N7819A

Part: GEARBOX — FAULTY (ZN 200 FUS TOP) · airframe 67,245 hrs · 40,912 cycles

FLAP LOCK OUT ON CLIMB OUT FLAPS SPLIT LEFT AT 2 RIGHT AT 5 NO OVERWEIGHT LANDING FLAP DRIVE COUPLING RR REF AMM 27-51-31 - TRQ SPEC 600-720 IN/LBS (50-60 FT/LBS)<[01] R & R?D RIGHT TEE ANGLE GEARBOX PER M/M 27-51-55.<BR>RIG AND OPS CHECK GOOD.;[02] PREFORMED PSEU BITE PER FIM 32-09 TASK 801; NO FAULTS FOUND;[03] C/W INSPECTION OF R & R?D RIGHT TEE ANGLE GEARBOX PER M/M 27-51-55. RIG AND OPS CHECK GOOD.

Part: BRACKET — CRACKED (ZN 700 LANDING G) · airframe 66,301 hrs · 40,320 cycles

LEFT MAIN WHEEL WELL UPPER T/E PANEL SUPPORT BRACKET CRACKED ON FORWARD SIDE<[01] REMOVED AND REPLACED LEFT MAIN WHEEL WELL UPPER T/E PANEL SUPPORT BRACKET IAW SRM 51-10-02 AND SRM 51-40-02.

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 66,301 hrs · 40,320 cycles

R1 DOOR SLIDE GIRT BAR'S FWD RETAINER CLIP LOOSE<[01] SECURED R1 DOOR SLIDE GRIT BAR RETAINER CLIP IN REF SRM 51-40-02

Part: SEAT — OBSTRUCTED (ZN 200 FUS TOP) · airframe 65,293 hrs · 39,704 cycles

SEAT RECLINE AT 10B IS UNLOCKED AND OBSTRUCTS EXIT ROW<[01] READJUSTED THE PASSENGER SEAT RECLINE HYDROKOCK TO THE LOCK POSITION AT 10B IN REF WITH CMM 25-21-42;[02] INSPECTED

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 65,235 hrs · 39,673 cycles

EMERGENCY LIGHTS FAIL TEST (INOP LIGHTS ROWS 16-23 LEFT AND 11-13 RIGHT INOP)<[01] PERFORMED TROBLESHOOT EMERGENCY LIGHT; FOUND BAD TWO BATTERIES PACK'S M1669 AND M1673. REPLACED BATTERY PACKS M1669 AND M1673 OP CHECK GOOD PER AMM 33-51-06-960-805 STEP E.

Part: SLAT — CRACKED (ZN 500 LEFT WING) · airframe 65,235 hrs · 39,673 cycles

SLAT #2 LEADING EDGE SLAT NOSE SKIN AT ACTUATOR RIB - UPON INSPECTION OF CUTOUT; FOUND TWO THROUGH FASTENERS AT THE TERMINAL FITTING TO BE CRACKED. MARKED LOCATIONS.<REMOVED #2 SLAT PER AMM 27-81-21-000-801. INSTALLED MAIN TRACKS ON #2 SLAT ASSY; VERIFIED FIT OF DOWN STOP ASSEMBLY BOLT IN MAIN SLAT TRACK IAW AMM 27-81-21-400-802 STEP 5.G(5) AND AMM 27-81-21-400-801 STEPS 3.H(3.C#2 SLAT INSTALLED; IB AND OB DOWN STOP ASSEMBLY BOLT TORQUED AND SAFETIED AUXILIARY ARMS ATTACHED TO #2 SLATCLOSED PANELS 521PB 521SB IAW AMM 57-41-02-400-801 AND #2 SLAT ACT DOOR PANEL IAW AMM 20-50-11-910-801<BR><BR>TOOL ID: ATS1310 DUE: 10/2023;[25] VERIFIED CORRECTIVE ACTIONS STEP 24.;[26] RAISED FAULT TTG8Q00K58B7 FOR ORIGINAL DISCREPANCY AGAINST OFF UNIT SLAT MPN 114A5020-3 S/N 001055;[27] VERIFIED SKIN TAB GAPS ARE GOOD; PRELOAD IS GOOD AND L/E FLAP AND SLAT OPERATIONAL TEST IS GOOD IAW MM 27-81-00-820-803 STEPS 4.I.(3-5).;[28] VERIFIED CORRECTIVE ACTIONS 26 AND 27

Part: BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,672 cycles

R/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68<[01] CORRECTION TASK DETAIL SHOULD STATE ' L/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68 ';[05] REMOVED DAMAGED SECTION UPPER ATTACH ANGLE ON VAPOR BARRIER LBL6-LBL12 BS663 WL167.68 AND PERFORMED DVI ON REPAIR AREA AND NO ADDITIONAL DAMAGED FOUND IAW SRM 57-10-10-2R-5 PAR. 4B AND D.;[06] VERIFIED CORRECTIVE ACTIONS STEP 5.;[07] REQUIRED NDI INSPECTION ON REPAIR AREA BS 663 LBL 6-12 WL 167; OPEN HOLES AND FREE CRACK CUT OUT IAW SRM 57-10-10-2R-5.;[08] INSTALLED EWIS PROTECTION ON REPAIR AREA IAW AMM 20-60-07.;[09] -1 AND -2 WHERE FABRICATED PER SRM 57-10-10-2R-5 REFER TO ATS BUILD SHEETS 553591 AND 553592.;[10] CORRECTION TO STEP 9. -1 AND -2 REPAIR PARTS WHERE FABRICATED PER SRM 57-10-10-2R-5 REFER TO ATS BUILD SHEETS 553591 AND 553592.;[12] LOCATED AND DRILLED REPAIR PARTS IAW SRM 57-10-10-2R-5. OK TO INSTALL.;[13] VERIFIED ITEM 12 CORRECTIVE ACTIONS. OK TO INSTALL.;[14] INSTALLED REPAIR PARTS ON BS 663 LBL 6-18 WL167 IAW SRM 57-10-10-2R-5.;[15] INSTALLED REPAIR PARTS ON BS 663 LBL 6-18 WL167 IAW SRM 57-10-10-2R-5 PAR. 4 L.;[16] VERIFIED INSTALLED REPAIR PARTS ON BS 663 LBL 6-18 WL167 IAW SRM 57-10-10-2R-5 PAR. 4 L(1)-(7) OF CORRECTIVE ACTION STEP 15. CAP SEAL REQUIRED.;

Part: SLAT — CRACKED (ZN 600 RIGHT WIN) · airframe 65,235 hrs · 39,673 cycles

#2 L/E SLAT NOSE SKIN AT ACTUATOR RIB. 2EA CRACKS FOUND IN FASTENER HOLE COUNTERSINK LOCATIONS MARKED.<[01] REMOVED PANELS 524CB; 524EB & FLEX SKIN AT ACTUATOR RIB ON #2 SLAT TO ACCESS REPAIR IAW SOPM 20-50-01.;[02] APPLICABLE REPAIR FOR #2 L/E SLAT NOSE SKIN AT ACTUATOR RIB. 2EA CRACKS FOUND IN FASTENER HOLE COUNTERSINK LOCATIONS MARKED THAT WILL BE USED FOR THIS REPAIR IS SRM 57-42-01-2R-8.REPAIR 8.;[03] VERIFIED APPLICABILITY OF SRM 57-42-01-2R-8 REPAIR 8.;[04] UPDATED MEASUREMENTS SECTION.;[05] REMOVED DAMAGE IAW SRM 57-42-01-2R-8 STEP 4.F (1)(A - C).;[06] VERIFIED ITEMS 4;5 CORRECTIVE ACTIONS.;[07] 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>2EA CRACKS NOTED IN TERMINAL FITTING. MARKED LOCATIONS.<BR><BR>HFEC INSPECTED COUNTERSINKS IAW 737 NDTM PART 6 53-30-00 PROCEDURE 3. <BR>NO CRACKS NOTED.<BR><BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS1465 CAL DUE: 09/23<BR><BR>NRC GENERATED ON CUSTOMER CARD: TTG8Q00JWJCL;[08] HFEC INSPECTION REVEALED CRACKS IN THE ACTUATOR ATTACH FITTING. THE #2 SLAT WILL BE REPLACED ON FAULT #TTG8Q00JWJCL.;[09] FAULT TTG8Q00K58B3 RAISED AGAINST OFF UNIT SLAT MPN 114A5020-3 S/N 001055;[10] THE #2 SLAT WILL BE REPAIRED ON FAULT TTG8Q00K58B3.;[11] VERIFIED CORRECTIVE ACTION 10;[12] CLOSING RII LABOR ROW NO RII WORK PERFORMED ON THIS FAULT;[13] VERIFIED MEASUREMENT TABLE

Part: SLAT — CRACKED (ZN 500 LEFT WING) · airframe 65,235 hrs · 39,673 cycles

#4 L/E SLAT NOSE SKIN AT ACTUATOR RIB FITTING FOUND 2EA CRACKS IN HOLE. LOCATIONS MARKED.<[01] OPENED PANEL 521GB FOR ACCESS PER AMM 57-41-02-000-801.;[02] REMOVED #4 SLAT PER AMM 27-81-21-000-801.;[03] SHIMMED I/B AND O/B MAIN TRACK STOPS AND GUIDES FOR #4 SLAT; TORQUED AND SAFETIED ATTACH BOLTS IAW MM 27-81-21-400-801 STEPS 3.H.(1)(A);(B)1)2).<BR>CAL TOOL: ID#4077A DUE 04/2023#4 L/E SLAT;[06] INSTALLED NEW SERVICEABLE I/B AND O/B MAIN SLAT TRACKS ONTO NEW #4 SLAT. TRACK AFT HOLES ARE SERVICEABLE. IAW MM 27-81-21-400-802 STEPS 5.G.(2;5).#4 SLAT INSTALLED; IB AND OB STOP FITTING INSTALLED ON MAIN TRACKS IAW AMM 27-81-400-802 STEPS 3.H(1.B.3A;B;D-J)<BR>TOOL ID ATS2842 DUE 01/2024 INSTALLED #4 SLAT IAW MM 27-81-21-400-801 STEPS 3.H.(3-8).<BR>CAL TOOL: ID#4077A DUE 04/2023. LEADING EDGE FLAP AND SLAT ACTIVATION WAS ACCOMPLISHED ON CUSTOMER CARD: TTG8Q003JG4R. CONNECTED SLAT #4 ACTUATOR ON CUSTOMER CARD: TTG8Q003JG4R; INSTALLED #4 SLAT IAW AMM 27-81-21-400-801 STEPS 3H (11) THRU (14).;[15] ADJUSTED #4 SLAT IAW AMM 27-81-00-820-803 STEPS 4 H (4)(A) THRU (D);(F);(J)(K)(L)2)(M)(A)& (B);(D)(L) AND (M) AND STEPS 4H (6);(7)(A);(C) AND (8) THRU (19).;[16] CAL TOOLS: 4223C DUE: 04/23; ATS292 DUE: 06/23;.CORRECTIVE ACTIONS 14 AND 15 SLAT INSTALLATION AND ADJUSTMENT RAISED FAULT TTG8Q00K58DS FOR ORIGINAL DISCREPANCY AGAINST OFF UNIT SLAT MPN 114A5040-3 S/N 001054; SLAT OPERATIONAL TEST IS GOOD IAW MM 27-81-00-820-803 STEPS 4.I.(3-5).

Part: SLAT — PULLED (ZN 600 RIGHT WIN) · airframe 65,235 hrs · 39,673 cycles

SLAT #2 LEADING EDGE SLAT NOSE SKIN AT ACTUATOR RIB SEVERAL FASTENERS ARE PULLED THROUGH.<[01] HFEC INSPECTION REVEALED CRACKS IN THE ACTUATOR ATTACH FITTING. THE #2 SLAT WILL BE REPLACED ON FAULT #TTG8Q00JWJCL.;[02] FAULT TTG8Q00K58AH RAISED AGAINST OFF UNIT SLAT MPN 114A5020-3 S/N 001055;[03] THE #2 SLAT WILL BE REPAIRED ON FAULT TTG8Q00K58AH.;[04] VERIFIED CORRECTIVE ACTION 3;[05] CLOSING RII LABOR ROW NO RII WORK ACCOMPLISHED ON THIS FAULT

Part: ATTACH ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 65,235 hrs · 39,673 cycles

CRACKED ATTACH ANGLE AT MID PAX CABIN BS663+30 RBL23 WL203.<[01] NOT ALLOWABLE LIMITS APPLICABLE FOR SPECIFIC LOCATION PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED ATTACH ANGLE AT MID PAX CABIN BS663+30 RBL23 WL203 I.A.W SRM 51-40-02-0G-0;[03] FABRICATED NEW ATTACH ANGLE FROM BAC1490-2782 7075-T0 CLAD LOT 1482272-2 AND HT ON R.O # 857530-SWA ALL I.A.W BOEING DWGS 273A9112;273A9110 AND SRM 51-40-05-0G-0;[04] VERIFIED CORRECTIVE ACTION ITEM 1; 2; 3.<BR>OKAY TO TREAT AND PRIME PART GIVEN.<BR>VERIFIED MEASUREMENT TABLE COMPLETED.;[05] APPLIED CHEMICAL CONVERSION COAT AND PRIMED NEW ATTACH ANGLE ALL I.A.W SRM 51-20-01 AND SOPM 20-43-03. SOPM 20-41-02. OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION ITEM 5.<BR>OKAY TO INSTALL ANGLE GIVEN.;[07] INSTALLED NEW ATTACH ANGLE AT MID PAX CABIN BS663+30 RBL23 WL203 I.A.W SRM 51-40-02-0G-0; BOEING DWGS 273A9112; 273A9110; 273A9111 COMPLETED TASK;[08] VERIFIED CORRECTIVE ACTION 7.

Part: FLOOR SUPPORT — CRACKED (ZN 200 FUS TOP) · airframe 65,235 hrs · 39,673 cycles

CRACKED FLOOR SUPPORT AT MID CABIN BS540 LBL1 WL208.<[01] NO ALLOWABLE DAMAGE FOUND ON SRM PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C REPLACEMENT OF THE PART;[02] REMOVED DAMAGED BREAK PANEL AT STA 540 LBL 1; WL 207 IAW SRM 51-40-02-0G-0.;[03] LOCATED AND DRILLED NEW PANEL BREAK I.A.W BOIEING DRAWING 143A0060 AND SRM. 51-10-05-OG-0. OK TO INSTALL.;[04] VERIFIED CORRECTIVE ACTIONS 1 AND 3; OK TO INSTALL GIVEN.;[05] VERIFIED MEASUREMENT TABLE.;[06] PRIOR TO REMOVED CRACKED FLOOR SUPPORT AT MID CABIN BS540 LBL1 WL208 REMOVED PASSENGER CABIN FLOOR PANEL 231UF FOR ACCESS PER AMM 53-21-00-000-801.;[07] INSTALLED NEW PANEL BREAK I.A.W BOEING DRAWING 143A0060 AND SRM. 51-40-02-OG-0.;[08] OK TO INSTALL PASSENGER CABIN FLOOR PANEL 231UF.;[09] VERIFIED CORRECTIVE ACTION 7.;[10] VERIFIED CORRECTIVE ACTION 7.;[11] INSTALLED PASSENGER CABIN FLOOR PANEL 231UF I.A.W AMM 53-21-00-400-801<BR>SCREW GUN USED<BR>ATS674<BR>S/N UNKNOWN<BR>DUE 10/2023<BR>COMPLETED TASK;[12] VERIFIED CORRECTIVE ACTION 11.

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 65,235 hrs · 39,673 cycles

CRACKED ATTACH ANGLE AT MID PAX CABIN BS663+28 RBL1 WL207.<[01] NOT ALLOWABLE LIMITS APPLICABLE FOR SPECIFIC LOCATION PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED ATTACH ANGLE AT MID PAX CABIN BS663+28 RBL1 WL207 I.A.W SRM 51-40-02-0G-0;[03] FABRICATED NEW ATTACH ANGLE FROM BAC1490-2883 7075-T0 CLAD LOT 1482272-1 AND HT ON R.O # 857528-SWA ALL I.A.W BOEING DWGS 273A9112;273A9110;273A9111 AND SRM 51-40-05-0G-0;[04] VERIFIED CORRECTIVE ACTION ITEM 1; 2; 3.<BR>OKAY TO TREAT AND PRIME PART GIVEN.<BR>VERIFIED MEASUREMENT TABLE COMPLETED.;[05] APPLIED CHEMICAL CONVERSION COAT AND PRIMED NEW ATTACH ANGLE ALL I.A.W SRM 51-20-01 AND SOPM 20-43-03. SOPM 20-41-02. AND BOEING DWG 273A9112 OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION ITEM 5.<BR>OKAY TO INSTALL ANGLE GIVEN.;[07] INSTALLED NEW ATTACH ANGLE AT MID PAX CABIN BS663+28 RBL1 WL207 I.A.W SRM 51-40-02-0G-0; BOEING DWGS 273A9112; 273A9110; 273A9111 COMPLETED TASK;[08] VERIFIED CORRECTIVE ACTION 7.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS535 S-25R RBL22. WL155. MARKED<[01] REMOVED DAMAGED SECTION OF STR 25R BS 500D+11' TO BS 540 IAW SRM 53-00-03-2R-1 REP.1;[07] 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>EQUIP USED:<BR>-NORTEC 600 ID: ATS1465 CAL DUE: 09/23;[08] RECEIVED REPAIR PARTS FROM OSS; U-CHANNEL (1EA) PO. 909977-SWA; STRINGER SECTION (1EA) PO. 909980-SWA; J-CHANNEL (2EA) PO.909978-SWA; LOCATED; DRILLED; APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON REPAIR PARTS AND REPAIR AREA IAW SRM 53-00-03-2R-1 REP.1 AND EA 23-153-00806 REV. A;[09] OK TO INSTALL ALL REPAIR PARTS; INTERCOSTAL BETWEEN BS 500D - 520 STR 25R; STRINGER CLIP BS 520 STR 25R; SHEAR TIE BETWEEN STR 25R AND 24R BS 520;[10] VERIFIED CORRECTIVE ACTIONS 8 AND 9.;[11] INSTALLED ALL REPAIR PARTS BETWEEN BS 500D +11' TO 540; STR 25R; INTERCOSTAL BETWEEN BS 500D - 520 STR 25R; STRINGER CLIP BS 520 STR 25R; SHEAR TIE BETWEEN STR 25R AND 24R BS 520 IAW SRM 53-00-03-2R-1 REP.1 AND EA 23-153-00806 REV. A;[16] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 23-153-00806. THIS IS A CATEGORY A REPAIR; AND NO SUPPLEMENTAL INSPECTIONS ARE REQUIRED.;[17] VERIFIED CORRECTIVE ACTION 16 AND THE MEASUREMENT TABLE.

Part: NUT PLATE — CORRODED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

CORROSION ON NUTPLATE STRIP BS 787+2 RBL 20 WL 157<[01] EVALUATED CORROSION ON NUTPLATE STRIP BS 787+2 RBL 20 WL 157; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] REMOVED; REPLACED AND INSTALLED NUTPLATE STRIP BS 787+1 - BS787+6 RBL 19 WL 157 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; AND DWG 146A8340.;[04] VERIFIED CORRECTIVE ACTION 3.

Part: ATTACH ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

CORROSION ON AFT CARGO BAY INTERCOSTAL ATTACH ANGLE BS 767+2 WL 157 RBL 21<[01] EVALUATED CORROSION ON ATTACH ANGLE BS 767+2 RBL 21 WL 157; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] REMOVED DAMAGED AFT CARGO BAY INTERCOSTAL ATTACH ANGLE BS 767 -BS787 WL 157 RBL 21 IAW SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW AFT CARGO BAY INTERCOSTAL ATTACH ANGLE BS 767 -BS787 WL 157 RBL 21 IAW SRM 51-40-05-0G-0 AND DWG 146A8123.;[05] OK TO INSTALL.;[06] VERIFIED STEPS 4 AND 5.;[07] INSTALLED NEW AFT CARGO BAY INTERCOSTAL ATTACH ANGLE BS 767 -BS787 WL 157 RBL 21 IAW SRM 51-40-02-0G-0 AND DWG 146A8123.;[08] VERIFIED CORRECTIVE ACTION 7 AND MEASUREMENT TABLE.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACKS ON AFT CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(2) AND (4)<BR>EQUIP USED;<BR>WELDING MACHINE E10583; CAL DUE 01/2024;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] PT INSPECTED AREA IAW SOPM 20-20-02. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-RADIOMETER ID: ATS2504-A; B; C CAL DUE: 05/23;[04] SANDED REPAIR AREAS PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(5);[05] VERIFIED CORRECTIVE ACTION 4.;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 53-60-15-2R-1 PAR 4. B. (6) AND (7);[07] VERIFIED CORRECTIVE ACTION 6 AND MEASUREMENT TABLE.

Part: INTERCOSTAL — CORRODED (ZN 200 FUS TOP) · airframe 65,235 hrs · 39,673 cycles

CORROSION ON AFT CARGO BAY INTERCOSTAL BS 787+9 RBL 6 WL 153<[01] EVALUATED CORROSION ON INTERCOSTAL BS 787+9 RBL 6 WL 153; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] REMOVED AFT CARGO BAY INTERCOSTAL BS 787 TO BS 807 RBL 6 WL 153 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW INTERCOSTAL BS 787 TO BS 807 RBL 6 WL 153 PER SRM 51-40-05-0G-0; AND DWG 146A8130. OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 4.<BR>OK TO INSTALL;[06] INSTALLED INTERCOSTAL BS 787 TO BS 807 RBL 6 WL 153 PER SRM 51-40-02-0G-0; AND DWG 146A8130.;[07] VERIFIED ITEM 6 CORRECTIVE ACTIONS.;[08] VERIFIED MEASUREMENTS.

Part: TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

CRACK ON AFT CARGO BAY TRACK AT LBL 17 BS 727C.<[01] CRACK ON CARGO TRACK WAS FOUND TO BE OUT OF LIMITS.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED AFT CARGO BAY TRACK AT LBL 17 BS 727+4 - BS 867 IAW SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW AFT CARGO BAY TRACK AT LBL 17 BS 727+4 - BS 867 IAW SRM 51-40-02-0G-0 AND DWG 146A7500. OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION ITEM 3-4; OK TO INSTALL.;[06] STARTED INSTALLING NEW AFT CARGO BAY TRACK AT LBL 17 BS 727+4 - BS 867 IAW SRM 51-40-02-0G-0; DWG 146A7500 AND DWG 146A0061;[07] INSTALLED NEW AFT CARGO BAY TRACK AT LBL 17 BS 727+4 - BS 867 IAW SRM 51-40-02-0G-0; DWG 146A7500 AND DWG 146A0061;[08] RII VERIFIED CORRECTIVE ACTION ITEM 6-7.;[09] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

MULTIPLE AREA OF CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727+5-767.<[01] EVALUATED CORROSION AT ALL LOCATION OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 747+10 RBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIGINAL 0.040 IN NUMEROUS 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE NCX000697 DUE 09/2023;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT BS 727 TO BS 767 RBL 21 PER SRM 51-40-05-0G-0 AND DWG 146A7500;[04] VERIFIED CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

MULTIPLE AREA OF CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500A+2-500C+18 WL 157.<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500C+2' REMOVED 0.015' IN AN AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS 2473 DUE 08/2023;[02] VERIFIED CORRECTIVE ACTION 1.;[03] LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT BS 500A TO 500D RBL 24 WL 157 PER SRM 51-40-05-0G-0 AND DWG 143A7500;[04] VERIFIED CORRECTIVE ACTION #3.;[05] VERIFIED CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

MULTIPLE AREA OF CORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 24 BS 480+15-500+11 WL 157.<[01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] LOCATED AND DRILLED NEW AFT DOOR SHIELD BS 492 TO 500A RBL 24 WL 157 PER SRM 51-40-05-0G-0 AND DWG 143A0080;[04] VERIFIED CORRECTIVE ACTION #3.;[05] VERIFIED CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.

Part: NUT PLATE — CORRODED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

CORROSION ON AFT CARGO BAY NUT PLATE BRACKET AT BS 787+8 RBL 19.<[01] EVALUATED CORROSION ON NUTPLATE STRIP BS 787+8 RBL 19 WL 157; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] REMOVED; REPLACED AND INSTALLED NUTPLATE STRIP BS 787+7 - BS787+14 RBL 19 WL 157 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; AND DWG 146A8340.;[04] VERIFIED CORRECTIVE ACTION 3.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

MULTIPLE AREA OF CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727E+10-847.<[01] EVALUATED CORROSION AT ALL LOCATION OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 767+10 LBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIGINAL 0.040 IN NUMEROUS 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE NCX000697 DUE 09/2023;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT BS 727 TO BS 847 LBL 21 PER SRM 51-40-05-0G-0 AND DWG 146A7500;[04] VERIFIED CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

MULTIPLE AREA OF CORROSION ON FWD CARGO BAY FWD DOOR SHIELD AT RBL 24 BS 420+10-420+18 WL 157.<[01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] LOCATED AND DRILLED NEW FWD DOOR SHIELD BS 420 TO 440 RBL 24 WL 157 PER SRM 51-40-05-0G-0 AND DWG 143A0080;[04] VERIFIED CORRECTIVE ACTION #3.;[05] VERIFIED CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

CRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH ANGLE AT LBL 24 BS 500A+19 WL 156.<[01] CRACK ON CLIP FOUND TO BE OUT OF LIMITS DUE TO NO LIMIT ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED AND REPLACED FWD CARGO BAY BAFFLE FRAME ATTACH ANGLE AT LBL 24 BS 500A+19 WL 156 IAW SRM 51-40-02 AND DWG 143A7505.;[04] VERIFIED CORRECTVE ACTION 3;[05] VERIFIED ALL STEPS COMPLETE

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

MULTIPLE AREA OF CORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847-867.<[01] EVALUATED CORROSION ON SHIELD BS 847-867 RBL 21 WL 164; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] LOCATED AND DRILLED NEW AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847-867 IAW SRM 51-40-05-0G-0 AND DWG 146A0081.;[04] VERIFIED CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

CRACK ON AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+8 RBL 12.<[01] EVALUATED STIFFENER BS 907+8 RBL 12 WL 170.5; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] REMOVED DAMAGED AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+8 RBL7- RBL19 IAW SRM 51-40-02-0G-0.;[03] LOCATED AND DRILLED NEW AFT CARGO BAY WATER SERVICE BRACKET BS 907+8 PER SRM 51-40-05-0G-0 AND DWG 147A7221. OK TO INSTALL;[04] VERIFIED ITEM 3 CORRECTIVE ACTIONS. <BR>OK TO INSTALL.;[05] INSTALLED AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+8 PER SRM 51-40-02-0G-0 AND DWG 147A7221;[06] VERIFIED ITEM 5 CORRECTIVE ACTIONS.;[07] ALL WORK IS COMPLETE.;[08] VERIFIED MEASUREMENT TABLE; CARD COMPLETE

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

MULTIPLE AREA OF CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727+5-727E+7.<[01] EVALUATED CORROSION AT ALL LOCATION OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 727D+10 LBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIGINAL 0.040 IN NUMEROUS 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE NCX000697 DUE 09/2023. FLOOR TO SIDEWALL SUPPORT ASSY TO BE REPLACED ON CUST CARD# TTG8Q00JD4V6;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] VERIFIED MEASUREMENTS TABLE.;[04] CERTIFY

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

CRACK ON FWD CARGO BAY END OF STRINGER AT BS 540 STRINGER 23R.<[01] REQUEST NDI VERIFY CRACK IN STRINGER END;[02] ACCOMPLISHED HFEC SURFACE SCAN IAW 73 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. VERIFIED CRACK IS PRESENT IN STRINGER END; 0.5'L.<BR><BR>EQUIPMENT USED: NORTEC 600 ID: ATS1465 CAL DUE: 09/2023;[03] REMOVED DAMAGED SECTION OF STR 23R BS 500D+11' TO BS 540 IAW SRM 53-00-03-2R-1 REP.1;[04] VERIFIED APPLICABILITY OF SRM 53-00-03-2R-1 REP.1;[05] UPDATED STEP 1-2.;[06] VERIFIED CORRECTIVE ACTION STEPS 4 AND 5.;[07] REQUIRED NDI INSPECTIONS FOR OPEN HOLES; COUNTERSINKS AND CRACK FREE CUTOUT. IAW SRM 53-00-03-2R-1 REP.1;[13] INSTALLED REPAIR PARTS; APPLIED SEALING AROUND REPAIR AND CIC ON REPAIR AREA BS 500D + 6' TO 540 S-23R IAW SRM 53-00-03-2R-1 REP.1 AND EA 23-153-00802.;[14] UPDATED STEPS 1; 2 AND EA 23-153-00802.;[15] RII REQUIREMENTS COMPLETE.;[16] VERIFIED CORRECTIVE ACTION ITEM 13-14; CARD COMPLETE; EXCEPT FOR SUB-TASK WIP.;[17] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 23-153-00802.

Part: STIFFENER — CRACKED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

CRACK ON AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+12 RBL 12.<[01] EVALUATED STIFFENER BS 907+12 RBL 12 WL 170.5; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] REMOVED DAMAGED AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+12 RBL7- RBL19 IAW SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW AFT CARGO BAY WATER SERVICE BRACKET BS 907 PER SRM 51-40-05-0G-0 AND DWG 147A7221. OK TO INSTALL;[05] VERIFIED ITEM 4 CORRECTIVE ACTIONS. <BR>OK TO INSTALL.;[06] INSTALLED AFT CARGO BAY WATER SERVICE BRACKET AT BS 907+12 PER SRM 51-40-02-0G-0 AND DWG 147A7221;[07] VERIFIED ITEM 6 CORRECTIVE ACTIONS.;[08] VERIFIED MEASUREMENTS.

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

MULTIPLE AREA OF CORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 21 BS 767-787.<[01] EVALUATED CORROSION ON SHIELD BS 767-787 RBL 21 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-0G-0;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] LOCATED AND DRILLED NEW AFT CARGO BAY FWD DOOR SHIELD AT RBL 21 BS 767-787 IAW SRM 51-40-05-0G-0 AND DWG 146A0081.;[04] VERIFIED CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.

Part: PANEL — CHAFED (ZN 100 FUS LOWER) · airframe 65,235 hrs · 39,673 cycles

PANEL 194AR MATING SURFACE IS CHAFED.<[01] IDENTIFIED 194AR PANEL IAW SRM 53-60-70-0I-1 PARA FIGURE 2; ITEM 1; TABLE 2<BR><BR>FOUND DAMAGE TO BE WITHIN ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1 PARA 4.B.(8).<BR><BR>WILL PERFORM WORK IAW SRM 53-60-70-1A-1 PARA 2.A.<BR><BR>REMOVED FINISH AND ALL CONTAMINATION FROM PANEL SURFACE. CLEANED AND PREPARED PANEL SURFACE TO BE PERMANENTLY SEALED AND REFINISHED. IAW SRM 53-60-70-1A PARA 2.A.(1-2)<BR><BR>OK TO SEAL AND REFINISH.;[02] CORRECTION TO ACTION 1: FOUND DAMAGE TO BE WITHIN ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1 PARA 4.B.(3).;[03] VALIDATED DAMAGE WITHIN ALLOWABLE DAMAGE LIMITS PER SRM 53-60-70-1A-1 PARA 4.B.(3);[04] VERIFIED CORRECTIVE ACTIONS 1-3;[05] PERMANENTLY SEALED USING BMS 8-207 LOT: 1252X1256V<BR>CURED SEALER USING THERMOMETER ATS2209 DUE: 10/2023. <BR>REFINISHED PANEL SURFACE IAW SRM 53-60-70-1A-1 PARA 2.A.(4).(A).(2).(A-C).;[06] VERIFIED CORRECTIVE ACTION 5<BR><BR>VERIFIED MEASUREMENTS TABLE;[07] UPLOADED CURE SHEET;[08] VERIFIED CORRECTIVE ACTION 7

Part: SLIDE — OUT OF ADJUST (ZN 800 DOOR) · airframe 65,226 hrs · 39,665 cycles

L1 ENTRY DOOR SLIDE FALLING OUT OF BUSTLE<[01] REINSTALLED L1 ESCAPE SLIDE AND BESSEL IAW MT 725-61-06

Part: COVER — LOOSE (PAX DOOR SLIDE) · airframe 64,808 hrs · 39,419 cycles

FWD ENTRY DOOR SLIDE COVER LOOSE LOWER PORTION OF SLIDE NOT STOWED<[01] COMPLIED WITH AMM 25-66-01 AND TASK 725-61-06

Part: NONE — OUT OF POSITION (PAX CABIN) · airframe 63,794 hrs · 38,792 cycles

EMERGENCY LIGHT LOOSE IN OVERHEAD BIN BULLNOSE AT 4ABC. / [01] SECURED EMERGENCY LIGHT LENS AT 4 ABC REF AMM 33-51-03;[02] C/W

Part: BATTERY PACK — INOPERATIVE (FWD CABIN) · airframe 63,356 hrs · 38,529 cycles

EMERGENCY LIGHTS AT R1 DOOR; IN AND OUT; ABOVE L1 DOOR AND RH CABIN AT ROW 6 INOP / [01] REMOVED AND REPLACED FWD RH EMERGENCY POWER SUPPLY BATTERY PACK PER AMM 33-51-06. OP CHECK GOOD

Part: LIGHT — INOPERATIVE · airframe 62,319 hrs · 37,943 cycles

PASSANGER CABIN RIGHT AFT EMERGENCY LIGHTS INOP / [01] R&R BATTERY PACK IAW AMM 33-51-06

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,899 hrs · 37,147 cycles

SEAT 12DEF EMERGENCY EXIT DOOR SIDEWALL LIGHT INOP / [01] RELAMPED IAW AMM 33-21-00

Part: BRAKE — CONTAMINATED (LT MLG) · airframe 60,234 hrs · 36,783 cycles

#2 BRAKE SMOKING ; / [01] PERFORMED HYDRAULIC LEAK CHECK IAW AMM 29-00-00. NO LEAK NOTED IN WHEEL WELL OR BRAKE SYSTEM BOTH RESERVOIRS FULL. SUSPECT RESIDUAL FLUID ON BRAKES CAUSE OF SMOKING. A/C OK FOR SERVICE.

Part: LENS — BROKEN (RT EMERG EXIT) · airframe 59,862 hrs · 36,580 cycles

R/H EMERGENCY EXIT LOWER EXIT LIGHT ASSY LENSE BROKEN ; / R/R R/H EMERGENCY EXIT LOWER SIGN PER AMM 33-51-01

Part: SENSOR — FAULTY (LT WING) · airframe 59,555 hrs · 36,409 cycles

AT APPROXIMATELY 130 KIAS TAKEOFF CONFIGURATION WARNING LIGHT AND WARNING HORN SOUNDED. AT FLAP RETRACTION SPEED FLAPS WOULD NOT RETRACT. (FLAPS 1 TAKEOFF) FLAPS INDICATED A SPLIT AT F1 DETENT. AFTER LANDING FLAP SPLIT INDICATION RETUNED TO NORMAL F1 INDICATIONS; AND FLAPS RETRACTED NORMALLY. PSEU LIGHT ILLUMINATED. / FOUND FC# 27-53252 ON FSEU AS WELL A FC# 32-62109; & 32-62110 ON PSEU. PERFOMED F.I.M. TASK 27-59 803. R&R'D #3 FLAP SKEW SENSOR PER A.M.M. 27-59-01. SYSTEM OPS CHK NORMAL. PSEU LIGHT EXTINGUISHED; AND NO FAULTS FOUND. RAR# 95257 P/N OFF S256A404-2 S/N OFF 9202 P/N ON 9000421-2 S/N ON 17751.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT (1 EA) / FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT REPAIRED BY WELDS IAW 737-700 SRM BOEING 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4B STEP (4) AND BAC 5975

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT (1 EA) / AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT REPAIRED BY WELDS IAW 737-700 SRM STEP (4) AND BAC 5975

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK FLOOR STRUCTURE LINK LOCATED BETWEEN BS520 TO BS540 AND BL0 AT CENTER SECTION / REPLACED FLOOR STRUCTURE LINK LOCATED BETWEEN BS 520 TO BS 540 AND BL0 AT CENTER SECTION IAW SRM B737-700 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DRAWING # 143A0060 SH 2 REV B PART USED 143A5595-21 PO 2021124105

Part: WEB — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK WEB - INTERCOSTAL LOC. BTW BS 500A TO BS 500B AT LEVEL STR26R AT FWD CARGO COMPARTMENT / REPLACED WEB- INTERCOSTAL (BAFLLE) LOCATED BTW BS 500A TO BS500B AT LEVEL STR 26R AT FWD CARGO COMPARMTMENT IAW B737-700 SRM 51-40-02-0G-0 STEP 9 AND DWG 143A7505 REV D AND REPAIRED IAW SRM 53-30-53-2R-1 REPAIR 1

Part: BRACKET — ELONGATED (L/H WING) · airframe 59,461 hrs · 36,357 cycles

ELONGATED HOLE SUPPORT BRACKET KRUEGER FLAP INTERNAL AREA AT LT WING / REPLACED SUPPORT BRACKET ON INTERNAL AREA KRUEGER FLAP AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02

Part: BRACKET — ELONGATED (L/H WING) · airframe 59,461 hrs · 36,357 cycles

ELONGATED HOLE SUPPORT BRACKET INTERNAL AREA KRUEGER FLAP AT LT WING / REPLACED SUPPORT BRACKET ON INTERNAL AREA KRUEGER FLAP AT LT WING IAW SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02

Part: WEB — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS312 TO BS328 AT LEVEL LBL48.5 FWD GALLEY AND LAV / REPLACED WEB-INTERCOSTAL FLOOR STRUCTURE LOCATED BS_312 TO BS328 AT LEVEL LBL48.5 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A5400 SHEET 39 REV.-

Part: ACCESS PANEL — CRACKED (L/H WING) · airframe 59,461 hrs · 36,357 cycles

CRACK SEAL ACCESS PANEL 532HB STRIP AT LT WING / REPLACED DOOR ASSY FUE ACCESS PANEL #532HB LT WING IAW AMM 28-11-11 AND A1PC28-11-11-08

Part: WEB — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AT LEVEL BL0 FWD GALLEY AND LAV / REPLACED WEB-INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS244.5 AT LEVEL BL0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A5400 SHEET 20 REV.-

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

DELAMINATED FLOOR PANEL 231YF AT PASSENGER CABIN / REPAIRED FLOOR PANEL 231YF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-7 REPAIR 7

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK ANGLE - SUPPORT LOCATED FWD CUT OUT DOOR AT BS 312 AT LEVEL S-9 L AT FWD GALLEY AREA / REPLACED ANGLE - SUPPORT LOCATED FWD CUT OUT DOOR AT BS 312 AT LEVEL STR9L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0 PARAGRAPH 4 ITEM B AND DWG 141A8220 SHEET 2 REV A

Part: SUPPORT — DAMAGED (FWD CARGO) · airframe 59,461 hrs · 36,357 cycles

ELONGATED HOLE SUPPORT ZEE BETWEEN BS500A TO BS500D AT LEVEL STR26R AT FWD CARGO COMPARTMENT / REPLACED SUPPORT ZEE LOCATED BTW BS500A TO BS500D AT LEVEL STR 26R AT FWD CARGO COMPARTMENT IAW B737- 700 SRM 51-10-02-0G-0 STEP 9 AND DWG 143A7500 REV A

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN / REPLACED NEW TIE CLIP LOCATED BS 277 AND STR10R PASSENGER CABIN IAW B737-700 SRM 51-40-02 PN USED 141A1250-92 DWG 141A1110 REV.-

Part: ANGLE — CRACKED (FWD CARGO) · airframe 59,461 hrs · 36,357 cycles

CRACK ANGLE CLIP FWD FACE BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT REPLACED ANGLE CLIP FWD FACE BS 500C AT LEVEL S26L FWD C.C IAW SRM B737700 514002 AND DWG @143A7505 REV R.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK STRINGER 26L AND BS540 FWD CARGO COMPARTMENT / PERFORMED PERMANENT REPAIR LOC. ON STR26L AND BTW BS540 TO BS500D FWD CARGO COMPARTMENT IAW B737- 700 SRM 53-00-02-1 REPAIR 1 MATERIAL USED ALUMINIUM SHEET 2075-D 0.045' PO 2020-203305 ALUMINUM SHEET 7075-TO 0.050' P/O 2020-213289

Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK STRINGER 23L AND BS540 FWD CARGO COMPARTMENT / PERFORMED PERMANENT REPAIR LOC ON STR23L BTW BS500D TO BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; MATERIAL USED 7075-TO-0.040' PO 2020-203286 ALUMINUM SHEET 7075-TO-0.036'

Part: BARRIER — CRACKED (CENTER WING) · airframe 59,461 hrs · 36,357 cycles

CRACK BODY STATION 663.75 VAPOR BARRIER RBL 10 APROX. AT MAIN WHEEL WELL COMPARTME / REPAIRED VAPOR BARRIER RH SIDE MAIN WHEEL WELL COMPARTMENT LOCATED BTW RBL 6.15 TO RBL 15.54 LOWER POSITION BS 663.75. DAMAGE SIZE L=1.66' W=0.04' IAW B737-700 SRM 57-10-10-2R-2 REPAIR 2 PARA 6 . THIS IS AN INTERIM REPAIR AND REQUIRE DO A DETAILED VISUAL INSPECTION O NTHE REPAIR AREA AT 3000 FLIGHT CYCLES INTERVALS IAW B737-700 SRM 57-10-10-2R-2 REPAIR 2.C FOR INSPECTION REQUIREMENTS SEE TLD SN T080637

Part: GUSSET — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT / REPLACED GUSSET LOC. BS 500D AND STR19R IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG #143A7902 SHEET 174 REV- PART USED PN 143A9481-5

Part: ACCESS PANEL — DELAMINATED (R/H HORIZ. STAB.) · airframe 59,461 hrs · 36,357 cycles

DELAMINATED ACCESS DOOR 343CB AT RT HORIZONTAL STABILIZER / REPAIRED ACCESS PANEL 343CB AT RT HORIZONTAL STABILIZER ASPER B737-700 SRM 51-70-04-2R-10 REPAIR 10 AND SRM 51-70-04-2R-0 REPAIR GENERAL TOOL USED CALIPER PN 500-197-30 SN 15121550 DUE DATE 24-MAY-21 HOT BONDER PN HCS9200B SN 18175478 DUE DATE 07-JUL- 21 SCALE PN CL5000 SN AE-407338 DUE DATE 30-MAR-21 MULTIMER PN FLUKE-87 SN 95100197 DUE DATE 12-AUG-21

Part: GUSSET — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED ON BS500D AND STRG19L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG #143A7902 SHEET 174 REV - PART USED PN 143A9481-6

Part: DOOR — OUT OF ADJUST (R1 DDOOR) · airframe 59,461 hrs · 36,357 cycles

OUT OF ADJUSTMENT SERVICE DOOR AT FWD GALLEY AREA / PERFORMED ADJUSTMENT ON SERVICE DOOR AT FWD GALLEY AREA IAW AMM 52-41-00-820-801 TOOL USED CALIPER PN 700-113-10 SN 0033205 DUE DATE 29-JUL-21 AND DEPTH GAGES PN 547-2185 SN 003739 DUE DATE 14-SEP-21

Part: SKIN — WORN (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

WEAR ON EXTERNAL SKIN CLOSURE ANGLE LOCATED BS 1132.02 APPROX RH SIDE AT UPPER FUSELAGE / PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN CLOSURE ANGLE LOC BS 1112 TO BS 1132 RH SIDE AT UPPER FUSELAGE IAW B737-700 53-80-71-2R-6 REPAIR 6 AND SRM 51-40-02 MATERIAL USED CLOSURE ANGLE 1(EA) P/N: 2024 TO / 0.063' PO: 2020-166830 STRAP 1(EA) P/N:2024-T3 / 0.080' PO: 2020-21-3566

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 59,461 hrs · 36,357 cycles

CRACK INDICATION ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB INBOARD SIDE 24 INCH FROM FWD EDGE . CRACK LENGTH = 1.500 INCH / PERFORMED REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 BETWEEN 12.5' AND 29' FROM FRONT EDGE IAW SRM B737-700 55-10-01 REPAIR 11 MATERIAL USED PN 2024 T3-090 PO 202020 234400101 THIS REPAIR IS CATEGORY B FOR INSPECTION REQUIREMENT SEE TLD NO T080554

Part: LIGHT — DETERIORATED (CABIN) · airframe 59,461 hrs · 36,357 cycles

DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (5 EA) / REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN THE INSTALLATION IS TO BE ACCOMPLISHED WITH WORK INSTRUCTION NO. 753-410-00- 02Y

Part: FLOOR PANEL — ELONGATED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

ELONGATED HOLE FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT / REPLACED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW DWG #453A2610 REV C AND SRM B737-700 51-10-02

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 59,461 hrs · 36,357 cycles

CRACK INDICATION ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB INBOARD SIDE ; 16.250 INCH FROM FWD EDGE . CRACK LENGTH = 1.100 INCH . / PERFORMED REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 BETWEEN 12.5' AND 29' FROM FRONT EDGE IAW SRM B737-700 55-10-01 RPEAIR 11 ALL STEPS ARE DOCUMENTED ON NON ROUTINE CARD L197183 MATERIAL USED PN 2024T3-090 PO: 202021111000101

Part: BARRIER — CRACKED (CENTER WING) · airframe 59,461 hrs · 36,357 cycles

CRACK BODY STATION 663.75 VAPOR BARRIER LBL10 APROX. AT MAIN WHEEL WELL COMPARTME / REPAIRED VAPOR BARRIER LH SIDE MAIN WHEEL WELL COMPARTMENT LOCATED BTW LBL 6.15 TO LBL 15.54 LOWER POSITION BS 663.75 DAMAGE SIZE L=6' W=0.03' ASPER B737-700 SRM 57-10-10-2R-2 REPAIR 2 PARAGRAPH 6 THIS IS AND INTERIM REPAIR AND REQUIRED A DETAILE DO AVISUAL INSPECTION ON THE REPAIR AREA AT 3000 FLIGHT CYCLES INTERVAKS IAW B737-700 SRM 57-10-10-2R-2 REPAIR 2 PAR 2C FOR INSPECTION REQUIREMENT SEE TLD S/N T080524

Part: WEB — CRACKED (PAX CABIN) · airframe 59,461 hrs · 36,357 cycles

CRACK INDICATION ON WEB PRESSURE DECK RBL 40 ON STA 663 AT PASSENGER CABIN (1 EA) (0.250 INCH APPROX.) / PERFORMED PERMANENT REPAIR ON WEB PRESSURE DECK BTW RBL 25' TO BSL60' STA 663 AT PASSENGER CABIN IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 TABLE 201 MATERIAL USED ALUMINUM SHEET PN 2024-T3 CLAD 0.80' ALUMINUM SHEET PN 2024T3-063 AND STIFFENER PN BAC 1505-100052

Part: SUPPORT ANGLE — CRACKED (CENTER WING) · airframe 59,461 hrs · 36,357 cycles

CRACK SUPPORT ANGLE LOCATED BS540 BETWEEN BL0 TO RBL24.5 CENTER SECTION / REPLACED SUPPORT ANGLE LOCATED BS540 BETWEEN BL0 TO RBL 24.5 CENTER SECTION IAW SRM B737-700 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 PART USED 143A5240U34 PO BATCH SW 2021000674

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK SUPPORT ANGLE LOCATED BS540 BETWEEN BL0 TO LBL 24.5 CENTER SECTION / REPLACED SUPPORT ANGLE LOCATED BS 540 BETWEEN BL0 TO LBL 24.5 CENTER SECTION IAW SRM B737-700 51-40 -02 SRM 51-10-02 PARAGRAPH 9 PART USED P/N 143A5240U33 P/O SW 2021000710

Part: ACCESS PANEL — ELONGATED (R/H PYLON) · airframe 59,461 hrs · 36,357 cycles

ELONGATED HOLE ACCESS PANEL 444CR AT RT PYLON / REPLACED ACCESS PANEL #444CR AT RT PYLON IAW DRAWING # 313A2730 MATERIAL USED 2024-T351 0.250' PO 2014-521219

Part: PLATE — CRACKED (#1 ENGINE) · airframe 59,461 hrs · 36,357 cycles

CRACK PLATE INTERNAL AREA I/B FAN COWL ON ENGINE 1 / REPLACED PLATE INTERNAL AREA I/B FAN COWL ON ENGINE 1 IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND CMM GOODRICH 71-13-30

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 59,461 hrs · 36,357 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER / PERFORMED PERMANENT REPAIR ON LOCATED AT 36 INCH FROM FRONT SPAR OF INSPAR RIB STAB STA 120.30 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09- 2R-4 REPAIR 4 FIGURE 202 DETAIL A AND DWG 55100003 REV B MATERIAL USED KIT T-SECTION PN 55100003-01

Part: SKIN — CRACKED (RT WING SLAT) · airframe 59,461 hrs · 36,357 cycles

CRACK LOWER SKIN SLAT 5 LOCATED ON SLAT STATION 85.19 AT RT WING / PERFORMED PERMANENT REPAIR ON SLAT 5 LOCATED ON STATION 85.19 AT RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 AND MATERIAL USED 7075-T6-071 ; 7075T6-063 PO #2021 103704; 2020 203089

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 59,461 hrs · 36,357 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER / PERFORMED PERMANENT REPAIR ON LOCATED AT 28INCH FROM FRONT SPAR OF INSPAR RIB STAB STA 120.30 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIG 202 DETAIL A AND DWG 55100003 REV B MATERIAL USED KIT T-SECTION PN 55100003-01

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 59,461 hrs · 36,357 cycles

CRACK INSPAR RIB LOCATED STAB STA 129.50 AT 26 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER / PERFORMED PERMANENT REPAIR LOC ON STAB STA 129.50 AT 26' FROM FRONT SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-S REPAIR 5 FIG 204 SHEET 1 DWG 55100003 REV B MATERIAL USED KIT T-SECTION PN 55100003-1 BAC 1490-7075T6 ALUMINUM SHEET PN 7075T6-020

Part: PANEL — CRACKED (FUSELAGE) · airframe 59,461 hrs · 36,357 cycles

CRACK BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT / REPLACED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT WITH NEW PANEL FABRICATE FROM 0.060 CONOLITE PO #2021 109992 IAW B737-700 AMM 25-52-01 AND DWG 453A2510 REV .-

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,456 hrs · 36,355 cycles

PANEL 193B IS DELAMINATED IN FWD LH CORNER MEASURING 1.8' X .8' / REMOVED AND REPLACED PANEL 193B PER AMM 53-51-21.

Part: LIGHT — INOPERATIVE (RT EMER EXIT) · airframe 59,456 hrs · 36,355 cycles

RT EMER EXIT SIDEWALL LIGHT INOP. / REMOVED AND REPLACED RT EMER EXIT SIDEWALL LIGHT ASSY IAW AMM 25-21-20 AND AMM 33-21-00

Part: MEGAPHONE — BROKEN (AFT CABIN) · airframe 58,946 hrs · 36,056 cycles

AFT MEGAPHONE BROKEN. R & R AFT MEGAPHONE, PER MM 25-64-00.

Part: STRUCTURE — DAMAGED (RT EMER EXIT) · airframe 58,887 hrs · 36,020 cycles

RIGHT OVERWING EXIT DOOR INTERIOR LOWER HANDLE MOLDING IS DAMAGED / REMOVED & REPLACED OVERWING EXIT DOOR LOWER HANDLE MOLDING REF AMM 52-22-51

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 58,132 hrs · 35,545 cycles

R1 DOOR SLIDE CONTAINER OPENED, REINSTALLED THE SLIDE PACK INTO CONTAINER IAW TASK CARD 725-61-06.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 57,958 hrs · 35,433 cycles

BATTERY PACK M1670 IS BAD / REMOVED; INSTALLED SERVICEABLE; AND TEST OF THE NEW BATTERY PACK M1670 GOOD IAW AMM 33-51-06-960-805.

Part: PLATE — CORRODED (CARGO BAY) · airframe 57,958 hrs · 35,433 cycles

***CORROSION*** ON AFT CARGO COMPARTMENT AFT RH NET TIEDOWN PLATE / REMOVED & REPLACED WITH NEW TIEDOWN PLATE P/N 453A2611-2 PO# 743576 AT AFT CARGO COMPARTMENT AFT R/H IAW DWG# 453A2600; SRM 51-40-02-0G-0.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 57,958 hrs · 35,433 cycles

***CORROSION*** ON STA 1016 FWD LOWER CORD SPLICE AT STA 1016 BETWEEN STR 27L AND 27R / EVALUATE CORROSON ON STA 1016 FWD LOWER CORD SPLICE P/N 148A2216-3. FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED LIMITS + 19% MATERIAL REMOVED. FABRICATED NEW 1016 LOWER FWD CHORD SPLICE. LOCATED + DRILLED; THEN INSTALLED IAW SRM 51-40-02-0G-0 + BOEING DWG 147A0070 + SRM 51-10-02-0G-0

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 56,766 hrs · 34,725 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1673 IN CABIN. / R&R BATTERY PER AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 56,766 hrs · 34,725 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1675 IN CABIN. / R&R BATTERY PER AMM.

Part: BRACKET — LOOSE (EVAC SLDIE) · airframe 56,473 hrs · 34,542 cycles

FO SIDE FORWARD SERVICE DOOR ESCAPE SLIDE BRACKET LOOSE. / SECURED BRACKET PER MM SIP.

Part: SCREW — MISSING (L1 DOOR SLIDE) · airframe 55,654 hrs · 34,014 cycles

L1 DOOR ESCAPE SLIDE LOOSE MISSING BOLT. INSTALLED SCREW IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 55,563 hrs · 33,955 cycles

RT OVERWING EXIT IDENTIFICATION SIGN DID NOT ILLUMINATE WHEN TESTED. R&R FUSE PER AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 55,563 hrs · 33,955 cycles

RT OVERWING EXIT IDENTIFICATION SIGN COVER MISSING. R&R LIGHT COVER PER AMM.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 55,252 hrs · 33,762 cycles

R/H EMERGENCY EXIT SIGN COVER ROW POPPED OFF. REATTACHED COVER PER SIP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,762 hrs · 33,471 cycles

EMERGENCY EXIT AISLE LIGHTS INOP BETWEEN BS. 500C TO BS. 560. R&R BATTERY PACK PER AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 54,762 hrs · 33,471 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED / REPAIRED AFT CARGO BAY FWD CORNER SCUFF PLATE IAW SWA EA 1-A53-2076 REV 11.

Part: STRINGER — CRACKED (BS 1013) · airframe 54,762 hrs · 33,471 cycles

STR 14 L/H CRACKED AT B.S. 1013. REPAIRED PER ATS ER# 19-02759 REV IR AND SWA EA-1-753-34620 REV IR.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 54,762 hrs · 33,471 cycles

VERTICAL PRESSURE WEB CRACKED AT BS. 663, RBL 35 AT DRAIN HOLE CUTOUT. REPAIRED WEB IAW EA AND ER.

Part: BAFFLE — DAMAGED (BS 727B) · airframe 54,762 hrs · 33,471 cycles

AFT CARGO BAY BAFFLE DAMAGED AT BS. 727B, LBL 25, FASTENER HOLE. / R&R BAFFLE PER SRM & DWG.

Part: DOOR FRAME — CORRODED (APU BAY) · airframe 54,762 hrs · 33,471 cycles

*APU COMPARTMENT L/H DOOR CUTOUT STRUCTURE CORRODED AT STA 1088+8 TO 1088+68, LBL 24 / REMOVED AND REPLACED APU DOOR CUTOUT CHORD IAW SRM 51-40-02-0G-0, BOEING DWG 148A8600 AND BOEING DWG 148A8540

Part: STRIP — CRACKED (AFT CARGO COMPT) · airframe 54,762 hrs · 33,471 cycles

AFT CARGO BAY CAPSTRIP BS 767 - 847 LBL 24 CRACKED AT HOLE AT AFT END / REPLACED AFT CARGO BAY CAP STRIP BS 767-847 LBL24 IAW AMM 25-52-10-400-801 E.(11) 59667U 18-APR-2019

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 54,762 hrs · 33,471 cycles

CABIN FLOOR PANEL 231ZF IS DELAMINATING / DUE TO THE EXTENT OF DAMAGE FOUND ON PANEL 231 2F. FABRICATED A NEW REPLACEMENT PANEL 231 2F FROM BMS 4-23 TYPE II; LOT# 1383314-1 AND INSTALLED ALL NEW INSERTS USING BMS 5-107; LOT# AK8KD4895K AND PART MARKED IAW SRM 53-00-50-2R-0 PARA 4A; 5(S) AND DWG# 144A5810-11 59278U 3/21/19

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 54,762 hrs · 33,471 cycles

CABIN FLOOR PANEL 242DF IS DELAMINATED / DUE TO EXTENT OF DAMAGE FABRICATED REPLACENT FOR CABIN FLOOR PANEL 242DF USING BMS 4-23 REV. F TY 2 LOT# 5068498-1 INSTALLED ALL THROUGH INSERTS WITH RESIN BMS 5-107 LOT# AK8KD4895K AND PART MARKED IAW SRM 53-00-5D-2R-0 PARA 4A DWG# 144A5810-3 59268U 3/22/19

Part: STRIP — CRACKED (AFT CARGO COMPT) · airframe 54,762 hrs · 33,471 cycles

AFT CARGO BAY CAPSTRIP BS 727 - 727D RBL 24 CRACKED AT AFT END / REPLACED AFT CARGO BAY CAPSTRIP BS727-727D RBL24 IAW AMM 25-52-10-400-801 E.(11) 59667U 18-APR-2019

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 54,762 hrs · 33,471 cycles

WING TO BODY FAIRING PANEL 195CL IS CRACKED IN AFT CORNER / REPLACED PANEL 195CL WITH A SERVICABLE PANEL ON CARD NUMBER T904057.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 54,762 hrs · 33,471 cycles

CABIN FLOOR PANEL 241DF IS DELAMINATED / CABIN FLOOR PANEL 241DF WITH DELAMINATED WAS REPLACED WITH NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0. PARA 1.A.(NOTE) AND DWG 144A5810-9. 59943U 15MAR19

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 54,762 hrs · 33,471 cycles

AFT CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 927 TO BS 947, RBL 20. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 54,762 hrs · 33,471 cycles

AFT CABIN FLOOR PANEL 242VF HAS INSERT PULLED THROUGH / REPAIRED ADDITIONAL DAMAGE FOUND ON AFT CABIN FLOOR PANEL 24 2VF UPPER SURFACE AND REPLACED ALL DAMAGE INSERTS IAW SRM 53-00-52-2R-2 AND DWG# 147A5810-350 59278U 3/21/19

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 54,762 hrs · 33,471 cycles

HORIZONTAL PRESSURE WEB SHEAR TIE CORRODED AT BS. 667, RBL 68. REPAIRED SHEAR TIE IAW EA & ER.

Part: SEAT TRACK — CORRODED (BS 480-520) · airframe 54,762 hrs · 33,471 cycles

SEAT TRACK CORRODED BETWEEN BS. 480 TO BS. 520, LBL 45. R&R SEAT TRACK PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 500D) · airframe 54,762 hrs · 33,471 cycles

FORWARD CARGO BAY ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE CORRODED AT BS. 500D, BETWEEN RBL 22 TO LBL 22. / R&R ANGLE IAW SRM AND DWG.

Part: WEB — CORRODED (BS 440-493) · airframe 54,762 hrs · 33,471 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS. 440 TO BS. 493, RBL 27. / R&R SUB THRESHOLD IAW SRM AND DWG.

Part: ANGLE — CRACKED (FWD CARGO) · airframe 54,762 hrs · 33,471 cycles

CRACKED INTERCOSTAL SUPPORT ANGLE AT FWD CARGO BAY BS440+1 LBL24 WL155. MARKED / REMOVED CRACKED INTERCOSTAL SUPPORT ANGLE AT FWD CARGO BAY BS 440+1 LBL 24 WL 155 AND REPLACED WITH NEW IAW DWG 143A7505 ID3 REV A; SRM 51-40-02-0G-0 4.B 92954U 3/28/19

Part: SHIELD — CORRODED (BS 500-500A) · airframe 54,762 hrs · 33,471 cycles

FORWARD CARGO BAY AFT SHIELD CORRODED BETWEEN BS. 500 TO BS. 500A, RBL 23. / R&R SHIELD ASSEMBLY IAW SRM AND DWG.

Part: SPAR — CORRODED (LT WING) · airframe 54,762 hrs · 33,471 cycles

LW AFT FUEL BOOST PUMP FAILS RESISTANCE MEASUREMENT (REF 723-150-00-01 STEP 2) DUE TO CORROSION NOTED AT BONDING STRAP LOCATIONS. LW IRSS 145 / REPAIRED CORROSION DAMAGE ON L/W REAR SPAR WEB BELOW FUEL BOOST PUMP AT BONDING STRAP LOCATIONS IAW ATS ER # 19-02491 REV IR AND CUSTOMER ACCEPTANCE SWA EA 1-757-16148 REV IR.

Part: ATTACH ANGLE — CORRODED (BS 767-787) · airframe 54,762 hrs · 33,471 cycles

AFT CARGO BAY INTERCOSTAL ATTACH ANGLE CORRODED BETWEEN BS. 767 TO BS. 787, RBL 19. / R&R ANGLE IAW SRM AND DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 887-947) · airframe 54,762 hrs · 33,471 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 887 TO BS. 947, RBL 21. / R&R SUPPORT IAW SRM & DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 727-847) · airframe 54,762 hrs · 33,471 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 847, LBL 20. / R&R SUPPORT IAW SRM AND DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 727-767) · airframe 54,762 hrs · 33,471 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 767, RBL 20. / R&R SUPPORT PER DWG AND SRM.

Part: WEB — CORRODED (THRESHOLD) · airframe 54,762 hrs · 33,471 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS. 794 TO BS. 847, RBL 25. R&R THRESHOLD IAW SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 54,762 hrs · 33,471 cycles

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

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 54,762 hrs · 33,471 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / FOWARD SERVICE DOOR #4 LOWER BEAM REMOVED AND REPLACED #4 BEAM ON RO # 0520055_E4R. (POS: SF; TAG NO.: 537992; P/N OFF: 141A6516-16; S/N OFF: 001052; P/N ON: 141A6516-16M; S/N ON: 001052)

Part: SHIELD — CORRODED (BS 767-787) · airframe 54,762 hrs · 33,471 cycles

AFT CARGO BAY FORWARD SHIELD CORRODED BETWEEN BS. 767 TO BS. 787, RBL 21. / R&R SHIELD IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 877) · airframe 54,762 hrs · 33,471 cycles

FLOOR SUPPORT SPLICE CORRODED AT AFT CARGO BAY BS 887, RBL 21 TO LBL 9, WL170. REMOVED AND REPLACED AFT CARGO BAY FLOOR SUPPORT B/S 887 RBL 21 - LBL 9. WL170 IAW SRM - 51-40-02-0G-0 AND BOEING DWG-146A7500. 56011U. 16APR19.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 54,762 hrs · 33,471 cycles

MAIN CABIN VERTICAL PRESSURE WEB CRACKED AT BS. 663, LBL 35. REPAIRED WEB IAW SRM.

Part: CHANNEL — CORRODED (BS 960-983) · airframe 54,762 hrs · 33,471 cycles

R2 DOOR CREASE BEAM WEB INBOARD CHORD MOP SILL CORRODED BETWEEN BS. 960 TO BS. 983, RBL 53. / R&R MOPSILL IAW SRM AND DWG.

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 54,762 hrs · 33,471 cycles

FWD CABIN FLOOR PANEL 221GF HAS BROKEN FWD I/B TANG / DUE TO THE EXTENT OF DAMAGE REPLACED FWD CABIN FLOOR PANEL 221GF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-32A ITEM 865. 87066U 3/20/19

Part: CHANNEL — CORRODED (BS 294.5-328) · airframe 54,762 hrs · 33,471 cycles

R1 DOOR CREASE BEAM WEB INBOARD CHORD (MOP SILL) SCUFF PLATE SUPPORT CORRODED BETWEEN BS. 294.5 TO BS. 328, RBL 61. / R&R SUPPORT IAW SRM AND DWG.

Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 54,762 hrs · 33,471 cycles

AFT CABIN FLOOR PANEL 242XF IS BROKEN / BROKEN AFT CABIN FLOOR PANEL 242XF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0. PARA.9.A.(1).

Part: STRAP — CORRODED (MAIN CABIN) · airframe 54,762 hrs · 33,471 cycles

***CORROSION*** ON TENSION STRAP AT B.S. 1024; L.B.L. 3; W.L. 208.1. / ACCOMPLISHED REPAIR IAW EA# 1-753-34582 REV IR AND ER# 19-02244 REV IR

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,762 hrs · 33,471 cycles

FLOORBEAM CORRODED AT BS. 986.5, BETWEEN LBL 35 TO LBL 44. REPAIRED FLOORBEAM PER EA.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 54,762 hrs · 33,471 cycles

AFT CABIN FLOOR PANEL 241AEF AFT EDGE DAMAGED, (BETWEEN BS. 887 TO BS. 1016). / REPAIRED FLOOR PANEL IAW SRM AND DWG.

Part: STRAP — CORRODED (MAIN CABIN) · airframe 54,762 hrs · 33,471 cycles

***CORROSION*** ON TENSION STRAP AT B.S. 1016; R.B.L. 3; W.L. 208.1. / ACCOMPLISHED REPAIR IAW EA # 1-753-34582 REV IR AND ER# 19-02244 REV IR

Part: INTERCOSTAL — CRACKED (BS 312-328) · airframe 54,762 hrs · 33,471 cycles

INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, LBL 47. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 54,762 hrs · 33,471 cycles

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

Part: ANGLE — CRACKED (BS 294.5) · airframe 54,762 hrs · 33,471 cycles

OUTBOARD OF THE R1 DOOR INBOARD CHORD MOP SILL L ANGLE CRACKED AT BS. 294.5, WL. 208.1. / R&R L ANGLE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (BS 294-328) · airframe 54,762 hrs · 33,471 cycles

L1 DOOR CREASE BEAM WEB INBOARD CHORD MOP SILL CORRODED BETWEEN BS. 294.5 TO BS. 328, W.L. 208.1. R&R MOP SILL IAW SRM AND DWG.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 54,762 hrs · 33,471 cycles

AFT CABIN FLOOR PANEL 242UF HAD DAMAGED UPPER SURFACE PLIES, (BETWEEN BS. 887 TO BS. 1016). / REPAIRED FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DAMAGED (FWD CABIN) · airframe 54,762 hrs · 33,471 cycles

FORWARD CABIN FLOOR PANEL 222BF HAD DAMAGED INSERTS AND DAMAGED OUTBOARD AFT CORNER, (BETWEEN BS. 270 TO BS. 420). / REPAIRED FLOOR PANEL IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,762 hrs · 33,471 cycles

FLOORBEAM UPPER SURFACE CORRODED AT BS. 328, RBL 56. REPAIRED FLOORBEAM IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 54,762 hrs · 33,471 cycles

INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, RBL 35. / R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 54,762 hrs · 33,471 cycles

AFT LAVATORY FLOOR SUPPORT CORRODED AT BS 994, LBL 19. R&R SUPPORT PER SRM & DWG.

Part: FRAME — CRACKED (BS 312) · airframe 54,762 hrs · 33,471 cycles

FRAME AT B.S. 312 IS CRACKED IN RADIUS, JUST ABOVE FORWARD ENTRY DOOR CUT OUT, REPAIRED B.S. 312 FRAME AT CRACK IN RADIUS JUST ABOVE FOWARD ENTRY DOOR CUTOUT PER ER 19-02671 REV IR AND SWA EA 1-753-34621 REV IR.

Part: FLOOR SUPPORT — CRACKED (BS 294.5) · airframe 54,762 hrs · 33,471 cycles

INTERCOSTAL CRACKED BETWEEN BS. 277 TO BS. 294.5, BL 0. R&R INTERCOSTAL PER SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,762 hrs · 33,471 cycles

FLOORBEAM CORRODED AT BS. 986.5, BETWEEN RBL 13 TO RBL 45. REPAIRED FLOORBEAM IAW EA.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 54,762 hrs · 33,471 cycles

LOWER COMPOSITE BULKHEAD VERTICAL STIFFENER CRACKED AT BS 663, LBL 24. R&R STIFFENER IAW SRM & DWG.

Part: COVER — CRACKED (LT WING) · airframe 54,762 hrs · 33,471 cycles

DURING L/H AILERON BALANCE TAB REMOVAL FOUND # 5 HINGE INBOARD COVER CRACKED / REMOVED AND REPLACED L/H AILERON BALANCE TAB #5 HINGE COVER IAW AMM 27-11-21-400-801 3.E.(4)(D) 59143U 17MAR19

Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 54,762 hrs · 33,471 cycles

LOWER COMPOSITE BULKHEAD HORIZONTAL STIFFENER CRACKED AT BS. 663, LBL 10, BELOW CENTER TANK LOWER SKIN. / R&R STIFFENER IAW SRM AND DWG.

Part: COVER — CRACKED (RT WING) · airframe 54,762 hrs · 33,471 cycles

DURING R/H AILERON BALANCE TAB REMOVAL FOUND # 5 HINGE INBOARD COVER CRACKED / REPLACED CRACKED HINGE COVER ON R/H AILERON BALANCE TAB #S IAW AMM 27-11-21-400-801 59143U 16MAR19

Part: PANEL — DELAMINATED (LT WING) · airframe 54,762 hrs · 33,471 cycles

L/W L/E PANEL 521RB CORNER IS DISBANDED. ( MARKED ) / DISBONDED CORNER ON L/E PANEL 521RB WAS REPAIRED IAW SRM 51-70-05-2R-6 59644U 4/4/19

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,418 hrs · 33,274 cycles

LT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,418 hrs · 33,274 cycles

LT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 53,402 hrs · 32,613 cycles

FORWARD ENTRY DOOR BOTTOM EMERGENCY FLASHLIGHT SECURITY STRAP BROKEN. R&R STRAP PER SIP.

Part: BRACKET — BROKEN (GIRT BAR) · airframe 52,739 hrs · 32,224 cycles

R1 DOOR SLIDE GIRT BAR BRACKET BROKEN. R&R SLIDE ASSEMBLY IAW AMM.

Part: INTERCOSTAL — CORRODED (AFT CARGO COMPT) · airframe 51,910 hrs · 31,718 cycles

TRANSFERRED FROM LOGPAGE: AFT CARGO COMPARTMENT HAS EVIDENCE OF CORROSION AROUND AFT LAVE SERVICING PANEL PAN / REPLACED AFT LAV SERVICE PAN INTERCOSTAL ASSY IAW SRM 51-40-02-0G-0 AND DWG 146A7400

Part: HOOK — LOOSE (GIRT BAR) · airframe 51,018 hrs · 31,205 cycles

R2 DOOR SLIDE GIRT BAR STOW HOOK LOOSE. SECURED THE HOOKS IAW SIP.

Part: CYLINDER — COLLAPSED (NLG) · airframe 50,927 hrs · 31,137 cycles

DECLARED EMERGENCY, ON TAKEOFF, AFTER RETRACTING THE LANDING GEAR, NOSE STRUT COLLAPSED. R&R NOSE LANDING GEAR INNER GEAR CYLINDER PER AMM.

Part: RIVET — LOOSE (L2 DOOR) · airframe 50,830 hrs · 31,072 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT STOWAGE HOOK LOOSE. R&R RIVET PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,206 hrs · 30,676 cycles

RT EMERGENCY ESCAPE HATCH FORWARD LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,871 hrs · 30,464 cycles

FORWARD OF RT OVERWING WALL MOUNTED EMERGENCY EXIT LIGHT BULB INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — UNSECURE (CABIN) · airframe 49,629 hrs · 30,325 cycles

R1 DOOR LOWER EXIT SIGN LIGHT ASSEMBLY FELL OFF. R&R LIGHT ASSEMBLY IAW AMM.

Part: FAN — FAULTY (CABIN) · airframe 49,470 hrs · 30,236 cycles

ELECTRICAL SMELL AND HAZE IN THE AFT GALLEY. TURNED RECIRCULATION SWITCH AND CABIN UTILIZATION OFF. SMELL AND HAZE DECREASED. R&R RECIRCULATION FAN PER AMM.

Part: COLLAR — DAMAGED (EVAC SLIDE) · airframe 48,875 hrs · 29,882 cycles

L1 DOOR SLIDE FORWARD GIRT BAR COLLAR ROLL PIN DAMAGED. R&R COLLAR PER MT AND AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,248 hrs · 29,509 cycles

RT EMERGENCY EXIT LIGHT INOP AT BS 1000, AFT OF TRAILING EDGE FLAP. R&R LIGHT IAW AMM.

Part: LIGHT — LOOSE (AFT CABIN) · airframe 47,956 hrs · 29,338 cycles

AFT LEFT EMERGENCY LIGHT STRIP LOOSE. SECURED THE LIGHT IAW SIP.

Part: COVER — BROKEN (CABIN) · airframe 45,524 hrs · 27,951 cycles

R1 FWD DOOR EMER EXIT LIGHT COVER BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,145 hrs · 27,739 cycles

EMERGENCY BULLNOSE LIGHT INOPERATIVE AT ROW 11 DEF. RELAMPED IAW MM.

Part: GIRT BAR — LOOSE (L2 DOOR) · airframe 44,230 hrs · 27,190 cycles

L2 DOOR GIRT BAR BRACKET LOOSE. SECURED GIRT BAR IAW SIP.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 43,358 hrs · 26,669 cycles

AFT GALLEY OVERHEAD EXIT SIGN LIGHT LENS FELL OFF. INSTALLED LENS ASSEMBLY IAW MM.

Part: SENSOR — FAULTY (CABIN TEMP) · airframe 43,162 hrs · 26,556 cycles

ON DESCENT BURNING SMELL IN COCKPIT AT 121,000', DISSIPATED BY 17,000'. MORE OF A PLASTIC BURNING SMELL. NO HOTSPOTS NOTED BY HAND IN COCKPIT. NO OVERHEATED WINDOWS. CAPTAIN MAP LIGHT WAS LEFT ON & WAS HOT BUT DID NOT SMELL. DISSIPATED SMELL NEVER RETURNED. R & R CONTROL CABIN TEMP SENSOR IAW SIP.

Part: LATCH — BROKEN (CABIN) · airframe 42,941 hrs · 26,426 cycles

EMERGENCY LIGHT CONNECTOR LATCH BROKEN AT BS 727E+18, LBL 19. REPLACED LATCH IAW WDM.

Part: SIGN — DISPLACED (CABIN) · airframe 42,941 hrs · 26,426 cycles

LEFT EMER EXIT CEILING PANEL SIGN DISPLACED AT ROW 18. REPLACED SIGN IAW EA.

Part: WIRE — DAMAGED (CABIN) · airframe 42,941 hrs · 26,426 cycles

LEFT AFT BULLNOSE EMER LIGHT INOPERATIVE. REPAIRED WIRE IAW ER & EA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

WING TO BODY FAIRING SUPPORT CRACKED AT BS 670, RBL 10. R & R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

INTERCOSTAL CORRODED AT STATION 847 - 857, RBL 26, WL 155. REPAIRED INTERCOSTAL IAW SRM.

Part: STRAP — CORRODED (EMERGENCY EXIT) · airframe 42,941 hrs · 26,426 cycles

RIGHT EMER EXIT HATCH ESCAPE STRAP HOOK END CORRODED. R & R STRAP IAW AMM.

Part: STRAP — CORRODED (EMERGENCY EXIT) · airframe 42,941 hrs · 26,426 cycles

LEFT EMER EXIT HATCH ESCAPE STRAP HOOK END CORRODED. R & R STRAP IAW AMM.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FORWARD APU BULKHEAD, RT VERTICAL STIFFENER TO FUSELAGE SKIN CLIP TEE FITTING CORRODED AT BS 1088, RBL 10. R & R TEE FITTING IAW SRM & DWG.

Part: SKIN — CRACKED (BS 540) · airframe 42,941 hrs · 26,426 cycles

FOUND THE FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED THE SKIN IAW EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 42,941 hrs · 26,426 cycles

RIGHT HORIZONTAL STABILIZER 101.90 RIB, 2ND FROM THE FRONT VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 42,941 hrs · 26,426 cycles

LEFT WING FIXED TE UPPER PANEL ABOVE PYLON AFT FAIRING, VERTICAL PANEL SUPPORT ANGLE CRACKED, AT OTBD RIVET HOLES. R & R ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FUSELAGE SKIN CORRODED AT WATER SERVICE PANEL CUT OUT FWD HINGE, APPROX STATION 967 - 986, STRINGER 24R. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

CREASE BEAM INBD CHORD CORRODED BETWEEN BS 947 - 995, RBL 52. R & R CHORD IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

CREASE BEAM INBD CHORD CORRODED BETWEEN BS 947 TO 986, LBL 52. R & R CHORD IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

LEFT NR 1 WINDOW FRAME CRACKED IN UPPER AFT CORNER. REPAIRED FRAME IAW ACO.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,941 hrs · 26,426 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.7, SECOND VERTICAL STIFFENER FROM LE. REPAIRED RIB IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FORWARD CARGO BAY FWD INTERCOSTAL ATTACH ANGLE CRACKED BETWEEN BS 500C - 500D, STRINGER 26L. R & R ANGLE IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 488 - 500D, LBL 24. R & R PLATE IAW SRM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE, CRACKED BETWEEN BS 400 - 488, LBL 24. R & R SUPPORT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

R1 DOOR FWD LOWER STUB FRAME COMMON TO INBD CHORD CRACKED AT STRINGER 17R. R & R FRAME IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FORWARD CARGO BAY FWD & AFT INTERCOSTAL ATTACH ANGLE CRACKED BETWEEN BS 500C - 500B, STRINGER 26L. R & R ANGLE IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 420 - 440, RBL 24. R & R PLATE IAW SRM & AMM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

REINFORCED STRAP AT INBD VERTICAL CHORD CORRODED BETWEEN BS 294 - 300, STRINGER 17R. R & R STRAP IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FORWARD CARGO BAY FWD INTERCOSTAL ATTACH ANGLE CRACKED BETWEEN BS 400 - 420, STRINGER 26L. R & R ANGLE IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FORWARD CARGO BAY FWD & AFT INTERCOSTAL ATTACH ANGLE CRACKED BETWEEN BS 500A - 500B, STRINGER 26L. R & R ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FORWARD CARGO BAY INTERCOSTAL UPPER FLANGE CRACKED AT FASTENER HOLE BETWEEN BS 500A - 500, STRINGER 26L. R & R INTERCOSTAL IAW SRM.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FORWARD CARGO BAY FWD INTERCOSTAL ATTACH ANGLE CRACKED BETWEEN BS 500C - 500D, STRINGER 26R. R & R ANGLE IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

INTERCOSTAL CRACKED AT STATION 500C - 500B, STRINGER 26R. REPAIRED INTERCOSTAL IAW EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FORWARD CARGO BAY AFT INTERCOSTAL ATTACH ANGLE CRACKED BETWEEN BS 500A - 500, STRINGER I6L. R & R ANGLE IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

AFT CARGO DOOR THRESHOLD WEB CORRODED AT STATION 774, RBL 21, WL 155. REPAIRED WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FLOOR SUPPORT CORRODED AT STATION 773, LBL 3, WL 155. REPAIRED SUPPORT IAW EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FLOOR STRAP CORRODED AT STATION 887, RBL 22 TO LBL 16, WL 155. REPAIRED STRAP IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FLOOR SUPPORT CORRODED AT STATION 773, LBL 8, WL 155. REPAIRED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FLOOR SUPPORT CORRODED AT STATION 773, RBL 3, WL 155. REPAIRED SUPPORT IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FLOOR SUPPORT CORRODED AT BS 773, RBL 8. REPAIRED SUPPORT IAW SRM & EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

FLOOR SUPPORT CORRODED AT STATION 773, LBL 13, WL 155. REPAIRED SUPPORT IAW EA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

BULKHEAD SUPPORT CRACKED AT BS 727+3, RBL 3. R & R SUPPORT IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,941 hrs · 26,426 cycles

BULKHEAD SUPPORT SPLICE ANGLE CRACKED AT BS 866, LBL 15. R & R ANGLE IAW SRM.