40-02.

Part: STRUCTURE — DENTED (COCKPIT) · airframe 48,368 hrs · 28,788 cycles

FLIGHT DECK FLOOR DENT STA 260 LBL 10 / REPAIRED IAW EA 1-A53-33179

Part: FLOORBOARD — PULLED (PAX CABIN) · airframe 48,368 hrs · 28,788 cycles

PASSENGER CABIN FLOORBOARD 242AF DENTED AND MULTIPLE FIBER STRANDS PULLED UP ON UPPER SURFACE / REPLACED PASSENGER CABIN FLOORBOARD 242AF PER AMM 53-21-00.

Part: RIB — DAMAGED (RT HORIZ STAB) · airframe 48,368 hrs · 28,788 cycles

R/H STAB HAS TOOLING DAMAGE AT #1 STIFFENER AT THE #7 RIB LOWER END; STAB STA.147.90.(MARKED) / REPAIRED RH STAB #7 RIB AT #1 STIFFENER PER SRM 55-10-09-2R-4.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 48,368 hrs · 28,788 cycles

R/H STAB HAS A CRACKED #3 STIFFENER AT THE #4 RIB LOWER END; STAB STA.120.3.(VERIFIED BY HFEC PART6; 51-00-00 PROC.23) / REPAIRED RIB PER SRM 55-10-09-2R-4. SEE SUB TASKS AND WIPS FOR DETAILS OF WORK ACCOMPLISHED.

Part: FLOORBOARD — PULLED (PAX CABIN) · airframe 48,368 hrs · 28,788 cycles

PASSENGER CABIN FLOORBOARD 241BF HAS MULTIPLE FIBER STRANDS PULLED UP ON UPPER SURFACE / REMOVED AND REPLACED PASSENGER CABIN FLOORBOARD 241BF PER AMM 53-21-00.

Part: PLATE — DEFORMED (R1 DOORWAY) · airframe 48,368 hrs · 28,788 cycles

FWD SERVICE DOOR THRESHOLD INNER CENTER TRIM PLATE BENT AND DEFORMED / REMOVED AND REPLACED FWD SERVICE DOOR THRESHOLD INNER CENTER TRIM PLATE PER AMM 53-11-01.

Part: SEAT TRACK — DAMAGED (BS 727B-887) · airframe 48,368 hrs · 28,788 cycles

SEAT TRACK #4 FROM STA 727B TO 887 NEEDS TO BE REPLACED DUE TO DAMAGE OUT OF LIMITS. / REMOVED AND REPLACED SEAT TRACK FROM STATION 727B-887 RBL45 PER SRM 51-10-02 AND SRM 51-40-02

Part: ANGLE — CORRODED (AFT CARGO) · airframe 48,368 hrs · 28,788 cycles

L/H AFT CARGO TRANS ANGLE HAS MULTIPLE DAMAGED NUT PLATES. / L/H AFT TRANSITION ANGLE HAD HEAVY CORROSION AND WAS REPLACED WITH NEW FROM STOCK TRANSITION ANGLE ALONG WITH BAD NUTPLATES ON NON ROUTINE #G720829

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 48,368 hrs · 28,788 cycles

#1 SEAT TRACK LOWER LANDING FINISH WORN STA 500C THRU STA 500D. / SEAT TRACK WILL BE REPAIR FROM STA 500C TO STA 520 ON N/R#G720806 DUE TO UPPER CROWN OUT OF LIMITS AT STA520).

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 48,368 hrs · 28,788 cycles

#1 SEAT TRACK UPPER CROWN GOUGED AND DAMAGED AT STA 520. / ACCOMPLISHED SPLICE REPAIR TO #1 SEAT TRACK FROM STA 500C+10 TO STA 520 IAW SRM 53-00-52-2R-4 REPAIR 4 AND EA 1-A53-11779.

Part: PLATE — SHEARED (RT WING) · airframe 48,368 hrs · 28,788 cycles

R/H WING WIGGLE PLATE IS SHEARED AWAY. LOCATED INBD, AND ABOVE #2 PYLONG REMOVABLE FAIRING. / REMOVED AND REPLACED WIGGLE LATE PER SRM. 51-10-02 AND SRM 51-40-02.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 48,368 hrs · 28,788 cycles

AFT CARGO DOOR REQUIRES REPLACEMENT DUE TO DAMAGE OUT OF LIMITS. / REMOVED AND REPLACED AFT CARGO DOOR PER AMM 52-31-00. TAG NO: 652420 PN ON: 146A6110-29 SN ON: 001885 PN OFF: SN OFF: 001973

Part: CLOSEOUT PANEL — BENT (BS 787) · airframe 48,368 hrs · 28,788 cycles

AFT CARGO DOOR CUT-OUT; FWD SIDE STA. 787 RBL23; CLOSEOUT PANEL 142KW; BENT AND DAMAGED. / REMOVED AND REPLACED PANEL PER SRM 51-40-02

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 48,368 hrs · 28,788 cycles

#1 SEAT TRACK LOWER LANDING FINISH WORN STA 500D THRU STA 520. / SEAT TRACK WILL BE REPAIR FROM STA 500C +10 TO STA 520 ON N/R#G720806 DUE TO UPPER CROWN OUT OF LIMITS AT STA520).

Part: STRUCTURE — DENTED (COCKPIT) · airframe 48,368 hrs · 28,788 cycles

FLIGHT COMPARTMENT FLOOR DENTED UNDER FIRST OBSERVERS SEAT. / DUPLICATE WRITE UP ; REFER TO NRC # G721906 FOR CORRECT NRC.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 48,368 hrs · 28,788 cycles

EXTERNAL POWER DOOR CUTOUT DAMAGED ON THE AFT SIDE IN THE MIDDLE. / FABRICATED DOUBLER AND FILLER; INSTALLED PARTS REF SRM 53-10-15-2R-4

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 48,368 hrs · 28,788 cycles

EXTERNAL POWER DOOR CUTOUT DAMAGED IN THE AFT LOWER CORNER. / REPAIRED ON N/R G720414

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,368 hrs · 28,788 cycles

MOD TYPE: 6 NBR: 28564 REV: POS: DURING SI # 12043-53, FOUND SKIN CRACK INDICATION, BS 540, BELOW STRINGER 22R, / SECOND FASTENER FROM THETOP IN THE AFT ROW. / REPAIRED PER EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,896 hrs · 28,478 cycles

CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M1669. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,896 hrs · 28,478 cycles

CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M1674. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,896 hrs · 28,478 cycles

CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M1672. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,896 hrs · 28,478 cycles

CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M1673. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,896 hrs · 28,478 cycles

CABIN EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M1670. R&R BATTERY PACK PER AMM AND DWG.

Part: LIGHT — CRACKED (CABIN) · airframe 46,851 hrs · 27,815 cycles

R/H EGRESS I LUMINESCENT STRIP IN FRONT OF SEAT 1 CRACKED. R&R STRIP IAW AMM.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR) · airframe 45,397 hrs · 26,902 cycles

R1 DOOR ESCAPE SLIDE FABRIC CAUGHT IN GIRT BAR. R&R GIRT BAR PER AMM.

Part: FAIRING — ELONGATED (LWR FUSELAGE) · airframe 44,850 hrs · 26,555 cycles

WING TO BODY PANEL 193B HAS SEVERAL HOLES THAT ARE OVER SIZED/ WORN/ ELONGATED. / REMOVED AND REPLACED 193B PER AMM 53-51-21.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,341 hrs · 25,559 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 42,091 hrs · 24,768 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER AMM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,931 hrs · 24,652 cycles

LEFT HORIZONTAL STABILIZER, HSS 120.30 RIB WAS FOUND CRACKED AT THE SECOND STIFFENER FROM FRONT. R & R THE RIB IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 41,931 hrs · 24,652 cycles

LEFT HORIZONTAL STAB RIB FRONT END FOURTH STIFFENER CRACKED AT HSS 120.30. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 41,931 hrs · 24,652 cycles

LEFT HORIZONTAL STAB RIB FRONT END THIRD STIFFENER CRACKED AT HSS 120.30. REPAIRED THE STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 41,931 hrs · 24,652 cycles

LEFT HORIZONTAL STAB RIB FRONT END THIRD STIFFENER CRACKED AT HSS 92.70. REPAIRED THE STRIFFENER IAW SRM.

Part: DOOR — CRACKED (FWD SERVICE DOOR) · airframe 41,931 hrs · 24,652 cycles

CRACK FOUND AT FWD SERVICE DOOR AT #4 BEAM PARALLEL TO I/B RADIUS / REPLACEMEAT OF FWD SERVICE DOOR #4 BEAM ACCOMPLISHED ON WORK ORDER # 0520055-B6R.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 41,931 hrs · 24,652 cycles

L1 DOOR MOP SILL CRACKED ON VERTICAL FLANGE AT BS 303.9, LBL 58. R&R MOPSILL IAW SRM AND DWG.

Part: SPLICE — CORRODED (AFT CARGO BAY) · airframe 41,931 hrs · 24,652 cycles

CORROSION ON AFT CARGO BAY BS 767+6 FLOOR SPLICE RBL 10 TO LBL10 / CORROSION ON AFT CARGO BAY B.S 767+6 FLOOR SPLICE WAS FOUND OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS RECIEVED NEW PART ON PO# 670176

Part: CREASE BEAM — CORRODED (BS 887-907) · airframe 41,931 hrs · 24,652 cycles

FUSELAGE CREASE BEAM CORRODED AT BS 887 TO 907, STRINGER 17L. R & R THE CREASE BEAM SECTION IAW SRM.

Part: BULKHEAD — CRACKED (AFT CARGO BAY) · airframe 41,931 hrs · 24,652 cycles

LOWER BULKHEAD CLIP IS CRACKED AT BS 947 LBL 20 / REMOVED AND REPLACED LOWER BULKHEAD CLIP BS 947 LBL20 IAW SRM 51-40-02 AND A1PC 53-42-51-03.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,931 hrs · 24,652 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 500D TO 520, BL 0. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (BS 827-847) · airframe 41,931 hrs · 24,652 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 827 TO 847, STRINGER 17R. R & R THE CREASE BEAM WEB IAW SRM AND DWG.

Part: SPLICE — CORRODED (AFT CARGO BAY) · airframe 41,931 hrs · 24,652 cycles

CORROSION ON AFT CARGO BAY BS 887 FLOOR SPLICE RBL 10 TO LBL10 / REMOVED AND REPLACED AFT CARGO BAY BS 887 FLOOR SPLICE ROB10 TO LBL10 IAW SRM 51-40-02 AND A1PC 53-42-11-30

Part: SPLICE — CORRODED (AFT CARGO BAY) · airframe 41,931 hrs · 24,652 cycles

CORROSION ON AFT CARGO BAY BS 727D FLOOR SPLICE RBL 10 TO LBL10 / CORROSION ON THE 727D CARGO BAY FLOOR SPLICE WAS FOUND OUT OF LIMITS DUE TO NO ALLOWABLE SRM LIMITS RECIEVED NEW FLOOR SLPICE ON PO#682471

Part: CREASE BEAM — CORRODED (BS 639-663) · airframe 41,931 hrs · 24,652 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 639 TO 663, RBL 66. R & R THE CREASE BEAM WEB IAW AMM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 380-400) · airframe 41,931 hrs · 24,652 cycles

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

Part: GUSSET — CRACKED (BS 500D) · airframe 41,931 hrs · 24,652 cycles

FORWARD CARGO BAY AFT BULKHEAD GUSSET CRACKED AT BS 500D, STRINGER 19L. R & R THE GUSSET IAW SRM & DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 41,931 hrs · 24,652 cycles

FORWARD CARGO BAY AFT BULKHEAD GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM & DWG.

Part: STRAP — CORRODED (BS 1024-1029) · airframe 41,931 hrs · 24,652 cycles

REINFORCEMENT STRAP CORRODED BETWEEN BS 1024 TO 1029, LBL 3. R & R THE STRAP IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (MAIN CABIN) · airframe 41,931 hrs · 24,652 cycles

CRACKED FLOOR SUPPORT BS 312-328 LBL 47 WL 208. / REMOVED AND INSTALLED NEW FLOOR SUPPORT AT BS 312-328 LBL47 WL208 IAW SRM 51-40-02-OG-0 PAGE 6; SRM 51-40-05-OG-0 AND DWG 141A5400 ID: 0026 REV:-

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 41,931 hrs · 24,652 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 328 TO BS 344, LBL 47. R&R SUPPORT IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,931 hrs · 24,652 cycles

MOP SILL CHORD CLIP ANGLE CRACKED AT BS 294.5, RBL 53. R&R ANGLE IAW SRM AND DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 41,931 hrs · 24,652 cycles

FWD CARGO BAY CENTER SCUFF PLATE IS DENTED AND CRACKED IN MULTIPLE AREAS / REMOVED AND REPLACED FWD CARGO BAY; DENTED AND CRACKED CENTER SCUFF PLATE PER AMM 53-11-02-020-801; AMM 53-11-02-408-801.

Part: SHEAR WEB — CORRODED (BS 1026-1028) · airframe 41,931 hrs · 24,652 cycles

AFT LEFT SHEAR WEB CORRODED BETWEEN BS 1026 TO 1028, LBL 17 TO LBL 28. R & R THE SHEAR WEB IAW SRM & DWG.

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 41,931 hrs · 24,652 cycles

AFT PASSENGER FLOOR PANEL 242UF FWD I/B CORNER IS BROKEN / REPAIRED FWD I/B CORNER PUNCTURE AND DELAMINATION DAMAGE ON AFT PASSENGER FLOOR PANEL 242UF SRM 53-00-50-2R-2 AND SRM 53-00-50-2R-9 (570660)

Part: STRAP — CORRODED (BS 1028) · airframe 41,931 hrs · 24,652 cycles

REINFORCEMENT STRAP CORRODED AT BS 1028, RBL 18. R & R THE STRAP IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (MAIN CABIN) · airframe 41,931 hrs · 24,652 cycles

CRACKED FLOOR SUPPORT BS 344-360 LBL 1-WL 208. / REMOVED AND REPLACED FLOOR SUPPORT AT B.S. 344-360; LBL 1 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 141A5400.

Part: CHANNEL — CORRODED (BS 947-986) · airframe 41,931 hrs · 24,652 cycles

R2 DOOR MOP SILL CORRODED BETWEEN BS 947 TO 986, RBL 60. R & R THE MOP SILL IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 41,931 hrs · 24,652 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294, BL 0. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 41,931 hrs · 24,652 cycles

MAIN PRESSURE BULKHEAD WEB CRACKED AT BS 663, BETWEEN LBL 25 TO LBL 48. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: STRINGER — CRACKED (LT WING) · airframe 41,506 hrs · 24,383 cycles

LEFT WING LEADING EDGE STRINGER FOUND CRACKED. R & R THE STRINGER IAW SRM.

Part: PANEL — CRACKED (MAIN CABIN) · airframe 41,506 hrs · 24,383 cycles

CABIN FLOORBOARD BREAK PANEL LEFT OF CENTER AT STA. 540 CRACKED. / REMOVED AND REPLACED PANEL REF SRM 51-40-02.

Part: PANEL — CRACKED (MAIN CABIN) · airframe 41,506 hrs · 24,383 cycles

CABIN FLOORBOARD BREAK PANEL RIGHT OF CENTER AT STA. 540 CRACKED. / REMOVED AND REPLACED PANEL REF SRM 51-40-02.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 39,457 hrs · 23,091 cycles

R1 DOOR LOWER EXIT SIGN FELL OFF. R & R THE SIGN IAW MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 37,574 hrs · 21,985 cycles

FWD ENTRY EXIT LIGHT LENS MISSING. R & R THE LIGHT ASSY IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 36,999 hrs · 21,644 cycles

RIGHT EMERGENCY LIGHT FAILED CAPACITY TEST. R & R THE BATTERY PACK IAW DWG.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 36,999 hrs · 21,644 cycles

R1 DOOR EMERGENCY SLIDE LENS LOOSE. R & R THE LENS IAW MT & AMM.

Part: WIRE — BROKEN (CABIN) · airframe 35,351 hrs · 20,640 cycles

R1 DOOR EMER EXIT LIGHT WIRE BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,885 hrs · 20,363 cycles

LEFT OVERWING EXIT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,885 hrs · 20,363 cycles

FORWARD LT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,885 hrs · 20,363 cycles

LEFT BATTERY PACK FAILED CAPACITY CHECK AT ROW 17. R & R BATTERY PACK IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,207 hrs · 19,974 cycles

EXTERIOR EMERGENCY LIGHT AFT OF L2 DOOR INOPERATIVE. REPLACED THE LAMP IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 32,970 hrs · 19,251 cycles

RIGHT OVERWING FWD EMER EXIT LIGHT LENS CRACKED. REPAIRED LENS IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 31,968 hrs · 18,661 cycles

VERTICAL PRESS DECK CRACKED AT BS 663.75, BETWEEN RBL 35 - 43. REPAIRED DECK IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 30,886 hrs · 18,029 cycles

SIDEWALL EXIT LIGHT COVER LENS LOOSE AT ROW 11. REPAIRED LENS IAW MM.

Part: NUT PLATE — BROKEN (BATTERY CHARGER) · airframe 30,375 hrs · 17,743 cycles

AFT LT BATTERY CHARGER AFT NUTPLATE BROKEN. R & R CHARGER ASSEMBLY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 30,375 hrs · 17,743 cycles

CENTER RT EMER BATTERY FAILED FUNCTIONAL CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 30,375 hrs · 17,743 cycles

AFT LT EMER BATTERY FAILED FUNCTIONAL CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 30,375 hrs · 17,743 cycles

AFT RT EMER BATTERY FAILED FUNCTIONAL CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 30,375 hrs · 17,743 cycles

FORWARD RT EMER BATTERY FAILED FUNCTIONAL CHECK. R & R BATTERY IAW AMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

OUTBOARD SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

OUTBOARD SEAT TRACK FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW EA.

Part: PLATE — CRACKED (LT WING) · airframe 28,745 hrs · 16,856 cycles

LEFT WING REAR SPAR WAFFLE PLATE CRACKED INBD OF NR 3 FLAP FAIRING. R & R WAFFLE PLATE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

INTERCOSTAL CRACKED BETWEEN BS 334 TO BS 360, RBL 11. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 33. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

INTERCOSTAL CRACKED BETWEEN BS 294 TO BS 312, RBL 15. R & R INTERCOSTAL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

INBOARD SEAT TRACK FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

INBOARD SEAT TRACK FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

AFT BAGGAGE BIN L ANGLE CRACKED AT BS 867, LBL 12. R & R ANGLE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

OUTBOARD SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

INBOARD SEAT TRACK FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

OUTBOARD SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

FORWARD CABIN INTERCOSTAL CRACKED AT BS 350, CBL 0. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

FORWARD CABIN INTERCOSTAL CRACKED AT BS 315, RBL 30. R & R INTERCOSTAL IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

FORWARD GALLEY Z ANGLE CORRODED BETWEEN BS 294 TO BS 360. R & R ANGLE IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

WEB STIFFENER STRAP CORRODED AT BS 1028, LBL 3. R & R STRAP IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

WEB STIFFENER STEP CORRODED AT BS 1028, RBL 3. R & R STRAP IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R & R INTERCOSTAL IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

AFT CARGO COMPARTMENT UNDERSIDE STRAP CORRODED JUST AFT OF THRESHOLD PLATE. R & R STRAP IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R & R INTERCOSTAL IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,745 hrs · 16,856 cycles

LEFT HORIZONTAL STABILIZER SKIN CRACKED ON INBD SIDE OF FRAME AT STAB STATION 129.50, 10 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 28,745 hrs · 16,856 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME E - F CRACKED AT NR 8 FASTENER HOLE. REPAIRED FRAME IAW SI.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,745 hrs · 16,856 cycles

RIGHT HORIZONTAL STABILIZER SKIN 5 INCHES CRACKED ON INBD SIDE OF FRAME AT STATION 184.7, 26 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,745 hrs · 16,856 cycles

LEFT HORIZONTAL STABILIZER SKIN 5 INCHES CRACKED ON INBD SIDE OF FRAME AT STATION 175.50, 10.5 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,745 hrs · 16,856 cycles

RIGHT HORIZONTAL STABILIZER SKIN CRACKED 5 INCHES ON FWD SIDE OF REAR SPAR AT STAB STATION 123. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,745 hrs · 16,856 cycles

LEFT HORIZONTAL STABILIZER SKIN CRACKED ON INBD SIDE OF FRAME AT STAB STATION 129.50, 18 INCHES FROM AFT SPAR. REPAIRED SKIN IAW SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,727 hrs · 16,841 cycles

AFT EMERGENCY FLASHLIGHTS INOPERATIVE. R & R BATTERIES IAW CMM.

Part: COVER — BROKEN (CABIN) · airframe 28,659 hrs · 16,803 cycles

L1 DOOR EXIT LIGHT COVER BROKEN. R & R L1 DOOR EXIT LIGHT ASSEMBLY.

Part: NUT PLATE — DAMAGED (R1 DOOR) · airframe 28,162 hrs · 16,510 cycles

R1 DOOR SLIDE COVER AFT ATTACH NUTPLATE DAMAGED. R & R NUTPLATE IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 24,967 hrs · 14,611 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSY IAW MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 24,230 hrs · 14,168 cycles

EXIT LIGHT LENS FWD ENTRY DOOR MISSING. INSTALLED NEW LENS FWD ENTRY EMERGENCY EXIT SIGN AS PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 23,901 hrs · 13,972 cycles

AFT SERVICE DOOR SLIDE OUT OF CONTAINER. RE-INSTALLED SLIDE ASSY PER 725-61-06.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 23,659 hrs · 13,837 cycles

L1 DOOR SLIDE LOWER FLAP REQUIRES REPOSITION. REPOSITIONED PER M/M L1 DOOR SLIDE, C/W T/C 725-61-06.

Part: BATTERY — FAILED (CABIN) · airframe 23,659 hrs · 13,837 cycles

ONE EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST FWD RIGHT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK FWD RIGHT (M01674) PER M/M AND SSM.

Part: LENS — CRACKED (R2 DOOR) · airframe 23,659 hrs · 13,837 cycles

R2 GALLEY DOOR SLIDE COVER LENS CRACKED. REMOVED AND REPLACED R2 GALLEY DOOR SLIDE COVER LENS IAW MT 25-66-01/401.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 23,659 hrs · 13,837 cycles

L2 DOOR SLIDE LOWER FLAP REQUIRES REPOSITION. REPOSITIONED L2 DOOR SLIDE LOWER FLAP IAW M/M.

Part: PLATE — CRACKED (RT WING) · airframe 23,659 hrs · 13,837 cycles

RIGHTT WING LOWER AFT T/E SHELF PANEL 651GB FWD SUPPORT BRACKET (WIGGLE PLATE) CRACKED AROUND SEVERAL RIVETS. REMOVED AND REPLACED RIGHT WING LOWER AFT T/E SHELF PANEL 651GB FWD SUPPORT BRACKET (WIGGLE PLATE) PER SRM 51-40-02 AND MM

Part: LIGHT — BROKEN (CABIN) · airframe 21,846 hrs · 12,833 cycles

LEFT EEPLS BROKEN AT ROW 1. REMOVED AND REPLACED EEPLS PER M/M.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 21,739 hrs · 12,770 cycles

LEFT FLOOR SUPPORT Z ANGLE UPPER SURFACE CORRODED BETWEEN BS 499 TO 500 + 5, LBL 22. REMOVED AND REPLACED Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,739 hrs · 12,770 cycles

RIGHT ZEE ANGLE CORRODED BETWEEN BS 767 TO BS 787. REMOVED AND REPLACED ZEE ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,739 hrs · 12,770 cycles

RIGHT Z-ANGLE IS CORRODED BETWEEN BS 727D TO BS 767. REPAIRED Z-ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,739 hrs · 12,770 cycles

RIGHT ZEE ANGLE CORRODED BETWEEN BS 767 TO BS 794. REMOVED AND REPLACED ZEE ANGLE IAW SRM AND DWG.

Part: SKIN — PUNCTURED (LT SPOILER) · airframe 21,739 hrs · 12,770 cycles

LEFT WING TRAILING EDGE GROUND SPOILER NR 6 LOWER SKIN PUNCTURED. REMOVED AND REPLACED NR 6 GROUND SPOILER IAW AMM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,739 hrs · 12,770 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED STA 101.90. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,441 hrs · 12,592 cycles

LT OVERWING EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED PER AMM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,441 hrs · 12,592 cycles

RT HORIZONTAL STAB LOWER IN-SPAR SKIN HAS 2" CRACK AT STAB STA. 139.7. REPAIRED SKIN PER SRM.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT) · airframe 20,985 hrs · 12,316 cycles

R2 WINDOW ARCED. REMOVED AND REPLACED NR 3 CONTROLLER, PIGTAIL, AND WINDOW PER MM.

Part: LENS — BROKEN (CABIN) · airframe 20,760 hrs · 12,193 cycles

EMERGENCY FLOOR TRACK LENS AT ROW 2 BROKEN. REMOVED AND REPLACED LENS PER AMM.

Part: COVER — BROKEN (CABIN) · airframe 19,966 hrs · 11,734 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER BROKEN AT ROW 22. REMOVED AND REPLACED COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 19,966 hrs · 11,734 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER BROKEN AT ROW 4. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,272 hrs · 11,330 cycles

RT EMERGENCY EXIT SIDEWALL LIGHT INOP BETWEEN ROW 12 TO ROW 13. REPAIRED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 19,152 hrs · 11,263 cycles

FWD EEPLS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 19,048 hrs · 11,200 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EEPLS LENS BROKEN AT ROW 11. REMOVED AND REPLACED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 17,394 hrs · 10,263 cycles

LT EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,164 hrs · 10,133 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 15,778 hrs · 9,302 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 19 TO ROW 23. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 15,778 hrs · 9,302 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 15,698 hrs · 9,259 cycles

L1 DOOR LOWER EMERGENCY EXIT LENS COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 14,606 hrs · 8,622 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 14,606 hrs · 8,622 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHTS BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,378 hrs · 8,473 cycles

DURING SCHEDULED SPV CHECK, FOUND AFT CABIN CENTER CEILING EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: BRACKET — BROKEN (GIRT BAR) · airframe 13,316 hrs · 7,865 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 12,373 hrs · 7,302 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 10,131 hrs · 5,942 cycles

FWD GALLEY EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,029 hrs · 5,885 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 8,839 hrs · 5,162 cycles

FOUND FIRST EMERGENCY EXIT FLOOR TRACK LIGHT INOP. RECONNECTED WIRES PER MM.

Part: WIRE — DISCONNECTED (CABIN) · airframe 8,808 hrs · 5,144 cycles

FOUND EMERGENCY EXIT FLOOR TRACK LIGHT INOP. RECONNECTED WIRES PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 8,541 hrs · 4,976 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 8,520 hrs · 4,961 cycles

L1 DOOR EMERGECNY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: COVER — LOOSE (CABIN) · airframe 6,129 hrs · 3,513 cycles

EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,140 hrs · 2,367 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 3,455 hrs · 1,971 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.