N7857B

Part: DATA PLATE — DETACHED (ENGINE) · airframe 61,796 hrs · 41,245 cycles

ENGINE DATA PLATE (P/N'S 649-804-020-0, 649-804-023-0, 649-804-024-0, 649-804-027-0), DETACHES FROM THE ENGINE FAN FRAME. <THIS ALL EA PROVIDES TEMPORARY RELIEF AND INITIATES EA M-20-172-00810-TLD TO AUTHORIZE A 45-DAY DEFERRAL OF REINSTALLATION OF DATA PLATE OR THE BRACKET AND DATA PLATE ASSEMBLY.

Part: ATTACH BOLT — CRACKED (ZONE 600 SLAT) · airframe 61,520 hrs · 41,051 cycles

RIGHT WING NR 8 SLAT ACTUATOR, ONE FASTENER CRACKED AT ATTACHMENT POINT. REMOVED AND REPLACED THE RT WING NR 8 SLAT AND OPS CHECKED GOOD IAW AMM 27-81-21.

Part: LAMP — INOPERATIVE (ZONE 800) · airframe 61,520 hrs · 41,051 cycles

PASSENGER CABIN LT EMERGENCY EXIT DOOR LIGHT IS INOPERATIVE. REPLACED THE LAMPS IN THE EXIT LIGHT IAW AMM 33-21-00.

Part: COUNTERWEIGHT — CORRODED (ZONE 300 RUDDER) · airframe 61,520 hrs · 41,051 cycles

THE RUDDER COUNTER BALANCE WEIGHT CORRODED AND MISSING PAINT. REPLACED THE RUDDER COUNTER BALANCE WEIGHT IAW CMM 55-40-09.

Part: COVER — CRACKED (ZONE 800) · airframe 61,520 hrs · 41,051 cycles

FWD ENTRY DOOR LINER HANDLE COVER IS CRACKED. R & R FWD ENTRY DOOR LINER HANDLE COVER IAW AMM 52-11-31.

Part: STARTER — FAULTED (NR 2 ENGINE) · airframe 61,380 hrs · 40,959 cycles

DURING NR 2 ENGINE START. THE ENGINE WOULD NOT ACCELERATE BEYOND 8 PERCENT. R & R THE NR 2 ENG STARTER AIR TURBINE IAW AMM 80-11-01. OPS CHECKED IAW AMM 71-00-00-800-811-F00, OPS CHECKED GOOD.

Part: COVER — BROKEN (ZONE 200) · airframe 60,008 hrs · 40,092 cycles

COVER FOR THE EXIT ROW LIGHT ON THE BULKHEAD OF THE FOS EXIT ROW BROKE OFF.<[01] INSTALLED/SECURED EMERGENCY EXIT LIGHT COVER @RH OVER WING EXIT IAW AMM 33-51-03

Part: PLATE — CRACKED (ZONE 800 TE) · airframe 59,335 hrs · 39,676 cycles

LT WING; UPPER WING FIXED T/E PANEL STRUCTURE THAT SERRATED PLATE ATTES TO IS CRACKED; PANEL JUST O/B OF 551CT<[01] REPAIRED LEFT WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB PER SRM 57-51-02-2R-3 REPAIR 3. THIS IS A PERMANENT REPAIR.;[02] REPAIRED LEFT WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB PER SRM 57-51-02-2R-3 REPAIR 3. THIS IS A PERMANENT REPAIR.;[03] C/W;[04] CHANGED MEASUREMENTS RII FROM 'NO' TO 'YES' AND AND FAILURE TYPE FROM 'NO' TO 'YES' FOR INSPECTOR;[05] CERTIFIED;[06] REPAIRED LEFT WING I/B TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB PER SRM 57-51-02-2R-3. AND ALL FASTENERS RE-INSTALLED PER SRM 51-40-02. EXCEPT ONE MOST FORWARD AT WING STATION 278.5; INSTALLED PER EA 25-157-00818;[07] ANSWERED MEASUREMENTS 4 THRU 11 FOR AMT.;[08] CERTIFIED

Part: WEB — CRACKED (ZONE 100) · airframe 59,090 hrs · 39,530 cycles

CRACK ON WEB LOCATED BTW BS400 TO BS420AT LEVEL OF STR 26L FWD CARGO COMPARTMENT 2025-93419<[01] REPLACED WEB LOCATED BTW BS400 TO BS420AT LEVEL OF STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET:2 REV.B.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: SKIN PANEL — DELAMINATED (ZONE 500) · airframe 59,090 hrs · 39,530 cycles

DELAMINATED FIXED TRAILING EDGE SKIN PANEL UPPER SURFACE AT LH WING 2025-93409<[01] TOOLS USED= CALIPER P/N: 500-197-30; S/N: B20189571; DUE DATE: 06-JUN-25;[02] TOOL USED= SCALE P/N: CR5200; S/N: 8342514625; DUE DATE: 24-FEB-25;[03] TOOL USED= HOT BONDER P/N: HCS9000B; S/N: 18175469; DUE DATE: 14-AUG-25;[04] REPAIRED FIXED TRAILING EDGE SKIN PANEL UPPER SURFACE AT LH WING IAW B737-700 SRM 51-70-08-0G-0. SEE INDIVIDUAL SIGN OFFS BELOW.;[05] REPAIRED FIXED TRAILING EDGE SKIN PANEL UPPER SURFACE AT LH WING IAW B737-700 SRM 51-70-08-0G-0. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: WEB — CRACKED (ZONE 100) · airframe 59,090 hrs · 39,530 cycles

CRACK ON WEB LOCATED BTW BS440 TO BS460 AT LEVEL OF STR 26L FWD CARGO COMPARTMENT 2025-93402<[01] REPLACED WEB LOCATED BTW BS440 TO BS460 AT LEVEL OF STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 3 REV A.<BR>SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CERTIFIED CORRECTIVE ACTION 1; COMPLETED

Part: WEB — CRACKED (ZONE 100) · airframe 59,090 hrs · 39,530 cycles

CRACK ON WEB LOCATED BTW BS500 TO BS500A AT LEVEL OF STR 26L FWD CARGO COMPARTMENT 2025-93403<[01] REPLACED WEB AND FASTENERS LOCATED BTW BS500 TO BS500A AT LEVEL OF STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 37 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB AND FASTENERS LOCATED BTW BS500 TO BS500A AT LEVEL OF STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 37 REV -. SEE INDIVIDUAL SIGN OFF BELOW.

Part: RIB — CRACKED (ZONE 300) · airframe 59,090 hrs · 39,530 cycles

CRACK LEADING EDGE RIB LOCATED LE STA 95.96 AT LT HORIZONTAL STABILIZER 2025-93380<[01] REPLACED CHORD OF THE RIB LOCATED LE STA 95.96 AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02;DWG 186A1303 SHEET 1 REV - AND DWG 186A1001 SHEET 10 REV A. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED CHORD OF THE RIB LOCATED LE STA 95.96 AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02;DWG 186A1303 SHEET 1 REV - AND DWG 186A1001 SHEET 10 REV A. SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT — CORRODED (ZONE 100) · airframe 59,090 hrs · 39,530 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS727B TO BS747 RBL22 WL156.5 AFT CARGO COMPARTMENT 2025-93368<[01] EQUIPMENT P/N 45MG; S/N 130061901; DUE DATE 12-JUN-25 WAS USED ON STEP 3;[02] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BTW BS727 TO BS767 RBL22 WL156.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A7500 SHEET 85 REV A; DWG 146A7502 SHEET 26 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BTW BS727 TO BS767 RBL22 WL156.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A7500 SHEET 85 REV A; DWG 146A7502 SHEET 26 REV-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 59,090 hrs · 39,530 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS727B TO BS807 LBL22 WL156.5 AFT CARGO COMPARTMENT 2025-93369<[01] EQUIPMENT P/N 45MG; S/N 130061901; DUE DATE 12-JUN-25 WAS USED ON STEP 3;[02] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS 847 LBL22 WL156.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9;SRM 53-00-53-2R-6 REPAIR 6; SRM 51-40-02 DWG 146A7500 SHEET 85 REV A AND DWG 146A7502 SHEET 27 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CERTIFIED CORRECTIVE ACTION 2; COMPLETED RII.

Part: ANGLE — CRACKED (ZONE 100) · airframe 59,090 hrs · 39,530 cycles

CRACK ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R AFT CARGO COMPARTMENT 2025-93374<[01] NSTALLED ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R AFT CARGO COMPARTMENT IAW. B737-700 SRM 51-40-02-0G AND DWG 147A7221 SHEET 17 REV D. SEE INDIVIDUAL SING-OFF BELOW.;[02] CORRECTED STEP 1<BR>NSTALLED ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R AFT CARGO COMPARTMENT IAW. B737-700 SRM 51-40-02-0G AND DWG 147A7221 SHEET 17 REV D. SEE INDIVIDUAL SIGN-OFF BELOW.;[03] REPLACED ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R AFT CARGO COMPARTMENT IAW. B737-700 SRM 51-40-02-0G AND DWG 147A7221 SHEET 17 REV D. SEE INDIVIDUAL SIGN-OFF BELOW.;[04] TASK COMPLETED; SEE INDIVIDUAL SIGN-OFF BELOW

Part: RIB — CRACKED (ZONE 300) · airframe 59,090 hrs · 39,530 cycles

CRACK LEADING EDGE RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER 2025-93381<[01] REPLACED CHORD OF THE RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02; DWG 186A1304 SHEET 1 REV - AND DWG 186A1001 SHEET 10 REV A. SEE INDIVIDUAL SIGN OFF BELOW<BR>01 - REMOVED AND REPLACED PER [SRM 51-10-02-0G-0-A00248 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)]<BR>01 - REMOVED AND REPLACED PER [SRM 51-10-02-0G-0-A00248 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)];[02] CORRECTED STEP 1<BR>REPLACED CHORD OF THE RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02; DWG 186A1304 SHEET 1 REV - AND DWG 186A1001 SHEET 10 REV A. SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED CHORD OF THE RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02; DWG 186A1304 SHEET 1 REV - AND DWG 186A1001 SHEET 10 REV A. SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 59,090 hrs · 39,530 cycles

CRACK ANGLE - SUPPORT LOCATED BTW BS807 TO BS827 AND LBL53 UPPER AREA AT AFT CARGO COMPARTMENT 2025-93367 <[01]. REPLACED ANGLE - SUPPORT LOCATED BTW BS727E TO BS847 AND LBL53 UPPER AREA AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG 149A9490; SHEET:21; REV:-; DWG:149A9491; SHEET:37; REV: - SEE INDIVIDUAL SIGNS OFF BELOW.; [02] CERTIFIED WORK PERFORMED. SEE INDIVIDUAL SIGN OFF BELOW.

Part: STRINGER — CRACKED (ZONE 100) · airframe 59,090 hrs · 39,530 cycles

CRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT 2025-93339<[01] STEP 2. ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 130066401 AND DUE DATE: 21-OCT-25.;[02] TOOL USED STEP 6: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 28 MAY 25.;[03] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 28-JAN-26. TEMPERATURE CONTROLLER: P/N: P3015GOES00000 S/N: 142811019 DUE DATE: 28-JAN-26.;[04] PERFORMED PERMANENT REPAIR STRINGER 26L LOCATED BS500D TO BS 540 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW;[05] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 59,090 hrs · 39,530 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS500 TO BS500D LBL21 AND WL156 FWD CARGO COMPARTMENT 2025-93324<[01] EQUIPMENT P/N 45MG; S/N 130061901; DUE DATE 12-JUN-25 WAS USED ON STEP 3.;[02] INSTALLED SUPPORT ZEE LOCATED BTW TO BS400 TO BS 500D LBL 21 WL156 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG 143A7500 ;REV: - DWG 143A7505 REV D SRM 53-00-53-2R-6 REPAIR 6 SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2 <BR>REPLACED SUPPORT ZEE LOCATED BTW TO BS400 TO BS 500D LBL 21 WL156 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG 143A7500 ;REV: - DWG 143A7505 REV D SRM 53-00-53-2R-6 REPAIR 6 SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPLACED SUPPORT ZEE LOCATED BTW TO BS400 TO BS 500D LBL 21 WL156 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG 143A7500 ;REV: - DWG 143A7505 REV D SRM 53-00-53-2R-6 REPAIR 6 SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 59,090 hrs · 39,530 cycles

CRACK ANGLE - CLIP LOCATED BS 500C AT LEVEL STR26L FWD FACE AT FWD CARGO COMPARTMENT 2025-93322 <[01]. REPLACED ANGLE - CLIP LOCATED BS 500C AT LEVEL STR26L FWD FACE AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 5 REV B. SEE INDIVIDUAL SIGN OFF BELOW.; [02] REPLACED ANGLE - CLIP LOCATED BS 500C AT LEVEL STR26L FWD FACE AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 5 REV B. SEE INDIVIDUAL SIGN OFF BELOW.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 59,090 hrs · 39,530 cycles

CORROSION WEB - INTERCOSTAL LOCATED BS 492.4 TO BS 500A AT LEVEL STR26R FWD CARGO COMPARTMENT 2025-93323 <[01]. REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BS 492.4 TO BS 500A AT LEVEL STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A0080 SHEET 19 REV -. SEE INDIVIDUAL SIGN OFF BELOW.; [02] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 59,090 hrs · 39,530 cycles

CRACK ANGLE - CLIP LOCATED BS 500B AT LEVEL STR26L FWD FACE AT FWD CARGO COMPARTMENT 2025-93321<[01] REPLACED ANGLE CLIP AND FASTENERS LOCATED BS 500B AT LEVEL STR26L FWD FACE AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ;SRM 51-40-02 AND DWG 143A7505 SHEET 5 REV B SEE INDIVUAL SING OFF BELOW;[02] REPLACED ANGLE CLIP AND FASTENERS LOCATED BS 500B AT LEVEL STR26L FWD FACE AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ;SRM 51-40-02 AND DWG 143A7505 SHEET 5 REV B SEE INDIVUAL SING OFF BELOW

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 59,090 hrs · 39,530 cycles

CRACK PLATE LOCATED BS 540 AT LEVEL BL 0 AT PASSENGER CABIN 2025-93320<[01] REPLACED BREAK ASSY AND FASTENERS LOCATED BS 540 AT LEVEL BL 0 TO RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 36 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] JOB COMPLETED; SEE INDIVIDUAL SIN OFF BELOW.

Part: ACCESS PANEL — CRACKED (ZONE 100) · airframe 59,090 hrs · 39,530 cycles

CRACK ACCESS PANEL 191D AT LOWER FUSELAGE 2025-93279<[01] REPAIRED ACCESS PANEL 191D AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-2 REPAIR 2. REFER TO INDIVIDUALS SIGNOFFS BELOW.;[02] TASK COMPLETED

Part: SKIN — DEBONDED (ZONE 600 FLAP) · airframe 59,090 hrs · 39,530 cycles

CUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT RT WING 2025-93281<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189443; DUE DATE: 06/MAR/25.;[02] TOOL USED ON STEP 4 ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 15-OCT-25;[03] TOOL USED; HOT BONDER PN: HCS9200B-AV; SN: 18196021; DUE DATE: 15/FEB/25; CALIPER PN: 500-196-30; SN: A22352364; DUE DATE: 29/AUG/25.;[04] STEP 20. ULTRASONIC EQUIPMENT USED P/N: EPOCH 650; S/N: 201036102 AND DUE DATE: 25-OCT-25.;[05] REPAIRED OB AFT FLAP ON IB SIDE AT RT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. REFER TO INDIVIDUALS SIGNOFFS BELOW.;[06] REPAIRED OB AFT FLAP ON IB SIDE AT RT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. REFER TO INDIVIDUALS SIGNOFFS BELOW.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 59,090 hrs · 39,530 cycles

INOP BATTERY PACK EMERGENCY EXIT LIGHT ON LOWERED CEILING LT SIDE AT AFT GALLEY AREA 2025-93184<[01] REPLACED BATTERY PACK EMERGENCY EXIT LIGHT ON LOWERED CEILING LT SIDE AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06-960-805 TEST IS OK;[02] CERTIFIED WORK PERFORMED; TEST OK

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 59,090 hrs · 39,530 cycles

INOP BATTERY PACK EMERGENCY EXIT LIGHT ON LOWERED CEILING RT SIDE AT AFT GALLEY AREA 2025-93185<[01] REPLACED BATTERY PACK EMERGENCY EXIT LIGHT ON LOWERED CEILING RT SIDE AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06-960-805 TEST IS OK;[02] CERTIFIED WORK PERFORMED; TEST OK

Part: INDICATOR — DETERIORATED (ZONE 200) · airframe 59,090 hrs · 39,530 cycles

DETERIORATED EMERGENCY EXIT INDICATOR ASSY ON SIDEWALL PANEL 232YHW AT PASSENGER CABIN 2025-93166 <[01]. INSTALLED EMERGENCY EXIT INDICATOR ASSY ON SIDEWALL PANEL 232YHW AT PASSENGER CABIN IAW B737-700 AMM 33-51-01-960-802 PERFORMED OPERATIONAL TEST IS OK; [02] INSTALLED EMERGENCY EXIT INDICATOR ASSY ON SIDEWALL PANEL 232YHW AT PASSENGER CABIN IAW B737-700 AMM 33-51-01-960-802 PERFORMED OPERATIONAL TEST IS OK.

Part: NUT — DETERIORATED (ZONE 800) · airframe 59,090 hrs · 39,530 cycles

DETERIORATED ENTRY DOOR LINING ASSIST HANDLE NUT UPPER AND LOWER POSITION AT FWD GALLEY AREA (4 EA) 2025-93122<[01] REPLACED ENTRY DOOR LINING ASSIST HANDLE NUT UPPER AND LOWER POSITION AT FWD GALLEY AREA (4 EA) IAW B737-700 AMM 52-11-31-400-802 STEP 3G. ITEM (2) (A);[02] REPLACED ENTRY DOOR LINING ASSIST HANDLE NUT UPPER AND LOWER POSITION AT FWD GALLEY AREA (4 EA) IAW B737-700 AMM 52-11-31-400-802 STEP 3G. ITEM (2) (A)

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 59,090 hrs · 39,530 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2025-93118 <[01]. TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N: B23399190; DUE DATE: 04 / MAR / 25.; [02] TOOL USED IN STEP 4: RADIOMETER PHOTOMETER KIT P/N: XRP-3000 S/N: 1753759 DUE DATE: 30-JUN-25;[03] REPAIRED BY WELDING FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.; [04] REPAIRED BY WELDING FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 58,182 hrs · 38,949 cycles

FA REPORTS FWD ENTRY GIRT BAR OUT OF ADJUSTMENT<[01] ADJ FWD EXIT DOOR EVAC SLIDE GIRT BAR BRACKET PER AMM 25-66-00

Part: LIGHT — CONTAMINATED (ROW 1) · airframe 57,340 hrs · 38,409 cycles

ROW 1 AISLE PHOTOLUMINESCENT STRIPS MOISTURE PRESENT.<[01] R&R ROW 1 AISLE PHOTOLUMINESCENT FLOOR STRIPS IAW AMM 25-00-00.

Part: SHUTOFF VALVE — FAILED (ZN 500 LEFT WING) · airframe 56,829 hrs · 38,115 cycles

LEFT WING SHUT OFF VALVE INOP<[01] CLEANED AND RESET S/O VLV OVERIDE SW AND FUELING VALVES OPS NORMAL IAW AMM 28-21-51. A/C O K FOR SERVICE.

Part: FLAP — DEBONDED (ZN 500 LEFT WING) · airframe 53,635 hrs · 36,075 cycles

LT WING O/B AFT FLAP I/B END UPPER SURFACE REPAIR DISBONDED AND MISSING<[01] REMOVED AND REPLACED AFT FLAP WITH NEW WORK PERFORMED IAW AMM 27-51-22;[02] ENTERED IN ERROR <BR>REMOVED AND REPLACED L/H AFT FLAP WITH NEW WORK PERFORMED IAW AMM 27-51-22

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 53,322 hrs · 35,875 cycles

CRACK ANGLE - SUPPORT LOCATED BS807 AT LEVEL STR26R AND RBL36 AT AFT CARGO COMPARTMENT 2023-116991<[01] REPLACED ANGLE - SUPPORT LOCATED BS807 AT LEVEL STR26R AND RBL36 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; DWG 146A8120 SHEET 31 REV- AND DWG 146A0081 SHEET 25 REV A. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

CRACK FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN AT PASSENGER CABIN 2023-116967<[01] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 38 REV. A. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 38 REV. A. RII;SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

CRACK FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13.24 AT PASSENGER CABIN 2023-116968<[01] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13.24 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 6 REV-. SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13.24 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 6 REV-. RII;SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

CRACK FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 RBL 8.283 AT PASSENGER CABIN 2023-116966<[01] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 RBL 8.283 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 6 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 RBL 8.283 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 6 REV-.<BR>RII ACCOMPLISHED <BR> SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 53,322 hrs · 35,875 cycles

CORROSION ANGLE - SUPPORT LOCATED BS947.5 AND BETWEEN STR27L TO STR25R AND WL 162 AT AFT CARGO COMPARTMENT 2023-116959<[01] REPLACED ANGLE - SUPPORT LOCATED BS947.5 AND BETWEEN STR27L TO STR25R AND WL 162 AT AFT CARGO COMPARTMENT AND FASTENER IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. IAW DWG 149A8117 SHEET 6 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE - SUPPORT LOCATED BS947.5 AND BETWEEN STR27L TO STR25R AND WL 162 AT AFT CARGO COMPARTMENT AND FASTENER IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. IAW DWG 149A8117 SHEET 6 REV-. SEE INDIVIDUAL SIGN OFF BELOW. RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 53,322 hrs · 35,875 cycles

CRACK ANGLE - CLIP LOCATED BS 480 FWD FACE STR 26L AT FWD CARGO COMPARTMENT 2023-116961<[01] REPLACED ANGLE - CLIP LOCATED BS 480 FWD FACE STR 26L AT FWD CARGO COMPARTMENT AND FASTENER IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG143A1220 SHEET 30 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK CARD COMPLETED <BR>SEE INDIVIDUAL SIGN OFFS BELOW <BR>RII

Part: INTERCOSTAL — CORRODED (ZN 100 FUS LOWER) · airframe 53,322 hrs · 35,875 cycles

CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS767 TO BS792AT LEVEL STR26R AND WL 154 AFT CARGO COMPARTMENT 2023-116957<[01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS767 TO BS792AT LEVEL STR26R AND WL 154 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG 146A0081 REV: A. SEE INDIVIDUAL SIGNOFFS BELLOW;[02] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS767 TO BS792AT LEVEL STR26R AND WL 154 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG 146A0081 REV: A. SEE INDIVIDUAL SIGNOFFS BELLOW AS RII

Part: BRACKET — CRACKED (ZN 400 NACELLE/P) · airframe 53,322 hrs · 35,875 cycles

CRACK ON BRACKET LOCATED ON OUTBOARD SIDE RT PYLON TRUST REVERSER AREA AT ENGINE 2 2023-116946<[01] REPLACED BRACKET LOCATED ON OUTBOARD SIDE RT PYLON TRUST REVERSER AREA AT ENGINE 2. IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 311A2683 SHEET 26 REV: -;[02] TASK CARD COMPLETED

Part: GIRT BAR — WORN (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

WEAR ON GIRT BAR FITTING HARDWARE AND PLATE ASSY ADAPTER SERVICE DOOR AT FWD GALLEY AREA 2023-116588<[01] REPLACED GIRT BAR FITTING HARDWARE AND PLATE ASSY ADAPTER SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801;[02] JOB COMPLETE

Part: GIRT BAR — WORN (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

WEAR ON GIRT BAR FITTING HARDWARE AND PLATE ASSY ADAPTER ENTRY DOOR AT FWD GALLEY AREA 2023-116583<[01] REPLACED GIRT BAR FITTING HARDWARE AND PLATE ASSY ADAPTER ENTRY DOOR AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801;[02] JOB COMPLETE

Part: DOUBLER — CRACKED (ZN 100 FUS LOWER) · airframe 53,322 hrs · 35,875 cycles

CRACK ON CUTOUT SURROUND DOUBLER OF ELECTRICAL GROUND POWER RECEPTACLE OF ACCESS PANEL 114AR 2023-116893<[01] TOOL USED EDDY CURRENT EQUIPMENT PN NORTEC 500D; SN: N500X12101V022237; 26 JAN 24.;[02] PERFORMED REPAIR ON LOWER HORIZONTAL RUBBING BLOCK AREA OF CUT OUT SURROUND DOUBLER OF ELECTRICAL GROUND POWER RECEPTACLE OF ACCESS PANEL 114AR IAW SRM B737-700 53-10-15-2R-4 REPAIR 4; ZONE 2 ; FIGURE 204; SHEET 1. SEE INDIVIDUAL SIGN OFF BELOW;[03] PERFORMED REPAIR ON LOWER HORIZONTAL RUBBING BLOCK AREA OF CUT OUT SURROUND DOUBLER OF ELECTRICAL GROUND POWER RECEPTACLE OF ACCESS PANEL 114AR IAW SRM B737-700 53-10-15-2R-4 REPAIR 4; ZONE 2 ; FIGURE 204; SHEET 1. SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2023-116859<[01] REPLACED SUPPORT ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG#146A7901 SHEET: 20; REV - SEE INDIVIDUALS SIGN OFF BELOW;[02] REPLACED SUPPORT ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG#146A7901 SHEET: 20; REV - SEE INDIVIDUALS SIGN OFF BELOW<BR>RII

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 53,322 hrs · 35,875 cycles

CRACK ANGLE TRAILING EDGE LOCATED ON ORSS 272 RT WING 2023-116833<[01] REPLACED ANGLE TRAILING EDGE LOCATED ON ORSS 272 RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND B737-700 SRM 51-40-02;[02] TASK COMPLETED

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 53,322 hrs · 35,875 cycles

CRACK ANGLE TRAILING EDGE AREA LOCATED AT LEVEL ORSS261 LT WING 2023-116836<[01] REPLACED ANGLE TRAILING EDGE AREA LOCATED AT LEVEL ORSS261 LT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9; AND B737-700 SRM 51-40-02 AND DRAWING 115A6200 REV: -;[02] TASK COMPLETED

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 53,322 hrs · 35,875 cycles

CRACK CORRUGATED PLATE TRAILING EDGE IRSS 232 RT WING 2023-116797<[01] REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 232 RT WING IAW B737-700 SRM 51-10-02; 51-40-02 AND DRAWING 115A2001 REV A;[02] CORRECTED STEP 1. REPLACED PLATE ASSY LOC. TRAILING EDGE IRSS 232 RT WING IAW B737-700 SRM 51-10-02; 51-40-02 AND DRAWING 115A2001 REV A;[03] ORRECTED STEP 1. REPLACED PLATE ASSY LOC. TRAILING EDGE IRSS 232 RT WING IAW B737-700 SRM 51-10-02; 51-40-02 AND DRAWING 115A2001 REV A

Part: FLASHLIGHT ASSY — BROKEN (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

BROKEN WINDSCREEN LT SIDE BASE FLASH LIGHT AT AFT GALLEY AREA (1 EA) 2023-116779<[01] REPLACED WINDSCREEN LT SIDE BASE FLASH LIGHT AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-200-802 STEP 10.B.(4) AND (6);[02] REPLACED WINDSCREEN LT SIDE BASE FLASH LIGHT AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-200-802 STEP 10.B.(4) AND (6)

Part: TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 53,322 hrs · 35,875 cycles

CRACK TRACK CARGO RBL14 LOCATED BS460 AT FWD CARGO COMPARTMENT 2023-116798<[01] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[02] PERFORMED REPAIR ON CARGO TRACK LOCATED RBL 14 BETWEEN BS396 TO BS500A PLUS 9.5 INCHES AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1; PARAGRAPH 4 FIG 203. AND DWG #143A7500 SHEET: 59 REV-. SEE INDIVIDUAL SIGN OFF BELOW

Part: FLASHLIGHT ASSY — BROKEN (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

BROKEN WINDSCREEN LT SIDE BASE FLASH LIGHT AT AFT GALLEY AREA (1 EA) 2023-116779<[01] REPLACED WINDSCREEN LT SIDE BASE FLASH LIGHT AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-200-802 STEP 10. B (6).;[02] REPLACED WINDSCREEN LT SIDE BASE FLASH LIGHT AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 25-64-00-200-802 STEP 10. B (6). JOB COMPLETED.

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 53,322 hrs · 35,875 cycles

CRACK CORRUGATED PLATE TRAILING EDGE IRSS 215 RT WING 2023-116796<[01] REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 215 RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 29 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] COMPLETED

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 53,322 hrs · 35,875 cycles

CRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 RT WING 2023-116794<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 261 RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] COMPLETE TASK CERTIFIED

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS312 TO BS328 AND LBL45 FWD GALLEY AND LAV 2023-116775<[01] REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 LBL45 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 26 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 LBL45 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 26 REV-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: BEAM — CRACKED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

CRACK FLOOR BEAM LOCATED BS294.5 RBL53 AT FWD GALLEY AREA 2023-116773<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23.;[02] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23.;[03] TOOLS USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE 01 FEB 24; P/N P3015GOES00000 S/N 112820025 DUE DATE 01 FEB 24.;[04] TOOL USED: POWER PACK P/N PE1068 S/N PE0118-94826 DUE DATE: 16-MAY-23. MULTIMETER P/N FLUKE 1587 S/N 38200035 DUE DATE: 15-DEC-23. FLUKE 566 S/N 58210036WS DUE DATE: 10-JAN-24.;[05] REPAIRED FLOOR BEAM LOCATED BS294.5 RBL12 TO RBL60 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16; FIGURE 202 DETAIL G. SEE INDIVIDUAL SIGN OFFS BELOW.;[06] REPAIRED FLOOR BEAM LOCATED BS294.5 RBL12 TO RBL60 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16; FIGURE 202 DETAIL G. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 53,322 hrs · 35,875 cycles

CRACK INTERNAL AREA RT SIDE BODY STA 663.75 AND RBL 9 SUPPORT ANGLE AT AIR CONDITIONING BAY 2023-116758<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE 01 FEB 24.;[02] REPLACED ANGLE INTERNAL AREA RT SIDE BODY STA 663.75 BETWEEN RBL 5.0 TO RBL 65.0 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02; DWG#111A1000 SHEET 160 REV- AND DWG#111A1000 SHEET 162 REV-<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] TASK CARD COMPLETED <BR>REPLACED ANGLE INTERNAL AREA RT SIDE BODY STA 663.75 BETWEEN RBL 5.0 TO RBL 65.0 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02; DWG#111A1000 SHEET 160 REV- AND DWG#111A1000 SHEET 162 REV- <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS344 TO BS360 AND BL0 FWD GALLEY AND LAV 2023-116765<[01] REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS344 TO BS360 BL0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 32 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS344 TO BS360 BL0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 32 REV-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 53,322 hrs · 35,875 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS847 TO BS867 CEILING AREA AFT CARGO COMPARTMENT 2023-116760<[01] REPLACED WEB - INTERCOSTAL (1 E/A) AND FASTENERS LOCATED BETWEEN BS847 TO BS867 CEILING AREA AFT CARGO COMPARTMENT IAW B737- 700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DRAWING # 149A8100 SHEET 1 REV: -;[02] CORRECTED STEP 1: REPLACED WEB - INTERCOSTAL (1 E/A) AND FASTENERS LOCATED BETWEEN BS847 TO BS867 CEILING AREA AFT CARGO COMPARTMENT IAW B737- 700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DRAWING # 149A8100 SHEET 1 REV: - <BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS344 TO BS360 AND LBL11 FWD GALLEY AND LAV 2023-116766<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS344 TO BS360 AND LBL11 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET: 12 REV: B SEE INDIVIDUAL SIGN OF BELOW;[02] CERTIFIED RII <BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS344 TO BS360 AND LBL11 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET: 12 REV: B SEE INDIVIDUAL SIGN OF BELOW

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS277 TO BS294.5 BL0 FWD GALLEY AND LAV 2023-116762<[01] REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 BL0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 20 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 BL0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 20 REV-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 53,322 hrs · 35,875 cycles

CRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 LT WING 2023-116748<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 261 LT WING AND FASTENER IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. AND DWG 15A2711 SHEET 6 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] COMPLETE TASK CERTIFIED

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 53,322 hrs · 35,875 cycles

CRACK CORRUGATED PLATE TRAILING EDGE IRSS 215 LT WING 2023-116749<[01] REPLACED CORRUGATED PLATE AND FASTENERS LOC. TRAILING EDGE IRSS 215 LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02. SEE INDIVIDUAL SIGNOFFS BELLOW.;[02] COMPLETE TASK CERTIFIED

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 53,322 hrs · 35,875 cycles

CRACK CORRUGATED PLATE TRAILING EDGE IRSS 232 AT LT WING 2023-116750<[01] REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 232 AT LT WING IAW B737-700 SRM 51-10-02; 51-40-02 AND DRAWING 115A2001 REV A;[02] CORRECTED STEP 1; REPLACED PLATE ASSY TRAILING EDGE IRSS 232 AT LT WING IAW B737-700 SRM 51-10-02; 51-40-02 AND DRAWING 115A2001 REV A;[03] CORRECTED STEP 1; REPLACED PLATE ASSY TRAILING EDGE IRSS 232 AT LT WING IAW B737-700 SRM 51-10-02; 51-40-02 AND DRAWING 115A2001 REV A

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 53,322 hrs · 35,875 cycles

CRACK ANGLE TRAILING EDGE DEFLECTION CONTEO RIB ORSS 272 LT WING 2023-116744<[01] REPLACED ANGLE AND FASTENERS TRAILING EDGE DEFLECTION CONTEO RIB ORSS 272 LT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND B737-700 SRM 51-40-02;[02] TASK COMPLETED

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 53,322 hrs · 35,875 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS312 TO BS328 AND RBL30 FWD GALLEY AND LAV 2023-116763<[01] REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 RBL30 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 26 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB- INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 RBL30 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 26 REV-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: BEAM — CORRODED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

CORROSION LOCATED ON FLOOR BEAM 986.5 RBL35 AND WL208.1 AT AFT GALLEY AREA 2023-116701<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N:45MG; S/N:221859911 DUE DATE: 07-NOV-23.;[02] REPAIRED FLOOR BEAM 986.5 RBL35 AND WL208.1 AT AFT GALLEY AREA IAW EA M-21-153-00612 SEE INDIVIDUALS SIGN OFF BELOW;[03] REPAIRED FLOOR BEAM 986.5 RBL35 AND WL208.1 AT AFT GALLEY AREA IAW EA M-21-153-00612 SEE INDIVIDUALS SIGN OFF BELOW

Part: BEAM — CORRODED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

CORROSION LOCATED ON FLOOR BEAM 986.5 RBL43 AND WL208.1 AT AFT GALLEY AREA 2023-116705<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N:45MG; S/N:221859911 DUE DATE: 07-NOV-23.;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[03] PERFORMED REPAIR ON FLOOR BEAM 986.5 RBL43 AND WL208.1 AT AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6 FIGURE 205 ALTERNATIVE 4 SEE IN INDIVIDUAL SIGN OFF BELOW.;[04] CORRECTED STEP 3 PERFORMED REPAIR ON FLOOR BEAM 986.5 RBL43 AND WL208.1 AT AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6 FIGURE 205 ALTERNATIVE 4 SEE INDIVIDUAL SIGN OFF BELOW.;[05] CORRECTED STEP 4 PERFORMED REPAIR ON FLOOR BEAM 986.5 RBL43 AND RBL39 WL208.1 AT AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6 FIGURE 205 ALTERNATIVE 4 SEE INDIVIDUAL SIGN OFF BELOW.;[06] PERFORMED REPAIR ON FLOOR BEAM 986.5 RBL43 AND RBL39 WL208.1 AT AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6 FIGURE 205 ALTERNATIVE 4 SEE INDIVIDUAL SIGN OFF BELOW. (RII ITEM)

Part: HANDLE — BROKEN (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

BROKEN SERVICE DOOR ASSIST HANDLE NUT AT AFT GALLEY AREA (2 EA) 2023-116716<[01] FAULT RAISED IN ERROR DUE TO THIS MT IS DUPLICATED WITH TTG8Q00HQ3UK.;[02] FAULT RESOLVED ON OTHER FAULT AND IS BEING CLOSED.

Part: BEAM — CORRODED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

CORROSION LOCATED ON FLOOR BEAM 986.5 LBL43 AND WL208.1 AT AFT GALLEY AREA 2023-116709<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N:45MG; S/N:221859911 DUE DATE: 07-NOV-23.;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[03] REPAIRED FLOOR BEAM 986.5 LBL43 AND WL208.1 AT AFT GALLEY AREAB737-700 SRM 53-70-51-2R-6 REPAIR 6 FIGURE 204 ALTERNATIVE 3 SEE INDIVIDUALS SIGN OFF BELOW;[04] CORRECTED STEP 3; REPAIRED FLOOR BEAM 986.5 LBL43 AND WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 FIGURE 204 ALTERNATIVE 3 SEE INDIVIDUALS SIGN OFF BELOW;[05] CERTIFIED STEP 4; COMPLETED <BR>ITEM RII

Part: BEAM — CORRODED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

CORROSION LOCATED ON FLOOR BEAM 986.5 RBL39 AND WL208.1 AT AFT GALLEY AREA 2023-116703<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N:45MG; S/N:221859911 DUE DATE: 07-NOV-23.;[02] REPAIRED FLOOR BEAM LOCATED ON BS 986.5 RBL39 AND WL208.1 AT AFT GALLEY AREA AND ALL STEPS ARE DOCUMENTED ON FAULT TTG8Q00HS19H SEE INDIVIDUAL SIGN OFF BELOW;[03] REPAIRED FLOOR BEAM LOCATED ON BS 986.5 RBL39 AND WL208.1 AT AFT GALLEY AREA AND ALL STEPS ARE DOCUMENTED ON FAULT TTG8Q00HS19H SEE INDIVIDUAL SIGN OFF BELOW (RII ITEM)

Part: STRAP — MISSING (ZN 100 FUS LOWER) · airframe 53,322 hrs · 35,875 cycles

MISSING STRAP FLOOR PANEL 140AF AT BS727 AND BETWEEN LBL 33.5 AND RBL 33.5 AT AFT CARGO COMPARTMENT 2023-116622<[01] INSTALLED STRAP LOCATED ON FLOOR PANEL 140AF AT BS727 AND BETWEEN LBL 33.5 AND RBL 33.5 AT AFT CARGO COMPARTMENT OAW B837-700 SRM 51-40-02;[02] TASK CARD COMPLETED

Part: SKIN — CRACKED (ZN 300 STABILIZE) · airframe 53,322 hrs · 35,875 cycles

CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.600 INCH. APPROX. 2023-116679<[01] TOOL USED PN:NORTEC 600D;PN:200053402;DUE DATE:13-MAY-23;[02] REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED BTW STAB STA184.70 TO STAB STA 203.10 AND BTW 12 INCH. FROM FRONT SPAR TO 23 INCH. FROM FRONT SPAR IAW SRM B737-700 55-10-01-2R-11 REPAIR 11; FIGURE 204; DETAIL B SEE INDIVIDUAL SIGN OFFS BELLOW;[03] REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED BTW STAB STA184.70 TO STAB STA 203.10 AND BTW 12 INCH. FROM FRONT SPAR TO 23 INCH. FROM FRONT SPAR IAW SRM B737-700 55-10-01-2R-11 REPAIR 11; FIGURE 204; DETAIL B SEE INDIVIDUAL SIGN OFFS BELLOW<BR>CERTIFIED AS RII

Part: GIRT BAR — WORN (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

WEAR ON GIRT BAR FITTING HARDWARE AND PLATE ASSY ADAPTER AFT ENTRY DOOR SIDE AT AFT GALLEY AREA 2023-116544<[01] REPLACED GIRT BAR FITTING HARDWARE AND PLATE ASSY ADAPTER AFT ENTRY DOOR SIDE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801;[02] TASK CARD COMPLETED

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

DOES NOT PASS THE OPERATIONAL TEST ON BATTERY PACK RH SIDE LOCATED ON LOWERED CEILING PANEL FWD AREA GALLEY 2023-116593<[01] REPLACED BATTERY PACK RH SIDE LOCATED ON LOWERED CEILING PANEL FWD AREA GALLEY I.A.W B737-700 AMM 33-51-06-960-805 TEST IS OK;[02] STEP 1 VERIFIED AND CORRECTIVE ACTION COMPLETED: <BR>REPLACED BATTERY PACK RH SIDE LOCATED ON LOWERED CEILING PANEL FWD AREA GALLEY I.A.W B737-700 AMM 33-51-06-960-805 TEST IS OK

Part: GIRT BAR — WORN (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

WEAR ON GIRT BAR FITTING HARDWARE AND PLATE ASSY ADAPTER AFT SERVICE DOOR SIDE AT AFT GALLEY AREA AT AFT GALLEY AREA 2023-116547<[01] REPLACED GIRT BAR FITTING HARDWARE AND PLATE ASSY ADAPTER AFT SERVICE DOOR SIDE AT AFT GALLEY AREA AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 STEP 3. D (1) (E) UP TO (J).;[02] CORRECTED STEP 1 <BR>REPLACED GIRT BAR FITTING HARDWARE AND PLATE ASSY ADAPTER AFT SERVICE DOOR SIDE AT AFT GALLEY AREA AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801;[03] TASK CARD COMPLETED

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 53,322 hrs · 35,875 cycles

DOES NOT PASS THE OPERATIONAL TEST ON BATTERY PACK LH SIDE LOCATED ON LOWERED CEILING PANEL FWD AREA GALLEY 2023-116589<[01] DOESED PASS THE OPERATIONAL TEST ON BATTERY PACK LH SIDE LOCATED ON LOWERED CEILING PANEL FWD AREA GALLEY I.A.W B737-700 AMM-33-51-06-960-805;[02] CORRECTED STEP 1 REPLACED BATTERY PACK LH SIDE LOCATED ON LOWERED CEILING PANEL FWD AREA GALLEY I.A.W B737-700 AMM-33-51-06-960-805 TEST IS OK;[03] STEP 2 VERIFIED AND CORRECTIVE ACTION COMPLETED: <BR>REPLACED BATTERY PACK LH SIDE LOCATED ON LOWERED CEILING PANEL FWD AREA GALLEY I.A.W B737-700 AMM-33-51-06-960-805 TEST IS OK .

Part: PANEL — ELONGATED (ZN 100 FUS LOWER) · airframe 53,322 hrs · 35,875 cycles

ELONGATED HOLE BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT 2023-116410<[01] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW:B737-700 AMM 25-52-01-201-801 AND DWG 453A2510 SHEET 8 REV A MATERIAL USED: CONOLITE P/N: BMS8-2TY45CL3GRA PO: 2022 229085;[02] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW:B737-700 AMM 25-52-01-201-801 AND DWG 453A2510 SHEET 8 REV A MATERIAL USED: CONOLITE P/N: BMS8-2TY45CL3GRA PO: 2022 229085

Part: PANEL — ELONGATED (ZN 100 FUS LOWER) · airframe 53,322 hrs · 35,875 cycles

ELONGATED HOLE BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT 2023-116414<[01] FABRICATED BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT FROM MATERIAL CONOLITE PN: BMS 8-2TY45CL3GRA; PO: 2022 229085 IAW B737-700 AMM 25-52-01-201-801; DWG# 453A2510 REV. A.;[02] FABRICATED BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT FROM MATERIAL CONOLITE PN: BMS 8-2TY45CL3GRA; PO: 2022 229085 IAW B737-700 AMM 25-52-01-201-801; DWG# 453A2510 REV. A.

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 53,322 hrs · 35,875 cycles

CRACK FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT 2023-116397<[01] FABRICATED NEW FLOOR PANEL 140AF LOCATED AT AFT CARGO COMPARTMENT FROM MATERIAL CONOLITE SHEET 0.090? P/N A90RG1W 48144 P/O 2022 229089 IAW B737-700 AMM 25-52-01-201-801 AND DWG: 453A2610 SHEET: 8 REV: D;[02] FABRICATED NEW FLOOR PANEL 140AF LOCATED AT AFT CARGO COMPARTMENT FROM MATERIAL CONOLITE SHEET 0.090? P/N A90RG1W 48144 P/O 2022 229089 IAW B737-700 AMM 25-52-01-201-801 AND DWG: 453A2610 SHEET: 8 REV: D

Part: GIRT BAR — OUT OF ADJUST (FWD SERVICE DOOR) · airframe 53,114 hrs · 35,743 cycles

FWD SERVICE DOOR SLIDE GURT BAR STUCK IN WINDSCREEN.<[01] REPACKED FWD SERVICE DOOR SLIDE PER AMM 25-66-01.

Part: LIGHT — INOPERATIVE (ROW 11) · airframe 52,734 hrs · 35,477 cycles

RIGHT SIDEWALL LIGHT INOP AT ROW 11. RELAMPED R/H ROW 11 WINDOW LIGHT IAW AMM 33-21-00. OPS CHECK GOOD. RELAMPED BLUE F/A CALL LIGHT UNDER AFT EXIT SIGN PER AMM 33-27-00 OPS CHECK GOOD CLEARS MEL

Part: MEGAPHONE — BROKEN (FWD CABIN) · airframe 52,719 hrs · 35,465 cycles

FWD MEGAPHONE HANDLE BROKEN. / [01] REMOVED AND REPLACED MEGAPHONE. REF AMM 25-64-00

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 52,486 hrs · 35,304 cycles

FWD CARGO DOOR CENTER SCUFF PLATE IS CRACKED AT OUTER EDGE 3' AFT OF FWD EDGE OF OF PLATE IN DENTED AREA. HFEC VERIFIED PER NDT PART 6; 51-00-00 PROC. 14 AND FPI PER SOPM 20-20-02. DURING ACCOMPLISHMENT 53-30-15-1A-2-A00074-INSP (DENTS - HFEC INSPECTION) - FWD CARGO CENTER SCUFF PLATE OUTER EDGE 3&AMP;#34; AFT OF FWD EDGE OF PLATE FOUND AREA TO BE CRACKED. / [01] REMOVED AND REPLACED FWD CARGO DOOR CENTER SCUFF PLATE PER AMM 53-11-02.

Part: NONE — INOPERATIVE · airframe 52,325 hrs · 35,202 cycles

LH OVERWING EXIT SIDEWALL LIGHT INOPERATIVE. REPLACED BULB PER SIP OPS CHECK OK.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 52,210 hrs · 35,122 cycles

AFT LEFT DOOR ESCAPE SLIDE HAS A WIRE HANGING DOWN. / [01] STOWED SLIDE PACK CHARGING CABLE BACK IN PLACE REF AMM 25-66-01

Part: FLAP — DELAMINATED (R/H WING) · airframe 51,677 hrs · 34,766 cycles

RH OB AFT FLAP PREVIOUS REPAIR DELAM- REQUIRES R/R / [01] REMOVED AND REPLACED THE RH OB AFT FLAP PER AMM 27-51-21.;[02] C/W RII

Part: FLAP — PEELING (R/H WING) · airframe 51,675 hrs · 34,764 cycles

METAL PEELING UP ON RIGHT OUTBOARD AFT FLAP. / [01] INSPECTED AREA OF DAMAGE ON RH O/B AFT FLAP INBOARD END. DAMAGE MEASURED 8? BY 12?. C/W EA 22-157-02190. REINSPECT EACH CYCLE; PERMANENT REPAIR REQUIRED WITHIN 5 CYCLES.

Part: CHARGER — FAILED (CABIN) · airframe 51,414 hrs · 34,591 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M164; M1670; M1672 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M164 M1670 M1672 / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT LOCATIONS M1672; M1670; AND M1674 CHANGED CHARGER PACK ASSY. PER AMM 33-51-06;[02] CHANGED CHARGER PACK ASSY. @ LOCATION M1674 OPS CHECK GOOD. PER AMM 33-51-06

Part: LIGHT — CRACKED · airframe 51,414 hrs · 34,591 cycles

R/H OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. / [01] REMOVED AND REPLACED LENS PER AMM 33-51-04;[02] ADDED PART INFO

Part: BATTERY — FAILED (CABIN) · airframe 51,414 hrs · 34,591 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M164; M1670; M1672 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M164 M1670 M1672 / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT LOCATIONS M1672; M1670; AND M1674 CHANGED CHARGER PACK ASSY. PER AMM 33-51-06;[02] CHANGED CHARGER PACK ASSY. @ LOCATION M1674 OPS CHECK GOOD. PER AMM 33-51-06

Part: NONE — INOPERATIVE (FWD SERVICE DOOR) · airframe 50,998 hrs · 34,314 cycles

FWD SERVICE DOOR EMERGENCY LTS INOP / [01] R&R FWD SERVICE DOOR EMER BATTERY PER AMM 33-51-06

Part: BRACKET — CRACKED (L/H WING) · airframe 50,863 hrs · 34,230 cycles

L/H WING UPPER PANEL SUPPORT FORWARD 'Z' ANGLE IS CRACKED / [01] R&R L/H WING UPPER PANEL SUPPORT FORWARD 'Z' ANGLE BRACKET IN REF TO SRM 51-40-02. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,834 hrs · 33,615 cycles

LAST 2 FEET OF PHOTOLUMINESCENT FLOOR LIGHTING ON AIRCRAFT LEFT INOP ; / [01] REPLACED LAST 2 FEET OF PHOTOLUMINESCENT FLOOR LIGHT ON AIRCRAFT LEFT SIDE IAW AMM 33-51-15. OPS CHK GOOD

Part: PANEL — ELONGATED (FUSELAGE) · airframe 49,783 hrs · 33,586 cycles

SUPPLEMENTAL INFORMATION: AFT WING-TO-BODY FAIRING PANEL 194E FASTENER HOLES ELONGATED. ; / [01] FABRICATED AND PAINTED NEW PANEL PER EA 5351-I-14642-NG AND AMM 53-51-21; [02] REMOVED &REPLACE PANEL PER AMM 53-51-21

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 49,783 hrs · 33,586 cycles

CENTER WHEEL WELL PANEL 193D DELAMINATED AND HOLES ELONGATED. ; / [01] FABRICATED AND PAINTED NEW 193D PANEL IAW AD 5351-I-14642-NG AND 53-51-21; [02] REMOVED & REPLACE PANEL PER AMM 53-51-21

Part: SKIN — CRACKED (EXT POWER DOOR) · airframe 48,490 hrs · 32,810 cycles

EXTERNAL POWER DOOR CUTOUT HAS A CRACK ON AFT LIP ; / [01] REINSTALLED REPAIR DOUBLER PER SRM 51-40-02

Part: ACTUATOR — FAULTY (CENTER WING) · airframe 47,538 hrs · 32,277 cycles

FUEL CROSSFEED VALVE WILL NOT CLOSE / R&R ENGINE FUEL CROSSFEED VALVE ACTUATOR PER AMM 28-22-00 RAR #92675 POS CROSSFEED P/N OFF MA30A100 S/N OFF AA145413D P/N ON MA30A1017 S/N ON AA767365

Part: STRINGER — CRACKED (FWD CARGO COMPT) · airframe 47,393 hrs · 32,204 cycles

CRACK STRINGER 26R LOCATED BS540 FWD CARGO COMPARTMENT REPAIRED STRINGER 26R LOCATED BS 500D TO BS 540 FWD CARGO COMPARTMENT I.A.W B73700 SRM 5300032R1 RAPAIR 1 MATERIAL USED PN:7075-0 P.O:2020-203305 PN:7075 TO P.O:2020-172955.

Part: FRAME — DENTED (FUSELAGE) · airframe 47,393 hrs · 32,204 cycles

DENT FRAME LOCATED BS460 AT LEVEL STRINGER 26L AT FWD CARGO COMPARTMENT / REPAIRED FRAME LOC AT BS 460 BTW STR 25L TO 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-30-07-2R-1 REPAIR 1 MATERIAL USED PN ALUMINIUM SHEET 7075-T6 0.063' 2020-206794 FOR INSPECTION REQUIREMENTS SEE TLD #T080528

Part: CARGO TRACK — CRACKED (AFT CARGO COMPT) · airframe 47,393 hrs · 32,204 cycles

CRACK TRACK RBBL 13.84 LOCATED BS727E BS747 AND BS767 AFT CARGO COMPARTMENT (3 LOCATION ). REPAIRED CARGO TRACK SECTION; TRACK SPLICE (2EA) LOCATED BTW BS 727 TO BS 787 RBBL 13.84 AT AFT CARGO COMPARTMENT IAW B737700 SRM 514002 AND 5300532R3 REPAIR 3 MATERIAL USED:BAC15201397 RO207476 AND BAC1502100688. P.O 217536

Part: GUSSET — CRACKED (FUSELAGE) · airframe 47,393 hrs · 32,204 cycles

CRACK GUSSET LOCATED BS500D AT STR21R FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED BS 500 D AT STR 21R FWD CARGO COMPARMTMENT IAW B737-700 SRM 51-40-02 AND DWG #143A7902 REV.- MATERIAL USED ALUMINION SHEET PN 7073-T0 0.040 PO #2020-203286

Part: GUSSET — CRACKED (FUSELAGE) · airframe 47,393 hrs · 32,204 cycles

CRACK GUSSET LOCATED BS500D AT STRINGER 19L FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED BS 500D AT STRINGER 19L FWD CARGO COMPARTMENT DUE TO CRACK NOT ALLOWABLE DAMAGE PART NUMBER USED 143A9481-6 P.O 2021-1060 47 IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 143A7902 REV- SHEET 174

Part: SUPPORT — DAMAGED (BS 727-767) · airframe 47,393 hrs · 32,204 cycles

ELONGATED HOLE SUPPORT ZEE LOCATED BETWEEN BS 767 AND BS 727 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT / REPLACED SUPPORT ZEE LOCATED BETWWEN BS767 AND BS727 AT LEVER STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND B737-700 DWG #146A 7502 REV A AND B737-700 DWG #140N4500 REV G. AND B737-700 SRM 51-10-02 ITEM 9. MATERIAL USED:SIDE PLATE 7075-T6 PART NUMBER:BAC1496-377-7075-T62 P.O.:2020213573

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 47,393 hrs · 32,204 cycles

CRACK ANGLE - SUPPORT LOCATED BS 867 AT LEVEL STRINGER 26L AFT CARGO COMPARTMENT / REPLACED ANGLE - SUPPORT LOCATED BS 867 AT LEVEL STRINGER 26L AFT CARGO COMPARTMENT DUE TO NOT FOUND ALLOWABLE DAMAGE IN SRM B737-700 TO CRACK; PART NUMBER USED 149A8109U114 P.O 2020-214810; INSTALLED ANGLE SUPPORT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.

Part: STRIP — CRAZED (CABIN) · airframe 47,393 hrs · 32,204 cycles

CRAZING IN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING (8EA) AT PASSENGER CABIN / REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING (8EA) AT PASSENGER CABIN IAW B737-700 AMM-33-51-15-400-802

Part: GUSSET — CRACKED (FUSELAGE) · airframe 47,393 hrs · 32,204 cycles

CRACK GUSSET LOCATED BS500D AT STRINGER 19R FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED BS 500D AT STRINGER 19R FWD CARGO COMPARTMENT DUE TO CRACK NOT ALLOWABLE DAMAGE PART NUMBER USED 143A 9481-5 P.O 2020-215355 IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 143A7902 REV -; SHEET 174

Part: ANGLE — CRACKED (FUSELAGE) · airframe 47,393 hrs · 32,204 cycles

CRACK ANGLE LOCATED BS500D AND BETWEEN STR25R TO STR26R AT FWD CARGO COMPARTMENT / REPLACED ANGLE LOCATED BS 500 D AND BETWEEN STR19R TO STR 26 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A9481 REV A SHEET 8 MATERIAL USED PN ALUMINIUN SHEET 7075-T0 PO #2020- 166195

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 47,393 hrs · 32,204 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED BS540 AT LBL24.75 TO RBL24.75 CENTER SECTION (2 EA) / REPLACED STIFFENER 2 (E/A) LOCATED BS 540 AT LBL 24.75 TO RBL 24.75 CENTER SECTION DUE TO CRACK NOT ALLOWABLE DAMAGE PART NUMBER USED ARE:143A5240- 35 P.O 2021-118065 143A5240-36 P.O 2021-118066 IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 143A0060 REV. A SHEET 36

Part: INTERCOSTAL — BENT (AFT CARGO COMPT) · airframe 47,393 hrs · 32,204 cycles

BENT WEB INTERCOSTAL LOCATED BETWEEN BS 767 AND BS 747 S25R AT AFT CARGO COMPARTMENT. REPLACED INTERCOSTAL LOCATED BETWEEN BS 767 AND BS747 STR 25R AT AFT CARGO COMPARTMENT IAW B737700 SRM 511002 AND DRAWING #146A7500 REV A.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 47,393 hrs · 32,204 cycles

CRACK SUPPORT ANGLE LOCATED BS695 AND RBL24.75 CENTER SECTION / REPLACED SUPPORT ANGLE LOCATED BS 695 AND RBL 24.75 CENTER SECTION I.A.W B737-700 SRM 51-10-02 PARAGRAPH 9 SRM 51-40-02 MATERIAL USED BAC1490- 2782 CONDITION TO AND HEAT TREATED A CONDITION T73 PO:2020-195969 DRAWING 111A6000 SHEET 304 REV -

Part: WEB — CRACKED (FUSELAGE) · airframe 47,393 hrs · 32,204 cycles

CRACK INDICATION FOUND ON PRESSURE DECK WEB AT BS 663 AND RBL 41 IN CENTER PAX CABIN LENGTH OF CRACK IS 0.400 IN / EVALUATED CRACK ON PRESSURE DECK WEB AT BS 663 AND RBL 41 IN CENTER PAX CABIN AND REPAIRED I.A.W B737-700 SRM 53-40-51-2R-2 REPAIR 2 FIG.202 DUE TO NO FOUND ALLOWABLE DAMAGE FOR CRACK ON SRM MODE REPAIR PARTS FROM MATERIAL ALUMINUM SHEET 0.080' 2024T3' P.O 2020-213281 ALUMINUM SHEET 0.063' 2024 T3 P.O 2020-221732 AND EXTRUSION BAC1505-100052 P.O 2020-163319.

Part: FAIRING — CRACKED (L/H WING) · airframe 47,393 hrs · 32,204 cycles

CRACK FLAP TRACK FAIRING 1 PRELOAD PAD AT LT WING REPLACED PRELOAD PAD ON FLAP TRACK FAIRING #1 LT WING IAW SRM B73770 5140020G0 AND B737700 AMM 275128820801.

Part: FASTENER — CRACKED (R/H HORIZ. STAB.) · airframe 47,393 hrs · 32,204 cycles

CRACK ON FASTENER OF LEADING EDGE RIB LOCATED LE STA 86.66 RT HORIZONTAL STAB (3EA) / REPLACED FASTENERS (3EA) ON LEADING RIB LOCATED ON LE STA 86.66 RT HORIZONTAL STAB IAW SRM B737-700 51-40-02 AND DRAWING #186A1001 REV A

Part: PANEL — CRACKED (FUSELAGE) · airframe 47,393 hrs · 32,204 cycles

CRACK CEILING PANEL 120YAC (SHROUD PANEL) FWD CARGO COMPARTMENT /

Part: PANEL — CRACKED (FUSELAGE) · airframe 47,393 hrs · 32,204 cycles

CRACK CEILING PANEL 121YAC (SHROUD PANEL) FWD CARGO COMPARTMENT /

Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 46,429 hrs · 31,626 cycles

CREW REPORTED EMERGENCY LIGHT LENS AT L2 DOOR IS THE WRONG ONE. / R/R L2 DOOR EMERGENCY LIGHT LENS OPS CHECK GOOD REF 33-51-04

Part: SLAT VALVE — OUT OF ADJUST (R1 DOOR) · airframe 45,658 hrs · 31,162 cycles

R1 DOOR SLIDE GIRT BAR DIFFICULT TO ARM AND STOW. / R&R SLIDE IAW MT.

Part: CIRCUIT BREAKER — FAULTY (EMERGENCY LIGHTS) · airframe 45,651 hrs · 31,158 cycles

DURING EMERGENCY LIGHT OPS CHECK WHEN P5 PANEL SWITCH IS PLACED IN THE ARM POSITION FRONT HALF OF EMERGENCY LIGHTS CAME ALL LIGHTS COME ON WITH SWITCH IN THE ON POSITION. / RESET CIRCUIT BREAKERS. PERFORMED EMERGENCY LIGHTING CHECK AND FOUND PASSENGER CABIN AREA EMERGENCY LIGHT AT 8DEF TO BE INOP. REMOVED AND REPLACED LAMP AT AREA LIGHT 8DEF.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,651 hrs · 31,158 cycles

L/H EMERGENCY EXIT LIGHTS INOP. / R&R BATTERY CHARGER IAW AMM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,651 hrs · 31,158 cycles

R/H EMERGENCY EXIT LIGHTS INOP. / R&R BATTERY CHARGER IAW AMM.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 45,651 hrs · 31,158 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140CF IS CORRODED ALONG EDGES ON TOP. / REMOVED CORROSION @ AFT CARGO PIT FLOOR PANEL #140 CF IAW SRM 53-00-53-1A-1 FIG 102 PG 4 CHECKED WITH 10X MAG VERIFIED MATERIAL LOSS AS ORIGINAL 'T' =.071 LOSS=.028 REMAINING=.043 AREA OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102 PG 4. VERIFIED NEW PANEL #140 CF AS P/N 453A2610-18 A-TAG WN 6822 IAW BOEING DWG 453A2610 REV: C PLACED NEW PANEL #140 CF ON AFT CARGO PANEL RACK

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 45,651 hrs · 31,158 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140AF IS CORRODED ALONG EDGES ON TOP. / EVALUATED DAME ON FLOOR PANEL 140AF. FOUND TOTAL DAMAGE LENGTH TO BE GREATER THEN 20'. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-1. FABRICATED NEW PANEL 140AF PER AMMM 25-52-01-201-801.

Part: BRACKET — CRACKED (R2 DOOR) · airframe 45,651 hrs · 31,158 cycles

PASSENGER CABIN AFT SERVICE DOOR (R2) LOWER HINGE ACCESS PNL 844DZ HAS 2EA RETENTION BRACKETS CRACKED AS MARKED / VERIFIED NEW BRACKET P/N 411A2119-193 ATAG CR3567 REPLACED ON BENCH REF JPANEL-844-CLOSE FOR INSTALLATION

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 45,651 hrs · 31,158 cycles

AFT CARGO COMPARTMENT; AFT CORNER SCUFF PLATE IS CRACKED. / RECEIVED RE-WORKED AFT SCUFF PLATE OF AFT CARGO DOOR PN # 146A8342-9 BECAUSE OF A CRACK ALL WORK PERFORMED ON EA NO # 1-A53-2076 REV 11 AND W/O # 40445/1600/0002 AND W/O NO # 40443/1600/0019 INSTALLED THE SCUFF PLATE IAW AMM 53-11-201-401 ON W/O NO # 40444/1600/0005

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 45,651 hrs · 31,158 cycles

RIGHT HORIZONTAL STAB LEADING EDGE PANEL 341B RIB CRACKED AT 105.25. / REMOVED AND REPLACED RIB AT R/H HORIZONTAL STAB. LEADING EDGE PANEL 341B AT 105.25 IAW B737 DWG 186A1304 REV.- AND SRM 51-40-02-0G-0. P/N 2 TAG# 186A1304-2 TAG# WN4012

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 45,651 hrs · 31,158 cycles

CABIN FLOOR BOARD 242VF HAS COMPOSITE TOP LAYER FIBER DAMAGE; MULTIPLE AREAS. / REPAIRED CABIN FLOOR BOARD 242VF TOP LAYER FIBER DAMAGE TO MULTIPLE AREAS AS MARKED I/A/W SRM 53-00-50-2R-0 REV 69 AND I/A/W SRM 53-00-50-2R-0 REV 69 AND I/A/W SRM 53-00-50-2R-1 REV 69 A79470; A72547

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 45,651 hrs · 31,158 cycles

PASSENGER CABIN FLOORBOARD 241BF HAS TOP LAYER OF FIBERS PULLED OFF ALONG LENGTH OF BOARD SEVERAL PLACES. / FABRICATED NEW FLOOR PANEL 241BF (USED ORIGINAL FLOOR PANEL AS SAMPLE) I/A/W SRM 53-00-50-2R-0 REV 69. BOEING DWG 144A5810 ID:0189 REV A- ; BAC5085 REV E A83881; WN4933; A29079

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 45,651 hrs · 31,158 cycles

PASSENGER CABIN FLOORBOARD 241DF HAS TOP LAYER OF FIBERS PULLED OFF ALONG LENGTH OF BOARD SEVERAL PLACES. / FABRICATED NEW FLOOR PANEL 241DF (USED ORIGINAL FLOOR PANEL AS SAMPLE) I/A/W SRM 53-00-50-2R-0 REV 69. BOEING DWG 144A5810 ID:0128 REV:- ; BAC5085 REV E A83881; WN4933; A29019

Part: FLOOR PANEL — PULLED (CABIN) · airframe 45,651 hrs · 31,158 cycles

PASSENGER CABIN FLOORBOARD 241AF HAS TOP LAYER OF FIBERS PULLED OFF ALONG LENGTH OF BOARD SEVERAL PLACES. / FABRICATED NEW FLOOR PANEL 241AF PER SAMPLE OF ORIGINAL FLOOR PANEL I/A/W SRM 53-00-50-2R-0 REV 69; BOEING DWG: 144A5810 ID: 0127 REV:-; BAC 5085 REV E WN4933; A83881; A29079

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 45,651 hrs · 31,158 cycles

PASSENGER CABIN FLOORBOARD 231XF HAS TOP LAYER OF FIBERS PULLED OFF ALONG LENGTH OF BOARD SEVERAL PLACES. / FABRICATED NEW FLOOR PANEL 231XF (USED ORIGINAL FLOOR PANEL AS SAMPLE) I/A/W SRM 53-00-50-2R-0 REV 69. BOEING DWG 144A5810 ID:0189 REV A ; BAC5085 REV E A83881; WN4933; A29079

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 45,651 hrs · 31,158 cycles

CABIN FLOOR BOARD 242UF HAS COMPOSITE TOP LAYER FIBER DAMAGE; MULTIPLE AREAS. / REPAIRED PASSENGER CABIN FLOORBOARD 242UF TOP LAYER FIBER DAMAGE ON MULTIPLE AREAS AS MARKED I/A/W SRM 53-00-50-2R-0 AND I/A/W SRM 53-00-50-2R-1 REV 69 A79470; A72547

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 45,651 hrs · 31,158 cycles

CABIN FLOOR BOARD 241ABF; HAS TOP LAYER COMPOSITE FIBER DAMAGE; IN MULTIPLE AREAS. / REPAIRED CABIN FLOOR BOARD 241 ABF TOP LAYER COMPOSITE FLOOR DAMAGE IN MULTIPLE AREAS I/A/W SRM 53-00-50-2R-0 REV 69 AND SRM 53-00-50-2R-0 REV 69.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 45,651 hrs · 31,158 cycles

CABIN FLOOR BOARD 241ADF HAS COMPOSITE TOP LAYER FIBER DAMAGE; FWD END. / REPAIRED FLOORBOARD 241ADF TOP LAYER FIBER DAMAGE FWD END I/A/W SRM 53-00-50-2R-0 REV 69 AND IAW SRM 53-00-50-2R-1 REV 69

Part: SIGN — PULLED (EMERGENCY LIGHT) · airframe 45,651 hrs · 31,158 cycles

L2 DOOR LOWER EMERGENCY EXIT SIGN WIRES WERE PULLED FROM THE CONNECTORS. / R&R EXIT SIGN PER AMM.

Part: FLOOR SUPPORT — CORRODED (BS 727-847) · airframe 45,651 hrs · 31,158 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE Z-ANGLE CORRODED BETWEEN BS. 727 TO BS. 847, LBL 20. / R&R ZEE ANGLE SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 727-767) · airframe 45,651 hrs · 31,158 cycles

DURING DTIP INSPECTION; AFT CARGO COMPARTMENT FLOOR STRUCTURE STA 727 TO 767; RBL 20; WL 156 R\H Z-ANGLE HAS CORROSION. / REMOVED DAMAGED ZEE SUPPORT AND REPLACED NEW IAW B-737 SRM 51-40-02-0G-0. NEW PART LOCATED AND DRILLED FASTENER LOCATIONS IAW B-737 SRM 51-40-05-0G-0. THE ORIGINAL PART WHEN REMOVING DAMAGE FOUND TO HAVE 100% MATERIAL LOSS FROM STA 727' TO 767'; RBL 20'; WL 156'. R/H ZEE SUPPORT FOUND TO BE OUT OF LIMITS IAW B-737 SRM 53-00-53-1A-2. NUTPLATES INSTALLED IAW B-737 SRM 51-40-10-2R-0. A-TAG #A86626

Part: SHIELD — CORRODED (BS 767-787) · airframe 45,651 hrs · 31,158 cycles

DURING DTIP INSPECTION; AFT CARGO COMPARTMENT FLOOR STRUCTURE STA 767 TO 787; RBL 20; WL 156 SHIELD HAS CORROSION. / DAMAGED SHIELD LOCATED AT AFT CARGO COMPARTMENT FLOOR STRUCTURE STA 767-787; RBL 20; WL 156 FOUND TO HAVE 100% MATERIAL LOSS. PART FAOUND OUT OF LIMITS IAW B-737 SRM 53-00-53-1A-2. NEW PARTS FASTENER LOCATION S LOCATED AND DRILLED IAW B737 SRM 51-40-05-0G-0. DAMAGED PART REMOVED AND REPLACED NEW IAW B 737 SRM 51-40-02-0G-0. CIC APPLIED IAW B-737 AMM 51-21-91-620-802. P/N 146A8127-12 A-TAG #WN5952

Part: THRESHOLD — CRACKED (FWD GALLEY) · airframe 45,651 hrs · 31,158 cycles

FWD GALLEY SERVICE DOOR LOWER CENTER THRESHOLD CRACKED. / REPAIRED FWD GALLEY SERVICE DOOR LOWER CENTER THRESHOLD IAW EA NO:1-A53-2076 REV 11 INSTALLED I.A.W. AMM 53-11-01-420-801

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 45,651 hrs · 31,158 cycles

AFT CARGO DOOR FWD SCUFF PLATE HAS A CRACK ON UPPER I/B EDGE PART #654A0004-97 / RECEIVED RE-WORKED FWD SCUFF PLATE OF AFT CARGO DOOR PN # 654A004-97 BECAUSE OF A CRACK ALL WORK PERFORMED ON EA NO # 1-A53-2076 REV 11 AND W/O # 40445/1600/0001 AND W/O NO # 40443/1600/0001 INSTALLED THE SCUFF PLATE ON W/O NO # 40444/1600/0005 IAW AMM 53-11-02-401

Part: STRIP — CORRODED (FWD CARGO) · airframe 45,651 hrs · 31,158 cycles

FWD CARGO COMPARTMENT LH FLOOR CAP STRIPS CORRODED / NEW PARTS VERIFIED IAW AIPC 25-52-10-01. NEW PARTS TAGGED AND PLACED ON RACK. CAPSTRIPS TO FWD CARGO COMPARTMENT L/H FLOOR A-TAGS #WN6306 #WN3197 #A05052 #WN1104

Part: STRIP — CORRODED (FWD CARGO) · airframe 45,651 hrs · 31,158 cycles

FWD CARGO COMPARTMENT RH FLOOR CAP STRIPS CORRODED / NEW PARTS VERIFIED IAW AIPC 25-52-10-01. NEW PARTS TAGGED AND PLACED ON RACK. CAPSTRIPS TO FWD CARGO COMPARTMENT R/N FLOOR A-TAGS #A01686 & # WN6261

Part: STRIP — CORRODED (FWD CARGO) · airframe 45,651 hrs · 31,158 cycles

FWD CARGO COMPARTMENT AFT CAP STRIP AT BS 500D FOR FLOOR IS CORRODED / REPLACED FWD CARGO AFT CAP STRIP AT STA 500D PART #453A1611-9 ON TABLE PER AIPC 25-52-10-01 ITEM 370. CAP STRIP INSTALLED ON CARD NO JPANEL-121-CLOSE ISSUE TAG #WN2258

Part: PLATE — CRACKED (LT WING) · airframe 43,625 hrs · 29,853 cycles

L/H WING WIGGLE PLATE CRACKED AT RSS. 261. R&R WIGGLE PLATE IAW SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 43,625 hrs · 29,853 cycles

FWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED / ACCOMPLISHED REPAIR PER EA NO 1-A53-2076 REV. 11. 92892U 15JUN19.

Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 43,625 hrs · 29,853 cycles

FLIGHT DECK FLOOR DENTED AT BS. 255, BETWEEN RBL 3 TO LBL 14. / REPAIRED FLOOR DECK PER SRM & EA.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 43,625 hrs · 29,853 cycles

2ND VERTICAL STIFFENER CRACKED ON R/H HORIZONTAL STABILIZER INSPAR RIB 120.30. REPAIRED STIFFENER IAW SRM.

Part: RIB — ELONGATED (LT WING) · airframe 43,625 hrs · 29,853 cycles

LEFT WING DEFLECTION CONTROL RIB HAS ELONGATED HOLES AT AFT ATTACH POINT. / REPAIRED ELONGATED AFT ATTACH POINT FASTENER HOLES ON LT WING DEFECTION CONTROL RIB IAW SRM 57-51-02-2R-4 SECT. 4.

Part: BEAM — CRACKED (R1 DOOR) · airframe 43,625 hrs · 29,853 cycles

R1 DOOR #4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. R&R BEAM PER MM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 43,625 hrs · 29,853 cycles

3RD VERTICAL STIFFENER CRACKED ON R/H HORIZONTAL STABILIZER INSPAR RIB 120.30. REPAIRED STIFFENER IAW SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,387 hrs · 29,042 cycles

FORWARD GALLEY EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,930 hrs · 28,724 cycles

LT EMERGENCY AREA LIGHT INOP AT ROW 24. RELAMPED LIGHT AMM.

Part: WIRE — OUT OF POSITION (L1 DOOR SLIDE) · airframe 39,404 hrs · 27,056 cycles

L1 DOOR SLIDE PACK WIRE OUT OF POSITION. REPOSITIONED THE WIRE IAW AMM.

Part: FLASHLIGHT ASSY — INOPERATIVE (FWD CABIN) · airframe 38,734 hrs · 26,628 cycles

FWD EMERGENCY FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT ASSY IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,417 hrs · 26,421 cycles

RIGHT INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 12. REPLACED THE LAMPS IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 37,775 hrs · 26,003 cycles

L1 DOOR SLIDE LOOSE. SECURED THE SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,505 hrs · 25,829 cycles

RT OVERWING EMERGENCY LIGHT INOP. R&R LIGHT IAW AMM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 37,056 hrs · 25,549 cycles

FUSELAGE SKIN DAMAGED AT BS 364, BETWEEN STR 23L TO STR 24L. REPAIRED SKIN PER EA.

Part: FUSE — BLOWN (CABIN) · airframe 37,056 hrs · 25,549 cycles

RT EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 8. R&R FUSE PER AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 37,056 hrs · 25,549 cycles

FWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED / FWD CARGO BAY FWD CORNER SCUFF PLATE REPAIRED IAW EA-1-A53-2076 REV 11

Part: SUPPORT BRACKET — CRACKED (MAIN CABIN) · airframe 37,056 hrs · 25,549 cycles

FLOOR PANEL SUPPORT BS 540 RBL-25 TO BL-0 IS CRACKED. / REMOVED AND REPLACED FLOOR PANEL SUPPORT AT BS 540 RBL 25 TO BL 0 WITH NEW SUPPORT IAW SRM 51-40-02 56105U 16MAY17

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 37,056 hrs · 25,549 cycles

L1 DOOR CUTOUT INTERNAL DOUBLER CLOSEOUT CRACKED BELOW LOWER HINGE CUTOUT. R & R DOUBLER IAW SRM AND DWG.

Part: COLLAR — BROKEN (L1 DOOR) · airframe 37,056 hrs · 25,549 cycles

L1 DOOR ESCAPE SLIDE GIRT BAR QUICK RELEASE COLLAR BROKEN. R&R COLLAR IAW AMM.

Part: SLIDE — WORN (R2 DOOR) · airframe 37,056 hrs · 25,549 cycles

R2 DOOR ESCAPE SLIDE SKIRT WORN. R&R SLIDE IAW MT.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 37,056 hrs · 25,549 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 847 TO BS 867, RBL 21. R&R SUPPORT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,056 hrs · 25,549 cycles

STUB FRAME BEAM CRACKED AT BS 294, RBL 65. REPAIRED STUB FRAME IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 37,056 hrs · 25,549 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 20. R&R SUPPORT IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 37,056 hrs · 25,549 cycles

AFT CARGO BAY FLOOR TRACK CORRODED AT BS 945, LBL 3. R&R FLOOR TRACK PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,056 hrs · 25,549 cycles

FUSELAGE INTERCOSTAL CRACKED AT STA 277 TO STA 294, RBL 3, WL 207. R&R INTERCOSTAL PER SRM.

Part: WEB — CORRODED (BS 440-496) · airframe 37,056 hrs · 25,549 cycles

THRESHOLD SUPPORT WEB CORRODED AT BS 440 TO 496, RBL 25. REPAIRED THE SUPPORT WEB PER SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 500A-500D) · airframe 37,056 hrs · 25,549 cycles

SIDEWALL SUPPORT CORRODED AT BS 500A TO 500D, RBL 20. REPAIRED THE SIDWALL SUPPORT IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 37,056 hrs · 25,549 cycles

FORWARD CARGO BAY BULKHEAD SUPPORT ANGLE CORRODED AT BS 400, RBL 20. R&R ANGLE IAW SRM AND EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 37,056 hrs · 25,549 cycles

RT HORIZONTAL STABILIZER RIB 92.5, 2ND FROM FORWARD VERTICAL STIFFENER CRACKED. REPAIRED RIB IAW EA.

Part: SIDEWALL SUPPORT — CORRODED (BS 727-767) · airframe 37,056 hrs · 25,549 cycles

SIDEWALL SUPPORT CORRODED AT BS 727 TO 767, RBL 21. REPAIRED THE SIDEWALL SUPPORT IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 37,056 hrs · 25,549 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 796 TO BS 802, BETWEEN RBL 22 TO RBL 26. R&R WEB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 37,056 hrs · 25,549 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BS 886 TO BS 887, RBL 21. R&R SUPPORT IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 400-420) · airframe 37,056 hrs · 25,549 cycles

SIDEWALL SUPPORT CORRODED AT BS 400 TO 420, RBL 20. REPAIRED THE SIDWALL SUPPORT IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,056 hrs · 25,549 cycles

FORWARD LOWER CORNER EXTERNAL SKIN CORRODED BETWEEN BS 440 TO BS 450, STR 24R. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,056 hrs · 25,549 cycles

AFT LOWER CORNER EXTERNAL SKIN CORRODED BETWEEN BS 480 TO BS 492.4, STR 24R. REPAIRED SKIN IAW ER AND EA.

Part: BULKHEAD WEB — CRACKED (RT MLG WW) · airframe 37,056 hrs · 25,549 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 35 TO 45. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 37,056 hrs · 25,549 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 45. REPAIRED THE BULKHEAD WEB IAW SRM.