N287WN

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 59,883 hrs · 36,253 cycles

GIRT BAR ON L1 DOOR HARD TO GET ON AND OFF CLIPS. RESECURED GIRT BAR ON L1 DOOR PER AMM 25-66-01.

Part: GIRT BAR — UNSECURE (ZONE 800) · airframe 59,862 hrs · 36,241 cycles

FAS REPORT L1 DOOR LEFT SIDE SLIDE GIRT BAR IS LOOSE. SECURED THE GIRT BAR TO CLIP IAW AMM 25-66-01. OPS CHKD GOOD.

Part: HANDLE — LOOSE (ZONE 800) · airframe 57,968 hrs · 35,069 cycles

FLT ATT ASSIST HANDLE AFT OF L1 DOOR IS LOOSE 2025-168124 <[01]. CORRECTED INSTALL ASSIST HANDLE AFT OF L1 DOOR I.A.W AMM 25-21-25-420-801 STEP 3. B. (5); [02] INSTALL ASSIST HANDLE AFT OF L1 DOOR I.A.W AMM 25-21-25-420-801 STEP 3. B. (5).

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,968 hrs · 35,069 cycles

FAULT RAISED TO CAPTURE MANDATORY MEASUREMENT OF CORROSION ON SUPPORT ZEE LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT ADDING RII LABOR ROW REMOVED BY ERROR ON FAULT TTG8Q00Z1GCE <[01]. REPLACED SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; [02] REPLACED SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. RII CERTIFIED.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 57,968 hrs · 35,069 cycles

CUSTOMER REQUEST AAI INSPECTION REFERENCE V909529 - PASSENGER CABIN STA 727B LBL 45.5 IB SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED. MISSING EA IDENTIFIER PER STEP 29 OF EA 130808. 2025-168072 <[01]. REPAIR SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. ON PASSENGER CABIN STA 727B LBL 45.5 IB IAW EA-130808 STEP 29.; [02] CORRECTED STEP 1. REPAIRED SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. ON PASSENGER CABIN STA 727B LBL 45.5 IB IAW EA-130808 REV P1 STEP 29.; [03] REPAIRED SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. ON PASSENGER CABIN STA 727B LBL 45.5 IB IAW EA-130808 REV P1 STEP 29.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 57,968 hrs · 35,069 cycles

CUSTOMER REQUEST AAI INSPECTION REFERENCE V909529 - PASSENGER CABIN STA 727B LBL 45.5 IB SEAT TRACK FLANGE AFT FASTENER HOLE CRACKED. MISSING EA IDENTIFIER PER STEP 29 OF EA 130808. 2025-168072<[01] REPAIR SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. ON PASSENGER CABIN STA 727B LBL 45.5 IB IAW EA-130808 STEP 29.;[02] CORRECTED STEP 1. REPAIRED SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. ON PASSENGER CABIN STA 727B LBL 45.5 IB IAW EA-130808 REV P1 STEP 29.;[03] REPAIRED SEAT TRACK FLANGE AFT FASTENER CORRECTLY MARKED LOC. ON PASSENGER CABIN STA 727B LBL 45.5 IB IAW EA-130808 REV P1 STEP 29.

Part: SKIN — CORRODED (ZONE 500) · airframe 57,968 hrs · 35,069 cycles

CORROSION ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 2025-168032<[01] TOOL USED ON STEP 4:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.;[02] TOOL USED ON STEP 5:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.;[03] TOOL USED ON STEP 7:ULTRASONIC THICKNESS GAGE P/N:45 MG; S/N:221860711; DUE DATE:20-DEC-25.;[04] PERFORMED PERMANENT REPAIR ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 EA #25-157-00651-WIP1 AND EA 25-157-00651. SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED PERMANENT REPAIR ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 EA #25-157-00651-WIP1 AND EA 25-157-00651. SEE INDIVIDUAL SIGN OFF BELOW.

Part: SKIN — CORRODED (ZONE 100) · airframe 57,968 hrs · 35,069 cycles

CORROSION ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 2025-168032 <[01]. TOOL USED ON STEP 4: EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.; [02] TOOL USED ON STEP 5: EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.; [03] TOOL USED ON STEP 7:ULTRASONIC THICKNESS GAGE P/N:45 MG; S/N:221860711; DUE DATE:20-DEC-25.; [04] PERFORMED PERMANENT REPAIR ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 EA #25-157-00651-WIP1 AND EA 25-157-00651. SEE INDIVIDUAL SIGN OFF BELOW.; [05] PERFORMED PERMANENT REPAIR ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 EA #25-157-00651-WIP1 AND EA 25-157-00651. SEE INDIVIDUAL SIGN OFF BELOW.

Part: BRACKET — CRACKED (ZONE 100) · airframe 57,968 hrs · 35,069 cycles

CRACK ON BRACKET STRUCTURE WING CENTER SECTION LOCATED BS540 AND BS578 AT LEVEL BL6 KEEL BEAM 2025-168021<[01]. REPLACED BRACKET LOCATED ON STRUCTURE WING CENTER SECTION BS540 AT LEVEL BL6 KEEL BEAM IAW B737 700 SRM 51-40-02-0G AND DWG 149A7701 SHEET 3 REV A.; [02] REPLACED BRACKET LOCATED ON STRUCTURE WING CENTER SECTION BS540 AT LEVEL BL6 KEEL BEAM IAW B737 700 SRM 51-40-02-0G AND DWG 149A7701 SHEET 3 REV A.

Part: PLATE — CRACKED (ZONE 600) · airframe 57,968 hrs · 35,069 cycles

CRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING 2025-168012 <[01]. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 45 REV-; AND EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMAGE IAW B737-700; MUST BE REPLACED; TOOK MEASURE OF CRACK IS L= 0.950? TOOL USED DIGITAL CALIPER P/N: 500-197-30; S/N: B23412298; DUE DATE: 10-NOV-25.; [02] CORRECTED STEP 1. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 45 REV-; AND EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMAGE IAW B737-700-SRM MUST BE REPLACED; TOOK MEASURE OF CRACK IS L= 0.950? TOOL USED DIGITAL CALIPER P/N: 500-197-30; S/N: B23412298; DUE DATE: 10-NOV-25.; [03] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS215 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 45 REV-; AND EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMAGE IAW B737-700-SRM MUST BE REPLACED; TOOK MEASURE OF CRACK IS L= 0.950? TOOL USED DIGITAL CALIPER P/N: 500-197-30; S/N: B23412298; DUE DATE: 10-NOV-25.

Part: SUPPORT — CORRODED (ZONE 10) · airframe 57,968 hrs · 35,069 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT 2025-167994<[01] FABRICATED A NEW SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW;[02] FABRICATED A NEW SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW

Part: SHIELD — CORRODED (ZONE 200) · airframe 57,968 hrs · 35,069 cycles

CORROSION ON SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT 2025-167993<[01] REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31 REV-.;[02] CORRECTED STEP 1. REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31 REV-. SEE INDIVIDUAL SING OFFS BELOW;[03] RII ITEM <BR>REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31 REV-. SEE INDIVIDUAL SING OFFS BELOW

Part: SHIELD — CORRODED (ZONE 100) · airframe 57,968 hrs · 35,069 cycles

CORROSION ON SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT 2025-167993<[01] REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31 REV-.;[02] CORRECTED STEP 1. REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31 REV-. SEE INDIVIDUAL SING OFFS BELOW;[03] RII ITEM <BR>REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL22 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 146A0081 SHEET 31 REV-. SEE INDIVIDUAL SING OFFS BELOW

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,968 hrs · 35,069 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT 2025-167994<[01] FABRICATED A NEW SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW;[02] FABRICATED A NEW SUPPORT ZEE LOCATED ON BTW BS727 TO BS767 WL156 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW

Part: TIE CLIP — CRACKED (ZONE 100) · airframe 57,968 hrs · 35,069 cycles

CRACK TIE CLIP LOCATED BS277 AND STR10R PASSENGER CABIN 2025-167974 <[01]. REPLACED NEW TIE CLIP LOCATED BS277 AND STR10R PASSENGER CABIN IAW B737-700 SRM-51-40-03-0G-O AND DWG-141A1110 SHEET 17 REV - . SEE INDIVIDUAL SIGN OFF BELOW.; [02] CERTIFIED CORRECTIVE ACTION STEP 1.

Part: ANGLE — CRACKED (ZONE 300) · airframe 57,968 hrs · 35,069 cycles

CRACK ANGLE BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB 2025-167865<[01] REPLACED ANGLE BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02;[02] REPLACED ANGLE BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02

Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 57,968 hrs · 35,069 cycles

CRACK ANGLE BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2025-167870<[01] REPLACED ANGLE BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02;[02] REPLACED ANGLE BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02

Part: NUT PLATE — CRACKED (ZONE 500) · airframe 57,968 hrs · 35,069 cycles

CRACK RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING 2025-167744<[01] REPLACED RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED

Part: STUB FRAME — CRACKED (ZONE 100) · airframe 57,968 hrs · 35,069 cycles

CRACK STUB FRAME LOCATED STA 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2025-167697 <[01]. REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02 AND DWG 141A8370 SHEET 16 REV - DWG 141A8370 SHEET 10 REV D SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1. REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02;DWG 141A8370 SHEET 16 REV - ; DWG 141A8370 SHEET 10 REV D AND DWG 141A8430 SHEET 4 REV B.; [03] CORRECTED STEP 1 AND 2. REPLACED STUB FRAME LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-10-2-0G-0 PARRG 9 AND SRM 51-40-02; DWG 141A8370 SHEET 16 REV - ; DWG 141A8370 SHEET 9 REV D AND DWG 141A8430 SHEET 4 REV B.; [04] TASK COMPLETED. CERTIFIED RII.

Part: NUT PLATE — CRACKED (ZONE 600) · airframe 57,968 hrs · 35,069 cycles

CRACK RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING 2025-167717<[01] REPLACED RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,968 hrs · 35,069 cycles

CORROSION ANGLE - SUPPORT LOCATED BTW STA 294.5 TO STA 312 RBL 56 AND WL 208.1 AT FWD GALLEY AREA 2025-167730 <[01]. REPLACED NEW ANGLE - SUPPORT LOCATED BTW STA 294.5 TO STA 312 RBL 56 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 SEE INDIVIDUAL SIGN OFF BELOW.; [02] REPLACED NEW ANGLE - SUPPORT LOCATED BTW STA 294.5 TO STA 312 RBL 56 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 SEE INDIVIDUAL SIGN OFF BELOW.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 57,968 hrs · 35,069 cycles

CRACK ON HOLES LOCATED ACCESS PANEL 661CB AT RT WING 2025-167784<[01] STEP 12 TOOL USED ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 10-JUN-25;[02] TOOL USED: MULTIMETER P/N: FLUKE 87-V; S/N: 65700125; DUE DATE: 09-JAN-26. TOOL USED HUMIDITY/TEMPERATURE CHART RECORDER P/N: RH550; S/N: 240531238 ; DUE DATE: 10-SEP-25.;[03] REPAIRED ACCESS PANEL 661CB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPAIRED ACCESS PANEL 661CB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FITTING — CRACKED (ZONE 500) · airframe 57,968 hrs · 35,069 cycles

CRACK SUPPORT ANGLE FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING 2025-167645<[01] REPLACED FITTING LOCATED FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEET:7 REV: -.;[02] COMPLETED JOB

Part: NUT PLATE — CRACKED (ZONE 500) · airframe 57,968 hrs · 35,069 cycles

CRACK RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING 2025-167744<[01] REPLACED RAIL NUT PLATE OFSS 371 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 57,968 hrs · 35,069 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV 2025-167675<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV -SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV -SEE INDIVIDUAL SIGN OFF BELOW. JOB COMPLETED

Part: NUT PLATE — CRACKED (ZONE 600) · airframe 57,968 hrs · 35,069 cycles

CRACK RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING 2025-167717<[01] REPLACED RAIL NUT PLATE OFSS 449 OUTBOARD FIXED LEADING EDGE AT RT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 57,968 hrs · 35,069 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND LBL 47 FWD GALLEY AND LAV 2025-167669<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND LBL 47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV -.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND LBL 47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV -.SEE INDIVIDUAL SIGN OFF BELOW. JOB COMPLETED

Part: SCUFF PLATE — CRACKED (ZONE 800) · airframe 57,968 hrs · 35,069 cycles

CRACK FWD SERVICE DOOR SCUFF PLATE AT PASSENGER CABIN 2025-167749 <[01]. TOOL USED: DIGITAL CALIPER P/N: 8647A42 S/N: B22440130 DUE DATE: 20-SEP-25; [02] STEP 4. TOOL USING RADIOMETER/PHOTOMETER P/N: XRP-3000; S/N: 1753759; DUE DATE: 30-JUN-25.; [03] REPAIRED BY WELDING FWD SERVICE DOOR SCUFF PLATE AT PASSENGER CABIN CENTER SECTION IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.; [04] REPAIRED BY WELDING FWD SERVICE DOOR SCUFF PLATE AT PASSENGER CABIN CENTER SECTION IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975. SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 600) · airframe 57,968 hrs · 35,069 cycles

CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING 2025-167685<REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING ; MEASURE OF CRACK IS L:0.600 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING ; MEASURE OF CRACK IS L:0.600 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26; REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING ; MEASURE OF CRACK IS L:0.600 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26

Part: SUPPORT ANGLE — CRACKED (ZONE 500) · airframe 57,968 hrs · 35,069 cycles

CRACK SUPPORT ANGLE FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING 2025-167645<[01] REPLACED FITTING LOCATED FIXED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEET:7 REV: -.;[02] COMPLETED JOB

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 57,968 hrs · 35,069 cycles

CRACK STUB FRAME LOCATED STA 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2025-167697<[01] REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02 AND DWG 141A8370 SHEET 16 REV - DWG 141A8370 SHEET 10 REV D SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02;DWG 141A8370 SHEET 16 REV - ;DWG 141A8370 SHEET 10 REV D AND DWG 141A8430 SHEET 4 REV B.;[03] CORRECTED STEP 1 AND 2. <BR>REPLACED STUB FRAME LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-10-2-0G-0 PARRG 9 AND SRM 51-40-02;DWG 141A8370 SHEET 16 REV - ;DWG 141A8370 SHEET 9 REV D AND DWG 141A8430 SHEET 4 REV B.;[04] TASK COMPLETED <BR>CERTIFIED RII

Part: ANGLE — CRACKED (ZONE 600) · airframe 57,968 hrs · 35,069 cycles

CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING 2025-167685<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING ; MEASURE OF CRACK IS L:0.600 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[02] CORRECTED STEP 1 REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING ; MEASURE OF CRACK IS L:0.600 INCH. REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 6 AT RT WING ; MEASURE OF CRACK IS L:0.600 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26

Part: WEB — CRACKED (ZONE 600) · airframe 57,968 hrs · 35,069 cycles

CRACK WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING 2025-167701<[01] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF BELOW.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 57,968 hrs · 35,069 cycles

CRACK ON HOLES LOCATED ACCESS PANEL 661CB AT RT WING 2025-167784<[01] STEP 12 TOOL USED ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 10-JUN-25;[02] TOOL USED: MULTIMETER P/N: FLUKE 87-V; S/N: 65700125; DUE DATE: 09-JAN-26. TOOL USED HUMIDITY/TEMPERATURE CHART RECORDER P/N: RH550; S/N: 240531238 ; DUE DATE: 10-SEP-25.;[03] REPAIRED ACCESS PANEL 661CB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPAIRED ACCESS PANEL 661CB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 57,968 hrs · 35,069 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV 2025-167681<[01] REPLACED WEB INTERCOSTAL WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB INTERCOSTAL WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -SEE INDIVIDUAL SIGN OFF BELOW.

Part: WEB — CRACKED (ZONE 600) · airframe 57,968 hrs · 35,069 cycles

CRACK WEB TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING 2025-167701<[01] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2512 SHEET 14 REV A. SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 57,968 hrs · 35,069 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 328 TO STA 344 AND LBL 47 FWD GALLEY AND LAV 2025-167671<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 328 TO STA 344 AND LBL 47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW STA 328 TO STA 344 AND LBL 47 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: NUT PLATE — CRACKED (ZONE 500) · airframe 57,968 hrs · 35,069 cycles

CRACK RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING 2025-167738<[01] REPLACED RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED

Part: NUT PLATE — CRACKED (ZONE 500) · airframe 57,968 hrs · 35,069 cycles

CRACK RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING 2025-167738<[01] REPLACED RAIL NUT PLATE OFSS 541 FIXED LEADING EDGE AT LT WING IAW B737-700 DWG 112A4402 SHEET 13 REV - AND SRM 51-40-02; SRM 51-10-02 SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 57,968 hrs · 35,069 cycles

CRACK INDICATION ON STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-8 TO STR-9 IN FORWARD GALLEY DOOR RH SIDE; CRACK LENGTH 1.272 INCHES APPROX. 2025-167597<[01] REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8370 SHEET 9 TO SHEET 11 REV D. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8370 SHEET 9 TO SHEET 11 REV D. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII VERIFIED

Part: ANGLE — CRACKED (ZONE 600) · airframe 57,968 hrs · 35,069 cycles

CRACK ANGLE ON INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING 2025-167631<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[02] STEP 1 CORRECTED REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK ANGLE OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[03] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK ANGLE OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.

Part: ANGLE — CRACKED (ZONE 500 SLATS) · airframe 57,968 hrs · 35,069 cycles

CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2025-167634<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING ; MEASURE OF CRACK IS L:0.450 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[02] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING ; MEASURE OF CRACK IS L:0.450 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[03] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING ; MEASURE OF CRACK IS L:0.450 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.

Part: ANGLE — CRACKED (ZONE 500) · airframe 57,968 hrs · 35,069 cycles

CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2025-167634<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING ; MEASURE OF CRACK IS L:0.450 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[02] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING ; MEASURE OF CRACK IS L:0.450 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[03] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING ; MEASURE OF CRACK IS L:0.450 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.

Part: ANGLE — CRACKED (ZONE 600 SLATS) · airframe 57,968 hrs · 35,069 cycles

CRACK ANGLE ON INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING 2025-167631<[01] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. TOOK MEASURE OF CRACK ANGLE INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[02] STEP 1 CORRECTED REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK ANGLE OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.;[03] REPLACED ANGLE LOC INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02-0G AND CMM-57-43-01 FIGURE 1 SHEET 13. MEASURE OF CRACK OF REMOVED INBOARD AUXILIARY TRACK ANGLE OF SLAT 8 AT RT WING ; MEASURE OF CRACK IS L:0.435 INCH TOOL USED CALIPER P/N:500-197-30 S/N:A21043208 DUE DATE:25-MAR-26.

Part: STUB FRAME — CRACKED (ZONE 100) · airframe 57,968 hrs · 35,069 cycles

CRACK INDICATION ON STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-8 TO STR-9 IN FORWARD GALLEY DOOR RH SIDE; CRACK LENGTH 1.272 INCHES APPROX. 2025-167597 <[01]. REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8370 SHEET 9 TO SHEET 11 REV D. SEE INDIVIDUAL SIGN OFF BELOW.; [02] REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8370 SHEET 9 TO SHEET 11 REV D. SEE INDIVIDUAL SIGN OFF BELOW. RII VERIFIED.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 57,968 hrs · 35,069 cycles

CRACK SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN 2025-167579 <[01]. TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26.; [02] REPLACED SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV A AND DWG 111A6000; SHEET 282; REV -. SEE INDIVIDUAL SIGN OFF BELOW.; [03] REPLACED SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV A AND DWG 111A6000; SHEET 282; REV -. SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT BRACKET — CRACKED (ZONE 200) · airframe 57,968 hrs · 35,069 cycles

CRACK SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN 2025-167579 <[01]. TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26.; [02] REPLACED SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV A AND DWG 111A6000; SHEET 282; REV -. SEE INDIVIDUAL SIGN OFF BELOW.; [03] REPLACED SUPPORT BRACKET LOCATED STA 695 AT LEVEL LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV A AND DWG 111A6000; SHEET 282; REV -. SEE INDIVIDUAL SIGN OFF BELOW.

Part: WEB — CRACKED (ZONE 100) · airframe 57,968 hrs · 35,069 cycles

CRACK VAPOR BARRIER WEB LOCATED BS663.75 AND LBL 40 AT MAIN WHEEL WELL COMPARTMENT 2025-167480 <[01]. TOOL USED CALIPER P/N 500-197-30 S/N A18135086 DUE DATE 21 JUN 25; [02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18175478 DUE DATE 22 FEB 26; [03] ON STEP 12; TOOL USED: ULTRASONIC FLAW DETECTOR; PN: EPOCH 600; SN: 130547106; DUE DATE: 30-SEP-25; [04] REPAIRED VAPOR VARRIER WEB LOCATED BS663.75 AND LBL 40 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW; [05] REPAIRED VAPOR VARRIER WEB LOCATED BS663.75 AND LBL 40 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW; [06] CORRECTED CORRECTIVE ACTION 5. REPAIRED VAPOR VARRIER WEB LOCATED BS663.75 AND LBL 40 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW. RII ACCOMPLISHED.

Part: SKIN — CRACKED (ZONE 500 SLAT) · airframe 57,968 hrs · 35,069 cycles

CRACK SKIN SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING 2025-167451<[01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138203; DUE DATE: 09-SEP-25;[02] PERFORMED REPAIR ON LOWER SKIN SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; SEE INDIVIDUAL SIGN OFFS BELOW;[03] PERFORMED REPAIR ON LOWER SKIN SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; SEE INDIVIDUAL SIGN OFFS BELOW

Part: SKIN — CRACKED (ZONE 500 SLAT) · airframe 57,968 hrs · 35,069 cycles

CRACK SKIN SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING 2025-167451<[01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138203; DUE DATE: 09-SEP-25;[02] PERFORMED REPAIR ON LOWER SKIN SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; SEE INDIVIDUAL SIGN OFFS BELOW;[03] PERFORMED REPAIR ON LOWER SKIN SLAT 4 LOCATED SLAT STATION 85.19 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8; SEE INDIVIDUAL SIGN OFFS BELOW

Part: SEAT — OUT OF ADJUST (ZONE 200) · airframe 56,132 hrs · 33,916 cycles

CAPTAINS SIDE EXIT ROW SEAT 12A STAYS RECLINED.<[01] ADJUSTED PAX SEAT IN 12A PER MM 25-22-00<BR>OPS CHECK GOOD

Part: GIRT BAR — OUT OF ADJUST (AFT DOOR) · airframe 55,703 hrs · 33,655 cycles

FA REPORTS FO SIDE AFT GIRT BAR BRACKET NEEDS ADJUSTED.<[01] ADJUSTED RETAINER CLIP IAW SIP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,274 hrs · 33,370 cycles

FWD ENTRY EMERGENCY EXIT LIGHTS INOP.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Part: ISOLATION MOUNT — CRACKED (DOOR SLIDE) · airframe 55,034 hrs · 33,221 cycles

FWD GALLEY SERVICE DOOR AFT SLIDE MOUNT ISOLATOR IS CRACKED.<[01] R&R FWD GALLEY SERVICE DOOR AFT SLIDE MOUNT ISOLATOR IAW SRM 51-40-02.

Part: HANDLE — BROKEN (DOOR ASSIST) · airframe 54,979 hrs · 33,183 cycles

F/OS ASSIST HANDLE BROKEN AT UPPER W/S FRAME<[01] R/R F/O?S ASSIST HANDLE ASSY PER AMM 56-11-11.

Part: ANGLE — DAMAGED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CUSTOMER REQUEST BROKEN BODY STA 663.75 ANGLE UPPER POSITION RBL 7 AT AIR CONDITIONING BAY 2023-378136<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 200048001; DUE DATE: 01-MAY-24.;[02] REPAIRED UPPER ANGLE BODY STA 663.75 BTW RBL 7 TO RBL 21 AT AIR CONDITIONING BAY IAW B737-700 SRM 57-10-10-2R-5 REPAIR 5;[03] STEP 2 ENTERED IN ERROR; CORRECT STEP IS:<BR>REPAIRED UPPER ANGLE BODY STA 663.75 BTW RBL 7 TO RBL 21 AT AIR CONDITIONING BAY IAW B737-700 SRM 57-10-10-2R-5 REPAIR 5<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[04] REPAIRED UPPER ANGLE BODY STA 663.75 BTW RBL 7 TO RBL 21 AT AIR CONDITIONING BAY IAW B737-700 SRM 57-10-10-2R-5 REPAIR 5 ; RII SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK FRAME STA 312 UPPER CHORD BETWEEN S-5L AND S-6L LBL 33 AT PASSENGER CABIN 2023-378124<[01] PERFORMED REPAIR ON BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L IAW EA M-22-153-01244<BR>SEE TASK CARD: TTG8Q00LLCPH;[02] PERFORMED REPAIR ON BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L IAW EA M-22-153-01244 <BR>SEE TASK CARD: TTG8Q00LLCPH

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 52,678 hrs · 31,753 cycles

CRACK ON RIB 8 LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER 2023-378132<[01] REPLACED RIB 8 LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A0103 SHEET 7 REV.- SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK CARD COMPLETED <BR>REPLACED RIB 8 LOCATED ACCESS PANEL 321A AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG 174A0103 SHEET 7 REV.- SEE INDIVIDUAL SIGNOFFS BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK INDICATION FOUND ON ANGLE CLIP LOCATED ON FLOOR STRUCTURE BTW BS 291.5 AND BS296.4 STR 17R RBL 52 AT FWD GALLEY AREA. 2023-378121<[01] TOOL USED: CALIPER P/N 500-752-20 S/N B21038528 CAL. DUE DATE 20 SEP 23.;[02] REPLACED NEW ANGLE CLIP LOCATED ON FLOOR STRUCTURE BTW BS 291.5 AND BS296.4 STR 17R RBL 52 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A8310 SHEET 25 REV-.;[03] CORRECTED STEP 2 <BR>REPLACED NEW ANGLE CLIP LOCATED ON FLOOR STRUCTURE BTW BS 291.5 AND BS296.4 STR 17R RBL 52 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A8310 SHEET 25 REV-. SEE INDIVIDUAL SIGN OFF BELOW;[04] CORRECTED STEP 2 <BR>REPLACED NEW ANGLE CLIP LOCATED ON FLOOR STRUCTURE BTW BS 291.5 AND BS296.4 STR 17R RBL 52 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A8310 SHEET 25 REV-. RII. SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 52,678 hrs · 31,753 cycles

CORROSION FLOOR STRUCTURE FLOOR BEAM 986.5 AT RBL 43 WL 208.1 AT AFT GALLEY AREA 2023-378096<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022235; DUE DATE: 03-AUG-23.;[02] TOOL USED P/N FPK-PRO-104 S/N PRO-3384 CAL DUE DATE 24 APR 23.;[03] PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE FLOOR BEAM 986.5 AT RBL 43 WL 208.1 AT AFT GALLEY AREA .IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. MATERIAL USED: STRAP 7075-T6 0.100? P.O: 2012 531818; ANGLE BAC1490-2887 P.O: 2023 124527; FILLER 7075-T6 0.150? P.O:2023 109423;[04] CORRECTED STEP 2: TOOL USED P/N: FPK-PRO-104 S/N PRO-3384 CAL DUE DATE: 24 APR 24.;[05] CORRECTED STEP 3:<BR>PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE FLOOR BEAM 986.5 AT RBL 43 WL 208.1 AT AFT GALLEY AREA .IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. MATERIAL USED: STRAP 7075-T6 0.100? P.O: 2012 531818; ANGLE BAC1490-2887 P.O: 2023 124527; FILLER 7075-T6 0.150? P.O:2023 109423. SEE INDIVIDUAL SIGN OFF BELOW;[06] CORRECTED STEP 3: <BR>PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE FLOOR BEAM 986.5 AT RBL 43 WL 208.1 AT AFT GALLEY AREA .IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. MATERIAL USED: STRAP 7075-T6 0.100? P.O: 2012 531818; ANGLE BAC1490-2887 P.O: 2023 124527; FILLER 7075-T6 0.150? P.O:2023 109423. RII SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOORBEAM — CORRODED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CORROSION FLOOR STRUCTURE FLOOR BEAM 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2023-378097<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022235; DUE DATE: 03-AUG-23.;[02] TOOL USED P/N FPK-PRO-104 S/N PRO-3384 CAL DUE DATE 24 APR 23.;[03] PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE FLOOR BEAM 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA.IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. MATERIAL USED : STRAP 7075-T6 0.100? P.O: 2012 531818; ANGLE BAC1490-2887 P.O: 2023 124527 FILLER 7075-T6 0.150? P.O:2023 109423. SEE INDIVIDUAL SIGN OFF BELOW;[04] CORRECTED STEP 2: <BR>TOOL USED P/N FPK-PRO-104 S/N PRO-3384 CAL DUE DATE 24 APR 24.;[05] PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE FLOOR BEAM 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA.IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. MATERIAL USED : STRAP 7075-T6 0.100? P.O: 2012 531818; ANGLE BAC1490-2887 P.O: 2023 124527 FILLER 7075-T6 0.150? P.O:2023 109423. RII SEE INDIVIDUAL SIGN OFF BELOW.

Part: STIFFENER — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK ON ANGLE LOCATED INTERNAL STRUCTURE BTW 907 TO BS 927 FWD POSITION BTW STR 26R TO STR 27R AFT CARGO COMPARTMENT 2023-378093CRACK ON STIFFENER LOCATED INTERNAL STRUCTURE BTW 907 TO BS 927 FWD POSITION BTW STR 26R TO STR 27R AFT CARGO COMPARTMENT<[01] REPLACED STIFFENER LOCATED INTERNAL STRUCTURE BTW 907 TO BS 927 FWD POSITION BTW STR 26R TO STR 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 24 REV - SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK ON UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND R BL 13 WL 208 AT FWD GALLEY AREA 2023-378071<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24;[02] REPLACED UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND RBL 13 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A5400;SHEE 38 REV A<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND RBL 13 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A5400;SHEE 38 REV A <BR>SEE INDIVIDUAL SIGN OFF BELOW AS RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK ON UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND RBL 1 WL 208 AT FWD GALLEY AREA 2023-378070<[01] REPLACED UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND RBL 1 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A5400;SHEET 92; REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1. REPLACED UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND RBL 1 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A5400;SHEET 38; REV: A.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND RBL 1 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A5400;SHEET 38; REV: A. <BR>SEE INDIVIDUAL SIGN OFF BELOW <BR>CERTIFIED RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK ON ANGLE LOCATED INTERNAL STRUCTURE BTW 907 TO BS 927 AFT POSITION AND BTW STR 26R TO STR 27R AFT CARGO COMPARTMENT 2023-378094CRACK ON STIFFENER LOCATED INTERNAL STRUCTURE BTW 907 TO BS 927 AFT POSITION AND BTW STR 26R TO STR 27R AFT CARGO COMPARTMENT<[01] REPLACED STIFFENER LOCATED INTERNAL STRUCTURE BTW 907 TO BS 927 AFT POSITION BTW STR 26R TO STR 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 24 REV - SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK STRINGER 23R BS 540 FWD CARGO COMPARTMENT 2023-378089<[01] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 45MG; S/N: 221860711; DUE DATE: 07 NOV 23.;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 60009161631; CAL DUE DATE: 31-JAN-24;[03] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER: P/N:P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24;[04] REPAIRED STR 23R LOC. BTW BS 500D TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[05] REPAIRED STR 23R LOC. BTW BS 500D TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 <BR>SEE INDIVIDUAL SIGN OFFS BELOW. AS RII

Part: CARGO TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK TRACK LBBL 17.24 LOCATED BS727E AFT CARGO COMPARTMENT 2023-378092<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101U102020; CAL DUE DATE: 30-AUG-23;[02] REPAIRED TRACK LBBL 17.24 LOCATED BS727E AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPAIRED TRACK LBBL 17.24 LOCATED BS727E AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 SEE INDIVIDUAL SIGNOFFS BELOW<BR><BR>ITEM RII

Part: CARGO TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK TRACK RBBL 13.84 LOCATED BS767 AFT CARGO COMPARTMENT 2023-378091<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101U102020; CAL DUE DATE: 30-AUG-23;[02] REPAIRED TRACK RBBL 13.84 LOCATED BS767 AFT CARGO COMPARTMENT IAW B373-700 SRM 53-00-53-2R-3 REPAIR 3 SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPAIRED TRACK RBBL 13.84 LOCATED BS767 AFT CARGO COMPARTMENT IAW B373-700 SRM 53-00-53-2R-3 REPAIR 3 SEE INDIVIDUAL SIGNOFFS BELOW<BR><BR>ITEM RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK ON INTERCOSTAL LOCATED BTW BS 312 TO BS 328 AT LBL 45 AND WL 208 AT FWD GALLEY AREA 2023-378068<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW BS 312 TO BS 328 AT LBL 45 AND WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 141A5400; SHEET 26; REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB - INTERCOSTAL LOCATED BTW BS 312 TO BS 328 AT LBL 45 AND WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 141A5400; SHEET 26; REV - <BR>SEE INDIVIDUAL SIGN OFF BELOW. RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK ON UPPER ANGLE OF INTERCOSTAL LOCATED BTW BS 380 TO BS 400 AND R BL 10 WL 208 AT FWD GALLEY AREA 2023-378069<[01] REPLACED ANGLE OF INTERCOSTAL AND FASTENER LOCATED BTW BS 380 TO BS 400 AND RBL 10 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; DWG 143A5410-170.<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE OF INTERCOSTAL AND FASTENER LOCATED BTW BS 380 TO BS 400 AND RBL 10 WL 208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; DWG 143A5410-170. <BR>SEE INDIVIDUAL SIGN-OFF BELOW<BR><BR>ITEM RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK ANGLE - SUPPORT LOCATED BS827 AND RBL19 WL155 AT AFT CARGO COMPARTMENT 2023-378095<[01] REPLACED ANGLE AND FASTENERS LOCATED BS827 AND RBL19 WL155 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG 146A8120 REV - DWG 146A0081 REV - <BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] TASK COMPLETED ; TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNOFF BELOW

Part: SCUFF PLATE — CRACKED (ZN 800 DOOR) · airframe 52,678 hrs · 31,753 cycles

CRACK FWD SERVICE DOOR SCUFF PLATE AT PASSENGER CABIN 2023-378048<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A21042019;DUE DATE:17-MAR-24.;[02] TOOL USED : LIGHT METER P/N XRP-3000 S/N 1998072 DUE DATE: 15-OCT-23.;[03] REPAIRED FWD SERVICE DOOR SCUFF PLATE AT PASSENGER CABIN I.A.W. BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975 SEE INDIVIDUAL SIGNOFFS BELOW;[04] JOB COMPLETED

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 52,678 hrs · 31,753 cycles

CRACK INSPAR RIB 92.70 AT 30 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2023-378014<[01] TOOL USED: EDDY CURRENT EQUIPMENT. P/N: NORTEC 600D. S/N: 210138003. DUE DATE: 27-MAR-24.;[02] REPAIRED INSPAR RIB 92.70 AT 30 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN-OFF BELOW.;[03] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: PLATE — CRACKED (ZN 800 DOOR) · airframe 52,678 hrs · 31,753 cycles

CRACK CUT OUT EMERGENCY DOOR PLATE LOC BTW STR 10L TO STR 11L AT PASSENGER CABIN 2023-378013<[01] REPLACED NEW PLATE LOC EMERGENCY DOOR BTW STR 10L TO STR 11L STA 621.73 TO STA 633.26 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 411A2857 SHEET 1 REV.D AND SRM 51-10-02 Ï¿½TEM 9 . SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED NEW PLATE LOC EMERGENCY DOOR BTW STR 10L TO STR 11L STA 621.73 TO STA 633.26 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 411A2857 SHEET 1 REV.D AND SRM 51-10-02 Ï¿½TEM 9 . SEE INDIVIDUAL SIGN OFF BELOW. RII CERTIFIED

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 52,678 hrs · 31,753 cycles

INOP LOWERED CEILING PANEL BATTERY PACK LT SIDE AT AFT GALLEY AREA (1 EA) 2023-378027<[01] REPLACED LOWERED CEILING PANEL BATTERY PACK LT SIDE AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-06-960-805;[02] REPLACED LOWERED CEILING PANEL BATTERY PACK LT SIDE AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-06-960-805

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT 2023-377908<[01] REPLACED GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 209 REV-.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 209 REV-.SEE INDIVIDUAL SIGN OFF BELOW.<BR>CERTIFIED AS RII

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT 2023-377910<[01] REPLACED GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV-<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV- <BR>SEE INDIVIDUAL SIGN OFF BELOW<BR>CERTIFIED AS RII

Part: DOOR — CRACKED (ZN 700 LANDING G) · airframe 52,678 hrs · 31,753 cycles

CUSTOMER REQUEST CRACK ON INTERNAL SURFACE OF CENTER MLG DOOR LH SIDE 2023-377973<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022235; DUE DATE: 03-AUG-23.;[02] TOOL USED: P/N; 500-193-30 S/N; 0000291 DUE DATE; 12-OCT-23;[03] REPAIRED CENTER MLG DOOR LH SIDE IAW B737-700 SRM 52-80-02-2R-3 FIG 202 SHEET 5; SHEET 6 AND SHEET 7. SEE INDIVIDUAL SIGNOFFS BELOW;[04] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,678 hrs · 31,753 cycles

CRACK ANGLE LOCATED BS 500C FWD SIDE AND S-26L FWD CARGO COMPARTMENT 2023-377912<[01] REPLACED ANGLE LOCATED BS 500C FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG 143A7505 SHEET 82;REV-.SEE INDIVIDUAL SIGN OFF BELOW;[02] COORECTED STEP 1:<BR>REPLACED ANGLE LOCATED BS 500C FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 AND DWG 143A7505 SHEET 82 REV-.;[03] REPLACED ANGLE LOCATED BS 500C FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 AND DWG 143A7505 SHEET 82 REV-.<BR>CERTIFIED AS RII

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 52,678 hrs · 31,753 cycles

INOP LOWER SIDEWALL PANEL BATTERY PACK ON BS 616 RT SIDE AT PASSENGER CABIN 2023-377921<[01] REPLACED LOWER SIDEWALL PANEL BATTERY PACK ON BS 616 RT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 AND B737-700 WDM 33-51-13. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] JOB COMPLETED

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 52,678 hrs · 31,753 cycles

CRACK ANGLE FLOOR STRUCTURE BTW STA 685 TO STA 706 AND RBL 24.75 AT PASSENGER CABIN 2023-377867<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24.;[02] REPLACED ANGLE FLOOR STRUCTURE BTW STA 685 TO STA 706 AND RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV: A<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED ANGLE FLOOR STRUCTURE BTW STA 685 TO STA 706 AND RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV: A <BR>SEE INDIVIDUAL SIGN OFF BELOW<BR>CERTIFIED AS RII

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 52,384 hrs · 31,573 cycles

R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP<[01] RELUMPED R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT PER AMM 33-51-04. OPS CHECKED GOOD

Part: FLAP — DELAMINATED (ZN 600 RIGHT WIN) · airframe 51,328 hrs · 30,909 cycles

RH I/B FLAP T/E WEDGE DELAMINATED. REMOVED RH I/B FLAP T/E WEDGE PER SRM 51-40-02. LOCATED AND DRILLED NEW WEDGE ASSY P/N: 113A2550-604 PER SRM 51-40-05.;[04] APPLIED SURFACE FINISH PER AMM 51-21-99;[05] INSPECTION VERIFIED CORRECTIVE ACTION STEPS 1 THRU 4. OK TO INSTALL WEDGE ASSEMBLY.;[06] INSTALLED NEW WEDGE ASSY P/N: 113A2550-604 PER SRM 51-40-02.;[07] INSPECTION VERIFIED CORRECTIVE ACTION STEP 6.;[08] INSTALLED PANEL 653ET REFERENCE SOPM 20-50-01.;[09] C/W OF INSPECTION STEP 8 ABOVE.;[10] C/W

Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 51,247 hrs · 30,865 cycles

FOUND 10 INCH LONG CRACK IN FWD CARGO COMPOSITE FLOOR PANEL AFT OF CARGO DOOR. REMOVED AND REPLACED THE FLOOR PANEL 120CF IAW AMM 25-52-10.

Part: PANEL — DEFORMED (ZN 200 FUS TOP) · airframe 50,959 hrs · 30,674 cycles

FLOOR GIVES WAY AND THUMPS BETWEEN ROW 13 AND 14 / [01] REMOVED AND REPLACED PASSENGER CABIN FLOOR PANEL BETWEEN ROW 13 AND 14 IAW AMM 53-21-00 NO DEFECTS NOTED.

Part: SEAL — CRACKED (RH HORIZ STAB) · airframe 49,460 hrs · 29,670 cycles

RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED / [01] R&R RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL REF AMM 53-31-31.

Part: LIGHT — LOOSE · airframe 48,745 hrs · 29,230 cycles

FLOOR LIGHTING AT ROW 8-9 AC LEFT NEEDS TO BE SECURED. / [01] RESECURED FLOOR EMERGENCY LIGHTING AT 8/9 ABC PER AMM 33-51-12.

Part: LIGHT — LOOSE · airframe 48,577 hrs · 29,128 cycles

FLOOR LIGHT STRIPS AT 9 & 10 DEF DETACHED FROM FLOOR CAUSING A TRIP HAZARD. ; / [01] RESECURED FLOOR PROXIMITY LIGHT AT 9& 10 DEF IN REF. TO AMM 33-51-14.

Part: LIGHT — LOOSE (CABIN) · airframe 47,956 hrs · 28,763 cycles

SUPPLEMENTAL INFORMATION: PHOTO LUMINESCENCE LIGHT STRIPE I FLIGHT AT SEAT 8/9 BOTH SIDES ; / [01] SECURED PHOTO IIIMINESCENCE EXIT LIGHT AT ROW 8/9 PER AMM 33-51-15

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,946 hrs · 28,145 cycles

FWD LOWERED CEILING L/H EMERGENCY LIGHT BATTERY PACK MO1675 IS BAD ; / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT FWD LH LOCATION MO1675 IAW AMM 33-51-06-960-805. OPS CHECK GOOD.; [02] VERIFIED STEP 1.<BR>AUDIT C/W

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,946 hrs · 28,145 cycles

PASSENGER CABIN - LH STOWBIN BULLNOSE EMERGENCY LIGHT INOP SEAT ROWS 17-24. ; / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT AFT LH LOCATION IAW AMM 33-51-06-960-805. OPS CHECK GOOD.; [02] VERIFIED STEP 1.<BR>AUDIT C/W

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 46,946 hrs · 28,145 cycles

AFT CARGO AFT CORNER SCUFF PLATE CRACKED ; / [01] REPAIRED CRACKED AFT CARGO AFT CORNER SVUFF PLATE IN BACKSHOP ON WO:42436-8300-0001.; [02] VERIFIED ITEM 1.<BR>AUDITED.

Part: ANGLE — CORRODED (BS 727C) · airframe 46,946 hrs · 28,145 cycles

AFT CARGO COMPT. Z-ANGLE STA 727C+10; RBL 25; WL 156 HAS CORROSION UPPER SURFACE DOT A-21-68 ; / [01] REMOVE CORROSION FROM RH Z-ANGLE IAW SRM 51-10-02-0G-0. PAR 15; AND VERIFIED WITH 10X MAG GLASS.; [02] VERIFIED MATERIAL LOSS. ORIGINAL THICKNESS .040'; LOSS OF .018'; REMAINING MATERIAL .022'. OUT OF LIMITS IAW SRM 53-00-53-1A-0 AAR TOOL 36649; CAL DATE 04 AUG 21.; [03] MATERIAL VERIFIED AS BAC1496-377 7075T6 A23339 IAW SRM 53-00-53-2R-5 REPAIR 5; [04] VERIFIED ITEMS 1 - 3.; [05] FABRICATED NEW Z-ANGLE IAW SRM 53-00-53-2R-5 REPAIR 5; [06] VERIFIED ITEM 5.<BR>OK TO TREAT & PRIME.; [07] TREATED AND PRIMED NEW Z ANGLE IAW SRM 53-00-53-2R-5 REPAIR 5; [08] VERIFIED ITEM 7 ON NEW Z-ANGLE; [09] INSTALLED NUTPLATES ON NEW Z-ANGLE FROM STA 727-767 IAW SRM 51-40-10-2R-0 STEPS 5 A-H; [10] VERIFIED ITEM 9; PUSH TEST NEEDS ACP; [11] REFERENCE ITEM 3; REPAIR Z-ANGLE IS FROM STA: 727 TO 767.; [12] PERFORMED NUTPLATE PUSH TEST. TESTS GOOD IAW SRM 51-40-10-2R-0. TOOL # 42641 DUE 12/14/21; [13] VERIFIED STEP 12; [14] FABRICATED NEW Z ANGEL FROM STA 727-767. NEW Z ANGLE INSTALLED ON TTG8Q004E6LY; [15] VERIFIED STEP 14; [16] AUDIT C/W

Part: ANGLE — CORRODED (BS 747) · airframe 46,946 hrs · 28,145 cycles

AFT CARGO COMPT. Z-ANGLE STA 747+18; RBL 25; WL 156 HAS CORROSION UPPER SURFACE DOT A-21-71 ; AFT CARGO COMPT. Z-ANGLE STA 747+18; RBL 25; WL 156 HAS CORROSION (LOWER) SURFACE DOT A-21-71 / [01] REMOVED CORROSION FROM RH Z-ANGLE IN AFT CARGO COMPARTMENT. IAW SRM 5-10-02-0G-0. PAR 15. VERIFIED WITH 102X MAG GLASS.; [02] VERIFIED MATERIAL LOSS TO BE AS FOLLOWS ORIGINAL THICKNESS .040'; LOSS .009'; REMAINING MATERIAL .031'. OUT OF LIMITS IAW SRM 53-00-53-1A-2. AAR TOOL 36949 CAL DUE DATE 04 AUG 21.; [03] NEW Z ANGLE FABRICATED ON TTG8Q005QK0Z. NEW Z ANGLE INSTALLED ON TTG8Q004E6LY.; [04] VERIFIED STEPS 1;2;3<BR>AUDIT C/W

Part: ANGLE — CORRODED (BS 767) · airframe 46,946 hrs · 28,145 cycles

AFT CARGO COMPT. Z-ANGLE STA 767+14; LBL 25; WL 156 HAS CORROSION UPPER SURFACE DOT A-21-64 ; / [01] EVALUATED CORROSION ON L/H ZEE ANGLE; ORIGINAL THICKNESS .040'; LOSS .020' REMAINING .020' OUT OF LIMITS IAW SRM 53-00-53-1A-2; [02] VERIFIED MATERIAL FOR ZEE ANGLE REPLACEMENT; BAC1496 7075-T62 ATAG 76442 IAW SRM 53-00-53-2R-5 TABLE 201.; [03] VERIFIED STEP 1.; [04] VERIFIED MATERIAL IN STEP 2.; [05] FABRICATED ZEE ANGLE REPLACEMENT SECTIONS FROM STA 727 TO 847 IAW SRM 53-00-53-2R-5 SECTION 4. D -H.; [06] INSPECTION CW STEP 5; [07] OK TO TREAT AND PRIME; [08] APPLIED CHEMICAL CONVERSION AND PRIMER TO ZEE ANGLE REPLACEMENT SECTION IAW SRM 53-00-53-2R-5 SECTION 4. I AND J.; [09] VERIFIED STEP 8.; [10] APPLIED NUTPLATES IAW SRM 51-40-10-2R-0 STEPS 5 A-H; [11] VERIFIED STEP 10 <BR>PUSH TEST NEEDS ACCOMPLISHED; [12] PERFORMED NUTPLATE PUSH TEST. TESTS GOOD IAW SRM 51-40-10-2R-0. TOOL # 42641 DUE 12/14/21; [13] VERIFIED STEP 12; [14] AFT CARGO COMPARTMENT LH Z-ANGLE; EVALUATED CORROSION VERIFED; ORIGINAL T .040'; LOSS .020'; REMAINING MATERIAL .020'. OUT OF LIMITS IAW SRM 53-00-53-1A-2. FABRICATED NEW Z-ANGLE BS 727-847; LBL 25 WL 156; IAW SRM 53-00-53-2R-5; LH Z-ANGLE INSTALLED ON (5360-E-16462-NG) TTG8Q004E6LY.; [15] C/W; [16] VERIFIED STEPS 14<BR>AUDIT C/W

Part: ATTACH BRACKET — CRACKED (L2 DOOR) · airframe 46,946 hrs · 28,145 cycles

DOT 045-001; L2 DOOR LOWER AFT ATTACH BRACKET IS CRACKED; COMMON TO DOOR AND SWEEPER SEAL PLATE. ; / [01] REMOVED L/2 SWEEPER SEAL BRACKET I/A/W SRM 51-40-02-0G-0; [02] DISPLACED L/2 DOOR LINER I/A/W SRM 51-40-02-0G-0; [03] REMOVED AND INSTALLED NEW L/2 DOOR LOWER AFT ATTACH BRACKETAT SWEEPER SEAL PLATE I/A/W SRM 51-40-02-0G-0 A TAG A63434; [04] VERIFIED STEP 3.<BR>OK TO INSTALL SWEEPER SEAL BRACKET AND LINER; [05] INSTALLED SWEEPER SEAL BRACKET AND LINER INSTALLED L/2 DOOR LOWER AFT ATTACH BRACKET COMMON TO FOOD AND SWEEPEF SEAL PLATE I/A/W AMM 52-13-31-400-802; [06] VERIFIED STEP 5.<BR>AUDIT C/W

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 46,946 hrs · 28,145 cycles

LEFT HORIZONTAL STAB INSPAR RIB 5 (STAB STA 129.50); STIFFENER 3 HAS CRACK NEAR LOWER SKIN DOT A-21-41 ; / [01] CUT AND REMOVED DAMAGE IAW SRM 55-10-09-2R-4 REPAIR 4; [02] PERFORMED GVI OF ALL AREAS WITHIN THE REPAIR AREA. NO DEFECTS NOTED IAW SRM 55-10-09-2R-4 REPAIR 4; [03] VERIFIED STEP 1<BR>COMPLETED STEP 2 GVI REPAIR AREAS; [04] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 23 & PROC 16. NO DEFECTS NOTED. TOOL#31822; DUE 12AUG21; [05] KIT VERIFIED AS P/N 55100003-01 WN5067 IAW SRM 55-10-09-2R-4 REPAIR 4 AND DWG 55100003 REV B; [06] VERIFIED STEP 5; [07] FABRICATED REPAIR PARTS IAW SRM 55-10-09-2R-4 REPAIR 4; [08] VERIFIED ITEM 7; [09] OK TO INSTALL; [10] INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4 REPAIR 4; [11] VERIFIED STEP 10<BR>OK TO CIC; [12] APPLIED CIC TO REPAIR AREA IAW SRM 55-10-09-2R-4 REPAIR 4; [13] VERIFIED STEP 12; [14] C/W; [15] AUDIT C/W

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 46,946 hrs · 28,145 cycles

FWD SERVICE DOOR #5 BEAM 141A6536-15 IS CRACKED IN RADIUS NEAR INBD HOLE. STARTED REMOVAL OF #5 BEAM IASW SRM 51-40-02-OG-0. LOCATED AND DRILLED NEW BEAM IAW EO 5241-C-1493-NG SRM 51-40-05-0G-0 DWG'S 141A6516 REV C. INSTALLED #5 BEAM IAW SRM 51-40-02-0G-0 AND DWG 141A6516 141A6535. REMOVED AND REPLACED #5 BEAM IN FWD SERVICE DOOR IAW SRM 51-40-02-0G-0 AND DWGS 141A6516 141A6535 AND EL 5241-C-1493-NG.

Part: SPRING — CRACKED (VERTICAL STAB) · airframe 46,946 hrs · 28,145 cycles

VERTICAL STAB FIXED L/E SPRING P/N 176A3101-26 R/H SIDE HAS CRACK AT RADIUS DOT A-21-11 ; / [01] REMOVED CRACKED FIXED L/E -26 SPRING IAW SRM 51-40-02-0G.; [02] RECEIVED NEW PART P/N 176A3101U26; A-TAG AK7947; LOCATED AND DRILLED ALL HOLES TO SIZE AND DEBURRED IAW IPC 55-33-11-02A AND SRM 51-40-05-0G; [03] VERIFIED STEP 1;2; [04] OK TO INSTALL P/N 176A3101U26; [05] INSTALLED NEW -26 SPRING IAW SRM 51-40-02-0G.; [06] VERIFIED STEP 5. OK TO CIC; [07] APPLIED CIC IAW AMM 51-21-91-620. ALL WORK COMPLETE.; [08] VERIFIED STEP 7; [09] AUDIT COMPLETE

Part: PLATE — CRACKED (RT WING) · airframe 46,946 hrs · 28,145 cycles

A-061 DOT 007 WIGGLE PLATE PHENOLIC CRACKER UNDER R/H WING PNL 661AB ; / [01] REMOVED AND REPLACED WIGGLE PLATE(P/N 115A3760Y26 ATAG: A62893) UNDER LOWER WING PANEL 651 AB I/A/W SRM 51-40-02 AND IPC 57-50-00-18; [02] OK TO TREAT AND PRIME LOWER WING SKIN; [03] TREATED AND PRIMED LOWER WING SKIN I/A/W AMM 51-21-41-370-803 AND AMM 51-21-72-370-804; [04] VERIFIED STEPS 1;3<BR>OK TO PAINT; [05] APPLIED TOPCOAT TO LOWER WING SKIN I/A/W AMM 51-21-73-370-804; [06] VERIFIED STEP 5<BR>AUDIT C\W

Part: RETAINER — CRACKED (RT WING SEAL) · airframe 46,946 hrs · 28,145 cycles

A-061DOT 008 CURVED BULB SEAL RETAINER CRACKER R/H WING 12'' INBD OF DEFLECTOR RIB ; CORRECTION CHANGE CRACKER TO CRACKED / [01] REMOVED WEB AND RETAINER IASW SRM 51-40-02-0G-0.; [02] VERIFIED NEW PART AS P/N 115A2953-2. A-TAG A24928. IAW BOEING DWG 115A2930 REV-.; [03] LOCATED AND DRILLED RETAINER IAW SRM <BR>51-40-05-0G-0.; [04] INSPECTION CW STEPS 1-3. OK TO INSTALL ON AIRCRAFT.; [05] INSTALLED RETAINER IAW SRM 51-40-02-0G-0. BOEING DWG 115A2930 REV-. ALL STEPS 1-5 C/W.; [06] VERIFIED STEP 5.<BR>AUDIT C/W

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 46,946 hrs · 28,145 cycles

FWD CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED ; / [01] RECIEVED REPAIRD SCUFF PLATE FROM BACKSHOP ON WORKORDER 42436-1400-0001; [02] VERIFIED STEP 1. AUDIT COMPLETE

Part: BEAM — CRACKED (R4 DOOR) · airframe 46,946 hrs · 28,145 cycles

FWD SERVICE DOOR #4 BEAM 141A3536-14 IS CRACKED NEAR INBD HOLE. REMOVED R/1 DOOR LINER I/A/W AMM 52-41-31-000-802 REMOVED R/1 DOOR HANDLE BOX ASSY IAW SRM 51-40-02-0G-0 REMOVED UPPER & LOWER SPICE ANGLE IAW SRM 51-40-02-000-0G. REMOVED R/1 DOOR PNL 841CZ841BZ BEGAN REMOVAL OF #4 BEAM IAW SRM 51-40-02-OG-0. BEGAN LOCATING AND DRILLING #4 BEAM IAW SRM 51-40-05-0G-0 DWG'S 141A6516 AND 141A6535REMOVED AND REPLACED FWD SERVICE DOOR # 4 BEAM P/N 141A3536-14 I/A/W ARM 51-40-02-0G-0 AND BOEING DWG # 141A6516 AND 141A6535.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 46,946 hrs · 28,145 cycles

CABIN FLOOR PANEL 242BF TOP SURFACE HAS AREAS OF PULLED FIBERS. EVALUATED PANEL 242BF AND DAMAGED FIBERS 1PLY TO UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR1A REV73. CLEAN AND PREP PANEL FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3ACE&F REV73. VERIFIED MATERIALS. (A51753)(A24484). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201 REV73. VERIFIED STEP 1 AND OK TO BOND BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3K-M REV73. AAR DIGITAL THERMOMETER 30347 4-29-22 150DEG 3HRS. REPAIRED DAMAGED AREA ON UPPER FACE SHEET OF PANEL 242BF. IAW B737-700 SRM 53-00-50-2R-1 SRM 53-00-50-2R-0.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 46,946 hrs · 28,145 cycles

FWD CARGO FLOOR PANEL 120BF IS CORRODED ALONG EDGE DOT A-203-006 ; / [01] VERIFIED MATERIAL AS 2024-T3; .071; IAW AMM 25-52-01-201-801. A-TAG # A53465.; [02] VERIFIED MATERIAL STEP 1.; [03] OK TO TREAT AND PRIME; [04] FABRICATED REPLACEMENT FWD CARGO FLOOR PANEL; VERIFIED MATERIAL AS 2024-T3 .071 A-TAG # A53465 IAW AMM 25-52-01-201-801. TREATED BACK OF PANEL IAW AMM 51-21-41-370-803. PRIMED TREATED SIDE IAW AMM 51-21-72-370-804; [05] VERIFIED STEP 4.<BR>AUDIT C/W

Part: HANDLE — LOOSE (LT OVRWG ASSIST) · airframe 45,271 hrs · 27,145 cycles

LT OVERWING EXIT ASSIST HANDLE HOUSING IS NOT SECURE. REPAIRED, PER AMM 20-60-11 BY INSTALLING MISSING SCREWS.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 45,031 hrs · 26,995 cycles

SF ESCAPE SLIDE GAUGE IN RED. R & R SF ESCAPE SLIDE, PER MT 725-61-00 + MT 25-66-20 RAR 71071 POS SF TAG 714864 P/N OFF/ON 5A3307-7 S/N OFF BNG 7842 S/N ON BNG 15978.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 44,921 hrs · 26,931 cycles

FA'S REPORT GIRT BER FLAG OVER R1 DOOR DIFFICULT TO SECURE IN ARMED POSITION CLEAN SLIDE LATCHES; CHECKS GOOD SIP FLAG

Part: STRIP — DAMAGED (CABIN) · airframe 44,355 hrs · 26,570 cycles

1FED EMERGENCY FLOOR TRACK STRIP DAMAGED. REMOVED & REPLACED 1FED EMERGENCY FLOOR TRACK STRIP; PER DWG 33500007.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 44,355 hrs · 26,570 cycles

FLOOR BOARD BREAK CRACKED AT STA 540 RIGHT OF BUTT LINE 0. / REMOVED AND REPLACED FLOOR BOARD BREAK ASSY AT STA 540 RIGHT OF BUTT LINE 0 IAW AMM 53-21-00 AND SRM 51-40-02

Part: FLOORBEAM — CRACKED (BS 540) · airframe 44,355 hrs · 26,570 cycles

FLOOR BOARD BREAK CRACKED AT STA 540 LEFT OF BUTT LINE 0. / REMOVED AND REPLACED FLOOR BOARD BREAK ASSY AT STA 540 LEFT OF BUTT LINE 0 IAW SRM 51-40-02 AND AMM 53-21-00

Part: STRIP — DAMAGED (CABIN) · airframe 44,355 hrs · 26,570 cycles

1ABC EMERGENCY FLOOR TRACK STRIP DAMAGED. REMOVED AND REPLACED 1ABC EMERGENCY FLOOR TRACK STRIP PER ENG DWG 33500007.

Part: SIGN — BROKEN (CABIN) · airframe 43,788 hrs · 26,246 cycles

OVERHEAD EXIT SIGN AFT GALLEY BROKEN. / R&R'D AFT OVERHEAD EXIT SIGN PER MM.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 43,527 hrs · 26,088 cycles

OVERHEAD OVERWING EMERG. EXIT SIGN HANGING BY WIRE. / REINSTALLED SEALING EXIT SIGN ASSEMBLY PER AMM 33-51-01 AC OK FOR SERVICE

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 41,646 hrs · 24,873 cycles

EMERGENCY BATTERY PACK M1674 DEFECTIVE AT FORWARD ENTRY RIGHT CEILING PANEL. R&R BATTERY PACK M1674 AS PER AMM.

Part: RIB — CRACKED (APU DOOR) · airframe 41,646 hrs · 24,873 cycles

APU DOOR RIB FWD SIDE OF FWD HINGE HAS WHAT APPEARS TO BE 3 OLD CRACKES BY BOLT AND RIVET HOLES / REMOVED DAMAGE RIB; FABRICATED AND INSTALLED NEW RIB AT RT APU DOOR FWD HINGE FWD SIDE PER REF B737 SRM 51-40-02-0G-0 AND DWG NO 148A6353

Part: SKIN — DAMAGED (AFT FUSELAGE) · airframe 41,646 hrs · 24,873 cycles

FUSELAGE SKIN AT APU DOOR FWD HINGE CUTOUT DAMAGED. / CUT OUT DAMAGED AREA AT FUSELAGE SKIN APU DOOR FWD HINGE PERFORMED ROTO INSP AND HFEC INSP NO CRAKCS NOTED; FABRICATED DOUBLER MAT USED 2024T3.125' PO #1354279 FILLER MAT USED 2024T3.100' PO #1596666 TREATED AND PRIMED REPAIR PARTS; INSTALLED REPAIR AND FILLER REF B737-700 SRM 51-40-02-0G-0; 53-80-01-2R-1 REPAIR 1; SOPM 20-41-02 ; NDTM P6 51-00-00 PROC 16 AND PROC 23

Part: RIB — CRACKED (APU DOOR) · airframe 41,646 hrs · 24,873 cycles

APU DOOR RIB AFT SIDE OF FWD HINGE HAS WHAT APPEARS TO BE 2 OLD CRACKES BY BOLT HOLE. / REMOVED DAMAGE RIB ;FABRICATED AND INSTALED NEW RIB AT RT APU DOOR FWD HINGE AFT SIDE PER REF B737 SRM 51-40-02-0G-0 ANDDWG NO 148A6353

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,646 hrs · 24,873 cycles

R/H HORIZONTAL STABILIZER INTERNAL RIB AT STA. 120.30 CRACKED AT MOST AFT VERTICAL STIFFENER AND LOWER CHORD. / REPAIRED LOWER CHORD PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,646 hrs · 24,873 cycles

R/H HORIZONTAL STABILIZER LEADING EDGE FAIRING 341B CRACKED AT 4TH RIB FROM INBOARD INTERNAL. R&R RIB IAW SRM & DWG.

Part: TRACK — CORRODED (AFT CARGO BAY) · airframe 41,646 hrs · 24,873 cycles

FLOOR TRACK AFT CARGO JUST O\B OF S27R HAS 5 NUTPLATE HOLES CORRODED JUST AFT OF STA 921. / REMOVED AND INSTALLED NEW FLOOR TRACK P/N 7530159 AT O/B OF STR 27R. RBL 13.8 FROM STA 887 TO STA 947 REF B737-700 SRM 51-40-02-0G-0 AND DW # 147A7500

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,646 hrs · 24,873 cycles

INTERCOSTAL JUST OUTBOARD CORRODED AT BS. 921, STR. 27L. R&R TRACK PER SRM AND DWG.

Part: CHANNEL — CORRODED (BS 727E-787) · airframe 41,646 hrs · 24,873 cycles

AFT CARGO COMPARTMENT L/H Z CHANNEL CORRODED BETWEEN BS. 727E+8 TO BS. 787+8. / R&R Z CHANNEL IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,646 hrs · 24,873 cycles

RT HORIZONTAL STAB INTERNAL RIB 4 AT STAB. STA. 120.30 HAD TWO CRACKS AT STIFFENERS LOWER AREA. REPAIRED RIB PER AMM, SRM, AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,646 hrs · 24,873 cycles

RT HORIZONTAL STABILIZER INTERNAL RIB 5 AT STAB. STA. 129.50 HAD ONE CRACK AT STIFFENER LOWER AREA. REPAIRED RIB PER SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 328) · airframe 41,646 hrs · 24,873 cycles

FORWARD CABIN WET AREA R1 DOOR ENTRY FLOOR SUPPORT INTERCOSTAL CRACKED AFT END AT BS. 328, RBL 30. / R&R FLOOR SUPPORT INTERCOSTAL PER SRM.

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 41,646 hrs · 24,873 cycles

FWD CARGO COMPARTMENT.R/H LOWER SIDE WALL Z CHANNEL SUPPORT FLOOR CORRODED AT STA 500 TO STA 500A ; S-25R MKD DOT 60-005 / REMOVED AND REPLACED DAMAGE Z CHANNEL SUPPORT AT FWD CARGO COMP. R/H SIDEWALL LOWER AREA STR 25 RT FROM STA 500 TO STA 500A PER REF B737 SRM 51-40-02-0G-0; AND DWG 143A8126

Part: CHANNEL — CORRODED (BS 767-787) · airframe 41,646 hrs · 24,873 cycles

AFT CARGO COMPARTMENT R/H LOWER SIDE WALL Z CHANNEL SUPPORT CORRODED BETWEEN BS. 767 TO BS. 787, STR. 25R. / R&R Z CHANNEL PER SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 260-360) · airframe 41,646 hrs · 24,873 cycles

FORWARD CABIN WET AREA FORWARD OF L1 DOOR CUTOUT FLOOR SUPPORT SURFACE CRACKED BETWEEN BS. 260 TO BS. 360, LBL 55. R&R FLOOR SUPPORT IAW SRM AND DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,646 hrs · 24,873 cycles

LT HORIZONTAL STABILIZER INTERNAL RIB INBOARD SIDE AT STAB. STA. 120.30 CRACKED AT STIFFENER LOWER AREAS. REPAIRED RIB IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 41,646 hrs · 24,873 cycles

LT MAIN WHEEL WELL VERTICAL PRESURE DECK WEB CRACKED. REPAIRED PER SRM.

Part: WEB — CORRODED (FWD CARGO) · airframe 41,646 hrs · 24,873 cycles

FORWARD CARGO THRESHOLD HAD SEVERAL AREAS OF CORRODED. R&R WEB IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,646 hrs · 24,873 cycles

FLOOR SUPPORT CORRODED. R&R FLOOR SUPPORT PER SRM AND DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 41,646 hrs · 24,873 cycles

FORWARD CARGO DOOR CUTOUT AFT SCUFF PLATE SECTION CRACKED. REPAIRED SCUFF PLATE PER EA.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 41,646 hrs · 24,873 cycles

AFT CARGO AFT CORNER SCUFF PLATE BROKEN. 8-22 (OFF AIRCRAFT) / AFT CARGO AFT CORNER SCUFF PLATE WELD REPAIRED ACCOMPLISHED ON EA NO: 1-A53-2076 REV 11 REF W/O 2015067 ; 1000 ; 0048

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 41,542 hrs · 24,808 cycles

UPPER FORWARD EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT BATTERY PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 41,523 hrs · 24,794 cycles

R1 DOOR SLIDE GIRT BAR HUNG UP ON DOOR FRAME, SLIDE INADVERTENTLY PULLED PARTIALLY FROM COVER, DID NOT DEPLOY, STILL OPERATIONAL. R&R SLIDE ASSEMBLY PER MT.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 40,790 hrs · 24,344 cycles

L1 DOOR SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: SKIN — DEBONDED (FUSELAGE) · airframe 40,658 hrs · 24,265 cycles

SUPPLEMENTAL INFORMATION: FUSELAGE SKIN DISBONDED FROM EGPR STIFFNER AT LOWER RUBBING BLOCK AREA WITH ASSOCIATED SKIN DAMAGE AT ELECTRICAL GROUND POWER RECEPTICLE SURROUND CUTOUT / ACCOMPLISHED PERMANENT REPAIR PER EA #1-753-34233 REF IR

Part: SKIN — DEBONDED (FUSELAGE) · airframe 40,658 hrs · 24,265 cycles

SUPPLEMENTAL INFORMATION: FUSELAGE SKIN DISBONDED AT DAMAGED AREA FROM EGPR STIFFNER AFT SIDE OF ELECTRICAL GROUND POWER RECEPTICLE SURROUND CUTOUT / ACCOMPLISHED PERMANENT REPAIR PER EA #1-753-34233 REV IR

Part: SKIN — DEBONDED (FUSELAGE) · airframe 40,658 hrs · 24,265 cycles

SUPPLEMENTAL INFORMATION: FUSELAGE SKIN AND EGPR STIFFINER BENT OUTWARD AT AFT SIDE OF GROUND POWER RECERTICLE CUTOUT WITH ASSOCIATED DISBONDED SKIN AND PULLED AWAY FROM FASTENERS. AT BS 235.80 AND WL 180. / ACCOMPLISHED PERMANENT REPAIR PER EA #1-753-34233 REV IR

Part: LIGHT — MISSING (EXIT SIGN) · airframe 40,568 hrs · 24,202 cycles

R2 DOOR LOWER EXIT SIGN MISSING. R&R LIGHT ASSEMBLY PER AMM.

Part: FLOOR PANEL — CRACKED (LOWER INT FUSELA) · airframe 39,947 hrs · 23,798 cycles

RAMP REPORTS CRACK IN BIN D FLOOR / REMOVED FABRICATED REPLACEMENT PANEL; AND INSTALLED NEW PANEL PER M/M 25-52-10. CL # 19522

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,923 hrs · 23,124 cycles

RT OVERWING EXTERNAL EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 38,658 hrs · 22,958 cycles

PASSENGER CABIN FLOORBOARD INTERCOSTAL STA 344 - STA 360 BL-0 IS CRACKED 1.75' LONG IN E&E / REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02 AND SRM 51-10-02

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 38,658 hrs · 22,958 cycles

PASSENGER CABIN FLOORBOARD INTERCOSTAL STA 328 - STA 344 BL-46'L IS CRACKED 1.75' LONG IN E&E / REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02 AND SRM 51-10-02

Part: BATTERY — FAILED (CABIN) · airframe 38,658 hrs · 22,958 cycles

EMERGENCY LIGHT BATTERY M1670 FAILED TEST. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 38,658 hrs · 22,958 cycles

EMERGENCY LIGHT BATTERY M1672 FAILED TEST. R&R BATTERY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 38,423 hrs · 22,803 cycles

FORWARD GALLEY EMERGENCY EXIT LIGHT HOUSING BROKEN. R&R SIGN ASSEMBLY PER MM.

Part: HOLDER — OUT OF ADJUST (L1 DOOR GIRT BAR) · airframe 36,659 hrs · 21,653 cycles

L1 DOOR EVAC SLIDE GIRT BAR HOLDER OUT OF ADJUST. / ADJUSTED GIRT BAR HOLDER PER MM.

Part: LAMP — DIM (EMERGENCY LIGHT) · airframe 36,552 hrs · 21,586 cycles

R/H OVERWING EXIT SIDEWALL LIGHT DIM. / RELAMPED LIGHT PER AMM.

Part: LIGHT — DELAMINATED (GALLEY) · airframe 36,552 hrs · 21,586 cycles

R/H AFT ESCAPE PATH LIGHT STRIP BY G3 GALLEY DELAMINATED. / R&R STRIP PER DWG.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 35,611 hrs · 20,960 cycles

L1 DOOR EMERGENCY LIGHT INOPERATIVE. R & R POWER SUPPLY FUSE IAW AMM.

Part: ANGLE — CORRODED (BS 727D-767) · airframe 35,081 hrs · 20,637 cycles

AFT CARGO BAY ZEE ANGLE CORRODED BETWEEN BS 727D TO 767, STRINGER 26R. R & R THE ANGLE IAW SRM.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 35,080 hrs · 20,637 cycles

AFT CARGO COMPARTMENT;5' AFT OF STA 767; FLOOR STRAP HAS AREAS OF CORROSION NEAR DOOR SIDE. / REMOVED CORROSION FOUND TO BE 100% MATERIAL LOSS. REMOVED & REPLACED FLOOR STRAP @ APPROX STA 772 IAW SRM 51-40-02-0G-0. ATAG WN2909

Part: ATTACH BRACKET — CRACKED (RT WING) · airframe 35,081 hrs · 20,637 cycles

RIGHT WING AT WING ROOT UPPER PANEL INBOARD ATTACH BRACKET CRACKED AT FORWARD ATTACH POINT. R & R THE ATTACH BRACKET IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 35,081 hrs · 20,637 cycles

RT WING TRAILING EDGE PANEL AFT OF PYLON VERTICAL BULB ATTACH ANGLE CRACKED. R&R ANGLE IAW DWG.

Part: BRACKET — CRACKED (LT WING) · airframe 35,081 hrs · 20,637 cycles

LEFT WING, ABOVE AND INBOARD OF THE NR 1 AFT FUEL BOOST PUMP BRACKET, ATTACHED TO UPPER REAR SPAR CRACKED. R & R THE BRACKET IAW SRM AND DWG.

Part: BRAKE — CRACKED (MAIN CABIN) · airframe 35,080 hrs · 20,637 cycles

PASSENGER CABIN FLOOR STRUCTURE STA 540 PANEL BREAK LBL 24-BL 0 IS CRACKED ON INBOARD END / REMOVED AND REPLACED FLOOR PANEL SPLICE IAW B737 DRAWING 143A0060 REV A LOCATED AND DRILLED SPLICE IAW B737 SRM 51-40-05-0G-0

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 35,081 hrs · 20,637 cycles

MAIN WHEEL WELL BULKHEAD WEB CRACKED AT BS 663, RBL 35. REPAIRED THE BULHEAD WEB IAW EA.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 34,396 hrs · 20,230 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01674. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 34,396 hrs · 20,230 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01673. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 34,396 hrs · 20,230 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01669. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 34,396 hrs · 20,230 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01668. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 34,396 hrs · 20,230 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01670. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 34,396 hrs · 20,230 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01675. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 34,396 hrs · 20,230 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01672. R & R THE BATTERY PACK IAW AMM.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 34,214 hrs · 20,124 cycles

R2 DOOR SLIDE GRIT BAR ANGLE LOOSE. SECURED THE GIRT BAR HANGER IAW SIP.

Part: DRAIN — SHEARED (BS 1016) · airframe 33,655 hrs · 19,766 cycles

VENT OUTLET AFT OF AFT PRESSURE BULKHEAD ON BOTTOM OF PLANE SHEARED AT BS 1016, STRINGER 26R. REPAIRED THE DRAIN TUBE ASSEMBLY IAW EA.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 32,302 hrs · 18,956 cycles

RIGHT AFT EMERGENCY LIGHT BATTERY FAILED TIME TEST. R & R THE BATTERY PACK IAW AMM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 31,431 hrs · 18,448 cycles

LEFT OVERWING EXIT LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: COVER — MISSING (EXIT SIGN) · airframe 30,285 hrs · 17,800 cycles

R2 DOOR EMERGENCY EXIT SIGN COVER MISSING. R&R LIGHT ASSEMBLY PER AMM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 30,008 hrs · 17,643 cycles

CENTER WING SPAR VAPOR WEB CRACKED AT BS 663, BETWEEN RBL 31 - 38. REPAIRED WEB IAW EA.

Part: SENSOR — FAULTY (RT MLG) · airframe 29,746 hrs · 17,479 cycles

AIR TURN BACK, RT LG GREEN LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE UP. RT LG RED DISAGREEMENT LIGHT WAS ILLUMINATED. R & R SENSOR S0073 IAW AMM.

Part: PLATE — GOUGED (L1 DOOR) · airframe 28,591 hrs · 16,806 cycles

L1 DOOR MOUNT PLATE FOR FWD GIRT BAR FITTING GOUGED. R & R MOUNT PLATE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,591 hrs · 16,806 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO 328, LBL 45. R & R INTERCOSTAL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,591 hrs · 16,806 cycles

AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS 827 TO 847, RBL 19. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,591 hrs · 16,806 cycles

AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS 794 TO 807, RBL 19. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,591 hrs · 16,806 cycles

AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS 807 TO 827, RBL 19. R & R SUPPORT IAW SRM.

Part: NUT PLATE — CORRODED (FUSELAGE) · airframe 28,591 hrs · 16,806 cycles

AFT CARGO AROUND NUTPLATE HOLE CORRODED AT BS 798, RBL 14. REPAIRED NUTPLATE IAW EA.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 28,591 hrs · 16,806 cycles

AFT CARGO DOOR THRESHOLD WEB CORRODED. R & R WEB IAW SRM.

Part: WINGLET — DELAMINATED (LT WING) · airframe 28,591 hrs · 16,806 cycles

LEFT WINGLET LE FRONT SPAR DELAMINATED AT STATION 4 AT UPPER & LOWER RADIUS. R & R LT WINGLET IAW MM.

Part: SIGN — MISSING (CABIN) · airframe 27,677 hrs · 16,266 cycles

RIGHT OVERWING EMER EXIT SIGN MISSING. INSTALLED SIGN IAW AMM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 25,149 hrs · 14,797 cycles

L2 WINDOW UPPER EDGE CRACKED. R & R WINDOW IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,410 hrs · 14,374 cycles

R2 DOOR AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. RE LAMPED LIGHT IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 23,184 hrs · 13,668 cycles

AFT EMERGENCY EXIT LIGHT BATTERY PACK FAIL CAPACITY TEST. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 23,184 hrs · 13,668 cycles

FWD EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY IAW AMM.

Part: COVER — MISSING (R2 DOOR) · airframe 22,819 hrs · 13,460 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER, R & R LIGHT ASSEMBLY IAW MM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 21,272 hrs · 12,588 cycles

LT HORIZONTAL STABILIZER RIB CRACKED AT STABILIZER STATION 147.9. REPAIRED RIB IAW EA.

Part: PANEL — CORRODED (CARGO BAY) · airframe 21,272 hrs · 12,588 cycles

AFT CARGO COMPARTMENT AFT FLOOR PANEL 140CF CORRODED AROUND ENTIRE TOP SURFACE TAPED EDGES. REPAIRED PANEL IAW SRM & SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 21,272 hrs · 12,588 cycles

SEAT TRACK FLANGE FORWARD FASTENER HOLE CRACKED AT STATION 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 21,272 hrs · 12,588 cycles

SEAT TRACK FLANGE CRACKED AT STATION 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 21,272 hrs · 12,588 cycles

SEAT TRACK FLANGE CRACKED AT STATION 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 21,272 hrs · 12,588 cycles

SEAT TRACK FLANGE FORWARD FASTENER HOLE CRACKED AT STATION 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,272 hrs · 12,588 cycles

"Z" ANGLE CORRODED BETWEEN STATION 500 - STATION 500D, LBL 24. REPAIRED Z-ANGLE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 21,272 hrs · 12,588 cycles

SEAT TRACK FLANGE FORWARD FASTENER HOLE CRACKED AT STATION 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 21,272 hrs · 12,588 cycles

G1 GALLEY EMERGENCY EXIT LIGHTS BROKEN. R&R LIGHTS IAW AMM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,272 hrs · 12,588 cycles

LT FLOOR SUPPORT Z ANGLE UPPER SURFACE CORRODED BETWEEN BS 807 - BS 747. R&R "Z" ANGLE IAW SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 21,272 hrs · 12,588 cycles

LT WING INBD FIXED TE UPPER PANEL LOWER MIDDLE BRACKET CRACKED. R&R BRACKET IAW SRM & DRAWING.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,272 hrs · 12,588 cycles

RT Z ANGLE UPPER SURFACE CORRODED BETWEEN BS 727E+10 - BS 767. REPAIRED Z ANGLE IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 21,272 hrs · 12,588 cycles

FWD LAVATORY EMERGENCY EXIT LIGHTS BROKEN. R&R LIGHTS IAW AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 21,069 hrs · 12,475 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MT AND AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 21,069 hrs · 12,475 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW AMM AND MT.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 21,069 hrs · 12,475 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MM AND MT.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 21,069 hrs · 12,475 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MT AND MM.

Part: COLLAR — BROKEN (L1 DOOR) · airframe 21,069 hrs · 12,475 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINING COLLAR BROKEN. R & R COLLAR ASSY IAW AMM.

Part: COLLAR — BROKEN (R1 DOOR) · airframe 21,069 hrs · 12,475 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINING COLLAR BROKEN. R & R COLLAR ASSY IAW AMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 21,069 hrs · 12,475 cycles

FUSELAGE EXTERNAL POWER RECEPTACLE DOOR CUTOUT INTERNAL DOUBLER SKIN CRACKED ON AFT EDGE RUB BLOCK AREA. REPAIRED DOUBLER IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 20,455 hrs · 12,107 cycles

EMERGENCY EXIT LIGHT CENTER CEILING BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 18,864 hrs · 11,197 cycles

RIGHT AFT GALLEY EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW M/M.

Part: SIGN — UNSECURE (CABIN) · airframe 18,331 hrs · 10,903 cycles

AFT GALLEY SERVICE DOOR EMERGENCY EXIT SIGN FELL OFF. RE-INSTALLED SIGN PER M/M.

Part: LENS — MISSING (CABIN) · airframe 17,477 hrs · 10,418 cycles

R2 DOOR EMERGENCY EXIT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER M/M.

Part: SIGN — BROKEN (CABIN) · airframe 17,037 hrs · 10,155 cycles

AFT RT EMERGENCY EXIT DOOR SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 16,577 hrs · 9,893 cycles

EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER AMM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 16,577 hrs · 9,893 cycles

RT HORIZONTAL STAB LOWER IN-SPAR SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 16,577 hrs · 9,893 cycles

LT HORIZONTAL STAB LOWER IN-SPAR SKIN CRACKED AT STA 129.5. REPAIRED SKIN IAW SRM.

Part: LENS — BROKEN (CABIN) · airframe 16,577 hrs · 9,893 cycles

LT EEPLS LENS BROKEN BETWEEN ROW 1 TO ROW 10. REMOVED AND REPLACED LENS PER AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 15,544 hrs · 9,292 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.

Part: COVER — CRACKED (CABIN) · airframe 15,436 hrs · 9,232 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 3. REMOVED AND REPLACED COVER PER MM.

Part: LENS — BROKEN (CABIN) · airframe 15,436 hrs · 9,232 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 15,436 hrs · 9,232 cycles

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

Part: LENS — MISSING (CABIN) · airframe 15,183 hrs · 9,088 cycles

EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 14,324 hrs · 8,600 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP BETWEEN ROW 11 TO ROW 17. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 14,242 hrs · 8,550 cycles

DURING SCHEDULED HC CHECK, LT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,242 hrs · 8,550 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 14,242 hrs · 8,550 cycles

DURING SCHEDULED HC CHECK, RT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 13,623 hrs · 8,195 cycles

R2 DOOR EMERGENCY EXIT SIGN LENS MISSING. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 11,433 hrs · 6,926 cycles

DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT LIGHT ON AFT LAV BY L2 DOOR INOP. CONNECTED LIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 9,713 hrs · 5,950 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 9,540 hrs · 5,846 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 7,330 hrs · 4,483 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINTER, DID NOT DEPLOY. REINSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,191 hrs · 3,793 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 5,914 hrs · 3,621 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LENS — BROKEN (CABIN) · airframe 5,982 hrs · 3,664 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED LENS PER MM.

Part: CAP — MISSING (CABIN) · airframe 5,369 hrs · 3,306 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EEPS END CAP MISSING. INSTALLED ENCAP PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 5,107 hrs · 3,145 cycles

FOUND FWD ENTRY FLOOR LEVEL EMERGENCY EXT SIGN LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 3,041 hrs · 1,841 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,345 hrs · 1,398 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 5 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 561 hrs · 339 cycles

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

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 549 hrs · 331 cycles

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

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 327 hrs · 200 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.