N470WN

Part: LAMP — BURNED OUT (ZONE 200) · airframe 71,124 hrs · 42,675 cycles

RIGHT EMERGENCY EXIT CUTOUT OVERHEAD LIGHTS ARE BURNED OUT. R & R CABIN EMERGENCY EXIT LIGHTS IAW AMM 33-51-01. INSPECTED IAW AMM 33-51-01-960-801-NG. EXIT SIGN - LAMP REPLACEMENT.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 71,125 hrs · 42,675 cycles

VERTICAL STIFFENER CRACKED BS 540, RBL 24 UPPER SECTION. REPLACED THE LBL 24 AND RBL 24 STIFFENERS AT BS 540 IAW SRM 51-40-02 IAW DRAWINGS. FABRICATION DEVIATION IAW EA 25-157-03419.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 71,125 hrs · 42,675 cycles

VERTICAL STIFFENER CRACKED BS 540, LBL 24 UPPER SECTION. REFER TO FAULT TTG8Q0197Q2R WHERE EA 25-157-03419 WAS ADDED AS A SUBTASK. C/W REPLACEMENT STIFFENER AT LBL 24 IAW SRM 51-40-02-0G-0 & DWG 111A2001 REV -. REMOVED AND REPLACED VERTICAL STIFFNER AT BS 540 LBL 24 IAW SRM 51-40-02-0G-0, AND DWG 111A2001 REV-.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 71,125 hrs · 42,675 cycles

EMERGENCY LIGHTS ABOVE OVERHEAD BINS ARE INOP ON LEFT SIDE. R & R CABIN CEILING NIGHT LIGHTS IAW AMM 33-22-00.

Part: HANDLE — BROKEN (ZONE 800) · airframe 71,033 hrs · 42,611 cycles

L1 DOOR ASSIST HANDLE BROKEN. SWAPPED ASSIST HANDLE FROM FWD LAV TO L1 DOOR PER AMM 52-11-31. L1 DOOR ASSIST HANDLE OPS CHECKS NORMAL. OK TO CONTINUE IAW MEL 25-10-01. C/W SP NR 1B. AUTH 294378. INSTALLED NEW ASSIST HANDLE IN FWD LAVATORY. CHECKED GOOD. IAW AMM 52-11-31.

Part: HANDLE — LOOSE (ZONE 800) · airframe 70,443 hrs · 42,222 cycles

FWD ENTRY DOOR HANDLE LOOSE. SECURED FWD ENTRY DOOR HANDLE IAW AMM 52-11-00.

Part: GIRT BAR — LOOSE (ZN 800 DOOR) · airframe 69,827 hrs · 41,840 cycles

FWD SERVICE DOOR GRIT BAR RETENTION BRACKET LOOSE. ADJUSTED FWD SERVICE DOOR GRIT BAR RETENTION BRACKET REF B737 SIP.

Part: LIMITER — FAULTY (ZN 100 FUS LOWER) · airframe 67,914 hrs · 40,687 cycles

B HYD SYSTEM ENG AND ELEC LOW PRESSURE; QUANTITY DROPPED TO ZERO IN FLIGHT; STBY HYD LOW QTY AT GATE<[01] 01 - REMOVED AND REPLACED PER [AMM 27-51-67-401-NG (TRAILING EDGE FLAP FLOW LIMITER - REMOVAL/INSTALLATION - PERMANENT)]. OPPS CHECK GOOD

Part: PANEL — CRACKED (ZONE 600) · airframe 67,617 hrs · 40,503 cycles

PANEL CRACKED AT FASTENER HOLE. RIGHT WING INBOARD FLAP TRACK LOWER WING SKIN PANEL. PANEL CRACKED AT FASTENER HOLE. APPROX. 0.5 IN. LENGTH TO EDGE OF PANEL. RIGHT WING INBOARD FLAP TRACK LOWER WING SKIN PANEL. ITEM (8) 115A2723 SRM 57-51-01-0I-1.<[01] 04 - REPAIRED PER [EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT)] 24-157-02934

Part: STRINGER — CRACKED (BS 727 S18AL) · airframe 66,313 hrs · 39,674 cycles

CRACK INDICATION FOUND IN OPEN HOLE LOC ON BS 727 INNER CHORD AT STRINGER 18A LEFT SIDE; CRACK DIRECTION IS: 2 O CLOCK( VIEW LOOKING INSIDE TO OUTSIDE) 2024-270318<[01] ON STEP 2. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 210136503. DUE DATE: 23-MAY-24.;[02] TOOLS USED: TEMPERATURA CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 23-JAN-25.;[03] CORRECTED STEP 2. TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 23-JAN-25.;[04] TOOL USED DIGITAL CALIPER P/N: 500-193-30 S/N: 0000291 DUE DATE: 01-NOV-24.;[05] REPAIRED INNER CHORD BSTA 727 AND AT S-18A LHS IAW EA# 24-153-01268-WIP1; 24-153-01268-WIP2; 24-153-01268-WIP3; 24-153-01268-WIP4 AND EA#24-153-01268; SEE INDIVIDUAL SIGNOFF BELOW.;[06] REPAIRED INNER CHORD BSTA 727 AND AT S-18A LHS IAW EA# 24-153-01268-WIP1; 24-153-01268-WIP2; 24-153-01268-WIP3; 24-153-01268-WIP4 AND EA#24-153-01268; SEE INDIVIDUAL SIGNOFF BELOW. COMPLETED RII

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,311 hrs · 39,673 cycles

INOP EMERGENCY LIGHT POWER SUPPLY M1668 AT MIDDLE PAX CABIN 2024-270302<[01] REPLACED EMERGENCY LIGHT POWER SUPPLY M1668 AT MIDDLE PAX CABIN I.A.W B737-700 AMM 33-51-06-960-806. TEST IS OK. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 66,313 hrs · 39,674 cycles

CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2024-269854<[01] TOOL USED: DIGITAL CALIPER P/N: 500-196-30; S/N: A23325649; DUE DATE: 31-DEC-24.;[02] TOOL USED; RADIOMETER/PHOTOMETER KIT ; P/N:XRP-3000; S/N:1859843; DUE DATE : 24/JUL/24;[03] REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975. TASK COMPLETED.

Part: LIGHT — DETERIORATED (CABIN) · airframe 66,313 hrs · 39,674 cycles

DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2024-270205<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802;[02] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802

Part: STRINGER — CRACKED (LT WING) · airframe 66,313 hrs · 39,674 cycles

CRACK FUEL TANK LOC. BTW RIB 19 AND RIB 20 STRINGER 8 UPPER SKIN LOWER SURFACE AFT AREA AT LT WING. REPAIRED UPPER STRINGER U8 - WSTA 564.5 TO WSTA 591.5 AND SKIN ATTACHMENT FLANGE IAW EA# 24-157-01168-WIP1 AND EA# 24-157-01168 SEE INDIVIDUAL SIGNOFF BELOW.;[04] REPAIRED UPPER STRINGER U8 - WSTA 564.5 TO WSTA 591.5 AND SKIN ATTACHMENT FLANGE IAW EA# 24-157-01168-WIP1 AND EA# 24-157-01168 SEE INDIVIDUAL SIGNOFF BELOW. CERTIFIED

Part: STRINGER — CRACKED (RT WING) · airframe 66,313 hrs · 39,674 cycles

CRACK FUEL TANK LOC. BTW RIB 19 AND RIB 20 STRINGER 8 UPPER SKIN LOWER SURFACE AFT AREA AT RT WING. REPAIRED UPPER STRINGER U8 - WSTA 564.5 TO WSTA 591.5 AND SKIN ATTACHMENT FLANGE RH WING IAW EA# 24-157-01169 WIP1 AND EA# 24-157-01169 SEE INDIVIDUAL SIGNOFF BELOW.;[04] REPAIRED UPPER STRINGER U8 - WSTA 564.5 TO WSTA 591.5 AND SKIN ATTACHMENT FLANGE RH WING IAW EA# 24-157-01169 WIP1 AND EA# 24-157-01169 SEE INDIVIDUAL SIGNOFF BELOW. CERTIFIED

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 66,313 hrs · 39,674 cycles

CRACK ANGLE LOCATED STA 1016 AT VERTICAL STABILIZER 2024-270178<[01] REPLACED ANGLE LOCATED STA 1016 AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DRAWING # 176A3001;REV D.SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMED

Part: SUPPORT BRACKET — CORRODED (RUDDER) · airframe 66,313 hrs · 39,674 cycles

CORROSION BONDING JUMPER SUPPORT BRAKET LOC APROX AT RUD STA 257.9 AT VERTICAL STABILIZER 2024-270179<[01] REPLACED SUPPORT BRACKET AND FASTENERS LOC. APROX AT RUD STA 257.9 AT VERTICAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND INSTALLED BONDING JUMPER LOC. NEW SUPPORT BRACKET AND FASTENER I.A.W SWPM 20-20-10.SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 66,313 hrs · 39,674 cycles

CRACK ON THRESHOLD SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-270149<[01] REPLACED THRESHOLD SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02; DRAWING # 146A8340 REV.- SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTED STEP 1.<BR>REPLACED THRESHOLD SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02; DRAWING # 146A8340 REV.- AND INSTALLATION OF THRESHOLD ON TASK CARD TTG8Q00376TY. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] CERTIFIED WORK PERFORMED

Part: STRINGER — CRACKED (BS 540 S26L) · airframe 66,313 hrs · 39,674 cycles

CRACK STRINGER 26L LOCATED BS540 FWD CARGO COMPARTMENT 2024-270153<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130061901; CAL DUE DATE: 09-JUN-24;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-25.;[03] ON STEP 9; EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 11-MAR-25.;[04] PERFORMED PERMANENT REPAIR LOCATED BETWEEN BS 500D MORE 10? TO BS 540 I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1; THIS REPAIR IS CAT A NOT FURTHER ACTION OR INSPECTION REQUIRED. SEE INDIVIDUAL SING-OFF BELOW.;[05] PERFORMED PERMANENT REPAIR LOCATED BETWEEN BS 500D MORE 10? TO BS 540 I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1; THIS REPAIR IS CAT A NOT FURTHER ACTION OR INSPECTION REQUIRED. RII VERIFIED.

Part: STRINGER — CRACKED (BS 540 S25R) · airframe 66,313 hrs · 39,674 cycles

CRACK STRINGER 25R LOCATED BS540 FWD CARGO COMPARTMENT 2024-270154<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130061901; CAL DUE DATE: 09-JUN-24;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-25.;[03] STEP 8 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 220272512; DUE DATE: 08-JAN-25;[04] PERFORMED PERMANENT REPAIR ON STRINGER 25R LOCATED BETWEEN BS 500C MORE 10? TO BS 540 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OF BELOW.;[05] PERFORMED PERMANENT REPAIR ON STRINGER 25R LOCATED BETWEEN BS 500C MORE 10? TO BS 540 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OF BELOW.;[06] PERFORMED PERMANENT REPAIR ON STRINGER 25R LOCATED BETWEEN BS 500C MORE 10? TO BS 540 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OF BELOW.

Part: WEB — CRACKED (BS 500-500A) · airframe 66,313 hrs · 39,674 cycles

CRACK ON WEB-INTERCOSTAL LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26R AT FWD CARGO COMPARTMENT 2024-270146<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 142820025 DUE DATE 22 JAN 25.;[02] REPLACED WEB-INTERCOSTAL; LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM: 51-10-02; DWG: 143A0080 SHEET 19 REV.? AND DWG: 143A8121 SHEET 1 REV.?;[03] CORRECTED STEP 2.<BR>REPLACED WEB-INTERCOSTAL; LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM: 51-10-02; DWG: 143A0080 SHEET 19 REV.? AND DWG: 143A8121 SHEET 1 REV.? SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPLACED WEB-INTERCOSTAL; LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM: 51-10-02; DWG: 143A0080 SHEET 19 REV.? AND DWG: 143A8121 SHEET 1 REV.?. RII VERIFIED

Part: STRINGER — CRACKED (BS 540 S25L) · airframe 66,313 hrs · 39,674 cycles

CRACK STRINGER 25L LOCATED BS540 FWD CARGO COMPARTMENT 2024-270152<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130061901; CAL DUE DATE: 09-JUN-24;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-25.;[03] ON STEP 9; EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 11-MAR-25.;[04] PERFORMED PERMANENT REPAIR LOCATED BETWEEN BS 500D MORE 10? TO BS 540 I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1; THIS REPAIR IS CAT A NOT FURTHER ACTION OR INSPECTION REQUIRED. SEE INDIVIDUAL SING-OFF BELOW.;[05] PERFORMED PERMANENT REPAIR LOCATED BETWEEN BS 500D MORE 10? TO BS 540 I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1; THIS REPAIR IS CAT A NOT FURTHER ACTION OR INSPECTION REQUIRED. RII VERIFIED

Part: FRAME — CRACKED (BS 727B S8-9R) · airframe 66,313 hrs · 39,674 cycles

CRACK ON FRAME LOCATED BS 727B BTW STR 8R TO STR 9R AT PASSENGER CABIN 2024-270112<[01] TOOL USED ON STEP 6 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] PERFORMED PERMANENT REPAIR ON FRAME LOCATED BS 727B BTW STR 8R TO STR 9R AT PASSENGER CABIN IAW B737-700 EA 1-A53-12114. SEE INDIVIDUAL SING OFF BELOW;[03] RII COMPLETED JOB

Part: FRAME — CRACKED (BS 727B-S8-9L) · airframe 66,313 hrs · 39,674 cycles

CRACK ON FRAME LOCATED BS 727B BTW STR 8L TO STR 9L AT PASSENGER CABIN 2024-270111<[01] TOOL USED ON STEP 6 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] PERFORMED PERMANENT REPAIR ON FRAME LOCATED BS 727B BTW STR 8L TO STR 9L AT PASSENGER CABIN IAW B737-700 EA 1-A53-12114.;[03] CORRECTION ACTION 2: PERFORMED PERMANENT REPAIR ON FRAME LOCATED BS 727B BTW STR 8L TO STR 9L AT PASSENGER CABIN IAW B737-700 EA 1-A53-12114. SEE INDIVIDUAL SING OFF BELOW;[04] CORRECTION ACTION 2: PERFORMED PERMANENT REPAIR ON FRAME LOCATED BS 727B BTW STR 8L TO STR 9L AT PASSENGER CABIN IAW B737-700 EA 1-A53-12114. SEE INDIVIDUAL SING OFF BELOW<BR>RII VERIFIED

Part: FRAME — CRACKED (BS 807 S8-9L) · airframe 66,313 hrs · 39,674 cycles

CRACK ON FRAME LOCATED BS 807 BTW STR 8L TO STR 9L AT PASSENGER CABIN 2024-270110 CRACK ON FRAME LOCATED BS 787 BTW STR 8L TO STR 9L AT PASSENGER CABIN<[01] TOOL USED ON STEP 5 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-JUN-24;[02] PERFORMED PERMANENT REPAIR ON FRAME LOCATED BS 787 BTW STR 8L TO STR 9L AT PASSENGER CABIN IAW B737-700 EA 1-A53-12114. SEE INDIVIDUAL SING OFF BELOW;[03] RII COMPLETED JOB

Part: ACCESS PANEL — CRACKED (HORIZONTAL STAB) · airframe 66,313 hrs · 39,674 cycles

CRACK LEADING EDGE RIB ACCESS PANEL 331B LE STA 114.55 LT HORIZONTAL STAB 2024-270077<[01] REPLACED LEADING EDGE CHORD RIB OF ACCESS PANEL 331B LE STA 114.55 AT LT HORIZONTAL STABILIZER I.A.W. B737-700 SRM 51-10-02; SRM 51-40-02. DWG 186A1305 SHEET 1 REV. 5 AND DWG 186A1001 SHEET 10 REV. A. SEE INDIVIDUAL SIGN OFFS BELOW;[02] STEP 1 CORRECTED.<BR>REPLACED LEADING EDGE CHORD RIB OF ACCESS PANEL 331B LE STA 114.55 AT LT HORIZONTAL STABILIZER I.A.W. B737-700 SRM 51-10-02; SRM 51-40-02. DWG 186A1305 SHEET 1 REV. - AND DWG 186A1001 SHEET 10 REV. A. SEE INDIVIDUAL SIGN OFFS BELOW;[03] REPLACED LEADING EDGE CHORD RIB OF ACCESS PANEL 331B LE STA 114.55 AT LT HORIZONTAL STABILIZER I.A.W. B737-700 SRM 51-10-02; SRM 51-40-02. DWG 186A1305 SHEET 1 REV. - AND DWG 186A1001 SHEET 10 REV. A. SEE INDIVIDUAL SIGN OFFS BELOW

Part: ANGLE — CORRODED (NR 2 NACELLE) · airframe 66,313 hrs · 39,674 cycles

CORROSION FWD STRUT FAIRING BONDING JUMPER SUPPORT ANGLE ON ENGINE 2 2024-270074<[01] REPLACED SUPPORT ANGLE AT FWD STRUT FAIRING BONDING JUMPER ON ENGINE 2 IAW B737-700 SRM 51-40-02.;[02] REPLACED SUPPORT ANGLE AT FWD STRUT FAIRING BONDING JUMPER ON ENGINE 2 IAW B737-700 SRM 51-40-02.

Part: VAPOR BARRIER — CRACKED (BS 664 LBL 16) · airframe 66,313 hrs · 39,674 cycles

CRACK ON WEB VAPOR BARRIER LOCATED BS 663.75 LBL 16 AT CENTER WING BOX 2024-270075<[01] TOOL USED: CALIPER P/N: 500-196-30; S/N: B21141522; DUE DATE: 07-NOV-24.;[02] TOOL USED= HOT BONDER P/N:HCS9200B; S/N: 16122983; DUE DATE: 15-FEB-25. REPAIRED VAPOR BARRIER LOCATED BS 663.75 LBL 16 AT CENTER WING BOX AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10. REPAIRED VAPOR BARRIER LOCATED BS 663.75 LBL 16 AT CENTER WING BOX AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: LIGHT — BROKEN (CABIN) · airframe 66,313 hrs · 39,674 cycles

BROKEN SIDEWALL PANEL 231YHW BASE EMERGENCY EXIT LIGHT AT PASSENGER CABIN (1 EA) 2024-270063<[01] REPLACED SIDEWALL PANEL 231YHW BASE EMERGENCY EXIT LIGHT AT PASSENGER CABIN (1 EA) I.A.W. B737-700 AMM 33-51-01-960-802 OPERATIONAL TEST IS OK;[02] REPLACED SIDEWALL PANEL 231YHW BASE EMERGENCY EXIT LIGHT AT PASSENGER CABIN (1 EA) I.A.W. B737-700 AMM 33-51-01-960-802 OPERATIONAL TEST IS OK

Part: ACCESS PANEL — CRACKED (HORIZONTAL STAB) · airframe 66,313 hrs · 39,674 cycles

CRACK SEAL - PLATE ACCESS PANEL 333AT LT HORIZONTAL STABILIZER. REPLACED SEAL PLATE ACCESS PANEL 333AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND SRM 51-40-02-0G-0.

Part: NUT PLATE — CRACKED (LT WING LE) · airframe 66,313 hrs · 39,674 cycles

CRACK INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS632 AT LT WING 2024-270037<[01] REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS632 AT LT WING . IAW B737-700 SRM 51-40-02; DWG: 112A4402 SHEET: 14 REV:- AND IAW B737-700 SRM 51-10-02 STEP 9 ITEMS A.;[02] CORRECT STEP 1: REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS632 AT LT WING . IAW B737-700 SRM 51-40-02; DWG: 112A4402 SHEET: 14 REV:- AND IAW B737-700 SRM 51-10-02 STEP 9 ITEMS A. MEASURE OF CRACK L:0.445' TOOL USED DIGITAL CALIPER P/N: 500-197-30<BR>DUE DATE 21-NOV-2024;[03] CORRECT STEP 2: REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS632 AT LT WING . IAW B737-700 SRM 51-40-02; DWG: 112A4402 SHEET: 14 REV:- AND IAW B737-700 SRM 51-10-02 STEP 9 ITEMS A. MEASURE OF CRACK L:0.445' TOOL USED DIGITAL CALIPER P/N: 500-197-30<BR>DUE DATE 21-NOV-24;[04] REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS632 AT LT WING . IAW B737-700 SRM 51-40-02; DWG: 112A4402 SHEET: 14 REV:- AND IAW B737-700 SRM 51-10-02 STEP 9 ITEMS A. MEASURE OF CRACK L:0.445' TOOL USED DIGITAL CALIPER P/N: 500-197-30<BR>DUE DATE 21-NOV-24

Part: NUT PLATE — CRACKED (LT WING LE) · airframe 66,313 hrs · 39,674 cycles

CRACK INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS449 AT LT WING 2024-270035<[01] REPLACED INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS449 AT LT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 112A4402 SHEETS 13 REV-.;[02] COMPLETED JOB

Part: NUT PLATE — CRACKED (RT WING LE) · airframe 66,313 hrs · 39,674 cycles

CRACK INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS574 AT RT WING 2024-270033<[01] REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS 574 AT RT WING .IAW B737-700 SRM 51-40-02; DWG:112A4402 SHEET:14 REV:-AND IAW B737-700 SRM 51-10-02 STEP 9 ITEMS A.;[02] CORRET STEP 1:REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS574 AT RT WING WING .IAW B737-700 SRM 51-40-02; DWG:112A4402 SHEET:14 REV:-AND IAW B737-700 SRM 51-10-02 STEP 9 ITEMS A. MEASURE OF CRACK L:0.445' TOOL USED DIGITAL CALIPER P/N: 500-197-30<BR>DUE DATE 21-NOV-2024;[03] CORRET STEP 2:REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS574 AT RT WING WING .IAW B737-700 SRM 51-40-02; DWG:112A4402 SHEET:14 REV:-AND IAW B737-700 SRM 51-10-02 STEP 9 ITEM A. MESURE OF CRACK L:0.445' TOOL USED DIGITAL CALIPER P/N: 500-197-30. DUE DATE 21-NOV-24.;[04] REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS574 AT RT WING WING .IAW B737-700 SRM 51-40-02; DWG:112A4402 SHEET:14 REV:-AND IAW B737-700 SRM 51-10-02 STEP 9 ITEM A. MESURE OF CRACK L:0.445' TOOL USED DIGITAL CALIPER P/N: 500-197-30. DUE DATE 21-NOV-24.

Part: NUT PLATE — CRACKED (RT WING LE) · airframe 66,313 hrs · 39,674 cycles

CRACK INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS449 AT RT WING 2024-270034<[01] REPLACED INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS449 AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 112A4402 SHEETS 13 REV-.;[02] COMPLETED JOB

Part: NUT PLATE — CRACKED (LT WING LE) · airframe 66,313 hrs · 39,674 cycles

CRACK INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS576 AT LT WING 2024-270036<[01] REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS576 AT LT WING. IAW B737-700 SRM 51-40-02; DWG: 112A4402 SHEET: 14 REV:- AND IAW B737-700 SRM 51-10-02 STEP 9 ITEMS A.;[02] CORRET STEP 1:REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS576 AT LT WING. IAW B737-700 SRM 51-40-02; DWG: 112A4402 SHEET: 14 REV:- AND IAW B737-700 SRM 51-10-02 STEP 9 ITEMS A. MEASURE OF CRACK L:0.445? TOOL USED DIGITAL CALIPER P/N: 500-197-30 DUE DATE 21-NOV-2024;[03] CORRET STEP 2:REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS576 AT LT WING. IAW B737-700 SRM 51-40-02; DWG: 112A4402 SHEET: 14 REV:- AND IAW B737-700 SRM 51-10-02 STEP 9 ITEMS A. MEASURE OF CRACK L:0.445? TOOL USED DIGITAL CALIPER P/N: 500-197-30 DUE DATE 21-NOV-24;[04] REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS576 AT LT WING. IAW B737-700 SRM 51-40-02; DWG: 112A4402 SHEET: 14 REV:- AND IAW B737-700 SRM 51-10-02 STEP 9 ITEMS A. MEASURE OF CRACK L:0.445? TOOL USED DIGITAL CALIPER P/N: 500-197-30 DUE DATE 21-NOV-24

Part: BRACKET — CRACKED (BS 948 S26L) · airframe 66,313 hrs · 39,674 cycles

CRACK BRACKET LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT 2024-270005<[01] REPLACED BRACKET LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 149A8103 SHEET: 6 REV: - SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED BRACKET LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 149A8103 SHEET: 6 REV: - SEE INDIVIDUAL SIGN OFF BELOW

Part: CARGO TRACK — CRACKED (BS 727E RBL 14) · airframe 66,313 hrs · 39,674 cycles

CRACK TRACK RBL 13.84 LOCATED BS727E AT AFT CARGO COMPARTMENT 2024-269998<[01] TOOL USED ON STEP 4 IS EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 190023010; DUE DATE: 24-JUL-24;[02] PERFORMED PERMANENT REPAIR ON CARGO TRACK LOC. RBL 13.84 BETWEEN BS 727D MORE 12 INCH TO BS 747 MORE 12 INCH AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 53-00-53-2R-3 REPAIR 3 SEE INDIVIDUAL SIGN OFFS BELOW.;[03] PERFORMED PERMANENT REPAIR ON CARGO TRACK LOC. RBL 13.84 BETWEEN BS 727D MORE 12 INCH TO BS 747 MORE 12 INCH AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 53-00-53-2R-3 REPAIR 3 SEE INDIVIDUAL SIGN OFFS BELOW.<BR>RII VERIFIED

Part: SUPPORT CHANNEL — CORRODED (BS 767-794 S25R) · airframe 66,313 hrs · 39,674 cycles

CORROSION CHANNEL SUPPORT LOCATED BS767 TO BS794 AT LEVEL STR25R AND WL154 AFT CARGO COMPARTMENT 2024-270000<[01] REPLACED CHANNEL SUPPORT AND FASTENERS LOCATED BS767 TO BS794 AT LEVEL STR25R AND WL154 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A0081 SHEET 25 REV A.;[02] REPLACED CHANNEL SUPPORT AND FASTENERS LOCATED BS767 TO BS794 AT LEVEL STR25R AND WL154 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A0081 SHEET 25 REV A.;[03] REPLACED CHANNEL SUPPORT AND FASTENERS LOCATED BS767 TO BS794 AT LEVEL STR25R AND WL154 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A0081 SHEET 25 REV A.

Part: SUPPORT CHANNEL — CORRODED (BS 847-867 S25R) · airframe 66,313 hrs · 39,674 cycles

CORROSION CHANNEL SUPPORT LOCATED BS847 TO BS867 AT LEVEL STR25R AND WL154 AFT CARGO COMPARTMENT 2024-270003<[01] TOOL USED ON STEP 3 IS THICKNESS EQUIPMENT PN: 45MG; SN: 221860711; DUE DATE: 21-NOV-24;[02] REPLACED CHANNEL SUPPORT LOCATED BS847 TO BS867 AT LEVEL STR25R AND WL154 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A8120 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED CHANNEL SUPPORT LOCATED BS847 TO BS867 AT LEVEL STR25R AND WL154 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A8120 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: FRAME — CRACKED (BS 500A S8-9R) · airframe 66,313 hrs · 39,674 cycles

CRACK ON FRAME LOCATED BS 500A BTW STR 8R TO STR 9R AT PASSENGER CABIN 2024-270012<[01] PERFORMED PERMANENT REPAIR ON FRAME LOCATED BS 500A BTW STR 8R TO STR 9R AT PASSENGER CABIN IAW B737-700 EA 1-A53-12114. SEE INDIVIDUAL SING OFF BELOW;[02] PERFORMED PERMANENT REPAIR ON FRAME LOCATED BS 500A BTW STR 8R TO STR 9R AT PASSENGER CABIN IAW B737-700 EA 1-A53-12114. SEE INDIVIDUAL SING OFF BELOW<BR>COMPLETED RII VERIFIED

Part: STUB FRAME — CRACKED (BS 295 S17R) · airframe 66,313 hrs · 39,674 cycles

CRACK ON STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-270002<[01] NEW STUB FRAME; DEPRESSOR; STOP FITTING AND FASTENERS. LOCATED BS 294.5 BTW STR14R TO STR 17R AT FWD GALLEY AREA ANDIAW B737-700 SRM 51-10-02 STEP 9 AND SRM 51-40-02. DWG 141A8370 SHEET 10 REV D. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8370 SHEET 10 REV: D SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2: REPLACED STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8370 SHEET 10 REV: D SEE INDIVIDUAL SIGN OFF BELOW.;[04] RII COMPLETED JOB

Part: ANGLE — CRACKED (BS 867 S2-3R) · airframe 66,313 hrs · 39,674 cycles

CRACK ON ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-270014<[01] REPLACED ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER IAW B737-700 SRM 51-40-02; DWG N:146A7901 SHEET: 58 REV:- AND IAWB737-700 SRM 51-10-02 Ï¿½TEM 9 .;[02] REPLACED ANGLE LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER IAW B737-700 SRM 51-40-02; DWG N:146A7901 SHEET: 58 REV:- AND IAWB737-700 SRM 51-10-02 Ï¿½TEM 9 .<BR>COMPLETED.

Part: SUPPORT ANGLE — CRACKED (BS 907-927) · airframe 66,313 hrs · 39,674 cycles

CRACK ANGLE - SUPPORT LOCATED BS907 TO BS927 BTW STR27R TO STR25R AT AFT CARGO COMPARTMENT (2 EA) 2024-270004<[01] REPLACED ANGLE - SUPPORTS LOCATED BS907 TO BS927 BTW STR27R TO STR25R AT AFT CARGO COMPARTMENT (2 EA) I.A.W B737-700 SRM 51-40-02 DWG 147A7221 REV. D SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE - SUPPORTS LOCATED BS907 TO BS927 BTW STR27R TO STR25R AT AFT CARGO COMPARTMENT (2 EA) I.A.W B737-700 SRM 51-40-02 DWG 147A7221 REV. D SEE INDIVIDUAL SIGN OFF BELOW. JOB COMPLETED.

Part: TIE CLIP — CRACKED (BS 277 S10R) · airframe 66,313 hrs · 39,674 cycles

CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2024-270010<[01] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; DRAWING 141A1110 SHEET 18 REV.-. AND DRAWING 141A8380 SHEET 14 REV.-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; DRAWING 141A1110 SHEET 18 REV.-. AND DRAWING 141A8380 SHEET 14 REV.-. SEE INDIVIDUAL SIGN OFF BELOW.RII ITEM

Part: INTERCOSTAL — CRACKED (BS500A-500B S26R) · airframe 66,313 hrs · 39,674 cycles

CRACK WEB - INTERCOSTAL LOCATED BTW BS 500A TO BS 500B AT LEVEL STR 26R AT FWD CARGO COMPARTMENT 2024-269968<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW BS 500A TO BS 500B AT LEVEL STR 26R AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG: 143A7505 SHEET: 6 REV: D; SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB - INTERCOSTAL LOCATED BTW BS 500A TO BS 500B AT LEVEL STR 26R AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG: 143A7505 SHEET: 6 REV: D; SEE INDIVIDUAL SIGN OFF BELOW

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 66,313 hrs · 39,674 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-269966<[01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: B20189531 DUE DATE: 26-JAN-25.;[02] TOOL USED STEP 4 RADIOMETER PHOTOMETER KIT PN: XRP-3000; SN: 1998072; DUE DATE: 16-MAY-24;[03] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT.IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFFS BELOW;[04] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT.IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFFS BELOW

Part: ANGLE — CRACKED (BS 400 S26L) · airframe 66,313 hrs · 39,674 cycles

CRACK ON CLIP ANGLE LOCATED BS 400 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-269965<[01] REPLACED CLIP ANGLE AND FASTENERS LOCATED ON BS 400 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 TEM 9 AND DRAWING 143A7505 SHEET 2 REV B. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED CLIP ANGLE AND FASTENERS LOCATED ON BS 400 AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 TEM 9 AND DRAWING 143A7505 SHEET 2 REV B. VERIFIED

Part: GUSSET — CRACKED (BS 500D-S19L) · airframe 66,313 hrs · 39,674 cycles

CRACK GUSSET LOCATED BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT 2024-269967<[01] REPLACED GUSSET LOCATED BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; DWG: 143A7902; SHEET: 174; REV: -; SEE INDIVIDUAL SIGN OFF BELOW.;[02] COMPLETED JOB

Part: SHIELD — CORRODED (BS 500-500A) · airframe 66,313 hrs · 39,674 cycles

CORROSION ON SHIELD PLATE LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26R WL 156 AT FWD CARGO COMPARTMENT 2024-269950<[01] REPLACED SHIELD PLATE AND FASTENERS LOC. BTW BS 492.4 TO BS 500A AT LEVEL STRG 26R WL 156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SHIELD PLATE AND FASTENERS LOC. BTW BS 492.4 TO BS 500A AT LEVEL STRG 26R WL 156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080 REV -. SEE INDIVIDUAL SIGN OFF BELOW. COMPLETED

Part: PRESSURE DECK — CRACKED (BS 663 RBL 14) · airframe 66,313 hrs · 39,674 cycles

CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 41 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.187 INCH 2024-269953<[01] TOOL USED ON STEP 5: EDDY CURRENT EQUIPMENT. P/N NORTEC 600D S/N 210136503 DUE DATE 23-MAY-24;[02] PERFORMED PERMANENT REPAIR ON PRESSURE DECK WEB RBL 30 TO RBL 60 STA 663 TO STA 675 AT PASSENGER CABIN IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2; SEE INDIVIDUAL SIGNOFF BELOW;[03] PERFORMED PERMANENT REPAIR ON PRESSURE DECK WEB RBL 30 TO RBL 60 STA 663 TO STA 675 AT PASSENGER CABIN IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2; SEE INDIVIDUAL SIGNOFF BELOW

Part: PRESSURE DECK — CRACKED (BS 663 LBL38) · airframe 66,313 hrs · 39,674 cycles

CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 38 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.187 IN 2024-269954<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[02] PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK WEB BTW LBL 25 TO LBL 65 AND BTW BS STA 663 TO BS 685 AT PASSENGER CABIN I.A.W B737-700 SRM 53-40-51-2R-2 REPAIR 2; SRM 51-40-02-0G-0; DWG# 144A7700; SHEET 132; REV.C. AND DWG# 144A7710; SHEET 99; REV.A. SEE INDIVIDUAL SIGN OF BELOW.;[03] RII COMPLETED JOB

Part: FLOORBEAM — CRACKED (BS 540) · airframe 66,313 hrs · 39,674 cycles

CRACK ON INTERCOSTAL LOCATED BS 540 BTW RBL 1 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN 2024-269923<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED BS 540 BTW RBL 1 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 143A0060 REV-A.;[02] REPLACED INTERCOSTAL AND FASTENERS LOCATED BS 540 BTW RBL 1 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 143A0060 REV-A. SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED WORK PERFORMED

Part: ANGLE — CRACKED (BS 695 BL 0) · airframe 66,313 hrs · 39,674 cycles

CRACK ON ANGLE LOCATED BS 695 BL 0 AFT POSITION RT SIDE AT PASSENGER CABIN 2024-269927<[01] REPLACED ANGLE LOCATED BS 695 BL 0 AFT POSITION RT SIDE AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND DWG 273A9110 SHEET 6. REV. A. SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED ANGLE LOCATED BS 695 BL 0 AFT POSITION RT SIDE AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND DWG 273A9110 SHEET 6. REV. A. SEE INDIVIDUAL SIGNOFF BELOW<BR>COMPLETED TASK

Part: ANGLE — CRACKED (BS 695 RBL 25) · airframe 66,313 hrs · 39,674 cycles

CRACK ON ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN 2024-269925<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-25.;[02] REPLACED ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG:273A9110 REV:A SHEET:6 SEE INDIVIDUAL SIGNS OFF BELOW;[03] REPLACED ANGLE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG:273A9110 REV:A SHEET:6 SEE INDIVIDUAL SIGNS OFF BELOW

Part: ANGLE — CRACKED (BS 695 BL0) · airframe 66,313 hrs · 39,674 cycles

CRACK ON ANGLE LOCATED BS 695 BL 0 FWD POSITION RT SIDE AT PASSENGER CABIN 2024-269926<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-25.;[02] REPLACED ANGLE LOCATED BS 695 BL 0 FWD POSITION RT SIDE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING #273A9110 . REV ?A? SEE INDIVIDUAL SIGN OFF BELOW.;[03] CERTIFIED WORK PERFORMED

Part: FLOORBEAM — CRACKED (BS 540 BL0-LBL25) · airframe 66,313 hrs · 39,674 cycles

CRACK ON INTERCOSTAL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN 2024-269924<[01] REPLACED NEW INTERCOSTAL AND FASTENERS LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A0060 REV:A SHEET:36. SEE INDIVIDUAL SIGNS OFF BELOW.;[02] REPLACED NEW INTERCOSTAL AND FASTENERS LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A0060 REV:A SHEET:36. SEE INDIVIDUAL SIGNS OFF BELOW.

Part: SKIN — CRACKED (RT NR 1 SLAT) · airframe 66,313 hrs · 39,674 cycles

CRACK LOWER SKIN SLAT 1 AROUND THE FASTENERS THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 451.97 AT LT WING 2024-269876<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[02] STEP 7 . ET TOOL USED PN: MIZ-21C; SN: 769680; DUE DATE: 25-JUL-24.;[03] PERFORMED PERMANTENT REPAIR ON LOWER SKIN SLAT 1 AROUND THE FASTENERS THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 451.97 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REAPIR 8; SEE INDIVIDUAL SIGN OFF BELOW.;[04] RII COMPLETED JOB

Part: SKIN — CRACKED (RT NR 2 SLAT) · airframe 66,313 hrs · 39,674 cycles

CRACK SLAT 2 ON THE SKIN AROUND THE FASTENERS THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 322.71 AT LT WING 2024-269877<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[02] STEP 7 ET TOOL USED PN: MIZ-21C; SN: 769680; DUE DATE: 25-JUL-24.;[03] PERFORMED PERMANENT REPAIR ON SLAT 2 LOWER SKIN AROUND THE FASTENERS THAT ATTACH THE ACTUATOR FITTING AT SLAT STATION 322.71 AT LT WING IAW B737-700 57-42-01-2R-8 REAPIR 8; SEE INDIVIDUAL SIGN OFF BELOW.;[04] RII COMPLETED JOB

Part: FRAME — CRACKED (BS 260 S9R) · airframe 66,313 hrs · 39,674 cycles

CRACK ON FRAME AT LEVEL OF BS259.5 AND S-9R FLIGHT COMPARTMENT. 2024-269873<[01] TOOL USED ON STEP 6: EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030457 DUE DATE: 15 OCT 24.;[02] REPAIRED FRAME - WEB AT BSTA 259.5 - BTW WL 240 & WL 280 AND BTW RBL 20 AND RBL 50 IAW EA # 24-153-01082-WIP1 AND EA# 24-153-01082 SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPAIRED FRAME - WEB AT BSTA 259.5 - BTW WL 240 & WL 280 AND BTW RBL 20 AND RBL 50 IAW EA # 24-153-01082-WIP1 AND EA# 24-153-01082 SEE INDIVIDUAL SIGNOFF BELOW. CERTIFIED AS RII

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 66,313 hrs · 39,674 cycles

CRACK ON CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT 2024-269848<[01] TOOL USED: DIGITAL CALIPER P/N: 500-196-30; S/N: A23325649; DUE DATE: 31-DEC-24.;[02] ON STEP 4. TOOL USED RADIOMETER/PHOTOMETER KIT; P/N:XRP-3000; S/N:1859843; DUE DATE:24/JUL/24.;[03] REPAIRED CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1; BAC 5975; SOPM 20-20-02; SOPM 20-30-03 AND SOPM 20-41-02. SEE INDIVIDUAL SIGNOFF BELOW.;[04] JOB TASK COMPLETED.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,313 hrs · 39,674 cycles

DOES NOT PASS TEST EMERGENCY LIGHTING BATTERY PACK CAPACITY (M1669) AT MIDLE PAX CABIN 2024-269771<[01] REPLACED EMERGENCY LIGHTING POWER SUPPLY BATTERY PACK (M1669) AT MIDDLE PAX CABIN I.A.W B737-700 AMM 33-51-06-960-805. TEST IS OK.;[02] CERTIFIED STEP 1 COMPLETED

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,313 hrs · 39,674 cycles

DOES NOT PASS TEST EMERGENCY LIGHTING BATTERY PACK CAPACITY (M1673) AT AFT PAX CABIN 2024-269773<[01] REPLACED EMERGENCY LIGHTING POWER SUPPLY BATTERY PACK (M1673) AT AFT PAX CABIN I.A.W B737-700 AMM 33-51-06-960-805. TEST IS OK. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,313 hrs · 39,674 cycles

DOES NOT PASS TEST EMERGENCY LIGHTING BATTERY PACK CAPACITY (M1668) AT MIDLE PAX CABIN 2024-269770<[01] REPLACED EMERGENCY LIGHTING POWER SUPPLY BATTERY PACK (M1668) AT MIDDLE PAX CABIN I.A.W B737-700 AMM 33-51-06-960-805. TEST IS OK.;[02] CORRECTED STEP 1.<BR>REPLACED EMERGENCY LIGHTING POWER SUPPLY BATTERY PACK (M1668) AT MIDDLE PAX CABIN I.A.W B737-700 AMM 33-51-06-960-805. TEST IS OK. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CERTIFIED STEP 2 COMPLETED

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,313 hrs · 39,674 cycles

DOES NOT PASS TEST EMERGENCY LIGHTING BATTERY PACK CAPACITY (M1675) AT FWD PAX CABIN 2024-269768<[01] REPLACED EMERGENCY LIGHTING POWER SUPPLY BATTERY PACK (M1675) AT FWD PAX CABIN I.A.W B737-700 AMM 33-51-06-960-805. TEST IS OK. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,313 hrs · 39,674 cycles

DOES NOT PASS TEST EMERGENCY LIGHTING BATTERY PACK CAPACITY (M1674) AT FWD PAX CABIN 2024-269767<[01] REPLACED EMERGENCY LIGHTING POWER SUPPLY BATTERY PACK (M1674) AT FWD PAX CABIN I.A.W B737-700 AMM 33-51-06-960-805. TEST IS OK. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,313 hrs · 39,674 cycles

DOES NOT PASS TEST EMERGENCY LIGHTING BATTERY PACK CAPACITY (M1670) AT STA 727C+13 LT SIDE PAX CABIN 2024-269769<[01] REPLACED EMERGENCY LIGHTING POWER SUPPLY BATTERY PACK (M1670) AT STA 727C+13 LT SIDE PAX CABIN I.A.W B737-700 AMM 33-51-06-960-805. TEST IS OK. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,313 hrs · 39,674 cycles

DOES NOT PASS TEST EMERGENCY LIGHTING BATTERY PACK CAPACITY (M1672) AT AFT PAX CABIN 2024-269772<[01] REPLACED EMERGENCY LIGHTING POWER SUPPLY BATTERY PACK (M1672) AT AFT PAX CABIN I.A.W B737-700 AMM 33-51-06-960-805. TEST IS OK. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED

Part: COFFEEMAKER — SMOKE (ZN 200 FUS TOP) · airframe 64,371 hrs · 38,477 cycles

FWD COFFEE MAKER SMELLS OF ELECTRIC OZONE TYPE ODER. NO SMOKE NOTED<[01] REMOVED AND REPLACED FWD COFFEE MAKER REF. AMM 25-30-01 OPS AND LEAK CHECK GOOD

Part: HANDLE — MISSING (ZN 800 DOOR) · airframe 64,201 hrs · 38,368 cycles

FWD CARGO DOOR ASSIST HANDLE ASSY MISSING<[01] INTALLED CARGO DOOR ASSIST HANDLE ASSEMBLY PER AMM 52-31-00

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,238 hrs · 37,764 cycles

ROW 16DEF AND 18DEF EMERGENCY AISLE LIGHTS INOP<[01] SLAVED IN AFT R/H EMERGENCY NEW POWER PACK AND NEW BATTERY PER AMM 33-51-06. NO FIX.;[02] REF WDM 33-51-14 FOUND HOUSING ASSY AT ROW 16 SHORTED INTERNALLY CAUSING FUSE IN CHARGER M1672 TO BLOW. REF AMM 33-51-06 REPLACED FUSE ; REF AMM 33-51-03 REPLACED HOUSING ASSY. LIGHTS OP?S NORMAL

Part: HANGER ASSY — LOOSE (GIRT BAR) · airframe 62,343 hrs · 37,185 cycles

FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE COMPT. FWD GRIT BAR HANGER LOOSE.<[01] RE-SECURED FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE COMPT FWD GIRT BAR REF AMM SIP.

Part: FLOOR PANEL — POPPED (FUSELAGE) · airframe 60,334 hrs · 35,829 cycles

FLOOR FLEXES AT ROW 7 AND POPS / [01] CW EA 22-153-01427 - PERMANENT REPAIR REQUIRED IN 10FC

Part: LIGHT — BROKEN (CABIN) · airframe 60,200 hrs · 35,739 cycles

BROKEN EMERGENCY EXIT LIGHT COVER LENS LOCATED ON SIDEWALL PANEL 232YHW LH SIDE AT PASSENGER CABIN (1 EA) 2022-158752 / [01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT COVER LENS LOCATED ON SIDEWALL PANEL 231YHW LH SIDE AT PASSENGER CABIN (1 EA) AMM 33-51-01-960-802-NG STEP 33-51-01-960-802 STEP 3C(5)(D) AND 3C(10);[02] REMOVED AND REPLACED EMERGENCY EXIT LIGHT COVER LENS LOCATED ON SIDEWALL PANEL 231YHW LH SIDE AT PASSENGER CABIN (1 EA) AMM 33-51-01-960-802-NG STEP 33-51-01-960-802 STEP 3C(5)(D) AND 3C(10)

Part: STRAP — CORRODED (AFT CARGO) · airframe 60,200 hrs · 35,739 cycles

CORROSION STRAP BTW FLOOR PANELS AT AFT CARGO COMPARTMENT 2022-158717 / [01] REPLACED STRAP BTW FLOOR PANELS AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DRAWING 146A9401 REV C SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED STRAP BTW FLOOR PANELS AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DRAWING 146A9401 REV C SEE INDIVIDUAL SIGN OFF BELOW<BR>RII

Part: WEB — CORRODED (FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

CORROSION WEB - INTERCOSTAL BETWEEN STA 747 TO STA 767 RBL 33.5; FLOOR STRUCTURE AT AFT CARGO COMPARTMENT 2022-158716 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23;[02] REPLACED WEB - INTERCOSTAL BETWEEN STA 747 TO STA 767 RBL 33.5; FLOOR STRUCTURE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING # 146A7500 REV: - SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED WEB - INTERCOSTAL BETWEEN STA 747 TO STA 767 RBL 33.5; FLOOR STRUCTURE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING # 146A7500 REV: - SEE INDIVIDUAL SIGN OFF BELOW AS RII

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 60,200 hrs · 35,739 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2022-158718 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A18135080; DUE DATE: 31-JUL-22.;[02] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SUPPORT ANGLE — CORRODED (AFT CARGO) · airframe 60,200 hrs · 35,739 cycles

CORROSION ANGLE - SUPPORT LOCATED IN STA 947 BTW STRG 24R TO STRG 25R; FLOOR STRUCTURE AT AFT CARGO COMPARTMENT 2022-158714 / [01] REPLACED ANGLE - SUPPORT LOCATED IN STA 947 BTW STRG 24R TO STRG 25R; FLOOR STRUCTURE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING 149A8117 SHEET 6 REV - SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE - SUPPORT LOCATED IN STA 947 BTW STRG 24R TO STRG 25R; FLOOR STRUCTURE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING 149A8117 SHEET 6 REV - SEE INDIVIDUAL SIGN OFF BELOW<BR>RII

Part: WEB — CRACKED (AFT CARGO) · airframe 60,200 hrs · 35,739 cycles

CRACK WEB - INTERCOSTAL BTW STA 927 TO STA 947 RBL 33.5; FLOOR STRUCTURE AT AFT CARGO COMPARTMENT 2022-158715 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[02] REPLACED WEB INTERCOSTAL LOCATED BTW STA 927 TO STA 947 RBL 33.5; FLOOR STRUCTURE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 AND DRAWING 147A7500 SHEET 18 REV.-;[03] JOB COMPLETED AND CERTIFIED AS RII.

Part: ANGLE — CRACKED (R/H MLG W/W) · airframe 60,200 hrs · 35,739 cycles

(CUSTOMER REQUEST) CRACK ON VERTICAL ANGLE LOC ON MAIN LANDING GEAR COMPARTMENT BS663 AND RBL 28 AT LOWER FUSELAGE 2022-158634 / [01] REPLACED VERTICAL ANGLE LOC ON MAIN LANDING GEAR COMPARTMENT BS663 AND RBL 28 AT LOWER FUSELAGE IAW B737-700 SRM-51-10-02 ITEM 9 AND DWG-11A1000 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK CARD COMPLETED <BR>RII<BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: ANGLE — CRACKED (L/H MLG W/W) · airframe 60,200 hrs · 35,739 cycles

(CUSTOMER REQUEST) CRACK ON VERTICAL ANGLE LOC ON MAIN LANDING GEAR COMPARTMENT BS663 AND LBL 28 AT LOWER FUSELAGE 2022-158633 / [01] REPLACED VERTICAL ANGLE AND FASTENERS LOC ON MAIN LANDING GEAR COMPARTMENT BS663 AND LBL 28 AT LOWER FUSELAGE I.A.W B737-700 SRM 51-10-02 ITEM 9 ; DWG 111A1000 REV- AND DWG 149A7210 REV- .;[02] REPLACED VERTICAL ANGLE AND FASTENERS LOC ON MAIN LANDING GEAR COMPARTMENT BS663 AND LBL 28 AT LOWER FUSELAGE I.A.W B737-700 SRM 51-10-02 ITEM 9 ; DWG 111A1000 REV- AND DWG 149A7210 REV- ... RII ITEM

Part: SUPPORT ANGLE — CORRODED (FWD FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

CORROSION ANGLE - SUPPORT LOCATED BETWEEN BS 303 AND BS 344 S-17L WL 208.1 AT FWD GALLEY AREA 2022-158538 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N:130064101 DUE DATE: 11-MAR-22;[02] REPLACED ANGLE - SUPPORT LOCATED BETWEEN BS 303 AND BS 344 S-17L WL 208.1 AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DRAWING 141A8110 SHEET 11 REV -;[03] CORRECTED STEP 2. REPLACED ANGLE - SUPPORT LOCATED BETWEEN BS 303 AND BS 344 S-17L WL 208.1 AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DRAWING 141A8110 SHEET 11 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPLACED ANGLE - SUPPORT LOCATED BETWEEN BS 303 AND BS 344 S-17L WL 208.1 AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DRAWING 141A8110 SHEET 11 REV - ITEM RII <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

CORROSION FLOOR STRUCTURE BEAM STA 986.5 LBL 42 WL208.1 AT AFT GALLEY AREA 2022-158500 / [01] TOOL USED ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 130066401; CAL DUE DATE: 17-JUN-22;[02] TOOL USED EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:190023010; DUE DATE:14-FEB-23;[03] TOOL USED EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:190023010; DUE DATE:14-FEB-23.;[04] TOOL USED FLAP SPEED PN: FPK-PRO-104; SN: PRO-3448; DUE DATE: 18-NOV-22;[05] PERFORMED PERMANENT REPAIR ON FLOOR STRUCTURE BEAM STA 986.5 LBL 42 WL208.1 AT AFT GALLEY AREA I.A.W. B737-700 SRM 53-70-51-2R-6. SEE INDIVIDUAL SIGN OFFS BELOW;[06] PERFORMED PERMANENT REPAIR ON FLOOR STRUCTURE BEAM STA 986.5 LBL 42 WL208.1 AT AFT GALLEY AREA I.A.W. B737-700 SRM 53-70-51-2R-6. RII .SEE INDIVIDUAL SIGN OFFS BELOW

Part: WEB — CRACKED (FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 RBL 31 FWD GALLEY AND LAV 2022-158490 / [01] REPLACED WEB LOCATED ON FLOOR STRUCTURE BETWEEN BS 312 AND BS 328 RBL 31 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; 51-10-02 AND DGW 141A5400 REV-;[02] CORRECTED STEP 1 REPLACED WEB LOCATED ON FLOOR STRUCTURE BETWEEN BS 312 AND BS 328 RBL 31 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; 51-10-02 AND DWG 141A5400 REV-;[03] CORRECTED STEP 1 Y 2 REPLACED WEB LOCATED ON FLOOR STRUCTURE BETWEEN BS 312 AND BS 328 RBL 31 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; 51-10-02 AND DWG 141A5400 REV- SEE INDIVIDUAL SIGN OFF BELOW;[04] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: TRACK — CRACKED (AFT CARGO) · airframe 60,200 hrs · 35,739 cycles

CRACK TRACK RBBL 13.84 BS 767 AT AFT CARGO COMPARTMENT 2022-158459 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 03-DEC-22.;[02] REPAIRED TRACK SECTION LOC. RBL 13.84 BS 747 MORE 11 INCHES TO BS 767 MORE 10 I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 AND ALTERNATIVE 2 AND SRM 51-40-02 SEE INDIVIDUAL SIGN OFF BELOW;[03] REPAIRED TRACK SECTION LOC. RBL 13.84 BS 747 MORE 11 INCHES TO BS 767 MORE 10 I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 AND ALTERNATIVE 2 AND SRM 51-40-02 SEE INDIVIDUAL SIGN OFF BELOW AS RII

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

CORROSION FLOOR STRUCTURE INNER CHORD LOCATED BETWEEN BS 947 AND BS 986.5 AT LEVEL S-17R WL208.1 AT AFT GALLEY AREA 2022-158501 / [01] REPLACED INNER CHORD AND FASTENERS LOC BTW BS 887 TO BS 1006 APROX AT RBL 47 AND WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A8501 SHEET 80 REV ?A?. SEE INDIVIDUAL SING OFFS BELOW.;[02] REPLACED INNER CHORD LOC BTW BS 887 TO BS 1006 APROX AT RBL 47 AND WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A8501 SHEET 80 REV ?A?. SEE INDIVIDUAL SING OFFS BELOW.;[03] REPLACED INNER CHORD LOC BTW BS 887 TO BS 1006 APROX AT RBL 47 AND WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 147A8501 SHEET 80 REV ?A?. SEE INDIVIDUAL SING OFFS BELOW. RII

Part: WEB — CRACKED (FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 AND BS 360 LBL12 FWD GALLEY AND LAV 2022-158489 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 AND BS 360 LBL12 FWD GALLEY AND LAV. IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 141A5400; REV A. SEE INDIVIDUAL SINGN OFF BELOW;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 AND BS 360 LBL12 FWD GALLEY AND LAV. IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 141A5400; REV A. SEE INDIVIDUAL SINGN OFF BELOW

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL 46 FWD GALLEY AND LAV 2022-158494 / [01] REPLACE WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL 46 FWD GALLEY AND LAV I.A.W. B737-700 SRM 51-10-02 AND DWG DWG 141A5400 SHEET:26 REV: -.;[02] CORRECTED STEP 1. REPLACE WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL 46 FWD GALLEY AND LAV I.A.W. B737-700 SRM 51-10-02 AND DWG DWG 141A5400 SHEET:26 REV: -. SEE INDIVIDUAL SING OFFS BELOW.;[03] REPLACE WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL 46 FWD GALLEY AND LAV I.A.W. B737-700 SRM 51-10-02 AND DWG DWG 141A5400 SHEET:26 REV: -. <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SING OFFS BELOW.

Part: PLATE — CORRODED (CORRODED) · airframe 60,200 hrs · 35,739 cycles

CORROSION FLOOR STRUCTURE PLATE LOCATED BS 1028 LBL 3 WL208.1 AT AFT GALLEY AREA 2022-158499 / [01] REPLACED FLOOR STRUCTURE PLATE LOCATED BS 1028 LBL 3 WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-10-02 AND 51-40-02 AND DWG 147A5600 SHEET 32 REV.B<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED FLOOR STRUCTURE PLATE LOCATED BS 1028 LBL 3 WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-10-02 AND 51-40-02 AND DWG 147A5600 SHEET 32 REV.B <BR>SEE INDIVIDUAL SIGN OFF BELOW CERTIFIED AS RII <BR>TASK COMPLETED

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 328 AND BS 344 LBL 46 FWD GALLEY AND LAV 2022-158495 / [01] REPLACE WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 328 AND BS 344 LBL 46 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET:44 REV: -. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACE WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 328 AND BS 344 LBL 46 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET:44 REV: -. <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGN-OFF BELOW.

Part: LENS — BROKEN (R/H CABIN) · airframe 60,200 hrs · 35,739 cycles

BROKEN EMERGENCY EXIT LIGHT COVER LENS LOCATED ON SIDEWALL PANEL 232YHW RH SIDE AT PASSENGER CABIN (1 EA) 2022-158487 / [01] REPLACED EMERGENCY EXIT LIGHT COVER LENS LOCATED ON SIDEWALL PANEL 232YHW RH SIDE AT PASSENGER CABIN (1 EA) IAW BOEING 737-700 AMM-33-51-01-960-802 STEP 3. C. ITEM (9) AND (10);[02] REPLACED EMERGENCY EXIT LIGHT COVER LENS LOCATED ON SIDEWALL PANEL 232YHW RH SIDE AT PASSENGER CABIN (1 EA) IAW BOEING 737-700 AMM-33-51-01-960-802 STEP 3. C. ITEM (9) AND (10)

Part: WEB — CRACKED (FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 277 AND BS 294.5 BL 0 FWD GALLEY AND LAV 2022-158492 / [01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 277 AND BS 294.5 BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9; DRAWING 141A5400 SHEET 20 REV -. AND SRM 51-40-02;SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 277 AND BS 294.5 BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9; DRAWING 141A5400 SHEET 20 REV -. AND SRM 51-40-02;SEE INDIVIDUAL SIGNOFFS BELOW.<BR>RII

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 60,200 hrs · 35,739 cycles

CORROSION ON SUPPORT ZEE CHANNEL LOC BETWEEN BS767 AND BS 807 AT LEVEL STR 26L AND LBL 21 AT AFT CARGO COMPARTMENT 2022-158389 / [01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS727 TO BS 847 AT LEVEL STR 26L AND LBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9 AND DWG 146A7500 SHEET 61 REV -SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED SUPPORT ZEE LOCATED BETWEEN BS727 TO BS 847 AT LEVEL STR 26L AND LBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9 AND DWG 146A7500 SHEET 61 REV -SEE INDIVIDUAL SIGNOFF BELOW. RII

Part: ACCESS PANEL — CRACKED (L/H PYLON) · airframe 60,200 hrs · 35,739 cycles

CRACK ACCESS PANEL 431AR SEAL PLATE AT LT PYLON 2022-158433 / [01] REPLACED SEAL PLATE ON ACCESS PANEL 431AR AT LT PYLON I.A.W SRM 51-10-02;[02] TASK COMPLETED

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 60,200 hrs · 35,739 cycles

CORROSION ON SUPPORT ZEE CHANNEL LOCATED BETWEEN BS 747 AND BS 767 AT LEVEL STR 26R AND RBL 21 AT AFT CARGO COMPARTMENT 2022-158388 / [01] REPLACED COMPLETE SUPPORT ZEE SECTION LOCATED BTW BS727 TO BS767 AT LEVEL STR 26R AND RBL 21 AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 PARAGRAPH 9. MADE AND DRILLED SUPPORT ZEE SECTION IAW B737-700 SRM 51-40-05 AND DWG 146A7502 SHEET 2 REV A. APPLIED PROTECTIVE TREATMENT IAW B737-700 SRM 51-20-01 AND INSTALLED NUT PLATES IAW DWG 140N4500 REV G.;[02] CORRECTED STEP 1. REPLACED COMPLETE SUPPORT ZEE SECTION LOCATED BTW BS727 TO BS767 AT LEVEL STR 26R AND RBL 21 AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 PARAGRAPH 9. MADE AND DRILLED SUPPORT ZEE SECTION IAW B737-700 SRM 51-40-05 AND DWG 146A7502 SHEET 2 REV A. APPLIED PROTECTIVE TREATMENT IAW B737-700 SRM 51-20-01 AND INSTALLED NUT PLATES IAW DWG 140N4500 REV G. SEE INDIVIDUAL SIGN OFF BELOW.;[03] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: LIGHT — BROKEN (AFT GALLEY) · airframe 60,199 hrs · 35,739 cycles

BROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) 2022-158418 / [01] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) IAW BOEING 737-700 AMM-33-23-00-960-801 STEP 4. C (1) (6);[02] CORRECTED STEP 1 : REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) IAW BOEING 737-700 AMM-33-23-00-960-801 STEP 4. C 1 (A) AND (C);[03] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) IAW BOEING 737-700 AMM-33-23-00-960-801 STEP 4. C 1 (A) AND (C)

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

CRACK ACCESS PANEL 193AR AT FUSELAGE EXTERIOR 2022-158379 / [01] TOOL USED: CALIPER P/N:500-464 S/N:B17030933 DUE DATE:01-OCT-22.;[02] TOOL USED: HOT BONDER. P/N:HCS9200B-AV S/N:18196127 DUE DATE:16/JAN/23.;[03] TOOL USED: SCALE P/N:CL5000 S/N:AE-39085 DUE DATE:03-SEP-22;[04] TOOL USED:SCALE P/N:CL5000 S/N:AE-409561 DUE DATE:24-MAY-22;[05] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18175478 DUE DATE:05-AUG-22;[06] REPAIRED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-04-2R-2 REPAIR 2. SEE INDIVIDUAL SIGN OFFS BELOW.;[07] REPAIRED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-04-2R-2 REPAIR 2. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: PLATE — CRACKED (VERT. STAB.) · airframe 60,200 hrs · 35,739 cycles

CRACK ACCESS PANEL 323BL PLATE VERTICAL STABILIZER 2022-158366 / [01] REPLACED PLATE LOCATED ON ACCESS PANEL 323BL VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 AND DRAWING 172A6120 SHEET 1 REV ?F?. SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED PLATE LOCATED ON ACCESS PANEL 323BL VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 AND DRAWING 172A6120 SHEET 1 REV ?F?. SEE INDIVIDUAL SIGNOFFS BELOW

Part: ANGLE — CRACKED (LT WING) · airframe 60,200 hrs · 35,739 cycles

CRACK ANGLE TRAILING EDGE REAR SPAR LOCATED ON ORSS 274 AT LT WING 2022-158323 / [01] REPLACED ANGLE TRAILING EDGE REAR SPAR LOCATED ON ORSS 274 AT LT WING IAW B737-700 SRM-51-10-02 ITEM 9 AND DWG-115A2930 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK CARD COMPLETED <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: ANGLE — CRACKED (R/H WING) · airframe 60,200 hrs · 35,739 cycles

CRACK REAR SPAR ANGLE LOCATED BETWEEN WS253 TO WS278 AT RT WING 2022-158299 / [01] REPLACED REAR SPAR ANGLE LOCATED BETWEEN WS253 TO WS278 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A6200;[02] REPLACED REAR SPAR ANGLE LOCATED BETWEEN WS253 TO WS278 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A6200;[03] REPLACED REAR SPAR ANGLE LOCATED BETWEEN WS253 TO WS278 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02.;[04] REPLACED REAR SPAR ANGLE LOCATED BETWEEN WS253 TO WS278 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02;[05] TASK COMPLETED

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

CRACK STRINGER 15L BETWEEN BS 294.5 AND BS 303 AT PASSENGER CABIN 2022-158277 / [01] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 03-DEC-22.;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[03] PERFORMED REPAIR ON STRINGER 15L BETWEEN BS 294.5 AND BS 303 AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; FIGURE 206; SHEET 1; 2 ;TABLE 201; SEE INDIVIDUAL SIGN OFF BELOW;[04] PERFORMED REPAIR ON STRINGER 15L BETWEEN BS 294.5 AND BS 303 AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; FIGURE 206; SHEET 1; 2 ;TABLE 201; SEE INDIVIDUAL SIGN OFF BELOW AS RII

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

CRACK FRAME ON BS 312 LOCATED AT LEVEL FWD UPPER DOOR CUT OUT LH SIDE AT FWD GALLEY AREA 2022-158274 / [01] TOOL USED : EDDY CURRENT TOOL; P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 02 JUN 22.;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 02-FEB-23. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 02-FEB-23;[03] PERFORMED REPAIR ON FRAME ON BS 312 LOCATED AT LEVEL FWD UPPER DOOR CUT OUT LH SIDE AT FWD GALLEY AREA IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 SEE INDIVIDUAL SIGNOFFS BELOW;[04] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: BRACKET — BROKEN (FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

BROKEN SUPPORT BRACKET INSULATOR LOCATED BS685 AND BETWEEN STR12R TO STR14R AT PASSENGER CABIN 2(EA) 2022-158318 / [01] REPLACED SUPPORT BRACKET INSULATOR LOCATED BS685 AND BETWEEN STR12R TO STR14R AT PASSENGER CABIN 2(EA) IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING 144A1401 REV -;[02] REPLACED SUPPORT BRACKET INSULATOR LOCATED BS685 AND BETWEEN STR12R TO STR14R AT PASSENGER CABIN 2(EA) IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING 144A1401 REV -

Part: NONE — CRACKED (LH WING) · airframe 60,200 hrs · 35,739 cycles

CRACK CORRUGATED PLATE TRAILING EDGE REAR SPAR LOCATED ON ORSS 261 AT LT WING 2022-158331 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE REAR SPAR LOCATED ON ORSS 261 AT LT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 115A2001 SHEET 29 REV -. SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED CORRUGATED PLATE TRAILING EDGE REAR SPAR LOCATED ON ORSS 261 AT LT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 115A2001 SHEET 29 REV -. SEE INDIVIDUAL SIGNOFFS BELOW

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 60,200 hrs · 35,739 cycles

CRACK REAR SPAR SUPPORT ANGLE LOCATED WS278.50 AT RT WING 2022-158305 / [01] REPLACED REAR SPAR SUPPORT ANGLE LOCATED WS278.50 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A6200.;[02] TASK COMPLETED

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 60,200 hrs · 35,739 cycles

CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2022-158279 / [01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWINGS 141A1110 REV - AND 141A8380 REV -;[02] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWINGS 141A1110 REV - AND 141A8380 REV -<BR>RII

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 60,200 hrs · 35,739 cycles

CRACK INSPAR RIB 120.30 LOCATED AT 9.5 INCHES FROM REAR SPAR AT LT HORIZONTAL STABILIZER 2022-158341 / [01] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101V022233 DUE DATE 02-JUN-22.;[02] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN. 60009161631; DUE DATE: 03-DEC-22;[03] PERFORMED REPAIR ON INSPAR RIB 120.30 LOCATED AT 9.5 INCHES FROM REAR SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 SEE INDIVIDUAL SIGNOFFS BELOW;[04] PERFORMED REPAIR ON INSPAR RIB 120.30 LOCATED AT 9.5 INCHES FROM REAR SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 CAT A<BR>SEE INDIVIDUAL SIGN OFF BELOW<BR>RII ACCOMPLISHED

Part: BRACKET — CRACKED (R/H WING) · airframe 60,200 hrs · 35,739 cycles

CRACK INBOARD TRAILING EDGE BRACKET LOCATED ON IRSS 140 AT RT WING 2022-158252 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500 D; S/N: N500X12101V022235; DUE DATE: 03-JUN-22.;[02] REPLACED BRACKET LOC ON INBOARD TRAILING EDGE ON IRSS 140 AT RT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING 115A2000 REV A SEE INDIVIDUALS SIGN OFF BELOW;[03] REPLACED BRACKET LOC ON INBOARD TRAILING EDGE ON IRSS 140 AT RT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING 115A2000 REV A SEE INDIVIDUALS SIGN OFF BELOW

Part: PLATE — CRACKED (R/H WING) · airframe 60,200 hrs · 35,739 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 226 AT RT WING 2022-158245 / [01] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ORSS 256 AT RT WING TRAILING EDGE IAW B737-700 SRM 51- 10-02 ITEM 9 AND DWG 115A2001 SHEET 30 REV A;[02] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ORSS 256 AT RT WING TRAILING EDGE IAW B737-700 SRM 51- 10-02 ITEM 9 AND DWG 115A2001 SHEET 30 REV A.SEE INDIVIDUAL SIGNOFF BELOW.;[03] TASK COMPLETED <BR>SEE INDIVIDUAL SIGNOFF BELOW

Part: PLATE — CRACKED (R/H WING) · airframe 60,200 hrs · 35,739 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 256 AT RT WING 2022-158246 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 256 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 29 REV -.;[02] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 256 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 29 REV -.

Part: ACCESS PANEL — CRACKED (L/H WING) · airframe 60,200 hrs · 35,739 cycles

CRACK ACCESS PANEL 544BB AT LT WING 2022-158116 / [01] TOOL USED: CALIPER P/N:500-464 S/N:15331926 DUE DATE:28-SEP-22.;[02] TOOL USED:SCALE P/N:CL5000 S/N:AE-39087 DUE DATE:07-JUL-22.;[03] REPAIRED ACCESS PANEL 544BB IAW B737-700 SRM 57-53-70-2R-5 REPAIR 5 TOOL USED: HOTBONDER PN: HCS9000B-AV; SN: 14081912; DUE DATE: 04-JUN-22 SEE INDIVIDUAL SIGNOFFS BELOW.;[04] TASK COMPLETED.

Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 60,200 hrs · 35,739 cycles

CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.000 INCH 2022-158170 / [01] TOOL USED CALIPER P/N 500-196-30 S/N A21029144 DUE DATE 07-OCT-22;[02] TOOL USED PN NORTEC 500D SN N500X1693P030456 DUE DATE 26-JAN-23;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N:600091631; DUE DATE:03-DEC-22.;[04] PERFORMED REPAIR ON LOWER IN-SPAR SKIN OF LH HORIZONTAL STABILIZER AT STATION 193.90 RIB; 16.50 INCH FROM FRONT SPAR IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11;[05] CORRECTED STEP 1 PERFORMED REPAIR ON LOWER IN-SPAR SKIN OF LH HORIZONTAL STABILIZER AT STATION 193.90 RIB; 16.50 INCH FROM FRONT SPAR IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11 SEE INDIVIDUAL SIGN OFF BELOW;[06] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: BRACKET — CRACKED (CENTER WING) · airframe 60,200 hrs · 35,739 cycles

CRACK BODY STATION 540 ON ANGLE AT AIR CONDITIONING BAY (L/H SIDE ) 2022-158146 / [01] REMOVED AND REPLACED BRACKET ASSY AT PNEUMATIC DUCT BODY STATION 540 LT AIR CONDITIONING BAY IAW SRM 51-40-02-0G-0 SEE INDIVIDUALS SING-OFFS BELOW.;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: LIGHT — BROKEN (CABIN) · airframe 60,200 hrs · 35,739 cycles

BROKEN EMERGENCY LIGHT LENS LOCATED ON OVERHEAD BIN RH AT PASSENGER CABIN (7 EA) 2022-158051 / [01] REPLACED EMERGENCY LIGHT LENS LOCATED ON OVERHEAD BIN RH AT PASSENGER CABIN (7 EA) IAW B737-700 AMM 33-51-03-960-801 STEP 2.D.(1) ITEM (A) AND (C);[02] REPLACED EMERGENCY LIGHT LENS LOCATED ON OVERHEAD BIN RH AT PASSENGER CABIN (7 EA) IAW B737-700 AMM 33-51-03-960-801 STEP 2.D.(1) ITEM (A) AND (C)

Part: LIGHT — CRACKED (CABIN) · airframe 60,200 hrs · 35,739 cycles

CRACK INDICATION ON EMERGENCY LIGHT LENS LOCATED ON OVERHEAD BIN LH AT PASSENGER CABIN (6 EA) 2022-158043 / [01] REPLACED INDICATION ON EMERGENCY LIGHT LENS LOCATED ON OVERHEAD BIN LH AT PASSENGER CABIN (6 EA) IAW B737-700 AMM 33-51-03-960-801 STEP 2.D.(1) ITEM (A) AND (C);[02] REPLACED INDICATION ON EMERGENCY LIGHT LENS LOCATED ON OVERHEAD BIN LH AT PASSENGER CABIN (6 EA) IAW B737-700 AMM 33-51-03-960-801 STEP 2.D.(1) ITEM (A) AND (C)

Part: CONNECTOR — INOPERATIVE (CABIN) · airframe 58,075 hrs · 34,486 cycles

RT HAND CABIN EMERGENCY LIGHTS POWERED BY MODULE M1669 INOP. FOUND CONNECTOR D10714 FOR MODULE M1669 NOT FULLY SECURED. RESECURED CONNECTOR D10714 IAW B737 AMM 33-51-06-960-806. OPS CHECKS GOOD.

Part: SKIN — CORRODED (LT WING) · airframe 58,075 hrs · 34,486 cycles

DOT 93-034 LH WING; WSTA 691.50+3 TO WSTA 691.5+6 AT STR L6 LOWER EXTERNAL SKIN HAS CORROSION. UT IAW NDT PART 4 51-00-00 PROC 2. ORIG .140' LOSS .007' REMAINING .133'. BLENDED TO REMOVE CORROSION AND VERIFIED WITH 10X MAG. VERIFIED MATERIAL LOSS TO BE .007' ORIGINAL .140' REMAINING .133' WITHIN LIMITS IAW SRM 57-20-01-1A-1. ROTO PEENED BLENDED AREA IAW SOPM 20-10-03. TREATED AND PRIMED IAW AMM 51-21-41 & 51-21-72.

Part: ATTACH ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 58,075 hrs · 34,486 cycles

CRACK INDICATION IN A/C BAY AT FWD SIDE OF BS 663 UPPER ANGLE AT RBL 9. CUT AND REMOVED ATTACH ANGLE IAW SRM 57-10-10-2R-5. PERFORMED DETAILED INSPECTION OF REPAIR AREA & UNDERLYING STRUCTURE, NO DEFECTS NOTED IAW SRM 57-10-10-2R-5 REPAIR 5. HFEC IAW NDT PART 6; 51-00-00 PROC 16. NO DEFECTS NOTED. FABRICATED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. TREATED AND PRIMED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. INSTALLED REPAIR IAW SRM 57-10-10-2R-5 REPAIR 5. CAP SEALED FASTENERS INSIDE FUEL TANK, FILLET SEALED AND CAP SEALED REPAIR IAW SRM 57-10-10-2R-5 REPAIR 5. ELECTRICAL BOND CHECK CHECKS GOOD.

Part: ATTACH ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 58,075 hrs · 34,486 cycles

CRACK INDICATION IN A/C BAY AT FORWARD SIDE OF STA 663 UPPER ANGLE AT LBL 9. CUT & REMOVED ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5. PERFORMED DETAILED INSPECTION OF REPAIR AREA & UNDERLYING STRUCTURE. NO DEFECTS NOTED IAW SRM 57-10-10-2R-5 REPAIR 5. HFEC IAW NDT PART 6; 51-00-00 PROC 16. NO DEFECTS NOTED. FABRICATED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. TREATED AND PRIMED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5 VERIFIED STEP 8. INSTALLED REPAIR IAW SRM 57-10-10-2R-5 REPAIR 5. CAP SEALED FASTENERS INSIDE FUEL TANK , FILLET SEALED AND CAP SEALED REPAIR IAW SRM 57-10-10-2R-5 REPAIR 5. REPAIR 5 ELECTRICAL BOND CHECK CHECKS GOOD.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 57,280 hrs · 34,015 cycles

AFT SVC DOOR EVAC SLIDE REQUIRES REPOSITIONING TO VIEW PRESSURE GUAGE / REMOVED AND REINSTALLED AFT SVC DOOR EVAC. SLIDE IAW MT 725-61-06

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,307 hrs · 32,840 cycles

EMERGENCY LIGHTS ASSOC. WITH M1673 POWER SUPPLY BATTERY PACK STA. 952 LBL 13. IS INOP / REPLACED M1673 POWER SUPPLY BATTERY PACK AT STA 952 LBL 13; OPS CHECK IS GOOD IAW AMM 33-51-06-960-805 A-TAG=E41653

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,307 hrs · 32,840 cycles

EMERGENCY LIGHTS ASSOC. WITH M1668 POWER SUPPLY BATTERY PACK STA. 603 LBL 67._IS INOP / REPLACED M1668 POWER SUPPLY BATTERY PACK AT STA 603 LBL 67; OPS CHECK GOOD IAW AMM 33-51-06-960-805 A-TAG=E41652

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

LH L/E WING TO BODY FAIRING SUPPORT ANGLE AT STATION 500D IS CRACKED. FOUND ON OK TO INSTALL PANEL 191FL. / REMOVED AND REPLACED L/H L/E WING TO BODY FAIRING SUPPORT ANGLE AT STA 500D IAW SRM 51-40-02-0G-0 AND DWG 149A7101 SHT 5 REV -

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

RH L/E WING TO BODY FAIRING SUPPORT ANGLE AT STATION 500D IS CRACKED. FOUND ON OK TO INSTALL PANEL 191FR. / REMOVED AND REPLACED R/H L/E WING TO BODY FAIRING SUPPORT ANGLE AT STA 500D. IAW SRM 51-40-02-0G-0 AND DWG # 116A3110 REV-. REMOVED AND REINSTALLED WING TO BODY FAIRING PANELS 191AR AND 195AR IAW AMM 53-51-21-400-803 TAG#A51025

Part: BOLT — WORN (VERTICAL STAB) · airframe 55,307 hrs · 32,840 cycles

CUSTOMER CARD J753-480-00-00; VERTICAL STAB L\H OTBD AFT SPAR FITTING BOLT HAS WEAR. / REMOVED AND REPLACED VERTICAL STAB L/H O/B AFT SPAR FITTING BOLT PER WORK CAR J753-480-00-00 PAGE 3 STEP 2A(1)(C) REFFERANCE AMM 55-30-00-400-801 STEP 3H(1)(C) TORQUE WRENCH AAR 8058 CAL DUE 09/26/20 WN6399

Part: SKATE ANGLE — WORN (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

UPPER EXTERNAL FUSELAGE STA 1005-1016; RBL 15 FUSELAGE VERTICAL SKATE ANGLE WORN / REMOVED AND REPLACED SKATE ANGLE P/N 114A3200-12 I/A/W SAM 51-40-02-0G-0 AND BOEING DRAWING 147A0030 REV B

Part: SPLICE — CORRODED (BS 767) · airframe 55,307 hrs · 32,840 cycles

AFT CARGO COMPARTMENT; FLOOR SPLICE AT STA 767+4' RBL 3 TO RBL 10; WL 159; HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES / REMOVED CORROSION AFT CARGO FLOOR SPLICE AT STA 767+4 RBL3 TO RBL10 WL159 ORG 'T' .070 LOSS .010 REMAINING .060 OUT OF LIMITS IAW SRM 53-00-53-1A-2 REPLACED FLOOR SPLICE STA 767+4 IAW AMM 25-52-10-400-801 P/N 146A9401-4

Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

AFT CARGO COMPARTMENT; LH Z ANGLE AT STA 727D TO STA 787+7'; LBL 21; WL 159; HAS CORROSION AROUND FASTENER HOLES / FOUND MATERIAL LOSS TO BE .004 WITH AN ORIGINAL T = .040 AND .036 REMAINING 'OUT OF LIMITS' IAW SRM 53-00-53-1A-1 REMOVED AND REPLACED L/H Z ANGLE STA 727E+10 - 847 IAW SRM 53-00-53-2R-5 REPAIR 5 AND BOEING DWG # 146A7502-1 REV A P/N 146A7502-1

Part: SKATE ANGLE — WORN (VERTICAL STAB) · airframe 55,307 hrs · 32,840 cycles

L/H VERTICAL STAB SKATE ANGLE WORN AND ERODDED / EVALUATED L/H VERTICAL SKATE ANGLE STA 1016 TO STA 1130 FOUND TO BE OUT OF LIMITS ORIGINAL THICKNESS .063' REMAINING THICKNESS .028' LOSS OF .035' I/A/W SRM 53-80-13-1A-1 REMOVED AND REPLACED SKATE ANGLE P/N A48A8310U3 I/A/W SRM 51-40-02-0G-0 AND BOEING DRAWING 148A8300 REV C

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

E&E COMPARTMENT SHEAR TIE AT STA 312 +8' AND 1' ABOVE STR 22L AT WL 155 HAS CORROSION AT LOWER FASTENER / REMOVED CORROSION FROM SHEAR TIE AT LOWER FASTENER AREA IN E+E COMPARTMENT AT STA 312+8' AND 1' ABOVE STR 22L WL 155. ORIGINAL THICKNESS .063'; LOSS .008'; REMAINING .055'. OUT OF LIMITS IAW SRM 53-10-15-1A-1 FIG 108. REMOVED AND REPLACED SHEAR TIE P/N 141A8240-26 IAW BOEING DWG 142A3210 REV C; BOEING DWG 141A8240 REV:- AND SRM 51-40-02-0G-0. APPLIED CIC TO AREA IAW AMM 51-21-91-620-802.

Part: SHIELD — CORRODED (BS 737-787) · airframe 55,307 hrs · 32,840 cycles

AFT CARGO COMPARTMENT; RH SIDE; SHIELD FWD OF CARGO DOOR STA 767 TO STA 787; RBL 21; WL 159; HAS CORROSION AROUND FASTENER HOLES / NO ALLOWABLE LIMITS. REMOVED DAMAGED SHIELD ASY. INSTALLED NEW SHIELD ASY AS REQUIRED I.A.W. BOEING DWG: 146A8127 REV: - & 146A0081 REV: A AFT CARGO FWD SHIELD ASY STA 767 - 787 RBL 21 P/N 146A8127-12

Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

AFT CARGO COMPARTMENT; RH Z ANGLE AT STA 727C+10' TO STA 767; RBL 21; WL 159; HAS CORROSION AROUND FASTENER HOLES / REMOVED AND REPLACED R/H Z ANGLE IN AFT PIT STA 727-767 IAW BOEING DWG # 146A7502 REV - CORROSION WAS FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1 FOUND TO BE 100% LOSS P/N 146A7502-2

Part: SHIELD — CORRODED (BS 420) · airframe 55,307 hrs · 32,840 cycles

FWD CARGO PIT FWD SHIELD AT STA 420 +18' RBL 18 WL 155 HAS CORROSION ON UPPER SURFACE / REMOVED CORROSION FWD CARGO PIT FWD SHEILD STA 420+18 RBL 18 WL 155 ORIG 'T' .032 LOSS .005 REMAINING .027 OUT OF LIMITS IAW SRM 53-00-53-1A-2. REPLACED SHEILD STA 420-440 IAW SRM 51-40-02-0G-0 P/N 143A8126-21 ATAG# WN4598

Part: SHIELD — CORRODED (BS 480-500) · airframe 55,307 hrs · 32,840 cycles

FWD CARGO PIT AFT SHIELD BETWEEN STA 480 +12' TO STA 500 +8' RBL 18 WL 155 HAS CORROSION ON UPPER SURFACE / REMOVED CORROSION ON FWD CARGO COMPARTMENT SHIELD P/N 143A8126-19 ORIGINAL THICKNESS .032' REMOVED .004' REMAINING .028' OUT OF LIMITS IAW SRM 53-00-53-1A-1 REMOVED SHIELD P/N 143A8126-19 FABRICATED REPLACEMENT AND INSTALLED IAW BOEING DRAWING 143A8126 REV A AND SRM 51-40-02-0G-0 P/N 143A8126-19

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

AFT CARGO LOWER SILL WEB HAS AREAS OF CORROSION FROM BS 792 TO BS 847 WL 156.4 RBL 25'. / EVALUATED CORROSION ON AFT CARGO DOOR CUTOUT LOWER SILL WEB FOUND TO BE OUT OF LIMITS I/A/W SRM 53-60-15-1A-1 MORE THAN 50% MATERIAL LOSS REMOVED AND REPLACED WEB P/N 146A8123U25 I/A/W SRM 51-40-02-0G-0 AND BOEING DRAWING 146A8126 REV A RESTORED CORROSION INHIBITING COMPOUND I/A/W AMM 51-21-91-620-802

Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

FWD CARGO PIT R/H Z ANGLE BETWEEN STA 500A +10' TO STA 500C +16' RBL 24' WL 155 HAS CORROSION ON UPPER SURFACE / REMOVED CORROSION FROM FWD CARGO COMPARTMENT Z-ANGLE BETWEEN STA 500A+10 TO STA 500C+16 RBL 24 WL 155 ORIGINAL THICKNESS .040' REMOVED .008 REMAINING .032' FOUND TO BE OUT OF LIMITS I/A/W SRM 53-00-53-1A-2 FABRICATED REPLACEMENT Z-ANGLE P/N 143A7501-4 AND INSTALLED REPLACEMENT Z-ANGLE I/A/W BOEING DRAWING 143A7501 AND 143A7500 REV A AND SRM 51-40-02-0G-0 A-TAG A21658

Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

FWD CARGO PIT L/H Z ANGLE FROM STA 480 +12' TO STA 500D LBL 24 WL 155 HAS CORROSION UPPER SURFACE / REMOVED DAMAGE. ORIGINAL 'T' .040'; LOSS .008'. MATERIAL REMAINING .032 FOUND TO BE OUT OF LIMITS PER 53-00-53-1A-2. REMOVED DAMAGE SECTION OF Z ANGLE L/H 480+12-500D LBL 24 I/A/W SRM 51-40-02-0G-0 INSTALLED A NEW ZEE CHANNEL SIDEPLATE (Z-ANGLE) AT STA 480+12 - 500D LBL 24 I/A/W SRM 53-00-53-2R-5 P/N 143A7501-80

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

FWD CARGO PIT AFT FLOOR SUPPORT AT STA 500D BETWEEN LBL 10 TO RBL14 WL 155 HAS CORROSION ON UPPER SURFACE / REMOVED CORROSION FWD CARGO PIT AFT FLOOR SUPPORT STA 500D ORIG 'T' .080 LOSS 100% OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED + REPLACED FLOOR SUPPORT IAW SRM 51-40-02-0G-0 + DWG 143A9481 REV: -

Part: CHANNEL — CRACKED (VERTICAL STAB) · airframe 55,307 hrs · 32,840 cycles

VERTICAL STAB STAB STA 1016; 7.5' ABOVE FUSELAGE SKIN @ VERTICAL STAB MOUNT. LATERAL SUPORT CHANNEL CRACKED AT BOTH SIDES AT RADIUS / REMOVED AND REPLALCED VERTICAL STABIZER SPRING ASSEMBLY P/N 176A3101-26 I/A/W SRM 51-40-02-0G-0 AND BOEING DRAWINGS 176A3101 REV- AND 176A3001 REV D

Part: GUSSET — CRACKED (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

FORWARD CARGO PIT LEFT GUSSET STA 500D STR 19L IS CRACKED / REMOVED FWD CARGO PIT L/H CRUSSL7 @ STA 500D STR 19L IAW SRM 51-40-02-0G-0; VERIFIED NEW PART AS P/N 143A9481-6 A-TAG E92974 IAW BOEING DWG 143A7902 REV:C; DRILLED & LOCATED NEW GUSSET IAW SRM 51-40-05-0G-0; AND INSTALLED FWD CARGO PIT L/H GUSSET @ STA 500D STR 19L IAW BOEING DWG 143A7902 REV:C

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

FORWARD CARGO PIT LEFT BAFFLE BETWEEN STA 500-500A IS CRACKED AT FORWARD END / REMOVED AND INSTALLED A NEW BAFFLE AT FORWARD CARGO LEFT SIDE STA 500-500A I/A/W BOEING DRAWING 143A7505 NRC 40679/1400/0028; DEFECT# Y203137 EY1637(ATAG)

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 55,307 hrs · 32,840 cycles

FORWARD SERVICE DOOR; UPPER BEAM IS CRACKED. / REMOVED AND REPLACED #5 BEAM ON FWD SERVICE DOOR IAW SRM 51-40-02-0G-0; BOEING DWG# 141A6516 REV D; BOEING DWG# 141A6535 REV C. ACCOMPLISHED ADJUSTMENT TEST IAW AMM 52-41-00-820-801. ADJUSTMENT TEST GOOD ATAG WN2839

Part: GUSSET — CRACKED (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

FORWARD CARGO PIT RIGHT GUSSET STA 500D STR 19R IS CRACKED / REMOVED AND REPLACED FORWARD CARGO PIT RIGHT GUSSET STA 500D STA 19R IAW DWG 143A7902 SHEET 69 REV C; SRM 51-40-05-0G-0; AND SRM 51-40-02-0G-0 APPLIED CIC IAW AMM 51-21-91-620-802. P/N 143A9481-5 ATAG A88358

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 55,307 hrs · 32,840 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STA 120.30; 3RD VERTICAL STIFFNER FROM FWD END IS CRACKED 1' FROM BOTTOM. / REPAIRED R/H HORIZONTAL STABILIZER RIB AT STA 120.30 3RD VERTICAL STIFFENER FROM FWD END IAW SRM 55-10-09-2R-4 REPAIR 4

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,307 hrs · 32,840 cycles

FORWARD CARGO PIT RIGHT BAFFLE CLIP FORWARD SIDE OF STA 500C FRAME IS CRACKED / REMOVED AND REPLACED CLIP AT BS 500C; RIGHT SIDE I/A/W DRAWING 143A7502; SRM 51-40-02-0G; AND SRM 51-40-05-0G A-TAG A00573

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 55,307 hrs · 32,840 cycles

LEFT HORIZONTAL STABILIZER RIB AT STA 120.30; 3RD VERTICAL STIFFNER FROM FWD END IS CRACKED 1' FROM BOTTOM. / L/H HORIZ STAB RIB AT STA 120.3 3RD VERTICAL STIFFENER FROM FWD END IAW CRACKED 1' FROM BOTTOM. REPAIR IAW SRM 55-10-09-2R-4 WN5631

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 55,307 hrs · 32,840 cycles

CABIN FLOOR BOARD 232SF LOWER SURFACE IS PUNCTURED 45' FROM AFT EDGE AND 2' FROM RIGHT EDGE / REPAIRED PUNCTURE DAMAGE TO CABIN FLOOR BOARD 232 SF IAW 737-700 SRM 53-00-50+-2R-2 REPAIR 2 REV 70 SRM 53-00-50-2R-0 REPAIR GENERAL REV 70 AND NDT M/M PART 4 51-00-05 (A27468) (A94414) (A94744)

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 55,307 hrs · 32,840 cycles

CABIN FLOOR BOARD 231XF UPPER SURFACE HAS FIBER DAMAGE ALONG LENGTH OF PANEL / FABRICATED NEW FLOORBOARD 231 XF IAW B737 SRM 53-00-50-2R-0 PAR (4A) TABLE 204; PAR 53(1) A-H & BAC5085 PG. 21-22 & BOEING DWG# 144A5810-I.D. 0007

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 55,307 hrs · 32,840 cycles

AFT CARGO PIT; FLOOR PANEL 140CF HAS CORROSION IN SEVERAL SPOTS AROUND THE EDGE OF THE PANEL. / REMOVED CORROSION AFT CARGO PIT FLOOR PANEL 140CF DAMAGE IS MORE THAN 20' AROUND EDGE OF PANEL OUT OF LIMITS IAW SRM 53-00-53-1A-1. RECEIVED NEW PANEL P/N 453A2610-2 IAW AIPC 25-52-10-02 ATAG WN9553

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 55,307 hrs · 32,840 cycles

CABIN FLOOR BOARD 242DF LOWER SURFACE IS PUNCTURED 2.5' FROM FORWARD EDGE AND 0.5' FROM RIGHT EDGE / REPAIRED CABIN FLOORBOARD #242DF; LOWER SURFACE AT 2.5' FROM FORWARD EDGE AND 0.5' FROM RIGHT SIDE IAW B737-700 SRM 53-00-50-2R-2 REV 70; 53-00-50-2R-0 REV 70 AND NDT 51-00-05. (A36551)(A89485)(A87145)

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 55,307 hrs · 32,840 cycles

CABIN FLOOR BOARD 241AF UPPER SURFACE HAS FIBER DAMAGE ALONG LENGTH OF PANEL / FABRICATED; REPLACED FLOOR PANEL 241AF IAW B737-700 SRM 53-00-50-2R-0 REV 70; BOC. DRAW 144A5810 TY:DWG ID: 0008 REV:B; BAC 5085 REV E; PER ORIGINAL FLOOR PANEL SAMPLE 241AF A29029; A18238; WN4933

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 55,307 hrs · 32,840 cycles

CABIN FLOOR BOARD 232SF UPPER SURFACE IS PUNCTURED 65' FROM FORWARD EDGE AND 3' FROM LEFT EDGE / REPAIRED PUNCTURE DAMAGE TO CABIN FLOORBOARD 232SF IAW 737-700 SRM 53-00-50-2R-2; REPAIR 2 REV. 70; SRM 53-00-50-2R-0 REPAIR GENERAL REV. 70 AND NDT M/M PART 4; 51-00-05 (A27468)(A94414)(A94744)

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 55,307 hrs · 32,840 cycles

CABIN FLOOR BOARD 242CF LOWER SURFACE IS PUNCTURED 5' FROM FORWARD EDGE AND 0.5' FROM RIGHT EDGE / REPAIRED CABIN FLOOR BOARD 242CF LOWER SURFACE 5' FROM FORWARD EDGE AND 0.5' FROM RIGHT EDGE IAW B737-SRM 53-00-50-2R-0 GENERAL REV 70; 53-00-50-2R-1 REV 70 AND NDT 51-00-05 (A36551)(A87145)(A89485)

Part: PLATE — CORRODED (AFT CARGO CUTOUT) · airframe 55,307 hrs · 32,840 cycles

AFT CARGO PIT; INTERIOR EDGE OF THE DOOR CUTOUT; METAL END PLATE AT FLOOR TRANSITION IS CORRODED. / EVALUATED CORROSION TO METAL ENDPLATE AT AFT CARGO PIT INTERIOR EDGE OF DOOR CUTOUT. NO ALLOWABLE LIMITS IN SRM. REPLACED PLATE 453A2611-1 IAW AIPC 25-52-10-02 ATAG E48814

Part: FLOOR PANEL — DENTED (CABIN) · airframe 55,307 hrs · 32,840 cycles

CABIN FLOOR BOARD 232SF UPPER SURFACE HAS A DENT 23.5' FROM FORWARD EDGE AND 1.5' FROM LEFT EDGE / REPAIRED DENT DAMAGE TO CABIN FLOOR BOARD 232 SF IAW 737-700 SRM 53-00-50-2R-1 REPAIR 1 REV 20 SRM 53-00-50-2R-0 REPAIR GENER REV 70 BOEING DRAWING 144A5810 REV A NDT M/M PART 4 51-00-05 (A27468) (A94414) (A94744) (A18238) (A29079)

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 55,307 hrs · 32,840 cycles

CABIN FLOOR BOARD 242DF UPPER SURFACE HAS FIBER DAMAGE ALONG LENGTH OF PANEL / REPAIRED CABIN FLOORBOARD #242DF UPPER SURFACE ALONG LENGTH OF PANEL IAW B737-700 SRM 53-00-50-2R-0 GENERAL REV 70; 53-00-50-2R-1 REV 70 (A36551)(A87145)

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 55,307 hrs · 32,840 cycles

CABIN FLOOR BOARD 232SF UPPER SURFACE IS PUNCTURED 3' FROM FORWARD EDGE AND 5.5' FROM RIGHT EDGE / REPAIRED PUNCTURE DAMAGE TO CABIN FLOOR BOARD 232SF IAW 737-700 SRM 53-00-50-2R-2 REPAIR 2 REV. 70; SRM 53-00-50-2R-0 REPAIR GENERAL REV. 70 AND NDT M/M PART 4; 51-00-05 (A27468)(A94414)(A94744)

Part: GUARD — CRACKED (EMERGENCY EXIT) · airframe 55,307 hrs · 32,840 cycles

LEFT SIDE EMERGENCY EXIT DOOR MECHANISM GUARD IS CRACKED. / REMOVED AND REPLACED CRACKED LEFT SIDE EMERGENCY EXIT DOOR MECHANISM GUARD IAW DWG 411A2803 REV - AND SRM 51-40-02-0G-0 P/N 411A2857-2 S/N 7252345 WN9484

Part: GUARD — CRACKED (EMERGENCY EXIT) · airframe 55,307 hrs · 32,840 cycles

RIGHT SIDE EMERGENCY EXIT DOOR MECHANISM GUARD IS CRACKED. / REMOVED AND REPLACED CRACKED RIGHT SIDE EMERGENCY EXIT DOOR MECHANISM GUARD DWG 411A2803 REV - AND SRM 51-40-02-0G-0 P/N 411A2857-2 S/I 7252345 WN0016

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 55,307 hrs · 32,840 cycles

CABIN FLOOR BOARD 232SF LOWER SURFACE IS PUNCTURED 41.5' FROM AFT EDGE AND 1' FROM RIGHT EDGE / REPAIRED PUNCTURE DAMAGE TO CABIN FLOOR BOARD 232SF IAW 737-700 SRM 53-00-50-2R-1 REPAIR 1 REV. 70; SRM 53-00-50-2R-0 REPAIR GENERAL REV 70; BOEING DRAWING 144A5810 REV. A; NDT M/M PART 4; 51-00-05 (A27468)(A94414)(A94744)(A18238)(A29079)

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 55,307 hrs · 32,840 cycles

CABIN FLOOR BOARD 241DF UPPER SURFACE HAS FIBER DAMAGE ALONG LENGTH OF PANEL / REPLACED FLOOR PANEL 241 DF BY FABRICATING NEW IAW B 737 SRM 53-00-50-2R-0 REPAIR GEN REV 70 PER BAC 5085 REV E & DWG 144A5810-128 REV - WN0395 A18238 A30438

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 55,307 hrs · 32,840 cycles

CABIN FLOOR BOARD 231ZF LOWER SURFACE IS PUNCTURED 43' FROM FORWARD EDGE AND 7' FROM RIGHT EDGE / REPAIRED PNL 231ZF LOWER SURFACE PUNCTURE 43' FROM FWD EDGE FROM RIGHT EDGE. IAW B737-700 SRM 53-00-50-2R-1 REV 70; SRM 53-00-50-2R-0 REV 70 A89485; A98172; A36551

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 55,307 hrs · 32,840 cycles

CABIN FLOOR BOARD 232RF UPPER SURFACE IS PUNCTURED 34' FROM FORWARD EDGE AND 4' FROM RIGHT EDGE / REPAIRED PUNCTURE DAMAGE AT UPPER FACESHEET ON FLOORBOARD 232RF IAW B737 SRM 53-00-50-2R-1; PAR 3(A-K1; L1; M1) + SRM 53-00-50-2R-0; PAR (5) - REV. 70

Part: LENS — UNSECURE (CABIN) · airframe 55,138 hrs · 32,727 cycles

FWD ENTRY DOOR EXIT LIGHT COVER FELL OFF INSTALLED FWD ENTRY DOOR LIGHT LENS PER S.I.P.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,779 hrs · 32,497 cycles

CABIN EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1672 AND M1675 INOPERATIVE. R&R BATTERY PACKS AT M1672 AND M1675 PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,643 hrs · 30,493 cycles

LT EMERGENCY EGRESS LIGHTS FOR AISLE ILLUMINATION INOP BETWEEN ROW 9 TO ROW 12. R&R BATTERY PACK PER AMM.

Part: SKIN — DAMAGED (FWD FUSELAGE) · airframe 51,643 hrs · 30,493 cycles

FASTENER HOLES HAVE EVIDENCE OF DAMAGE ON S17L; STA 377; 380 AND 384 / REAMED UP HOLE AT STA 377 AND STA 380 AND STA 384- STR. 17L TO .199' IAW SRM 51-40-02. ACCOMPLISHED HFEC HOLE PROBE INSP OF 3 EA FASTENER HOLES PER NDT PART 6 51-00-00 PROC. 16 NO DEFECTS NOTED. FASTENERS TO BE REINSTALLED UNDER EA 1-753-34269. REPAIRED IN ACCORDANCE WITH EA #1-753-34269

Part: STRINGER — CRACKED (FUSELAGE) · airframe 51,643 hrs · 30,493 cycles

LOWER LEG OF STRINGER CRACKED AT BS 360, STR 16L. REPAIRED STRINGER PER EA.

Part: SKIN — DENTED (FWD FUSELAGE) · airframe 51,643 hrs · 30,493 cycles

DENT AT STA 380 6' ABOVE S 17L L=4.25' W=4.00' DEPTH=.033' DENT HAS CREASE ALONG THE STA. 380 FRAME. A/Y=121. / INSTALL REPAIR DOUBLER PER EA 1-753-34269. REPAIRED PER EA 1-753-34269.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,317 hrs · 29,650 cycles

RT EMERGENCY LIGHT INOP AT ROW 18. R&R LIGHT IAW AMM.

Part: LENS — UNSECURE (CABIN) · airframe 50,142 hrs · 29,533 cycles

LT EMERGENCY EXIT SIGN LENS COVER FELL OFF. R&R COVER ASSEMBLY IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 50,038 hrs · 29,461 cycles

LT WING OUTBOARD TRAILING EDGE AFT FLAP INBOARD END DELAMINATED ON LOWER AND UPPER SIDE. R&R AFT FLAP PER AMM.

Part: UNKNOWN — ODOR (CABIN) · airframe 49,526 hrs · 29,129 cycles

CHANGED NR 2 INTEGRATED DRIVE GENERATOR (PRECAUTIONARY) DUE TO ELECTRICAL SMELL IN CABIN. R&R GENERATOR PER AMM.

Part: GCU — FAULTY (E&E BAY) · airframe 49,526 hrs · 29,129 cycles

AIR TURNBACK/DECLARED EMERGENCY, CLIMBING OUT OF ATL AT 15,000 WE NOTICED A STRONG ELECTRICAL ODOR. R&R GENERATOR CONTROL UNIT IAW AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 49,439 hrs · 29,075 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. R&R CHARGER PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,439 hrs · 29,075 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,439 hrs · 29,075 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 49,439 hrs · 29,075 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOP. R&R CHARGER PER AMM.

Part: STRUCTURE — CRACKED (RT WING) · airframe 48,737 hrs · 28,639 cycles

RIGHT WING FIXED LOWER TRAILING EDGE, JUST OUTBOARD OF SAIL TAIL, WAFFLE BOARD CRACKED AT FASTENER HOLE. R & R THE WAFFLE BOARD IAW SRM AND DWG.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 48,737 hrs · 28,639 cycles

LEFT WING TRAILING EDGE, INBOARD OF THE NR 3 FLAP TRACK FAIRING, PANEL SUPPORT BRACKET CRACKED. R & R THE SUPPORT BRACKET IAW SRM & DWG.

Part: PLATE — CRACKED (LT WING TE FLAP) · airframe 48,737 hrs · 28,639 cycles

LEFT WING TRAILING EDGE INBOARD OF NR 3 FLAP TRACK FAIRING WAFFLE PLATE CRACKED. R & R THE PLATE IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 48,737 hrs · 28,639 cycles

LEFT WING GEAR WELL AT AFT SPAR, UPPER INBOARD END, SUPPORT BRACKET CRACKED. R & R THE SUPPORT BRACKET IAW SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,737 hrs · 28,639 cycles

PASS CABIN FLR PNL 242AF IS DISBONDED AT FWD OTBD CORNER; UPR SURFACE. / REPAIRED PASS CABIN FLOOR PANEL242AF OF LIGHT DISBOND + DENTS AT UPPER SURFACE AND LOWER SURFACE AT BOTH CORNERS IAW B737 SRM 53-00-50-2R-6 REV 64 AND B737 SRM 53-00-50-2R-0 REPAIR GENERAL REV 64 A26386; A68593; A51273

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 48,737 hrs · 28,639 cycles

LEFT WING AFT SPAR ABOVE PYLON SAIL TAIL, SEAL SUPPORT BRACKET CRACKED. R & R THE SUPPORT BRACKET IAW SRM AND DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,737 hrs · 28,639 cycles

PASS CABIN FLR PNL 242BF IS DELAMINATED AT AFT OTBD CORNER; UPR SURFACE. / REMOVED PASS CABIN FLOOR PANEL 242BF OF DELAM AT BOTH AFT CORNERS ON UPPER SURFACE IAW B737 SRM 53-00-50-2R-2 REV 64; B737 SRM 53-00-50-2R-0 REPAIR GENERAL REV 64 A26386; A68593; A51273

Part: STRUCTURE — CRACKED (RT WING) · airframe 48,737 hrs · 28,639 cycles

RIGHT WING FIXED LOWER TRAILING EDGE, INBOARD NR 6 FLAP TRACK HAS A WAFFLE BOARD CRACKED AT FASTENER HOLE. R & R THE WAFFLE IAW SRM AND DWG.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 48,737 hrs · 28,639 cycles

RIGHT WING FIXED UPPER TRAILING EDGE PANEL AT SAILTAIL, AFT UPPER SUPPORT BRACKET CRACKED. R & R THE SUPPORT BRACKET IAW SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 48,445 hrs · 28,460 cycles

DIVERSION, L2 WINDOW ARCED. R&R L2 SLIDING WINDOW IAW MT.

Part: SPOILER — DELAMINATED (RT WING) · airframe 47,072 hrs · 27,586 cycles

RT WING NR 12 GROUND SPOILER DELAMINATED. R&R NR 12 GROUND SPOILER PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 45,900 hrs · 26,864 cycles

CENTER CABIN EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R & R THE BATTERY IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,412 hrs · 25,973 cycles

AFT ENTRY DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW MM. .

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,742 hrs · 25,556 cycles

L/H OVERWING EXIT LIGHT INOPERATIVE. REPLACED THE LAMP IAW MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FORWARD CARGO Z ANGLE CORRODED, BETWEEN BS 500- 3 - 500+18, STRINGER 26R. R & R SHIELD IAW SRM & DWG.

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 42,558 hrs · 24,873 cycles

R1 DOOR LOWER CLOSE OUT FRAME CRACKED AT BS 294.5 AT CREASE BEAM ATTACH FASTENERS. REPAIRED FRAME IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

LEFT INTERCOSTAL CRACKED AT BS 1016 AT FLOOR LINE. R & R INTERCOSTAL IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R CLIP IAW SRM & DWG.

Part: STIFFENER — CRACKED (LT WING) · airframe 42,558 hrs · 24,873 cycles

LEFT WING UPPER FIXED PANEL ATTACHED TO THE DEFLECTOR BEAM, AFT CTR TRIANGLE SHAPED STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

MAIN CABIN INTERCOSTAL UPPER FLANGE CRACKED AT BS 317, RBL 33. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

INTERCOSTAL CORRODED AT BS 270, BETWEEN RBL 11 - LBL 12. R & R INTERCOSTAL IAW SRM & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

LEFT CREASE BEAM INNER INBD SURFACE CORRODED, BETWEEN BS 312 - 348.5. R & R BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

R1 DOOR CREASE BEAM CORRODED BETWEEN BS 303.5 - 336.1. R & R CREASE BEAM IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

INTERCOSTAL CORRODED BETWEEN BS 616 - 639, STRINGER 15R. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

INTERCOSTAL CORRODED, BETWEEN BS 270 - 260, BL 0. R & R INTERCOSTAL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

AFT CARGO COMPARTMENT, FLOOR SUPPORT CORRODED, BETWEEN BS 767 - 792, STRINGER 25I. R & R SUPPORT IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

L2 DOOR CREASE BEAM CORRODED, BETWEEN BS 951 - 992. R & R CREASE BEAM IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

R2 DOOR CREASE BEAM CORRODED, BETWEEN BS 951 - 992. R & R CREASE BEAM IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

AFT CARGO COMPARTMENT LT Z ANGLE CORRODED, BETWEEN BS 727E+10 - 817. R & R Z ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: PLATE — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FORWARD GALLEY DOOR CUT OUT SURROUND STRUCTURE DOOR SILL INBD ATTACH PLATE CORRODED. R & R PLATE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FORWARD CARGO Z ANGLE CORRODED AT BS 480, STRINGER 26L. R & R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FORWARD CARGO Z ANGLE CORRODED, BETWEEN BS 500+9 - 500+15, STRINGER 26L. R & R Z ANGLE IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

FORWARD CARGO Z ANGLE SHIELD CORRODED, BETWEEN BS 500-3 TO 500+18, STRINGER 26R. R & R SHIELD IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 42,558 hrs · 24,873 cycles

RIGHT WING UPPER TE RIB CURVED ANGLE CRACKED AT THE VERTICAL FLANGE. R & R ANGLE IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 42,558 hrs · 24,873 cycles

MAIN CABIN FLOOR STRUCTURE FLOOR SUPPORT AT CRACKED BS 540, BETWEEN BL 0 - RBL 24. R & R SUPPORT IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 42,558 hrs · 24,873 cycles

RIGHT WING UPPER TE PANEL ANGLE CRACKED AT THE VERTICAL FLANGE. R & R ANGLE IAW SRM & DWG.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 42,558 hrs · 24,873 cycles

LEFT MAIN WW BULKHEAD CRACKED AT BS 663, LBL 35. REPAIRED WEB IAW SRM.

Part: PLATE — CORRODED (L1 DOOR) · airframe 42,558 hrs · 24,873 cycles

L1 DOOR CUT OUT SURROUND STRUCTURE, AFT GIRT BAR FLOOR LATCH ATTACH PLATE CORRODED. R & R PLATE IAW SRM & DWG.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 39,658 hrs · 23,208 cycles

THE L1 DOOR SLIDE WAS FOUND LOOSE. REINSTALLED THE SLIDE IAW MT.

Part: ACTUATOR — INOPERATIVE (FUEL SYSTEM) · airframe 38,858 hrs · 22,750 cycles

FUEL CROSS FEED VLV INOPERATIVE. R & R CROSS FEED VLV ACTUATOR IAW AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 38,457 hrs · 22,524 cycles

L1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,579 hrs · 22,007 cycles

M01675 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,579 hrs · 22,007 cycles

M01672 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,579 hrs · 22,007 cycles

M01673 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,169 hrs · 21,181 cycles

RIGHT SEAT TRACK FWD CRACKED AT BS 727B, RBL 45.5, INBD AFT FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,169 hrs · 21,181 cycles

LEFT SEAT TRACK FWD OF BS 727B, LBL 24.5 CRACKED AT INBD FWD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 36,169 hrs · 21,181 cycles

RIGHT FLOORBEAM U BRACKET CRACKED AT BS 727B, RBL 45.5, AFT SIDE, LOWER FASTENER HOLE. REPAIRED BRACKET IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 36,169 hrs · 21,181 cycles

LEFT CABIN FLOORBEAM U BRACKET CRACKED AT BS 727B LBL 24.5, AFT SIDE LOWER FASTENER HOLE. R & R BRACKET IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,169 hrs · 21,181 cycles

RIGHT SEAT TRACK FWD OF BS 727B, RBL 24.5 CRACKED AT INBD FWD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,169 hrs · 21,181 cycles

RIGHT SEAT TRACK FWD OF BS 727B, RBL 24.5 CRACKED AT INBD AFT FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,169 hrs · 21,181 cycles

RIGHT SEAT TRACK FWD OF BS 727B, RBL 24.5 CRACKED AT OTBD AFT FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 36,169 hrs · 21,181 cycles

LEFT CABIN FLOORBEAM ANGLE BRACKET DAMAGED AT BS 727B, LBL 24.5. R & R ANGLE IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,169 hrs · 21,181 cycles

RIGHT SEAT TRACK FWD CRACKED AT BS 727B, RBL 45.5, INBD FWD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 36,169 hrs · 21,181 cycles

LEFT NR 3 WINDOW FRAME E-F POST CRACKED AT 2ND HOLE FROM THE BOTTOM. REPAIRED FRAME IAW SRM & ACO.

Part: WINDOW — CRACKED (COCKPIT) · airframe 36,169 hrs · 21,181 cycles

FLIGHT DECK LT NR 1 WINDOW UPPER OTBD CORNER CRACKED. REPAIRED WINDOW IAW SRM & ACO.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 36,169 hrs · 21,181 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 101.9, APPROX 11 INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,169 hrs · 21,181 cycles

SEAT TRACK UPPER FLANGE CRACKED OTBD FWD HOLE AT BS 727A+18, LBL 46. R & R FLANGE IAW ACO.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 36,169 hrs · 21,181 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 129.5, APPROX 18 INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 36,169 hrs · 21,181 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 147.9, APPROX 9 INCHES FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 33,371 hrs · 19,528 cycles

CREW REPORTS SMELL IN CABIN WITH RECIRCULATING FAN ON IN AFT CABIN. R&R AFT INBD COFFEE MAKER IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 33,217 hrs · 19,438 cycles

MID CABIN CEILING EMERGENCY EXIT SIGN LOOSE. R&R SIGN IAW MM.

Part: SIGN — MISSING (CABIN) · airframe 33,021 hrs · 19,321 cycles

LT OVERWING EXIT SIGN MISSING. INSTALLED SIGN IAW MM.

Part: PIN — LOOSE (R1 DOOR) · airframe 32,887 hrs · 19,240 cycles

R1 DOOR EMERGENCY EVAC SLIDE CASE PIN LOOSE. SECURED PIN IAW AMM.

Part: LENS — CRACKED (RT WING) · airframe 30,894 hrs · 18,060 cycles

RIGHT WINGTIP GREEN POSITION LIGHT LENS IS CRACKED. REMOVED AND REPLACED PER AMM.

Part: COVER — BROKEN (CABIN) · airframe 30,195 hrs · 17,637 cycles

EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,178 hrs · 17,018 cycles

EEPLS BULBS INOP. RELAMPED BULBS PER AMM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 29,178 hrs · 17,018 cycles

LEFT HORIZONTAL STABILIZER RIB STIFFENER CRACKED AT STA 92.7 LOWER CHORD. REPAIRED RIB STIFFENER PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,178 hrs · 17,018 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.50. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,694 hrs · 16,740 cycles

RIGHT HORIZONTAL STABILIZER SKIN CRACKED AT LOWER IN-SPAR SKIN STA 139.15. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,694 hrs · 16,740 cycles

RIGHT HORIZONTAL STABILIZER SKIN CRACKED AT LOWER IN-SPAR SKIN STA 100.98. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 27,498 hrs · 16,041 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1. R&R COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 27,498 hrs · 16,041 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 12L. R&R COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 27,498 hrs · 16,041 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 14L. R&R COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 26,332 hrs · 16,365 cycles

AFT EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 25,630 hrs · 14,959 cycles

DURING SCHEDULED RON CHECK, R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. SECURED SLIDE ASSY PER MT.

Part: LENS — BROKEN (CABIN) · airframe 25,527 hrs · 14,891 cycles

FWD EEPLS LENS BROKEND. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 23,888 hrs · 13,950 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 23,853 hrs · 13,932 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 23,853 hrs · 13,932 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 22,816 hrs · 13,308 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MT.

Part: SKIN — CRACKED (R1 DOOR) · airframe 22,576 hrs · 13,164 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR OUTER SKIN AT UPPER AFT CORNER CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: SKIN — CRACKED (R1 DOOR) · airframe 22,576 hrs · 13,164 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR OUTER SKIN AT UPPER AFT CORNER CRACKED. REMOVED AND REPLACED DOOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,488 hrs · 13,100 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD EEPLS INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,027 hrs · 12,833 cycles

DURING SCHEDULED 6Y CHECK, FOUND FITTING CRACKED AT BS 947, LBL 9. REMOVED AND REPLACED FITTING PER SRM AND BAC DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,027 hrs · 12,833 cycles

DURING SCHEDULED 6Y CHECK, FOUND EEPLS INOP AT ROW 2. REPAIRED EEPLS ASSY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,894 hrs · 12,755 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,827 hrs · 12,143 cycles

DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP AT ROW 10. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 19,692 hrs · 11,438 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SENSOR — DAMAGED (NLG) · airframe 18,351 hrs · 10,612 cycles

AIR TURNBACK, WITH GEAR HANDLE IN OFF POSITION, NLG FELL TO DOWN POSITION WITH UNSAFE LIGHT INDICATION. FOUND NLG S854 SENSOR DAMAGED AND OBSTRUCTING UPLOCK ASSY. REMOVED AND REPLACED S854 UPLOCK SENSOR PER MM.

Part: STRIP — CRACKED (CABIN) · airframe 17,376 hrs · 10,021 cycles

DURING SCHEDULED HC1 CHECK, FOUND BLUE EEPLS STRIPS CRACKED. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 24,764 hrs · 14,250 cycles

FOUND FWD ENTRY EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,798 hrs · 8,436 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT LOWER AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 14,109 hrs · 8,016 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 11,681 hrs · 6,564 cycles

EEPLS INOP BETWEEN ROW 13 ABC AND ROW 17 ABC. FOUND LOOSE CONNECTOR, SECURED CONNECTOR PER MM.

Part: LANYARD — BROKEN (EVAC SLIDE) · airframe 10,721 hrs · 6,022 cycles

R1 DOOR EMERGENCY EVAC SLIDE LANYARD BROKEN. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 10,502 hrs · 5,903 cycles

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

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 9,751 hrs · 5,477 cycles

DURING SCHEDULED HC2 CHECK, LEFT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 9,751 hrs · 5,477 cycles

DURING SCHEDULED HC2 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — LOOSE (CABIN) · airframe 9,308 hrs · 5,220 cycles

EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 9,100 hrs · 5,084 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 9,092 hrs · 5,078 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: LIGHT — WORN (CABIN) · airframe 4,813 hrs · 2,700 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP WORN AT FWD END. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 194 hrs · 112 cycles

DURING SPV, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 9 hrs · 10 cycles

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