N493WN

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 62,520 hrs · 37,424 cycles

WHILE AT CRUISE WITH FUEL IN THE CENTER TANK AND CENTER TANK PUMPS ON FUEL BEGAN TO DECREASE FROM #1 TANK. UPON RUNNNG THE QRH DETERMINED A FUEL LEAK BY TURNING OFF THE CENTER PUMPS AND WATCHING FUEL RAPIDLY DECREASE FROM #1 TANK.<[01] OP/LEAK CHECKED ALL FUEL SYSTEM TANKS; NO DEFECT NOTED REF AMM?S 28-22-00;12-11-00 & FIM 28-21 TASK 803

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 61,302 hrs · 36,661 cycles

MT1669 FAILED BATTERY CAPACITY CHECK. R & R MT1669 BATTERY PACK PER AMM 33-51-06.

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 61,302 hrs · 36,661 cycles

MT1673 FAILED CAPACITY CHECK. R & R MT1673 BATTERY PACK PER AMM 33-51-06.

Part: BATTERY — FAILED (ZN 200 FUS TOP) · airframe 61,302 hrs · 36,661 cycles

MT1672 FAILED CAPACITY CHECK. R & R MT1672 BATTERY SUPPLY PER AMM 33-51-06.

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 62,493 hrs · 37,374 cycles

FORWARD SERVICE DOOR ESCAPE SLIDE EXCESS MATERIAL<[01] ADJUSTED SLIDE PER AMM 25-66-01

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 61,152 hrs · 36,566 cycles

REFERENCE TTG8Q0064NT9 FWD ENTRY DOOR SLIDE REPLACEMENT. PN 5A3307-9 REQUIRED FOR REPLACEMENT.<[01] ORDERED PART. REF TTG8Q0064NT9 FOR MT REPLACEMENT

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 61,152 hrs · 36,566 cycles

REFERENCE TTG8Q0064NT2 FWD SERVICE DOOR SLIDE REPLACEMENT. PN 5A3307-9 REQUIRED<[01] ORDERED PART. REF TTG8Q0064NT2 FOR MT REPLACEMENT

Part: STOP — LOCKED (ZN 200 FUS TOP) · airframe 60,331 hrs · 36,033 cycles

SEAT 11D RECLINES. SHOULD BE LOCKED UP FOR EXIT ROW<[01] LOCKED OUT THE RECLINE STOP ON SEAT 11D PER CMM 25-21-45.;[02] VERIFIED SEAT RECLINE IS LOCKED IAW CMM 25-21-45

Part: LENS — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 60,331 hrs · 36,033 cycles

LH OVERWING EMERGENCY EXIT LIGHT LENS IMPORPERLY INSTALLED<[01] ADJUSTED LH OVERWING EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01. OK FOR SERVICE.;[02] C/W THE BUY ON THE L/H EMER EXIT LIGHT LENS

Part: NONE — BURNED (PAX CABIN) · airframe 58,674 hrs · 34,928 cycles

BURNED EMERGENCY EXIT LIGHT BULBS ON SIDEWALL PANEL 231YJW AT PASSENGER CABIN 2022-410336 / [01] REPLACED EMERGENCY EXIT LIGHT BULBS ON SIDEWALL PANEL 231YJW AT PASSENGER CABIN I.A.W. B737-700 AMM 33-51-01-960-801. TEST IS OK.;[02] CERTIFIED WORK PERFORMED.

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 58,674 hrs · 34,928 cycles

CRACK WEB - INTERCOSTAL LOCATED BS500A TO 500B STR 26R FWD CARGO COMPARTMENT 2022-410309 / [01] PERFORMED DVI ON WEB - INTERCOSTAL LOCATED BS500A TO BS 500B STR 26R FWD CARGO COMPARTMENT AND NOT FOUND CRACK ONLY PROTECTIVE TREATMENT DAMAGED IAW SRM B737-700 51-10-02 AND APPLIED PROTECTIVE TREATMENT IAW SRM B737-700 51-20-01;[02] PERFORMED DVI ON WEB - INTERCOSTAL LOCATED BS500A TO BS 500B STR 26R FWD CARGO COMPARTMENT AND NOT FOUND CRACK ONLY PROTECTIVE TREATMENT DAMAGED IAW SRM B737-700 51-10-02 AND APPLIED PROTECTIVE TREATMENT IAW SRM B737-700 51-20-01

Part: NONE — ELONGATED (FWD CARGO BAY) · airframe 58,674 hrs · 34,928 cycles

ELONGATED HOLE WEB - INTERCOSTAL LOCATED BTW STA 400 TO STA 420 STRINGER 25L AT FWD CARGO COMPARTMENT 2022-410300 / [01] REPLACED WEB INTERCOSTAL LOCATED BTW STA 400 TO STA 420 STRINGER 25L AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG 143A7505 REV:B;[02] CORRECTED STEP 1. REPLACED WEB INTERCOSTAL LOCATED BTW STA 400 TO STA 420 STRINGER 25L AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG 143A7505 REV:B.SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] REPLACED WEB INTERCOSTAL LOCATED BTW STA 400 TO STA 420 STRINGER 25L AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 AND DWG 143A7505 REV:B.<BR>RII <BR>SEE INDIVIDUAL STEP SIGN OFFS BELOW

Part: ANGLE — CRACKED (CABIN FLOOR) · airframe 58,674 hrs · 34,928 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BTW BS 380 TO BS 400 AT BL 0 AT PASSENGER CABIN 2022-410231 / [01] REPLACED ANGLE FLOOR STRUCTURE LOCATED BTW BS 380 TO BS 400 AT BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING #143A5400 REV :D SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATED BTW BS 380 TO BS 400 AT BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING #143A5400 REV :D SEE INDIVIDUAL SIGN OFF BELOW.. RII ITEM

Part: ANGLE — CRACKED (FWD GALLEY FLOOR) · airframe 58,674 hrs · 34,928 cycles

CRACK EXTERNAL SKIN SERVICE DOOR R1 DEPRESSOR ANGLE UPPER AT FWD GALLEY AREA 2022-410232 / [01] REPLACED DEPRESSOR ANGLE UPPER SERVICE DOOR R1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND 51-40-02. SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED DEPRESSOR ANGLE UPPER SERVICE DOOR R1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND 51-40-02. SEE INDIVIDUAL SIGNOFF BELOW ITEM RII

Part: WEB — CORRODED (FWD GALLEY FLOOR) · airframe 58,674 hrs · 34,928 cycles

CORROSION IN WEB LOCATED BTW BSTA 294 AND BSTA 310 WL208.1 LBL50 AT FWD GALLEY AREA 2022-410229 / [01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN: 130066701; DUE DATE: 08-APR-23;[02] EVALUATED REWORKED AREAS LOCATED BTW BSTA 294 AND BSTA 310 WL208.1 LBL50 AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW B737-700 SRM 53-10-15-1A-1 PARAGRAPH 4D STEP (2). FIGURE 108 SHEET 5 SEE INDIVIDUAL SING OFFS STEPS BELOW;[03] CORRECTED STEP 2; EVALUATED REWORK AREAS LOCATED BTW BSTA 294 AND BSTA 310 WL208.1 LBL50 AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW B737-700 SRM 53-10-15-1A-1 PARAGRAPH 4D STEP (2). FIGURE 108 SHEET 5 SEE INDIVIDUAL SING OFFS STEPS BELOW;[04] EVALUATED REWORK AREAS LOCATED BTW BSTA 294 AND BSTA 310 WL208.1 LBL50 AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW B737-700 SRM 53-10-15-1A-1 PARAGRAPH 4D STEP (2). FIGURE 108 SHEET 5 .SEE INDIVIDUAL SING OFFS STEPS BELOW.

Part: NONE — CRACKED (RH WING) · airframe 58,674 hrs · 34,928 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 268 AT RT WING 2022-410204 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 268 AT RT WING I.A.W.B737-700 SRM 51-40-02 AND DRAWING # 116A2781 REV ?B?;[02] COMPLETE TASK CERTIFIED

Part: ANGLE — CRACKED (PAX CABIN) · airframe 58,674 hrs · 34,928 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 695 BL 0 AND WL 208.1 AT PASSENGER CABIN 2022-410201 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES500000; S/N: 112820015; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820015; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23.;[03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23.;[04] REPLACED ANGLE FLOOR STRUCTURE LOCATED ON BS 695 BL 0 AND WL 208.1 AT PASSENGER CABIN I.A.W.B737-700 SRM 51-40-02 AND DRAWING #273A9110 REV?A? SEE INDIVIDUAL SING OFF BELLOW;[05] REPLACED ANGLE FLOOR STRUCTURE LOCATED ON BS 695 BL 0 AND WL 208.1 AT PASSENGER CABIN I.A.W.B737-700 SRM 51-40-02 AND DRAWING #273A9110 REV?A? SEE INDIVIDUAL SING OFF BELLOW ITEM RII

Part: NONE — CRACKED (LH WING) · airframe 58,674 hrs · 34,928 cycles

CRACK ON CORRUGATED PLATE LOCATED IRSS 215 OF TRAILING EDGE LT WING 2022-410197 / [01] REPLACED CORRUGATED PLATE LOCATED IRSS 215 OF TRAILING EDGE LT WING I.A.W.B737-700 SRM 51-40-02 AND DRAWING #115A2001 REV ?A?.;[02] TASK COMPLETED

Part: ANGLE — CRACKED (CABIN FLOOR) · airframe 58,674 hrs · 34,928 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 AND WL 208.1 AT PASSENGER CABIN 2022-410203 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE: 01-FEB-23;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING # 273A9110 REV : A . SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED ANGLE FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING # 273A9110 REV : A . SEE INDIVIDUAL SIGN OFF BELOW RII COMPLETED

Part: NONE — CRACKED (LH WING) · airframe 58,674 hrs · 34,928 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT LT WING 2022-410188 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT LT WING I.A.W.B737-700 SRM 51-40-02 AND DRAWING# 115A2001 REV ?;[02] COMPLETE TASK CERTIFIED

Part: NONE — WORN · airframe 58,674 hrs · 34,928 cycles

WEAR ON GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA 2022-409815 / [01] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA I.A.W. B737-700 AMM 25-66-02-400-801 STEP 3.D.(1) ITEM (H) THRU (I);[02] REPLACED GIRT BAR FITTING HARDWARE ENTRY AND SERVICE DOOR AT FWD GALLEY AREA I.A.W. B737-700 AMM 25-66-02-400-801 STEP 3.D.(1) ITEM (H) THRU (I)

Part: NONE — CORRODED (AFT CARGO BAY) · airframe 58,674 hrs · 34,928 cycles

CORROSION FLOOR STRUCTURE SHIELD PLATE BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 157 AT AFT CARGO COMPARTMENT 2022-410070 / [01] REPLACED SHIELD PLATE BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 157 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9. SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1 REPLACED SHIELD PLATE BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 157 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9. SEE INDIVIDUAL SIGN-OFF BELOW;[03] TASK CARD COMPLETED <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: RETAINER — CRACKED (RH WING) · airframe 58,674 hrs · 34,928 cycles

CRACK ACCESS PANEL 642BB RUBSTRIP RETAINER SEAL AT RT WING 2022-410084 / [01] REPLACED RUBSTRIP RETAINER SEAL LOC. AT RT WING IAW B737-700 SRM 51-40-02; DWG#113A9350 REV:F AND 51-10-02;[02] TASK CARD COMPLETED

Part: ANGLE — CRACKED (RH WING) · airframe 58,674 hrs · 34,928 cycles

CRACK TRAILING EDGE SUPPER ANGLE LOCATED WS275 AT RT WING 2022-410103 / [01] TRAILING EDGE SUPPER ANGLE LOCATED WS275 AT RT WING IAW SRM 737-700 51-40-02 AND DWG 115A6299 REV -. SEE INDIVIDUAL SIGN OF BELLOW.;[02] TASK CARD COMPLETED <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: SUPPORT ANGLE — CORRODED (RH WING) · airframe 58,674 hrs · 34,928 cycles

CORROSION FUEL BOOST PUMP SUPPORT ANGLE LOCATED IRSS145 WBL94.24 AND WL183 AT RT WING 2022-410127 / [01] REPLACED FUEL BOOST PUMP SUPPORT ANGLE LOCATED IRSS145 WBL94.24 AND WL183 AT RT WING IAW B737-700 AMM 28-22-41-400-802 AND RSM 51-40-02-0G-0;[02] CORRECTED STEP 1<BR>REPLACED FUEL BOOST PUMP SUPPORT ANGLE LOCATED IRSS145 WBL94.24 AND WL183 AT RT WING IAW B737-700 AMM 28-22-41-400-802 AND SRM 51-40-02-0G-0;[03] REPLACED FUEL BOOST PUMP SUPPORT ANGLE LOCATED IRSS145 WBL94.24 AND WL183 AT RT WING IAW B737-700 AMM 28-22-41-400-802 AND SRM 51-40-02-0G-0

Part: NONE — CRACKED (RH WING) · airframe 58,674 hrs · 34,928 cycles

CRACK REAR SPAR CORRUGATED PLATE LOCATE BETWEEN WS204 TO WS228 AT RT WING 2022-410120 / [01] REPLACED REAR SPAR CORRUGATED PLATE LOCATE BETWEEN WS204 TO WS228 AT RT WING I.A.W. B737-700 SRM 51-40-02 AND DRAWING # 115A2001 REV ?A?;[02] TASK COMPLETED

Part: SUPPORT BRACKET — CRACKED (RH WING) · airframe 58,674 hrs · 34,928 cycles

CRACK SUPPORT BRACKET TRAILING EDGE LOCATED WS253 RT WING 2022410108 / [01] REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED WS253 RT WING IAW B737-700 SRM 51-40-05 AND DRAWING# 115A2930 REV. - REPLACED BRACKET DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 57-51-02. TOOK MEASURE OF CRACK ARE L=0.750 INCH TOOL USED P/N: 500-196-30; S/N A21033429; DUE DATE 02-NOV-22;[02] CORRECTED STEP 1.<BR>REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED WS253 RT WING IAW B737-700 SRM 51-10-02 ITEM 9. AND DRAWING# 115A2930 REV. - REPLACED BRACKET DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 57-51-02. TOOK MEASURE OF CRACK ARE L=0.750 INCH TOOL USED P/N: 500-196-30; S/N A21033429; DUE DATE 02-NOV-22;[03] CORRECTED STEP 1 AND 2.<BR>REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED WS253 RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING# 115A2930 REV. - REPLACED BRACKET DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 57-51-02. TOOK MEASURE OF CRACK ARE L=0.750 INCH TOOL USED P/N: 500-196-30; S/N A21033429; DUE DATE 02-NOV-22. SEE INDIVIDUAL SIGN-OFFS BELOW;[04] REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED WS253 RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING# 115A2930 REV. - REPLACED BRACKET DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 57-51-02. TOOK MEASURE OF CRACK ARE L=0.750 INCH TOOL USED P/N: 500-196-30; S/N A21033429; DUE DATE 02-NOV-22. SEE INDIVIDUAL SIGN-OFFS BELOW

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 58,674 hrs · 34,928 cycles

CORROSION ANGLE BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 157 AT AFT CARGO COMPARTMENT 2022-410074 / [01] REPLACED ANGLE BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 157 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; DWG # 146A0081. REV. ?A?. AND DWG # 146A8123. REV. ?-?. SEE INDIVIDUAL SIGN-OFF BELOW ITEM RII;[02] REPLACED ANGLE BTW BS 767 TO BS 787 AT LEVEL STR 25R AND WL 157 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; DWG # 146A0081. REV. ?A?. AND DWG # 146A8123. REV. ?-?. SEE INDIVIDUAL SIGN-OFF BELOW ITEM RII

Part: NONE — CORRODED (AFT CARGO BAY) · airframe 58,674 hrs · 34,928 cycles

CORROSION WEB - INTERCOSTAL LOCATED BTW BS 747 TO BS 767 AT LEVEL STR 25R AND WL 157 AT AFT CARGO COMPARTMENT 2022-410081 / [01] REPLACED WEB - INTERCOSTAL LOCATED BTW BS 747 TO BS 767 AT LEVEL STR 25R AND WL 157 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DRAWING #146A7500 REV:A;[02] ALCIDES MIRANDA (TECHNICIAN); 24-AUG-2022 20:09 UTC <BR>CORRECTED STEP 1 REPLACED WEB - INTERCOSTAL LOCATED BTW BS 747 TO BS 767 AT LEVEL STR 25R AND WL 157 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DRAWING #146A7500 REV:A. SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED WEB - INTERCOSTAL LOCATED BTW BS 747 TO BS 767 AT LEVEL STR 25R AND WL 157 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DRAWING #146A7500 REV:A. SEE INDIVIDUAL SIGN-OFF BELOW ITEM RII

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 58,674 hrs · 34,928 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL STR 25R AT WL 157 AT AFT CARGO COMPARTMENT 2022-410066 / [01] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL STR 25R AT WL 157 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 146A7500 REV A; SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: NONE — CORRODED (AFT GALLEY) · airframe 58,674 hrs · 34,928 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BS 986.5 WL208.1 AND LBL 43 AT AFT GALLEY AREA 2022-409984 / [01] EDDY CURRENT EQUIPMENT USED: P/N: NORTEC 600D; S/N: 60009161631<BR>DUE DATE: 03-DEC-22;[02] TOOL USED: FLAPSPEED; PN: FPK-PR0-104; SN: PR0-3344; DUE DATE: 06/MAY/23.;[03] TOOL USED: EDDY CURRENT EQUIPMENT; PN: 600D; SN: 200048001; DUE DATE: 30-MAY-23;[04] PERFORMED REPAIR ON FLOOR STRUCTURE BEAM LOCATED BS 986.5 WL 208.1 AND LBL 43 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 .SEE INDIVIDUAL SIGN OFF BELOW;[05] PERFORMED REPAIR ON FLOOR STRUCTURE BEAM LOCATED BS 986.5 WL 208.1 AND LBL 43 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; RII .SEE INDIVIDUAL SIGN OFF BELOW

Part: INTERCOSTAL — CORRODED (AFT GALLEY) · airframe 58,674 hrs · 34,928 cycles

CORROSION FLOOR STRUCTURE INTERCOSTAL LOCATED BETWEEN BS947.5 TO BS967 WL208.1 RBL8 AT AFT GALLEY AREA 2022-409992 / [01] REPLACED INTERCOSTAL LOCATED BETWEEN BS947.5 TO BS967 WL208.1 RBL8 AT AFT GALLEY AREA. IAW B737-700 SRM: 51-10-02 AND DWG 147A5760 REV._;[02] CORRECTED STEP 1; REPLACED INTERCOSTAL LOCATED BETWEEN BS947.5 TO BS967 WL208.1 RBL8 AT AFT GALLEY AREA. IAW B737-700 SRM: 51-10-02 AND DWG 147A5760 REV._ SEE INDIVIDUAL SING OFFS BELOW.;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — CORRODED (FWD GALLEY FLOOR) · airframe 58,674 hrs · 34,928 cycles

CORROSION FLOOR BEAM AROUND HOLE LOCATED ON BS344 WL208.1 BL0 AT FWD GALLEY AREA 2022-409983 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600; S/N: 60007161486; DUE DATE: 06-DEC-22;[02] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 130060401; DUE DATE: 26-JAN-23;[03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE: 01-FEB-23;[04] PERFOMED REPAIR ON FLOOR BEAM BS344 BTW LBL 10 TO RBL 10 WL208.1 AT FWD GALLEY AREA IAW EA-22-153-02372 AND EA-22-153-02372 WIP1. SEE INDIVIDUAL SING OFFS STEPS BELOW.;[05] PERFOMED REPAIR ON FLOOR BEAM BS344 BTW LBL 10 TO RBL 10 WL208.1 AT FWD GALLEY AREA IAW EA-22-153-02372 AND EA-22-153-02372 WIP1. SEE INDIVIDUAL SING OFFS STEPS BELOW.

Part: NONE — CORRODED (AFT GALLEY) · airframe 58,674 hrs · 34,928 cycles

CORROSION FLOOR STRUCTURE INNER CHORD LOCATED BETWEEN BS 947.5 TO BS 986.5 WL 208.1 AND RBL 51 AFT GALLEY AND LAV 2022-409988 / [01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 130066701; CAL DUE DATE: 08-APR-23;[02] REWORKED AREA ON FLOOR STRUCTURE INNER CHORD LOCATED BETWEEN BS 947.5 TO BS 986.5 WL 208.1 AND RBL 51 AFT GALLEY AREA EVAULATED AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-70-15-1A-1 PARAGRAPH 4 STEP D (2) FIGURE 103 (SHEET 2). SEE INDIVIDUAL SING OFFS STEP BELOW.;[03] REWORKED AREA ON FLOOR STRUCTURE INNER CHORD LOCATED BETWEEN BS 947.5 TO BS 986.5 WL 208.1 AND RBL 51 AFT GALLEY AREA EVAULATED AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-70-15-1A-1 PARAGRAPH 4 STEP D (2) FIGURE 103 (SHEET 2). SEE INDIVIDUAL SING OFFS STEP BELOW

Part: BRACKET — CRACKED (RH WING) · airframe 58,674 hrs · 34,928 cycles

CRACK ON BRACKET LOCATED IRSS140 AT RT WING 2022-410000 / [01] REPLACED BRACKET LOCATED IRSS140 AT RT WING IAW B737-700 SRM 51-40-02 AND 51-10-02.<BR>TOOL USED CALIPER DIGITAL P/N:50P-197-30 S/N:A21147765 DUE DATE:15-OCT22;[02] TASK CARD COMPLETED

Part: BRACKET — CRACKED (LH WING) · airframe 58,674 hrs · 34,928 cycles

CRACK ON SUPPORT BRACKET LOCATED ORSS 297 AT LT WING 2022-410008 / [01] REMOVED AND REPLACED SUPPORT BRACKET LOCATED ORSS 297 AT LT WING AND FASTENERS IAW B737-700 SRM 51-10-02 AND DRAWING 115A3700 SHEET 31 REV -;[02] TASK CARD COMPLETED

Part: NONE — CORRODED (AFT GALLEY) · airframe 58,674 hrs · 34,928 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BS 986.5 WL 208.1 AND RBL 43 AT AFT GALLEY AREA 2022-409985 / [01] EDDY CURRENT EQUIPMENT USED: P/N: NORTEC 600D; S/N: 60009161631<BR>DUE DATE: 03-DEC-22;[02] TOOL USED: FLAPSPEED; PN: FPK-PR0-104; SN: PR0-3344; DUE DATE: 06/MAY/23.;[03] TOOL USED EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:210138203; DUE DATE:11-APR-23.;[04] PERFORMED REPAIR ON FLOOR STRUCTURE BEAM LOCATED BS 986.5 WL 208.1 AND RBL 43 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 .SEE INDIVIDUAL SIGN OFF BELOW;[05] PERFORMED REPAIR ON FLOOR STRUCTURE BEAM LOCATED BS 986.5 WL 208.1 AND RBL 43 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; RII .SEE INDIVIDUAL SIGN OFF BELOW

Part: INTERCOSTAL — CORRODED (AFT GALLEY) · airframe 58,674 hrs · 34,928 cycles

CORROSION FLOOR STRUCTURE INTERCOSTAL LOCATED BS 947.5 PLUS 4 IN WL 208.1 AND BETWEEN RBL 29 TO RBL 48 AT AFT GALLEY AREA 2022-409991 / [01] REPLACED INTERCOSTAL LOCATED BS 947.5 PLUS 4 IN WL 208.1 AND BETWEEN RBL 29 TO RBL 48 AT AFT GALLEY AREA. IAW B737-700 SRM: 51-10-02 AND DWG: 147A5760 REV._;[02] CORECTED STEP 1; REPLACED INTERCOSTAL LOCATED BS 947.5 PLUS 4 IN WL 208.1 AND BETWEEN RBL 29 TO RBL 48 AT AFT GALLEY AREA. IAW B737-700 SRM: 51-10-02 AND DWG: 147A5760 REV._ SEE INDIVIDUAL SING OFFS BELOW.;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — CORRODED (AFT GALLEY) · airframe 58,674 hrs · 34,928 cycles

CORROSION FLOOR STRUCTURE INNER CHORD LOCATED BETWEEN BS 947.5 TO BS 986.5 WL 208.1 AND LBL 51 AFT GALLEY AND LAV 2022-409987 / [01] TOOL USED: CALIPER; PN: 500-197-30; SN: A21147752; DUE DATE: 06-OCT-22.;[02] REPLACED INNER CHORD LOCATED BETWEEN BS 867.5 TO BS 1006 WL 208.1 AND LBL 51 AFT GALLEY AND LAV IAW B737-700 AND SRM 51-40-02 AND DWG 147A8501 SHEET #39 REV:C.SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] REPLACED INNER CHORD LOCATED BETWEEN BS 867.5 TO BS 1006 WL 208.1 AND LBL 51 AFT GALLEY AND LAV IAW B737-700 AND SRM 51-40-02 AND DWG 147A8501 SHEET #39 REV:C.SEE INDIVIDUAL STEP SIGN OFFS BELOW.. RII ITEM

Part: SKIN PANEL — CRACKED (RH HOR STAB) · airframe 58,674 hrs · 34,928 cycles

CRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 AND 16 INCH. FROM FRONT SPAR. CRACK LENGTH = 0.700 INCH. APPROX. 2022-409904 / [01] EDDY CURRENT EQUIPMENT USED: P/N: NORTEC 600D; S/N: 60009161631<BR>DUE DATE: 03-DEC-22;[02] PERFORMED PERMANENT REPAIR ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 AND 16 INCH IAW B737-700 SRM 55-10-01-2R-11. REPAIR 11; SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2. PERFORMED REPAIR ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 AND 16 INCH IAW B737-700 SRM 55-10-01-2R-11. REPAIR 11; SEE INDIVIDUAL SIGN OFF BELOW.;[04] TASK CARD COMPLETED <BR>SEE INDIVIDUAL SIGN OFFS BELOW <BR>RII

Part: NONE — CORRODED (FWD GALLEY) · airframe 58,674 hrs · 34,928 cycles

CORROSION FLOOR BEAM LOCATED ON BS312 WL208.1 LBL12 AT FWD GALLEY AREA 2022-409946 / [01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 130066701; CAL DUE DATE: 08-APR-23;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[03] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[04] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES500000; S/N: 112820015; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23.;[05] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820015; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23;[06] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23;[07] TOOL USED RADIUS GAUGE: P/N: S167C; S/N: AE-28534; DUE DATE: 02-FEB-23;[08] PERFORMED REAPAIR ON FLOOR BEAM LOCATED ON BS312 WL208.1 LBL12 AT FWD GALLEY AREA IAW EA-22-153-02384 WIP1 ; EA-22-153-02384 WIP2 AND EA-22-153-02384; SEE INDIVIDUAL SINGOFFS STEPS BELOW.;[09] PERFORMED REAPAIR ON FLOOR BEAM LOCATED ON BS312 WL208.1 LBL12 AT FWD GALLEY AREA IAW EA-22-153-02384 WIP1 ; EA-22-153-02384 WIP2 AND EA-22-153-02384; RII. SEE INDIVIDUAL SINGOFFS STEPS BELOW.

Part: SKIN PANEL — CRACKED (RH HOR STAB) · airframe 58,674 hrs · 34,928 cycles

CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 203.1 AND 23 INCH. FROM FRONT SPAR. CRACK LENGTH = 0.800 INCH. APPROX. 2022-409903 / [01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 190023010; DUE DATE: 14-FEB-23.;[02] ET TOOL USED: PN: MIZ-21C ; SN: 769680; DUE DATE: 07-JUL-23;[03] PERFORMED REPAIR ON HORIZONTAL STABILIZER LOWER SKIN PANEL LOCATED AT STAB STA 203.1 AND 23 INCH. FROM FRONT SPAR I.A.W. EA#22-155-02528-WIP1 AND EA#22-155-02528. SEE INDIVIDUAL SIGN-OFF BELOW;[04] CORRECTED STEP 3<BR>PERFORMED REPAIR ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL LOCATED AT STAB STA 203.1 AND 23 INCH. FROM FRONT SPAR I.A.W. EA#22-155-02528-WIP1 AND EA#22-155-02528. SEE INDIVIDUAL SIGN-OFF BELOW;[05] PERFORMED REPAIR ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL LOCATED AT STAB STA 203.1 AND 23 INCH. FROM FRONT SPAR I.A.W. EA#22-155-02528-WIP1 AND EA#22-155-02528. SEE INDIVIDUAL SIGN-OFF BELOW.<BR>CERTIFIED AS RII.

Part: NONE — CORRODED (FWD GALLEY FLOOR) · airframe 58,674 hrs · 34,928 cycles

CORROSION FLOOR BEAM LOCATED ON BS328 WL208.1 RBL41 AT FWD GALLEY AREA 2022-409932 / [01] TOOL USED: CALIPER; PN: 500-196-30; SN: A21125629; DUE DATE: 24-OCT-22; RADIUS GAUGE; PN: 2204A3; SN: AE-408657; DUE DATE: 14-FEB-23.;[02] PERFORMED PERMANENT REPIAR ON FLOOR BEAM BS 328 I.A.W SRM B737-700 53-10-51-2R-7 REPAIR 7 . SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] CORRECTED STEP 2. PERFORMED PERMANENT REPIAR ON FLOOR BEAM BS 328 WL 208 BTW LBL 1.1 TO RBL 64 I.A.W SRM B737-700 53-10-51-2R-7 REPAIR 7 . SEE INDIVIDUAL STEP SIGN OFFS BELOW;[04] CORRECTED STEP 2. PERFORMED PERMANENT REPIAR ON FLOOR BEAM BS 328 WL 208 BTW LBL 1.1 TO RBL 64 I.A.W SRM B737-700 53-10-51-2R-7 REPAIR 7 . SEE INDIVIDUAL STEP SIGN OFFS BELOW ITEM RII

Part: FRAME — CRACKED (CABIN FLOOR) · airframe 58,674 hrs · 34,928 cycles

CRACK FRAME BS 312 AT LEVEL S-6L WL 282 AT PASSENGER CABIN 2022-409933 / [01] PERFORMED REPAIR LOC. BS 312 FRAME UPPER CHORD AT LBL 33 BETWEEN S-5L AND S-6L) I.A.W.B737-700 EA# M-22-153-01244;[02] PERFORMED REPAIR LOC. BS 312 FRAME UPPER CHORD AT LBL 33 BETWEEN S-5L AND S-6L) I.A.W.B737-700 EA# M-22-153-01244

Part: NONE — CRACKED (FWD GALLEY FLOOR) · airframe 58,674 hrs · 34,928 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS328 TO BS344WL208.1 LBL43 FWD GALLEY AND LAV 2022-409934 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS328 TO BS344WL208.1 LBL43 FWD GALLEY AREA IAW B737-700 SRM 51-10-02;51-40-02 AND DWG 141A5400 REV-. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS328 TO BS344WL208.1 LBL43 FWD GALLEY AREA IAW B737-700 SRM 51-10-02;51-40-02 AND DWG 141A5400 REV-. SEE INDIVIDUAL SIGN OFF BELOW. AS RII.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 58,674 hrs · 34,928 cycles

CRACK ON FWD CORNER SCUFF PLATE IN FWD CARGO DOOR CUT OUT 2022-409967 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N B20189527; DUE DATE 30-NOV-22.;[02] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT (DOOR CUT OUT) IN ACCORDANCE WITH BOEING 737-700; SRM 53-30-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT (DOOR CUT OUT) IN ACCORDANCE WITH BOEING 737-700; SRM 53-30-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW

Part: WEB — CRACKED (FWD GALLEY FLOOR) · airframe 58,674 hrs · 34,928 cycles

CRACK WEB LOCATED BETWEEN BS277 TO BS294.5 WL208.1 BL0 AT FWD GALLEY AREA 2022-409926 / [01] REPLACED WEB LOCATED BETWEEN BS277 TO BS294.5 WL208.1 BL0 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02 AND DWG 141A5400 REV -;[02] TASK CARD COMPLETED <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: SUPPORT BRACKET — CRACKED (AC BAY) · airframe 58,674 hrs · 34,928 cycles

CRACK BODY STATION 540 SUPPORT BRACKET; LBL 8 AT AIR CONDITIONING BAY 2022-409961 / [01] REPLACED BODY STATION 540 SUPPORT BRACKET; LBL 8 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02.;[02] REPLACED BODY STATION 540 SUPPORT BRACKET; LBL 8 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02.

Part: STUB FRAME — CRACKED (CABIN FLOOR) · airframe 58,674 hrs · 34,928 cycles

CRACK FRAME STUB LOCATED AT BS 294.5 AT LEVEL S-17R WL208.1 AT PASSENGER CABIN 2022-409940 / [01] REPLACED NEW FRAME STUB AND FASTENERS LOCATED AT BS 294.5 AT LEVEL S-17R WL 208.1 AT PASSENGER CABIN. I.A.W.B737-700 SRM 51-40-02 AND DRAWING #141A8370 REV?D? SEE INDIVIDUAL SING OFF BELLOW.;[02] REPLACED NEW FRAME STUB AND FASTENERS LOCATED AT BS 294.5 AT LEVEL S-17R WL 208.1 AT PASSENGER CABIN. I.A.W.B737-700 SRM 51-40-02 AND DRAWING #141A8370 REV?D? SEE INDIVIDUAL SING OFF BELLOW.

Part: NONE — CRACKED (AFT CARGO BAY) · airframe 58,674 hrs · 34,928 cycles

CRACK ON AFT CORNER SCUFF PLATE IN AFT CARGO DOOR CUT OUT. 2022-409970 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A21147750;DUE DATE:29-JUN-23.;[02] REPAIRED BY WELDS AFT CORNER SCUFF PLATE OF AFT CARGO DOOR CUT OUT IAW BOEING 737-700 SRM 53-60-15-2R-1; REPAIR 1 PARAGRAPH 4.B. STEPS ( 2 ) TO ( 7 ) AND BAC 5975. SEE INDIVIDUAL SIGN OFF BELOW;[03] JOB TASK COMPLETED.

Part: NONE — CORRODED (FWD GALLEY FLOOR) · airframe 58,674 hrs · 34,928 cycles

CORROSION FLOOR BEAM LOCATED ON BS312 WL208.1 LBL12 AT FWD GALLEY AREA 2022-409946 / [01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 130066701; CAL DUE DATE: 08-APR-23;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[03] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[04] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES500000; S/N: 112820015; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23.;[05] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820015; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23;[06] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23;[07] TOOL USED RADIUS GAUGE: P/N: S167C; S/N: AE-28534; DUE DATE: 02-FEB-23;[08] PERFORMED REAPAIR ON FLOOR BEAM LOCATED ON BS312 WL208.1 LBL12 AT FWD GALLEY AREA IAW EA-22-153-02384 WIP1 ; EA-22-153-02384 WIP2 AND EA-22-153-02384; SEE INDIVIDUAL SINGOFFS STEPS BELOW.;[09] PERFORMED REAPAIR ON FLOOR BEAM LOCATED ON BS312 WL208.1 LBL12 AT FWD GALLEY AREA IAW EA-22-153-02384 WIP1 ; EA-22-153-02384 WIP2 AND EA-22-153-02384; RII. SEE INDIVIDUAL SINGOFFS STEPS BELOW.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 58,674 hrs · 34,928 cycles

CRACK ON AFT CORNER SCUFF PLATE IN FWD CARGO DOOR CUTOUT 2022-409968 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A21147750;DUE DATE:29-JUN-23.;[02] REPAIRED BY WELDS AFT CORNER SCUFF PLATE OF FWD CARGO DOOR IAW BOEING 737-700 SRM 53-30-15-2R-1; REPAIR 1 PARAGRAPH 4.B. STEPS ( 2 ) TO ( 7 ) AND BAC 5975 SEE INDIVIDUAL SIGN OFF BELOW;[03] REPAIRED BY WELDS AFT CORNER SCUFF PLATE OF FWD CARGO DOOR IAW BOEING 737-700 SRM 53-30-15-2R-1; REPAIR 1 PARAGRAPH 4.B. STEPS ( 2 ) TO ( 7 ) AND BAC 5975 SEE INDIVIDUAL SIGN OFF BELOW.COMPLETED

Part: NONE — CRACKED (CABIN FLOOR) · airframe 58,674 hrs · 34,928 cycles

CRACK STRINGER 16L LOCATED BETWEEN BS 294.5 AND BS 303.9 WL 216 AT PASSENGER CABIN 2022-409931 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60007161486; DUE DATE: 06-DEC-22.;[02] PERFORMED REPAIR ON STRINGER 16L BETWEEN BS 294.5 AND BS 303.9 WL 216 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — CRACKED (FWD GALLEY FLOOR) · airframe 58,674 hrs · 34,928 cycles

CRACK ANGLE - SUPPORT LOCATED AT LEVEL S-17R BETWEEN BS 291.5 AND BS 294.5 WL 208.1 AT FWD GALLEY AREA 2022-409938 / [01] REPLACED ANGLE LOCATED AT LEVEL S-17R BETWEEN BS 291.5 AND BS 294.5 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ;51-40-02 AND DWG 141A8310 REV-SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE LOCATED AT LEVEL S-17R BETWEEN BS 291.5 AND BS 294.5 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ;51-40-02 AND DWG 141A8310 REV-SEE INDIVIDUAL SIGN OFF BELOW. ITEM RII

Part: SUPPORT BRACKET — CRACKED (AC BAY) · airframe 58,674 hrs · 34,928 cycles

CRACK BODY STATION 540; RBL 8 SUPPORT BRACKET AT AIR CONDITIONING BAY 2022-409947 / [01] REPLACED BODY STATION 540; RBL 8 SUPPORT BRACKET AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02.;[02] REPLACED BODY STATION 540; RBL 8 SUPPORT BRACKET AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02.

Part: SUPPORT ANGLE — CRACKED (AC BAY) · airframe 58,674 hrs · 34,928 cycles

CRACK SUPPORT ANGLE BS 661.95 AND LBL 42 AIR CONSITIONING BAY CENTER SECTION 2022-409945 / [01] REPLACED SUPPORT ANGLE BS 661.95 AND LBL 42 AIR CONSITIONING BAY CENTER SECTION I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 111A1000 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED SUPPORT ANGLE BS 661.95 AND LBL 42 AIR CONSITIONING BAY CENTER SECTION I.A.W. B737-700 SRM 57-10-10-2R-5 REPAIR 5 AND SRM 51-40-02 AND DWG 111A1000 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[03] TASK CARD COMPLETED <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — CORRODED (FWD GALLEY FLOOR) · airframe 58,674 hrs · 34,928 cycles

CORROSION ANGLE - SUPPORT LOCATED BS300.5 AT LEVEL STR17R WL208.1 RBL56 AT FWD GALLEY AREA 2022-409958 / [01] REPLACED ANGLE LOCATED BS300.5 AT LEVEL STR17R WL208.1 RBL56 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 141A8310 REV -;[02] REPLACED ANGLE LOCATED BS300.5 AT LEVEL STR17R WL208.1 RBL56 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 141A8310 REV - SEE INDIVIDUAL SIGN OFF BELOW;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — CRACKED (CABIN FLOOR) · airframe 58,674 hrs · 34,928 cycles

CRACK FRAME STUB LOCATED AT BS 294.5 AT LEVEL S-9R WL 267.1 AT PASSENGER CABIN 2022-409941 / [01] REPLACED FRAME STUB AND FASTENERS LOCATED AT BS 294.5 AT LEVEL S-9R WL 267.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 141A8370 REV D.SEE INDIVIDUAL SIGNOFF BELLOW.;[02] REPLACED FRAME STUB AND FASTENERS LOCATED AT BS 294.5 AT LEVEL S-9R WL 267.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 141A8370 REV D.SEE INDIVIDUAL SIGNOFF BELLOW.

Part: NONE — CRACKED (FWD GALLEY FLOOR) · airframe 58,674 hrs · 34,928 cycles

CRACK INNER CHORD LOCATED BETWEEN BS303.9 WL208.1 LBL50 AT FWD GALLEY AREA 2022-409927 / [01] REPLACED INNER CHORD AND FASTENERS IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 141A8110 REV-.SEE INDIVIDUAL SIGNOFF BELLOW;[02] REPLACED INNER CHORD AND FASTENERS IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 141A8110 REV-.SEE INDIVIDUAL SIGNOFF BELLOW ITEM RII

Part: NONE — MISSING · airframe 58,674 hrs · 34,928 cycles

#6 SLAT O/B AUX ARM SKIN TAB MISSING 2022-409965 / [01] REPLACED SKIN TAB LOC. ON #6 SLAT O/B AUX ARM. IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9.;[02] REPLACED SKIN TAB LOC. ON #6 SLAT O/B AUX ARM. IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 58,674 hrs · 34,928 cycles

CRACK ANGLE LOCATED AT BS 1016 BETWEEN S-3L AND S-3R WL 308.5 AT VERTICAL STABILIZER 2022-409878 / [01] REPLACED ANGLE AND FASTENER LOCATED AT BS 1016 BETWEEN S-3L AND S-3R WL 308.5 AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DRAWING 176A3101 REV -: SEE INDIVIDUAL SING OFFS BELOW.;[02] REPLACED ANGLE AND FASTENER LOCATED AT BS 1016 BETWEEN S-3L AND S-3R WL 308.5 AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND DRAWING 176A3101 REV -: SEE INDIVIDUAL SING OFFS BELOW. COMPLETED RII

Part: ANGLE — CRACKED (LH WING) · airframe 58,674 hrs · 34,928 cycles

CRACK OUTBOARD TRAILING EDGE LOC ORSS 272 AT LT WING 2022-409831 / [01] REPLACED ANGLE LOC. OUTBOARD TRAILING EDGE ORSS 272 AT LT WING A.W SRM B737-700 51-40-02 AND DRAWING #115A2930 REV. - DUE TO NOT FOUND ALLOWABLE DAMAGE B737-700 SRM 57-51-02. TOOK MEASURES OF CRACK IS L=0.650? TOOL USED CALIPER P/N:500-196-30 S/N:A21033429; DUE DATE : 02-NOV-22.;[02] TASK CARD COMPLETED

Part: NONE — DEBONDED (R/H WING) · airframe 58,674 hrs · 34,928 cycles

CUSTOMER REQUEST - DEBONDED EXISTING REPAIR INBOARD CORNER ON OB AFT FLAP AT RT WING. 2022-409841 / [01] TOOL USED CALIPER P/N: 500-197-30 S/N: 15120589 DUE DATE: 28-NOV-22.;[02] TOOL USED: ULTRASONIC FLAW DETECTOR P/N:EPOCH 600 S/N: 120357005 DUE DATE: 07-JAN-23.;[03] HOT BONDER P/N:HCS9000B S/N:18175469 DUE DATE:05-AUG-22;[04] EQUIPMENT P/N S-3; S/N 064; DUE DATE 19-JUL-23 WAS USED;[05] TOOL USED; HOT BONDER PN:HCS9200B-AV ; SN:18185733 DUE DATE 16/JAN/23.;[06] REPAIRED OB AFT FLAP AT RT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. SEE INDIVIDUAL SIGN OFFS BELOW.;[07] COMPLETED TASK. RII

Part: ANGLE — CRACKED (LH WING) · airframe 58,674 hrs · 34,928 cycles

CRACK OUTBOARD TRAILING EDGE ANGLE LOC ORSS 282 AT LT WING 2022-409826 / [01] REPLACED ANGLE LOC. OUTBOARD TRAILING EDGE ANGLE; ORSS 282 AT LT WING IAW B737-700 SRM-51-10-02 ITEM 9 AND DWG-115A6200 REV:- SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE LOC. OUTBOARD TRAILING EDGE ANGLE; ORSS 282 AT LT WING IAW B737-700 SRM-51-10-02 ITEM 9 AND DWG-115A6200 REV:- SEE INDIVIDUAL SIGN-OFF BELOW

Part: BATTERY PACK — INOPERATIVE (FWD CABIN) · airframe 58,528 hrs · 34,835 cycles

EMERGENCY LIGHTS AT FWD ENTRY; ROW 3DEF; 6DEF; AND EXTERIOR SVC DOOR ARE INOP. / [01] REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK M1674 ABOVE FWD GALLEY LIGHT. REF AMM 33-51-06. OPS CHECKS GOOD.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 56,699 hrs · 33,698 cycles

193B PANEL HAS SEVERAL ELONGATED/DAMAGED HOLES. ; / [01] REPLACED PANEL PER SRM 51-40-02 AND SIP

Part: PANEL — ELONGATED (FUSELAGE) · airframe 56,616 hrs · 33,651 cycles

LOWER WHEEL WELL PANEL 193D HAS CHAFING ON T/E AND ELONGATED HOLES ; LOWER WHEEL WELL PANEL 193D HAS CHAFING ON TE AND ELONGATED HOLES / [01] REMOVED AND INSTALLED NEW PANEL PER AMM 53-51-21; [02] C/W

Part: HOLDER — LOOSE (R1 DOOR) · airframe 56,369 hrs · 33,486 cycles

FORWARD SERVICE DOOR GIRT BAR HOLDER UNSECURED ; / [01] RESECURED PER SIP.

Part: BAFFLE — CRACKED (BS 500C-500D) · airframe 53,633 hrs · 31,840 cycles

FWD CARGO BAY BAFFLE CRACKED BS 500C - BS 500D LBL23 WL 156 / REMOVED AND REPLACED FCB BAFFLE AT BS500D-500C LBL23 WL156 I.A.W SRM 51-40-02-0G-0 AND DWG 143A7505 REV:A

Part: FLOOR SUPPORT — CRACKED (BS 727A-727B) · airframe 53,633 hrs · 31,840 cycles

AFT CARGO BAY INTERCOSTAL CRACKED AT FASTENER HOLE BS 727A-727B LBL 25 WL 156. REMOVED AND REPLACED AFT CARGO BAY INTERCOSTAL AT 727A-727B LBL 25 WL 156, IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV A.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 53,633 hrs · 31,840 cycles

LT & RT OVERWING EMERGENCY EXIT SIGNS HAVE BURNT OUT BULBS. RELAMPED & PERFORMED A GOOD REPLACEMENT TEST OF THE LT & RT OVERWING EMERGENCY EXIT SIGNS, PER AMM 33-51-01-960-801.

Part: FLOOR SUPPORT — CRACKED (BS 827-847) · airframe 53,633 hrs · 31,840 cycles

AFT CARGO BAY INTERCOSTAL CRACKED AT FASTENER HOLE BS 827-BS 847 LBL 25 WL 156. REMOVED AND REPLACED INTERCOSTAL P/N 146A7505-9 PO NR 802309/1 AT ACB BS 827 TO BS 847 LBL 23 WL 156, IAW SRM 51-40-02 AND DWG NR 146A7505 REV C 57049U 09SEP2020.

Part: WEB — CRACKED (BS 500-500A) · airframe 53,633 hrs · 31,840 cycles

FWD CARGO BAY WEB CRACKED AT FASTENER HOLE BS 500- BS 500A RBL 23 WL 157 / REMOVED FCB CRACKED WEB BS - 500 - 500A; RBL - 23; WL - 157. LOCATED AND INSTALLED REPLACEMENT WEB ALL IAW SRM 51-40-02-0G-0 & DWG 143A0080 SHT - 1

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 53,633 hrs · 31,840 cycles

MECHANICAL DAMAGE ON PASSENGER CABIN SEAT TRACK AT B.S. 520; L.B.L. 45; W.L. 208.1. / REMOVED AND REPLACED CABIN SEAT TRACK AT B.S.520 LBL 45 WL 208.1 IAW SRM 51-40-02; BOEING DWG 143A5310 SH 40 REV A AND E.A.#20-153-01693

Part: WEB — CORRODED (THRESHOLD) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS794 - BS847 RBL26 WL159. / REMOVED CORROSION ON MULTIPLE AREAS ON SUBTHRESHOLD WEB AT AFT CORGO BAY BS 794-BS 847 RBL 26 IAW. SRM. 53-60-15-1A-1 FOUN TO BE OUT OF. LIMITS REMOVED. AND. REPLACEMENT SUBTHESHOLD WEB. AT. AFT CORGO BAY B.S 794-BS847-RBL 26 W.L. 156 IAW SRM 51-40-02-0G-0 END. SRM 51-40-05. AND. DWG. NO: 146A8340 ID: 0021 SHT 21 & DWG NO: 146A.8120 & 146A8123-25. 59826U 09-08-2020

Part: SUPPORT — CORRODED (BS 867-947) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS867 - BS947 RBL21 WL168. / REMOVED CORRODED FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 867 - BS 947 RBL 21 WL 168 AND REPLACED WITH NEW IAW SRM 53-00-53-1A-2; DWG 147A7500 ID 1; DWG 147A7500 ID 4; DWG 147A7501; SRM 51-40-05; DWG 147A7502; AMM 51-21-72-370-804; AMM 51-21-41-370-802 92954U 09/5/20

Part: SEAT TRACK — CRACKED (AFT CARGO) · airframe 53,633 hrs · 31,840 cycles

CRACKED FLOOR TRACK AT ACB BS 766 LBL 17 WL 156. REPAIRED CRACKED FLOOR TRACK WITH NEW PARTS FROM BS 747+10-767+10 LBL 17 WL 156, IAW SRM 53-00-53-2R-3 AND DWG NR 146A7500 REV A 59042U 05SEP20.

Part: STRINGER CLIP — CORRODED (BS 827) · airframe 53,633 hrs · 31,840 cycles

CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS 827 LBL 6 WL 157. REMOVED AND REPLACED STRINGER CLIP AT BS 827 LBL 6 S-27L PER DWG 146A1280 SHEET 30 AND SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CORRODED (BS 727D) · airframe 53,633 hrs · 31,840 cycles

CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS 727D S-21R WL 175, MARKED. REMOVED AND REPLACED STRINGER CLIP AT BS 727D S-21R PER DWG NR 146A1220 SHEET 49 AND SRM 51-40-02-0G-0.

Part: FLOORBEAM — CORRODED (BS887 LBL7-RBL21) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS887 LBL7 TO RBL21 WL168. / REMOVED SUPPORT SPLICE AT ACB BS887; RECIEVED NEW SUPPORT SPLICE ON P.O. 761896. LOCATED AND DRILLED IAW SRM 51-40-05; 51-40-08; AND DWG#146A9401. 59118U 08SEP20 OK TO INSTALL 8612C 08SEP20 INSP 15 08SEP20 INSTALLED SUPPORT SPLICE AT ACB BS887 IAW SRM 51-40-02. 59118U 08SEP20 SPLICE FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 SEC.9. 59118U 08SEP20

Part: SEAT TRACK — CORRODED (AFT CARGO) · airframe 53,633 hrs · 31,840 cycles

CORROSION ON RAIL AT AFT CARGO BAY BS 767-BS 787 RBL 8 WL 156. REMOVED EXISTING REPAIR AND INSTALLED NEW REPAIR ON RAIL BS 767-787 RBL 8 WL 156, IAW SRM 53-00-53-2R-2 92892U 02SEP20.

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON RAIL AT AFT CARGO BAY BS889 RBL7.5 WL170. / REPLACED AFT CARGO BAY RAIL BS 887 - BS 947 RBL 7.5 IAW SRM 51-40-05-0G-0; SRM 53-70-53-01-2; DWG 147A7500

Part: CARGO TRACK — CORRODED (BS 935) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS935 RBL13 WL176. / REMOVED AND REPLACED ACB TRACK TIEDOWN SECTION BETWEEN BS 887-947.5 RBL13 WL176 PER SRM 51-40-02 AND DWG # 147A7500 REV:-.

Part: STRINGER CLIP — BENT (BS 727E) · airframe 53,633 hrs · 31,840 cycles

BENT STRINGER CLIP AT AFT CARGO BAY BS 727E S-22L WL 169 BS 727E. STRINGER CLIP AT S22L IS REMOVED AND REPLACED ON CUSTOMER CARD NR U201864.

Part: FRAME — DENTED (BS 727B) · airframe 53,633 hrs · 31,840 cycles

DENT ON FRAME AT AFT CARGO BAY BS 727B S-22R WL 169. DENT ON FRAME AT BS 727B STR 22R WL 169 FOUND TO BE OUT OF LIMITS, PER SRM 53-00-07-1A-1. ACCOMPLISHED FRAME REPAIR BS 727B STR 22R, IAW ER 20-03199 REV IR AND EA 20-153-01727 REV IR.

Part: SEAT TRACK — CORRODED (BS 727B-887) · airframe 53,633 hrs · 31,840 cycles

CORROSION, MULTIPLE AREAS OF CORROSION ON PASSENGER CABIN SEAT TRACK AT BS 727B-887 RBL 45 WL 208.1. REMOVED CORROSION ON SEAT TRACK BS 727B-887 RBL 45 WL 208.1, MAX MATERIAL LOSS ON TOP OF CROWN AT 727C+17 .027' DEEP. FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-52-1A-1. REMOVED AND REPLACED WITH NEW SEAT TRACK AT BS 727B-887 RBL 45, IAW SRM 51-40-02 AND DWG 146A5300 59641U 03SEP20.

Part: STRINGER CLIP — CORRODED (BS 727E) · airframe 53,633 hrs · 31,840 cycles

CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS 727E S-23R WL 163, MARKED. REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-23R, PER DWG NR 146A1221 SHEETS 37 AND 39 AND SRM 51-40-02-0G-0.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON AFT SHIELD AT AFT CARGO BAY BS847 - BS867 RBL21 WL163. / REMOVED AND REPLACED SHIELD AT ACB BETWEEN BS+847 TO BS867 RBL21 WL163 IAW SRM 51-40-02 AND DWG 146A0081 REV A 57049U 04SEP2020

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS915 RBL2.5 WL173. / REPLACED AFT CARGO BAY RAIL B.S 887 - B.S 947 RBL 2.5 IAW SRM 51-40-05-0G-0; SRM 53-70-53-01-2; DWG 147A7500

Part: SHIELD — CORRODED (BS 767-787) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON FWD SHIELD AT AFT CARGO BAY BS767 - BS787 RBL22 WL156. / REMOVED AND INSTALLED NEW SHIELD IN ACB BS 767-787 RBL 22 WL 156 IAW SRM 51-40-05; DWG # 146A0081 REV A 59042U 04SEP20

Part: FRAME — DENTED (BS 727E) · airframe 53,633 hrs · 31,840 cycles

DENT ON FRAME AT AFT CARGO BAY BS 727E 2' BELOW S-22L WL 168. REMOVED DAMAGE ON FRAME AFT CARGO BAY BS 727E 2' BELOW STR 22 LT W/L 168 AND REPAIRED, PER ATS ER 20-03200 REV IR AND SWA EA 20-153-01704 REV IR.

Part: SEAT TRACK — CORRODED (BS 645-727B) · airframe 53,633 hrs · 31,840 cycles

CORROSION, MULTIPLE AREAS OF CORROSION ON PASSENGER CABIN SEAT TRACK AT BS 645-727B RBL 45 WL 208.1. REMOVED CORROSION ON SEAT TRACK BS 645-727B RBL 45 WL 208.1. MAX MATERIAL LOSS AT BS 648 IN WELL IS .042', FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-52-1A-1. REMOVED AND REPLACED WITH NEW SEAT TRACK FROM BS540-727B RBL45 WL208.1, IAW DWG 144A5300 AND SRM 51-40-02 59641U 1SEP20.

Part: SEAT TRACK — CORRODED (BS 767-787) · airframe 53,633 hrs · 31,840 cycles

CORROSION ON RAIL AT AFT CARGO BAY BS 767 - BS 787 RBL 3 WL 156. REPAIRED IAW SRM 53-00-53-2R-2, LOCATION ON RAIL AT ACB BS 767 - BS 787 RBL 3 WL 156. 59042U 04SEP20.

Part: STRINGER CLIP — CORRODED (BS 727E) · airframe 53,633 hrs · 31,840 cycles

CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS 727E S-22R WL 159, MARKED. REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-22R, PER DWG NR 146A1221 SHEETS 37 AND 39 AND SRM 51-40-02-0G-0.

Part: STRAP — CORRODED (BS 776-847) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON STRAP AT AFT CARGO BAY BS776 - BS847 RBL20 WL157. / REMOVED CORRODED STRAP ACB BS 776-847 RBL 20 WL 157 AND REPLACED WITH NEW IAW SRM 53-60-15-1A-1. DWG 146A8120 REV-; DWG 146A0081 REV A 92954U 09/9/20

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT AFT CARGO BAY BS947 RBL22 WL180. / REMOVED AND REPLACED FOR NEW AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT ACB BS947 RBL22 WL180 I.A.W. BOEING DWG 149A8117 REV:-; DWG 147A8110 REV: B SRM 51-40-02

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727 - BS767 RBL21 WL156. / REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT ACB BS727 TO BS767 RBL21 WL156 IAW SRM 51-40-02 AND DWG# 146A7500 REV.A 57049U 08SEP20

Part: ATTACH ANGLE — CRACKED (BS 866) · airframe 53,633 hrs · 31,840 cycles

BULKHEAD SUPPORT ATTACH ANGLE IS CRACKED AT ACB BS866 LBL10 WL165. MARKED / REMOVED AND REPLACED BULKHEAD SUPPORT ATTACH ANGLE AT-ACB BS-866 LBL10 WL165 I.A.W. SRM-51-40-02. AND BOEING DWG 149A8102 REV - 59361U 08SEP20

Part: FRAME SPLICE — CORRODED (AFT CARGO) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON FRAME AT AFT CARGO BAY BS787 RBL24 WL157. / REMOVED EXISTING FRAME SPLICE AND REPLACED NEW FABRICATED FRAME SPLICE AT ACB B/S 787; RBL 24 - RBL 31 IAW SRM 51-40-02-0G-0; DWG # 146A1262. 92892U 03SEP20.

Part: FLOOR SUPPORT — CORRODED (BS 727A-727B) · airframe 53,633 hrs · 31,840 cycles

CORROSION ON INTERCOSTAL AT ACB BS727A - BS727B LBL3 WL154. / REMOVED CORROSION ON INTERCOSTAL AT ACB BS727A-727B LBL3 WL154 IN AREA OF L=1' X W=1.25' D=.002' REMAINING THICKNESS .034' FROM ORIGINAL THICKNESS .036' FOUND TO BE IN LIMITS; APPLIED CHEMICAL CONVERSION & PRIMER IAW SRM 53-00-53-1A-2; 51-10-02; AMM 20-60-02-100-801 92954U 08/29/20

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT AFT CARGO BAY BS914 RBL12 WL170. / REMOVED AND REPLACED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS 914 RBL 12 WL 170 I.A.W SRM 51-40-02-0G-0 AND DWG 147A7221 REV:F

Part: PRESSURE DECK — OUT OF TOLERANCE (COCKPIT) · airframe 53,633 hrs · 31,840 cycles

DURING COMPLETION OF CCN 1-A53-33179 R1 U201423 STEP 7 FOUND 2 EACH HOLES COMMON TO FLIGHT DECK FLOOR REPAIR AREA TO BE OUT OF ROUND. AREAS MARKED. / REAMED 2 EA. HOLES TO CORRECT OUT-OF-ROUND CONDITION AND REPAIRED AREA PER E.R 20-03177 REV. IR AND E.A 20-153-01696 REV IR;

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 53,633 hrs · 31,840 cycles

PASSENGER CABIN FLOOR PANEL 242CF UPPER SURFACE HAS DAMAGE TO INBOARD EDGE, 25' FROM AFT EDGE, MARKED. PASSENGER CABIN FLOOR PANEL 242CF WITH UPPER SURFACE DAMAGED TO INBOARD EDGE, 25' FROM AFT EDGE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL USING BMS 4-23 TY2 LOT NR 142A456-1 BMS 5-107 LOT NR AK9GP5303K. DUE TO AMOUNT OF ALL DAMAGE, IAW SRM 53-00-50-2R-0. PARA 1A NOTE, 5.S.(1) DWG 144A5810-125.

Part: CARGO TRACK — CORRODED (BS 767-867) · airframe 53,633 hrs · 31,840 cycles

CORROSION ON AFT CARGO BAY RT TIE DOWN TRACK BS 767-867 RBL 14 WL 156. REMOVED CORROSION AT MULTIPLE LOCATIONS OF RBL 13.84 CARGO TRACK BS 727+4- BS 887. LARGEST BLEND MEASURED 2.0'L X 1.8'W X 0.029'D. DAMAGE IS OUT OF LIMITS, PER SRM 53-00-53-1A-2. REMOVED AND REPLACED CARGO TRACK RBL 13.84 BS 727+4-BS 887, PER DWG NR 146A7500 AND DWG NR 146A0061. FABRICATED BS 747+7.5 REPAIR SPLICE FROM BAC 1509-100688 7050 T6511 LOT NR 1433672 AND INSTALLED SPLICE, PER SRM 53-00-53-2R-3.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FWD CARGO BAY BS500D LBL23 TO RBL23 WL157. / REMOVED AND REPLACED AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FCB BS 500D LBL 23 TO RBL 23 WL 157 I.A.W SRM 51-40-02-0G-0 AND DWG 143A9481 REV:-

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 53,633 hrs · 31,840 cycles

PASSENGER CABIN FLOOR PANEL 231YF UPPER SURFACE HAS DAMAGE 13.5' FROM AFT EDGE, 4' FROM INBOARD EDGE, MARKED. PASSENGER CABIN FLOOR PANEL 231YF WITH UPPER SURFACE DAMAGED AT 13.5' FROM AFT EDGE, 4' FROM INBOARD EDGE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL USING BMS 4-23 TY 2 LOT NR 1428456-1 BMS5-107 LOT NR AK9GP5303K, DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0 PARA 1A NOTE 5S(1) DWG 144A5810-124.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FWD CARGO BAY BS500D RBL25 WL157. / FOUND NO ALLOWABLE DAMAGE IN SRM; REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0; (9); PG 7. REMOVED AND REPLACED; FWD CARGO BAY; AFT BULKHEAD TO SIDE--WALL SUPPORT ANGLE; BS500D; RBL25; WL157 IAW SRM 51-40-02-0G-0; SRM 51-46-08-0G-0; SRM 51-40-05-0G-0; DWG 143A7902. 6679U 03SEP20

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS460 - BS500C LBL23 WL157. / REMOVED CORROSION FROM MULTIPLE LOCATIONS MAX DIMESION L- 1' X W= 1' X D= .006' ORIGINAL THICKNESS; .040 REMAINING THICKNESS .034 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED. & REPLACEMENTS FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY B.S 460 - BS 500C IAW.SRM 51-40-02-0G-1 END SRM 51-40-05-0G-0 AND-SRM 51-40-080G-0 AND. DWG. NO: 143A7501 END DWG. 143A7500

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 53,633 hrs · 31,840 cycles

PASSENGER CABIN FLOOR PANEL 242DF UPPER SURFACE HAS DAMAGE 15' FROM FWD EDGE, 3.5' FROM INBOARD EDGE, MARKED. PASSENGER CABIN FLOOR PANEL 242DF WITH UPPER SURFACE DAMAGE 15' FROM FWD EDGE, 3.5' FROM INBOARD EDGE AS MARKED WAS REPLACED WITH A SERVICEABLE FLOOR PANEL, PER SRM 51-10-02-0G-0 PARA 9A(1) DUE TO AMOUNT OF ALL DAMAGE.

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 53,633 hrs · 31,840 cycles

CORROSION AFT CARGO BAY FLOOR BEAM AFT END SUPPORT AT STA 947 LBL 9 WL 177. REMOVED AND REPLACED AFT CARGO BAY FLOOR BEAM AFT END SUPPORT AT STA 947 LBL 9 WL 177, IAW SRM 51-40-02-0G-0 AND DWG 147A1047 REV.

Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 53,633 hrs · 31,840 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS 500C AFT SIDE LBL25 WL156. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C AFT SIDE LBL25 WL156 I.A.W SRM 51-40-02-0G-0. DWG 143A7902 REV:- AND DWG 143A7505 REV:B

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500 - BS500D RBL23 WL157. / REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 500-500D RBL23 WL157 I.A.W SRM 51-40-02-0G-0 AND DWG 143A7500 REV.-

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,633 hrs · 31,840 cycles

PASSENGER CABIN FLOOR PANEL 241AF UPPER SURFACE HAS DAMAGE AT FWD LEFT CORNER, MARKED. DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 241AF, FABRICATED NEW PANEL FROM BMS 4-23 TY2 LOT NR 1437364-1, IAW DWG 144A5810-127 & SRM 53-00-50-2R-0 PARA 1 A NOTE & TABLE 204 57885U 08-27-2020 13742C 08-27-20. INSTALLED INSERTS WITH BMS 5-107 LOT NR AK9GP5303K, IAW DWG 144A5810-127 & SRM 53-00-50-2R-0 PARA 5 S 57885U 08-28-2020.

Part: FRAME — DENTED (BS 500) · airframe 53,633 hrs · 31,840 cycles

DENT ON FRAME AT FWD CARGO BAY BS 500 BS 24R WL 162. REMOVED DAMAGE ON FRAME. FWD CARGO BAY BS 500B STR 24 RT W/L 162 REPAIRED, IAW ATS ER NR 20-03226 REV IR AND SWA EA 20-153-01738 REV IR.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS420 RBL23 WL157. / REPLACED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT B.S 400 - 420 RBL 23 W.L 157 IAW DWG 143A7501. DWG 143A7500 SRM 51-40-02 0G-0

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 53,633 hrs · 31,840 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / FOUND NO ALLOWABLE DAMAGE IN SRM; REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0. REMOVED AND REPLACED; FWD CARGO BAY; AFT BULKHEAD SUPPORT GUSSET IAW SRM 51-40-02-0G-0; SRM 51-40-08-0G-0; SRM 51-40-05-0G-0; DWG 143A7902. 6679U 03SEP20

Part: ATTACH ANGLE — CRACKED (BS 400) · airframe 53,633 hrs · 31,840 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS 400 RBL25 WL156. / REMOVED AND REPLACED ATTACH ANGLE AT FCB BS 400 RBL 25 WL 156 IAW SRM 51-40-02 AND DWG 143A7505 57049U 03SEP2020

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 53,633 hrs · 31,840 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / REMOVED AND REPLACED AFT BULKHEAD SUPPORT GUSSET AT FCB BS 500D S19L WL 193 IAW SRM 51-40-02 AND DWG 143A7902

Part: SHIELD — CORRODED (AFT CARGO) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON AFT SHIELD AT FWD CARGO BAY BS494 - BS500A RBL23 WL157. / REMOVED; CORODED AFT SHEID BS - 494 - 500A RBL - 23. WL - 157. LOCATED AND INSTALLED REPLACEMENT SHEILD ALL WORK ACCOMPLISHED PER SRM - 51-40-02-0G-0; DWG 143A0080 SHT - 1

Part: STRINGER — CRACKED (BS 540) · airframe 53,633 hrs · 31,840 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS 540 S-23L WL 167, MARKED. REPAIRED STR 23 LT BS 540 WL 167, IAW SRM 53-00-03-2R-1 AND EA 20-153-01695 REV IR AND ATS ER 20-03172 REV IR.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 53,633 hrs · 31,840 cycles

AFT CARGO DOOR FWD SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO DOOR FWD SCUFF PLATE IAW SRM 53-60-15-2R-1. SCUFF PLATE IS INSTALLED ON CUSTOMER CARD 753-140-00-027

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 53,633 hrs · 31,840 cycles

CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT BS 727-847 LBL 25 WL 156 / REMOVED AND REPLACED L/H FLOOR TO SIDEWALL SUPPORT ASSY AT BS727 TO BS847 LBL 25 WL 156 IAW SRM 51-40-02 AND DWG # 146A7500 REV. A 57049U; 09SEP2020; INSTALLED SPLICE REPAIR AT BS 747+11' LBL 25 WL 156 IAW SRM 53-00-53-2R-5

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 53,633 hrs · 31,840 cycles

PASSENGER CABIN FLOOR PANEL 231ZF UPPER SURFACE HAS DAMAGE 25.5' FROM AFT EDGE, 5' FROM INBOARD EDGE, MARKED. DUE TO EXTENT OF DAMAGE TO FLOOR PANEL 231ZF, FABRICATED NEW PANEL FROM BMS 4-23 TY2 LOT NR 14373G4-1. INSTALLED INSERTS WITH BMS 5-107 LOT NR AK9GP5303K, IAW DWG 114A5810-160 & SRM 53-00-50-2R-0 PARA 1A NOTE, TABLE 204 & PARA 5S 57885U 08-27-2020.

Part: SHIELD — CORRODED (BS 420-440) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL23 WL157. / REMOVED AND INSTALLED NEW FWD SHIELD AT FWD CARGO BAY BS420-BS440 RBL23 WL157. IAW DWG 143A8126; SRM 51-40-02; SRM 51-40-05; SRM 51-40-06; SRM 53-30-15-1A-1; DWG 143A0080

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FWD CARGO BAY BS500D LBL26 WL157. / REMOVED AND REPLACED AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT FCB BS500D LBL26 WL157 IAW SRM 51-40-02 AND DWG 143A7902 57049U 05SEP2020

Part: THRESHOLD — CORRODED (FWD CARGO) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS440 - BS492 RBL26 WL157. MARKED / REMOVED CORRODED SUBTHRESHOLD WEB AT FCB BS440-BS492 RBL26 WL157 AND REPLACED WITH NEW IAW SRM 51-40-02-0G-0; DWG 146A8123; DWG 143A8330; SRM 53-30-15-0I-1; SRM 53-30-15-1A-1 92954U 09/3/20

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON SUPPORT ANGLE AT PASSENGER CABIN BS720 LBL65 WL203. / THE DAMAGE IS INSPECTED AND REPAIRED PER EA 20-153-01725 REV IR (ATS ER 20-03181 REV IR)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON SUPPORT ANGLE AT PASSENGER CABIN BS709.5 LBL65 WL203. / THE DAMAGE IS INSPECTED AND REPAIRED PER EA 20-153-01725 REV IR (ATS ER 20-03181 REV IR).

Part: SUPPORT ANGLE — CORRODED (BS 694) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON SUPPORT ANGLE AT PASSENGER CABIN BS694 RBL65 WL203. / THE DAMAGE IS INSPECTED AND REPAIRED PER EA 20-153-01725 REV IR (ATS ER 20-03181 REV IR).

Part: FLOORBEAM — CORRODED (BS 705 RBL 65) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON SUPPORT ANGLE AT PASSENGER CABIN BS705 RBL65 WL203. / THE DAMAGE IS INSPECTED AND REPAIRED PER EA 20-153-01725 REV IR (ATS ER 20-03181 REV IR).

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON SUPPORT ANGLE AT PASSENGER CABIN BS694 LBL65 WL203. / THE DAMAGE IS INSPECTED AND REPAIRED PER EA 20-153-01725 REV IR (ATS ER 20-03181 REV IR).

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON SUPPORT ANGLE AT PASSENGER CABIN BS715 LBL65 WL203. / THE DAMAGE IS INSPECTED AND REPAIRED PER EA 20-153-01725 REV IR (ATS ER 20-03181 REV IR).

Part: ATTACH ANGLE — CRACKED (BS 695) · airframe 53,633 hrs · 31,840 cycles

CRACKED ATTACH ANGLE AT PASSENGER CABIN BS695 RBL1 WL206. MARKED / REMOVED AND REPLACED CRACKED ATTACH ANGLE AT BS695 RBL1 WL206 PER EA 20-153-01663 REV IR; ATS ER 20-03211 REV IR; DWG# 273A9110 REV A; SRM 51-40-02; SRM 51-20-01 AND SOPM 20-41-02

Part: ATTACH ANGLE — CRACKED (BS 695) · airframe 53,633 hrs · 31,840 cycles

CRACKED ATTACH ANGLE AT PASSENGER CABIN BS695 LBL1 WL203. MARKED / REMOVED AND REPLACED ATTACH ANGLE AT BS695 LBL1 WL203 PER SRM 51-40-05; SRM 51-40-02; AND DWG 273A9110.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON SUPPORT ANGLE AT PASSENGER CABIN BS720 RBL65 WL203. / THE DAMAGE IS INSPECTED AND REPAIRED PER EA 20-153-01725 REV IR (ATS ER 20-03181 REV IR)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON SUPPORT ANGLE AT PASSENGER CABIN BS688 LBL65 WL203. / THE DAMAGE IS INSPECTED AND REPAIRED PER EA 20-153-01725 REV IR (ATS ER 20-03181 REV IR).

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON SUPPORT ANGLE AT PASSENGER CABIN BS715 RBL65 WL203. / THE DAMAGE WAS INSPECTED AND REPAIRED PER EA 20-153-01725 REV IR AND (ATS ER 20-03181 REV IR)

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON SUPPORT ANGLE AT PASSENGER CABIN BS709 RBL65 WL203. / THIS DAMAGE IS INSPECTED AND REPAIRED PER EA 20-153-01725 REV IR (ATS ER 20-03181 REV IR).

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 53,633 hrs · 31,840 cycles

***CORROSION*** ON SUPPORT ANGLE AT PASSENGER CABIN BS698 LBL65 WL203. / THE DAMAGE IS INSPECTED AND REPAIRED PER EA 20-153-01725 REV IR (ATS ER 20-03181 REV IR).

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 53,633 hrs · 31,840 cycles

FLIGHT DECK FLOOR IS DENTED AT BS 255 RBL 4 LBL 14 WL 207.54. REMOVED DAMAGED SECTION OF FLIGHT DECK FLOOR AT BS 255 RBL 4 LBL 14 WL 207.54 AND REPAIRED FLOOR, PER EA 1-A53-33179 REV 1.

Part: LENS — BROKEN (CABIN) · airframe 53,223 hrs · 31,581 cycles

R/H EMERGENCY EXIT LENS COVER BROKEN R& R/H EMERGENCY EXIT LIGHT ASSEMBLY PER M/M 33.51.04.

Part: SIGN — UNSECURE (CABIN) · airframe 53,214 hrs · 31,575 cycles

CENTER CABIN EXIT LIGHT FALL OFF REINSTALLED EXIT SIGN IAW AMM 33-51-02, OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,751 hrs · 30,651 cycles

L/H GROUND OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. R&R POWER SUPPLY PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,751 hrs · 30,651 cycles

L/H GROUND OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. R&R BATTERY PACK PER AMM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,751 hrs · 30,651 cycles

R/H GROUND OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. R&R POWER SUPPLY PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,751 hrs · 30,651 cycles

R/H GROUND OVERWING EXIT EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: SEAL — CRACKED (LH HOR STAB) · airframe 51,559 hrs · 30,509 cycles

LH HORIZONTAL STABILIZER UPPER SLIDING SEAL IS CRACKED / REMOVED AND REPLACED LH HORIZONTAL STABILIZER UPPER SLIDING SEAL PER AMM 53-31-31

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,559 hrs · 30,509 cycles

BATTERY PACKS FAILED CAPACITY TEST AT M1670. R&R BATTERY PACKS PER DWG AND MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,559 hrs · 30,509 cycles

BATTERY PACKS FAILED CAPACITY TEST AT M1669. R&R BATTERY PACKS PER DWG AND MM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 51,559 hrs · 30,509 cycles

LT FWD UPPER WING TO BODY FAIRING AFT CENTER SUPPORT BRACKET CRACKED. / REMOVED AND REPLACED L/H FWD UPPER WING TO BODY FAIRING AFT CENTER SUPPORT BRACKET IAW SRM 51-40-02.

Part: BATTERY — DISCHARGED (COCKPIT) · airframe 51,477 hrs · 30,459 cycles

LT AFT EMERGENCY LIGHT CHARGER CIRCUIT BREAKER WILL NOT RESET AT BS 603. R&R BATTERY PER AMM.

Part: CHARGER — INOPERATIVE (COCKPIT) · airframe 51,477 hrs · 30,459 cycles

LT AFT EMERGENCY LIGHT CHARGER CIRCUIT BREAKER WILL NOT RESET AT BS 603. R&R LIGHT CHARGER PER AMM.

Part: GIRT BAR — MISALIGNED (R1 DOOR) · airframe 51,203 hrs · 30,283 cycles

R1 DOOR GIRT BAR MISALIGNED. REALIGNED GIRT BAR PER SIP.

Part: SLIDE — UNSECURE (R2 DOOR) · airframe 50,247 hrs · 29,709 cycles

R2 DOOR SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: SLIDE — TORN (L1 DOOR) · airframe 49,324 hrs · 29,131 cycles

L1 DOOR ESCAPE SLIDE SKIRT TORN. R&R SLIDE IAW MT.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 49,324 hrs · 29,131 cycles

R1 DOOR ESCAPE SLIDE SKIRT PLACARD LOOSE. R&R SLIDE IAW MT.

Part: SIGN — LOOSE (CABIN) · airframe 48,952 hrs · 28,899 cycles

MID CABIN OVERHEAD "EMERGENCY EXIT" SIGN LOOSE. R&R SIGN ASSEMBLY PER AMM.

Part: PLACARD — LOOSE (CABIN) · airframe 48,718 hrs · 28,755 cycles

LT OVERWING FORWARD EMERGENCY EXIT SIGN EXIT PLACARD LOOSE. SECURED SIGN IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 48,598 hrs · 28,683 cycles

AFT SERVICE EMERGENCY EXIT LENS BROKEN. R&R LIGHT ASSEMBLY PER AMM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 48,453 hrs · 28,593 cycles

R1 DOOR SLIDE INADVERTENTLY FELL OUT OF COMPARTMENT, DID NOT DEPLOY, STILL OPERATIONAL. REPAIRED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,331 hrs · 28,510 cycles

LT EMERGENCY BIN LIGHT INOP AT ROW 17. R&R LIGHT ASSEMBLY IAW AMM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 48,331 hrs · 28,510 cycles

FUEL TANK TO VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, RBL 7. REPAIRED ANGLE IAW EA.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 48,331 hrs · 28,510 cycles

AFT CARGO DOOR CUT OUT AFT CORNER SCUFF PLATE IS CRACKED / RECIEVED NEW AFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE PO# 7048241. LOCATED AND DRILLED IAW SRM 51-40-05-0G-0 56800U 21SEP18

Part: BRACKET — CRACKED (LEFT WING) · airframe 48,331 hrs · 28,510 cycles

L/H WING FIXED TRAILING EDGE SEAL RETAINER BRACKET IS CRACKED BETWEEN I/B AND 0/B FLAPS OBSS 271 / REMOVED L/H WING FIXED TRAILING EDGE SEAL FROM RETAINER BRACKET; I.A.W. S.R.M. 51-40-02-0G-0; LOCATED AND DRILLED HOLES ON NEW RETAINER BRACKET; PART # 115A2982-9. I.A.W. DRAWING #11A2982-9 AND S.R.M. 51-40-05-0G-0. INSTALLED EDGE SEAL ON NEW RETAINED BRACKET; I.A.W. DRAWING #115A29892-9 AND S.R.M. 51-40-02-06-0; BETWEEN I/B AND O/B FLAPS OBSS 271.

Part: LATCH — INOPERATIVE (L1 DOOR) · airframe 48,331 hrs · 28,510 cycles

L1 DOOR EMERGENCY ESCAPE SLIDE LATCH INOP. R&R LATCH IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,772 hrs · 28,142 cycles

EMERGENCY EXIT LIGHT INOP AT ROW 9 ABC. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,772 hrs · 28,142 cycles

EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. R&R BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 47,741 hrs · 28,122 cycles

L2 DOOR EVAC SLIDE LIGHT INOP. R&R LIGHT PER MM.

Part: SIGN — MISSING (R2 DOOR) · airframe 47,701 hrs · 28,098 cycles

R2 DOOR EXIT SIGN MISSING. R&R SIGN ASSEMBLY PER MM.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 47,350 hrs · 27,864 cycles

PANEL 193B R/H FWD CORNER DELAMINATED 1.5' WIDE X 1.5'LONG . DAMAGED AREA HAS EROSION DAMAGE AT LEAST 4 PLYS DEEP. / REPAIR OF FWD R/H CORNER DELAMINATION 1.5'WIDE X 1.5'LONG OF PANEL 193B WAS ACCOMPLISHED ON DEFECT NO. N161084

Part: FLAP — DELAMINATED (LT WING) · airframe 47,350 hrs · 27,864 cycles

LT WING OUTBOARD AFT FLAP DELAMINATED AT TRAILING EDGE. R&R AFT FLAP PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 46,311 hrs · 27,201 cycles

OVERWING EMERGENCY EXIT LIGHT COVER LENS BROKEN. R&R LENS PER AMM.

Part: COVER — BROKEN (CABIN) · airframe 46,311 hrs · 27,201 cycles

AFT EMERGENCY EXIT LIGHT COVER BROKEN OFF. R&R LIGHT ASSEMBLY PER AMM.

Part: SKIN — BROKEN (FUSELAGE) · airframe 46,177 hrs · 27,120 cycles

GROUND POWER DOOR METAL AROUND DOOR OPENING BROKEN. REPAIRED CUTOUT PER EA.

Part: FSEU — FAULTY (E&E BAY) · airframe 46,089 hrs · 27,065 cycles

DIVERSION, ON TAKEOFF DURING FLAP RETRACTION, FLAPS LOCKED UP BETWEEN 0 & 1 RIGHT FLAP LAGGED WITH LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED RAN QRH & LANDED FLAPS 0. R&R FLAP SLAT ELECTRONIC UNIT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,242 hrs · 26,516 cycles

RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 43,055 hrs · 25,225 cycles

KEELBEAM TO FAIRING PANEL SUPPORT BRACKET CRACKED AT BS 546, RBL6. R&R BRACKET IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 43,055 hrs · 25,225 cycles

KEELBEAM TO FAIRING PANEL SUPPORT BRACKET CRACKED AT BS 546, LBL 6. R&R BRACKET IAW SRM.

Part: LIGHT — CRACKED (GALLEY) · airframe 41,882 hrs · 24,522 cycles

NR 4 GALLEY EXIT LIGHT ASSEMBLY CRACKED. R & R LIGHT ASSEMBLY IAW AMM.

Part: CREASE BEAM — CRACKED (BS 520) · airframe 41,882 hrs · 24,522 cycles

LEFT CREASE BEAM TEE CAP CRACKED AT BS 520, LBL 64. REPAIRED THE CREASE BEAM IAW EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,882 hrs · 24,522 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.7, 2ND VERTICAL STIFFENER. REPAIRED THE RIB IAW EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,882 hrs · 24,522 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT HSS 166.3, THIRD VERTICAL STIFFENER FROM FORWARD SPAR. REPAIRED THE RIB IAW EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,882 hrs · 24,522 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.70, FORWARD INBOARD LOWER FLANGE. REPAIRED THE RIB IAW EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 41,882 hrs · 24,522 cycles

BULKHEAD FRAME ATTACH ANGLE CRACKED AT BS 867. R & R ANGLE IAW SRM & DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,882 hrs · 24,522 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT HSS 92.7, FOURTH RIB STIFFENER AFT OF FORWARD SPAR. REPAIRED THE RIB IAW EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,882 hrs · 24,522 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 120.3, 4TH RIB STIFFENER AFT OF FORWARD SPAR. REPAIRED THE RIB IAW SRM AND EA.

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 41,882 hrs · 24,522 cycles

VAPOR BARRIER ATTACH ANGLE CRACKED AT BS 663, LBL 9.5. REPAIRED ANGLE IAW EA.

Part: BRACKET — CORRODED (L1 GIRT BAR) · airframe 41,882 hrs · 24,522 cycles

L1 DOOR EMERGENCY EVAC SLIDE FORWARD GIRT BAR FITTING BRACKET CORRODED. R & R THE BRACKET IAW AMM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 41,882 hrs · 24,522 cycles

RIGHT HORIZONTAL STABILIZER INBOARD SIDE RIB CRACKED AT HSS 92.7, FIRST VERTICAL STIFFENER. R & R THE STIFFENER IAW EA.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 41,882 hrs · 24,522 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT HSS 129.5, INBOARD SIDE THIRD STIFFENER FROM FORWARD SPAR. REPAIRED THE STIFFENER IAW EA.

Part: LATCH — CORRODED (FUSELAGE) · airframe 41,882 hrs · 24,522 cycles

STAB COMPARTMENT DOOR 311BL INBD LATCH CORRODED. R & R LATCH IAW DWG & MM.

Part: FLOOR SUPPORT — CORRODED (BS 294) · airframe 41,882 hrs · 24,522 cycles

PASSENGER CABIN FLOOR SUPPORT CORRODED AT BS 294+12, LBL 12. / R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 41,882 hrs · 24,522 cycles

R1 DOOR CREASE BEAM ATTACH ANGLE CORRODED BETWEEN BS 293 TO BS 328, LBL 65. R & R ANGLE IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 41,882 hrs · 24,522 cycles

FLOORBEAM ANGLE CORRODED AT BS 312, BETWEEN LBL 12 TO LBL 30. R &R THE FLOORBEAM ANGLE IAW SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,882 hrs · 24,522 cycles

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

Part: FRAME — CRACKED (BS 500A) · airframe 41,882 hrs · 24,522 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,882 hrs · 24,522 cycles

FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,882 hrs · 24,522 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,882 hrs · 24,522 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,882 hrs · 24,522 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,882 hrs · 24,522 cycles

FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (BS 947-994) · airframe 41,882 hrs · 24,522 cycles

UPPER SURFACE OF CREASE BEAM CORRODED BETWEEN BS 947 TO 994, RBL 54. R & R THE CREASE BEAM IAW DWG AND SRM.

Part: FRAME — CRACKED (BS 440) · airframe 41,882 hrs · 24,522 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,882 hrs · 24,522 cycles

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

Part: FRAME — CRACKED (BS 400) · airframe 41,882 hrs · 24,522 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,882 hrs · 24,522 cycles

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

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,882 hrs · 24,522 cycles

AFT PIT AT FLOOR SHIELD CORRODED BETWEEN BS 767 TO BS 787, RBL 21. R & R SHIELD IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,882 hrs · 24,522 cycles

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

Part: ANGLE — CORRODED (BS 500-500A) · airframe 41,882 hrs · 24,522 cycles

FORWARD CARGO COMPARTMENT ZEE CHANNEL CORRODED BETWEEN BS 500 TO 500A, RBL 23. R & R THE ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (BS 500B-500D) · airframe 41,882 hrs · 24,522 cycles

FORWARD CARGO COMPARTMENT ZEE CHANNEL CORRODED BETWEEN BS 500B TO 500D, RBL 23. R & R THE ANGLE IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,882 hrs · 24,522 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 120.3, THIRD STIFFENER AFT OF FORWARD SPAR. REPAIRED THE RIB IAW SRM AND EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 41,882 hrs · 24,522 cycles

RIGHT WING L/E NR 8 SLAT LOWER SKIN, AT THE ACTUATOR ATTACH POINT CRACKED. REPAIRED NR 8 SLAT SKIN IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 41,882 hrs · 24,522 cycles

LEFT WING OTBD AFT FLAP INBD CORNER T/E DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 41,882 hrs · 24,522 cycles

RIGHT WING OUTBOARD AFT FLAP INBOARD CORNER DELAMINATED. REPAIRED THE FLAP IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 41,882 hrs · 24,522 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT STA 663, RBL 36. / REPAIRED WEB IAW SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 41,882 hrs · 24,522 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MAINTENANCE.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 41,243 hrs · 24,136 cycles

LEFT WING WEB SUPPORT ANGLE CRACKED INBOARD OF MID FLAP DEFLECTION BEAM. R & R SUPPORT ANGLE IAW SRM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 41,243 hrs · 24,136 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1675. R & R THE BATTERY IAW AMM.

Part: GIRT BAR — DISLODGED (L2 DOOR) · airframe 41,243 hrs · 24,136 cycles

L2 DOOR EMERGENCY EVACUATION SLIDE GIRT INADVERTENTLY FELL OUT, SLIDE DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED THE GIRT BAR ASSEMBLY IAW MT & MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 41,243 hrs · 24,136 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1668. R & R THE BATTERY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,806 hrs · 23,873 cycles

RIGHT LOWER AFT FUSELAGE EMER LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,917 hrs · 22,790 cycles

EMER LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT M01674. R & R BATTERY PACK IAW MT & AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,917 hrs · 22,790 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,917 hrs · 22,790 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,917 hrs · 22,790 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,596 hrs · 21,456 cycles

RIGHT OVERWING EXIT SIDEWALL LIGHT BALLAST INOPERATIVE. R & R LIGHT IAW MM.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 36,596 hrs · 21,456 cycles

RIGHT EMER FLOOR TRACK LIGHTING FWD GLOW STRIP INOPERATIVE AT ROW 1. R & R STRIP IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,132 hrs · 20,627 cycles

SKIN CRACKED AT BS 540 STRINGER 22L. REPAIRED SKIN IAW EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,132 hrs · 20,627 cycles

CABIN FLOOR SEAT TRACK CORRODED AT STATION BS 500+14 RBL 45. REPAIRED SEAT TRACK IAW SRM & EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,132 hrs · 20,627 cycles

CABIN FLOOR SEAT TRACK CORRODED AT STATION BS 500+ 14 RBL 25. REPAIRED SEAT TRACK IAW SRM & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,132 hrs · 20,627 cycles

SEAT TRACK CRACKED AT STATION 727B LBL 45.5. REPAIRED TRACK IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,132 hrs · 20,627 cycles

R1 COCKPIT WINDOW FRAME CRACKED AT UPPER OTBD CORNER. REPAIRED WINDOW FRAME IAW AC.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,132 hrs · 20,627 cycles

SEAT TRACK CRACKED AT STATION 727B LBL 24.75. REPAIRED TRACK IAW EA.

Part: WEB — CRACKED (LT WING) · airframe 35,132 hrs · 20,627 cycles

LEFT WING FIXED TE PANEL INBD OF DEFLECTOR RIB WEB CRACKED. R & R WEB IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 35,132 hrs · 20,627 cycles

SEAT BRAKE CHANNEL CRACKED AT BS 540 LBL 1. R & R CHANNEL IAW DWG & SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 35,132 hrs · 20,627 cycles

LEFT WING TE DEFLECTOR RIB FIXED ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,132 hrs · 20,627 cycles

SEAT TRACK CRACKED AT STATION 727B RBL 45.5. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,132 hrs · 20,627 cycles

SEAT TRACK CRACKED AT STATION 727B RBL 24.75. REPAIRED TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,132 hrs · 20,627 cycles

SEAT TRACK CRACKED AT STATION 727B+2 LBL 24.75. REPAIRED TRACK IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,132 hrs · 20,627 cycles

FUSELAGE SKIN CRACKED AT STATION 540 STRINGER 22R. REPAIRED SKIN IAW EA.

Part: SIGN — BROKEN (CABIN) · airframe 33,892 hrs · 19,890 cycles

MID CABIN CEILING EMER EXIT SIGN BROKEN. R & R SIGN ASSEMBLY IAW MM.

Part: GIRT BAR — LOOSE (EVAC SLIDE) · airframe 33,397 hrs · 19,608 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED SLIDE IAW SIP.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 31,480 hrs · 18,483 cycles

LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING IAW EA.

Part: COVER — MISSING (EXIT SIGN) · airframe 31,194 hrs · 18,311 cycles

OVERHEAD CENTER AISLE OVERWING EMERGENCY EXIT SIGN COVER MISSING. INSTALLED COVER IAW SIP.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 29,626 hrs · 17,409 cycles

L3 COCKPIT WINDOW FRAME CRACKED. REPAIRED FRAME PER ACO.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,677 hrs · 16,863 cycles

LEFT WING OVERWING EMERGENCY LIGHT INOP & LENS CRACKED. FOUND DIODE IN BATTERY PACK OPEN. REMOVED AND REPLACED BATTERY PACK & REPLACED BROKEN LENS COVER WITH NEW ONE IAW MM, OPS CHECK GOOD.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,264 hrs · 16,639 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 175.5. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,264 hrs · 16,639 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 101.9. REPAIRED SKIN IAW SRM.

Part: COVER — CRACKED (CABIN) · airframe 26,730 hrs · 15,712 cycles

LEFT CABIN FLOOR EMERGENCY EXIT LIGHT COVERS CRACKED BETWEEN ROW 1 TO ROW 13. REMOVED AND REPLACED COVERS IAW M/M.

Part: LENS — LOOSE (CABIN) · airframe 25,435 hrs · 14,970 cycles

EEPLS LENS LOOSE AT ROW 9. SECURED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 24,571 hrs · 14,440 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 2. REMOVED AND REPLACED COVER PER MM.

Part: BRACKET — BROKEN (EVAC SLIDE) · airframe 24,571 hrs · 14,440 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LATCH BRACKET ASSY BROKEN. REMOVED AND REPLACED BRACKET ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 23,847 hrs · 14,008 cycles

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

Part: LENS — OUT OF POSITION (CABIN) · airframe 23,643 hrs · 13,895 cycles

MID CABIN EMERGENCY EXIT SIGN LENS FELL OFF. RE-INSTALLED LENS PER MM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 22,210 hrs · 13,045 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EVACUATION SLIDE BOTTLE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,107 hrs · 12,991 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD EEPLS INOP. RELAMPED PER MM.

Part: COVER — CRACKED (CABIN) · airframe 22,004 hrs · 12,929 cycles

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

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 21,881 hrs · 12,866 cycles

DURING SCHEDULED 6Y CHECK, FOUND CARGO PIT FLOOR TRACK CORRODED AT BS 767+5, RBL 14. REMOVED AND REPLACED CHANNEL PER EA.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 21,881 hrs · 12,866 cycles

DURING SCHEDULED 6Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 17. REMOVED AND REPLACED FITTING PER MM.

Part: FITTING — CRACKED (CENTER WING) · airframe 21,881 hrs · 12,866 cycles

DURING SCHEDULED 6Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, RBL 14. REMOVED AND REPLACED FITTING PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,881 hrs · 12,866 cycles

DURING SCHEDULED 6Y CHECK, FOUND R2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 21,881 hrs · 12,866 cycles

DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO CHANNEL CORRODED AT BS 772, RBL 8. REPAIRED CHANNEL PER EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,881 hrs · 12,866 cycles

DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO Z-ANGLE CRACKED AT BS 747+17. REPAIRED Z-ANGLE PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,633 hrs · 12,719 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 21,356 hrs · 12,547 cycles

DURING SCHEDULED MV3 CHECK, FOUND EEPLS LOOSE AT ROW 11. SECURED EEPLS PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 21,101 hrs · 12,391 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 20,642 hrs · 12,106 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD ENTRY EMERGENCY EXIT SIGN LIGHT LOOSE. REMOVED AND REPLACED SIGN PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 18,416 hrs · 10,769 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: RECTIFIER — FAULTY (E&E BAY) · airframe 17,799 hrs · 10,385 cycles

EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY DURING TAKEOFF AND CLIMBOUT. REMOVED AND REPLACED ST11 RECTIFIER, S7 AND S2 SWITCHES PER MM.

Part: CONTROL UNIT — FAULTY (E&E BAY) · airframe 17,799 hrs · 10,385 cycles

EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY DURING TAKEOFF ROLL AND INITIAL CLIMBOUT. REMOVED AND REPLACED SPCU PER MM.

Part: CONTROL UNIT — LOOSE (E&E BAY) · airframe 17,799 hrs · 10,385 cycles

DURING DESCENT AND AFTER LANDING EMERGENCY EXIT LIGHTS CAME ON INTERMITTENTLY. FOUND SPCU LOOSE. RE-SECURED SPCU PER MM.

Part: TRACK — CRACKED (CABIN) · airframe 17,704 hrs · 10,331 cycles

FWD EEPLS TRACK CRACKED. REMOVED AND REPLACED TRACK PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHTS) · airframe 17,047 hrs · 9,914 cycles

EMERGENCY LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 15,992 hrs · 9,266 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 14,688 hrs · 8,483 cycles

FOUND EMERGENCY EXIT FLOOR LIGHT COVER MISSING AT SEAT 1C. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 12,284 hrs · 6,982 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 12,284 hrs · 6,982 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 9,325 hrs · 5,279 cycles

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

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 8,357 hrs · 4,724 cycles

MID CABIN EMERGENCY EXIT SIGN LOOSE. SECURED EXIT SIGN PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 8,052 hrs · 4,558 cycles

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

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 7,876 hrs · 4,462 cycles

FLIGHT ATTENDANT REPORTED SMOKE AND SPARKS FROM AFT COFFEEMAKER. INSPECTED AFT GALLEY AREA, NO EVIDENCE OF SMOKE, ARCHING OR SPARKS. REMOVED AND REPLACED COFFEEMAKERS PER MM AS PRECAUTION.

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 2,053 hrs · 1,163 cycles

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