N8328A

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 41,060 hrs · 19,560 cycles

LEFT OWE EMERGENCY LIGHTS INOPERATIVE. R & R LT OVERWING EMERGENCY LIGHTS BATTERY PACK AND OPS CHECK GOOD IAW AMM 33-51-06-960-805

Part: SEAT — OUT OF ADJUST (ZONE 200) · airframe 40,852 hrs · 19,443 cycles

EMERGENCY EXIT ROW PASSENGER SEAT BACK NOT FULLY LOCKED OUT AT SEAT 13D. RELOCKED SEAT BACK FULLY AT SEAT 13D PER AMM 25-22-00.

Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 40,296 hrs · 19,153 cycles

EMERGANCY LIGHT ON FWD SERVICE DOOR IS INOP <[01]. REVAMPED LIGHT PER AMM 33-51-04 OPS CHECK GOOD AT THIS TIME.

Part: WEB — CRACKED (ZN 400 NACELLE/P) · airframe 38,576 hrs · 18,243 cycles

CRACK INBOARD FAN COWL SUPPORT WEB ON ENGINE 1 2024-645717<[01] REPLACED SHIELD P/N: 314-2259-4; AND FASTENERS LOCATED INBOARD FAN COWL ON ENGINE 1 I.A.W B737-800 SRM 51-40-02 ; SRM 51-10-02 PARAGRAPH 9 AND CMM 71-13-30 ITEM (P) PAGE 10092;[02] CORRECTED STEP 1<BR>REPLACED SHIELD P/N: 314-2259-4; AND FASTENERS LOCATED INBOARD FAN COWL ON ENGINE 1 I.A.W B737-800 SRM 51-40-02 ; SRM 51-10-02 PARAGRAPH 9 AND CMM 71-13-30 ITEM (P) PAGE 10092. SEE INDIVIDUAL SIGN OFFS BELOW;[03] REPLACED SHIELD P/N: 314-2259-4; AND FASTENERS LOCATED INBOARD FAN COWL ON ENGINE 1 I.A.W B737-800 SRM 51-40-02 ; SRM 51-10-02 PARAGRAPH 9 AND CMM 71-13-30 ITEM (P) PAGE 10092. SEE INDIVIDUAL SIGN OFFS BELOW

Part: FITTING — CORRODED (ZN 600 RIGHT WIN) · airframe 38,576 hrs · 18,243 cycles

CORROSION FITTING ACCESS PANEL 642BB AT RT WING 2024-645707<[01] REPLACED FITTING AND FASTENERS LOC. ACCESS PANEL 624BB AT RT WING I.A.W. B737-800 SRM 51-40-02 SRM 51-10-02; DWG 113A9350 SHEET 7 REV. E. SEE INDIVIDUAL SING OFFS BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SING OFFS BELOW

Part: ANGLE — CORRODED (ZN 500 LEFT WING) · airframe 38,576 hrs · 18,243 cycles

CORROSION ANGLE LOCATED ORSS423 UPPER SIDE TRAILING EDGE AT LT WING 2024-645624<[01] REPLACED ANGLE LOCATED ORSS423 UPPER SIDE TRAILING EDGE AT LT WING IAW B737-800 SRM-51-40-02-0G-0 AND DWG-115A3500 SHEET 31; REV: A;[02] TASK COMPLETED

Part: ANGLE — CORRODED (ZN 500 LEFT WING) · airframe 38,576 hrs · 18,243 cycles

CORROSION ANGLE LOCATED ORSS412 AND ORSS404 UPPER SIDE TRAILING EDGE AT LT WING 2024-645623<[01] REPLACED ANGLE LOCATED ORSS412 TO ORSS404 UPPER SIDE TRAILING EDGE AT LT WING IAW B737-800 SRM 51-40-02-0G-0 AND DRAWING 115A3500 SHEET 31 REV. A;[02] REPLACED ANGLE LOCATED ORSS412 TO ORSS404 UPPER SIDE TRAILING EDGE AT LT WING IAW B737-800 SRM 51-40-02-0G-0 AND DRAWING 115A3500 SHEET 31 REV. A

Part: ANGLE — CORRODED (ZN 500 LEFT WING) · airframe 38,576 hrs · 18,243 cycles

CORROSION ANGLE LOCATED ORSS390 UPPER SIDE TRAILING EDGE AT LT WING 2024-645625<[01] REPLACED ANGLE LOCATED ORSS390 UPPER SIDE TRAILING EDGE AT LT WING IAW B737-800 SRM-51-40-02-0G-0 AND DWG-115A3500 SHEET 31; REV: A;[02] REPLACED ANGLE LOCATED ORSS390 UPPER SIDE TRAILING EDGE AT LT WING IAW B737-800 SRM-51-40-02-0G-0 AND DWG-115A3500 SHEET 31; REV: A

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 38,576 hrs · 18,243 cycles

CRACK ANGLE LOCATED DEFLECTION CONTROL RIB ORSS279 AT LT WING 2024-645629<[01] REPLACED ANGLE LOCATED DEFLECTION CONTROL RIB ORSS279 AT LT WING IAW B737-800 SRM-51-40-02 AND DWG-115A6200 REV: A;[02] TASK COMPLETED

Part: ANGLE — CORRODED (ZN 500 LEFT WING) · airframe 38,576 hrs · 18,243 cycles

CORROSION ANGLE LOCATED ORSS450 TO ORSS472 UPPER SIDE TRAILING EDGE AT LT WING 2024-645621<[01] REPLACED ANGLE LOCATED ORSS450 TO ORSS472 UPPER SIDE TRAILING EDGE AT LT WING IAW B737-800 SRM-51-40-02 AND DWG-115A3551 SHEET 3 REV: -;[02] REPLACED ANGLE LOCATED ORSS450 TO ORSS472 UPPER SIDE TRAILING EDGE AT LT WING IAW B737-800 SRM-51-40-02 AND DWG-115A3551 SHEET 3 REV:

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 38,576 hrs · 18,243 cycles

CRACK CORRUGATED PLATE LOCATED IRSS 216 TRAILING EDGE AT LT WING 2024-645630<[01] REPLACED CORRUGATED PLATE LOCATED IRSS 216 TRAILING EDGE AT LT WING IAW B737-800 SRM 51-40-02-0G-0 AND DRAWING 115A2713 SHEET 6 REV. A;[02] REPLACED CORRUGATED PLATE LOCATED IRSS 216 TRAILING EDGE AT LT WING IAW B737-800 SRM 51-40-02-0G-0 AND DRAWING 115A2713 SHEET 6 REV. A

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ON SCUFF PLATE AFT CORNER LOCATED AFT CARGO COMPARTMENT. 2024-645608<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30;S/N:B23399190;DUE DATE:04-MAR-25.;[02] EQUIPMENT P/N XRP-3000; S/N 1753759; DUE DATE 07-DEC-24 WAS USED ON STEP 4;[03] REPAIRED SCUFF PLATE AFT CORNER LOCATED AFT CARGO COMPARTMENT IAW BOEING 737-800 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED SCUFF PLATE AFT CORNER LOCATED AFT CARGO COMPARTMENT IAW BOEING 737-800 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT ANGLE — CRACKED (ZN 800 DOOR) · airframe 38,576 hrs · 18,243 cycles

CRACK ON SUPPORT ANGLE LOCATED ACCESS PANEL 834DZ AT AFT ENTRY DOOR 2024-645596<[01] REPLACED SUPPORT ANGLE LOCATED ACCESS PANEL 834DZ AT AFT ENTRY DOOR IAW B737-800 SRM 51-10-02-OG-0 ITEM 9; SRM-51-40-02-OG-PRODURE-GENERAL-FASTENERS-INSTALLATION-AND-REMOVAL AND DWG_411A2119-175A SHS REV:-; LENGHT OF DAMAGE IS 0.298 TOOL USED: DIGITAL CALIPER PN: 500-197-30; SN: B23394221; DUE DATE: 04-FEB-2025.;[02] EDITED STEP 1(CORRECTED DRAWING NUMBER)<BR>REPLACED SUPPORT ANGLE LOCATED ACCESS PANEL 834DZ AT AFT ENTRY DOOR IAW B737-800 SRM 51-10-02-OG-0 ITEM 9; SRM-51-40-02-OG-PRODURE-GENERAL-FASTENERS-INSTALLATION-AND-REMOVAL AND DWG_411A2119 REV -; LENGHT OF DAMAGE IS 0.298 TOOL USED: DIGITAL CALIPER PN: 500-197-30; SN: B23394221; DUE DATE: 04-FEB-2025.;[03] TASK COMPLETED

Part: NUT PLATE — CORRODED (ZN 600 RIGHT WIN) · airframe 38,576 hrs · 18,243 cycles

CORROSION RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS308 AT RT WING 2024-645602<[01] REMOVED PART AND PERFORMED GVI ON AREA NOT FOUND MORE DAMAGE AND REPLACED LEADING EDGE RAIL NUTPLATE LOCATED ON OFSS308 AT RT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 STEP 9;[02] REMOVED PART AND PERFORMED GVI ON AREA NOT FOUND MORE DAMAGE AND REPLACED LEADING EDGE RAIL NUTPLATE LOCATED ON OFSS308 AT RT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 STEP 9

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ANGLE - CLIP LOCATED BS500H AND RBL23 AFT POSITION FWD CARGO COMPARTMENT 2024-645592 CRACK ANGLE - CLIP LOCATED BS500H AND RBL25 AFT POSITION FWD CARGO COMPARTMENT<[01] REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS500H RBL25 AFT POSITION. FWD CARGO COMPARTMENT. IAW B737-800 SRM 51-40-02 SRM 51-10-02 Ï¿½TEM 9. AND DWG 143A7505 SHEETS 108 REV- SEE INDIVIDUAL SIGNS OF BELOW.;[02] REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS500H RBL25 AFT POSITION. FWD CARGO COMPARTMENT. IAW B737-800 SRM 51-40-02 SRM 51-10-02 Ï¿½TEM 9. AND DWG 143A7505 SHEETS 108 REV- SEE INDIVIDUAL SIGNS OF BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ANGLE - CLIP LOCATED BS500H AND LBL23 FWD POSITION FWD CARGO COMPARTMENT 2024-645577 CRACK ANGLE - CLIP LOCATED BS500H AND LBL25 FWD POSITION FWD CARGO COMPARTMENT<[01] REPLACED ANGLE - CLIP. LOCATED BS500H AND LBL25 FWD POSITION FWD CARGO COMPARTMENT. IAW B737-800 SRM 51-40-02-0G. AND DWG 143A7505 SHEET 108 REV.-.;[02] CORRECTED STEP 1:<BR>REPLACED ANGLE - CLIP. LOCATED BS500H AND LBL25 FWD POSITION FWD CARGO COMPARTMENT. IAW B737-800 SRM 51-40-02-0G. AND DWG 143A7505 SHEET 108 REV.-. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED ANGLE - CLIP. LOCATED BS500H AND LBL25 FWD POSITION FWD CARGO COMPARTMENT. IAW B737-800 SRM 51-40-02-0G. AND DWG 143A7505 SHEET 108 REV.-. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ANGLE - CLIP LOCATED BS440 AND LBL23 AFT POSITION FWD CARGO COMPARTMENT 2024-645575 CRACK ANGLE - CLIP LOCATED BS440 AND LBL25 AFT POSITION FWD CARGO COMPARTMENT<[01] REPLACED ANGLE - CLIP LOCATED ON BS440 AND LBL23 AFT POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG #143A7505 SHEET 108 REV-:. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE - CLIP LOCATED ON BS440 AND LBL23 AFT POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DWG #143A7505 SHEET 108 REV-:. <BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ANGLE - CLIP LOCATED BS500G AND RBL23 FWD POSITION FWD CARGO COMPARTMENT 2024-645579<[01] REPLACED ANGLE - CLIP LOCATED ON BS500G AND RBL25 FWD POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G. AND DWG 143A7505 SHEET 108 REV-.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED ANGLE - CLIP LOCATED ON BS500G AND RBL25 FWD POSITION FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02-0G. AND DWG 143A7505 SHEET 108 REV-.<BR><BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ANGLE - CLIP LOCATED BS400 AND LBL23 FWD CARGO COMPARTMENT 2024-645574 CRACK ANGLE - CLIP LOCATED BS400 AND LBL25 FWD CARGO COMPARTMENT<[01] REPLACED ANGLE-CLIP LOCATED ON BS400 AND LBL23 FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND 143A7505 SHEET 108 REV-:. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED ANGLE-CLIP LOCATED ON BS400 AND LBL23 FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND 143A7505 SHEET 108 REV-:. <BR>SEE INDIVIDUAL SIGN-OFF BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ANGLE - CLIP LOCATED BS500H AND RBL23 FWD POSITION FWD CARGO COMPARTMENT 2024-645578 CRACK ANGLE - CLIP LOCATED BS500H AND RBL25 FWD POSITION FWD CARGO COMPARTMENT<[01] REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS500H AND RBL23 FWD POSITION FWD CARGO COMPARTMENT.IAW B737-800 SRM 51-40-02 AND DWG 143A7505 SHEETS 108 REV- SEE INDIVIDUAL SIGNS OF BELOW.;[02] REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS500H AND RBL23 FWD POSITION FWD CARGO COMPARTMENT.IAW B737-800 SRM 51-40-02 AND DWG 143A7505 SHEETS 108 REV- SEE INDIVIDUAL SIGNS OF BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ANGLE - CLIP LOCATED BS500G AND LBL23 AFT POSITION FWD CARGO COMPARTMENT 2024-645576<[01] REPLACED ANGLE - CLIP. LOCATED BS500G AND LBL25 AFT POSITION FWD CARGO COMPARTMENT. IAW B737-800 SRM 51-40-02-0G. AND DWG 143A7505 SHEET 108 REV.-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED ANGLE - CLIP. LOCATED BS500G AND LBL25 AFT POSITION FWD CARGO COMPARTMENT. IAW B737-800 SRM 51-40-02-0G. AND DWG 143A7505 SHEET 108 REV.-. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ON ANGLE - SUPPORT LOCATED BS867 AND LBL10 AT AFT CARGO COMPARTMENT 2024-645571<[01] REPLACED SUPPORT LOCATED BS867 AND LBL10 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02 AND DWG 149A8102 REV: A LENGTH OF DAMAGE IS 0.125 TOOL USED: DIGITAL CALIPER PN: 500-752-20; SN: B21037208; DUE DATE: 17-APR-2025;[02] TASK COMPLETED

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 38,576 hrs · 18,243 cycles

CORROSION ON FLOOR BEAN LOCATED BS 947.5 LBL 50 WL 208.1 AT AFT GALLEY AREA 2024-645560 CORRECTED FAULT NAME: CORROSION ON FLOOR BEAM LOCATED BS 947.5 LBL 50 WL 208.1 AT AFT GALLEY AREA< REMOVED AND REPLACED PARTS PER 737-800 SRM 51-40-02 AS SHOWN IN 15/OCT/20 REFERENCE NRC D166540.;[06] CORRECTED STEP 5 <BR><BR>REMOVED AND REPLACED PARTS PER 737-800 SRM 51-40-02 AS SHOWN IN 15/OCT/20 REFERENCE NRC D166540.<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[07] CORRECTED STEP 6<BR><BR>REPLACED REPAIR PARTS [1] T-CHORD LOC. ON BS947.5 WL208.1 AND LBL 7.8 TO LBL 61 AFT GALLEY AREA IAW B737-800 SRM-53-70-51-2R-5 REPAIR 5 AS SHOWN IN 15/OCT/20 REFERENCE NRC D166540.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[08] CORRECTED STEP 7<BR><BR>REMOVED AND REPLACED REPAIR PART [1] T-CHORD LOC. ON BS947.5 WL208.1 AND LBL 7.8 TO LBL 61 AFT GALLEY AREA IAW B737-800 SRM-51-40-02 AS SHOWN IN EA-20-153-02001; ISSUE DATE: 15/OCT/20 REFERENCE NRC D166540.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[09] REMOVED AND REPLACED REPAIR PART [1] T-CHORD LOC. ON BS947.5 WL208.1 AND LBL 7.8 TO LBL 61 AFT GALLEY AREA IAW B737-800 SRM-51-40-02 AS SHOWN IN EA-20-153-02001; ISSUE DATE: 15/OCT/20 REFERENCE NRC D166540.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.<BR>RII ITEM

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 38,576 hrs · 18,243 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-645554<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. IAW B737-800. SRM 51-40-02-0G. AND DWG 141A8310 SHEET 33. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT BRACKET — CRACKED (ZN 200 FUS TOP) · airframe 38,576 hrs · 18,243 cycles

CRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-645563<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-800 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02 AND DWG-146A7901-88B REV A; LENGHT OF DAMAGE IS 0.135 TOOL USED: DIGITAL CALIPER PN: 500-752-20; SN: B21037208; DUE DATE: 17-APR-2025.;[02] TASK COMPLETED

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ON INTERCOSTAL WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA 2024-645510<[01] REPLACED INTERCOSTAL WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING 141A5400 SHEET 32 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INTERCOSTAL WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING 141A5400 SHEET 32 REV - SEE INDIVIDUAL SIGN OFF BELOW.

Part: WEB — CRACKED (ZN 200 FUS TOP) · airframe 38,576 hrs · 18,243 cycles

CRACK ON WEB LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA 2024-645514<[01] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 0; WL 208.10 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02-0G-0. SRM 51-10-02 ITEM 9 AND DRAWING 141A5400; SHEET 20; REV -. SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTED STEP 1<BR>REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 0; WL 208.10 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02-0G-0. AND DRAWING 141A5400; SHEET 20; REV -. SEE INDIVIDUAL SIGN OFFS BELOW;[03] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 0; WL 208.10 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02-0G-0. AND DRAWING 141A5400; SHEET 20; REV -. SEE INDIVIDUAL SIGN OFFS BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ON SUPPORT ANGLE LOCATED ON FLOOR STRUCTURE BTW BS 380 TO BS 400 LBL 12 AT PASSENGER CABIN 2024-645507<[01] REPLACED SUPPORT ANGLE LOCATED ON FLOOR STRUCTURE BTW BS 380 TO BS 400 LBL 12 AT PASSENGER CABIN AW B737-800 SRM 51-40-01 AND DWG 143A5400 SHEET 142 REV-.<BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ANGLE LOCATED ON FLOOR STRUCTURE BTW BS 380 TO BS 400 LBL 12 AT PASSENGER CABIN AW B737-800 SRM 51-40-01 AND DWG 143A5400 SHEET 142 REV-.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ON SUPPORT ANGLE LOCATED ON FLOOR STRUCTURE BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN 2024-645509<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN I.A.W B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 143A5400 SHEET: 140 REV: -. SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN I.A.W B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 143A5400 SHEET: 140 REV: - AND DWG: 143A5400 SHEET: 142 REV: -. SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN I.A.W B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 143A5400 SHEET: 140 REV: - AND DWG: 143A5400 SHEET: 142 REV: -. SEE INDIVIDUAL SIGN OFF BELOW

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 38,576 hrs · 18,243 cycles

CRACK INNER CHORD LOCATED BS 303.9 AT LEVEL STR 17L AT FWD GALLEY AREA 2024-645515<[01] REPLACED INNER CHORD AND FASTENERS LOCATED ON BS270 TO BS360 WL 208.10 STR 17L AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02. SRM 51-10-02 Ï¿½TEM 9. DWG 141A8110 SHEET 9 REV:A. DWG 141A8110 SHEET 11 REV:- AND DWG 140A9810 SHEET 48 REV:- SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED INNER CHORD AND FASTENERS LOCATED ON BS270 TO BS360 WL 208.10 STR 17L AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02. SRM 51-10-02 Ï¿½TEM 9. DWG 141A8110 SHEET 9 REV:A. DWG 141A8110 SHEET 11 REV:- AND DWG 140A9810 SHEET 48 REV:- SEE INDIVIDUAL SIGN OFFS BELOW. CERTIFIED AS RII.

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CORROSION ON SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL21 AT AFT CARGO COMPARTMENT 2024-645517<[01] REPLACED SHIELD LOCATED BTW BS767 TO BS794.3 WL156 AND RBL21 AT AFT CARGO COMPARTMENT I.A.W B737-800 SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0; DWG 146A0081 SHEET 46 REV ?-?<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 38,576 hrs · 18,243 cycles

CRACK ON SUPPORT ANGLE LOCATED ON FLOOR STRUCTURE BTW BS 380 TO BS 400 LBL 51 AT PASSENGER CABIN 2024-645508<[01] REPLACED SUPPORT ANGLE LOCATED ON FLOOR STRUCTURE BTW BS 380 TO BS 400 LBL 51 AT PASSENGER CABIN I.A.W B737-800 SRM 51-10-02-0G-0 AND DWG 143A5400 SHEET 141 REV ?-? AND DWG 143A5400 SHEET 138 REV ?-?<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT ANGLE LOCATED ON FLOOR STRUCTURE BTW BS 380 TO BS 400 LBL 51 AT PASSENGER CABIN I.A.W B737-800 SRM 51-10-02-0G-0 AND DWG 143A5400 SHEET 141 REV ?-? AND DWG 143A5400 SHEET 138 REV ?-?<BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: WEB — CRACKED (ZONE 200) · airframe 38,576 hrs · 18,243 cycles

CRACK ON WEB LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 LBL 47.5 AT FWD GALLEY AREA 2024-645516<[01] REPLACED WEB LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 LBL 47.5 AT FWD GALLEY AREA IAW. B737-800 SRM 51-40-02-0G AND DRAWING 141A5400 REV - SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED WEB LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 LBL 47.5 AT FWD GALLEY AREA IAW. B737-800 SRM 51-40-02-0G AND DRAWING 141A5400 REV - SEE INDIVIDUAL SIGN OFFS BELOW.<BR>TASK CERTIFIED

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS727I TO BS767 WL156 AND RBL21 AT AFT CARGO COMPARTMENT 2024-645518<[01] STEP 3 TOOL USED THICKNESS GAGE PN:45MG; SN: 232019809; DUE DATE: 08-OCT-2025;[02] REPLACED SUPPORT ZEE SECTION LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 10; SRM 51-40-02; SRM 53-00-53-2R-6 REPAIR 6; DWG 146A7500 SHEET 213 REV - AND DWG 146A7502 SHEET 50 REV - SEE INDIVIDUAL SIGN OFFS BELOW;[03] REPLACED SUPPORT ZEE SECTION LOCATED BTW BS727E TO BS767 WL156 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 10; SRM 51-40-02; SRM 53-00-53-2R-6 REPAIR 6; DWG 146A7500 SHEET 213 REV - AND DWG 146A7502 SHEET 50 REV - SEE INDIVIDUAL SIGN OFFS BELOW AS RII

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ON INTERCOSTAL WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 LBL 12 AT FWD GALLEY AREA 2024-645511<[01] REPLACED INTERCOSTAL WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 LBL 12 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING 141A5400 SHEET 46 REV A SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED INTERCOSTAL WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 LBL 12 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING 141A5400 SHEET 46 REV A SEE INDIVIDUAL SIGN OFF BELOW

Part: CHANNEL — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK CHANNEL SUPPORT LOCATED ON BS727 AND RBL6 BULKHEAD AREA AT AFT CARGO COMPARTMENT 2024-645519<[01] REPLACED SUPPORT CHANNEL LOCATED ON BS727 AND RBL6 BULKHEAD AREA AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9 AND DWG-144A9401 SHEET 4 REV: C.;[02] CERTIFIED WORK PERFORMED.

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 38,576 hrs · 18,243 cycles

CRACK ON INTERCOSTAL WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 12 AT FWD GALLEY AREA 2024-645512<[01] REPLACED INTERCOSTAL WEB AND FASTENER LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 12 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING 141A5400 SHEET 13 REV- SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INTERCOSTAL WEB AND FASTENER LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 12 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02 AND DRAWING 141A5400 SHEET 13 REV- SEE INDIVIDUAL SIGN OFF BELOW.

Part: COVER — MISSING (ZONE 200) · airframe 38,576 hrs · 18,243 cycles

MISSING COVER PLATE ON CENTER EMERGENCY LIGHT ON PASSENGER CABIN (2EA) 2024-645427<[01] INSTALLED COVER PLATE ON CENTER EMERGENCY LIGHT ON PASSENGER CABIN (2EA) IAW KOITO MANUFACTURING CMM 33-24-03 REV. 24 PAGE 7008 STEP 8.A.14.(17) AND PAGE 10032 ITEM 380.;[02] INSTALLED COVER PLATE ON CENTER EMERGENCY LIGHT ON PASSENGER CABIN (2EA) IAW KOITO MANUFACTURING CMM 33-24-03 REV. 24 PAGE 7008 STEP 8.A.14.(17) AND PAGE 10032 ITEM 380.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 38,576 hrs · 18,243 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 692 AT BL 0 WING CENTER SECTION AT PASSENGER CABIN 2024-645431<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-25.;[02] REPLACED ANGLE AND FASTENERS FLOOR STRUCTURE LOCATED ON BS 692 AT BL 0 WING CENTER SECTION AT PASSENGER CABIN IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV A SEE INDIVIDUAL SIGN OFFS BELOW;[03] REPLACED ANGLE AND FASTENERS FLOOR STRUCTURE LOCATED ON BS 692 AT BL 0 WING CENTER SECTION AT PASSENGER CABIN IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV A SEE INDIVIDUAL SIGN OFFS BELOW

Part: SKIN — DEBONDED (ZONE 500 FLAP) · airframe 38,574 hrs · 18,242 cycles

CUSTOMER REQUEST - DEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT LT WING 2024-645390<[01] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18175478 DUE DATE 25/JAN/25. POSITECTOR P/N NSA S/N 110098 DUE DATE 05/SEP/25.;[02] CORRECTIVE ACTION 1 ENTERED AS IN ERROR CORRECT CORRECTIVE ACTION IS TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18175478 DUE DATE 25/JAN/25. POSITECTOR P/N NS2 S/N 110098 DUE DATE 05/SEP/25.;[03] EQUIPMENT P/N BONDMASTER 600M; S/N 220052310; DUE DATE 17-NOV-24 WAS USED ON STEP 9;[04] TOOL USED SCALE P/N: SPX621; S/N: 8340225453; DUE DATE: 01-SEP-25.;[05] REPAIRED IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT LT WING IAW B737-800 SRM 57-53-01-2R-7 REPAIR 7. SEE INDIVIDUAL SIGN OFFS BELOW.;[06] REPAIRED IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT LT WING IAW B737-800 SRM 57-53-01-2R-7 REPAIR 7. SEE INDIVIDUAL SIGN OFFS BELOW. COMPLETED TASK;[07] REPAIRED IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT LT WING IAW B737-800 SRM 57-53-01-2R-7 REPAIR 7. SEE INDIVIDUAL SIGN OFFS BELOW. COMPLETED TASK. RII.

Part: FLAP — DEBONDED (ZN 500 LEFT WING) · airframe 38,574 hrs · 18,242 cycles

CUSTOMER REQUEST - DEBONDED EXTERNAL SKIN OB AFT FLAP LOWER SURFACE IB SIDE AT LT WING 2024-645399<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189521 DUE DATE: 26-JAN-25;[02] STEP 3. TOOL USED ULTRASONIC EQUIPMENT PN: USM GO+ ; SN: USMGO11040089; DUE DATE: 21-MAY-25.;[03] TOOL USED; CALIPER PN: 500-197-30; SN: A18229508; DUE DATE: 14-JAN-25 ;HOT BONDER PN: HCS9200B-AV; SN: 18185733; DUE DATE: 25-JAN-25.;[04] TOOL USED HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 15 FEB 25.;[05] TOOL USED STEP 15: ULTRASONIC EQUIPMENT; P/N: BONDMASTER 6004; S/N: 220052310; DUE DATE: 17 NOV 24.;[06] REPAIRED OB AFT FLAP LOWER SURFACE IB SIDE AT LT WING IAW B737-800 SRM 57-53-01-2R-16 REPAIR 16. SEE INDIVIDUAL SIGN OFFS BELOW.;[07] CORRECTIVE ACTION #6 ENTER BY ERROR<BR><BR>THE CORRECT CORRECTIVE ACTION IS:<BR><BR>REPAIRED OB AFT FLAP LOWER SURFACE IB SIDE AT LT WING IAW B737-800 SRM 57-53-01-2R-16-REPAIR 16. (REPAIR 16 - OUTBOARD AFT FLAP TRAILING EDGE WEDGE ASSEMBLY REPAIR - TAP TEST EVERY 6;875 CYC OR 30 MONTHS - INTERIM REPAIR ). SEE INDIVIDUAL SIGN OFFS BELOW.;[08] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: SKIN — DEBONDED (ZONE 600 SLAT) · airframe 38,574 hrs · 18,242 cycles

CUSTOMER REQUEST - DEBONDED EXTERNAL SKIN SLAT 8 TRAILING EDGE LOWER SURFACE OB SIDE AT RT WING 2024-645395<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189521; DUE DATE: 26/JAN/25.;[02] TOOL USED; HOT BONDER PN: HCS9200B; SN: 15102320; DUE DATE: 25-JAN-25.;[03] TOOL USED; POSITECTOR PN: NS2; SN: 110098; DUE DATE: 05-SEP-25.;[04] REPAIRED EXTERNAL SKIN SLAT 8 TRAILING EDGE LOWER SURFACE OB SIDE AT RT WING IAW B737-800 SRM 51-70-10-2R-4 REPAIR 4. SEE INDIVIDUAL SIGNOFF BELOW;[05] REPAIRED EXTERNAL SKIN SLAT 8 TRAILING EDGE LOWER SURFACE OB SIDE AT RT WING IAW B737-800 SRM 51-70-10-2R-4 REPAIR 4. SEE INDIVIDUAL SIGNOFF BELOW. COMPLETED TASK

Part: FLAP — DEBONDED (ZN 600 RIGHT WIN) · airframe 38,574 hrs · 18,242 cycles

CUSTOMER REQUEST - DEBONDED EXTERNAL SKIN IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT RT WING 2024-645392<[01] TOOL USED; CALIPER PN: 500-196-30; SN: A19317217; DUE DATE: 16-MAY-25.;[02] TOOL USED CALIPER PN: 500-196-30; SN: A19317217; DUE DATE: 16-MAY-25.;[03] HOT BONDER P/N HCS9200B-AV S/N 18175478 DUE DATE 25/JAN/25.;[04] EQUIPMENT P/N BONDMASTER 600M; S/N 220052310; DUE DATE 17-NOV-24 WAS USED ON STEP 12;[05] TOOL USED SCALE P/N: SPX621; S/N: 8340225453; DUE DATE: 01-SEP-25.;[06] REPAIRED IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT RT WING IAW B737-800 SRM 57-53-01-2R-7 REPAIR 7. SEE INDIVIDUAL SIGNOFF BELOW.;[07] REPAIRED IB MAIN FLAP TRAILING EDGE WEDGE LOWER SURFACE AT RT WING IAW B737-800 SRM 57-53-01-2R-7 REPAIR 7. SEE INDIVIDUAL SIGNOFF BELOW.

Part: LIGHT — DELAMINATED (ZN 200 FUS TOP) · airframe 38,576 hrs · 18,243 cycles

DELAMINATED PHOTOLUMINESCENT STRIP ALONG PAX CABIN (10EA) 2024-645380<[01] REPLACED PHOTOLUMINESCENT STRIP ALONG PAX CABIN (10E) IAW B737-800 AMM 33-51-15-400-802 STEP 1.A.THRU E. EXCEPT E.(1) AND DWG 417A5775 REV-;[02] REPLACED PHOTOLUMINESCENT STRIP ALONG PAX CABIN (10E) IAW B737-800 AMM 33-51-15-400-802 STEP 1.A.THRU E. EXCEPT E.(1) AND DWG 417A5775 REV-

Part: LENS — UNSECURE (ZONE 200) · airframe 38,543 hrs · 18,227 cycles

AFT SERVICE DOOR EMER EXIT LIGHT LENS WILL NOT STAY ATTACHED TO LIGHT ASSY<[01] REATTACHED LENS PER EA M-21-133-00720

Part: HANDLE — BROKEN (DOOR ASSIST) · airframe 37,557 hrs · 17,685 cycles

DOOR ASSIST HANDLE ON FWD ENTRY DOOR BROKEN<[01] REMOVED ASSIST HANDLE FROM FORWARD LAV AND INSTALLED ON L1 DOOR PER AMM 52-11-31. FORWARD LAV ASSIST HANDLE PLACED ON MEL OK TO CONTINUE PER MEL 25-10-01 SP#1B AUTH 199464;[02] ADDED MEASUREMENTS;[03] INSTALL FWD LAV ASSIST HANDLE REF SIP. THIS CLEARS MEL 25-10-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,706 hrs · 17,247 cycles

ILLUMINATED STRIP ON THE FLOOR CAPTAIN SIDE REAR FWD CABIN DOOR NOT ILLUMINATING<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-15-960-801-NG (FLOOR PROXIMITY LIGHT - PHOTOLUMINESCENT STRIP REPLACEMENT - PERMANENT)] ABOUT 8'5'

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,672 hrs · 17,227 cycles

EMERGENCY LIGHT ABOVE ROW 8ABC IS INOP.<[01] FOUND CONNECTOR FOR LIGHT UNPLUGGED; RE-PLUGGED IN CONNECTOR AND LIGHTS OP CHECK GOOD PER S.I.P.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,644 hrs · 17,216 cycles

EMERGENCY EXIT LIGHTS INOP AT AFT RIGHT HAND SIDE<[01] REMOVED AND REPLACED AFT RIGHT HAND SIDE EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 36,282 hrs · 17,011 cycles

RH OUTBOARD TE FLAP ASSY DELAMINATING INBOARD TRAILING EDGE.<[01] REMOVED AND REPLACED RH OUTBOARD TE FLAP ASSY REF AMM 27-51-22. OPS AND RIG CHECK GOOD.;[02] REMOVED AND REPLACED RT OUTBOARD T/E; PERFORMED AFT FLAP ADJUSTMENT.<BR>REF: AMM 27-51-22. OPPS CHECK GOOD.

Part: ENGINE — SHUTDOWN (ZN 400 NACELLE/P) · airframe 35,543 hrs · 16,597 cycles

AT FL 190 NOTICED QUANTITY DROPPING ( INDICATOR IN REVERSE ) WE MONITORED CLOSELY BUT ALL OTHER INDICATIONS NORMAL. IN DESCENT ; OIL QUANTITY WENT TO ZERO; THEN OIL PRESSURE FLUCTUATED THEN DROPPED CAUSING AMBER THEN RED BOX TO FLASH WE DID A PRECAUTIONARY SHUT DOWN PER THE QRH. NO EGT OR OIL TEMP EXCEEDANCE. ALSO DID NOT NOTICE LOW OIL PRESSURE LIGHT OR MASTER CAUTION LIGHT. (#2 ENGINE)<[01] R&R #2 ENGINE; SEE TTG8Q008TSZX FOR CORRECTIVE ACTION.

Part: TRANSMITTER — FAULTY (ZN 200 FUS TOP) · airframe 33,916 hrs · 15,697 cycles

DURING APPROACH FLAP HANDLE SELECTE FLAPS 30* AS FLAP POSITION INDICATOR MOVED THROUGH 25 ASSYMETRY WAS NOTED. FLAP POSSIN STOPPED AT 25/27. LE FLAP TRANSIT LIGHT ILLUMINATED & STAYED ON EVEN AFTER FLAP HANDLE SELECTED FLAPS 25 PER QRH PROCEDURE<[01] FOUND TE FLAP SENSOR R FAULT. R&R RH T/E FLAP POSITION TRANSMITTER ADJUSTED LH T/E FLAP TRANSMITTER; OPS CHECK GOOD REF AMM 27-51-00;[02] INSPECTED FLAPS NO DEFECTS NOTED. REF AMM 27-51-00;[03] FOUND TE FLAP SENSOR R FAULT. R&R RH T/E FLAP POSITION TRANSMITTER ADJUSTED LH T/E FLAP TRANSMITTER; OPS CHECK GOOD REF AMM 27-58-01

Part: COWLING — DELAMINATED (ZN 400 NACELLE/P) · airframe 33,843 hrs · 15,657 cycles

#2 ENGINE RIVETS AROUND ENGINE COWLING (INLET COWL FROM 10OCLOCK TO 3 OCLOCK) POPPED AND MISSING; ALSO DELAMINATION<[01] R/R #2 INLET COWL IAW AMM 71-11-01 EV#E021593

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,013 hrs · 15,198 cycles

R/H FWD EMERGENCY LIGHT INOPERATIVE. ] REPLACED THE LAMP IAW AMM 33-51-04.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 32,801 hrs · 15,069 cycles

ROW 7DEF FO SIDE WALL LIGHT INOP. ROW 7DEF FO SIDE WALL LIGHT INOP.MULTIPLE WRITE UPS.<[01] R&RED 6DEF AND 7DEF SIDEWALL LT ASSY PER AMM 33-21-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,317 hrs · 14,782 cycles

MAIN CABIN SEVERAL EMERGENCY LIGHTS AND SERVERAL EXIT SIGN INOPS. / [01] REMOVED AND REPLACED BATTERY PACKS OPS CHECK GOOD; PER AMM 33-51-06.

Part: SUPPORT — CRACKED (ZN 600 RIGHT WIN) · airframe 32,317 hrs · 14,782 cycles

R/H WING PANEL SUPPORT CRACKED INBOARD OF DEFLECTION RIB. / [01] LOCATED AND DRILLED NEW SUPPORT ANGLE PER SRM 51-40-02;[02] INSP THE LOCATED AND DRILLED NEW SUPPORT ANGLE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,250 hrs · 14,751 cycles

LEFT OVER WING AFT EMERGENCY LIGHT INOP. / [01] RELAMPED IAW B737 AMM 33-51-04 OPS GOOD.

Part: NONE — OUT OF POSITION (PAX CABIN) · airframe 32,132 hrs · 14,698 cycles

EMERGENCY LIGHT LENS ABOVE ROW FOUR FELL OFF . REPORTED BY CREW / [01] REPLACED LENS COVER REF AMM 33-51-01

Part: BEAM — CRACKED (FUSELAGE) · airframe 32,116 hrs · 14,687 cycles

LH CENTER FLOOR SUPPORT BEAM CRACKED AT STATION 540 ABOVE AIR CONDITIONING DISTRIBUTION BAY / [01] REMOVED AND REPLACED LH CENTER FLOOR SUPPORT BEAM AT STATION 540 ABOVE AIR CONDITIONING DISTRIBUTION BAY IAW SRM 51-40-02

Part: BEAM — CRACKED (FUSELAGE) · airframe 32,116 hrs · 14,687 cycles

RH CENTER FLOOR SUPPORT BEAM CRACKED AT STATION 540 ABOVE AIR CONDITIONING DISTRIBUTION BAY / [01] REMOVED AND REPLACED RH CENTER FLOOR SUPPORT BEAM AT STATION 540 ABOVE AIR CONDITIONING DISTRIBUTION BAY IAW SRM 51-40-02

Part: NONE — DELAMINATED (R/H WING) · airframe 32,121 hrs · 14,691 cycles

RH O/B AFT FLAP IS DELAMINATED ON BOTTOM I/B CORNER / [01] REMOVED AND REPLACED R/H O/B AFT FLAP PER AMM 27-51-22.

Part: NONE — INOPERATIVE (AFT ENTRY DOOR) · airframe 32,019 hrs · 14,638 cycles

AFT ENTRY DOOR EXTERIOR EMERGRNCY LIGHT INOP. / [01] R & R AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT PER AMM 33-51-00.

Part: PUMP — FAULTY (#1 ENGINE) · airframe 31,956 hrs · 14,601 cycles

LOSS OF A SYSTEM ENGINE DRIVEN PUMP. LOW PRESSURE LIGHT ON. QTY DROPPED TO 19 / [01] REF LP 0277698E; 0277700E #1 ENG EMP REMOVED AND REPLACED IAW AMM 29-11-11 OPS CK GOOD; LEAK CK GOOD. REF LP 0277700E FOR EV# 014571

Part: FIRE LOOP — BROKEN (#2 ENGINE) · airframe 31,266 hrs · 14,203 cycles

#2 ENG OVHT LIGHT DURING CLIMB OUT ENG 2 OVERHEAT LIGHT ILLUMINATED. WITHIN 10 SEC FAULT LIGHT ALSO ILLUMINATED. ENG 2 OVERHEAT LIGHT AND FAULT LT CONTINUED TO FLASH ON AND OFF. AT TIMES THE ENG 2 OVHT LT WAS ILLUMINATED WITHOUT FAULT LT NO ABNORMAL ENG INDICATIONS NOTED. FIRE OVHT TEST SUCCESSFUL / [01] FOUND #2 ENGINE FIRE LOOP B BROKEN REMOVED AND REPLACED #2 ENGINE FIRE LOOP B PER AMM 26-11-01

Part: LIGHT — INOPERATIVE (L/H OVERWING) · airframe 31,063 hrs · 14,110 cycles

LFT FWD OVERWING EXIT; EXIT SIGN LIGHTS INOP / [01] RELAMPED OVERWING EXIT SIGN LIGHTS AT THE LFT FWD OVERWING EXIT PER AMM 33-51-01

Part: PANEL — CRACKED (AFT CARGO BAY) · airframe 29,961 hrs · 13,564 cycles

AFT CARGO PANEL #141FW HAS 2 EA CRACKS ON BOTTOM OF PANEL WITHIN 2 INCHES OF EDGE ; / [01] ACCOMPLISHED EA 1-A25-4142 MXI #M-21-125-00669 ACCOMPLISH PERMANENT REPAIR BY REPLACING DAMAGED PANEL OR REPAIR -25EA-03644

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,818 hrs · 28,284 cycles

EXTERIOR AFT ONLY DOOR EMERGENCY EXIT LIGHT INOP (SLIDE LIGHT) / RELAMPED PER AMM 33-51-04

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 27,696 hrs · 12,547 cycles

RH WHEEL WELL VAPOR BARRIER IS CRACKED AT RBL 31.83; JUST FWD OF B SYSTEM RETURN FILTERS. CRACK MEASURES APROX 6'.REPETITIVE ACTION REQUIRED: DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLES OR MORE FREQUENTLY. MAKE SURE THE CRACK HAS NOT GROWN PAST THE INTERIM SEAL; PER SRM 57-10-10-1A-2. /

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 27,663 hrs · 12,531 cycles

TRANSFERRED FROM LOG PAGE 0251623E: ON TAKE OFF AT 200 300' ENCOUNTERED BIRD STRIKE ON LOWER NOSE FUSELAGE. NO ABNORMAL ENGINE OR HYDRAULIC INDICATIONS OR ABNORMAL SMELLS.(ORIG INAL DEFECT FROM LP# 0281622E TRANSFERRED BACK TO AIRCRAFT LOGBOOK FROM NRC D460725 DUE TO ONE TIME FERRY FLIGHT FOR REPAIRS TO PAE) REPAIRED BULKHEAD BS 172 BETWEEN RBL8 LBL8 PER EA 2115301267 REV IR & ATS ER 2101833 REV IR

Part: SEAL — DISLODGED (COCKPIT WINDOW) · airframe 26,749 hrs · 12,031 cycles

AN UNIDENTIFIED LOUD CRACKLING SOUND STARTED IN THE COCKPIT AT 8000 FEET. UNSUCCESSFUL TO FIND THE SOUND WE SLOWED THE AIRCRAFT TO A SAFE SPEED OF 230 KTS AND BELOW. THE SOUND CONTINUED UP TO LANDING. DURING TAXI IN HNL THE WINDOW SEAL OF R1 DISLODGED FROM THE WINDOW FRAME AND WAS VISIBLE IN THE COCKPIT. THE SEAL WAS THE SOURCE OF THE SOUND. FOUND R1 WINDOW PREMOLDED SEAL DISLODGED. REPAIRED SEALANT, IAW AMM 56-11-00, REF LOG PAGE 0201493E FOR SEALANT CURE.

Part: FLOOR PANEL — DENTED (FWD CARGO) · airframe 26,402 hrs · 11,862 cycles

FWD CARGO GWD FLOOR PANEL HAS NUMEROUS DENTS 120CF / FORWARD CARGO PANEL 120CF OUT OF LIMITS; REPLACED WITH NEW PANEL I/A/W SRM 53-00-53-1A-1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,402 hrs · 11,862 cycles

EMERGENCY LIGHTS AT AISLE ROW 17, ROW 21 AND RT AFT OVERWING EXIT SIDEWALL SIGN INOPERABLE. REMOVED AND REPLACED BATTERY PACK AT STA 727 RT, PER MM 33-51-06. EMERGENCY LIGHTS OPERATIONS CHECKED GOOD, PER MM 33-51-00 POS 727R P/N OFF/ON D717-01-100 S/N OFF 217573 SN ON WN0012.

Part: STRINGER CLIP — CRACKED (BS 500I) · airframe 26,402 hrs · 11,862 cycles

STRINGER CLIP AT STA 500I, STR 26L CRACKED. REMOVED AND REPLACED CLIP, PER SRM 51-40-02 REFERENCE N/R CARD NR D442036 & SAM 326 NR A1200861 INSP D95.

Part: GUSSET — CRACKED (BS 500I S19R) · airframe 26,402 hrs · 11,862 cycles

FWD CARGO GUESSET CRACKED BS 500I STR19R / FWD CARGO REMOVED AND REPLACED GUSSET AT STA-500 I/ STR-19R PER SRM 51-40-02SA-M 326 A1200850

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 26,402 hrs · 11,862 cycles

FWD CARGO STA 500I; LOWER BULKHEAD SUPPORT ANGLE CORRODED. / REPLACED BULKHEAD SUPPORT ANGLE PER SRM 53-40-02SA-M 326 A1184532

Part: PLATE — CORRODED (FUSELAGE) · airframe 26,402 hrs · 11,862 cycles

FWD CARGO L/H SIDEPLATE; CORROSION AT FASTENER HOLES BETWEEN STATIONS 500H- 500I. / REPAIRED PER SRM 53-00-53-2R-5 ; SEE INDIVIDUAL SIGNOFFS FOR ALL WORK ACCOMPLISHED SEE SAM326: A1184521

Part: FLOORBEAM — CORRODED (BS 947) · airframe 26,402 hrs · 11,862 cycles

AFT CABIN R/H LAV; AFT OUTBOARD HARD POINT FITTING HAS AREA OF SURFACE CORROSION PRESENT. (MARKED) / REPAIRED FLOOR BEAM AT STA 947.5 PER SRM 53-70-51-2R-5 AND EA 20-153-02001.SEE SA-M 326: A1184514

Part: MOUNT — CORRODED (AFT LAVATOR) · airframe 26,402 hrs · 11,862 cycles

AFT CABIN L/H LAV; AFT INBOARD HARD POINT FITTING HAS VARIOUS AREA OF SURFACE CORROSION PRESENT (MARKED) / INSTALLED REPAIR PER EA 20-153-02001 AND SRM 53-70-51-2R-5. SEE INDIVIDUAL SIGNOFFS FOR ALL WORK ACCOMPLISHED. SEE SAM 326: A1184515

Part: BRACKET — CORRODED (L2 DOOR GIRT BAR) · airframe 26,402 hrs · 11,862 cycles

FWD GALLEY LT AFT GIRT BAR MOUNT BRACKET STA 345 LBL 58 HAS CORROSION AT FASTNER HOLE. R & R LT AFT GIRT BAR MOUNT BRACKET PAT NR 141A5220-4, IAW SRM 51-40-02.

Part: PLATE — CORRODED (BS 492-500A) · airframe 26,402 hrs · 11,862 cycles

FWD CARGO R/H SIDEPLATE RBL 20 CORROSION AT FASTNER HOLES STA. 492.4-500A. / REMOVED AND REPLACED SIDEPLATE PER SRM 51-40-02.SA-M 326 A1200846

Part: PLATE — CORRODED (BS 500-500A) · airframe 26,402 hrs · 11,862 cycles

FWD CARGO L/H SIDEPLATE CORRODED LBL 20 AT FASTNER HOLES STA 500-500A / REPAIRED L/H TRANSITION ANGLE FROM STA. 480 + 10 TO STA. 500A PER SRM. 53-00-53-2R-5SA-M 326 S/N A1184516

Part: PLATE — CORRODED (FUSELAGE) · airframe 26,402 hrs · 11,862 cycles

FWD CARGO L/H SIDE PLATE LBL 20 CORRODED AT FASTNER HOLES STA. 500I -520 / DAMAGED LOCATION INCORRECTLY IDENTIFIED. DAMAGE TO BE ADDRESSED ON N/R D442002.

Part: PLATE — CORRODED (FUSELAGE) · airframe 26,402 hrs · 11,862 cycles

FWD CARGO R/H SIDEPLATE RBL 20 CORRODED AT FASTNERS HOLES STA. 500C-500D / REMOVED CORROSION ON SIDEPLATE IN FWD CARGO BBL20 STA 500C-500D (REMOVED .010' OF .040') FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED DAMAGED SIDEPLATE RBL 20 STA 500B+9 TO STA 500D+9 IAW SRM 53-00-53-2R-5. SEE SA-M FORM A1200847 FOR INDIVIDUAL SIGN OFFS OF WORK PERFORMED.SA-M 326 A1200847

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 26,402 hrs · 11,862 cycles

FWD CARGO STA. 520 SUPPORT ANGLE RBL 20-LBL 20 CORRODED. / INCORRECT FRAME STATION. DAMAGE IS AT STATION 500I AND WILL BE ADDRESSED ON N/R D442012.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,060 hrs · 11,603 cycles

EMERGENCY LIGHT AT R1 INSIDE AND OUTSIDE INOP / REPLACED BATTERY PACK FOR M2816 POWER SUPPLY PER AMM 33-51-06.

Part: CIRCUIT BREAKER — OPEN (CABIN) · airframe 25,841 hrs · 11,477 cycles

BOTH RIGHT FORWARD AND AFT OVERWING EMERGENCY EXIT LIGHTS ILLUMINATED ON TAKE OFF POWER UP. FOUND RT OVERWING EXIT LIGHT C/B OPEN AT P6-2 D1 COMPLIED WITH FIM TASK 52-20-00810-801 ALL FAULTS CLEARED ON PSEUFAULT CODES 52-72008; 52-72009.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 25,841 hrs · 11,477 cycles

RT WHEEL WELL VAPOR BARRIER IS CRACKED AT RBL 31.83; JUST FWD OF B SYSTEM RETURN FILTERS. CRACK MEASURES APROX 6'. REPETITIVE ACTION REQUIRED: DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLES OR MORE FREQUENTLY. MAKE SURE THE CRACK HAS NOT GROWN PAST THE INTERIM SEAL PER SRM 57-10-10-1A-2.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 25,784 hrs · 11,438 cycles

RH WHEEL WELL VAPOR BARRIER IS CRACKED AT RBL 31.83; JUST FWD OF B SYSTEM RETURN FILTERS. CRACK MEASURES APROX 6'.REPETITIVE ACTION REQUIRED: DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLES OR MORE FREQUENTLY. MAKE SURE THE CRACK HAS NOT GROWN PAST THE INTERIM SEAL; PER SRM 57-10-10-1A-2. /

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,758 hrs · 11,426 cycles

EMERGENCY LIGHTS ON CAPTAIN'S SIDE UPPER FIRST 2 INOP TROUBLE SHOT TO BATTERY PACK AT FS 500C +7 (ROW 8). R&R EMERGENCY LIGHTS BATTERY AT FS 500C +7 WL 213 LBL 67 PER AMM 32-51-06 OPS CHECK GOOD.

Part: WEB — CORRODED (FWD CARGO) · airframe 25,224 hrs · 11,133 cycles

EVIDENCE OF CORROSION FOUND BETWEEN FWD CARGO COMPARTMENT MIDDILE SCUFF PLATES. / REMOVED AND REPLACED WEB PER SRM 51-10-02 AMT 102665 (SA-M 326 ATTACHED. SN A1146945)

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 25,215 hrs · 11,130 cycles

FWD CARGO COMPARTMENT FWD SIDE SCUFF PLATE IS CRACKED. / R&R FWD SIDE SCUFF PLATE IN FWD CARGO BIN FWD LOWER CORNER OF DOOR OPENING PER AMM 53-11-02

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 25,215 hrs · 11,130 cycles

FWD CARGO COMPARTMENT AFT SIDE SCUFF PLATE IS CRACKED / R&R AFT SIDE SCUFF PLATE IN FWD CARGO DOOR OPENING LOWER AFT CORNER PER AMM 53-11-02

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 23,725 hrs · 10,414 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1675. / R&R BATTERY PER AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 23,725 hrs · 10,414 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1673. / R&R BATTERY PER AMM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 23,182 hrs · 10,171 cycles

PHOTOLUMINESCENT STRIP LOOSE ROW 12. RESECURED REF AMM.

Part: COVER PLATE — MISSING (EXIT SIGN) · airframe 22,670 hrs · 9,916 cycles

OVERWING EXIT SIGN MISSING A COVER PLATE ON AFT SIDE. R&R COVER PLATE PER AMM.

Part: TRANSMITTER — FAULTY (E&E BAY) · airframe 22,061 hrs · 9,645 cycles

DECLARED EMERGENCY, FLAPS LOCKED OUT AT 9 UNITS WITH 15 FLAPS SELECTED. R&R LT FLAP POSITION TRANSMITTER PER AMM.

Part: SENSOR — FAULTY (TE FLAP) · airframe 22,061 hrs · 9,645 cycles

DECLARED EMERGENCY, FLAPS LOCKED OUT AT 9 UNITS WITH 15 FLAPS SELECTED. R&R LT NR 1 SKEW SENSOR PER AMM.

Part: COVER — BROKEN (CABIN) · airframe 21,976 hrs · 9,602 cycles

LT FORWARD OVERWING EMERGENCY EXIT SEAT BELT LIGHT COVER BROKEN. R&R COVER PER MM.

Part: HMU — FAULTY (NR 2 ENGINE) · airframe 21,141 hrs · 9,228 cycles

ABORTED TAKEOFF, RIGHT ENGINE DID NOT ACHIEVE TAKE OFF THRUST SETTING OF 89.7% N1. R&R NR 2 ENGINE HYDRO MECHANICAL UNIT PER MT.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 21,141 hrs · 9,228 cycles

ABORTED TAKEOFF, RIGHT ENGINE DID NOT ACHIEVE TAKE OFF THRUST SETTING OF 89.7% N1. R&R NR 2 ENGINE FUEL PUMP PER MT.

Part: RETAINER — CRACKED (RT WING) · airframe 21,034 hrs · 9,186 cycles

RH WING #6 AFT FLAP TRACK FAIRING; O/B FWD SEAL RETAINER CRACKED / REPLACED RH WING #G AFT FLAP TRACK FAIRING OUTBD FWD CRACKED SEAL RETAINER WITH A NEW SEAL RETAINER IAW B737-700 SRM 51-40-02-0G-0 STEP #9 ATAG# ZE0037

Part: ANGLE — CRACKED (FUSELAGE) · airframe 20,389 hrs · 8,894 cycles

FORWARD CARGO COMPARTMENT CLIP ANGLE CRACKED AT BS 500H, LBL 25. R&R CLIP ANGLE IAW SRM AND DWG.

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 21,034 hrs · 9,186 cycles

FWD CARGO COMAPARTMENT; AT LBL 25; BS 500H; AFT SIDE OF FRAME; UNDER Z ANGLE; CLIP IS CRACKED / FWD CARGO LBL 25 STA 500H AFT SIDE CLIP ANGLE CRACKED. DRILLED AND REMOVED CRACKED CLIP ANAGLE. I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW CLIP ANGLE I/A/W SRM 51-40-05-0G-0 ALSO BOEING DWG 143A 7505 REV:-. INSTALLED NEW CLIP ANGLE I/A/W SRM 51-40-02-0G-0 ALSO BOEING DWG 143A7505 REV-

Part: SHIELD — CORRODED (FUSELAGE) · airframe 20,389 hrs · 8,894 cycles

AFT CARGO COMPARTMENT FLOOR SHIELD ANGLE CORRODED BETWEEN BS 767 TO BS 794.50. R&R SHIELD IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (FWD CARGO BAY) · airframe 21,034 hrs · 9,186 cycles

FWD CARGO BAFFLE ATTACH ANGLE CRACKED AT BS 500H STR 25LH. / FWD CARGO LBL 25 STA 500H FWD SIDE CLIP ANGLE CRACKED. DRILLED AND REMOVED CRACKED ANGLE I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NW CLIP ANGLE I/A/W SRM 51-40-05-0G-0 ALSO BOEING DWG 143A7505 REV -. INSTALLED NEW CLIP ANGLE I/A/W SRM 51-40-02-0G-0 ALSO BOEING DWG 143A7505 REV -. ISSUE TAG:A28816.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 20,389 hrs · 8,894 cycles

FORWARD CARGO STRINGER CLIP CRACKED AT BS 500I, STR 26R. R&R STRINGER CLIP IAW SRM AND DWG.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 21,034 hrs · 9,186 cycles

AFT CARGO COMPARTMENT AT STA 767 RBL 22.50 SMALL STRAP THAT CONNECTS THE FRAME TO THE FWD FLOOR SHIELD IS CORRODED 2 EA AREAS AS MARKED / REMOVED CORROSION. ORIGINAL MATERIAL .063' MATERIAL LOSS .026' MATERIAL REMAINING .034' FOUND TO BE OUT OF LIMITS I/A/W SRM 53-60-15-1A-1. REMOVED STRAP; FABRICATED NEW STRAP AND INSTALLED NEW STRAP I/A/W B737 SRM 51-40-02-0G-0 AND BOEING DRAWING 146A8125 REV:-

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 21,034 hrs · 9,186 cycles

FWD CARGO BS 500I S19RH SUPPORT GUSSET CRACKED. / REMOVED/REPLACED SUPPORT GUSSET AT FWD CARGO BS 500I S-19R IAW SRM 51-40-02-0G-0/ DWG#143A7902 REV A / DWG# 143A9481 REV A. APPLIED C.I.C IAW AMM 51-21-91-620-802. TAG# A35250

Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 21,034 hrs · 9,186 cycles

FWD CARGO COMPT. STA 500I LBL 24 TO RBL 24 LOWER BULKHEAD ANGLE HAS CORROSION ON UPPER SURFACE / REMOVED AND REPLACED BULKHEAD ANGLE IN FWD CARGO PIT STA 500I RBL24 TO LBL24 IAW BOEING 737 DWG 143A7902 AND SRM 51-40-02

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,389 hrs · 8,894 cycles

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

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 21,034 hrs · 9,186 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140EF HAS CORROSION AROUND EDGES OF PANEL / REPLACED DAMAGED AFT CARGO FLOOR PANEL #140EF IAW SWA IPC 25-52-10-19. PANEL IS TO BE INSTALLED ON DEFECT# X833391. PANEL PART# 453A2610-58; ATAG WN9441.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 20,389 hrs · 8,894 cycles

FORWARD CARGO BAFFLE ATTACH ANGLE CRACKED AT BS 500H, STR 25L. R&R ANGLE IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FWD CARGO BAY) · airframe 21,034 hrs · 9,186 cycles

FWD CARGO BAFFLE ATTACH ANGLE CRACKED AT BS 500H STR 25RH. / REMOVED AND REPLACED CRACKED FWD CARGO BAFFLE ATTACH ANGLE AT STA 500H STR 25R WITH P/N 163A75024 IAW DWG 143A7505 REV- AND SRM 51-40-02 ATAG#A53146

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 21,034 hrs · 9,186 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140CF HAS CORROSION AROUND EDGES. / REPLACED DAMAGED AFT CARGO FLOOR PANEL #140CF IAW BOEING DWG# 453A2610 REV C. PANEL TO BE INSTALLED ON SA-M 565S W/O # 35926 PANEL PART # 453A2610-18 ATAG WN9409

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 21,034 hrs · 9,186 cycles

AFT CARGO COMPARTMENT BETWEEN STA 767 AND 794.50 FWD FLOOR SHIELD IS CORRODED TOP AND BOTTOM SIDES SEVERAL AREAS AS MARKED / REMOVED CORROSION PER SRM 51-10-02-0G-0; ORIGINAL MATERIAL THICKNESS .050' LOSS OF .024' WITH .026' REMAINING BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED AFT CARGO DOOR FWD SHIELD PER SRM 51-40-02-0G-0 AND DWG 146A0081 REV A

Part: SUPPORT FRAME — CRACKED (AFT CARGO BAY) · airframe 21,034 hrs · 9,186 cycles

AFT CARGO COMPARTMENT STA 864 LBL 10 LOWER BRACKET FOR WASTE WATER REMOVABLE BULKHEAD FRAME SUPPORT IS CRACKED / REMOVED AND INSTALLED A NEW BRACKET AT AFT CARGO COMPARTMENT STA 864 LBL 10 IAW B737 SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (FWD CARGO BAY) · airframe 21,034 hrs · 9,186 cycles

FWD CARGO AT BS 500I S26RH; STRINGER CLIP UNDER Z ANGLE HAS CRACKS AT UPPER ATTACH RIVET . / REMOVED AND REPLACED FWD CARGO STRINGER CLIP AT BS500I526RRH UNDER Z ANGLE WITH NEW PART P/N 143A1016-48 IAW SRM 51-40-02 AND BOEING DWG 143A1234 REV A ATAG#A33336

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 20,389 hrs · 8,894 cycles

FORWARD CARGO BAFFLE ATTACH ANGLE CRACKED AT BS 500H, STR 25R. R&R ANGLE IAW DWG AND SRM.

Part: ATTACH ANGLE — CORRODED (AFT CARGO BAY) · airframe 21,034 hrs · 9,186 cycles

AFT CARGO COMPARTMENT BETWEEN STA 767 AND 794.50 UNDER FWD FLOOR SHIELD ANGLE THAT CONNECTS THE FLOOR SHIELD TO THE WEB INTERCOASTAL IS CORRODED AROUND THE NUT PLATES BOTTOM SIDE / REMOVED CORROSION IAW B737 SRM 51-10-02-0G-0; ORIGINAL MATERIAL .050'; LOSS .013'; MATERIAL REMAINING .037' FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-60-15-1A-1. REMOVED AND INSTALLED A NEW SHIELD IAW B737 SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND BOEING DRAWING # 146A8125 REV A

Part: ANGLE — CORRODED (AFT CARGO) · airframe 21,034 hrs · 9,186 cycles

AFT CARGO COMPARTMENT BETWEEN STA 727D AND 767 R/H Z ANGLE IS CORRODED BOTH TOP AND BOTTOM SIDES IN SEVERAL AREAS / REMOVED CORROSION. ORIGINAL MATERIAL .040'; MATERIAL LOSS .011' MATERIAL REMAINING .029 FOUND TO BE OUT OF LIMITS I/A/W SRM 53-00-53-1R-2. CUT OUT DAMAGE FABRICATED. TRATED AND PRIME REPAIR PARTS. INSTALLED REPAIR PARTS I/A/W B737 SMR 53-00-53-2R-5.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 21,034 hrs · 9,186 cycles

AFT CARGO COMPARTMENT BETWEEN STA 727D AND 807 L/H Z ANGLE IS CORRODED BOTH TOP AND BOTTOM SIDES IN SEVERAL AREAS / BLENDED CORROSION FROM AFT CARGO L/H ZEE ANGLE STA 727D TO STA 807. ONE AREA OUT OF LIMITS. ORIGINAL .040'; .033' REMAINING; LOSS .007' IAW SRM 53-00-53-1A-2. CUT TO REMOVE ZEE SIDEPLATE STA 727 H+10' TO STA 787+14.5'. REPAIRED L/H ZEE IAW SRM 53-00-53-2R-5 REPAIR 5. TREAT AND PRIMED AREAS WITHIN LIMITS IAW SRM 53-00-53-1A-2 STEP 2 E (1) AND (2). APPLIED CIC TO REPAIR AREA TREATED AREAS AND L/H ZEE SIDEPLATE IAW SRM 53-00-53-2R-5 REPAIR 5 STEP 4N.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 21,034 hrs · 9,186 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140BF HAS CORROSION AROUND EDGES. / REPLACED DAMAGE AFT CARGO FLOOR PANEL #140BF IAW BOEING DWG# 453A2610 REV E. PANEL TO BE INSTALLED ON SA-M 565S # 359526 PANE PART # 453A2610-32. ATAG WN9989

Part: ANGLE — CORRODED (FUSELAGE) · airframe 20,389 hrs · 8,894 cycles

AFT CARGO COMPARTMENT LT Z ANGLE CORRODED BETWEEN BS 727D TO BS 807. REPAIRED ZEE ANGLE IAW SRM.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 21,034 hrs · 9,186 cycles

FORWARD CARGO PIT FLOOR PANEL 120DF HAS CORROSION ALONG THE EDGES / REPLACED DAMAGED FWD CARGO FLOOR PANEL #120DF IAW SWA IPC 25-52-10-17. PANEL TO BE INSTALLED ON SA-M 5655 W/O # 359526. PANEL PART# 453A1610-20 ATAG WN9990.

Part: LENS — CRACKED (CABIN) · airframe 20,389 hrs · 8,894 cycles

RT MAIN CABIN STOWBIN EMERGENCY LIGHT LENS CRACKED AT ROW 25. R&R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 20,389 hrs · 8,894 cycles

LT OVERHEAD EMERGENCY LIGHT LENS CRACKED BETWEEN ROW 8 TO ROW 26. R&R LENS IAW AMM.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 21,034 hrs · 9,186 cycles

FORWARD CARGO PIT FLOOR PANEL 120CF HAS CRACKED FASTENER HOLE WITH PIECE OF COUNTERSINK MISSING 15' FROM FORWARD EDGE AND 4' FROM LEFT EDGE / REPLACED DAMAGED FWD CARGO FLOOR PANEL @120CF IAW SWA IOC 25-52-10-17. PANEL TO BE INSTALLED ON SA-M 565S W/O # 359526 PANEL PART# 453A1610-103 ATAG WN9988

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 20,943 hrs · 9,141 cycles

L1 DOOR SLIDE OUT OF POSITION. R&R SLIDE PER MT.

Part: LENS — LOOSE (R1 DOOR) · airframe 20,830 hrs · 9,082 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS COVER LOOSE. R&R LIGHT ASSEMBLY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 20,027 hrs · 8,733 cycles

LT AFT EMERGENCY EXIT LIGHT LOOSE. R&R LIGHT ASSEMBLY PER MM.

Part: COVER — DETACHED (EXIT SIGN) · airframe 19,433 hrs · 8,466 cycles

LT AFT LAVATORY EXIT SIGN DETACHED. R&R COVER PER SIP.

Part: NONE — CRACKED (AFT SERVICE DOOR) · airframe 18,052 hrs · 7,817 cycles

AFT SERVICE DOOR LOWER ATTACH PAN CRACKED AND NOT SECURE / R & R PAN ASSY AS PER AMM 52-41-31INSP# H52

Part: NONE — DELAMINATED (RT WING) · airframe 18,017 hrs · 7,800 cycles

RIGHT WING OTBD AFT FLAP LOWER T/E SURFACE DELAMINATED 84' X 10' (FROM INBD CORNER TO 7' OTBD) / REMOVED & REPLACED T/E PER AMM 27-51-22 ISSUE # 1903353POS RT P/N OFF 113A3700-26 S/N OFF 004304 P/N ON 113A3700-22 S/N ON 001590

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 18,020 hrs · 7,801 cycles

R1 DOOR ESCAPE SLIDE LOW PRESSURE. R&R SLIDE PER MT.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 16,384 hrs · 7,093 cycles

RT WING OUTBOARD AFT FLAP LOWER TRAILING EDGE SURFACE DELAMINATED. R&R AFT FLAP PER AMM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 16,896 hrs · 7,316 cycles

ROW 21 CEILING EMERGENCY EGRESS LIGHT LENS COVER MISSING. INSTALLED COVER IAW SIP.

Part: COVER — MISSING (CABIN) · airframe 16,291 hrs · 7,053 cycles

CENTER AISLE OVERWING EXIT SIGN ACCESS PANEL MISSING COVER. INSTALLED COVER PER SIP.

Part: LENS — MISSING (CABIN) · airframe 16,291 hrs · 7,053 cycles

BULLNOSE AISLE EMERGENCY LIGHT LENS MISSING. INSTALLED LENS PER SIP.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 16,188 hrs · 7,009 cycles

AFT GALLEY EXIT SIGN LENS BROKEN. R & R SIGN IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 14,843 hrs · 6,417 cycles

FWD ENTRY OVERHEAD EXIT LIGHT ASSY LOOSE. INSTALLED LIGHT ASSY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 12,755 hrs · 5,482 cycles

EXIT LIGHT LENS MISSING AT ROW 29 DEF. INSTALLED LENS IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 11,314 hrs · 4,861 cycles

RIGHT EMER AISLE LIGHT LOOSE AT ROW 14. R & R LIGHT IAW MM.

Part: PUMP — FAULTY (NR 1 ENGINE) · airframe 10,886 hrs · 4,672 cycles

INFLIGHT SHUTDOWN & DECLARED EMERGENCY. NR 1 ENG FAIL MESSAGE ON EGT INDICATION ON DESCENT. R & R FUEL PUMP IAW MT.

Part: LENS — MISSING (CABIN) · airframe 10,623 hrs · 4,563 cycles

LEFT EMER LIGHT, LENS COVER MISSING AT ROW 23. INSTALLED COVER IAW MM.

Part: LENS — MISSING (CABIN) · airframe 9,492 hrs · 4,090 cycles

RIGHT BULLNOSE EMER LIGHT LENS MISSING AT ROW 15. INSTALLED LENS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 93,820 hrs · 4,042 cycles

RIGHT BULLNOSE EMER LIGHT LENS MISSING AT ROW 15. INSTALLED LENS IAW MM.

Part: RETAINING CLIP — LOOSE (EMERGENCY EXIT) · airframe 6,254 hrs · 2,652 cycles

RIGHT AFT EMER EXIT DOOR HANDLE COVER PLATE RETAINING CLIP LOOSE. R & R CLIP IAW AMM.

Part: SIGN — UNSECURE (CABIN) · airframe 5,848 hrs · 2,481 cycles

L1 DOOR EMER EXIT SIGN FELL OFF. REINSTALLED SIGN IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,641 hrs · 2,402 cycles

R2 DOOR EMER EXIT LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 2,542 hrs · 1,042 cycles

FWD GALLEY LOWER RT SIDE EMERGENCY EXIT SIGN BROKEN. R&R SIGN IAW MM.