N279WN

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 60,678 hrs · 36,764 cycles

AFT SERVICE DOOR EMERGENCY SLIDE GIRT BAR HANGING TOO LOW. SECURED THE GIRT BAR IAW AMM 25-66-01.

Part: LENS — DETACHED (ZONE 200) · airframe 59,600 hrs · 36,091 cycles

MID- CABIN EXIT SIGN BROKEN OFF. INSTALLED MID-CABIN EMERGENCY EXIT SIGN LENS PER SIP.

Part: SIGN — OUT OF ADJUST (ZONE 200) · airframe 58,935 hrs · 35,672 cycles

OVERHEAD CEILING EMERGENCY EXIT LIGHT BEZEL DETACHED AT OVERWING EXIT.<[01] RE-ATTACHED OVERHEAD CEILING EMERGENCY EXIT LIGHT BEZEL PER AMM 33-51-01.

Part: PLACARD — MISSING (ZONE 800) · airframe 58,323 hrs · 35,289 cycles

OVERWING EMERGENCY PLACARD BELOW WINDOW IS MISSING ON AIRCRAFT RIGHT<[01] REINSTALLED. EMERGENCY EXIT LIGHT COVER PER AMM 33-51-00.

Part: LENS — DAMAGED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

IN-CORRECTED EMERGENCY LENS ON DOOR R1 AT FWD GALLEY AREA 2024-758993<[01] REPLACED EMERGENCY LENS ON DOOR R1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 STEP 3.C.(D)(6)(7)(10)(13);[02] CORRECTED STEP 1: REPLACED EMERGENCY LENS ON DOOR R1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(D)(6)(7)(10)(13);[03] CORRECTED STEP 2: REPLACED EMERGENCY LENS ON DOOR R1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(D)(6)(7)(10)(13)<BR>TEST IS OK;[04] CORRECTED STEP 3: REPLACED EMERGENCY LENS ON DOOR R1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(5)(D)(6)(7)(10)<BR>TEST IS OK;[05] REPLACED EMERGENCY LENS ON DOOR R1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(5)(D)(6)(7)(10)<BR>TEST IS OK

Part: LENS — DAMAGED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

IN-CORRECTED EMERGENCY LENS ON DOOR L2 AT AFT GALLEY AREA 2024-758994<[01] REPLACED EMERGENCY LENS ON DOOR L2 AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(D)(6)(7)(10)(13);[02] CORRECTED STEP 1: REPLACED EMERGENCY LENS ON DOOR L2 AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(5)(D)(6)(7)(10)<BR>TEST IS OK;[03] REPLACED EMERGENCY LENS ON DOOR L2 AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(5)(D)(6)(7)(10)<BR>TEST IS OK

Part: LENS — DAMAGED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

IN-CORRECTED EMERGENCY LENS ON DOOR L1 AT FWD GALLEY AREA 2024-758992<[01] REPLACED EMERGENCY LENS ON DOOR L1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(D)(6)(7)(10)(13);[02] CORRECTED STEP 1: REPLACED EMERGENCY LENS ON DOOR L1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(5)(D)(6)(7)(10)<BR>TEST IS OK;[03] REPLACED EMERGENCY LENS ON DOOR L1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(5)(D)(6)(7)(10)<BR>TEST IS OK

Part: LENS — DAMAGED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

IN-CORRECTED EMERGENCY LENS ON DOOR R2 AT AFT GALLEY AREA 2024-758995<[01] REPLACED EMERGENCY LENS ON DOOR R2 AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(D)(6)(7)(10)(13);[02] CORRECTED STEP 1: REPLACED EMERGENCY LENS ON DOOR R2 AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(5)(D)(6)(7)(10)(13) <BR>TEST IS OK;[03] CORRECTED STEP 1: REPLACED EMERGENCY LENS ON DOOR R2 AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(5)(D)(6)(7)(10)<BR>TEST IS OK;[04] CORRECTED STEP 3: REPLACED EMERGENCY LENS ON DOOR R2 AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(5)(D)(6)(7)(10)<BR>TEST IS OK;[05] REPLACED EMERGENCY LENS ON DOOR R2 AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(5)(D)(6)(7)(10)<BR>TEST IS OK

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,090 hrs · 35,145 cycles

CUSTOMER REQUEST AAI INSPECTION MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75 2024-758945<[01]. REPLACED BREAK ASSY PANEL AND FASTENERS IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 46 REV-.SEE INDIVIDUAL SIGN OFFS BELOW;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT — CRACKED (ZONE 200) · airframe 58,090 hrs · 35,145 cycles

CUSTOMER REQUEST AAI INSPECTION MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2024-758947<[01]. REPLACED BREAK ASSY PANEL AND FASTENERS AT STA 540; BL 0 TO LBL 24.75 IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 46 REV- SEE INDIVIDUAL SIGN OFFS BELOW; [02] BATCH NO 563580 ENTER BY ERROR. THE CORRECT BATCH NO IS 449126.; [03] CERTIFIED WORK PERFORMED. SEE INDIVIDUAL SIGN OFF BELOW.

Part: RIB — CRACKED (ZONE 300) · airframe 58,093 hrs · 35,146 cycles

CRACK ON LOWER CHORD INSPAR RIB 4 LOCATED AT 18 INCHES FROM FRONT SPAR LT HORIZONTAL STAB. 2024-758920<[01] TOOL USED P/N: NORTEC 500D; S/N: N500X12101V022235; CAL DUE: 07-OCT-25.;[02] TOOL USED P/N: NORTEC 500D; S/N: N500X12101V022235; CAL DUE: 07-OCT-25.;[03] PERFORMED PERMANENT REPAIR INSPAR RIB LOCATED AT 18 INCHES FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5; [04] PERFORMED PERMANENT REPAIR INSPAR RIB LOCATED AT 18 INCHES FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5.

Part: PLATE — CRACKED (ZONE 500) · airframe 58,093 hrs · 35,146 cycles

CRACK ON CORRUGATED PLATE LOCATED AT LEVEL IRSS 212 TRAILING EDGE AT LT WING 2024-758889<[01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL IRSS 212 TRAILING EDGE AT LT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 TOOK MEASURES OF CRACK L= 1.160? TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A23304099 DUE DATE: 09-NOV-25;[02] REPLACED CORRUGATED PLATE LOCATED AT LEVEL IRSS 212 TRAILING EDGE AT LT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 TOOK MEASURES OF CRACK L= 1.160? TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A23304099 DUE DATE: 09-NOV-25

Part: WEB — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK ON WEB LOCATED BTW BS 400 TO BS 420 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-758854<[01] REPLACED WEB LOCATED BTW BS 400 TO BS 420 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505 REV.-<BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB LOCATED BTW BS 400 TO BS 420 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505 REV

Part: WEB — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK ON WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-758850<[01] REPLACED WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 83 REV-.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK ON ANGLE LOCATED FWD FACE BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-758852<[01] REPLACED ANGLE LOCATED FWD FACE BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G-0 ITEM 9 AND DRAWING 143A7505 SHT 81.;[02] REPLACED ANGLE LOCATED FWD FACE BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G-0 ITEM 9 AND DRAWING 143A7505 SHT 81.

Part: GUSSET — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK GUSSET LOCATED BS 500D AT LEVEL STR 19R AT FWD CARGO COMPARTMENT 2024758857<[01] REPLACED GUSSET LOCATED BS500D AT LEVEL STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV -. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED GUSSET LOCATED BS500D AT LEVEL STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV -.

Part: ANGLE — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK ON ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-758838<[01] REPLACED ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7505 SHEET:82 REV.-SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7505 SHEET:82 REV.-SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK ON ANGLE LOCATED FWD FACE BS 420 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-758853<[01]. REPLACED ANGLE LOCATED FWD FACE BS 420 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7505 SHEET:81 REV.- SEE INDIVIDUAL SIGN OFFS BELOW.; [02] REPLACED ANGLE LOCATED FWD FACE BS 420 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7505 SHEET:81 REV. - SEE INDIVIDUAL SIGN OFFS BELOW.

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

CRACK INDICATION ON STUB FRAME LOCATED ON BS 296 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.187 IN. APPROX. AT PASSENGER CABIN 2024-758860<[01] REPLACED STUB FRAME LOCATED ON BS296 BTW STR 7R TO STR 10R AT FWD GALLEY DOOR AREA I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 141A8370 SHEET 9 REV D AND DWG 141A3330 SHEET 4 REV-.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED STUB FRAME LOCATED ON BS296 BTW STR 7R TO STR 10R AT FWD GALLEY DOOR AREA I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 141A8370 SHEET 9 REV D AND DWG 141A3330 SHEET 4 REV-.<BR>SEE INDIVIDUAL SIGN OFF BELOW AS RII

Part: GUSSET — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK GUSSET LOCATED BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT 2024-758858<[01]. REPLACED GUSSET LOCATED BS500D AT LEVEL STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV - . SEE INDIVIDUAL SIGN-OFF BELOW; [02] REPLACED GUSSET LOCATED BS500D AT LEVEL STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV - . SEE INDIVIDUAL SIGN-OFF BELOW.

Part: WEB — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK ON WEB LOCATED BTW BS 500A TO BS 500B AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-758842<[01] TOOL USED ON STEP 2. ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] REPLACED WEB LOCATED BTW BS 500A TO BS 500B AT LEVEL STR 26L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 82 REV-. <BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2<BR>REPLACED AND REPAIRED WEB LOCATED BTW BS 500A TO BS 500B AT LEVEL STR 26L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 53-30-53-2R-1 REPAIR 1 AND DWG 143A7505 SHEET 82 REV-. <BR>SEE INDIVIDUAL SIGN OFF BELOW.;[04] CERTIFIED RII MAJOR REPAIR WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: PLATE — CRACKED (ZONE 400) · airframe 58,093 hrs · 35,146 cycles

CRACK ON INBOARD AND OUTBOARD PLATE LOCATED ACCESS PANEL 431AT AT ENGINE 1 (2 E/A) 2024-758822<[01] REPLACED INBOARD AND OUTBOARD PLATE LOCATED ACCESS PANEL 431AT AT ENGINE 1 (2 E/A) IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 . LENGTH OF CRACK IS: 0.626? TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N:B23394214 DUE DATE:06/FEB/25.;[02] PART REQUIREMENT WITH BN 533725 SIGNED BY ERROR; THE CORRECTED PART NUMBER IS KT313A2114U1 BN 564110;[03] TASK 1 AND 2 VERIFIED; COMPLETE.

Part: PLATE — CRACKED (ZONE 400) · airframe 58,093 hrs · 35,146 cycles

CRACK ON INBOARD PLATE OF ACCESS PANEL 441AT AT ENGINE 2 2024-758821<[01] REPLACED INBOARD PLATE OF ACCESS PANEL 441AT AT ENGINE 2 IAW B737-700 SRM 51-10-02 AND SRM 51-40-02;[02] CORRECTED STEP 1<BR>REPLACED INBOARD PLATE OF ACCESS PANEL 441AT AT ENGINE 2 IAW B737-700 SRM 51-10-02 AND SRM 51-40-02<BR>LENGTH OF CRACK IS: 0.601? TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N:B23267756 DUE DATE: 10/NOV/25;[03] REPLACED INBOARD PLATE OF ACCESS PANEL 441AT AT ENGINE 2 IAW B737-700 SRM 51-10-02 AND SRM 51-40-02<BR>LENGTH OF CRACK IS: 0.601? TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N:B23267756 DUE DATE: 10/NOV/25. JOB COMPLETE.

Part: ANGLE — CRACKED (ZONE 600) · airframe 58,093 hrs · 35,146 cycles

CRACK ANGLE SLAT 6 LOCATED ON AUXILIARY TRACK LOWER AREA INTERNAL CAVITY AT RT WING 2024-758726<[01] REPLACED ANGLE SLAT 6 LOCATED ON AUXILIARY TRACK LOWER AREA INTERNAL CAVITY AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 114A5030 SHEET 14 REV.B <BR>MEASURE OF CRACK IS: 1.200' TOOL USED CALIPER P/N:500-197-30 S/N:B23412298 DUE DATE:10NOV25;[02] CERTIFIED WORK PERFORMED.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK WEB - INTERCOSTAL LOCATED STA 847 AT LBL 20 AT AFT CARGO COMPARTMENT 2024-758705<[01] REPLACED WEB INTERCOSTAL LOCATED STA 847 AT LBL 20 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G-0 ITEM 9 AND DRAWING 149A8100 SHEET 1;[02] REPLACED WEB INTERCOSTAL LOCATED STA 847 AT LBL 20 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G-0 ITEM 9 AND DRAWING 149A8100 SHEET 1

Part: ANGLE — CRACKED (ZONE 500) · airframe 58,093 hrs · 35,146 cycles

CRACK ANGLE SLAT 3 LOCATED AUXILIARY TRACK LOWER AREA INTERNAL CAVITY AT LT WING 2024-758738<[01] REPLACED ANGLE SLAT 3 LOCATED ON AUXILIARY TRACK LOWER AREA INTERNAL CAVITY AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 114A5030 SHEET 14 REV.B<BR>MEASURE OF CRACK IS: 2.00' TOOL USED CALIPER P/N:500-197-30 S/N:B23412298 DUE DATE:10NOV25;[02] CERTIFIED WORK PERFORMED.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CORROSION SUPPORT ZEE LOCATED BS727D TO BS747 AT LEVEL STR25R AFT CARGO COMPARTMENT 2024-758704<[01] REPLACED SUPPORT ZEE LOCATED BS727 TO BS767 AT LEVEL STR25R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG:146A7500 SHEET:85 REV.A;[02] CORRECTED STEP 1.<BR>REPLACED SUPPORT ZEE LOCATED BS727 TO BS767 AT LEVEL STR25R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG:146A7500 SHEET:85 REV.A SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED SUPPORT ZEE LOCATED BS727 TO BS767 AT LEVEL STR25R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG:146A7500 SHEET:85 REV.A SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SUPPORT — CORRODED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

CORROSION SUPPORT ZEE LOCATED BS727C TO BS807 AT LEVEL STR25L AFT CARGO COMPARTMENT 2024-758703<[01] REPLACED SUPPORT ZEE LOCATED BS727 TO BS847 AT LEVEL STR25L AFT CARGO COMPARTMENT IAW B737-700 SRM51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A7500; SHEET 85; REV: A SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED;RII<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: ANGLE — CRACKED (ZONE 600) · airframe 58,093 hrs · 35,146 cycles

CRACK ANGLE SLAT 8 LOCATED ON AUXILIARY TRACK LOWER AREA INTERNAL CAVITY AT RT WING 2024-758727<[01] REPLACED ANGLE SLAT 8 LOCATED ON AUXILIARY TRACK LOWER AREA INTERNAL CAVITY AT RT WING WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 114A5030 SHEET 14 REV.B<BR>MEASURE OF CRACK IS: 2.00' TOOL USED CALIPER P/N:500-197-30 S/N:B23412298 DUE DATE:10NOV25;[02] CORRECTED STEP 1<BR>REPLACED ANGLE SLAT 8 LOCATED ON AUXILIARY TRACK LOWER AREA INTERNAL CAVITY AT RT WING WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 114A5010 SHEET 14 REV.C<BR>MEASURE OF CRACK IS: 2.00' TOOL USED CALIPER P/N:500-197-30 S/N:B23412298 DUE DATE:10NOV25;[03] CERTIFIED WORK PERFORMED.

Part: PLATE — CRACKED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

CRACK PLATE LOCATED BS907 TO BS927 BTW STR25R TO STR27R AT AFT CARGO COMPARTMENT (1 EA) 2024-758706<[01] REPLACED PLATE LOCATED BS907 TO BS927 BTW STR25R TO STR27R AT AFT CARGO COMPARTMENT (1 EA) IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG DWG 141A7221; SHEET 24; REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CORROSION SUPPORT ZEE LOCATED BS727 TO BS727B AT LEVEL STR25L AFT CARGO COMPARTMENT 2024-758701<[01]. FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00XJGWK;[02] FAULT RESOLVED ON OTHER FAULT.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK ANGLE - SUPPORT LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-758702<[01] REPLACED ANGLE - SUPPORT LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 149A8102; SHEET 17; REV - SEE INDIVIDUAL SIGN OFF BELOW; [02] REPLACED ANGLE - SUPPORT LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 149A8102; SHEET 17; REV -SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN 2024-758679<[01]. REPLACED ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 92 REV-. SEE INDIVIDUAL SIGN OFF BELOW; [02] TASK COMPLETED. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

CRACK ON ANGLE LOCATED BS 695 LBL 24.75 AT PASSENGER CABIN 2024-758670<[01]. TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 112820025 DUE DATE 22 JAN 25.; [02]. REPLACED ANGLE LOCATED BS 695 LBL 24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG:111A6000 SHEET:282 REV.- SEE INDIVIDUAL SIGN OFFS BELOW.; [03] TASK COMPLETED; RII. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

CRACK ON INTERCOSTAL WEB LOCATED BTW BS 344TO BS 360 RBL 50.5 WL 208.1 AT FWD GALLEY AREA 2024-758680<[01] REPLACED INTERCOSTAL WEB LOCATED BTW BS 344TO BS 360 RBL 50.5 WL 208.1 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 14 REV-. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

CRACK ON ANGLE LOCATED FWD FACE BS 695 BL 0 RT SIDE AT PASSENGER CABIN 2024-758671<[01] TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 112820025 DUE DATE 22 JAN 25.; [02] REPLACED ANGLE AND FASTENERS LOCATED FWD FACE BS 695 BL 0 RT SIDE AT PASSENGER CABIN IAW B837-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 273A9110 REV A. SEE INDIVIDUAL SIGN-OFFS BELLOW; [03] CORRECTED STEP 2. REPLACED ANGLE AND FASTENERS LOCATED FWD FACE BS 695 BL 0 RT SIDE AT PASSENGER CABIN IAW B837-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 273A9110 REV A. SEE INDIVIDUAL SIGN-OFFS BELOW.

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 58,093 hrs · 35,146 cycles

CRACK ANGLE TRAILING EDGE ORSS 278 LT WING 2024-758676<[01] REPLACED ANGLE LOCATED TRAILING EDGE ORSS 278 LT WING IAW B737-700 SRM 51-10-02 AND DWG 115A6200 SHEET 11 REV.B LENGTH OF CRACK IS: 1.756? TOOL USED CALIPER P/N:500-197-30 S/N:A23304029 DUE DATE:10/NOV/25.;[02] REPLACED ANGLE LOCATED TRAILING EDGE ORSS 278 LT WING IAW B737-700 SRM 51-10-02 AND DWG 115A6200 SHEET 11 REV.B LENGTH OF CRACK IS: 1.756? TOOL USED CALIPER P/N:500-197-30 S/N:A23304029 DUE DATE:10/NOV/25.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2024-758691<[01] REPLACED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 141A8180 SHEET: 27 REV: C<BR>SEE INDIVIDUAL SIGNS OFF BELOW.;[02] CERTIFIED CORRECTIVE ACTION 1; COMPLETED<BR>RII

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK SUPPORT BRACKET OF PNEUMATIC DUCT BS 540 AND RBL 6 AT AR CONDITIONING BAY 2024-758669 <[01] REPLACED SUPPORT BRACKET OF PNEUMATIC DUCT BS 540 AND RBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 212A1101 SHEET: 1 REV: A;[02] REPLACED SUPPORT BRACKET OF PNEUMATIC DUCT BS 540 AND RBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 212A1101 SHEET: 1 REV: A

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

CRACK ON INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 AT FWD GALLEY AREA 2024-758674<[01]. REPLACED WEB - INTERCOSTAL LOCATED BTW BS 344 TO BS 360 LBL 11 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 46 REV A<BR>SEE INDIVIDUAL SIGNOFF BELOW.;[02] JOB COMPLETED.

Part: ANGLE — CRACKED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

CRACK ON ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN 2024-758668<[01]. TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 112820025 DUE DATE 22 JAN 25.; 02] REPLACED ANGLE AND FASTENERS LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 111A6000 REV -. SEE INDIVIDUAL SIGN-OFFS BELOW; [03] CERTIFIED RII WORK PERFORMED. SEE INDIVIDUAL SIGN OFF BELOW.; [04] CERTIFIED RII WORK PERFORMED. SEE INDIVIDUAL SIGN OFF BELOW.

Part: TIE CLIP — CRACKED (ZONE 200) · airframe 58,093 hrs · 35,146 cycles

CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2024-758692<[01]. REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV-. SEE INDIVIDUAL SIGN OFF BELOW; [02] CERTIFIED CORRECTIVE ACTION STEP 1 RII.

Part: FLAP — DEBONDED (ZN 500 LEFT WING) · airframe 58,090 hrs · 35,145 cycles

CUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP LOWER SURFACE AT LT WING 2024-758672<[01] TOOL USED CALIPER PN: 500-196-30; SN: A23325649; DUE DATE: 31/DEC/24.;[02] TOOL USED ON ITEM 3: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 600; S/N: 120357005; DUE DATE: 10-JUN-25;[03] TOOL USED POSITECTOR PN: DF-631235; SN: AE-406428; DUE DATE: 26/AUG/25.<BR>HOT BONDER PN: HCS9200B-AV; SN: 18185733; DUE DATE: 25/JAN/25;[04] TOOL USED POSITECTOR PN: NS2; SN: 110098; DUE DATE: 05/SEP/25;[05] TOOL USED ON STEP 18 TOOL USED: AUDIBLE BOND TESTER P/N: S-3; S/N: 064; DUE DATE: 27-AUG-25;[06] REPAIRED OB AFT FLAP LOWER SURFACE AT LT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. REFER TO INDIVIDUALS SIGNOFFS BELOW;[07] JOB COMPLETED <BR>ITEM RII.

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 58,093 hrs · 35,146 cycles

CRACK ANGLE TRAILING EDGE ORSS 271 AT RT WING 2024-758675<[01] REPLACED ANGLE TRAILING EDGE ORSS 271 AT RT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02-0G-0 AND DWG 115A2930 SHEET:8 REV:- AND MEASURES OF CRACK IS :L= 0.879? INCHES TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/ :D23329421 DUE DATE:22- FEB-25.;[02] REPLACED ANGLE TRAILING EDGE ORSS 271 AT RT WING IAW B737-700 SRM 51-10-02 ITEM:9; SRM 51-40-02-0G-0 AND DWG 115A2930 SHEET:8 REV:- AND MEASURES OF CRACK IS :L= 0.879? INCHES TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/ :D23329421 DUE DATE:22- FEB-25.;[03] REPLACED ANGLE TRAILING EDGE ORSS 271 AT RT WING IAW B737-700 SRM 51-10-02 ITEM:9; SRM 51-40-02-0G-0 AND DWG 115A2930 SHEET:8 REV:- AND MEASURES OF CRACK IS :L= 0.879? INCHES TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/ :D23329421 DUE DATE:22- FEB-25.

Part: ANGLE — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK SUPPORT STRUCTURE WING TO BODY FAIRING ANGLE BS 500D LEVEL STRINGER 19R AT LOWER FUSELAGE 2024-758593<[01] TOOL USED DIGITAL CALIPER P/N: 500-197-30; S/N:B233116868; DUE DATE:04-FEB-25.;[02] REPLACED SUPPORT STRUCTURE WING TO BODY FAIRING ANGLE BS 500D LEVEL STRINGER 19R AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 116A3010; SHEET 37; REV -.<BR><BR><BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[03] TASK COMPLETED; SEE INDIVIDUAL SIGN-OFF BELOW

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-758548<[01] TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N: A21147752 DUE DATE: 20-SEP-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1859843 ; DUE DATE : 10/MAR/25;[03] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDING WITH BOEING 737-700 SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) TO (7); REFER TO BAC 5975. SEE INDIVIDUAL SIGNOFF BELOW.;[04] TASK COMPLETED.

Part: FITTING — DETERIORATED (ZONE 800) · airframe 58,093 hrs · 35,146 cycles

DETERIORATED GIRT BAR FITTING HARDWARE SIDE RT AT AFT GALLEY AREA 2024-758388<[01] REPLACED GIRT BAR FITTING HARDWARE SIDE RT AT AFT GALLEY AREA IAW AMM 25-66-02-400-801 THE INSTALLATION IS DOCUMENTED ON TTG8Q0028AYT STEP 2.A.(13);[02] CORRECTED STEP 1 REPLACED GIRT BAR FITTING HARDWARE SIDE RT AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS DOCUMENTED ON TTG8Q0028AYT STEP 2.A.(13);[03] REPLACED GIRT BAR FITTING HARDWARE SIDE RT AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS DOCUMENTED ON TTG8Q0028AYT STEP 2.A.(13)

Part: BRACKET — DETERIORATED (ZONE 800) · airframe 58,093 hrs · 35,146 cycles

DETERIORATED HARDWARE GIRT BAR FLOOR BRACKET SERVICE DOOR AT FWD GALLEY AREA 2024-758410<[01] REPLACED HARDWARE GIRT BAR FLOOR BRACKET SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS DOCUMENTED ON TTG8Q0028B17 STEP 2.A.(12);[02] REPLACED HARDWARE GIRT BAR FLOOR BRACKET SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS DOCUMENTED ON TTG8Q0028B17 STEP 2.A.(12)

Part: BRACKET — DETERIORATED (ZONE 800) · airframe 58,093 hrs · 35,146 cycles

DETERIORATED HARDWARE GIRT BAR FLOOR BRACKET ENTRY DOOR AT FWD GALLEY AREA 2024-758409<[01] REPLACED HARDWARE GIRT BAR FLOOR BRACKET ENTRY DOOR AT FWD GALLEY AREA THE INSTALLATION IS<BR>DOCUMENTED ON TTG8Q0028B17 STEP 2.A.(12);[02] CORRECTED STEP 1 REPLACED HARDWARE GIRT BAR FLOOR BRACKET ENTRY DOOR AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS DOCUMENTED ON TTG8Q0028B17 STEP 2.A.(12);[03] REPLACED HARDWARE GIRT BAR FLOOR BRACKET ENTRY DOOR AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS DOCUMENTED ON TTG8Q0028B17 STEP 2.A.(12)

Part: FITTING — DETERIORATED (ZONE 8000) · airframe 58,093 hrs · 35,146 cycles

DETERIORATED GIRT BAR FITTING HARDWARE SIDE LH AT AFT GALLEY AREA 2024-758387<[01] REPLACED GIRT BAR FITTING HARDWARE SIDE LT AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS DOCUMENTED ON TTG8Q0028AYT STEP 2.A.(13);[02] CORRECTED STEP 1 REPLACED GIRT BAR FITTING HARDWARE SIDE LH AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS DOCUMENTED ON TTG8Q0028AYT STEP 2.A.(13);[03] REPLACED GIRT BAR FITTING HARDWARE SIDE LH AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS DOCUMENTED ON TTG8Q0028AYT STEP 2.A.(13)

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK VAPOR BARRIER BS 663.75 AND RBL 52 MAIN WHEEL WELL COMPARTMENT 2024-758459<[01] TOOL USED: HOT BONDER PN: HCS9200B; SN: 15102320; DUE DATE: 25-JAN-25.;[02] ON STEP 12; TOOL USED: ULTRASONIC FLAW DETECTOR; PN: EPOCH 650; SN: 190984811; DUE DATE: 11-JAN-25;[03] REPAIRED VAPOR BARRIER BS 663.75 AND RBL 52 MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. TOOL USED SCALE P/N CR5200 S/N 8342514597 DUE DATE 28 FEB 25; TOOL USED: SCALE P/N: SPX621; S/N: 8340225441; DUE DATE: 02-JUL-25; CALIPER P/N 500-197-30 S/N:A18229508 DUE DATE 14-JAN-25. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPAIRED VAPOR BARRIER BS 663.75 AND RBL 52 MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. TOOL USED SCALE P/N CR5200 S/N 8342514597 DUE DATE 28 FEB 25; TOOL USED: SCALE P/N: SPX621; S/N: 8340225441; DUE DATE: 02-JUL-25; CALIPER P/N 500-197-30 S/N:A18229508 DUE DATE 14-JAN-25.RII COMPLETED.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 58,093 hrs · 35,146 cycles

CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2024-758458<[01] TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N: A21147752 DUE DATE: 20-SEP-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1859843 ; DUE DATE : 10/MAR/25;[03] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] TASK COMPLETED.

Part: RIB — CRACKED (ZONE 300) · airframe 58,093 hrs · 35,146 cycles

CRACK INSPAR RIB 4 LOCATED AT 36 INCH LT HORIZONTAL STAB 2024-758454<[01] TOOL USED ON STEP 4. ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] PERFORMED PERMANENT REPAIR INSPAR RIB 4 LOCATED AT 36 INCH LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] REJECTED FINAL CORRECTIVE ACTION DUE TO INCORRECT REFERENCE USED WHEN STATING THE REPAIR AND IT DOES NOT MATCH REFERENCE AND WRITTEN STEP 3;[04] CORRECTED REJECTION; REFERENCE USED ON STEP 3 WAS CORRECTED TO MATCH WITH THE JOB PERFORMED;[05] CORRECTED REJECTION; REFERENCE USED ON STEP 3 WAS CORRECTED TO MATCH WITH THE JOB PERFORMED;[06] PERFORMED PERMANENT REPAIR INSPAR RIB 4 LOCATED AT 36 INCH LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[07] TASK COMPLETED; RII<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 57,046 hrs · 34,492 cycles

LEFT AND RIGHT OVERWING ESCAPE SLIDE EMERGENCY LIGHTS INOP<[01] R AND R M1670 BATTERY PACK AND O/W AND BULLNOSE EMERGENCY LIGHTS CK OK REF AMM 33-51-04

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 57,046 hrs · 34,492 cycles

LEFT AND RIGHT OVERWING ESCAPE SLIDE EMERGENCY LIGHTS INOP<[01] R AND R M1670 BATTERY PACK AND O/W AND BULLNOSE EMERGENCY LIGHTS CK OK REF AMM 33-51-04

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,714 hrs · 34,291 cycles

LH OVERWING EXIT SIGN NEAR FLOOR MISSING LENS COVER<[01] REPLACED LENS IAW AMM 33-51-01

Part: SLIDE — FAULTED (L2 DOOR) · airframe 56,391 hrs · 34,094 cycles

L2 DOOR ESCAPE SLIDE GIRT REPACK REQUIRED.<[01] REPACKED GIRT ON L2 DOOR ESCAPE SLIDE PER AMM 25-66-01.

Part: GIRT BAR — FOD (FWD DOOR) · airframe 56,217 hrs · 33,984 cycles

FWD SERVICE DOOR GIRT BAR DIFFICULT TO LATCH.<[01] FOUND DEBRIS IN FWD BRACKET. REMOVED DEBRIS. OPS CHECKED PER AMM 25-66-02. OPS CHECK GOOD.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 55,479 hrs · 33,532 cycles

EXIT SIGN COVER CAME OFF<[01] REINSTALLED CENTER EXIT SIGN IAW AMM 33-51-01

Part: HANDLE — BROKEN (ZN 800 DOOR) · airframe 55,268 hrs · 33,410 cycles

FWD GALLEY SERVICE DOOR ASSIST HANDLE BROKEN.<[01] R&R'D FWD GALLEY SERVICE DOOR ASSIST HANDLE PER AMM 52-41-31.;[02] C/W INSP. R&R'D FWD GALLEY SERVICE DOOR ASSIST HANDLE PER AMM 52-41-31.

Part: SLIDE — LOW PRESSURE (ZN 800 DOOR) · airframe 54,350 hrs · 32,849 cycles

FWD ENTRY DOOR ESCAPE SLIDE BOTTLE PRESSURE BELOW LIMITS<[01] R&R FWD ENTRY DOOR ESCAPE SLIDE AS PER MT 725-61-06 REFERENCED FROM AMM 25-66-01

Part: SKIRT — OUT OF POSITION (ZN 800 DOOR) · airframe 52,335 hrs · 31,548 cycles

R2 DOOR SLIDE SKIRT RUBS AGAINST SCUFF PLATE.<[01] REPOSITION R2 DOOR SLIDE SKIRT IN REF. MT. 725-61-06;[02] VALIDATED STEP 1

Part: BATTERY PACK — DEFECTIVE (ZN 200 FUS TOP) · airframe 52,342 hrs · 31,551 cycles

EMERGENCY LIGHTING INOP FWD MAIN CABIN<[01] PERFORMED T/S AS PER B737 SSM 33-51-12; SSM 33-51-14; WDM 33-51-12; AND WDM 33-51-14 AND FOUND DEFECTIVE BATTERY PACKS AT POSITION M1673; M1674; AND M1675.;[02] REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M1673; M1674; AND M1675 AND PERFORMED INSTALLATION TEST AS PER B737 AMM 33-51-06-960-805. TEST OK.;[03] ACCOMPLISHED MXI PARTS TRANSACTION.;[04] VERIFIED STEPS 1-3

Part: LIGHT — CRAZED (ZN 200 FUS TOP) · airframe 52,335 hrs · 31,548 cycles

EPL STRIPS ARE CRAZED AND SCRATCH<[01] WORK ACCOMPLISHED ON TASK CARD 733-080-00-01; TTG8Q00AVTPP;[02] VERIFIED STEP 1

Part: WEDGE — DELAMINATED (ZN 500 LEFT WING) · airframe 52,335 hrs · 31,548 cycles

L/W I/B MAIN FLAP T/E OUTBD LOWER SURFACE DELAMINATED<[01] REMOVED L/W OUTBOARD FLAP INBOARD UPPER AND LOWER SEALS AS PER AMM 27-51-11;[02] REMOVED L/W INBOARD FLAP OUTBOARD UPPER SEAL AS PER AMM 27-51-11;[03] VERIFIED STEP 1 AND 2;[04] REMOVED L/W INBOARD T/E MAIN FLAP WEDGE IN REF. SRM 57-53-01-2R-7 AND 51-40-02-0G-0;[05] VERIFIED STEP 4 ; OK TO INSTALL NEW INBOARD T/E MAIN FLAP WEDGE .;[06] STEP 5 ENTERED IN ERROR.;[07] VERIFIED AND INSPECTED STEP #4. LWR IB T/E MAIN FLAP WEDGE REMOVED. OK TO INSTALL NEW SERVICEABLE LWR IB T/E MAIN FLAP WEDGE.;[08] INSTALLED L/W I/B MAIN FLAP T/EO/B WEDGE REF SRM 57-53-01-2R-7 AND 51-40-02-0G-0. PENDING SEALS INSTALLATION;[09] INSTALLED L/W I/B MAIN FLAP TRAILING EDGE WEDGE SEALS AS PER AMM 27-51-11-400-803;[10] VERIFIED STEP 8;[11] VERIFIED STEP 9

Part: FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

MAIN CABIN FRAME CRACKED ABOVE L-1 DOOR CUT-OUT AT FWD UPPER CORNER STA. 312<[01] CRACK CONFIRMED AT MAIN CABIN FRAME ABOVE L-1 DOOR CUTOUT FWD UPPER CORNER STA.312 ; IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK LENGTH : 0.218'.<BR>[NORTEC 600 ; B/C 172389 ; CALIB.DUE- 3/23];[02] ACCOMPLISHED EA:M-22-153-01244.;[03] VERIFIED STEP 2

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

FWD CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED<[01] RECEIVED SERVICEABLE(REPAIRED) AFT CORNER SCUFF PLATE P/N: 143A8331-4; ISSUE TAG: WN26166; CONTROL TAG: 439779.<BR>THIS PLATE WILL BE INSTALLED ON CARD: TTG8Q0028838.;[02] VERIFIED STEP1

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

AFT CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE CRACKED<[01] JOB WAS DONE BY OUTSIDE SERVICE J.L WELDING ISUE TAG # WN26163 P/N 146A8343-7 . PARTIAL REPAIR TAG FROM J.L WELDING W/O 16348;[02] CORRECTION JOB WAS DONE BY OUTSIDE SERVICE J.L WELDING ISUE TAG # WN26162 P/N 146A8343-5 . PARTIAL REPAIR TAG FROM J.L WELDING W/O 16348;[03] VERIFIED STEP #2.

Part: PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

AFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED<[01] JOB WAS DONE BY OUTSIDE SERVICE J.L WELDING ISUE TAG # WN26163 P/N 146A8343-7 . PARTIAL REPAIR TAG FROM J.L WELDING W/O 16348;[02] VERIFIED STEP #1.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

MAIN CABIN INTERCOSTAL ANGLE BETWEEN STA 380-400 RBL10' CRACKED<[01] REMOVED DAMAGED INTERCOSTAL ANGLE AT MAIN CABIN BETWEEN STA 380-400 RBL10' AS PER SRM-51-40-02-OG-O.;[02] LOCATED AND DRILLED NEW INTERCOSTAL ANGLE AT MAIN CABIN BETWEEN STA 380-400 RBL10' AS PER REF SRM-51-40-05-OG-0 AND DWG-143A5400.;[03] VERIFIED STEP 1;[04] VERIFIED STEP 2. OK TO INSTALL INTERCOSTAL.;[05] INSTALLED NEW INTERCOSTAL ANGLE AT MAIN CABIN BETWEEN STA 380-400 RBL10' AS PER REF SRM -51-40-02-OG-2 AND DWG-143A5400.;[06] VERIFIED STEP 5

Part: INTERCOSTAL — CORRODED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

MAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM STA 986.5 BETWEEN RBL 36'-45'<[01] REMOVED CORROSION ON MAIN CABIN AFT WET AREA AT FLOOR BEAM STA 986.5 BETWEEN RBL 36' TO RBL 45' REF SRM 51-10-02-0G.;[02] VERIFIED STEP 1;[03] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THK. NOTED 0.148'<BR>TOOL USED : OLYMPUS 27MG B/C 172139 04/23;[04] THIS CORROSION IS PRESENT ON AN EXISTING REPAIR; NO REWORK IS PERMITTED ON EXISTING REPAIRS PER SRM 53-70-51-2R-4. EXISTING REPAIR NEEDS REPLACEMENT;[05] REMOVED TWO (2 EAS) INTERCOSTAL ANGLES AT FLOOR BEAM STA 986.5 RBL 40 REF SRM 51-40-02-0G-0.;[06] REMOVED INTERCOSTAL AT FLOOR BEAM STA 986.5 RBL 40 REF SRM 51-40-02-0G-0.;[07] REMOVED LOWER ANGLE STA 986.5 RBL 45 REF SRM 51-40-02-0G-0.;[08] REMOVED ALL REPAIR FASTENERS AT FLOOR BEAM STA 986.5 BETWEEN RBL 30' TO RBL 45' REF SRM 51-40-02-0G-0;[09] THIS CORROSION IS LOCATED ADJACENT TO ANOTHER CORROSION THAT IS OUT OF LIMITS AND BOTH CORROSIONS ARE LOCATED ON A SECTION OF THE FLOOR BEAM THAT HAS A PREVIOUS REPAIR WHICH WILL NEED REPLACEMENT; THEREFORE; WORK WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00H7R9S;[10] VERIFIED STEP 9. FINAL.

Part: SUPPORT — ELONGATED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

MAIN CABIN FWD WET AREA STA 270 RBL 43' FASTENER HOLE ELONGATED<[01] REAMED ELONGATED HOLE AT MAIN CABIN FWD WET AREA STA 270 RBL 43 FINAL SIZE FOUND 0.375 DIAMETER TOOL USE D/C 172991 CAL: DUE DATE 15/07/23 REF SRM 51-10-02-0G-0 `;[02] PERFORMED ROTO INSP ON REAMED HOLE AT MAIN CABIN WET AREA STA 270 RBL43 IAW B737 NDT P6 51-00-00 PROC.16; NO CRACKS<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[03] VERIFIED STEP 1.;[04] REMOVED FLOOR SUPPORT AT MAIN CABIN STA 270 RBL 43' AS PER SRM 51-40-02;[05] RECEIVED NEW FLOOR SUPPORT P/N: 141A5751-2; FROM MACHIN SHOP; ISSUE TAG: WN26388; PO# 1792296; REQUEST PENETRANT INSPECTION; AS PER DWG. 141A5751.;[06] VERIFIED STEPS 4 AND 5;[07] PERFORMED PENETRANT INSP AT FLOOR SUPPORT IAW BOEING SOPM 20-20-02; NO CRACKS NOTED<BR>TOOL USED : TFS4 B/C 174662 CALDUE: 31-MAR-23;[08] INSTALLED ALL (HI LOK) ON NEW FLOOR SUPPORT AT MAIN CABIN FWD WET AREA STA 270 RBL 43 REF DWG #141A5710. PENDING X5 NUT PLATE TO BE INSTALLED.;[09] LATE ENTRY: OK TO INSTALL FLOOR SUPPORT. VERIFIED STEP 8.;[10] COMPLETED INSTALLATION OF NEW FLOOR SUPPORT AT MAIN CABIN FWD WET AREA STA 270 RBL 43 AS PER SRM 51-40-02 AND DWG 141A5710;[11] STEPS 8 AND 9 ARE RII STEPS;[12] VERIFIED STEP 10;[13] TASK C/W

Part: BEAM — CORRODED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

MAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM UPPER AND LOWER SURFACE STA 986.5 RBL 32'<[01] REMOVED CORROSION ON MAIN CABIN AFT WET AREA AT FLOOR BEAM UPPER AND LOWER SURFACE STA 986.5 RBL 32' REF SRM 51-10-02-0G.[12] REMOVED EXISTING REPAIR PARTS AT FLOOR BEAM STA 986.5 BETWEEN RBL 20' TO RBL 50' REF SRM 51-40-02-0G-0;[17] VERIFIED 63 MICROINCHES ON CUT OUT EDGES AND REPAIR PARTS REF SRM 51-20-13-0G-0. TOOL USED B/C 172331. OK TO FLAP PEENING THE AREA AND PARTS.;[18] ACCOMPLISHED FLAP PEENING ON EXISTING CUT OUT EDGES OF INTERCOSTAL AND FLOOR BEAM REF SRM SOPM 20-10-03. TOOL USED B/C 19433; DUE DATE. 22-AUG-23;[19] PERFORMED FPI INSP ON MACHINED AREAS AT FLOOR BEAM STA 986.5 RBL 32' IAW BOEING SOPM 20-20-02;[20] LOCATED AND DRILLED NEW T-CHORD PN 53100011-005 AND LOWER ANGLES PN 53100011-002 REF SRM 53-70-51-2R-4; ALTERNATIVE 2 AND ATS ER 19-01683 IR;[26] INSTALLED REPAIR PARTS AT FLOOR BEAM STA 986.5 BETWEEN RBL 20' TO RBL 50' REF SRM 53-70-51-2R-4; ALTERNATIVE 2 AND ATS ER 19-01683 IR;[27] CORRECTION STEP 26. INSTALLED REPAIR PARTS AT FLOOR BEAM STA 986.5 BETWEEN RBL 20' TO RBL 50' REF SRM 53-70-51-2R-4;[30] INSTALLED LOWER ANGLE AT STA 986.5 RBL 45 REF SRM 51-40-02-0G-0.;[31] INSTALLED AN INTERCOSTAL (1 EA) AND TWO INTERCOSTAL ANGLES (2 EAS) AT FLOOR BEAM STA 986.5 RBL 40 REF SRM 51-40-02-0G-0;[32] VERIFIED AND INSPECTED STEP #30 AND #31.;[33] INSPECTED.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

CENTER WING REAR SPAR VAPOR BARRIER WEB UPPER ANGLE CRACKED AT LBL 8'<[01] PERFORMED HFEC SURFACE INSP ON CENTER WING REAR SPAR VAPOR BARRIER WEN UPPER ANGLE AT LBL8 IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED<BR>TOOL USED : NORTEC 600 B/C 172389 03/23;04] FORMED REPLACEMENT ANGLE MAT. USED 2024-T3 CLAD .0.063'' AND SPLICE ANGLE MAT. USED 2024-T3 CLAD .071''PER. REF. SRM 51-30-01-0G-0;[07] PERFORMED HFEC INSP. ON FORMED REPLACEMENT ANGLE AND SPLICE ANGLE IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. NO CRACKS NOTED<BR>TOOL: NORTEC 600 B/C: 166317 DUE: 10/31/23;[08] CUT THE ATTACH ANGLE AT CENTER WING REAR SPAR VAPOR BARRIER WEB (UPPER ANGLE) REF SRM 57-10-10-2R-5 FIGURE 202 REPAIR 5 SHEET 4.;[09] VERIFIED STEP 8;[10] FINALIZED FABRICATION ON REPLACEMENT ANGLE AS PER SRM 57-10-10-2R-5. REPAIR 5; FIG. 202; DETAIL B.;[11] PERFORMED HFEC ROTO INSP ON FASTENER OPEN HOLES; IAW B 737 NDT PART 6 51-00-00 PROCE 16. TOOL NORTEC 600. BC 166316. CALIB DUE 10-17-23. NO CRACKS FOUND.;[12] FINALIZED FABRICATION ON SPLICE ANGLE AS PER SRM 57-10-10-2R-5. REPAIR 5; FIG. 202; DETAIL B.;[13] LOCATED & DRILLED REPAIR PARTS AS PER SRM 57-10-10-2R-5. REPAIR 5; FIG. 202; DETAIL B.

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

MAIN CABIN INTERCOSTAL ANGLE BETWEEN STA 380-400 RBL40' CRACKED<[01] REMOVED INTERCOSTAL ANGLE AT MAIN CABIN BETWEEN STA 380-400 RBL 40'' AS PER SRM 51-40-02-0G-0;[02] FABRICATED INTERCOSTAL ANGLE P/N 143A5410-174 . PER DWG # 1434A5400. AND 143A5410. FROM MATERIAL BAC1490 2843- 7075-0. PENDING FOR HEAT TREATMENT.;[03] VERIFIED STEP 1;[04] VERIFIED STEP 2;[05] HEAT TREATED INTERCOSTAL ANGLE TO T62 AS PER REF BAC 5602 AND FORMED OP 84;[06] VERIFIED STEP 5;[07] OK TO TREAT AND PRIME;[08] TREATED AND PRIMED INTERCOSTAL ANGLE AT MAIN CABIN BETWEEN STA 380-400 RBL40' AS PER REF AMM-51-21-72-370-803 AND SRM-51-20-01-OG-0.;[09] VERIFIED STEP 8;[10] OK TO INSTALL INTERCOSTAL;[11] INSTALLED INTERCOSTAL AT MAIN CABIN BETWEEN STA 380-400 RBL 40' AS PER SRM 51-40-02 AND DWG 143A5400.;[12] C/W;[13] VERIFIED STEP 11

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

MAIN CABIN FLOOR PANEL 221GF O/B FWD END CRACKED<[01] RECEIVED FLOORBOARD AND WILL BE INSTALLED ON T/C TTG8Q00FV86G;[02] VERIFIED STEP 1

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

MAIN CABIN INTERCOSTAL ANGLE BETWEEN STA 380-400 LBL13' CRACKED<[01] REMOVED INTERCOSTAL ANGLE AT MAIN CABIN BETWEEN STA 380-400 LBL13' AS PER SRM 51-40-02.;[02] VERIFIED STEP 1 OK TO INSTALL NEW ANGLE;[03] INSTALLED NEW ANGLE AT MAIN CABIN STA 380-STA 400 LBL 13' AS PER SRM 51-40-02 AND DWG 143A5400.;[04] VERIFIED STEP 3

Part: BEAM — CORRODED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

MAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM UPPER SURFACE STA 986.5 LBL 42'<[01] REMOVED CORROSION AT MAIN CABIN AFT WET AREA AT FLOOR BEAM UPPER SURFACE STA 986.5 LBL 42' REF SRM 51-10-02-0G-0.<BR><BR>ORIGINAL MATERIAL 0.150'; REMAINING MATERIAL 0.090'; MATERIAL REMOVED 0.060'. THEREFORE; THE REWORKED AREA IS OUT OF LIMITS REF SRM 53-70-51-1A-1; FIGURE103; DETAIL C] FABRICATED ONE REPAIR STRAP FROM 0.100' 7075-T6 CLAD SHEET; ONE REPAIR ANGLE FROM BAC1490-2887 7075-T6 AND ONE FILLER FROM 0.150' 7075-T6 REF SRM 53-70-51-2R-6 REPAIR 6; TABLE 204; ALTERNATIVE 4. JOB ACCOMPLISHED BY RICARDO SAMANIEGO EMP. #35463<BR><BR>ACCOMPLISHED 125 MICROINCHES SURFACE TEST ON REPAIR PARTS REF SRM 51-20-13-0G-0. TOOL ID# 172331. JOB ACCOMPLISHED BY RICARDO SAMANIEGO EMP. #35463;[19] LOCATED AND DRILLED REPAIR PARTS AND REPAIR AREA REF SRM 53-70-51-2R-6 REPAIR 6; FIGURE 205; ALTERNATIVE 4 AND SRM 51-40-05-0G-0. JOB ACCOMPLISHED BY RICARDO SAMANIEGO EMP. #35463[26] INSTALLED REPAIR PARTS (REPAIR STRAP; REPAIR ANGLE AND FILLER) AND NUTPLATE AT FLOOR BEAM UPPER SURFACE STA 986.5 LBL 42' REF SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 4; FIGURE 205<BR><BR>MIXED SEALANT 21:00 PM; APPLIED SEALANT 21:15PM; SQUEEZE OUT 21:30PM

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

MAIN CABIN INTERCOSTAL BETWEEN STA 270-294.5 BL0' CRACKED<[01] REMOVED INTERCOSTAL AT MAIN CABIN BETWEEN STA; 270-294.5 BLO ' PER. REF. SRM 51-40-02-0G-0;[02] DRILLING IN PLACE NEW INTERCOSTAL PER. REF. 51-40-05-0G-0;[03] VERIFIED STEPS 1AND 2 OK TO INSTALL NEW INTERCOSTAL;[04] INSTALLED NEW INTERCOSTAL AT MAIN CABIN BETWEEN STA.270-294.5 BL0'' PER. REF. SRM51-40-02-0G-0 AND DRW.141A5400;[05] CORRECTION ON STEP 4 INSTALLED NEW INTERCOSTAL AT MAIN CABIN BETWEEN STA.270-294.5 BL0'' PER. REF. SRM51-40-02-0G-0 AND DWG.141A5400;[06] VERIFIED STEP 5

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

MAIN CABIN INTERCOSTAL BETWEEN STA 312-328 RBL33' CRACKED<[01] REMOVED INTERCOSTAL AT MAIN CABIN BETWEEN STA 312-328 RBL 33' 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. 312 - 328; RBL 33; AS PER SRM 51-40-02-0G-0 & DWG. 141A5410 & 141A5400.;[04] VERIFIED STEP 3

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

MAIN CABIN FLOOR PANEL 221BF O/B AFT END CRACKED AND TWO EACH DAMAGE INSERTS<[01] RECEIVED FLOOBOARD AND WILL BE INSTALLED ON T/C TTG8Q00FV86S;[02] CORRECTION ON STEP 1 RECEIVED FLOORBOARD AND WILL BE INSTALLED ON T/C TTG8Q00FV86S;[03] VERIFIED STEP 2;[04] THIS TTG8Q00H7EWV ITEM WAS CLOSED IN ERROR GENERATED NEW ITEM TTG8Q00HFHX5;[05] CORRECTION ON STEP 3 ENTER IN ERROR

Part: SEAT TRACK — CORRODED (ZN 100 FUS LOWER) · airframe 52,335 hrs · 31,548 cycles

MAIN CABIN CORROSION AT SEAT TRACK CROWN TOP RBL 24.75 STA 380+1'<[01] REMOVED CORROSION AT MAIN CABIN SEAT TRACK CROWN TOP RBL 24.75 STA 380+1' AS PER SRM 51-10-02;[02] MATERIAL REMOVED AT TOP CROWN: 0.032'; FOUND OUT OF LIMITS AS PER SRM 53-00-52-1A-1; FIG. 103.;[03] REMOVED FASTENERS AS REQUIRED AT SEAT TRACK RBL 24.75 STA. 380+1'' PER REF SRM 51-40-02-0G-0;[04] CUT & REMOVED THE DAMAGED PART OF THE SEAT TRACK BETWEEN STA 400 - 420. CUT THE WEB & THE LOWER HORZ. FLANGES OF INITIAL SEAT TRACK WHERE THE SPLICE WILL BE MADE; AS PER SRM 53-00-52-2R-4 REPAIR 4; FIG.202.;[05] STARTED FABRICATION THE NEW SEAT TRACK SECTION FROM EXTRUSION BAC1520-2789 7178-T6511; AS PER SRM 53-00-52-2R-4 REPAIR 4;[17] RE-LOCATED & RE-INSTALLED SEAT TRACK FROM STA 420- STA 460 RBL 24.75 DISPLACED ON STEP 11; REF SRM 53-00-52-2R-4 REPAIR 4;[18] RE-LOCATED & RE-INSTALL FASTENERS OF PULLEY BRACKET AT STA 400 RBL 24.75 X3 (HI LOK); DISPLACED ON STEP #10; REF SRM 51-40-02-0G-0.;[19] VERIFIED STEPS 16-17;[20] TASK C/W

Part: SLIDE — DISLODGED (FWD SERVICE DOOR) · airframe 52,326 hrs · 31,543 cycles

FWD SERVICE DOOR SLIDE FELL OUT OF CASE<[01] REPACKED FWD SERVICE DOOR SLIDE INTO CASE AND INSTALLED ON FWD SERVICE DOOR PER AMM 25-66-01

Part: LIGHT — LOOSE (CABIN) · airframe 52,243 hrs · 31,485 cycles

EXIT SIDE LIGHT ASSEMBLY FORWARD ENTRYT DOOR COVER LOOSE AND LIGHT INOPERATIVE. REMOVED & REPLACED EXIT SIDE LIGHT ASSY. FWD ENTRY DOOR IAW MM 33-51-01.

Part: SLIDE — LOW PRESSURE (ZN 900 LAV/GALLE) · airframe 52,212 hrs · 31,467 cycles

DOOR 2R SLIDE PRESSURE AT LOW LIMIT<[01] REMOVED AND REPLACED R2 ESCAPE SLIDE PER AMM 25-66-01

Part: PANEL — ELONGATED (FUSELAGE) · airframe 49,543 hrs · 29,710 cycles

FAIRING PANEL 193D HAS MULTIPLE ELONGATED FASTENER HOLES / [01] NEW PANEL INSTALLED<BR>TSR 2022001125

Part: PANEL — CRACKED · airframe 49,543 hrs · 29,710 cycles

FAIRING PANEL 193D HAS MULTIPLE BULGING/CRACKING FASTENER HOLES / [01] NEW PANEL INSTALLED<BR>TSR 2022001125

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,589 hrs · 27,959 cycles

RIGHT AFT WING TO BODY FAIRING EXTERNAL EMERGENCY LIGHT INOP. / RELAMPED RIGHT AFT WING TO BODY FAIRING EXTERNAL EMERGENCY LIGHT AS PER BOEING B737 AMM 33-51-04-960-801 OPS CHECK NORMAL

Part: ANGLE — WORN (FUSELAGE) · airframe 46,589 hrs · 27,959 cycles

R/H UPPER FUSELAGE AFT FIN TO BODY INTERFACE CLOSURE ANGLE FWD SECTION HAS WEAR MARK. / REPAIRED FUSELAGE FIN TO BODY INTERFACE- CLOUSURE ANGLE R/H FWD SECTION PER REF B737-700 SRM 53-80-71-2R-6 REPAIR 6. STA 1026 RBL 12; WATER LINE 305.5

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 46,589 hrs · 27,959 cycles

FLIGHT COMPARTMENT COCKPIT DOOR FLOOR AREA STA 250 TO STA 270 RBL10 EXISTING REPAIR HAS A DENT / RESTORED AREA TO PRIOR CONFRIGURATIONREFERENCE EA 1-753-34270 REVIR DATED 28-FEB-2019.' ANY FOLLOW ON INSPECTION WILL CONTINUE TO BE TRACKED ON ORIGINAL NRC T893111'

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 46,589 hrs · 27,959 cycles

R/H HORIZONTAL STABILIZER INTERNAL SURFACE RIB #4 STIFFENER #3 CRACKED. / REPAIRED R/HORIZNTAL STAB. MACHINED INSPAR RIB #4 SHIFFENER #3 PER REF B737-700 SRM 55-10-09-2R-4

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 46,589 hrs · 27,959 cycles

L/H STABILIZER INTERNAL SURFACE RIB #4 STIFFENER #3 CRACKED. / ACCOMPLISHED REPAIR AT LH INTERNAL SURFACE RIB #4 STIFFENER #3 PER B737-700 SRM 55-10-09-2R-4

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 46,589 hrs · 27,959 cycles

AFT CARGO COMPARTMENT PANEL 142YEC CRACKED. /

Part: SHROUD — CRACKED (AFT BULKHEAD) · airframe 46,589 hrs · 27,959 cycles

AFT CARGO FWD BULKHEAD SHROUD P/N 453A2510-2 CRACK AND PREVIOUS REPARED / REMOVED DAMAGE SHROUD P/N 453A2510-2 AND INSTALLED NEW PANEL; P/N 453A2510-2;ON AFT CARGO FWD BULKHEAD PER REF B737 AMM 25-52-18-000-801 AND 25-52-18-400-801

Part: SIDEWALL PANEL — CRACKED (AFT CARGO) · airframe 46,589 hrs · 27,959 cycles

AFT CARGO COMPARTMENT L/H SIDEWALL PANEL 141AW CRACKED. /

Part: SIDEWALL PANEL — CRACKED (AFT CARGO) · airframe 46,589 hrs · 27,959 cycles

AFT CARGO COMPARTMENT L/H SIDEWALL PANEL 141EW CRACKED. /

Part: SIDEWALL PANEL — CRACKED (AFT CARGO) · airframe 46,589 hrs · 27,959 cycles

AFT CARGO COMPARTMENT R/H SIDEWALL PANEL 142BW CRACKED AND TORN. /

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 46,589 hrs · 27,959 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140BF CRACKED. / REMOVED AFT CARGO COMPT. FLOOR PANEL 140BF AS PER REF B7377 AMM 25-52-10-000-801. FABRICATED NEW FLOOR PANEL 140 BF AS PER REF B737 AMM 25-52-01-201-801 USING REMOVED PANEL AS A TEMPLATE. INSTALLED NEW AFT CARGO COMPT. FLOOR PANEL 140BF AS PER REF B737 AMM 25-52-10-400-801.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 46,589 hrs · 27,959 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140AF CRACKED AND TORN. / REMOVED AFT CARGO COMPT. FLOOR PANEL 140AF AS PER REF B737 AMM 25-52-10-000-801.FABRICATED NEW PANEL 140AF AS PER REF B737 AMM 25-52-01-201-801 USING REMOVED LINER AS A TEMPLATE. INSTALLED AFT CARGO COMPT. FLOOR PANEL 140AF AS PER REF B737 AMM 25-52-10-400-801.

Part: SCUFF PLATE — CORRODED (AFT CARGO) · airframe 46,589 hrs · 27,959 cycles

CORROSION AFT CARGO COMPARTMENT FLOOR @ STA 787 FWD SCUFF PLATE HAS CORROSION. RBL 13' AND W.L. 155.5 / REMOVED CORRORED PLATE AND INSTALLED NEW PLATE PN AFT CARGO COMPARTMENT STA 787 RBL 13; PER REF 737 SRM 51-40-02-0G-0 AND DRAWING NO. 453A2611

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 46,223 hrs · 27,731 cycles

FWD OUTSIDE EMERGENCY FLASHLIGHT INOPERABLE. R & R FWD OUTBOARD EMERGENCY FLASHLIGHT BATTERY ASSEMBLY, PER AMM 25-64-00. OPERATIONS CHECK GOOD.

Part: BULKHEAD WEB — CANNING (BS 663) · airframe 45,817 hrs · 27,480 cycles

REFERENCE WORK CARD J11415446 DURING REINSPECTION OF THE CRACK AT LBL 45 LEFT WHEEL WELL FOUND CRACK TO GROW TO A TOTAL LENGTH OF APPROX 8.25 INCHES. / STOPPED DRILLED THE CRACK PER SRM 51-10-02 AND EA 1-A57-13410. APPLIED SPEED TAPE

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 45,687 hrs · 27,400 cycles

DURING INSPECTION OF THE CENTER REAR SPAR VAPOR BARRIER WEB FOUND APPROXIMATELY 3.75 INCH VERTICAL HAIR LINE CRACK BETWEEN RBL 40-43 RT WHEEL WELL REF SRM 57-10-10 FOR ALLOWABLE LIMITS. MOD/PERFORMED INTERIM REPAIR OF CENTER REAR SPAR VAPOR WEB @ RBL 40-43, REF EA 1-A57-13410. PERMANENT ACTION REQUIRED: ACCOMPLISH A PERMANENT REPAIR AS GIVEN IN 737-700 SRM 51-70-04. REPAIR 10 OR AS AN ALTERNATIVE REPAIR PART OF THE CRACK SO THAT THE CRACK LENGTH IS LESS THAN OR EQUAL TO THE MAXIMUM ALLOWABLE DAMAGE LIMIT. APPLY THE INTERIM SEAL OVER THE CRACK THAT IS LEFT AS GIVEN IN 737-700 SRM 57-10-10 PARA 2.C.(4) ALLOWABLE DAMAGE 2.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 45,687 hrs · 27,400 cycles

DURING INSPECTION OF THE CENTER WING REAR SPAR VAPOR WEB FOUND CRACK RUNNING VERTICALLY APPROX 7.75 INCHES IN LENGTH AT LBL 45 LEFT WHEEL WELL, REF SRM 57-10-10 FOR ALLOWABLE LIMITS. MOD / PERFORMED INTERIM REPAIR OF CENTER WING REAR SPAR VAPOR WEB @ LBL 45 REF EA 1-A57-13410. PERMANENT ACTION REQUIRED: ACCOMPLISH A PERM REPAIR AS PER 737-700 SRM 51-70-04, REPAIR 10 OR AS AN ALTERNATIVE; REPAIR PART OF THE CRACK SO THAT THE CRACK LENGTH IS LESS THAN THE TOTAL ALLOWABLE DAMAGE LIMIT. APPLY THAT INTERIM SEAL OVER THE CRACK THAT IS LEFT AS GIVEN IN 737-700 SRM 57-10-10 PARA 2.C. (4) ALLOWABLE DAMAGE 2.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 44,955 hrs · 26,937 cycles

AFT SVC DOOR ESCAPE SLIDE NEEDS REPOSITIONED. / REPOSITIONED AFT SVC DOOR ESCAPE SLIDE PER MT 725-61-05.

Part: COUNTER — FAULTY (COCKPIT) · airframe 43,631 hrs · 26,111 cycles

DIVERSION/DECLARED EMERGENCY--------------------------------------------------------IN CRUISE AT FL 380, NOTICED SMOKE COMING FROM CAPTAIN'S TRIP IDENTIFICATION COUNTER. FOLLOWED SMOKE, FIRE, FUME CHECKLIST AND TURNED MAIN PANEL LIGHTING KNOB TO OFF. SMOKE DISSIPATED BUT ELECTRICAL ODOR IS STILL PRESENT. ODOR DISSIPATED AFTER ARRIVING AT GATE. / PERFORMED FIM TASK 21-00 TASK 806 FOUND CAPTAIN'S TRIP IDENTIFICATION COUNTER AT FAULT. R&R CAPTAIN'S TRIP COUNTER PER AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 41,217 hrs · 24,597 cycles

R1 DOOR SLIDE LOOSE. R&R SLIDE PER MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,169 hrs · 24,567 cycles

EMERGENCY EXIT LIGHTS BATTERY PACK M1673 INOP. R&R BATTERY PACK IAW AMM.

Part: GUARD — BROKEN (EMERGENCY LIGHT) · airframe 41,169 hrs · 24,567 cycles

AFT FLIGHT ATTENDANT CONTROL PANEL EMERGENCY LIGHT SWITCH GUARD SPRING BROKEN. R&R SWITCH GUARD PER AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 41,169 hrs · 24,567 cycles

EMERGENCY EXIT LIGHTS INOP AT LOCATION M1669. R&R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 41,169 hrs · 24,567 cycles

EMERGENCY EXIT LIGHTS INOP AT LOCATION M1668. R&R POWER SUPPLY IAW AMM.

Part: STRAP — FRAYED (L2 DOOR) · airframe 41,169 hrs · 24,567 cycles

L2 DOOR ASSIST HANDLE STRAP FRAYED. R&R STRAP IAW AMM.

Part: HANDLE — CRACKED (L2 DOOR) · airframe 41,169 hrs · 24,567 cycles

L2 DOOR ASSIST HANDLE CRACKED. R&R HANDLE IAW AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 41,169 hrs · 24,567 cycles

FWD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. / REPAIRED PER: EA 1-A53-2076 REV 11

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

AFT CARGO BAY WEB ATTACH ANGLE CORRODED BETWEEN BS 767 TO BS 787, RBL 21. R&R ANGLE PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 400 TO BS 420, RBL 26. R&R INTERCOSTAL PER DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

AFT CARGO BAY ON RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 22. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

AFT CARGO BAY FORWARD BULKHEAD SUPPORT CRACKED AT BS 727, RBL 5. R&R SUPPORT PER DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

AFT CARGO BAY ON LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 22. REPAIRED SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CRACKED (AFT CARGO BAY) · airframe 41,169 hrs · 24,567 cycles

ACB R/H FLOOR TO SIDEWALL CRACKED AT STA 727 RBL 20 WL 163(MARKED) / ACB R/H FLOOR TO SIDEWALL SUPPORT AT BS 727 WILL BE REPLACED SWA DEFECT # T893299

Part: SPLICE — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

AFT CARGO BAY FLOOR T SPLICE CORRODED AT BS 887, BETWEEN LBL 9 TO RBL 12. R&R T SPLICE PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

AFT CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT CORRODED AT BS 947, RBL 16. R&R SUPPORT PER SRM AND DWG.

Part: SPLICE — CORRODED (AFT CARGO BAY) · airframe 41,169 hrs · 24,567 cycles

***CORROSION*** ON ACB FLOOR T SPLICE STA 767+6 LBL 9 RBL 12 WL 169 (MARKED) / OUT OF LIMITS - NO SRM LIMITS GIVEN. RECEIVED NEW PART ACB FLOOR T SPLICE STA. 767+6; LBL 9 - RBL 12; WL 169 P.O. # 723471/1 TO BE INSTALLED ON SWA CARD NO: JPANEL-141-CLOSE

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 767+6, RBL 3. R&R SUPPORT PER SRM & EA.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 22. R&R SHIELD PER SRM & DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

BULKHEAD TO FLOOR SUPPORT ANGLE BRACKET CRACKED AT BS 847+18, LBL 10. R&R BRACKET PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

AFT CARGO BAY ON RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 887 TO BS 947, RBL 22. R&R SUPPORT ASSEMBLY PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

AFT CARGO BAY ON RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 887, RBL 22. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

FORWARD CARGO RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 415 TO BS 420, RBL 21. R&R SUPPORT PER DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

FORWARD CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 480+10 SPLICE TO BS 500D, LBL 21. R&R SUPPORT IAW DWG & SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 41,169 hrs · 24,567 cycles

FWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED. / REPAIRED PER: EA 1-A53-2076 REV 11

Part: ANCHOR — CORRODED (AFT CARGO BAY) · airframe 41,169 hrs · 24,567 cycles

***CORROSION*** ON ACB NET TIE DOWN ANCHOR PLATE AFT OF DOOR / REMOVED & REPLACED A.C.B. TIE DOWN ANCHOR PLATE AFT OF DOOR INSTALLED PER AMM 25-52-10-400-801

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

FORWARD CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 21. R&R SUPPORT PER SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

FORWARD CARGO DOORWAY LOWER THRESHOLD SUB WEB CORRODED BETWEEN BS 440 TO BS 495, RBL 22. R&R WEB PER SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

FORWARD CARGO FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 495 TO BS 500A, RBL 21. R&R SHIELD IAW DWG & SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

FORWARD CARGO FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 420 TO BS 440, RBL 21. R&R SHIELD IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

AFT CARGO DOORWAY LOWER THRESHOLD INBOARD STRAP LOWER SURFACE NUTPLATE STRIP CORRODED BETWEEN BS 794 TO BS 802, RBL 21. R&R STRAP PER SRM AND DWG.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 41,169 hrs · 24,567 cycles

***CORROSION*** AFT CARGO DOORWAY; LWR THRESHOLD IB STRAP; BS 787 TO BS 850; RBL 21; WL 156 / CORROSION ON STRAP P/N 146A8128-14 WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; REMOVED STRAP BS 787-BS850; RBL 21; WL156 PER SRM 51-40-02-0G-0; INSTALLED NEW THRESHOLD STRAP BS 787-BS850; RBL21; WL156 PER SRM 51-40-02-0G-0; DWG 146A8120; DWG 146A8349 DWG 146A0081 93114U 26FEB19

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

AFT CARGO DOORWAY, LOWER THRESHOLD INBOARD INTERCOSTAL UPPER FLANGE, LOWER SURFACE AT NUTPLATE HOLES CORRODED BETWEEN BS 794 TO BS 847, RBL 21. R&R INTERCOSTAL PER SRM & DWG.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

AFT CARGO BAY DOOR CUT OUT AFT CORNER SCUFF PLATE CRACKED. R&R SCUFF PLATE ASSEMBLY PER AMM.

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 41,169 hrs · 24,567 cycles

***CORROSION*** AFT CARGO DOORWAY; LWR THRESHOLD SUBWEB; BS 794 TO BS 847; RBL 22; WL 156 / CORROSION ON WEB P/N 156A8123-25 WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; REMOVE LWR THRESHOLD WEB BS794-BS847 RBL 22; WL 156; PER SRM 51-40-02-0G-0; INSTALLED NEW ACB LWR THRESHOLD WEB BS 794-BS847; WL 156 PER SRM 51-40-02-G0-0 DWG 146A8340

Part: STRIP — CORRODED (AFT CARGO) · airframe 41,169 hrs · 24,567 cycles

***CORROSION*** AFT CARGO FLOOR TO SIDEWALL SHIELD; BS 767 TO BS 794; RBL 21; WL 156 / CORROSION ON SHIELD P/N 156A8127-12 WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; REMOVED ACB SHIELD BS 767-BS794 RBL 21; WL 156. PER SRM 51-40-02-0G-0 INSTALLED NEW SHIELD BS767-BS794; RBL 21; WL 156 PER SRM 51-40-02-0G-0; DWG 146A0081

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

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

Part: SEAL — CRACKED (RH HOR STAB) · airframe 41,169 hrs · 24,567 cycles

RT HORIZ. STAB UPPER FWD SLIDE SEAL IS CRACKED. / REMOVED AND REPLACED R/H HORIZONTAL STAB CRACKED UPPER FWD SLIDE SEAL IAW AMM 53-31-31-000-802 PAR. 2 D AND E AND 53-31-31-400-802 PAR 3D AND E. 57048U 26FEB19

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

FLOOR SUPPORT CRACKED AT BS 540, BETWEEN BL 0 TO LBL 25. R&R FLOOR SUPPORT IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

FORWARD CARGO FLOOR TO AFT BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN LBL 20 TO RBL 20. R&R ANGLE PER SRM AND DWG.

Part: BULKHEAD — DEBONDED (RT MLG WW) · airframe 41,169 hrs · 24,567 cycles

LOWER COMPOSITE BULKHEAD REPAIR DEBONDED AT BS 663, RBL 32. REPAIRED BULKHEAD IAW SRM.

Part: BULKHEAD — DEBONDED (LT MLG WW) · airframe 41,169 hrs · 24,567 cycles

LOWER COMPOSITE BULKHEAD REPAIR DEBONDED AT BS 663, LBL 32. REPAIRED BULKHEAD IAW SRM.

Part: PANEL — CORRODED (NLG WHEEL WELL) · airframe 41,169 hrs · 24,567 cycles

NOSE WHEEL WELL PANEL 113BW HAS CORROSION / RECEAVED NEW PANEL 7320579/NEW FOR TRACKING ONLY TO BE INSTALLED ON NRC T892801

Part: RETAINER — CRACKED (RT WING) · airframe 41,169 hrs · 24,567 cycles

RT WING UPPER T/E PANEL JUST AFT OF #2 PYLON VERT SEAL RETAINER IS CRACKED. / REMOVED AND REPLACED RT WING UPPER T/E PANEL AFT OF #2 PYLON VERTICAL SEAL RETAINER IAW SOPM 20-50-01 AND SRM 51-40-02-0G-0 84036U 13FEB19

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 41,169 hrs · 24,567 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN LBL 25 TO LBL 45. REPAIRED WEB PER SRM.

Part: PANEL — CORRODED (NLG WHEEL WELL) · airframe 41,169 hrs · 24,567 cycles

NOSE WHEEL WELL PANEL 113AC HAS CORROSION / RECEAVED NEW PANEL 7320265 FOR TRACKING ONLY TO BE INSTALL ON NRC T892801

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

COCKPIT FLOOR CREASED AT BS 257, BETWEEN LBL 4 TO LBL 15. REPAIRED COCKPIT FLOOR PER ER & EA.

Part: PANEL — CORRODED (NLG WHEEL WELL) · airframe 41,169 hrs · 24,567 cycles

NOSE WHEEL WELL PANEL 114AC HAS CORROSION / RECEAVED PANEL 7320265/NEW FOR TRACKING ONLY TO BE INSTALLED ON NRC T892801

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

FLOOR SUPPORT ANGLE CRACKED BETWEEN BS 380 TO BS 400, LBL 1. R&R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

FLOOR SUPPORT ANGLE CRACKED AT BS 540, BETWEEN BL 0 TO RBL 25. R&R ANGLE IAW SRM & DWG.

Part: PANEL — CORRODED (NLG WHEEL WELL) · airframe 41,169 hrs · 24,567 cycles

NOSE WHEEL WELL PANEL 114BW HAS CORROSION / RECEAVED NEW PANEL 7320579/NEW FOR TRACKING ONLY TO BE INSTALLED ON NRC T892801

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

R1 DOOR CUTOUT ANGLE CRACKED AT BS 294, RBL 52. R&R ANGLE PER SRM AND DWG.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

L1 DOOR MOPSILL INNER CHORD CRACKED AT BS 303, LBL 51. R&R MOPSILL IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 986, RBL 45. REPAIRED BEAM PER ER AND EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

R1 DOOR MOPSILL CORRODED BETWEEN BS 950 TO BS 993, RBL 50. R&R MOPSILL PER SRM & DWG.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 41,169 hrs · 24,567 cycles

LT CREASE BEAM INNER CHORD CRACKED COMMON TO FASTENER HOLE CRACKED AT BS 639, LBL 65. R&R CHORD PER SRM PER DWG & SRM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 40,815 hrs · 24,320 cycles

L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER (DID NOT DEPLOYED). REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 40,463 hrs · 24,082 cycles

L1 DOOR SLIDE DISLODGED. R&R SLIDE PER MT.

Part: INTERCOSTAL — CRACKED (E & E COMPT) · airframe 38,781 hrs · 22,975 cycles

ELECTRICAL AND ELECTRONICS COMPARTMENT CENTER INTERCOSTAL LOCATED BETWEEN BS344 AND BS360 IS CRACKED AT THE NUTPLATE / REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02 AND SRM 51-10-02

Part: BATTERY — FAILED (CABIN) · airframe 38,781 hrs · 22,975 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01672. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 38,781 hrs · 22,975 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01670. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 38,781 hrs · 22,975 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01675. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 38,781 hrs · 22,975 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01669. R&R BATTERY PER AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 38,253 hrs · 22,627 cycles

L2 DOOR SLIDE OUT OF POSITION. R & R THE SLIDE IAW MT.

Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 38,053 hrs · 22,495 cycles

FWD CARGO BIN; AFT FLOOR BOARD FWD EDGE IS CRACKED THROUGH LINE. / R&R'D FLOOR PANEL PER M/M 25-52-10

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,685 hrs · 20,409 cycles

LEFT EMERGENCY EXIT ROW SIDE WALL LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 34,552 hrs · 20,330 cycles

LEFT MLG WHEEL WELL BULKHEAD WEB CRACKED AT BS 663, LBL 35. REPAIRED THE BULKHEAD WEB IAW EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 34,468 hrs · 20,285 cycles

LEFT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FACE FITTING CORRODED. REPAIRED THE FITTING IAW EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 34,468 hrs · 20,285 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FACE FITTING CORRODED. REPAIRED THE FITTING IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 34,345 hrs · 20,211 cycles

RT MAIN WHEEL WELL VAPOR BARRIER CRACKED AT BS 663, RBL 40. REPAIRED BARRIER IAW SRM.

Part: WEB — CRACKED (RT WING) · airframe 34,345 hrs · 20,211 cycles

RT WING TRANSVERSE WEB CRACKED AT UPPER OUTBOARD FASTENER HOLE. R&R WEB IAW SRM.

Part: HOOK — CORRODED (CABIN) · airframe 34,345 hrs · 20,211 cycles

RT EMERGENCY EXIT HATCH STRAP HOOK CORRODED. R&R HOOK IAW AMM.

Part: FAIRING — CRACKED (RT WING TE FLAP) · airframe 34,345 hrs · 20,211 cycles

RIGHT WING FLAP TRACK FAIRING 642AB, FOUND CRACKED ON INBOARD SIDE. REPAIRED THE FAIRING IAW EA.

Part: HOUSING — BROKEN (CABIN) · airframe 34,345 hrs · 20,211 cycles

CENTER CEILING EXIT LIGHT HOUSING ASSEMBLY BROKEN. R&R LIGHT ASSEMBLY PER AMM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 34,345 hrs · 20,211 cycles

RT MAIN WHEEL WELL BULKHEAD CRACKED AT BS 663, RBL 43. REPAIRED BULKHEAD PER SRM.

Part: LENS — MISSING (EXIT SIGN) · airframe 34,327 hrs · 20,194 cycles

RT OVERWING EMERGENCY EXIT SIGN LIGHT LENS MISSING. R&R LENS IAW AMM.

Part: PRESSURE SWITCH — FAILED (FUEL SYSTEM) · airframe 33,668 hrs · 19,817 cycles

AIR TURNBACK, ON CLIMB THROUGH FL 280 NR 1 FUEL BOOST PUMP FORWARD LIGHT ILLUMINATED STEADY UNTIL OFF AT FL320. R&R NR 1 FORWARD FUEL BOOST PUMP PRESSURE SWITCH IAW AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 33,521 hrs · 19,736 cycles

FORWARD LOWER FLASHLIGHT STRAP BROKEN. R&R STRAP PER SIP.

Part: SIGN — BROKEN (CABIN) · airframe 32,130 hrs · 18,935 cycles

RIGHT EMER EXIT DOOR SIGN BROKEN. R & R SIGN IAW MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 32,060 hrs · 18,889 cycles

R2 DOOR SLIDE PRESS LOW. R & R SLIDE IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 30,679 hrs · 18,107 cycles

L1 DOOR, LOWER EMER EXIT LENS BROKEN. R & R LENS ASSEMBLY IAW SIP.

Part: FLAP — DELAMINATED (RT WING) · airframe 28,187 hrs · 16,625 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED AT AFT INBD CORNER. REPAIRED AFT FLAP IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

FORWARD GALLEY Z ANGLE CORRODED AROUND NUTPLATE HOLES. R & R Z ANGLE IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,187 hrs · 16,625 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STABILIZER STATION 92.70, CRACKED IN VERTICAL WEB STIFFENER 19" FROM FWD SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 28,187 hrs · 16,625 cycles

LEFT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT STABILIZER STATION 101.90, 19" AFT OF FRONT SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 28,187 hrs · 16,625 cycles

LEFT HORIZONTAL STABILIZER INBD SIDE OF RIB CRACKED AT STABILIZER STATION 101.90, 28" AFT OF FRONT SPAR ON LOWER FLANGE. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,187 hrs · 16,625 cycles

RIGHT HORIZONTAL STABILIZER INBD SIDE OF RIB AT STABILIZER STATION 92.70, CRACKED IN VERTICAL WEB STIFFENER 9.5" FROM FWD SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 28,187 hrs · 16,625 cycles

LEFT HORIZONTAL STABILIZER INBD SIDE OF RIB CRACKED AT STAB STATION 101.90, 19" AFT OF FRONT SPAR ON LOWER FLANGE. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 28,187 hrs · 16,625 cycles

LEFT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT STABILIZER STATION 101.90, 28" AFT OF FRONT SPAR. REPAIRED RIB IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

INTERCOSTAL CRACKED AT BS 338, LBL 44. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

INTERCOSTAL CRACKED AT BS 320, LBL 44. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

INTERCOSTAL CRACKED AT BS 312, RBL 30. R & R INTERCOSTAL IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

FLOORBEAM WEB CRACKED AT BS 727B, LBL 45.5, AT THE VERTICAL FACE TOP HOLE. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

ANGLE CRACKED AT BS 727B, RBL 45.5. R & R ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

FLOORBEAM WEB CRACKED AT BS 727B, RBL 45.5, AT THE VERTICAL FACE 3RD HOLE UP. REPAIRED WEB IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

AFT CARGO CUT OUT STRUCTURE CLOSE OUT WEB UNDER CTR THRESHOLD SCUFF PLATE CORRODED BETWEEN BS 792 - 849. R & R WEB IAW SRM.

Part: PANEL — CORRODED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

FORWARD CARGO COMPARTMENT DOOR THRESHOLD PANEL CORRODED BETWEEN BS 400 - 492.5. R & R PANEL IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

ANGLE CRACKED AT BS 727B, LBL 24.75. R & R ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

KEPT ANGLE CRACKED AT BS 727B, LBL 45.5. REPAIRED ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

FLOORBEAM CRACKED AT BS 727B, RBL 45.5, AT THE INBD OF THE SEAT TRACK. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 24.75, AT THE UPPER FASTENER HOLE. REPAIRED BEAM IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

ANGLE CRACKED AT BS 727B, RBL 24.75. R & R ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

FLOORBEAM CRACKED AT BS 727B, LBL 45.5, OTBD OF THE SEAT TRACK. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

FLOORBEAM CRACKED AT BS 727B, RBL 45.5, INBD OF THE SEAT TRACK. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

FLOORBEAM CRACKED AT BS 727B, RBL 24.75, OTBD OF THE SEAT TRACK. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

FLOORBEAM CRACKED AT BS 727B, RBL 24.75, INBD OF THE SEAT TRACK. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

FLOORBEAM CRACKED AT BS 727B, RBL 45.5, OTBD OF THE SEAT TRACK. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

FLOORBEAM CRACKED AT BS 727B, LBL 24.75, OTBD OF THE SEAT TRACK. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

FLOORBEAM CRACKED AT BS 727B, LBL 45.5, INBD OF THE SEAT TRACK. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

FLOORBEAM CRACKED AT BS 727B, LBL 24.75, INBD OF THE SEAT TRACK. REPAIRED BEAM IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,187 hrs · 16,625 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 28,152 hrs · 16,601 cycles

M1675 EMER BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 28,152 hrs · 16,601 cycles

M1672 EMER BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 28,152 hrs · 16,601 cycles

M1668 EMER BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 28,152 hrs · 16,601 cycles

M1674 EMER BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 28,152 hrs · 16,601 cycles

M1670 EMER BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 28,152 hrs · 16,601 cycles

M1673 EMER BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 28,152 hrs · 16,601 cycles

M1669 EMER BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 25,903 hrs · 15,263 cycles

CEILING OVERWING EMER EXIT LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,903 hrs · 15,263 cycles

FORWARD ENTRY EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,346 hrs · 12,611 cycles

FLOORBEAM INTERCOSTAL CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24.5. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 21,346 hrs · 12,611 cycles

FLOORBEAM INTERCOSTAL CRACKED AT BS 540, BETWEEN BL 0 TO LBL 24.5. REMOVED AND REPLACED INTERCOSTAL IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,346 hrs · 12,611 cycles

AFT CARGO ANGLE CRACKED AT BS 865, LBL 11. REMOVED AND REPLACED ANGLE PER SRM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 21,346 hrs · 12,611 cycles

RIGHT WHEEL WELL FIBERGLASS BULKHEAD CRACKED AT BS 663, RBL 42. REPAIRED BULKHEAD PER EA.

Part: PLATE — CRACKED (RT WING) · airframe 21,346 hrs · 12,611 cycles

RIGHT WING LOWER SHELF PANEL WAFFLE PLATE CRACKED UNDER PANEL 651EB I/B OF NR 6 FLAP TRACK. REMOVED AND REPLACED WAFFLE PLATE PER SRM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 21,346 hrs · 12,611 cycles

RIGHT WHEEL WELL FIBERGLASS BULKHEAD CRACKED AT BS 663, RBL 33. REPAIRED BULKHEAD PER EA.

Part: LIGHT — LOOSE (CABIN) · airframe 21,346 hrs · 12,611 cycles

RIGHT FWD EEPLS LOOSE. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 20,148 hrs · 11,919 cycles

AFT GALLEY EXIT LENS COVER LOOSE. RE-SECURED LENS IAW M/M.

Part: GIRT BAR — WORN (L1 DOOR) · airframe 19,012 hrs · 11,294 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOP RELEASE COLLAR WORN. REMOVED AND REPLACED GIRT BAR ASSY PER AMM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 19,012 hrs · 11,294 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 19,012 hrs · 11,294 cycles

LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 129.5. REPAIRED SKIN IAW SRM.

Part: COVER — LOOSE (CABIN) · airframe 18,961 hrs · 11,263 cycles

LEFT EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER IAW M/M.

Part: LENS — BROKEN (CABIN) · airframe 18,257 hrs · 10,871 cycles

LEFT EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED LENS PER MM.

Part: FASTENER — LOOSE (GIRT BAR) · airframe 17,767 hrs · 10,582 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED FASTENER PER SRM.

Part: LENS — MISSING (CABIN) · airframe 16,219 hrs · 9,700 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 2. REMOVED AND REPLACED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 15,450 hrs · 9,249 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 14,206 hrs · 8,522 cycles

DURING SCHEDULED HC2 CHECK FOUND, LT EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT ROW 16. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — CRACKED (CABIN) · airframe 14,206 hrs · 8,522 cycles

DURING SCHEDULED HC2 CHECK FOUND, EEPLS LENS CRACKED AT 1ABC. REMOVED AND REPLACED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 14,137 hrs · 8,478 cycles

EMERGENCY EXIT LIGHT COVER BROKEN/LOOSE L1 DOOR. REMOVED AND REPLACED L1 DOOR EXIT LIGHT ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 13,827 hrs · 8,293 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 10,115 hrs · 6,115 cycles

FWD EEPLS LOOSE. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 2,998 hrs · 1,748 cycles

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