N792SW

Part: SHEAR TIE — CORRODED (ZN 100 FUS LOWER) · airframe 77,105 hrs · 45,931 cycles

CORROSION ON SHEAR TIE P/N 143A3010-123 BS 400 BETWEEN STR'S 21L AND 22L<[01] UPDATED STEPS 1-5 AND MEASUREMENT PARAMETERS.;[02] TASK CARD COMPLETED.;[03] REMOVED COROSION ON SHEAR TIE; (REMOVED OF DAMAGED MATERIAL ON EDGE) DIMENSION X= WITH OF MATERIAL REMOVED: 0.250' IAW SRM 51-10-02 PARAGRAPH 15.EVALUATED REWORKED AREA; MATERIAL LOSS 0.250' ON AT EDGE FOUND OUT ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-07-1A-1. REMOVED SHEAR TIE. FABRICATED A REPLACEMENT; AND INSTALLED NEW SHEAR TIE; IAW SRM 51-40-05; AMM 51-21-72-370-804; SRM 51-40-02; DWG 143A7902 REV: -; DWG 143A1211 REV: -;[04] VERIFIED CORRECTIVE ACTION #3<BR>VERIFIED MEASUREMENTS

Part: SKIN — CORRODED (ZN 100 FUS LOWER) · airframe 77,105 hrs · 45,931 cycles

FUSELAGE SKIN BULGED WITH EVIDENCE OF SURFACE CORROSION LOCATED AT STATION 400 ON STRINGER 22L<[01] UPDATED MEASUREMENT TABLE; STEP 1 AND 3;[02] REPAIRED FUSELAGE SKIN AT STA 400; STRINGER 22L PER SRM 53-00-01-2R-36.<BR>TASK CARD COMPLETED.;[03] VERIFIED COMPLETE.

Part: SLIDE — OUT OF ADJUST (ZN 800 DOOR) · airframe 77,102 hrs · 45,930 cycles

FORWARD ENTRY DOOR ESCAPE SLIDE. EMERGENCY PULL HANDLE SAFETY FLAP IS NOT COVERING PULL HANDLE.<[01] ADJUSTED FWD ENTRY DOOR ESCAPE SLIDE PULL HANDLE SAFETY FLAP. REF 725-61-06 [TTG8Q00NZW6P] FOR WORK PERFORMED.

Part: SKIN — CORRODED (ZN 100 FUS LOWER) · corrosion level 2 · airframe 77,102 hrs · 45,930 cycles

FUSELAGE SKIN BULGED WITH EVIDENCE OF SURFACE CORROSION LOCATED AT STATION 400 ON STRINGER 22L. ALL WORK ACCOMPLISHED ON CUST CARD TTG8Q00PATM7.

Part: SEAT — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 76,145 hrs · 45,328 cycles

SEAT 11B RECLINE NEEDS LOCKED OUT FOR EMERGENCY EXIT<[01] LOCKED OUT RECLINE AT SEAT 11B AS REQUIRED REFERENCING CMM 25-21-42.

Part: GIRT BAR — LOW (ZN 800 DOOR) · airframe 76,145 hrs · 45,328 cycles

R2 SLIDE GIRT HANGING LOW; SCRUBBING THE FLOOR<[01] ACCOMPLISHED PER MT 725-61-06-AS

Part: PROBE — LEAKING (ZN 400 NACELLE/P) · airframe 76,107 hrs · 45,304 cycles

DURING CLIMB OUT AT 20;000 FT. WE NOTICED FUEL QUANTITY DROPPING IN TANK #1 BY 10-30 LBS EVERY 20-30 SECONDS.DROPPED FROM 8 TO 7400 IN ABOUT 5 MINUTES. FAS DID NOT NOTICE SPRAY FROM ENGINE OR PYLON. PRECAUTIONARY SHUTDOWN FUEL LOSS STOPPED FOLLOWING ENGINE SHUTDOWN.06/30/23 #1 TANK COMP AND TANK PROBE 9 OUT OF LIMITS HGR REQ 2468SCHEDULED FOR 02JUL PHX<[01] PERFORMED #1 ENGINE PART POWER LEAK CHECK IAW AMM 71-00-00; TEST #3B. NO EXTERNAL LEAKS NOTED. ENGINE FUEL USAGE EVEN WITH #2 AT SAME POWER SETTING. PERFORMED TANK AND COMPENSATOR UNIT CAPACITANCE CHECK IAW AMM 28-41-21. FOUND #1 MAIN TANK COMPENSATOR AND TANK UNIT #9 OUT OF TOLERANCE. #1 MAIN FUEL TANK COMP AND TANK UNIT #9 NEED REPLACEMENT. OK TO CONTINUE PER MEL 28-6-01 SP1; SP3 AND SP28. <BR>TRK #142132;[02] R/R #1 MAIN TANK COMPENSATOR; AND F9 PROBE; WORK PERFORMED BY AEROTEAMS; W/O # 66-23101. L/H WING FUEL QUANTITY OPS CHECK GOOD PER AMM 28-41-01. THIS CLEARS MEL; S/PS C/W; REF. LOG PAGE: 2376673.

Part: COMPENSATOR — LEAKING (ZN 400 NACELLE/P) · airframe 76,107 hrs · 45,304 cycles

DURING CLIMB OUT AT 20;000 FT. WE NOTICED FUEL QUANTITY DROPPING IN TANK #1 BY 10-30 LBS EVERY 20-30 SECONDS.DROPPED FROM 8 TO 7400 IN ABOUT 5 MINUTES. FAS DID NOT NOTICE SPRAY FROM ENGINE OR PYLON. PRECAUTIONARY SHUTDOWN FUEL LOSS STOPPED FOLLOWING ENGINE SHUTDOWN.06/30/23 #1 TANK COMP AND TANK PROBE 9 OUT OF LIMITS HGR REQ 2468SCHEDULED FOR 02JUL PHX<[01] PERFORMED #1 ENGINE PART POWER LEAK CHECK IAW AMM 71-00-00; TEST #3B. NO EXTERNAL LEAKS NOTED. ENGINE FUEL USAGE EVEN WITH #2 AT SAME POWER SETTING. PERFORMED TANK AND COMPENSATOR UNIT CAPACITANCE CHECK IAW AMM 28-41-21. FOUND #1 MAIN TANK COMPENSATOR AND TANK UNIT #9 OUT OF TOLERANCE. #1 MAIN FUEL TANK COMP AND TANK UNIT #9 NEED REPLACEMENT. OK TO CONTINUE PER MEL 28-6-01 SP1; SP3 AND SP28. <BR>TRK #142132;[02] R/R #1 MAIN TANK COMPENSATOR; AND F9 PROBE; WORK PERFORMED BY AEROTEAMS; W/O # 66-23101. L/H WING FUEL QUANTITY OPS CHECK GOOD PER AMM 28-41-01. THIS CLEARS MEL; S/PS C/W; REF. LOG PAGE: 2376673.

Part: RETAINER — UNSECURE (GIRT BAR) · airframe 74,795 hrs · 44,463 cycles

FA REPORTS THAT THE FORWARD MAIN ENTRY DOOR EMERGENCY SLIDE ARMING (GIRT) BAR RETAINER CLIPS ARE LOOSE<[01] SECURED GIRT BAR RETAINER REF SRM 51-40-02.

Part: PLATE — CRACKED (ZN 300 STABILIZE) · airframe 74,242 hrs · 44,128 cycles

CRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER 2022-593541 / [01] REPLACED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. PART NUMBER USED:186A3005-2WE. CRACK LENGTH IS: 0.235 INCHES; TOOL USED: DIGITAL CALIPER P/N:500-196-30; S/N:A21033429; DUE DATE: 02-NOV-22.;[02] CERTIFIED WORK PERFORMED.

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 74,242 hrs · 44,128 cycles

CORROSION ON SHIELD LOCATED BTW BS 420 TO BS 440 RBL 24 WL 152.7 AT LEVEL STR 26R FWD CARGO COMPARTMENT 2022-593470 / [01] REPLACED SHIELD LOCATED BTW BS 420 TO BS 440 RBL 24 WL 152.7 AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080 SHEET 15; REV -. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] REPLACED SHIELD LOCATED BTW BS 420 TO BS 440 RBL 24 WL 152.7 AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080 SHEET 15; REV -. SEE INDIVIDUAL SIGNS-OFF BELOW. Ï¿½TEM RII

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 74,242 hrs · 44,128 cycles

CORROSION ON SHIELD LOCATED BTW BS 492.4 TO BS 500A RBL 24 WL 152.7 AT LEVEL STR 26R FWD CARGO COMPARTMENT 2022-593471 / [01] REPLACED SHIELD LOCATED BTW BS 492.4 TO BS 500A RBL 24 WL 152.7 AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080 SHEET 15; REV -. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] REPLACED SHIELD LOCATED BTW BS 420 TO BS 440 RBL 24 WL 152.7 AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080 SHEET 15; REV -. SEE INDIVIDUAL SIGNS-OFF BELOW.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 74,242 hrs · 44,128 cycles

CORROSION SUPPORT ZEE LOCATED ON BS727 TO BS847 LBL 21 WL 156 AFT CARGO COMPARTMENT 2022-593467 / [01] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS847 LBL 21 WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG# 146A7500; SHEET: 37; REV: C; AND SRM 53-00-53-2R-6 REPAIR 6<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[02] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 74,242 hrs · 44,128 cycles

CORROSION SUPPORT ZEE LOCATED ON BS 727 TO BS 767 RBL 21 WL 156 AFT CARGO COMPARTMENT 2022-593466 / [01] REPLACED SUPPORT ZEE LOCATED BTW BS727 AND BS767 RBL 21; WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-60-53-0I-2 IDENTIFICATION 2 AND DWG 146A7502; SHEET: 2; REV: A<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[02] REPLACED SUPPORT ZEE LOCATED BTW BS727 AND BS767 RBL 21; WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-60-53-0I-2 IDENTIFICATION 2 AND DWG 146A7502; SHEET: 2; REV: A <BR>SEE INDIVIDUAL SIGNS-OFF BELOW.<BR>COMPLETED AND CERTIFIED AS RII.

Part: SUPPORT — BROKEN (ZN 500 LEFT WING) · airframe 74,242 hrs · 44,128 cycles

BROKEN HYDRAULIC TUBES GROMMET SUPPORT LOCATED ON TRAILING EDGE AT LEVEL IRSS 177 AT LT WING (FALSE SPAR AREA) 2022-576710 / [01] REPLACED HYDRAULIC TUBES GROMMET SUPPORT LOCATED ON TRAILING EDGE AT LEVEL IRSS 177 AT LT WING IAW B737-700 SRM 51-40-02-0G-0;[02] CORRECTIVE STEP 1 <BR>INSPECTED HYDRAULIC TUBES GROMMET SUPPORT LOCATED ON TRAILING EDGE AT LEVEL IRSS 177 AT LT WING AND WAS FOUND IN SERVICEABLE CONDITION AND IT CHANGED WIRING CLAMP DUE TO WAS FOUND DAMAGE IAW B737-700 SWPM 20-10-12;[03] CORRECTIVE STEP 1 <BR>INSPECTED HYDRAULIC TUBES GROMMET SUPPORT LOCATED ON TRAILING EDGE AT LEVEL IRSS 177 AT LT WING AND WAS FOUND IN SERVICEABLE CONDITION AND IT CHANGED WIRING CLAMP DUE TO WAS FOUND DAMAGE IAW B737-700 SWPM 20-10-12

Part: SKIN — CRACKED (ZN 800 DOOR) · airframe 74,242 hrs · 44,128 cycles

CUSTOMER REQUEST CRACK INTERNAL SKIN LOCATED AFT EDGE AT 20.5 INCH FROM LOWER EDGE FWD ENTRY DOOR. REPAIRED INTERNAL SKIN LOCATED AFT EDGE AT 20.5 INCH FROM LOWER EDGE FWD ENTRY DOOR IAW EA#22-152-03179-WIP1 AND EA#22-152-03179. REPAIRED INTERNAL SKIN LOCATED AFT EDGE AT 20.5 INCH FROM LOWER EDGE FWD ENTRY DOOR IAW EA#22-152-03179-WIP1 AND EA#22-152-03179 RII ACCOMPLISHED.

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 74,242 hrs · 44,128 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING 2022-576711 / [01] TOOL USED: DIGITAL CALIPER P/N:500-752-20; S/N:B20317422; DUE DATE:29-AUG-23.;[02] REPLACED CORRUGATED PLATE AND FASTENERS TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG #115A2001; SHEET 18; REV ?. PART NUMBER USED: 115A2781-16; P.O:2022-208007.<BR>SEE INDIVIDUAL SING OFFS BELOW.;[03] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 74,242 hrs · 44,128 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT LT WING 2022-576642 / [01] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ON TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG # 115A2001; SHEET 18; REV.?. PART NUMBER USED: 115A2781-13; P.O:2022-208006.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ON TRAILING EDGE LOCATED AT LEVEL ORSS 261 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG # 115A2001; SHEET 18; REV.?. PART NUMBER USED: 115A2781-13; P.O:2022-208006. <BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 74,242 hrs · 44,128 cycles

CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2022-576747 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189362;DUE DATE:03-DEC-22.;[02] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.

Part: PLATE — CRACKED (ZN 400 NACELLE/P) · airframe 74,242 hrs · 44,128 cycles

CRACK INBOARD FAN COWL SPRINT PLATE ON ACCESS DOOR 423BL ON ENGINE 2 2022-576731 / [01] REPLACED INBOARD FAN COWL SPRINT PLATE ON ACCESS DOOR 423BL ON ENGINE 2 IAW SRM B737-700 51-40-02;[02] REPLACED INBOARD FAN COWL SPRINT PLATE ON ACCESS DOOR 423BL ON ENGINE 2 IAW SRM B737-700 51-40-02

Part: SUPPORT ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 74,242 hrs · 44,128 cycles

CRACK ON SUPPORT ANGLE ON ACCESS PANEL 651GB AT RT WING 2022-576749 / [01] REPLACED SUPPORT ANGLE ON ACCESS PANEL 651GB AT RT WING IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02;[02] REPLACED SUPPORT ANGLE ON ACCESS PANEL 651GB AT RT WING IAW. B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 74,242 hrs · 44,128 cycles

CRACK ANGLE FLOOR STRUCTURE LOC. BL0 TO LBL 24.75 AND BS 540 AT PASSENGER CABIN 2022-576381 / [01] REPLACED ANGLE FLOOR STRUCTURE LOC. BL0 TO LBL 24.75 AND BS 540 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02; ITEM 9; REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 74,242 hrs · 44,128 cycles

CRACK ANGLE FLOOR STRUCTURE LOC. BL0 TO RBL 24.75 AND BS 540 AT PASSENGER CABIN 2022-576376 / [01] REPLACED ANGLE FLOOR STRUCTURE LOC. BL0 TO RBL 24.75 AND BS 540 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02; ITEM 9; REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: BULB — BURNED (ZN 200 FUS TOP) · airframe 74,242 hrs · 44,128 cycles

BURNED WINDSCREEN LT SIDE EMERGENCY FLASHLIGHTS BULB AT AFT GALLEY AREA (1 EA) 2022-576546 / [01] REPLACED WINDSCREEN LT SIDE EMERGENCY FLASHLIGHTS BULB AT AFT GALLEY AREA (1 EA) IAW ASTRONICS CMM 25-60-02 ASSEMBLY ITEM 2.A(3);[02] TASK CARD COMPLETE.

Part: RETAINER — MISSING (ZN 100 FUS LOWER) · airframe 74,242 hrs · 44,128 cycles

MISSING DOOR CUTOUT RETAINER UPPER SILL AT FWD CARGO COMPARTMENT (4 EA) 2022-576478 / [01] REPLACED RETAINER DOOR CUTOUT UPPER SILL AT FWD CARGO DOOR COMPARTMENT (4EA) IAW B737-700 SRM 51-10-02 Ï¿½TEM 9;[02] CORRECTIVE ACTION CERTIFIED

Part: SUPPORT ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 74,242 hrs · 44,128 cycles

CRACK ON SUPPORT ANGLE ON ACCESS PANEL 551GB OF TRAILING EDGE AT LT WING 2022-576548 / [01] REPLACED SUPPORT ANGLE ON ACCESS PANEL 551GB OF TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. PART NUMBER USED: 115A2752-17; P.O:2022-207563. CRACK LENGTH IS: 0.300 INCHES. TOOL USED: DIGITAL CALIPER: P/N:500-196-30; S/N:A21334251; DUE DATE:04-JUL-23.;[02] TASK COMPLETED

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 74,242 hrs · 44,128 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 218 AT LT WING 2022-576425 / [01] TOOL USED: DIGITAL CALIPER P/N:500-196-30;S/N:A21033429; DUE DATE:02-NOV-22.;[02] REPLACED CORRUGATED PLATE TRAILING EDGE AND FASTENERS LOCATED AT LEVEL IRSS 218 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG #115A2001; SHEET 1; REV.B. PART NUMBER USED: 115A2781-3ATSMRO; P.O: 2022-207712.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED CORRUGATED PLATE TRAILING EDGE AND FASTENERS LOCATED AT LEVEL IRSS 218 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG #115A2001; SHEET 1; REV.B. PART NUMBER USED: 115A2781-3ATSMRO; P.O: 2022-207712. <BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 74,242 hrs · 44,128 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 236 AT LT WING 2022-576431 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 236 AT LT WINGL IAW B737-700 SRM 51-40-02 AND DWG 115A2001; SHEET 1; REV B SEE INDIVIDUAL;[02] STEP 1 CORRECTED.<BR>REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 236 AT LT WINGL IAW B737-700 SRM 51-40-02 AND DWG 115A2001; SHEET 1; REV B. SEE INDIVIDUAL SIGNS-OFF BELOW.;[03] CORRECTIVE ACTION STEP 2 CERTIFIED

Part: LENS — BROKEN (ZN 200 FUS TOP) · airframe 74,242 hrs · 44,128 cycles

BROKEN LENS EMERGENCY LIGHT OVERHEAD STOWAGE BIN 3 LT (1EA) 2022-576242 / [01] REPLACED LENS EMERGENCY LIGHT OVERHEAD STOWAGE BIN 3 LT (1EA) IAW B737-700 AMM-33-51-03-960-802;[02] CORRECTED STEP 1<BR>REPLACED LENS EMERGENCY LIGHT OVERHEAD STOWAGE BIN 3 LT (1EA) IAW BOEING SOPM 20-50-12;[03] REPLACED LENS EMERGENCY LIGHT OVERHEAD STOWAGE BIN 3 LT (1EA) IAW BOEING SOPM 20-50-12

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 74,242 hrs · 44,128 cycles

CRACK BRACKET BS 685 AND LBL 42.75 AT CENTER WING BOX 2022-576229 / [01] TOOLS 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 BRACKET LOCATED EXACTLY AT BS685 AND LBL24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9 DWG 273A9110 SHEET: 3 REV: -;[03] CORRECTED STEP 2<BR>REPLACED BRACKET LOCATED EXACTLY AT BS685 AND LBL24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9 DWG 273A9110 SHEET: 3 REV: - SEE INDIVIDUAL SIGNOFFS BELOW;[04] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 74,242 hrs · 44,128 cycles

CRACK BRACKET LOC BS 685 AND RBL 24.75 AT CENTER WING BOX 2022-576227 / [01] TOOLS 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 BRACKET AND FASTENERS LOC BS 685 AND RBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9 DWG 273A9110 SHEET: 5 REV: A SEE INDIVIDUAL SIGNOFFS BELOW;[03] CERTIFIED STEP 2; COMPLETED. ITEM RII

Part: BATTERY — INOPERATIVE (ZN 900 LAV/GALLE) · airframe 74,242 hrs · 44,128 cycles

INOP CEILING PANEL BATTERY PACK LH AT FWD GALLEY AREA (1 EA) 2022-576232 / [01] REPLACED CEILING PANEL BATTERY PACK LH AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM-33-51-06-960-805;[02] CORRECTED STEP 1<BR>REPLACED CEILING PANEL BATTERY PACK LH AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM-33-51-06-960-805 PERFORMED TEST IS OK;[03] CORRECTIVE ACTION STEP 2 CERTIFIED

Part: BATTERY — INOPERATIVE (ZN 900 LAV/GALLE) · airframe 74,242 hrs · 44,128 cycles

INOP CEILING PANEL BATTERY PACK RH AT FWD GALLEY AREA (1 EA) 2022-576233 / [01] REPLACED CEILING PANEL BATTERY PACK RH AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM-33-51-06-960-805;[02] CORRECTED STEP 1<BR>REPLACED CEILING PANEL BATTERY PACK RH AT FWD GALLEY AREA (1 EA) IAW B737-700 AMM-33-51-06-960-805 PERFORMED TEST IS OK;[03] CORRECTIVE ACTION STEP 2 CERTIFIED

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 74,242 hrs · 44,128 cycles

CRACK ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 270 OF DEFLECTION CONTROL RIB AT RT WING 2022-576154 / [01] REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 270 OF DEFLECTION CONTROL RIB AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. PART NUMBER USED: 115A2963-2; P.O:2022-196669. CRACK LENGTH IS:0.868 INCHES; TOOL USED: DIGITAL CALIPER P/N:500-196-30; S/N:B21140348;DUE DATE:16-JUL-23.;[02] REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 270 OF DEFLECTION CONTROL RIB AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. PART NUMBER USED: 115A2963-2; P.O:2022-196669. CRACK LENGTH IS:0.868 INCHES; TOOL USED: DIGITAL CALIPER P/N:500-196-30; S/N:B21140348;DUE DATE:16-JUL-23.

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 74,242 hrs · 44,128 cycles

CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 18 INCH FROM FRONT SPAR LT HORIZONTAL STAB 2022-576071 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022240; CAL DUE DATE: 27-JAN-23;[02] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 210138503 AND DUE DATE: 19-MAY-23.;[03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER P/N: 112820025; DUE DATE: 01-FEB-23.;[04] PERFORMED REPAIR ON INSPAR RIB LOCATED STAB STA 129.50 AND 18 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW EA #22-155-03137 [TTG8Q00FU9HP]; EA# 22-155-03137-WIP1 [TTG8Q00FMTB7] AND EA# 22-155-03137-WIP2 [TTG8Q00FP0KV];[05] PERFORMED REPAIR ON INSPAR RIB LOCATED STAB STA 129.50 AND 18 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW EA #22-155-03137 [TTG8Q00FU9HP]; EA# 22-155-03137-WIP1 [TTG8Q00FMTB7] AND EA# 22-155-03137-WIP2 [TTG8Q00FP0KV]<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[06] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — OUT OF POSITION (FWD ENTRY DOOR) · airframe 73,967 hrs · 43,939 cycles

FWD ENTRY CAUTION FLAP FOR EMERGENCY SLIDE / [01] RESCURED FWD ENTRY DOOR CAUTION FLAP IAW AMM 25-66-01.

Part: SLIDING SLEEVE — LOOSE (L1 DOOR) · airframe 73,693 hrs · 43,758 cycles

FOWARD ENTRY (L1) DOOR- CAUTION INFLATABLE FLAG EXPOSED / [01] PERFORMED SAFETY OPERATIONAL CHECK OF ESCAPE SLIDE; RESECURED VELCRO OVER FLAG REF AMM. 25-66-00

Part: BATTERY — FAULTY (FWD CABIN) · airframe 73,510 hrs · 43,629 cycles

1 FWD GALLEY EMERGENCY FLASHLIGHT BATTERY NEEDS REPLACEMENT. / [01] R&R 1 FWD GALLEY EMERGENCY FLASHLIGHT BATTERY PER AMM 25-64-00.

Part: SEAL — CRACKED (R/H HORIZ. STAB.) · airframe 73,510 hrs · 43,629 cycles

RH HORIZONTAL STABILIZER LOWER FRONT SPAR SLIDING SEAL IS CRACKED. / [01] R&R RH HORIZONTAL STABILIZER LOWER FRONT SPAR SLIDING SEAL REF AMM 53-31-31.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 70,047 hrs · 41,477 cycles

R1 DOOR FWD EMERGENCY LIGHT LENS LOOSE. ; / REMOVED & REPLACED R1 DOOR FWD EMERGENCY LIGHT LENS REF AMM 33-51-01 NO DEFECTS NOTED.

Part: ANGLE — CRACKED (LT WING) · airframe 68,919 hrs · 40,833 cycles

CRACK FRONT SPAR ANGLE AREA FUEL BOOST PUMP AT LT WING / REPLACED FRONT SPAR ANGLE LOCATED AT FUEL BOOST PUMP LT WING AT 1FS 120 IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING #112A2004 AND 112A2003 AND IAW EA NÏ¿½ 57-0723-20 PART 1

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,919 hrs · 40,833 cycles

CRACK INDICATION FOUND IN OPEN HOLE FROM FIRST FASTENER HOLE FWD BS 540 S-22R FUSELAGE SKIN. CRACK DIRECTIONS: 1 O`CLOCK AND 11 O`CLOCK APPROXIMATE. PERFORMED REPAIR ON DRAG LINK ON BS 540 STR 22R FUSELAGE SKIN, IAW EO 5331-E-14523 REV 1.

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 68,919 hrs · 40,833 cycles

DENT FLOOR PANEL BS 257 LBL 12 AT COCKPIT (1 EA). REPAIRED FLIGHT DECK FLOOR WEB LOCATED FROM BS 250 TO BS 270 BETWEEN RBL 10 AND LBL 20, IAW SWA EA NR 1-A53-33179 REV 1.

Part: COVER — CRACKED (BS 291) · airframe 68,919 hrs · 40,833 cycles

(CRACK ON GAP COVER LOCATED AT FORWARD GALLEY DOOR AREA BSTA 291.5) / REPLACED GAP COVER LOCATED AT FORWARD GALLEY DOOR AREA BSTA 291.5 IAW B737-700 SRM 51-40-02 AND DWG 141A8350 REV

Part: CARGO TRACK — CRACKED (FWD CARGO) · airframe 68,919 hrs · 40,833 cycles

CRACK TRACK ON RBL 14 AT BS 460 AT FWD CARGO COMPARTMENT. REPAIRED CARGO TRACK LOCATED RBL 14 FROM BS 400 TO BS 500A, IAW SRM B737-700 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1; FIG 203 AND DWG 143A7500 REV -.

Part: SUPPORT ANGLE — CRACKED (BS 907-927) · airframe 68,919 hrs · 40,833 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS 907 TO BS 927 AND STRINGER 25 R AND SRINGER 26R AT AFT CARGO COMPARTMENT (1 EA) / INSTALLED ANGLE-SUPPORT LOCATED BETWEEN BS 907 TO BS 927 AND STR 25R AND STR 26R AT AFT AFT CARGO COMPARTMENT IAW B737-700 DWG 147A7221-37 SHEET 17 REV.0

Part: STUB FRAME — CRACKED (FUSELAGE) · airframe 68,919 hrs · 40,833 cycles

CRACK FRAME STUB LOCATED S-7 TO S-9 AND BS 294.5 RT SIDE AT PASSENGER CABIN (1 EA). REPLACED FRAME STUB LOCATED S-7 TO S-9 AND BS 294.5 RT SIDE AT PASSENGER CABIN, IAW B737-700 SRM 51-40 -02 AND DWG 141A8370 REV D.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 68,919 hrs · 40,833 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727D TO BS 767 RBBL 22.5 AT LEVEL STRINGER 25R AFT CARGO COMPARTMENT LOCATED AT WL157 (1 EA). REPLACED SUPPORT ZEE LOCATED BS 727 TO BS 767 RBL 22.5 AT LEVEL STRINGER 25R AFT CARGO COMPARTMENT, IAW B737-700 SRM 51-40-07 AND DRAWING 146A7500.

Part: SUPPORT ANGLE — CRACKED (BS 500C S25R) · airframe 68,919 hrs · 40,833 cycles

CRACK ANGLE - SUPPORT LOCATED BS 500C AT LEVEL STR 25R FWD CARGO COMPARTMENT / REPLACED ANGLE-SUPPORT LOCATED ON BS 500C AT LEVEL STR 25R FWD CARGO COMPARTMENT IAW B737- 700 SRM 51-40-02 AND DWG #143A7505; SHEET 6; REV D.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,919 hrs · 40,833 cycles

CRACK STRINGER 26L AT BS 540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 26L AT BS 540 FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIG 206.

Part: ANGLE — BROKEN (BS 663) · airframe 68,919 hrs · 40,833 cycles

BROKEN ANGLE WING TO BODY FAIRING LOCATED ON BS 663 AT LEVEL LBBL 28 AT LOWER FUSELAGE / REPLACED ANGLE WING TO BODY FAIRING LOCATED ON BS663 AT LEVEL LBL 28 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-07 AND DWG #149A7210 SHEET 6 REV B

Part: STRINGER — CRACKED (FWD CARGO) · airframe 68,919 hrs · 40,833 cycles

CRACK STRINGER 25L AT BS 540 AT FWD CARGO COMPARTMENT. REPAIRED STRINGER 25L AT BS 540 AT FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIG 206.

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 68,919 hrs · 40,833 cycles

CRACK GUSSET LOCATED BS 500D STRINGER 19R FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED BS 500D STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 21 REV E

Part: FITTING — ELONGATED (BS 1016 BL0) · airframe 68,919 hrs · 40,833 cycles

ELONGATED HOLE ON BS 1016 FITTING; BL 0; UPPER POSITION AT AFT G ALLEY AREA (2 EA) / REPLACED FITTING LOCATED OB BS 1016 BLO UPPER POSITION AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND DRAWING #148A2230 REV.C

Part: STRINGER — CRACKED (FWD CARGO BAY) · airframe 68,919 hrs · 40,833 cycles

CRACK STRINGER 25R AT BS 540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 25R AT BS 540 FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-212-1 REPAIR 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 68,919 hrs · 40,833 cycles

CRACK STRINGER 26R AT BS 540 FWD CARGO COMPARTMENT. REPAIRED STRINGER 26R BETWEEN BS 500D AND BS 540 FWD CARGO COMPARTMENT, IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206.

Part: GUSSET — CRACKED (BS 500D S21R) · airframe 68,919 hrs · 40,833 cycles

CRACK GUSSET LOCATED BS500D STRINGER 21R FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED BS 500D STRINGER 21R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DRAWING #143A7902

Part: SCUFF PLATE — BROKEN (FWD CARGO) · airframe 68,919 hrs · 40,833 cycles

BROKEN AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT / REPAIRED BY WELDS AFT CORNER SCUFF PLATE AT FWD CARGO COMPARMTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4B STEP #4 AND BAC 5975

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 68,919 hrs · 40,833 cycles

CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT / REPAIRED BY WELDS FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4B STEP #4 AND BAC 5975

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 68,919 hrs · 40,833 cycles

CRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG PAX CABIN CENTER SECTION (6 EA). REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ALONG PAX CABIN CENTER SECTION (6 EA), IAW WORK INSTRUCTION N 733-50-01.

Part: SPAR — CORRODED (LT WING) · airframe 68,919 hrs · 40,833 cycles

CORROSION FUEL BOOST PUMP FAYING SURFACE FRONT SPAR AT LT WING LOCATED AT WBL 94.24 AND IFSS 120.00. / REPAIRED FRONT SPAR WEB AT IFSS 120.00 WBL 94.24 FAYING SURFACE I.A.W. SWA EA N.20-157-02253 REV IR AND AE EA N.57-0723-20 REV #0 AND 1

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,919 hrs · 40,833 cycles

CRACK INDICATION FOUND FROM FASTENER HOLE NEAR FITTING LATCHING ON BEAR STRAP AT STA 294.5 3 INCH BELOW STRINGER 8R FWD GALLEY DOOR AREA, CRACK LENGTH= 0.150 INCH APPROXIMATE. PERFORMED CATEGORY B REPAIR ON EXTERNAL SKIN AND BEAR STRAP LOCATED BETWEEN BS 286 AND BS318 AND BETWEEN STRG 7R AND STRG 10R, IAW B737-700 SRM 53-10-01-2R-6 REPAIR 6 FIGURE 202 FOR REQUIREMENT INSPECTION SEE TLD T080502.

Part: MOUNT — DETERIORATED (R1 DOOR) · airframe 68,919 hrs · 40,833 cycles

DETERIORATED EMERGENCY DOOR RT MOUNT AT PASSENGER CABIN. REPLACED SHOCK MOUNT EMERGENCY DOOR RT AT PASSENGER CABIN, IAW B737-700 SRM 51-40-02-0G-0, 51-40-03-0G-0 AND DWG 144A8111 SHEET 7 REV D.

Part: PLATE — DETERIORATED (R2 DOOR GIRT BAR) · airframe 68,919 hrs · 40,833 cycles

DETERIORATED GIRT BAR FITTING HARDWARE, PLATE ASSEMBLY AT AFT GALLEY AREA. REPLACED HARDWARE GIRT BAR FITTING, PLATE ASSEMBLY AFT GALLEY AREA, IAW AMM 25-66-02-400-801.

Part: PLATE — DETERIORATED (R1 DOOR GIRT BAR) · airframe 68,919 hrs · 40,833 cycles

DETERIORATED GIRT BAR FITTING HARDWARE, PLATE ASSEMBLY AT FWD GALLEY AREA. REPLACED GIRT BAR FITTING HARDWARE PLATE ASSEMBLY AT FWD GALLEY AREA, IAW B737-700 AMM 25-66-02-400-801.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,919 hrs · 40,833 cycles

CRACK TIE CLIP ON BS 270 AT LEVEL STR 10R AT PASSENGER CABIN. REPLACED TIE CLIP LOCATED ON BS 270 AT LEVEL STR 10R AT PASSENGER CABIN, IAW B737-700 SRM 51-40-02 DWG 141A1110 SHEET 18 REV- SRM 51-40-02 ITEM 9.

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,919 hrs · 40,833 cycles

CRACK INDICATION FROM FIRST FASTENER HOLE FWD BS 540 ABOVE S-22R, FUSELAGE SKIN DRAG LINK AREA, CRACK LENGTH: 0.100 INCH APPROXIMATE. FASTENER MUST BE REMOVED TO CONFIRM BY ROTOTEST INSPECTION, IAW NDT MANUAL PART 453-30-02 IN FWD CARGO COMPARTMENT. THIS REPAIR WAS ACCOMPLISHED ON EO 5331-E-14523 AND STEPS ARE DOCUMENTED ON LOG PAGE L182548.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 68,919 hrs · 40,833 cycles

CRACK SLAT 6 LOWER SURFACE AT RT WING (3 EA). REPAIRED SKIN SLAT 6 LOWER SURFACE AT RT WING, IAW EA NR 20-157-02216 REV IR EA NR 57-0724-20 REV O AND EA NR 57-0724-20 PART 1 (ACTUATOR RIB AREA).

Part: SUPPORT ANGLE — CRACKED (VERTICAL STAB) · airframe 68,919 hrs · 40,833 cycles

CRACK ACCESS DOOR 323AL ON SUPPORT ANGLE VERTICAL STABILIZER. REPLACED SUPPORT ANGLE LOCATED ON ACCESS PANEL 323AL AT VERTICAL STABILIZER, IAW B737-700 SRM 51-10-02 SRM 51-40-02 AND DRAWINGS 172A6122 REV B.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,919 hrs · 40,833 cycles

CRACK INSPAR RIB LOCATED STAB STA 129.50 AT 35 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER. REPAIRED INSPAR RIB LOCATED AT STAB STA 129.50 AT 35' FROM FRONT SPAR AT RT HORIZONTAL STABILIZER, IAW SRM B737-700 55-10-09-2R-5 REPAIR 5 FIG 204 AND REPAIR STEPS ARE DOCUMENTED ON NRC NR L182220.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,919 hrs · 40,833 cycles

CRACK INSPAR RIB LOCATED STAB STA 129.50 AT 27 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER. REPAIRED INSPAR RIB LOCATED AT STAB STA 129.50 FROM 22' TO 38' FROM FRONT SPAR RT HORIZONTAL STABILIZER, IAW SRM B737-700 55-10-09-2R-5 REPAIR 5 FIG 204.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,919 hrs · 40,833 cycles

CRACK LEADING EDGE RIB LOCATED LEADING EDGE STA114.55 LT HORIZONTAL STABILIZER. INSTALLED NEW RIB LOCATED LEADING EDGE STA 114.5 LT HORIZONTAL STABILIZER, IAW B737-700 SRM 51-40-02 AND DWG 186A1001 SHEET 10 REV A.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,919 hrs · 40,833 cycles

CRACK INSPAR RIB LOCATED STAB STA 129.50 AT 27 INCH FROM FRONT SPAR LT HORIZONTAL STAB. PERFORMED REPAIR INSPAR RIB LOCATED STAB 129.50 AT 27 INCH FROM FRONT SPART LT HORIZONTAL STAB, IAW B737-700 SRM 55-10-09-2R-4 FIGURE 202.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,919 hrs · 40,833 cycles

CRACK LEADING EDGE RIB LOCATED AT LEADING EDGE STA 78.29 RT HORIZONTAL STABILIZER. REPLACED LEADING EDGE RIB LOCATED AT LEADING EDGE STA 86.66 RT HORIZONTAL STAB, IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 186A 1001 REV A.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,919 hrs · 40,833 cycles

CRACK LEADING EDGE RIB LOCATED AT LE STA 86.66 AT LT HORIZONTAL STABILIZER. REPLACED RIB LOCATED LEADING EDGE STA 95.96 AT LT HORIZONTAL STABILIZER, IAW B737-700 SRM 51-40-02 DWG 186A1001 REV A AND SRM 51-10-02 ITEM 9.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 68,919 hrs · 40,833 cycles

CRACK LEADING EDGE RIB LOCATED AT LEADING EDGE STA 95.96 RT HORIZONTAL STABILIZER. INSTALLED NEW RIB LOCATED AT LEADING EDGE HORIZONTAL STABILIZER LEADING EDGE STA 105.25, IAW B737-700 SRM 51-40-02 DWG 186A1001 SHEET 10 REV A.

Part: FAIRING — CRACKED (LT WING) · airframe 68,883 hrs · 40,813 cycles

REAR LANDING GEAR SUPPORT BEAM LOWER T/E PANEL LOWER FAIRING IS CRACKED / REMOVED AND REPLACED L/H WING REAR LANDING GEAR SUPPORT BEAM LOWER T/E PANEL LOWER FAIRING IAW AMM 20-50-11.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 68,883 hrs · 40,813 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01669. R & R EMERGENCY LIGHT BATTERY PACK AT LOCATION M01669, PER AMM 33-51-06.

Part: FAIRING — BROKEN (RT WING) · airframe 68,883 hrs · 40,813 cycles

RIGHT WING AFT LANDING GEAR SUPPORT BEAM LOWER PANEL AERODYNAMIC FAIRING BROKEN. / REMOVED AND REPLACED RIGHT WING AFT LANDING GEAR SUPPORT BEAM LOWER PANEL AERODYNAMIC FAIRING IAW AMM 20-50-11.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 68,098 hrs · 40,283 cycles

SEVERAL EMERGENCY LTS IN CABIN LH SIDE INOP. / REPLACED BATTERY & PACK CHARGER AT STA. 727 IAW MM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,098 hrs · 40,283 cycles

SEVERAL EMERGENCY LTS IN CABIN LH SIDE INOP. / REPLACED BATTERY & PACK CHARGER AT STA. 727 IAW MM 33-51-06.

Part: BATTERY — DISCHARGED (CABIN) · airframe 67,987 hrs · 40,212 cycles

FWD L/H EMERGENCY LIGHT BATTERY INOP / REMOVED AND REPLACED FWD L/H EMERGENCY LIGHT BATTERY REF AMM 33-51-06. OPS CHECKED GOOD.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,949 hrs · 40,190 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING; LOWER I/B LUG; OUTER FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,949 hrs · 40,190 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING; LOWER I/B LUG; OUTER FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,949 hrs · 40,190 cycles

R/H MLG FWD TRUNNION SUPORT FITTING UPPER I/B LUG BORE HAS EVIDENCE OF CORROSION. / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,949 hrs · 40,190 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING; UPPER I/B LUG BORE HAS EVIDENCE OF CORROSION. / REPAIRED PER EA NO: 1-A57-3246

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,949 hrs · 40,190 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING LOWER O/B LUG; INNER LUG FACE HAS EVIDENCE OF CORROSION. / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,949 hrs · 40,190 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING; LOWER O/B LUG; OUTER FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,949 hrs · 40,190 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING LOWER O/B LUG BORE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,949 hrs · 40,190 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING; UPPER I/B LUG; OUTER FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,949 hrs · 40,190 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING LOWER I/B LUG; INNER LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,949 hrs · 40,190 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING; LOWER O/B LUG; INNER LUG FACE HAS EVIDENCE OF CORROSION. / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,949 hrs · 40,190 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING; LOWER O/B LUG; OUTER FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,949 hrs · 40,190 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING LOWER I/B LUG; INNER LUG FACE HAS EVIDENCE OF CORROSION. / REPAIRED PER EA NO: 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,949 hrs · 40,190 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING; UPPER O/B LUG; OUTER FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,949 hrs · 40,190 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING; UPPER O/B LUG; OUTER FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,949 hrs · 40,190 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING; UPPER I/B LUG; OUTER FACE HAS EVIDENCE OF CORROSION. / REPAIRED PER EA NO: 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,949 hrs · 40,190 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING; LOWER O/B LUG BORE HAS EVIDENCE OF CORROSION. / REPAIRED PER EA NO: 1-A57-3246

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,949 hrs · 40,190 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING; LOWER I/B LUG BORE HAS EVIDENCE OF CORROSION. / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,949 hrs · 40,190 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING UPPER O/B LUG BORE HAS EVIDENCE OF CORROSION. / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,949 hrs · 40,190 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING LOWER I/B LUG BORE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,949 hrs · 40,190 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING UPPER O/B LUG BORE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,218 hrs · 39,125 cycles

R/H EMERGENCY LIGHTS ON OVERHEAD BINS INOP BETWEEN ROW 2 TO ROW 6. R&R BATTERY PACK M1674 IAW AMM.

Part: WINDOW — ARCED (COCKPIT) · airframe 64,787 hrs · 38,202 cycles

L1 WINDOW ARCED IN LOWER RIGHT CORNER. R&R L1 WINDOW ASSEMBLY PER AMM.

Part: CONTROLLER — DEFECTIVE (COCKPIT) · airframe 64,787 hrs · 38,202 cycles

L1 WINDOW ARCED IN LOWER RIGHT CORNER. R&R WINDOW HEAT CONTROLLER PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 64,448 hrs · 37,978 cycles

FORWARD ENTRY ESCAPE SLIDE NOT SECURE. REPOSITIONED SLIDE INSIDE CASE PER MT.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 64,188 hrs · 37,825 cycles

FLIGHT ATTENDANT REPORTED R2 DOOR SLIDE GIRT BAR CLIP WAS LOOSE. R&R SLIDE PER MT.

Part: SLIDER — CRACKED (R/H HORIZ. STAB.) · airframe 63,312 hrs · 37,248 cycles

RIGHT HAND HORIZONTAL STABILIZER UPPER FORWARD SLIDER SEAL CRACKED / REMOVED AND REPLACED RIGHT HAND HORIZONTAL STABILIZER UPPER FORWARD SLIDER IN REF TO AMM 53-31-31.

Part: SLIDER — CRACKED (L/H HORIZ. STAB.) · airframe 63,312 hrs · 37,248 cycles

LEFT HAND HORIZONTAL STABILIZER UPPER FORWARD SLIDER SEAL CRACKED / R AND R SLIDER PER M/M REF. 53-31-31.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,278 hrs · 37,225 cycles

OVERHEAD BIN EMERGENCY LIGHT INOP AT ROW 13. R&R LIGHT IAW AMM.

Part: STRIP — BROKEN (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

AFT CARGO BAY FLOOR SPLICE STRIP ASSEMBLY BROKEN AT BS 727D-5. R&R FLOOR STRIP PER SRM AND DWG.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

FORWARD CARGO COMPARTMENT BAFFLE CRACKED BETWEEN BS 500B TO BS 500C. R&R BAFFLE IAW SRM AND DWG.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 63,278 hrs · 37,225 cycles

FORWARD SIDE LOWER RT VAPOR BARRIER WEB STIFFENER CRACKED AT BS 663. R&R STIFFENER IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

FORWARD CARGO BAY INTERCOSTAL BAFFLE CRACKED BETWEEN BS 500A TO BS 500B, LBL 24. REPAIRED INTERCOSTAL PER ER AND EA.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,278 hrs · 37,225 cycles

SUPPLEMENTAL INFORMATION: AFT CABIN FLOOR BOARD PANEL 241ABF HAS DAMAGE AT CENTER AFT EDGE / AFT CABIN FLOOR BOARD PANEL 241ABF DAMAGE AT CENTER AFT EDGE REPAIRED IAW SRM 53-00-50-2R-6.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,278 hrs · 37,225 cycles

FLOORBOARD 222BF HAS DISBOND AT (5) INSERT LOCATIONS / FLOOR BOARD 222BF DISBOND A (5) INSERT LOCATIONS REPAIRED IAW SRM 53-00-50-2R-1

Part: BRACKET — CORRODED (LOWER INT FUSELA) · airframe 63,278 hrs · 37,225 cycles

***CORROSION*** FOUND ON INTERIOR SURFACE OF TOILET SERVICE PAN. APPROX. STA 852 S24L. / REMOVED CORRODED INT AREA OF LAV PAN BRACKET + REPLACED WITH NEW INT. OF LAV PAM BRACKETS P/N 145A7401-1 IAW SRM 51-10-02-0G-0 + 51-40-02-0G-0 + 51-40-05-0G-0; DWG 146A7400.7401

Part: FLOOR PANEL — DEBONDED (CABIN) · airframe 63,278 hrs · 37,225 cycles

FLOORBOARD 242UF HAS DISBOND AT PREVIOUS REPAIR / FLOORBOARD 242UF DISBOND AT PREVIOUS REPAIR-REPAIRED IAW SRM 53-00-50-2R-0 AND IAW SRM 53-00-50-2R-7. PREVIOUS REPAIR REMOVED AND REPLACED

Part: SUPPORT — CORRODED (LOWER INT FUSELA) · airframe 63,278 hrs · 37,225 cycles

**CORROSION ** ON WASTE TANK FWD POST BS 947 RBL 21 BULKHEAD FLOOR SUPPORT / REMOVED AND REPLACED BULKHEAD FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 149A8117 REV C AND DWG 149A818 REV B AT STA 947 RBL 21 80003U 5NOV18

Part: TRACK — CORRODED (CABIN) · airframe 63,278 hrs · 37,225 cycles

SEAT TRACK PITTED ON UPPER SURFACE AT STATION 592 LBL 24 / REMOVAL AND INSTALLATION OF NEW SEAT TRACK FROM STA. 540 TO STA. 727 LBL 24 ON CUSTOMER CARD N162878 800976 INTER-5096

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

FORWARD CARGO RT FORWARD SHIELD CORRODED AROUND MULTIPLE FASTENER HOLES. R&R SHIELD IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

FORWARD CARGO RT AFT SHIELD CORRODED AROUND MULTIPLE FASTENER HOLES. R&R SHIELD IAW SRM & DWG.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

CABIN FLOOR BOARD PANEL 221FF HAS DELAMINATION AT CENTER OF PANEL LOWER SURFACE. / REPAIRED DELAMINATION AT CENTER OF CABIN FLOOR PANEL 221FF LOWER SURFACE PER SRM 53-00-50-2R-7

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

VAPOR BARRIER FORWARD SIDE SUPPORT BRACKET CRACKED AT BS 663, RBL 8. R&R ANGLE IAW ER AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

AFT CARGO PIT FLOORBEAM CORRODED AT BS 727+12, RBL 14. R&R FLOORBEAM IAW SRM & DWG.

Part: SUPPORT STRAP — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

FLOORBEAM SUPPORT STRAP CORRODED AT BS 772, BETWEEN RBL 21 TO LBL 21. REPAIRABLE STRAP IAW SRM.

Part: PAN — CORRODED (LOWER INT FUSELA) · airframe 63,278 hrs · 37,225 cycles

AFT CARGO COMPARTMENT; STA 910 S27R HAS CORROSION AT FWD. POTABLE WATER PAN / REPAIRED POTABLE WATER PAN STA 910 STR 27 R/H PER ATS ER 18-04936 REV IR AND SWA EA 1-753-33567 REV IR.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

FORWARD CARGO RT FLOOR TO SIDEWALL SUPPORT CHANNEL CORRODED BETWEEN BS 494 TO BS 500D. R&R SUPPORT IAW SRM AND DWG.

Part: WEB — CORRODED (FWD CARGO THRESH) · airframe 63,278 hrs · 37,225 cycles

FWD CARGO DOOR SUB THRESHOLD HAS SEVERAL SPOTS OF CORROSION ON UPPER SURFACE / EVALUATED CORROSION ON FWD CARGO DOOR SUB THRESHOLD WEB. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1; G; (2);(B) FIG 103 DETAIL D. REMOVED AND REPLACED FWD CARGO DOOR SUB THRESHOLD WEB WITH NEW P/O# 706219. IAW SRM 51-40-02-0G-0 AND DWG# 143A8330 ID:21. 57403U 10/21/2018

Part: INTERCOSTAL — CORRODED (LOWER INT FUSELA) · airframe 63,278 hrs · 37,225 cycles

AFT CARGO COMPARTMENT; STA 862; S25L TOILET SERVICE PAN HAS CORROSION / REMOVED CORRODED TOILET SERVICE PAN SUPPORT BRACKET + REPLACED WITH NEW P/N 146A7401-1 IAW SRM 51-40-02-0G-0; 51-40-05-0G-0 + BOEING DWG# 1461A7400

Part: SKIN — CORRODED (AFT FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

SEVERAL AREAS OF LIGHT CORROSION ON EXTERIOR FUSELAGE SKIN; STA 927 - STA 1006; BETWEEN STR'S 2L & 2R / REPAIRED FUSELAGE SKIN BS 927-1006 STR 2L-2R PER ATS ER 18-05087 REV IR AND SWA EA 1-753-33564 REV IR.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,278 hrs · 37,225 cycles

AFT CARGO COMPARTMENT TRACK CORRODED AT BS 934, RBL 14. R&R TRACK IAW SRM & DWG.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 63,278 hrs · 37,225 cycles

AFT CARGO COMPARTMENT; STA 867 TO 887 LBL 10 ANGLE SUPPORT HAS 05 NUT PLATE CORRODED. / REMOVED AND REPLACED CORRODED NUT PLATES ON AFT CARGO ANGLE SUPPORT STA 867 TO 887 LBL 10 IAW SRM 51-40-02-0G-0 57305U 11/1/18

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

FORWARD CARGO LT FLOOR TO SIDEWALL SUPPORT CHANNEL CORRODED BETWEEN BS 440 TO BS 500D. R&R CHANNEL IAW SRM AND DWG.

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 63,278 hrs · 37,225 cycles

FORWARD SERVICE DOOR 141A6535-4 LOWER BEAM #4 ASSEMBLY IS CRACKED ON THE INBOARD; FORWARD RADIUS. REF TO CUSTOMER CARD NBR: 14079 STEP 4.B. / DUE TO LOWER BEAM #4 ASSY BEING CRACKED; FORWARD SERVICE DOOR BEING REPLACED. ALL WORK REPLACING FORWARD SERVICE DOOR ON CUSTOMER CARD #N162619.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,278 hrs · 37,225 cycles

RT HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 663, RBL 44. REPAIRED WEB IAW EA.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 63,278 hrs · 37,225 cycles

***CORROSION*** AFT CARGO COMPARTMENT R/H TRANSITION STRIP HAS CORROSION STA. 727 TO 767 RBL 21 / CORROSIO ON R/H FLOOR TO SIDEWAL SUPPORT FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; REMOVED AND REPLACED R/H FLOOR TO SIDEWALL SUPPORT; ITEM BAC 1496-377; P.O.# 679044/1; LOT# 5067496-1; IAW SRM 51-40-02-0G-0; AND BOEING DWG'S 146A7500; 146A7502 57649U 10/26/18 R/H TRANSITION STRIP CHANGED FROM BS 727-767

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

AFT CARGO COMPARTMENT RT TRANSITION STRIP CORRODED BETWEEN BS 867 TO BS 947, RBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

AFT CARGO COMPARTMENT RT AFT SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 21. R&R SHIELD IAW SRM AND DWG.

Part: TRACK — CORRODED (AFT CARGO BAY) · airframe 63,278 hrs · 37,225 cycles

***CORROSION*** AFT CARGO COMPARTMENT TRACK HAS MANY AREAS OF CORROSION STA. 777 TO STA. 847 RBL 14 / REMOVED; LOCATED & DRILLED; & INSTALLED NEW AFT CARGO COMPARTMENT TRACK FROM STA 777- STA 841 RBL 14 IAW SRM 51-40-02-0G-0; SRM 51-40-05; DWG 146A7501; & DWG 146A7500 SHEET 2. REMOVED CORROSION FROM MULTIPL MULTIPLE AREAS ON OR ORIGINAL SEAT TRACK WITH THE AREA OF L 10.0' X W 1.00 X D0.010' AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG. 103. 56379U 07NOV18

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 63,278 hrs · 37,225 cycles

***CORROSION*** AFT CARGO COMPARTMENT R/H FWD SHIELD ON BOTTOM SURFACE HAS CORROSION STA. 767 TO 787 RBL 21 / REMOVED DAMAGED SHIELD IN AFT CARGO BAY FWD BS 767- 787 RBL 21 & INSTALLED NEW SHIELD P/N 146A8127- IAW DWG 146A0081 REV A & SRM 51-40-02-0G-0. SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 63,278 hrs · 37,225 cycles

***CORROSION*** AFT CARGO COMPARTMENT L/H TRANSITION STRIP HAS CORROSION STA. 727 TO 847 LBL 21 / CORROSION ON L/H FLOOR TO SIDEWALL SUPPORT AT STA 727-847 LBL 21 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED L/H FLOOR TO SIDEWAL SUPPORT; ITEM #BAC 1496-377; P.O# 679044/ 1; LOT # 5067496-1; IAW SRM 51-40-02-0G-0; SRM 53-00-53-2R-5; REPAIR 5; AND BOEING DWG'S 146A7500; 146A7502; VERIFIED SPLICE LOCATION AT L/H STA 7276E10. 57649U 10/23/18

Part: PLATE — CORRODED (AFT CARGO BAY) · airframe 63,278 hrs · 37,225 cycles

***CORROSION*** AFT CARGO COMPARTMENT THRESHOLD SUB PLATE HAS CORROSION STA. 801 TO 837 RBL 26 / REMOVED AND REPLACED AFT CARGO SUB THRESHOLD WEB PORT #7530091 PO# 708855 IAW SRM 51-40-02 AND BOEING DRAWING 146A8340 93036U 10-29-18

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS 807 TO BS 827, RBL 19. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 63,278 hrs · 37,225 cycles

**CORROSION** STA. 951; WL 208; RBL 32 CORROSION MARKED AROUND FASTNER HOLE. / REMOVE + REPLACED INTERCOSTAL STA. 951 WL208 RBL32 IAW SRM 51-40-02 80003U 31OCT18

Part: RETAINER — CRACKED (LT WING) · airframe 63,278 hrs · 37,225 cycles

L/H WING ORSS 261 +10 INCHES HAS SEAL RETAINER BRACKET CRACKED ON AFT SIDE.( MARKED) / REMOVED & REPLACED L/H WING SEAL RETAINER BRACKET FITTING & WEB AT ORSS 261 + 10 INCHES IAW SRM 51-40-02-0G-0 PAR 4

Part: WEB — CORRODED (MAIN CABIN) · airframe 63,278 hrs · 37,225 cycles

**CORROSION** STA. 1016; WL 208; RBL 5 CORROSION MARKED IN FLOOR WEB. / REPAIRED DAMAGE FLOOR WEB AT BS 1016; WL 208; RLB 5 IAW ATS ER 18-05024 IR & SWA EA 1-753-33545IR

Part: BEAM — CORRODED (MAIN CABIN) · airframe 63,278 hrs · 37,225 cycles

**CORROSION** STA. 986.5; WL 208; LBL 0-48 CORROSION MARKED IN SEVERAL AREAS ALONG BEAM. / THE DAMAGE IS REPAIRED PER ATS ER 18-04724 REV IR EA 1-753-33523 REV IR. ALL WORK PREFORMED ON DEFECT N167502 23959R 11/8/18

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

L2 DOOR LOWER SILL INNER CORD CORRODED AT BS 967, LBL 54. REPAIRED CHORD IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 0 TO RBL 48. REPAIRED FLOOR BEAM IAW ER & EA.

Part: STRUCTURE — CORRODED (R2 DOOR) · airframe 63,278 hrs · 37,225 cycles

R2 DOOR INNER CHORD CORRODED BETWEEN BS 967 TO BS 975, WL 208. R&R INNER CHORD PER SRM & DWG.

Part: FRAME — CRACKED (FWD SERVICE DOOR) · airframe 63,278 hrs · 37,225 cycles

STUB FRAME FWD OF R1 DOOR IS CRACKED AT STA. 296.5 WL 208 RBL 53 (MARKED) / REPAIRED R1 STUB FRAME AT BS 296.5; WL 208 RBL 53 IAW ATS 18-0-4716; IR AND SWA EA 1- 753-33515 IR

Part: PANEL — DELAMINATED (LT WING) · airframe 63,278 hrs · 37,225 cycles

L/H WING PANEL 521WB HAS DISBONDED FWD O/B CORNER (MARKED) / REPAIRED LH WING PANEL 521WB DISBOND ON FWD O/B CORNER I.A.W 737 SRM 57-41-01-2R-1 PARA 1; 4E TABLE 202 250Ï¿½F CURE PER 737 SRM 51-70-05 REPAIR 10

Part: PANEL — DELAMINATED (RT WING) · airframe 63,278 hrs · 37,225 cycles

R/H WING PANEL 621YB HAS DISBONDED FWD I/B CORNER (MARKED) / REPAIRED RH WING PANEL 621YB DISBOND ON FWD I/B CORNER I.A.W 737 SRM 57-41-01-2R-1 PARA 1; 4E TABLE 202; 250Ï¿½F CURE PER 51-70-05 REPAIR 10

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, BL 30.5. R&R INTERCOSTAL PER SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

L1 DOOR INNER ANGLE CUTOUT CORRODED BETWEEN BS 312 TO BS 344, LBL 57. R&R INNER ANGLE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL PER SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

L1 DOOR LOWER CUTOUT INNER CHORD CORRODED BETWEEN BS 312 TO BS 344, LBL 54. R&R INNER CHORD IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500D, STR 21L. R&R GUSSET IAW DWG AND SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

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

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

ANGLE ASSEMBLY CRACKED BETWEEN BS 294 TO BS 312, RBL 15. R&R ANGLE ASSEMBLY IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 63,278 hrs · 37,225 cycles

LOWER VAPOR BARRIER BULKHEAD CRACKED AT BS 663, LBL 25. REPAIRED BULKHEAD IAW SRM.

Part: ANGLE — CORRODED (MAIN CABIN) · airframe 63,278 hrs · 37,225 cycles

***CORROSION*** CORROSION ON OUTER Z ANGLE ON L1 DOOR CUTOUT BS 312 TO BS 344 LBL 60 WL 208 / REMOVED AND REPLACED OUTER Z AGLE ON L1 DOOR CUTOUT BS 312 TO BS 344 LBL 60 WL 208. ANGLE P/N 7530973 PO# 701508 IAW SRM 51-40-02-0G-0 DWG 141A8110 80819U 10/15/18

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,278 hrs · 37,225 cycles

R1 DOOR LOWER CUTOUT CORRODED BETWEEN BS 312 TO BS 344, RBL 57. R&R CUTOUT IAW SRM & DWG.

Part: SKIN — CRACKED (LT WING) · airframe 63,278 hrs · 37,225 cycles

CRACK AROUND FASTENER HOLE ON #3 L/E SLAT BULLNOSE SKIN; WHERE ACTUATOR BRACKET ATTACHES / #3 SLAT TO BE REPLACED ON NRC #N162450

Part: GUIDE VANE — CRACKED (NR 1 ENGINE) · airframe 62,378 hrs · 36,655 cycles

NR 1 ENGINE FOUND 2 EACH SEGMENT OF INLET GUIDE VANE WITH LEADING EDGE TO TRAILING EDGE AXIAL AT 2 DIFFERENT LOCATION 8 O'CLOCK & 3 O'CLOCK AXIAL CRACKED. R&R NR 1 ENGINE PER MT.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 61,367 hrs · 36,012 cycles

AFT RT EMERGENCY EXIT BATTERY PACK FAILED A TEST. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,367 hrs · 36,012 cycles

AFT LEFT EMERGENCY LIGHT BATTERY PACK FAILED TO TEST. R & R THE BATTERY PACK IAW AMM.

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 61,360 hrs · 36,007 cycles

R/H MAIN GEAR WHEEL WELL VERTICAL STIFFENER IS CRACKED JUST O/B OF THE R/H PACK EXHAUST DUCT / REMOVED AND REPLACED VERTICAL STIFFENER PER SRM 51-40-02

Part: RIVET — SHEARED (R1 DOOR) · airframe 60,925 hrs · 35,733 cycles

R1 DOOR GIRT BAR RETAINING CLIP RIVET SHEARED. R&R RIVET ASSEMBLY PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,673 hrs · 34,905 cycles

RT EMERGENCY AREA LIGHT INOP AT ROW 18. RELAMPED LIGHT PER AMM.

Part: STIFFENER — CRACKED (LT WHEEL WELL) · airframe 59,336 hrs · 34,691 cycles

LEFT HAND WHEEL WELL STA 663 LBL 29 STIFFENER CRACKED BEHIND AND INBD OF MAIN HYDRAULIC FILTER / REMOVED AND REPLACED LEFT HAND WHEEL WELL STA 663 LBL 29 STIFFENER PER SRM 51-40-02.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,247 hrs · 34,640 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 59,211 hrs · 34,617 cycles

RT FORWARD GALLEY EXIT SIGN LENS COVER BROKEN. R&R LENS PER AMM.

Part: COVER — MISSING (CABIN) · airframe 57,631 hrs · 33,692 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT COVER MISSING. R&R LIGHT ASSEMBLY IAW MM.

Part: STIFFENER — CRACKED (BS 663) · airframe 56,752 hrs · 33,172 cycles

STIFFENER CRACKED BS 663, LBL 9.5. R & R STIFFENER IAW SRM AND DWG.

Part: COVER — CRACKED (EMERGENCY EXIT) · airframe 56,752 hrs · 33,172 cycles

RT EMERGENCY EXIT HATCH UPPER RELEASE HANDLE COVER CRACKED. R&R COVER IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 56,752 hrs · 33,172 cycles

KEELBEAM WEB ANGLE CRACKED AT BS 663, LBL 9.5. REPAIRED ANGLE IAW EA.

Part: STIFFENER — CRACKED (RT WING) · airframe 56,752 hrs · 33,172 cycles

RIGHT WING TRAILING EDGE INBOARD OF THE DEFLECTOR RIB, FORWARD SIDE OF THE VERTICAL INTERCOSTAL, MID SPAN VERTICAL STIFFENER WEB CRACKED. R&R WEB PER DWG AND SRM.

Part: FITTING — CRACKED (RT WING) · airframe 56,752 hrs · 33,172 cycles

RIGHT WING TRAILING EDGE INBOARD OF THE DEFLECTOR RIB, AFT SIDE OF THE VERTICAL INTERCOSTAL, MID SPAN VERTICAL STIFFENER FITTING CRACKED. R & R THE FITTING IAW DWG AND SRM.

Part: RIB — CRACKED (LT WING) · airframe 56,752 hrs · 33,172 cycles

LEFT WING TRAILING EDGE INBOARD OF THE DEFLECTOR RIB, FORWARD SIDE OF THE VERTICAL INTERCOSTAL, MID SPAN VERTICAL STIFFENER CRACKED. R & R RIB IAW SRM AND DWG.

Part: BRACKET — CRACKED (BS 663 BULKHEAD) · airframe 56,752 hrs · 33,172 cycles

LEFT WHEEL WELL BULKHEAD BRACKET CRACKED AT BS 663, ON THE INBOARD SIDE. REPAIRED THE BRACKET IAW SRM AND DWG.

Part: COVER — LOOSE (R2 DOOR) · airframe 56,646 hrs · 33,108 cycles

R2 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. R & R COVER IAW AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 55,490 hrs · 32,444 cycles

FORWARD FLIGHT ATTENDANT FLASHLIGHT STRAP BROKEN. R & R STRAP IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,243 hrs · 31,696 cycles

LEFT OVERWING EXIT LIGHT INOPERATIVE. R & R LIGHT BALLAST IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 54,143 hrs · 31,646 cycles

L1 DOOR SLIDE FELL OUT OF POSITION. REINSTALLED SLIDE IAW MM.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 50,460 hrs · 29,494 cycles

LEFT HORIZONTAL STABILIZER LE STATION 78.29, INBD UPPER SURFACE SKIN CREASED ACROSS RIB ATTACHMENT. REPAIRED SKIN IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,460 hrs · 29,494 cycles

LEFT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT LT STAB STATION 101.9, 19 INCHES AFT OF FWD SPAR, 3/4 INCHES ABOVE LOWER FLANGE. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,460 hrs · 29,494 cycles

LEFT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT LT STAB STATION 101.9, 28 INCHES AFT OF FWD SPAR, 3/4 INCHES ABOVE LOWER FLANGE. REPAIRED RIB IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,460 hrs · 29,494 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 138.7, 9 INCHES FROM TE. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,460 hrs · 29,494 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 120.30, 10 INCHES FROM TE. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,460 hrs · 29,494 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 129.5, 17.5 INCHES FROM TE. REPAIRED SKIN IAW SRM.

Part: FASTENER — SHEARED (LT WING) · airframe 50,460 hrs · 29,494 cycles

LEFT WING PANEL 551GB FWD WIGGLE PLATE FASTENERS SHEARED AT SPAR. R & R WIGGLE PLATE IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 50,460 hrs · 29,494 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 129.5, 9 INCHES FROM LE. REPAIRED SKIN IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,460 hrs · 29,494 cycles

CABIN SEAT TRACK CRACKED AT OTBD POSITION RBL 24.75, AFT TRACK HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,460 hrs · 29,494 cycles

CABIN SEAT TRACK CRACKED AT OTBD POSITION RBL 45.5, AFT TRACK HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,460 hrs · 29,494 cycles

CABIN SEAT TRACK CRACKED AT INBD POSITION LBL 45.5, FWD TRACK HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 50,460 hrs · 29,494 cycles

RIGHT WING NR 6 LOWER SKIN CRACKED AT SECOND INBD FASTENER FROM AFT EDGE ON ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,460 hrs · 29,494 cycles

CABIN SEAT TRACK CRACKED AT OTBD POSITION LBL 45.5, FWD TRACK HOLE. REPAIRED SEAT TRACK IAW EA.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 50,460 hrs · 29,494 cycles

LEFT WING UPPER TRAILING PANEL 551AT FWD INBD ATTACH BRACKET CRACKED. REPAIRED BRACKET IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,460 hrs · 29,494 cycles

LEFT WING NR 3 SLAT LOWER SKIN CRACKED AT AFT OTBD FASTENER ON THE ACTUATOR RIB. REPAIRED SKIN IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,460 hrs · 29,494 cycles

CABIN SEAT TRACK CRACKED AT INBD POSITION RBL 45.5, FWD TRACK HOLE, INBD FLANGE FWD & AFT HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 50,460 hrs · 29,494 cycles

RIGHT WING NR 7 LOWER SKIN CRACKED AT SECOND OTBD FASTENER FROM AFT EDGE ON ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 50,460 hrs · 29,494 cycles

RIGHT WING NR 8 LOWER SKIN CRACKED AT SECOND INBD FASTENER FROM AFT EDGE ON ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 50,171 hrs · 29,318 cycles

EXIT ROW CEILING EXIT SIGN BROKEN. R & R SIGN IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 47,654 hrs · 27,871 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 46,535 hrs · 27,204 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER OUT OF POSITION. REPOSITIONED SLIDE IAW TC.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FRAME WEB CRACKED ON UPPER EDGE BS 243.7 WL 230 LEFT FRAME. FRAME WEB CRACK ON UPPER EDGE BS 243.7 WL 230 LEFT FRAME WAS REPAIRED PER ER 12-03612 AND EA 1-753-21163.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 43,614 hrs · 25,479 cycles

RIGHT HORIZONTAL STAB RIB AT STAB STA 120.3 CRACKED AT 2ND VERTICAL STIFFENER AFT. REPAIRED RIGHT HORIZ STAB RIB AT STAB STA 120.3, 2ND VERTICAL STIFFENER PER SRM 55-10-09-WR-4. 4318U, 21NOV12.

Part: FASTENER — SHEARED (L1 DOOR) · airframe 43,614 hrs · 25,479 cycles

FWD ENTRY DOOR ESCAPE SLIDE SHROUD AFT GIRT BAR STOW HOOK HAS A SHEARED FASTENER. INSTALLED NEW FASTENER IN FED ESCAPE SLIDE SHROUD AFT GIRT BAR STOW HOOK PER SRM 51-40-02 STEP 4 B AND C.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FORWARD CARGO BAY GUSSET BS 500D STRINGER 19 LEFT IS CRACKED. REMOVED FCB GUSSET AT BS 500D STR 19 LEFT. FORMED AND INSTALLED NEW GUSSET AT BS 500D STR 19 LEFT PER SRM 51-20-01, SRM 51-40-02, SRM 51-40-05, SRM 51-10-02 AND DWG 143A9483.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FLOOR PANEL 222BF HAS A DELAMINATION ON THE LOWER SURFACE FWD O/B AREA. REPAIRED FLOOR PANEL 222BF IAW SRM 53-00-50 6490U 18NOV12.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

CORROSION, FLOOR PANEL 241ABF HAS CORRODED INSERTS. REPAIRED FLOOR PANEL 241ABF IAW SRM 53-00-50 6490U, 15NOV12.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 43,614 hrs · 25,479 cycles

LEFT NR 1 WINDOW FRAME IS CRACKED AT UPPER O/B CORNER. LEFT NR 1 WINDOW FRAME IS CRACKED AT UPPER O/B CORNER / WILL BE REPAIRED BY REMOVING & REPLACING LEFT NR 1 WINDOW FRAME PER ACO 8338-53.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

LEFT NR 3 WINDOW FRAME IS CRACKED 5.7" UP FROM LOWER FWD CORNER. REMOVED AND INSTALLED NEW LEFT NR 3 WINDOW FRAME PER SRM 51-40-05, SRM 51-40-02 AND DWG 141A8800.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

CORROSION BS 986.5 FLOORBEAM UPPER AND LOWER FLANGE, NUT PLATE AND NUTCLIP HOLES RBL 44 - LBL 44. REPAIRED BEAM PER SRM EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FORWARD CARGO BAY INTERCOSTAL ATTACH ANGLE CRACKED BS 500B AFT SIDE OF LBL 25. REMOVED CRACKED ATTACK ANGLE AT BS 500B AFT SIDE OF FRAME LBL 25, RECEIVED NEW ANGLE, LOCATED, DRILLED AND INSTALLED IAW SRM 51-40-05-0G-0 & SRM 51-40-02-0G-0.

Part: SILL — CORRODED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

CORROSION, CORROSION ON FWD SERVICE DOOR MOP SILL IN NUMEROUS AREAS BS 325-345 WL 208. REMOVED AND INSTALLED NEW MOP SILL ON FWD SERVICE DOOR IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FWD CARGO BAY INTERCOSTAL TO ATTACH ANGLE CRACKED BS 500C AFT SIDE LBL 25. REMOVED CRACKED ATTACH ANGLE AT BS 500C AFT SIDE OF FRAME LBL 25, RESCUED NEW ANGLE, LOCATED, DRILLED AND INSTALLED IAW SRM 51-40-05-0G-0 & SRM 51-40-02-0G-0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FUSELAGE FRAME CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BETWEEN STR 8-9R, BS 360. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

CRACK BS 727D FRAME AT STR 8LT A/C BRACKET ATTACH PT, I/B FASTENER. REPAIRED CRACKED FRAME AT BS 727D STR 8 LT A/C BRACKET ATTACH POINT PER EA 1-A53-12114 REV 2.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

CORROSION WEB UPPER SURFACE BS 1016 RBL 7 WL 208.1. REMOVED AND EVALUATED CORRODED WEB AT BS 1016 RBL 7 FABRICATED NEW WEB AND RE-INSTALLED IAW BOEING DWG 147A5730 AND APPLICABLE DATA 84840U, 11/21/2012

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

CRACK BS 867 FRAME AT STR 8LT A/C BRACKET ATTACH PT, I/B FASTENER. INSTALLED REPAIR BS 867 STR 8LT IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FUSELAGE FRAME IS CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BETWEEN STR 8-9R BS 747. REPAIRED CRACKED FRAME BS 747 AT A/C BRACKET ATTACH POINT PER EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FUSELAGE FRAME IS CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BETWEEN STR 8-9R BS 480. REPAIRED CRACKED FRAME BS 480 AT A/C BRACKET A

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FUSELAGE FRAME IS CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BETWEEN STR 8-9R BS 867. INSTALLED REPAIR BS 867 STR 8-9R IAW EA 1-A53-12114 REV 2.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FUSELAGE FRAME IS CRACKED AT AIR CONDITIONING BRACKET ATTACHMENT BETWEEN STR 8-9R BS 827. INSTALLED REPAIR BS 827 STR 8-9R IAW EA 1-A53-12114 REV 2.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

CRACKED STRINGER CLIP, BS,360, STR 8R. REMOVED AND REPLACED BS 360 STR 8R CTR CLIP IAW SRM 51-40-02

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FORWARD CARGO BAY CRACKED INTERCOSTAL BS 480 STR 25L. REMOVED AND REPLACED WITH NEW INTERCOSTAL FWD CARGO BAY BS 480 STR 25L IAW SRM 51-40-02 81705U 12NOV12.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FWD CARGO BAY INTERCOSTAL TO FRAME ATTACH ANGLE CRACKED BS 400 LBL 25. REMOVED CRACKED ATTACH ANGLE BS400 LBL 25. RECEIVED NEW ANGLE, LOCATED, DRILLED AND INSTALLED NEW ATTACH ANGLE IAW SRM 51-40-05-0G-0, AND SRM 51-40-02-0G-0.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FWD CARGO BAY INTERCOSTAL TO FRAME ATTACH ANGLE CRACKED BS 500B LBL 25. REMOVED ATTACH ANGLE AT BS 500B LBL 25, LOCATED, DRILLED AND INSTALLED IAW SRM 51-40-05-0G-0 & SRM 51-40-02-0G-0.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

CORROSION AT FWD CARGO BAY LT BULKHEAD ANGLE BS 500D LBL25. REMOVED AND REPLACED ANGLE PER SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

FORWARD CARGO BAY INTERCOSTAL TO FRAME ATTACH ANGLE CRACKED BS 500C LBL 25. REMOVED AND REPLACED FWD CARGO BAY INTERCOSTAL TO FRAME ANGLE P/N 143A7502 PER SRM 51-40-05 AND SRM 51-40-02. BS 500C LBL 25.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,614 hrs · 25,479 cycles

LEFT MAIN WHEEL WELL FWD BULKHEAD IS CRACKED AT LBL 8 WL 145-160. REPAIRED CRACK ON LEFT MAIN WHEEL WELL FWD BULKHEAD AT LBL 8, WL 145-160 PER EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 42,361 hrs · 24,693 cycles

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

Part: REVEAL — CRACKED (L1 DOOR) · airframe 43,613 hrs · 25,479 cycles

FWD ENTRY DOOR REVEAL ABOVE UPPER HINGE CUTOUT CRACKED. REMOVED AND REPLACED REVEAL PER SRM.

Part: COVER — MISSING (CABIN) · airframe 39,474 hrs · 23,005 cycles

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

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 38,864 hrs · 22,655 cycles

R2 DOOR EMERGENCY EVAC SLIDE PULLED OUT OF CASE, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,852 hrs · 22,078 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY OPER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 36,715 hrs · 21,396 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING NR 2 L/E SLAT LOWER SKIN CRACKED. REPAIRED SLAT SKIN PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,715 hrs · 21,396 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 732D, LBL 3.0. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,715 hrs · 21,396 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 732D, RBL 8.1. REPAIRED BEAM PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,181 hrs · 20,492 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REMOVED AND REPLACED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,181 hrs · 20,492 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REMOVED AND REPLACED FITTING PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,546 hrs · 20,128 cycles

DURING SCHEDULED CV CHECK, FOUND RT EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,546 hrs · 20,128 cycles

DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (FUSELAGE) · airframe 32,350 hrs · 18,813 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: FLAP — PUNCTURED (LT WING) · airframe 30,744 hrs · 17,810 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B TRAILING EDGE FLAP PUNCTURED. REMOVED AND REPLACED FLAP PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 30,356 hrs · 17,554 cycles

DURING SCHEDULED 8Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 6. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 30,356 hrs · 17,554 cycles

DURING SCHEDULED 8Y CHECK, FOUND R2 DOOR ENTRY WAY CREASE BEAM CORRODED BETWEEN BS 967 TO BS 986. REMOVED AND REPLACED BEAM PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 30,356 hrs · 17,554 cycles

DURING SCHEDULED 8Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, BETWEEN RBL 32 TO RBL 40. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 30,356 hrs · 17,554 cycles

DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR LOWER FRAME CRACKED AT BS 291. REPAIRED FRAME PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 30,356 hrs · 17,554 cycles

DURING SCHEDULED 8Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 6. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 30,356 hrs · 17,554 cycles

DURING SCHEDULED 8Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 32. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 30,356 hrs · 17,554 cycles

DURING SCHEDULED 8Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 30,356 hrs · 17,554 cycles

DURING SCHEDULED 8Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (BS 540) · airframe 30,356 hrs · 17,554 cycles

DURING SCHEDULED 8Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 40. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 28,213 hrs · 16,239 cycles

DECLARED EMERGENCY. FLIGHT CREW REPORTED SMELL OF SMOKE IN AFT CABIN. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 27,478 hrs · 15,968 cycles

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

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 26,454 hrs · 15,128 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 23,950 hrs · 13,647 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,324 hrs · 10,961 cycles

DURING SCHEDULED MV2 CHECK, FOUND CABIN EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 10 DEF. RELAMPED LIGHT PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 18,630 hrs · 10,535 cycles

R2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED R2 WINDOW AND HEAT CONTROLLER PER MM.

Part: STRAP — MISSING (EMERGENCY EXIT) · airframe 18,484 hrs · 10,453 cycles

DURING SCHEDULED 5Y CHECK, FOUND RT OVERWING EMERGENCY EXIT ESCAPE STRAP RETAINING STRAP MISSING. INSTALLED STRAP PER MM.

Part: SKIN — CORRODED (LWR FUSELAGE) · airframe 18,484 hrs · 10,453 cycles

DURING SCHEDULED 5Y CHECK, FOUND FUSELAGE SKIN CORRODED UNDER FWD AIRPHONE ANTENNA. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (LWR FUSELAGE) · airframe 18,484 hrs · 10,453 cycles

DURING SCHEDULED 5Y CHECK, FOUND FUSELAGE SKIN CORRODED UNDER AFT AIRPHONE ANTENNA. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (BS 773) · airframe 18,484 hrs · 10,453 cycles

DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 773, RBL 8. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 773) · airframe 18,484 hrs · 10,453 cycles

DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 773, RBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 773) · airframe 18,484 hrs · 10,453 cycles

DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 773, LBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 773) · airframe 18,484 hrs · 10,453 cycles

DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAM CORRODED AT BS 773, LBL 12. REPAIRED FLOORBEAM PER SWA EA.

Part: HOOK — LOOSE (L1 DOOR SLIDE) · airframe 16,492 hrs · 9,329 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,758 hrs · 7,771 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 13 DEF, INOP. RELAMPED LIGHT PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 9,513 hrs · 5,448 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS NR 11 AND 13. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 8,309 hrs · 4,798 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED BETWEEN ROW NR 2 AND ROW NR 22. REMOVED AND REPLACED COVERS PER MM.

Part: SLIDE — OUT OF ADJUST (FWD ENTRY DOOR) · airframe 4,761 hrs · 2,853 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — LOOSE (CABIN) · airframe 2,587 hrs · 1,595 cycles

EEPLS COVER LOOSE. SECURED COVER PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 1,770 hrs · 1,099 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. INSTALLED EMERGENCY EVAC SLIDE PER MM.