N8610A

Part: SLIDE — OUT OF ALIGNMENT (ZONE 800) · airframe 43,627 hrs · 20,831 cycles

FORWARD GALLEY SLIDE LOOKS MISALIGNED. RESCURED EXCESS MATERIAL AT BOTTOM OF R1 DOOR SLIDE COMPARTMENT. VERIFIED GIRT BAR OPERATION; GIRT OPS NORMAL AND SLIDE PRESSURE GAUGE IS READABLE THROUGH SLIDE PACK WINDOW IAW AMM 25-66-01.

Part: SHIELD — BROKEN (FLASHLIGHT) · airframe 42,455 hrs · 20,214 cycles

AFT LT OTBD EMERGENCY FLASHLIGHT SHEILD BROKEN. R&R FLASHLIGHT SHEILD REF AMM 25-64-00.

Part: DOOR FRAME — CORRODED (ZONE 200) · airframe 41,519 hrs · 19,704 cycles

AFT LEFT LAVATORY DOOR POST HAS EVIDENCE OF CORROSION AT LOWER SIDE<[01] REMOVED LH AFT LAV DOOR; AND AFT DOOR FRAME TRIM. REMOVED CORRODED SECTION OF THE AFT DOOR FRAME. NO FURTHER CORROSION NOTED. FABRICATED REPAIR PART AND INSTALLED ON AFT DOOR FRAME PER CMM 25-48-25. DOOR AND DOOR TRIM INSTALLATION REQUIRED.;[02] INSTALLED TRIM AND DOOR PER AMM 25-40-14.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 41,155 hrs · 19,517 cycles

EXTERIOR EMERGENCY LIGHT AFT OF R/H WING INOP<[01] RELAMPED EXTERIOR EMERGENCY LIGHT AFT OF R/H WING IAW AMM 33-51-04

Part: FLAP SYSTEM — LOCKED (ZONE 600) · airframe 40,858 hrs · 19,379 cycles

ON APPROACH FLAP INDICATION WAS 10 WHILE FLAP HANDLE WAS AT 30. WE EXECUTED A GO AROUND AND RAN THE TRAILING EDGE FLAP DISAGREE CHECKLIST. WE EXTENDED THE FLAPS WITH THE ALTERNATE FLAPS SWITCH AND THE EXTENDED TO 15 AT A NORMAL RATE WITH NO ASYMMETRY. LANDED AND TAXIED TO THE GATE UNEVENTFULLY.<[01] PERFORMED FSEU BITE IAW FIM 27-51 TASK 801 AND TE FLAPS LOCKOUT TASK IAW FIM 27-51 TASK 836. NO FAULT LOGGED ON LAST FLIGHT LEG AND NO EXISTING FAULTS. CYCLED FLAPS IN PRIMARY MODE IAW AMM 27-81-00-710-801 AND NO FAULTS NOTED. A/C OKAY FOR SERVICE.

Part: HANDLE — OUT OF ADJUST (ZONE 800) · airframe 40,598 hrs · 19,242 cycles

FWD GALLEY SERVICE DOOR HANDLE CAM CONTACTING LOWER 4 FASTENERS.<[01] FWD GALLEY SERVICE DOOR HANDLE ADJUSTED REF. AMM 52-41-00 AND REMOVED AND REPLACED FASTENERS REF. SRM 51-40-02.

Part: PANEL — DELAMINATED (ZONE 100) · airframe 40,488 hrs · 19,180 cycles

PANEL 193AL HAS DELAMINATION<[01]. EVALUATED DAMAGE ON PANEL 193AL. FOUND PUNCTURE LENGTH .5''; WIDTH .3''; DEPTH 0.05''. APPLIED TEMPORARY SEAL PER SRM 53-40-70-1A-1. INSPECTED PER [SRM 53-40-70-1A-1-B00369 (DAMAGE NOT MORE THAN 1 PLY DEEP - SEAL WITH SPEED TAPE - 8 DAY REPEAT GVI; [02] PERFORMED NDT TAP TEST NO DEFECTS NOTED BEYOND INITIAL EVALUATION.; [03] PERFORMED REVIEW VERIFIED SRM REFERENCE.

Part: INTERCOSTAL — ELONGATED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

ELONGATED HOLE WEB - INTERCOSTAL LOC BTW BS500G TO BS500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-764829<[01] REPLACED WEB - INTERCOSTAL LOC BTW BS500G TO BS500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 AND DWG 143A7505 SHEET 108 REV. -<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: INTERCOSTAL — ELONGATED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

ELONGATED HOLE WEB - INTERCOSTAL LOC BTW BS500B TO BS500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-764828<[01] REPLACED WEB - INTERCOSTAL LOC BTW BS500B TO BS500C AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 AND DWG 143A7505 SHEET 108 REV. -<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: INTERCOSTAL — ELONGATED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

ELONGATED HOLE WEB - INTERCOSTAL LOC BTW BS500C TO BS500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT 2024-764827<[01] REPLACED WEB - INTERCOSTAL LOC BTW BS500C TO BS500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 108 REV. - <BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED WEB - INTERCOSTAL LOC BTW BS500C TO BS500D AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 108 REV. -<BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

CRACK SUPPORT BRACKET BODY STATION 540 AND LBL 6 AT KEEL BEAM 2024-764808<[01] REPLACED SUPPORT BRACKET LOCATED ON BS 540 AND LBL6 AT KEEL BEAM. IAW B737-800 SRM 51-40-02.;[02] CERTIFIED WORK PERFORMED

Part: PLATE — CRACKED (ZONE 500) · airframe 40,440 hrs · 19,154 cycles

CRACK ON CORRUGATED PLATE LOCATED IRSS 215 AT TRAILING EDGE AT LT WING 2024-764797<[01] REPLACED CORRUGATED PLATE LOCATED IRSS 215 AT TRAILING EDGE AT LT WING IAW B737-800 SRM 51-10-02 ITEM 9 MEASURE OF CRACK IS 0.500 IN TOOL USED DIGITAL CALIPER: P/N: 500-197-30 S/N: A23304029 DUE DATE: 10-NOV-25;[02] CERTIFIED WORK PERFORMED.

Part: RIB — CRACKED (ZONE 500 TE) · airframe 40,440 hrs · 19,154 cycles

CRACK ON DEFLECTION CONTROL RIB TRAILING EDGE AT LT WING 2024-764746<[01] TOOL USED STEP 6 EDDY CURRENT EQUIPMENT PN: NORTEC 600D SN: 240497907 DUE DATE: 27-AUG-25;[02] PERFORMED REPAIR ON DEFLECTION CONTROL RIB TRAILING EDGE AT LT WING IAW B737-800 SRM 57-51-02-2R-3 REPAIR 1 SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 2 <BR>PERFORMED REPAIR ON DEFLECTION CONTROL RIB TRAILING EDGE AT LT WING IAW B737-800 SRM 57-51-02-2R-3 REPAIR 3 SEE INDIVIDUAL SIGN OFF BELOW;[04] CERTIFIED CORRECTIVE ACTION 3 AS RII <BR>PERFORMED REPAIR ON DEFLECTION CONTROL RIB TRAILING EDGE AT LT WING IAW B737-800 SRM 57-51-02-2R-3 REPAIR 3 SEE INDIVIDUAL SIGN OFF BELOW

Part: ANGLE — CRACKED (ZONE 500 TE) · airframe 40,440 hrs · 19,154 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS 317 AT LT WING 2024-764745<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 317 AT LT WING IAW B737-800 SRM 51-40-02 AND DWG 115A3712 SHEET 5 REV -;[02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 317 AT LT WING IAW B737-800 SRM 51-40-02 AND DWG 115A3712 SHEET 5 REV -

Part: NUT — DETERIORATED (ZONE 800) · airframe 40,440 hrs · 19,154 cycles

DETERIORATED NUT ON ASSIST HANDLE AT AFT SERVICE DOOR (2EA) 2024-764740<[01] REPLACED NUT ON ASSIST HANDLE AT AFT SERVICE DOOR (2EA) IAW SOPM 20-50-01 REV. 38 AND DWG 411A2204 REV A SHEET 65;[02] REPLACED NUT ON ASSIST HANDLE AT AFT SERVICE DOOR (2EA) IAW SOPM 20-50-01 REV. 38 AND DWG 411A2204 REV A SHEET 65

Part: NUT — DETERIORATED (ZONE 800) · airframe 40,440 hrs · 19,154 cycles

DETERIORATED NUT ON ASSIST HANDLE AT FWD SERVICE DOOR 2024-764739<[01] REPLACED NUT ON ASSIST HANDLE AT FWD SERVICE DOOR IAW B737-800 AMM 52-41-31-400-802 STEP 3.F ITEM (2);[02] JOB COMPLETED

Part: PLATE — BROKEN (ZONE 500) · airframe 40,440 hrs · 19,154 cycles

BROKEN CORRUGATED PLATE LOC ON IRSS 143 AT REAR SPAR LT WING 2024-764768<[01] REPLACED CORRUGATED PLATE LOC ON IRSS 143 LT WING IAW B737-800 SRM 51-40-02 AND DRAWING 115A2001 SHEET 49 REV:-.<BR>?SEE INDIVIDUAL SIGN OFF BELOW?.;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: RIB — CRACKED (ZONE 300) · airframe 40,440 hrs · 19,154 cycles

CRACK ON RIB ACCESS PANEL 331B LOCATED LE STA105.26 AT LT HORIZONTAL STABILIZER 2024-764729<[01] REPLACED RIB AND FASTENERS LOCATED ON L/E STA 105.26 AT LT HORIZONTAL STABILIZER. IAW B737-800 SRM 51-40-02 AND DWG# 186A1001 SHEET 19 AND REV -.;[02] REPLACED RIB AND FASTENERS LOCATED ON L/E STA 105.26 AT LT HORIZONTAL STABILIZER. IAW B737-800 SRM 51-40-02 AND DWG# 186A1001 SHEET 19 AND REV -.

Part: RIB — CRACKED (ZONE 300) · airframe 40,440 hrs · 19,154 cycles

CRACK ON RIB ACCESS PANEL 331B LOCATED LE STA114.55 AT LT HORIZONTAL STABILIZER 2024-764730<[01] REPLACED RIB & FASTENERS LOCATED ON L/E STA 114.55 AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02 AND DWG# 186A1001 SHEET 19 AND REV -.;[02] REPLACED RIB & FASTENERS LOCATED ON L/E STA 114.55 AT LT HORIZONTAL STABILIZER IAW B737-800 SRM 51-40-02 AND DWG# 186A1001 SHEET 19 AND REV -.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CRACK SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN 2024-764690<[01] TOOLS USED TEMPERATURE CONTROLLER P/N: 38615K71; S/N: AE-40585; DUE DATE: 26-JUL-25.;[02] TOOLS USED: POWER PACK: P/N: FMK0003223; S/N: PE0412/63335; DUE DATE: 17-JUN-25; THERMOMETER: P/N: FLUKE 566; S/N: 65900157WS; DUE DATE: 23-OCT-25; MULTIMETER: P/N: FLUKE 87; S/N: 58430097; DUE DATE: 17-JUN-25.;[03] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW B737-800 SEM 51-10-02 ITEM 9 AND DWG 146A7901 SHEET 99 REV. -<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[04] CERTIFIED CORRECTIVE ACTION 3; COMPLETED

Part: CHANNEL — CORRODED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

CORROSION CHANNEL SUPPORT ZEE LOCATED BTW BS 500H TO BS 500I AT LEVEL S 26L AND WL 154.5 AT FWD CARGO COMPARTMENT 2024-764658<[01] TOOL USED ON STEP 4 UT EQUIPMENT. P/N: 45MG; S/N: 232017609; CAL DUE DATE: 08-OCT-25;[02] THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EAM-22-153-01550 SEE TTG8Q00XQKL7;[03] THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EAM-22-153-01550 SEE TTG8Q00XQKL7<BR>CERTIFIED AS RII.

Part: SUPPORT CHANNEL — CORRODED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

CORROSION CHANNEL SUPPORT ZEE LOCATED BTW BS 500C TO BS 500G AT LEVEL S 26L AT WL 154.5 AT FWD CARGO COMPARTMENT 2024-764656<[01] THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EAM-22-153-01550;[02] THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EAM-22-153-01550 AS RII

Part: WEB — CORRODED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

CORROSION WEB - INTERCOSTAL LOCATED BTW BS747 TO BS767 RBL21 WL 156.5 AFT CARGO COMPARTMENT. REPLACED WEB LOCATED BTW BS 747 TO BS 767 RBL 21 WL 156 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02 DWG: 146A7500 SHEET: 236 REV: - AND DWG: 146A7502 SHEET: 50 REV: - .

Part: STRAP — CORRODED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

CORROSION STRAP LOCATED BS767 BTW LBL21 TO RBL21 WL 156.5 AT AFT CARGO COMPARTMENT 2024-764667<[01] REPLACED STRAP LOCATED BS767 BTW LBL21 TO RBL21 WL 156.5 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 AND DWG 146A7500 REV-;[02] CORRECTED STEP 1<BR>REPLACED STRAP LOCATED BS767 BTW LBL21 TO RBL21 WL 156.5 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 AND DWG 146A7500 REV- SHEET 233;[03] REPLACED STRAP LOCATED BS767 BTW LBL21 TO RBL21 WL 156.5 AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 AND DWG 146A7500 REV- SHEET 233.

Part: SHIELD — CORRODED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

CORROSION WEB (SHIELD) LOCATED BTW BS794 TO 767 RBL 21 WL 156.5 AT AFT CARGO COMPARTMENT 2024-764657<[01] REPLACED WEB(SHIELD)AND FASTENERS LOCATED BETWEEN BS767 TO BS 794 RBL21 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02 AND DRAWING 146A0081 SHEET 49 REV A. SEE INDIVIDUAL STEP SIGN OFF BELLOW.;[02] TASK COMPLETED; RII<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

CORROSION BILGE AREA SHEAR PLATE BTW BS 500 TO BS 500A AT LEVEL S 26R AND WL 154.5 AT FWD CARGO COMPARTMENT 2024-764668<[01] REPLACED SHIELD PLATE BTW BS 492.4 TO BS 500A AT LEVEL STR 26R AND WL 154.5 AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG: 143A0080 SHEET: 39 REV: -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED; RII<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

CRACK ANGLE - SUPPORT LOCATED BS867 AT LEVEL STR27L AT AFT CARGO COMPARTMENT 2024-764669<[01] REPLACED ANGLE - SUPPORT LOCATED FLOOR STRUCTURE STA 867 AT LEVEL STR 27L AT AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02-0G AND 51-40-02 AND DWG 149A8102 SHEET: 19 REV: A<BR><BR>MEASURE OF CRACK ON SUPPORT BRACKET: L:0.982?<BR>TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N: B23394214 AND DUE DATE IS: 06-FEB-25.;[02] TASK COMPLETED

Part: SUPPORT — CORRODED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS727D TO BS807 LBL21 WL156.5 AT AFT CARGO COMPARTMENT. ZEE CHANNEL SIDEPLATE ( SUPPORT ZEE) LOCATED BTW BS 727C+11 TO BS 787+ 11. SPLICE SIDEPLATE 4EA LOCATED BTW BS 727D TO BS 727E. BTW BS 727H TO BS 727I. BTW BS 727I TO BS 727J AND BTW 767 TO BS 787. AT LBL 21 WL156.5 AND FASTENERS AT AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-5 REPAIR 5, SRM 51-40-02 AND DWG 146A7500 SHEET 233 REV. -.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS727F TO BS767 RBL21 WL156.5 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE AND CLIP ZEE-SUPPORT(1E/A) BTW BS727F TO BS767 RBL21 WL156.5 AT AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-6 REPAIR 6; SRM 51-40-02 AND DWG 146A7500 SHEET 233 REV. - AND DWG 146A7502 SHEET 50 REV. -.

Part: BALANCE WEIGHT — OUT OF BALANCE (ZONE 300) · airframe 40,440 hrs · 19,154 cycles

DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR RT PN: 183A0103-26 SN: 006328 FOUND BALANCE WEIGHTS PN: 183A0210-15 (1 EA) ON BAY 4 PN: 183A0210-14 (1EA) ON BAY 3 PN: 183A0210-14 (1 EA) ON BAY 2 2024-764624<[01] ACCOMPLISHED ELEVATOR BALANCING IAW M-22-155-03767;[02] ACCOMPLISHED ELEVATOR BALANCING IAW M-22-155-03767<BR>RII

Part: WEB — CRACKED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CRACK FLOOR STRUCTURE WEB LOCATED BTW BS 380 TO BS 400 AT LBL 13 AT PASSENGER CABIN 2024-764625<[01] REPLACED FLOOR STRUCTURE WEB (UPPER CHORD ANGLE) LOCATED BTW BS 380 TO BS 400 AT LBL 13 AT PASSENGER CABIN IAW DRAWING 143A5400 REV-B AND B737-800 SRM 51-10-02- ITEM 9 SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED FLOOR STRUCTURE WEB (UPPER CHORD ANGLE) LOCATED BTW BS 380 TO BS 400 AT LBL 13 AT PASSENGER CABIN IAW DRAWING 143A5400 REV-B AND B737-800 SRM 51-10-02- ITEM 9 SEE INDIVIDUAL SIGN OFF BELOW

Part: BALANCE WEIGHT — OUT OF BALANCE (ZONE 300) · airframe 40,440 hrs · 19,154 cycles

DURING WEIGHT AND BALANCE PROCEDURE OF ELEVATOR LT PN: 183A0103-25 SN: 006113 FOUND BALANCE WEIGHTS PN: 183A0210-15 (1 EA) ON BAY 4 PN: 183A0210-14 (1EA) ON BAY 3 PN: 183A0210-14 (1 EA) ON BAY 2 2024-764623<[01] ACCOMPLISHED ELEVATOR BALANCING IAW EA M-22-155-03766;[02] JOB COMPLETED IAW EA M-22-155-03766 AND CERTIFIED RII

Part: FASTENER — DETERIORATED (ZONE 800) · airframe 40,440 hrs · 19,154 cycles

DETERIORATED HARDWARE GIRT BAR FITTING IN ENTRY AND SERVICE DOOR AT FWD GALLEY AREA 2024-764587<[01] REPLACED HARDWARE GIRT BAR FITTING IN ENTRY AND SERVICE DOOR AT FWD GALLEY AREA IAW B737-800 AMM 25-66-02-400-801;[02] REPLACED HARDWARE GIRT BAR FITTING IN ENTRY AND SERVICE DOOR AT FWD GALLEY AREA IAW B737-800 AMM 25-66-02-400-801

Part: FASTENER — DETERIORATED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

DETERIORATED GIRT BAR FITTING HARDWARE ON AFT ENTRY AND GALLEY AT AFT GALLEY AREA 2024-764576<[01] REPLACED GIRT BAR FITTING HARDWARE ON AFT ENTRY AND GALLEY AT AFT GALLEY AREA IAW B737-800- AMM 25-66-02-400-801;[02] CERTIFIED WORK PERFORMED.

Part: FRAME — CRACKED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CRACK FRAME ON BS 312 BETWEEN S-5L AND S-6L AT FWD GALLEY AREA 2024-764593<[01] REPAIRED FRAME ON BS 312 BETWEEN S-5L AND S-6L AT FWD GALLEY AREA IAW B737-800 EA EA-GENERAL M-22-153-01244<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] STEP 1 CORRECTED:<BR>REPAIRED FRAME ON BS 312 BETWEEN S-5L AND S-6L AT FWD GALLEY AREA IAW B737-800 EA NO: M-22-153-01244<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[03] REPAIRED FRAME ON BS 312 BETWEEN S-5L AND S-6L AT FWD GALLEY AREA IAW B737-800 EA NO: M-22-153-01244<BR>SEE INDIVIDUAL SIGN-OFF BELOW.

Part: GUSSET — CRACKED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

BROKEN ANGLE GUSSET LOCATED ON BS 500I AT STR 19R AT FWD CARGO COMPARTMENT 2024-764608<[01] REPLACED ANGLE GUSSET AND FASTENERS LOCATED ON BS 500I AT STRINGER 19R AT FWD CARGO COMPARTMENT IAW BOEING 737-800 SRM 51-40-02; BOEING 737-800 SRAND BOEING 737-800 DWG 143A7802 SHEET 257 REV B. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: WEB — CRACKED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CRACK WEB LOCATED BTW BS 340 TO BS 360 AT RBL 13 AT FWD GALLEY AREA 2024-764535 CRACK WEB LOCATED BTW BS 344 TO BS 360 AT RBL 13 AT FWD GALLEY AREA<[01] TOOL USED: ET EQUIPMENT; P N: NORTEC600D; SN: 60007161486; CAL DUE DATE: 06-SEP-25.;[02] PERFORMED PERMANENT REPAIR ON WEB LOCATED BTW BS 340 TO BS 360 AT RBL 13 AT FWD GALLEY AREA IAW B737-800 SRM 53-10-51-2R-20 REPAIR 20. SEE INDIVIDUAL SIGN OFFS BELOW;[03] CORRECTED ITEM 2 <BR>PERFORMED PERMANENT REPAIR ON WEB LOCATED BTW BS 344 TO BS 360 AT RBL 13 AT FWD GALLEY AREA IAW B737-800 SRM 53-10-51-2R-20 REPAIR 20. SEE INDIVIDUAL SIGN OFFS BELOW;[04] PERFORMED PERMANENT REPAIR ON WEB LOCATED BTW BS 344 TO BS 360 AT RBL 13 AT FWD GALLEY AREA IAW B737-800 SRM 53-10-51-2R-20 REPAIR 20.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.<BR>CERTIFIED AS RII.

Part: WEB — CRACKED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CRACK WEB LOCATED BTW BS 270 TO BS 294 AT LEVEL BL0 AT FWD GALLEY AREA 2024-764534<[01] REPLACED WEB AND FASTENERS LOC. BTW BS 270 TO BS 294 AT LEVEL BL0 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 141A5400; SHEET: 20; REV: ?. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: STIFFENER — CORRODED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CORROSION STIFFENER LOCATED BTW BS967 TO BS986.5 RBL 17 WL 208.1 AT AFT GALLEY AREA 2024-764557<[01] REPLACED STIFFENER AND FASTENER LOCATED BTW BS967 TO BS986.5 RBL 17 WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM-51-40-02; SRM-51-10-02 ITEM 9 AND DWG:140A9870 SHEET:23 REV:-. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED STIFFENER AND FASTENER LOCATED BTW BS967 TO BS986.5 RBL 17 WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM-51-40-02; SRM-51-10-02 ITEM 9 AND DWG:140A9870 SHEET:23 REV:-. SEE INDIVIDUAL SIGN-OFF BELOW

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CORROSION FLOOR BEAM LOCATED BS986.5 RBL43 WL 208.1 AT AFT GALLEY AREA 2024-764543<[01] EQUIPMENT P/N 45MG; S/N 130061901; DUE DATE 12-JUN-25 WAS USED ON STEP 6;[02] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 9;[03] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 12;[04] STEP 13 TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N: 240497907; DUE DATE: 27-AUG-25;[05] PERFORMED REPAIR FLOOR BEAM LOCATED BS 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.;[06] TASK COMPLETED <BR>CERTIFIED AS RII

Part: STIFFENER — CORRODED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CORROSION STIFFENER LOCATED BTW BS947.5 TO BS967 RBL 50 WL 208.1 AT AFT GALLEY AREA 2024-764549<[01] TOOL USED P/N: 45MG; S/N: 130066401; CAL DUE: 21-OCT-25.;[02] REPLACED STIFFENER AND FASTENERS LOCATED BTW BS947.5 TO BS967 RBL 50 WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM 51-40-02 AND DWG 147A5650 SHEET 71 REV: A.<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED STIFFENER AND FASTENERS LOCATED BTW BS947.5 TO BS967 RBL 50 WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM 51-40-02 AND DWG 147A5650 SHEET 71 REV: A.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.

Part: WEB — CRACKED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CRACK WEB LOCATED BTW BS 340 TO 360 AT LBL 12 AT FWD GALLEY AREA 2024-764536<[01] REPLACED WEB AND FASTENERS LOCATED BTW BS 340 TO 360 AT LBL 12 AT FWD GALLEY AREA IAW B737-800 SRM-51-40-02; SRM-51-10-02 ITEM 9 AND DWG:141A5400 SHEET:46 REV:A. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED WEB AND FASTENERS LOCATED BTW BS 340 TO 360 AT LBL 12 AT FWD GALLEY AREA IAW B737-800 SRM-51-40-02; SRM-51-10-02 ITEM 9 AND DWG:141A5400 SHEET:46 REV:A. SEE INDIVIDUAL SIGN-OFF BELOW

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CORROSION EXISTING REPAIR FLOOR BEAM LOCATED BS947.5 LBL 23 WL 208.1 AT AFT GALLEY AREA 2024-764548<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 05-AUG-25.;[02] REPAIRED EXISTING REPAIR FLOOR BEAM LOCATED BS947.5 LBL 23 WL 208.1 AT AFT GALLEY AREA IAW B 737-800 SRM 53-70-51-2R-5 AND E.A 25-153-00005 WIP1 AND E.A 25-153-00005 SUMMARY.SEE INDIVIDUAL STEP SING-OFF BELLOW;[03] REPAIRED EXISTING REPAIR FLOOR BEAM LOCATED BS947.5 LBL 23 WL 208.1 AT AFT GALLEY AREA IAW B 737-800 SRM 53-70-51-2R-5 AND E.A 25-153-00005 WIP1 AND E.A 25-153-00005 SUMMARY.SEE INDIVIDUAL STEP SING-OFF BELLOW<BR>RII

Part: ANGLE — CORRODED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CORROSION ANGLE LOCATED BTW BS927 TO BS947.5 LBL 23 WL 208.1 AT AFT GALLEY AREA 2024-764553<[01] REPLACED ANGLE LOCATED BTW BS927 TO BS947.5 LBL 23 WL 208.1 AT AFT GALLEY AREA I.A.W B373-800 SRM 51-40-02; SRM 51-10-02 ITEM 9. AND DWG 147A5400 SHEET: 21; REV: -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] JOB COMPLETED

Part: STIFFENER — CORRODED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CORROSION STIFFENER LOCATED BTW BS967 TO BS986.5 LBL 17 WL 208.1 AT AFT GALLEY AREA 2024-764554<[01] REPLACED STIFFENER AND FASTENERS LOCATED BTW BS967 TO BS986.5 LBL 17 WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM-51-40-02; SRM-51-10-02 ITEM 9 AND DWG:140A9870 SHEET:23 REV:-. SEE INDIVIDUAL SIGN-OFF BELOW;[02] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CORROSION FLOOR BEAM LOCATED BS 986.5 LBL43 WL 208.1 AT AFT GALLEY AREA 2024-764542<[01] EQUIPMENT P/N 45MG; S/N 130061901; DUE DATE 12-JUN-25 WAS USED ON STEP 6;[02] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 9;[03] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 12;[04] STEP 13 TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N: 240497907; DUE DATE: 27-AUG-25.;[05] PERFORMED REPAIR FLOOR BEAM LOCATED BS 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.;[06] TASK COMPLETED <BR>CERTIFIED AS RII

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2024-764498<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N:B23399190;DUE DATE: 04/MAR/25;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1859843 ; DUE DATE : 10/MAR/25;[03] REPAIRED THE AFT CORNER SCUFF PLATE OF FWD CARGO COMPARTMENT I.A.W. BOEING 737-800 SRM 53-30-15-2R-1 REPAIR 1; AND BAC 5975. SEE INDIVIDUAL SIGN OFF BELOW.;[04] JOB COMPLETED.

Part: CRADLE — BROKEN (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

BROKEN LAVATORY E BRACKET EMERGENCY FLASH LIGHT AT AFT GALLEY AREA (1 EA) 2024-764448<[01] REPLACED LAVATORY E BRACKET EMERGENCY FLASH LIGHT AT AFT GALLEY AREA (1 EA) IAW B737-800- AMM 25-64-00-200-802;[02] TASK COMPLETED

Part: HANDLE — BROKEN (ZONE 800) · airframe 40,440 hrs · 19,154 cycles

BROKEN HANDLE ASSY ON EMERGENCY EXIT 842 2024-764452<[01] REPLACED HANDLE ASSY ON EMERGENCY EXIT 842 I.A.W. B737-800 AMM 52-22-51-000-801 STEP 2. C. (1) (F) AND (G) AND AMM 52-22-51-400-801 STEP 3. D. (2) (E) AND (F);[02] 1. ESAU VELASCO (TECHNICIAN); 07-JAN-2025 19:47 UTC<BR>REPLACED HANDLE ASSY ON EMERGENCY EXIT 842 I.A.W. B737-800 AMM 52-22-51-000-801 STEP 2. C. (1) (F) AND (G) AND AMM 52-22-51-400-801 STEP 3. D. (2) (E) AND (F). VERIFIED

Part: STRAP — MISSING (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

MISSING LAVATORY E TAMPER EMERGENCY FLASHLIGHT AT AFT GALLEY AREA (2 EA) 2024-764450<[01] INSTALLED LAVATORY E TAMPER EMERGENCY FLASH LIGHT AT AFT GALLEY AREA (2 EA) IAW B737-800- AMM 25-64-00-200-802 STEP 10.C.(7);[02] INSTALLED LAVATORY E TAMPER EMERGENCY FLASH LIGHT AT AFT GALLEY AREA (2 EA) IAW B737-800- AMM 25-64-00-200-802 STEP 10.C.(7)

Part: BRACKET — CRACKED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

CRACK ON LOWER PAN ASSY AFT BRACKET AT AFT ENTRY DOOR 2024-764322<[01] REPLACED BRACKET AND FASTENERS LOCATED LOWER PAN ASSY AT AFT ENTRY DOOR IAW B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 411A2119 SHEET 72 REV ?;[02] TASK CARD COMPLETE.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

CRACK ON VAPOR BARRIER LOCATED BS 663 LBL 30 AT MAIN WHEEL WELL COMPARTMENT 2024-764338<[01] TOOL USED: CALIPER: P/N:500-196-30 S/N:A23325649 DUE DATE:31-DEC-24.;[02] TOOL USED SCALE P/N CR5200 S/N 8342514649 DUE DATE 27/FEB/25;[03] TOOL USED: HOTBONDER: P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 15-FEB-25;[04] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18175478 DUE DATE 25/JAN/25.;[05] TOOL USED P/N: EPOCH 650; S/N: 190984811; CAL DUE: 11-JAN-25.;[06] PERFORMED PERMANENT REPAIR ON VAPOR BARRIER LOCATED BS 663 LBL 30 AT MAIN WHEEL WELL COMPARTMENT IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW;[07] PERFORMED PERMANENT REPAIR ON VAPOR BARRIER LOCATED BS 663 LBL 30 AT MAIN WHEEL WELL COMPARTMENT IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW;[08] CORRECTED STEP 7. PERFORMED PERMANENT REPAIR ON VAPOR BARRIER LOCATED BS 663 LBL 30 AT MAIN WHEEL WELL COMPARTMENT IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW. RII ACCOMPLISHED

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 40,440 hrs · 19,154 cycles

CRACK ON VAPOR BARRIER LOCATED BS 663 RBL 31 AT MAIN WHEEL WELL COMPARTMENT 2024-764340<[01] TOOL USED: CALIPER PN:500-196-30 SN:A23400730 DUE DATE:11-SEP-25;[02] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 25/JAN/25.;[03] TOOL USED: ULTRASONIC FLAW DETECTOR; P/N: USM GO +; S/N: USMGO11040089; DUE DATE: 21-MAY-25.;[04] REPAIRED VAPOR BARRIER LOCATED BS 663 RBL 31 AT MAIN WHEEL WELL COMPARTMENT IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] REPAIRED VAPOR BARRIER LOCATED BS 663 RBL 31 AT MAIN WHEEL WELL COMPARTMENT IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW. RII COMPLETED;[06] REPAIRED VAPOR BARRIER LOCATED BS 663 RBL 31 AT MAIN WHEEL WELL COMPARTMENT IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW. RII COMPLETED

Part: SKIN — DEBONDED (ZONE 600 FLAP) · airframe 40,437 hrs · 19,153 cycles

CUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT RT WING 2024-764357<[01] TOOL USED CALIPER: PN: 500-196-30; SN: A23325649; DUE DATE: 31-DEC-24;[02] TOOL USED: BOND TESTING UNIT; P N: BONDMASTER 600M; S N: 230106912; CAL DUE DATE: 09-JAN-25;[03] TOOL USED; HOTBONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 25-JAN-25.;[04] TOOL USED ON STEP 15 ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190984811; CAL DUE DATE: 11-JAN-25;[05] REPAIRED OB AFT FLAP ON IB SIDE AT RT WING IAW B737-800 SRM 57-53-01-2R-16 REPAIR 16. REFER TO INDIVIDUALS SIGNOFFS BELOW.;[06] TASK COMPLETED. RII COMPLETED.

Part: SKIN — DEBONDED (ZONE 500 FLAP) · airframe 40,437 hrs · 19,153 cycles

CUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT LT WING 2024-764363<[01] TOOL USED CALIPER PN: 500-196-30; SN: A23325649; DUE DATE: 31-DEC-24;[02] TOOL USED: BOND TESTING UNIT; P N: BONDMASTER 600M; S N: 230106912; CAL DUE DATE: 09-JAN-25;[03] TOOL USED: HOT BONDER PN: HCS9200B-AV; SN: 18185733; DUE DATE: 25/JAN/25<BR>TOOL USED: CALIPER PN: 500-197-30; SN: A18229508; DUE DATE: 14/JAN/25;[04] TOOL USED: BOND TESTER; P/N: S-3; S/N: 064; DUE DATE: 27-AUG-25.;[05] TOOL USED SCALE PN: CR5200; SN: 8342514511; DUE DATE: 27/FEB/25.;[06] PERFORMED INTERIM REPAIR ON OB AFT FLAP ON IB SIDE AT LT WING IAW B737-800 SRM 57-53-01-2R-16 REPAIR 16. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] PERFORMED INTERIM REPAIR ON OB AFT FLAP ON IB SIDE AT LT WING IAW B737-800 SRM 57-53-01-2R-16 REPAIR 16. SEE INDIVIDUAL SIGNOFFS BELOW. RII COMPLETED

Part: SUPPORT ANGLE — CRACKED (ZONE 500) · airframe 40,440 hrs · 19,154 cycles

CRACK SLAT ACTUATOR 4 SUPPORT ANGLE AT LT WING 2024-764316<[01] REPLACED SLAT ACTUATOR 4 SUPPORT ANGLE AT LT WING IAW B737-800 SRM 51-10-02. CRACK L: 0.500 INCH TOOL USED DIGITAL CALIPER PN: 500-197-30 SN: B20189527 DUE DATE: 28-JAN-25;[02] REPLACED SLAT ACTUATOR 4 SUPPORT ANGLE AT LT WING IAW B737-800 SRM 51-10-02. CRACK L: 0.500 INCH TOOL USED DIGITAL CALIPER PN: 500-197-30 SN: B20189527 DUE DATE: 28-JAN-25

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 40,440 hrs · 19,154 cycles

DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT AND LT SIDE AT PASSENGER CABIN (10 EA) 2024-764226<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT AND LT SIDE AT PASSENGER CABIN (10 EA) IAW B737-800 AMM 33-51-15-400-802;[02] JOB COMPLETED

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 40,331 hrs · 19,098 cycles

EMERGENCY LIGHT INOP OUTSIDE OF AFT LEFT SERVICE DOOR<[01] RELAMPED AFT LEFT SERVICE DOOR EXT EMER LITE PER AMM 33-51-04.

Part: COVER — DETACHED (ZONE 200) · airframe 39,902 hrs · 18,868 cycles

AFT OVERHEAD EMERGENCY EXIT LIGHT COVER FELL OFF<[01] OK TO CONTINUE PER MEL 33-15-02 SP1 AUTH #217972;[02] INSTALLED EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-03 OPS CK GOOD

Part: SENSOR — FALSE INDICATION (TE FLAPS) · airframe 39,773 hrs · 18,797 cycles

ON APP SELECTING FLAPS 5 SAW INDICATOR BETWEEN 0 AND 1 W/ FLAP ASYMMETRY. FOLLOWED QRH PROCEDURES USING ALT FLAPS. 0 FLAP LANDING W/ ASSOCIATED BRAKE COOLING BRAKE ENERGY 34.2M - HIGH ENERGY STOP<[01] REF. TTG8Q00W0NV2 / LP: 2724161 FOR THE HIGH ENERGY STOP CONDITIONAL INSPECTION.;[02] T/S THE TE FLAP SKEW SYSTEM IAW FIM 27-59 809/807. FOUND FC: 27-53256 ?FLAP 7 SKEW?. NOTED #2 TO #7 SPLIT OF 44.5. REMOVED AND REPLACED THE #7 FLAP SKEW SENSOR IAW AMM 27-59-01. ADJUSTMENT CHECK GOOD. #2 (288.5) TO #7 (288.4) SPLIT OF 0.1 AT POS 40. OPS CHECK GOOD.

Part: SLIDE — LOOSE (ZN 800 DOOR) · airframe 39,060 hrs · 18,395 cycles

FWD ENTRY L1 SLIDE NOT SECURE.<[01] RESECURED SLIDE PER MT 725-61-06

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 38,367 hrs · 18,021 cycles

RIGHT AFT EMERGECY EXIT SIDEWALL LIGHT INOP.<[01] OK TO CONT. PER MEL#33-2-04; SP1B.;[02] PERFORMED OPERATIONAL CHECK OF EMERGENCY EXIT ROW LIGHTS IAW AMM 33-51-00; NO DEFECTS NOTED.

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 37,904 hrs · 17,791 cycles

LEFT MAIN WHEEL WELL WING CENTER SECTION REAR SPAR LOWER LEFT WEB GFRP VAPOR BARRIER HAS A 4 INCH CRACK LOCATED BETWEEN LBL 40.0 AND LBL 31.83<[01] 04 - REPAIRED PER [SRM 57-10-10-1A-2-B00453 (CRACK - STOP DRILL AND SEAL - DVI EVERY 1200 CYC - INTERIM REPAIR)] AND AVIATION PARTNERS BOEING 737-800 SRM SUPPLEMENT AP 37.7-0615.;[02] ADDED MEASUREMENTS

Part: SLIDE — OUT OF POSITION (ZN 800 DOOR) · airframe 37,490 hrs · 17,563 cycles

FWD ENTRY SLIDE PACK DOESNT LOOK IN PROPER POSITION<[01] INSPECTED L1 SIDE. VELCRO WAS ATTACHED ON FOLD.TUCKED EXTRA FLAP AS REQUIRED. REF MM25-66-01

Part: SLIDE — OUT OF POSITION (ZN 800 DOOR) · airframe 37,477 hrs · 17,557 cycles

FLIGHT ATTENDANT REPORTS FORWARD ENTRY DOOR SLIDE PACK NOT IN PROPER POSITION<[01] RE ATTACHED Z FOLD FLAP TO THE VELCRO ON THE BACKING PAN. RE TUCKED ANY EXCESS GIRT MATERIAL UP IN THE SLIDE COMPARTMENT PER AMM 25-66-01. MT 725-61-06 STEP I

Part: SLIDE — OUT OF ADJUST (ZN 800 DOOR) · airframe 37,198 hrs · 17,400 cycles

FWD ENTRY DOOR SLIDE NEEDS TO BE RESTOWED.<[01] FWD ENTRY DOOR SLIDE SECURED PER MT 725-61-06; ACFT OK FOR SERVICE.

Part: WINGLET — CRACKED (ZN 500 LEFT WING) · airframe 36,741 hrs · 17,137 cycles

UPON REMOVAL OF LH WING VENTRAL STRAKE FOUND WINGLET CRACKED IN 2 PLACES UNDER STRAKE MOUNTING POINT APPROX 10 FROM AFT EDGE<[01] REMOVED LH WINGLET IAW AMM 57-21-21;[02] INSTALLED LH WINGLET IAW AMM 57-21-21;[03] C/W EA 23-157-03232

Part: LIGHT — FAULTY (ZN 200 FUS TOP) · airframe 35,396 hrs · 16,343 cycles

*INFO ONLY* LOST POWER AT GATE EMERGENCY EXIT LIGHTS ILLUMINATED BRIEFLY. AND READING LIGHTS ON FO SIDE ILLUMINATED. RESTORED PO EVERYTHING OPS CHECKS NORMAL. NOTIFIED BRIAN MOC.<[01] NOTED BY MX

Part: LIGHT — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 34,833 hrs · 16,041 cycles

EMERGENCY EXIT COVER FELL OFF<[01] REPLACED COVER ON EMERGENCY LIGHT ASSY IN L/H EXIT ROW USING S.I.P.

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 34,269 hrs · 15,729 cycles

RT. HORIZONTAL FWD UPPER METAL SLIDING SEAL CRACKED.<[01] LOCATED AND DRILL REPLACEMENT SEAL PER SRM 51-40-05.;[02] INSPECTED WORK IN C/A #1;[03] REMOVED AND REPLACED R/H HORIZONTAL FWD UPPER SLIDING SEAL PER AMM 53-31-31.;[04] REMOVED AND REPLACED R/H HORIZONTAL FWD UPPER SLIDING SEAL PER AMM 53-31-31. INSPECTION C/W.

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 34,269 hrs · 15,729 cycles

LT. HORIZ. STAB FWD UPPER METAL SLIDING SEAL CRACKED.<[01] DRILLED AND INSTALLED ATTACH BRACKET TO SLIDING SEAL AS REQUIRED I.A.W. SRM 51-40-02.;[02] 1. DANIEL BUCKMAN (TECHNICIAN); 31-JAN-2023 16:51 UTC<BR>DRILLED AND INSTALLED ATTACH BRACKET TO SLIDING SEAL AS REQUIRED I.A.W. SRM 51-40-02. INSPECTED.;[03] REMOVED AND REPLACED SLIDING SEAL AS REQUIRED I.A.W. M/M 53-31-31. SEE ATTACHED SIGN OFFS FOR ALL WORK PERFORMED.;[04] VERIFIED WORK IN C/A #3

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 34,269 hrs · 15,729 cycles

IN THE MAIN CABIN FLOOR AREA AT STATION 540; THE FLEXIBLE INTERCOSTAL HAS A CRACK AT BL 0.<[01] REMOVED AND REPLACED INTERCOSTAL WITH FASTENERS PER SRM 51-40-02.;[02] REMOVED AND REPLACED INTERCOSTAL WITH FASTENERS PER SRM 51-40-02.<BR>INSPECTION C/W.

Part: FAIRING — PULLED (ZN 500 LEFT WING) · airframe 34,269 hrs · 15,729 cycles

#3 FLAP TRACK FAIRING PANEL 542BB O/B SEAL RETAINER RIVETS PULLED THROUGH SIN. MRKD<[01] ACCOMPLISHED REPAIR TO AREA PER SRM 57-53-70-2R-2. SEE STEPS FOR INDIVIDUAL SIGNOFFS.;[02] SIGNED FOR PARTS.;[03] C/W

Part: SLIDE — DISLODGED (AFT DOOR) · airframe 34,093 hrs · 15,626 cycles

AFT DOOR FO SIDE HAS A SLIDE THAT IS FALLING OUT. REPOSITIONED AFT SERVICE DOOR SLIDE IN THE COMPARTMENT IAW MT 725-61-06.

Part: PANEL — CRACKED (A/C BAY) · airframe 33,781 hrs · 15,464 cycles

AIR CONDITIONING DISTRIBUTION BAY IN FORWARD CARGO COMPARTMENT CABIN FLOOR BOARD RIGHT BREAK PNL CRACKED. / [01] REMOVED AND REPLACED BREAK PANEL ON R/H SIDE OF AIR CONDITIONING DISTRIBUTION BAY FOR CABIN FLOOR AT STA. 540 PER SRM 51-40-02.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 33,781 hrs · 15,464 cycles

LT WING O/B AFT FLAP; INBOARD LOWER SURFACE IS DELAMINATED LT WING O/B AFT FLAP INBOARD LOWER SURFACE IS DELAMINATED AT OTEF STA 63 / [01] PERFORMED REPAIR IAW SRM 57-53-01-1A-5 STEP 9 ZONE 5.;[02] REVIEWED THE FAULT FOR CORRECT REPAIR REFERENCE SELECTION AND OTHER APPLICABLE REQUIREMENTS. REF MPM 52.02.06.01

Part: SLIDE — LOOSE (R2 DOOR) · airframe 33,240 hrs · 15,162 cycles

AFT SERVICE DOOR SLIDE CONNECTION LOOSE / [01] SECURED AFT SERVICE DOOR SLIDE AS REQUIRED REF MM 25-66-00.

Part: LIGHT — INOPERATIVE (L/H OVERWING) · airframe 31,507 hrs · 14,160 cycles

LEFT WING GROUND ILLUMINATION EMERGENCY LIGHT INOP / [01] RELAMPED PER AMM 33-51-04

Part: LIGHT — INOPERATIVE (AFT ENTRY) · airframe 31,507 hrs · 14,160 cycles

AFT ENTRY EXTERIOR EMERGENCY LIGHT INOP / [01] RELAMPED PER AMM 33-51-04

Part: LIGHT — FAILED (CABIN FLOOR) · airframe 31,437 hrs · 14,123 cycles

PHOTO ILLUMINESCENT STRIPS NEAR ROW 12 BOTH SIDES OF ISLE DETACHED / [01] RESECURED STRIPS NEAR ROW 12 PER SIP

Part: BATTERY PACK — INOPERATIVE (CABIN)

EMERGENCY LIGHTS FAILED OPERATIONAL TEST. / REMOVED AND REPLACED NBATTERIEWS PACKS AT POSITIONS (M1670; M1671; M1672; M1676; M1694; AND M2335. AS PER REFERENCE B737 AMM 33-51-06-960-805. PERFORMED OPERATIONAL TEST. TEST NORMAL.

Part: LANYARD — MISSING (FWD CARGO DOOR)

FWD CARGO DOOR RELEASE LANDYARD IS APPART AND MISSING SEVERAL PIECES / REMOVED AND REPLACED FWD CARGO DOOR ASSIST LANYARD REF B737 AMM 52-31-00-400-801.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

FLOOR PANEL 241D DELAMINATED / PREPARED DAMAGED AREA FOR REPAIR AND REPAIRED AT FLOOR PANEL 241D AS PER B737-800 SRM 53-00-50-2R-7 MATERIAL USED PO 1694548 AND PO 1714421

Part: FLOOR PANEL — DELAMINATED (FUSELAGE)

FLOOR PANEL 241D DELAMINATED / PREPARED DAMAGED AREA FOR REPAIR AND REPAIRED AT FLOOR PANEL 241D AS PER B737-800 SRM 53-00-50-2R-7 MATERIAL USED PO 1694548 AND PO 1714421

Part: LANYARD — MISSING (FWD CARGO DOOR)

FWD CARGO DOOR RELEASE LANDYARD IS APPART AND MISSING SEVERAL PIECES / REMOVED AND REPLACED FWD CARGO DOOR ASSIST LANYARD REF B737 AMM 52-31-00-400-801.

Part: SKIN — DENTED (ZONE 200) · airframe 27,927 hrs · 12,263 cycles

REFERENCE DEFECT NR 9282 SEC 43 FUSELAGE SKIN DENT LOCATED AT STA 360+5.5' BETWEEN STR 14R AND 15R. EVALUATED DENT ON FUSELAGE SKIN AT STA 360+5.5' BETWEEN STR 14R AND 15R. FOUND OUT OF LIMITS DUE TO PROXIMITY TO STA 360 BUTT SPLICE & STR 14R LAP SPLICE, IAW B737 SRM 53-00-01-1A-1. REPAIRED DENT, IAW EA 210003 REV P1; P2; P3; IR SWA W/I 21-153-00131 REV IR REPAIR FOLLOW-ON ACTIONS BEING TRACKED ON SWA EC: 21-153-00131-DTI.

Part: BATTERY PACK — INOPERATIVE (CABIN L2 DOOR) · airframe 27,927 hrs · 12,263 cycles

EMERGENCY EXIT LIGHT ABOVE L2 DOOR IS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1673; OPS CHECK GOOD IAW AMM 33-51-06-960-805. WW095

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 27,927 hrs · 12,263 cycles

FORWARD ENTRY HEADER PANEL EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK M1675. OPS CHECK GOOD IAW AMM 33-51-06-960-805. WW094

Part: FLOOR PANEL — PULLED (CABIN) · airframe 27,927 hrs · 12,263 cycles

FOUND DURING OK TO INSTALL; CABIN FLOORBOARD PANEL 222BF HAS PULLED FIBERS ON UPPER SURFACE. / REMOVED AND REPLACED APU AIR INLET SEAL I-A-W AMM 49-15-11-000-801 AND AMM 49-15-11-400-801 WW0942

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,927 hrs · 12,263 cycles

DURING FWD WET AREA RESTORATION DVI FWD WET AREA INTERCOSTAL CRACKED AT FASTENER HOLE BETWEEN STA 312 TO 328 LBL45. REMOVED AND REPLACED INTERCOSTAL PN 141A5410-140 TAG WN0990 AT WET AREA STA 312 TO 328 LBL 45 IAW B737 SRM 51-10-02-0G-0 AND DWG 141A5400 REV.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 27,927 hrs · 12,263 cycles

CABIN FLOORBOARD PANEL 221BF HAS DAMAGED FIBERS ON UPPER SURFACE / REPAIRED CABIN FLOORBOARD PANEL 221BF WITH DAMAGED FIBERS ON UPPER SURFACE AND BROKEN TAB ON AFT O/B CORNER IAW B737 SRM 53-00-50-2R-1 AND B737 SRM 53-00-50-2R-0

Part: INTERCOSTAL — CORRODED (FWD CABIN FLOOR) · airframe 27,927 hrs · 12,263 cycles

FORWARD CABIN FLOOR STRUCTURE; STA 305; LBL11; WL208; INTERCOSTAL FLOOR SUPPORT UPPER SURFACE; 2 EA SPOTS OF CORROSION; MRK'D IN RED. REMOVED CORROSION AT FWD CABIN FLOOR STRUCTURE STA 305 LBL11 INTERCOSTAL FLOOR SUPPORT IAW B737 SRM 51-10-02-0G-0 AND 53-10-51-1A-1. EVALUATED DAMAGE AS 100% MATERIAL LOSS DUE TO CORROSION INTERCOSTAL FLOOR SUPPORT IS OUT OF LIMITS IAW B737 SRM 53-10-15-1A-1. REMOVED AND REPLACED INTERCOSTAL IAW B737 SRM 51-40-02-0G-0 AND DWG 141A5600 REV PN 141A5690-1.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,927 hrs · 12,263 cycles

AFT PASSENGER CABIN FLOOR BOARD 241XF HAS 40% OF TOP SURFACE WITH COMPOSITE FIBER STRANDS PULLED. REPAIRED DAMAGE TO UPPER SURFACE OF FLOORBOARD 241XE IAW 737-800 SRM 53-*00-50-2R-1 REV. 71 REPAIR 1; SRM 53-00-50-2R-0 REV. 71 REPAIR GENERAL. TAP TEST GOOD.

Part: FLOOR PANEL — DAMAGED (PASS CABIN) · airframe 27,927 hrs · 12,263 cycles

AFT PASSENGER CABIN FLOOR BOARD 242UF HAS TOP SURFACE WITH COMPOSITE FIBER STRANDS PULLED. REPAIRED FLOOR PANEL 242UF IAW B737-800 SRM 53-00-50-2R-0 REPAIR 1 A13436; A33702; A95094; A89382; A94665

Part: FLOORBOARD — PULLED (PASS CABIN) · airframe 27,927 hrs · 12,263 cycles

AFT PASSENGER CABIN FLOOR BOARD 242E HAS TOP SURFACE WITH COMPOSITE FIBER STRANDS PULLED. REPAIRED DAMAGE TO UPPER SURFACE OF FLOORBOARD 242E IAW 737-800 SRM 53-00-50-2R-1 REV. 71; SRM 53-00-50-2R-0 REV. 71 REPAIR GENERAL. TAP TEST GOOD A72547 A85487.

Part: FLOOR PANEL — DAMAGED (PASS CABIN) · airframe 27,927 hrs · 12,263 cycles

AFT PASSENGER CABIN FLOOR BOARD 241AAF HAS TOP SURFACE WITH COMPOSITE FIBER STRANDS PULLED. REPAIRED DAMAGE TO UPPER SURFACE OF FLOORBOARD 241AAF IAW 737-800 53-00-50-2R-1 REV. 71; SRM 53-00-50-2R-0 REV. 71 REPAIR GENERAL. TAP TEST GOOD A72547 A85487.

Part: FLOORBOARD — DAMAGED (PASS CABIN) · airframe 27,927 hrs · 12,263 cycles

AFT PASSENGER CABIN FLOOR BOARD 241ABF HAS TOP SURFACE WITH COMPOSITE FIBER STRANDS PULLED. REPAIRED FLOOR PANEL 241ABF IAW B737-800 SRM 53-00-50-2R-0 REPAIR 1 A13436; A33702; A95094; A89382; A94665.

Part: FLOORBOARD — DAMAGED (PASS CABIN) · airframe 27,927 hrs · 12,263 cycles

AFT PASSENGER CABIN FLOOR BOARD 241E HAS TOP SURFACE WITH COMPOSITE FIBER STRANDS PULLED. REPAIRED DAMAGE TO UPPER SURFACE OF FLOORBOARD 241E IAW 737-800 SRM 53-00-50-2R-1 RREV 71; SRM 53-00-50-2R-0 REV 71 REPAIR GENERAL TAP TEST GOOD. A72547 A85487

Part: FITTING — CORRODED (LAV FLOOR STRUC) · airframe 27,927 hrs · 12,263 cycles

PASSENGER CABIN FLOOR STRUCTURE LAV FITTING AREA CORRODED INBD SIDE STA.947 LBL 31 WL 208. REMOVED CORROSION AND VERIFIED LIMITS ON FLOOR STRUCTURE STA 947 LBL 31 WL 208. ORIGINAL T=.180 MATERIAL LOSS = .065 REMAINING .115 OUT OF LIMITS IAW SRM 53-70-51-1A-1. ACCOMPLISH A T-CAP REPAIR AT STA 947 FROM LBL 7 TO LBL 45 IAW SRM 53-70-51-2R-5 P/N 147A5504-29.

Part: FITTING — CORRODED (LAVATORY) · airframe 27,927 hrs · 12,263 cycles

PASSENGER CABIN FLOOR STRUCTURE;LAV FITTING AREA CORRODED INBD SIDE STA.947 LBL 50 WL 208 / REMOVED CORROSION AND VERIFIED LIMITS ON FLOOR STRUCTURE STA. 947 LBL 50 WL 208. ORIGINAL T= .180 MATERIAL LOSS = .050 REMAINING .0130 OUT OF LIMITS IAW SRM 53-70-51-1A-1 T-CAP REPAIR WAS ACCOMPLISHED ON NRC Y247552 P/N 147A5504-29

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 27,927 hrs · 12,263 cycles

RIGHT SIDE; VERTICAL FIN SKATE ANGEL; WORN/CHAFFING; STA. 1119-1127. / REMOVED DAMAGE FROM RT VERTICAL FIN SKATE ANGLE IAW SRM 51-10-02-0G-0 ORIG THICKNESS .063' LOSS OF .001' REMAINING .062' FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED SRM ALLOWABLES FOR THE CLOSURE ANGLE REPAIRED SKATE ANGLE AT STA 1119-1127 IAW EA 210016 IR AND SWA EA 21-153-00125 REV IR

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 27,927 hrs · 12,263 cycles

AFT PIT FLOOR PANEL 140EF HAS AREAS OF CORROSION AROUND UPPER OUTER EDGES. / EVALUATED CORROSION AT AFT CARGO PNL 140EF FOUND CORROSION THAN 20' FOUND OUT OF LIMITS IA-W SRM 53-00-53-1A-1 FABRICATED NEW FLOOR PNL IAW MM 25-52-01-201-801 AND BOEING DWG 453A2610-58 REV: D

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,927 hrs · 12,263 cycles

AFT PIT STA 727C+10 TO 767 ;RBL21; Z-ANGLE HAS 18 SPOTS OF CORROSION ADJACENT TO FASTENER HOLES; MRK'D IN RED. WL 158. REMOVED CORROSION AT AFT PIT STA 727C+10 TO 767 RBL 21 Z ANGLE IAW B 737 SRM 51-10-02-0G-0 ITEM 15 ORIGINAL 'T' .040 REMAINING .029 LOSS .011 FOUND TO BE OUT OF LIMITS IAW B 737 SRM 53-00-53+-1A-2 FIG 103. FABRICATED REPAIR Z ANGLE AND SPLICE FROM BETWEEN STA 727F TO 727G TO 767 AND INSTALLED IAW B 737 SRM 53-00-53-1A-1 REPAIR 5 ITEM 4 A-N P/N 146A7502-52.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,927 hrs · 12,263 cycles

AFT PIT STA 727C TO 727J+6; LBL21; Z-ANGLE HAS 21 SPOTS OF CORROSION MOSTLY ADJACENT TO FASTENER HOLES; MRK'D IN RED. WL 158. REMOVED CORROSION AT AFT PIT STA 727C TO 727J+6' Z ANGLE IAW B 737 SRM 51-10-02-0G-0 ITEM 15 ORIGINAL 'T' .040 REMAINING .029 LOSS .011 FOUND TO BE OUT OF LIMITS IAW B 737 SRM 53-00-53-1A-2 FIG 103. FABRICATED REPAIR SECTION AND SPLICE FROM BETWEEN STA 787-807 TO 727C - 727D LBL 21 AND INSTALLED IAW B 737 SRM 53-00-53-2R-5 REPAIR 5 ITEM 4 A-N PN 146A7502-31.

Part: BAFFLE — CRACKED (BS 500E-500F) · airframe 27,927 hrs · 12,263 cycles

FWD PIT LH BAFFLE AT BS 500E TO 500F WL 158 IS CRACKED ON THE FWD UPPER FLANGE / REMOVED AND REPLACED FWD PIT L/H BAFFLE STA 500E TO 500F WL 158 IAW SRM 51-40-02-0G-0 AND DWG: 143A7505 REV: -

Part: SHIELD — CORRODED (BS 768-787) · airframe 27,927 hrs · 12,263 cycles

AFT CARGO COMPT. STA 768 - 787; RBL22; WL156 SHIELD HAS CORROSION UPPER SURFACE / REMOVED CORROSION AT AFT CARGO COMPARTMENT STA 767-787 RBL 22 SHIELD AND VERIFIED LIMIT FOUND TO BE 100% MATERIAL LOSS IAW B737 SRM 53-60-15-1A-1 REOVED AND REPLACED SHIELD IAW B737 SRM 51-40-02-0G-0 AND DWG 146A0081 REV A. P/N 146A8127-12

Part: ANGLE — CORRODED (FWD CARGO COMPT) · airframe 27,927 hrs · 12,263 cycles

FORWARD CARGO COMPARTMENT RT Z-ANGLE; CORROSION AROUND FASTENER HOLES STA.500A-500E RBL 24' WL 158. REMOVED CORROSION ON RT Z-ANGLE; STA 500A - 500E; IAW SRM 51-10-02-0G-0. VERIFIED LIMITS; ORIGINAL .040'; LOSS .007'; REMAINING .033' OUT OF LIMITS IAW SRM 53-00-53-1A-2. ACCOMPLISHED Z-ANGLE REPAIR FROM STA 500A - 500I IAW SRM 53-00-53-2R-5 APPLIED CIC IAW AMM 51-21-91-620-802 PN 143A7501-188.

Part: ANGLE — CORRODED (FWD CARGO COMPT) · airframe 27,927 hrs · 12,263 cycles

FORWARD CARGO COMPARTMENT RT Z-ANGLE; CORROSION AROUND FASTENER HOLES STA 500E-500I RBL 24' WL 158. REMOVED CORROSION ON RT Z-ANGLE; STA 500E - 500I IAW SRM 51-10-02-0G-0 VERIFIED LIMITS; ORIGINAL .040'; LOSS .010'; REMAINING .030' OUT OF LIMITS IAW SRM 53-00-53-1A-2. Z-ANGLE REPAIR ACCOMPLISHED ON WO 41754-1400-0008 DEFECT Y247456 PN 143A7501-188.

Part: ANGLE — CORRODED (FWD CARGO COMPT) · airframe 27,927 hrs · 12,263 cycles

FORWARD CARGO COMPARTMENT LT Z-ANGLE; CORROSION AROUND FASTENER HOLES STA.500E-500H LBL 24' WL 158. REMOVED CORROSION FROM FWD CARGO BAY LT ZEE ANGLE STA 500E - 500H LBL 24 WL 158 IAW SRM 51-10-02-0G-0 PAR 15 AND INSPECTED W/ 10X MAG GLASS. NO DEFECTS NOTED. VERIFIED MATERIAL LOSS: ORIGINAL T = .040' REMAINING T = .031' LOSS = .009' LIMIT = .004'. ZEE ANGLE IS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DETAIL D. FWD CARGO BAY LT ZEE ANGLE WAS REMOVED AND REPLACED ON WORK CARD 41754/1400/0006 DEFECT Y247454 PN 143A7501-187.

Part: ANGLE — CORRODED (CARGO COMPT) · airframe 27,927 hrs · 12,263 cycles

FORWARD CARGO COMPARTMENT LT Z-ANGLE; CORROSION AROUND FASTENER HOLES STA.500C-500E LBL 24' WL 158. REMOVED CORROSION FROM FWD CARGO BAY LT ZEE ANGLE STA 500C - 500E LBL 24 WL 158 IAW SRM 51-10-02-0G-0 PAR. 15 AND INSPECTED W/ 10X MAG GLASS. NO DEFECTS NOTED. VERIFIED MATERIAL LOSS: ORIGINAL T = .040' REMAINING T = .032' LOSS = .008' LIMIT = .004'. ZEE ANGLE IS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DETAIL D. REMOVED AND REPLACED FWD CARGO BAY LT ZEE ANGLE STA 500C TO 500H IAW 53-00-53-2R-5; DWG: 143A7500 REV: - AND SRM 51-40-02-0G-0. APPLIED CIC TO NEW ZEE ANGLE IAW AMM 51-21-91-620-802 P/N 143A7501-187.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 27,927 hrs · 12,263 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140CF HAS CORROSION AROUND EDGES / EVALUATED CORROSION ON FLOOR PANEL 140CF FROM AFT CARGO COMPARTMENT CORROSION WAS FOUND TO BE OUT OF LIMITS EXCEEDS 20' IAW B737 SRM 53-00-53-1A-1. FABRICATED FLOOR PANEL IAW B737 AMM 25-52-01-201-801 AND DWG 453A2610 REV. C.

Part: GIRT BAR — STUCK (R1 DOOR) · airframe 27,607 hrs · 12,108 cycles

FWD SERVICE DOOR GIRT BAR STUCK. REPOSITIONED FWD SERVICE GIRT BAR, PER AMM 25-66-01.

Part: BRACKET — LOOSE (R1 DOOR GIRT BAR) · airframe 27,207 hrs · 11,896 cycles

GIRT BAR BRACKET ON FWD SERVICE DOOR APPEARS LOOSE. SECURED BRACKET WITH HARDWARE, PER SRM 51-40-02 AND COMPLIED WITH MT 725-61-06.

Part: SMOKE DETECTOR — INTERMITTENT (LAVATORY) · airframe 26,227 hrs · 11,386 cycles

SMOKE ALARM IN AFT LAV, FO SIDE WAS INTERMITTENT. NO SMOKE IN LAV, REPLACED SMOKE DETECTOR PER AMM 26-14-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,545 hrs · 11,063 cycles

FORWARD R/H EXTERIOR EMERGENCY LIGHT INOPERATIVE. / R&R BATTERY PACK PER AMM.

Part: SIGN — BROKEN (CABIN) · airframe 25,305 hrs · 10,942 cycles

SECOND WINDOW OF EMERGENCY EXIT ON FIRST OFFICER SIDE HAD A BROKEN EXIT SIGN BRACKET ON FLOOR LEVEL EMERGENCY EXIT SIGN. R&R SIGN ASSEMBLY IAW MM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 22,638 hrs · 9,731 cycles

L1 DOOR SLIDE FELL OUT OF COMPARTMENT. REINSTALLED SLIDE IAW MT.

Part: SIGN — MISSING (CABIN) · airframe 22,115 hrs · 9,504 cycles

RT EMERGENCY EXIT "EXIT/SALIDA" ILLUMINATING PLACARD MISSING AT ROW 14. R&R EMERGENCY EXIT HOUSING AND LENS PER AMM.

Part: SIGN — MISSING (CABIN) · airframe 22,163 hrs · 9,521 cycles

RT EMERGENCY EXIT "EXIT/SALIDA" ILLUMINATING PLACARD MISSING AT ROW 14. REATTACHED SIGN IAW EA.

Part: CHANNEL — CRACKED (RIGHT WING) · airframe 21,922 hrs · 9,427 cycles

AIRCRAFT DAMAGE RIGHT WING #5 FLAP TRACK UPPER U CHANNEL DOOR U CHANNEL CRACKED / REMOVED AND REPLACED R/H FLAP #5 FLAP TRACK UPPER 'U' CHANNEL FLAP TRACK FLAPPER DOOR IAW B737 DWG 149A7331 REV- AND IAW EA 190146 REV IR AND SWA EA REPAIR-57EA-0G455 REV 1 AND SRM SI-40-02-0G-0

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 21,922 hrs · 9,427 cycles

FWD CARGO COMPARTMENT FLOOR PANEL # 120AF CORROSION ON UPPER SURFACE. / FWD CARGO COMPARTMENT FLOOR PANEL 120AF FOUND TO BE MORE 20' OF CORROSION; OUT OF LIMITS IAW SRM 53-00-53-1A-1. FIG 102. REPLACED PANEL IAW IPC 25-52-10-17. PANEL INSTALLED ON SA-M 565S W/O #457678 PG 6. P/N 453A1610-14.

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 21,922 hrs · 9,427 cycles

FWD CARGO COMPARTMENT FLOOR PANEL # 120DF CORROSION ON UPPER AND LOWER SURFACE. / FWD CARGO COMPARTMENT FLOOR PANEL 120DF FOUND TO BE MORE THEN 20' OF CORROSION OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102. REPLACED PANEL IAW IPC 25-52-10-17. PANEL INSTALLED ON SA-M 565S W/O #457678 PG 7. P/N 453A1610-20

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 21,922 hrs · 9,427 cycles

FWD CARGO COMPARTMENT FLOOR PANEL # 120CF CORROSION ON UPPER SURFACE. / FWD CARGO COMPTMENT FLOOR PANEL 120CF FOUND TO BE MORE THEN 20' OF CORROSION; OUT OF LIMITS IAW SRM 53-00-53-1A-1. FIG 102. REPLACED PANEL IAW IPC 25-52-10-17. PANEL INSTALLED ON S-AM 565S WO 457678 PG 7. P/N 453A1610-103

Part: ANGLE — CRACKED (AFT CARGO COMPT) · airframe 21,922 hrs · 9,427 cycles

AFT CARGO COMPARTMENT STA 867 LBL 12 STANCHION LOWER ATTACH ANGLE CRACKED. / REMOVED DAMAGED ANGLE INSTALLED NEW ANGLE AS REQUIRED AFT CARGO STA 867 LBL 12. IAW SRM 51-40-02-0G-0

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 21,922 hrs · 9,427 cycles

AFT CARGO COMPT FLOOR PANEL 140BF IS CORRODED ALONG THE EDGES. MARKED. / REPLACED AFT CARGO COMPARTMENT FLOOR PANEL 140BF PIN: 453A2610-32 IAW B737-800 SIPC 25-52-10-19; SRM 51-10-02-0G-0 AND SRM 53-00-53-1A-1 ATAG: WN5844

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 21,922 hrs · 9,427 cycles

AFT CARGO COMPT FLOOR PANEL 140DF IS CORRODED ALONG THE EDGES. MARKED. / REPLACED AFT CARGO COMPARTMENT FLOOR PANEL 140DF P/N: 453A2610-20 IAW B737-800 AIPC 25-52-10-19 AND SRM 51-10-02-0G-0 AND SRM 53-00-53-1A-1

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 21,922 hrs · 9,427 cycles

AFT CARGO COMPT FLOOR PANEL 140EF IS CORRODED ALONG THE EDGES. MARKED. / REPLACED AFT CARGO FLOOR PANEL 140EF; P/N 453A2610-58 IAW B737-800 AIPC 25-52-10-19; SRM 51-10-02-0G-0 AND SRM 53-00-53-1A-1. ATAG: WN4541

Part: FLOOR PANEL — CORRODED (AFT CARGO COMPT) · airframe 21,922 hrs · 9,427 cycles

AFT CARGO COMPT FLOOR PANEL 140CF IS CORRODED ALONG THE EDGES. MARKED. / REPLACED AFT CARGO COMPARTMENT FLOOR PANEL 140CF P/N 453A2610-18 IAW B737-800 AIPC 25-52-10-19. SRM 51-10-02-0G-0 AND SRM 53-00-53-1A-1.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 21,922 hrs · 9,427 cycles

RH WING TE; UPR TE FIXED PNL; OTBD SUPT BRKT FWD SIDE CRACKED AT DEFLECTOR SUPT RIB. / REMOVED AND REPLACED R/H WING T/E FIXED PANEL OUTBD SUPPORT BRACKET IAW B737 SRM 51-40-02-0G-0 PARA 4; DWG 115A6200 ID2002 REV B.

Part: ANGLE — CORRODED (FWD CARGO COMPT) · airframe 21,922 hrs · 9,427 cycles

FWD CARGO COMPARTMENT AT STA. 500I; LBL 25 TO RBL 25; FLOOR ANGLE HAVE SEVERAL AREAS OF CORROSION. / NO ALLOWABLE LIMITS. REMOVED DAMAGED ANGLE INSTALLED NEW ANGLE AS REQUIRED. FWD CARGO STA 500I LBL25-RBL25. IAW BOEING DWG: 143A9481 REV:-. SRM 51-40-02-0G-0

Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 21,922 hrs · 9,427 cycles

FWD CARGO COMPARTMET; STA. 500C+11 - 500F; R/H Z-ANGLE HAVE SEVERAL AREAS OF CORROSION. / REMOVED AND REPLACED FWD CARGO R/H Z ANGLE STA 500A-500F + 12' IAW B737 SRM 51-10-02-0G-0; SRM 53-00-53-2R-5. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DETAIL D. ORIGINAL 'T' .040 LOSS OF .021 REMAINING .019.

Part: WEB — CRACKED (LEFT WING) · airframe 21,922 hrs · 9,427 cycles

LEFT WING; UPPER TRAILING EDGE PANEL BETWEEN SPOILERS #5 AND #6; INBOARD OF DEFLECTION RIB; HAVE WEB THAT IS CRACKED. MARKED. / REMOVED AND REPLACED WEB AT L/H WING T/E BETWEEN SPOILERS 5 & 6. P/N 115A215607 ATAG A12511 IAW BOEING DWG 115A2512 B737-800 SRM 51-40-02-0G-0

Part: BRACKET — CRACKED (RIGHT WING) · airframe 21,922 hrs · 9,427 cycles

RH WING TE; UPR TE FIXED PNL; CENTER SUPT BRKT CRACKED ON FWD SIDE. MARKED. / R/H WING T/E FIXED PNL CENTER SUPPORT BRACKET CRACKED. REMOVED CRACKED SUPPORT ANGLE I/A/W SRM 51-40-02-06-0. LOCATED AND DRILLED NEW SUPPORT ANGLE BRACKET I/A/W SRM 51-40-05-0G-0 ALSO AIPC 57-50-00-25. INSTALLED NEW CENTER SUPPORT ANGLE BRACKET I/A/W SRM 51-40-02-0G-0 ALSO AIPC 57-50-00-25.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 21,603 hrs · 9,294 cycles

RT WING TRAILING EDGE UPPER TRAILING EDGE FIXED PANEL, CENTER SUPPORT BRACKET CRACKED ON FORWARD SIDE. R&R BRACKET IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,603 hrs · 9,294 cycles

FORWARD CARGO COMPARTMENT RT Z-ANGLE CORRODED BETWEEN BS 500C+11 TO BS 500F. R&R Z ANGLE IAW SRM.

Part: WEB — CRACKED (LT WING) · airframe 21,603 hrs · 9,294 cycles

LT WING UPPER TRAILING EDGE PANEL BETWEEN SPOILERS 5 AND 6, INBOARD OF DEFLECTION RIB, HAVE WEB CRACKED. R&R WEB IAW SRM AND DWG.

Part: VAPOR BARRIER — DEBONDED (RT MLG WW) · airframe 21,603 hrs · 9,294 cycles

RT LOWER VAPOR BARRIER WEB INTERIM REPAIR DISBONDED AT BS 663. REPAIRED BARRIER IAW SRM.

Part: COVER — MISSING (CABIN) · airframe 21,828 hrs · 9,391 cycles

RT EMERGENCY EXIT LIGHT COVER MISSING AT ROW 6. R&R COVER IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 21,667 hrs · 9,320 cycles

MID CABIN EXIT SIGN ON CEILING BROKEN. R&R SIGN PER AMM.

Part: LENS — UNSECURE (CABIN) · airframe 21,355 hrs · 9,188 cycles

CENTER AISLE EXIT SIGN LENS DISPLACED. SECURED LENS PER MM.

Part: COVER — MISSING (EXIT SIGN) · airframe 20,802 hrs · 8,951 cycles

CENTER CABIN CEILING EMERGENCY EXIT SIGN MISSING COVER ON ONE SIDE. REINSTALLED COVER SIS.

Part: SLIDE — FAILED (R1 DOOR) · airframe 20,437 hrs · 8,797 cycles

R1 DOOR SLIDE FAILED. R&R SLIDE IAW MT.

Part: COVER — LOOSE (EXIT SIGN) · airframe 20,404 hrs · 8,778 cycles

RT MID CABIN EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER SIP.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 17,920 hrs · 7,731 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. ADJUSTED CLIPS PER AMM.

Part: COVER — MISSING (CABIN) · airframe 16,854 hrs · 7,252 cycles

RT EMERGENCY LIGHT LENS COVER MISSING AT ROW 10. INSTALLED COVER PER MM.

Part: LIGHT — DETACHED (CABIN) · airframe 16,209 hrs · 6,967 cycles

MAIN CABIN CEILING EMERGENCY EXIT LIGHT DETACHED. R&R LIGHT ASSEMBLY IAW AMM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 14,444 hrs · 6,215 cycles

RIGHT EMERGENCY LIGHT LENS BROKEN AT ROW 14. R & R THE LENS IAW SIP.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 14,444 hrs · 6,215 cycles

EMERGENCY LIGHT LENS BROKEN BETWEEN ROW 8 TO ROW 12. R & R THE LENS IAW SIP.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 14,263 hrs · 6,138 cycles

LEFT FORWARD OVERWING DOOR EXIT SIGN LENS MISSING. INSTALLED THE LENS IAW MM.

Part: LENS — MISSING (CABIN) · airframe 13,859 hrs · 5,964 cycles

LT EMERGENCY LIGHT LENS MISSING AT ROW 4. INSTALLED LENS ASSEMBLY PER SIP.

Part: VAPOR BARRIER — CRACKED (RT WING WW) · airframe 13,415 hrs · 5,743 cycles

RIGHT NR 2 WHEEL WELL FORWARD VAPOR BARRIER SEAL CRACKED AT RBL 31.83. REPAIRED BARRIER IAW SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 12,900 hrs · 5,508 cycles

RIGHT OVERHEAD EMERGENCY LIGHT LENS MISSING AT ROW 6. INSTALLED THE LENS IAW MM.

Part: LENS — MISSING (CABIN) · airframe 12,492 hrs · 5,332 cycles

LEFT EMERGENCY LIGHT LENS MISSING AT ROW 19. INSTALLED LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,575 hrs · 4,960 cycles

RIGHT OVERWING EMER EXIT LIGHT INOPERATIVE AT ROW 14. REPAIRED LIGHT IAW MM.

Part: LIGHT — MISSING (CABIN) · airframe 11,557 hrs · 4,952 cycles

LEFT EMER AISLE LIGHT MISSING AT ROW 27. INSTALLED LIGHT IAW MM.

Part: LENS — MISSING (CABIN) · airframe 7,249 hrs · 3,108 cycles

RIGHT OVERHEAD BIN, EMER EXIT LIGHT LENS MISSING AT ROW 6. INSTALLED LENS IAW SIP.

Part: LENS — MISSING (CABIN) · airframe 7,202 hrs · 3,085 cycles

RIGHT EMER LIGHT LENS MISSING AT ROW 6. INSTALLED LENS IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 975 hrs · 401 cycles

EMERGENCY EXIT SIGN AT EXIT ROW ON CEILING LOOSE. SECURED SIGN IAW MM.