N773SA

Part: WEB — ELONGATED (ZN 100 FUS LOWER) · airframe 77,822 hrs · 46,128 cycles

FWD CARGO DOOR LOWER SILL WEB HAS ELONGATED FSTENER HOLES AT STA 460+3' WL 156 RBL 27<[01] LOCATED AND DRILLED FWD CARGO WEB SILL AND INSTALLED NUT PLATES ON NEW WEB . I/A/W SRM 51-40-02-0G-0.;[02] VERIFIED ITEM 1;[03] C/S DRILLED HOLES I.A.W SRM 51-40-05-0G-0 AND BOEING DWG <BR>143A8120 REV:-;[04] STEP 3 COUNTERSINK VERIFIED;[05] AUDIT C/W

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 77,822 hrs · 46,128 cycles

FWD CARGO FWD CORNER SCUFF PLATE CRACKED<[01] SCUFF PLATE REPAIRED IN BACK SHOP ON N/R 45187/0000/0022 I.A.W<BR>SRM 53-30-15-2R-1;[02] SCUFF PLATE REPAIRED IN BACK SHOP ON N/R 45187/0000/0022 I.A.W<BR>SRM 53-30-15-2R-1;[03] BACK SHOP WORK ORDER #45189/0000/0001<BR>NOT N/R 45187/0000/0022 WROTE IN ERROR;[04] BACK SHOP WORK ORDER #45189/0000/0001<BR>NOT N/R 45187/0000/0022 WROTE IN ERROR;[05] VERIFIED ITEM 4<BR>AUDIT C/W

Part: SKIN — CORRODED (ZN 100 FUS LOWER) · airframe 77,822 hrs · 46,128 cycles

DOT A24-3 EXTERNAL FUSELAGE SKIN CORRODED AROUND VACUUM WASTE EXHAUST PORT BETWEEN STRINGERS 22L AND 23L SATION 917.<[01] REMOVED CORROSION AND EXAMINED AREA WITH 10X MAGNIFIER I.A.W SRM 53-70-01-0L-1. NO DEFECTS FOUND.;[02] REMOVED CORROSION ; VISUALLY INSPECTED AREA WITH 10X MAGNIFIER NO DEFECTS NOTED I.A.W SRM <BR>51-10-02-0G-0 AND SRM53-00-01-1A-5;[03] VERIFIED ITEM 2;[04] ORIGINAL .125'; REMAINING .104'; LOSS .021'. UT IAW B737 NDT PART 4 51-00-00 PROCEDURE 2. TOOL# 40084 DUE 01AUG24;[05] VERIFIED MATERIAL THICKNESS USING SRM 53-70-01-0I-1 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A-1;[06] VERIFIED ITEM 5;[07] RECHECKED MATERIAL LOSE BY NDT ORGINAL 0.125 REMAIN 0.103 REMOVED 0.022 I.A.W SRM53-00-01-1A-1;[08] REPAIRED BLENDED AREA IAW EA 23-153-03118-WIP1 AND EA 23-153-03118;[09] AUDIT C/W

Part: DOOR — CORRODED (ZN 100 FUS LOWER) · airframe 77,822 hrs · 46,128 cycles

DOT A24-1 WATER SERVICE DOOR CORRODED NEAR HINGES AND OUTER EDGE.<[01] AUDIT CW

Part: SKIN — CORRODED (ZN 100 FUS LOWER) · airframe 77,822 hrs · 46,128 cycles

LOWER EXTERNAL FUSELAGE STA.450 LBL 12'; CORROSION FOUND AROUND RADIO ALTIMETER CABLE ACCESS HOLE<[01] REMOVED CORROSION LOWER EXTERNAL FUSELAGE SKIN IAW SRM 51-10-02 ITEM 15;[02] VISUAL INSPECTED AREA WITH 10X MAGNIFYNG GLASS IAW SRM 51-10-02 ITEM 15;[03] STEP 2 C/W;[04] ACCOMPLISHED UT GRID OF THE AFFECTED AREA IAW B737 NDT P4 51-00-00 P2 TOOL 36285 DUE 16DEC23<BR><BR>FOUND .080' ORIGINAL; .076' REMAINING; .004' LOSS<BR><BR>GRID SKETCH SUPPLIED WITH UT GRID FOR NRC TTG8Q00NZ6HB;[05] FAULT RESOLVED ON FAULT TTG8Q00NZ6HB WHERE EA 23-153-03085 ADDED;[06] ALL RII COMPLETE

Part: SLIDE — OUT OF POSITION (ZN 800 DOOR) · airframe 77,759 hrs · 46,087 cycles

AFT ENTRY DOOR SLIDE GIRT NEEDS TO BE RETUCKED<[01] REPOSITIONED AFT ENTRY DOOR SLIDE AS PER MT 725-61-06 REFERENCED FROM AMM 25-66-01

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 77,697 hrs · 46,046 cycles

FLIGHT ATTENDANT REPORTED FAINT SMELL ENROUTE FROM LAS-LAX AND SAID IT WAS GONE. ON FINAL APPROACH AND CLEARING THE RUNWAY WE GOT A CALL BACK THAT IT SMELL LIKE A RAGING FIRE BUT NO SMOKE. ARF (FIRE) WAS CALLED ON TAXIWAY AND DID INSPECTION. SAID THERE WERE NO ABNORMAL INDICATIONS.<[01] PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-56. FOUND RAG WEDGED UNDER #2 COFFEE MAKER RAIL ASSY WITH INDICATION OF BURNING. REMOVED BURNT RAG AND PERFORMED OPS CHECK OF #1 & #2 COFFEE MAKERS. NO SMELLS OR DEFECTS NOTED.<BR><BR>MX ALSO PERFORMED BY 69014

Part: SLIDE — LOOSE (ZN 800 DOOR) · airframe 76,677 hrs · 45,400 cycles

FWD ENTRY DOOR SLIDE FELL OUT.<[01] R?RD FWD ENTRY DOOR SLIDE PER MT 725-61-06.

Part: FLAP — LOW (ZN 200 FUS TOP) · airframe 76,431 hrs · 45,235 cycles

FWD ENTRY DOOR SLIDE GIRT BAR FLAP HANGING TO LOW.<[01] RESECURED VELCRO FOR GIRT BAR FLAP PER M/M 25-66-01.NO DEFECTS NOTED.

Part: COVER — OUT OF ADJUST (R1 DOOR) · airframe 74,660 hrs · 44,093 cycles

FORWARD SERVICE DOOR SLIDE PULL HANDLE COVER NEEDS ADJUSTMENT / [01] ADJUSTED COVER PER AMM 25-66-01.

Part: HANDLE — LOOSE (L1 DOOR) · airframe 74,222 hrs · 43,795 cycles

L1 DOOR AFT FLIGHT ATTENDANT HANDLE LOOSE 2022-384798 / [01] TIGHTENED L1 DOOR AFT FLIGHT ATTENDANT HANDLE 20-50-12 REVISION NO.38;[02] TASK CARD COMPLETE.

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 74,222 hrs · 43,795 cycles

INOP EMERGENCY EXIT LIGHT LOCATED ON OVERWING UPPER FUSELAGE LT 2022-384785 / [01] REPLACED INOP EMERGENCY EXIT LIGHT LOCATED ON OVERWING UPPER FUSELAGE LT IAW B737-700 AMM 33-51-04-960-801; TEST IS OK;[02] CORRECTED STEP 1: REPLACED INOP EMERGENCY EXIT LIGHT LOCATED ON OVERWING UPPER FUSELAGE LT IAW B737-700 AMM 33-51-04-960-801; STEP 2.A THRU 2.F(1)(A) AND 2.F(2); TEST IS OK;[03] REPLACED INOP EMERGENCY EXIT LIGHT LOCATED ON OVERWING UPPER FUSELAGE LT IAW B737-700 AMM 33-51-04-960-801; TEST IS OK;[04] TASK COMPLETED<BR><BR>TEST OK

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 74,222 hrs · 43,795 cycles

R1 DOOR AFT GIFT BAR FITTING LOOSE 2022-384792 / [01] TIGHTENED R1 DOOR AFT GIFT BAR FITTING IAW SOPM 20-50-01 REV.38;[02] TASK CARD COMPLETE.

Part: ANGLE — CRACKED (LH WING) · airframe 74,222 hrs · 43,795 cycles

CRACK ANGLE ON ACCESS PANEL 551GB AT LT WING 2022-384737. / [01] REPLACED ANGLE ON ACCESS PANEL 551GB AT LT WING IAW B737-700 SRM 51-40-02 AND DRAWING 115A2714 REV A:;[02] CORRECTED STEP 1; REPLACED ANGLE ON ACCESS PANEL 551GB AT LT WING IAW B737-700 SRM 51-40-02 AND DRAWING 115A2714 REV A: SEE INDIVIDUAL SINGOFFS ITEM BELOW.;[03] JOB COMPLETED.

Part: BARRIER — CRACKED (CENTER WING) · airframe 74,222 hrs · 43,795 cycles

CUSTOMER REQUEST-CRACK ON VAPOR BARRIER LOC. ON AIR CONDITIONER BAY BS663.75 LH SIDE 2022-384687 / [01] TOOL USED CALIPER P/N 500-196-30; S/N A21033526; DUE DATE: 18-OCT-22.;[02] TOOL USED SCALE P/N CL5000; S/N AE-39087; DUE DATE: 07-JUL-22.;[03] PERFORMED AN INTERIM REPAIR ON VAPOR BARRIER LOC. ON AIR CONDITIONER BAY BS663.75 AND LBL 35.83 AT LH SIDE AS PER B737-700 SRM 57-10-10-2R-2 REPAIR 2; PARAGRAPHS 1.A;C; 2.C. AND 6. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] PERFORMED AN INTERIM REPAIR ON VAPOR BARRIER LOC. ON AIR CONDITIONER BAY BS663.75 AND LBL 35.83 AT LH SIDE AS PER B737-700 SRM 57-10-10-2R-2 REPAIR 2; PARAGRAPHS 1.A;C; 2.C. AND 6. SEE INDIVIDUAL SIGNOFFS BELOW.<BR>RII ACCOMPLISHED

Part: ANGLE — CRACKED (RH WING) · airframe 74,222 hrs · 43,795 cycles

CRACK ANGLE TRAILING EDGE LOCATED FALSE SPAR ORSS 280 AT RT WING 2022-384734 / [01] REPLACED ANGLE AND FASTENER ON TRAILING EDGE LOCATED FALSE SPAR ORSS 280 AT RT WING IAW B737-700 SRM 51-40-02 AND DRAWING 115A6200 REV A: SEE INDIVIDUAL STEP SINGOFFS BELOW;[02] REPLACED ANGLE AND FASTENER ON TRAILING EDGE LOCATED FALSE SPAR ORSS 280 AT RT WING IAW B737-700 SRM 51-40-02 AND DRAWING 115A6200 REV A: SEE INDIVIDUAL STEP SINGOFFS BELOW

Part: WEB — CRACKED (RH WING) · airframe 74,222 hrs · 43,795 cycles

CRACK WEB TRAILING EDGE LOCATED ON FALSE SPAR ORSS 261 AND ORSS 280 AT RT WING 2022-384733 / [01] REPLACED WEB AND FASTENERS LOC TRAILING EDGE LOCATED ON FALSE SPAR ORSS 261 AND ORSS 280 AT RT WING IAW B737-700 SRM 51-40-02.;[02] CORRECTED STEP 1. REPLACED WEB AND FASTENERS LOC TRAILING EDGE LOCATED ON FALSE SPAR ORSS 261 AND ORSS 280 AT RT WING IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] CORRECTED STEP 2. REPLACED WEB AND FASTENERS LOC TRAILING EDGE LOCATED ON FALSE SPAR ORSS 261 AND ORSS 280 AT RT WING IAW B737-700 SRM 51-40-02 AND 51-10 02 ITEM 9 SEE INDIVIDUAL SIGN OFFS BELOW.;[04] REPLACED WEB AND FASTENERS LOC TRAILING EDGE LOCATED ON FALSE SPAR ORSS 261 AND ORSS 280 AT RT WING IAW B737-700 SRM 51-40-02 AND 51-10 02 ITEM 9 SEE INDIVIDUAL SIGN OFFS BELOW.

Part: PLATE — CRACKED (LH WING) · airframe 74,222 hrs · 43,795 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 261 AT LT WING 2022-384731 / [01] REPLACED CORRUGATED PLATE AND FASTENER LOCATED ON TRAILING EDGE ORSS 261 AT LT WING IAW B737-700 SRN 51-40-02 AND DRAWING 114A2714 REV A:;[02] REPLACED CORRUGATED PLATE AND FASTENER LOCATED ON TRAILING EDGE ORSS 261 AT LT WING IAW B737-700 SRN 51-40-02 AND DRAWING 114A2714 REV A:

Part: PANEL — CRACKED (FUSELAGE) · airframe 74,222 hrs · 43,795 cycles

CRACK ON FASTENER HOLES ON 193AR ACCESS PANEL AT LOWER FUSELAGE 2022-384725 / [01] TOOL USED CALIPER PN: 500-197-30; SN: 15120589; D/D: 28/NOV/22.;[02] TOOL USED SCALE PN: SCA-301; SN: AE-412136; D/D: 14/MAR/23;[03] TOOL USED HOTBONDER P/N:HCS9200B S/N:18196126 DUE DATE: 24 FEB 23.;[04] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18196021; D/D: 16/JAN/23.;[05] TOOL USED SCALE PN: SCA-301; SN: AE-412136; D/D: 14/MAR/23.;[06] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 18820031 ; DUE DATE: 04-DEC-22;[07] REPAIRED ACCESS PANEL 193AR AT LOWER FUSELAGE. IAW B737-700 SRM 51-70-05-2R-9 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] TASK COMPLETED.

Part: PANEL — CRACKED (FUSELAGE) · airframe 74,222 hrs · 43,795 cycles

CRACK ON FASTENER HOLES ON ACCESS PANEL 193AL AT LOWER FUSELAGE 2022-384724 / [01] TOOL USED CALIPER PN: 500-197-30; SN: 15120589; D/D: 28/NOV/22.;[02] TOOL USED SCALE PN: SCA-301; SN: AE-412136; D/D: 14/MAR/23.;[03] TOOL USED HOTBONDER P/N:HCS9200B S/N:18196126 DUE DATE: 24 FEB 23.;[04] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18196126; D/D: 24/FEB/23.;[05] REPAIRED ACCESS PANEL 193AL AT LOWER FUSELAGE. IAW B737-700 SRM 51-70-05-2R-9 REPAIR 9. TOOL USED HOT BONDER PN: HCS9200B-AV SN: 18196021 DUE DATE: 16-JAN-23 SEE INDIVIDUAL SIGNOFFS BELOW.;[06] TASK COMPLETED.

Part: SUPPORT — CORRODED · airframe 74,222 hrs · 43,795 cycles

CORROSION ON ZEE SUPPORT LOC. BTW BS 492.4 TO BS 500 AT LEVEL STR26R 2022-384711 / [01] REPLACED ZEE SUPPORT LOC. BTW BS 492.4 TO BS 500 AT LEVEL STR26R IAW B737-700 SRM-51-40-02 AND DWG-143A0080 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETED <BR>RII

Part: MEGAPHONE — INOPERATIVE (PAX CABIN) · airframe 74,222 hrs · 43,795 cycles

DETERIORATED WINDSCREEN LT SIDE THE BATTERIE MEGAPHONE EMERGENCY EQUIPMENT AT FWD GALLEY AREA (8 EA) 2022-383181 / [01] REPLACED WINDSCREEN LT SIDE THE BATTERIE MEGAPHONE EMERGENCY EQUIPMENT AT FWD GALLEY AREA (8 EA) IAW B737-700 AMM 25-64-00-900-804;[02] REPLACED WINDSCREEN LT SIDE THE BATTERIE MEGAPHONE EMERGENCY EQUIPMENT AT FWD GALLEY AREA (8 EA) IAW B737-700 AMM 25-64-00-900-804;[03] REPLACED WINDSCREEN LT SIDE THE BATTERIES MEGAPHONE EMERGENCY EQUIPMENT AT FWD GALLEY AREA (8 EA) IAW B737-700 AMM 25-64-00-900-804

Part: MEGAPHONE — INOPERATIVE (PAX CABIN) · airframe 74,222 hrs · 43,795 cycles

DETERIORATED WINDSCREEN LT SIDE THE BATTERIE MEGAPHONE EMERGENCY EQUIPMENT AT AFT GALLEY AREA (8 EA) 2022-383174 / [01] REPLACED WINDSCREEN LT SIDE THE BATTERIE MEGAPHONE EMERGENCY EQUIPMENT AT AFT GALLEY AREA (8 EA) IAW B737-700 AMM 25-64-00-900-804;[02] REPLACED WINDSCREEN LT SIDE THE BATTERIES MEGAPHONE EMERGENCY EQUIPMENT AT AFT GALLEY AREA (8 EA) IAW B737-700 AMM 25-64-00-900-804

Part: PANEL — ELONGATED (AFT CARGO) · airframe 74,222 hrs · 43,795 cycles

ELONGATED HOLE BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT 2022-383004 / [01] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT FROM MATERIAL CONOLITE P/N:A60SG4W AND P/O: 2022-127802 IAW B737-700 AND AMM 25-52-01-201-801 AND DWG 453A2510 REV-;[02] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT FROM MATERIAL CONOLITE P/N:A60SG4W AND P/O: 2022-127802 IAW B737-700 AND AMM 25-52-01-201-801 AND DWG 453A2510 REV-

Part: WEB — CRACKED (#1 ENG IB FAN CO) · airframe 74,222 hrs · 43,795 cycles

CRACK ON WEB INBOARD FAN COWL LOC.INTERNAL AREA ACCESS DOOR 414AR ON ENGINE 1 2022-382902. / [01] INSTALLED WEB AND FASTENERS LOC INBOARD FAN COWL LOC.INTERNAL AREA ACCESS DOOR 414AR ON ENGINE 1 IAW B737-700 SRM 51-40-02 . SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRECTED STEP 1.REPLACED WEB AND FASTENERS LOC INBOARD FAN COWL LOC.INTERNAL AREA ACCESS DOOR 414AR ON ENGINE 1 IAW B737-700 SRM 51-40-02 . SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED WEB AND FASTENERS LOC INBOARD FAN COWL LOC.INTERNAL AREA ACCESS DOOR 414AR ON ENGINE 1 IAW B737-700 SRM 51-40-02 . SEE INDIVIDUAL SIGN OFFS BELOW.

Part: STRINGER — CRACKED (FWD CARGO BAY) · airframe 74,222 hrs · 43,795 cycles

CRACK STRINGER 26L ON BS 540 AT FWD CARGO COMPARTMENT 2022-382753 / [01] TOOL USED ULTRASONIC THICKNESS GAGE PN 45MG SN 130061901 DUE DATE 08-APR-23;[02] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022237; DUE DATE: 06-OCT-22.;[03] TOOL USED: CALIPER; PN: 500-197-30; SN: A21146102; DUE DATE: 16-OCT-22; PRECISION RADIUS GAUGE; PN: 2204A3; SN: AE-408651; DUE DATE: 24-FEB-23;[04] TOOL USED TEMPERATURE CONTROLLER P/N:P3015GOES00000;S/N:142811020;DUE DATE:02-FEB-23;P/N:P3015GOES00000;P/N:142811019;DUE DATE:02-FEB-23.;[05] PERFORMED REPAIR ON STRINGER 26L BTW. BSTA 500D. TO BSTA 520. AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1. AND SRM 51-40-02. SEE INDIVIDUAL SING OFFS STEP BELOW.;[06] TASK CARD COMPLETED <BR>RII

Part: STRINGER — CRACKED (FWD CARGO BAY) · airframe 74,222 hrs · 43,795 cycles

CRACK STRINGER 27R ON BS 540 AT FWD CARGO COMPARTMENT 2022-382754 / [01] TOOL USED ULTRASONIC THICKNESS GAGE PN 45MG SN 130061901 DUE DATE 08-APR-23;[02] EDDY CURRENT EQUIPMENTP/N: NORTEC500D; S/N: N500X12101V022237; DUE DATE:06-OCT-22;[03] TOOL USED: CALIPER; PN: 500-197-30; SN: A21146102; DUE DATE: 16-OCT-22; PRECISION RADIUS GAUGE; PN: 2204A3; SN: AE-408651; DUE DATE: 24-FEB-23;[04] TOOL USED TEMPERATURE CONTROLLER P/N:P3015GOES00000;S/N:142811020;DUE DATE:02-FEB-23;P/N:P3015GOES00000;P/N:142811019;DUE DATE:02-FEB-23.;[05] REPAIRED STRINGER 27R LOCATED BTW BS 500D AND BS 540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. FIG. 206 SEE INDIVIDUAL SIGNOFF BELOW.;[06] REPAIRED STRINGER 27R LOCATED BTW BS 500D AND BS 540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. FIG. 206 SEE INDIVIDUAL SIGNOFF BELOW. AS RII

Part: ANGLE — CRACKED (AFT CARGO BAY) · airframe 74,222 hrs · 43,795 cycles

CRACK ANGLE - CLIP BS 867 BTW S 26L TO S 27L AT AFT CARGO COMPARTMENT 2022-382756 / [01] REPLACED ANGLE CLIP AND FASTENER BS 867 BTW STR26L AND STR 27L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 AND DRAWING 149A8102 REV -: SEE INDIVIDUAL STEP SINGOFF BELOW.;[02] REPLACED ANGLE CLIP AND FASTENER BS 867 BTW STR26L AND STR 27L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 AND DRAWING 149A8102 REV -: SEE INDIVIDUAL STEP SINGOFF BELOW.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 74,222 hrs · 43,795 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2022-353217 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A18135080; DUE DATE 31-JUL-22.;[02] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4) TO (7); PER BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4) TO (7); PER BAC 5975

Part: SUPPORT BRACKET — CRACKED (RH WING) · airframe 74,222 hrs · 43,795 cycles

CRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 273 RT WING 2022-353017 / [01] REPLACED SUPPORT BRACKET AND FASTENERS LOC TRAILING EDGE LOCATED ORSS 273 RT WING IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED SUPPORT BRACKET AND FASTENERS LOC TRAILING EDGE LOCATED ORSS 273 RT WING IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: SKIN PANEL — CRACKED (LH HOR STAB) · airframe 74,222 hrs · 43,795 cycles

CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.90 AND 16 INCH. FROM FRONT SPAR. CRACK LENGTH = 0.700 INCH. APPROX. 2022-352802 / [01] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N:210138203; DUE DATE:11-APR-23.;[02] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N:210138203; DUE DATE:11-APR-23.;[03] TOOL USED: CALIPER; PN: 4996A52; SN: 170846216; DUE DATE: 19-JAN-23. PRECISION RADIUS GAUGE; PN:S167C; SN: AE-28449; DUE DATE: 11-JUL-22;[04] PERFORMED REPAIR ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL LOCATED AT STAB STA 193.90 IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11 SEE INDIVIDUAL STEP SING OFFS BELOW.;[05] PERFORMED REPAIR ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL LOCATED AT STAB STA 193.90 IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11 SEE INDIVIDUAL STEP SING OFFS BELOW. AS RII

Part: SKIN — CRACKED (RH WING) · airframe 74,222 hrs · 43,795 cycles

CUSTOMER REQUEST-CRACK ON LOWER SKIN LEADING EDGE SLAT 7 AT RT WING 2022-352868 / [01] TOOL; USED PN:NORTEC 600D; SN:210138003; DUE DATE:22- FEB-23;[02] TOOL USED EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 60009161631 DUE DATE 03-DEC-22.;[03] TOOL USED EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 60009161631 DUE DATE 03-DEC-22.;[04] ET TOOL USED: PN: NORTEC 600D; SN: 210138203; DUE DATE: 11-APR-23;[05] REPAIRED LOC. ON LOWER SKIN LEADING EDGE SLAT 7 AT RT WING IAW EA 22-151-01069-WIP1 BARCODE TTG8Q00DJA3E AND EA 22-151-01069 BARCODE TTG8Q00DM25Q;[06] TASK CARD COMPLETED RII

Part: BRACKET — CRACKED (CENTER WING BOX) · airframe 74,222 hrs · 43,795 cycles

CRACK BRACKET ANGLE LOCATED. BS 695 RBL 24.82 AT CENTER WING BOX 2022-353010 / [01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[02] REPLACED BRACKET ANGLE LOCATED BS 695 RBL 24.82 AT CENTER WING BOX IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 111A6000 REV-A SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPLACED BRACKET ANGLE LOCATED BS 695 RBL 24.82 AT CENTER WING BOX IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 111A6000 REV-A SEE INDIVIDUAL SIGNOFF BELOW.<BR>RII

Part: BRACKET — CRACKED · airframe 74,222 hrs · 43,795 cycles

CRACK BRACKET LOCATED BS 540 AND BETWEEN BL 0 TO RBL 24.82 AT PASSENGER CABIN 2022-353013 / [01] REPLACED BRACKET (PANEL BREAK ASSY )LOCATED BS 540 AND BETWEEN BL 0 TO RBL 24.82 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED BRACKET (PANEL BREAK ASSY )LOCATED BS 540 AND BETWEEN BL 0 TO RBL 24.82 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OFF BELOW.<BR><BR>RII ACCOMPLISHED

Part: RIB — CRACKED (LH HOR STAB) · airframe 74,222 hrs · 43,795 cycles

CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 27 INCH FROM FRONT SPAR LT HORIZONTAL STAB 2022 352601 / [01] TOOL USED: CALIPER; PN: 500-197-30; SN:A21146102; DUE DATE: 16-OCT-22;[02] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N:210138203; DUE DATE:11-APR-23.;[03] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 210138103; DUE DATE: 11-APR-23;[04] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 210138103; DUE DATE: 11-APR-23;[05] TOOL USED: CALIPER; PN: 500-197-30; SN: A21042060; DUE DATE: 11-AUG-22;[06] PERFORMED REPAIR ON INSPAR RIB LOCATED STAB STA 129.50 AND 27 FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5. SEE INDIVIDUAL STEP SIGNOFFS BELOW;[07] CORECTED STEP 6<BR>PERFORMED REPAIR ON INSPAR RIB LOCATED STAB STA 129.50 AND 27 FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5. SEE INDIVIDUAL SIGNOFFS BELOW;[08] PERFORMED REPAIR ON INSPAR RIB LOCATED STAB STA 129.50 AND 27 FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5. SEE INDIVIDUAL SIGNOFFS BELOW<BR>CERTIFIED AS RII

Part: RIB — CRACKED (RH HOR STAB) · airframe 74,222 hrs · 43,795 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 27 FROM FRONT SPAR AT RT HORIZONTAL STABILIZER 2022 352599 / [01] TOOL USED: CALIPER; PN: 500-197-30; SN:A21146102; DUE DATE: 16-OCT-22;[02] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N:210138203; DUE DATE:11-APR-23.;[03] PERFORMED REPAIR ON INSPAR RIB LOCATED STAB STA 120.30 AND 27 FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL STEP SIGN OFFS BELOW.;[04] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: BATTERY PACK — FAILED (PAX CABIN) · airframe 74,222 hrs · 43,795 cycles

DONT PASS OPERATIONAL TEST EMERGENCY LIGHT BATTERY PACK M01673 AT PASSENGER CABIN 2022-352719 / [01] REPLACED BATTERY PACK M1673 AT PASSENGER CABIN IAW B737-700 AMM 33-51-06?960-805 AND PERFORMED INSTALLATION TEST OK.;[02] TASK CARD COMPLETED

Part: PLATE — CORRODED (L/H WING) · airframe 73,771 hrs · 43,510 cycles

654A0003-85 PLATE ATTACHED TO ELEPHANT EAR FAIRING IS CORRODED. / [01] REPLACED FAIRING PLATE AS REQUIRED REF SRM 51-40-02

Part: CIRCUIT BREAKER — TRIPPED (EMERGENCY LIGHTS) · airframe 73,723 hrs · 43,480 cycles

INFO ONLY EMER EXIT LIGHTS INOP. FOUND CB OPEN ON PREFLT. CLOSED CB PER MOC ROBBY. NO FAULTS NOTED. / [01] NOTED BY MX.

Part: PLATE — ELONGATED (WING) · airframe 73,076 hrs · 43,083 cycles

WIGGLE PLATE ASSY DAMAGED/FASTENER HOLES ELONGATED AND WORN. PLATE ASSY REMOVED . ; WIGGLE PLATE ASSY DAMAGEDFASTENER HOLES ELONGATED AND WORN. PLATE ASSY REMOVED . / [01] REPLACED WIGGLE PLATE REF LINE #90 TTG8QOOASWM71 STEP 2 AND EA 22-157-00412 REV A .

Part: BATTERY PACK — FAULTY (CABIN) · airframe 72,970 hrs · 43,025 cycles

FWD EMERGENCY CABIN LIGHTS INTERMITTING ; / [01] R AND R L/H FWD POWER SUPPLY ASSY. R AND R L/H AND R/H BATTERY PACK REF AMM 33-51-06

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 72,970 hrs · 43,025 cycles

FWD SERVICE DOOR ESCAPE SLIDE GIRT MATERIAL HANGING TOO LOW. ; / [01] REMOVED AND REINSTALLED FWD SERVICE ESCAPE SLIDE IAW MT 725-61-06.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 72,970 hrs · 43,025 cycles

FWD EMERGENCY CABIN LIGHTS INTERMITTING ; / [01] R AND R L/H FWD POWER SUPPLY ASSY. R AND R L/H AND R/H BATTERY PACK REF AMM 33-51-06

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,548 hrs · 42,762 cycles

SUPPLEMENTAL INFORMATION: R2 DOOR EMER LIGHT INOP (OUTSIDE) ; / [01] RELAMPED EXT EMER LIGHT PER AMM 33-51-00

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 72,282 hrs · 42,605 cycles

RH HORIZONTAL STAB UPPER SLIDER SEAL CRACKED ; / [01] R & RD SLIDING SEAL PER AMM 53-31-31. OPS NORMAL.; [02] C/W INSPECTION

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 71,741 hrs · 42,274 cycles

AFT EMERGENCY EXIT SIGN COVER LOOSE ; / [01] REINSTALLED AFT GALLEY EMERGENCY EXIT SIGN LENS IAW MM 33-51-01

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,119 hrs · 40,733 cycles

RH GROUND ILLUMINATION EXIT LIGHT IS OUT. RELAMPED AND PERFORMED GOOD TEST OF RH GROUND ILLUMINATION EXIT LIGHT. IAW AMM 33-51-04-960-801.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,119 hrs · 40,733 cycles

FWD ENTRY DOOR THRESHOLD EMERGENCY LIGHTS OUT / RELAMPED FWD ENTRY DOOR THRESHOLD EMERGENC EXIT LIGHT AND OPS CHECKED PER AMM 33-51-01-960-801 CHECKED GOOD

Part: SPLICE — CORRODED (AFT CARGO) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR PNL SPLICE BS 772 LBL 20-RBL 20 W/L 156 / REMOVED AND REPLACED AFT CARGO BAY FLOOR PNL SPLICE BS772 LBL20-RBL20 W/L156 I.A.W SRM 51-40-02-0G-0. AMM 25-52-10-400-801 AND DWG 146A7500 REV C

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 69,119 hrs · 40,733 cycles

MID CABIN OVER HEAD CEILING EMERGENCY EXIT LIGHT HOUSING IS BROKEN. / REMOVED AND REPLACED MID CABIN OVERHEAD CEILING EMERGENCY EXIT LIGHT HOUSING IAW AMM 33-51-01-960-802. PERFORMED OPS CHECK. OPS CHECK GOOD.

Part: CARGO TRACK — CRACKED (BS 460) · airframe 69,119 hrs · 40,733 cycles

FWD CARGO FLOOR TRACK CRACKED AT LWR RADIUS; BS 460; RBL 14; WL 154; MARKED / REMOVED FWD CARGO FLOOR TRACK AT BS 400 - 500+10 RBL 14; WL 154 AND REPLACED WITH NEW IAW DWG # 143A7500 REV A; DWG # 284A0603 REV A. 59042U 14AUG20 SRM 51-40-02-0G-0

Part: STRIP — DAMAGED (AFT CARGO) · airframe 69,119 hrs · 40,733 cycles

AFT CARGO R/H FWD CAP STRIP DAMAGED / REMOVED DAMAGED AFT CARGO R/H FWD CAP STRIP IAW AMM 25-52-10-000-801 RECEIVED A NEW CAP STRIP FROM STORES REF: PO 799913. INSTALLED A NEW CAP STRIP IAW AMM 25-52-10-400-801; PER 3E; STEP 11

Part: STRIP — DAMAGED (AFT CARGO) · airframe 69,119 hrs · 40,733 cycles

AFT CARGO L/H CAP STRIPS DAMAGED. / REMOVED DAMAGED AFT CARGO L/H FLOOR CAP STRIPS AT BS 727D-847 IAW AMM 25-52-10-000-801; PAR 2E; STEP (2). RECEIVED (2) NEW CAP STRIPS FROM STORES REF: PO 773161; 799414. INSTALLED NEW CAP STRIPS IAW AMM 25-52-10-400-801; PAR 3E; STEP (11) FIG 401. SH3

Part: STRIP — DAMAGED (FWD CARGO) · airframe 69,119 hrs · 40,733 cycles

FWD CARGO BAY R/H AFT CAP STRIP IS DAMAGED / REPLACED FWD CARGO BAY R/H AFT CAP STRIP IAW M/M 25-52-10-000-801 STEP 2E(2) AND M/M 25-52-10-400-801 STEP 3E(11)

Part: STRIP — DAMAGED (AFT CARGO) · airframe 69,119 hrs · 40,733 cycles

AT CARGO BAY R/H # 2 CAP STRIP IS DAMAGED / REMOVED AFT CARGO BAY R/H #2 CAP STRIP (DAMAGED) IAW AMM 25-52-10-000-801 PAR 2E; STEP (2). RECEIVED NEW CAP STRIP FROM STORES. REF: PO 767521. INSTALLED A NEW CAP STRIP IAW AMM 25-52-10-400-801; PAR 3E; STEP 11

Part: SKIN — DENTED (BS 383) · airframe 69,119 hrs · 40,733 cycles

REPAIR DENT AT FUSELAGE SKIN SECTION 43; STA 383; STR 17L. REMOVED DAMAGE ON FUSELAGE SKIN BS 383 STR 17 L/H REPAIRED PER ATS ER 20-03030 REV IR AND EA 20-153-01449 REV IR.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 69,119 hrs · 40,733 cycles

RIGHT HAND HORIZONTAL STAB FWD UPPER SLIDE SEAL IS CRACKED / REMOVED & REPLACED RIGHT HAND HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-000-801 AND 53-31-31-400-801 56790U 28JUL20 56790U 7/28/20

Part: STRINGER CLIP — CORRODED (BS 947) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON STRINGER CLIP AT AREA AFT OF ACB BS947+4 RBL56 WL198. MARKED / CORROSION ON STRINGER CLIP AT BS947+4 RBL56 WL198 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-1. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02; SRM 51-40-05; AND DWG 147A8110.

Part: SPLICE ANGLE — CORRODED (BS 1016) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON SPLICE AT AREA AFT OF ACB BS1016 BL0 WL187. MARKED / REMOVED SPLICE ANGLE AT AREA AFT OF ACB BS1016 BL0 WL187 I.A.W SRM 51-40-02-0G-0. REPLACED NEW SPLICE I.A.W SRM 51-40-02-0G-0 AND DWG 147A0070

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,119 hrs · 40,733 cycles

CORROSION ON STRINGER CLIP AT ARE AFT OF ACB BS968 RBL24 WL184. MARKED / REMOVED AND REPLACED NEW STRINGER CLIP (BRACKET) B/S968 RBL24 WL184 P/N 147A7427-11 PO:799248/1 IAW SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 AND DWG 147A0002 REV: 5990U 06AUG20

Part: STRINGER CLIP — CORRODED (BS 966) · airframe 69,119 hrs · 40,733 cycles

CORROSION ON STRINGER CLIP AT ARE AFT OF ACB BS966 RBL32 WL185. MARKED / REMOVED AND REPLACED STRINGER CLIP (BRACKET) AT B/S 966; RBL32; WL185 IAW SRM 51-40-02-0G-0; DWG #147A0002.

Part: FRAME — CORRODED (BS 951) · airframe 69,119 hrs · 40,733 cycles

CORROSION ON FRAME AT AREA AFT OF ACB BS951.07 RBL45 WL189. MARKED / REMOVED AND REPLACED EXISTING DOUBLER ON FRAME IAW SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9 AND DWG 147A8110 REV:C LOCATED B/S 951.07. BTW STRINGER 20R TO STRINGER 21R.

Part: STRAP — CORRODED (BS 697) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON STRAP AT AREA AFT OF ACB BS967 RBL40 WL193. MARKED / REMOVED CORROSION ON STRAP B/S 967 RBL40 WL193 DIMENSIONS L=1' W=0.700' ORIGINAL THICKNESS 0.056' REMAINING THICKNESS 0.053' MATERIAL LOSS 0.003' IAW SRM 51-10-02 PARAGRAPH 15 AND FOUND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-07-1A-1 ALLOWABLE DAMAGE 1 FIGURE 103 DETAIL D

Part: FITTING — CORRODED (BS 1011) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON STRINGER END FITTING AT AREA AFT OF ACB BS1011 LBL9 WL187. MARKED / CORROSION ON STRINGER END FITTING BS1011 LBL9 WL187 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. REMOVED DAMAGED END FITTING; RECEIVED NEW FITTING; LOCATED; DRILLED AND INSTALLED NEW FITTING AT BS1011 LBL9 WL187 IAW SRM 51-40-02; SRM 51-40-05; DWG 147A0070

Part: STRINGER CLIP — CORRODED (BS 968) · airframe 69,119 hrs · 40,733 cycles

CORROSION ON STRINGER CLIP AT ARE AFT OF ACB BS968 RBL32 WL185. REMOVED AND REPLACED STRINGER CLIP B/S 968 RBL 32 WL185 P/N 147A7427-12 PO: 799199/1 IAW SRM 51-40-02 SRM 51-10-02 PARAGRAPH 9 AND DWG 147A0002 REV:.

Part: STRINGER CLIP — CORRODED (BS 967) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON STRINGER CLIP AT AREA AFT OF ACB BS967 S-19R WL196. MARKED / REMOVED AND REPLACED STRINGER CLIP B/S 967 S-19R WL196 P/N 147A3500-14 PO:799170/1 IAW SRM 51-40-02 AND DWG 147A0020 REV: 59900U 06AUG20

Part: HOOK — CORRODED (ESCAPE STRAP) · airframe 69,119 hrs · 40,733 cycles

LH EMERGENCY ESCAPE STRAP HOOK IS CORRODED. / REMOVED L/H EMERGENCY ESCAPE STRAP PER AMM 25-61-10-000-802. 53456C 23JUL20 OK TO INSTALL NEW ESCAPE STRAP. 53456C 22JUL20 INSP 345 22JUL20 INSTALLED L/H EMERGENCY ESCAPE STRAP PER AMM 25-61-10-400-802 STEPS 6A. THROUGH 6.E.(4).

Part: STRAP — CORRODED (EMERGENCY EXIT) · airframe 69,119 hrs · 40,733 cycles

RH EMERGENCY EXIT ESCAPE STRAP HOOK IS CORRODED. / REMOVED R/H EMERGENCY ESCAPE STRAP PER AMM 25-61-10-000-802. 22JUL20 53956C OK TO INSTALL NEW ESCAPE STRAP. 53456C 22JUL20 INSP 345 22JUL20 INSTALLED R/H EMERGENCY ESCAPE STRAP PER AMM 25-61-10-400-802 STEPS 6.A. THROUGH 6.E.(4). 53456C 22JUL20

Part: DOUBLER — CRACKED (BS 663 BULKHEAD) · airframe 69,119 hrs · 40,733 cycles

LH BS 663 VAPOR BARRIER DUCT SEAL ASSY DOUBLER IS CRACKED BETWEEN LBL 15-25 WL 148 / REMOVED & REPLACED DOUBLER ON N/R U191293. RECEIVED NEW DOUBLER FROM OUTSIDE;

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 867-887; R.B.L. 21; W.L. 154. / REMOVED AND REPLACED WITH NEW FLOOR TO SIDEWALL SUPPORT AT BS 867-887 RBL 21; WL 154 IAW SRM 51-40-02; DWG# 146A7500 REV C; DWG# 417A7500 REV D 59042U 31JULY20

Part: FLOOR SUPPORT — CORRODED (BS 772) · airframe 69,119 hrs · 40,733 cycles

CORROSION ON AFT CARGO BAY CARGO FLOOR PANEL SUPPORT AT B.S. 772; R.B.L. 3; W.L. 154. / REMOVED CORROSION AT ACB BS772 RBL3 WL.154 IAW SRM 51-10-02 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1; CUT OUT THE DAMAGE AND REPAIRED FLOOR SUPPORT PANEL AT DIMENTION L=3.4' BY W=.800' IAW SRM 53-00-53-2R-2.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR SHIELD AT B.S. 767-794; R.B.L. 21; W.L. 154. / REMOVED AND REPLACED ON AFT CARGO BAY FLOOR NEW SHIELD AT B/S 767 - 794 RBL 21 P/N 7530271 PO # 761893/1 IAW SRM 51-40-02 AND DWG 146A0081 REV: A 59899U 05AUG20

Part: BEAM — CRACKED (R1 DOOR) · airframe 69,119 hrs · 40,733 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #5 (UPPER) BEAM TO BE CRACKED IN THE RADIUS COMMON TO THE CENTER FASTENER HOLE AT THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / FOWARD SERVICE DOOR #5 LOWER BEAM REPAIRED ON CUSTOMER PO #0520055-H5R

Part: DOUBLER — CORRODED (ANTENNA) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON FORWARD CARGO BAY ANTENNA DOUBLER AT B.S. 500A+11; B.L. 0; W.L. 147. / REMOVED AND REPLACED ANTENN DOUBLER AT BS500A+11; BLO; IAW SRM 51-40-2; SRM 51-40-05; SRM 51-40-06; DWG 143A3233

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 400-420; W.L. 154; R.B.L. 24. / REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT B/S 400 - 420 W.L 154; RBL 24 MATERIAL USED BAC1496-444 # 7075J62 LOT: 1412169-1 IAW SRM 51-40-02; SRM 51-10-02 PARA 9 AND DWG 143A7500 REV: A AND DWG 143A7505 REV:- 59899U 3AUG20

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON AFT CARGO BAY CARGO TRACK AT B.S. 935; R.B.L. 14; W.L. 154. / REMOVED CORROSION ON ACB CARGO TRACK AT BS935 RBL14 IN A 1'X1' AREA; MAX DEPTH .036'. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED ACB CARGO TRACK AT BS887-947; RBL 14 PER SRM 51-40-05; SRM 51-40-02; AND DWG 147A7500

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON AFT CARGO BAY CARGO TRACK AT B.S. 935; L.B.L. 3; W.L. 154. / DAMAGE ON AFT CARGO BAY CARGO TRACK AT BS 935; LBL 3; WL 154 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARA 9 REMOVED DAMAGED TRACK IAW SRM 51-40-02-0G-0. INSTALLED A NEW TRACK IAW SRM 51-40-05; SRM 51-40-02 AND DWG 147A7500

Part: SUPPORT — CORRODED (BS 727-847) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 727-847; L.B.L. 21; W.L. 154. / REMOVED AND REPLACED CORRODED AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 727-847; L.B.L 21; W.L 154 IAW BOEING DRAWING 146A7500; 146A7502 AND SRM 51-40-02. 59807U 8-1-20

Part: SKATE ANGLE — CHAFED (RIGHT) · airframe 69,119 hrs · 40,733 cycles

AFT RH SKATE ANGLE IS CHAFED / REMOVED DAMAGED AFT RH SKATE ANGLE; AND INSTALLED NEW SKATE ANGLE PER SRM 51-40-02 AND DWG 148A8300 SH 1.

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 69,119 hrs · 40,733 cycles

CRACKED GUSSET AT B.S. 500D AT STRINGER 19 LEFT. / REMOVED AND REPLACED NEW GUSSET AT B.S 500D AT STRINGER 19 LEFT P/N 143A9481.5 IAW SRM 51-40-02 AND DWG 143A7902 REV: E 59899U 31JUL20

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 69,119 hrs · 40,733 cycles

CRACKED GUSSET AT B.S. 500D AT STRINGER 19 RIGHT. / REMOVED AND REPLACED NEW GUSSET AT B/S 500D AT STRINGER 19 RIGHT P/N 143 A9481-6 IAW SRM 51-40-02 AND DWG 143A7902 REV: E 59899U 31JUL20

Part: WEB — CORRODED (BS 440-494) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON FORWARD CARGO BAY DOOR SUB WEB THRESHOLD AT B.S. 440-494; W.L. 154; R.B.L. 25. / REMOVED AND REPLACED SUB WEB THRESHOLD AT FORWARD CARGO BAY B/S 440-494 RBL25 WL154 P/O:798180/1 IAW SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 143A8330 REV: A 59900U 01AUG20 (CORROSION OUT OF LIMITS)

Part: CARGO TRACK — CORRODED (BS 790-817) · airframe 69,119 hrs · 40,733 cycles

CORROSION ON AFT CARGO BAY CARGO TRACK AT B.S. 790-817; R.B.L. 14; W.L. 154. / REPLACED AFT CARGO BAY TIE DOWN TRACK BS747+8-B.S 887 RBL 13.8 W.L 156 IAW DWG 146A7500 AND SRM 53-00-53-2R-3

Part: SKATE ANGLE — CHAFED (LEFT) · airframe 69,119 hrs · 40,733 cycles

FWD LH SKATE ANGLE IS CHAFED / REMOVED DAMAGED FWD LH SKATE ANGLE; AND INSTALLED NEW SKATE ANGLE; PER SRM 51-40-02 AND DWG 147A0030 SH. 5.

Part: SHIELD — CORRODED (FWD CARGO) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON FORWARD CARGO BAY FLOOR SHIELD AT B.S. 420-440; W.L. 154; R.B.L. 24. / REMOVED AND REPLACED SHIELD AT FCB BS 420 TO BS 440 RBL 24 WL 154 IAW SRM 51-40-02 AND DWG 143A0080 57049U 30JULY2020

Part: SKATE ANGLE — CHAFED (LEFT) · airframe 69,119 hrs · 40,733 cycles

AFT LH SKATE ANGLE IS CHAFED / REMOVED AND REPLACEMENT L/H SKATE ANGLE AT BS 1016 TO BS 1132 STR. 2L IAW SRM 51-40-02; DWG 148A8300 REV C AND DWG 148A3590 57049U 31JUL2020

Part: SHIELD — CORRODED (FWD CARGO) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON FORWARD CARGO BAY FLOOR SHIELD AT B.S. 494-500A; W.L. 154; R.B.L. 24. / REMOVED & REPLACED FLOOR SHIELD ON FORWARD CARGO BAY AT B.S. 494-500A; RBL 24; WL 154 IAW SRM 51-40-02-0G-0 & DWG 143A0080 REV 59191U 04AUG-20

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,119 hrs · 40,733 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 727-767, RBL 21, WL 154. REMOVED ACB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0. INSTALLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV: C

Part: WEB — CORRODED (BS 794-887) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON AFT CARGO BAY DOOR SUB WEB THRESHOLD AT B.S. 794-887; W.L. 154; R.B.L. 25. / REMOVED AND REPLACED THRESHOLD WEB AT ACB BS 794 TO BS 847 IAW SRM 51-40-02 AND DWG 146A8340 51049U 01AUG20 (CORROSION OUT OF LIMITS)

Part: STRAP — CORRODED (BS 788-800) · airframe 69,119 hrs · 40,733 cycles

***CORROSION*** ON AFT CARGO BAY CARGO TENSION STRAP AT B.S. 788-800; R.B.L. 20; W.L. 154. / REMOVED AND REPLACED TENSION STRAP AT ACB BS774 TO BS862 RBL20 WL154 IAW SRM 51-40-02; DWG 146A0081 REV A AND DWG 146A8120 REV.B 5104U 03AUG20

Part: FLOOR SUPPORT — CORRODED (BS 772) · airframe 69,119 hrs · 40,733 cycles

CORROSION ON AFT CARGO BAY CARGO FLOOR SUPPORT AT BS 772, RBL 8, WL 154. REMOVED CORROSION AT ACB IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. CUT OUT THE DAMAGE AND REPAIRED FLOOR SUPPORT CUT DIMENTION L=3.4' BY W.800' IAW SRM 53-00-53-2R-2.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,119 hrs · 40,733 cycles

RIGHT HORIZONTAL STAB REMOVABLE L/E #2 RIB IS CRACKED / REMOVED RIGHT HORIZONTAL REMOVABLE L/E #2 RIB IAW SRM 51-40-02-0G-0 PARA 4.E & FIG 8. REPLACED RIGHT HORIZONTAL STAB REMOVABLE L/E #2 RIB IAW SRM 51-40-02-0G-0 PARA 4.A THRU D. AND FIGS 3 & 7.

Part: SKATE ANGLE — CHAFED (RIGHT) · airframe 69,119 hrs · 40,733 cycles

FWD RH SKATE ANGLE IS CHAFED / REMOVED DAMAGED FWD RH SKATE ANGLE; AND INSTALLED NEW SKATE ANGLE PER SRM 51-40-02 AND DWG 147A0030 SH. 5.

Part: BOOT — DAMAGED (RADOME) · airframe 69,119 hrs · 40,733 cycles

NOSE RADOMR BOOT IS DAMAGED. / REMOVED AND REPLACED NOSE RADOME PROTECTIVE BOOT IAW AMM 53-52-00-000-802 AND AMM 53-52-00-400-802. 6645U 07/29/20

Part: SKIN — DEBONDED (FAIRING) · airframe 69,119 hrs · 40,733 cycles

FAIRING 193CL OUTER SKIN IS DISBONDED. (MARKED) / FAIRING 193CL OUTER SKIN DISBONDED WAS REPAIRED IAW SRM 51-70-05-2R-2 56144U. 07/23/2020

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 69,119 hrs · 40,733 cycles

INTERIOR SEAT TRACK HAS MECHANICAL DAMAGE AT BS 520 LBL 45; WL 208. MECHANICAL DAMAGE ON SEAT TRACK AT BS520; LBL45; WL208 MEASURES 1.4'X.4'X.050'; FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1. REMOVED AND REPLACED SEAT TRACK AT BS 480-520; LBL 45; PER SRM 51-40-02; SRM 51-40-05; AND DWG 143A5300.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 69,119 hrs · 40,733 cycles

CRACKED LOWER L/H COMPOSITE BULKHEAD AT BS 663, LBL15, WL 148. REPAIRED THE CRACKS ON LOWER L/H COMPOSITE BULKHEAD (VAPOR BARRIER) AT BS663 LBL15 WL148 PER SRM 51-70-04-2R-10.

Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 69,119 hrs · 40,733 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / DENT IN FLIGHT DECK FLOOR AT BS255; RBL4-LBL14; WL207.54 FOUND TO BE OUT OF LIMITS DUE TO NO DENTS ALLOWED PER SRM 53-10-51. REPAIRED FLIGHT DECK FLOOR AT BS255 RBL4-LBL14 PER EA 1-A53-33179 R1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,117 hrs · 40,732 cycles

RIGHT OVERWING EXIT EMERGENCY LIGHT AT LWR FWD CORNER, 1 EA BULB INOPERATIVE.

Part: COVER — MISSING (R2 DOOR SLIDE) · airframe 68,854 hrs · 40,563 cycles

R2 DOOR SLIDE SAFETY COVER MISSING EXPOSING THE RELEASE HANDLE / RETRIEVED AND INSTALLED VELCRO COVER IN PLACE IAW MT.

Part: TRUNNION — CORRODED (LT MLG) · airframe 68,226 hrs · 40,138 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG HAD EVIDENCE OF CORROSION. / REPAIRED LUG PER SWA TASK CARD.

Part: TRUNNION — CORRODED (LT MLG) · airframe 68,226 hrs · 40,138 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG HAD EVIDENCE OF CORRODED. / REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 68,226 hrs · 40,138 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD LUG HAD EVIDENCE OF CORROSION. / REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 68,226 hrs · 40,138 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG HAD EVIDENCE OF CORROSION. / REPAIRED LUG PER EA.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 67,591 hrs · 39,742 cycles

L1 DOOR SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: NONE — BROKEN (LWR FUSELAGE) · airframe 65,927 hrs · 38,687 cycles

LOWER EDGE OF EGPR DOUBLER IS BROKEN WITH MISSING MATERIAL AND ASSOCIATED DISBANDED SKIN. / ACCOMPLISHED REPAIR OF THE ELECTIRCAL GROUND POWER RECEPTACLE SURROUND LOWER EDGE; IAW SRM 53-10-15.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,192 hrs · 36,911 cycles

RT FORWARD INTERIOR EMERGENCY LIGHTS INOP. R&R BATTERY PACK IAW MM.

Part: FAIRING — CRACKED (RT WING) · airframe 63,161 hrs · 36,896 cycles

RIGHT OVERBAORD CANOE APPEARS TO HAVE CRACKS / CLEARING DMA LG PG 0092810 INSTALLED #8 TAIL CONE IAW M/M 27-51-28 CLEARING# 77888

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,061 hrs · 36,835 cycles

RT EXIT UPPER LIGHT INOP. R&R LIGHT IAW AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 63,053 hrs · 36,829 cycles

AFT CARGO DOOR CUTOUT FWD CORNER SCUFF PLATE IS CRACKED / ACCOMPLISHED REPAIR OF FWD CORNER SCUFF PLATE ON AFT CARGFO DOOR CUTOUT IAW SWA E/A 1-A53-2076 REV 11

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,053 hrs · 36,829 cycles

PASSENGER CABIN FLOOR PANEL 231YF HAS EDGE DAMAGE AT AFT INBD SIDE / EVALUATED; PREPPED; CLEANED AND REPAIRED DAMAGE TO TOP FACE SHEET AND AFT EDGE ON FLOORBOARD 231YF IAW B737 SRM 53-00-50-2R-4; PARA3 (A - K1; L1; M1) REV 64.

Part: NONE — CRACKED (LT WING) · airframe 63,053 hrs · 36,829 cycles

SUPPLEMENTAL INFORMATION: LH TE WING PANEL T/E BEAM FOR 561AB BROKEN / INSTALLED LH T/E WING PANEL BEAM FOR PANEL 561 AB IAW B737-700 SRM 51-40-02-0G-0.TAG WN4447

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

SUPPLEMENTAL INFORMATION: PASSENGER CABN AFT WET AREA FLOOR PANEL 242UF; TOP SURFACE IS DELAMINATED. / INSTALLED NEW FLOO PANEL 242UF AT AFT WET AREA IAW-AMM 53-21-00-400-801 WN4989

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS 727A TO BS 727B, RBL 13.8. REPAIRED INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 294 TO BS 312, RBL 31. R&R INTERCOSTAL IAW DWG AND SRM.

Part: PANEL — DELAMINATED (L/H WING) · airframe 63,053 hrs · 36,829 cycles

LH WING PANEL 521JB HAS DELAM / REPAIRED PANEL 521 JB EDGE EROSION STRIP IAW B737-700 SRM B737 700 SRM 57-41-01-2R-6 REV 64; AMM 51-21-89-300-801 REV 65

Part: PANEL — DELAMINATED (L/H WING) · airframe 63,053 hrs · 36,829 cycles

LH WING PANEL 521 WB HAS DELAM / REPAIRED LH WING PANEL 521 WB ON I/B MID CORNER AT EDGE STRIP IAW B737 SRM 57-41-01-2R-6 REV 64. CURED IN OVEN FOR 1HR IN AT 2:00PM OUT AT 3:00PM OVEN (EO-01 EXP 7-23-18) A61722

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 63,053 hrs · 36,829 cycles

PAX CABIN FLOOR BOARD 231WF; SEGMENT OF UPPER SURFACE FIBERGLASS PULLED UP. / REPAIRED PASSENGER CAIN FLOORBOARD 231WF UPPER SURFACE 4 1/2' AFT OF FWD EDGE ON I/B SIDE IAW B737 SRM 53-00-50-2R-1. CURED IN OVEN FOR 1 HR. IN AT 9:30 - OUT AT 10:30 A94393 A59142

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 63,053 hrs · 36,829 cycles

FWD CARGO COMPARTMENT LH BAFFLE CLIP CRACKED AT FWD SIDE BS 500B / FWD CARGO L/H CLIP ANGLE AT BAFFLE FWD SIDE OF STA 500B CRACKED . DRILLED AND REMOVED CRACKED ANGLE CLIP I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW ANGLE CLIP I/A/W SRM 51-40-02-0G-0 ALSO BOEING DWG 143A7505 REV B. INSTALLED NEW ANGLE CLIP I/A/W SRM 51-40-02-0G-0 ALSO BOEING DWG 143A7505 REV B TAG A05262

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

AFT CARGO COMPARTMENT BULKHEAD SUPPORT ANGLE AT BS 947, LBL 9. R&R SUPPORT IAW SRM AND DWG.

Part: PANEL — DELAMINATED (L/H WING) · airframe 63,053 hrs · 36,829 cycles

LH WING PANEL 521 DB HAS DELAM ON 3 EA CORNERS / REPAIRED L/H WING PANEL 521DB OF LIGHT DELAM AT THREE CORNERS (MARKED) IAW B737 SRM 57-41-01-2R-6 REV 64

Part: PANEL — DELAMINATED (#1 PYLON) · airframe 63,053 hrs · 36,829 cycles

#1 PYLON PANEL 431DR AFT UPPER CORNER IS DELAM / REPAIRED #1 PYLON PANEL 431DR AFT UPPER CORNER I/A/W 737-700 SRM 51-70-04-2R-13 REV 64 PER 737-700 SRM 54-50-70-2R-2 REV 64.

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 63,053 hrs · 36,829 cycles

FWD CARGO COMPARTMENT LH BAFFLE CLIP CRACKED ON AFT SIDE BS 500C / FWD CARGO L/H BAFFLE WEB CLIP CRACKED AT AFT SIDE OF STA 500C. DRILLED AND REMOVED CRACKED WEB CLIP I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW WEB CLIP I/A/W SRM51-40-05-0G-0 ALSO BOEING DWG 142A7505 REV A. INSTALLED NEW L/H WEB BAFFLE CLIP AT AFT SIDE OF STA 500C I/A/W SRM 51-40-02-0G-0 ALSO BOEING DWG 142A7505 REV A.

Part: PANEL — DELAMINATED (L/H WING) · airframe 63,053 hrs · 36,829 cycles

LH WING PANEL 521 TB HAS DELAM ON CORNER / REPAIRED LH WINE PANEL 521TB DELAM ON I/B UPPER CORNER IAW B737 SRM 57-41-01-2R-6 REV 64 A09712

Part: PANEL — DEBONDED (R/H WING) · airframe 63,053 hrs · 36,829 cycles

RIGHT WING; LWR INBD FIXED T/E PANE 621DB; EDGE IS DISBONDED / REPAIRED RIGHT WING ;WR INBD FIXED T/E PANEL 621DB OF LIGHT EDGE DELAMUNATION IAW B737 SRM 57-41-01-2R-6 REV 64.

Part: FLOOR PANEL — PULLED (CABIN FLOOR) · airframe 63,053 hrs · 36,829 cycles

PAX CABIN FLOOR BOARD 241DF; UPPER SURFACE; NUMEROUS AREAS OF PULLED FIBERGLASS THREADS. / FABRICATED NEW FLOOR PANEL 241OF IAW B737 SRM 53-00-50-2R-0 PARA 1A REV 64 1 BAC 5085 REV D PER DWG 144A5810 5H9

Part: PANEL — DEBONDED (R/H WING) · airframe 63,053 hrs · 36,829 cycles

RIGHT WING; LWR INBD FIXED T/E PANE 621UB; CORNER IS DISBONDED / EVALUATED AND REPAIRED RIGHT WING LWR INBD FIXED T/E PANEL 621UB OF A DISBONDED CORNER AS MARKED IAW B737-700 SRM 57-41-01-2R-6 REV 64. AG1722

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 63,053 hrs · 36,829 cycles

FWD CARGO COMPARTMENT LH BAFFLE CLIP CRACKED AT FWD SIDE BS 500C / FWD CARGO L/H BAFFLE CLIP ANGLE CRACKED AT STA 500C; FWD SIDE . DRILLED AND REMOVED ANGLE CLIP I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW ANGLE CLIP I/A/W SRM 51-40-02-0G-0 ALSO BOEING DWG 143A7505 REV- B. INSTALLED NEW ANGLE CLIP I/A/W SRM 51-*40-02-0G-0 ALSO BOEING DWG 143A7505 REV-B AND BAFFLE STA 500B TO STA 500C. TAG A05262

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 63,053 hrs · 36,829 cycles

PAX CABIN FLOOR BOARD 241AF; UPPER AND LOWER SURFACES HAVE AREAS OF PULLED UP/OUT FIBERGLASS THREADS. / FABRICATED NEW FLOORBOARD 241AF USING 9WN1135) FLOORBOARD (A29251) INSERTS AND (A24893) ADHESIVE IAW B737 SRM 53-0-50-2R-0 (PAR 4A) & BOEING DWG # 144A5-810; (FRAME 3) REV B. BAC5085- REV; 4. AAR OVEN (EO-01) DUE 07-23-18; TIME IN 7.AM TIME OUT 8AM @ 140 DEGREE F.

Part: PANEL — DELAMINATED (L/H WING) · airframe 63,053 hrs · 36,829 cycles

LH WING PANEL 521 NB HAS DAMAGE AND DELAM / REPAIRED PANEL 521NB METAL EROSION STRIP DISBOND IAW B737 SRM 57-41-01-2R-6.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

AFT CARGO COMPARTMENT Z ANGLE CRACKED AT BS 747. R&R Z ANGLE IAW SRM & DWG.

Part: INSERT — CORRODED (FLOORBOARD) · airframe 63,053 hrs · 36,829 cycles

CABIN FLOOR BOARD 221 AF INSERTS CORRODED. R&R INSERTS IAW SRM.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

WING TO BODY PANEL 193AR LOWER INBOARD FASTENER HOLES ARE OBLONG AND ELONGATED (MARKED) / REPAIRED FASTENER HOLES ALONG LOWER EDGE AS MARKED ON PANEL 193AR. IAW B737-700 SRM 53-40-70-1A-1 ALLOWABLE DAMAGE 1; SRM 53-40-70-2R-1 REPAIR 1; SRM 51-70-05-2R-8 REPAIR 8; SRM 51-70-05-2R-0 REPAIR GENERAL; AMM 51-21-99-300-801.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 63,053 hrs · 36,829 cycles

FWD CARGO COMPARTMENT LH FLOOR BAFFLE IS CRACKED AT BS 500-500A; BELOW Z ANGLE / FWD CARGO L/H FLOOR BAFFLE STA 500 TO STA 500A CRACKED. DRILLED AND REMOVED CRACKED L/H BAFFLE I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW L/H BAFFLE I/A/W SRM 51-40-02-0G-0 ALSO BOEING DWG 143A7505 REV-. INSTALLED NEW L/H BAFFLE AT STA 500 TO STA 500A I/A/W SRM 51-40-02-0G-0 ALSO BOEING DWG 143A7505 REV- TAG A58739

Part: PANEL — CORRODED (NOSE WHEEL WELL) · airframe 63,053 hrs · 36,829 cycles

NOSE WHEEL WELL PANEL 113AC MATING SURFACE HAS CORROSION AROUND FASTENER HOLES (MARKED) / NO ALLOWABLE DAMAGE LIMITS FOUND REPLACED PANEL P/N 141A7900-6 SI# 7320265 ATAG: WN 4042 IAW B737-700 AIPC 32-22-11-02 VERIFIED PLACARDS MARKER IAW B737-700 AIPC 11-22-03-02 BAC27 DBY 0170; BAC27DBY 194; AND BAC27DBY 195 AND AMM 20-10-14-400-801

Part: ANGLE — CRACKED (AFT CARGO BAY) · airframe 63,053 hrs · 36,829 cycles

AFT PIT (LEEKA ANGLE) STA 867 LBL 16 AT THE LAV TANK STANCHON IS CRACKED / AFT PIT (LEEKA ANGLE) STA 867 LBL 16 CRACKED. REPLACED WITH NEW BRACKET P/N 149A81090114 ATAG A25822 IAW BOEING DWG 149A8109 REV -

Part: PANEL — CORRODED (NOSE WHEEL WELL) · airframe 63,053 hrs · 36,829 cycles

NOSE WHEEL WELL PANEL 113BW MATING SURFACE HAS CORROSION AROUND FASTENER HOLES (MARKED) / NO ALLOWABLE LIMITS FOUND REPLACED PANEL 113BW RKED) P/N:141A7900-4 SI# 7320579 ATAG:KJ1227 IAW B737-700 AIPC 32-22-11-02 AND PLACARD IAW AIPC 11-22-03-02 NOSE WHEEL WELL PANEL

Part: FLOOR PANEL — CORRODED (CABIN FLOOR) · airframe 63,053 hrs · 36,829 cycles

CABIN FLOORBOARD 222 BF INSERTS ARE CORRODED / REPAIRED AND INSTALLED NEW INSERTS ON PANEL 222BF IAW B737-700 SRM 53-00-50-2R-6 REV 64; SRM 53-00-50-2R-0 REV 64

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 63,053 hrs · 36,829 cycles

FWD CARGO COMPARTMENT LH FLOOR BAFFLE BS 500A-500B IS CRACKED; BELOW Z ANGLE / FWD CARGO L/H SIDE CRACKED BAFFLE STA 500A TO STA 500B . DRILLED AND REMOVED CRACKED BAFFLE I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW L/H BAFFLE I/A/W SRM 51-40-02-0G-0 ALSO BOEING DWG 143A7505 REV B. INSTALLED NEW L/H BAFFLE AT STA 500A TO STA 500B I/A/W SRM 51-40-02-0G-0 ALSO BOEING DWG 143A7505 REV B

Part: FLOOR PANEL — DEBONDED (CABIN FLOOR) · airframe 63,053 hrs · 36,829 cycles

CABIN FLOORBOARD 221 GF CORNER IS DISBONDED / REPAIRED DISBONDED CORNER OF PANEL 221GF; IAW B737-700 SRM 53-00-50-2R-9 REV 64; SRM 53-00-50-2R-0 REV 64

Part: PANEL — CORRODED (NOSE WHEEL WELL) · airframe 63,053 hrs · 36,829 cycles

NOSE WHEEL WELL PANEL 114AC MATING SURFACE HAS CORROSION AROUND FASTENER HOLES (MARKED) / NO ALLOWABLE LIMITS FOUND REPLACED PANEL 114AC P/N: 141A7900-6 SI#: 732026 ATAG:KJ1221 IAW B737-700 AIPC 32-22-11-02 AND PLACARDS IAW AIPC 11-22-03-02 NOSE WHEEL WELL PANEL

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

FORWARD WET AREA FLOOR INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, BL 0. R&R INTERCOSTAL IAW SRM & DWG.

Part: WEB — CORRODED (CABIN) · airframe 63,053 hrs · 36,829 cycles

CABIN FLOOR NUT PLATE HOLE AT STA. 1005 LBL 40 HAS CORROSION / CABIN FLOOR NUT PLATE HOLE AT STA 1005 LBL 40 WEB CORROSION FOUND TO BE 'OUT OF LIMITS' AT ORIGINAL .020' REMOVED .006 REMAINING 014'. REPLACED WITH PN:147A562002 SI#7531092 TAG#WN0745 IAW BOEING DWG #147A5600 REV H AND SRM 51-40-02-0G-0

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,053 hrs · 36,829 cycles

AFT CARGO COMPARTMENT; STA 887; FLOOR BOARD SPLICE STRAP; HAS MULTIPLE AREAS OF CORROSION / REMOVED CORROSION ON AFT CARGO STA 887 FLOOR SPLICE STRAP IAW B737 SRM 51-10-02-08-0 100% MATERIAL LOSS RELOCATED AND DRILLED NEW FLOOR SPLICE IAW B737-700 SRM 51-40-05 AND DWG 146A9401 REV: A INSTALLED NEW FLOOR SPLICE IAW B737 SRM 51-40-02 AND DWG 147A 7500 REV :B APPLIED CIC IAW B737 AMM 51-21--81-620-802.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

FORWARD WET AREA FLOOR INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R&R INTERCOSTAL IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

R1 DOOR SURROUND STRUCTURE STUB FRAME CRACKED AT BS 294, RBL 55. R&R STUB FRAME IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 11. REPAIRED INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

FORWARD WET AREA FLOOR MACHINED INTERCOSTAL CRACKED BETWEEN BS 294 TO BS 312, RBL 16. R&R INTERCOSTAL IAW DWG & SRM.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 63,053 hrs · 36,829 cycles

_AFT CARGO COMPARTMENT STA 727A + 18' TO STA 807 + _10' L/H 'Z' ANGLE CORRODED. 'MARKED IN RED' / AFT CARGO COMPARTMENT STA 727A+18' TO STA 807+10' L/H Z-ANGLE CORRODED. REPLACE Z-ANGLE ON L/H SIDE FROM STA 727 TO STA 847 ON NON-ROUTINE X752154

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 63,053 hrs · 36,829 cycles

AFT CARGO COMPARTMENT; SHIELD AFT OF CARGO DOOR; HAS MULTIPLE AREAS OF CORROSION / REMOVED CORROSION IAW SRM 51-10-02-0G-0 PARA 15 VERIFIED BY 10X MAG; ORIGINAL 'T'=.050; LOSS=.015; REMIANING MATERIAL=.035 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 AAR 36649 DUE CAL 7-5-18. VERIFIED NEW PART SHIELD ASSY 146A8127Y5 SI 7530336 ATAG WN4325 IAW BOEING 146A0081 REV:C; LOCATED AND DRILLED NEW SHIELD ASSY IAW SRM 51-40-05-0G-0 AND BOEING DWG 146A0081 REV:C INSTALLED NEW SHIELD ASSY IAW B737-700 SRM 51-40-02-0G-0 AND BOEING DWG 146A0081 REV:C TAG WN4325

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

FORWARD CARGO COMPARTMENT LT Z ANGLE CORRODED BETWEEN BS 500A+10 TO BS 500D. R&R Z ANGLE IAW SRM.

Part: CHANNEL — CORRODED (AFT CARGO COMPT) · airframe 63,053 hrs · 36,829 cycles

AFT CARGO COMPARTMENT; R/H Z-CHANNEL; HAS MULTIPLE AREA OF CORROSION; STA 887 TO 947 / REMOVED CORROSION FROM AFT CARGO COMPARTMENT R/H Z ANGLE STA 887 TO 947 AND CHECK LIMITS FOUND TO BE OUT OF LIMITS ORIGINAL 'T' .040' LOSS .014' REMAIN .026' FABRICATED Z ANGLE REPAIR TREATED PRIMED AND INSTALLED Z ANGLE IAW SRM 51-10-02; SRM 53-00-53-1A-2 62-40-02. SRM 51-40-05DWG 147A7500 REV - AMM 51-21-41-370-803 AND AMM 51-21-72-370-801 # ATAG 51-21-72-370-801 # ATAG A21656

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

R1 DOOR CREASE BEAM INNER CHORD ANGLE CORRODED BETWEEN BS 304 TO BS 324, RBL 60. R&R ANGLE IAW DWG AND SRM.

Part: ANGLE — CRACKED (BS 500D) · airframe 63,053 hrs · 36,829 cycles

FORWARD CARGO BAY, ZEE ANGLE CRACKED AT BS 500D, STRINGER 26L. R & R THE ANGLE IAW SRM & DWG.

Part: STRIP — BROKEN (FWD CARGO RH) · airframe 63,053 hrs · 36,829 cycles

FWD CARGO COMPARTMENT STA 440 STR 26R; UNDER FRAME UPPER LIP HAS NUTPLATE SUPPORT STRIP BROKEN. / REMOVED AND REPLACED FWD CARGO COMP STA. 440 NUTPLATE STRIP UNDER FRAME UPPER LIP @ S-26R P/N:143A8200 - 7. FABRICATION APPROVAL GRANTED BY SMAL REQUEST P/O:1544198 AND CONFORMITY INSPECTION VERIFIED IAW BAC DWG 143A8200 REV. H PART INSTALLED IAW B737-700 SRM 51-40-02-0G-0 AND AMM 51-31-00-390-805 AND BAC DWG 143A8200 REV. H.

Part: PLATE — CORRODED (LOWER INT FUSELA) · airframe 63,053 hrs · 36,829 cycles

FWD CARGO COMPARTMENT FLOOR STA 500 TO STA 500A BL 0; INTERNAL ANTENNA SUPPORT PLATE HAS CORROSION. / FWD CARGO COMPARTMENT FLOOR STA 500-500A BLO ANTENNA SUPPORT PLATE HAS CORROSION BLENDED CORROSION AND FOUND CRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED AND REPLACED WITH NEW SUPORT PLATE IAW BOEING DWG #143A3230 REV A AMD SRM 51-40-02-0G-0

Part: CHANNEL — CORRODED (AFT CARGO COMPT) · airframe 63,053 hrs · 36,829 cycles

AFT CARGO COMPARTMENT; STA 867 TO 887; R/H Z-CHANNEL HAS CORROSION / REMOVED CORROSION FRM AFT CARGO COMPARTMENT STA 867 TO 887 R/H CHANNEL AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS WIH ORIGINAL 'T' .040' LOSS .10' REMAININ .030' FABRICATED Z ANGLE REPAIR ; TREATED AND PRIMED REPAIR INSTALLED Z ANGLE IAW SRM 51-10-02 SRM 53-00-53-1A-2 SRM 51-40-02; DWG 147A7500 REV -AMM 51-21-41-370-803 AND AMM 51-21-72-370801

Part: SHIELD — CORRODED (FWD CARGO RH) · airframe 63,053 hrs · 36,829 cycles

FWD CARGO COMPARTMENT STA 492 TO STA 500A STR 26R; FLOOR SUPPORT SHIELD HAS CORROSION. / BLENDED OUT CORROSION ON FLOOR SUPPORT SHIELD STA 492-500 IAW B737 SRM 51-10-02-0G-0. ORIGINAL THICKNESS 0.032'; MAT LOSS: 0.009'; MAT REMAINING 0.023'; THE AREA FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-30-15-1A-1; FIGURE 103; LOCATED AND DRILLED NEW SHIELD P/N :145A8126V31 IAW B737 SRM 51-40-05 AND DWG 143A0080 REV:-; INSTALLED NEW SHIELD IAW B737-700 SRM 51-40-02 AND DWG 143A0080; REV:- ATAG: WN1923

Part: ANGLE — CORRODED (FWD CARGO COMPT) · airframe 63,053 hrs · 36,829 cycles

FWD CARGO COMPARTMENT FLOOR STRUCTURE STA 500D LBL 24 TO RBL 24 L-ANGLE HAS CORROSION. / REMOVED CORROSION FROM FWD CARGO COMPARTMENT FLOOR STRUCTURE STA 500D LBL 24 TO RBL 24 L-ANGLE AND CHECKED LIMIT FOUND TO BE OUT OF LIMIT WITH .017' LOSS REMAIN .054' ORIG T' .071'; RECEIVED; LOCATED DRILLED NEW PART INSTALLED NEW PART IAW SRM 51-10-02; SRM 53-00-53-1A-2; SRM 51-40-02; DWG 143A9481 REV B; AND DWG 143A9485 REV B

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

FORWARD WET AREA FLOOR INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL IAW SRM AND DWG.

Part: WEB — CORRODED (FWD CARGO THRESH) · airframe 63,053 hrs · 36,829 cycles

FWD CARGO COMPARTMENT THESHOLD SILL WEB HAS CORROSION. / REMOVED CORROSION I/A/W SRM 51-10-02-0G-0; ORIGINAL MATERIAL .045'; LOSS .014' REMAINING .031' FOUND TO BE OUT OF LIMITS I/A/W SRM 53-30-15-1A-1 FIGURE 103 D. REMOVED AND INSTALLED NEW WEB AT FORWARD CARGO COMPARTMENT THRESHOLD I/A/W B737 SRM 51-40-02-0G-0 AND BOEING DRAWING

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

AFT CARGO COMPARTMENT FRAME CORRODED AT BS 947, BETWEEN LBL 23 TO RBL 23. R&R FRAME IAW SRM & DWG.

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 63,053 hrs · 36,829 cycles

AFT CARGO COMPARTMENT STA 767 TO STA 787 FWD SHIELD CORRODED. / REMOVED CORROSION ORIGINAL 'T' IS .050' AFTER REWORK .042' .008' MATERIAL LOSS; OUT OF LIMITS IAW SRM 53-60-15-1A-1. AAR TOOL #18173 CAL DUE #11/27/18. REMOVED OUT OF LIMITS SHIELD STA 767 TO 794 RH AND INSTALLED NEW SHIELD ALL IAW SRM 51-40-02-0G-0 AND DWG #146A8127 REV C.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

AFT CARGO COMPARTMENT STRINGER CORRODED AT BS 727A+9, STR 26R. REPAIRED STRINGER IAW SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

L1 DOOR CREASE BEAM INNER CHORD CRACKED AT BS 302, LBL 55. R&R CHORD PER DWG AND SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 32. R&R INTERCOSTAL IAW SRM & DWG.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 63,053 hrs · 36,829 cycles

AFT CARGO COMPARTMENT; STA 947; AFT BULKHEAD SUPPORT ANGLE; HAS MULTIPLE AREAS OF CORROSION / REMOVED CORROSION/VERIFIED LIMITS AFT BULKHEAD SUPPORT ANGLE @ STA 947 (ORIGINAL T: .080')(LOSS: .009') (REMAINING: .071') OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103(D). REMOVED/REPLACED AFT BULKHEAD SUPPORT ANGLE IAW SRM 51-40-02-0G-0/ BOEING DWG# 149A8118 REV D. TAG# WN3822 TOOL ID# 36307 DUE: 10/17/18

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,053 hrs · 36,829 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R&R INTERCOSTAL IAW SRM AND DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,053 hrs · 36,829 cycles

HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS 663 TO BS 675, BETWEEN LBL 30 TO LBL 45. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — DELAMINATED (RT MLG WW) · airframe 63,053 hrs · 36,829 cycles

RT MAIN WHEEL VERTICAL BULKHEAD VAPOR BARRIER DELAMINATED AT BS 663, INBOARD EDGE. REPAIRED BARRIER IAW SRM.

Part: VALVE — OPEN (NR 2 ENGINE) · airframe 62,314 hrs · 36,362 cycles

THE NR 2 ENGINE FAILED AT FL 370 WHILE IN DESCENT TO FL 350. R & R THE VALVE IAW MM.

Part: PLATE — CRACKED (LT WING) · airframe 61,965 hrs · 36,124 cycles

LT WING LOWER TRAILING EDGE SHELF PANEL WIGGLE PLATE CRACKED. R & R WIGGLE PLATE IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,966 hrs · 36,124 cycles

AFT PRESSURE BULKHEAD WEB OIL CANNED BETWEEN STR 3L AND STR 4L FROM Y CORD TO THE FIRST CIRCUMFERENTIAL STRAP. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,965 hrs · 36,124 cycles

EMERGENCY BATTERY PACK FAILED A CAPACITY CHECK AT LOCATION M01670. R & R THE BATTERY PACK IAW AMM.

Part: BULKHEAD WEB — CANNING (BS 1016) · airframe 61,965 hrs · 36,124 cycles

AFT PRESSURE BULKHEAD WEB OIL CANNED BETWEEN STRINGER 3L AND 4L . REPAIRED THE BULKHEAD WEB IAW ER AND EA.

Part: PLATE — PULLED (RT WING) · airframe 61,965 hrs · 36,124 cycles

RT WING LOWER FIXED T/E PANEL WIGGLE PLATE O/B OF AFT PYLON RIVETS PULLED / R&R RT WING LOWER FIXED T/E PANEL WIGGLE PLATE O/B OF AFT PYLON PER SRM 51-40-02

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,965 hrs · 36,124 cycles

EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01673. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,965 hrs · 36,124 cycles

EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01672. R & R THE BATTERY PACK IAW AMM.

Part: GIRT BAR — LOOSE (R2 DOOR SLIDE) · airframe 61,965 hrs · 36,124 cycles

R2 DOOR SLIDE GIRT BAY MATERIAL LOOSE. SECURED THE SLIDE IAW MT.

Part: RETAINER — CRACKED (RT WING) · airframe 61,965 hrs · 36,124 cycles

AFT OF #2 PYLON T/E VERTICAL SEAL RETAINER CRACKED / REMOVED AND REPLACED SEAL RETAINER IAW 51-40-02 SRM

Part: NONE — BROKEN (LOWER EXT FUSELA) · airframe 61,251 hrs · 35,665 cycles

RH FWD FAIRING RAM AIR INLET AFT CLIP OUTBD SIDE IS BROKEN OFF. (LOCATED INSIDE RAM AIR AIR DUCT PATH) / REPLACED RH RAM AIR INLET AFT CLIP PER SRM 51-40-02. REMOVED AND REINSTALLED RH RAM INLET MODULATION PANELS PER MM 21-51-23.

Part: RIB — CRACKED (LT WING) · airframe 61,106 hrs · 35,581 cycles

LEFT WING MID SPAN DEFLECTION RIB UPPER TAB CRACKED 2.0 + INCHES / REMOVED AND REPLACED LEFT WING MID SPAN DEFLECTOR RIB PER SRM 51-40-02.

Part: WEB — CRACKED (BS 665) · airframe 60,016 hrs · 34,917 cycles

RIGHT WHEEL WELL CEILING FORWARD BEADED WEB CRACKED AT BS 665, RBL 43. REPAIRED THE WEB PER EA.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 60,016 hrs · 34,917 cycles

FORWARD GALLEY FLASHLIGHT RESTRAINING STRAP BROKEN. R & R THE STRAP IAW MM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 59,905 hrs · 34,847 cycles

FORWARD LT PHOTO LUMINESCENT STRIP CRACKED. R&R STRIP PER MM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 59,905 hrs · 34,847 cycles

RT FORWARD PHOTO LUMINESCENT STRIP CRACKED. R&R STRIP PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 59,257 hrs · 34,477 cycles

L1 DOOR EMERGENCY EXIT LENS MISSING. REPLACED THE LENS IAW AMM.

Part: CASTING — CRACKED (R1 DOOR) · airframe 57,809 hrs · 33,635 cycles

R1 DOOR CRACKED IN CASTING BELOW THE BOX ASSEMBLY HOUSING AT THE FORWARD INBOARD ATTACH BOLT. R & R R1 DOOR IAW MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 57,020 hrs · 33,206 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN LENS MISSING. REPLACED THE LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,808 hrs · 33,087 cycles

RIGHT OVERWING FORWARD LOWER EMER EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,808 hrs · 33,087 cycles

FORWARD ENTRY, FORWARD LOWER EMERGENCY EXIT LIGHT BULB INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

FRAME CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

RIGHT BULKHEAD LOWER FRAME WEB CRACKED AT BS 727, INBD OPEN FASTENER HOLE AT WL 200. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,808 hrs · 33,086 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 28. REPAIRED WEB ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,808 hrs · 33,086 cycles

FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,808 hrs · 33,086 cycles

RIGHT WING NR 6 SLAT LOWER LE SKIN CRACKED AT ACTUATOR RIBS. REPAIRED SLAT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,808 hrs · 33,086 cycles

LEFT WING NR 2 SLAT LOWER LE SKIN CRACKED AT ACTUATOR RIBS. REPAIRED NR 2 SLAT IAW SRM.

Part: FLAP — LOOSE (LT WING) · airframe 56,653 hrs · 32,992 cycles

LEFT WING OTBD TE AFT FLAP LOOSE. R & R AFT FLAP IAW AMM.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 56,475 hrs · 32,882 cycles

DIVERSION, WHILE CRUISING AT FL 390 CABIN ALTITUDE RATE OF CHANGE WENT TO 4000 FPM CLIMB. R & R AFT OUTFLOW VLV ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,408 hrs · 32,845 cycles

RIGHT OVERHEAD EMER LIGHT BULB, BETWEEN ROW 18 - 19 INOPERATIVE. R & R BULB IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 56,229 hrs · 32,740 cycles

R2 DOOR LOWER EMER EXIT SIGN LIGHT BROKEN. R & R POWER SUPPLY IAW MM.

Part: LIGHT — BROKEN (EXIT SIGN) · airframe 56,229 hrs · 32,740 cycles

R2 DOOR LOWER EMER EXIT SIGN LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 56,127 hrs · 32,684 cycles

EXTERNAL POWER DOOR CUT OUT CRACKED AT THE AFT LOWER SIDE & THE FWD LOWER SIDE. REPAIRED CUT OUT DOUBLER IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 55,985 hrs · 32,598 cycles

FORWARD ENTRY DOOR, EMER EXIT LIGHT LENS LOOSE. SECURED LENS IAW AMM.

Part: ROLL PIN — MISSING (R1 DOOR) · airframe 55,861 hrs · 32,523 cycles

R1 DOOR EMER EVAC SLIDE LATCH BLOCK MISSING ROLL PIN. INSTALLED ROLL PIN IAW SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,861 hrs · 32,523 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M10675. R & R BATTERY PACK IAW AMM.

Part: GLOWSTRIP — CHIPPED (CABIN) · airframe 55,861 hrs · 32,523 cycles

RIGHT PHOTO LUMINESCENT STRIP CHIPPED AT ROW 1. R & R STRIP IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,861 hrs · 32,523 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M10668. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,861 hrs · 32,523 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M10669. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,861 hrs · 32,523 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT LOCATION M10674. R & R BATTERY PACK IAW AMM.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 55,070 hrs · 32,064 cycles

INFLIGHT SHUTDOWN, AIR TURN BACK, DECLARED EMER. AT ROTATION, RT ENG SURGED & STALLED, BANGING NOISE, RETARDED THROTTLE. RAN QRH SINGLE ENG & APPROACH. EGT INDICATION WENT RED 965 DEGREES. FLIGHT ATTENDANT REPORTED FLAMES FROM ENG. R & R NR 3 MOTOR ASSEMBLY IAW MT.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 54,668 hrs · 31,810 cycles

FORWARD ENTRY DOOR EXIT SIGN FELL OFF. REINSTALLED LENS IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,771 hrs · 31,290 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 53,657 hrs · 31,226 cycles

M01672 EMER LIGHTS BATTERY PACKS FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 53,657 hrs · 31,226 cycles

M01673 EMER LIGHTS BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 53,507 hrs · 31,133 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE AMM.

Part: POST — CRACKED (FUSELAGE) · airframe 53,497 hrs · 31,127 cycles

LEFT NR 3 FLIGHT DECK WINDOW FRAME E - F POST CRACKED AT THE SECOND LOWER FASTENER HOLE. REPAIRED POST IAW ACO.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 53,177 hrs · 30,930 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. REINSTALLED SLIDE IAW MT.

Part: LENS — LOOSE (EXIT SIGN) · airframe 52,591 hrs · 30,588 cycles

L1 DOOR EMER EXIT SIGN LIGHT HOUSING LENS LOOSE. REPAIRED LIGHT IAW EA.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 52,076 hrs · 30,293 cycles

R1 DOOR EVACUATION SLIDE LOOSE. SECURED SLIDE APR MM.

Part: COVER — MISSING (CABIN) · airframe 51,872 hrs · 30,187 cycles

R2 DOOR EXIT LIGHT COVER ON MIDDLE SIDE WALL MISSING. INSTALLED COVER IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 51,272 hrs · 29,828 cycles

L1 DOOR EXIT SIGN LOOSE. R & R SIGN IAW MM.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 51,080 hrs · 29,711 cycles

DIVERSION A SYS HYD FLUID LOSS IN FLIGHT. R & R NR 1 ENG TO PRESS MODULE UNION O RING IAW MM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,310 hrs · 29,265 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75. R & R SEAT TRACK IAW EA.

Part: FITTING — LOOSE (R1 DOOR) · airframe 50,310 hrs · 29,265 cycles

R1 DOOR EMERGENCY EVAC SLIDE FLOOR MOUNTED GIRT FITTING LOOSE AFT POSITION. SECURED FITTING IAW AMM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 50,310 hrs · 29,265 cycles

L2 DOOR EMERGENCY EVAC SLIDE FLOOR MOUNTED GIRT BAR FITTINGS LOOSE. SECURED FITTINGS IAW AMM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 50,310 hrs · 29,265 cycles

R2 DOOR EMERGENCY EVAC SLIDE FLOOR MOUNTED GIRT BAR FITTINGS LOOSE. SECURED FITTINGS IAW AMM.

Part: ANGLE — CRACKED (RT WING) · airframe 50,310 hrs · 29,265 cycles

RIGHT WING TE OTBD OF NR 2 PYLON AFT FAIRING, LOWER SEAL RETAINER ANGLE CRACKED AT NUTPLATE. R & R ANGLE IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 50,310 hrs · 29,265 cycles

CENTER WING SECTION LOWER BULKHEAD ATTACH ANGLE CRACKED AT BS 661, RBL 8. REPAIRED ANGLE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,310 hrs · 29,265 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5, OTBD FWD & AFT HOLES. REPAIRED SEAT TRACK IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,310 hrs · 29,265 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 101.9, 10 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,310 hrs · 29,265 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75, INBD AFT HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,310 hrs · 29,265 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75, OTBD FWD & AFT HOLES. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,310 hrs · 29,265 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.5, OTBD FWD HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,310 hrs · 29,265 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75 OTBD FWD HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,310 hrs · 29,265 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.5, INBD FWD & AFT HOLES. REPAIRED SEAT TRACK IAW EA.

Part: WINDOW — CRACKED (COCKPIT) · airframe 50,310 hrs · 29,265 cycles

RIGHT NR 3 FLIGHT DECK WINDOW INBD CRACKED COMING FROM THE 2ND FROM BOTTOM FASTENER HOLE. REPAIRED WINDOW IAW ACO.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,310 hrs · 29,265 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 129.5, 26 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,310 hrs · 29,265 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5, INBD FWD & AFT HOLES. REPAIRED SEAT TRACK IAW SRM.

Part: LENS — UNSECURE (CABIN) · airframe 49,505 hrs · 28,797 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. REPAIRED LENS IAW EA.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 49,347 hrs · 28,704 cycles

AIR TURN BACK NR 2 ENG WOULD ONLY PRODUCE 58% THRUST AFTER ROTATION. ALL OTHER INDICATIONS NORMAL. R & R NR 2 EEC IAW MM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 48,352 hrs · 28,092 cycles

R1 & R2 VAPOR BARRIER BAYS CRACKED VERTICAL FROM THE LOWER OTBD SECTION UP TO THE UPPER INBD SECTION. REPAIRED CRACK IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 47,001 hrs · 27,288 cycles

CAPTAIN'S SIDE L1 WINDOW C/D POST CRACKED AT UPPER CORNER ALL THE WAY ACROSS THE POST. REPAIRED POST IAW EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 47,001 hrs · 27,288 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 45,835 hrs · 26,565 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT LENS PER AMM.

Part: POWERPACK — INOPERATIVE (CABIN) · airframe 45,835 hrs · 26,565 cycles

RIGHT OUTSIDE OVERWING EMERGENGY LIGHT INOP. REMOVED AND REPLACED RIGHT OUTSIDE OVERWING EMERGENGY LIGHT POWER PACK M1669 PER AMM.

Part: SLAT — CRACKED (RT WING) · airframe 44,835 hrs · 25,938 cycles

RIGHT WING NR 7 SLAT CRACKED. REMOVED AND REPLACED NR 7 SLAT PER AMM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,438 hrs · 25,058 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147.9. REPAIRED SKIN IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 43,438 hrs · 25,058 cycles

LEFT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STA 92.7. REMOVED AND REPLACED RIB IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,438 hrs · 25,058 cycles

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

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 43,438 hrs · 25,058 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STA 92.7. REMOVED AND REPLACED RIB IAW SRM.

Part: HOLDER — BROKEN (CABIN) · airframe 43,438 hrs · 25,058 cycles

FWD BATTERY CHARGER HOLD DOWN BROKEN. REMOVED AND REPLACED BATTERY IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 25,058 cycles

FRAME CRACKED AT BS 440, BETWEEN STR 8L AND STR 9L. REPAIRED FRAME PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,438 hrs · 25,058 cycles

BULKHEAD CRACKED AT BS 663, LBL42. REPAIRED BULKHEAD IAW ATS ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 25,058 cycles

FRAME CRACKED AT BS 747 , BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 25,058 cycles

FRAME CRACKED AT BS 480, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,438 hrs · 25,058 cycles

BULKHEAD CRACKED AT BS 663, RBL 35. REPAIRED BULKHEAD IAW ATS ER AND EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 25,058 cycles

FRAME CRACKED AT BS 400, BETWEEN STR 8L AND STR 9L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 25,058 cycles

FRAME CRACKED AT BS 440, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,438 hrs · 25,058 cycles

BULKHEAD CRACKED AT BS 663, RBL 28. REPAIRED BULKHEAD IAW ATS ER AND EA / RBL 35.

Part: STRAP — CORRODED (FUSELAGE) · airframe 43,438 hrs · 25,058 cycles

FLOOR SPLICE STRAP CORRODED AT BS 767+6, LBL 3. REMOVED AND REPLACED STRAP IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,438 hrs · 25,058 cycles

FLOOR SUPPORT CORRODED AT BS 767+6, LBL 8. REPAIRED SUPPORT IAW SRM & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 43,438 hrs · 25,058 cycles

AFT CARGO DOOR CUTOUT SUB THRESHOLD WEB CORRODED. REMOVED AND REPLACED WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,438 hrs · 25,058 cycles

FLOORBEAM CORRODED AT BS 986.5, WL 208. REPAIRED BEAM IAW ER AND EA.

Part: RIB — CRACKED (RT WING) · airframe 43,438 hrs · 25,058 cycles

RIGHT WING UPPER T/E SUPPORT RIB CRACKED. REMOVED AND REPLACED RIB IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 43,438 hrs · 25,058 cycles

LEFT WING O/B AFT FLAP DELAMINATED AT I/B TRAILING EDGE. REPAIRED AFT FLAP IAW SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 42,525 hrs · 24,547 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: BRACKET — LOOSE (GIRT ABR) · airframe 42,052 hrs · 24,244 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT STRAP BRACKETS LOOSE. REMOVED AND REPLACED BRACKET PER SRM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 42,052 hrs · 24,244 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT STRAP BRACKETS LOOSE. REMOVED AND REPLACED BRACKET PER SRM.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 40,498 hrs · 23,332 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS FADED BETWEEN ROW 19 TO ROW 22. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 40,272 hrs · 23,204 cycles

FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: VALVE — FAULTY (AC BAY) · airframe 38,301 hrs · 22,036 cycles

DECLARED EMERGENCY/DIVERSION. PASSENGER O2 MASKS AUTO DEPLOYED DUE TO DEPRESSURIZATION EVENT. FOUND 350 VALVE INOP. REMOVED AND REPLACED VALVE PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,745 hrs · 21,111 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR ANGLE CORRODED AT BS 270, BETWEEN LBL 11 TO RBL 11. REPAIRED ANGLE PER AAR EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 36,745 hrs · 21,111 cycles

DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR ANGLE CORRODED BETWEEN BS 265 TO BS 270, BETWEEN LBL 4 TO RBL 4. REPAIRED ANGLE PER AAR EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 36,745 hrs · 21,111 cycles

DURING SCHEDULED 10Y CHECK, FOUND EEPLS DAMAGED. REMOVED AND REPLACED EEPLS PER MM.

Part: FLAP — PUNCTURED (LT WING) · airframe 36,016 hrs · 20,673 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING I/B AFT FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 36,016 hrs · 20,673 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 36,016 hrs · 20,673 cycles

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

Part: FLAP — PUNCTURED (RT WING) · airframe 36,016 hrs · 20,673 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B AFT FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,625 hrs · 20,423 cycles

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

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,625 hrs · 20,423 cycles

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

Part: ENGINE — FIRE (NR 2) · airframe 32,371 hrs · 18,468 cycles

AIR TURNBACK / INFLIGHT SHUTDOWN / DECLARED EMERGENCY. AT APPROX 200 FT, AFTER RAISING GEAR HANDLE HEARD LOUD NOISE WITH VIBRATION. TOWER REPORTED FLAMES COMING OUT OF NR 2 ENG, SHUT ENG DOWN LANDED HEAVY WEIGHT (146,000). REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 30,968 hrs · 17,637 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 30,629 hrs · 17,424 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,280 hrs · 17,197 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 36. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 30,280 hrs · 17,197 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER TEE CAP CORRODED AT BS 328, RBL 20. REPAIRED TEE CAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,280 hrs · 17,197 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOOR BEAM CORRODED AT BS 986.5, RBL 14.5. REPAIRED FLOOR BEAM PER SRM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 28,194 hrs · 15,929 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,869 hrs · 14,604 cycles

DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,403 hrs · 14,341 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIDE LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT BALLAST PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 24,595 hrs · 13,893 cycles

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

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 24,595 hrs · 13,893 cycles

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

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 24,595 hrs · 13,893 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,020 hrs · 13,568 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 22,034 hrs · 12,443 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING T/E OUTBOARD FLAP DELAMINATED. REMOVED AND REPLACED LT T/E FLAP PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 20,307 hrs · 11,454 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,597 hrs · 10,516 cycles

DURING SCHEDULED RON CHECK, FOUND BATTERY PACK INOP FOR FWD RT SIDE BULLNOSE LIGHTS & R1 DOOR EVAC SLIDE LIGHTS. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,151 hrs · 9,681 cycles

DURING SPV, FOUND EMERGENCY EXIT LIGHT ABOVE ROWS 18 AND 19 INOP. RELAMPED PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 16,442 hrs · 9,265 cycles

LEFT FWD EMERGENCY EXIT LIGHT MISSING LENS. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 14,676 hrs · 8,337 cycles

L2 DOOR EMERGENCY EXIT OVERHEAD LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 13,728 hrs · 7,834 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SLIDE — LOOSE (R1/L2 DOORS) · airframe 12,426 hrs · 7,122 cycles

DURING SCHEDULED C3 CHECK, FOUND BOTH R1 AND L2 DOOR EVACUATION SLIDES OUT OF ADJUST. REINSTALLED SLIDES PER MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 11,255 hrs · 6,453 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVER BROKEN AT ROW NR 1. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 11,171 hrs · 6,401 cycles

EEPLS COVER LOOSE. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: COLLAR — WORN (NLG) · airframe 8,292 hrs · 4,807 cycles

AFTER PUSHBACK RUDDER PEDAL MOVEMENT CAUSED A BANG/THUMP IN THE NOSE WHEEL AREA. REMOVED AND REPLACED NLG STEERING COLLAR AND LOWER PLATE PER MM.

Part: COVER — MISSING (CABIN) · airframe 7,900 hrs · 4,593 cycles

EEPLS COVER MISSING AT ROW NR 14. INSTALLED COVER PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 7,744 hrs · 4,504 cycles

DURING SCHEDULED C3 CHECK, FOUND RT ELEVATOR TAB NR 4 HINGE WORN. REMOVED AND REPLACED NR 4 HINGE HARDWARE AND BUSHING PER MM.

Part: COVER — MISSING (CABIN) · airframe 7,358 hrs · 4,289 cycles

DURING SCHEDULED PM CHECK, FOUND EEPLS TRACK COVERS CRACKED AND MISSING AT ROW NR 3 AND AT BOTH ENDS. INSTALLED COVERS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 971 hrs · 563 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVER CRACKED. REMOVED AND REPLACED TRACK COVER PER MM.

Part: BULB — FAILED (FUEL PANEL.) · airframe 225 hrs · 148 cycles

ELECTRICAL SMELL IN CABIN, FUELING CONTROL C/B TRIPPED. DEFERRED PER MEL. LATER AT MDW RELAMPED BOTH FUELING PANEL LIGHTS AND TIGHTENED LIGHT ASSY BACK SHELL PER MM.