N8316H

Part: HANDLE — UNSECURE (ZONE 800) · airframe 43,526 hrs · 20,711 cycles

R1 DOOR, AIRFRAME ASSIST HANDLES UNSECURE. SECURED R1 DOOR AIRFRAME ASSIST HANDLES IAW AMM TASK 52-11-31-400-802.

Part: HANDLE — OUT OF ADJUST (ZONE 800) · airframe 43,526 hrs · 20,711 cycles

L1 DOOR, AIRFRAME ASSIST HANDLES UNSECURE. SECURED L1 DOOR AIRFRAME SIDE ASSIST HANDLES IAW AMM TASK 52-11-31-400-802.

Part: HANDLE — OUT OF ADJUST (ZONE 800) · airframe 43,526 hrs · 20,711 cycles

R1 DOOR ASSIST HANDLE UNSECURE. SECURED R1 DOOR ASSIST HANDLE IAW AMM TASK 52-11-31-400-802.

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 42,844 hrs · 20,346 cycles

FWD MEGAPHONE INOPERATIVE. REMOVED AND REPLACED FWD MEGAPHONE IAW AMM 25-64-00. OPS CHECK GOOD.

Part: SKIN — DELAMINATED (ZONE 500 FLAP) · airframe 39,661 hrs · 18,646 cycles

LEFT WING OB TE FLAP HAS DELAM ON TE APPR 16 FROM IB END<[01] REPLACED LEFT WING OUTBOARD AFT FLAP REF <BR>01 - REMOVED AND REPLACED PER [AMM 27-51-22-400-801-NG (OUTBOARD AFT FLAP INSTALLATION - PERMANENT)]

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 39,467 hrs · 18,545 cycles

MULTIPLE EMERGENCY LIGHTS INOP ON AFT LEFT SIDE OF THE AIRCRAFT<[01] REMOVED AND REPLACED AFT LEFT EMERGENCY LIGHT BATTERY PACK (AT SEAT 21A) PER AMM 33-51-06. ALL LIGHTS OPS CK GOOD.

Part: LAMP — INOPERATIVE (EMERENCY LIGHTS) · airframe 39,266 hrs · 18,446 cycles

AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP.<[01] RELAMPED AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.

Part: GIRT BAR — OUT OF ADJUST (FWD SERVICE DOOR) · airframe 38,915 hrs · 18,260 cycles

FWD SERVICE DOOR SLIDE; GIRT IS NOT PROPERLY PACKED<[01] REPACKED GIRT ON FWD SERVICE DOOR SLIDE PER MT <BR>725-61-06.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 38,682 hrs · 18,136 cycles

EMER EXIT LIGHT COVER(FLOOR) F/O SIDE MISSING<[01] INSTALLED NEW EMERGENCY EXIT COVER PER AMM 33-51-03; OPS CHECK GOOD

Part: SKIN — CRACKED (NR 1 FAN COWL) · airframe 37,868 hrs · 17,710 cycles

CRACK ON OUTBOARD FAN COWL LOCATED ON UPPER FWD EDGE ENGINE 1. CRACK EDGE DISTANCE FIRSTS FASTENER ARE EDGE FWD: 2 INCHES AND UPPER EDGE: 1.500 INCHES 2024-48994<[01] REFER TO FAULT TTG8Q00R0BZQ WHERE EA 24-171-00344 WAS ADDED AS A SUBTASK;[02] TASK CARD COMPLETED <BR>REFER TO FAULT TTG8Q00R0BZQ WHERE EA 24-171-00344 WAS ADDED AS A SUBTASK

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 37,868 hrs · 17,710 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS297 AT RT WING 2024-48965<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS297 AT RT I.A.W B737-800 SRM 51-40-02 AND DWG: 115A3700 SHEET: 61 REV: -;[02] CORRECTED STEP 1<BR>REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS297 AT RT I.A.W B737-800 SRM 51-40-02 SRM 51-10-02 Ï¿½TEM 9 AND DWG: 115A3700 SHEET: 61 REV: -;[03] TASK COMPLETED

Part: PLATE — CRACKED (RT WING) · airframe 37,868 hrs · 17,710 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS217 AT RT WING 2024-48966<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS217 AT RT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9. LENGT OF CRACK IS: 0.921?. TOOL USED CALIPER P/N:500-197-30; S/N: A21147758 AND DUE DATE: 21-NOV-24;[02] TASK CARD COMPLETED

Part: ANGLE — CORRODED (ZN 600 RIGHT WIN) · airframe 37,868 hrs · 17,710 cycles

CORROSION ANGLE TRAILING EDGE LOCATED ORSS464 UPPER SIDE AT RT WING 2024-48952<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS464 UPPER SIDE AT RT WING IAW B737-700 SRM 51-40-02 AND DRAWING # 115A3551 REV: -.;[02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS464 UPPER SIDE AT RT WING IAW B737-700 SRM 51-40-02 AND DRAWING # 115A3551 REV

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,868 hrs · 17,710 cycles

CRACK ANGLE LOCATED BS500I AT LEVEL STR28L AT FWD CARGO COMPARTMENT 2024-48927<[01] REPLACED ANGLE AND FASTENERS LOC. BS500I AT LEVEL STR28L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 160; REV-B. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE AND FASTENERS LOC. BS500I AT LEVEL STR28L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 160; REV-B. SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,868 hrs · 17,710 cycles

CRACK ANGLE LOCATED BS500I AT LEVEL STR28R AT FWD CARGO COMPARTMENT 2024-48928<[01] REPLACED ANGLE AND FASTENERS LOC. BS500I AT LEVEL STR28R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 160; REV-B. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE AND FASTENERS LOC. BS500I AT LEVEL STR28R AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 160; REV-B. SEE INDIVIDUAL SIGN OFF BELOW.

Part: WINGLET — CORRODED (ZN 500 LEFT WING) · airframe 37,868 hrs · 17,710 cycles

CORROSION ON WINLET TIP LOCATED LT WING 2024-48910<[01] PERFORMED PERMANENT REPAIR ON WINLET TIP LOCATED LT WING IAW B737-NG SRM AP37.1-0632. 57-30-01 REPAIR 6; SEE INDIVIDUAL SIGN-OFF BELOW;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 37,868 hrs · 17,710 cycles

CRACK ON SUPPORT BRACKET ASSY LOCATED BTW BS540 AND BS559 LH SIDE AT AIR CONDITIONING BAY 2024-48878<[01] REPLACED SUPPORT BRACKET ASSY LOCATED BTW BS5040 TO BS559 LH SIDE AT AIR CONDITIONING BAY I.A.W. B737-800 SRM 51-40-02 AND DWG 212A1101 SHEET 7 REV. -<BR><BR>CRACK LENGTH: 1? <BR><BR>TOOL USED CALIPER P/N: 500-197-30 S/N: A21147761 DUE DATE: 12/MAR/24;[02] REPLACED SUPPORT BRACKET ASSY LOCATED BTW BS5040 TO BS559 LH SIDE AT AIR CONDITIONING BAY I.A.W. B737-800 SRM 51-40-02 AND DWG 212A1101 SHEET 7 REV. -<BR>CRACK LENGTH: 1? <BR>TOOL USED CALIPER P/N: 500-197-30 S/N: A21147761 DUE DATE: 12/MAR/24

Part: FRAME — CRACKED (BS 312 S5-6L) · airframe 37,868 hrs · 17,710 cycles

CRACK FRAME LOCATED STA 312 AND BETWEEN STR 5L TO STR 6L AT PASSENGER CABIN 2024-48868<[01] PERFORMED PERMANENT ON FRAME IAW M-22-153-01244 SEE INDIVIDUAL SIGN OFF BELOW;[02] PERFORMED PERMANENT ON FRAME IAW M-22-153-01244 SEE INDIVIDUAL SIGN OFF BELOW

Part: TIE CLIP — CRACKED (BS 277 S10R) · airframe 37,868 hrs · 17,710 cycles

CRACK TIE CLIP LOCATED STA 277 AND STR 10R AT PASSENGER CABIN 2024-48870<[01] REPLACED TIE CLIP AND FASTENERS LOCATED STA 277 AND STR 10R AT PASSENGER CABIN; IAW B737-800 SRM 51-40-02 AND DWG: 141A1110; SHEET: 39; REV: -; SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED TIE CLIP AND FASTENERS LOCATED STA 277 AND STR 10R AT PASSENGER CABIN; IAW B737-800 SRM 51-40-02 AND DWG: 141A1110; SHEET: 39; REV: -; SEE INDIVIDUAL SIGN-OFF BELOW.<BR>RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 37,868 hrs · 17,710 cycles

CRACK ANGLE LOCATED BS867 LBL11 AND WL165 AT AFT CARGO COMPARTMENT 2024-48882<[01] REPLACED ANGLE LOCATED BS867 LBL11 AND WL165 AT AFT CARGO COMPARTMENT I.A.W B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; DWG: 149A8102 SHEET: 19 REV: A; TOOK MEASUREMENT CRACK IS L:1.216?;[02] COMPLETED

Part: LIGHT — BROKEN (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

BROKEN GALLEY 4B EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA ( 2024-48818<[01] REPLACED GALLEY 4B EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA I.A.W B737-800 AMM 33-51-01-960-802. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: LIGHT — BROKEN (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

BROKEN GALLEY 1 EMERGENCY EXIT ASSY LIGHT AND LENS AT FWD GALLEY AREA 2024-48843<[01] REPLACED GALLEY 1 EMERGENCY EXIT ASSY LIGHT AND LENS AT FWD GALLEY AREA IAW B737-800 AMM 33-51-01-960-802 SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED GALLEY 1 EMERGENCY EXIT ASSY LIGHT AND LENS AT FWD GALLEY AREA IAW B737-800 AMM 33-51-01-960-802 SEE INDIVIDUAL SIGNOFFS BELOW

Part: SUPPORT ANGLE — BROKEN (RT WING) · airframe 37,868 hrs · 17,710 cycles

BROKEN OUTBOARD TRAILING EDGE SUPPORT ANGLE LOCATED ORSS 277 AT DEFLECTION CONTROL RIB AREA AT RT WING 2024-48816<[01] REPLACED SUPPORT ANGLE LOCATED ORSS 277 AT DEFLECTION CONTROL RIB AREA AT RT WING I.A.W B737-800 SRM 51?40-02 AND DWG: 115A6200 SHEET: 17 REV: A;[02] CERTIFIED STEP 1 COMPLETED

Part: BRACKET — CRACKED (BS 867 S3-4R) · airframe 37,868 hrs · 17,710 cycles

CRACK BRACKET LOCATED BS 867 BETWEEN S-3R TO S-4R AT PASSENGER CABIN EXACTLY LOCATION:CRACK BRACKET LOCATED BS 867 BETWEEN S- 2R TO S-3R AT PASSENGER CABIN 2024-48782<[01] REPLACED BRACKET LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN IAW B737-800 SRM: 51-10-02 ITEM 9 AND SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE IAW B737-800 SRM 53-00-07-1A-1;[02] TASK COMPLETED

Part: INTERCOSTAL — CORRODED (ZN 200) · airframe 37,868 hrs · 17,710 cycles

CORROSION INTERCOSTAL LOCATED BS 947.5 TO BS 967 AND LBL 22 WL 208.1 AT AFT GALLEY AREA 2024-48763<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 24-JUL-24;[02] TOOL USED: ULTRASONIC THICKNESS GAGE. P/N: 45MG. S/N: 232017609. DUE DATE: 22-SEP-24.;[03] REPLACED INTERCOSTAL LOCATED ON BTW BS947.5 TO BS967 AND LBL22 WL208.1 AT AFT GALLEY AREA I.A.W. B737-800 SRM 51-40-02 AND DWG 147A5650 SHEET 55 REV. A <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[04] REPLACED INTERCOSTAL LOCATED ON BTW BS947.5 TO BS967 AND LBL22 WL208.1 AT AFT GALLEY AREA I.A.W. B737-800 SRM 51-40-02 AND DWG 147A5650 SHEET 55 REV. A <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: INTERCOSTAL — CORRODED (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

CORROSION INTERCOSTAL LOCATED BS 947.5 TO BS 967 AND LBL 25 WL 208.1 AT AFT GALLEY AREA 2024-48762<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 24-JUL-24;[02] EQUIPMENT P/N 45MG; S/N 232019809; DUE DATE 22-SEP-24 WAS USED;[03] REPLACED INTERCOSTAL LOCATED BS 947.5 TO BS 967 AND LBL 25 WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM 51-40-02 AND DWG 147A5660 REV:A. SEE INDIVIDUAL SIGN OFF BELOW.;[04] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: STIFFENER — CRACKED (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED STA540 BL0 TO RBL24.75 AT PASSENGER CABIN 2024-48707<[01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED STA540 BL0 TO RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM: 51-10-02 Ï¿½TEM 9 AND 51-40-02. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] COMPLETE TASK CERTIFIED

Part: STIFFENER — CRACKED (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL0 TO LBL 24.75 AT PASSENGER CABIN 2024-48705<[01] REPLACED NEW STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A0060 SHEET 64 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED NEW STIFFENER FLOOR STRUCTURE LOCATED BS 540 BETWEEN BL0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A0060 SHEET 64 REV -. SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOOR PANEL — DELAMINATED (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

DELAMINATED FLOOR PANEL 232JF AT PASSENGER CABIN 2024-48720<[01] TOOL USED CALIPER PN: 500-197-30; SN: A18135081; DUE DATE: 21/JUL/24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 15102320; DUE DATE: 22-JAN-24;[03] TOOL USED: SCALE P/N: SPX621 S/N: 8340225489 DUE DATE: 15/AUG/24.;[04] TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18175478 DUE DATE: 25-JAN-25.;[05] TOOL USED: SCALE PN: CR5200 SN: 8343110765 DUE DATE: 20-FEB-24;[06] TOOL USED: HOT BONDER PN:HCS9000B-AV SN: 18185761 DUE DATE: 24-JAN-25;[07] REPAIRED FLOOR PANEL 232JF AT PASSENGER CABIN IAW B737-800 SRM 53-00-50-2R-1 REPAIR 1.SEE INDIVIDUAL SIGN OFF BELOW.;[08] JOB COMPLETED RII.

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

CRACK ANGLE LOCATED STA294.5 RBL54 WL208.1 AT FWD GALLEY AREA 2024-48703<[01] REPLACED ANGLE LOCATED ON BS294.5 RBL54 WL208.1 AT FWD GALLEY AREA I.A.W. B737-800 SRM 51-40-02 AND DWG 141A8310 SHEET 33 REV. - AND DWG 140A9810 SHEET 35 REV. A<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] CERTIFIED AS RII <BR>REPLACED ANGLE LOCATED ON BS294.5 RBL54 WL208.1 AT FWD GALLEY AREA I.A.W. B737-800 SRM 51-40-02 AND DWG 141A8310 SHEET 33 REV. - AND DWG 140A9810 SHEET 35 REV. A<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400 LBL13 WL208.1 AT PASSENGER CABIN 2024-48704<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA380 TO STA400 LBL13 WL208.1 AT PASSENGER CABIN I.A.W B737-800 SRM 51-40-02 AND DWG: 143A5400 SHEET: 140 REV: - SEE INDIVIDUAL SIGN OFF BELOW;[02] COMPLETE TASK CERTIFIED

Part: FLOOR SUPPORT — CRACKED (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA312 TO STA328 RBL31 WL 208.1 AT FWD GALLEY AREA 2023-48696<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA312 TO STA328 RBL31 WL 208.1 AT FWD GALLEY AREA IAW B737-800 SRM 51-10-02; SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV - . SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: FLOOR PANEL — DELAMINATED (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

DELAMINATED FLOOR PANEL 232RF AT PASSENGER CABIN 2024-48688<[01] TOOL USED CALIPER: 500-197-30; SN: A18135081; DUE DATE: 21/JUL/24.;[02] TOOL USED: HOT BONDER PN: HCS9000B-AV SN: 18185761 DUE DATE: 24-JAN-25.;[03] TOOL USED: SCALE P/N: CR5200 S/N: 8343110765 DUE DATE: 20-FEB-24.;[04] TOOL USED: SCALE PN: CR5200 SN:8343110765 DUE DATE: 20-FEB-24; HOT BONDER PN:HCS9200B-AV SN:15102320 DUE DATE:25-JAN-25.;[05] REPAIRED FLOOR PANEL 232RF AT PASSENGER CABIN IAW B737-800 SRM 53-00-50-2R-6 REPAIR 6. SEE INDIVIDUAL SIGNOFFS BELOW;[06] JOB COMPLETED RII.

Part: FLOOR PANEL — DELAMINATED (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

DELAMINATED FLOOR PANEL 232SF AT PASSENGER CABIN 2024-48689<[01] TOOL USED CALIPER: 500-197-30; SN: A18135081; DUE DATE: 21/JUL/24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 15102320; DUE DATE: 22-JAN-24.;[03] TOOL USED: SCALE PN: SPX621 SN: 8340225489 DUE DATE: 15-AUG-24;[04] TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18175478 DUE DATE: 25-JAN-25.;[05] REPAIRED FLOOR PANEL 232SF AT PASSENGER CABIN IAW B737-800 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW;[06] REPAIRED FLOOR PANEL 232SF AT PASSENGER CABIN IAW B737-800 SRM 53-00-50-2R-1 REPAIR 1 RII COMPLETED.

Part: FLOOR SUPPORT — CRACKED (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA277 TO STA294.5 BL0 WL208.1 AT FWD GALLEY AREA 2024-48697<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA277 TO STA294.5 BL0 WL208.1 AT FWD GALLEY AREA IAW B737-800 SRM 51-10-02 ; SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV - . SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED STEP 1 COMPLETED

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 37,868 hrs · 17,710 cycles

CRACK AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUTOUT 2024-48672<[01] TOOL USED DIGITAL CALIPER P/N: 500-197-30; S/N: A23272233; DUE DATE: 31-DEC-24.;[02] TOOL USED P/N XRP 3000; S/N 1753759; DUE DATE 12-APR-24;[03] REPAIRED BY WELDING AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUTOUT I.A.W. BOEING 737-800 SRM 53-60-15-2R-1; REPAIR 1 AND BAC5975 SEE INDIVIDUAL SIGNOFFS BELOW SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPAIRED BY WELDING AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUTOUT I.A.W. BOEING 737-800 SRM 53-60-15-2R-1; REPAIR 1 AND BAC5975 SEE INDIVIDUAL SIGNOFFS BELOW;[05] REPAIRED BY WELDING AFT CORNER SCUFF PLATE AT AFT CARGO DOOR CUTOUT I.A.W. BOEING 737-800 SRM 53-60-15-2R-1; REPAIR 1

Part: LENS — BROKEN (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

BROKEN SIDEWALL PANEL EMERGENCY EXIT LENS LH SIDE AT PASSENGER CABIN 2024-48561<[01] REPLACED SIDEWALL PANEL EMERGENCY EXIT LENS LH SIDE AT PASSENGER CABIN I.A.W B737-800 AMM 33-51-01-960-802 STEP 3 C (10).;[02] REPLACED SIDEWALL PANEL EMERGENCY EXIT LENS LH SIDE AT PASSENGER CABIN I.A.W B737-800 AMM 33-51-01-960-802 STEP 3 C (10).

Part: FLOOR PANEL — DELAMINATED (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

DELAMINATED FLOOR PANEL 232KF AT PASSENGER CABIN 2024-48680<[01] TOOL USED CALIPER PN: 500-197-30; SN: A18135081; DUE DATE: 21/JUL/24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 15102320; DUE DATE: 22-JAN-24.;[03] TOOL USED: SCALE PN:CR5200 SN: 8343110765 DUE DATE: 20-FEB-24;[04] CURED REPAIR PLIES AND DRILLED INSERT HOLES ON REPAIR AREAS IAW B737-800 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3.M(1)(A);N AND B737-800 SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 5.R;S(1)(A)(B).TOOL USED HOT BONDER PN:HCS9000B ; SN:18175469 DUE DATE 24/JAN/25;[05] CORRECTED ITEM 4 OF CORRECTIVE ACTIONS IS: TOOL USED HOT BONDER PN:HCS9000B ; SN:18175469 DUE DATE 24/JAN/25;[06] TOOL USED: SCALE PN: CR5200 SN:8343110765 DUE DATE: 20-FEB-24; HOT BONDER PN:HCS9200B-AV SN:15102320 DUE DATE:25-JAN-25;[07] REPAIRED FLOOR PANEL 232KF AT PASSENGER CABIN IAW B737-800 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] JOB COMPLETED RII.

Part: FLOOR PANEL — DELAMINATED (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

DELAMINATED FLOOR PANEL 242GF AT PASSENGER CABIN 2024-48681<[01] TOOL USED CALIPER: 500-197-30; SN: A18135081; DUE DATE: 21/JUL/24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 15102320; DUE DATE: 22-JAN-24.;[03] TOOL USED: SCALE PN: SPX621 SN: 8340225489 15-AUG-24.;[04] TOOL USED: HOT BONDER PN: HCS9000B-AV SN:18185761 DUE DATE: 24-JAN-25.;[05] TOOL USED: SCALE PN: CR5200 SN:8343110765 DUE DATE: 20-FEB-24.;[06] TOOL USED: HOT BONDER PN:HCS9000B-AV SN: 18185761 DUE DATE: 24-JAN-25;[07] REPAIRED FLOOR PANEL 242GF AT PASSENGER CABIN IAW B737-800 SRM 53-00-50-2R-1 REPAIR 1.SEE INDIVIDUAL SIGN OFF BELOW.;[08] JOB COMPLETED RII.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 37,868 hrs · 17,710 cycles

CRACK FWD CORNER SCUFFF PLATE AT FWD CARGO DOOR CUT OUT 2024-48669<[01] TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N: A21144622; DUE DATE: 29-MAR-24.;[02] TOOL USED ON STEP 4; RADIOMETER/PHOTOMETER KIT PN: XRP-3000; SN: 1753759; DUE DATE: 12-APR-2024.;[03] REPAIRED FWD CORNER SCUFFF PLATE AT FWD CARGO DOOR CUT OUT IN ACCORDANCE WITH BOEING 737-800; SRM 53-30-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] JOB TASK COMPLETED.

Part: LIGHT — SCRATCHED (CABIN FLOOR) · airframe 37,868 hrs · 17,710 cycles

SCRATCH ON STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE AT PASSENGER CABIN (9 EA) 2024-48644<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE AT PASSENGER CABIN (9 EA) I.A.W B737-800 AMM 33-51-15-400-802 STEP 1A ITEM (1)(B);[02] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH SIDE AT PASSENGER CABIN (9 EA) I.A.W B737-800 AMM 33-51-15-400-802 STEP 1A ITEM (1)(B)

Part: LIGHT — BROKEN (CABIN FLOOR) · airframe 37,868 hrs · 17,710 cycles

BROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE AT PASSENGER CABIN (9 EA) 2024-48645<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE AT PASSENGER CABIN (9 EA) I.A.W B737-800 AMM 33-51-15-400-802 STEP 1A ITEM (1)(B);[02] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH SIDE AT PASSENGER CABIN (9 EA) I.A.W B737-800 AMM 33-51-15-400-802 STEP 1A ITEM (1)(B)

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 37,868 hrs · 17,710 cycles

BROKEN LENS EMERGENCY LIGHT LAVATORY D 2024-48480<[01] REPLACED LENS EMERGENCY LIGHT LAVATORY D IAW B737-700 AMM 33-51-01-960-802 STEP 3(C) ITEM (10);[02] CORRECTED STEP 1 <BR><BR>REPLACED LENS EMERGENCY LIGHT LAVATORY D IAW B737-800 AMM 33-51-01-960-802 STEP 3(C) ITEM (10);[03] REPLACED LENS EMERGENCY LIGHT LAVATORY D IAW B737-800 AMM 33-51-01-960-802 STEP 3(C) ITEM (10)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,868 hrs · 17,710 cycles

INOP BATTERY PACK 2024 48434 INOP CEILING PANEL BATTERY PACK (M1673) AT AFT GALLEY AREA (1 EA)<[01] REPLACED POWER SUPPLY BATTERY PACK (M1673) AT AFT GALLEY AREA IAW B737-800 AMM 33-51-06-960-805 TEST OK;[02] REPLACED POWER SUPPLY BATTERY PACK (M1673) AT AFT GALLEY AREA IAW B737-800 AMM 33-51-06-960-805 TEST OK

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,868 hrs · 17,710 cycles

INOP BATTERY PACK 2024 48435 INOP CEILING PANEL BATTERY PACK (M1672) AT AFT GALLEY AREA (1EA)<[01] REPLACED POWER SUPPLY BATTERY PACK (M1672) AT AFT GALLEY AREA IAW B737-800 AMM 33-51-06-960-805 TEST OK;[02] REPLACED POWER SUPPLY BATTERY PACK (M1672) AT AFT GALLEY AREA IAW B737-800 AMM 33-51-06-960-805 TEST OK

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 37,868 hrs · 17,710 cycles

INOP BATTERY PACK 2024 48433 INOP BATTERY PACK EMERGENCY EXIT LIGHT LOWER POSITION ROW 13CBA(M1694) CENTER SECTION (1EA)<[01] REPLACED POWER SUPPLY BATTERY PACK EMERGENCY EXIT LIGHT LOWER POSITION ROW13 ABC (M1694) CENTER SECTION IAW B737-800 AMM 33-51-06-960-805 TEST OK;[02] REPLACED POWER SUPPLY BATTERY PACK EMERGENCY EXIT LIGHT LOWER POSITION ROW13 ABC (M1694) CENTER SECTION IAW B737-800 AMM 33-51-06-960-805 TEST OK

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,868 hrs · 17,710 cycles

INOP BATTERY PACK 2024 48432 INOP BATTERY PACK EMERGENCY EXIT LIGHT LOWER POSITION ROW 13 FED (M1695) CENTER SECTION (1EA)<[01] REPLACED POWER SUPPLY BATTERY PACK EMERGENCY EXIT LIGHT LOWER POSITION ROW13 FED (M1695) CENTER SECTION IAW B737-800 AMM 33-51-06-960-805 TEST OK;[02] REPLACED POWER SUPPLY BATTERY PACK EMERGENCY EXIT LIGHT LOWER POSITION ROW13 FED (M1695) CENTER SECTION IAW B737-800 AMM 33-51-06-960-805 TEST OK

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 35,923 hrs · 16,631 cycles

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

Part: BATTERY PACK — INOPERATIVE (ZN 800 DOOR) · airframe 34,228 hrs · 15,695 cycles

BOTH RH OVER WING EXIT DOOR EXIT SIGNS DO NOT ILLUMINATE. / [01] R&R PACK CHARGER ASSY (MID RH) AND BATTERY PACK. OPS CHK GOOD. REF AMM 33-51-06.

Part: CHARGER — INOPERATIVE (ZN 800 DOOR) · airframe 34,228 hrs · 15,695 cycles

BOTH RH OVER WING EXIT DOOR EXIT SIGNS DO NOT ILLUMINATE. / [01] R&R PACK CHARGER ASSY (MID RH) AND BATTERY PACK. OPS CHK GOOD. REF AMM 33-51-06.

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 33,390 hrs · 15,217 cycles

R/H FWD UPPER HORIZONTAL STABILIZER TO BODY SLIDING SEAL (UPPER FWD SLIDER)IS CRACKED. / [01] REMOVED AND REPLACED R/H FWD UPPER HORIZONTAL STABILIZER TO BODY SLIDING SEAL IAW AMM 51-40-02

Part: COFFEEMAKER — ODOR (FWD GALLEY) · airframe 32,500 hrs · 14,738 cycles

FLIGHT ATTENDANT REPORTED ELECTRICAL BURNING ODOR COMING FROM FWD GALLEY COFFEE POT. PULLED THE CB.NO INDICATION OF SMOKE ODOR EVENTUALLY WENT AWAY. / [01] VERIFIED ODOR WAS COMING FROM FWD CM. COMPLIED WITH CONDITIONAL INSPECTION PER AMM 05-51-56. R&R FWD COFFEE MAKER PER AMM 25-30-01. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE · airframe 31,712 hrs · 14,339 cycles

EMERGENCY LIGHTS FOR FWD OVER WING L/H FWD OF DOOR INOP. EMERGENCY LIGHTS FOR FWD OVER WING EXIT L/H FWD OF DOOR INOP. / [01] R/R M1694 EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06; OPS CHECK GOOD;[02] PARTS DATA UPDATE ONLY;[03] R/R M1694 EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06; OPS CHECK GOOD<BR>PN:D717-01-100SWA<BR>SN: WN0560;[04] INSPECTED THE INSTALLATION OF THE EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06. NO FAULT NOTED.

Part: SIGN — INOPERATIVE · airframe 31,712 hrs · 14,339 cycles

SIDEWALL PANEL 231ZKW AND 232ZKW BOTH EMERGENCY LIGHT SIGN INOP. / [01] REMOVED AND REPLACED BATTERY PACK M1694 IAW AMM 33-51-06 OPS CHECK GOOD;[02] REMOVED AND REPLACED BATTERY PACK M1694 IAW AMM 33-51-06 OPS CHECK GOOD PN#D717-01-100SWA SERIAL# WN0560;[03] INSPECTED THE REMOVAL; REPLACEMENT AND OPS CHECK OF THE EMERGENCY BATTERY PACK PER 33-51-06.NO FAULT NOTED.

Part: PLATE — CRACKED (L/H WING) · airframe 31,712 hrs · 14,339 cycles

LEFT WING REAR SPAR LOWER WIGGLE PLATE CRACKED NEAR ORSS 297; BELOW #5 SPOILER. / [01] REMOVE AND REPLACED LOWER WIGGLE PLATE PER SRM 51-40-02.;[02] REMOVE AND REPLACED LOWER WIGGLE PLATE PER SRM 51-40-02. C/W

Part: ANGLE — CRACKED (L/H WING) · airframe 31,712 hrs · 14,339 cycles

LH WING TRAILING EDGE ANGLE JUST INBOARD OF DEFLECTION CONTROL RIB IS CRACKED. PART # 115A2156U7 / [01] REMOVED AND REPLACED TRAILING EDGE ANGLE PER SRM 51-40-02.

Part: ANGLE — CRACKED (R/H WING) · airframe 31,712 hrs · 14,339 cycles

RH WING TRAILING EDGE ANGLE JUST INBOARD OF DEFLECTION CONTROL RIB IS CRACKED. (MPN IS 115A2156-8) / [01] REMOVED CRACKED TRAILING EDGE ANGLE AND ATTACHED SEAL RETAINER FOR REPLACEMENT.;[02] LOCATED AND DRILLED UP NEW TRAILING EDGE ANGLE MPN 115A2156-8 PER SRM 51-40-05.;[03] INSPECTED LOCATED AND DRILLED UP NEW TRAILING EDGE ANGLE MPN 115A2156-8 PER SRM 51-40-05;[04] INSTALLED NEW TRAILING EDGE ANGLE MPN 115A2156-8 SRM 51-40-02;[05] INSPECTED THE INSTALLATION OF NEW TRAILING EDGE ANGLE MPN 115A2156-8 SRM 51-40-02 WITH NO DEFECT.

Part: PANEL — LOOSE · airframe 31,712 hrs · 14,339 cycles

PANEL 192CR R/H A/C BAY DOOR HAS PLAY AT ALL 4 HINGES; MOST VISIBLE WITH DOOR IN CLOSED POSITION. MRKD ; PANEL 192CR RH AC AY DOOR HAS PLAY AT ALL 4 HINGES; MOST VISILE WITH DOOR IN CLOSED POSITION. MRKD /

Part: ACCESS DOOR — CORRODED (STABILIZER) · airframe 31,712 hrs · 14,339 cycles

STABILIZER TRIM ACCESS DOOR 311BL HAS FILIFORM CORROSION ON EXTERIOR SURFACE SKIN AT FWD SIDE OF HANDLE CUT-OUT. ; /

Part: SKIN — CORRODED (FUSELAGE) · airframe 31,712 hrs · 14,339 cycles

FUSELAGE SKIN HAS FILIFORM CORROSION ON EXTERIOR SURFACE AT STA. 909 STR 26R. MRKD (FWD OF WATER SERVICE PANEL 146AR) ; FSELAGE SKIN HAS FILIFORM CORROSION ON EXTERIOR SRFACE AT STA. 909 STR 26R. MRKD (FWD OF WATER SERVICE PANEL 146AR) /

Part: SKIN — CRACKED (NR1 FAN COWL) · airframe 31,712 hrs · 14,339 cycles

#1 O/B FAN COWL FWD UPPER CORNER SKIN IS CRACKED AT RIVET HOLE. MRKD / [01] R&R?D #1 ENG OUTBOARD FAN COWL IAW AMM 71-11-02

Part: PANEL — CORRODED · airframe 31,712 hrs · 14,339 cycles

WATER SERVICE PANEL 146AR HAS LIGHT FILIFORM CORROSION ON OUTER FWD SURFACE. MRKD ; WATER SERVICE PANEL 146AR HAS LIGHT FILIFORM CORROSION ON OTER FWD SRFACE. MRKD /

Part: PANEL — LOOSE · airframe 31,712 hrs · 14,339 cycles

PANEL 192CL L/H A/C BAY DOOR HAS PLAY AT ALL 4 HINGES; MOST VISIBLE WITH DOOR IN CLOSED POSITION. MRKD ; PANEL 192CL LH AC AY DOOR HAS PLAY AT ALL 4 HINGES; MOST VISILE WITH DOOR IN CLOSED POSITION. MRKD /

Part: PLATE — LOOSE (L/H WING) · airframe 31,712 hrs · 14,339 cycles

LH WING REAR SPAR LOWER CHORD WAFFLE PLATE LOOSE AND HOLES ELONGATED JUST IB OF #3 FLAP TRACK (MARKED) / [01] REPLACED PLATE PER SRM 51-10-02 & SRM 51-40-02.;[02] INSPECTION C/W TASK CARD

Part: SUPPORT — ELONGATED (L/H WING) · airframe 31,712 hrs · 14,339 cycles

LH WING DEFLECTION RIB UPPER SHELF PANEL SUPPORT WORN AND HOLES ELONGATED ; / [01] REMOVED DAMAGED AREA IN DEFLECTION RIB PER ARM 57-51-02-2R-4; [02] REMOVED DAMAGED AREA IN DEFLECTION RIB PER ARM 57-51-02-2R-4; [03] ACCOMPLISHED HFEC OF CUTOUT AREA PER 737NDT PART 6 51-00-00 PROCEDURE 23 AND 737NDT PART 6 51-00-00 PROCEDURE 16..NO DEFECTS NOTED; [04] L/H WING TRAILING EDGE FLAP DEFLECTION CONTROL RIB PANEL SUPPORT .CUT OUT DAMAGED AREA ON WING FIXED TRAILING EDGE SUPPORT BEAM PER SRM 57-51-02-2R-1; [05] INSPECTED CUT OUT ON CORRECTIVE ACTION #4 ABOVE.; [06] LOCATED AND DRILLED PART (1) DOUBLER AND INBOARD SERRATED PLATE. ALL WORK DONE IAW SRM 57-51-02-2R-1 & SRM 57-51-02-2R-4. OK TO INSTALL PART (1) DOUBLER AND INBOARD SERRATED PLATE.; [07] LOCATED; DRILLED OUTBOARD SERRATED PLATE AND FILLER FOR DEFLECTION RIB CUT OUT. OUTBOARD DOUBLER FABRICATED; DRILLED; HEAT TREATED AND CAB PLATED ON WO#MS53475. TREATED; PRIMED AND PAINTED ALL REPAIR PARTS. ALL WORK DONE IAW SRM 57-51-02-2R-4. OK TO INSTALL.; [08] INSPECTED LINE # 6 AND #7; [09] INSTALLED REPAIR PARTS PER SRM 57-51-02-2R-4 AND SRM 57-51-02-2R-1; [10] INSPECTED LINE #9

Part: PLATE — LOOSE (L/H WING) · airframe 31,712 hrs · 14,339 cycles

LH WING REAR SPAR LOWER CHORD WAFFLE PLATE LOOSE AND HOLES ELONGATED JUST IB OF #3 FLAP TRACK (MARKED) ; / [01] REPLACED PLATE PER SRM 51-10-02 & SRM 51-40-02.; [02] INSPECTION C/W TASK CARD

Part: DOUBLER — ELONGATED (L/H WING) · airframe 31,712 hrs · 14,339 cycles

LH WING DEFLECTION RIB UPPER SHELF PANEL SUPPORT WORN AND HOLES ELONGATED / [01] REMOVED DAMAGED AREA IN DEFLECTION RIB PER ARM 57-51-02-2R-4;[02] REMOVED DAMAGED AREA IN DEFLECTION RIB PER ARM 57-51-02-2R-4;[03] ACCOMPLISHED HFEC OF CUTOUT AREA PER 737NDT PART 6 51-00-00 PROCEDURE 23 AND 737NDT PART 6 51-00-00 PROCEDURE 16..NO DEFECTS NOTED;[04] L/H WING TRAILING EDGE FLAP DEFLECTION CONTROL RIB PANEL SUPPORT .CUT OUT DAMAGED AREA ON WING FIXED TRAILING EDGE SUPPORT BEAM PER SRM 57-51-02-2R-1;[05] INSPECTED CUT OUT ON CORRECTIVE ACTION #4 ABOVE.;[06] LOCATED AND DRILLED PART (1) DOUBLER AND INBOARD SERRATED PLATE. ALL WORK DONE IAW SRM 57-51-02-2R-1 & SRM 57-51-02-2R-4. OK TO INSTALL PART (1) DOUBLER AND INBOARD SERRATED PLATE.;[07] LOCATED; DRILLED OUTBOARD SERRATED PLATE AND FILLER FOR DEFLECTION RIB CUT OUT. OUTBOARD DOUBLER FABRICATED; DRILLED; HEAT TREATED AND CAB PLATED ON WO#MS53475. TREATED; PRIMED AND PAINTED ALL REPAIR PARTS. ALL WORK DONE IAW SRM 57-51-02-2R-4. OK TO INSTALL.;[08] INSPECTED LINE # 6 AND #7;[09] INSTALLED REPAIR PARTS PER SRM 57-51-02-2R-4 AND SRM 57-51-02-2R-1;[10] INSPECTED LINE #9;[11] PARTS DATA UPDATE ONLY;[12] UPPER PANEL WILL NOT PASS CLEARANCE CHECK AS IS.;[13] C/W EA 22-157-00513;[14] C/W;[15] C/W INSPECTION<BR>INSTALLED REPAIR PARTS PER SRM 57-51-02-2R-4 AND SRM 57-51-02-2R-1 <BR>C/W EA 22-157-00513

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 31,316 hrs · 14,184 cycles

ELECTRICAL GROUND POWER RECEPTACLE LOWER RUBBING STRIP SHEET METAL IS CRACKED. ; / [01] ACCOMPLISH EA 21-153-03708 ASSIGNED AS A SUBTASK.; [02] PERFORMED INTERIM REPAIR OF ELECTRICAL GROUND POWER RECEPTACLE LOWER RUBBING STRIP SKIN DOUBLER IAW EA 21-153-03708.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 31,248 hrs · 14,153 cycles

LEFT PASSENGER SIDE AND L/H EXTERIOR EMERGENCY LIGHTS INOP ; / [01] R&R EMERGENCY LIGHT BATTERY AT 13DEF IAW AMM 33-51-06<BR>R&R EMERGENCY LIGHT BATTERY AT 21DEF IAW AMM 33-51-06<BR>R&R EMERGENCY LIGHT BATTERY AT 727C+17 IAW AMM 33-51-06<BR>FWD GALLEY EMERGENCY VALANCE LIGHT STILL REMAINS INOP; [02] R&R?D PACK CHARGER ASSY PER AMM 33-51-06 AT STATION 737C+17 L/H SIDE OF AIRCRAFT; [03] R/R ENTRY LIGHT - DIM ENTRY LIGHT ASSEMBLY AND RELAY R34 AND OPERATIONAL<BR>CHECK OF ENTRY LIGHT- DIM LIGHT SATISFACTORY. PERFORMED OPERATIONAL CHECK OF<BR>THE EMERGENCY LIGHTS AND FOUND ALL SATISFCTORY PER A.M.M. 33-51-00

Part: CHARGER — INOPERATIVE (CABIN) · airframe 31,248 hrs · 14,153 cycles

LEFT PASSENGER SIDE AND L/H EXTERIOR EMERGENCY LIGHTS INOP ; / [01] R&R EMERGENCY LIGHT BATTERY AT 13DEF IAW AMM 33-51-06<BR>R&R EMERGENCY LIGHT BATTERY AT 21DEF IAW AMM 33-51-06<BR>R&R EMERGENCY LIGHT BATTERY AT 727C+17 IAW AMM 33-51-06<BR>FWD GALLEY EMERGENCY VALANCE LIGHT STILL REMAINS INOP; [02] R&R?D PACK CHARGER ASSY PER AMM 33-51-06 AT STATION 737C+17 L/H SIDE OF AIRCRAFT; [03] R/R ENTRY LIGHT - DIM ENTRY LIGHT ASSEMBLY AND RELAY R34 AND OPERATIONAL<BR>CHECK OF ENTRY LIGHT- DIM LIGHT SATISFACTORY. PERFORMED OPERATIONAL CHECK OF<BR>THE EMERGENCY LIGHTS AND FOUND ALL SATISFCTORY PER A.M.M. 33-51-00

Part: STRIP — LOOSE (CABIN)

PASSENGER CABIN PHOTOIUMINESCENT STRIP LOOSE AT SEAT ROW 12ABC / RESECURED PHOTOLUMINESCENT STRIP AT SEAT ROW 12ABC PER AMM 33-51-15.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 13,500 hrs · 29,785 cycles

SLIDE CAME LOOSE FROM FRWD ENTRY DOOR / R&R FWD ENTRY SLIDE PER MT# 725-61-06 POS: FWD ENTRY GRB#: 929658 PART# ON 5A3307-7 S/N # ON: BNG30563 PART # OFF: 5A3307-7 S/N OFF: BNG26798ISSUE# 3380896

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 27,725 hrs · 12,456 cycles

RIGHT HORIZONTAL STAB FWD UPPER SLIIDING SEAL CRACKED. / R&R RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31AMT 105556INSP 67932

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 27,725 hrs · 12,456 cycles

DELAY PURPOSE ONLY - LEFT OUTBD AFT FLAP DELAMINATED. / R/R LEFT OTBD FLAP.RTS - 1600C

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 27,725 hrs · 12,456 cycles

LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED / R&R LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31.AMT 105556INSP 67932

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 27,725 hrs · 12,456 cycles

L/H WING O/B AFT FLAP DELAMED AT I/B LOWER SKIN SURFACE 14' FROM I/B END & 10' FROM TRAILING EDGE / R&R L/H O/B AFT FLAP PER AMM 27-51-22. ISSUE# 3035246.P/N OFF 113A3700-25; S/N OFF 004131; P/N ON 113A3700-7; S/N ON 00619.

Part: WINDSHIELD — CRACKED (R1) · airframe 27,153 hrs · 12,098 cycles

HAIL DAMAGE TO A/C AND BROKEN R1 WINDSHIELD / HAIL DAMAGE TO A/C TRANSFERRED TO NRC D351300 AND BROKEN R1 WINDSHIELD TRANSFERRED TO NRC D351301

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,739 hrs · 11,858 cycles

CEILING EMERGENCY EXIT LIGHT OVER ROW 27 ABC INOP. / REMOVED AND REPLACED CEILING AISLE EMERGENCY EXIT LIGHT ASSEMBLY OVER SEAT ROW 27 ABC PER AMM 33-51-03. OPS CHECK NORMAL AT THIS TIME

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,045 hrs · 11,515 cycles

EMERGENCY LIGHT POWER BY M1676 / (FORWARD CABIN) WERE INOP. / R&R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,045 hrs · 11,515 cycles

EMERGENCY LIGHT POWER BY M2816 (FORWARD CABIN) WERE INOP. / R&R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,045 hrs · 11,515 cycles

EMERGENCY LIGHT POWER BY M1675 ( / FORWARD CABIN ) WERE INOP. / R&R POWER SUPPLY IAW AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 26,352 hrs · 11,691 cycles

DURING OK TO INSTALL FOUND FWD CARGO COMPARTMENT FWD CARGO SCUFF PLATE FOR LOWER DOOR CUTOUT IS CRACKED AS MARKED / RECIEVED WELDED FWD CARGO SCUFF PLATE FOR LOWER DOOR CUTOUT FWD SCUFF PLATE FROM BACK SHOP ON W/O 40450-1400-0004

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,352 hrs · 11,691 cycles

EMERGENCY LIGHT POWER BY M2816; M1675 AND M1676 ' '(FWD CABIN) ARE INOP. / REPLACED EMERGENCY LIGHT BATTERY PACK POWER SUPPLY M2816; M1675; M1676; OPS TEST GOOD IAW AMM 33-51-06-960-805 AND AMM 33-51-0G-960-806 ' 'WN6839; CP4369; WN5541; CP4370; WN6354; CP4371

Part: ANGLE — CORRODED (GALLEY) · airframe 26,352 hrs · 11,691 cycles

G4 GALLEY LOWER RH OTBD STOAGE COMPARTMENT AFT SIDE L ANGLE CORRODED. / REMOVED AND REPLACED G4 GALLEY LOWER R/H OUTBOARD COMPARTMENT; AFT L ANGLE STOP IAW CMM 25-31-76 PG 3002 STEP 20 AND PG 7002 STEP 20 ' 'A-TAG # A02984

Part: ANGLE — CORRODED (GALLEY) · airframe 26,352 hrs · 11,691 cycles

G4 GALLEY LOWER RH OTBD STOAGE COMPARTMENT2ND FROM BOTTOM; AFT SIDE L ANGLE CORRODED. / REMOVED AND REPLACED G4 GALLEY LOWER R/H OUTBOARD COMPARTMENT; 2ND FROM BOTTOM; L ANGLE AFT STOP IAW CMM 25-31-76 PG 3002 STEP 20 AND PG 7002 STEP 20 ' 'A-TAG # A02984

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 26,352 hrs · 11,691 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED P/N 146A8343-5 / RECIEVED REPAIRED CORNER SCUFF PLATE P/N 146A8343-5 FOR AFT CARGO BAY OFF SIDE PER W/O# 40458-1600-0001 FROM BACK SHOP

Part: STRINGER CLIP — CRACKED (BS 500I, S25L) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO AT BS 500I STR 25LH STRINGER CLIP CRACKED AT FRAME ATTACH RIVET WL 155 LBL22. / REMOVED AND REPLACED STR CLIP ON STR 25L; STA 500I IAW SRM 51-40-02-0G-0; BOEING DWG NO 143A1234 ID 0002 REV 1; ' 'A TAG A07227

Part: ANGLE — CORRODED (BS 727J-747) · airframe 26,045 hrs · 11,515 cycles

AFT CARGO PIT L/H Z ANGLE HAD 3 NUTPLATES WITH CORROSION BETWEEN BS. 727J TO BS. 747. / R&R L/H Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO RH Z ANGLE CORRODED AT BS 500A TO 500D +12' WL 160 RBL 22'. / EVALUATED CORROSION DAMAGE; FOUND TO BE OUT OF LIMITS; REMOVED ZEE ANGLE STA 500A TO 500I RBL 22; REMOVED ZEE ANGLE STA 400 TO 420 RBL 22; REMOVED FWD BULKHEAD LOWER ATTACH BRKT STA 400 LBL 22 TO RBL 22; DISPLACED FWD BULKHEAD R/H ATTACH ANGLE FOM; VERIFIED MATERIAL AS BAC 1496-44 7075T6; FABRICATED NEW ZEE ANGLES; TREATED AND PRIMED; ASSEMBLED REPAIR PARTS; INSTALLED NUTPLATES. INSTALLED NEW ZEE ANGLE STA 500A TO 500I; INSTALLED NEW ZEE ANGLE STA 400 TO 420 RBL 22; REINSTALLED FWD BULKHEAD LOWER ATTACH BRKT; REINSTALLED R/H ATTACH ANGLE IAW SRM 53-00-53-1A-2 FIG 103 DETAAIL D; SRM 53-00-53-2R-5; SRM 51-40-02-0G-0; AMM 51-21-41-370-802; AMM 51-21-72-370-804; SRM 51-40-10 FOUND OUT OF LIMITS DUE TO DAMAGE BEING ON EDGE OF HOLE IAW SRM 53-00-53-1A-2 FIG 103 DET D Z-ANGLE P/N 193A750-188 ATAG A50377; A50388 P/N 143A7501-184

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

AFT CARGO PIT LH Z ANGLE STA. 727J TO 747 HAS 3 NUTPLATES WITH MINOR CORROSION / REMOVED CORROSION AT AFT CARGO L/H Z ANGLE STA 727 J TO STA 747 I.A.W SRM 53-00-53-1A-2. VERIFIED MATERIAL LOSS ORIGINAL .040 REMOVED .006 REMAIN .034 ALLOWABLE 10% MAX FOUND OUT OF LIMITS USED AAR TOOL #36649 DUE 07AUG20 I.A.W SRM 53-00-53-1A-2. REMOVED Z ANGLE FROM STA 727C +12' TO STA 847 I.A.W SRM 51-40-02-0G-0 DRILLED Z ANGLE SPLICE REPAIR I.A.W SRM 53-00-53-2R-S INSTALLED Z ANGLE AND REPAIR SPLICES I.A.W SRM 53-00-53-2R-5 ' '(2 EA ANGLE) P/N 146A7502-31

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO LH Z ANGLE CORRODED AT BS 440 +3' WL 160 LBL 22'. / REMOVED CORROSION ON FWD CARGO L/H Z-ANGLE AT ATS 440+3'; WL 160 LBL 22' IAW SRM 51-10-02 + FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; DETAIL D. CORROSION IS NUT PLATE REPLACED NEW FABRICATED Z-ANGLE IAW SRM 53-00-53-2R-5 FROM STA 440+3 TO 500I. TREATED + PRIMED IAW SRM 51-20-01 & AMM 51-21-72-370-804. APPLIED CIC PER AMM 51-21-91-620-802 (ZEE- ANGLE) PN 143A7501-187

Part: FLOOR PANEL — FRAYED (CABIN) · airframe 26,352 hrs · 11,691 cycles

CABIN FLOOR PANEL #222DF; UPPER SIDE OF PANEL; SEVERAL AREAS OF FRAYED UPPER SKIN SURFACE; AREAS MARKED IN BLUE / REPAIRED CABIN FLOOR PANEL #222DF UPPER SIDE ' 'SEVERAL AREA'S OF FRAYED SKIN I.A.W B737-800 SRM'S ' '53-00-50-2R-1 REV 68 & 53-00-50-2R-0' '(A36551) ' '(A98054)

Part: ANGLE — CORRODED (BS 727F-727G) · airframe 26,045 hrs · 11,515 cycles

AFT CARGO PIT L/H Z ANGLE HAD 4 NUTPLATES WITH MINOR CORROSION BETWEEN BS. 727F TO BS. 727G. / R&R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

AFT CARGO PIT LH Z ANGLE STA. 747 TO 767 5 NUTPLATES HAVE MINOR CORROSION / REMOVED CORROSION ON L/H Z ANGLE IN AFT CARGO PIT AT STA 747 TO STA 767 IAW SRM 51-10-02-0G-0 VERIFIED WITH 10X. VERIFIED MATERIAL AS ORIGINAL .040' LOSS OF .006' REMAINING .034' FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. REPAIRED Z ANGLE ON NRC Y173445 ' '(ZEE ANGLE) P/N 146A7502-31

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,352 hrs · 11,691 cycles

FLOORBOARD 242D HAS FACE SHEET FIBERS PULLED / REPAIRED UPPER FACE SHEET PLY IAW SRM ' '53-00-50-2R-1 PG'S 1;2; STEPS 3 (A-N)' 'A94592; ' 'A06130; A05073; A78614

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO RH Z ANGLE CORRODED AT BS 400 TO 420 WL 160 RBL 22'. / EVALUATED CORROSION DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DET D; REPAIR ACCOMPLISHED ON Y173420 (ZEE ANGLE) PN 143A2501-184

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO AFT BLKD LOWER SUPPORT ANGLE CORRODED AT BS 500I WL 160 RBL 22' TO LBL22. / NO ALLOWABLE CORROSION LIMITS. REMOVED AFT BULKHEAD LOWER SUPPORT ANGLE AT STA 500I. VERIFIED NEW PART AS P/N 143A9485Y35; LOCATED AND DRILLED; INSTALLED NEW SUPPORT ANGLE. IAW SRM 51-40-02-0G-0; BOEING DWG NO 143A9484 REV A; SRM 51-40-05-0G-0. A TAG WN9109 SUPPORT ANGLE P/N 103A9483Y35.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

AFT CARGO PIT RH Z ANGLE STA. 747 TO 767 HAS 2 NUTPLATES WITH MINOR CORROSION / AFT CARGO PIT R/H 'Z' ANGLE WAS REPLACED FROM STA 727 + 11' TO 767 ON SWA SA-M112 DEFECT # Y173444 W/O # 40456-1600-0013 (ZEE ANGLE) P/N 146A7502-52

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO RH Z ANGLE CORRODED AT BS 500I TO 500D +12' WL 160 RBL 22'. / EVALUATED CORROSION DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DET D; REPAIR ACCOMPLISHED ON Y173420

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,352 hrs · 11,691 cycles

FLOORBOARD 241AAF HAS FACE SHEET FIBERS PULLED / REPAIRED UPPER FACE SHEET ON FLOORBOARD 241 AAF IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS 3 (A-N). ' 'A05073; A94592

Part: STRINGER CLIP — CRACKED (BS 500I, S26R) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO COMPARTMENT STR CLIP IS CRACKED AT STA 500I STR 26R (P/N 143A1010-48) / REMOVED AND REPLACED STRINGER CLIP ON STR 26R AT STA 500I IAW SRM 51-40-02-0G-0; BOEING DWG NO 143A1234 ID 0002 REV A; SRM 51-40-05-0G-0 ' 'P/N 143A1010-48 ' 'A TAG A94753

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO LH Z ANGLE CORRODED AT BS 500C + 6'TO 500D +12' WL 160 LBL 22'. / ACCOMPLISHED ALL WORK STEPS ON W/O #40456/1400/0005; DEFECT NO Y173414. EVALUATED CORROSION ON FWD CARGO L/H Z ANGLE AT STA 500D+12' TO STA 500C +6' LBL 22 AND WL160; FOUND OUT OF LIMITS DUE TO CORROSION ON FASTENER HOLE IAW SRM 53-00-53-1A-2 DET D (ZEE ANGLE) PN 143A7501-187

Part: SHIELD — CORRODED (BS 496-500A) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO RH SHIELD CORRODED AT BS 496 TO 500A WL 160 RBL 22'. / REMOVED CORROSION FROM FWD CARGO R/H SHIELD STA 496 TO 500A RBL 22; VERIFIED WITH 10X MAGNIFYING GLASS; VERIFIED MATERIAL LOSS ORIG .032' REMAINING .026' LOSS .006' FOUND TO BE OUT OF LIMITS; REMOVED SHIELD STA 496 TO 500A RBL 22; RECEIVED FORMED SHIELD FROM BACK SHOP PER W/O40458-1400-0002; LOCATED AND DRILLED; INSTALLED NEW SHIELD STA 496 TO 500A RBL 22. IAW SRM 51-10-02-0G-0; SRM 53-30-151A-1 FIG 103 DET E; SRM 51-40-02-0G-0; BOEING DWG NO 143A8126 REV -; SRM 51-40-05-0G-0; SRM 40-06-0G-0; SRM 51-20-01; AMM 51-21-73-370-804 SHIELD P/N 143A8126-38

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

AFT CARGO PIT LH Z ANGLE STA. 727F TO 727G HAS 4 NUTPLATES WITH MINOR CORROSION / REMOVED CORROSION AFT PIT LH Z ANGLE P/N 146A7502-31 IAW SRM 51-10-02-0G-0. OT .040 REM .034 LOSS .006. FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103. ZEE ANGLE REPLACED ON N/R Y173445. ' 'ZEE ANGLE P/N 146A7502-31

Part: FLOOR PANEL — FRAYED (CABIN) · airframe 26,352 hrs · 11,691 cycles

CABIN FLOOR PANEL #221EF; UPPER SIDE OF PANEL; AREAS OF FRAYED SKIN ON PANEL; AREAS MARKED IN BLUE / REPAIRED CABIN FLOOR PANEL #221EF UPPER SIDE IAW B737 SRM 53-00-50-2R-1 REPAIR 1 PARA 3 ' 'A36551 A98054

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,352 hrs · 11,691 cycles

FLOORBOARD 242F HAS FACE SHEET FIBERS PULLED / REPAIRED UPPER FACESHEET SURFACE PULLED FIBERS ON FLOORBOARD PANEL (242F) WITH WET-LAY-UP REPAIR IAW B737-800 SRM 53-00-50-2R-1 (3) A-N (REV 68)

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,352 hrs · 11,691 cycles

FLOORBOARD 241XF FACE SHEET FIBRES PULLED / REPAIRED UPPER FACESHEET PULLED FIBERS ON ' 'FLOORBOARD PANEL (241 XF) WITH WET-LAY-UP REPAIR ' 'I/A/W B737-800 SRM 53.00.50.2R21 (3) A-N (REV 68)

Part: FLOORBOARD — PULLED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

FLOORBOARD 241ABF HAS FACE SHEET FIBERS PULLED; ALSO ONE INSERT PULLED JUST AFT OF FWD TROUGH DRAIN / REPAIRED UPPER FACESHEET PULLED FIBERS ON FLOORBOARD PANEL (241 ABF) WITH WET LAY-UP REPAIR AND INSTALLED NEW INSERT IAW B737-800 SRM 53-00-50-2R-1 (3) A-N (REV 68)

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

AFT CARGO PIT RH Z ANGLE STA. 727 J TO 747 HAS 5 NUTPLATES WITH MINOR CORROSION / BLEND CORROSION ON AFT CARGO R/H '2' ANGLE AND FOUND A MATERIAL LOSS OF .009' (ORIG=.040' REMAINING=.031') TO BE 'OUT OF LIMITS' AS PER B737 SRM 53-00-53-1A-2 FIG 103. REMOVED AND REPLACED SECTION OF 'Z' ANGLE FROM STA 727H+11' TO 767 AS PER B737 SRM 53-00-53-2R-5 (ZEE ANGLE) P/N 146A7502-52

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO LH Z ANGLE CORRODED AT BS 500 + 10'TO 500B +12' WL 160 LBL 22'. / ACCOMPLISHED REPAIR ON W/O# 40456/1400/0005 DEFECT #Y173414. EVALUATED DAMAGE ON FWD CARGO L/H Z ANGLE AT BS 500+10' TO 500B+12'; LBL 22 AND WL 160; FOUND OUT OF LIMITS DUE TO CORROSION ON FASTENER HOLE IAW SRM 53-00-53-1A-2 DET D. (ZEE ANGLE) P/N 143A7501-187

Part: ANGLE — CORRODED (BS 727J-747) · airframe 26,045 hrs · 11,515 cycles

AFT CARGO PIT R/H Z ANGLE CORRODED BETWEEN BS. 727J TO BS. 747. / R&R Z ANGLE PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

AFT CARGO PIT LH Z ANGLE STA. 767 TO 787 HAS SEVERAL SPOTS OF CORROSION / REMOVED CORROSION AFT PIT LH Z ANGLE P/N 146A7502-31 IAW SRM 51-10-02-0G-0. OT .040 REM .034 LOSS .006. FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103. ZEE ANGLE REPLACED ON N/R Y173445. ' 'ZEE ANGLE P/N 146A7502-31

Part: FLOORBOARD — CRUSHED (CABIN) · airframe 26,352 hrs · 11,691 cycles

FLOORBOARD 242UF HAS FACE SHEET FIBERS PULLED ALSO FWD UNDERSIDE INBD CORNER CRUSHED / REPAIRED UPPER FACESHEET AND UNDERSIDE INBD CORNER ON FLOORBOARD PANEL (242 UF) WITH WET LAY-UP REPAIR IAW B737-800 SRM 53-00-50-2R-1 (3) A-M (REV 68)

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,352 hrs · 11,691 cycles

FLOORBOARD 241D HAS FACE SHEET FIBERS PULLED / REPAIRED UPPER FACESHEET PLY ON FLOORBOARD 241D ' 'IAW SRM 53-00-50-2R-1; PG 1;2; STEPS 3 (A-N) ' '' '' 'A05073; A94592

Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO LH Z ANGLE CORRODED AT BS 500I TO 500D +12' WL 160 LBL 22'. / ACCOMPLSIHED REPAIR ON W/O #40456/1400/0005 DEFECT NO Y173414. EVAULATED CORROSION ON FWD CARGO L/H Z ANGLE AT STA 500D+12' TO STA 500I; LBL 22 AND WL160 FOUND OUT OF LIMITS DUE TO CORROSION ON FASTENER HOLE IAW SRM 53-00-53-1A-2 DET D (ZEE ANGLE) PN 143A750H87

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO AFT CORNER SCUFF PLATE IS CRACKED / FWD CARGO AFT CORNER SCUFF PLATE CRACK-WELD REPAIR ACCOMPLISHED ON W/O 40458 - 1400 - 0001 IAW B737-800 SRM 53-30-15-2R-1 SN; 4626274

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,352 hrs · 11,691 cycles

FLOORBOARD 241F HAS FACE SHEET FIBERS PULLED / REPAIRED UPPER FACESHEET SURFACE PULLED FIBERS ON FLOORBOARD PANEL (241F) WITH WET-LAY-UP REPAIR IAW B737-800 SRM 53-00-50-2R-1 (3) A-N (REV 68)

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,352 hrs · 11,691 cycles

FLOORBOARD 242E HAS FACE SHEET FIBERS PULLED / REPAIRED UPPER FACE SHEET PLY ON FLOORBOARD 242 E ' 'IAW SRM 53-00-50-2R-1; PG'S 1;2; STEP 3(A-N)' '' 'A05073; A94592

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 26,352 hrs · 11,691 cycles

FLOORBOARD 241YF HAS FACE SHEET FIBERS PULLED / REPAIR UPPER SURFACE PLY ON FLOORBOARD 241YF IAW SRM 53-00-50-2R-1; PG'S 1;2; STEPS 3(A-N)

Part: ANGLE — CORRODED (BS 767-787) · airframe 26,045 hrs · 11,515 cycles

AFT CARGO PIT L/H Z ANGLE HAD SEVERAL SPOTS CORRODED BETWEEN BS. 767 TO BS. 787. / R&R Z ANGLE IAW SRM.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 26,352 hrs · 11,691 cycles

AFT CARGO FLOOR PANEL 140BF CORROSION AROUND FASTENER HOLES; AS MARKED. / FOUND CORROSION ON PANEL 140BF TO EXCEED ALLOWABLE LIMITS; VERIFIED NEW PANEL AS P/N 453A2610-32 IAW SRM 53-00-53-1A-1; AIPC 25-52-10-19 ITEM 25. P/N 453A2610-32 A TAG WN4945.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 26,352 hrs · 11,691 cycles

AFT CARGO FLOOR PANEL 140EF CORROSION AROUND FASTENER HOLES; AS MARKED. / EVALUATED CORODED FLOOR PNL 140EF AT AFT CARGO FOUND IS MORE THAN 20 INCHES IN LENGTH IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 REPLACED FLOOR PNL WITH NEW PNL IAW IPC 25-52-10-19 AND BOEING DWG 453A2610 (PANEL) P/N 453A2610-58

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 26,352 hrs · 11,691 cycles

AFT CARGO FLOOR PANEL 140DF CORROSION AROUND FASTENER HOLES; AS MARKED. / EVALUATED FLOOR PANEL 140DF IAW B737 SRM 53-00-53-1A-1 AND FOUND TO BE OUT OF LIMITS (EXCEEDS 20') CORROSION. FABRICATED NEW PANEL 140 DF IAW BOEING DRAWING 453A2610 REV B AND REV K (PANEL) 453A2610-20

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 26,352 hrs · 11,691 cycles

AFT CARGO FLOOR PANEL 140CF CORROSION AROUND FASTENER HOLES; AS MARKED. / FOUND CORROSION TO EXCEED ALLOWABLE LIMITS VERIFIED NEW PANEL 140CF AS P/N 453A2610-18 IAW SRM 53-00-53-1A-1; AIPC 25-52-10-19 ITEM 35 P/N 453AA2610-18 A TAG WN5161.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 26,352 hrs · 11,691 cycles

CUSTOMER REQUEST - JC - R/H 663 VAPOR WEB HAS CRACK EMITTING FROM PREVIOUS REPAIR / EVALUATED ST 663 RH VAPOR BARRIER CRACK AND FOUND TO BE REPAIRABLE CLEANED AND PREPPED AREA FOR REPAIR ON BONDED REPAIR PER SRM 57-10-10-2R-2; SRM 51-70-04-2R-0 AND SRM 51-70-04-2R-10

Part: FAIRING — DELAMINATED (WNG-BODY) · airframe 26,352 hrs · 11,691 cycles

WING TO BODY FAIRING PANEL 194CL IS DELAMINATED ON OUTER SURFACE (CIRCLED IN BLACK) / REPAIRED AND APPLIED DECORATIVE FINISH ON WING TO ' 'BODY FAIRING PANEL 194CL DELAMINATED ON OUTER ' 'SURFACE AS MARKED IAW B737 SRM 51-70-04-2R-11 REV ' '68; B737 SRM 51-70-04-2R-2 REV; 68; B737 SRM ' '51-70-04-2R-0 REV 68; B737 SRM 51-70-08-0G-0 REV ' '68 AND B737 AMM 51-21-99-300-801 REV 70.' 'A50541 ' 'A37286 A50534 A37688 A33874

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO COMP. PANEL 120CF CORROSION AROUND FASTNER HOLES FWD RH SIDE OF PANEL / RECEIVED IDENTIFIED + REPLACED CORRODED FWD CARGO COMPARTMENT FLOOR PANEL 120CF IAW AIPC 25-52-10-17 ITEM 25 + ATAG WN1763 PN 4251047.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 26,352 hrs · 11,691 cycles

FWD CARGO COMP. PANEL 120DF CORROSION AROUND THE SIDES OF PANEL AT THE FASTNER HOLES / RECEIVED IDENTIFIED + REPLACED CORRODED FWD CARGO PANEL 120DF IAW AIPC 25-52-10-17 ITEM 35 + ATAG WN 1838 PN 4251048

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,352 hrs · 11,691 cycles

ALL EMERGENCY LIGHTS POWERED BY M1672 (AFT R/H BATTERY) ARE INOP. / REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY ' 'PACK M1672; OPS CHECK GOOD IAW AMM ' '33-51-06-960-805 AND AMM 33-51-06-960-806' 'WN0071; ' 'CP4323

Part: ANGLE — CORRODED (BS 440) · airframe 26,045 hrs · 11,515 cycles

FWD CARGO LH Z ANGLE CORRODED AT BS 440 +3" WL 160 LBL 22". / REMOVED CORROSION ON FWD CARGO L/H Z-ANGLE AT ATS 440+3", WL 160 LBL 22" IAW SRM 51-10-02 + FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2, DETAIL D. CORROSION IS NUT PLATE REPLACED NEW FABRICATED Z-ANGLE IAW SRM 53-00-53-2R-5 FROM STA 440+3 TO 500I. TREATED + PRIMED IAW SRM 51-20-01 & AMM 51-21-72-370-804. APPLIED CIC PER AMM 51-21-91-620-802 (ZEE- ANGLE) PN 143A7501-187.

Part: SHIELD — CORRODED (BS 496-500A) · airframe 26,045 hrs · 11,515 cycles

FWD CARGO RH SHIELD CORRODED AT BS 496 TO 500A WL 160 RBL 22". / REMOVED CORROSION FROM FWD CARGO R/H SHIELD STA 496 TO 500A RBL 22, VERIFIED WITH 10X MAGNIFYING GLASS, VERIFIED MATERIAL LOSS ORIG .032" REMAINING .026" LOSS .006" FOUND TO BE OUT OF LIMITS, REMOVED SHIELD STA 496 TO 500A RBL 22, RECEIVED FORMED SHIELD FROM BACK SHOP PER W/O40458-1400-0002, LOCATED AND DRILLED, INSTALLED NEW SHIELD STA 496 TO 500A RBL 22. IAW SRM 51-10-02-0G-0, SRM 53-30-151A-1 FIG 103 DET E, SRM 51-40-02-0G-0, BOEING DWG NO 143A8126 REV -, SRM 51-40-05-0G-0, SRM 40-06-0G-0, SRM 51-20-01, AMM 51-21-73-370-804 SHIELD P/N 143A8126-38.

Part: STRINGER CLIP — CRACKED (BS 500I) · airframe 26,045 hrs · 11,515 cycles

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

Part: SUPPORT ANGLE — CORRODED (BS 500I BULKHEAD) · airframe 26,045 hrs · 11,515 cycles

FORWARD CARGO AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS. 500I, BETWEEN RBL 22 TO LBL 22. / R&R ANGLE IAW SRM & DWG.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,045 hrs · 11,515 cycles

ALL EMERGENCY LIGHTS POWERED BY M1672 (AFT R/H BATTERY) WERE INOP. / R&R POWER SUPPLY IAW AMM.

Part: STRINGER CLIP — CRACKED (BS 500I) · airframe 26,045 hrs · 11,515 cycles

FORWARD CARGO STRINGER CLIP CRACKED AT FRAME ATTACH RIVET BS. 500I, STR. 25L. / R&R STRINGER CLIP IAW SRM & DWG.

Part: ANGLE — CORRODED (BS 500A-500D) · airframe 26,045 hrs · 11,515 cycles

FWD CARGO RH Z ANGLE CORRODED AT BS 500A TO 500D +12" WL 160 RBL 22". / EVALUATED CORROSION DAMAGE, FOUND TO BE OUT OF LIMITS, REMOVED ZEE ANGLE STA 500A TO 500I RBL 22, REMOVED ZEE ANGLE STA 400 TO 420 RBL 22, REMOVED FWD BULKHEAD LOWER ATTACH BRKT STA 400 LBL 22 TO RBL 22, DISPLACED FWD BULKHEAD R/H ATTACH ANGLE FOM, VERIFIED MATERIAL AS BAC 1496-44 7075T6, FABRICATED NEW ZEE ANGLES, TREATED AND PRIMED, ASSEMBLED REPAIR PARTS, INSTALLED NUTPLATES. INSTALLED NEW ZEE ANGLE STA 500A TO 500I, INSTALLED NEW ZEE ANGLE STA 400 TO 420 RBL 22, REINSTALLED FWD BULKHEAD LOWER ATTACH BRKT, REINSTALLED R/H ATTACH ANGLE IAW SRM 53-00-53-1A-2 FIG 103 DETAAIL D, SRM 53-00-53-2R-5, SRM 51-40-02-0G-0, AMM 51-21-41-370-802, AMM 51-21-72-370-804, SRM 51-40-10 FOUND OUT OF LIMITS DUE TO DAMAGE BEING ON EDGE OF HOLE IAW SRM 53-00-53-1A-2 FIG 103 DET D Z-ANGLE P/N 193A750-188 ATAG A50377, A50388 P/N 143A7501-184.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 26,045 hrs · 11,515 cycles

R/H BS. 663 VAPOR WEB HAD CRACK EMITTING FROM PREVIOUS REPAIR. / REPAIRED WEB PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,045 hrs · 11,515 cycles

ALL EMERGENCY LIGHTS POWERED BY M1672 (AFT R/H BATTERY) WERE INOP. / R&R BATTERY PACK IAW AMM.

Part: ANGLE — CORRODED (BS 400-420) · airframe 26,045 hrs · 11,515 cycles

FWD CARGO RH Z ANGLE CORRODED AT BS 400 TO 420 WL 160 RBL 22". / EVALUATED CORROSION DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DET D, REPAIR ACCOMPLISHED ON Y173420 (ZEE ANGLE) PN 143A2501-184.

Part: SEAL — CRACKED (RH HOR STAB) · airframe 25,566 hrs · 11,282 cycles

RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-13-13AMT 65147

Part: PANEL — CRACKED (CABIN) · airframe 25,566 hrs · 11,282 cycles

FLOOR BOARD SUPPORT BRAKE PANEL CRACKED LEFT OF CENTER AT STA 540 / R+R CRACKED FLOORBOARD SUPPORT BRAKE PANEL ASSY LEFT OF CENTER AT STA 540 AS PER SRM 51-40-02 AND AMM 53-21-00AMT 59828

Part: PANEL — CRACKED (CABIN) · airframe 25,566 hrs · 11,282 cycles

FLOOR BOARD SUPPORT BRAKE PANEL CRACKED RIGHT OF CENTER AT STA 540 / R+R CRACKED FLOORBOARD SUPPORT BRAKE PANEL ASSY AS PER SRM 51-40-02 AND AMM 53-21-00; LOCATED RIGHT OF CENTER AT STA 540AMT 59828

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 24,764 hrs · 10,915 cycles

R1 DOOR EMERGENCY SLIDE FELL FROM HOUSING. REPACKED SLIDE IAW MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,030 hrs · 9,595 cycles

L2 DOOR EMERGENCY EXIT SIGN LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,030 hrs · 9,595 cycles

L2 DOOR EXTERIOR EMERGENCY EXIT SIGN LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 21,563 hrs · 9,392 cycles

AFT OVER WING EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: RELIEF VALVE — MALFUNCTIONED (LT WING) · airframe 19,958 hrs · 8,657 cycles

AIR TURNBACK, ON TAKEOFF OTHER AIRCRAFT REPORTED SEEING FUEL VENTING HEAVY OUT OF LT WING. RESET PRESSURE RELIEF VALVE PER AMM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 19,370 hrs · 8,370 cycles

CEILING EMERGENCY LIGHT INOP AT SEAT ROW 21. CONNECTED LIGHT IAW AMM.

Part: LENS — CRACKED (L1 DOOR) · airframe 19,370 hrs · 8,370 cycles

L1 DOOR EMERGENCY SLIDE COVER LENS CRACKED. R&R LENS IAW MT.

Part: BRACKET — CRACKED (LT WING) · airframe 19,370 hrs · 8,370 cycles

LT WING TRAILING EDGE BRACKET CRACKED ON INBOARD SIDE OF THE DEFLECTION CONTROL RIB. R&R BRACKET IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,370 hrs · 8,370 cycles

AFT CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727D-6 TO BS 847, LBL 20. REPAIRED SUPPORT IAW SRM & DWG.

Part: GUSSET — CRACKED (FWD CARGO RH) · airframe 19,947 hrs · 8,650 cycles

FWD CARGO GUSSET CRACKED STR19R STA 500I / REMOVED AND REPLACED FWD CARGO GUSSET AT STA. 500I STR 19R IAW SRM 51-40-02-0G-0 AND DWG 143A7902.

Part: GUSSET — CRACKED (BS 500I) · airframe 19,370 hrs · 8,370 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500I, STRINGER 19R. R & R THE GUSSET IAW SRM AND DWG.

Part: PANEL — DELAMINATED (LEFT WING) · airframe 19,947 hrs · 8,650 cycles

LT WING ACCESS PANE 521 PB HAS DELAMINATION ON THE CORNER / REPAIRED DELAMINATION OF EROSION . STOP ON CORNER OF L/H WING ACCESS PANEL 521PB PER SRM 57-41-01-2R-6

Part: SUPPORT — CORRODED (FWD CARGO LH) · airframe 19,947 hrs · 8,650 cycles

***CORROSION*** FWD CARGO FLOOR TO SIDEWALL SUPPORT BS 500B+13 TO 500D+10 LBL23 / CORROSION ON FWD CARGO FLOOR TO SIDEWALL SUPPORT STA 500B+13 - 50D+10 LBL23 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT STA 500B+12 - 500D+12 AND INSTALLED SIDEPLATE SPLICES AT STD 500B+132 AND 500D+12 IAW SRMS 51-40-02-0G-0; 53-00-53-2R-5; AND BOEING DWG 143A7505 54110 REV-

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 19,947 hrs · 8,650 cycles

***CORROSION*** AFT CARGO FLOOR TO SIDEWALL SUPPORT BS 727B+6 TO 767 / DAMAGE AT AFT CARGO FLOOR TO SIDEWALL SUPPORT BS 727B+6 - 767 FOUND TO BE L1.5 W1' D.010 ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED DAMAGED SECTION 727B+6 - 767 IAW SRM 51-40-02-0G-0 FABRICATED REPLACEMENT SUPPORT FROM BAC1496-377 7075T62 LOT # 5062573-1 IAW SRM 53-00-53-2R-5 TREATED + PRIMED IAW SRM 51-20-01-0G-0 + SOPM 20-41-02 INSTALLED NUT PLATES IAW BOEING DWG # 146A7502 REV A INSTALLED REPLACEMENT SUPPORT IAW BOEING DWG 146A7502 REV A + SRM 51-40-02-0G-0 WITH SPLICES LOCATED AT 727B+8 + 727H + 11

Part: BRACKET — BROKEN (LOWER EXT FUSELA) · airframe 19,947 hrs · 8,650 cycles

SUPPORT BRACKET BROKEN ON KEEL BEAM FWD R/H BS.550 RBL5 / REMOVED ADN REPLACED SUPPORT BRACKET ON KEEL BEAM FWD R/H B.S. 550 RBL 5 IAW DWG 149A7701 AND SRM 51-40-02-0G-0.

Part: SUPPORT — CORRODED (FWD CARGO RH) · airframe 19,947 hrs · 8,650 cycles

***CORROSION*** FWD CARGO FLOOR TO SIDEWALL SUPPORT BS 500A TO 500I RBL23 / REMOVED CORROSION FROM AFFECTED AREA. ORIGINAL MATERIAL THCKNESS WAS .040'. MATERIAL LOSS WAS GREATER THAN 10% AND WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG. 103 REPAIRED FLOOR TO SIDEWALL SUPPORT ANGLE. FABRICATED NEW FLOOR TO SIDEWALL REPAIR ANGLE AND SPLICE PART #BAC1496-444 #7075T6 LOT #5061427-3 IAW SRM 53-00-53-2R-5 REPAIR SPLICE LOCATED AT STA. 500D+12' RBL23

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 19,947 hrs · 8,650 cycles

***CORROSION*** AFT CARGO FLOOR TO SIDEWALL SUPPORT BS 727D - 6 TO 847 LBL 20 / DAMAGE AT AFT CARGO FLOOR TO SIDEWALL SUPPORT B727D+6-847 FOUND TO BE L 2' W 1.5' D .010' ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITS. IAW SRM 53-00-53-1A-2. REMOVED DAMAGED SECTION FROM 727D+6-847 IAW SRM 51-40-02-0G-0. FABRICATED NEW SUPPORT FROM BAC 1496-377 7075 T62 LOT #5062573-41 IAW SRM 53-00-53-2R-5 TREATED & PRIMED IAW SRM 51-20-01-06 & SOPM 20-41-02 INSTALLED NUT PLATES IAW BOEING DWG #146A7502 REV A INSTALLED NEW SUPPORT IAW BOEING DWG 146A7502 REV A & SRM 51-40-02-0G-0 WITH SPLICES LOCATED AT 727C+11 & 727I+17

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 19,370 hrs · 8,370 cycles

AFT CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727B+6 TO BS 767. R&R SUPPORT IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,370 hrs · 8,370 cycles

FORWARD CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500I, RBL 23. R&R ANGLE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 19,370 hrs · 8,370 cycles

FORWARD CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500B+13 TO BS 500D+10, LBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: BRACKET — CRACKED (LEFT WING) · airframe 19,947 hrs · 8,650 cycles

LEFT WING TRAILING EDGE BRACKET CRACKED ON INBOARD SIDE OF THE DEFLECTION CONTROL RIB. (MARKED) / REMOVED AND REPLACED LEFT WING TRAILING EDGE BRACKET IAW SRM 51-40-02-OG-04. AND DRAWING NUMBER 115A6200 REV. B

Part: LENS — CRACKED (CABIN) · airframe 19,370 hrs · 8,370 cycles

LT EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 12. R&R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 19,370 hrs · 8,370 cycles

LT EMERGENCY EXIT LIGHT LENS CRACKED BETWEEN ROW 8 TO ROW 9. R&R LENS IAW AMM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 19,787 hrs · 8,574 cycles

RIGHT OVERWING EMERGENCY LIGHT LENS BROKEN. R & R THE LENS IAW MM.

Part: SENSOR — FAULTY (LE FLAPS) · airframe 18,318 hrs · 7,875 cycles

LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED DURING CLIMBOUT. RETURNED TO DEPARTURE. R & R LEADING EDGE FLAP NR 3 EXTEND SENSOR IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 17,661 hrs · 7,568 cycles

L2 DOOR EXIT SIGN LOOSE. SECURED SIGN PER SIP.

Part: PUMP — LOW PRESSURE (B HYD SYSTEM) · airframe 17,467 hrs · 7,483 cycles

B SYSTEM HYDRAULIC LOW PRESSURE AND QUANTITY LOSS IN FLIGHT. EMERGENCY DECLARED AND DIVERTED. R & R THE NR 2 ENGINE DRIVEN PUMP IAW MMM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 15,946 hrs · 6,804 cycles

FWD ENTRY EXIT LIGHT LENS BROKEN. R & R THE LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 14,090 hrs · 5,960 cycles

LEFT EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 27. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 12,549 hrs · 5,281 cycles

CABIN OVERHEAD EXIT LIGHT LENS CRACKED AT ROW 14 DEF. R & R LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 12,157 hrs · 5,117 cycles

CABIN EMER LIGHT LENS CRACKED AT ROW 23 ABC. R & R LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 12,549 hrs · 5,281 cycles

CABIN OVERHEAD EXIT LIGHT LENS CRACKED AT ROW 25 DEF. R & R LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 12,549 hrs · 5,281 cycles

CABIN OVERHEAD EXIT LIGHT LENS CRACKED AT ROW 23 ABC. R & R LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 12,157 hrs · 5,117 cycles

CABIN EMER LIGHT LENS CRACKED AT ROW 15 ABC. R & R LENS IAW MM.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 12,157 hrs · 5,117 cycles

RIGHT WING NR 9 SPOILER UPPER SKIN DELAMINATED. R & R SPOILER IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 12,157 hrs · 5,117 cycles

CABIN EMER LIGHT LENS CRACKED AT ROW 14 DEF. R & R LENS IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 12,549 hrs · 5,281 cycles

CABIN OVERHEAD EXIT LIGHT LENS CRACKED AT ROW 15 ABC. R & R LENS IAW MM.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 12,157 hrs · 5,117 cycles

RIGHT WING NR 10 SPOILER UPPER SURFACE DELAMINATED. R & R SPOILER ASSEMBLY IAW MM.

Part: LENS — CRACKED (CABIN) · airframe 12,157 hrs · 5,117 cycles

CABIN EMER LIGHT LENS CRACKED AT ROW 25 DEF. R & R LENS IAW MM.

Part: LENS — MISSING (CABIN) · airframe 12,146 hrs · 5,114 cycles

L1 DOOR EMER EXIT LIGHT LENS MISSING. INSTALLED LENS IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 12,026 hrs · 5,064 cycles

LEFT FWD EMER EXIT SIGN BROKEN. R & R SIGN IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 9,969 hrs · 4,192 cycles

FORWARD SERVICE DOOR LOWER EXIT LIGHT COVER LOOSE. R & R LIGHT ASSEMBLY IAW AMM.

Part: SWITCH — FAULTY (CABIN) · airframe 9,391 hrs · 3,953 cycles

EMERGENCY LIGHTS ILLUMINATED WHEN FLIGHT DECK SWITCH FAULTY. R & R SWITCH IAW AMM.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 9,121 hrs · 3,832 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR FWD HANGER LOOSE. SECURED GIRT BAR IAW SRM.