N248WN

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 62,891 hrs · 38,088 cycles

EMERGENCY LIGHTS / BIN OVHD AREA LAMP INOP AT SEAT 16 FED AND 19 FED. REMOVED AND REPLACED LAMP BULBS FOR EMERGENCY LIGHTS / BIN OVHD AREA LAMP AT SEAT 16 FED AND 19 FED IAW AMM 33-51-03. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 62,083 hrs · 37,609 cycles

AFT GALLEY ENTRANCE DOOR (R2) EMERGENCY LIGHT IS INOP.<[01] REMOVED AND REPLACED AFT GALLEY ENTRANCE DOOR SLIDE LIGHT LAMP IN REF TO AMM 33-51-04. OPS CEHCK GOOD AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 62,052 hrs · 37,586 cycles

ODD ODOR NEAR EMER EXIT ROW<[01] ACCOMPLISHED FIM TASK 21-00 TASK 806. CUSTOMER REPORTED DRY CLEANNG SMELL. INSPECTED AREA. NO SMELLS AT THIS TIME

Part: SLIDE — JAMMED (ZONE 800) · airframe 61,144 hrs · 37,039 cycles

WHILE PERFORMING SAMPLE OF AFT SERVICE DOOR ESCAPE SLIDE; DOOR BECAME JAMMED BECAUSE SLIDE COMPARTMENT DID NOT OPEN WITH LOWER LATCH RELEASED. WHEN DOOR WAS FORCED OPEN; SLIDE DROPPED AND DEPLOYED<[01]. INSPECTED DOOR AND ESCAPE SLIDE ENCLOSURE; NO DEFECTS NOTED. REMOVED AND REPLACED AFTER SERVICE DOOR SLIDE IAW AMM 25-66-01. SEE TTG8Q00CW0EY.

Part: RETAINER — LOOSE (ZONE 200) · airframe 60,290 hrs · 36,497 cycles

FWD ENTRY FWD GIRT BAR RETAINER CLIP FASTENERS LOOSE<[01] SECURED FWD ENTRY FWD GIRT BAR RETAINER CLIP FASTENERS AS REQUIRED PER SRM 51-40-02

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 59,511 hrs · 35,990 cycles

INOP BATTERY PACK ON POWER SUPPLY UNIT M1670 AT PASSENGER CABIN 1 E/A. 2024-345852<[01] REPLACED EMERGENCY POWER SUPPLY BATTERY M1670 AND<BR>PERFORMED TEST IAW B737-700 AMM 33-51-06-960-805. TEST<BR>IS OK.;[02] CERTIFIED WORK PERFORMED.

Part: WEB — INCORRECT (ZONE 300) · airframe 59,511 hrs · 35,990 cycles

REJECT - IMPROPERLY WEB REPAIR PROCEDURE AT RT HORIZONTAL STABILIZER (TRIMMED OUT WEB INSTEAD STOP DRILL PROCEDURE) 2024-345807<[01] FOR STEP 2; TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N:190023010; DUE DATE: 24-JUL-24;[02] REPAIRED FRONT SPAR WEB LOC. BETWEEN STAB STA 138.70 TO STAB STA 147.90 AT RT HORIZONTAL STABILIZER IAW B737-700 EA 24-155-01688-WIP1; SRM B737-700 55-10-10-2R-1. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] CORRECTED STEP 2: REPAIRED FRONT SPAR WEB LOC. BETWEEN STAB STA 138.70 TO STAB STA 147.90 AT RT HORIZONTAL STABILIZER IAW EA 24-155-01688-WIP1; EA# EA 24-155-01688 AND SRM B737-700 55-10-10-2R-1.<BR> SEE INDIVIDUAL SIGN OFFS BELOW.;[04] CERTIFIED RII MAJOR REPAIR WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 59,511 hrs · 35,990 cycles

CRACK ON ANGLE LOCATED BTW BS 380 UP TO 400 RBL 43 WL 208.1 2024-345758<[01] REPLACED ANGLE <BR>LOCATED BTW BS 380 UP TO BS400 RBL 43 WL 208.1<BR>IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02<BR>DWG: 143A5400 SHEET: 38 REV: A<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] ACCOMPLISHED STEP <BR><BR>REPLACED ANGLE <BR>LOCATED BTW BS 380 UP TO BS400 RBL 43 WL 208.1<BR>IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02<BR>DWG: 143A5400 SHEET: 38 REV: A<BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SPAR WEB — CRACKED (ZONE 300) · airframe 59,511 hrs · 35,990 cycles

(CUSTOMER REQUEST) CRACK ON FRONT SPAR WEB LOCATED BETWEEN STAB STA 138.70 TO STAB STA 147.90 AT RT HORIZONTAL STABILIZER 2024-345743<[01] TOOL USED ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[02] REFER TO FAULT TTG8Q00TT24M WHERE EA-24-155-01688 WAS ADDED AS A SUBTASK. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] CORRECTED STEP 2.<BR>REPAIRED FRONT SPAR WEB LOCATED BETWEEN STAB STA 138.70 TO STAB STA 147.90 AT RT HORIZONTAL STABILIZER IAW 737-700 SRM 55-10-10-2R-1 WITH A DEVIATION OF THE TRIM OUT DOCUMENTED IN EA 24-155-01688 (TTG8Q00UJER3).<BR>SEE INDIVIDUALS SIGN OFF BELOW.;[04] CERTIFIED RII MAJOR REPAIR WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT ANGLE — CRACKED (ZONE 500) · airframe 59,511 hrs · 35,990 cycles

CRACK ON SUPPORT ANGLE LOCATED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2024-345719<[01] REPLACED SUPPORT ANGLE LOCATED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G-2 ;SRM 51-10-02-0G-0 PARAGRAPH 9 CHECK CLARENCE BETWEEN SKIN FLEX AND SKIN TAB IS OK IAW CMM 57-43-01 PAGE 708 FIGURE 702 .TOOL USED DIGITAL CALIPER P/N:500-196-30 S/N:A22348307 DUE DATE:23-AUG-24.;[02] REPLACED SUPPORT ANGLE LOCATED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02-0G-2 ;SRM 51-10-02-0G-0 PARAGRAPH 9 CHECK CLARENCE BETWEEN SKIN FLEX AND SKIN TAB IS OK IAW CMM 57-43-01 PAGE 708 FIGURE 702 .TOOL USED DIGITAL CALIPER P/N:500-196-30 S/N:A22348307 DUE DATE:23-AUG-24.

Part: ACCESS PANEL — CRACKED (ZONE 200) · airframe 59,511 hrs · 35,990 cycles

CRACK LOWER EDGE ACCESS PANEL 211B AT CONTROL CABIN 2024-345710<[01] REPAIRED LOWER EDGE ACCESS PANEL 211B AT CONTROL CABIN IAW B737-700 AMM 25-00-00-340-801 PROCEDURE 8.E MEASURED DAMAGE AREA IS (24IN2) TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A23218437; DUE DATE 14-FEB-25.;[02] REPAIRED LOWER EDGE ACCESS PANEL 211B AT CONTROL CABIN IAW B737-700 AMM 25-00-00-340-801 PROCEDURE 8.E MEASURED DAMAGE AREA IS (24IN2) TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A23218437; DUE DATE 14-FEB-25. COMPLETED TASK.

Part: FITTING — DETERIORATED (GIRT BAR) · airframe 59,511 hrs · 35,990 cycles

DETERIORATED AFT SERVICE DOOR GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA 2024-345681<[01] REPLACED AFT SERVICE DOOR GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801;[02] REPLACED AFT SERVICE DOOR GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801

Part: FITTING — DETERIORATED (ZN 800 DOOR) · airframe 59,511 hrs · 35,990 cycles

DETERIORATED ENTRY DOOR GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA 2024-345684<[01] REPLACED ENTRY DOOR GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801.;[02] REPLACED ENTRY DOOR GIRT BAR FITTING HARDWARE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801.

Part: MOUNT — CRACKED (WX RADAR) · airframe 59,511 hrs · 35,990 cycles

CRACK ON WEATHER RADAR MOUNT SUPPORT STRUCTURE 2024-345680<[01] REPLACED SUPPORT OF WEATHER RADAR MOUNT STRUCTURE IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND DWG# 141A9194 REV D. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT OF WEATHER RADAR MOUNT STRUCTURE IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND DWG# 141A9194 REV D. SEE INDIVIDUAL SIGN OFF BELOW.

Part: PLATE — CRACKED (ZONE 600) · airframe 59,511 hrs · 35,990 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 305 AT RT WING 2024-345622<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 305 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND DWG # 115A3700 REV-;[02] COMPLETED TASK CERTIFIED

Part: PLATE — CRACKED (ZONE 600) · airframe 59,511 hrs · 35,990 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING 2024-345621<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 115A3700 SHEET: 41 REV: - TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N:B20189527 DUE DATE:28-JUN-24;[02] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 115A3700 SHEET: 41 REV: - TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N:B20189527 DUE DATE:28-JUN-24

Part: BRACKET — CRACKED (ZONE 100) · airframe 59,511 hrs · 35,990 cycles

CRACK ON BRACKET LOCATED BS 540 AIR CONDITIONING BLEED DUCT RT SIDE 2024-345627<[01] REPLACED BRACKET LOCATED BS 540 AIR CONDITIONING BLEED DUCT RT SIDE IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02-0G-0;DWG 212A1101 SHEET 3 REV -.TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N:B20189527 DUE DATE:28-JUN-24.;[02] REPLACED BRACKET LOCATED BS 540 AIR CONDITIONING BLEED DUCT RT SIDE IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02-0G-0;DWG 212A1101 SHEET 3 REV -.TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N:B20189527 DUE DATE:28-JUN-24.;[03] CORRECTED STEP 1.<BR>REPLACED BRACKET LOCATED BS 540 AIR CONDITIONING BLEED DUCT RT SIDE IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02-0G-0;DWG 212A1101 SHEET 3 REV -.TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N:B20189527 DUE DATE:28-JUN-24 AND TORQUE WRENCH P/N:QD150 S/N:0612058996 DUE DATE:02-APR-25.;[04] CORRECTED STEP 2 <BR>REPLACED BRACKET LOCATED BS 540 AIR CONDITIONING BLEED DUCT RT SIDE IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02-0G-0;DWG 212A1101 SHEET 3 REV -.TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N:B20189527 DUE DATE:28-JUN-24 AND TORQUE WRENCH P/N:QD150 S/N:0612058996 DUE DATE:02-APR-25.

Part: PANEL — CORRODED (ZONE 600) · airframe 59,511 hrs · 35,990 cycles

CORROSION ON REFUELING PANEL ON LEADING EDGE AT RT WING 2024-345588<[01] ON STEP 4. TOOL USED: THICKNESS GAGE. P/N: 45MG. S/N: 221859911. DUE DATE: 17-NOV-24. <BR><BR>ON STEP 5. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 60009161631. DUE DATE: 11-MAR-25.;[02] REPAIRED REFUELING PANEL ASSY (FUEL SYSTEM ONLY) LOCATED ON LEADING EDGE BETWEEN SS163.95 AND SS150.81 AT RT WING IAW EA# 24-157-01549-WIP1; EA# 24-157-01549<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[03] COMPLETED TASK CERTIFIED

Part: FITTING — CORRODED (HORIZONTAL STAB) · airframe 59,511 hrs · 35,990 cycles

CORROSION ON REAR SPAR CENTER SECTION LOWER AFT CLEVIS LOCATED FWD FACE RT HORIZONTAL STABILIZER 2024-345590<[01] FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION RT<BR>HORIZONTAL STABILIZER SEE FAULT TTG8000TL5VX.;[02] CORRECTED CORRECTIVE ACTIONS 1.<BR>FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION RT<BR>HORIZONTAL STABILIZER SEE FAULT TTG8000TL5VX; AE 24-155-01561.;[03] CORRECTED CORRECTIVE ACTIONS 2.<BR>FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION RT<BR>HORIZONTAL STABILIZER SEE FAULT TTG8000TL5VX; EA 24-155-01561.;[04] FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION RT<BR>HORIZONTAL STABILIZER SEE FAULT TTG8000TL5VX; EA 24-155-01561.

Part: FITTING — CORRODED (ZONE 300) · airframe 59,511 hrs · 35,990 cycles

CORROSION ON LOWER LUG FITTING LOCATED AFT FACE POSITION LT HORIZONTAL STABILIZER 2024-345584<[01] FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION LT HORIZONTAL STABILIZER SEE FAULT TTG8Q00TL6U8;[02] FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION LT HORIZONTAL STABILIZER SEE FAULT TTG8Q00TL6U8;[03] CORRECTED CORRECTIVE ACTIONS 1..<BR>FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION LT HORIZONTAL STABILIZER SEE FAULT TTG8Q00TL6U8; AE 24-155-01567.;[04] CORRECTED CORRECTIVE ACTIONS 2<BR>FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION LT HORIZONTAL STABILIZER SEE FAULT TTG8Q00TL6U8; AE 24-155-01567.

Part: SUPPORT ANGLE — CRACKED (ZONE 600) · airframe 59,511 hrs · 35,990 cycles

CRACK ON SUPPORT ANGLE LOCATED ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING 2024-345585<[01] REPLACED SUPPORT ANGLE (FITTING) LOCATED ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING (1 E/A) IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 PARAGRAPH 9 DWG 115A2930 SHEET 8 REV-.;[02] REPLACED SUPPORT ANGLE (FITTING) LOCATED ORSS 271 DEFLECTION CONTROL RIB AREA AT RT WING (1 E/A) IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 PARAGRAPH 9 DWG 115A2930 SHEET 8 REV-.

Part: ANGLE — CRACKED (ZONE 500) · airframe 59,511 hrs · 35,990 cycles

CRACK ON ANGLE LOCATED ON ACCESS PANEL 551FB TRAILING EDGE AT LT 2024-345592<[01] REPLACED ANGLE LOCATED ON ACCESS PANEL 551FB TRAILING EDGE AT LT IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02.;[02] COMPLETED TASK CERTIFIED

Part: FITTING — CORRODED (ZONE 300) · airframe 59,511 hrs · 35,990 cycles

CORROSION ON LOWER LUG FITTING LOCATED AFT FACE POSITION RT HORIZONTAL STABILIZER 2024-345586<[01] FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION LT<BR>HORIZONTAL STABILIZER SEE FAULT TTG8000TL5VX.;[02] CORRECTED CORRECTIVE ACTIONS 1.<BR>FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION RT<BR>HORIZONTAL STABILIZER SEE FAULT TTG8000TL5VX.;[03] CORRECTED CORRECTIVE ACTIONS 2.<BR>FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION RT<BR>HORIZONTAL STABILIZER SEE FAULT TTG8000TL5VX; EA 24-155-01561.;[04] FOR REPAIR OF LUG FITTING LOCATED AFT FACE POSITION RT<BR>HORIZONTAL STABILIZER SEE FAULT TTG8000TL5VX; EA 24-155-01561.

Part: SUPPORT BEAM — CRACKED (ZONE 500) · airframe 59,511 hrs · 35,990 cycles

CRACK ON SUPPORT BEAN ON DEFLECTION CONTROL RIB TRAILING EDGE AT LT WING 2024-345553<[01] TOOL USED STEP 8: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 21 JUL 24.;[02] PERFORMED PERMANENT REPAIR ON DEFLECTION CONTROL RIB AREA LH WING IAW B737-700 SRM 57-51-02-2R-3 REPAIR 3 AND B737-700 SRM 57-51-02-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CERTIFIED CORRECTIVE ACTION 2; COMPLETED

Part: ANGLE — CRACKED (ZONE 500) · airframe 59,511 hrs · 35,990 cycles

CRACK ON SUPPORT ANGLE LOCATED ORSS 251 AREA OF DEFLECTION CONTROL RIB AT LT TRAILING EDGE 2024-345552<[01] REPLACED SUPPORT ANGLE LOCATED ORSS 251 AREA OF DEFLECTION CONTROL RIB AT LT TRAILING EDGE IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 115A2930 SHEET 7 REV - DUE TO NO FOUND ALLOWABLE DAMAGE LIMITS ON B737-700 SRM 57-51-02-1A-1 AD1 MEASURE OF CRACK IS: L=0.700' TOOL USED CALIPER P/N: 500-196-30 S/N: B21141522 DUE DATE: 07-NOV-24;[02] COMPLETED TASK CERTIFIED

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 59,511 hrs · 35,990 cycles

CRACK SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN 2024-345574<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW DRAWING # 146A7901-1 SHEET 66 REV: A; B737-700 SRM 51-40-02-0G-0 AND 51-10-02-0G-0 SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1 REPLACED SUPPORT ANGLE AND FASTENERS LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW DRAWING # 146A7901-1 SHEET 66 REV: A; B737-700 SRM 51-40-02-0G-0 AND 51-10-02-0G-0 PARAGRAPH 9 SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2 CORRECTED STEP 1 REPLACED SUPPORT ANGLE AND FASTENERS LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW DRAWING # 146A7901-1 SHEET 66 REV: A; B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 PARAGRAPH 9 SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW DRAWING # 146A7901-1 SHEET 66 REV: A; B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 PARAGRAPH 9 SEE INDIVIDUAL SIGN OFF BELOW.

Part: TIE CLIP — CRACKED (ZN 200 FUS TOP) · airframe 59,511 hrs · 35,990 cycles

CRACK TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN 2024-345554<[01] REPLACED TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV-; DWG 141A8380 SHEET 21 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV-; DWG 141A8380 SHEET 21 REV-. RII; SEE INDIVIDUAL SIGN OFFS BELOW.

Part: LIGHT — DETERIORATED (CABIN) · airframe 59,511 hrs · 35,990 cycles

DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA). 2024-345547<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) IAW B737-700 AMM 33-51-15-400-802;[02] TASK CARD COMPLETE.

Part: STRAP — CORRODED (ZN 200 FUS TOP) · airframe 59,511 hrs · 35,990 cycles

CORROSION ON STRAP LOCATED BTW BS1016 TO BS1040 WL208.1 RBL4 AFT GALLEY AREA 2024-345534<[01] REPLACED STRAP LOCATED BTW BS1016 TO BS1040 WL208.1 RBL4 AFT GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DRAWING# 147A5730 SHEET 23 REV: C<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED STRAP LOCATED BTW BS1016 TO BS1040 WL208.1 RBL4 AFT GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DRAWING# 147A5730 SHEET 23 REV: C<BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: STRAP — CORRODED (ZONE 200) · airframe 59,511 hrs · 35,990 cycles

CORROSION ON STRAP LOCATED BTW BS1016 TO BS1040 WL208.1 LBL3 AFT GALLEY AREA 2024-345535<[01] REPLACED STRAP AND FASTENERS LOCATED BTW BS1016 TO BS1040 WL208.1 LBL3 AFT GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 147A5600 SHEET: 32; REV: B. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED STRAP AND FASTENERS LOCATED BTW BS1016 TO BS1040 WL208.1 LBL3 AFT GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 147A5600 SHEET: 32; REV: B. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SCUFF PLATE — CRACKED (ZONE 200) · airframe 59,511 hrs · 35,990 cycles

CRACK ON CENTER SCUFF PLATE AT FWD SERVICE DOOR. 2024-345515<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23272782; DUE DATE: 06-MAR-25.;[02] EQUIPMENT P/N XRP-3000; S/N 1859843; DUE DATE 24-JUL-24 WAS USED ON STEP 4;[03] REPAIRED CENTER SCUFF PLATE AT FWD SERVICE DOOR I.A.W. BOEING 737-700 SRM TASK 53-10-15-2R-2; REPAIR 2; PARAGRAPH 4. B; STEPS (3) TO (6) AND (8); FIGURE 203 AND BAC 5975. SEE INDIVIDUAL SIGNOFF BELOW.;[04] TASK COMPLETED.

Part: FLOORBEAM — CRACKED (ZN 100 FUS LOWER) · airframe 59,511 hrs · 35,990 cycles

CRACK FLOOR BEAM LOCATED STA328 AND RBL24.75 WL208.1 AT FWD GALLEY AREA 2024-345526<[01] TOOL USED EDDY CURRENT EQUIPMENT PN:NORTEC 600D;SN:60007161486;DUE DATE:28-JUL-24.;[02] REPAIRED FLOOR BEAM LOCATED STA328 BETWEEN LBL7 TO RBL 65 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 SEE INDIVIDUALS SIGN OFF BELOW;[03] REPAIRED FLOOR BEAM LOCATED STA328 BETWEEN LBL7 TO RBL 65 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 SEE INDIVIDUALS SIGN OFF BELOW<BR><BR>ITEM RII

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 59,511 hrs · 35,990 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND LBL 11 FWD GALLEY AND LAV 2024-345506<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS360 AND LBL 11 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DRAWING 141A5400 SHEET: 46 REV: A. SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS360 AND LBL 11 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DRAWING 141A5400 SHEET: 46 REV: A. SEE INDIVIDUAL SIGN OFFS BELOW

Part: SUPPORT PLATE — CORRODED (ZONE 100) · airframe 59,511 hrs · 35,990 cycles

CORROSION ON SUPPORT PLATE LOCATED BETWEEN BS 787 TO BS 790 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT 2024-345508<[01] REPLACED SUPPORT PLATE LOCATED BETWEEN BS 787 TO BS 790 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9.;[02] CORRECT STEP 1. REPLACED SUPPORT PLATE LOCATED BETWEEN BS 787 TO BS 790 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT AND PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND MORE DAMAGE I.A.W B737-700 SRM 51-10-02 ITEM 9.;[03] REPLACED SUPPORT PLATE LOCATED BETWEEN BS 787 TO BS 790 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT AND PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND MORE DAMAGE I.A.W B737-700 SRM 51-10-02 ITEM 9.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 59,511 hrs · 35,990 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 312 TO BS 328 AND LBL 46 FWD GALLEY AND LAV 2024-345501<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BS 312 TO BS 328 AND LBL 46 FWD GALLEY AREA AND LAV; IAW BOEING 737-700 SRM 51-40-02; IAW BOEING 737-700 SRM 51-10-02 ITEM 9; AND DRAWING 141A5400 SHEET 26 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BS 312 TO BS 328 AND LBL 46 FWD GALLEY AREA AND LAV; IAW BOEING 737-700 SRM 51-40-02; IAW BOEING 737-700 SRM 51-10-02 ITEM 9; AND DRAWING 141A5400 SHEET 26 REV -. SEE INDIVIDUAL SIGN OFF BELOW.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 59,511 hrs · 35,990 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-345503<[01] REPLACED WEB INTERCOSTAL AND FASTENERS LOC. FLOOR STRUCTURE BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV. IAW B737-700 SRM 51-10-02; 51-40-02 AND DRAWING 141A5400 REV - SEE INDIVIDUALS SIGN OFF BELOW;[02] CERTIFIED CORRECTIVE ACTION 1; COMPLETED

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 59,511 hrs · 35,990 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS344 TO BS 360 AND BL 0 FWD GALLEY AND LAV 2024-345505<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS344 TO BS 360 AND BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02-0G-0; 51-40-02-0G AND DWG 147A7221 SHEET 24 REV- SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS344 TO BS 360 AND BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02-0G-0; 51-40-02-0G AND DWG 147A7221 SHEET 24 REV- SEE INDIVIDUAL SIGN OFF BELOW.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 59,511 hrs · 35,990 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 328 TO BS 344 AND LBL 46 FWD GALLEY AND LAV 2024-345502<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED<BR>BS 328 TO BS 344 AND LBL 46 FWD GALLEY AND LAV.<BR>IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02<BR>DWG: 141A5400 SHEET: 44 REV: - <BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED<BR>BS 328 TO BS 344 AND LBL 46 FWD GALLEY AND LAV.<BR>IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02<BR>DWG: 141A5400 SHEET: 44 REV: - <BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SUPPORT ANGLE — CORRODED (GIRT BAR FITTING) · airframe 59,511 hrs · 35,990 cycles

CORROSION ON SUPPORT ANGLE GIRT BAR FITTING LOCATED BS312 TO BS 344 AND LBL 56 WL 208.1 AT FWD GALLEY AREA 2024-345507<[01] REPLACED SUPPORT ANGLES 2 E/A GIRT BAR FITTING LOCATED BS312 AND BS344 AND LBL 56 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND B737-700 SRM 51-40-02;[02] CORRECTED STEP 1: REPLACED SUPPORT ANGLES 2 E/A GIRT BAR FITTING LOCATED BS312 AND BS344 AND LBL 56 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND B737-700 SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 53-10-51-1A-1;[03] REPLACED SUPPORT ANGLES 2 E/A GIRT BAR FITTING LOCATED BS312 AND BS344 AND LBL 56 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND B737-700 SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 53-10-51-1A-1

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 59,511 hrs · 35,990 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 312 TO BS328 AND RBL 31 FWD GALLEY AND LAV 2024-345504<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 312 TO BS328 AND RBL 31 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DRAWING 141A5400 SHEET: 39 REV: -. SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 312 TO BS328 AND RBL 31 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DRAWING 141A5400 SHEET: 39 REV: -. SEE INDIVIDUAL SIGN OFFS BELOW

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 59,511 hrs · 35,990 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-345451<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23272782; DUE DATE: 06-MAR-2024.;[02] CORRECTED STEP 1. TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23272782; DUE DATE: 06-MAR-25.;[03] TOOL USED IN STEP 4: RADIOMETER/PHOTOMETER KIT ; P/N: XRP-3000; S/N: 1859843; DUE DATE : 24/JUL/24;[04] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.

Part: HANDLE — DETERIORATED (ZN 800 DOOR) · airframe 59,511 hrs · 35,990 cycles

DETERIORATED NUT ASSIT HANDLE ON FWD ENTRY DOORWAY LINNING AT GALLEY AREA (2EA) 2024-345413<[01] REPLACED NUT ASSISTANT HANDLE ON FWD ENTRY DOORWAY LINNING AT GALLEY AREA (2EA) IAW SOPM-20-50-01 REV.38 AND DWG 411A2600-4B REV.A SHEET 2;[02] REPLACED NUT ASSISTANT HANDLE ON FWD ENTRY DOORWAY LINNING AT GALLEY AREA (2EA) IAW SOPM-20-50-01 REV.38 AND DWG 411A2600-4B REV.A SHEET 2

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 59,511 hrs · 35,990 cycles

(CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOCATED ON BS 663 RH SIDE AT WING CENTER SECTION 2024-345335<[01] TOOL USED: CALIPER: P/N:500-197-30 SN: B20189521; DUE DATE: 26-JAN-25.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 15-FEB-25.;[03] TOOL USED SCALE P/N: CR5200 S/N: 8342514509 DUE DATE: 27-FEB-25.;[04] TOOL USED: HOT BONDER P/N:HCS9200B-AV ; S/N:18185781 DUE DATE: 15-FEB-25;[05] TOOL USED: UT EQUIPMENT P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 04-OCT-24;[06] REPAIRED VAPOR BARRIER LOCATED ON BS 663 RH SIDE AT WING CENTER SECTION IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW;[07] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: DOOR — CORRODED (WASTE SERVICE) · airframe 59,511 hrs · 35,990 cycles

CORROSION INTERNAL SKIN TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE 2024-345277<[01] TOOL USED STEP 4 ULTRASONIC THICKNESS GAGE; P/N: 45 MG; S/ N: 221860711; DUE DATE: 21-NOV-24;[02] EQUIPMENT P/N 45MG; S/N 221861811; DUE DATE 30-NOV-24 WAS USED ON STEP 8;[03] REPAIRED TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE IAW B737-700 SRM 52-40-01-2R-8 REPAIR 8 SEE INDIVIDUALS SIGN OFF BELOW;[04] CERTIFIED CORRECTIVE ACTION 3 <BR>REPAIRED TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE IAW B737-700 SRM 52-40-01-2R-8 REPAIR 8 SEE INDIVIDUALS SIGN OFF BELOW

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 59,464 hrs · 35,961 cycles

EMERGENCY LIGHTS M1673 BATTERY PACK WILL NOT HOLD A CHARGE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 59,464 hrs · 35,961 cycles

RIGHT SIDE EXTERIOR WTB EMERGENCY LIGHT JUST AFT OF FLAPS IS INOP<[01] PERFORMED EMERGENCY LIGHTS-OPERATIONAL TEST I.A.W AMM 33-51-00-710-801<BR>OPS CHECK:GOOD;[02] PERFORMED EMERGENCY LIGHTS-OPERATIONAL TEST I.A.W AMM 33-51-00-710-801 FAILS OPS CHECK NEEDS BATTERY;[03] BATTERY REPLACE ON TTG8Q00T1L7Z. PERFORMOED OPS CHECK OF R/H EXTERIOR WTB EMERGENCY LIGHT IAW AMM 33-51-06-960-805 OPS CHECK GOOD;[04] VERIFIED STEPS 2 AND 3<BR>AUDIT C/W

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 59,464 hrs · 35,961 cycles

LEFT SIDE EXTERIOR WTB EMERGENCY LIGHT JUST AFT OF FLAP IS INOP<[01] PERFORMED EMERGENCY LIGHTS-OPERATIONAL TEST I.A.W AMM 33-51-00-710-801<BR>OPS CHECK:GOOD;[02] PERFORMED EMERGENCY LIGHTS-OPERATIONAL TEST I.A.W AMM 33-51-00-710-801 FAILS OPS CHECK NEEDS BATTERY;[03] REMOVED AND REPLACED M1670 BATTERY PACK AND OPS CHECKED L/H WTB EMERGENCY LIGHT IAW AMM 33-51-06-960-805 OPS CHECK GOOD;[04] COMPLETE<BR>AUDIT C/W

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,464 hrs · 35,961 cycles

MID CABIN LEFT SIDE EMERGENCY LIGHTS AT APPROX ROW 9 AND 12 ABC ARE OUT STOWBIN BULLNOSE. REPLACED EMERGENCY LIGHT BATTERY PACK M1668 IAW 33-51-06-960-805. ACCOMPLISHED OPS CHECK IAW AMM 33-51-06-960-805 STEP 4.E. OPS CHECKED GOOD

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 59,464 hrs · 35,961 cycles

EMERGENCY LIGHTS AT FWD RIGHT STOWBIN BULLNOSE APPROX 3 AND 6 DEF ARE OUT<[01] REPLACED BATTERY PACK M1674 I.A.W AMM 33-51-06-960-805 STEP:4.E.5 TO 4.FOPS CHECKS:GOOD;[02] VERIFIED STEP 1<BR>AUDIT CW

Part: GLOWSTRIP — FAILED (CABIN) · airframe 58,804 hrs · 35,548 cycles

FLIGHT ATTENDANT REPORTS THAT THE PHOTOLUMINESCENT FLOOR EMERGENCY LIGHTING DOES NOT GLOW AT ALL<[01] INSPECTED PHOTOLUMINESCENT FLOOR LIGHTING IAW AMM 33-51-15. OPS CHECK GOOD

Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 58,336 hrs · 35,261 cycles

FWD EMERGENCY FLASHLIGHT BATTERY DEAD<[01] R & R BATTERY PER AMM 25-64-00

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,751 hrs · 34,244 cycles

FWD SERVICE DOOR; FWD GALLEY; AND FWD ENTRY DOOR SLIDE EMERGENCY LIGHTS INOP.<[01] REMOVED AND REPLACED FWD LH EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 56,491 hrs · 34,070 cycles

RIGHT HAND 663 VAPOR BARRIER WEB IS CRACKED AT RBL 31 W/L 162<[01] EVALUATED R/H 663 VAPOR BARRIER AND FOUND PREVIOUS REPAIR 6.0' FAILED. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 57-10-10-2R-2 PAR 1A& NOTE. CLEAN AND PREP. IAWB737-700 SRM 51-70-04-2R-10 PAR4A-C. VERIFIED MATERIALS AS: BMS 8-301 (A182489); BMS 9-3 (A162523). IAW B737-700 SRM 51-70-04-2R-0 TABLE 203. NEED OK TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES. IAW B737-700 SRM 51-70-04-2R-10 PAR 4 D-G. AAR OVEN BO-06 D.D. 7-27-23 150DEG 2HRS.;[04] VERIFIED STEP 3;[05] RESTORED DECORATIVE FINISHES TO 2EA. REPAIR AREAS IAW SRM 57-70-04-2R-0 STEP 4.P.;[06] VERIFIED STEP 5;[07] AUDIT CW

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 56,491 hrs · 34,070 cycles

LEFT HAND 663 VAPOR BARRIER WEB IS CRACKED AT LBL 31 W/L 162<[01] EVALUATED DAMAGE; LEFT HAND 663 VAPOR BARRIER IS REPAIRABLE IAW B737 57-10-10-2R-2 REPAIR 2. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 51-70-04-2R-10 REPAIR 10 PAR 4 STEP A;B; AND C.<BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 51-70-04-2R-0 TABLE 203; FIBERGLASS CLOTH BMS9-3(A164924); RESIN EY3804 (A182489).<BR><BR>REQUIRES OKAY TO BOND.;[02] VERIFIED ACTION ITEM 1<BR><BR>OK GIVEN TO BOND REPAIR;[03] BONDED REPAIR PLIES IAW B737 SRM 51-70-04-2R-10 PAR 4 STEPS D;E;F; AND G. TAP TEST GOOD. OVEN B0-06 CAL DUE 7/27/23.;[04] VERIFIED ACTION ITEM 3;[05] RESTORED FINISHES TO REPAIR AREAS IAW SRM 51-70-04-2R-0 STEP4.P.;[06] VERIFIED TASK COMPLETE

Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 56,491 hrs · 34,070 cycles

DOT 114-012. CABIN FLOOR BOARD 232YF HAS AREAS OF PULLED FIBERS.<[01] EVALUATED PANEL 232YF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2R-1 PAR 3A;C;E&F. VERIFY MATERIALS AS: BMS 8-201 (A176813); BMS 9-3 (A164924). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3K-M.;[04] REPAIRED DAMAGE TO UPPER SURFACE OF PANEL 232YF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4

Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 56,491 hrs · 34,070 cycles

DOT 114-010. CABIN FLOOR BOARD 232RF HAS AREAS OF PULLED FIBERS.<[01] EVALUATED PANEL 232RF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2R-1 PAR 3A;C;E&F. VERIFIED MATERIALS AS: BMS 8-201 (A176813); BMS 9-3 (A164924). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3 K-M.;[04] REPAIRED DAMAGE TO UPPER SURFACE OF PANEL 232RF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4

Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 56,491 hrs · 34,070 cycles

DOT A24-20 MID CABIN FLOOR BOARD 231XF HAS COMPOSITE PULLED FIBERS ON UPPER SURFACE.<[01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; RESIN EPOCAST50A(A178552); FIBERGLASS CLOTH BMS9-3(A164924). <BR><BR>CLEANED; PREPPED DAMAGED AREAS IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;C;E;F; AND J. <BR><BR>REQUIRES OKAY TO BOND.;[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. TAP TEST GOOD. OVEN B0-06 CAL DUE 7/27/23.;[04] REPAIRED CABIN FLOOR BOARD 231XF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1.;[05] VERIFIED STEPS 3-4

Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 56,491 hrs · 34,070 cycles

DOT A24-21 MID CABIN FLOOR BOARD 241AF HAS COMPOSITE PULLED FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. RESIN (A178557); FABRIC (A164924).<BR><BR>REQUEST OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. TAP TEST GOOD.;[04] REPAIRED MID CABIN FLOOR BOARD 241AF UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3-4

Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 56,491 hrs · 34,070 cycles

DOT 114-015. CABIN FLOOR BOARD 242AF HAS AREAS OF PULLED FIBER.<[01] EVALUATED PANEL 242AF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2R-1 PAR 3A;E E&F. VERIFY MATERIALS AS: BMS 8-201 (A176813); BMS 9-3 (A164924). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3K-M.;[04] REPAIRED DAMAGE TO UPPER SURFACE ON PANEL 242AF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4

Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 56,491 hrs · 34,070 cycles

DOT 114-002. CABIN FLOOR BOARD 232SF HAS PULLED FIBERS.<[01] EVALUATED PANEL 232SF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3A;C;E&F. VERIFIED MATERIALS: BMS 8-201 (A176813); BMS 9-3 (A164924). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3K-M.;[04] REPAIRED DAMAGE TO UPPER SURFACE ON PANEL 232SF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,491 hrs · 34,070 cycles

L2 OUTER FUSELAGE EMERGENCY LIGHT IS INOP<[01] REPLACED POWER SUPPLY BATTERY PACK AT POSITION M1673 STA 952 WL 290 LBL 14 IAW AMM33-51-06-960-805 STEP 4E (1-3)(E)(4)(5).;[02] STEP 1 WDM 33-51-14 PG 13 SH1.;[03] STEPS 1 & 2 C/W;[04] ACCOMPLISHED BATTERY AND LIGHT OPS CHECK IAW AMM 33-51-06-960-805. TESTS GOOD;[05] CERTIFIED STEP 4. <BR>AUDIT COMPLETE.

Part: LIGHT — LOOSE (ZN 200 FUS TOP) · airframe 56,491 hrs · 34,070 cycles

WHILE REMOVING AFT L/H WINDSCREEN FOUND AFT LOWERED CEILING EXIT LIGHT LOOSE<[01] REPLACED AFT LOWERED CEILING EXIT LIGHT IAW AMM 33-51-01-960-802<BR><BR>TEST WAS GOOD <BR><BR>A TAG# WN5757;[02] VERIFIED STEP 1<BR>AUDIT C/W

Part: LIGHT — INOPERATIVE (AFT CABIN) · airframe 54,643 hrs · 32,830 cycles

AFT ENTRY EMERGENCY LIGHT INOP / [01] REMOVED AND REPLACED AFT ENTRY EMERGENCY LIGHT LAMP IAW AMM 33-51-03 OPS CHECK GOOD

Part: RETAINER SEAL — CRACKED (RH WING) · airframe 53,726 hrs · 32,221 cycles

RH WING TE CAVITY UNDER SPOILER N8 LOCATION LOWER PANEL INB SEAL RETAINER CRACKED 2022-284074 / [01] REPLACED SEAL RETAINER AND FASTENERS LOCATED RH WING TE CAVITY UNDER SPOILER N8 LOWER PANEL INB SEAL IAW SRM 51-40-02 AND SRM 51-10-02.;[02] COMPLETE TASK CERTIFIED

Part: FITTING — CRACKED (AFT CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CRACK INDICATION FOUND ON FITTING ( SEAT TRACK FASTENER HOLE A ) LOCATED STA 727B LBL 45.5 AFT CARGO COMPARTMENT. 2022-284060 / [01] TOOL USED CALIPER PN 500-197-30; SN A18229518; CAL DUE DATE 21 SEP 22;[02] REPLACED NEW FITTING LOCATED STA 727B LBL 45.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A5502 REV: B SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED NEW FITTING LOCATED STA 727B LBL 45.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A5502 REV: B; RII SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,726 hrs · 32,221 cycles

PERFORM REPAIR LOCATED ON EXTERNAL SKIN 10 INCHES AFT BS 1016 ON BL 0 AT LEVEL WL 308.5 AT UPPER FUSELAGE DUE TO AFTER EVALUATION CORROSION FOUND OUT LIMITS 2022-284059 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 03-DEC-22;[02] PERFORMED PERMANENT REPAIR LOC BTW BS 1016+5? AND BS1016+15 AND BTW LBL 5 TO RBL 15 IAW B737-700 SRM 53-80-01-2R-4 REPAIR 4 MATERIAL USED: DOUBLER 2024T3 0.090? P.O: 2021 163769 STRUCTURAL FILLER 2024T3 0.080? P.O: 2022 135797 SEE INDIVIDUAL SING OFF BELOW.;[03] PERFORMED PERMANENT REPAIR LOC BTW BS 1016+5? AND BS1016+15 AND BTW LBL 5 TO RBL 15 IAW B737-700 SRM 53-80-01-2R-4 REPAIR 4 MATERIAL USED: DOUBLER 2024T3 0.090? P.O: 2021 163769 STRUCTURAL FILLER 2024T3 0.080? <BR>P.O: 2022 135797 SEE INDIVIDUAL SING OFF BELOW.<BR>COMPLETED RII

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2022-284030 / [01] REMOVED GUSSET AND FASTENER LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SIGN OFFS BELOW.;[02] STEP 1 CORRECTED <BR>REPLACED GUSSET AND FASTENER LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SIGN OFFS BELOW.;[03] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: INTERCOSTAL — CORRODED (FWD CARGO) · airframe 53,726 hrs · 32,221 cycles

CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS492.4 TO BS500A STR26R AND WL156 FWD CARGO COMPARTMENT 2022-284006 / [01] TOOL USED : ELECTRONIC CALIPER ; P/N : 500-196-30 ; S/N : A20230758 ; DUE DATE : 13/AUG/22;[02] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS492.4 TO BS500A STR26R AND WL156 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-01 ITEM 9 AND DWG 143A0040 REV:? SEE INDIVIDUAL SIGNOFFS BELOW;[03] CERTIFIED STEP 2. COMPLETED

Part: STRINGER — CRACKED (FWD CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CRACK STRINGER 25R LOCATED BS540 FWD CARGO COMPARTMENT 2022-284012 / [01] TOOL USED ULTRASONIC EQUIPMENT PN:38PLPLUS; SN:120398603; DUE DATE: 18OCT-22;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101V022235; DUE DATE: 03 JUN 22.;[03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 02-FEB-23. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 02-FEB-23;[04] REPAIRED STR 25R IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 LOCATED BS540 FWD CARGO COMPARTMENT;[05] REPAIRED STR 25R IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 LOCATED BS540 FWD CARGO COMPARTMENT SEE SIGN OFF BELOW;[06] REPAIRED STR 25R IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 LOCATED BS540 FWD CARGO COMPARTMENT SEE SIGN OFF BELOW.<BR>TASK COMPLETED;[07] CORRECTED REFERENCE SRM 53-00-03-2R-1;[08] UPDATED REFERENCE TO INCLUDE COMPLETE NUMBER.<BR><BR>53-00-03-2R-1-A01573

Part: SKIN — CRACKED (LH HOR STAB) · airframe 53,726 hrs · 32,221 cycles

CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STA 193.90 RIB. 24.5 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK L = 1.0 INCH. 2022-284003 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 190023010 DUE DATE: 14-FEB-23;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 190023010 DUE DATE: 14-FEB-23;[03] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101V022235; DUE DATE: 03 JUN 22.;[04] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[05] UT TOOL USED PN: 38DLPLUS ; SN: 120398603. DUE DATE: 18-OCT-22 <BR>ET TOOL USED: PN: NORTEC 600; SN: 200048001; DUE DATE: 30-MAR-23;[06] PERFORMED PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN IAW EA#22-155-01621 REV[1] AND EA#22-155-01621-WIP1 REV[1] SEE INDIVIDUAL SIGNS OFF BELOW;[07] CERTIFIED STEP 6 COMPLETED. ITEM RII

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 53,726 hrs · 32,221 cycles

INOP EMERGENCY BATTERY PACK ON AFT LOWERED CEILING PANEL 2022-284009 / [01] REPLACED EMERGENCY BATTERY PACK ON AFT LOWERED CEILING PANEL (2EA) IAW B737-700 AMM 33-51-06-960-805 TEST OK. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED EMERGENCY BATTERY PACK ON AFT LOWERED CEILING PANEL (2EA) IAW B737-700 AMM 33-51-06-960-805 TEST OK. SEE INDIVIDUAL SIGN OFF BELOW. COMPLETED

Part: STRINGER — CRACKED (FWD CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CRACK STRINGER 23L LOCATED BS540 FWD CARGO COMPARTMENT 2022-284013 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101V022235; DUE DATE: 03 JUN 22.;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[03] TOOL USED CALIPER P/N 500-197-30 S/N A21147759 CAL DUE DATE 15 OCT 22. RADIUS GAGE P/NS167C S/N AE-28530 CAL DUE DATE 26 FEB 23.;[04] PERFORMED PERMANENT REPAIR ON STRINGER 23L LOCATED BS540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. MATERIAL USED: ALUMINUM SHEET 7075-T0 0.036? PO: 2021 131796 ( CONVERTER TO 7075 T6); CHANNEL BAC1493-249 PO: 2021 147833 ; ANGLES (2E/A) BAC1493-659 PO: 2021 149606 SEE INDIVIDUAL SING OFF BELOW.;[05] PERFORMED PERMANENT REPAIR ON STRINGER 23L LOCATED BS540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. MATERIAL USED: ALUMINUM SHEET 7075-T0 0.036? PO: 2021 131796 ( CONVERTER TO 7075 T6); CHANNEL BAC1493-249 PO: 2021 147833 ; ANGLES (2E/A) BAC1493-659 PO: 2021 149606 SEE INDIVIDUAL SING OFF BELOW. COMPLETED RII

Part: SUPPORT — CRACKED (FWD CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CRACK SUPPORT ZEE LOCATED BS500A STR26L AND WL156 AT FWD CARGO COMPARTMENT 2022-284007 / [01] INSTALLED SUPPORT ZEE AND FASTENERS LOC. BS400 AT 500D STR26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 DWG 143A7500 REV A <BR>SEE INDIVIDUAL SINGNOFF BELOW;[02] INSTALLED SUPPORT ZEE AND FASTENERS LOC. BS400 AT 500D STR26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 DWG 143A7500 REV A <BR>SEE INDIVIDUAL SINGNOFF BELOW

Part: INTERCOSTAL — CORRODED (AFT CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 787 AND BS 767 S-25R WL 156 APPROX AT AFT CARGO COMPARTMENT 2022-283991 / [01] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 787 AND BS 767 S-25R WL 156 APPROX AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02; SRM 51-10-02 STEP 9 AND DWG 146A0081 SHEET 31 REV -;[02] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 787 AND BS 767 S-25R WL 156 APPROX AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02; SRM 51-10-02 STEP 9 AND DWG 146A0081 SHEET 31 REV -

Part: STRAP — CORRODED (AFT CARGO) · airframe 53,726 hrs · 32,221 cycles

CORROSION STRAP LOCATED BS 727D BETWEEN S-25R AND S-25L WL156 AT AFT CARGO COMPARTMENT 2022-283999 / [01] REPLACED STRAP LOCATED BS 727D BETWEEN S-25R AND S-25L WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND 51-10-02.;[02] REPLACED STRAP LOCATED BS 727D BETWEEN S-25R AND S-25L WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND 51-10-02.

Part: FRAME — CRACKED (FWD GALLEY) · airframe 53,726 hrs · 32,221 cycles

CRACK FRAME ON BS 312 AT LEVEL STR 5L FWD GALLEY AND LAV 2022-283988 / [01] PERFORMED REPAIR FRAME ON BS 312 AT LEVEL STR 5L FWD GALLEY AND LAV IAW EA # M-22-153-01244 BARCODE TTG8Q00CKYM0 SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: PLATE — CORRODED (AFT CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CORROSION CHANNEL PLATE LOCATED BS 887 BETWEEN S-26L AND S-25R WL 156 AFT CARGO COMPARTMENT 2022-283990 / [01] REPLACED CHANNEL PLATE LOCATED BS 887 BETWEEN S-26L AND S-25R WL 156 AFT CARGO COMPARTMENT IAW B737-700 51-40-02 AND 51-10-02;[02] CORRECTED STEP 1<BR>REPLACED CHANNEL PLATE LOCATED BS 887 BETWEEN S-26L AND S-25R WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02; SEE INDIVIDUAL SIGNOFF BELOW;[03] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 747 AND BS 727D S-25R WL 156 APPROX AT AFT CARGO COMPARTMENT 2022-283993 / [01] REPAIRED SUPPORT ZEE LOCATED LOCATED BETWEEN BS 727 AND BS 767 S-25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5;[02] COMPLETE TASK CERTIFIED RII

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 807 AND BS 727 S-25L WL 156 AT AFT CARGO COMPARTMENT 2022-283994 / [01] REPAIRED SUPPORT ZEE IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5 LOCATED BETWEEN BS727 TO BS847 S-25L WL 156 AT AFT CARGO COMPARTMENT SEE INDIVIDUAL SINGOFF BELOW;[02] COMPLETE TASK CERTIFIED RII

Part: SKIN — CORRODED (FUSELAGE) · airframe 53,726 hrs · 32,221 cycles

CORROSION EXTERNAL SKIN LOCATED BETWEEN BS 1016 AND BS 1040 BETWEEN S-3R AND S-3L WL308.5 AT UPPER FUSELAGE 2022-283998 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 60007161486; CAL DUE DATE: 06-DEC-22;[02] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 130066401; CAL DUE DATE: 17-JUN-22;[03] REMOVED CORROSION ON EXTERNAL SKIN LOCATED BETWEEN BS 1016 AND BS 1040 BETWEEN S-3R AND S-3L WL308.5 AT UPPER FUSELAGE IAW B737-700 SRM 51-10-02-0G-0; AND EVALUATED REWORKED AREA POINT 1; POINT 2; POINT 4 AND POINT 5 FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH 4.C.(2)(A) FIGURE 103 DETAIL D EXCEPT POINT 3 THAT IS OUT LIMITS MUST BE REPAIRED; REPAIR DOCUMENTED ON TTG8Q00CNEGC.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[04] CORRECTED STEP 3<BR>REMOVED CORROSION ON EXTERNAL SKIN LOCATED BETWEEN BS 1016 AND BS 1040 BETWEEN S-3R AND S-3L WL308.5 AT UPPER FUSELAGE IAW B737-700 SRM 51-10-02-0G-0; AND EVALUATED REWORKED AREA POINT 1; POINT 2; POINT 4 AND POINT 5 FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH 4.C.(2)(A) FIGURE 103 DETAIL D; NO FURTHER ACTION OR INSPECTION REQUIRED. EXCEPT POINT 3 THAT IS OUT LIMITS MUST BE REPAIRED; REPAIR DOCUMENTED ON TTG8Q00CNEGC.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[05] CERTIFIED STEP 4 COMPLETED

Part: CHANNEL — CRACKED (AFT CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CRACK CHANNEL SUPPORT LOCATED BETWEEN BS 907 AND BS 927 BETWEEN S-25R AND S-27R WL 156 APPROX AFT CARGO COMPARTMENT 2022-283989 / [01] REPLACED CHANNEL SUPPORT LOCATED BETWEEN BS 907 AND BS 927 BETWEEN S-25R AND S-27R WL 156 APPROX AFT CARGO COMPARTMENT IAW B737-700 SRM-51-10-02 ITEM 9 AND DWG:147A7221 SHEET:24 REV:;[02] COMPLETE TASK CERTIFIED RII

Part: SKIN — DELAMINATED (R/H WING) · airframe 53,726 hrs · 32,221 cycles

DELAMINATED WINGLET LOWER SKIN LOC. RIB STA 0 AT RT WING 2022-284000. ACCOMPLISED EA# 22-157-01566 (COMPONENT - AEM - REPAIR - RH WING - BLENDED WINGLET - LWR SKIN INSTL AT RIB STA 0 - DELAMINATION. P/N 737-0010-36; S/N C0021.) ON WINGLET RT WING AND IS DOCUMENTED TTG8Q00CUCB4; ACCOMPLISHED EA# 22-157-01566 (COMPONENT - AEM - REPAIR - RH WING - BLENDED WINGLET - LWR SKIN INSTL AT RIB STA 0 - DELAMINATION. P/N 737-0010-36; S/N C0021.) ON WINGLET RT WING AND IS DOCUMENTED TTG8Q00CUCB4. COMPLETED WIP: #22-157-01566 WIP1 (COMPONENT - AEM - REPAIR - RH WING - BLENDED WINGLET - LWR SKIN INSTL AT RIB STA 0 - DELAMINATION. P/N 737-0010-36; S/N C0021.) ON WINGLET RT WING AND IS DOCUMENTED TTG8Q00CUCB4.

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CORROSION FLOOR STRUCTURE WEB LOCATED BETWEEN BS 767 AND BS 747 S-25R WL156 APPROX AT AFT CARGO COMPARTMENT 2022-283992 / [01] REPLACED WEB ON FLOOR STRUCTURE LOCATED BETWEEN BS 767 AND BS 747 S-25R WL156 APPROX AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02-0G-0 AND DWG #146A7500 SHEET 88 REV: A.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED WEB ON FLOOR STRUCTURE LOCATED BETWEEN BS 767 AND BS 747 S-25R WL156 APPROX AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02-0G-0 AND DWG #146A7500 SHEET 88 REV: A. <BR>SEE INDIVIDUAL SIGN OFFS BELOW. COMPLETED

Part: SEAT TRACK — CRACKED (PAX CABIN) · airframe 53,726 hrs · 32,221 cycles

CRACK SEAT TRACK STA 727B LBL 24.75 FASTENER B AT PASSENGER CABIN (1 EA) 2022-283970 / [01] INSTALLED FASTENER ON SEAT TRACK STA 727B LBL 24.75 FASTENER B AT PASSENGER CABIN (1 EA) IAW B737-700 SRM 51-40-02 SEE INDIVIDUAL SIGN OFFS BELOW.;[02] STEP 1 CORRECTED <BR>INSTALLED FASTENER ON SEAT TRACK STA 727B LBL 24.75 FASTENER B AT PASSENGER CABIN (1 EA) IAW B737-700 SRM 51-40-02 AND SOPM 20-50-19 SEE INDIVIDUAL SIGN OFFS BELOW.;[03] STEP 1 AND 2 CORRECTED <BR>INSTALLED FASTENER ON SEAT TRACK STA 727B LBL 24.75 FASTENER B AT PASSENGER CABIN (1 EA) IAW WIP1 2-153-01601 AND EA 2-153-01601 AND SRM B737-700 51-40-02<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[04] INSTALLED FASTENER ON SEAT TRACK STA 727B LBL 24.75 FASTENER B AT PASSENGER CABIN (1 EA) IAW WIP1 2-153-01601 AND EA 2-153-01601 AND SRM B737-700 51-40-02 <BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: RIB — CORRODED (RH WING) · airframe 53,726 hrs · 32,221 cycles

CORROSION RIB 27 OUTBOARD FACE AT RT WING 2022-283969 / [01] TOOL USED PN NORTEC 500D SN N500X1693P030456 DUE DATE 26-JAN-23;[02] PERFORMED REPAIR ON RIB 27 OUTBOARD FACE AT RT WING IAW EA 22-157-0606 AND WIP1 22-157-01606-WIP1. SEE INDIVIDUAL SIGNOFF BELOW;[03] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CRACK GUSSET LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT 2022-283951 / [01] REMOVED GUSSET AND FASTENER LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SING OFFS.;[02] CORRECTED STEP 1 <BR>REMOVED GUSSET AND FASTENER LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SIGNOFFS BELOW;[03] REMOVED GUSSET AND FASTENER LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SIGN OFFS BELOW. CERTIFIED RII;[04] REMOVED GUSSET AND FASTENER LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SIGN OFFS BELOW.

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2022-283950 / [01] REMOVED GUSSET AND FASTENER LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SING OFFS.;[02] REMOVED GUSSET AND FASTENER LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SING OFFS. CERTIFIED RII;[03] REMOVED GUSSET AND FASTENER LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SING OFFS.;[04] REMOVED GUSSET AND FASTENER LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SIGN OFFS.;[05] CORRECTED STEP.<BR>REMOVED GUSSET AND FASTENER LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SIGN OFFS. CERTIFIED RII

Part: ANGLE — CRACKED (FWD CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CRACK ANGLE - CLIP LOCATED BS400 AFT FACE AND STR26L FWD CARGO COMPARTMENT 2022-283957 / [01] REPLACED ANGLE-CLIP LOCATED BS400 AFT FACE AND STR26L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM:9 AND DWG:143A7505 SHEET:81 REV:-.;[02] REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS400 AFT FACE AND STR26L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM:9 AND DWG:143A7505 SHEET:81 REV:-. SEE INDIVIDUAL SIGNS OFF BELOW. ITEM RII

Part: ANGLE — CRACKED (FWD CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

CRACK ANGLE - CLIP LOCATED BS500C FWD FACE AND STR26L FWD CARGO COMPARTMENT 2022-283956 / [01] REPLACED ANGLE CLIP LOCATED BS500C FWD FACE AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE CLIP LOCATED BS500C FWD FACE AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED ANGLE CLIP LOCATED BS500C FWD FACE AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9. SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT BRACKET — CRACKED (PAX CABIN) · airframe 53,726 hrs · 32,221 cycles

CRACK SUPPORT BRACKET ASSY LOCATED BS540 AND LBL24.75 TO RBL45.5 AT PASSENGER CABIN (3 EA) 2022-283935 / [01] REPLACED SUPPORT BRACKET ASSY (3E/A) LOCATED BS540 AND LBL24.75 TO RBL 45.5 AT PASSENGER CABIN IAW SRM B737-700 51-40-02 AND SRM B737-700 51-10-02 ITEM 9 SEE INDIVIDUAL SIGNED STEPS BELOW;[02] REPLACED SUPPORT BRACKET ASSY (3E/A) LOCATED BS540 AND LBL24.75 TO RBL 45.5 AT PASSENGER CABIN IAW SRM B737-700 51-40-02 AND SRM B737-700 51-10-02 ITEM 9 SEE INDIVIDUAL SIGNED STEPS BELOW

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 53,726 hrs · 32,221 cycles

CRACK ANGLE LOCATED BS695 AND RBL24.75 AT CENTER WING BOX 2022-283938 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[02] REPLACED ANGLE LOCATED BS695 AND RBL24.75 AT CENTER WING BOX IAW B737-700 DWG 273A9110 REV:A <BR>SEE INDIVIDUAL SING OFFS.;[03] REPLACED ANGLE LOCATED BS695 AND RBL24.75 AT CENTER WING BOX IAW B737-700 DWG 273A9110 REV:A <BR>SEE INDIVIDUAL SING OFFS. AS RII

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 53,726 hrs · 32,221 cycles

CRACK ANGLE LOCATED BS695 AND LBL24.75 AT CENTER WING BOX 2022-283936 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[02] REPLACED ANGLE LOCATED BS695 AND LBL24.75 AT CENTER WING BOX IAW B737-700 DWG 273A9110 REV:A SEE INDIVIDUAL SING OFFS.;[03] REPLACED ANGLE LOCATED BS695 AND LBL24.75 AT CENTER WING BOX IAW B737-700 DWG 273A9110 REV:A SEE INDIVIDUAL SING OFFS. AS RII

Part: FITTING — CORRODED (FUSELAGE) · airframe 53,726 hrs · 32,221 cycles

CORROSION ON FITTING OF WASTE DOOR PANEL 145AL LBL 28 WL 156 LOWER FUSELAGE (2 E/A) 2022-283939 / [01] REPLACED FITTING OF WASTE DOOR PANEL 145AL LBL 28 WL 156 LOWER FUSELAGE (2 E/A) IAW B737-700 SRM 51-40-02 AND 51-10-02 .;[02] REPLACED FITTING OF WASTE DOOR PANEL 145AL LBL 28 WL 156 LOWER FUSELAGE (2 E/A) IAW B737-700 SRM 51-40-02 AND 51-10-02 .

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 53,726 hrs · 32,221 cycles

CRACK ANGLE LOCATED BS695 AND BL0 AT CENTER WING BOX 2022-283937 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23.;[02] REPLACED ANGLE LOCATED BS695 AND BL0 AT CENTER WING BOX IAW B737-700 DWG 273A9110 SHEET:6 REV:A <BR>SEE INDIVIDUAL SING OFFS.;[03] STEP 2 CORRECTED <BR>REPLACED ANGLE LOCATED BS695 AND BL0 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND DWG 273A9110 SHEET:6 REV:A <BR>SEE INDIVIDUAL SING OFFS.;[04] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: HANDLE — MISSING (FWD CARGO BAY) · airframe 53,726 hrs · 32,221 cycles

MISSING STUD HANDLE DOOR FWD CARGO COMPARTMENT 2022-283837 / [01] INSTALLED STUD HANDLE DOOR FWD CARGO COMPARTMENT IAW B737-700 IAW 51-10-02.;[02] INSTALLED STUD HANDLE DOOR FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02.;[03] CORRECTED STEP 1 AND 2 <BR>INSTALLED STUD HANDLE DOOR FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02.;[04] INSTALLED STUD HANDLE DOOR FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02.

Part: RETAINER SEAL — CRACKED (LH WING) · airframe 53,726 hrs · 32,221 cycles

CRACK ON RETAINER SEAL ON ACCESS PANEL 542BB LT WING. 2022-283838 / [01] REPLACED ON RETAINER SEAL ON ACCESS PANEL 542BB LT WING IAW B737-700 SRM 51-10-02;[02] CERTIFIED WORK PERFORMED

Part: WEB — CRACKED · airframe 53,726 hrs · 32,221 cycles

CUSTOMER REQUEST CRACK ON VAPOR BARRIER ( WEB) LOCATED ON BS 663 AT RBL 41 AND WL 163 LOWER FUSELAGE 2022-283870 / [01] TOOL USED CALIPER P/N 500-197-30; S/N A21041924; DUE DATE: 01-SEP-22.;[02] TOOL USED SCALE P/N CL5000; S/N AE-39087; DUE DATE: 07-JUL-22.;[03] PERFORMED AN INTERIM REPAIR ON VAPOR BARRIER ( WEB) LOCATED ON BS 663 AT RBL 41 AND WL 163 LOWER FUSELAGE AS PER B737-700 SRM 57-10-10-2R-2 REPAIR 2; PARAGRAPHS 1.A;C; 2.C. AND 6. SEE INDIVIDUAL SIGNOFFS BELOW;[04] PERFORMED AN INTERIM REPAIR ON VAPOR BARRIER ( WEB) LOCATED ON BS 663 AT RBL 41 AND WL 163 LOWER FUSELAGE AS PER B737-700 SRM 57-10-10-2R-2 REPAIR 2; PARAGRAPHS 1.A;C; 2.C. AND 6. RII VERIFIED

Part: PANEL — CRACKED (FUSELAGE) · airframe 53,726 hrs · 32,221 cycles

CRACK ACCESS PANEL 194HR BODY FAIRING AT LOWER FUSELAGE 2022-283834 / [01] TOOL USED CALIPER P/N:500-197-30 S/N:15120589 DUE DATE: 28 NOV 22.;[02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18185733 DUE DATE 16/JAN/23.;[03] TOOL USED: SCALE P/N SCA-301 S/N AE-412132 DUE DATE 14-MAR-23.;[04] TOOL USED: HOT BONDER P/N HCS9200B-AV S/N 18185733 DUE DATE: 16-JAN-23.;[05] TOOL USED: SCALE P/N SCA-301 S/N AE-412132 DUE DATE 14-MAR-23.;[06] TOOL USED SCALE PN: CL5000; SN: AE-408752; D/D: 14/MAR/23.;[07] TOOL USED: SCALE P/N SCA-301 S/N AE-412123 DUE DATE 14-MAR-23;[08] REPAIRED ACCESS PANEL 194HR BODY FAIRING AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10 SEE INDIVIDUAL SIGN OFFS BELOW.;[09] REPAIRED ACCESS PANEL 194HR BODY FAIRING AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10 SEE INDIVIDUAL SIGN OFFS BELOW

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 52,664 hrs · 31,593 cycles

WING TO BODY FAIRING PANEL 193B IS DELIMITATED ON CORNER AT HOLE LOCATION 20 TO 21; ALSO FASTENER HOLES ARE ENLARGED AT LOCATIONS 1; 3; 4; 5; 24; 25; 28; 29; 30; 31; 33 AND 34 ; WING TO ODY FAIRING PANEL 193B IS DELIMITATED ON CORNER AT HOLE LOCATION 20 TO 21; ALSO FASTENER HOLES ARE ENLARGED AT LOCATIONS 1; 3; 4; 5; 24; 25; 28; 29; 30; 31; 33 AND 34 / [01] REPLACED 193B PANEL IAW 5351-I-14108-NG

Part: PANEL — ELONGATED (FUSELAGE) · airframe 52,212 hrs · 31,332 cycles

WING TO BODY PANEL 194E HAS 3(EA) FASTENER HOLES DELAMINATED AND 4(EA) FASTENER HOLES ELONGATED ; / [01] REMOVED AND REPLACED PANEL PER SRM 51-40-02

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 52,212 hrs · 31,332 cycles

WING TO BODY PANEL 193D HAS 1(EA) FASTENER DELAMINATED. ; / [01] REMOVED AND REPLACED PANEL PER SRM 51-40-02

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 49,250 hrs · 29,555 cycles

AFT LT EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED, PER AMM.33-51-06.

Part: SLIDER — BROKEN (HORIZONTAL STAB) · airframe 48,392 hrs · 29,038 cycles

PANEL 343AT SLIDER CLOSE OUT; FOR RIGHT HORZ STAB; AIRCRAFT SIDE BROKEN AND THE SLIDING SEAL LIFTS INTO THE SLIP STREAM. / REPLACED HORIZONTAL SLIDER CLOSEOUT R/H UPPER POSITION PER SRM 51-40-02

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 48,392 hrs · 29,038 cycles

CABIN FLOOR PANEL 241EF DAMAGED. / REPAIRED DAMAGED AREA PER SRM 53-00-50-2R-11.

Part: ANGLE — CRACKED (RT WING) · airframe 48,392 hrs · 29,038 cycles

RT WING LOWER T/E PANEL #651FB HAS CRACKED ANGLE. (M) / REMOVED AND REPLACED ANGLE PER SRM 51-10-02 AND SRM 51-40-02

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 48,392 hrs · 29,038 cycles

F/O'S AFT INBD SEAT TRACK HAS SEAT ADJ HOLES ELONGATED / REMOVED AND REPLACED SEAT TRACK AS PER AMM 25-11-11

Part: SEAT TRACK — DAMAGED (FLIGHT DECK) · airframe 48,392 hrs · 29,038 cycles

CAPTS AFT OUTBD SEAT TRACK HAS SEAT ADJ HOLES ELONGATED / REMOVED AND INSTALLED SERVICEABLE CAPT'S AFT. OUTBRD SEAT TRACK PER AMM 25-11-11.

Part: SEAT TRACK — ELONGATED (COCKPIT) · airframe 48,392 hrs · 29,038 cycles

F/O'S AFT OUTBD SEAT TRACK HAS SEAT ADJ HOLES ELONGATED / REMOVED AND REPLACED SEAT TRACK AS PER AMM 25-11-11

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 48,392 hrs · 29,038 cycles

R/H HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY #4 (STAB STA. 120.30) HAS A CRACK IN LOWER FLANGE OF 1ST STIFFENER FROM FRONT. / ACCOMPLISHED REPAIR IAW SRM 55-10-06-2R-4.

Part: SEAT TRACK — ELONGATED (FLIGHT DECK) · airframe 48,392 hrs · 29,038 cycles

CAPTS AFT INBD SEAT TRACK HAS SEAT ADJ HOLES ELONGATED. REMOVED AND INSTALLED SERVICEABLE CAPT'S AFT. INBOARD SEAT TRACK PER AMM 25-11-11.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 48,392 hrs · 29,038 cycles

R/H HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY #4 (STAB STA. 120.30) HAS A CRACK IN LOWER FLANGE OF 4TH STIFFENER FROM FRONT. / ACCOMPLISHED REPAIR IAW SRM 55-10-06-2R-4.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 48,392 hrs · 29,038 cycles

CABIN FLOOR BOARD 242AF DENTED IN SEVERAL PLACES AND PULLED/MISSING FIBERS / REMOVED AND REPLACED CABIN FLOOR BOARD 242AF PER AMM 53-21-00. REFERENCE G736160.

Part: HINGE — CHAFED (L1 DOOR) · airframe 48,392 hrs · 29,038 cycles

FWD ENTRY DOOR UPPER HINGE LOWER RADIUS LINK CHAFED ON FUSELAGE CUTOUT. REMOVED AND REPLACED HINGE LOWER AND UPPER RADIUS LINKS AND SHIMMED IAW AMM 52-11-11, AND AMM 52-11-21.

Part: FLOORBOARD — PULLED (CABIN) · airframe 48,392 hrs · 29,038 cycles

CABIN FLOOR BOARD 241BF DENTED IN SEVERAL PLACES AND PULLED FIBERS / REMOVED AND REPLACED CABIN FLOOR BOARD 241BF PER AMM 53-21-00.

Part: SEAT TRACK — CORRODED (BS 727D) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #4 @ STA 727D / SEAT TRACK TO BE REPLACED ON NRC # G735913.

Part: SEAT TRACK — CORRODED (BS 618) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #4 @ STA 618 / SEAT TRACK TO BE REPLACED ON NRC # G735910.

Part: SEAT TRACK — CORRODED (BS 700) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #2 @ STA 700 / REMOVED AND REPLACED #2 SEAT TRACK FROM STA.540 TO STA. 727B ( P/N # 144A5350-3 ) PER SRM 51-40-02 .

Part: SEAT TRACK — CORRODED (BS 600) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #4 @ STA 600 / SEAT TRACK TO BE REPLACED ON NRC # G735910.

Part: SEAT TRACK — CORRODED (BS 727B) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #4 @ STA 727B+6 / SEAT TRACK TO BE REPLACED ON NRC # G735913.

Part: SEAT TRACK — CORRODED (BS 800) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #4 @ STA 800 / SEAT TRACK TO BE REPLACED ON NRC # G735913.

Part: SEAT TRACK — CORRODED (BS 580) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #2 @ STA 580 / REMOVED AND REPLACED #2 SEAT TRACK FROM STA.540 TO STA. 727B ( P/N # 144A5350-3 ) PER SRM 51-40-02 .

Part: SEAT TRACK — CORRODED (BS 580) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK NR 4 AT BS 580, THE SEAT TRACK TO BE REPLACED ON NRC # G735910.

Part: SEAT TRACK — CORRODED (BS 870) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #4 @ STA 870 / SEAT TRACK TO BE REPLACED ON NRC # G735913.

Part: SEAT TRACK — CORRODED (BS 827) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #4 @ STA 827 / SEAT TRACK TO BE REPLACED ON NRC # G735913.

Part: SEAT TRACK — CORRODED (BS 685) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #4 @ STA 685 / SEAT TRACK TO BE REPLACED ON NRC # G735910.

Part: SEAT TRACK — CORRODED (BS 767) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #4 @ STA 767 / SEAT TRACK TO BE REPLACED ON NRC # G735913.

Part: SEAT TRACK — CORRODED (BS 740) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #4 @ STA 740 / SEAT TRACK TO BE REPLACED ON NRC # G735913.

Part: SEAT TRACK — CORRODED (BS 860) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #4 @ STA 860 / SEAT TRACK TO BE REPLACED ON NRC # G735913.

Part: SEAT TRACK — CORRODED (BS 727E) · airframe 48,392 hrs · 29,038 cycles

CORROSION ON CABIN SEAT TRACK #4 @ STA 727E+10 / SEAT TRACK TO BE REPLACED ON NRC # G735913.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 48,392 hrs · 29,038 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY NR 4, STAB STA 120.30, HAD A CRACK IN LOWER FLANGE OF THE THIRD STIFFENER FROM FRONT. REPAIRED THE RIB STIFFENER IAW SRM 55-10-09-2R-4.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 48,392 hrs · 29,038 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY NR 4, STAB STA. 120.30, HAD A CRACK IN THE LOWER FLANGE OF THE SECOND STIFFENER FROM FRONT. REPAIRED THE RIB STIFFENER IAW SRM 55-10-09-2R-4.,

Part: LANDING — GOUGED (PRESSURE SEAL) · airframe 48,392 hrs · 29,038 cycles

AFT CARGO DOOR UPPER PRESSURE SEAL LANDING WAS GOUGED AND DENTED, APPROXIMATELY 19 INCHES FROM FRONT OF THE DOOR. FOUND DURING A POST REPAIR INSPECTION.

Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 48,392 hrs · 29,038 cycles

FLIGHT COMPARTMENT FLOOR DENTED UNDER FIRST OBSERVERS SEAT. REPAIRED IAW EA -A53-33179.

Part: THRESHOLD — CRACKED (FWD CARGO) · airframe 48,392 hrs · 29,038 cycles

FWD CARGO FWD THRESHOLD CORNER CRACKED / REMOVED AND REPLACED FWD CARGO FWD THRESHOLD CORNER PER AMM 53-11-02.

Part: THRESHOLD — CRACKED (FWD CARGO) · airframe 48,392 hrs · 29,038 cycles

FWD CARGO AFT THRESHOLD CORNER CRACKED / REMOVED AND REPLACED FWD CARGO AFT THRESHOLD CORNER PER AMM 53-11-02.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 47,528 hrs · 28,468 cycles

RUDDER WEIGHT HAS CORROSION / REMOVED AND REPLACED RUDDER WEIGHT PER CMM 55-40-09

Part: SLIDE — FAULTY (L1 DOOR) · airframe 46,851 hrs · 28,044 cycles

L1 DOOR GIRT BAR DIFFICULT TO ARM / DISARM. / R&R SLIDE IAW MT.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 46,598 hrs · 27,880 cycles

L1 DOOR SLIDE PACK MISALIGNED AND DIFFICULT TO ARM/DISARM. / REPOSITIONED GIRT BAR PER MT.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 44,874 hrs · 26,743 cycles

MID CABIN EMERGENCY EXIT SIGN LOOSE. R&R SIGN PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,405 hrs · 26,430 cycles

AFT R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 43,775 hrs · 26,016 cycles

FWD BULKHEAD EMERGENCY EXIT SIGN LOOSE. R&R SIGN ASSY PER MM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 42,012 hrs · 24,866 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS OUT OF POSITION. REPAIRED LENS IAW AMM & SIP.

Part: FASTENER — CORRODED (EMERGENCY EXIT) · airframe 42,012 hrs · 24,866 cycles

RT OVERWING EMERGENCY LOWER SILL LATCH STOP (FOR HINGED CLOSEOUT PANEL HOLD-OPEN TOGGLE LATCH). R&R FASTENERS IAW SRM AND DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,012 hrs · 24,866 cycles

LT HORIZONTAL STABILIZER RIB AT STA 120.3 FORWARD STIFFENER CRACKED. R&R RIB IAW DWG AND SRM.

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

PANEL 193AR HAS A DELAMINATION ON THE INNER SKIN LOWER AREA MID SPAN / DELAMINATION ON THE SKIN OF PANEL 193AR WAS REPAIRED IAW SRM 51-70-05-2R-4.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520, LBL 1. R&R INTERCOSTAL PER DWG AND SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

AFT CARGO BAY L ANGLE UNDER THE SHIELD FORWARD OF THE CARGO DOOR CORRODED BETWEEN BS 767 TO BS 787, RBL 23. R&R L ANGLE PER SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, LBL 14. R&R INTERCOSTAL PER DWG AND SRM.

Part: SEAL — CRACKED (RH HOR STAB) · airframe 42,012 hrs · 24,866 cycles

RT HORIZ. STAB UPPER FWD SLIDE SEAL IS CRACKED. / REMOVED AND REPLACED RT. HORIZONTAL STAB. UPPER FWD SLIDE SEAL AND CHECKS GOOD IAW MM 53-31-31-000-802 AND MM 53-31-31-400-802

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, LBL 1. R&R INTERCOSTAL PER DWG AND SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, RBL 8.283. R&R INTERCOSTAL PER DWG AND SRM.

Part: SPLICE — CORRODED (FLOOR PANEL) · airframe 42,012 hrs · 24,866 cycles

AFT CARGO BAY FLOOR PANEL SPLICE CORRODED AT BS. 887, BETWEEN RBL 10 TO LBL 10. R&R SPLICE IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

AFT CARGO BAY FORWARD OF THE CARGO DOOR SHIELD CORRODED BETWEEN BS 767 TO BS 787, RBL 23. R&R SHIELD PER SRM & DWG.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

AFT CARGO BAY FLOOR SUPPORT FITTING CRACKED AT BS 947+1, LBL 12.5. R&R FITTING IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 42,012 hrs · 24,866 cycles

RT HORIZONTAL STABILIZER RIB AT STA 129.5 2ND AND 3RD VERTICAL STIFFENERS CRACKED. REPAIRED RIB IAW SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

CABIN FLOOR PANEL 232SF FWD I/B CORNER DELAMINATED / REPAIRED DAMAGE TO FWD I/B CORNER OF FLOOR PANEL 232SF IAW SRM 53-00-50-2R-10. 56749U 12JUN18

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,012 hrs · 24,866 cycles

LT HORIZONTAL STABILIZER RIB AT STA 120.3 2ND THRU 4TH VERTICAL STIFFENERS CRACKED. REPAIRED RIB IAW SRM.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 42,012 hrs · 24,866 cycles

AFT CARGO BAY; FLOOR PANEL SPLICE AT BS773 HAS AREAS OF CORROSION RBL10 TO LBL10 / RECEIVED NEW ACB FLOOR PANEL SPLICE BS 773 ON PO # 681622

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET PER SRM & DWG.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 42,012 hrs · 24,866 cycles

AFT CARGO BAY TIE DOWN TRACK CRACKED AT BS 767, RBL 14. R&R TRACK PER SRM & DWG.

Part: FLOOR PANEL — BROKEN (FWD CABIN) · airframe 42,012 hrs · 24,866 cycles

FWD CABIN FLOOR PANEL 221GF HAS BROKEN FWD O/B CORNER / REPAIRED BROKEN FWD O/B CORNE ON FWD CABIN FLOOR PANEL 221GF IAW SRM 53-00-50-2R-9. 7066U 06/12/18

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30.5. R&R INTERCOSTAL IAW DWG AND SRM.

Part: PANEL — DEBONDED · airframe 42,012 hrs · 24,866 cycles

PANEL 193B HAS DISBONDS ON THE INNER SURFACE SKIN / REPAIRED DISBONDS ON INNER SURFACE OF PANEL 193B IAW SRM 53-40-70 SRM 53-40-70-2R-1; SRM 51-70-05-2R-2; SRM 51-70-05-2R-11

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

R1 DOOR MOPSILL SCUFF PLATE ATTACH ANGLE CORRODED BETWEEN BS 304 TO BS 326, RT WL 209. R&R ANGLE IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

R1 DOOR MOPSILL CORRODED BETWEEN BS 294.5 TO BS 336, WL 209. R&R MOPSILL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, BL 45.5. R&R INTERCOSTAL IAW DWG AND SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 45.5. R&R INTERCOSTAL PER SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

MOPSILL ATTACH ANGLE CRACKED BETWEEN BS 290 TO BS 294, RBL 53. R&R ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, BL 0. R&R INTERCOSTAL IAW DWG AND SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

R2 DOOR MOPSILL CORRODED BETWEEN BS 947 TO BS 990, WL 208. R&R MOPSILL IAW SRM & DWG.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 42,012 hrs · 24,866 cycles

KEEL BEAM PANEL T FITTING CRACKED AT BS 551, RBL 16. R&R T FITTING PER SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 42,012 hrs · 24,866 cycles

AFT CARGO BAY; FWD CORNER SCUFF PLATE IS CRACKED / AFT CARGO BAY; FWD CORNER SCUFF PLATE WAS REPAIRED PER EA 1-A53-2076.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 42,012 hrs · 24,866 cycles

BULKHEAD VERTICAL WEB CRACKED AT BS 663, LBL 42. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 42,012 hrs · 24,866 cycles

#2 SLAT LE NOSE SKIN CRACKED AT ACTUATOR RIB / REPAIRED #2 SEAT LOWER BULL NOSE SKIN COMMON TO ACTUATOR ATTACHMNT RIB PER SRM 57-42-01-2R-8.

Part: SKIN — CRACKED (RT WING) · airframe 42,012 hrs · 24,866 cycles

#8 SLAT LE NOSE SKIN CRACKED AT ACTUATOR RIB / REPAIRED DAMAGE TO #8 SLAT L/E NOSE SKIN AT ACTUATOR RIB IAW SOPM 20-50-01; SRM 51-40-02-0G-0; AND SRM 57-42-01-2R8

Part: BEAM — CRACKED (R1 DOOR) · airframe 42,012 hrs · 24,866 cycles

R1 DOOR NR 4 BEAM CRACKED. REPAIRED NR 4 BEAM PER MM.

Part: SKIN — CRACKED (RT WING) · airframe 42,012 hrs · 24,866 cycles

#6 SLAT LE NOSE SKIN CRACKED AT ACTUATOR RIB / REPAIRED DAMAGED NOSE SKIN AT ACTUATOR RIB ON #6 SLAT L/E IAW SRM 51-40-02-0G-0; SRM 57-43-01-2R8; AND SOPM 20-50-01

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 40,560 hrs · 23,937 cycles

LT WHEEL WELL BULKHEAD CRACKED AT BS 663, LBL 42. REPAIRED BULKHEAD IAW EA.

Part: FUSE — INOPERATIVE (CABIN) · airframe 39,546 hrs · 23,286 cycles

FORWARD EMERGENCY LIGHT JUST AFT OF L1 DOOR INOP. R&R FUSE PER AMM.

Part: BRACKET — CRACKED (LOWER EXT FUSELA) · airframe 39,022 hrs · 22,973 cycles

LOWER FUSELAGE KEEL BEAM PANEL 192E SUPPORT BRACKET IS CRACKED / REPLACED SUPPORT BRACKET TO KEEL BEAM PANEL 192E PER SRM 51-40-02.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 39,022 hrs · 22,973 cycles

LEFT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / R&R'D L/H HORIZONTAL UPPER FWD SLIDING SEAL REF AMM 53-31-31.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 39,022 hrs · 22,973 cycles

EXTERNAL POWER DOOR FRAME DOUBLER CRACKED. REPAIRED DOUBLER PER SRM.

Part: BRACKET — CRACKED (LOWER EXT FUSELA) · airframe 39,022 hrs · 22,973 cycles

R/H WING TO BODY FAIRING 192AR AFT CENTER SUPPORT BRACKET IS CRACKED / REMOVED AND REPLACED BRACKET PER SRM51-40-02

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 39,022 hrs · 22,973 cycles

RIGHT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / R&R'D R/H HORIZONTAL UPPER FWD SLIDING SEAL REF AMM 53-31-31.

Part: GIRT BAR — LOOSE (R1 DOOR SLIDE) · airframe 38,152 hrs · 22,448 cycles

R1 DOOR SLIDE GIRT BAR LOOSE. R & R THE SLIDE IAW MT.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,304 hrs · 20,689 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED ALONG INBOARD EDGE OF RIB STA 184.70, 9.5" FORWARD OF AFT EDGE OF SKIN. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 34,710 hrs · 20,321 cycles

RIGHT HORIZONTAL STABILIZER LOWER INTER SPAR SKIN CRACKED AT STAB STATION 129.5, 25" FROM FWD SPAR. REPAIRED SKIN IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 34,710 hrs · 20,321 cycles

RIGHT EMER BATTERIES FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 34,710 hrs · 20,321 cycles

LEFT EMER BATTERIES FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 33,108 hrs · 19,423 cycles

R2 DOOR EMER EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,519 hrs · 19,062 cycles

EMERGENCY BATTERY PACKS FAILED CAPACITY TEST AT M01673. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,519 hrs · 19,062 cycles

EMERGENCY BATTERY PACKS FAILED CAPACITY TEST AT M01672. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,519 hrs · 19,062 cycles

EMERGENCY BATTERY PACKS FAILED CAPACITY TEST AT M01675. R & R BATTERY PACK IAW AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 29,890 hrs · 17,555 cycles

R1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 28,441 hrs · 16,703 cycles

R1 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: COVER — MISSING (EXIT SIGN) · airframe 28,417 hrs · 16,688 cycles

RIGHT OVERWING EMER EXIT SIGN COVER MISSING. INSTALLED COVER IAW MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

Z ANGLE CORRODED AT STATION 312, WL 208 BELOW THRESHOLD PLATE. R & R ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

INTERCOSTAL CRACKED AT STATION 344 TO 360, BL 0. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

INTERCOSTAL CRACKED AT STATION 294.5 TO 312, RBL 16. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

INTERCOSTAL CRACKED AT STATION 312 TO 326, RBL 31.60. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

INTERCOSTAL CRACKED AT STATION 317, RBL 15. R & R INTERCOSTAL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

FLOOR SUPPORT BEAM CORRODED AT STATION 321, RBL 10. R & R SUPPORT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

INTERCOSTAL CRACKED AT STATION 335, LBL 34. R & R INTERCOSTAL IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

FLOOR SUPPORT BEAM CORRODED AT STATION 303, RBL 10. R & R SUPPORT IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

Z ANGLE CRACKED AT STATION 302 BELOW L1 DOOR , WL 208. R & R ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

INTERCOSTAL CRACKED AT STATION 295, RBL 15. R & R INTERCOSTAL IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

FORWARD CARGO DOOR THRESHOLD WEB CORRODED AT STATION 481, RBL 28. R & R WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

FRAME CHORD CRACKED AT STATION 540, STRINGER 22R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

FRAME CHORD CRACKED AT STATION 540, LT SIDE OF BULKHEAD. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,363 hrs · 16,655 cycles

FRAME CHORD CRACKED AT STATION 540, RT SIDE OF BULKHEAD. REPAIRED FRAME IAW EA.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 28,363 hrs · 16,655 cycles

COCKPIT RT SIDE NR 1 WINDOW POST CRACKED. REPAIRED POST IAW ACO.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 28,363 hrs · 16,655 cycles

COCKPIT LT SIDE NR 1 WINDOW POST CRACKED. REPAIRED POST IAW ACO.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 28,363 hrs · 16,655 cycles

MLG BULKHEAD VERTICAL PRESS WEB CRACKED AT STATION 663, RBL 35. REPAIRED WEB IAW ACO.

Part: WINDOW — ARCED (COCKPIT) · airframe 27,171 hrs · 15,979 cycles

L1 COCKPIT WINDOW ARCED IN UPPER LT HAND CORNER. R & R WINDOW IAW MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 26,347 hrs · 15,493 cycles

R1 COCKPIT WINDOW ARCED. R &R R1 WINDOW ASSEMBLY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,697 hrs · 15,095 cycles

EXTERNAL POWER DOOR CUTOUT FWD EDGE LIP UNDER LATCH CONTACT POINT CRACKED. REPAIRED CUTOUT IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 25,496 hrs · 14,969 cycles

AFT GALLEY DOOR EXIT SIGN BROKEN. R&R SIGN ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,689 hrs · 13,305 cycles

L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: COVER — MISSING (CABIN) · airframe 22,401 hrs · 13,113 cycles

LEFT EEPLS COVER MISSING. INSTALLED COVER IAW MM.

Part: LENS — MISSING (CABIN) · airframe 21,869 hrs · 12,776 cycles

EEPLS LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 21,813 hrs · 12,742 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 21,771 hrs · 12,715 cycles

R1 DOOR EVAC SLIDE PRESSURE GAUGE OUT OF LIMIT. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 21,545 hrs · 12,585 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MT.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 21,454 hrs · 12,533 cycles

AFT CARGO DOOR WAY SUB-THRESHOLD WEB CORRODED BETWEEN BS 807 TO BS 847. REMOVED AND REPLACED SUB THRESHOLD IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 21,454 hrs · 12,533 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT STA 147.9. REPAIRED RIB IAW EA AND ER.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,454 hrs · 12,533 cycles

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

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,454 hrs · 12,533 cycles

RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 157.10. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 21,454 hrs · 12,533 cycles

LEFT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 157.10. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,454 hrs · 12,533 cycles

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

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,454 hrs · 12,533 cycles

RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED STA 147.90. REPAIRED SKIN IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 21,454 hrs · 12,533 cycles

AFT BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS 947, LBL 9. REMOVED AND REPLACED ANGLE PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 21,454 hrs · 12,533 cycles

CARGO FLOOR SUPPORT BEAM CORRODED BETWEEN BS 888 TO BS 910, RBL 13. REMOVED & REPLACED BEAM IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 21,307 hrs · 12,447 cycles

FUSELAGE SKIN CRACKED AT BS 727E +8, STR 27L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 21,307 hrs · 12,447 cycles

FUSELAGE SKIN CRACKED AT BS 747, STR 27L. REPAIRED SKIN PER EA.

Part: LENS — MISSING (CABIN) · airframe 20,667 hrs · 12,074 cycles

EMERGENCY EXIT LIGHT LENS MISSING AT ROW 12. INSTALLED LENS IAW THE MM.

Part: COVER — CRACKED (CABIN) · airframe 20,211 hrs · 11,801 cycles

EEPLS COVER CRACKED BETWEEN ROW 11 TO ROW 17 RT SIDE. REMOVED AND REPLACED TRACK COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 20,211 hrs · 11,801 cycles

EPLS COVER CRACKED BETWEEN ROW 18 TO ROW 23 RT SIDE. REMOVED AND REPLACED TRACK COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 20,935 hrs · 12,396 cycles

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

Part: COVER — MISSING (EXIT SIGN) · airframe 17,675 hrs · 10,345 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,627 hrs · 10,312 cycles

DURING SCHEDULED MV1 CHECK FOUND, EEPLS INOP BETWEEN ROW 1 TO ROW 4. RELAMPED PER MM.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 17,201 hrs · 10,061 cycles

DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN PUNCTURED AT BS 339, BETWEEN STR 15R TO STR 17R. REPAIRED SKIN PER EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 17,201 hrs · 10,061 cycles

DURING SCHEDULED OTS CHECK, FOUND RT WING T/E EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.

Part: FUEL SYS — LEAKING (NR 2 ENGINE) · airframe 16,320 hrs · 9,559 cycles

ENGINE SUTDOWN, DIVERSION, DECLARED EMERGENCY. SURGE/VIBRATION ON NR 2 ENGINE FIRE WARN LIGHT INDICATION. SHUTDOWN ENGINE. FIRE INDICATION WENT OUT AFTER FIRE HANDLE PULLED. REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: LIGHT — BROKEN (CABIN) · airframe 15,792 hrs · 9,273 cycles

R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 15,192 hrs · 8,929 cycles

OVERWING EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 15,120 hrs · 8,887 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LATCH — WORN (EVAC SLIDE) · airframe 14,671 hrs · 8,617 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH ASSY WORN. REMOVED AND REPLACED LATCH ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 14,671 hrs · 8,617 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: HOOK — LOOSE (L1 DOOR) · airframe 13,146 hrs · 7,748 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW HOOK LOOSE. SECURED HOOK PER MM.

Part: LENS — MISSING (CABIN) · airframe 12,930 hrs · 7,612 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS LENS MISSING AT ROW 11. INSTALLED LENS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 12,351 hrs · 7,272 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY LIGHTS BATTERIES FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERIES PER MM.

Part: LENS — BROKEN (CABIN) · airframe 11,909 hrs · 7,003 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 11,825 hrs · 6,947 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS COVER OUT OF POSITION AT ROW 2. SECURED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,763 hrs · 6,910 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP AT ROW 12. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,341 hrs · 6,648 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 11,309 hrs · 6,625 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM.

Part: FITTING — LOOSE (R1 DOOR) · airframe 11,244 hrs · 6,592 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW CLIPS OUT OF ADJUST. ADJUSTED CLIPS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 10,671 hrs · 6,262 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LENS — MISSING (CABIN) · airframe 10,594 hrs · 6,206 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 9,998 hrs · 5,857 cycles

EMERGENCY EXIT LIGHT BROKEN AT R2 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WIRE — UNSECURE (E&E BAY) · airframe 8,528 hrs · 4,974 cycles

AIR TURNBACK, LANDING GEAR WOULD NOT RETRACT AFTER T/O GEAR LEVER WOULD NOT GO PAST "OFF" POSITION. WHILE RAISING FLAPS GEAR WARNING HORN SOUNDED. WITH FLAPS FULLY RETRACTED, GEAR SYSTEM 100 PERCENT NORMAL. SECURED S1050 SENSOR WIRE PER MM.

Part: PSEU — FAULTY (LANDING GEAR) · airframe 8,492 hrs · 4,954 cycles

AIR TURNBACK, ON T/O LANDING GEAR WOULD NOT RETRACT NORMALLY. AFTER REFERRING TO QRH, LANDING GEAR RETRACTED NORMALLY WITH FLAPS UP. T/O WARNING HORN SOUNDED WITH GEAR IN TRANSIT AND UP UNTIL CANCELLED. REMOVED AND REPLACED PSEU AND GROUND SPOILER INTERLOCK CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 6,612 hrs · 3,844 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,894 hrs · 3,395 cycles

EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 2,690 hrs · 1,510 cycles

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