N250WN

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 62,933 hrs · 38,108 cycles

AFT ENTRY DOOR ON THE LEFT SIDE EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT ENTRY DOOR OUTER EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.

Part: SIGN — DETACHED (ZONE 200) · airframe 62,356 hrs · 37,756 cycles

FWD ENTRY EXIT/SALIDA SIGN COVER ADJACENT (OUTBOARD) OF FAS JUMPSEAT FELL OFF. RESECURED FWD ENTRY DOOR EXIT/SALIDA SIGN LENS PER AMM 33-51-01. OPS CHECK GOOD.

Part: SLIDE — DISLODGED (ZONE 800) · airframe 62,234 hrs · 37,683 cycles

FORWARD ENTRY DOOR SLIDE FELL OUT OF BOX<[01] REINSTALLED FWD ENTRY DOOR ESCAPE SLIDE IN THE COMPARTMENT AND THE COMPARTMENT ASSEMBLY PER MT 725-61-06 & AMM 25-66-01.

Part: SIGN — BROKEN (ZONE 200) · airframe 61,627 hrs · 37,316 cycles

CENTER OVERHEAD EMERGENCY EXIT SIGN IS BROKEN. <[01] CENTER OVERHEAD EMERGENCY EXIT SIGN ASSEMBLY WAS REMOVED AND REPLACED IN REF TO AMM 33-51-01. LIGHT OPS CHECKS GOOD.

Part: FLOORBEAM — CRACKED (BS 540 BL0-LBL25) · airframe 58,718 hrs · 35,496 cycles

AAI: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2024-286868<[01] REPLACED PASSENGER CABIN; FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO LBL 24.75 AND FASTENERS I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9<BR>SEE INDIVIDUAL SING OFF BELOW.;[02] REPLACED PASSENGER CABIN; FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO LBL 24.75 AND FASTENERS I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9

Part: STRAP — MISMANUFACTURED (BS 727B LBL46) · airframe 58,718 hrs · 35,496 cycles

AFT CARGO BAY SPLICE STRAP MOD HAS SHORT FASTENER INSTALLED AT BS 727B, LBL 45.5. REPLACED SHORE FASTENER ON SPLICE STRAP MOD INSTALLED AT BS 727B, LBL45.5 IAW EA 1-753-33801 AND SRM 51-40-02.

Part: FLOORBEAM — CRACKED (BS 540 BL0-RBL25) · airframe 58,718 hrs · 35,496 cycles

AAI: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75. 2024-286867<[01] REPLACED PASSENGER CABIN; FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO RBL 24.75 AND FASTENERS I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9<BR>SEE INDIVIDUAL SING OFF BELOW.;[02] REPLACED PASSENGER CABIN; FLOOR STRUCTURE SUPPORT AT STA 540; BL 0 TO RBL 24.75 AND FASTENERS I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9<BR>SEE INDIVIDUAL SING OFF BELOW.

Part: PLATE — CRACKED (LT WING TE) · airframe 58,718 hrs · 35,496 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS450 TO ORSS472 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS450 TO ORSS472 AT LT WING IAW SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW SRM 51-40-02 AND DRAWING # 115A3760 REV -.

Part: RIB — CRACKED (LT WING) · airframe 58,718 hrs · 35,496 cycles

CRACK FITTING CONTROL RIB LOCATED ORSS278 AT LT WING. PERFORMED REPAIR ON DEFLECTION CONTROL RIB AREA LT WING IAW SRM 57-51-02-2R-3 REPAIR 3 & SRM 57-51-02-2R-1 REPAIR 1.

Part: WEB — CORRODED (ZN 600 RIGHT WIN) · airframe 58,718 hrs · 35,496 cycles

CORRODED WEB, FUEL INDICATOR LOCATED INTERNAL CAVITY LE AT RT WING. PERFORMED PERMANENT REPAIR ON WEB IAW EA 24-157-01348 AND EA 24-157-01348-WIP1.

Part: ANGLE — CRACKED (LT WING TE) · airframe 58,718 hrs · 35,496 cycles

CRACK ANGLE TE LOCATED DEFLECTION CONTROL RIB AREA ORSS 275 AT LT WING. REPLACED ANGLE AND FASTENERS TRAILING EDGE LOCATED DEFLECTION CONTROL RIB IAW SRM 51-40-02; SRM 51-10-02,ITEM 9 AND DWG 115A6200 SHEET 11 REV B. MEASURE OF CRACK IS: L 1.727.

Part: WEB — CRACKED (LT WING) · airframe 58,718 hrs · 35,496 cycles

CRACK WEB TE LOCATED DEFLECTION CONTROL RIB AREA ORSS 272 AT LT WING. REPLACED WEB AND FASTENERS TRAILING EDGE LOCATED DEFLECTION CONTROL RIB AREA ORSS 272 AT LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9 & DWG 115A2512, SHEET 14, REV A. MEASURE OF CRACK IS L: 0.725.

Part: ANGLE — CRACKED (LT WING TE) · airframe 58,718 hrs · 35,496 cycles

CRACK ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB AREA ORSS269 AT LT WING. REPLACED ANGLE TRAILING EDGE LOCATED DEFLECTION CONTROL RIB AREA ORSS269 AT LT WING IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 115A2930 SH 8; REV -.

Part: ANGLE — CRACKED (RT WING TE) · airframe 58,718 hrs · 35,496 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS 267 RT WING. REPLACED ANGLE ON TRAILING EDGE LOCATED ORSS 267 IAW SRM 51-40-02;SRM 51-10-02 AND DWG 115A2930 SHEET: 8 REV. -. MEASURES OF CRACK IS : L=1.062 INCH.

Part: WEB — CRACKED (RT WING) · airframe 58,718 hrs · 35,496 cycles

CRACK WEB TRAILING EDGE LOCATED BTW ORSS261 TO ORSS275 AT RT WING. REPLACED WEB AND FASTENERS ON TRAILING EDGE LOCATED BTW ORSS261 TO ORSS275 AT RT WING IAW B737-700 SRM 51-40-02;SRM 51-10-02 AND DWG 115A 2512 SHEET 14; REV. A.

Part: CARGO TRACK — CRACKED (BS 727E) · airframe 58,718 hrs · 35,496 cycles

CRACK TRACK RBBL 13.84 LOCATED STA727E AFT CARGO COMPARTMENT 2024-286833<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[03] FAULT WAS RESOLVED ON ANOTHER FAULT SEE TTG8Q00T580W;[04] CORRECTED STEP 3 <BR>FAULT WAS RESOLVED ON ANOTHER FAULT DUE TO REPAIR WAS PERFORMED FROM BS 727D PLUS 13 INCHES TO BS 767 PLUS 10 INCHES SEE TTG8Q00T580W;[05] FAULT WAS RESOLVED ON ANOTHER FAULT DUE TO REPAIR WAS PERFORMED FROM BS 727D PLUS 13 INCHES TO BS 767 PLUS 10 INCHES SEE TTG8Q00T580W

Part: SKIN — CRACKED (LT NR 2 SLAT LE) · airframe 58,718 hrs · 35,496 cycles

CRACK LEADING EDGE SKIN SLAT 2 LOWER SURFACE AT LT WING 2024-286837<[01] ON STEP 3. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 210136503. DUE DATE: 23-MAY-24.;[02] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[03] PERFORMRD REPAIR ON LEADING EDGE SKIN SLAT 2 LOWER SURFACE AT LT WING IAW B737-700 SRM SRM 57-42-01-2R-8 REPAIR 8 SEE INDIVIDUAL SIGN OFF BELOW;[04] PERFORMED REPAIR ON LEADING EDGE SKIN SLAT 2 LOWER SURFACE AT LT WING IAW B737-700 SRM SRM 57-42-01-2R-8 REPAIR 8 SEE INDIVIDUAL SIGN OFF BELOW

Part: STRAP — DAMAGED (BS 794-807) · airframe 58,718 hrs · 35,496 cycles

ELONGATED HOLE STRAP LOCATED BTW STA 794.3 TO STA 807 RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT 2024-286832<[01] REPLACED STRAP LOCATED BTW STA 794.3 TO STA 807 RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND DWG 146A8340 SHEET: 24 REV: A.;[02] REPLACED STRAP LOCATED BTW STA 794.3 TO STA 807 RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND DWG 146A8340 SHEET: 24 REV: A.

Part: CARGO TRACK — CRACKED (BS 767) · airframe 58,718 hrs · 35,496 cycles

CRACK TRACK RBBL 13.84 LOCATED STA767 AFT CARGO COMPARTMENT 2024-286835<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[03] PERFORMED REPAIR ON TRACK RBBL 13.84 BETWEEN BS 727D + 13? TO BS 767 + 10? AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 SEE INDIVIDUAL SIGNOFFS BELOW;[04] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: ANGLE — CRACKED (BS 948 LBL 10) · airframe 58,718 hrs · 35,496 cycles

CRACK ANGLE LOCATED STA947.5 AND LBL10 AFT CARGO COMPARTMENT 2024-286829<[01] REPLACED ANGLE AND FASTENERS LOCATED BS947.5 AT LEVEL STR26L LBL10 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 149A8103 SHEET: 7 REV: A SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE AND FASTENERS LOCATED BS947.5 AT LEVEL STR26L LBL10 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 149A8103 SHEET: 7 REV: A SEE INDIVIDUAL SIGN OFF BELOW. JOB COMPLETED.

Part: STRAP — DAMAGED (BS 847-856) · airframe 58,718 hrs · 35,496 cycles

ELONGATED HOLE STRAP LOCATED BTW STA 847 TO 856 AND RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT 2024-286831<[01] REPLACED STRAP LOCATED BTW STA 847 TO 856 AND RBL18 AT LEVEL FLOOR STRUCTURE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9. AND DWG 146A0081 SHEET: 34 REV:-.;[02] TASK COMPLETED

Part: ANGLE — CRACKED (BS 540 LBL18) · airframe 58,718 hrs · 35,496 cycles

CRACK BRACKET ANGLE LOCATED BS 540 PLUS 3 INCHES LBL18 AT AIR CONDITIONING BAY. REPLACED THE BRACKET ANGLE IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02. CRACK LENGTH IS: 0.367.

Part: FLOORBEAM — CRACKED (BS 867 LBL10) · airframe 58,718 hrs · 35,496 cycles

CRACK ANGLE LOCATED STA867 AND LBL10 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT 2024-286830<[01] REPLACED ANGLE LOCATED STA867 AND LBL10 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9. AND DWG 149A8102 SHEET: 16 REV:-; DWG 149A8104 SHEET: 1 REV: B.;[02] REPLACED ANGLE LOCATED STA867 AND LBL10 AT LEVEL FLOOR STRUCTURE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9. AND DWG 149A8102 SHEET: 16 REV:-; DWG 149A8104 SHEET: 1 REV: B.

Part: INTERCOSTAL — CRACKED (BS 500-500A S26L) · airframe 58,718 hrs · 35,496 cycles

CRACK WEB - INTERCOSTAL LOCATED BTW STA 500 TO STA500A AT LEVEL STR 26L FWD CARGO COMPARTMENT 2024-286774<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 500 TO STA500A AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM-51-10-02-0G-0 ITEM 9; B737-700 SRM 51-40-02-0G-0 AND DWG:143A7505 SHEET 81 REV-:.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 500 TO STA500A AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM-51-10-02-0G-0 ITEM 9; B737-700 SRM 51-40-02-0G-0 AND DWG:143A7505 SHEET 81 REV-:.SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT ANGLE — CRACKED (LT WG ACES PANEL) · airframe 58,718 hrs · 35,496 cycles

BROKEN ACCESS PANEL 551FB SUPPORT ANGLE AT LT WING. REPLACED THE SUPPORT ANGLE ON ACCESS PANEL 551FB IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A2710 SHEET: 7 REV -.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 58,718 hrs · 35,496 cycles

CRACK AFT CORNER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4.B, STEPS (2) & (4) TO (7).

Part: GIRT BAR — DETERIORATED · airframe 58,718 hrs · 35,496 cycles

DETERIORATED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA 2024-286711<[01] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA IAW B737-700-AMM 25-66-02-400-801 STEP 3.D.(1) (A) TO (J);[02] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA IAW B737-700-AMM 25-66-02-400-801 STEP 3.D.(1) (A) TO (J)

Part: STRUCTURE — CORRODED (BS 312-328) · airframe 58,718 hrs · 35,496 cycles

CORROSION INNER CHORD LOCATED BETWEEN BS312 TO BS328 RBL60 AND WL208 AT FWD GALLEY AREA. REPLACED INNER CHORD INNER CHORD LOC. BTW BS 259.5 - 360; ANGLE & STRAP LOC. ON INNER CHORD IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 & DWG 141A8310 SHEET 25 REV, DWG 141A8310 SHEET 23 REV.

Part: STRUCTURE — CRACKED (BS 303 LBL 55) · airframe 58,718 hrs · 35,496 cycles

CRACK INNER CHORD LOCATED BS303 LBL55 AND WL208 AT FWD GALLEY AREA 2024-286679<[01] REPLACED INNER CHORD AND FASTENERS LOCATED BETWEEN BS 270 TO BS 360 LBL55 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG #141A8110 SHEET: 11; REV: -. AND DWG #141A5220 SHEET: 1; REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INNER CHORD AND FASTENERS LOCATED BETWEEN BS 270 TO BS 360 LBL55 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG #141A8110 SHEET: 11; REV: -. AND DWG #141A5220 SHEET: 1; REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED

Part: WEB — CRACKED (BS 277-294 BL 0) · airframe 58,718 hrs · 35,496 cycles

CRACK WEB LOCATED BETWEEN BS277 TO BS294 BL0 AND WL208 AT FWD GALLEY AREA 2024-286676<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS277 TO BS294 BL0 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AMD DWG 141A5400 SHEET 20 REV:?.SEE INDIVIDUAL STEP SIGNOFF BELOW;[02] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS277 TO BS294 BL0 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AMD DWG 141A5400 SHEET 20 REV:?.SEE INDIVIDUAL STEP SIGNOFF BELOW<BR>RII CERTIFIED

Part: WEB — CRACKED (BS 312-328 LBL47) · airframe 58,718 hrs · 35,496 cycles

CRACK WEB LOCATED BETWEEN BS312 TO BS328 LBL47 AND WL208 AT FWD GALLEY AREA 2024-286678<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS312 TO BS328 LBL47 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV: ?. SEE INDIVIDUAL STEP SING-OFF BELOW;[02] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS312 TO BS328 LBL47 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV: ?. SEE INDIVIDUAL STEP SING-OFF BELOW

Part: WEB — CRACKED (BS 328-344 LBL47) · airframe 58,718 hrs · 35,496 cycles

CRACK WEB LOCATED BETWEEN BS328 TO BS344 LBL47 AND WL208 AT FWD GALLEY AREA 2024-286680<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS328 TO BS344 LBL47 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV:? .SEE INDIVIDUAL STEP SING-OFF BELOW;[02] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS328 TO BS344 LBL47 AND WL208 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV:? .SEE INDIVIDUAL STEP SING-OFF BELOW

Part: FLOORBEAM — CORRODED (BS 986 RBL 43) · airframe 58,718 hrs · 35,496 cycles

CORROSION ON FLOOR BEAM LOCATED BS986.5 RBL43 AND WL208 AFT GALLEY AREA. PERFORMED REPAIR ON FLOOR BEAM LOCATED BS986.5 BTW RBL40 TO RBL 50 AND WL208 AFT GALLEY AREA. IAW EA 24-153-01239.

Part: PRESSURE DECK — CRACKED (BS 663) · airframe 58,718 hrs · 35,496 cycles

CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK LBL 31 STA 663 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.312 INCH APPROX 2024-286661<[01] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[02] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[03] STEP 14 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 220272512; DUE DATE: 08-JAN-25;[04] PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK BTW BS 663.75 TO BS STA 675 AND LBL 25 TO LBL 60 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 FIG 203 . SEE INDIVIDUAL SIGN-OFF BELOW.;[05] PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK BTW BS 663.75 TO BS STA 675 AND LBL 25 TO LBL 60 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 FIG 203 . SEE INDIVIDUAL SIGN-OFF BELOW.<BR>AS RII

Part: WEB — CORRODED (BS 1016 LBL 12) · airframe 58,718 hrs · 35,496 cycles

CORRODED WEB LOCATED BS 1016 PLUS 11INCH, LBL12 AND WL208, AFT GALLEY AREA. REPLACED WITH A NEW WEB AND FASTENERS IAW 51-40-02, SRM 51-10-02 ITEM 9, & DRAWING 147A5600 SHEET 32 REV B.

Part: SUPPORT BRACKET — CRACKED (BS 695) · airframe 58,718 hrs · 35,496 cycles

CRACK ON SUPPORT BRACKET LOCATED BS695 AND RBL24.75 AT PASSENGER CABIN 2024-286612<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-25.;[02] REPLACED SUPPORT BRACKET LOCATED BS695 AND RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG: 273A9110 SHEET:6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTIVE ACTION CERTIFIED

Part: SUPPORT BRACKET — CRACKED (BS 695) · airframe 58,718 hrs · 35,496 cycles

CRACK ON SUPPORT BRACKET LOCATED ON BS695 AND BL0 RH SIDE AT PASSENGER CABIN 2024-286610<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-25.;[02] REPLACED SUPPORT BRACKET LOCATED ON BS695 AND BL0 RH SIDE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG: 273A9110 SHEET: 6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED SUPPORT BRACKET LOCATED ON BS695 AND BL0 RH SIDE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG: 273A9110 SHEET: 6 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.

Part: ISOLATION MOUNT — DETERIORATED (PAX DOOR) · airframe 58,718 hrs · 35,496 cycles

DETERIORATED INSOLATER MOUNT ON FWD ENTRY DOOR CUTOUT PANELS 3(EA) 2024-286532<[01] REPLACED INSOLATER MOUNT ON FWD ENTRY DOOR CUTOUT PANELS 3(EA) IAW B737-700 SRM 51-10-02-0G ITEM 9 AND B737-700 SRM 51-40-02.;[02] JOB COMPLETED

Part: BEAM — CRACKED (BS 299-328) · airframe 58,718 hrs · 35,496 cycles

CRACK INDICATION FOUND ON INBOARD RADIUS ADJACENT TO FASTENER HOLE; ON 141A6536-14 BEAM #4 ON FWD SERVICE DOOR. CRACK LENGTH = 0.860 INCHES. 2024-286507<[01] REPLACED BEAM #4 LOCATED BTW BSTA 299 TO BSTA 328. AT FWD SERVICE DOOR. IAW B737-700 SRM 51-40-02. SRM 51-10-02 PARAGRAPH 9. AND DWG # 141A6516 SHEET 92. REV. ?-?. SEE INDIVIDUAL SING OFF BELOW.;[02] REPLACED BEAM #4 LOCATED BTW BSTA 299 TO BSTA 328. AT FWD SERVICE DOOR. IAW B737-700 SRM 51-40-02. SRM 51-10-02 PARAGRAPH 9. AND DWG # 141A6516 SHEET 92. REV. ?-?. SEE INDIVIDUAL SING OFF BELOW.<BR>AS RII

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 58,718 hrs · 35,496 cycles

DELAMINATED FLOOR PANEL 241FF AT PASSENGER CABIN 2024-286469<[01] TOOL USED: CALIPER P/N:500-196-30 S/N: A23327546 DUE DATE: 04-MAR-25.;[02] TOOL USED: HOT BONDER P/N:HCS9200B; S/N:16122983; DUE DATE: 15-FEB-25;[03] TOOL USED:<BR>SCALE PN: CR5200 SN:8342514551 DUE DÏ¿½TE: 17-FEB-25.;[04] TOOL USED SCALE P/N: CR5200; S/N: 8342514551; DUE DATE: 17-FEB-25;[05] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18185847; DUE DATE: 25-OCT-24;[06] REPAIRED FLOOR PANEL 241FF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] STEP 6 ENTERED IN ERROR ; CORRECT CORRECTIVE ACTION IS: REPAIRED FLOOR PANEL 241FF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] CORRECTIVE ACTION 6; 7 ENTERED IN ERROR. <BR>CORRECT CORRECTIVE ACTION IS: REPAIRED FLOOR PANEL 241FF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.;[09] REPAIRED FLOOR PANEL 241FF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII COMPLETED

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 58,718 hrs · 35,496 cycles

CRACK ON FWD INBOARD CAPTAIN AND F/O SEAT TRACK AT COCKPIT (2EA) 2024-286474<[01] REPLACED FWD INBOARD CAPTAIN AND F/O SEAT TRACK AT COCKPIT (2EA) I.A.W B737-700 AMM-25-11?11-400-801<BR>TOOL USED: TRACK SETTING FIXTURE NG BOEING<BR>P/N: 0T900-0247<BR>S/N: AE-33472;[02] REPLACED FWD INBOARD CAPTAIN AND F/O SEAT TRACK AT COCKPIT (2EA) I.A.W B737-700 AMM-25-11?11-400-801<BR>TOOL USED: TRACK SETTING FIXTURE NG BOEING<BR>P/N: 0T900-0247<BR>S/N: AE-33472

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 58,718 hrs · 35,496 cycles

DELAMINATED FLOOR PANEL 241EF AT PASSENGER CABIN 2024-286467<[01] TOOL USED: CALIPER P/N:500-196-30 S/N: A23327546 DUE DATE: 04-MAR-25.;[02] TOOL USED: HOT BONDER P/N:HCS9200B; S/N:16122983; DUE DATE: 15-FEB-25;[03] TOOL USED:SCALE PN: CR5200 SN:8342514551 DUE DÏ¿½TE: 17-FEB-25.;[04] TOOL USED SCALE P/N: CR5200; S/N: 8342514551; DUE DATE: 17-FEB-25.;[05] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18185847; DUE DATE: 25-OCT-24;[06] REPAIRED FLOOR PANEL 241EF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] CORRECTIVE ACTION 6 ENTERED IN ERROR. <BR>CORRECT CORRECTIVE ACTION IS: REPAIRED FLOOR PANEL 241EF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW;[08] REPAIRED FLOOR PANEL 241EF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII COMPLETED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,718 hrs · 35,496 cycles

DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (8 EA 2024-286419<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (8 EA) IAW B737-700 AMM-33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (8 EA) IAW B737-700 AMM-33-51-15-400-802

Part: WEDGE — DEBONDED (LT WING TE FLAP) · airframe 58,718 hrs · 35,496 cycles

DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE OB SIDE AT LT WING. PERFORMED PERMANENT REPAIR ON I/B MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING IAW SRM 57-53-01-2R-7 REPAIR 7.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 58,314 hrs · 35,229 cycles

FORWARD CARGO FLOOR HAS CRACK<[01] OK TO CONT PER MEL 25-16-01 SP1B;[02] 01 - REMOVED AND REPLACED PER [AMM 25-52-10-401-NG (CARGO FLOOR PANEL - REMOVAL/INSTALLATION - PERMANENT)]

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 56,923 hrs · 34,364 cycles

DOT A24-3 MID CABIN FLOOR PANEL 231XF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] BONDTEST IAW B737 NDT PART 4; 51-00-05. NO DEFECTS NOTED. TOOL#40082; DUE 10OCT23<BR>UT IAW B737 NDT 4; 51-00-03. NO DEFECTS NOTED. TOOL#36285; DUE 16DEC23. REF EA 23-153-02790-WIP1 STEP 2;[02] EVALUATED PANEL 231XF 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 (A197641); BMS 9-3 (A178073). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO BOND.;[03] VERIFIED STEPS 1 AND 2 C/W AND OK TO BOND GRANTED;[04] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3 K-M.;[05] REPAIRED UPPER SURFACE ON PANEL 231XF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[06] REFER TO FAULT TTG8Q00NDBZJ WHERE EA 23-153-02790 WAS ADDED AS A SUBTASK.;[07] VERIFIED STEPS 4-6.<BR>AUDIT C/W.

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 56,923 hrs · 34,364 cycles

RIGHT HAND STA 663 VAPOR BARRIER WEB IS CRACKED AT EXISTING REPAIR AT APPROX RBL 32 AND RBL 57<[01] REMOVED AND REPLACED WEB 111A1151Y10 ON SHELD IAW SRM 51-40-05-0G-0DWG 111A1151 REV A;[02] VERIFIED STEP 1<BR>AUDIT C/W

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 56,923 hrs · 34,364 cycles

DOT A24-6 MID CABIN FLOOR PANEL 242AF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND FLOOR PANEL TO B.E.R.. REPLACE BY FABRICATION IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204 AND DWG 144A5810-189. NEW FLOOR BOARD (A1257); EPIBOND 420 (A186981); INSERTS (A201251); FOAM TAPE (A197687);[02] REPLACED BY FABRICATION AND SAMPLE OF MID CABIN FLOOR PANEL 242AF IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARA 4; DWG 144A5810-189 AND BAC5085 STEP 8.4.2;[03] VERIFIED STEPS 1-2.<BR>AUDIT C/W.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 56,923 hrs · 34,364 cycles

DOT A24-7 MID CABIN FLOOR PANEL 232RF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MULTIPLE AREAS OF DAMAGE TO FLOOR BOARD AND IS B.E.R. FABRICATE NEW FLOOR BOARD PER SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 4<BR><BR>VERIFIED MATERIALS AS FLOOR BOARD STOCK (A1257); INSERTS (A201251); ADHESIVE (A186981); FOAM TAPE (A197687) IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204 AND BOEING DRW. 144A5810;[02] VERIFIED MATERIAL FOR STEP 1.;[03] FABRICATED NEW FLOORBOARD PER SAMPLE BOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 4; BOEING DRW; 144A5810 AND BAC5085 PARAGRAPH 8.4.2.;[04] VERIFIED ITEM 3.<BR>AUDITED.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 56,923 hrs · 34,364 cycles

DOT A24-5 MID CABIN FLOOR PANEL 241BF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND FLOOR PANEL TO B.E.R.. REPLACE BY FABRICATION IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204 AND DWG 144A5810-189. NEW FLOOR BOARD (A1257); EPIBOND 420 (A186981); INSERTS (A201251); FOAM TAPE (A197687);[02] VERIFIED MATERIAL FOR STEP 1.;[03] REPLACED BY FABRICATION AND SAMPLE OF MID CABIN FLOOR PANEL 241BF IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARA 4; DWG 144A5810-189 AND BAC5085 STEP 8.4.2;[04] VERIFIED ITEM 3.<BR>AUDITED.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 56,923 hrs · 34,364 cycles

DOT A24-4 MID CABIN FLOOR PANEL 241AF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] BONDTEST IAW B737 NDT PART 4; 51-00-05. NO DEFECTS NOTED. TOOL#40082; DUE 10OCT23<BR>UT IAW B737 NDT 4; 51-00-03. NO DEFECTS NOTED. TOOL#36285; DUE 16DEC23. REF EA 23-153-02790-WIP1 STEP 2;[02] EVALUATED PANEL 241AF 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 3 A; C; E&F. VERIFIED MATERIALS AS: BMS 8-201 (A197641); BMS 9-3 (A178073). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO BOND.;[03] VERIFIED STEP 1 AND 2 C/W AND OK TO BOND GRANTED;[04] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3 K-M.;[05] REPAIRED DAMAGE TO UPPER SURFACE ON PANEL 241AF. IAW B737-700 53-00-50-2R-1; SRM 53-00-50-2R-0& EA 23-153-02790.;[06] VERIFIED STEPS 4-5.<BR>AUDIT C/W.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,923 hrs · 34,364 cycles

CABIN STOWBIN BULLNOSE EMERGENCY LIGHT AT ROW 12 ABC IS INOP<[01] REPLACED LAMPED STOWBIN BULLNOSE EMERGENCY LIGHT AT ROW 12 ABC IAW AMM 33-51-03-960-801 OPS CHECK GOOD;[02] VERIFIED ITEM 1<BR>C/W

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,762 hrs · 34,262 cycles

EMERGENCY LIGHTS L1 &R1 BATTERY PACK INOP<[01] R&R BATTERY PACK FOR EMERGENCY LIGHTS R1&R2 M-01674 PER 33-51-06 .OPS CHK GOOD .

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 55,776 hrs · 33,592 cycles

AFT W4142 EMERGENCY LIGHT BATTERY PACK NEEDS TO BE REPLACED.<[01] REMOVED AND REPLACED AFT W4142 EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (FWD CABIN) · airframe 53,552 hrs · 32,116 cycles

2 FORWARD LH BULLNOSE EMERGENCY LIGHTS INOP / [01] R & R LH FWD. BULLNOSE EMERGECY LIGHT BATTERY PACK IAW AMM 33-51-06.

Part: LIGHT — INOPERATIVE · airframe 52,927 hrs · 31,715 cycles

BURNED EMERGENCY EXIT LIGHT ON SIDEWALL DOOR LH SIDE AND AFT FUSELAGE RH SIDE AT PASSENGER CABIN (2 EA) 2022-228627 / [01] REPLACED EMERGENCY EXIT LIGHT ON SIDEWALL DOOR LH SIDE AND AFT FUSELAGE RH SIDE AT PASSENGER CABIN (2 EA) I.A.W B737-700 AMM 33-51-01-960-802 AND AMM 33-51-04-960-801. TESTS ARE OK.;[02] TASK CARD COMPLETED

Part: VAPOR BARRIER — CRACKED (WHEEL WELL) · airframe 52,927 hrs · 31,715 cycles

CRACK VAPOR BARRIER LOCATED ON BS 663 LBL 65 ON MAIN WHEEL WELL LH SIDE 2022-228599 / [01] TOOL USED CALIPER P/N 500-197-30; S/N A18234378; DUE DATE: 21-SEP-22.;[02] TOOL USED HOT BONDER P/N: HCS9000B; S/N: 15092096; DUE DATE: 16-JAN-23;[03] TOOL USED SCALE P/N CL5000; S/N AE-407336; DUE DATE: 16-AUG-22.;[04] REPAIRED VAPOR BARRIER LOCATED ON BS 663 LBL 65 ON MAIN WHEEL WELL LH SIDE IAW B737-700 SRM 51-70-04-2R-10 REPAIR # 10 AND SRM 51-70-04-2R-0 REPAIR GENERAL TOOL USED CALIPER P/N 500-197-30 S/N A18234378 DUE DATE 21-SEP-22; HOT BONDER P/N ;HCS9000B; S/N: 15092096; DUE DATE: 16-JAN-23; SCALE P/N CL5000; S/N AE-407336; DUE DATE: 16-AUG-22.

Part: BRACKET — ELONGATED (TOILET DOOR) · airframe 52,927 hrs · 31,715 cycles

ELONGATE HOLE ON BRACKET LOCATED ON ACCESS PANEL 145AL AT LOWER FUSELAGE 2022-228600 / [01] REPLACED BRACKET LOCATED ON ACCESS PANEL 145AL AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 PART USED HINGE ASSY P/N USED: 146A7414-9 PO: 2022-123293 1;[02] TASK CARD COMPLETED

Part: ANGLE — CRACKED (WHEEL WELL) · airframe 52,927 hrs · 31,715 cycles

(CUSTOMER REQUEST) CRACK ON BRACKET LOCATED AT BS 663 BETWEEN LBL 45.64 TO LBL 54.21 L/H SIDE MAIN WHEEL WELL 2022-228593 / [01] TOOLS USED: POWER PACK P/N: FMK0003223; S/N: PE0412/63335; DUE DATE: 26-JAN-23; MULTIMETER P/N: FLUKE 87-5; S/N: 98740068; DUE DATE: 08-NOV-22; THERMOMETER P/N: 42510A; S/N: 200813258; DUE DATE: 29-JUN-22.;[02] REPLACED ANGLE ON BS 663 LBL 45.64 A I.A.W SRM B737-700 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DRAWING #276A9183 REV:-; 111A1001 REV:A ; SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] REPLACED ANGLE ON BS 663 LBL 45.64 A I.A.W SRM B737-700 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DRAWING #276A9183 REV:-; 111A1001 REV:A ; SEE INDIVIDUAL STEP SIGN OFFS BELOW

Part: TRACK — CRACKED (AFT CARGO BAY) · airframe 52,927 hrs · 31,715 cycles

CRACK TRACK RBBL 13.84 LOCATED BS 747 AT AFT CARGO COMPARTMENT 2022-228574 / [01] ET TOOL USED: PN: PHASEC 3D; SN: 587435 /03; DUE DATE: 22 -DEC -22;[02] PERFORMED REPAIR ON TRACK LOCATED BS 727E TO BS 767 RBBL 13.84 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR . SEE INDIVIDUAL SIGN-OFF BELOW;[03] PERFORMED REPAIR ON TRACK LOCATED BS 727E TO BS 767 RBBL 13.84 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR . SEE INDIVIDUAL SIGN-OFF BELOW;[04] CORRECTED STEP 3<BR>PERFORMED REPAIR ON TRACK LOCATED BS 727E TO BS 767 RBBL 13.84 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-53-2R-3 REPAIR . SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII

Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 52,927 hrs · 31,715 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727D TO BS 847 LBL 31.1 WL 156 AFT CARGO COMPARTMENT 2022-228573 / [01] INSPECTION REJECT IN STEP 11 SEE TTG8Q00CK7LW;[02] REPLACED SUPPORT ZEE LOCATED BTW BS 727D TO BS 847 LBL 31.1 WL 156 AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-40-02;SRM 51/10/02 ITEM 9 AND DRAWING 146A7500 SHEET 85 REV A. SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] REPLACED SUPPORT ZEE LOCATED BTW BS 727D TO BS 847 LBL 31.1 WL 156 AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-40-02;SRM 51/10/02 ITEM 9 AND DRAWING 146A7500 SHEET 85 REV A. <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL STEP SIGN OFFS BELOW

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 52,927 hrs · 31,715 cycles

CORROSION STRAP LOCATED BTW BS 807 TO BS 827 WL 156.1 RBL 18.84 AT AFT CARGO COMPARTMENT 2022-228576 / REPLACED STRAP LOCATED BTW BS 807 TO BS 827 WL 156.1 RBL 18.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING 146A8120 REV

Part: SUPPORT — CRACKED (AFT CARGO BAY) · airframe 52,927 hrs · 31,715 cycles

CRACK ANGLE - SUPPORT LOCATED BTW BS 907 TO BS 927 AND STR 25/27R AFT CARGO COMPARTMENT 2022-228571 / [01] REPLACED ANGLE - SUPPORT LOCATED BTW BS 907 TO BS 927 AND STR 25/27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7221 REV. D;[02] REPLACED ANGLE - SUPPORT LOCATED BTW BS 907 TO BS 927 AND STR 25/27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7221 REV. D. SEE INDIVIDUAL SIGN OFF BELOW;[03] JOB COMPLETED.

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 52,927 hrs · 31,715 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 WL 156.1 RBL 21.84 AFT CARGO COMPARTMENT 2022-228575 / [01] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 WL 156.1 RBL 21.84 AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM-51-40-02; SRM 51-10-02 ITEM 9 AND DWG-146A7500 REV: A;[02] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 WL 156.1 RBL 21.84 AFT CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM-51-40-02; SRM 51-10-02 ITEM 9 AND DWG-146A7500 REV: A<BR>CERTIFIED AS RII

Part: PLATE — CORRODED (AFT CARGO BAY) · airframe 52,927 hrs · 31,715 cycles

CORROSION LOWER SILL LOCATED BTW BS 794.37 TO BS 847 RBL 26.84 WL 157.1 AFT CARGO COMPARTMENT 2022-228572 / [01] REPLACED LOWER SILL LOCATED BTW BS 794.37 TO BS 847 RBL 26.84 WL 157.1 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A8330 SHEET 30 REV:- <BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK CARD COMPLETED <BR>RII<BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: WEB — CORRODED (FWD CARGO BAY) · airframe 52,927 hrs · 31,715 cycles

CORROSION ON WEB-INTERCOSTAL (SHIELDS) LOCATED BTW BS 420 TO BS 440 AT LEVEL STR 26R RBL 23.3 AND WL 152.2 FWD CARGO COMPARTMENT 2022-228543 / [01] REPLACED NEW WEB INTERCOSTAL SHIELDS LOCATED BTW BS 420 TO BS 440 AT LEVEL STR 26R RBL 23.3 AND WL 152.2 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080 REV -. SEE INDIVIDUAL SIGN OFF BELLOW.;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: ANGLE — CRACKED (FWD CARGO) · airframe 52,927 hrs · 31,715 cycles

CRACK ON ANGLE LOCATED ON BS 500C FWD FACE AT LEVEL STR 26L FWD CARGO COMPARTMENT 2022-228539 / [01] REPLACED ANGLE LOCATED ON BS 500C FWD FACE AT LEVEL STR 26L FWD CARGO COMPARTMENT I.A.W. B737-700 SR 51-10-02 ITEM 9 AND DWG DWG 143A7505 REV.-.;[02] CORRECTED STEP 1<BR>REPLACED ANGLE LOCATED ON BS 500C FWD FACE AT LEVEL STR 26L FWD CARGO COMPARTMENT I.A.W. B737-700 SR 51-10-02 ITEM 9 AND DWG DWG 143A7505 REV.-. SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED ANGLE LOCATED ON BS 500C FWD FACE AT LEVEL STR 26L FWD CARGO COMPARTMENT I.A.W. B737-700 SR 51-10-02 ITEM 9 AND DWG DWG 143A7505 REV.-. SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII

Part: WEB — CORRODED (FWD CARGO BAY) · airframe 52,927 hrs · 31,715 cycles

CORROSION WEB - INTERCOSTAL LOCATED BTW BS 460 TO BS 500A RBL 23.4 AND WL 152.2 AT FWD CARGO COMPARTMENT 2022-228549 / [01] REPLACE NEW WEB INTERCOSTAL LOCATED BTW BS 460 TO BS 500A RBL 23.4 AND WL 152.2 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING 143A0080 REV- SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACE NEW WEB INTERCOSTAL LOCATED BTW BS 460 TO BS 500A RBL 23.4 AND WL 152.2 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING 143A0080 REV- SEE INDIVIDUAL SIGN OFF BELOW<BR>CERTIFIED AS RII

Part: PANEL — CRACKED (LH WING) · airframe 52,927 hrs · 31,715 cycles

CRACK ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2022-228544 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 15331926; DUE DATE: 28-SEP-22.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18196126; DUE DATE: 24-FEB-23.;[03] TOOL USED SCALE P/N: SCA-301; S/N: AE-412125; DUE DATE: 14-MAR-23.;[04] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 18196126 DUE DATE: 24-FEB-23.;[05] TOOL USED SCALE P/N: SCA-301 S/N: AE-412123 DUE DATE: 14-MAR-23.;[06] TOOL USED: MULTIMETER P/N: FLUKE87 S/N: AE-23149 DUE DATE: 10-NOV-22.;[07] REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] COMPLETED TASK.

Part: SUPPORT ANGLE — CORRODED (FWD CARGO BAY) · airframe 52,927 hrs · 31,715 cycles

CORROSION ON SUPPORT ANGLE LOCATED ON BS 500D BTW STR 26R TO STR 26L WL 152.2 AND BTW LBL 23.3 TO RBL 23.3 FWD CARGO COMPARTMENT 2022-228551.REPLACED SUPPORT ANGLE LOCATED ON BS 500D BTW STR 26R TO STR 26L WL 152.2 AND BTW LBL 23.3 TO RBL 23.3 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; P/N USED: 143A9485Y35

Part: SUPPORT — CRACKED (WHEEL WELL) · airframe 52,927 hrs · 31,715 cycles

(CUSTOMER REQUEST) CRACK ON SUPPORT ANGLE LOCATED AT BS 663 LH SIDE A T MAIN WHEEL WELL COMPARTMENT 2022-228566 / INSPECTION REJECT IN STEP 8 SEE TTG8Q00CJGX6;[05] REPLACED SUPPORT ANGLE LOCATED AT BS 663 LH SIDE A T MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-40?02 AND DRAWING # 111A1000 REV. A . SEE INDIVIDUAL SIGN OFF BELOW;[06] REPLACED SUPPORT ANGLE LOCATED AT BS 663 LH SIDE A T MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-40?02 AND DRAWING # 111A1000 REV. A .

Part: FRAME — CRACKED (FWD GALLEY) · airframe 52,927 hrs · 31,715 cycles

CRACK FRAME ON BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA 2022-228529 PERFORMED REPAIR ON FRAME ON BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY B IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 STEP 2 A FOR INSPECTION THRESHOLD SEE STEP 5. SEE INDIVIDUAL SIGN-OFF BELOW; PERFORMED REPAIR ON FRAME ON BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY B IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 STEP 2 A FOR INSPECTION THRESHOLD SEE STEP 5.

Part: BRACKET — BROKEN (RH ENG) · airframe 52,927 hrs · 31,715 cycles

BROKEN SUPPORT BRACKET LOC. FAN CASE AT 6 OCLOCK ON ENGINE 2 2022-228510 / [01] REPLACED SUPPORT BRACKET LOC. FAN CASE AT 6 OCLOCK ON ENGINE 2 I.A.W B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT BRACKET LOC. FAN CASE AT 6 OCLOCK ON ENGINE 2 I.A.W B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 52,927 hrs · 31,715 cycles

CRACK CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT 2022-228520 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A18135080;DUE DATE:31-JUL-22.;[02] REPAIRED BY WELD CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1. AND BAC 5975 SEE INDIVIDUAL SIGNOFFS BELOW;[03] TASK COMPLETED

Part: LIGHT — BROKEN (PAX CABIN) · airframe 52,927 hrs · 31,715 cycles

BROKEN SIDEWALL PANEL 231YHW EMERGENCY EXIT COVER LENS AT PASSENGER CABIN (1 EA) 2022-228494 / [01] REPLACED SIDEWALL PANEL 231YHW EMERGENCY EXIT COVER LENS AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 33-51-01-960-801 2 C (3);[02] REPLACED SIDEWALL PANEL 231YHW EMERGENCY EXIT COVER LENS AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 33-51-01-960-801 2 C (3)

Part: BRACKET — CORRODED (TOILET DOOR) · airframe 52,927 hrs · 31,715 cycles

CORROSION ON BRACKET LOCATED ON ACCESS PANEL DOOR 145AL AT LOWER FUSELAGE 2022-228523 / [01] REPLACED SUPPORT BRACKET LOCATED ON ACCESS PANEL DOOR 145AL AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM-51-40-02; P/N USED: 149A7414-9 PO: 2022/123293;[02] REPLACED SUPPORT BRACKET LOCATED ON ACCESS PANEL DOOR 145AL AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM-51-40-02; P/N USED: 149A7414-9 PO: 2022/123293

Part: STRINGER — CRACKED (FWD CARGO) · airframe 52,927 hrs · 31,715 cycles

CRACK STRINGER 26L BS 540 AT FWD CARGO COMPARTMENT 2022-228530 / [01] TOOL USED: P/N: 45MG; S/N:130061901; DUE DATE: 08-APR-23;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210136503 DUE DATE: 11-APR-23;[03] PERFORMED PERMANENT REPAIR CATEGORÏ¿½A ?A? ON STRINGER LOC BTW BS 500D TO BS 540 AND STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW;[04] PERFORMED PERMANENT REPAIR CATEGORÏ¿½A ?A? ON STRINGER LOC BTW BS 500D TO BS 540 AND STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW AS RII

Part: STRINGER — CRACKED (FWD CARGO) · airframe 52,927 hrs · 31,715 cycles

CRACK STRINGER 25R BS 540 AT FWD CARGO COMPARTMENT 2022-228528 PERFORMED REPAIR ON STRINGER 25R BTW BS 500C TO BS.540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. PERFORMED REPAIR ON STRINGER 25R BTW BS 500C TO BS.540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1.

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 52,927 hrs · 31,715 cycles

CRACK GUSSET LOCATED BS 500D AND S-19R FWD CARGO COMPARTMENT 2022-228450 / [01] REPLACED GUSSET LOCATED BS 500D AND S-19R FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 REV:-. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED GUSSET LOCATED BS 500D AND S-19R FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 REV:-. SEE INDIVIDUAL SIGN-OFF BELOW RII

Part: ANGLE — CRACKED (FWD CARGO BAY) · airframe 52,927 hrs · 31,715 cycles

CRACK ANGLE - SUPPORT LOCATED BS 400 AFT SIDE AND S-26L FWD CARGO COMPARTMENT 2022-228452 / [01] REPLACED ANGLE - SUPPORT LOCATED BS 400 AFT SIDE AND S-26L FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG DWG 143A7505 REV.-. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE - SUPPORT LOCATED BS 400 AFT SIDE AND S-26L FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG DWG 143A7505 REV.-. SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII

Part: ANGLE — CRACKED (RH IB FAN COWL) · airframe 52,927 hrs · 31,715 cycles

CRACK ANGLE INBOARD FAN COWL LOC. INTERNAL AREA IDG SERVICE DOOR ON ENGINE 2 (1 EA) 2022-228463. / [01] REPLACED NEW ANGLE INBOARD FAN COWL LOC. INTERNAL AREA IDG SERVICE DOOR ON ENGINE 2 IAW B737-700 SRM 51-10-02 ITEM 9 AND CMM <BR>71-13-30;[02] TASK COMPLETED

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 52,927 hrs · 31,715 cycles

CRACK ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR 2022-228392 REPAIRED ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-04-2R-2 REP.2; REPAIRED ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-04-2R-2 REP.2;

Part: GUSSET — CRACKED (FWD CARGO BAY) · airframe 52,927 hrs · 31,715 cycles

CRACK GUSSET LOCATED BS 500D AND S-19L FWD CARGO COMPARTMENT 2022-228449 / [01] REPLACED GUSSET LOCATED BS 500D AND S-19L FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 REV:-. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED GUSSET LOCATED BS 500D AND S-19L FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 REV:-. SEE INDIVIDUAL SIGN-OFF BELOW RII

Part: PANEL — CRACKED (RH WING) · airframe 52,927 hrs · 31,715 cycles

CRACK ACCESS PANEL 661BB TRAILING EDGE AROUND HOLES RT WING 2022-228136 / [01] TOOL USED: CALIPER P/N: 500-464; S/N: 15331926; DUE DATE: 28-SEP-22.;[02] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18196126; DUE DATE: 24-FEB-23.;[03] TOOL USED SCALE P/N: SCA-301; S/N: AE-412125; DUE DATE: 14-MAR-23.;[04] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 18196126 DUE DATE: 24-FEB-23.;[05] TOOL USED SCALE P/N: SCA-301 S/N: AE-412123 DUE DATE: 14-MAR-23.;[06] TOOL USED: MULTIMETER P/N: FLUKE87 S/N: AE-23149 DUE DATE: 10-NOV-22.;[07] REPAIRED ACCESS PANEL 661BB TRAILING EDGE RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] COMPLETED TASK.

Part: SKIN — CRACKED (RH HOR STAB) · airframe 52,927 hrs · 31,715 cycles

CRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.0 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.100 INCH 2022-228134 / [01] ET TOOL USED: PN: PHASEC 3D; SN: 587435 /03; DUE DATE: 22 -DEC -22. CALIPER TOOL USED: PN: 500-197-30; SN: A21043164. DUE DATE : 01-SEP-22.;[02] FAULT TTG8Q00C79K0 WHERE EA 22-155-01485 HAS BEEN ATTACHED AS A SUBTASK;[03] REFER TO FAULT TTG8Q00C79K0 WHERE EA 22-155-01485 HAS BEEN ATTACHED AS A SUBTASK;[04] REFER TO FAULT TTG8Q00C79K0 WHERE EA 22-155-01485 HAS BEEN ATTACHED AS A SUBTASK.

Part: SKIN — CRACKED (RH HOR STAB) · airframe 52,927 hrs · 31,715 cycles

CRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 25.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.600 INCH 2022-228133 PERFORMED REPAIR ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 25.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB <BR>IAW EA 22-155-01485 WIP 1 AND EA COVER 22-155-01485 SEE INDIVIDUAL SIGN OFF BELOW;[06] CERTIFIED RII MAJOR REPAIR PERFORMED.

Part: VAPOR BARRIER — CRACKED (WHEEL WELL) · airframe 52,927 hrs · 31,715 cycles

CUSTOMER REQUEST CRACK VAPOR VARRIER LOCATED ON BS 663 LBL 54 AND WL 141.5 ON MAIN WHEEL WELL LH SIDE AT MAIN WHEEL WELL COMPARTMENT 2022-228077 / [01] TOOL USED; HOT BONDER PN: HCS9200B; SN: 18175478; DUE DATE: 05/AUG/22.;[02] TOOL USED; SCALE PN: SCA-301; SN: AE-412138; DUE DATE: 14/MAR/23.;[03] REPAIRED VAPOR BARRIER LOCATED ON BS 663 LBL 54 AND WL 141.5 ON MAIN WHEEL WELL LH SIDE AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. TOOL USED CALIPER PN: 500-197-30; SN: A21147745; DUE DATE: 09/APR/23. SCALE P/N:SCA-301 S/N:AE-412123 DUE DATE:14-MAR-23.;[04] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: PANEL — CRACKED (FWD FUSELAGE) · airframe 52,770 hrs · 31,622 cycles

RAMP PERSONEL FOUND 13 CRACK AT FWD COMP FLOOR CENTER MID AREA PANEL 120CF / [01] INSTALLED PERMANENT REPAIR FIBERGLASS REINFORCEMENT AT FWD CARGO COMPARTMENT REF. AMM 25-52-01

Part: PANEL — CRACKED (AFT CARGO) · airframe 52,770 hrs · 31,622 cycles

RAMP PERSONEL FOUND 15 CRAC AT AFT CARGO FLOOR AFT AREA .PANEL 140BF / [01] PERFORMED REPAIR ON AFT CARGO PANEL PER AMM 25-52-01. WORK ACCOMPLISHED BY E78913

Part: BATTERY — INOPERATIVE (CABIN) · airframe 51,451 hrs · 30,834 cycles

AFT GALLEY OB FLASHLIGHT HAS DEAD BATTERY ; / [01] REPLACED BATTERY IAW CMM 25-60-02 OPS CHECK GOOD

Part: RIB — DAMAGED (HORIZONTAL STAB) · airframe 49,983 hrs · 29,972 cycles

CARD # TTG8Q00537XS L/H HORIZONTAL LEADING EDGE RIB AT STA 142.45 DAMAGED; SIGNED OFF WITHOUT RII. ; / REMOVED AND REPLACED RIB AT STA 142.45 PER SRM 51-40-02.<BR>SEE FAULT # TTG8Q00537XS FOR COMPLETED WORK AND SIGN-OFFS.

Part: RIB — DAMAGED (HORIZONTAL STAB) · airframe 49,983 hrs · 29,972 cycles

L/H HORIZONTAL LEADING EDGE RIB AT STA 142.45 DAMAGED / REMOVED AND REPLACED RIB AT STA 142.45 PER SRM 51-40-02

Part: DOUBLER — BROKEN (FUSELAGE) · airframe 48,661 hrs · 29,190 cycles

GROUND POWER RECEPTACLE SURROUND REPAIR BROKEN AT BOTTOM TAB. PERFORMED REPAIR OF GROUND POWER RECEPTACLE SURROUND DOUBLER WITH FABRICATION AND INSTALLATION OF NEW DOUBLER, PER SRM 53-10-15-2R-4 REPAIR 4. WORK PERFORMED UNDER CAT A REPAIR. NO FURTHER INSPECTION REQUIRED.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 47,873 hrs · 28,673 cycles

R/H HORIZ. STAB RIB #5 ;SS.129.50 HAS CRACKED #3 VERT. STIFFENER. / REPAIRED R/H HORIZ STAB RIB #5; SS129.50; #3 VERTICAL STIFFENER PER SRM 55-10-09-2R-4 REPAIR 4.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 47,873 hrs · 28,673 cycles

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

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,873 hrs · 28,673 cycles

CABIN FLOOR PANEL 241AF IS DELAMINATED. REMOVED AND REPLACED CABIN FLOOR PANEL 241AF PER AMM 53-21-00.

Part: PLATE — CRACKED (LT WING) · airframe 47,873 hrs · 28,673 cycles

LEFT WING TRAILING EDGE STRUCTURE HAS A CRACKED WIGGLE PLATE I/B OF #3 FLAP TRACK AND O/B OF PANEL 551DB. / REMOVED AND REPLACED L/H WING LOWER SURFACE WIGGLE PLATE; I/B OF #3 FLAP TRACK AND O/B OF PANEL 551DB IAW SRM 51-40-05; SRM 51-20-01;SRM 51-40-02.

Part: PLATE — CRACKED (RT WING) · airframe 47,873 hrs · 28,673 cycles

RIGHT WING TRAILING EDGE STRUCTURE HAS A CRACKED WIGGLE PLATE I/B OF #7 FLAP TRACK AND O/B OF PANEL 651DB. / REMOVED DAMAGED WIGGLE PLATE AND INSTALLED NEW PLATE PER SRM 51-40-02.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 47,873 hrs · 28,673 cycles

R/H HORIZ. STAB RIB #5 ;SS.129.50 HAS CRACKED #2 VERT. STIFFENER. / PERFORMED REPAIR PER SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN OFFS FOR WORK ACCOMPLISHED.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,873 hrs · 28,673 cycles

CABIN FLOOR PANEL 241DF IS DELAMINATED. / REMOVED AND REPLACED FLOOR PANEL 241DF PER AMM 53-21-00

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 47,873 hrs · 28,673 cycles

FWD CARGO; AFT CORNER SCUFF PLATE CRACKED. / REPAIRED PER W/O#RA22N1. INSTALLED FWD CARGO AFT SCUFF PLATE PER AMM 53-11-02.

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 47,873 hrs · 28,673 cycles

PASSENGER SEAT TRACK #1 AT STA 520 HAS DAMAGE TO UPPER CROWN. REPAIRED PER SRM 53-00-52-2R-4; SEE WIPS AND SUBTASKS FOR INDIVIDUAL SIGNOFFS

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,873 hrs · 28,673 cycles

CABIN FLOOR PANEL 241KF IS DELAMINATED. / REMOVED AND REPLACED CABIN FLOOR PANEL 241KF PER AMM 53-21-00.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 47,873 hrs · 28,673 cycles

R/H HORIZONTAL STABILIZER LEADING EDGE HAS A DENT AT LE STATION 130 MEASURING 9.5'L X 3'W X .265' DEEP FROM RIB TO RIB WHICH IS OUT OF ALLOWABLE LIMITS PER SRM / REMOVED AND REPLACED R/H HORIZONAL LEADING EDGE PER AMM 27-41-21. TAG NO: 684872 PN ON: 186A1001-16 SN ON: WN259 PN OFF: SN OFF: WN250

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 47,873 hrs · 28,673 cycles

AFT CARGO; AFT CORNER SCUFF PLATE CRACKED. / REMOVED AND REPLACED PER AMM.53-11-02

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 47,873 hrs · 28,673 cycles

FWD CARGO; FWD CORNER SCUFF PLATE CRACKED. / REPAIRED PER W/O#RA22N0. INSTALLED FWD CARGO FWD SCUFF PLATE PER AMM 53-11-02.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,873 hrs · 28,673 cycles

CABIN FLOOR PANEL 241NF IS DELAMINATED. / REMOVED AND REPLACED CABIN FLOOR PANEL 241NF PER AMM 53-21-00.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 47,873 hrs · 28,673 cycles

EMERGENCY LIGHT LENS IS NOT SECURE IN BULLNOSE ABOVE SEAT 1ABC / REMOVED AND REPLACED LENS PER AMM 33-51-03

Part: BALLAST — INOPERATIVE (COCKPIT) · airframe 47,706 hrs · 28,568 cycles

CO-PILOT SIDE EMER EXIT TUBE LIGHT INOP. (SIDE WALL LIGHT) / DMA # 0167599 R&R R/H OVERWING SIDEWALL LIGHT BALLAST IAW MM 33-21-00. CL # 37516

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,568 hrs · 28,489 cycles

RT FLASHLIGHT AFT GALLEY INOP OK TO CONT PER MEL 25-12-01 SP 1B TRACKING # 35103 / R&R AFT FLIGHT ATTENDANT FLASH LIGHT BATTERY PER 'SIP'. CLEARING # 35110

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,554 hrs · 28,480 cycles

AFT GALLEY EMERGENCY FLASHLIGHT RED LIGHT WON'T BLINK. / R&R BATTERY IAW AMM 25-64-00

Part: FLASHLIGHT — NOT SEATED (CABIN) · airframe 47,485 hrs · 28,440 cycles

AFT EMERGENCY FLASHLIGHT INOP RESEATED AFT EMERGENCY FLASHLIGHT IN HOLDER. OPS CHECKS GOOD PER AMM 25-64-00

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,471 hrs · 28,432 cycles

OVERHEAD OVERWING EXIT EMERGENCY LIGHT INOP AND ALL L/H OVERWING EMERGENCY LIGHTS INOP R&R L/H OVERWING EXIT BATTER PACK PER AMM 33-51-06 OPS NORMAL

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,471 hrs · 28,432 cycles

OVERHEAD OVERWING EXIT EMERGENCY LIGHT INOP AND ALL L/H OVERWING EMERGENCY LIGHTS INOP / R&R L/H OVERWING EXIT BATTER PACK PER AMM 33-51-06 OPS NORMAL

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 46,961 hrs · 28,095 cycles

BATTERY PACKS AT M01670 AND M01673 WILL NOT ILLUMINATE EMERGENCY LIGHTS FOR 15 MINUTES. REMOVED AND REPLACED PER AMM 33-51-06

Part: BATTERY — DISCHARGED (CABIN) · airframe 46,916 hrs · 28,065 cycles

RT EMERGENCY EXIT LIGHTS INOP NEAR OVERWING EXIT. R&R BATTERY PER AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 44,968 hrs · 26,840 cycles

L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED MAIN DOOR SLIDE IAW AMM.

Part: FAIRING — ELONGATED (LWR FUSELAGE) · airframe 44,785 hrs · 26,713 cycles

PANEL 193B HAS ELONGATED/ENLARGED FASTENER HOLES WITH PULLING THROUGH FASTENERS AT LOCATIONS 3; 4; 5; 6; 7; 8; 12; 13; 14; 15; 16; 19; 20; 21; 22; 28; 29; 30; 31; 32; 33; 34; 35; AND 36 / REPLACED PANEL B193 AS PER AMM 53-51-21

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,690 hrs · 26,657 cycles

L/H OVERHEAD EMERGENCY LIGHT INOP BETWEEN SEAT 17 TO SEAT 20. / R&R POWER SUPPLY ASSEMBLY PER AMM.

Part: LIGHT — INOPERATIVE (SEATS 17-20) · airframe 44,690 hrs · 26,657 cycles

L/H OVERHEAD EMERGENCY LIGHT INOP BETWEEN SEAT 17 TO SEAT 20. / R&R LIGHT ASSEMBLY PER AMM.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 42,207 hrs · 25,093 cycles

R2 DOOR EMERGENCY SLIDE EGRESS LIGHT INOP. RELAMPED LIGHT PER MM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,796 hrs · 24,821 cycles

INTERCOSTAL CORRODED BETWEEN BS 747 TO BS 767, STR 26R. R&R INTERCOSTAL PER SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 41,786 hrs · 24,814 cycles

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

Part: SIGN — INOPERATIVE (CABIN) · airframe 41,786 hrs · 24,814 cycles

FORWARD GALLEY OUTBOARD LOWER EMERGENCY EXIT LIGHT INOP. R&R SIGN PER MM.

Part: PANEL — BROKEN (WHEEL WELL LH) · airframe 41,786 hrs · 24,814 cycles

BOW-TIE PANEL IN L/H WHEEL WELL BROKEN PN# 149A7656-1. / REMOVED AND REPLACED BOW-TIE PANEL IN L/H WHEEL WELL PN# 149A7656-1 PER SRM 51-40-02

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 41,786 hrs · 24,814 cycles

FWD CARGO; FWD CORNER SCUFF PLATE CRACKED. / REMOVED AND REPLACED SCUFF PLATE PER AMM 53-11-02.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,786 hrs · 24,814 cycles

LT HORIZONTAL STABILIZER INSPAR RIB CRACKED ON LOWER FLANGE NEXT TO STIFFENER RADIUS AT APPROX 18" FROM FORWARD EDGE. REPAIRED RIB PER SRM.

Part: INTERCOSTAL — CRACKED (FWD CARGO BAY) · airframe 41,786 hrs · 24,814 cycles

FORWARD CARGO INTERCOSTAL CRACKED ABOVE STR 26L AT STA 500A. / REMOVED AND REPLACED INTERCOSTAL AT STA. 500A-500B ABOVE STR 26L IAW SRM 51-40-02. SEE TASK AND WIPS FOR INDIVIDUAL SIGN OFFS.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,786 hrs · 24,814 cycles

FORWARD CARGO STRINGER CLIP CRACKED AT BS 500D, STR 19R. R&R CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,786 hrs · 24,814 cycles

AFT CARGO COMPARTMENT RT WALL SUPPORT IN LAV TANK AREA ANGLE CRACKED AT BS 867, LBL 10. R&R ANGLE PER SRM.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 41,786 hrs · 24,814 cycles

AFT CARGO; LEFT HAND TRANSITION ANGLE; FROM STATION 727D TO 807; HAS MULTIPLE AREAS OF CORROSION. / REMOVED CORROSION AT MARKED AREAS AND IS OUT OF LIMITS I/A/W SRM 53-00-53-1A-2. CUT OUT DAMAGED AREA FROM STATION 727C+7 TO 814 LBL 24 I/A/W SRM 53-00-53-2R-5. REMOVED AND REPLACED TRANSITION ANGLE FROM STA.727C+10 TO STA.807+10 PER SRM.53-00-53-2R-5

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,786 hrs · 24,814 cycles

INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, RBL 9. R&R ANGLE PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,786 hrs · 24,814 cycles

INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, BETWEEN LBL 12 TO LBL 13. R&R ANGLE PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,786 hrs · 24,814 cycles

INTERCOSTAL CRACKED BETWEEN BS 500B TO BS 500C, STR 25L. R&R INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,786 hrs · 24,814 cycles

INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520, BL 0. R&R INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,786 hrs · 24,814 cycles

INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, BL 0. R&R ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,786 hrs · 24,814 cycles

GALLEY FLOORBEAM CORRODED AT BS 986, LBL 44. REPAIRED BEAM PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 41,786 hrs · 24,814 cycles

AFT GALLEY WEB CORRODED AT BS 1026, LBL 18.5. R&R WEB PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,786 hrs · 24,814 cycles

INTERCOSTAL CRACKED AT BS 328, RBL 35. R&R INTERCOSTAL PER SRM.

Part: SPLICE STRAP — CORRODED (AFT CARGO BAY) · airframe 41,786 hrs · 24,814 cycles

AFT CARGO FLOOR BOARD STRAP SPLICE IS CORRODED AT STA 772 / R&R AFT CARGO FLOOR BOARD STRAP SPLICE AT STA 772 PER SRM 51-40-02

Part: SPLICE STRAP — CORRODED (AFT CARGO BAY) · airframe 41,786 hrs · 24,814 cycles

AFT CARGO FLOOR BOARD STRAP SPLICE IS CORRODED AT STA 887. / REMOVED AND REPLACED SPLICE STRAP PER SRM 51-40-02. SEE INDIVIDUAL WIPS FOR PROGRESSION.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,786 hrs · 24,814 cycles

FORWARD GALLEY DOOR SURROUND STRUCTURE STRINGER CLIP CRACKED EAT BS 277, STR 10R. R&R CLIP IAW SRM.

Part: ANGLE — CRACKED (GALLEY DOOR) · airframe 41,786 hrs · 24,814 cycles

FORWARD GALLEY DOOR L ANGLE CRACKED AT BS 294.5, STR 17L. R&R L ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,786 hrs · 24,814 cycles

R2 DOOR THRESHOLD Z ANGLE CORRODED ON UPPER SURFACE BETWEEN BS 960 TO BS 980. R&R Z ANGLE IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,786 hrs · 24,814 cycles

LT HORIZONTAL STABILIZER INSPAR RIB CRACKED ON VERTICAL STIFFENER, 19" AFT OF FORWARD SPAR STAB STA 120.30. REPAIRED RIB PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,786 hrs · 24,814 cycles

STRINGER CLIP CRACKED AT BS 500D, STR 19L. R&R CLIP PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,786 hrs · 24,814 cycles

LT HORIZONTAL STABILIZER INSPAR RIB CRACKED ON VERTICAL STIFFENER 27" AFT OF FORWARD SPAR AT STAB STA 120.30. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 41,786 hrs · 24,814 cycles

LT HORIZONTAL STABILIZER INSPAR RIB CRACKED ON VERTICAL STIFFENER, 36" AFT OF FORWARD SPAR STAB STA 120.30. REPAIRED RIB PER SRM.

Part: FLOORBEAM — CORRODED (MAIN CABIN) · airframe 41,786 hrs · 24,814 cycles

GALLEY FLOOR BEAM AT STA. 986 RBL 44 HAS EXFOLIATED INNER GRANULAR CORROSION AT FASTENER HOLE.((MARKED) / REPAIRED FLOOR BEAM UPPER CHORD AT STA 986.5 PER EA 1-753-32834 SEE EA FOR INDIVIDUAL WORK. C/W EA 1-753-32834

Part: TRANSITION PANEL — CORRODED (FWD CARGO BAY) · airframe 41,786 hrs · 24,814 cycles

THE FWD CARGO COMPARTMENT L/H TRANSITION ANGLE HAS CORROSION AROUND THE FASTENER HOLES FROM STA 509 TO 500B +11. / WP:E41753-CHAPPA; LEE - 06/20/2018 09:28 COMPLETE: REMOVED AND REPLACED DAMAGED SECTION OF L/H TRANSITION ANGLE FROM STA. 480 TO STA. 500D PER SRM 53-00-53-2R-5. SEE INDIVIDUAL SUB TASKS AND WIPS FOR PROGRESSION.

Part: PANEL — CRACKED (LT WING) · airframe 41,786 hrs · 24,814 cycles

LEFT WING PANEL 561AB HAS SEVERAL SCREW HOLES BULGEDAND CRACKING ON LEADING EDGE UNDER SEAL AREA MARKED / REPAIRED HOLES PER SRM 51-70-04; REPAIR #9. RESTORED FINISH PER AMM 51-21-73 AND AMM 51-21-81.

Part: LENS — CRACKED (CABIN) · airframe 41,786 hrs · 24,814 cycles

LT CLEAR EMERGENCY LIGHT LENS CRACKED ABOVE SEATS BETWEEN ROW 14 TO ROW 24. R&R LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 41,786 hrs · 24,814 cycles

RT CLEAR EMERGENCY LIGHT LENS CRACKED ABOVE SEATS BETWEEN ROW 13 TO ROW 19. R&R LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 41,786 hrs · 24,814 cycles

LT EMERGENCY LIGHT LENS CRACKED AT ROW 1. R&R LENS PER AMM.

Part: LENS — CRACKED (CABIN) · airframe 41,786 hrs · 24,814 cycles

LT EMERGENCY LIGHT LENS CRACKED AT ROW 9. R&R LENS PER MM.

Part: RETAINER — LOOSE (R1 DOOR GIRT BAR) · airframe 41,363 hrs · 24,552 cycles

R1 DOOR SLIDE FWD GIRT BAR RETAINER LOOSE. SECURED RETAINER IAW MM.

Part: RETAINER — LOOSE (R1 DOOR GIRT BAR) · airframe 41,363 hrs · 24,552 cycles

R1 DOOR SLIDE AFT GIRT BAR RETAINER LOOSE. SECURED RETAINER IAW MM.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 40,855 hrs · 24,246 cycles

R1 DOOR EMERGENCY LIGHT IN THE LOWER FORWARD CORNER INOPERATIVE. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: HANDLE — BROKEN (L2 DOOR) · airframe 39,971 hrs · 23,705 cycles

L2 DOOR ASSIST HANDLE BROKEN. R&R HANDLE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,277 hrs · 23,256 cycles

R2 DOOR OUTER SIGN LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,277 hrs · 23,256 cycles

R2 DOOR INNER SIGN INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,277 hrs · 23,256 cycles

AFT OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 38,896 hrs · 23,029 cycles

CABIN FLOOR INTERCOSTAL LOCATED BETWEEN STA 344 AND STA 360 AT LBL 0 IS CRACKED. / REMOVED AND REPLACED REF SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 38,896 hrs · 23,029 cycles

CABIN FLOOR INTERCOSTAL LOCATED BETWEEN STA 312 AND STA 328 ON THE LH SIDE BELOW THE FWD. ENTRY DOORWAY IS CRACKED. / REMOVED AND REPLACED REF SRM 51-40-02.

Part: PANEL — DEFECTIVE (COCKPIT) · airframe 36,762 hrs · 21,755 cycles

DIVERSION, SHORTLY AFTER LEVELING AT CRUISE, HEARD A POP FOLLOWED BY NR 1 FORWARD AND NR 2 AFT FUEL PUMP LOW PRESSURE LIGHTS ILLUMINATED, AS WELL AS FORWARD LEFT AND RIGHT SIDE WINDOW HEAT OVERHEAT LIGHTS ON. R&R PG1 PANEL PER AMM.

Part: PROBE — LEAKING (FUEL SYSTEM) · airframe 35,896 hrs · 21,234 cycles

NR 2 MAIN TANK HAD POSSIBLE FUEL LEAK, LEFT MAIN AT 8500 RIGHT MAIN AT 8480. AT 1505Z LEFT MAIN AT 8100 RIGHT MAIN AT 7720 - 380LB IMBALANCE IN 14 MINUTES. COMPLIED WITH QRH AND SHUT DOWN NR 2. FUEL FLOW AT FL 370 WAS DEAD EVEN. CENTER TANKS WERE BEING USE PRIOR TO QRH AND NR 2 MAIN WAS NOTICEABLY DECREASING FUEL QUANTITY WHERE NR 1 MAIN REMAINED AS EXPECTED WITH CENTERS ON.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 35,452 hrs · 20,982 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITIONED. REPOSITIONED SLIDE IAW MAINTENANCE.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 35,080 hrs · 20,779 cycles

RIGHT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 35,080 hrs · 20,779 cycles

LOWER COMPOSITE WEB CRACKED AT BS 663, BETWEEN RBL 30 TO RBL 33. REPAIRED WEB IAW EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,362 hrs · 19,225 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1669. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,362 hrs · 19,225 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1672. R & R BATTERY PACK IAW AMM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 32,362 hrs · 19,225 cycles

R1 DOOR SLIDE, AFT GIRT BAR HOOK LOOSE. SECURED HOOK IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,362 hrs · 19,225 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1673. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,362 hrs · 19,225 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1670. R & R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,839 hrs · 18,365 cycles

R2 DOOR EMER EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 30,096 hrs · 17,932 cycles

FORWARD RT EMER LIGHT BATTERY PACK FAILED LONG TEST. R & R BATTERY IAW AMM.

Part: FLAP — CRACKED (RT WING) · airframe 29,213 hrs · 17,428 cycles

RIGHT WING INBD LE FLAP CRACKED. R & R LE FLAP ASSEMBLY IAW MM.

Part: LIGHT — UNSECURE (CABIN) · airframe 28,277 hrs · 16,872 cycles

R1 DOOR ABOVE EMER EXIT LIGHT INOPERATIVE. SECURED LIGHT IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 28,277 hrs · 16,872 cycles

EMERGENCY EXIT LIGHT ON AFT WALL OF FWD LAVATORY LENS BROKEN. R & R LENS IAW MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,277 hrs · 16,872 cycles

FLOORBEAM CRACKED AT STATION 727B, RBL 45. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,277 hrs · 16,872 cycles

LONGITUDINAL FLOORBEAM, INBD FLANGE CRACKED AT BS 727B LBL 45. REPAIRED FLANGE IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,277 hrs · 16,872 cycles

LONGITUDINAL FLOORBEAM INBD FLANGE CRACKED AT BS 727B RBL 45. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,277 hrs · 16,872 cycles

LONGITUDINAL FLOORBEAM OTBD FLANGE CRACKED AT BS 727B RBL 24. REPAIRED FLANGE IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 28,277 hrs · 16,872 cycles

CENTER WING WEB CRACKED AT STATION 663, LBL 42. REPAIRED WEB IAW SRM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 28,277 hrs · 16,872 cycles

LEFT NR 3 COCKPIT WINDOW FRAME POST E - F, 2ND HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW SI.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 28,277 hrs · 16,872 cycles

AFT CARGO COMPARTMENT Z ANGLE DAMAGED AT STATION 727D+10, LBL 22. REPAIRED Z ANGLE IAW SRM.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 28,277 hrs · 16,872 cycles

RIGHT NR 3 COCKPIT WINDOW FRAME POST E - F 2ND HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW SI.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,277 hrs · 16,872 cycles

AFT CARGO COMPARTMENT Z ANGLE CORRODED BETWEEN STATION 747 TO 767, RBL 22. R & R Z ANGLE IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 28,277 hrs · 16,872 cycles

RIGHT HORIZONTAL STABILIZER RIB STIFFENER CRACKED AT STATION 92.70. REPAIRED STIFFENER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,277 hrs · 16,872 cycles

RIGHT HORIZONTAL STABILIZER RIB STIFFENER CRACKED AT STATION 120.30. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,277 hrs · 16,872 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70. REPAIRED RIB IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,867 hrs · 16,633 cycles

LEFT EXTERIOR EMERGENCY LIGHT NR 3 INOPERATIVE. RELAMPED IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 27,243 hrs · 16,273 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS ASSEMBLY IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 27,178 hrs · 16,237 cycles

R2 DOOR EMERGENCY EXIT LENS BROKEN. R & R LENS IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 24,049 hrs · 14,383 cycles

FWD ENTRY DOOR EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT LIGHT ASSY IAW M/M.

Part: LENS — BROKEN (CABIN) · airframe 23,964 hrs · 14,326 cycles

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

Part: IDG — FAULTY (NR 1 ENGINE) · airframe 23,358 hrs · 13,948 cycles

DIVERSION -- FUEL TANKS BOOST PUMPS LOW PRESS LIGHTS INDICATIOS, LEFT FWD & RIGHT FWD COCKPIT WINDOWS OVHT LIGHTS IND, ACARS INOP. ALL OTHER INDICATIONS NORMAL. FOUND TRANSFER BUS SEC-2 C/B TRIPPED. REMOVED AND REPLACED NR 1 ENGINE IDG & GCU.

Part: COVER — BROKEN (CABIN) · airframe 21,741 hrs · 12,942 cycles

LEFT EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,648 hrs · 12,895 cycles

FWD EEPLS INOP. RELAMPED EEPLS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 21,648 hrs · 12,895 cycles

EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER M/M.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,371 hrs · 12,727 cycles

FLOORBEAM CORRODED AT BS 767+7 , LBL 8.1. REPAIRED BEAM IAW EA.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 21,371 hrs · 12,727 cycles

Z-CHANNEL CORRODED AT BS 907. REPAIRED Z-CHANNEL IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,371 hrs · 12,727 cycles

RIGHT HORIZONTAL LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,371 hrs · 12,727 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 21,371 hrs · 12,727 cycles

LEFT HORIZONTAL LOWER SKIN CRACKED AT STA 175.5. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,931 hrs · 12,464 cycles

EMERGENCY EGRESS LIGHT INOP AT ROW 2. REMOVED AND REPLACED LIGHT IAW MM.

Part: BRACKET — BROKEN (L1 DOOR) · airframe 18,747 hrs · 11,203 cycles

L1 DOOR EMERGENCY EVAC SLIDE BRACKET LOOSE. SECURED BRACKET PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 18,245 hrs · 10,914 cycles

CENTER OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: LENS — BROKEN (CABIN) · airframe 18,019 hrs · 10,777 cycles

L1 DOOR EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 17,293 hrs · 10,337 cycles

R2 DOOR LOWER EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 17,088 hrs · 10,219 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 16,650 hrs · 9,933 cycles

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

Part: WIRE — LOOSE (CABIN) · airframe 16,511 hrs · 9,855 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS INOP AT FWD END. SECURED EEPLS WIRING PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 16,107 hrs · 9,622 cycles

LT OVERWING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER EPR MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 15,347 hrs · 9,180 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 15,155 hrs · 9,066 cycles

EMERGENCY LIGHTS ARE BROKEN AT ROW 1. REMOVED & REPLACED EMERGENCY LIGHTS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 13,684 hrs · 8,190 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS BROKEN AT ROW 4. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,684 hrs · 8,190 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 4. RELAMPED PER MM.

Part: COVER — LOOSE (L1 DOOR) · airframe 13,546 hrs · 8,108 cycles

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

Part: LENS — MISSING (CABIN) · airframe 12,654 hrs · 7,541 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (SLIDE GAUGE) · airframe 12,528 hrs · 7,465 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INSPECTION WINDOW CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: SIGN — BROKEN (EMEGENCY LIGHTS) · airframe 10,308 hrs · 6,085 cycles

AFT CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 9,826 hrs · 5,799 cycles

EEPLS LIGHT BROKEN NEAR FWD GALLEY. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 9,764 hrs · 5,757 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 8,934 hrs · 5,262 cycles

R1 DOOR AFT GIRT BAR HOOK LOOSE. REPLACED HOOK PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 5,743 hrs · 3,313 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 5,011 hrs · 2,895 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LENS — LOOSE (CABIN) · airframe 5,011 hrs · 2,895 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 4,768 hrs · 2,740 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 4,759 hrs · 2,735 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 4,661 hrs · 2,675 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — MISSING (CABIN) · airframe 1,772 hrs · 989 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 15 ABC. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 1,134 hrs · 639 cycles

EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM.