N411WN

Part: HANDLE — DID NOT STOW (ZONE 800) · airframe 76,101 hrs · 45,420 cycles

FWD CARGO DOOR HANDLE DIFFICULT TO OPERATE<[01] R/R FWD CARGO DOOR EXTERIOR HANDLE PER AMM 52-31-14

Part: COVER — UNSECURE (ZONE 200) · airframe 75,947 hrs · 45,328 cycles

OVERWING EXIT CA SIDE; COVER NEEDS SECURING<[01] RESECURED OVERWING CAP. SIDE EXIT DOOR PER SIP.

Part: LIGHT — BROKEN (ZONE 200) · airframe 75,895 hrs · 45,296 cycles

L1 FWD ENTRY DOOR EXIT LT COVER BROKEN OFF<[01] R&R L1 DOOR LOWER EMERGENCY EXIT LT ASSY PER AMM 33-51-01

Part: SENSOR — SPLIT (ZONE 500) · airframe 75,684 hrs · 45,162 cycles

SPLIT FLAP LANDING; FLAPS ON LEFT SIDE 1.5 / RIGHT SIDE 2<[01] REMOVED AND REPLACED #6 T/E FLAP SKEW SENSOR PER AMM 27-59-01.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 73,971 hrs · 44,150 cycles

FWD SERVICE DOOR LOWER EXIT SIGN COVER OFF<[01] COMPLETED M-21-133-00720<BR><BR>LENS IS TAPED UP WITH CLEAR TAPE IAW M-21-133-00720

Part: GIRT BAR — LOOSE (ZN 800 DOOR) · airframe 73,616 hrs · 43,933 cycles

FORWARD SERVICE DOOR GIRT BAR HOLDER LOOSE.<[01] SECURED FWD SVC DOOR'S GIRT BAR HANGER PER SIP.

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 73,558 hrs · 43,898 cycles

FWD ENTRY GIRT BAR LOOSE<[01] INSPECTED FWD ENTRY GIRL BAR PER AMM 25-66-01. NO DEFECTS NOTED

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 72,372 hrs · 43,147 cycles

OVER WING EXIT LOWER EMERGENCY LIGHTS INOP<[01] RELAMPED RIGHT SIDE OVERWING DOOR INDICATOR LIGHT ASSEMBLY AND TESTED PER AMM 33-51-01-960-801. NO DEFECTS NOTED.;[02] VERIFIED CORRECTIVE ACTION #1

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 72,372 hrs · 43,147 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED<[01] WELDED CRACKED RADIUS OF AFT CARGO BAY; FWD CORNER SCUFF PLATE USING ER4043 ALUMINUM FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2) AND (4). REPAIR REQUIRES DYE PENETRANT INSPECTION.<BR>EQUIP USED: WELDING MACHINE E10583 CAL DUE DATE 01/2024;[02] VERIFIED CORRECTIVE ACTION 1;[03] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-RADIOMETER ID: ATS2561-1; 2; 3 CAL DUE: 08/23;[04] SANDED REPAIR WELD AREA PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(5);[05] VERIFIED CORRECTIVE ACTION 4;[06] OK TO INSTAL FWD CORNER SCUFF PLATE GIVEN;[07] SCUFF PLATE INSTALLED <BR>REFERENCE ATTACHMENT FOR WORK ACCOMPLISHED<BR>LEAK CHECK TO BE COMPLETED ON TTG8Q00M713S;[08] VERIFIED CORRECTIVE ACTION #7

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 72,372 hrs · 43,147 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED<[01] WELDED CRACKED RADIUS OF AFT CARGO BAY; AFT CORNER SCUFF PLATE USING ER4043 ALUMINUM FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2) AND (4). REPAIR REQUIRES DYE PENETRANT INSPECTION.<BR>EQUIP USED: WELDING MACHINE E10583 CAL DUE DATE 01/2024;[02] VERIFIED CORRECTIVE ACTION 1;[03] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-RADIOMETER ID: ATS2561-1; 2; 3 CAL DUE: 08/23;[04] SANDED REPAIR WELD AREA PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(5);[05] VERIFIED CORRECTIVE ACTION 4;[06] OK TO INSTALL AFT CORNER SCUFF PLATE GIVEN.;[07] SCUFF PLATE INSTALLED <BR>REFERENCE ATTACHMENT FOR WORK ACCOMPLISHED<BR>LEAK CHECK TO BE COMPLETED ON TTG8Q00M713S;[08] VERIFIED CORRECTIVE ACTION #7 AND MEASUREMENT TABLE

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 72,372 hrs · 43,147 cycles

FWD CARGO BAY - CRACK ON STRINGER 24L BS 540 (MARKED)<[01] VERIFIED APPLICABILITY IAW SRM 53-30-03-01-1 AND SRM 53-00-03-1A-1;[02] THERE IS NO ALLOWABLE DAMAGE FOR FCB STRINGER CRACK AT BS 540 24L IAW SRM 53-00-03-1A-1. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 53-00-03-2R-1;[03] REMOVED FWD WTB FAIRING PNL 191CL IAW AMM 53-51-21-000-803;[04] VERIFIED CORRECTIVE ACTIONS 1 AND 2.;[05] VERIFIED APPLICABILITY FOR STR 24L/H IAW SRM 53-00-03-2R-1 PAR 4. FIG 205;[06] CUTOUT AND REMOVED DAMAGE STRINGER SECTION BETWEEN BS 500D+12' TO BS 539 ON STR 24L IAW SRM 53-00-03-2R-1 PAR 4;STEPS A-B.LOCATED AND DRILLED NEW STRINGER SECTION AT FCB STR 24L/H BETWEEN BS 500D+12' TO BS 539 AND HAT SECTION BETWEEN BS 500D+5' TO BS 500D+19' AND APPLIED CHEMICAL CONVERSION COATING ON REPAIR PARTS IAW SRM 53-00-03-2R-1 PAR 4;STEPS D - I; FIG 205; ;APPLIED PRIME ON REPAIR PARTS IAW SOPM 20-41-02. REQUEST OK TO INSTALL REPAIR PARTS.;[17] VERIFIED APPLICATION OF PRIME ON REPAIR PARTS; ONLY.;[18] REQUEST OKAY TO INSTALL STRINGER REPAIR.;COMPLETED INSTALLATION OF REPAIR PARTS IAW SRM 53-00-03-2R-1; PARA 4K-L <BR>PARTIAL ON STEP 2; 3; 4;REJECTED STEP 3 OK TO INSTALL LANDING LIGHT DUE TO FOD AND CREATED STEP 5.;[24] COMPLETED STEP 5;[25] REQUEST OK TO INSTALL L/H RETRACTABLE LANDING LIGHT.;[26] INSTALLED L/H RETRACTABLE LANDING LIGHT PER AMM 33-42-02-960-802 INSTALLED PNL 191CL.; L/H RETRACTABLE LANDING LIGHT OPS CHECKED GOOD PER AMM 33-42-02-960-802.;[35] VERIFIED CORRECTIVE ACTION 34

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 72,372 hrs · 43,147 cycles

WING CENTER SECTION BREAK PANEL IS CRACKED IN RADIUS NEAR FASTENER BS 540; RBL 1; WL 207<[01] UPDATED PARTS AND MEASUREMENT TABLE;[02] COMPLETED STEP 1;[03] COMPLETED STEP 1 AND VERIFIED MEASURMENT TABLE;[04] REMOVED FLOOR PANEL COMMON TO WING CENTER SECTION BREAK PANEL IAW AMM 53-21-00-000-801; REMOVED AND REPLACED WING CENTER SECTION BREAK PANEL BS 540 RBL 1 PER AMM 51-40-02-0G-0; DWG 143A060 REV B AND REINSTALLED FLOOR PANEL IAW AMM 53-21-00-000-801;[05] VERIFIED CORRECTIVE ACTION #4;[06] CARD COMPLETE.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 72,372 hrs · 43,147 cycles

FWD CARGO BAY - CRACK ON STRINGER 23L BS 540 (MARKED)<[01] EVALUATED CRACK AT FCB STRINGER 23L/H BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL A;[02] VERIFIED APPLICABILITY FOR STR 23L/H IAW SRM 53-00-03-2R-1 PAR 4; FIG 205.;[03] CUTOUT AND REMOVED DAMAGE STRINGER SECTION BETWEEN BS 500D+12' TO BS 539 IAW SRM 53-00-03-2R-1 PAR 4; STEPS A-B.;[04] UPDATE STEP 1.;[05] VERIFIED CORRECTIVE ACTION #'S 1 AND 3;[06] VERIFIED CORRECTIVE ACTION #2;[07] UPDATE STEP 2.;[08] PERFORM HFEC INSPECTION TO DAMAGE CUTOUT ON STRINGER SECTION AND ALL OPEN HOES COMMON TO REPAIR AREA;[09] RECEIVED NEW STRINGER SECTION P/N:HFAB53-SN-011;LOT:1534490-3;PO/N:929434/3 AND HAT SECTION P/N:HFAB53-HS-011;LOT:1534422-1;PO/N:929434/1.;[10] LOCATED AND DRILLED NEW STRINGER SECTION AT FCB STR 23L/H BETWEEN BS 500D+12' TO BS 539 AND HAT SECTION BETWEEN BS 500D+6' T0 BS 500D+18' AND APPLIED CHEMICAL CONVERSION COATING ON REPAIR PARTS IAW SRM 53-00-03-2R-1; PAR 4; FIG 205.APPLIED PRIME ON REPAIR PARTS IAW SOPM 20-41-02 REQUEST OK TO INSTALL REPAIR PARTS.;[15] VERIFIED CORRECTIVE ACTION #14; OK TO INSTALL REPAIR PARTS;[16] INSTALLED REPAIR PARTS AT FCB STR 23L/H STRINGER SECTION BETWEEN BS 500D+12' TO BS 539 AND HAT SECTION BETWEEN BS 500D+6' T0 BS 500D+18' IAW SRM 53-00-03-2R-1; PAR 4; FIG 205;

Part: WEB — CRACKED (ZN 600 RIGHT WIN) · airframe 72,372 hrs · 43,147 cycles

RT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE CRACKED; AFT OF PYLON STRUT; MARKED<[01] REMOVED AND REPLACED RT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE IAW SRM 51-40-02;[02] REJECTION: UPPER ATTACH BOLTS ARE LOOSE; SEE STEP 1;[03] COMPLETED STEP 1;[04] VERIFIED STEP 1 COMPLETED. TASK COMPLETE

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 72,372 hrs · 43,147 cycles

LT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE CRACKED; AFT OF PYLON STRUT; MARKED<[01] REMOVED AND REPLACED LT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE IAW SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION 1

Part: WEB — CRACKED (ZN 500 LEFT WING) · airframe 72,372 hrs · 43,147 cycles

LT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE CRACKED; AFT OF PYLON STRUT; MARKED<[01] REMOVED AND REPLACED LT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE IAW SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION 1

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 72,372 hrs · 43,147 cycles

RT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE CRACKED; AFT OF PYLON STRUT; MARKED<[01] REMOVED AND REPLACED RT WING TE TRANSITION WEB; AFT LOWER BULB SEAL ANGLE IAW SRM 51-40-02;[02] REJECTION: UPPER ATTACH BOLTS ARE LOOSE; SEE STEP 1;[03] COMPLETED STEP 1;[04] VERIFIED STEP 1 COMPLETED. TASK COMPLETE

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 72,372 hrs · 43,147 cycles

FWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED<[01] WELDED CRACKED RADIUS ON FWD CARGO BAY; FWD CORNER SCUFF PLATE USING ER4043 ALUMINUM FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARAGRAPH 4.B. (2) AND (4). REPAIR STILL REQUIRES A DYE PENETRANT INSPECTION.<BR>EQUIP USED: WELDING MACHINE E10583; CAL DUE DATE 01/24;[02] VERIFIED CORRECTIVE ACTION 1.;[03] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-RADIOMETER ID: ATS2561-1; 2; 3 CAL DUE: 08/23;[04] SANDED REPAIR AREA PER SRM 53-30-15-2R-1 PARAGRAPH 4.B. (5);[05] VERIFIED CORRECTIVE ACTION 4 AND MEASUREMENT TABLE.;[06] TREATED AND PRIMED FCB FWD SCUFF PLATE IAW AMM 51-21-41-370-802 AND AMM 51-21-72-370-804<BR><BR>PART WILL BE INSTALLED IN CUSTOMER CARD # TTG8Q00M713M;[07] VERIFIED ACTION 6

Part: SKIN — CRACKED (LT WING SLAT) · airframe 72,372 hrs · 43,147 cycles

CRACK AROUND THE FASTENER AT NO.1 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. MARKED<[01] REMOVED COVE PANELS 525DAB; 525DBB; 525CB IAW SOPM 20-50-01.;[02] REMOVED COVE PANEL 525EB IAW SOPM 20-50-01.;[03] REMOVED SLAT FLEX SKIN IAW SRM 57-42001-2R-8 PARA. 4.;[04] REMOVED INITIAL FASTENERS AS REQUIRED IN REPAIR AREA AND CUT AND REMOVED DAMAGED PART OF SLAT NOSE SKIN IAW SRM 57-42-01-2R-8 PARA. 4.;[05] VERIFIED CORRECTIVE ACTION STEP 4.;[06] VALIDATED APPLICABILITY OF SRM 57-42-01-2R-8.;[07] VERIFIED CORRECTIVE ACTION STEP 6.;[08] FABRICATED REPAIR DOUBLER (1) FROM 7075T6 0.071' CLAD ; LOT # 1497836-1. REPAIR FILLER (2) FROM 7075T6 0.063' CLAD; LOT# 1533932-1. INSTALLED COUNTERSINK REPAIR WASHERS AS REQUIRED IN SLAT NOSE SKIN. APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO REPAIR PARTS AND BARE AREA OF REPAIR AREA ON SLAT NOSE SKIN IAW SRM 57-42-01 2R-8 PARA. 4.F. OK TO INSTALL.

Part: COFFEEMAKER — FAULTY (ZN 200 FUS TOP) · airframe 71,332 hrs · 42,438 cycles

ACRID ODOR AFT SERVICE DOOR AREA; SEEMS TO BE COFFEE MAKER; DISSIPATES WHEN OFF<[01] ACCOMPLISHED CONDITIONAL INSPECTION PER AMM 05-51-56; FOUND SOURCE OF ELECTRICAL SMELL TO BE COMING FROM AFT COFFEE MAKERS. PLACING BOTH AFT COFFEE MAKERS ON MEL. OK TO CONTINUE PER MEL 25-10-01; SP1B AND SP2 COMPLIED WITH.;[02] REPLACED BOTH AFT COFFEE MAKERS IAW AMM 25-30-01. OPS CHECK GOOD.

Part: SIGN — DETACHED (CABIN) · airframe 70,560 hrs · 41,933 cycles

FO SIDE LOWER OVER WING EXIT SIGN FELL OFF / [01] SECURED EXIT SIGN LENS PER AMM 33-51-03

Part: RETAINER — LOOSE (R2 DOOR) · airframe 69,504 hrs · 41,214 cycles

AFT SLIDE F/O SIDE IS NOT SECURE IN CONTAINER. / [01] FOUND AFT SERVICE DOOR (R2) AFT GIRTH BAR RETAINER TO BE LOOSE; ADJUSTED AFT SERVICE DOOR (R2) AFT GIRTH BAR RETAINER PER S.I.P.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 69,479 hrs · 41,199 cycles

AFT F/A COMPLAINED BOTH AFT SLIDES ARE FALLING OUT OF CASES / [01] INSPECTED BOTH SLIDES NO DEFECTS NOTED IAW M/M 25-66-01

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 69,479 hrs · 41,199 cycles

AFT F/A COMPLAINED BOTH AFT SLIDES ARE FALLING OUT OF CASES / [01] INSPECTED BOTH SLIDES NO DEFECTS NOTED IAW M/M 25-66-01

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 68,316 hrs · 40,447 cycles

L1 DOOR SLIDE Z FOLD IN CORRECT NEEDS REPOSITION L1 DOOR SLIDE FOLD IN CORRECT NEEDS REPOSITION / [01] CORRECTED ?Z? FOLD IAW AMM25-66-01 AND MT 725-61-06;[02] VERIFIED C/W PER AMM 25-66-01 & MT 725-61-01;[03] C/W

Part: HANDLE — BROKEN (FWD ENTRY DOOR) · airframe 68,088 hrs · 40,300 cycles

FOWARD ENTRY DOOR LOWER HANDLE BROKE ; / [01] INSTALLED NEW ASSIST HANDLE PER A.M.M. 52-11-34

Part: BRACKET — BROKEN (LT WING) · airframe 67,597 hrs · 40,030 cycles

LEFT WING DEFLECTION RIB OUTBRD SUPPORT BRACKET BROKE ; / [01] REMOVE DAMAGE PER SRM 57-51-02-2R-1.; [02] REMOVE THE LEFT WING DEFLECTION RIB PANEL OUTBOARD SEAL SUPPORT BRACKET WITH 11 SCREWS PER SRM 51-40-02.; [03] C/W DAMAGE REMOVAL INSP AND PERFORMED H.F.E.C. INSP PER NDT MANUAL PART 6 51-00-00 PROCEDURE 23. NO DEFECTS NOTED.; [04] FLAPPED PEEN THE REWORKED AREAS OF THE DEFLECTION CONTROL RIB IAW. SOPM 20-10-03.; [05] LOCATED AND DRILLED THE DEFLECTION RIB FOR REPAIR FITTING PER SRM 57-51-02-2R-3; [06] INSTALLED RIB PANEL OUTBOARD SEAL SUPPORT BRACKET PER SRM 51-40-02; [07] REPAIRED PER SRM 57-51-02-2R-3; [08] C/W INSPECTION

Part: GAUGE — DAMAGED (R1 DOOR SLIDE) · airframe 66,859 hrs · 39,576 cycles

FOUND FWD SERVICE DOOR SLIDE FOAM MISSING FROM PRESSURE GAUGE ; / [01] REMOVED FWD SERVICE DOOR SLIDE AND INSTALLED FOAM AND REINSTALLED ORIGINAL SLIDE REF TC 725-61-06-FS AND S.I.P

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 66,799 hrs · 39,541 cycles

FWD SVC DOOR EMER. SLIDE NEEDS ADJ. ; / [01] ADJUSTED FWD GALLEY SERVICE DOOR SLIDE PER MM 25-666-00

Part: LIGHT — FAULTED (EXTERIOR) · airframe 66,574 hrs · 39,412 cycles

EMERGENCY LIGHT RH ABOVE FWD CARGO DOOR INOP ; 2021-311869 / [01] PERFORMED VISUAL INSPECTION OF THE LIGHT ABOVE FWD CARGO DOOR AND THE LIGHT IN THIS LOCATION IS THE WING ILLUMINATION LIGHT; NOT THE EMERGENCY LIGHT; AND PERFORMED OPERATIONAL TEST OF THE WING ILLUMINATION LIGHT AS PER B737-700 AMM 33-41-00-710-801 TEST IS OK; WING ILLUMINATION LIGHT IS OPERATIVE.; [02] TASK COMPLETE<BR>WING ILLUMINATION LIGHT IS OPERATIVE

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 66,574 hrs · 39,412 cycles

DELAMINATED FLOOR PANEL 222BF AT FWD GALLEY AREA ; 2021-311838 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] REPAIRED FLOOR PANEL 222BF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [03] REPAIRED FLOOR PANEL 222BF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 66,574 hrs · 39,412 cycles

DELAMINATED FLOOR PANEL 221BF AT FWD GALLEY AREA ; 2021-311840 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] TOOL USED HOT BONDER P/N:HCS9000B S/N:15092096 DUE DATE:14/DEC/21.; [03] TOOL USED SCALE P/N CL5000 S/N AE-408752 DUE DATE 19/MAR/22.; [04] REPAIRED FLOOR PANEL 221BF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [05] REPAIRED FLOOR PANEL 221BF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 66,574 hrs · 39,412 cycles

DELAMINATED FLOOR PANEL 242WF AT AFT GALLEY AREA ; 2021-311841 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] TOOL USED SCALE P/N SCA-301 S/N AE-412122 DUE DATE 24/FEB/22.; [03] REPAIRED FLOOR PANEL 242WF AT AFT GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [04] REPAIRED FLOOR PANEL 242WF AT AFT GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 66,574 hrs · 39,412 cycles

DELAMINATED FLOOR PANEL 221GF AT FWD GALLEY AREA ; 2021-311842 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/2; [02] TOOL USED HOT BONDER P/N:HCS9200B S/N:18165044 DUE DATE:15-FEB-22; [03] TOOL USED SCALE P/N CL5000 S/N AE-408752 DUE DATE 19/MAR/22.; [04] REPAIRED FLOOR PANEL 221GF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [05] REPAIRED FLOOR PANEL 221GF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 66,574 hrs · 39,412 cycles

DELAMINATED FLOOR PANEL 231AF AT FWD GALLEY AREA ; 2021-311844 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] TOOL USED: SCALE P/N:SCA-301 S/N:AE-412137 DUE DATE:24-FEB-22; [03] REPAIRED FLOOR PANEL 231AF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [04] REPAIRED FLOOR PANEL 231AF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 66,574 hrs · 39,412 cycles

DELAMINATED FLOOR PANEL 232AF AT FWD GALLEY AREA ; 2021-311843 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] REPAIRED FLOOR PANEL 232AF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [03] REPAIRED FLOOR PANEL 232AF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 66,574 hrs · 39,412 cycles

DELAMINATED FLOOR PANEL 241ZF AT AFT GALLEY AREA ; 2021-311839 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] REPAIRED FLOOR PANEL 241ZF AT AFT GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [03] REPAIRED FLOOR PANEL 241ZF AT AFT GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 66,574 hrs · 39,412 cycles

DELAMINATED FLOOR PANEL 222AF AT FWD GALLEY AREA ; 2021-311837 / [01] TOOL USED HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 15/FEB/22.; [02] TOOL USED SCALE P/N SCA-301 S/N AE-412122 DUE DATE 24/FEB/22.; [03] REPAIRED FLOOR PANEL 222AF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [04] REPAIRED FLOOR PANEL 222AF AT FWD GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,574 hrs · 39,412 cycles

DONT WORK CORRECTLY LOWER SIDEWALL BATTERY PACK ON EMERGENCY EXIT DOOR AT PASSENGER CABIN (1 EA) ; 2021-311822 / [01] REPLACED LOWER SIDEWALL BATTERY PACK ON EMERGENCY EXIT DOOR AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-06-960-805.; [02] REPLACED LOWER SIDEWALL BATTERY PACK ON EMERGENCY EXIT DOOR AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-06-960-805. COMPLETED

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY & LAV) · airframe 66,574 hrs · 39,412 cycles

DELAMINATED FLOOR PANEL 241ADF AT AFT GALLEY AND LAV ; 2021-311814 / [01] TOOL USED: HOT BONDER P/N:HCS9200B S/N:15102320 DUE DATE:19-NOV-21; SCALE P/N:SCA-301 S/N:AE-412137 DUE DATE:24-FEB-22; [02] TOOL USED: SCALE P/N:SCA-301 S/N:AE-412125 DUE DATE: 24-FEB-22; [03] REPAIRED FLOOR PANEL 241ADF AT AFT GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1 TOOL USED CALIPER P/N: 500-197-20 S/N: 13083235 DUE DATE: 18-AUG-21. SCALE P/N: SCA-301; S/N: AE-412133; DUE DATE: 24/FEB/22.; [04] REPAIRED FLOOR PANEL 241ADF AT AFT GALLEY AREA AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1 TOOL USED CALIPER P/N: 500-197-20 S/N: 13083235 DUE DATE: 18-AUG-21. SCALE P/N: SCA-301; S/N: AE-412133; DUE DATE: 24/FEB/22.

Part: FLOOR PANEL — DELAMINATED (E/E BAY) · airframe 66,572 hrs · 39,411 cycles

DELAMINATED FLOOR PANEL J23 PANEL ASSY P/N: 284A6223-1 AT EQUIPMENT EL ECTRONIC COMP ; 2021-311795 / [01] TOOL USED: CALIPER PN: 500-464; SN: B17030925. DUE DATE: 06/AUG/21.; [02] TOOL USED: HOT BONDER P/N: HCS9200B SN: 18165044 DUE DATE: 15/FEB/22.; [03] TOOL USED: SCALE PN: SCA-301 SN: AE-412137 DUE DATE: 24/FEB/22.; [04] REPAIRED FLOOR PANEL J23 PANEL ASSY P/N: 284A6223-1 AT EQUIPMENT ELECTRONIC COMPARTMENT AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [05] REPAIRED FLOOR PANEL J23 PANEL ASSY P/N: 284A6223-1 AT EQUIPMENT ELECTRONIC COMPARTMENT AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.COMPLETED

Part: FLOORBEAM — ELONGATED (BS 294) · airframe 66,572 hrs · 39,411 cycles

ELONGATED HOLE BS 294.5 ANGLE - SUPPORT BTW RBL 45 TO RBL 55; FLOOR STRUCTURE AREA AT FWD GALLEY AREA ; 2021-311792 / [01] TOOLS USED: POWER PACK P/N: PE1068; S/N: PE0118-94826; DUE DATE: 23-FEB-22; MULTIMETER P/N: 2217-20; S/N: B83B914290479; DUE DATE: 14-APR-22; THERMOMETER P/N:FLUKE63; S/N: 31330088; DUE DATE: 18-MAY-22.; [02] REPLACED ANGLE SUPPORT LOC. AT FLOOR BEAM 294.5 BTW RBL 45 TO RBL 55; FLOOR STRUCTURE AREA AT FWD GALLEY I.A.W SRM B737-700 51-40-02; 51-10-02 AND DRAWINGS 141A5400 REV -;141A5502 REV C; [03] REPLACED ANGLE SUPPORT LOC. AT FLOOR BEAM 294.5 BTW RBL 45 TO RBL 55; FLOOR STRUCTURE AREA AT FWD GALLEY I.A.W SRM B737-700 51-40-02; 51-10-02 AND DRAWINGS 141A5400 REV -;141A5502 REV C. COMPLETED RII

Part: FITTING — CRACKED (R1 DOOR) · airframe 66,572 hrs · 39,411 cycles

CUSTOMER REQUEST CRACK LOWER FITTING FWD SERVICE DOOR AT FWD GALLEY AREA ; 2021-311773 / [01] REPLACED FITTING I.A.W SRM B737-700 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DWG # 141A6535 REV B; [02] REPLACED FITTING I.A.W SRM B737-700 51-40-02; SRM B737-700 51-10-02 ITEM 9 AND DWG # 141A6535 REV B.. RII ITEM

Part: STRAP — CRACKED (BS 420-440) · airframe 66,572 hrs · 39,411 cycles

CRACK STRAP LOCATED BS 420 TO BS 440 AND BETWEEN S-27R TO S-26L AT FWD CARGO COMPARTMENT ; 2021-311714 / [01] REPLACED STRAP LOCATED BS420 TO BS440 AND BETWEEN S-27R TO S-26L AT FDW CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 AND SRM 51-40-02.; [02] REPLACED STRAP LOCATED BS420 TO BS440 AND BETWEEN S-27R TO S-26L AT FDW CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 AND SRM 51-40-02. AS RII

Part: FLOORBEAM — CRACKED (BS 294) · airframe 66,572 hrs · 39,411 cycles

CRACK FLOOR BEAM BS 294.5 RBL 57 FWD GALLEY AND LAV ; 2021-311692 / [01] TOOL USED: P/N: NORTEC 600 D; S/N: 210136503; DUE DATE: 05-MAR-22.; [02] PERFORMED PERMANENT REPAIR ON FLOOR BEAM BS 294.5 RBL 57 FWD GALLEY AND LAVATORY AREA IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16 PARAGRAPH 4. FIG 202. AND B737-700 SRM 51-40-02 DWG 141A5400 REV. A.; [03] PERFORMED PERMANENT REPAIR ON FLOOR BEAM BS 294.5 RBL 57 FWD GALLEY AND LAVATORY AREA IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16 PARAGRAPH 4. FIG 202. AND B737-700 SRM 51-40-02 DWG 141A5400 REV. A. RII

Part: STRAP — CORRODED (BS 294-312) · airframe 66,572 hrs · 39,411 cycles

CORROSION INNER CHORD STRAP LOCATED BTW BS 294.5 TO BS 312 RBL 51 AND WL 208 AT FWD GALLEY AREA ; 2021-311693 / [01] REPLACED INNER CHORD STRAP LOCATED BS 294.5 TO BS 312 RBL 51 AND WL 208 AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 TEM 9 AND DRAWING 141A8310 REV:-; [02] REPLACED INNER CHORD STRAP LOCATED BS 294.5 TO BS 312 RBL 51 AND WL 208 AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 TEM 9 AND DRAWING 141A8310 REV:-<BR>RII

Part: SUPPORT ANGLE — CRACKED (BS 380-400 BL0) · airframe 66,572 hrs · 39,411 cycles

CRACK SUPPORT ANGLE LOCATED BETWEEN BS 400 AND BS 380 BL 0 AT PASSENGER CABIN ; 2021-311691 / [01] REPLACED SUPPORT ANGLE LOCATED BETWEEN BS 400 AND BS 380 BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0. PARAGRAPH 9. AND DWG 143A5400 REV -.; [02] REPLACED SUPPORT ANGLE LOCATED BETWEEN BS 400 AND BS 380 BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0. PARAGRAPH 9. AND DWG 143A5400 REV -.<BR>RII ACCOMPLISHED

Part: WEB — CRACKED (BS 312-320 LBL47) · airframe 66,572 hrs · 39,411 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 320 LBL47 FWD GALLEY AND LAV ; 2021-311689 / [01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND 320 LBL47 FWD GALLEY AND LAV. IAW SRM B737-700 51-10-02 AND DWG 141A5400 REV -; [02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND 320 LBL47 FWD GALLEY AND LAV. IAW SRM B737-700 51-10-02 AND DWG 141A5400 REV - RII

Part: WEB — CRACKED (BS 312-328) · airframe 66,572 hrs · 39,411 cycles

CRACK WEB LOCATED BTW BS 312 TO BS 328 RBL 29 AND WL 208 AT FWD GALLEY AREA ; 2021-311694 / [01] REPLACED WEB LOC. BTW BS 312 TO BS 328 RBL 29 AND WL 208 AT FWD GALLEY AREA IAW SRM B737-700 51-10-02 AND DWG 141A5400 REV -; [02] JOB COMPLETED;RII ACCOMPLISHED.

Part: SKIN — CRACKED (BS 685 S1-2R) · airframe 66,572 hrs · 39,411 cycles

CRACK INDICATION FOUND ON HOLE LOCATED ON BS 685-3 INCHES ON RH SIDE BETWEEN STR 1R TO STR 2R ON ADF ANTENNA MOUNTING BOLT ; 2021-311669 / [01] TOOL USED: P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 24-FEB-22; [02] TOOL USED: P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 24-FEB-22; [03] TOOL USED: DIGITAL CALIPER P/N: 700-113-10. S/N: 0010815. DUE DATE: 06 MAY 22.; [04] TOOL USED PN NORTEC 600D SN 60009161631 DUE DATE 01-DEC-21; [05] TOOL USED PN NORTEC 600D SN 60009161631 DUE DATE 01-DEC-21; [06] TOOL USED P/N: 45MG; S/N: 130060401; DUE DATE: 22-APR-22.; [07] REPAIRED FUSELAGE SKIN I.A.W EA 21-153-02075 WIP 1; WIP 2 AND EA COVER 21-153-02075; [08] TASK COMPLETED

Part: STRINGER — CRACKED (BS 727-727A S27L) · airframe 66,572 hrs · 39,411 cycles

CRACK STRINGER 27L KEEL BEAM LOCATED BTW BSTA 727 TO BSTA 727A AT AFT CARGO COMPARTMENT ; 2021-311663 / [01] TOOLL USED RADIUS GAUGE P/N: 2204A3 S/N: AE-408651 DUE DATE:02-FEB-22 DIGITAL CALIPER P/N:700-113-10 S/N:0023244 DUE DATE:28-SEP-22; [02] TOOL USED PN: NORTEC500D; SN: N500X12101V022235; DUE DATE: 03 JUN 21.; [03] TOOL USED PN: NORTEC500D; SN: N500X12101V022235; DUE DATE: 03 JUN 22.; [04] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22; [05] TOOLS USED: TEMPERATURE CONTROLLER P/N:P3015GOES00000; S/N:112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER P/N:P3015GOES00000; S/N:112820025; DUE DATE: 22-JAN-22;; [06] TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N: B20189521; DUE DATE: 22-NOV-21.; [07] PERFORMED PERMANENT REPAIR ON STRINGER 27L KEEL BEAM LOCATED BTW BSTA 727 TO BSTA 727A AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-60-12-2R-1 REPAIR 1 FIGURE 202. MATERIAL USED: ALUMINUM SHEET P/N 7075T0/0.125 PO: 2012-531798. HEAT TREATED TO T62. AND ALUMINUM BLOCK P/N 7150-T77511 PO: 2020-201542.; [08] PERFORMED PERMANENT REPAIR ON STRINGER 27L KEEL BEAM LOCATED BTW BSTA 727 TO BSTA 727A AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-60-12-2R-1 REPAIR 1 FIGURE 202. MATERIAL USED: ALUMINUM SHEET P/N 7075T0/0.125 PO: 2012-531798. HEAT TREATED TO T62. AND ALUMINUM BLOCK P/N 7150-T77511 PO: 2020-201542. RII ITEM

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 66,572 hrs · 39,411 cycles

CRACK GUSSET LOCATED BS500D AT LEVEL STR19R FWD CARGO COMPARTMENT (1 EA) ; 2021-311646 / [01] OK TO INSTALL GUSSET; [02] DRILLED NEW GUSSET AND APPLIED PROTECTIVE TREATMENT ON OPEN HOLE LOCATED BS 500D AT LEVEL STR 19R IAW B737-700 SRM 51-40-02 AND SRM 51-20-01; OK TO INSTALL NEW GUSSET LOCATED ON BS 500D AND S-19R GRANTED; [03] REPLACED GUSSET AND FASTENERS LOCATED BS500D AT LEVEL STR19R FWD CARGO COMPARTMENT (1 EA) IAW B737 700 SRM 51- 40-02. SRM 51-10-02 ITEM 9 AND DWG 143A7902. REV. A.; [04] REPLACED GUSSET AND FASTENERS LOCATED BS500D AT LEVEL STR19L FWD CARGO COMPARTMENT (1 EA) IAW B737 700 SRM 51- 40-02. SRM 51-10-02 ITEM 9 AND DWG 143A7902. REV. A.; [05] REPLACED GUSSET AND FASTENERS LOCATED BS500D AT LEVEL STR19R FWD CARGO COMPARTMENT (1 EA) IAW B737 700 SRM 51- 40-02. SRM 51-10-02 ITEM 9 AND DWG 143A7902. REV. A.; [06] THIS STEP WAS SIGN OFF WITH THE INCORRECT LABOR AND CREATE CORRECT LABOR FOR CORRECTIVE ACTION OF AMT; [07] REPLACED GUSSET AND FASTENERS LOCATED BS500D AT LEVEL STR19R FWD CARGO COMPARTMENT (1 EA) IAW B737 700 SRM 51- 40-02. SRM 51-10-02 ITEM 9 AND DWG 143A7902. REV. A.; [08] REPLACED GUSSET AND FASTENERS LOCATED BS500D AT LEVEL STR19R FWD CARGO COMPARTMENT (1 EA) IAW B737 700 SRM 51- 40-02. SRM 51-10-02 ITEM 9 AND DWG 143A7902. REV. A. RII.

Part: STRINGER — CRACKED (BS 540 S25L) · airframe 66,572 hrs · 39,411 cycles

CRACK STRINGER 25L LOCATED BS540 FWD CARGO COMPARTMENT (1 EA) ; 2021-311647 / [01] TOOL USED PN: 45MG; SN:130063701; DUE DATE: 11-MAY-22; [02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [03] TOOL USED P/N: NORTEC 500D; S/N: N500X12101V022240; DUE DATE: 01-DEC-21.; [04] REPAIRED CRACK STRINGER 25L LOCATED BS540 FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG# 143A3230 REV -; [05] REPAIRED CRACK STRINGER 25L LOCATED BS540 FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG# 143A3230 REV - RII; [06] REPAIRED CRACK STRINGER 25L LOCATED BS540 FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG# 143A3230 REV - RII

Part: STRINGER — CRACKED (BS 540 S26R) · airframe 66,572 hrs · 39,411 cycles

CRACK STRINGER 26R LOCATED BS540 AT FWD CARGO COMPARTMENT (1 EA) ; 2021-311650 / [01] TOOL USED: P/N: 45MG; S/N: 130060401; DUE DATE: 22-APR-22; [02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [03] TOOL USED P/N: NORTEC 500D; S/N: N500X12101V022240; DUE DATE: 01-DEC-21.; [04] REPAIRED CRACK STRINGER 26R LOCATED BS540 AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG# 143A3230 REV -; [05] REPAIRED CRACK STRINGER 26R LOCATED BS540 AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG# 143A3230 REV -RII; [06] REPAIRED CRACK STRINGER 26R LOCATED BS540 AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG# 143A3230 REV - RII

Part: SUPPORT ANGLE — CRACKED (BS 907-927) · airframe 66,572 hrs · 39,411 cycles

CRACK ANGLE - SUPPORT LOCATED BTW BSTA 907 TO BSTA 927 AND STR 25R TO STR 27R AT AFT CARGO COMPARTMENT ; 2021-311659 / [01] TOOL USED:SOLAR POWER CALIPER P/N:500-464;S/N:11572544;DUE DATE:15/JAN/22; [02] REPLACED ANGLE - SUPPORT LOCATED BTW BSTA 907 TO BSTA 927 AND STR 25R TO STR 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G AND DRAWING #147A7221 REV:D.; [03] TASK COMPLETED; VERIFIED AS RII.<BR><BR>REPLACED ANGLE - SUPPORT LOCATED BTW BSTA 907 TO BSTA 927 AND STR 25R TO STR 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G AND DRAWING #147A7221 REV:D.

Part: CARGO TRACK — CRACKED (BS 747) · airframe 66,572 hrs · 39,411 cycles

CRACK INTERNAL STRUCTURE CARGO TRACK LOCATED AT BSTA 747 AND RBL 13.8 LEVEL STR 26R AT AFT CARGO COMPARTMENT. REPAIRED CARGO TRACK LOCATED BETWEEN BS 727E TO BS 787 AND RBL 13.8 LEVEL STR 26R AT AFT CARGO COMNPARTMENT IAW SRM B737-700 53-00-53-2R-3 REPAIR 3

Part: FLOOR SUPPORT — DETERIORATED (BS 270-380) · airframe 66,572 hrs · 39,411 cycles

DETERIORATED FLOOR STRUCTURE CIC STA 270 TO STA 380 AT FWD GALLEY AREA ; 2021-311651 / [01] OK TO APPLY CIC FLOOR STRUCTURE AREA ON STA 270 AT STA 380.; [02] APPLIED ON FLOOR STRUCTURE CIC STA 270 TO 380 AT FWD GALLEY AREA I.A.W. B737-700 AMM 51-21-91-620-802.; [03] APPLIED ON FLOOR STRUCTURE CIC STA 270 TO 380 AT FWD GALLEY AREA I.A.W. B737-700 AMM 51-21-91-620-802.; [04] APPLIED ON FLOOR STRUCTURE CIC STA 270 TO 380 AT FWD GALLEY AREA I.A.W. B737-700 AMM 51-21-91-620-802.

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 66,572 hrs · 39,411 cycles

CRACK GUSSET LOCATED BS500D AT LEVEL STR19L FWD CARGO COMPARTMENT (1 EA) ; 2021-311645 / [01] OK TO INSTAL GUSSET.; [02] DRILLED NEW GUSSET AND APPLIED PROTECTIVE TREATMENT ON HOLES LOCATED ON BS 500D AND S-19L IAW B737-700 SRM 51-40-02;51-20-01. OK TO INSTALL NEW GUSSET LOCATED ON BS 500D AND S-19L GRANTED; [03] REPLACED GUSSET AND FASTENERS LOCATED BS500D AT LEVEL STR19L FWD CARGO COMPARTMENT (1 EA) IAW B737 700 SRM 51- 40-02. SRM 51-10-02 ITEM 9 AND DWG 143A7902. REV. A.; [04] COMPLETED RII INSPECTION

Part: STRINGER — CRACKED (BS 540 S26L) · airframe 66,572 hrs · 39,411 cycles

CRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT (1 EA) ; 2021-311649 / [01] TOOL USED PN: 45MG; SN:130063701; DUE DATE: 11-MAY-22; [02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015 GOES00000 S/N 112031023 DUE DATE: 22-JAN-22; [03] TOOL USED P/N: NORTEC 500D; S/N: N500X12101V022240; DUE DATE: 01-DEC-21.; [04] REPAIRED CRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG# 143A3220 REV -; [05] REPAIRED CRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG# 143A3220 REV - RII; [06] REPAIRED CRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND DWG# 143A3220 REV - RII

Part: FRAME — CRACKED (BS 480 S8-9R) · airframe 66,572 hrs · 39,411 cycles

CRACK FRAME BS 480 BTW STR 8R TO STR 9R AT PASSENGER CABIN ; 2021-311625 / [01] PERFORMED LAY OUT ON REPAIR AREA LOC. FRAME BS 480 BTW STR 8R TO STR 9R AT PASSENGER CABIN I.A.W B 737-700 EA 1-A53-12114 FIGURE 1 SHEET 2 TOOL USED:CALIPER 700-113-10 S/N:0019289 DUE DATE:25MAR22.; [02] PERFORMED PERMANENT REPAIR ON FRAME I.A.W EA#1-A53-12114 REV 6; [03] PERFORMED PERMANENT REPAIR ON FRAME I.A.W EA#1-A53-12114 REV 6.. RII ITEM

Part: FRAME — CRACKED (BS 312) · airframe 66,572 hrs · 39,411 cycles

CRACK FRAME BS 312 AT LH UPPER CORNER CUT OUT AT PASSENGER CABIN ; 2021-311623 / [01] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101V022236 DUE DATE: 02-JUN-22.; [02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22. TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [03] PERFORMED REPAIR ON FRAME 312 I.A.W SRM B737-700 53-10-07-2R-1; [04] PERFORMED REPAIR ON FRAME 312 I.A.W B737-700 SRM 53-10-07-2R-1; COMPLETED RII INSPECTION

Part: FRAME — CRACKED (BS 500C S8-9R) · airframe 66,572 hrs · 39,411 cycles

CRACK FRAME BS 500C BTW STR 8R TO STR 9R AT PASSENGER CABIN ; 2021-311626 / [01] PERFORMED LAY OUT ON REPAIR AREA LOC. FRAME BS 500C BTW STR 8R TO STR 9R AT PASSENGER CABIN I.A.W B 737-700 EA 1-A53-12114 FIGURE 1 SHEET 2 TOOL USED:CALIPER 700-113-10 S/N:0019289 DUE DATE:25MAR22.; [02] STEP 2 VERIFIED; RII; [03] PERFORMED PERMANENT REPAIR ON FRAME I.A.W EA#1-A53-12114 REV 6; [04] PERFORMED PERMANENT REPAIR ON FRAME I.A.W EA#1-A53-12114 REV 6.. RII ITEM

Part: SUPPORT ANGLE — CRACKED (BS 685-706) · airframe 66,572 hrs · 39,411 cycles

CRACK SUPPORT ANGLE LOCATED BS 685 TO BS 706 AND RBL 24.82 AT PASSENGER CABIN ; 2021-311606 / [01] TOOL USED: PRECISION RADIUS P/N:2204A3;S/N:AE-408655;DUE DATE:24/NOV/21.; [02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 21-JAN-22. TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 21-JAN-22.; [03] REPLACED SUPPORT ANGLE AND FASTENER LOCATED BS 685 TO BS 706 AND RBL 24.82 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 ; SRM 51-10-02 AND DWG 273A9110 REV ; [04] TASK COMPLETED; VERIFIED AS RII.<BR><BR>REPLACED SUPPORT ANGLE AND FASTENER LOCATED BS 685 TO BS 706 AND RBL 24.82 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 ; SRM 51-10-02 AND DWG 273A9110 REV

Part: SUPPORT ANGLE — CRACKED (BS 685-706) · airframe 66,572 hrs · 39,411 cycles

CRACK SUPPORT ANGLE LOCATED BTW BS 685 TO BS 706 AND LBL 0.07 AT PASSENGER CABIN ; 2021-311607 / [01] REPLACED SUPPORT ANGLE LOC BS 685 AT BS 706 LBL 0.07 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; 51-10-02 AND DRAWING 273A9110 REV -; [02] CERTIFIED RII WORK PERFORMED.

Part: SUPPORT ANGLE — CRACKED (BS 685-706) · airframe 66,572 hrs · 39,411 cycles

CRACK SUPPORT ANGLE LOCATED BTW BS 685 TO BS 706 AND LBL 24.82 AT PASSENGER CABIN ; 2021-311604 / [01] TOOL USED: PRECISION RADIUS P/N:2204A3;S/N:AE-408655;DUE DATE:24/NOV/21.; [02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 21-JAN-22. TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 21-JAN-22.; [03] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS685 TO BS706 AND LBL 24.82 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND DWG 273A9110 REV -; [04] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS685 TO BS706 AND LBL 24.82 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND DWG 273A9110 REV - RII

Part: STIFFENER — BROKEN (BS 540) · airframe 66,572 hrs · 39,411 cycles

BROKEN FLOOR STRUCTURE STIFFENER ASSY LOCATED AT BS 540 AND BTW LBL 0 TO LBL 45.57 AT PASSENGER CABIN (2 EA) ; 2021-311602 / [01] INSTALLED STIFFENER ASSY 2 E/A LOCATED AT BS 540 AND BTW LBL 0 TO LBL 45.57 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND 51-10-02 AND DRAWING 143A5240 REV:-; [02] REPLACED STIFFENER ASSY 2 E/A LOCATED AT BS 540 AND BTW LBL 0 TO LBL 45.57 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND 51-10-02 AND DRAWING 143A5240 REV:-; [03] JOB COMPLETED;RII ACCOMPLISHED.

Part: SHEAR TIE — CRACKED (BS 277 S10R) · airframe 66,572 hrs · 39,411 cycles

CRACK FWD SERVICE DOOR COTOUT TIE CLIP BS 277 AND STRINGER 10R AT PASSENGER CABIN ; 2021-311573 / [01] REPLACED TIE CLIP AND FASTENERS ON BS 277 STR 10R PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 DWG. #141A1110 REV.-; [02] TASK CARD COMPLETE AND CERTIFIED AS RII.

Part: WEB — CRACKED (BS 294 S16L) · airframe 66,572 hrs · 39,411 cycles

CRACK ENTRY DOOR CUT OUT WEB BS 294.5 AND STRINGER 16L AT FWD GALLEY AREA ; 2021-311574 / [01] TOOL USED:CALIB PIE DE REY P/N:DIGITAL 150;S/N:AE-412597;DUE DATE:25/MAY/22.; [02] REPLACED ENTRY DOOR CUT OUT WEB BS 294.5 AND STRINGER 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02;51-10-02 AND DRAWING 141A8180 REV C; [03] REPLACED ENTRY DOOR CUT OUT WEB BS 294.5 AND STRINGER 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02;51-10-02 AND DRAWING 141A8180 REV C. RII

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 66,572 hrs · 39,411 cycles

CRACK INSPAR RIB LOWER INBOARD FLANGE AT 27 INCH FROM FRONT SPAR LOCATED STAB STA 175.50 LT HORIZONTAL STAB ; 2021-311539 / [01] TOOLS USED: CALIPER P/N DIGITAL 150; S/N AE-412610; DUE DATE 21-MAY-22; RADIUS GAUGE P/N 2204A3; S/N AE-408655; DUE DATE 24-NOV-21.; [02] TOOL USED P/N: NORTEC 500D S/N: N500X12101V022240 AND DUE DATE: 01-DEC-21.; [03] PERFORMED PERMANENT REPAIR ON INSPAR RIB LOWER INBOARD FLANGE AT 27 INCH FROM FRONT SPAR LOCATED STAB STA 175.50 LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 FIGURE 204 DEATIL A. MATERIAL USED: ALUMINUM SHEETS P/N 7075T6 0.050 P.O. 2014 532264; P/N 7075T6 0.016 P.O. 2021 124913; ANGLE P/N BAC1490-2738 P.O. 2017 503185; T-EXTRUSION P/N BAC1505-101210 BATCH 201958870200102.; [04] PERFORMED PERMANENT REPAIR ON INSPAR RIB LOWER INBOARD FLANGE AT 27 INCH FROM FRONT SPAR LOCATED STAB STA 175.50 LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 FIGURE 204 DEATIL A. MATERIAL USED: ALUMINUM SHEETS P/N 7075T6 0.050 P.O. 2014 532264; P/N 7075T6 0.016 P.O. 2021 124913; ANGLE P/N BAC1490-2738 P.O. 2017 503185; T-EXTRUSION P/N BAC1505-101210 BATCH 201958870200102.<BR>RII INSPECTION DONE.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 66,572 hrs · 39,411 cycles

CRACK INDICATION ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STA 193.90 AND 16 INCH. FROM THE FRONT SPAR. CRACK LENGTH = 0.75 INCH. APPROX. ; 2021-311490 / [01] TOOL USED PN: NORTEC500D; SN: N500X12101V022235; DUE DATE: 03 JUN 22.; [02] MADE REPAIR PART (DOUBLER; FILLER) LOC LT HORIZONTAL STABILIZER LOWER SKIN PANEL BTW STA 184.70 TO STA 203.10 IAW B 737-700 SRM 55-10-01-2R-11 REPAIR 11 STEP 4. G (1) TO (3) AND STEP 4.H TO M. FIGURE 204 DETAIL B; [03] REPAIRED LOWER SKIN OF HORIZONTAL STABILIZER STA193.90 AND 16 FROM THE FRONT SPAR ;I.A.W SRM B737-700 55-10-01-2R-11; [04] REPAIRED LOWER SKIN OF HORIZONTAL STABILIZER STA193.90 AND 16 FROM THE FRONT SPAR ;I.A.W B737-700 SRM 55-10-01-2R-11; COMPLETED RII INSPECTION

Part: SKIN — CRACKED (RT WING) · airframe 66,572 hrs · 39,411 cycles

CRACK LOWER SURFACE SLAT 8 LEADING EDGE NOSE SKIN ACTUATOR STA 451.97 RT WING ; 2121-311456 / [01] TOOL USED P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE DATE: 30-NOV-21; [02] CRACK ON LOWER SUERFACE SLAT 8 WAS DOCUMENTED ON FAULT TTG8Q005PWEN REPALCEMENT SLAT 8; [03] NO MAINTENANCE ACTION IS REQUIRED DUE TO SLAT 8 IS GOING TO BE REPLACED WITH FAULT TTG8Q005PWEN; [04] JOB COMPLETED.

Part: PLATE — ELONGATED (LT WING) · airframe 66,420 hrs · 39,324 cycles

LH WING I/B FIXED LWR T/E PANEL WIGGLE PLATE DAMAGE FASTENER HOLES ELONGATED OUT OF LIMITS. / REMOVED AND REPLACED WIGGLE PLATE IAW SRM 57-20-01-2R-2 AND SRM 51-40-02; REMOVED AND REPLACED WIGGLE PLATE IAW SRM 57-20-01-2R-2 AND SRM 51-40-02

Part: PLATE — CRACKED (LT WING) · airframe 66,420 hrs · 39,324 cycles

LEFT WING WIGGLE PLATE HOLE DAMAGE ; WHILE PERFORMING OPEN HOLE INSP. FOUND 2 HOLE WITH CRACK INDICATION PER NDT PT. 6 51-00-00 PRO. 16 / REAMED FASTENER HOLES ON LT FIXED T/E LOWER PANEL PER AMM 57-50-02. / SRM 57-20-01-2R-2. REQUIRED NDT ON HOLE FASTENERS.; INSTALLED NEW WIGGLE PLATE WITH NEW FASTENERS IAW SRM 57-20-01-2R-2; INSTALLED NEW WIGGLE PLATE WITH NEW FASTENERS IAW SRM 57-20-01-2R-2

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 65,831 hrs · 39,005 cycles

L2 EMERGENCY EXIT SIGN LENS IS MISSING. REPLACED LENS IAW AMM 33-51-11.

Part: HOOK AND LOOP — LOOSE (R1 DOOR SLIDE) · airframe 65,729 hrs · 38,955 cycles

PORTION OF FWD SVC DOOR SLIDE IS EXPOSED / REATTACHED VELCRO STRIP TO GIRT FWD SERVICE DOOR SLIDE AS PER MM 25-66-01

Part: TRUNNION — OUT OF TOLERANCE (RT MLG) · airframe 64,743 hrs · 38,356 cycles

R/H GEAR FWD TRUNNION FITTING-ALL FOUR LUGS HAVE BORE DIAMTERS THAT ARE BEYONG THE 'NOMINAL' BORE DIMENSION OF 1.5602' TO 1.5610' / REPAIRED PER EA 1-A57-3246 REF D&M ENTERPRISES A/R WORK ORDER SSR# 1244

Part: TRUNNION — CORRODED (LT MLG) · airframe 64,743 hrs · 38,356 cycles

L/H GEAR FWD TRUNNION FITTING-LOWER OUTBOARD LUG- INNER FACE HAS CORROSION / REPAIRED PER EA 1-A57-3246 REF D&M ENTERPRISES A/R WORK ORDER SSR# 1243

Part: TRUNNION — CORRODED (LT MLG) · airframe 64,743 hrs · 38,356 cycles

L/H GEAR FWD TRUNNION FITTING-LOWER OUTBOARD LUG- OUTER FACE HAS CORROSION / REPAIRED PER EA 1-A57-3246 REF D&M ENTERPRISES A/R WORK ORDER SSR# 1243

Part: TRUNNION — CORRODED (MLG) · airframe 64,743 hrs · 38,356 cycles

GEAR FWD TRUNNION FITTING-UPPER OUTBOARD LUG OUTER FACE HAS CORROSION. / REPAIRED PER EA 1-A57-3246 REF D&M ENTERPRISES A/R WORK ORDER SSR# 1243

Part: TRUNNION — CORRODED (RT MLG) · airframe 64,743 hrs · 38,356 cycles

R/H GEAR FWD TRUNNION FITTING-UPPER OUTBOARD OUTER FACE HAS CORROSION / REPAIRED PER EA 1-A57-3246 REF D&M ENTERPRISES A/R WORK ORDER SSR# 1244

Part: TRUNNION — CORRODED (LT MLG) · airframe 64,743 hrs · 38,356 cycles

L/H GEAR FWD TRUNNION FITTING-LOWER INBOARD LUG- INNER FACE HAS CORROSION. / REPAIRED PER EA 1-A57-3246; REF D&M ENTERPRISES A/R WORK ORDER SSR# 1243

Part: TRUNNION — CORRODED (RT MLG) · airframe 64,743 hrs · 38,356 cycles

R/H GEAR FWD TRUNNION FITTING-LOWER INBOARD INNER FACE HAS CORROSION / REPAIRED PER EA 1-A57-3246 REF D&M ENTERPRISES A/R WORK ORDER SSR# 1244

Part: TRUNNION — CORRODED (LT MLG) · airframe 64,743 hrs · 38,356 cycles

L/H GEAR FWD TRUNNION FITTING-UPPER INBOARD LUG OUTER FACE HAS CORROSION. / REPAIRED PER EA 1-A57-3246 REF D&M ENTERPRISES A/R WORK ORDER SSR# 1243

Part: TRUNNION — CORRODED (LT MLG) · airframe 64,743 hrs · 38,356 cycles

L/H GEAR FWD TRUNNION FITTING-LOWER INBOARD LUG- OUTER FACE HAS CORROSION. / REPAIRED PER EA 1-A57-3246 REF D&M ENTERPRISES A/R WORK ORDER SSR# 1243

Part: TRUNNION — OUT OF TOLERANCE (RT MLG) · airframe 64,743 hrs · 38,356 cycles

R/H GEAR FWD TRUNNION FITTING-ALL FOUR LUG BORE DIAMETERS ARE BEYOND THE 'NOMINAL' BORE DIMENSIONS OF 1.5602' TI 1.5610' / REPAIRED PER EA 1-A57-3246 REF D&M ENTERPRISES A/R WORK ORDER SSR# 1243

Part: TRUNNION — CORRODED (RT MLG) · airframe 64,743 hrs · 38,356 cycles

R/H GEAR FWD TRUNNION FITTING-LOWER INBOARD OUTER FACE HAS CORROSION / REPAIRED PER EA 1-A57-3246 REF D&M ENTERPRISES A/R S WORK ORDER SSR# 1244

Part: TRUNNION — CORRODED (RT MLG) · airframe 64,743 hrs · 38,356 cycles

R/H GEAR FWD TRUNNION FITTING-LOWER OUTBOARD OUTER FACE HAS CORROSION / REPAIRED PER EA 1-A57-3246 REF D&M ENTERPRISES A/R WORK ORDER SSR# 1244

Part: TRUNNION — CORRODED (RT MLG) · airframe 64,743 hrs · 38,356 cycles

R/H GEAR FWD TRUNNION FITTING-LOWER OUTBOARD INNER FACE HAS CORROSION / REPAIRED PER EA 1-A57-3246 D&M ENTERPRISES A/R WORK ORDER SSR# 1244

Part: SUPPORT BRACKET — CRACKED (RT WING TE PANEL) · airframe 64,718 hrs · 38,342 cycles

RIGHT WING UPPER FIXED TRAILING EDGE PANEL BETWEEN #6 AND # 7 SPOILER; THE LOWER SUPPORT BRACKET IS CRACKED AT THE LEADING EDGE LOWER FASTENER. MARKED. / REMOVED AND REPLACED PER SRM 51-40-02.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 63,237 hrs · 37,430 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1169M, M1670 AND M1673 IN CABIN. / R&R BATTERIES PER MM.

Part: COVER — BROKEN (CABIN) · airframe 62,457 hrs · 36,930 cycles

RIGHT OVERWING EXIT LIGHT COVER BROKEN. / REPLACED COVER PER AMM 33-51-01.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,828 hrs · 36,520 cycles

L1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R LIGHT FUSE PER AMM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,828 hrs · 36,520 cycles

L1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R THE BALLAST FUSE IAW AMM.

Part: SUPPORT — CRACKED (LWR FUSELAGE) · airframe 61,828 hrs · 36,520 cycles

STRAP CRACKED AT RIGHT WING FWD WTB FAIRING SUPPORT I/B END OF FIXED LEADING EDGE / REMOVED AND REPLACED STRAP AT R/W FWD WTB FAIRING SUPPORT I/B END OF FIXED L/E IN REF B737-700 SRM 51-40-02-0G-0 JS 5083

Part: SUPPORT PLATE — CRACKED (LT WING) · airframe 61,828 hrs · 36,520 cycles

L/H WING INBOARD REAR SPAR LOWER CHORD PANEL 551GB FORWARD FASTENER SUPPORT PLATE CRACKED. R&R PLATE IAW SRM.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 61,828 hrs · 36,520 cycles

AFT CARGO FLOOR AREA FLOOR SUPPORT T-ANGLE AT STA 795 AND RBL 18 SHOWS SOME HOLES WITH CORROSION. 82-114. / REMOVED CORROSION ON AFT CARGO COMP. FLOOR SUPPORT 'T' ANGLE AT STA: 795 AND RBL-18 PER REF B737 SRM 51-10-02-0G-0; AREA WITHIN LIMITS PER REF. B737 SRM 53-00-53-1A-2 FIG 103 DITAIL H. / AFTER SECOND INVESTIGATION ON ALLOWABLE DAMAGED; FOUND ON STEP 4B DETAIL D' FIG. 103; NO CORROSION NOTE ALLOWABLE AT HOLE; FWD AND AFT CARGO COMP. FLOOR STRUCTURES; REMOVED AND REPLACED SUPPORT TRACK FROM EXISTING REPAIR SPLICE AT STA 779.5 TO EXISTING SPLICE STD: 887; RBL 13.8 PER REF B-737 SRM 53-00-53-2R-3 AND E.A. 1-453-8210.

Part: FAIRING — CRACKED (RT WING) · airframe 61,828 hrs · 36,520 cycles

RIGHT WING FLAP TRACK # 6 MID FAIRING 642BB CRACKS AT INT. AFT FWD OF O/B DRAIN HOLE MKD DOT 60-080 / CLEANED & REPAIRED SMALL 1/2' DAMAGE ON R/W FLAP TRACK FAIRING 642BB INT SURFACE AFT FWD OF O/B DRAIN HOLE AS PER B737-700 SRM 51-70-0G2 R-3 REPAIR #3 MATERIALS USED PO#1150387 & PO#1615845 NO CORE DAMAGE NO WATER FOUND

Part: SUPPORT ANGLE — CRACKED (LWR FUSELAGE) · airframe 61,828 hrs · 36,520 cycles

LATE ENTRY R/W FWD WING TO BODY FAIRING SUPPORT ANGLE CRACKS AT I/B END OF FIXED L/E MKD DOT 60-078 / REMOVED AND REPLACED R/W FWD WTB FAIRING SUPPORT ANGLE AT I/B END OF FIXED L/E IN REF B737-700 SRM 51-40-02-0G-0_AND DWG # 116A3118 JS 5083

Part: BRACKET — ELONGATED (L/H WING) · airframe 61,828 hrs · 36,520 cycles

LEFT WING FIXED T/E PANEL # 551FB I/B AFT SUPPORT LINK ATTACHED BRACKET FASTENER HOLE ELONGATED MKD DOT60-076 / REMOVED AND INSTALLED NEW BRACKET; AT L/W FIXED T/E PANEL # 551FB AFT SUPPORT LINK ; IN REF B737-700 SRM 51-40-02-0G-0

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 61,828 hrs · 36,520 cycles

PASSENGER CABIN AFT WET FLOOR PANEL 242UF AFT EDGE DAMAGED, BETWEEN BS. 887 TO BS. 1016. / REPAIRED FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 61,828 hrs · 36,520 cycles

PASSENGER CABIN AFT WET FLOOR PANEL 241AAF AFT EDGE DAMAGED BETWEEN BS. 887 TO BS. 1016. / REPAIRED FLOOR PANEL 21AAF PER SRM.

Part: SKIN — DAMAGED (BS 962) · airframe 61,828 hrs · 36,520 cycles

L2 DOOR CREASE FUSELAGE SKIN DAMAGED AT BS. 962, BETWEEN STR. 19L TO STR. 21L. REPAIRED DOUBLER PER EA.

Part: SHIELD — CRACKED (#2 ENGINE) · airframe 61,828 hrs · 36,520 cycles

NO-2 ENG I/B FAN COWL INTERNAL INTERCOSTAL CRACKED AT UPPER EDGE AFT OF FWD HOLD OPEN ROD MKD DOT 60-071 / REMOVED AND REPLACED SHIELD P/N: 314-2259-4 REF B737-700 SRM 51-40-02-0G-0; SRM 51-30-01-0G-0 AND SRM 51-20-01-0G-0 AND CMM 71-13-30.

Part: FLOOR SUPPORT — CRACKED (BS 327-328) · airframe 61,828 hrs · 36,520 cycles

MAIN CABIN FORWARD WET AREA FLOOR SUPPORT BEAM FLANGE CRACKED AT FASTENER HOLE FORWARD BETWEEN BS. 327 TO BS. 328, BETWEEN RBL 1 TO RBL 65. / REPAIRED FLOOR BEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 61,828 hrs · 36,520 cycles

FLOOR BEAM CORRODED AT BS. 986.5, BETWEEN RBL 50 TO LBL 50. / REPAIRED FLOOR BEAM PER EA.

Part: ANGLE — CRACKED (BS 663) · airframe 61,828 hrs · 36,520 cycles

FUSELAGE WHEEL WELL WEB ANGLE CRACKED AT BS. 663.5, LBL 10. / R&R ANGLE IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 767-787) · airframe 61,828 hrs · 36,520 cycles

AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS. 767 TO BS. 787, 22" RIGHT OF CENTER LINE. R&R SHIELD IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 727D-847) · airframe 61,828 hrs · 36,520 cycles

AFT CARGO "Z" CHANNEL FLOOR SUPPORT CORRODED BETWEEN BS. 727D TO BS. 847, BETWEEN RBL 22 OF CENTER LINE TO LBL 22. / R&R SIDE PLATE PER SRM.

Part: FLOOR SUPPORT — CORRODED (BS 727D-767) · airframe 61,828 hrs · 36,520 cycles

AFT CARGO FLOOR SUPPORT "Z" CHANNEL CORRODED BETWEEN BS. 727D TO BS. 767, 22 INCHES R/H OF CENTER LINE. INSTALLED 'Z' CHANNEL PER SRM.

Part: FLOORBEAM — CORRODED (BS 887) · airframe 61,828 hrs · 36,520 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS. 887, BETWEEN RBL 16 TO LBL 16. R&R TEE SUPPORT PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 727D) · airframe 61,828 hrs · 36,520 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS. 727D, BETWEEN RBL 22 TO LBL 22. / R&R SUPPORT TEE PER SRM AND DWG.

Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 61,828 hrs · 36,520 cycles

R/H A/C BAY FORWARD VAPOR BARRIER WEB ONE HORIZONTAL "L" ANGLE CRACKED, LOCATED 6" ABOVE PACK EXHAUST CUTOUT AT BS. 663. / R&R "L" ANGLE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,828 hrs · 36,520 cycles

CABIN FORWARD WET AREA INTERCOSTAL CRACKED BETWEEN BS. 280 TO BS. 294.5, RBL 1. R&R INTERCOSTAL IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 61,828 hrs · 36,520 cycles

R/H HORIZONTAL STABILIZER INSPAR RIB #4 STIFFENER #3 CRACKED. / REPAIRED STIFFENER PER SRM.

Part: FLOOR SUPPORT — CORRODED (BS 312-328) · airframe 61,828 hrs · 36,520 cycles

PASSENGER CABIN FORWARD WET AREA INTERCOSTAL CORRODED BETWEEN BS. 312 TO BS. 328, RBL 11. R&R PANEL BREAK PER SRM & DWG.

Part: WEB — CORRODED (FWD CARGO) · airframe 61,828 hrs · 36,520 cycles

FORWARD CARGO COMPARTMENT DOOR CUTOUT LOWER SILL WEB UPPER SURFACE SPOTS CORRODED. / R&R SILL WEB IAW DWG & SRM.

Part: SUPPORT ANGLE — CORRODED (L1 THRESHOLD) · airframe 61,828 hrs · 36,520 cycles

L1 DOOR THRESHOLD INBOARD SUPPORT ANGLE CORRODED. R & R ANGLE PER SRM AND DWG.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 61,828 hrs · 36,520 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB NR 4 STIFFENER CRACKED. REPAIRED THE STIFFENER PER SRM.

Part: PRESSURE DECK — CRACKED (BS 663-675) · airframe 61,828 hrs · 36,520 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED BETWEEN BS. 663 TO BS. 675, BETWEEN LBL 30 TO LBL 60. / REPAIRED WEB PER SRM.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 61,828 hrs · 36,520 cycles

PASSENGER CABIN FWD WET AREA THERE IS AN INTERCOSTAL CRACKED AT STA 312 TO 328 STA AND LBL46. DOT 82-077. / REMOVED AND INSTALLED INTERCOSTAL FROM STA 312 TO STA 328 LBL 46' PER B737-7 SRM 51-40-02-0G-0 JM 1878 7-30-19

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 61,828 hrs · 36,520 cycles

PASSENGER CABIN AFT WET AREA PANEL NUMBER 242WF HAS A DELAMINATED CORNER. DOT 82-063. / CLEANED AREA OF DAMAGED OF PASSENGER CABIN AFT WET AREA PANEL NUMBER 242WF REF B737-700 SRM 53-00-50-2R-8-(3.D) INSTALLED FIBER GLASS REPAIR REF B737-700 SRM 53-00-50-2R-8-(3.J). MATERIAL USED PO#1614988; PO#1608196 AND PO#1602224.

Part: SUPPORT ANGLE — CORRODED (L1 THRESHOLD) · airframe 61,828 hrs · 36,520 cycles

L1 DOOR CENTER THRESHOLD SUPPORT ANGLE CORRODED. R & R ZEE CHORD IAW SRM AND DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 61,828 hrs · 36,520 cycles

PASSENGER CABIN AFT WET AREA PANEL NUMBER 241ABF HAS A DELAMINATED CORNER. DOT 82-057. / CLEANED AREA AND REPAIRED FLOOR PANEL # 241ABF AT CORNER IN REF B737 SRM 53-00-50-2R-8; MAT USED EPO CAST 50A / 546 PO # 1602224 AND PO # 1614988.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 61,828 hrs · 36,520 cycles

L/H HORIZONTAL STABILIZER INSPAR RIB NR 5, STIFFENER NR 3 CRACKED. REPAIRED THE NR 3 STIFFENER IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,828 hrs · 36,520 cycles

PASSENGER CABIN FORWARD WET AREA THERE INTERCOSTAL CRACKED BETWEEN BS. 328 TO BS. 344, LBL 46. R&R INTERCOSTAL PER SRM.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 61,828 hrs · 36,520 cycles

R/W REAR SPAR T/E UP FIXED PANEL LWR SURFACER ATTACHED SEAL RETAINER IS CRACKED O/B OF SPOILER #7 / REMOVED AND INSTALLED NEW RETAINER AT R/W SURFACE SPAR TE UP FIXED PANEL LOWER IN REF B737-700 SRM 51-40-02-0G-0.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 61,828 hrs · 36,520 cycles

PASSENGER CABIN FORWARD WET AREA PANEL NUMBER 221CF INSERTS CORRODED, BETWEEN BS. 270 TO BS. 420. R&R INSERTS PER SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 61,828 hrs · 36,520 cycles

R/H HORIZONTAL STABILIZER INSPAR RIB #4 STIFFENER #2 CRACKED. / REPAIRED STIFFENER PER SRM.

Part: CREASE BEAM — CORRODED (BS 295-380) · airframe 61,828 hrs · 36,520 cycles

L1 DOOR CREASE BEAM CORRODED BETWEEN BS. 295 TO BS. 380, BETWEEN LBL 60 TO LBL 62. R&R CREASE BEAM CHORD PER SRM AND DWG.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 61,828 hrs · 36,520 cycles

FORWARD GALLEY AND LAV FLOOR PANEL 222BF SCREW INSERTS CORRODED, BETWEEN BS. 270 TO BS. 420. R&R INSERTS PER SRM.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 61,828 hrs · 36,520 cycles

FORWARD GAL AND LAV FLOOR PANEL 221BF SCREW INSERTS CORRODED, BETWEEN BS. 270 TO BS. 420. R&R INSERTS IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 61,828 hrs · 36,520 cycles

WING CENTER SECTION REAR SPAR VAPOR BARRIER CRACKED AT BS. 663, LBL 38. REPAIRED BARRIER PER SRM.

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 61,828 hrs · 36,520 cycles

FORWARD GAL AND LAV FLOOR PANELS 222AF SCREW INSERTS CORRODED, BETWEEN BS. 270 TO BS. 420. R&R INSERTS PER SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 61,828 hrs · 36,520 cycles

CENTER WING SECTION REAR SPAR VAPOR BARRIER CRACKED AT BS. 663, BETWEEN RBL 12 TO RBL 20. REPAIRED BARRIER IAW SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 61,828 hrs · 36,520 cycles

AFT CARGO DOOR CUTOUT;AFT SCUFF PLATE CORNER WITH TWO CRACKS / RECEIVED SERVICEABLE AFT CARGO COMP. DOOR CUT-OUT AFT CORNER SCUFF PLATE; IT WILL BE INSTALLED ON T/C J753-140-00-02Y. COPY ATTACHED. LOCATED AND DRILLED HOLES ON NEW AFT SCUFF PLATE CORNER PER REF B-737-700 SRM 51-40-05-0G-0

Part: INSERT — CORRODED (FLOOR PANEL) · airframe 61,828 hrs · 36,520 cycles

FORWARD GAL AND LAV FLOOR PANEL 221DF SCREW INSERTS CORRODED, BETWEEN BS. 270 TO BS. 420. / R&R INSERTS PER SRM.

Part: WEB — CRACKED (BS 663) · airframe 61,828 hrs · 36,520 cycles

LOWER FUSELAGE WEB CRACKED AT BS. 663.75, LBL 38. R&R WEB IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 61,828 hrs · 36,520 cycles

LOWER FUSELAGE WEB CRACKED AT BS. 663.75, BETWEEN RBL 6 TO RBL 72. / R&R WEB PER SRM AND DWG.

Part: RIB — CRACKED (RT WING) · airframe 61,828 hrs · 36,520 cycles

R/H WING TRAILING EDGE STRUCTURE SHOWS DEFLECTION CONTROL RIB UPPER AFT SUPPORT ANGLE CRACKED AT LOWER AREA. REPAIRED RIB PER SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING TE) · airframe 61,828 hrs · 36,520 cycles

L/H WING TRAILING EDGE BELOW OF DEFLECTION CONTROL RIB, SUPPORT ANGLE CRACKED. R&R SUPPORT ANGLE IAW DWG AND SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 61,828 hrs · 36,520 cycles

AFT CARGO COMPT TRESHOLD LOWER FWD CORNER SCUFF PLATE IS CRACKED AT TWO LOCATIONS. / RECEIVED SERVICEABLE AFT CARGO COMPT. THRESHOLD LOWER CORNER SCUFF PLATE. IT WILL BE INSTALLED ON T/C J753-140-00-02Y. LOCATED AND DRILLED HOLES AT NEW SCUFF PLATE IN REF B737-700 SRM 51-40-05-0G-0.

Part: BEAM — CRACKED (R1 DOOR) · airframe 61,514 hrs · 36,334 cycles

R1 DOOR CRACKED ON BEAM IN RADIUS BELOW CAM BOX ASSEMBLY NEXT TO FORWARD INBOARD MOUNTING BOLT. REPAIRED DOOR IAW MM.

Part: FAIRING — CRACKED (RT WNG TO BODY) · airframe 61,514 hrs · 36,334 cycles

RIGHT WING TO BODY FAIRING 191FR HAD A PIECE CRACKED OFF AT TRAILING EDGE. REPAIRED PANEL PER EA.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,077 hrs · 36,051 cycles

R1 DOOR OVERHEAD EXIT SIGN LIGHT INOP. R&R BATTERY PACK PER AMM.

Part: CHARGER — ABNORMAL (CABIN) · airframe 61,077 hrs · 36,051 cycles

R1 DOOR OVERHEAD EXIT SIGN LIGHT INOP. R&R CHARGER PER AMM.

Part: RETAINER — BROKEN (WHEEL WELL RH) · airframe 60,253 hrs · 35,545 cycles

R/H W/W CENTER WING REAR SPAR SEAL ASSY'S IS SEVERED FROM STIFFINER AT RBL 15.54. AND HAS BROKEN FASTENERS / R&R #2 PACK EXAUST SEAT RETAINER PER SRM 51-40-02

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 60,253 hrs · 35,545 cycles

R/H W/W LOWER STIFFINER CRACKED AT RBL 25.00 / R&R W/W LOWER SIFFINER PER SRM 51-40-02

Part: BATTERY — FAILED (CABIN) · airframe 59,368 hrs · 34,975 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PER AMM.

Part: SUPPORT — CRACKED (VERTICAL STABILI) · airframe 59,368 hrs · 34,975 cycles

PANEL 324AL LOWER AND SIDE MOUNT SUPPORTS ARE CRACKED / REPLACED PANEL 324AL LOWER AND SIDE MOUNT SUPPORTS PER SRM.51-40-02

Part: BATTERY — FAILED (CABIN) · airframe 59,368 hrs · 34,975 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,368 hrs · 34,975 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,368 hrs · 34,975 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1674. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,368 hrs · 34,975 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,580 hrs · 34,462 cycles

LT OVERWING EXIT EMERGENCY LIGHT INOP. R&R LIGHT PER AMM.

Part: GUIDE VANE — CRACKED (NR 1 ENGINE) · airframe 58,437 hrs · 34,359 cycles

NR 1 ENG STAGE 1 NOSE GUIDE VANE CRACKS. R&R NR 1 ENG PER MT.

Part: RETAINER — CRACKED (LT WING) · airframe 57,250 hrs · 33,608 cycles

L/H WING FIXED TRAILING EDGE VERTICAL SEAL RETAINER RETAINER IS CRACKED DIRECTLY ABOVE #1 ENG PYLON AFT FAIRING / REMOVED AND REPLACED L/H WING TRAILING EDGE VERTICAL SEAL BRACKET IAW SRM 51-40-02.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 57,250 hrs · 33,608 cycles

L/H WING #3 SLAT SKIN DELAMINATED AT THE OUTBOARD AFT END. / R&R SLAT SKIN PER MM.

Part: HOUSING — LOOSE (RT OVERWING) · airframe 57,243 hrs · 33,604 cycles

RIGHT OVERWING EMERGENCY EXIT PULL DOWN STRAP HOUSING LOOSE. REINSTALLED THE HARDWARE IAW SIP.

Part: EEC — FAILED (NR 1 ENGINE) · airframe 56,488 hrs · 33,124 cycles

INFLIGHT SHUTDOWN, AT APPROX 3000' 20NM FROM KLIT ABOUT 220 KTS THE NR 1 ENGINE ROLLED BACK. NR 1 GENERATOR LIGHT FOLLOWED BY ENGINE FAIL. R&R NR 1 ENGINE ELECTRONIC ENGINE CONTROL IAW MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 56,018 hrs · 32,820 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE OUT OF POSITION. REPOSITIONED SLIDE PACK IAW SOPM & MT.

Part: HOUSING — DAMAGED (CABIN) · airframe 56,018 hrs · 32,820 cycles

L2 DOOR LOWER CEILING EMERGENCY EXIT LIGHT HOUSING DAMAGED. R&R LIGHT HOUSING IAW AMM.

Part: SKIN — CORRODED (BS 867-887) · airframe 56,018 hrs · 32,820 cycles

CROWN SKIN CORRODED BETWEEN BS 867& 887, STRINGERS 2L - 2R. REPAIRED THE SKIN IAW EA & ER.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,018 hrs · 32,820 cycles

CROWN SKIN CORRODED BETWEEN BS 887 TO BS 1016, BETWEEN STR 3L TO STR 3R. REPAIRED SKIN IAW EA & ER.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 56,018 hrs · 32,820 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS 665, RBL 40.5. REPAIRED DECK IAW EA.

Part: FORMER — CRACKED (LOWER EXT FUSELA) · airframe 56,018 hrs · 32,820 cycles

L/H FAIRING FORMER AT BS 500D BETWEEN STR18L AND 19L IS CRACKED / REMOVED AND REPLACED L/H FAIRING FORMER BS 500D B/W STR 18L + 19L IAW SRM 51-40-02;51-40-05; DWG #116A3010 + DWG #116A3118; DWG #116A3310

Part: FAIRING — DAMAGED (FUSELAGE) · airframe 56,018 hrs · 32,820 cycles

SUPPLEMENTAL INFORMATION: FAIRING # 193B HAS OVERSIZED HOLES AND CHAFFING ON THE INTERNAL SIDE OF PANEL / OVERSIZED HOLES & CHAFTING DAMAGE TO INNER SURFACE OF FAIRING 193 B WERE REPAIRED IAW SRM 53-40-70; SRM 51-70-05-2R-G; & SRM 51-40-05

Part: SKIN — CRACKED (LE SLAT) · airframe 55,479 hrs · 32,481 cycles

RT WING NR 5 SLAT SKIN CRACKED. R&R NR 5 SLAT SKIN PER AMM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 55,071 hrs · 32,241 cycles

LT HORIZONTAL STABILIZER LEADING EDGE RIB AT STA 92.5 CRACKED. R&R RIB IAW SRM AND DWG.

Part: SKIN — CRACKED (BS 540) · airframe 52,236 hrs · 30,575 cycles

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

Part: LENS — MISSING (CABIN) · airframe 52,206 hrs · 30,556 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 50,273 hrs · 29,462 cycles

LEFT OVERWING EMER EXIT ROW SIGN LENS MISSING. INSTALLED LENS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 44,234 hrs · 25,977 cycles

R1 DOOR FLOOR EMERGENCY EXIT LIGHT LENS MISSING. R & R LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,305 hrs · 24,822 cycles

RT EMERGENCY EXIT DOOR EMERGENCY EXIT LIGHT BULB INOPERATIVE. R&R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,305 hrs · 24,822 cycles

R1 DOOR EMERGENCY EXIT LIGHT BULB INOPERATIVE. R&R BULB IAW AMM.

Part: CHARGER — BROKEN (CABIN) · airframe 42,305 hrs · 24,822 cycles

AFT EMERGENCY EXIT LIGHT BATTERY CHARGER BROKEN. R&R BATTERY CHARGER IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

RT WW FWD VERTICAL BULKHEAD CRACKED FROM LOWER EDGE AT RBL 14. REPAIRED BULKHEAD IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

LT WW FWD VERTICLE BULKHEAD CRACKED FROM LOWER EDGE AT LBL 14. REPAIRED BULKHEAD IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

FRAME CRACKED AT STATION 867, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW ER.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 42,305 hrs · 24,822 cycles

LT HORIZONTAL STABILIZER RIB 92.70 2ND VERTICAL STIFFENER CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

CREASE BEAM INBD CHORD CORRODED AT BS 722, LBL 65. REPAIRED CHORD IAW ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

FLOOR BEAM CORRODED AT BS 986.5, RBL 43. REPAIRED BEAM IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

CREASE BEAM INBD CHORD CORRODED AT BS 706, LBL 65. REPAIRED CHORD IAW ER & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

FWD CARGO DOOR CUTOUT SUB-THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 492, BETWEEN RBL 23 TO RBL 30. R&R WEB IAW SRM & DRAWING.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727C TO BS 767, RBL 22. REPAIRED SUPPORT IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 42,305 hrs · 24,822 cycles

MLG WW VERTICAL PRESSURE DECK CRACKED AT BS 663, BETWEEN LBL 40 TO LBL 42. REPAIRED DECK IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

NR 3 LT WINDOW SECOND LOWER CORNER FASTENER HOLE CRACKED. REPAIRED FRAME IAW EA.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 42,305 hrs · 24,822 cycles

RT WING TE UPPER PANEL SUPPORT ANGLE AT PROGRAM TRACK CRACKED ORSS 281. R&R ANGLE IAW SRM & SOPM.

Part: FLAP — DELAMINATED (LT WING) · airframe 42,305 hrs · 24,822 cycles

LT WING OTBD AFT FLAP DELAMINATED AT AFT INBD CORNER. REPAIRED AFT FLAP IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

NR 3 RT WINDOW SECOND LOWER CORNER FASTENER HOLE CRACKED. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 42,305 hrs · 24,822 cycles

RT WING TE BULKHEAD WEB SEAL RETAINER ANGLE CRACKED AT ORSS 271. R&R ANGLE IAW SRM & SOPM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

NR 3 RT WINDOW THIRD LOWER FASTENER HOLE CRACKED. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 42,305 hrs · 24,822 cycles

RT WING NR 6 SLAT LE LOWER SURFACE SKIN CRACKED AT STATION 202.45. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

FIRST OFFICER'S NR 1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER. REPAIRED FRAME IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

EXTERNAL POWER RECEPTACLE DOOR CUTOUT CRACKED AT AFT EDGE. REPAIRED CUTOUT IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 42,305 hrs · 24,822 cycles

RT WING NR 7 SLAT LE LOWER SURFACE SKIN CRACKED AT FASTENER AT ACTUATOR ATTACHMENT FITTING SLAT STATION 322.71. REPAIRED SKIN IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 42,305 hrs · 24,822 cycles

CAPTAIN'S NR 1 WINDOW FRAME CRACKED IN UPPER OTBD CORNER. REPAIRED FRAME IAW EA.

Part: BRACKET — CRACKED (LT WING) · airframe 40,353 hrs · 23,625 cycles

LEFT WING AFT SPAR LOWER BULB SEAL BRACKET IS CRACKED ABOVE WING PANEL 551GB. REMOVED AND REPLACED BRACKET PER AMM.

Part: BRACKET — CRACKED (LT WING) · airframe 40,353 hrs · 23,625 cycles

LEFT WING AFT SPAR UPPER BULB SEAL BRACKET IS CRACKED ABOVE WING PANEL 551GB. REMOVED AND REPLACED BRACKET PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,294 hrs · 22,969 cycles

RIGHT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 39,294 hrs · 22,969 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 39,294 hrs · 22,969 cycles

LEFT EEPLS COVERS CRACKED BETWEEN ROW 6 TO ROW 11. REMOVED AND REPLACED COVERS PER MM.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 37,924 hrs · 22,157 cycles

FWD EMERGENCY FLOOR LIGHT INOPERATIVE. RECONNECTED WIRES TO LIGHT ASSY IAW MM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 36,603 hrs · 21,385 cycles

DURING SCHEDULED 10Y CHECK, FOUND F/O'S SEAT OUTBD TRACK CORRODED. REMOVED AND REPLACED SEAT TRACKS PER MM.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 36,603 hrs · 21,385 cycles

DURING SCHEDULED 10Y CHECK, FOUND F/O'S SEAT INBD TRACK CORRODED. REMOVED AND REPLACED SEAT TRACKS PER MM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,603 hrs · 21,385 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLIGHT DECK FLOOR ENTRY WAY, LOWER FLOOR STRUCTURE UNDER ACCESS PANEL CORRODED AT BS 270, RBL 5. REPAIRED INTERCOSTAL IAW EA.

Part: WEB — CRACKED (CENTER WING) · airframe 36,603 hrs · 21,385 cycles

DURING SCHEDULED 10Y CHECK, FOUND CRACKS IN CENTER WING SECTION, STA 663, RBL 33 TO RBL 45, 9 INCHES BELOW CABIN CENTER FLOOR LINE. REMOVED AND REPLACE DAMAGED WEB POT PER EA.

Part: LENS — MISSING (CABIN) · airframe 36,213 hrs · 21,153 cycles

EEPLS LENS MISSING AT ROW 17. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 36,107 hrs · 21,091 cycles

DURING SCHEDULED HC2 CHECK, RT AFT GALLEY EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 36,107 hrs · 21,091 cycles

DURING SCHEDULED HC2 CHECK, LT AFT GALLEY EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 33,661 hrs · 19,674 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 33,661 hrs · 19,674 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 4. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 33,661 hrs · 19,674 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LOOSE AT ROW 11. SECURED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 33,661 hrs · 19,674 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS LOOSE AT ROW 11. SECURED EEPLS PER MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 33,621 hrs · 19,647 cycles

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

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 33,621 hrs · 19,647 cycles

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

Part: LENS — MISSING (CABIN) · airframe 32,662 hrs · 19,094 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS LENS MISSING AT ROW 15. INSTALLED LENS PER MM.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 32,164 hrs · 18,796 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT EMERGENCY LIGHTS INOP AT ROW 1. RECONNECTED WIRE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,801 hrs · 18,571 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP AT ROW 1. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 31,489 hrs · 18,386 cycles

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

Part: LENS — MISSING (CABIN) · airframe 31,265 hrs · 18,266 cycles

DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING AT ROW 16. INSTALLED LENS PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 30,931 hrs · 18,093 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD EEPLS SECTION INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 29,647 hrs · 17,305 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. SECURED CONNECTOR PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,569 hrs · 17,250 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, LBL 5. REPAIRED BEAM PER EA.

Part: LIGHT — BROKEN (CABIN) · airframe 29,561 hrs · 17,242 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS BROKEN. REPAIRED EEPLS PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,538 hrs · 17,222 cycles

DURING SCHEDULED 8Y CHECK, FOUND LOWER FWD CORNER STUB FRAME CRACKED AT R1 DOOR. REPAIRED FRAME PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 29,432 hrs · 17,157 cycles

FWD EEPLS COVER LOOSE AT ROW 1. SECURED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,432 hrs · 17,157 cycles

LT EEPLS INOP AT ROW 1. RELAMPED PER MM.

Part: LENS — MISSING (CABIN) · airframe 29,432 hrs · 17,157 cycles

EEPLS LENS MISSING AT ROW 2. INSTALLED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 29,362 hrs · 17,101 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS LOOSE AT ROW 1. REMOVED AND REPLACED TRACK ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 27,556 hrs · 15,950 cycles

EEPLS LIGHT LOOSE AT ROW 1. SECURED EEPLS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 27,203 hrs · 15,708 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING O/B TRAILING EDGE FLAP I/B AFT END DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,203 hrs · 15,708 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL TEST. CHARGED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 27,203 hrs · 15,708 cycles

DURING SCHEDULED HC2 CHECK, FWD LT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 26,387 hrs · 15,226 cycles

LT EEPLS TRACK LIGHT LENS MISSING AT ROW 1. REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,863 hrs · 14,893 cycles

DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 13 SEAT D. RELAMPED LIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 24,634 hrs · 14,156 cycles

EEPLS LENS LOOSE AT ROW 4 ABC. SECURED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,659 hrs · 13,568 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 18 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — MISSING (CABIN) · airframe 23,659 hrs · 13,568 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,600 hrs · 13,532 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 22,806 hrs · 13,048 cycles

EEPLS ASSY BROKEN AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 22,777 hrs · 13,031 cycles

EEPLS COVER LOOSE AT ROW 3 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 22,353 hrs · 12,780 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 22,353 hrs · 12,780 cycles

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

Part: LENS — CRACKED (CABIN) · airframe 22,353 hrs · 12,780 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS LIGHT LENS CRACKED AT ROW 5 ABC. REMOVED AND REPLACED LENS PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 22,139 hrs · 12,638 cycles

DURING SCHEDULED 6Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 180. REPAIRED SKIN PER SRM.

Part: COVER — MISSING (CABIN) · airframe 21,650 hrs · 12,346 cycles

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

Part: COVER — MISSING (CABIN) · airframe 21,217 hrs · 12,102 cycles

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

Part: COFFEEMAKER — FAULTY (CABIN) · airframe 19,339 hrs · 11,032 cycles

AFT COFFEEMAKER HAD BURNING SMELL DURING FLIGHT, OPENED C/B SMELL DISSIPATED. REMOVED AND REPLACED COFFEEMAKER PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 17,445 hrs · 9,976 cycles

DURING SCHEDULED HC2 CHECK, FWD CABIN EMERGENCY EXIT LIGHT BATTERY FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 17,445 hrs · 9,976 cycles

DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY EXIT LIGHT BATTERY FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — LOOSE (CABIN) · airframe 17,345 hrs · 9,917 cycles

EEPLS LIGHT COVER LOOSE AT ROW 1 ABC. SECURED LIGHT COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 12,479 hrs · 7,139 cycles

FWD END OF EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L2 & R2 DOORS) · airframe 11,583 hrs · 6,631 cycles

L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R2 DOOR EVAC SLIDES PER MM.

Part: FITTING — LOOSE (FWD ENTRY DOOR) · airframe 4,487 hrs · 2,622 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD ATTACH FITTING LOOSE. SECURED FITTING PER MM.

Part: CLOCK — OVERHEATED (COCKPIT) · airframe 1,293 hrs · 777 cycles

DECLARED EMERGENCY, DIVERSION, ELECTRICAL SMOKE IN COCKPIT. FOUND CAPT'S CLOCK TO BE SOURCE, REMOVED AND REPLACED CAPT'S CLOCK PER MM.

Part: COALESCER BAG — CONTAMINATED (A/C BAY) · airframe 115 hrs · 69 cycles

AIR TURNBACK, AFTER T/O THERE WAS A PUNGENT ELECTRICAL ODOR IN THE CABIN ACCOMPANIED BY FAILURE OF ELECTRIC STAB TRIM ON BOTH SIDES. ELECTRIC TRIM BEGAN WORKING AFTER LANDING. REMOVED AND REPLACED WATER SEPARATOR BAGS PER MM AND OPS CK'D STAB TRIM PER MM, NO DISCREPANCIES FOUND.