N560WN

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 74,745 hrs · 37,022 cycles

FORWARD ENTRY DOOR GIRT BAR LOOSE<[01] ADJUSTED FORWARD ENTRY DOOR GIRT BAR HOOKS PER AMM 25-66-01<BR>A/C OK TO CONTINUE.

Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 73,537 hrs · 36,338 cycles

TOP FLASHLIGHT AT FWD FA STATION INOP<[01] REPLACED TOP FLASH LT BATTERY AT FWD F/A STATION IAW AMM 25-64-00

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,908 hrs · 35,359 cycles

EMERGENCY LIGHT ON FWD HORSESHOE PANEL INOP<[01] RELAMPED EMERGENCY LIGHT ON FWD HORSESHOE PANEL AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-03-960-801;[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 71,908 hrs · 35,359 cycles

PANEL BREAK CRACKED AT ATTACH POINTS BS 540 WL 208 BL 0 - RBL 24.<[01] REMOVED; LOCATED; DRILLED AND INSTALLED PANEL BREAK AT B.S 540 BL 0-RBL 24; WL 208 IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0;[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 71,908 hrs · 35,359 cycles

PANEL BREAK CRACKED AT ATTACH POINTS BS 540 WL 208 BL 0 - LBL 24.<[01] REMOVED; LOCATED; DRILLED AND INSTALLED PANEL BREAK AT B.S 540 BL 0-LBL 24; WL 208 IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0;[02] VERIFIED CORRECTIVE ACTION #1

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,824 hrs · 35,312 cycles

ROW 24DEF WINDOW LIGHT INOPERATIVE. RELAMPED SIDEWALL LIGHT 24 DEF REF AMM 33-21-00.

Part: SLIDE — OUT OF ADJUST (ZN 800 DOOR) · airframe 71,229 hrs · 34,964 cycles

R1 ESCAPE SLIDE COMING OFF COMPARTMENT / [01] R/R R1 (FWD/SERVICE) DOOR ESCAPE SLIDE ASS'Y PER MM: 25-66-01 &<BR>MT #: 725-61-06.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 70,886 hrs · 34,755 cycles

L1 DOOR GIRT BAR STOP RING MISSING HARD WARE / [01] R&R L1 DOOR GRIT BAR SDTOP RING PER CMM 25-60-37

Part: LIGHT — INOPERATIVE · airframe 70,697 hrs · 34,642 cycles

EMERGENCY LIGHTS ON THE LH MID EMERGENCY DOOR DOES NOT ILLUMINATE. / [01] REPLACED BATTERY PACKS M1672; M1670 AND M1668 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-805.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. BATTERY TESTS GOOD.;[03] UPDATED PARTS BLOCK.;[04] VERIFIED CORRECTIVE ACTION 3 AND COMPLETED OK TO CLOSE PANELS;[05] COMPLETED STEP 1.;[06] VERIFIED CORRECTIVE ACTION 5 COMPLETED

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,697 hrs · 34,642 cycles

CRACK ON ACB INTERCOSTAL BS440 LBL24 / [01] UPDATED FAULT ENTRY : CRACK ON FCB INTERCOSTAL BS440 LBL 24;[02] EVALUATED FCB INTERCOSTAL BS440 LBL24 IAW SRM 53-00-53-1A-2 PARAGRAPH 4C. AND FOUND TO BE OUT OF LIMITS L=0.8'' TOOL USED DIGITAL CALIPER ID:ATS2738 S/N:A22004095 DUE:04/20/23. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 PART 9C.;[03] VERIFIED CORRECTIVE ACTION 1 AND 2;[04] FABRICATED ON FWD CARGO INTERCOCTAL BS.440 RBL 24 FROM ITEM 7075T6 - 0.020' SH LOTE 1489798-1 PER DWG 143A7510 OK TO PRIMR;[05] CORRECTION: TO ACTION ITEM 4 REMOVED INTERCOSTAL BS 440 LBL 24 IAW SRM 51-40-02;[06] FORMED INTERCOSTAL; AT FWD CARGO BAY BS440 LBL24 WITH MATERIAL( 7075T6 #0.020') LOTE 1489798-1 PER DWG 143A7510 OK TO LOCATE AND DRILL;[07] LOCATED AND DRILLED NEW INTERCOSTAL FWD CARGO BAY BS440-460 LBL24 IAW SRM 51-40-05-0G-0 AND DRAWING 143A7510.<BR>APPLIED CHEMICAL CONVERSION COATING IAW AMM 51-21-41-370-802.<BR>OK TO PRIME;[08] VERIFIED CORRECTIVE ACTIONS #4; #5; #6; #7.<BR>VERIFIED OK TO PRIME.;[09] APPLIED PRIMER TO NEW INTERCOSTAL IAW SOPM 20-41-02 OK TO INSTALL;[10] VERIFIED CORRECTIVE ACTION #9.<BR>VERIFIED OK TO INSTALL INTERCOSTAL.;[11] INSTALLED INTERCOSTAL AT FCB BS 440-BS 460; LBL 24 IAW SRM 51-40-02-0G-0 AND DWG#143A7505 REV-A;[12] UPDATED MEASUREMENTS;[13] VERIFIED CORRECTIVE ACTION #11.<BR>VERIFIED MEASUREMENT TABLE.

Part: NONE — CRACKED (FWD CARGO) · airframe 70,697 hrs · 34,642 cycles

CRACKED INTERCOSTAL CLIP AT FCB FWD SIDE OF BS 420 FRAME RBL 24 / [01] CRACKED INTERCOSTAL CLIP AT FCB FWD SIDE OF BS 420 FRAME RBL 24; WL 154; FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PAR 9C .;[02] REMOVED INTERCOSTAL CLIP AT FCB FWD SIDE OF BS 420 FRAME RBL 24; WL 154 I.A.W SRM 51-40-02-0G-0.;[03] LOCATED AND DRILLED NEW INTERCOSTAL CLIP AT FCB FWD SIDE OF BS 420 FRAME RBL 24; WL 154 I.A.W SRM 51-40-05-02-0G-0 AND DWG 145A7505.;[04] LOCATED AND DRILLED NEW INTERCOSTAL CLIP AT FCB FWD SIDE OF BS 420 FRAME RBL 24; WL 154 I.A.W SRM 51-40-05-02-0G-0 AND DWG 145A7505.OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 3 AND 4 COMPLETED AND OK TO INSTALL COMPLETED. <BR><BR>VERIFIED MEASUREMENT TABLE;[06] INSTALLED NEW INTERCOSTAL CLIP AT FCB FWD SIDE OF BS 420 FRAME RBL 24; WL 154 I.A.W SRM 51-40-02-0G-0 AND DWG 145A7505.;[07] VERIFIED CORRECTIVE ACTION 6 COMPLETED;[08] VERIFIED JOB COMPLETED

Part: INTERCOSTAL — ELONGATED (FUSELAGE) · airframe 70,697 hrs · 34,642 cycles

INTERCOSTAL HAS ELONGATED HOLE COMMON TO FLOOR RAIL BS 727A-727B RBL 13 / [01] REMOVED INTERCOSTAL HAS ELONGATED HOLE COMMON TO FLOOR RAIL BTW BS 727A-727B RBL 13 IAW SRM 51-40-02-0G-0.;[02] REMOVED (2EA) CLIPS FOR ACCESS LOCATED BTW BS 727A - 727B IAW SRM 51-40-02.;[03] RECEIVED THE INTERCOSTAL FROM THE MACHINE SHOP HT TO T6 AND PENETRANT INSPECTED ON CUSTOMER RO# 879198-SWA (JOB#552221).;[04] FABRICATED/ LOCATED AND DRILLED INTERCOSTAL FROM BS 727A-BS 727B RBL 13. TREATED.... IAW SRM 51-40-05 AND IAW DWG#146A7500... OK TO PRIME;[05] VERIFIED CORRECTIVE ACTION 3 AND 4.<BR>OK TO PRIME;[06] APPLIED TWO LAYERS OF BMS 10-11 PRIMER TO THE INTERCOSTAL IAW SOPM 20-41-02 AND IAW DWG#146A7505.... OK TO INSTALL;[07] VERIFIED CORRECTIVE ACTION 6.<BR>OK TO INSTALL;[08] INSTALLED ACB INTERCOSTAL AT BS 727A-BS 727B RBL 13 IAW SRM 51-40-02-0G-0 AND DWG#146A7500 REV-C;[09] VERIFIED CORRECTIVE ACTION #8.

Part: NONE — ELONGATED (FUSELAGE) · airframe 70,697 hrs · 34,642 cycles

FRAME TO RAIL CLIP HAS ELONGATED HOLE BS 767 RBL 13 / [01] LOCATED AND DRILLED NEW CLIP PN# 146A1310U6; PO#879079 IAW SRM 51-40-05 AND IAW DWG#146A1261... OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION 1.<BR>OK TO INSTALL;[03] INSTALLED NEW CLIP AT BS 767 RBL 13 IAW SRM 51-40-02 AND IAW DWG#146A1261;[04] VERIFIED CORRECTIVE ACTION 3;[05] VERIFIED COMPLETE

Part: FITTING — CRACKED (FUSELAGE) · airframe 70,697 hrs · 34,642 cycles

CRACK FOUND AT LH PORTABLE WATER TANK SUPPORT ANGLE TO BULKHEAD ATTACH ANGLE BS PR7 LBL 9 CRACK FOUND AT LH PORTABLE WATER TANK SUPPORT ANGLE TO BULKHEAD ATTACH ANGLE BS 947 LBL 9 / [01] CRACK FOUND AT LH PORTABLE WATER TANK SUPPORT ANGLE TO BULKHEAD ATTACH ANGLE BS PR7 LBL 9 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR.9C;[02] RECEIVED NEW FITTING P/N 149A8113U6 LOT#1497212-2 LOCATED AND DRILLED IAW SRM 51-40-05-0G-0 AND INSTALLED IAW SRM 51-40-02-0G-0 AND DWG#149A8103;[03] VERIFIED CORRECTIVE ACTION #2.<BR>VERIFIED MEASUREMENT TABLE.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 70,697 hrs · 34,642 cycles

CRACK ON FWD CARGO BAY STRINGER END AT BS 540 L/H STRINGER 25. / [01] SRM 53-00-03-1A-1 ALLOWABLE DAMAGE 1 AND SRM 53-00-03-2R-1 REPAIR 1 ARE APPLICABLE TO THIS A/C;[10] FABRICATED REPAIR PARTS -7 REPLACEMENT STRINGER SECTION FROM HFAB53-STS-011 PO NUMBER 878532 /1; -1 HAT SECTION SPLICE FROM MATERIAL 69-78188-14 LOT# 1460965-1 LOCATED AND DRILLED REPAIR PARTS AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 53-00-03-2R-1 REPAIR 1 OK TO PRIMER;[11] VERIFIED CORRECTIVE ACTION 9 AND 10. OK TO PRIME;[12] APPLIED PRIMER ON REPAIR PARTS; STRINGER SECTION AND HAT SECTION SPLICE IAW SRM 53-00-03-2R-1 REPAIR 1; OK TO INSTALL;[13] VERIFIED CORRECTIVE ACTION 12. OK TO INSTALL STRINGER SECTION AND HAT SPLICE.;[14] INSTALLED REPAIR PARTS -7 REPLACEMENT STRINGER SECTION AND -1 HAT SECTION IAW SRM 53-00-03-2R-1 REPAIR 1<BR><BR>COMPLETED PARTIAL STEPS 1 AND 2;[15] VERIFIED CORRECTIVE ACTION 14.<BR><BR>COMPLETED STEPS 1 AND 2;[16] VERIFIED MEASUREMENT TABLE

Part: STRINGER — CRACKED (FWD CARGO) · airframe 70,697 hrs · 34,642 cycles

CRACK ON FWD CARGO BAY STRINGER END AT BS 540 R/H STRINGER 26. / [01] SRM 53-00-03-1A-1 ALLOWABLE DAMAGE 1 AND SRM 53-00-03-2R-1 REPAIR 1 ARE APPLICABLE TO THIS A/C [09] RECIVED NEW STRINGER SECTION FORMED FROM OSS PO NUMBER 878535 /1 DYE PENETRANT INSPECTED IAW BAC5423 AND COSTUMER RO NO 878535-SWA.;[10] FABRICATED REPAIR PARTS NEW REPLACEMENT STRINGER SECTION FROM HFAB53-STS-011 PO NUMBER 878535 /1; -1 HAT SECTION SPLICE FROM MATERIAL 69-78188-14 LOT# 1460965-1 LOCATED AND DRILLED REPAIR PARTS AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 53-00-03-2R-1 REPAIR 1 OK TO PRIMER;[11] VERIFIED CORRECTIVE ACTION 10.<BR>OK TO PRIME;[12] APPLIED PRIMER AT REPAIR PARTS STRINGER SECTION AND SPLICE PER SRM 53-00-03-2R-1 REP.1.<BR>OK TO INSTALL REPAIR PARTS;[13] VERIFIED CORRECTIVE ACTION 12.<BR>OK TO INSTALL;[14] INSTALLED STRINGER SECTION AND HAT SECTION SPLICE AT STR 26R BETWEEN BS 500D + 11 TO BS 540 PER SRM 53-00-03-2R-1 REPAIR 1;[15] VERIFIED CORRECTIVE ACTION 14;[16] COMPLETED STEPS 1-2;[17] APPLIED FILLET SEALANT AND CORROSION INHIBITING COMPOUND TO THE REWORKED AREAS IAW SRM 53-00-03-2R-1 REPAIR 1 STEPS K & L;[18] COMPLETED STEPS 1 AND 2;[19] VERIFIED CORRECTIVE ACTION 17.<BR>VERIFIED MEASUREMENT TABLE

Part: STRINGER — CRACKED (FWD CARGO) · airframe 70,697 hrs · 34,642 cycles

CRACK ON FWD CARGO BAY STRINGER END AT BS 540 R/H STRINGER 25. / [01] SRM 53-00-03-1A-1 ALLOWABLE DAMAGE 1 AND SRM 53-00-03-2R-1 REPAIR 1 ARE APPLICABLE TO THIS A/C;[13] FABRICATED/LOCATED AND DRILLED -7 REPLACEMENT STRINGER SECTION. TREATED; IAW SRM 53-00-03-2R-1 REPAIR 1 AND IAW EA#22-153-02453-WIP1... OK TO PRIME;[14] VERIFIED CORRECTIVE ACTIONS 12 AND 13. OK TO PRIME;[15] PRIMED -7 REPLACEMENT STRINGER SECTIONT AND REWORKED AREA. <BR>IAW SRM 53-00-03-2R-1 REPAIR 1 AND IAW EA#22-153-02453-WIP1... OK TO INSTALL;[16] VERIFIED PRIMER APPLICATION TO REPLACEMENT STRINGER SECTION. OK TO INSTALL REPLACEMENT STRINGER SECTION ONLY.;[17] RECIEVED (3EA) -2 ANGLES AND (3EA) -3 CHANNELS FROM OSS TO HT T6 IAW SR 53-00-03-2R-1 REPAIR 1. CUSTOMER RO#878780-SWA/JOB# 552154 AND CUSTOMER RO#878781-SWA/JOB#552155;[18] FABRICATED/LOCATED AND DRILLED A -2 CHANNEL AND (2EA) -3 ANGLES AND EXTENDED THE -3 ANGLES MINIMUM 0.1 INCH PAST THE STRINGER FLANGE LIP. TREATED; IAW SRM 53-00-03-2R-1 REPAIR 1 AND IAW EA#22-153-02453-WIP1. OK TO PRIME[22] INSTALLED REPAIR PARTS -7 REPLACEMENT STRINGER SECTION; -2 CHANNEL AND -3 (2EA) ANGLES IAW SRM 53-00-03-2R-1 REPAIR 1 AND PER EA#22-153-02453-WIP1.<BR><BR>COMPLETED PARTIAL STEPS 1 AND 2;[23] VERIFIED CORRECTIVE ACTION 22.<BR>COMPLETED STEPS 1 AND 2;[24] CRACK ON FORWARD CARGO BAY STRINGER END AT BS 540 RH STRINGER 25 WAS REPAIRED IAW EA 22-153-02453;[25] VERIFIED ALL STEPS COMPLETE.<BR>VERIFIED MEASUREMENTS.

Part: STRINGER — CRACKED (FWD CARGO) · airframe 70,697 hrs · 34,642 cycles

CRACK ON FWD CARGO BAY STRINGER END AT BS 540 L/H STRINGER 26. / [01] SRM 53-00-03-1A-1 ALLOWABLE DAMAGE 1 AND SRM 53-00-03-2R-1 REPAIR 1 ARE APPLICABLE TO THIS A/C;[10] FABRICATED REPAIR PARTS -7 REPLACEMENT STRINGER SECTION FROM HFAB53-STS-011 PO NUMBER 878533 /1; -1 HAT SECTION SPLICE FROM MATERIAL 69-78188-14 LOT# 1460965-1 LOCATED AND DRILLED REPAIR PARTS AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 53-00-03-2R-1 REPAIR 1 OK TO PRIMER;[11] VERIFIED CORRECTIVE ACTIONS 9 AND 10;[12] APPLIED PRIMER ON REPAIR PARTS; STRINGER SECTION AND HAT SECTION SPLICE IAW SRM 53-00-03-2R-1 REPAIR 1; OK TO INSTALL;[13] VERIFIED CORRECTIVE ACTION 12. OK TO INSTALL STRINGER SECTION AND HAT SPLICE.;[14] INSTALLED REPAIR PARTS -7 REPLACEMENT STRINGER SECTION AND -1 HAT SECTION IAW SRM 53-00-03-2R-1 REPAIR 1;[15] COMPLETED PARTIAL STEP 5;[16] VERIFIED CORRECTIVE ACTION 14.<BR>COMPLETED STEP 5;[17] PARTIAL STEPS 1-4.<BR>OK TO INSTALL;[18] COMPLETED STEP 3 AND 4;[19] COMPLETED STEP 1 AND 2;[20] VERIFIED STEPS 1 AND 2 COMPLETE.;[21] VERIFIED MEASUREMENT TABLE AND WORK SCOPE COMPLETE.

Part: TRACK — CRACKED (AFT CARGO) · airframe 70,697 hrs · 34,642 cycles

CRACK ON AFT CARGO BAY TRACK AT RBL 13 BS 727E. / [01] EVALUATED CRACK ON AFT CARGO BAY TRACK RBL13 BS727E IAW SRM 53-00-53-1A-2 PARAGRAPH 4B. FIG. 103 AND FOUND TO BE OUT OF LIMITS. PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0.;[02] UPDATED STEP 1;[03] VERIFIED CORRECTIVE ACTION #1.;[04] PARTIAL STEP 1.;[05] VERIFIED PARTIAL UPDATE STEP 1.;[06] OK TO INSTALL RAIL GIVEN;[07] COMPLETED STEP 1;[08] VERIFIED COMPLETE STEP 1.<BR>VERIFIED MEASUREMENT TABLE.

Part: TIE DOWN — CORRODED (AFT CARGO) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON AFT CARGO BAY TIE DOWN AT RBL 14 BS 747. / [01] UPDATED STEP 1;[02] VERIFIED COMPLETE STEP 1.<BR>VERIFIED MEASUREMENT TABLE.

Part: TIE DOWN — CORRODED (FUSELAGE) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON AFT CARGO BAY TIE DOWN AT RBL 14 BS 727A; BS 727B; BS 727D. / [01] UPDATED STEP 1-3;[02] UPDATED STEP 1-3;[03] VERIFIED COMPLETE STEPS 1-3.<BR>VERIFIED MEASUREMENT TABLE.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 21 BS 767+4; BS 767+16. / [01] DAMANGE FOUND ON ACB FWD SHIELD BS 767-797 RBL 21 WL159 P/N 146A8127-1 FOUND TO BE OUT OF LIMIT IAW SRM PART WILL BE REPAIRED BY REMPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C;[02] VERIFIED CORRETIVE ACTION 1;[03] RECIVED NEW SHIELD ITEM 146A8127-1 LOT1482004 LOCATED AND DRILLED NEW SHIELD AT BS 767 TO 794 RBL21; IAW 737-700 SRM 51-40-05-0G-0 DWG 146A0081.-;[04] PART USAGE INFO;[05] VERIFIED CORRECTIVE ACTION 3

Part: BRACKET — CRACKED (FWD CARGO) · airframe 70,697 hrs · 34,642 cycles

CRACK ON AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+11.5 RBL 14. / [01] REMOVED ANGLE AT AFT CARGO BAY WATER SERVICE PAM BS 907+ 11 RBL 14 PER SRM 51-40-02;[02] NO FOUND ALLOWABLE DAMAGE LIMITS FOR AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+11.5 RBL 14; MUST BE REPLACED IAW SRM 51-10-02 PARAEGRAPH 9;[03] LOCATED AND DRILLED NEW WATER SERVICE BRACKET AT BS 907+11.5 RBL 14 P/N: 147A7221Y32 LOT#1493584 IAW SRM 51-40 -05 AND DWG 147A7221 REV :D;[04] OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 2 AND 3.<BR>OK TO INSTALL;[06] INSTALLED NEW WATER SERVICE BRACKET AT BS 907+11.5 RBL 14 IAW SRM 51-40 -02 AND DWG 147A7221 REV :D;[07] VERIFIED CORRECTIVE ACTION 6;[08] VERIFIED MEASUREMENT TABLE

Part: RAIL — CORRODED (AFT CARGO) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON AFT CARGO BAY RAIL AT LBL 12 BS 767+5. / [01] CORROSION AREA IS LOCATED ON PREVIOUS REPAIR SECTION THEREFORE FOUND TO BE OUT OF LIMITS PER REF SRM 51-10-02-0G-0;[02] REMOVED DAMAGE SECTION PER REF SRM 53-00-53-2R-2 REPAIR 2;[03] CORRECTION ENTRY 1 AND 2 : VERIFY APPLICABILITY PER REF SRM 53-00-53-1A-2 AND SRM 53-60-53-0I-2<BR><BR>REMOVED CORROSION ON AFT CARGO BAY RAIL AT LBL 12 BS 767+5 REF SRM 53-00-53-1A-2 L=2 W=1;[04] CORRECTION ENTRY 1 : NOT FOUND PREVIOUS REPAIR AT DISCREPANCY AREA .;[05] VERIFIED CORROSION REMOVED AND APPLICABILITY OF SRM 53-00-53-1A-2;[06] BLEND OUT EVALUATION;THE MATERIAL LOST IS .005?? ORIGINAL MATERIAL THICKNESS IS .063'' .THEREFORE FOUND TO BE WITHIN LIMITS PER REF SRM 53-00-53-1A-2 TOOLING USED ATS2472 DUE DATE 12/2022;[07] REMOVED 2EA NUT PLATES AT DISCREPANCY AREA PER REF SRM 51-40-02.;[08] VERIFIED CORRECTIVE ACTION 6. OK TO TREAT AND PRIME.;[09] APPLIED CHEMICAL CONVERSION COATING AND PRIMER AT DISCREPANCY AREA PER REF SRM 51-20-01 AND SOPM 20-41-02;[10] VERIFIED CORRECTIVE ACTION 9;[11] INSTALLED NUTPLATES PER REF SRM 51-40-02 AND DWG NBR 146A7503;[12] VERIFIED CORRECTIVE ACTION #11.<BR>VERIFIED MEASUREMENT TABLE.

Part: STRINGER CLIP — CORRODED (AFT CARGO) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON AFT CARGO BAY STRINGER CLIP AT BS 767 LBL 15. / [01] NO FOUND ALLOWABLE DAMAGED FOR THIS PART IN SRM; REPAIR PART BY REMPLACEMENT PER SRM 51-10-02-0G-0 STEP 9;[02] REMOVED STRINGER CLIP AT AFT CARGO BAY BS 767 LBL 15 STR-26L PER SRM 51-40-02;[03] VERIFIED CORRECTIVE ACTION 1 AND 2;[04] LOCATED AND DRILLED NEW STRINGER CLIP AT B/S 767 STR 26L/H LOT# 1480783-2 IAW SRM 51-40-05 AND DWG: 146A1260 REV:-;[05] OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION 4.<BR>OK TO INSTALL;[07] INSTALLED NEW STRINGER CLIP AT B/S 767 STR 26L/H IAW SRM 51-40-02 AND DWG: 146A1260 REV:-;[08] VERIFIED CORRECTIVE ACTION #7.<BR>VERIFIED MEASUREMENT TABLE.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727A+10; BS 727B+10; BS 727B+14; BS 727C+10; BS 727D+3; BS 727D+7; BS 727D+10; BS 727E+6; BS 727E+10; BS 747+6. / [01] UPDATED STEPS 1;10 TO PARTIAL;[02] VERIFY APPLICABILITY OF SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21; BS 727-767 WL 160;[03] COMPLETED STEPS 1-10.<BR>VERIFIED CORRECTIVE ACTION 2;[04] RECIVED NEW FLOOR TO SIDEWALL ITEM 146A7502-51 LOT: 1496140-1 LOCATED AND DRILLED NEW FLOOR TO SIDEWALL AT BS 727 TO 767 RBL 21 WL 160; IAW 737-700 SRM 51-40-05-0G-0 DWG 146A7500.-;[05] VERIFIED CORRECTIVE ACTION 4.<BR>VERIFIED MEASUREMENT TABLE

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727+15; BS 727A+6; BS 727B+14; BS 727C+6; BS 727C+10; BS 727C+18; BS 727D+5; BS 727D+10; BS 727D+14; BS 727E+6. / [01] PARTIAL STEPS 1-10.;[02] VERIFIED CORRECTIVE ACTION FOR PARTIAL OF STEP 1-10.;[03] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF ACB FLOOR TO SIDEWALL SUPPORT LBL 21 SRM 53-00-53-1A-2 .;[04] REMOVED CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727B+14 WL 156 P/N 146A7504-1;AREA OT=0.040;RT=0.033 ;L=1.200';W=0.750'' ;X=0.007 WITH DEPTH GAGE ID:ATS2678<BR>S/N:UNKNOWN<BR>DATE:04/2022<BR>DUE:04/2023. FOUND TO BE OUT LIMITS I.A.W SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE AND SRM 53-60-53-0L-2 FOR IDENTIFICATION AND IT WILL REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PAR 9C .;[05] VERIFIED CORRECTIVE ACTION 3 AND 4.<BR>COMPLETED STEPS 1-10;[06] FABRICATED; LOCATED AND DRILLED REPLACEMENT FLOOR TO SIDEWALL SUPPORT ACB BS 727+4 TO BS 847 LBL21 USING BAC1496-377-7075T62 LOT: 1494598-1 IAW SRM 51-40-05 AND DWG 146A7502.<BR><BR>FABRICATED FLOOR TO SIDEWALL SUPPORT SPLICE REPAIR BTW BS 727E -BS747 USING BAC1496-377-7075T62 LOT: 1494598-1 IAW SRM 53-00-53-2R-6 AND SRM 51-40-05.<BR>APPLY CHEMICAL CONVERSION COATING AND PRIMER.;[[15] INSTALLED SIDEWALL SUPPORT SPLICE REPAIR ACB LBL21 BTW BS 727E-BS747 I.A.W SRM 53-00-53-2R-6.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727E+10; BS 747+6; BS 747+10; BS 747+18; BS 767+6; BS 767+10; BS 767+14; BS 787+2; BS 787+10. / [01] PARTIAL STEPS 1-9.;[02] CORRECTED CORRECTIVE ACTIONS 1.;[03] VERIFIED CORRECTIVE ACTION OF PARTIAL OF STEP 1-9;[04] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF ACB FLOOR TO SIDEWALL SUPPORT LBL 21 IAW SRM 53-00-53-1A-2.;[05] REMOVED CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727E+10 WL 156 P/N 146A7504-1;AREA OT=0.040;RT=0.030 ;L=1.00';W=0.700'' ;X=0.010 WITH DEPTH GAGE ID:ATS2678<BR>S/N:UNKNOWN<BR>DATE:04/2022<BR>DUE:04/2023. FOUND TO BE OUT LIMITS I.A.W SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE AND SRM 53-60-53-0L-2 FOR IDENTIFICATION AND IT WILL REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PAR 9C .;[06] VERIFIED CORRECTIVE ACTIONS 4 AND 5.<BR>COMPLETED STEPS 1-9;[07] THIS FAULT WILL BE ACCOMPLISHED ON CARD TTG8Q00E2HR6.;[08] VERIFIED CORRECTIVE ACTION 7.<BR>VERIFIED MEASUREMENT TABLE

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON AFT CARGO BAY FWD LOWER BULKHEAD SUPPORT AT BS 727+5 RBL 16. / [01] CORROSION ON AFT CARGO BAY FWD LOWER BULKHEAD SUPPORT AT BS 727+5 RBL FOUND TO BE OUT LIMITS DUE TO NO HAS ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.AW SRM 51-10-02-0G-0 PARG.9.C;[02] VERIFIED CORRODED PART WAS THE CAP STRIP ASSEMBLY. VERIFIED NO LIMITS ARE GIVEN FOR DAMAGE OF THIS PART IN THE SRM.<BR>CONCUR OF APPLICABILITY OF SRM 51-10-02-0G-0 PARG.9.C. FOR REPLACEMENT.;[03] RECEIVED NEW CAP STRIP ASSY. P/N 453A2611-25 AND LOT. 1494246-1. THE INSTALLATION WILL BE ACCOMPLISHED WITH THE CUSTOMER CARD TTG8Q0049YCS STEP# 59.;[04] VERIFIED CORRECTIVE ACTION 3. VERIFIED MEASUREMENT TABLE

Part: SHIELD — CORRODED (AFT CARGO) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847+2; BS 847+6; BS 847+19. / [01] DAMANGE FOUND ON ACB FWD SHIELD BS 847-867 RBL 21 WL159 P/N 146A8127-1 FOUND TO BE OUT OF LIMIT IAW SRM PART WILL BE REPAIRED BY REMPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C;[02] VERIFIED CORRETIVE ACTION 1;[03] RECIVED NEW SHIELD ITEM 146A8127-5 LOT 1492406-1 LOCATED AND DRILLED NEW SHIELD AT BS 847 TO 867 RBL21; IAW 737-700 SRM 51-40-05-0G-0 DWG 146A0081.-;[04] UPDATED PARTS USAGE;[05] VERIFIED CORRECTIVE ACTION 3

Part: ANGLE — CRACKED (FWD CARGO) · airframe 70,697 hrs · 34,642 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C AFT SIDE RBL25. / [01] REMOVED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C RBL25 WL156 IAW SRM 51-40-02;[02] LOCATED AND DRILLED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C AFT SIDE RBL25. P/N 143A7502-156 LOT#1488491-11 PO#864293/11 IAW SRM 51-40-05 AND DWG 143A7502 REV:G ;OK TO INSTALL;[03] VERIFIED CORRECTIVE ACTION 2.<BR>OK TO INSTALL;[04] INSTALLED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C AFT SIDE RBL25. WL 156 IAW SRM 51-40-02 AND DWG 143A7502 REV:G;[05] VERIFIED CORRECTIVE ACTION #4.;[06] VERIFIED MEASUREMENT TABLE.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500B; 500B+15 RBL23. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF FCB FLOOR TO SIDEWALL SUPPORT; BS500A - BS500B; 500B+15 RBL23 IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[02] REMOVED CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS500A RBL23 DIMENSIONS L=1' W= 0.750 DEPTH:0.010' IAW SRM 51-10-02 PARAGRAPH 15 ; EVALUATED REWORKED AREA ;ORIGINAL MATERIAL THICKNESS 0.040' REMAINING THICKNESS : 0.030' AND FOUND TO BE OUT LIMITS; ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2;TOOL USED CALIPER ID: ATS2739 S/N: A22004232 DUE: 04/2023;[03] FABRICATED ; LOCATED AND DRILLED REPLACEMENT FLOOR TO SIDEWALL SUPPORT USING BAC1496-444#7075T62 LOT:1497019-1 IAW SRM 51-40-05-0G-0; AND DWG 143A7501 REV: A. BS500A-BS500D RBL23 APPLY CHEMICAL CONVERSION COATING AND PRIMER;[04] VERIFIED CORRECTIVE ACTION 1-3.<BR>OK TO TREAT AND PRIME;[05] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON FLOOR SIDEWALL SUPPORT AT FWD CARGO BAY BS500A-BS500D RBL 23. IAW SRM 51-20-01 AND AMM 51-21-72-370-804;[06] VERIFIED CORRECTIVE ACTION 5

Part: SHIELD — CORRODED (FWD CARGO) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL24. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPACEMENT IAW SRM 51-10-02-0G-0 PARAGRAPH # 9;[02] LOCATED AND DRILLED FCB NEW SHIELD AT RBL 24 WL 156 BS 480+14 TO BS 500A P/N 143A8126-31 LOT: 1492239/1 PO:869254/1 IAW SRM 51-40-05 AND DWG 143A8126 REV:A.;[03] VERIFIED CORRECTIVE ACTION 1 AND 2.<BR>VERIFIED MEASUREMENT TABLE

Part: ANGLE — CRACKED (FWD CARGO) · airframe 70,697 hrs · 34,642 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500A FWD SIDE LBL25. / [01] REMOVED CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500A FWD SIDE LBL25. IAW SRM 51-40-02.;[02] RECEIVED INTERCOSTAL ATTACH ANGLE (CLIP) ITEM: 143A7502-159 LOT: 1496083 ; LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 143A7505. OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTION 2.<BR>OK TO INSTALL;[04] INSTALLED NEW ATTACH ANGLE (CLIP) ITEM: 143A7502-159 LOT: 1496083 I.A.W SRM 51-40-02-0G-0 AND DWG 143A7505.;[05] RII VERIFIED CORRECTIVE ACTION 4 COMPLETE;[06] VERIFIED JOB COMPLETED AND MEASUREMENT TABLE

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY LBL23 BS500A+2; BS500A+10. / [01] REMOVED CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 23 BS 500A+2DIMENSIONS L=1' W= 0.750 DEPTH:0.010' IAW SRM 51-10-02 PARAGRAPH 15 ; EVALUATED REWORKED AREA ;ORIGINAL MATERIAL THICKNESS 0.040' REMAINING THICKNESS : 0.030' AND FOUND TO BE OUT LIMITS; ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2;TOOL USED CALIPER ATS2739 S/N A22004232 DUE 04/2023.;[02] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF FCB FLOOR TO SIDEWALL SUPPORT;LBL 23WL 156 ; IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[03] :FABRICATED ; LOCATED AND DRILLED REPLACEMENT FLOOR TO SIDEWALL SUPPORT USING BAC1496-444#7075T62 LOT:1490548-1 IAW SRM 51-40-05-0G-0;; AND DWG 143A75001 ID:0001 REV: B. FABRICATED FLOOR TO SIDEWALL SUPPORT SPLICE REPAIR AT BTW B/S 480 TO BS 500 USING BAC1496-444#7075T62 LOT:1490548-1 IAW SRM 53-00-53-2R-6 AND SRM 51-40-05. APPLY CHEMICAL CONVERSION COATING AND PRIMER.

Part: BRACKET — CRACKED (CENTER WING BOX) · airframe 70,697 hrs · 34,642 cycles

CRACKED DUCT SUPPORT STA 540+5; LBL 5; WL 163. / [01] REMOVED AND REPLACED P/N 212A1116-1 BRACKET AT BS540 +5; LBL 5; WL 163 IAW SOPM 20-50-01 AND AMM 20-50-11-910-801 TABLE 226;[02] VERIFIED CORRECTIVE ACTION 1 COMPLETED

Part: FASTENER — MISSING (FUSELAGE) · airframe 70,697 hrs · 34,642 cycles

FLOOR SUPPORT O/B ATTACH BOLT IS MISSING AT STA 540+1; LBL 23; WL 207.5 / [01] INSTALLED NEW FASTENER FLOOR SUPPORT O/B AT BS 540+1 LBL 23 WL 207.5 IAW SRM 51-40-02-0G-0 ADN DWG 143A0060;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED MEASUREMENT TABLE

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 70,697 hrs · 34,642 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 45 BS 660; BS 727A+8. / [01] COMPLETED ALL STEPS;[02] COMPLETED STEPS 1 AND 2;[03] APPLIED A CHEMICAL CONVERSION COATING AND ONE LAYER OF ALUMINIZED EPOXY PRIMER TO THE REWORKED AREA; IAW SRM 51-20-01 AND SOPM 20-41-04.;[04] VERIFIED CORRECTIVE ACTION 3.<BR>VERIFIED MEASUREMENT TABLE

Part: FAIRING — BROKEN (R/H WING) · airframe 70,697 hrs · 34,642 cycles

RT WING T/E PANEL 551FB LOWER I/B END FAIRING IS BROKEN (MARKED) RT WING T/E PANEL 651FB LOWER I/B END FAIRING IS BROKEN (MARKED) / [01] REMOVED AND REPLACED BROKEN LOWER I/B END FAIRING ON PANEL 651FB PER BOEING DRAWING 115A2200. FLAG NOTES 7. AND 8.;[02] REMOVED AND REPLACED BROKEN LOWER I/B END FAIRING ON PANEL 651FB PER <BR> AMM 20-50-11-910-801 STEPS 2. C. (1); D. TBL 210 AND BOEING DRAWING 115A2200. FLAG NOTES 7. AND 8. TOOL ID: ATS2267 DD: 02/2023;[03] REMOVED AND REPLACED BROKEN LOWER I/B END FAIRING ON PANEL 651FB PER AMM 20-50-11-910-801 STEPS 2. C. (1); D. TBL 210 AND BOEING DRAWING 115A2200. FLAG NOTES 7. AND 8.TOOL ID: ATS2267<BR>DD: 02/2023<BR>UPON FURTHER INVESTIGATION FOUND THE PANEL IS ACTUALLY 651FB;[04] VERIFIED CORRECTIVE ACTION 3 COMPLETED

Part: PANEL — ERODED (L/H WING) · airframe 70,697 hrs · 34,642 cycles

LT WING L/E PANEL 521WB HAS WIND EROSION ON FWD I/B CORNER (MARKED) / [01] PART/MATERIAL IDENTIFIED PER SRM 57-41-01-0I-4 FIG 2 TABLE 2 ITEM 1 .<BR>FOUND PANEL TO HAVE ADDITIONAL DAMAGE & PREVIOUS REPAIR REMOVED OUTER SURFACE FINISH & INNER SURFACE FOIL FOR FURTHER EVALUATION. PER SRM 57-41-01-1A-1 PARA 2. C.. STARTED DAMAGE REMOVAL AT FWD I/B CORNER IAW SRM51-70-05-2R-6 PARA 4 .STEPS A & B .;[02] DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-21-01-1A-1 PARAGRAPH4.A.(2).(A) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-6 PER SRM 57-41-01-2R-1 PARAGRAPH 2.F. COMPLETED REMOVING INNER EDGEBAND DAMAGE FROM A .625'X'33' LOCATED ON THE FORWARD INBOARD EDGE; TAPER SANDED AREA AND CLEANED AREA WITH NO DISBOND OR CONTAMINATION NOTED; WORK ACCOMPLISHED IAW SRM 51-70-05-2R-6 PARAGRAPH 4.A-D15] FABRICATED FOIL PLY FROM BMS8-289 LOT NUMBER 1484605-1; INSTALLED FOIL PLY WITH BMS5-128 LOT NUMBER JH1LAR7523; VACUUM BAGGED; VERIFIED 5X5 AND SET FOIL REPAIR TO CURE WITH THE HOTBONDER ID: NCX000523 DUE: 06/2023; WORK PERFORMED IAW SRM 51-70-14-2R-2 PARAGRAPH 4.A.(3-4); (5).(A) AND (11).(A-K).

Part: NONE — CRACKED (R/H WING) · airframe 70,697 hrs · 34,642 cycles

LOWER SURFACE OF #7 L/E SLAT NOSE SKIN IS CRACKED AT ACTUATOR RIB FASTENER HOLE. (MARKED) / [01] TRIMMED OUT THE DAMAGE PART OF THE SLAT NOSE SKIN; CUT OUT DIMENSIONS 6.4' X 3.0' IAW SRM 57-42-01-2R-8;[02] HFEC REQUEST AT THE EDGES OF THE CUT OUT AND OPEN HOLES WITHIN THE REPAIR AREA TO ENSURE NO OTHER DAMAGE EXIST;;[03] HFEC INSPECTED CUTOUT AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR><BR>HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16. <BR>NO CRACKS NOTED.<BR><BR><BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23<BR>-MINIMITE ID: IS000934 CAL DUE: 08/22;[04] VERIFIED CORRECTIVE ACTION #1;[05] FABRICATED REPAIR PARTS (1)DOUBLER 7075 T6 CLAD 0.071' LOT# 1478276-1; (2) FILLER 7075 T6 CLAD 0.063' LOT# 1375297-3 APPLIED CHEMICAL CONVERSION COATING IAW SRM 57-42-01-2R-8 FIG 202 ALTERNATIVE 1; OK TO PRIME;

Part: SUPPORT BEAM — BROKEN (R/H WING) · airframe 70,697 hrs · 34,642 cycles

RT WING T/E PANEL 661AB AFT SUPPORT BEAM IS BROKEN ON I/B END / [01] FOUND NO APPLICABLE SRM REPAIR FOR BROKEN RT WING ACCESS PANEL 661AB AFT SUPPORT BEAM; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9. REMOVED AND INSTALLED NEW SUPPORT BEAM PER SRM 51-40-02-0G-0 PARAGRAPH 4 AND PARAGRAPH 7. VERIFIED INSTALLATION FASTENERS PER AIPC 57-50-00-18 ITEM 115 (RIVET) AND AIPC 57-50-00-45 ITEM 125. (COLLARS) INSTALLED CABLE FAIRLEAD ON NEW SUPPORT BEAM PER AMM 20-50-11 TABLE 234. CALIBRATED TOOL USED: PER2271 DUE: 04/2023;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE

Part: PANEL — DELAMINATED (R/H WING) · airframe 70,697 hrs · 34,642 cycles

R/W L/E PANEL 621CB HAS CORNER DELAMINATION ON CORNER (MARKED) / [01] IDENTIFIED PANEL IAW SRM 57-41-01-0I-4 TABLE 5; FIG.5; ITEM 3. CORNER EROSION DAMAGE TO L/E IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A(5)(C) DAMAGE TO BE REPAIRED IAW SRM 51-70-05-2R-6 AS DIRECTED BY SRM 57-41-01-2R-1 PARA. 4.B (2) TABLE 202. REMOVED INNER SURFACE ALUMINUM FOIL IAW SRM 51-70-14-2R-3 PARA. 4.A(1)-(2)(B)&(E). FOIL TO INNER SURFACE WILL BE REPAIRED IAW SRM 51-70-14-2R-3. SANDED OUTER SURFACE IAW AMM 51-21-99-300-802 PARA 3.C.(1) REMOVED (2EA) BACKUP PLATES IAW SRM 51-40-02-0G-0 PARA 4(E).[05] FABRICATED REPAIR PLIES USING BMS5-129 TY2 LOT#1497186-1; BMS8-79 120 LOT#1493863-1; BMS8-79 1581 LOT#1495935-1 IAW SRM 51-70-05-2R-6 PARA 4.E;[07] FABRICATED AND INSTALLED MESH WITH BMS8-336 LOT#1360513-1 AND BMS 5-129 LOT#1481053-1 IAW SRM 51-70-14-2R-4 PARA 6.C-E;H;I;K(1-12). VACUUM BAGGED; LEAK CHECK GOOD USING VACUUM GAUGE ID:ATS2107 DUE:09/2022 AND CURED USING HOT BONDER ID:ATS532 DUE:06/2023; UNBAGGED; LIGHTLY SANDED AND CLEANED REPAIR AREA IAW SRM 51-70-05-2R-6 PARA 4.F;G&I.[13] INSTALLED FOIL PLY USING BMS8-289 LOT# 148605-1 AND RESIN BMS5-128 LOT# JH1LAR7523 AND VACUUM BAGGED; LEAK CHECKED GOOD USING VACUUM GAUGE ID: ATS2107 CAL DUE: 09/2022; AND CURED FOIL PLY USING THERMOMETER ID: ATS2208 CAL DUE: 10/2022 IAW SRM 51-70-14-2R-3 PARAGRAPH 4.A(2)(E)2-3)(3)-(5)(A)(1)(11)(A)-(L).

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 70,430 hrs · 34,479 cycles

L1 DOOR SLIDE COVER OPEN / [01] REPACK SLIDE PER AMM 25-66-01

Part: PANEL — DAMAGED · airframe 68,850 hrs · 33,602 cycles

PANEL 194E HAS ELONGATED HOLES. REMOVED AND REPLACED PANEL 194E PER AMM 53-51-21

Part: DOOR — LOOSE (R2 DOOR) · airframe 68,058 hrs · 33,166 cycles

AFT FLIGHT ATTENDANT REPORTS AFT SERVICE DOOR HANDLE APPEARS TO BE TOO LOOSE; AND DOES NOT STAY FULLY SEATED IN DOWN POSITION WHILE AIRBORNE. ; / [01] ADJUSTED AFT SERVICE DOOR FOR SOFT LATCH IAW AMM 52-41-00. OPS CHECKS NORMAL AT THIS TIME

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 67,752 hrs · 32,996 cycles

#1 EMERGENCY EXIT LIGHT INOP OVERWING SIDEWALL LIGHT. OK TO CONT PER MEL 33-2-03 SP1B. REMOVED AND REPLACED LH EMERG EXIT LIGHT FUSE ASSY IAW AMM 33-51-06 OPS CHECK GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,414 hrs · 32,804 cycles

LEFT EMERGENCY OVER WING EXIT LIGHT INOP. ; / [01] REMOVED AND REPLACED LH EMERGENCY OVER WING EXIT LIGHT FUSE REF AMM 33-21-00 OPS CHECK GOOD

Part: SUPPORT ROD — BROKEN (RT WING) · airframe 65,823 hrs · 31,927 cycles

RIGHT WING MOST INBOARD LOWER FIXED PANEL'S MOST INBOARD MOUNT POINT HAS ONE BROKEN AND ONE BENT SUPPORT RED. / REMOVED AND REPLACED BOTH MOST INBD SUPPORT RODS REF AMM 57-50*-02-400-801

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,823 hrs · 31,927 cycles

INTERIOR EMERGENCY EXIT LIGHT ABOVE THE R-2 DIIR HAS ONE BURNT OUT BULB. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BULB ABOVE R-2 DOOR, REF AMM 33-51-01. OPERATIONS CHECK GOOD.

Part: HANDLE — BROKEN (LT EMER EXIT) · airframe 65,823 hrs · 31,927 cycles

L/H OVERWING EXIT LIFT HANDLE IS BROKEN / REMVOED & REPLACED OVERWING EXIT LIFT HANDLE REF AMM 25-21-12

Part: TRACK — CRACKED (HORIZONTAL STAB) · airframe 65,400 hrs · 31,679 cycles

RT HORIZONTAL STAB UPPER REAR SPAR SLIDING SEAL TRACK IS CRACKED. / REMOVED AND REPLACED SLIDING SEAL TRACK AT RT HZONTAL STAB UPPER REAR SPAR AS PER REF B737-700 SRM 51-40-02-0G-0 ACCOMPLISHED STABILIZER ELECTRIC TRIM SYSTEM TEST; REF: AMM 27-41-00-700-803

Part: PIN — RECESSED (LIGHT CONNECTOR) · airframe 65,400 hrs · 31,679 cycles

LEFT SIDE EMERGENCY AISLE LIGHT (L1085) INOP BETWEEN SEAT ROW 11 & 12. PERFORMED T/S, FOUND RECESSED PIN ON GD-3744. RESECURED PIN AND PERFORMED EMERGENCY LIGHTS OPS TEST. FOUND NORMAL AT LIGHT L1085 BETWEEN ROW 11 & ROW 12 LEFT SIDE, AS PER REF B737 AMM 33-51-00-710-801.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 65,400 hrs · 31,679 cycles

JUST O/B OF LT WHEEL WELL AFT SPAR TOP ANGEL CRACKED MKD WING TO BODY FAIRING AREA PANEL 195CL / REMOVED AND REPLACED ANGLE OF LT WHEEL WELL AT AFT SPAR TOP WING TO BODY FAIRING IN REF B737-700 SRM 51-40-02-0G-0 AND DWG #115A2000

Part: WEB — DAMAGED (BS 500) · airframe 65,400 hrs · 31,679 cycles

FOUND DAMAGE WEB AT FWD CARGO COMP UNDER RT SIDE PLATE AT STA 500 / REMOVED AND REPLACED WEB AT FWD CARGO COMP. UNDER SIDE PLATE RT AT STA 500 IAW B-737-700 SRM 51-40-02-0G-0 AND DWG # 143A8122-2.

Part: FRAME — CRACKED (BS 400) · airframe 65,400 hrs · 31,679 cycles

SUSPECT FRAME CRACKED ON AFT SIDE AT RIVET HOLE BS 400 STR 8R. CUT-OUT DAMAGED AREA. PERFORMED HFEC INSPECTION. PERFORMED DVI AROUND DAMAGED AREA. FABRICATED FILLER, LAY OUT AND DRILLER, TRIME AND DRILLED NEW RAPAIR PART (P/N 1530809 AND P/N 1530812). TREATED AND PRIMED REPAIR PART AND INSTALLED, AS PER EA-1-A53-12114 REV 4; SRM 51-40-05-0G-0; AMM 51-21-72-370-804; NDT PART 6 51-00-00 PROC 23.

Part: FLOOR SUPPORT — CRACKED (BS 767-787) · airframe 65,400 hrs · 31,679 cycles

AFT CARGO COMPARTMENT LONGITUDINAL FLOOR SUPPORT CRACKED BETWEEN STA.767 AND STA.787 RBL25 / REMOVED DAMAGE LONGITUDINAL FLOOR SUPPORT AND INSTALLED NEW AT AFT CARGO COMPT. BETWEEN STA 767 TO STA 787 RBL 25' PER B737-700 SRM 51-40-02-0G-0 AND DWG # 146A8127

Part: CHANNEL — CRACKED (BS 500-500A) · airframe 65,400 hrs · 31,679 cycles

FWD CARGO COMPARTMENT RT SIDE WALL STA 500 TO 500A AT PANEL SUPPORT CHANNEL (Z CHANNEL) HAS CRACK. DOT 82-032. REMOVED & REPLACED NEW SUPPORT CHANNEL (Z CHANNEL) AT STA 500 TO 500A FWD CARGO COMPARTMENT, IAW SRM 51-40-02-0G-0 AND DWG 143A0080.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 65,400 hrs · 31,679 cycles

FWD CARGO DOOR FWD CORNER SCUFF PLATE CRACKED. / FWD CARGO DOOR FWD CORNER SCUFF PLATE WELD REPAIRED PER SRM 53-30-15-2R-1.

Part: ANGLE — CRACKED (BS 270) · airframe 65,400 hrs · 31,679 cycles

COCKPIT FLOOR PANEL 211AF AFT ATTACH FLANGE HAS A CRACK BS 270 LBL 8.5. TRIMMED OUT DAMAGE AREA AT LATERAL INTERCOSTAL BS 270 LBL 8.5. FABRICATED-1 REPAIR ANGLE MAT USED BAC 1490-2738 7075 T6. FABRICATED-2 TAPERED FILLERS MAT USED 7075 T6 .063' AND INSTALLED REPAIR PARTS, PER REF RES NR 2016182-2 AND EA NO: 20-153-01600 REV IR.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 65,400 hrs · 31,679 cycles

AFT CARGO AFT CORNER SCUFF PLATE IS CRACKED ON THE UPPER SURFACE EDGE. DOT 82-029. / AFT CARGO COMPARTMENT AFT CORNER SCUFF PLATE WELD REPAIRED PER SRM 53-60-15-2R-1.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 65,400 hrs · 31,679 cycles

CRACK INDUCTION FOUND AT HORIZONTAL PRESSURE WEB AT STA 663 + 1''; RBL 41. APPROXIMATE LENGTH OF CRACK: 0.591''. ACCOMPLISHED REPAIR AT HORIZONTAL PRESSURE DECK WEB ON RT BETWEEN STA 663.75 AND STA 675 FROM RBL 38 TO RBL 60, REF B737-700 SRM 53-40-51-2R-2 FIG 202 TABLE 201.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 65,400 hrs · 31,679 cycles

RT HORIZONTAL STAB NR 5 RIB AT STA 129.50 HAS A CRACK AT NR 2 STIFFENER LOWER END. ACCOMPLISHED PERMANENT REPAIR AT RT HORIZONTAL STAB NR 5 RIB STA 129.50 STIFFENER NO 2, PER REF B737 SRM 55-10-09-2R-5.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 65,400 hrs · 31,679 cycles

RT HORIZONTAL STAB RIB NR 5 STA 129.50 HAS A CRACK AT NR 3 STIFFENER LOWER END. INSTALLED REPAIR PARTS AT RT HORIZONTAL STAB RIB NR 5 STA 129.50 STIFFENER NR 3 REPAIR 4, PER B737-700 SRM 55-10-09-2R-4.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 65,400 hrs · 31,679 cycles

CENTER CABIN RT CENTER FLOOR PANEL 242AF HAS PEELED FIBERS ON INBOARD SIDE. DOT 124 059. RECEIVED PANEL NR 242AF TO BE INSTALLED ON T/C JPANEL-231-CLOSE.

Part: NUT PLATE — BENT (BS 178 BULKHEAD) · airframe 65,400 hrs · 31,679 cycles

STA. 178 PRESSURE BULKHEAD FWD SIDE - LOWER TWO RADOME ATTACHMENT FITTING NUT PLATES HAVE BENT OR BROKEN NUT TABS. [DOT 124-062] / REMOVED AND REPLACED NUT PLATES AT STA 178 PRESSURE BULKHEAD FWD SIDE LOWER IAW B-737-700 SRM 51-40-02-0G-0

Part: FLOOR PANEL — PULLED (CABIN) · airframe 65,400 hrs · 31,679 cycles

CENTER CABIN CENTER FLOOR PANEL 231XF HAS PEELED UPPER SURFACE FIBERS. DOT 124-056. RECEIVED PANEL 231XF TO BE INSTALLED ON T/C JPANEL-231-CLOSE.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 65,400 hrs · 31,679 cycles

CENTER CABIN CENTER FLOOR PANEL 241AF HAS PEELED UPPER SURFACE FIBERS. DOT 124-057. RECEIVED PANEL 241AF TO BE INSTALLED ON T/C JPANEL 231-CLOSE.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 65,400 hrs · 31,679 cycles

CENTER CABIN RT FLOOR PANEL 242SF HAS PEELED FIBERS ON INBOARD SIDE. DOT 124 060. RECEIVED PANEL NR 232SF TO BE INSTALLED ON T/C JPANEL 231-CLOSE.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 65,400 hrs · 31,679 cycles

CENTER CABIN CENTER FLOOR PANEL 241DF HAS PEELED UPPER SURFACE FIBERS. DOT 124-058. RECEIVED PANEL 241DF TO BE INSTALLED ON T/C JPANEL-231-CLOSE.

Part: CHANNEL — CORRODED (BS 259-270) · airframe 65,400 hrs · 31,679 cycles

CORROSION, FLIGHT DECK FLOOR STRUCTURE UNDER PANEL 211AF WITH CORROSION ON UPPER SURFACE OF INTERCOSTAL SUPPORT CHANNEL AT BL-0 FROM BS 259.5 TO BS 270. REMOVED AND REPLACED INTERCOSTAL SUPPORT CHANNEL AT FLIGHT DECK FLOOR UNDER PANEL NR 211AF BL-0 FROM BS 259.5 TO BS 270, PER REF B737-700 SRM 51-40-02-0G-0; B737-700 SRM 51-40-05-0G-0 AND DWG 141A5210.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 65,400 hrs · 31,679 cycles

GROUND POWER RECEPTICLE CUTOUT HAS A CRACK ON THE FWD SIDE. / GROUND POWER RECEPTICLE DOUBLER REMOVED & REPLACED REF. B737-700 SRM 51-40-02-0G-0 & DRAWING NO # 141A3702.

Part: SUPPORT BRACKET — CRACKED (RT A/C BAY) · airframe 65,376 hrs · 31,665 cycles

RIGHT PACK BAY FWD DUCT; SUPPORT BRACKET IS CRACKED AT MOUNT POINT. / REMOVED AND REPLACED DUCT SUPPORT BRACKET REF AMM 36-13-01

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 65,235 hrs · 31,584 cycles

LIGHT LENS HANGING DOWN FROM CEILING AT FLIGHT DECK DOOR. (F/A ALERT LIGHT LENS) / (PER CLOSING DMA #0152337) CL #45903 R&R LIGHT PLATE ASSY AND RE SECURED LENS PER M/M 33-51-01

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 65,235 hrs · 31,584 cycles

LIGHT LENS HANGING DOWN FROM CEILING AT FLIGHT DECK DOOR. (F/A ALERT LIGHT LENS) / (PER CLOSING DMA #0152337) CL #45903 R&R LIGHT PLATE ASSY AND RE SECURED LENS PER M/M 33-51-01

Part: PUMP — FAILED (HYD SYSTEM) · airframe 64,634 hrs · 31,216 cycles

DECLARED EMERGENCY-------------------------------------------------------#1 ENGINE DRIVEN HYDRAULIC PUMP FAIL. / R&R #1 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM.

Part: LIGHT — INOPERATIVE (AFT EXTERIOR) · airframe 64,627 hrs · 31,210 cycles

AFT ENTRY EXTERIOR EMERGENCY LIGHT INOPERATIVE. / R&R LIGHT PER AMM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 64,229 hrs · 30,957 cycles

L/H EMERGENCY LIGHT COVER BROKEN UNDER L/H OVERWING EXIT. R&R COVER PER AMM.

Part: INTERCOSTAL — CRACKED (BS 540) · airframe 64,140 hrs · 30,905 cycles

FORWARD CARGO DISTRIBUTION BAY INTERCOSTAL CRACKED AT BS. 540, L/H OF BL 0. / R&R INTERCOSTAL PER SRM.

Part: BRACKET — CRACKED (L/H WING) · airframe 64,140 hrs · 30,905 cycles

LEFT WING FIXED UPPER TRAILING EDGE PANEL BETWEEN #5 AND #6 SPOILER; SEAL RETAINER BRACKET CRACKED. / REMOVED AND REPLACED SEAL RETAINER BRACKET IAW SRM 5-40-02

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 64,140 hrs · 30,905 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. / R&R BATTERY PER AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 64,140 hrs · 30,905 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 64,140 hrs · 30,905 cycles

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

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 63,326 hrs · 30,389 cycles

SLIDE FELL OUT OF HOUSING. RE-INSTALLED SLIDE INTO HOUSING PER MT 725-61-06.

Part: HOOK AND LOOP — LOOSE (EMERGENCY EXIT) · airframe 62,167 hrs · 29,625 cycles

RT EMERGENCY EXIT HANDLE COVER HOOK AND LOOP LOOSE. SECURED COVER HOOK AND LOOP PER SIP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,076 hrs · 28,962 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT AFT INOP. RELAMPED LIGHT IAW AMM.

Part: COVER — CRACKED (HORIZONTAL STAB) · airframe 61,010 hrs · 28,915 cycles

TRACK ASSY SLIDING SEAL COVER HAS CRACK (PN 181A8060-15) / REMOVED AND REPLACED LH UPPER FWD SLIDING SEAL TRACK ASSY; P/N 181A8060-15; PER SOPM 20-50-01 AND DRAWING 181A8050.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 61,010 hrs · 28,915 cycles

FORWARD CARGO DOOR CUTOUT. LOWER FWD CORNER SCUFF PLATE CRACKED / RECEIVED NEW PRE-DRILLED FWD CARGO FWD CORNER SCUFF PLATE MPN# 143A8331-3 SI# 7530028 P.O. #717532 RECEIPT #5076795. PART TO BE INSTALLD ON CUSTOMER CARD #753-140-00-01Y

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 61,010 hrs · 28,915 cycles

RT HORIZONTAL LEADING EDGE RIB CRACKED AT FASTENER HOLE AT LEADING EDGE STAB STA 95. R&R RIB IAW SRM AND DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO TEE SPLICE CORRODED BETWEEN BS 767 TO BS 787, BETWEEN LBL 21 TO RBL 21. R&R TEE SPLICE IAW SRM & DWG.

Part: SKIN — CORRODED (EMPENNAGE) · airframe 61,010 hrs · 28,915 cycles

***CORROSION*** MULTIPLE SPOTS OF CORROSION AROUND APU INLET AT BS 1088 BULKHEAD / REMOVE CORROSION AND REPAIRED THE APU INLET STA 1018 PER ATS ER 18-06071 REV IR AND SWA EA 1-753-33882 REV IR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

DOUBLER CROWN SKIN CORRODED BETWEEN BS 1037 TO BS 1041, BETWEEN STR 2R TO STR 2L. REPAIRED SKIN IAW ER AND EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

VERTICAL STABILIZER WIRING HARNESS SUPPORT ANGLE CORRODED AT BS 1036, BETWEEN STR 2R TO STR 2L. REPAIRED ANGLE IAW ER AND EA.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

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

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

SKIN DAMAGED AT BS 453.5, STR 28L. REPAIRED SKIN IAW SRM.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

FORWARD CARGO INTERCOSTAL DAMAGED BETWEEN BS 500A TO BS 500B, RBL 24. R&R INTERCOSTAL PER SRM, ER, & EA.

Part: WEB — CORRODED (ASD THRESHOLD) · airframe 61,010 hrs · 28,915 cycles

*CORROSION* L-2 DOOR CUT OUT LOWER MAIN SILL WEB HAS CORROSION AROUND FASTENER HOLES STA. 951.07 TO 992.80 WL 208 / REPAIRED L-2 DOOR CUT OUT LOWER MAIN SILL STA 951.07 TO STA 992.8; WL 209 PER ATS ER 18-05773 REV IR AND SWA EA 1-753-33863 REV IR.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

FRAME DAMAGED AT BS 887, BETWEEN STR 4R TO STR 5R, UNDER GROUND BLOCK LOCATION. REPAIRED FRAME IAW ER AND EA.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 61,010 hrs · 28,915 cycles

LT HORIZONTAL STABILIZER FLANGE AT STAB STA 120.3, BELOW NR 4 STIFFENER CRACKED. REPAIRED #4 STIFFENER IAW SRM.

Part: SKIN — CORRODED (AFT FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

***CORROSION*** ON EXTERNAL SKIN UNDER VERTICAL STAB 1013-1093 BETWEEN STR 3L-3R / CORROSION WAS FOUND ON EXTERNAL SKIN STA. 1016-1088; STR. 3L-3R IN AREA OF 78.0'L X 30.0'W X .005'D FOUND IN LIMITS PER SRM 53-00-01-1A-1; FIG. 103; DET. C+D. AREA @ STA. 1030-1041 STR. 2L-2R EXCEEDS .10' AROUND EXISTING DOUBLER. NO DAMAGE PERMITTED PER SRM 53-00-01-1A-1 FIG 103 DET. IV. REPAIRED SKIN @ STA. 1016-1088 PER ER# 18-06120 REV IR AND EA# 1-753-33912 REV IR

Part: FRAME — DAMAGED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

FRAME FACE DAMAGED AT BS 706, BETWEEN STR 4L TO STR 5L. REPAIRED FRAME IAW ER, EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

FRAME WEB DAMAGED FORWARD SIDE AT BS 887, STR 16L. R&R WEB IAW SRM, ER, AND EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

FRAME WEB FORWARD SIDE DAMAGED AT BS 685, BETWEEN STR 6R TO STR 7R. REPAIRED FRAME IAW ER, EA.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

FRAME FACE DAMAGED AT BS 807, BETWEEN STR 5R TO STR 6R. R&R FRAME IAW ER AND EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO SIDEWALL ATTACH ANGLE CORRODED AT BS 727D, RBL 26. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO BULKHEAD SUPPORT ANGLE CORRODED AT BS 947.5, BETWEEN RBL12 TO LBL 10. R&R ANGLE IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO TOP OF FLOOR TRACK CORRODED BETWEEN BS 787 TO BS 867, RBL 13. R&R FLOOR TRACK ASSEMBLY IAW SRM & DWG.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 61,010 hrs · 28,915 cycles

RT HORIZONTAL STABILIZER RIB AT STA 111.1 NR 4 STIFFENER CRACKED. R&R STIFFENER IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO TOP OF INTERCOSTAL CORRODED BETWEEN BS 747 TO BS 767, RBL 22. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 61,010 hrs · 28,915 cycles

LT HORIZONTAL STAB RIB NR 2 STIFFENER CRACKED AT STA 120.30. REPAIRED STIFFENER PER SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO FLOOR TOP OF TRACK CORRODED AT BS 932, RBL 13. R&R FLOOR TRACK IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO FLOOR TOP OF TRACK CORRODED AT BS 932, LBL 3. R&R FLOOR TRACK IAW SRM AND DWG.

Part: TEAR STRAP — CORRODED (AFT FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

PASSENGER CABIN; STA 727 BETWEEN S1L TO S3L; HAS SIGNS OF CORROSION. AT SEAM BETWEEN FRAME SHEAR TIE AND TEAR STRAP. / REMOVED CORROSION ON FAIL SAFE STRAP AT STA. 727 BETWEEN STR 1L TO STR 3L BETWEEN FRAME SHEAR TIE AND TEAR STRAP L4.0' X W.5' REMAINING MATERIAL THICKNESS IS .048' REPAIRED AFFECTED AREA ON FAIL SAFE STRAP BY BLENDING IAW EA 18-05969 REV IR AND EA 1-753-33833 REV IR

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

FORWARD CARGO RH FLOOR TO SIDEWALL Z CHANNEL CORRODED BETWEEN BS 500A TO BS 500D. R&R SUPPORT IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

AFT CABIN WL208, FLOORBEAM CORRODED AT BS 986.5, RBL 43. R&R FLOORBEAM CAP IAW SRM, ER, AND EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

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

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 61,010 hrs · 28,915 cycles

FLOORBOARD 221GF HAS DAMAGE TO UPPER AND LOWER SURFACES; FWD EDGE / FLOOR BOARD 221GF DAMAGE TO UPPER AND LOWER SURFACES; FWD EDGE REPAIRED IAW SRM 53-00-50-2R-1. PRIOR TO REPAIR DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4 F DELAMINATIONS NOT PERMITTED.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

FORWARD CARGO FLOOR TO SIDEWALL SHIELD CORRODED AT BS 506, RBL 24. R&R SHIELD IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 61,010 hrs · 28,915 cycles

LT HORIZONTAL STABILIZER RIB NR 3 STIFFENER CRACKED AT STAB STA 120.3. REPAIRED STIFFENER IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO DOOR SUB THRESHOLD WEB CORRODED BETWEEN BS 805 TO BS 820. R&R WEB IAW SRM AND DWG.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 61,010 hrs · 28,915 cycles

RT HORIZONTAL STABILIZER RIB AT STAB STA 111.1, NR 3 STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

FORWARD PIT AFT BULKHEAD ATTACH ANGLE CORRODED BETWEEN RBL 24 TO LBL 24. R&R ANGLE IAW SRM AND DWG.

Part: WEB — CORRODED (CABIN) · airframe 61,010 hrs · 28,915 cycles

***CORROSION*** AFT CABIN WL208; STA. 1016;LBL 5 FASTENER HAS EVIDENCE OF CORROSION. ( MARKED) / CORROSION @ BS 1016 WL 208 SHEAR WEB LBL 5 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS FOUND IN SRM ALLOWABLE DAMAGE. REPAIRED DAMAGE IAW ER 18-05702 REV IR AND EA 1-753-33825 REV IR

Part: WEB — CORRODED (FWD CARGO THRESH) · airframe 61,010 hrs · 28,915 cycles

***CORROSION*** FWD CARGO DOOR CUTOUT SUB THRESHOLD WEB HAS CORROSION STA 443-490 / CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1. REMOVED AND REPLACED FWD CARGO SUB THRESHOLD WEB IAW SRM 51-40-02-0G-0 AND BOEING DRAWING 143A8120. 92679U 12-8-18

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 61,010 hrs · 28,915 cycles

LT HORIZONTAL STAB LEADING EDGE SEGMENT 331BZ INBOARD END BAY RIB ANGLE CRACKED AT LOWER TRAILING EDGE END. R&R RIB IAW SRM AND DWG.

Part: NONE — CORRODED (AED THRESHOLD) · airframe 61,010 hrs · 28,915 cycles

**CORROSION** L2 DOOR INNER CHORD CORRODED IN SEVERAL SPOTS WL 208; STA. 967-992. (MARKED) / EVALUATED CORROSION ON L2 DOOR INNER CHORD STA 967-992 WL 208 FOUND DAMAGE AROUND NUMEROUS FASTENER HOLES FOUND TO BE OUT OF LIMITS IAW SRM 57-70-15-1A-1 FIG 103 DETAIL. INSTALLED EWIS PROTECTION IAW AMM 20-60-07-913-801. REMOVED INNER CHORD IAW SRM 51-40-02-0G-0 LOCATED & DRILLED NEW INNER CHORD ITEM # 7530247 PO# 714419 IAW SRM 40-05-0G-0. INSTALLED NEW INNER CHORD IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A8501. REMOVED EWIS IAW 20-60-07-913-801

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

L1 DOOR CUTOUT AFT GIRT BAR SUPPORT BRACKET CORRODED. R&R BRACKET IAW SRM AND DWG.

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 61,010 hrs · 28,915 cycles

HORIZONTAL STIFFENER CRACKED STA. 663 FROM RBL 7 TO RBL 30 WL 155 PART# (111A1301-6) / REMOVED AND REPLACED DAMAGED HORIZONTAL STIFFENER @ STA 663 RBL7 TO RBL30 WITH NEW PO# 717075 PER SRM 51-40-05 SRM 51-40-02 AND DWG 111A1000

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 61,010 hrs · 28,915 cycles

ATTACHED ANGLE CRACKED BS 663, RBL 7. REPAIRED ANGLE IAW SRM & EA.

Part: TRACK — CORRODED (CABIN) · airframe 61,010 hrs · 28,915 cycles

***CORROSION*** R/H SEAT TRACK CROWN HAS CORROSION AT STATION 705 RBL 24 / SEAT TRACK TO BE REPLACED ON CUSTOMER CARD #175397.

Part: PLATE — CRACKED (RT WING) · airframe 61,010 hrs · 28,915 cycles

R/H WING TRAILING EDGE PANEL 651GB WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

SEAT TRACK CROWN CORRODED AT BS 691, LBL 24. R&R SEAT TRACK CROWN IAW SRM AND DWG.

Part: TRACK — CORRODED (CABIN) · airframe 61,010 hrs · 28,915 cycles

***CORROSION*** R/H SEAT TRACK CROWN HAS PITTING AT STATION 673 RBL 24 / SEAT TRACK TO BE REPLACED ON CUSTOMER CARD #175397

Part: TRACK — CORRODED (CABIN) · airframe 61,010 hrs · 28,915 cycles

***CORROSION*** R/H SEAT TRACK CROWN HAS PITTING AT STATION 723 RBL 24 / SEAT TRACK TO BE REPLACED ON CUSTOMER CARD #175397

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS 847 TO BS 855, STR 25R. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

SEAT TRACK CROWN CORRODED AT BS 645, RBL 45. R&R SEAT TRACK SECTION IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

SEAT TRACK CROWN CORRODED AT BS 661, LBL 45. R&R SEAT TRACK CROWN IAW SRM AND DWG.

Part: BEAM — CRACKED (FSD) · airframe 61,010 hrs · 28,915 cycles

REMOVE AND REPLACE R1 SERVICE DOOR DUE TO CRACKS IN #4 AND #5 BEAMS / REMOVED AND REPLACED R1 SERVICE DOOR IAW AMM 52-41-00 PERFORMED DOOR WORNING SYSTEM ADJUSTMENT IAW 52-71-11 ALL TEST GOOD (POS: R1; TAG NO: 490177; P/N OFF:141A6516-8; S/N OFF:000524; P/N ON:141A6516-18; S/N ON: 001692)

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO DOOR CUT OUT; FWD LOWER CORNER SCUFF PLATE CRACKED / LOCATED AND DRILLED NEW SCUFF PLATE; AFT CARGO FWD LOWER CORNER SCUFF PLATE. MPN 7530659 IAW B737 SRM 51-40-02-0G-0 STEP 2D 1; 2 FIG 1.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 61,010 hrs · 28,915 cycles

LT VAPOR BARRIER CRACKED AT BS 663. REPAIRED BARRIER PER SRM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 61,010 hrs · 28,915 cycles

RT VAPOR BARRIER CRACKED AT BS 663. REPAIRED BARRIER IAW SRM.

Part: GUSSET — CRACKED (FWD CARGO LH) · airframe 61,010 hrs · 28,915 cycles

FWD. CARGO; STA 500D; S19L HAS CRAKED GUSSET (MARKED) / REMOVED AND REPLACED FWD CARGO GUSSET AT STA 500D STR 19L PER SPM 51-40-02-0G-0 AND BOEING DWG# 143A7902 92389U 12/10/18

Part: BEAM — CRACKED (FSD) · airframe 61,010 hrs · 28,915 cycles

FORWARD SERVICE DOOR; #4 LOWER 141A6536-14 BEAM IS CRACKED IN THE INBOARD UPPER RADIUS. / FWD. SERVICE DOOR TO BE REPLACED ON CARD N175349

Part: GUSSET — CRACKED (FWD CARGO RH) · airframe 61,010 hrs · 28,915 cycles

FWD. CARGO; STA 500D; S19R HAS CRAKED GUSSET (MARKED) / REMOVED AND REPLACED FWD CARGO GUSSET AT STA 500D STR 19R PER SPM 51-40-02-0G-0 AND BOEING DWG# 143A7902 92385U 12/10/18

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

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

Part: PLATE — CRACKED (LT WING) · airframe 61,010 hrs · 28,915 cycles

LT WING LOWER TRAILING EDGE WIGGLE PLATE CRACKED AT REAR SPAR STA 261. R&R WIGGLE PLATE PER SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO COMPARTMENT FORWARD SHIELD CORRODED BETWEEN BS 767 TO BS 792, RT. R&R SHIELD IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

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

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

R1 DOOR CUT OUT FORWARD LOWER STUB BEAM CRACKED AT BS 294, STR 17R. REPAIRED STUB BEAM IAW ER AND EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO COMPARTMENT RT FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED BETWEEN BS 807+4 TO BS 887. R&R SUPPORT IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

L1 DOOR LOWER CUTOUT INNER CHORD CORRODED AT BS 328, LBL 60. R&R CHORD IAW SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO COMPARTMENT AFT SHIELD CORRODED BETWEEN RT BS 847 TO BS 637. R&R SHIELD IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO COMPARTMENT LT FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED BETWEEN BS 727B TO BS 847. R&R SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, RBL 30. R&R INTERCOSTAL PER SRM AND DWG.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

INTERCOSTAL DAMAGED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL IAW DWG & SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 61,010 hrs · 28,915 cycles

AFT CARGO COMPARTMENT RT FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED BETWEEN BS 727B TO BS 767. R&R SUPPORT IAW SRM AND DWG.

Part: FITTING — BROKEN (RIGHT WING) · airframe 61,010 hrs · 28,915 cycles

*RIGHT WING* BROKEN ATTACHED FITTING LOCATED AT LOWER REAR SPAR ABOUT STA IRSS 210. / REMOVED AND REPLACED BROKEN ATTACH FITTING ON RH WING LOWER REAR SPAR APPROX IRSS 210 PER SRM 51-40-02-0G-0 AND DRAWING 115A2001

Part: BRACKET — CRACKED (RIGHT WING) · airframe 60,260 hrs · 28,445 cycles

INBD SHELF OTBD ANGLE BRACKET CRACKED. / REMOVED AND REPLACED WITH NEW BRACKET PER SRM 5140-02

Part: RIB — CRACKED (RIGHT WING) · airframe 60,260 hrs · 28,445 cycles

RIGHT WING DEFLECTION RIB UPPER ATTACH POINT TO FIXED PANEL CRACKED / REMOVED AND REPLACED PER SRM 57-51-02-2R.

Part: BRACKET — CRACKED (WHEEL WELL RH) · airframe 60,260 hrs · 28,445 cycles

RIGHT GEAR WHEEL WELL UPPER FIXED PANEL BRACKET CRACKED ABOVE # 2 AFT BOOST PUMP / REMOVED AND REPLACED RH GEAR WELL UPPER PANEL BRACKET I.A.W. SRM 51-40-02

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 59,742 hrs · 28,131 cycles

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

Part: ENGINE — FAULTY (LEFT) · airframe 59,355 hrs · 27,896 cycles

ON CLIMB OUT NR 1 ENGINE OIL QUANTITY DROPPED TO 20% THEN WENT BETWEEN 22 TO 34% UNTIL LEVEL OFF AT ALTITUDE, THE OIL QUANTITY RETURNED TO NORMAL. R&R NR 1 ENGINE PER MT.

Part: ELECTRONIC UNIT — FAULTY (NR 1 ENGINE) · airframe 59,355 hrs · 27,896 cycles

ON CLIMB OUT NR 1 ENGINE OIL QUANTITY DROPPED TO 20% THEN WENT BETWEEN 22 TO 34% UNTIL LEVEL OFF AT ALTITUDE, THE OIL QUANTITY RETURNED TO NORMAL. R&R NR 1 DISPLAY ELECTRONIC UNIT PER AMM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 58,739 hrs · 27,544 cycles

LEFT EMERGENCY EXIT SIDEWALL LIGHT LENS CRACKED. R&R LENS IAW SIP.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 58,576 hrs · 27,452 cycles

L2 DOOR EMERGENCY SLIDE LOW PRESSURE. R & R THE SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,317 hrs · 27,314 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT AFT INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — MISSING (CABIN) · airframe 58,167 hrs · 27,227 cycles

EMERGENCY EXIT LIGHT NOT ARMED LIGHT MISSING. INSTALLED LIGHT IAW SWPM.

Part: COMPRESSOR BLADE — TORN (NR 2 ENGINE) · airframe 57,895 hrs · 27,064 cycles

DIVERSION, LEVELING AT FL 340 WE FELT A SHUDDER AND TWO POPS. THE NR 2 ENGINE N1 ROLLED BACK TO 53% AND THE EGT, FUEL FLOW & N2 DECREASED. FOUND COMPRESSOR BLADES TORN. R&R NR 2 ENGINE PER MT.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 57,585 hrs · 26,877 cycles

WHEN LEVELING OFF AT FL 390, EXPERIENCED A NR 2 ENGINE COMPRESSOR STALL WITH THRUST LEVEL AT CRUISE. DIVERTED. R & R THE NR 2 ENGINE HYDRO MECHANICAL UNIT IAW MT.

Part: LIGHT — LOOSE (CABIN) · airframe 56,044 hrs · 25,964 cycles

LT OVERWING EXIT LIGHT LOOSE. R&R LIGHT ASSY PER MM.

Part: LENS — DEFECTIVE (EXIT SIGN) · airframe 55,018 hrs · 25,355 cycles

R1 DOOR LOWER EMERGENCY EXIT SIGN LENS MISSING DIRECTIONAL ARROW. R&R LENS IAW AMM.

Part: LENS — DEFECTIVE (EXIT SIGN) · airframe 55,018 hrs · 25,355 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN LENS MISSING DIRECTIONAL ARROW. R&R LENS IAW AMM.

Part: LENS — DEFECTIVE (EXIT SIGN) · airframe 55,018 hrs · 25,355 cycles

L2 DOOR EXIT SIGN COVER LENS MISSING ARROW. R&R LENS IAW AMM.

Part: LENS — DEFECTIVE (EXIT SIGN) · airframe 55,018 hrs · 25,355 cycles

R2 DOOR EXIT SIGN COVER LENS MISSING ARROW. R&R LENS IAW AMM.

Part: RIB — CRACKED (LT WING) · airframe 54,411 hrs · 25,018 cycles

LEFT WING NR 1 SLAT LEADING EDGE LOWER AT ACTUATOR RIB CRACKED. R & R NR 1 SLAT IAW AMM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 54,411 hrs · 25,018 cycles

FORWARD CARGO DOOR CUTOUT CENTER SCUFF PLATE CRACKED AT AFT END. R&R SCUFF PLATE IAW AMM & EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,411 hrs · 25,018 cycles

RT WING NR 8 SLAT LEADING EDGE LOWER NOSE SKIN AT ACTUATOR RIB CRACKED AT STA 451.9. REPAIRED NR 8 SLAT IAW SRM.

Part: ATTACH FITTING — CRACKED · airframe 54,258 hrs · 24,921 cycles

KEEL BEAM ACCESS PANEL 192E LT & RT FORWARD ATTACHMENT FITTINGS CRACKED. R & R THE ATTACH FITTINGS IAW SRM.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,730 hrs · 24,077 cycles

RIGHT WING TE OTBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,065 hrs · 23,693 cycles

LEFT BULLNOSE EMER LIGHTS INOPERATIVE, BETWEEN ROW 5 - 9. R & R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,065 hrs · 23,693 cycles

RIGHT BULLNOSE EMER LIGHTS INOPERATIVE, BETWEEN ROW 11 - 13. R & R LIGHT ASSEMBLY IAW AMM.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 49,088 hrs · 22,074 cycles

AIR TURN BACK, NR 2 PACK TRIPPED WILL NOT RESET. R & R NR 2 ACM IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,744 hrs · 21,870 cycles

LEFT EMER OVERWING EXIT HATCH LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 47,872 hrs · 21,380 cycles

R2 DOOR EMER EVAC OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 47,872 hrs · 21,380 cycles

L2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 47,872 hrs · 21,380 cycles

RIGHT OVERHEAD EMER LIGHT INOPERATIVE AT ROW 11. R & R BATTERY CHARGER IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 47,872 hrs · 21,380 cycles

RIGHT OVERHEAD EMER LIGHT INOPERATIVE AT ROW 8. R & R BATTERY CHARGER IAW AMM.

Part: LENS — BROKEN (EXTERIOR LIGHT) · airframe 47,872 hrs · 21,380 cycles

RIGHT WING EXTERIOR EMER EXIT DOOR LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

BULKHEAD FITTING CRACKED AT BS 1016 BETWEEN STRINGER 2R TO 6R AT 12 O'CLOCK POSITION. REPAIRED FITTING IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

RIGHT FLIGHT DECK NR 1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER. REPAIRED FRAME IAW ACO.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

BULKHEAD OTBD BOLT HOLE FITTING DAMAGED AT BS 1016 STRINGER 2L. REPAIRED FITTING IAW SI.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

BULKHEAD INBD BOLT HOLE FITTING DAMAGED AT BS 1016 STRINGER 2L. REPAIRED FITTING IAW SI.

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 47,872 hrs · 21,380 cycles

RIGHT EMER EXIT HATCH PULL HANDLE LOOSE. SECURED HANDLE IAW SOPM.

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 47,872 hrs · 21,380 cycles

LEFT EMER EXIT HATCH PULL HANDLE LOOSE. SECURED HANDLE IAW SOPM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 47,872 hrs · 21,380 cycles

CABIN FLOOR PANEL 221AF DELAMINATED ON AFT INBD CORNER. REPAIRED FLOOR PANEL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FRAME CRACKED AT BS 480 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FLOOR PANEL 242BF DAMAGED AT FWD & AFT LT CORNERS. R & R FLOOR PANEL IAW DWG & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

LEFT NR 1 FLIGHT DECK WINDOW FRAME CRACKED AT UPPER OTBD CORNER. REPAIRED FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

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

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

AFT LT FLOOR PANEL 242CF DAMAGED AT CORNERS. R & R PANEL IAW DWG & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FRAME CRACKED AT BS 867 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FORWARD LT FLOOR PANEL 242CF DAMAGED AT CORNERS. R & R PANEL IAW DWG & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

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

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FLOOR PANEL 231ZF DAMAGED AT AFT RT CORNER & ALONG FWD EDGE. R & R FLOORBOARD IAW DWG & EA.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FLOOR PANEL 241FF DAMAGED AT AREA ALONG EDGES. R & R FLOOR PANEL IAW DWG & EA.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

AFT RT FLOOR PANEL 242CF DAMAGED AT CORNERS. R & R PANEL IAW DWG & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

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

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FLOOR PANEL 241CF DAMAGED AT AREAS ALONG EDGES. REPAIRED FLOOR PANEL IAW DWG.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FLOOR PANEL 231YF DAMAGED AT AREAS ALONG EDGES. R & R FLOOR PANEL IAW SRM & DWG.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FLOOR PANEL 241EF DAMAGED. R & R FLOOR PANEL IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

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

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FLOOR PANEL 232SF DAMAGED AT AFT LT CORNER & ALONG FWD EDGE. R & R FLOORBOARD IAW DWG & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FRAME CRACKED AT BS 380 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FLOOR PANEL 242AF DAMAGED AT AFT LT CORNER. REPAIRED FLOOR PANEL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

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

Part: ANGLE — CRACKED (RT WING) · airframe 47,872 hrs · 21,380 cycles

RIGHT WING FIXED TE UPPER PANEL, SEAL RETAINER ANGLE CRACKED JUST AFT OF PYLON. R & R ANGLE IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 47,872 hrs · 21,380 cycles

LEFT WING WAFFLE PLATE CRACKED INBD OF NR 1 PYLON STATION RSS 260. R & R PLATE IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 47,872 hrs · 21,380 cycles

RIGHT WING WAFFLE PLATE CRACKED INBD OF NR 1 PYLON STATION RSS 260. R & R PLATE IAW SRM.

Part: WEB — CRACKED (LT WING) · airframe 47,872 hrs · 21,380 cycles

LEFT WING TRANSVERSE WEB CRACKED JUST INBD OF MAIN FLAP PROGRAM ROLLER ATTACH ANGLE. R & R WEB IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

INTERCOSTAL CORRODED BETWEEN BS 986 TO 1006, STRINGER 19L. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

RIGHT AFT PRESS BULKHEAD INTERCOSTAL CRACKED AT BS 1016. R & R INTERCOSTAL IAW ER & EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 47,872 hrs · 21,380 cycles

RIGHT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED ON THE LOWER END OF IN SPAR RIB CRACKED AT STATION 92.70. REPAIRED RIB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

RIGHT NR 3 WINDOW FRAME HOLE AT EF POST 2ND HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

LEFT NR 3 EF WINDOW POST CRACKED AT 2ND HOLE FROM BOTTOM. REPAIRED POST IAW ACO.

Part: PANEL — CORRODED (CARGO BAY) · airframe 47,872 hrs · 21,380 cycles

FORWARD CARGO BAY PANEL 120CF CORRODED. R & R PANEL IAW DWG & SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,872 hrs · 21,380 cycles

LEFT EMER LIGHT INOPERATIVE ROW 14. R & R LIGHT IAW MM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B RBL 24. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B LBL 24. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B RBL 45. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

SEAT TRACK HORIZONTAL FLANGE CRACKED AT BS 727B LBL 45. REPAIRED SEAT TRACK IAW ER & EA.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

OUTBOARD EDGE OF PANEL 221DF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

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

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 47,872 hrs · 21,380 cycles

MAIN WW LT INTERIOR SIDE, VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN LBL 45 TO 25. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 47,872 hrs · 21,380 cycles

MAIN WW RT INTERIOR SIDE, VERTICAL PRESS WEB CRACKED AT BS 663 BETWEEN RBL 45 TO 25. REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FLOORBEAM UPPER CORD AFT FLANGE LOWER SURFACE CORRODED AT BS 947.5 LBL 53. BEAM WILL BE REPAIRED IAW ACO.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

RIGHT CREASE BEAM CORRODED BETWEEN BS 945 TO 952.5 RBL 55. R & R CREASE BEAM IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

SKIN CRACKED AT BS 540, BETWEEN STRINGER 22R TO 23R. R & R SKIN IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

FLOORBEAM UPPER CORD CORRODED AT BS 986.5 BETWEEN LBL 22 TO LBL 37. REPAIRED CHORD IAW ACO.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

LEFT CREASE BEAM CORRODED BETWEEN BS 947.5 TO 956 LBL 54. R &R CREASE BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 47,872 hrs · 21,380 cycles

LEFT CREASE BEAM CORRODED AT BS 993 LBL 45. R & R CREASE BEAM IAW SRM & DWG.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 47,872 hrs · 21,380 cycles

AFT LT EMER EXIT LIGHT POWER SUPPLY M1673 INOPERATIVE. R & R POWER SUPPLY IAW AMM.