N212WN

Part: GIRT BAR — LOOSE (ZONE 800) · airframe 67,682 hrs · 40,801 cycles

R1 SERVICE DOOR SLIDE FWD GIRT BAR CLIP LOOSE CORRECTED GIRT BAR CLIP PER AMM 25-66-01, NO DEFECTS NOTED.

Part: ATTACH BRACKET — CRACKED (ZONE 100) · airframe 65,987 hrs · 39,755 cycles

FWD KEEL BEAM PANEL #192E L/H FWD ATTACH BRACKET CRACKED<[01] REMOVED AND REPLACED FWD KEEL BEAM PANEL #192E L/H FWD ATTACH BRACKET PER SRM 51-40-02.

Part: HANDLE — LOOSE (ZONE 800) · airframe 65,820 hrs · 39,654 cycles

FWD SERVICE DOOR ASSIST HANDLE IS LOOSE<[01] TIGHTENED FWD SERVICE DOOR ASSIST HANDLE IAW AMM 52-41-31-400-802 STEP 3.F(2).;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: HANDLE — LOOSE (ZONE 800) · airframe 65,820 hrs · 39,654 cycles

ASSIST HANDLE JUST AFT OF FWD ENTRY DOOR IS LOOSE<[01] TIGHTENED ASSIST HANDLE JUST AFT OF FWD ENTRY DOOR IAW AMM 25-21-31-420-802 STEP 3.B(6).;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: FUSE — BLOWN (ZONE 200) · airframe 65,820 hrs · 39,654 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1672 INOP<[01] REPLACED BLOWN FUSE 1F IN M1672 BATTERY CHARGER AND PERFORMED GOOD INSTALLATION TEST OF M1672 BATTERY PACK IAW AMM 33-51-06-960-804.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 65,820 hrs · 39,654 cycles

EMERGENCY EXIT LOCATOR LIGHT FWD OF R/H OWE HAS INOP BULBS<[01] RELAMPED INOP BULBS AND PERFORMED GOOD OPERATIONAL TEST OF EMERGENCY EXIT LOCATOR FWD OF RH OWE I.A.W AMM 33-51-01-960-801.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

ACB AFT CORNER SCUFF PLATE IS CRACKED.<[01] WELDED THE CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1594362-1 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(4). REFERRED TO BAC5975.

Part: WEB — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON ACB LOWER MAIN SILL AT STA 787+7 TO STA 787+14; 787+16.5; AND 787+18; RBL18; WL152<[01] REMOVED AND REPLACED ACB LOWER MAIN SILL WEB BS 787+6 TO BS 847 RBL18; WL152 IAW SRM 51-40-02 AND DWG# 146A8120 ID:0031 REV: - AND DWG# 146A8121 ID:0005 REV: -;[02] VERIFIED ACTION 1.

Part: WEB — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON ACB LOWER MAIN SILL AT STA 787+7 TO STA 787+14; 787+16.5; AND 787+18; RBL18; WL152<

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 65,820 hrs · 39,654 cycles

CRACKED STR CLIP AT PAX CABIN BS727C S-5R. MARKED<[01] REMOVED AND INSTALLED NEW STR CLIP PN# 143A1010U1; LOT#1598900-1 AT DISCREPANCY AREA PER SRM 51-40-02; DWG#146A1103 REV:- TASK CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION 1

Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CRACKED STR CLIP AT PAX CABIN BS727B S-6R. MARKED<[01] REMOVED AND INSTALLED NEW STR CLIP PN# 143A1010U1; LOT#1598900-1 AT DISCREPANCY AREA PER SRM 51-40-02; DWG#146A1102 REV:- TASK CARD COMPLETED.;[02] VERIFIED CORRECTIVE ACTION 1

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 65,820 hrs · 39,654 cycles

CRACKED STR CLIP AT PAX CABIN BS727E S-4R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP BS 727E; S-4R PER SRM 51-10-02; 51-40-02 AND DWG 146A1112 REV:-;[02] VERIFIED CORRECTIVE ACTION 1

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 65,820 hrs · 39,654 cycles

CRACKED STR CLIP AT PAX CABIN BS727D S-6R. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727D S-6R IAW SRM 51-40-02-0G-0 AND DWG 146A1111.;[02] VERIFIED CORRECTIVE ACTION 1

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 65,820 hrs · 39,654 cycles

CRACKED STR CLIP AT PAX CABIN BS727D S-4R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP BS 727D; S-4R PER SRM 51-10-02 51-40-02 AND DWG 146A1111 REV:-;[02] VERIFIED CORRECTIVE ACTION 1

Part: SUPPORT — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT LBL 24; FROM STA 727+18 TO STA 808+15; WL 156.<[01] REMOVED AND REPLACED FLOOR/SIDEWALL SUPPORT<BR>IAW SRM 51-40-02 AND DWG 146A7500<BR>ACB BS 727 TO BS 847 LBL24 WL 156;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CRACKED SUPPORT ANGLE IN FCB AT STRINGER S-18L STA 500D.<[01] REMOVED AND REPLACED GUSSET WITH P/N 143A9481-6 LOT:1583773-1 AT FCB STR19L STA 500D. IAW SRM 51-40-02 & DWG#143A7902 REV: -;[02] VERIFIED

Part: SHIELD — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON FWD CARGO COMPARTMENT DOOR CUT-OUT FWD SHIELD FROM STA 420+5 TO 440; RBL 24; WL 156.<[01] REMOVED AND REPLACED FWD SHIELD BS 420-BS440 RBL 24 WL 156<BR>IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AND DWG# 143A0080 REV:-<BR>CARD COMPLETED;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CAPTAIN'S FWD I/B SEAT TRACK CRACKED <[01]. CAPTAIN'S FWD I/B SEAT TRACK CRACKED WAS REPLACED IAW IPC 25-11-01-55 AND WILL BE INSTALLED IN THE TASK CARD NUMBER TTG8Q003KP1W; [02] VERIFIED ITEM 1 AND TASK CARD CLOSED.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT RBL 24; FROM STA 727+4 TO STA 767; WL 158.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT RBL 24 PER REF SRM 51-40-02-0G-0 AND DWG 146A7500.;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 65,820 hrs · 39,654 cycles

F/O'S FWD I/B SEAT TRACK CRACKED<[01] F/O'S FWD I/B SEAT TRACK CRACKED WAS REPLACED IAW IPC 25-11-01-55 AND WILL BE INSTALLED IN THE TASK CARD NUMBER TTG8Q003KP1W;[02] VERIFIED

Part: WEB — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON AFT CARGO DOOR CUT-OUT SUB-THRESHOLD WEB AT STA 787+8; RBL 23; AND AT STA 827 TO 827+5; RBL 25; WL 156.<[01] REMOVED AND REPLACED NEW ON AFT CARGO DOOR CUT-OUT SUB-THRESHOLD WEB BS794 TO BS847 RBL 23. IAW SRM 51-40-02 AND DWG 146A8340 ID:0021 REV:-;[02] REJECTION: NOT ABLE TO VERIFY INSTALLATION. THRESHOLD INSTALLED;[03] REJECTION; SEE TTG8Q00ZQCEE;[04] THE REJECTION WAS CORRECTED ON FAULT TTG8Q00ZQCEE;[05] ACTION ITEM 4 VERIFIED;[06] ALL THIS FAULT COMPLETED;[07] CARD COMPLETE

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT ANGLE FROM STA 480+12 TO STA 500D; LBL 24; WL 157.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BETWEEN BS.480+12' - BS.500D LBL 24; WL156 IAW SRM 53-00-53-2R-6 REPAIR 6 TABLE 201 ITEM [1] & SRM 51-40-02 AND DWG# 143A7500 ID:0058 REV: -

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT ANGLE FROM STA 480+12 TO STA 500D; LBL 24; WL 157.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BETWEEN BS.480+12' - BS.500D LBL 24; WL156 IAW SRM 53-00-53-2R-6 REPAIR 6 TABLE 201 ITEM [1] & SRM 51-40-02 AND DWG# 143A7500 ID:0058 REV: -

Part: CARGO TRACK — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON AFT CARGO BAY RBL 14 FLOOR RAIL AT STA 847+4; WL 156.<[01] ACB TRACK TIEDOWN WAS REPLACED IN CUSTOMER CARD TTG8Q00ZC6JA BETWEEN BS767+14 AND BS887 RBL14 WL156.;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: THRESHOLD WEB — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON FWD CARGO COMPARTMENT SUB THRESHOLD WEB FROM STA 440+7 TO 480+4; RBL 29; WL 156.<[01] STEPS 1-3 COMPLETED.;[02] REMOVED AND REPLACED FWD CARGO COMPARTMENT SUB THRESHOLD WEB BS 440 TO BS 500 RBL 29; WL 156 IAW SRM 51-40-0; 51-40-02 AND DGW:143A8330 ID:0028 REV:-<BR>CARD COMPLETED;[03] CORRECTIVE ACTION ITEM 2 VERIFIED; CARD COMPLETE.

Part: SHIELD — CORRODED (ZONE 200) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON FWD CARGO COMPARTMENT DOOR CUT-OUT FWD SHIELD FROM STA 420+5 TO 440; RBL 24; WL 156.<[01] REMOVED AND REPLACED FWD SHIELD BS 420-BS440 RBL 24 WL 156<BR>IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AND DWG# 143A0080 REV:-<BR>CARD COMPLETED;[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

F/O'S FWD I/B SEAT TRACK CRACKED <[01]. F/O'S FWD I/B SEAT TRACK CRACKED WAS REPLACED IAW IPC 25-11-01-55 AND WILL BE INSTALLED IN THE TASK CARD NUMBER TTG8Q003KP1W; [02] VERIFIED.

Part: WEB — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON AFT CARGO DOOR CUT-OUT SUB-THRESHOLD WEB AT STA 787+8; RBL 23; AND AT STA 827 TO 827+5; RBL 25; WL 156.

Part: SHIELD — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON AFT CARGO BAY DOOR CUT-OUT FWD SHIELD FROM STA 767+6 TO 767+12; RBL 25; WL 156.<[01] REMOVED AND REPLACED ON AFT CARGO BAY DOOR CUT-OUT FWD SHIELD FROM STA 767 TO STA 787+6 RBL 25 WL 156 IAW SRM 51-40-02 AND DGW 146A0081 REV: A.

Part: PRESSURE DECK — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON MLG PRESSURE DECK WEB STIFFENER AT STA 707+8 RBL 65; WL 200.<[01] 'REFER TO FAULT TTG8Q00ZBDUT WHERE EA 25-153-00723 WAS ADDED AS A SUBTASK'.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: STRINGER CLIP — CRACKED (ZN 100 FUS LOWER) · airframe 65,820 hrs · 39,654 cycles

SMALL CRACK ON STRINGER CLIP - BS 440; STR. 14R<[01] REMOVED AND INSTALLED STRINGER CLIP - BS 440; STR. 14R. IAW SRM 51-40-02; DWG 143A0082 REV:- AND DWG 143A0102 REV:B;[02] VERIFIED CORRECTIVE ACTION 1

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 65,820 hrs · 39,654 cycles

STA 540 BREAK PANEL IS CRACKED AT LBL 1; WL 208<[01] REMOVED AND REPLACED BREAK PANEL ITEM:143A5240-63 BETWEEN BS540 BL0 TO LBL 24.75 WL 208. IAW SRM 51-40-02 DWG 143A0060 ID: 001 REV: -;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 65,820 hrs · 39,654 cycles

STA 540 BREAK PANEL IS CRACKED AT RBL 1; WL 208<[01] REMOVED AND REPLACED BREAK PANEL ITEM:143A5240-64 LOT: 1598659-1; BETWEEN BS540 BL0 TO RBL 24.75 WL 208. IAW SRM 51-40-02 DWG 143A0060 REV:A;[02] VERIFIED CORRECTIVE ACTION ETNRY 1.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 65,820 hrs · 39,654 cycles

STA 540 BREAK PANEL IS CRACKED AT RBL 1; WL 208<[01] REMOVED AND REPLACED BREAK PANEL ITEM:143A5240-64 LOT: 1598659-1; BETWEEN BS540 BL0 TO RBL 24.75 WL 208. IAW SRM 51-40-02 DWG 143A0060 REV:A;[02] VERIFIED CORRECTIVE ACTION ETNRY 1.

Part: SKIN — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CROWN SKIN UNDER VERT STAB HAS AREAS OF SURFACE CORROSION FROM STA 1016 TO STA 1040 AND S-2AL TO S-2AR (MARKED) <[01]. AS PER EA 25-153-00790; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS; [02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS. <[01] PANEL 241DF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: STIFFENER — CORRODED (ZONE 100) · airframe 65,820 hrs · 39,654 cycles

CORROSION ON MLG PRESSURE DECK WEB STIFFENER AT STA 707+2; RBL 61; WL 200.<[01] REPAIR PER EA# 25-153-00723<BR><BR>EA-GENERAL' REPAIR REFERENCE IS SELECTED.;[02] REMOVED CORROSION ON MLG PRESSURE DECK WEB STIFFENER AT STA 707+2; RBL 61; WL 200 AND REWORKED AREA PER EA 25-153-00723.;[03] VERIFIED CORRECTIVE ACTION #2

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 65,820 hrs · 39,654 cycles

FLOOR PANEL 242AF LOWER SKIN HAS AN AREA OF PULLED STRANDS. <[01] PANEL 242AF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-0.; [02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 65,820 hrs · 39,654 cycles

FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241DF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: SEAL — CRACKED (ZONE 300) · airframe 65,820 hrs · 39,654 cycles

LT HORIZONAL STAB UPPER FWD SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED LT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.;[02] VERIFIED CORRECTIVE ACTION 1

Part: SEAL — CRACKED (ZONE 300) · airframe 65,820 hrs · 39,654 cycles

RT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED RT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.

Part: SEAL — CRACKED (ZONE 300) · airframe 65,820 hrs · 39,654 cycles

RT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED RT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.;[02] VERIFIED ITEM 1 AND TASK CARD COMPLETED.

Part: RELEASE SYSTEM — BROKEN (ZN 800 DOOR) · airframe 64,946 hrs · 39,143 cycles

UPON ARRIVAL; FLIGHT ATTENDANTS REPORT THAT PLASTIC GUIDE LOOP IS BROKEN OFF OF FORWARD SERVICE DOOR GIRT BAR.<[01] REPLACED FWD SVC DOOR GIRT BAR RELEASE STOP ASSY PER <BR>MM 25-66-01

Part: COVER — MISSING (ZONE 200) · airframe 64,448 hrs · 38,844 cycles

EMERGENCY EXIT COVER AT ROW 12DEF MISSING<[01] REINSTALLED EMERGENCY OVERWING EXIT LIGHT SIGN/COVER IAW AMM SIP 20-00-00

Part: LAMP — INOPERATIVE (WARNING IND) · airframe 63,471 hrs · 38,219 cycles

FLT ATT VISUAL ALERTING SYSTEM IN AFT GALLEY INOP<[01] REMOVED AND REPLACED AFT EXIT SIGN LAMP PER AMM 33-51-01. OPS CHECK GOOD.

Part: SLIDE — LOOSE (ZN 800 DOOR) · airframe 61,464 hrs · 37,000 cycles

FWD ENTRY DOOR SLIDE FELL OUT OF CONTAINER<[01] REINSTALLED SLIDE INTO CONTAINER PER 725-61-06 AND AMM 25-66-01.

Part: ENGINE — OVERHEATED (ZN 400 NACELLE/P) · airframe 60,650 hrs · 36,462 cycles

AFTER LIFTOFF WE NOTICED EGT. @ AROUND 968 DEG ON THE #1 ENGINE FOR APPROXIMATELY 30 SECONDS. IT WAS A MAX POWER TAKEOFF DUE TO WINDSHEAR ; AS REPORTED BY ATIS. AFTER COMPLETING THE NON-NORMALS AND NORMAL CHECKLIST WE DID AN UNEVENTFUL 15 DEG FLAP AUTOBREAK 3 LANDING AND EXITED THE RUNWAY 10300 FT FROM THE APPROACH END. WE ACCOMPLISHED 30 MINUETS BREAK COLING OFF THE GATE.<[01] TROUBLESHOOT PER EA M-21-177-01860; FOUND FAULT CODE 77-20861 AND FOUND T49.5 PROBE (CHB) S3 RESISTANCE OUT OF LIMITS.<BR>REPLACED T49.5 PROBE (CHB) S3 IAW AMM 77-21-01.<BR>ALL OPS CKS GOOD AT THIS TIME.

Part: THERMOCOUPLE — OVERTEMP (ZN 400 NACELLE/P) · airframe 60,512 hrs · 36,367 cycles

ON CLIMB OUT #2 ENGINE EGT WENT RED AT 962 INDICATED<[01] REMOVED AND REPLACED #2 ENG OTBD UPPER THERMOCOUPLET49.5; CJ9 HARNESS;J9 HARNESS OPS CHECK GOOD IAW AMM 77-21-01

Part: WIRE HARNESS — OVERTEMP (ZN 400 NACELLE/P) · airframe 60,512 hrs · 36,367 cycles

ON CLIMB OUT #2 ENGINE EGT WENT RED AT 962 INDICATED<[01] REMOVED AND REPLACED #2 ENG OTBD UPPER THERMOCOUPLET49.5; CJ9 HARNESS;J9 HARNESS OPS CHECK GOOD IAW AMM 77-21-01

Part: LENS — BROKEN (ZN 200 FUS TOP) · airframe 60,157 hrs · 36,132 cycles

LOWER OVERWING EXIT SIGN ON CAPTAINS SIDE IS BROKEN<[01] REPLACED L/H OVERWING EMERGENCY EXIT LENS PER AMM 33-51-12.

Part: LIGHT — BROKEN (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

BROCKEN CONTACT HOUSING EMERGENCY LIGHT STOWAGE BIN ROW 11 AT PASSENGER COMPARTMENT 2023-143150<[01] REPLACED HOUSING EMERGENCY LIGHT STOWAGE BIN ROW 11 RT AT PASSENGER COMPARTMENT IAW AMM 33-51-03-960-802 TEST IS OK;[02] TASK CARD COMPLETE.

Part: LIGHT — BURNED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

BURNED OVERHEAD STOWAGE BIN ON ROW POSITION 13 RH SIDE AT PASSENGER CABIN (1 EA) 2023-143132<[01] PERFORMED EMERGENCY LIGHT PROBLEM FIM 33-50 TASK 801 THEN FOUND MISSING STOWAGE BIN ROW 13 POSITION RH GROUND LIGHT PLATE EMERGENCY LIGHT THE FAULT WAS RESOLVED REPLACED HOUSING ASSY AND PERFORMED EMERGENCY LIGHT OPERATIONAL TEST IAW AMM 33-51-00-710-801 TEST IS OK;[02] TASK CARD COMPLETE.

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

CORROSION ANGLE LOCATED BS 727 BTW STRG 25L TO STR 25R AT AFT CARGO COMPARTMENT 2023-143124<[01] REPLACED ANGLE LOCATED BS 727 BTW STRINGER 25L TO STRINGER 25R AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02.;[02] TASK COMPLETED

Part: ANGLE — BROKEN (ZN 100 FUS LOWER) · airframe 59,557 hrs · 35,743 cycles

BROKEN SUPPORT ANGLE ON ACCESS PANEL 834DZ ENTRY DOOR L2 AT PASSENGER CABIN 2023-143117<[01] REPLACED SUPPORT ANGLE ON ACCESS PANEL 834DZ ENTRY DOOR L2 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND DWG 411A2119 REV. -;[02] CORRECTED STEP 1<BR>REPLACED SUPPORT ANGLE ON ACCESS PANEL 834DZ ENTRY DOOR L2 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG 411A2119 REV. -;[03] CERTIFIED STEP 2 COMPLETED

Part: COVER — BROKEN (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

BROKEN SLIDE COVER VISOR ENTRY DOOR AT AFT GALLEY AREA (1 EA) 2023 143111<[01] REPLACED SLIDE COVER VISOR ENTRY DOOR AT AFT GALLEY AREA (1 EA) IAW SOPM 20-50-01 REV.38;[02] REPLACED SLIDE COVER VISOR ENTRY DOOR AT AFT GALLEY AREA (1 EA) IAW SOPM 20-50-01 REV.38. JOB COMPLETED.

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 59,558 hrs · 35,743 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS214 AT RT WING 2023-143012<[01] REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED IRSS 214 AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG # 115A2001; SHEET 32 AND REV -.;[02] REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED IRSS 214 AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG # 115A2001; SHEET 32 AND REV -.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 59,558 hrs · 35,743 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING 2023-143018<[01] REPLACED CORRUGATED PLATE LOCATED ON ORSS 241 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 30 AND REV A.;[02] CORRECTED STEP 1.<BR>REPLACED CORRUGATED PLATE LOCATED ON ORSS 241 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 30 AND REV A. SEE INDIVIDUALS SIGN-OFF BELOW.;[03] REPLACED CORRUGATED PLATE LOCATED ON ORSS 241 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 30 AND REV A. SEE INDIVIDUALS SIGN-OFF BELOW.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 59,558 hrs · 35,743 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT LT WING 2023-143014<[01] REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED ORSS 261 AT LT WING. IAW B737-700 SRM 51-40-02. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: RADOME — DELAMINATED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

DELAMINATED WIFI ANTENNA RADOME AT UPPER FUSELAGE 2023-143006<[01] TOOL USED: CALIPER P/N:500-196-30 S/N:A20226522 DUE DATE: 12-SEP-23;[02] TOOL USED HOT BONDER PN:HCS9200B-AV ; SN:18196127 DUE DATE 22/JAN/24;[03] TOOL USED: MULTIMETER P/N: FLUKE 87 S/N: 44560136 DUE DATE: 07-MAR-24.;[04] REPAIRED WIFI ANTENNA RADOME AT UPPER FUSELAGE IAW SAINT GOBAIN SRM 5214-100 SECTION III; D.4.(CLASS 2;3;4 MAJOR REPAIR PROCEDURES). SEE INDIVIDUAL SIGNOFFS BELOW.;[05] TASK COMPLETED.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 59,558 hrs · 35,743 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS214 AT LT WING 2023-143016<[01] REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED IRSS 214 AT LT WING. IAW B737-700 SRM 51-40-02. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 59,558 hrs · 35,743 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING 2023-143011<[01] REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED ORSS 261 AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG # 115A2001; SHEET 32 AND REV -.;[02] CORRECTED STEP 1.<BR>REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED ORSS 261 AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG # 115A2001; SHEET 32 AND REV -. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[03] REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED ORSS 261 AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG # 115A2001; SHEET 32 AND REV -. ?SEE INDIVIDUAL SIGNOFFS BELOW?.<BR>TASKCARD COMPLETED

Part: DEPRESSOR — CRACKED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

CRACK SERVICE DOOR CUT OUT REVEAL DEPRESSOR LOCATED AT BS 294.5 AND STR 9R AT FWD GALLEY AREA 2023-142992<[01] REPLACED REVEAL DEPRESSOR LOCATED AT BS 294.5 AND STRINGER 9R AT FWD GALLEY AREA. IAW B737-700 SRM 51-40-02; DWG # 141A8370 SHEET 9; REV D. AND EA # M-21-153-03542 REV A.;[02] CORRECTED STEP 1.<BR>REPLACED REVEAL DEPRESSOR LOCATED AT BS 294.5 AND STRINGER 9R AT FWD GALLEY AREA. IAW B737-700 SRM 51-40-02; DWG # 141A8370 SHEET 9; REV D. AND EA # M-21-153-03542 REV A. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[03] REPLACED REVEAL DEPRESSOR LOCATED AT BS 294.5 AND STRINGER 9R AT FWD GALLEY AREA. IAW B737-700 SRM 51-40-02; DWG # 141A8370 SHEET 9; REV D. AND EA # M-21-153-03542 REV A. ?SEE INDIVIDUAL SIGNOFFS BELOW.

Part: STUB FRAME — CRACKED (ZN 900 LAV/GALLE) · airframe 59,558 hrs · 35,743 cycles

CRACK SERVICE DOOR CUT OUT STUB FRAME LOCATED AT BS 294.5 AND BTW STR 8R AND STR 9R AT FWD GALLEY AREA 2023-142991<[01] REPLACED STUB FRAME LOCATED AT BS 294.5 AND BTW STRINGER 8R AND 9R AT FWD GALLEY AREA. IAW B737-700 SRM 51-40-02; DWG # 141A8370 SHEET 9; REV D; AND DWG# 141A3310; SHEET 20 AND REV -. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[02] REPLACED STUB FRAME LOCATED AT BS 294.5 AND BTW STRINGER 8R AND 9R AT FWD GALLEY AREA. IAW B737-700 SRM 51-40-02; DWG # 141A8370 SHEET 9; REV D; AND DWG# 141A3310; SHEET 20 AND REV -. ?SEE INDIVIDUAL SIGNOFFS BELOW?.<BR>TASKCARD COMPLETED

Part: WEB — BROKEN (ZN 400 NACELLE/P) · airframe 59,557 hrs · 35,743 cycles

BROKEN WEB OUTBOARD FAN COWL ON RT ENGINE 2023-142964<[01] REPLACED WEB AND FASTENERS LOCATED OUTBOARD FAN COWL ON RT ENGINE; IAW BOEING 737-700 SRM 51-40-02 AND BOEING 737-700 CMM 71-13-30 FIGURE 3 (SHEET 5 OF 8).;[02] REPLACED WEB AND FASTENERS LOCATED OUTBOARD FAN COWL ON RT ENGINE; IAW BOEING 737-700 SRM 51-40-02 AND BOEING 737-700 CMM 71-13-30 FIGURE 3 (SHEET 5 OF 8).

Part: ANGLE — CORRODED (ZN 500) · airframe 59,558 hrs · 35,743 cycles

CORROSION FUEL BOOST PUMP ANGLE LOCATED IRSS145 AFT POSITION AT LT WING 2023-142943<[01] REPLACED FUEL BOOST PUMP ANGLE LOCATED IRSS145 AFT POSITION AT LT WING IAW B737-700 SRM 51-10-02-0G-0<BR>SEE INDIVIDUAL SIGNOFF STEP BELOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: STRAP — CORRODED (ZN 600 RIGHT WIN) · airframe 59,558 hrs · 35,743 cycles

CORROSION FRONT SPAR LOWER STRAP LOCATED OFSS463 AT RT WING 2023-142947<[01] TOOL USED USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138103 CAL DUE DATE: 11-APR-23<BR><BR>TOOL USED PN ULTRASONIC EQUIPMENT PN:45MG; SN: 130066701; DUE DATE: 08-APR-23;[02] REPAIRED FRONT SPAR LOWER STRAP LOCATED OFSS463 AND OSS 227.95 AT RT WING IAW EA 23-157-00877 REV. 1 AND EA 23-157-00877 WIP1 REV. 1. SEE INDIVIDUAL SIGNOFF BELOW.;[03] CERTIFIED STEP 2; COMPLETED

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

CRACK SUPPORT BRACKET BODY STATION 540 AND RBL 6 RH SIDE AT AIR CONDITIONING BAY 2023-142939<[01] REPLACED SUPPORT BRACKET BODY STATION 540 AND RBL 6 RH SIDE AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9;[02] TASK COMPLETED

Part: TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

CRACK TRACK RBBL 13.84 LOCATED BS727E AT AFT CARGO COMPARTMENT 2023-142890<[01] TOOL USED : EDDY CURRENT EQUIPMENT P/N NORTEC500D S/N N500X12101U102020 DUE DATE: 30-AUG-23.;[02] TOOL USED : EDDY CURRENT EQUIPMENT P/N NORTEC500D S/N N500X12101U102020 DUE DATE: 30-AUG-23.;[03] REPAIRED CRACK TRACK RBBL 13.84 LOCATED BS727E TO BS 787 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 AND ALTERNATIVE 2. SEE INDIVIDUAL SIGNOFF BELOW;[04] REPAIRED CRACK TRACK RBBL 13.84 LOCATED BS727E TO BS 787 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 AND ALTERNATIVE 2. RII;SEE INDIVIDUAL SIGNOFF BELOW.

Part: STRAP — CORRODED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

CORROSION STRAP LOC BS 794 TO BS 807 AFT CARGO COMPARTMENT 2023-142900<[01] REPLACED STRAP AND FASTENERS LOC. BS 794 TO BS 807 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 146A8340 REV: ?. SEE INDIVIDUAL SIGNOFFS BELLOW.;[02] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: INTERCOSTAL — CORRODED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

CORROSION WEB - INTERCOSTAL LOC BS 787 TO BS 807 AT LEVEL STR 27R AFT CARGO COMPARTMENT 2023-142901<[01] REPLACED WEB - INTERCOSTAL LOC BS 787 TO BS 807 AT LEVEL STR 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 146A8130 SHEET 12 REV B. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

CORROSION SUPPORT ZEE BS 747 TO BS 767 RBL 22 WL 156 AFT CARGO COMPARTMENT 2023-142903<[01] EQUIPMENT P/N 45MG; S/N 130066701; DUE DATE 08-APR-23 WAS USED.;[02] REPLACED SUPPORT ZEE LOCATED BS 727 TO BS 767 RBL 22 WL 156 AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-10-02 AND DWG 146A7502; SHEET 26; REV. - AND DWG 146A7500; SHEET 85; REV. A.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[03] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PANEL — ELONGATED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

ELONGATED HOLE ON PLATE LOCATED ON ACCESS PANEL 431AT LT PYLON (2 E/A ) 2023-142871<[01] REPLACED PLATE LOCATED ON ACCESS PANEL 431AT LT PYLON (2 E/A ) IAW B737-700 SRM 51-10-02;[02] REPLACED PLATE LOCATED ON ACCESS PANEL 431AT LT PYLON (2 E/A ) IAW B737-700 SRM 51-10-02

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

CORROSION SUPPORT ZEE BS 787 AT LEVEL STR 26L WL 156 LBL 22 AFT CARGO COMPARTMENT 2023-142902<[01] REPLACED SUPPORT ZEE LOCATED BS 727 TO BS 847 AT LEVEL STR 26L WL 156 LBL 22 AT AFT CARGO IAW B737-700 SRM 51-10-02 AND SRM 53-00-53-2R-5 REPAIR 5 FIGURE 202; DWG 146A7500 SHEET 1 REV B. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT ZEE LOCATED BS 727 TO BS 847 AT LEVEL STR 26L WL 156 LBL 22 AT AFT CARGO IAW B737-700 SRM 51-10-02 AND SRM 53-00-53-2R-5 REPAIR 5 FIGURE 202; DWG 146A7500 SHEET 1 REV B. RII;SEE INDIVIDUAL SIGN OFF<BR>BELOW.

Part: STRAP — CORRODED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

CORROSION STRAP LOC BS 787 TO BS 794 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT 2023-142899<[01] REPLACED STRAP LOC BS 787 TO BS 794 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 146A0081 REV. A <BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: BEAM — CRACKED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

CRACK TRACK RBBL 13.84 LOCATED BS767 AT AFT CARGO COMPARTMENT 2023-142892<[01] REPAIRED OF TRACK RBBL 13.84 LOCATED BS767 AT AFT CARGO COMPARTMENT IS DOCUMENTED ON CARD TTG8Q00J692J. SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPAIRED FLOOR BEAM LOCATED BS 294.5 RBL 20 TO RBL 60 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16. SEE INDIVIDUAL SIGNOFF BELOW.

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

CRACK ANGLE - SUPPORT LOCATED BS867 AND BTW LBL8.1 AND LBL12.5 AT AFT CARGO COMPARTMENT 2023-142895<[01] REPLACED ANGLE - SUPPORT LOCATED BS867 AND BTW LBL8.1 AND LBL12.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 149A8102 REV: ?. SEE INDIVIDUAL SIGNOFFS BELLOW.;[02] REPLACED ANGLE - SUPPORT LOCATED BS867 AND BTW LBL8.1 AND LBL12.5 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 149A8102 REV: ?. SEE INDIVIDUAL SIGNOFFS BELLOW.

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

CRACK ON SUPPORT ANGLE ON CEILING AREA LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2023-142814<[01] REPLACED SUPPORT ANGLE AND FASTENERS ON CEILING AREA LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN; IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND BOEING 737-700 DWG 146A7901; SHEET 17; REV:-. ?SEE INDIVIDUAL SIGN OFF BELOW?.;[02] REPLACED SUPPORT ANGLE AND FASTENERS ON CEILING AREA LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN; IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND BOEING 737-700 DWG 146A7901; SHEET 17; REV:-. ?SEE INDIVIDUAL SIGN OFF BELOW?. RII

Part: INTERCOSTAL — CRACKED (ZN 900 LAV/GALLE) · airframe 59,558 hrs · 35,743 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY 2023-142736<[01] TOOL USED CALIPER P/N: 500-196-30:; S/N: A21126170; DUE DATE: 09-NOV-23.;[02] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED ON FLOOR STRUCTURE LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY I.A.W.B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 141A5400 SHEET 44 REV-. <BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: STRUCTURE — CRACKED (ZN 200 FUS TOP) · airframe 59,557 hrs · 35,743 cycles

CRACK ON WEB FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 RBL33 AT FWD GALLEY AREA 2023-142728<[01] REPLACED WEB FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 RBL33 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 DWG 141A5400 SHEET : 39 REV - . SEE INDIVIDUAL SIGN-OFF BELOW;[02] RII ITEM <BR>REPLACED WEB FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 RBL33 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 DWG 141A5400 SHEET : 39 REV - . SEE INDIVIDUAL SIGN-OFF BELOW<BR>TASKCARD COMPLETÏ¿½D;[03] RII ITEM <BR>REPLACED WEB FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 RBL33 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 DWG 141A5400 SHEET : 39 REV - . SEE INDIVIDUAL SIGN-OFF BELOW <BR>TASKCARD COMPLETÏ¿½D

Part: BEAM — CRACKED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

CRACK ON FLOOR BEAN LOCATED BS 294.5 RBL 52 WL 208.1 AT FWD GALLEY AREA 2023-142732<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X12101V022235; DUE DATE: 03 AUG 23;[02] TOOL USED P/N: XRP-3000; S/N: 1998072; DUE DATE: 03-MAY-2023;[03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24.;[04] REPAIRED FLOOR BEAM LOCATED BS 294.5 RBL 20 TO RBL 60 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16. SEE INDIVIDUAL SIGNOFF BELOW.;[05] REPAIRED FLOOR BEAM LOCATED BS 294.5 RBL 20 TO RBL 60 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16. RII;SEE INDIVIDUAL SIGNOFF BELOW.

Part: INTERCOSTAL — CRACKED (ZN 900 LAV/GALLE) · airframe 59,557 hrs · 35,734 cycles

CRACK ON WEB INTERCOSTAL FLOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 33 AT FWD GALLEY AREA 2023-142729<[01] REPLACED WEB INTERCOSTAL LOC. FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 33 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02;SRM 51-40-02 DWG 141A5400 SHEET: 33 REV -SEE INDIVIDUAL SIGN-OFF BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: BEAM — CORRODED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

CORROSION ON EXISTING REPAIR OF FLOOR BEAM BS986.5 LBL43 AND WL208 AT AFT GALLEY AREA 2023-142745<[01] REPLACED EXISITNG REPAIR ON FLOOR BEAM BS986.5 LBL50 TO RBL50 AND WL208 IAW EA 23-153-00763 REV1; EA 23-153-00763-WIP1 REV1; EA 23-153-00763-WIP2 REV1 AND EA 23-153-00763-WIP3 REV3. SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED EXISITNG REPAIR ON FLOOR BEAM BS986.5 LBL50 TO RBL50 AND WL208 IAW EA 23-153-00763 REV1; EA 23-153-00763-WIP1 REV1; EA 23-153-00763-WIP2 REV1 AND EA 23-153-00763-WIP3 REV3. SEE INDIVIDUAL SIGNOFF BELOW RII VERIFIED

Part: INTERCOSTAL — CRACKED (ZN 900 LAV/GALLE) · airframe 59,558 hrs · 35,743 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 15 AT FWD GALLEY AREA 2023-142735<[01] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 15 AT FWD GALLEY AREA I.A.W.B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 141A5400 SHEET 13 REV -:. <BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

CORROSION ON SUPPORT ANGLE LOCATED BTW BS 294.5 TO BS 328 RBL 53 WL 208.1 AT LEVEL STR 17R AT FWD GALLEY AREA 2023-142734<[01] TOOL USED DIGITAL CALIPER P/N: 500-197-30; S/N:A18109059; DUE DATE:04-SEP-23;[02] REPLACED SUPPORT ANGLE LOCATED BTW BS 294.5 TO BS 328 RBL 53 WL 208.1 AT LEVEL STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8310 SHEET 23 AND REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2. REPLACED SUPPORT ANGLE LOCATED BTW BS 294.5 TO BS 328 RBL 53 WL 208.1 AT LEVEL STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8310 SHEET 25 AND REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPLACED SUPPORT ANGLE LOCATED BTW BS 294.5 TO BS 328 RBL 53 WL 208.1 AT LEVEL STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8310 SHEET 25 AND REV -. SEE INDIVIDUAL SIGN OFF BELOW.

Part: INTERCOSTAL — CRACKED (ZN 900 LAV/GALLE) · airframe 59,558 hrs · 35,743 cycles

CRACK ON WEB-INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 294.5 TO BS 312 RBL 17 FWD GALLEY AREA 2023-142730<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30; S/N:A21043225; DUE DATE:06-SEP-23.;[02] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED ON FLOOR STRUCTURE LOCATED BTW BS 294.5 TO BS 312 RBL 17 FWD GALLEY AREA I.A.W. B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 ITEM 9; AND DRAWING #141A5400 SHEET 41 ; REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED TASK COMPLETE RII <BR>REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED ON FLOOR STRUCTURE LOCATED BTW BS 294.5 TO BS 312 RBL 17 FWD GALLEY AREA I.A.W. B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 ITEM 9; AND DRAWING #141A5400 SHEET 41 ; REV -. <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: GIRT BAR — DETERIORATED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

DETERIORATED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT AFT GALLEY AREA 2023-142686<[01] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT AFT GALLEY AREA I.A.W. B737-700 AMM 25-66-02-400-801. THE INSTALLATION IS DOCUMENTED ON MT 725-025-00-02Y STEP 4.A(13);[02] TASK COMPLETED

Part: GIRT BAR — DETERIORATED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

DETERIORATED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA 2023-142685<[01] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA I.A.W. B737-700 AMM 25-66-02-400-801. THE INSTALLATION IS DOCUMENTED ON MT 725-025-00-01Y STEP 4.A(11);[02] TASK COMPLETED

Part: PANEL — ELONGATED (ZN 100 FUS LOWER) · airframe 59,558 hrs · 35,743 cycles

ELONGATED HOLE BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT 2023-142714<[01] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DWG 453A2510 SHEET:12 REV: - MATERIAL USED CONOLITE P/N:A60SG4W 60144 P/O:2022-195910;[02] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DWG 453A2510 SHEET:12 REV: - MATERIAL USED CONOLITE P/N:A60SG4W 60144 P/O:2022-195910

Part: PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 59,558 hrs · 35,743 cycles

CRACK ACCESS PANEL 661BB ON HOLES AT RT WING 2023-142656<[01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 17-OCT-23.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 24-JAN-24.;[03] TOOL USED SCALE P/N: SPX621 S/N: 8340225441 DUE DATE: 20-JUL-23.;[04] TOOL USED: MULTIMETER P/N: FLUKE-37 S/N: 5115017 DUE DATE: 08-MAR-23.;[05] REPAIRED ACCESS PANEL 661BB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW;[06] REPAIRED ACCESS PANEL 661BB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: FLOOR PANEL — CRACKED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

CRACK FLOOR PANEL 242XF AT AFT GALLEY AREA 2023-142652<[01] TOOL USED CALIPER: P/N: 500-464 S/N:B17030933 DUE DATE: 17-OCT-23.;[02] TOOL USED: SCALE P/N: SPX621 S/N: 8340225441 DUE DATE: 20-JUL-23;[03] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18175478; DUE DATE: 24-SEP-23;[04] REPAIRED FLOOR PANEL 242XF AT AFT GALLEY AREA IAW B737- 700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] TASK COMPLETED. RII COMPLETED

Part: PANEL — ELONGATED (ZN 600 RIGHT WIN) · airframe 59,558 hrs · 35,743 cycles

ELONGATED HOLE ACCESS PANEL 621NB AT RT WING 2023-142654<[01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 17-OCT-23.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 24-JAN-24.;[03] TOOL USED: SCALE: P/N:SPX621 S/N:8340225441 DUE DATE:20-JUL-23.;[04] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 24-JAN-24.;[05] TOOL USED: MULTIMETER P/N: 2217-20 S/N: B83B914290482 DUE DATE: 16-DEC-23.;[06] REPAIRED ACCESS PANEL 621NB AT RT WING IAW B737-700 SRM 51-70-04-2R-9. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] REPAIRED ACCESS PANEL 621NB AT RT WING IAW B737-700 SRM 51-70-04-2R-9.

Part: INTERCOSTAL — CRACKED (ZN 900 LAV/GALLE) · airframe 59,557 hrs · 35,743 cycles

CRACK ON INTERCOSTAL LOCATED BTW BS 291.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2023-142635<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 291.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02-0G-0;SRM 51-10-02-0G-0 ITEM 9 AND DWG 141A8180 SHEET 27 REV C.SEE INDIVIDUAL SING-OFF BELOW.;[02] CORRECTED STEP 1: REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 291.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02-0G-0;SRM 51-10-02-0G-0 ITEM 9 AND DWG 141A8180 SHEET 27 REV C.SEE INDIVIDUAL SIGN-OFF BELOW.;[03] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 291.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02-0G-0;SRM 51-10-02-0G-0 ITEM 9 AND DWG 141A8180 SHEET 27 REV C.SEE INDIVIDUAL SIGN-OFF BELOW.<BR>RII

Part: BEAR STRAP — CRACKED (ZN 900 LAV/GALLE) · airframe 59,557 hrs · 35,743 cycles

CRACK ON BEAR STRAP LOCATED BS 291.5 PLUS 4 INCHES BTW STR 9R TO STR 10R AT FWD GALLEY AREA 2023-142633<[01] REPAIRED BEARSTRAP AT R1 DOOR UPPER FWD CORNER LOC BS 277+11? TO BS 312 AND BTW STRINGER 6R TO 10R AT FWD GALLEY AREA. IAW EA# M-21-153-03542 REV.3. SEE INDIVIDUAL SIGNOFF BELOW.;[02] CORRECTED STEP 1: REPAIRED BEARSTRAP AT R1 DOOR UPPER FWD CORNER LOC BS 277+11? TO BS 312 AND BTW STRINGER 6R TO 10R AT FWD GALLEY AREA. IAW 737-700 SRM 53-10-01-2R-6 AND EA M-21-153-03542. SEE INDIVIDUAL SIGNOFF BELOW.;[03] TASK COMPLETED ; RII ; SEE INDIVIDUAL SIGNOFF BELOW

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 59,557 hrs · 35,743 cycles

CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2023-142632<[01] TOOL USED DIGITAL CALIPER P/N:500-193-30;S/N:0000293;DUE DATE:12-OCT-23.;[02] TOOL USED: RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1998072; DUE DATE: 03-MAY-23.;[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 SIGNOFFS 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.

Part: FLOOR PANEL — DELAMINATED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

DELAMINATED FLOOR PANEL 241ADF AT AT AFT GALLEY AREA 2023-142651<[01] TOOL USED CALIPER: 500-196-30 S/N:0000288 DUE DATE: 27-DEC-23.;[02] TOOL USED: HOT BONDER P/N: HCS9000B S/N: 16122983 DUE DATE: 24-JAN-24;[03] TOOL USED SCALE P/N: 1863T62 S/N: AE-40571 DUE DATE: 09 JUN 23;[04] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 16122983; DUE DATE: 24-JAN-24.;[05] TOOL USED: SCALE P/N: SPX621; S/N: 8340225441; DUE DATE: 20-JUL-23.;[06] REPAIRED FLOOR PANEL 241ADF AT AFT GALLEY AREA IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] JOB COMPLETED RII.

Part: FRAME — CRACKED (ZN 900 LAV/GALLE) · airframe 59,558 hrs · 35,743 cycles

CRACK FRAME ON BS 312 BTW STR 5L TO 6L AT FWD GALLEY AREA 2023-142624<[01] REPAIRED FRAME LOCATED AT BS 312 BTW STR 5L TO 6L AT FWD GALLEY AREA IAW EA: M-22-153-01244 REV 2;[02] CORRECTED ITEM 1.<BR>REPAIRED FRAME LOCATED AT BS 312 BTW STR 5L TO 6L AT FWD GALLEY AREA IAW EA: M-22-153-01244 REV 2. SEE INDIVIDUAL SIGNOFFS BELOW;[03] CERTIFIED STEP 2; COMPLETED

Part: TIE CLIP — CRACKED (ZN 900 LAV/GALLE) · airframe 59,558 hrs · 35,743 cycles

CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-142627<[01] REPLACED TIE CLIP LOC. ON BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 AND REV -.<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED TIE CLIP LOC. ON BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 AND REV -. <BR>SEE INDIVIDUAL SIGNOFF BELOW RII CERTIFIED

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

CRACK SUPPORT ANGLE LOCATED BS 695 BL 0 RH SIDE CENTER SECTION 2023-142554<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS 695 BL 0 RH SIDE CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 111A6000; SHEET 50; REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS 695 BL 0 RH SIDE CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 111A6000; SHEET 50; REV: A. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 59,558 hrs · 35,743 cycles

CRACK ANGLE TRAILING EDGE SEAL LOCATED DEFLECTOR CONTROL RIB IRSS 271 AT RT WING 2023-142546<[01] REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTOR CONTROL RIB IRSS 271 AT RT WING IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 115A2930 SHEET 8; REV. -;[02] REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTOR CONTROL RIB IRSS 271 AT RT WING IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 115A2930 SHEET 8; REV. -<BR>TASKCARD COMPLETED

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 CENTER SECTION 2023-142553<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] REPLACED SUPPORT ANGLE LOCATED FLOOR STRUCTURE; BS 695 RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV A. MATERIAL USED: 7075-T0 P.O: 2022 227459 SEE INDIVIDUAL SIGNSOFF BELOW.;[03] CORRECTED STEP 2: REPLACED SUPPORT ANGLE LOCATED FLOOR STRUCTURE; BS 695 RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 111A6000 SHEET 234 REV -. MATERIAL USED: 7075-T0 P.O: 2022 227459 SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPLACED SUPPORT ANGLE LOCATED FLOOR STRUCTURE; BS 695 RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 111A6000 SHEET 234 REV -. MATERIAL USED: 7075-T0 P.O: 2022 227459 SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

INOP BATTERY PACKS ON LOWERED CEILING AT FWD GALLEY AREA (2EA). 2023-142560<[01] REPLACED BATTERY PACKS ON LOWERED CEILING AT FWD GALLEY AREA LT AND RT SIDE I.A.W B737-700 AMM 33-51-06-960-805. SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] REPLACED BATTERY PACKS ON LOWERED CEILING AT FWD GALLEY AREA LT AND RT SIDE I.A.W B737-700 AMM 33-51-06-960-805. SEE INDIVIDUAL SIGN-OFFS BELOW.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

INOP BATTERY PACKS ON LOWERED CEILING AT FWD GALLEY AREA (2EA). 2023-142560<[01] REPLACED BATTERY PACKS ON LOWERED CEILING AT FWD GALLEY AREA LT AND RT SIDE I.A.W B737-700 AMM 33-51-06-960-805. SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] REPLACED BATTERY PACKS ON LOWERED CEILING AT FWD GALLEY AREA LT AND RT SIDE I.A.W B737-700 AMM 33-51-06-960-805. SEE INDIVIDUAL SIGN-OFFS BELOW.

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 BL 0 CENTER SECTION 2023-142550<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 695 BL 0 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DWG 273A9112 SHEET 31 REV -. MATERIAL USED: BAC1490-2883; P.O. 2022 17809. SEE INDIVIDUAL SIGNSOFF BELOW.;[03] CORRECTED STEP 2: REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 695 BL 0 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV A. MATERIAL USED: BAC1490-2883; P.O. 2022 17809. SEE INDIVIDUAL SIGN OFF BELOW.;[04] CORRECTED STEP 3: REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 695 BL 0 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV A. MATERIAL USED: BAC1490-2883; P.O. 2022 178029. SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 695 BL 0 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV A. MATERIAL USED: BAC1490-2883; P.O. 2022 178029. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

INOP BATTERY PACK ON LOWERED CEILING AT AFT GALLEY AREA (1 EA) 2023-142562<[01] REPLACED BATTERY PACK ON LOWERED CEILING AT AFT GALLEY AREA RT SIDE I.A.W B737-700 AMM 33-51-06-960-805.<BR>SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] REPLACED BATTERY PACK ON LOWERED CEILING AT AFT GALLEY AREA RT SIDE I.A.W B737-700 AMM 33-51-06-960-805. <BR>SEE INDIVIDUAL SIGN-OFFS BELOW.

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 59,558 hrs · 35,743 cycles

CRACK ANGLE TRAILING EDGE SEAL LOCATED DEFLECTOR CONTROL RIB AT LT WING 2023-142545<[01] REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTOR CONTROL RIB AT LT WING IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 115A2930 SHEET 7; REV. -;[02] REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTOR CONTROL RIB AT LT WING IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 115A2930 SHEET 7; REV. -<BR>TASKCARD COMPLETED

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 BL 0 LT SIDE CENTER SECTION 2023-142557<[01] REPLACED ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE BS 695 BL 0 LT SIDE CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 111A6000; SHEET 50; REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE BS 695 BL 0 LT SIDE CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 111A6000; SHEET 50; REV: A. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: LIGHT — DETERIORATED (ZN 200 FUS TOP) · airframe 59,558 hrs · 35,743 cycles

DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT AND RT SIDE AT PASSENGER CABIN (7 EA) 2023-142484<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT AND RT SIDE AT PASSENGER CABIN (7 EA) IAW B737-700-AMM 33-51-15-400-802;[02] TASK COMPLETED

Part: SLAT — CRACKED (ZN 600 RIGHT WIN) · airframe 59,558 hrs · 35,743 cycles

CRACK LOWER SURFACE SLAT 8 EXTERNAL SKIN AT LEVEL SLAT STATION 451.97 RT WING 2023-142481<[01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN:210138103; DUE DATE: 11-APR-23;[02] TOOL USED PN NORTEC 600D SN 220272712 DUE DATE 17-DEC-23;[03] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138203 AND DUE DATE: 11-APR-23.;[04] PERFORMED PERMANENT REPAIR LOWER SURFACE SLAT 8 EXTERNAL SKIN AT LEVEL SLAT STATION 451.97 RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1 FIGURE 202 SHEET 1 .SEE INDIVIDUAL STEP SIGNOFF BELOW;[05] PERFORMED PERMANENT REPAIR LOWER SURFACE SLAT 8 EXTERNAL SKIN AT LEVEL SLAT STATION 451.97 RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1 FIGURE 202 SHEET 1 .SEE INDIVIDUAL STEP SIGNOFF BELOW<BR>RII

Part: FLOORBOARD — CRACKED (AFT CARGO) · airframe 58,797 hrs · 35,236 cycles

AFT CARGO FLOORBOARD 140BF HAS AN 18 IN CRACK IN THE CENTER AFT SECTION. / [01] OK TO CONTINUE PER MEL 25-16-01 SP#1B;[02] R&R AFT CARGO FLOOR PANEL PER AMM 25-52-10

Part: WEB — CRACKED (CENTER WING BOX) · airframe 58,046 hrs · 34,711 cycles

STA 663 RIGHT HAND CENTER TANK LOWER ATTACH ANGLE COMMON TO VAPOR BARRIER WEB IS CRACKED AT RBL 42 AND WL 167.68 / [01] APPLIED EWIS PROTECTION TO REPAIR AREA IAW AMM 20-60-07;[02] REMOVED OTBD U CHANNEL TO FOM IAW SRM 57-10-1-2R-5;[03] DISPLACE WING TO BODY SUPPORT STIFFENER TO FOM IAW SRM 57-10-10-2R-5;[04] REMOVED ALL FASTENERS FROM REPAIR AREA IAW SRM 57-10-10-2R-5;[05] VERIFIED ACTIONS 1 - 4 ARE COMPLETE;[06] CUT OUT DAMAGED AREA OF ANGLE IAW SRM 57-10-10-2R-5;[07] PERFORMED DETAILED VISUAL INSPECTION OF REPAIR AREA AND UNDERLYING STRUCTURE; NO DEFECTS NOTED IAW SRM 57-10-10-2R-5;[08] RECEIVED -1 REPLACEMENT ANGLE FABRICATED ON BACK SHOP W/O 44079-6000-0001 AND -2 SPLICE ANGLE FABRICATED ON BACK SHOP W/O 44079-6000-0002 IAW SRM 51-10-10-2R-5;[09] VERIFIED ACTIONS 6 - 8 ARE COMPLETE;[10] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 16. NO DEFECTS NOTED. TOOL#31823; DUE 23DEC22;[11] VERIFIED STEPS 6; 7 & 8 C/W;[12] FABRICATE REPAIR PARTS IAW SRM 57-10-10-2R-5;[19] INSTALLED U CHANNEL REMOVED IN ITEM 2 IAW SRM 51-40-02-0G-0 AND DWG 111A1000 SH 171.;[20] INSTALLED ALL REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. ALL FASTENERS INSTALLED WET WITH BMS5-95 B-2 MIXED AT 1200 19AUG22. SQUEEZE OUT AT 1600 19AUG22; FINAL CURE AT 1200 21AUG22. ALL PERMANENT FASTENERS INSTALLED BEFORE SQUEEZE OUT.

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,046 hrs · 34,711 cycles

DOT A-24-04. MID CABIN FLOOR PANEL 232SF HAS PULLED FIBERS ON TOP SIDE OF PANEL / [01] EVALUATED DAMAGE; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD; NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR IAW B737 SRM 53-00-50-2R-1; PAR 3 STEPS A;C;E; AND F.<BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201 RESIN EPOCAST 50A (A137335); FIBERGLASS CLOTH BMS9-3 (A10269).<BR><BR>REQUIRES OKAY TO BOND REPAIR PLIES.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1; PAR 3 STEPS K;L; AND M. CURED AT 150 DEGREES; THERMOMETER AAR30347; CAL DUE 4/30/23. TAP TEST GOOD.;[04] REPAIRED CABIN FLOOR PANEL 232SF TOP SIDE IAW B737 SRM 53-00-50-2R-1; PAR 3.;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,046 hrs · 34,711 cycles

DOT A-24-03. MID CABIN FLOOR PANEL 231XF HAS PULLED FIBERS ON TOP SIDE OF PANEL / [01] EVALUATED FLOOR PANEL 231XF FOUND WITH IN REPAIRABLE LIMITS OF B737-700 SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED FLOOR PANEL 231XF FOR WET LAY UP IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (A-J);[03] VERIFIED MATIERIALS TO BE USED FOR WET LAY-UP ON UPPER SURFACE OF FLOOR PANEL 231XF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 TABLE 201 FABRIC- BMS9-3 TYPE H3 (A13436) RESIN- BMS8-201 TYPE IV (137346) POTTING COMPOUND- BMS5-28 TYPE 19 (A133227);[04] OK TO BOND WET LAY-UP TO UPPER SURFACE OF FLOOR PANEL 231XF;[05] VERIFIED STEPS 1-4 C/W; OK TO BOND GIVEN;[06] BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 231XF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS (K-O) REPAIR COMPLETE;[07] JOB COMPLETE; AUDIT C/W

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,046 hrs · 34,711 cycles

DOT A-24-05. MID CABIN FLOOR PANEL 242BF HAS PULLED FIBERS ON TOP SIDE OF PANEL / [01] EVALUATED DAMAGE ON UPPER SURFACE OF FLOOR PANEL 242BF; FOUND WITH-IN LIMITS OF SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED UPPER SURFACE OF FLOOR PANEL 242BF FOR WET LAY-UP IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (A-J);[03] VERIFIED MATERIALS FOR WET LAY-UP ON UPPER SURFACE OF FLOOR PANEL 242BF IAW B737-700 SRM 53-00-50-2R-1 REPAIR TABLE 201<BR><BR>FABRIC BMS9-3 TYPE H3 (A13436)<BR>RESIN BMS8-201 TYPE IV (A137346)<BR>POTTING COMPOUND BMS5-28 TYPE 19 (A133227);[04] OK TO BOND WET LAY-UP TO UPPER SURFACE OF FLOOR PANEL 242BF;[05] VERIFIED STEPS 1-4 C/W; OK TO BOND GIVEN;[06] BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 242BF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS (K-O)<BR><BR>REPAIR COMPLETE;[07] JOB COMPLETE; AUDIT C/W

Part: WEB — CRACKED (CENTER WING BOX) · airframe 58,046 hrs · 34,711 cycles

STA 663 LEFT HAND CENTER TANK LOWER ATTACH ANGLE COMMON TO VAPOR BARRIER WEB IS CRACKED AT LBL 6.8 (JUST OB OF KEEL BEAM) AND WL 167.68 / [01] APPLIED EWIS PROTECTION TO REPAIR AREA IAW AMM 20-60-07;[02] REMOVED ALL FASTENERS IN AREA AND CUT OUT DAMAGED SECTION OF ANGLE IAW SRM 57-10-10-2R-5;[03] PERFORMED DETAILED VISUAL INSPECTION OF REPAIR AREA AND UNDERLYING STRUCTURE; NO DEFECTS NOTED IAW SRM 57-10-10-2R-5;[04] VERIFIED STEPS 1 - 3 ARE COMPLETE;[05] RECEIVED -1 REPLACEMENT ANGLE FABRICATED ON BACK SHOP W/O 44079-5000-0001 AND -2 SPLICE ANGLE FABRICATED ON BACK SHOP W/O 44079-5000-0002 IAW SRM 51-10-10-2R-5;[06] VERIFIED ACTION 5 IS COMPLETE;[07] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 16. NO DEFECTS NOTED. TOOL#31823; DUE 23DEC22;[08] VERIFIED STEPS 2; 3 & 5 C/W;[09] FABRICATED REPAIR PARTS IAW SRM 57-10-10-2R-5;[10] VERIFIED STEP 9 C/W; OK GIVEN TO TREAT AND PRIME;[11] APPLIED ALODINE AND PRIMER REPAIR PARTS IAW SRM 51-20-01 AND AMM 51-21-72-370-804;[12] VERIFIED STEP 11 C/W; OK GIVEN TO INSTALL REPAIR PARTS;[13] FAULT TTG8Q00EA1AG GENERATED TO TRACK EWIS PROTECTION;[14] INSTALLED ALL REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. ALL FASTENERS INSTALLED WET WITH BMS5-95 B-2 MIXED AT 1200 19AUG22. SQUEEZE OUT AT 1600 19AUG22; FINAL CURE AT 1200 21AUG22. ALL PERMANENT FASTENERS INSTALLED BEFORE SQUEEZE OUT.;

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,046 hrs · 34,711 cycles

DOT A-24-01. MID CABIN FLOOR PANEL 231ZF HAS PULLED FIBERS ON TOP SIDE OF PANEL. / [01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;C;E; AND F. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; FIBERGLASS CLOTH BMS9-3 (A10269); RESIN EPOCAST 50A (A137335). REQUIRES OKAY TO BOND REPAIR PLIES.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEPS 3K;L;M. TAP TEST GOOD. TOOLING-- AAR30347 DUE 4-30-23;[04] REPAIRED DAMAGE TO UPPER SURFACE OF FLOOR BOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD;[05] VERIFIED STEPS COMPLETE; AUDIT COMPLIED WITH

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 58,046 hrs · 34,711 cycles

DOT A-24-02. MID CABIN FLOOR PANEL 231YF HAS PULLED FIBERS ON TOP SIDE OF PANEL / [01] EVALUATED AND FOUND PULLED FIBERS ON UPPER SURFACE. DAMAGE IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1 CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3A;C;E;F VERIFIED REPAIR MATERIALS AS GLASS--BMS9-3 (A10269); RESIN--EPOCAST 50A/9816 (A137335) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEPS 3K;L;M. CURED IN OVEN--B0-06 DUE 11-8-22. TAP TEST GOOD;[04] REPAIRED DAMAGE TO UPPER SURFACE OF FLOOR BOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD.;[05] VERIFIED STEPS COMPLETE; AUDIT COMPLIED WITH

Part: LAMP — INOPERATIVE (L/H OVERWING) · airframe 57,797 hrs · 34,550 cycles

LH SLIDE/OVERWING EMERGENCY LIGHT INOP. / [01] REPLACED LH SLIDE/OVERWING EMERGENCY LIGHT LAMP REF AMM 33-51-04. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 57,733 hrs · 34,506 cycles

CABIN EMERGENCY EXIT LIGHTS IN BULLNOSE AT ROWS 8;11;13 RH SIDE INOP / [01] R&R EMERGENCY LIGHT BATTERY PACK PER AM 33-51-06; OPS CK GOOD

Part: BRACKET — CORRODED (L1 DOOR) · airframe 56,760 hrs · 33,874 cycles

CORROSION ON FWD ENTRY DOOR GIRT BAR BRACKET MOUNTING FIXTURES ARE CORRODED. STA 312; LBL 55; WL 208.6; AND STA 344; LBL 59; WL 208.6 / [01] REMOVED CABIN FLOOR PANEL 221GF FOR ACCESS IAW AMM 53-21-00-000-801;[02] CORROSION ON FED GIRT BAR BRACKET MOUNTING FIXTURE BS 344 LBL 59 WL 208.6 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS GIVEN IN SRM. REMOVED AND REPLACED MOUNTING FIXTURE PER SRM 51-40-02-0G-0.;[03] VERIFIED CORRECTIVE ACTION 2; INSTALLATION OF BRACKET BS 344 LBL 59 WL 208 COMPLETE.;[04] FED GIRT BAR BRACKET MOUNTING FIXTURE BS 312; LBL 55; WL 208.6 TO BE REPLACED ON CUSTOMER CARD# TTG8Q00B8A52;[05] VERIFIED CORRECTIVE ACTION 4; FED GIRT BAR BRACKET MOUNTING FIXTURE BS 312; LBL 55; WL 208.6 TO BE REPLACED ON CUSTOMER CARD# TTG8Q00B8A52;[06] COMPLETED STEP 1;[07] COMPLETED STEP 2;[08] OK TO CLOSE FLOOR PANEL 221GF;[09] VERIFIED OK TO CLOSE FLOOR PANEL 221GF (ALSO ACCOMPLISHED IN STEP 2);[10] COMPLETED STEP 3;[11] VERIFIED COMPLETION OF STEP 3;[12] FLOOR PANEL IN STEP 3 WAS ACCOMPLISHED USING TOOL ID PER1762; S/N ALO23649; CAL DATE 12/2022;[13] ADDED CAL TOOL ID

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 56,760 hrs · 33,874 cycles

CORROSION ON FLOOR SUPPORT AT STA 294.5+10; RBL 10; WL 208.1. / [01] VERIFIED APPLICABILITY OF SRM 53-10-51-1A-1 ALLOWABLE DAMAGE; REMOVED CORROSION ON FLOOR SUPPORT AT STA 294.5+10 RBL10; WL208.1; MEASURES L: .5' W: .4' D: .012' FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1 STEP 4.F TOOL ID:ATS2677; S/N:UNKNOWN; DUE:11/2022;[02] CERTIFY;[03] VERIFIED CORRECTIVE ACTION 1; OUT OF LIMITS;[04] REMOVED FLOOR SUPPORT AT BS 294.5-312; RBL10 PER SRM 51-40-02. LOCATED AND DRILLED NEW FLOOR SUPPORT PER SRM 51-40-05 AND DWG 141A5400; REQUEST OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION #4;[06] INSTALLED FLOOR SUPPORT AT BS 294.5-312; RBL10 PER SRM 51-40-02 AND DWG 141A5400;[07] VERIFIED CORRECTIVE ACTION 6

Part: BRACKET — CORRODED (L1 DOOR) · airframe 56,760 hrs · 33,874 cycles

CORROSION ON FED GIRT BAR BRACKET MOUNTING FIXTURE BS 312; LBL 55; WL 208.6 / [01] CORROSION ON FED GIRT BAR BRACKET MOUNTING FIXTURE BS 312; LBL 55; WL 208.6 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS GIVEN IN THE SRM. REMOVED AND REPLACED PER SRM 51-40-02-0G-0;[02] REJECTION OF INSTALLATION OF BRACKET BS 312 LBL 55 DUE TO O/B ATTACH FASTENER MISSING WASHER UNDER NUT; SEE STEP 1 FOR REJECTION.;[03] COMPLETED STEP 1;[04] VERIFIED COMPLETION OF STEP 1. ALL WORK COMPLETE.;[05] CORRECTED STEP 1 ITEM WAS ACCOMPLISHED USING TOOL ID PER 324; S/N ALM08209 CAL DATE 5-22;[06] ADDED CAL TOOL ID

Part: INTERCOSTAL — CORRODED (FWD FUSELAGE) · airframe 56,760 hrs · 33,874 cycles

CORROSION ON FLOOR SUPPORT AT STA 270+14; LBL 12; WL 208.1 / [01] NO SRM FOUND FOR ALLOWABLE DAMAGE ; REPACEMENT OF THE PART IAW SRM 51-10-02-0G-0 STEP 9;[02] CERTIFY;[03] VERIFIED CORRECTIVE ACTION 1;[04] COMPLETED STEPS 1; 5; AND 8;[05] COMPLETED STEP 2;[06] ALL REMOVALS DONE PER SRM 51-40-02-0G-0;[07] LOCATING AND DRILLING ACCOMPLISHED IN STEP 2 DONE PER SRM 51-40-05;[08] VERIFIED COMPLETION OF STEPS 1; 2; 5; AND 8 AND CORRECTIVE ACTIONS 4-7.;[09] COMPLETED STEP 3;[10] COMPLETED STEP 3; OK TO INSTALL;[11] COMPLETED STEP 6.;[12] COMPLETED STEP 6. OK TO INSTALL;[13] COMPLETED STEP 9 OK TO INSTALL;[14] COMPLETED STEP 9;[15] VERIFY APPLICABILITY FOR SRM 51-40-02-0G-0.;[16] CORRECTION TO STEP 15. <BR>NO APPLICABILITY STATEMENT NEEDED.;[17] UPON FURTHER INVESTIGATION BEFORE COMPLETING INSTALLATION OF INTERCOSTAL AT BL 0 BS270 TO 294.5 WAS FOUND CRACKED AND NEEDS TO BE REPLACED.<BR>LOCATED AND DRILLED NEW INTERCOSTAL AT BS 270 TO 294 BL 0 PER SRM 51-40-02 AND DWG 141A5400.<BR>REQUEST OK TO INSTALL.;[18] VERIFIED CORRECTIVE ACTION #17.<BR>VERIFIED OK TO INSTALL.;[19] UPDATED STEPS 4;7 AND 10.;[20] CERTIFIED;[21] COMPLETED CORRECTIVE ITEM 18 COVERED<BR>BY STEP 10 INSTALLED INTERCOSTAL BS 277-294 BL 0 WL 204-208 PER SRM 51-40-02 AND DWG 141A5400. PER;[22] COMPLETED STEP 4 AND 7;[23] VERIFIED COMPLETE;[24] CHECKED PARTS REQUIREMENT;[25] CORRECTED P/N IN MEASUREMENT TABLE FROM A U3 TO A -3;[26] CERTIFY

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 56,760 hrs · 33,874 cycles

CORROSION ON LAV MOUNT INTERCOSTAL BS 294-312; LBL 11; WL 208 / [01] CORRODED LAV MOUNT INTERCOSTAL BS 294-312; LBL 11; WL 208 OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS GIVE IN SRM.;[02] REMOVED 2EA FASTENERS BS 294.5 FLOOR BEAM COMMON TO LOWER CHORD LBL 6-7 PER SRM 51-40-02-0G-0;[03] UPDATED MEASUREMENT TABLE AND COMPLETED STEPS 1; 5; 7; 10; 13; 16; 19; AND 22;[04] ALL REMOVALS DONE PER SRM 51-40-02-0G-0;[05] COMPLETED STEPS 2 AND 3.;[06] COMPLETED STEPS 2 AND 3; OK TO INSTALL;[07] COMPLETED STEP 4; PARTIAL UPDATE STEP 6.;[08] VERIFIED CORRECTIVE ACTION 7.;[09] COMPLETED STEP 6. INSTALLED PULLEY BRACKET IAW SRM 51-40-02.;[10] VERIFIED CORRECTIVE ACTION 9; INSTALLED PULLEY BRACKET IAW SRM 51-40-02.;[11] UPDATED STEPS 8;11; 14; 17 AND 20.;[12] VERIFIED APPLICABILITY FOR SRM 51-40-02-0G-0.;[13] VERIFIED APPLICABILITY FOR SRM 51-40-02-0G-0. <BR>VERIFIED COMPLETE STEPS 8; 11; 14; 17; 20.;[14] CORRECTION TO STEP 12.<BR>NO APPLICABILITY STATEMENT NEEDED.;[15] UPDATED STEPS 9; 12; 15; 18; 21 AND 23.;[16] CERTIFIED;[17] COMPLETED STEPS 9;15;18;23;[18] COMPLETED STEPS 12 AND 21;[19] CHECKED PARTS REQUIREMENT;[20] VERIFIED COMPLETE

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,760 hrs · 33,874 cycles

CORROSION ON EXTERIOR FUSELAGE SKIN BS 887 +0.5' BETWEEN STR 24L AND STR 25L / [01] VERIFIED SRM 53-00-01-1A-1 IS APPLICABLE FOR ALLOWABLE LIMITS TO FUSELAGE SKIN BS 887-1016 STR 23L-23R;[02] VERIFIED CORRECTIVE ACTION 1;[03] REMOVED 4EA FASTENERS IN AFFECTED AREA PER SRM 51-40-02-0G-0 FIG. 8;[04] MECHANICALLY REMOVED EXTERIOR FINISH IN DISCREPANT AREA 9.2'X2.6' PER AMM 51-21-72-370-801 PARA. 2E(5)(B)2; BLENDED CORROSION AT BS 887 - 887+1' BETWEEN STR 24L AND 25L IN AN AREA OF 4.4'X1.0' PER SRM 51-10-02 NDI TO DETERMINE REMAINING THICKNESS; ORIGINAL IS .063';[05] VERIFIED CORRECTIVE ACTION 4;[06] REQUEST NDI TO UT INSPECT BLEND AREA FOR REMAINING THICKNESS. ORIGINAL IS .063';[07] UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.049' ADJACENT TO 0.063'. <BR>EQUIP USED: EPOCH 650 ID: ATS2031;[08] BLEND AT BS 887 BETWEEN STR 24L AND 25L FOUND TO BE OUT OF LIMITS PER SRM 53-00-01-1A-1;[09] VERIFIED CORRECTIVE ACTION 8; OUT OF LIMITS;[10] AS PER EA 22-153-00749; THE DAMAGE IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.;[11] RESTORED EXTERIOR DECORATIVE PAINT PER AMM 51-21-73-370-801;[12] REPAIRED PER EA 22-153-00749;[13] VERIFIED CORRECTIVE ACTIONS #10;11 AND 12;[14] VERIFIED TASK COMPLETE;[15] UPDATED MEASUREMENT TABLE;[16] CHANGED REPAIR TYPE IN MEASUREMENT TABLE

Part: THRESHOLD — CORRODED (FWD FUSELAGE) · airframe 56,756 hrs · 33,873 cycles

FWD LAVATORY THRESHOLD IS CORRODED / [01] REMOVED CORRODED AND INSTALLED NEW FWD LAV THRESHOLD INSERTS IAW CMM 25-00-66 REPAIR 8-1 SECT. 1-3;[02] AFTER FURTHER INSPECTION; FWD LAVATORY THRESHOLD IS NOT CORRODED. INSERTS WERE FOUND TO BE CORRODED UNDER THE THRESHOLD. REMOVED CORRODED AND INSTALLED NEW FWD LAV THRESHOLD INSERTS IAW CMM 25-00-66 REPAIR 8-1 SECT. 1-3;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2

Part: PANEL — DELAMINATED (LT WING) · airframe 54,267 hrs · 32,412 cycles

LEFT WING PANEL 521 WB DAMAGED WITH A CURLED CORNER. ; / C/W EA 21-157-01346; C/W EA 21-157-01346; C/W EA 21-157-01346

Part: PANEL — DELAMINATED (LT WING) · airframe 54,267 hrs · 32,412 cycles

LEFT WING PANEL 521 WB DAMAGED WITH A CURLED CORNER. ; / C/W EA 21-157-01346; C/W EA 21-157-01346; C/W EA 21-157-01346

Part: PAN — CRACKED (R2 DOOR) · airframe 53,993 hrs · 32,250 cycles

R-2 DOOR PAN ASSY CRACKED AND BENT IN SEVERAL PLACES ASSY # 411A2119-174A / REMOVED & REPLACED R2 DOOR PAN ASSY PER B737 AMM 52-41-31-400-802.

Part: DOUBLER — CRACKED (VAPOR BARRIER) · airframe 53,993 hrs · 32,250 cycles

FOUND EXTERNAL DOUBLER AT LT HAND VAPOR BARRIER CRACK AT STA 663.5 ; LBL 20 ; WL 148 . / FABRICATED EXTERNAL DOUBLER FOR LT HAND VAPORT BARRIER AS PER DRAWING REF 111A1511-23. LOCATED AND DRILLED PART AS PER SRM B737-7 51-40-05-0G-0. TREATED AND PRIMED DOUBLER AS PER AMM 737-7 51-21-41-701 AND 51-21-72-370-803. INSTLLATION WILL BE ACCOMPLISHED ON N/R W208792 REF 2017142/1000/0040

Part: FLOORBEAM — CORRODED (FWD CARGO) · airframe 53,993 hrs · 32,250 cycles

CORROSION AT FWD CARGO AFT BULKHEAD FLOOR SUPPORT STA 500D; S-25L TO S-25R; WL 154. / REMOVED AND INSTALLED NEW FLOOR SUPPORT AT FWD CARGO STA 500D BETWEEN STR 25L AND 25R IAW B737-700 SRM 51-40-02-0G-0

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 53,993 hrs · 32,250 cycles

Z CHANEL AT ST 460 TO 480 ;LBL 23 HAVE SURFACE CORROSION AROUND 3 NUTPLATE (228-036)_WL 154 / REMOVED AND INSTALLED NEW 'Z' CHANNEL (SIDE PLATE) AT FWD CARGO LBL 23' FROM 396 TO STA 480+11' IAW B737-700 SRM 51-40-02-0G-0; 53-00-53-2R-5 AND DOCUMENT NUMBER 143A7500 (WL 154)

Part: SHIELD — CORRODED (FWD CARGO) · airframe 53,993 hrs · 32,250 cycles

SHIELD AT ST 500 TO 500A ;RBL 24 HAVE SURFACE CORROSION AROUND 2 NUTPLATE (228-037) WL 154 / REMOVED; REPLACED AND INSTALLED NEW SHIELD PLATE AT FWD CARGO COMPARTMENT AT STA 500 TO STA 500A RBL 24' IAW B737-700 SRM 51-40-02-0G-0; 51-40-05-0G-0 AND DWG #143A8126 (WL 154)

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 53,993 hrs · 32,250 cycles

CORROSION AFT CARGO COMP BILGE AREA TRACK FITTING TOP SURFACE EVIDENCE OF SURFACE CORROSION FROM BS 787 TO BS 887 RBL-14 .MKD 126-018. WL 148; RBL 14 / REMOVED AND REPLACED TRACK FITTING FOR AFT CARGO FLOOR SUPPORT STRUCTURE LOCATED AT RBL 14; WL 148 BETWEEN STA 767+12' TO STA 887 AS PER B737-7 SRM 51-40-02-0G-0 AND DWG REF 146A7501. ACCOMPLISHED SQUEEZED OUT AND FASTENER INSTALLATION AS PER B737-7 SOPM 20-50-19. (TIME MIXED 11:00 HRS; TIME APPLIED 11:30 HRS)

Part: FLOORBEAM — CRACKED (PAX CABIN) · airframe 53,993 hrs · 32,250 cycles

PASSENGER CABIN FLOOR SUPPORT CRACKED AT B S. 540 R.BL.1'.(51-005) / REMOVED AND REPLACED FLOOR SUPPORT AT MAIN CABIN; STA 540; RBL 1' TO RBL 23' REF B-737-700 SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 DW: 143A5240.

Part: FLOORBEAM — CRACKED (CABIN) · airframe 53,993 hrs · 32,250 cycles

PASSENGER CABIN FLOOR SUPPORT ANGLE CRACKED AT B.S. 540 L.BL. 1'.(51-004) / REMOVED AND REPLACED FLOOR SUPPORT AT MAIN CABIN; STA 540; LBL 1' TO LBL 23' REF B-737-700 SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 DW: 143A5240.

Part: CHANNEL — CORRODED (AFT CARGO) · airframe 53,993 hrs · 32,250 cycles

CORROSION AFT CARGO COMP RH ZEE ANGLE SHOWS SEVERAL SPOTS OF SURFACE CORROSION FROM BS 727C TO BS 767 .MKD 126-020.RBL 21 WL 155.5. / CLEANED CORROSION AT AFT CARGO R/H 'Z' CHANNEL FROM STA 727 TO 767 AS PER B737-7 SRM 51-10-02-0G-0; CORROSION REMAIN ON PART AND EXFOLIATION FOUDN AT STA 727E TO 747 FOUND TO BE OUT OF LIMITS AS PER B737-7 SRM 51-10-02-0G-0 AND 53-00-53-1A-2. REMOVED 'Z' CHANNEL AS PER B737-7 SRM 51-40-02-0G-0. FABRICATED NEW 'Z' CHANNEL AS PER B737-7 51-40-05-06-0; SRM 51-40-08-0G-0 AND DWNG 146A7502. INSTALLED NEW 'Z' CHANNEL AT AFT CARGO R/H AS PER B737-7 SRM 51-40-02-0G-0 AND DWGN 146A7500

Part: SUPPORT ANGLE — CORRODED (AFT CARGO) · airframe 53,993 hrs · 32,250 cycles

CORROSION AFT CARGO COMP FWD BULKHEAD CENTER SECTION PNEUMATIC DUCT COVER SUPPORT ANGLE BROKEN BS 727 RBL-2 .MKD 126-24 / REMOVED AND REPLACED AFT CARGO FWD BULKHEAD CENTER SECTION PNEUMATIC DUCT COVER SUPPORT ANGLE AS PER B737-7 SRM 51-40-02-06-0

Part: WEB — CORRODED (AFT CARGO) · airframe 53,993 hrs · 32,250 cycles

CORROSION AFT CARGO COMP WEB UPPER SURFACE SEVERAL SPOTS WITH SURFACE CORROSION FROM BS 767 TO BS 787.RBL-22 . MKD 126-021 WL 155.5 / REMOVED AND REPLACED FLOOR STRUCTURE WEB FOR AFT CARGO COMP BETWEEN STA 767 TO 787 RBL-22 AS PER REF B737-7 SRM 51-40-02-0G-0 AND DWG REF 146A8127. TREATED AND PRIMED AREA AS REQUIRED AS PER B737-7 AMM 51-21-72-370-803 AND 51-21-72-370-803.

Part: CHANNEL — CORRODED (AFT CARGO) · airframe 53,993 hrs · 32,250 cycles

CORROSION>>>>>>> AFT CARGO COMP L/H ZEE ANGLE SEVERAL SPOTS WITH SURFACE CORROSION FROM BS-827 TO BS-727C .MKD 126-019 WL 155; LBL 21. / CLEANED AND REMOVED CORROSION FROM 'Z' CHANNEL AT LT SIDE FROM STA 727C TO STA 827. CORROSION STILL NOTED PASSED 50% OF MATERIAL; FOUND OUT OF LIMITS AS PER SRM 53-00-53-1A-2. REMOVED 'Z' CHANNEL AS PER SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW 'Z' CHANNEL SRM 51-40-08-0G-0. FABRICATED NEW SPLICE REPAIR FOR LH 'Z' CHANNEL AS PER SRM 53-00-53-2R-5. INSTALLED NEW 'Z' CHANNEL AND SPLICE BETWEEN STA 737E TO STA 747 AS PER B737 SRM 51-40-02-0G AND DWG 146A7502

Part: PANEL — CORRODED (FWD CARGO) · airframe 53,993 hrs · 32,250 cycles

CORROSION ON FWD CARGO COMPARTMENT AFT BLKHD PANEL 121HW RIGHT SIDE LOWER CORNER.(51-001) / REPLACED FWD CARGO COMPARTMENT AFT BULKHEAD PANEL 121HW IAW B737-700 SRM 53-00-53-1A-2 FIG 103 DETAIL D / SRM 51-40-0-0G-0 (PANEL WILL BE INSTALL ON CUSTOMER ORDER / CARD JPANEL-121-CLOSE SEQUENCE # 212 - 1193)

Part: SKIRT — OUT OF POSITION (L1 DOOR SLIDE) · airframe 53,993 hrs · 32,250 cycles

L1 DOOR SLIDE SKIRT DRAGGING / REPOSITIONED L1 DOOR SLIDE SKIRT PER B737 AMM 25-66-01-400-803.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 53,993 hrs · 32,250 cycles

L1 DOOR SLIDE GIRT HANGING LOW EXCESSIVELY / REPOSITIONED L1 DOOR SLIDE GIRT PER B737 AMM 25-66-01-400-803.

Part: BEAM — CRACKED (R1 DOOR) · airframe 53,993 hrs · 32,250 cycles

PERFORMED HFEC INSPECTION ON LOWER BEAM 141A6536-14. CRACK INDICATION OBTAINED AT FILLET REGION OF FWD HOLE IAW NDTM PART 6;51-00-00 PROCEDURE 23. R-1 DOOR / REMOVED; REPLACED AND INSTALLED NEW LOER BEAM AT FOWARD SERVICE DOOR (R-1 DOOR) AS PER CMM 52-41-05; DRWG # 141A6516 DRWG# 141A6535; B737-700 SRM 51-40-02-0G-0; 51-440-05-0G-0

Part: GIRT BAR — OUT OF POSITION (L2 DOOR) · airframe 53,993 hrs · 32,250 cycles

L2 DOOR SLIDE GIRT HANGING LOW EXCESSIVELY / REPOSITIONED L2 DOOR SLIDE GIRT PER B737 AMM 25-66-01-400-803.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,993 hrs · 32,250 cycles

CABIN FLOOR PANEL 241AF IS DELAMINATE (228-010) / CLEANED REMOVED DAMAGE AND REPAIRED DAMAGE AREA AS MARKED ON MAIN CABIN FLOOR PANEL TAP-TEST FOUND NO DELAMINATION ON REPAIRED AREAS AS PER B737 NDTM 51-05-01 (SEC 5) MATERIAL USED PO # 1700692 AND PO # 1150387.

Part: BULKHEAD WEB — CRACKED (MLG WW) · airframe 53,993 hrs · 32,250 cycles

LH STA 663 VAPOR BARRIER CRACKED / PERFORMED TAP TEST AND VISUAL INSPECTION AT VAPOR BARRIER PER REF B737 NDTM 51-05-01. PERFORMED STOP DRILL ON CRACK SRM 57-10-10-2R-2; APPLY DRY-OUT VAPOR BARRIER PER SRM 51-70-04-2R-0; REPAIR DAMAGED AREA AT VAPOR BARRIER ON STA. 663 PER REF SRM 51-70-04-2R-0. MATERIAL USED RESING EY 3804 P.O. 1707887; PERFORMED TAP TEST NO DELAMINATION FOUND ON REPAIR AREA IAW B737 NTM 51-05-01 LOCATED AND DRILLED HOLES TO REPAIRED AREA VAPOR BARRIER STA 663 IAW 51-40-05-06-0. PERPARED AND PAINTED ON L/H STA 663 VAPOR BARRIER AS REQUIRED IAW B737 AMM 51-21-81-370-80 DWG. 111A1001 SA 2503 3-21-21.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 53,993 hrs · 32,250 cycles

LEFT WING UPPER PANEL TO REAR SPAR SUPPORT ANGLE IS CRACKED AT UPPOER SIDE ABOVE FASTENER. ( SI # 7570629 ) / REMOVED AND REPLACED SUPPORT ANGLE AT LEFT WING UPPER PANEL TO REAR SPAR IAW 737-700 SRM 51-40-02-0G-0 & SRM 51-40-05-0G-0 AND BOEING DWG # 115A2000

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 53,993 hrs · 32,250 cycles

RIGHT WING UPPER PANEL TO REAR SPAR SUPPORT ANGLE IS CRACKED AT UPPER SIDE ABOVE FASTENER.( SI # 7570628 ) / REMOVED AND REPLACED SUPPORT ANGLE AT RIGHT WING UPPER PANEL TO REAR SPAR IAW 737-700 SRM 51-40-02-0G-0 & SRM 51-40-05-0G-0 AND BOEING DWG # 115A2000

Part: FILTER — FAULTY (CABIN) · airframe 52,483 hrs · 31,332 cycles

DURING CLIMBOUT WE NOTICED A SMELL (LIKE BURNT BAGELS). NO SMOKE WAS VISIBLE. THE FLIGHT ATTENDANTS REPORTED THE SAME CONDTIONS IN THE CABIN. WE DECLARED AN EMERGENCY, COMPLIED WITH CHECKLISTS AND RETURNED TO DEN. THE CONDITIONS MAY HAVE IMPROVED SLIGHTLY WHEN WE TURNED OFF THE RECIRC FAN. COMPLIED WITH FIM 21-00 TASK 806 R&R RECIRCULATION AIR FILTER IN REF TO AMM 21-25-01, R&R R AND L COALESCER BAGS IN REF TO AMM 21-51-05, PERFORMED SUCCESSFUL ENGINE RUN IN REF TO AMM 71-00-00. NO ODORS OR DISCREPENCIES NOTED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,582 hrs · 30,748 cycles

R/H EMERGENCY LIGHT BULB INOPERATIVE AT SEAT 3. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,582 hrs · 30,748 cycles

R/H EMERGENCY LIGHT BULB INOPERATIVE AT SEAT 7. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,582 hrs · 30,748 cycles

R/H EMERGENCY LIGHT BULB INOPERATIVE AT SEAT 9. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,582 hrs · 30,748 cycles

R/H EMERGENCY LIGHT BULB INOPERATIVE AT SEAT 4. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,582 hrs · 30,748 cycles

R/H EMERGENCY LIGHT BULB INOPERATIVE AT SEAT 23. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,582 hrs · 30,748 cycles

L/H EMERGENCY LIGHT BULB INOP AT SEAT 3. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,582 hrs · 30,748 cycles

L/H EMERGENCY LIGHT BULB INOP AT SEAT 5. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,582 hrs · 30,748 cycles

L/H EMERGENCY LIGHT BULB INOP AT SEAT 2. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,582 hrs · 30,748 cycles

R/H EMERGENCY LIGHT BULB INOPERATIVE AT SEAT 5. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,582 hrs · 30,748 cycles

L/H EMERGENCY LIGHT BULB INOP AT SEAT 11. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,582 hrs · 30,748 cycles

R/H EMERGENCY LIGHT BULB INOPERATIVE AT SEAT 21. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,582 hrs · 30,748 cycles

L/H EMERGENCY LIGHT BULB INOP AT SEAT 9. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,582 hrs · 30,748 cycles

L/H EMERGENCY LIGHT BULB INOP AT SEAT 20. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,582 hrs · 30,748 cycles

R/H EMERGENCY LIGHT BULB INOPERATIVE AT SEAT 10. / R&R BULB PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,582 hrs · 30,748 cycles

L/H EMERGENCY LIGHT BULB INOP AT SEAT 8. / R&R BULB PER AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 51,327 hrs · 30,599 cycles

L/H OUTBOARD FORWARD FLOOR BOARD SUPPORT INTERCOSTAL BETWEEN BS. 312 TO BS. 328 CRACKED AT CENTER FLOOR BOARD ATTACH FASTENER HOLE / R&R INTERCOSTAL PER SRM.

Part: COVER — MISSING (RT OVRWNG LIGHT) · airframe 49,945 hrs · 29,683 cycles

R/H OVERWING EMERGENCY EXIT LIGHT MISSING COVER. INSTALLED LIGHT IAW AMM.

Part: HANDLE — BROKEN (L2 DOOR) · airframe 49,938 hrs · 29,678 cycles

AFT ENTRY DOOR ASSIST HANDLE BROKEN. R&R ASSIST HANDLE PER AMM.

Part: RIVET — LOOSE (SERVICE DOOR) · airframe 49,644 hrs · 29,498 cycles

ESCAPE SLIDE GIRT BAR STOWAGE HOOKS LOOSE. R&R RIVETS PER SRM.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 49,035 hrs · 29,131 cycles

R/H OVER WING EMERGENCY EXIT FORWARD LIGHT HAD 3 BULBS BURNT OUT. / R&R BULBS IAW AMM.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 49,035 hrs · 29,131 cycles

L/H OVER WING EMERGENCY EXIT LIGHT HAD 2 BULBS BURNT OUT. / R&R BULBS IAW AMM.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 49,035 hrs · 29,131 cycles

R/H OVERWING EMERGENCY EXIT AFT LIGHT HAD 3 BULBS BURNT OUT. / R&R BULBS IAW AMM.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 49,035 hrs · 29,131 cycles

AFT OUTBOARD WHEEL WELL PANEL 193CR IS DELAMINATED ON FWD EDGE. / REFERENCE DEFECT NO. T914544 PANEL 193CR ROBBED FROM N7723E AND INSTALLED ON DEFECT NO. T914544

Part: DOOR — CORRODED (LOWER EXT FUSELA) · airframe 49,035 hrs · 29,131 cycles

***CORROSION*** WHILE REPLACING LAV SERVICES DOOR HINGES; DOOR PANEL WAS FOUND TO BE CORRODED THROUGH AT BONDING STRAP ATTACHMENT POINT. / CORROSION ON LAV SERVICE DOOR WAS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED LAV SERVICE DOOR WITH NEW ASSY. IAW AMM 52-49-07-000-801 AND AMM 52-49-07-400-801 VERIFIED DOOR FIT; FIT CHECKED GOOD IAW AMM 52-49

Part: SKIN — CRACKED (L1 DOOR) · airframe 49,035 hrs · 29,131 cycles

FORWARD ENTRY DOOR INNER SKIN CRACKED AT THE 4TH FROM BOTTOM STOP PIN FITTING. / REPAIRED SKIN IAW EA AND ER.

Part: FRAME — CRACKED (L1 DOOR) · airframe 49,035 hrs · 29,131 cycles

FORWARD ENTRY DOOR AFT FRAME CRACKED AT THE 4TH FROM BOTTOM STOP PIN FITTING. / REPAIRED FRAME IAW EA AND ER.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 49,035 hrs · 29,131 cycles

R/W T/E BULB SEAL RETAINER AT ORSS 271 IS CRACKED. / REMOVED AND REPLACED R/W I/E BULB SEAL RETAINER AT ORSS 271 IAW SRM 51-40-02-0G-2

Part: PANEL — DELAMINATED (LT WING) · airframe 49,035 hrs · 29,131 cycles

PANEL 521KB CUTOUT CORNERS ARE DELAMINATED / PANEL 521KB CUTOUT CORNERS DELAMINATIONS WERE REPAIRED IAW SRM 51-70-05-2R-6 56144U 04/17/2019.

Part: FLOOR SKIN — DAMAGED (COCKPIT) · airframe 49,035 hrs · 29,131 cycles

FLIGHT DECK FLOOR DAMAGED AT BS. 253, BETWEEN LBL 15 TO RBL 4. / REPAIRED FLIGHT DECK FLOOR IAW EA AND ER.

Part: SCUFF PLATE — CRACKED (CARGO DOOR FRAME) · airframe 49,035 hrs · 29,131 cycles

AFT CARGO DOOR CUT OUT AFT CORNER SCUFF PLATE CRACKED. / R&R SCUFF PLATE IAW EA AND AMM.

Part: SCUFF PLATE — CRACKED (CARGO DOOR FRAME) · airframe 49,035 hrs · 29,131 cycles

AFT CARGO DOOR CUTOUT FORWARD CORNER SCUFF PLATE CRACKED. / R&R SCUFF PLATE IAW AMM AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,908 hrs · 28,418 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 47,774 hrs · 28,333 cycles

LT WING INBOARD AFT FLAP DELAMINATED. R&R AFT FLAP PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 47,702 hrs · 28,284 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01670. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 47,702 hrs · 28,284 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01675. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 47,702 hrs · 28,284 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01672. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 47,702 hrs · 28,284 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01673. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 47,702 hrs · 28,284 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01674. R&R BATTERY PER AMM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 47,702 hrs · 28,283 cycles

RT CABIN PHOTO LUMINESCENT STRIP WATER DAMAGED AT ROW 1. R&R STRIP PER AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 47,672 hrs · 28,267 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,117 hrs · 27,927 cycles

FORWARD LT EMERGENCY LIGHT NEAR FORWARD ENTRY DOOR INOP. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,625 hrs · 26,955 cycles

FORWARD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 45,423 hrs · 26,822 cycles

NOTED BY RAMP AFT CARGO CENTER SCUFF PLATE HAS A CRACK / R&R AFT CENTER SCUFF PLATE PER AMM 53-11-02

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,352 hrs · 26,776 cycles

EXTERNAL GROUND POWER RECEPTACLE CUTOUT DOUBLER DOOR LOWER HINGE AREA CRACKED. REPAIRED THE SKIN IAW EA.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 45,342 hrs · 26,770 cycles

R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 44,951 hrs · 26,524 cycles

L1 DOOR SLIDE PACK INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED SLIDE MT.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 44,543 hrs · 26,271 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF COMPARTMENT DID NOT DEPLOY. / SECURED SLIDE IAW MT.

Part: SPLICE — CRACKED (BS 540) · airframe 42,190 hrs · 24,806 cycles

LEFT SPLICE CRACKED AT BS 540, STRINGER 22L. REPAIRED THE SPLICE IAW EA.

Part: FAIRING — CRACKED (LT WING TE FLAP) · airframe 42,190 hrs · 24,806 cycles

LEFT WING NR 3 FLAP SUPPORT FAIRING 542BB, CRACKED ON FORWARD END. REPAIRED THE FAIRING IAW EA.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 42,190 hrs · 24,806 cycles

MAIN CABIN FLOORBEAM CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24. REPAIRED THE FLOORBEAM IAW SRM

Part: ANGLE — CORRODED (BS 506) · airframe 42,190 hrs · 24,806 cycles

FORWARD CARGO RT ZEE ANGLE SHIELD CORRODED AT BS 506, STRINGER 25R. R & R THE SHIELD ASSEMBLY IAW DWG & SRM.

Part: ATTACH ANGLE — CORRODED (BS 500D) · airframe 42,190 hrs · 24,806 cycles

FORWARD CARGO BULKHEAD LOWER ATTACH ANGLE CORRODED AT BS 500D, BETWEEN LBL 25 TO RBL 25. R & R THE ATTACH ANGLE IAW DWG & SRM.

Part: BAFFLE — CRACKED (BS 500C) · airframe 42,190 hrs · 24,806 cycles

FORWARD CARGO LEFT SIDE BAFFLE ANGLE CRACKED AT BS 500C, STRINGER 25L. R & R THE BAFFLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 500A-500D) · airframe 42,190 hrs · 24,806 cycles

FORWARD CARGO RT ZEE ANGLE CORRODED BETWEEN BS 500A TO 500D, STRINGER 25R. R & R THE ANGLE IAW DWG AND SRM.

Part: ANGLE — CORRODED (BS 727D-767) · airframe 42,190 hrs · 24,806 cycles

AFT CARGO BAY RT ZEE ANGLE CORRODED BETWEEN BS 727D TO 767. R & R ZEE ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 42,190 hrs · 24,806 cycles

MAIN CABIN FLOORBEAM CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24. R & R THE FLOORBEAM IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 42,190 hrs · 24,806 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT HSS 120.30, THIRD STIFFENER BACK FROM FORWARD SPAR. REPAIRED THE RIB IAW EA.

Part: WEB — CORRODED (BS 794-847) · airframe 42,190 hrs · 24,806 cycles

AFT CARGO COMPARTMENT THRESHOLD WEB CORRODED BETWEEN BS 794 TO 847, STRINGER 25R. R & R WEB IAW DWG.

Part: ANGLE — CORRODED (BS 747-807) · airframe 42,190 hrs · 24,806 cycles

LEFT ZEE ANGLE CORRODED BETWEEN BS 807 TO 747. R & R THE ANGLE IAW SRM.

Part: SEAT TRACK — CORRODED (BS 747-767) · airframe 42,190 hrs · 24,806 cycles

RIGHT OTBD SEAT TRACK CROWN CORRODED, BETWEEN BS 747+12 - 767+6. R & R THE SEAT TRACK IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,190 hrs · 24,806 cycles

FRAME CREASE BEAM CORRODED BETWEEN BS 947 TO BS 987, ON UPPER AND LOWER SIDE OF T-CAP. R&R CREASE BEAM IAW DWG.

Part: BAFFLE — CRACKED (BS 400) · airframe 42,190 hrs · 24,806 cycles

FORWARD CARGO BAY BAFFLE ANGLE CRACKED AT BS 400, STRINGER 25L. R & R THE ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (BS 344-360) · airframe 42,190 hrs · 24,806 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO 360, BL 0. R & R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 42,190 hrs · 24,806 cycles

FUSELAGE INTERCOSTAL CRACKED AT BS 312 - 328, RBL 33. R & R THE INTERCOSTAL IAW SRM.

Part: CREASE BEAM — CORRODED (BS 291-332) · airframe 42,190 hrs · 24,806 cycles

R1 DOOR INNER CREASE BEAM BETWEEN CORRODED BETWEEN BS 291.5 TO 332.1. R & R CREASE BEAM IAW DWG & SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 42,190 hrs · 24,806 cycles

FLOOR STRUCTURE CUTOUT CORRODED AT BS 270, BETWEEN RBL 11 AND LBL 11. REPAIRED CUTOUT IAW EA.

Part: FRAME — CORRODED (BS 303) · airframe 42,190 hrs · 24,806 cycles

FRAME CORRODED AT BS 303.9, STRINGER 17L. REPAIRED THE FRAME IAW EA.

Part: CREASE BEAM — CORRODED (BS 293-348) · airframe 42,190 hrs · 24,806 cycles

L1 DOOR CREASE BEAM INNER CHORD CORRODED BETWEEN BS 293 TO 348.2. R & R CREASE BEAM IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (BS 344-360) · airframe 42,190 hrs · 24,806 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO 360, LBL 12. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (BS 261-270) · airframe 42,190 hrs · 24,806 cycles

INTERCOSTAL CORRODED BETWEEN BS 261 TO 270, BL 0. R & R INTERCOSTAL IAW SRM AND DWG.

Part: FRAME — CORRODED (BS 986.5) · airframe 42,190 hrs · 24,806 cycles

FRAME CORRODED AT BS 986.5 ON UPPER AND LOWER SIDE OF TEE CAP. REPAIRED THE FRAME IAW SRM.

Part: BRACKET — CRACKED (BS 291-296) · airframe 42,190 hrs · 24,806 cycles

CREASE BEAM L BRACKET CRACKED BETWEEN BS 291.5 TO 296.5. R & R THE BRACKET IAW DWG & SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,190 hrs · 24,806 cycles

FORWARD RIGHT EMERGENCY EXIT LIGHT BATTERY PACK M1674 INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: STRAP — OUT OF POSITION (CABIN) · airframe 41,403 hrs · 24,346 cycles

LT EMERGENCY EXIT ESCAPE STRAP OUT OF POSITION. REPOSITIONED STRAP PER AMM.

Part: LENS — MISSING (CABIN) · airframe 41,196 hrs · 24,220 cycles

RT AFT GALLEY EMERGENCY EXIT LIGHT COVER LENS MISSING. INSTALLED LENS PER EA.

Part: SLIDE — DETACHED (R2 DOOR) · airframe 40,904 hrs · 24,045 cycles

R2 DOOR EMERGENCY SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. REINSTALLED THE SLIDE IAW TC.

Part: HANDLE — BROKEN (MEGAPHONE) · airframe 40,616 hrs · 23,868 cycles

AFT MEGAPHONE HANDLE BROKEN. R & R THE MEGAPHONE IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 39,530 hrs · 23,221 cycles

FORWARD ENTRY EXIT LIGHT BROKEN. R & R FWD EMER EXIT LIGHT ASSEMBLY IAW MM.

Part: COVER — FAULTY (CABIN) · airframe 39,484 hrs · 23,200 cycles

RIGHT AFT EMER EXIT LIGHT COVER FAULTY. R & R COVER IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 38,966 hrs · 22,900 cycles

R1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW AMM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 38,727 hrs · 22,747 cycles

R2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW TC.

Part: LENS — MISSING (CABIN) · airframe 38,102 hrs · 22,373 cycles

EXIT LIGHT LENS MISSING AT R1 DOOR. INSTALLED LENS IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,288 hrs · 21,913 cycles

R1 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: FILTER — FAULTY (AC BAY) · airframe 37,089 hrs · 21,793 cycles

SMELLED EXHAUST FUMES IN COCKPIT. R & R RECIRC AIR FILTER IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,957 hrs · 21,157 cycles

RIGHT NR 1 FLIGHT DECK WINDOW ALUMINUM FRAME WEB UPPER INBD FASTENER HOLE CRACKED. REPAIRED WEB IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,957 hrs · 21,157 cycles

FORWARD SEAT TRACK FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, LBL 24. REPAIRED FLANGE IAW FAS EA.

Part: POST — CRACKED (FUSELAGE) · airframe 35,957 hrs · 21,157 cycles

RIGHT NR 3 WINDOW FRAME E - F POST SECOND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,957 hrs · 21,157 cycles

FORWARD SEAT TRACK INBD FLANGE FWD & AFT FASTENER HOLE ARE CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,957 hrs · 21,157 cycles

LEFT NR 1 WINDOW POST FRAME UPPER CORNER CRACKED. R & R FRAME ASSEMBLY IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,957 hrs · 21,157 cycles

RIGHT NR 1 WINDOW FRAME CRACKED UPPER CORNER. REPAIRED FRAME IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 35,957 hrs · 21,157 cycles

LEFT NR 3 WINDOW FRAME E - F POST SECOND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW ACO.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 35,591 hrs · 20,949 cycles

RIGHT MAIN WW 3" BELOW UPPER WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 35,591 hrs · 20,949 cycles

RIGHT MAIN WW 2" BELOW UPPER WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 35,591 hrs · 20,949 cycles

LEFT MAIN WW UPPER WEB CRACKED AT BS 663, LBL 43. REPAIRED WEB IAW EA.

Part: LIGHT — BROKEN (CABIN) · airframe 35,313 hrs · 20,798 cycles

OVERWING OVERHEAD EMER LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 35,086 hrs · 20,658 cycles

R2 DOOR, EXIT & SALIDA, SIGN BROKEN. R & R SIGN IAW MM.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 34,890 hrs · 20,542 cycles

LEFT WW FWD BULKHEAD LOWER VAPOR BARRIER CRACKED. REPAIRED BARRIER IAW EA.

Part: WINDOW — ARCED (COCKPIT) · airframe 34,858 hrs · 20,526 cycles

R1 COCKPIT WINDOW HEAT WIRE WAS ARCING. R & R R1 WINDOW ASSEMBLY IAW MM.

Part: CHECK VALVE — BROKEN (AC BAY) · airframe 33,901 hrs · 19,988 cycles

DIVERSION CLIMBING THROUGH 19,000 FEET CABIN ALTITUDE WARNING HORN SOUNDED. FOUND GND CONDITIONED AIR CHECK VLV BROKEN AT HINGE. R & R VLV IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,105 hrs · 18,955 cycles

RT FWD OVERWING EXIT INTERIOR EGRESS LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: STRINGER — CRACKED (LT WING) · airframe 32,041 hrs · 18,912 cycles

LT WING STATION 206.32, AFT MOST STRINGER CRACKED. R & R STRINGER IAW SRM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 31,865 hrs · 18,815 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 31,332 hrs · 18,481 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R & R SLIDE IAW MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 29,621 hrs · 17,479 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 29,035 hrs · 17,120 cycles

R1 DOOR EXIT SIGN BROKE. REMOVED AND REPLACED R1 DOOR EXIT SIGN PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 28,784 hrs · 16,965 cycles

R2 DOOR EMERGENCY EXIT LIGHT WIRES BROKEN. REPAIRED WIRE PER SWPM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,784 hrs · 16,965 cycles

RIGHT HORIZONTAL STABILIZER IN SPAR RIB AT STAB STA 129.50 CRACKED AT THE LOWER END OF THE 3RD VERTICAL STIFFENER FROM THE FWD END. REPAIRED RIB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,784 hrs · 16,965 cycles

FLOORBEAM CORRODED AT BS 772, LBL 8. REPAIRED FLOORBEAM IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,784 hrs · 16,965 cycles

FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED FLOORBEAM IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,784 hrs · 16,965 cycles

BULKHEAD LOWER FLOOR SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN LBL 22 TO RBL 22. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,784 hrs · 16,965 cycles

FLOORBEAM CORRODED AT BS 772, RBL 7. REPAIRED FLOORBEAM IAW EA.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 28,784 hrs · 16,965 cycles

PASSENGER CABIN FLOOR PANEL 221BF LOWER SURFACE FWD EDGE IS BROKEN. REPAIRED PANEL IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,784 hrs · 16,965 cycles

FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED FLOORBEAM IAW EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 28,784 hrs · 16,965 cycles

SKIN CORRODED AT BS 887, BETWEEN STR 24L TO STR 25L. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,784 hrs · 16,965 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,784 hrs · 16,965 cycles

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

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,784 hrs · 16,965 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.70. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,784 hrs · 16,965 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 28,267 hrs · 16,641 cycles

FWD LEFT CABIN AND GALLEY FAILED BATTERY CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES PER M/M.

Part: SPHERICAL BEARIN — LOOSE (TE FLAP) · airframe 28,267 hrs · 16,641 cycles

INBOARD LEFT FLAP INBOARD TRAILING FLT TRACK SPHERICAL BEARING IS LOOSE. REMOVED AND REPLACED BEARING PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 28,267 hrs · 16,641 cycles

AFT CABIN ROWS 8 TO 19 RIGHT SIDE FAILED CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES PER M/M.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,301 hrs · 16,091 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 25,265 hrs · 14,950 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 23,819 hrs · 14,090 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,819 hrs · 14,090 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 23,819 hrs · 14,090 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,309 hrs · 13,222 cycles

DURING SCHEDULED 6Y CHECK, FOUND LT EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,283 hrs · 13,205 cycles

DURING SCHEDULED 6Y CHECK FOUND, AFT CARGO FLOORBEAM CORRODED AT BS 904, RBL 8. REPAIRED BEAM PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 21,663 hrs · 12,852 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 20,366 hrs · 12,067 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 4. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 20,366 hrs · 12,067 cycles

DURING SCHEDULED CV CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SLIDE — DEPLOYED (L2 DOOR) · airframe 18,239 hrs · 10,773 cycles

L2 DOOR EMERGENCY EXIT SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MT.

Part: SIGN — BROKEN (CABIN) · airframe 17,710 hrs · 10,452 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 17,231 hrs · 10,185 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 17,071 hrs · 10,082 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 16,997 hrs · 10,034 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LENS — CRACKED (CABIN) · airframe 16,601 hrs · 9,791 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT EEPLS LENS CRACKED AT ROW 1. REMOVED AND REPLACED LENS PER MM.

Part: RIVET — BROKEN (GIRT BAR HOOK) · airframe 16,157 hrs · 9,519 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER HOOK BROKEN. REMOVED AND REPLACED RIVET PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 15,214 hrs · 8,946 cycles

DURING SCHEDULED RON CHECK, FOUND FWD EEPLS INOP BETWEEN ROW 1 TO ROW 4. REPAIRED WIRE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,214 hrs · 8,946 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP BETWEEN ROW 1 TO ROW 4. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,151 hrs · 8,912 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 14,082 hrs · 8,236 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED&R LIGHT ASSY. PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 12,360 hrs · 7,151 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 10,368 hrs · 5,933 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 5,548 hrs · 3,123 cycles

LT FWD CABIN EEPLS COVER LOOSE. SECURED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 1,678 hrs · 962 cycles

EEPLS TRACK LOOSE AT ROW 1. SECURED TRACK PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 1,372 hrs · 779 cycles

EEPLS TRACK LENS LOOSE AT FWD END. SECURED LENS PER MM.