N7850B

Part: GIRT BAR — LOOSE (ZN 200 FUS TOP) · airframe 62,988 hrs · 41,580 cycles

FWD SERVICE DOOR GIRT BAR HOLDER LOOSE<[01] RESECURE & OP?S CK?D GIRT BAR PER AMM 26-66-01.OP?S CK?D GOOD.

Part: SLAT — CRACKED (ZN 400 NACELLE/P) · airframe 53,028 hrs · 29,664 cycles

#2 ENGINE RTF STRUT 15 AT C2 LOCATION HAS .500 CRACK INDICATION. AND STRUT 16 AT C2LOCATION HAS A .400 CRACK INDICATION AND STRUT 1 AT C2 LOCATION HAS A.200 CRACK INDICATION AND STRUT 2 AT C2 LOCATION HAS A .200 CRACK INDICATION.<[01] OK FOR REINSPECTION IN 700 CYCLES

Part: LENS — LOOSE (EMERGENCY LIGHTS) · airframe 60,374 hrs · 39,866 cycles

LIGHT LENS OVER LH/RH EMERGENCY EXIT WINDDOWS LOOSE. RESECURED LIGHT LENSES PER AMM 33-21-00.

Part: NONE — INOPERATIVE (PAX CABIN) · airframe 59,789 hrs · 39,475 cycles

EXIT SIGN AFT RIGHT SIDE INOP / [01] C/W TASK CARD M-21-133-00720 OK TO CONTINUE PER TLD. SIGN TAPED SECURE AND OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: ASSIST ASSY — LOOSE (L1 DOOR) · airframe 59,194 hrs · 39,098 cycles

FED SURROUND; AFT DOOR ASSIST HANDLE UPPER END IS LOOSE. / [01] TIGHTENED FED SURROUND AFT DOOR ASSIST HANDLE UPPER END PER AMM 25-21-31-420-802.;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.

Part: BULB — INOPERATIVE (AFT CABIN) · airframe 59,194 hrs · 39,098 cycles

AFT EMERGENCY COVE LIGHT DOES NOT ILLUMINATE. / [01] REPLACED AFT EMERGENCY COVE LIGHT BULB PER <BR>AMM 33-51-03-960-801-NG STEPS 2.D;[02] TEST OF BULB WAS GOOD;[03] TEST OF BULB DONE PER AMM 33-51-03-960-801-NG;[04] VERIFIED WORK IN ACTION ITEMS 1 THRU 3.;[05] VERIFIED CORRECTIVE ACTION ITEMS 1 - 4.

Part: LIGHT — INOPERATIVE (FWD CABIN) · airframe 59,194 hrs · 39,098 cycles

FORWARD ENTRY LIGHT CENTER BULB AND AFT CENTER INDICATOR LEFT SIDE LIGHT BULB 2 IN BURNED OUT. / [01] REPLACED FORWARD ENTRY CENTER BULB PER AMM 33-51-03-960-801-NGSTEPS 2.D.;[02] TEST OF BULB WAS GOOD;[03] TEST OF BULB WAS DONE PER AMM 33-51-03-960-801-NG;[04] VERIFIED REPLACEMENT AND SATISFACTORY TEST OF FORWARD CENTER ENTRY LIGHT PER AMM 33-51-03-960-801.;[05] REJECTION: FORWARD ENTRY LIGHT (LOWER LIGHT ASSEMBLY ATTACHED TO FWD LAV WALL) CENTER BULB REMAINS OUT.;[06] RE-LAMPED AND PERFORMED GOOD OPS TEST OF AFT CENTER INDICATOR LIGHT PER AMM 33-51-01-960-801. REMOVED AND REPLACED FWD ENTRY EXIT SIGN LIGHT ASSEMBLY AND PERFORMED GOOD OPS TEST OF FWD ENTRY EXIT SIGN LIGHT ASSEMBLY PER AMM 33-51-01-960-802.;[07] VERIFIED CORRECTIVE ACTIONS STEP 6.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 59,194 hrs · 39,098 cycles

EMERGENCY LIGHTS ATTACHED TO M1669 ARE INOPERATIVE. / [01] CORRECTION TO ORIGINAL FAULT: CORRECT POWER SUPPLY IS M1668.;[02] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 1.;[03] REMOVED EMERGENCY LIGHT BATTERY PACK M1668 AND INSTALLED SERVICEABLE BATTERY PACK AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-06-960-805;[04] VERIFIED CORRECTIVE ACTIONS STEP 3.

Part: SPLICE — CORRODED (AFT CARGO) · airframe 59,194 hrs · 39,098 cycles

CORROSION ON AFT CARGO BAY FLOOR SPLICE BS 727D+5' LBL 21-RBL 21; P/N 146A9401-8 / [01] NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM; REPAIR BY REPLACEMENT IAW SRM 51-10-02 PARAGRAPH 9. RECEIVED NEW PART ITEM: 146A9401-8 PO NUMBER: 864547 /1;[02] UPDATED MEASUREMENTS;[03] VERIFIED CORRECTIVE ACTION 1-2;[04] MEASUREMENT TABLE VERIFIED

Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,194 hrs · 39,098 cycles

CORRODED ANGLE ASSY; LOCATED AT APU COMPT CUTOUT LH SIDE; LBL 22; BS 1092 TO BS 1135 / [01] ADDED MEASUREMENTS.;[02] PARTIAL UPDATE TO STEP 1;[03] PARTIAL UPDATE TO STEPS 2-3.;[04] PARTIAL UPDATE TO STEPS 4-6;[05] PARTIAL UPDATE TO STEP 7.;[06] STEPS 2-7 PARTIAL UPDATED.;[07] ANGLE WAS FOUND TO BE OUT OF LIMITS; WILL BE REPAIRED BY REPLACE PART IAW SRM 51-10-02 PAR. 9.<BR><BR>RECEIVED NEW ANGLE P/N: 148A8615-54 ; LOT: 1493960-1 ; P.O/N: 871423/1.;[08] RECEIVED LOCATED AND DRILLED NEW ANGLE ASSY LOCATED FROM B/S 1088 TO B/S 1156 AT APU COMPT CUT OUT L/H SIDE LBL22 ; P/N: 148A8615-54; LOT#1493960-1 IAW SRM 51-40-05 AND DWG 148A8600 REV:- DWG 148A1670 REV:B;[09] OK TO INSTALL NEW ASSY ANGLE;[10] VERIFIED CORRECTIVE ACTIONS 7; 8 AND 9. OK TO INSTALL GIVEN..;[11] INSTALLED NEW ANGLE ASSY LOCATED FROM B/S 1088 TO B/S 1156 AT APU COMPT CUT OUT L/H SIDE LBL22 IAW SRM 51-40-02 AND DWG 148A8600 REV:-;[12] VERIFIED CORRECTIVE ACTION 11 AND MEASUREMENT TABLE.;[13] WORKSCOPE COMPLETE.

Part: PANEL — DEBONDED (L/H WING) · airframe 59,194 hrs · 39,098 cycles

L/W L/E PANEL 521TB DISBONDED ON CORNER / [01] IDENTIFIED LEADING EDGE PANEL 521TB MATERIAL IAW SRM 57-41-01-OI-4; FIGURE 3; ITEM 1; TABLE 3. FOUND DAMAGED PANEL NOT TO BE WITHIN ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 TABLE 101. PARA 4.A.5. AND WILL REPAIRED IAW SRM 57-41-01-2R-1 PARA 4.E AND SRM 51-70-05-2R-6. REMOVED 2EA BACKUP PLATE TO FACILITATE REPAIR IAW SRM 51-40-02-OG-0 PARA 4.E.<BR>STARTED REMOVING ALUMINUM FOIL TO FACILITATE REPAIR IAW SRM 51-70-14-2R-3 PARA 4.A.(2).E.;[02] VALIDATED APPLICABILITY OF SRM 51-70-05-2R-6.;[03] COMPLETED REMOVING ENTIRE ALUMINUM FOIL TO FACILITATE REPAIR IAW SRM 51-70-14-2R-3 PARA 4.A.(2).E.;[04] REMOVED DAMAGED PLIES AND CLEANED REPAIR AREA IAW SRM 51-70-05-2R-6 PARA 4.A-D.;[05] VERIFIED CORRECTIVE ACTION ENTRY 4.;[06] VERIFIED CORRECTIVE ACTIONS 1-3;[07] FABRICATED AND INSTALLED REPAIR PLIES USING REPAIR FABRIC BMS 8-79 ST 120 LOT#1488453-1; BMS 8-79 ST 1581 LOT#1486928-1 AND ADHESIVE FILM BMS 5-129 GR 05 LOT#1491228-1. ALL IAW SRM 51-70-05-2R-6 PARA 4. E.;[11] FABRICATED ALUMINUM FOIL USING BMS 8-289 LOT#1484605-1 INSTALLED USING BMS 5-128 LOT#JH1LAA7523 VACUUM BAGGED; LEAK CHECK GOOD USING VACUUM GAUGE ID: ATS2107 DUE: 09/2022 IAW SRM 51-70-14-2R-3 PARA 4.A.3-7;11(A-J).;

Part: PANEL — DEBONDED (L/H WING) · airframe 59,194 hrs · 39,098 cycles

L/W L/E PANEL 521DB HAS DISBONDED CORNERS / [01] IDENTIFIED PANEL IAW SRM 57-41-01-0I-4 FIGURE 5 ITEM [2]. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 57-41-1A-1 PARAGRAPH 4.A.(5).(A) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-6 PER SRM 57-41-01-2R-1 PARAGRAPH 2.F. REMOVED 1 EA BACKUP PLATE IAW SRM 51-40-02-0G-0 PARAGRAPH 4.E. REMOVED INNER FOIL PLY IAW SRM 51-70-14-2R-3 PARAGRAPH 4.A(1-2). REMOVED INNER SURFACE EDGEBAND PLY DAMAGE FROM THE THREE INBOARD MOST LEADING EDGE CORNERS; THE LARGEST AREA OF DAMAGE REMOVED WAS 0.75'X0.25'; TAPERS AND ALL AREAS AND CLEANED ALL AREAS; WORK PERFORMED IAW SRM 51-70-05-2R-6 PARAGRAPH 4.A-D.;[04] FABRICATED REPAIR PLIES FROM BMS5-129 GRADE 05 LOT NUMBER 1488462-1; BMS8-79 STYLE 1581 LOT NUMBER 1486928-1 AND BMS8-79 STYLE 120 LOT NUMBER 1488453-1; INSTALLED PLIES; VERIFIED 5X5 AND SET PLIES TO CURE USING HOTBONDER ID: ATS883 DUE: 10/2022; WORK PERFORMED IAW SRM 51-70-05-2R-6 PARAGRAPH 4.E-G.[08] FABRICATED REPAIR FOIL FORM BMS8-289 LOT NUMBER 1484605-1; INSTALLED FOIL WITH BMS5-128 LOT NUMBER JH1LAA7523; VACUUM BAGGED REPAIR; VERIFIED SATISFACTORY 5X5 USING VACUUM GAUGE ID: ATS2438 DUE: 03/2023; CURED REPAIR UNDER HEAT LAMP USING THERMOMETER ID: ATS2209 DUE: 10/2022; TO VERIFY TEMPERATURE; UNBAGGED FOIL; TRIMMED EDGES; AND REFINISHED PANEL'S TOOLSIDE IAW SRM 51-70-14-2R-3 PARAGRAPH 4.A.(3-4).(5).(A) AND (11). INSTALLED REMOVED BACK-UP PLATES IAW SRM 51-40-02-0G-0 PARAGRAPH 4.A-C AND 10; ALSO IAW DRAWING 116A9110 SHEET 14.;

Part: PANEL — DEBONDED (L/H WING) · airframe 59,194 hrs · 39,098 cycles

L/W L/E PANEL 521RB DISBONDED ON CORNER / [01] IDENTIFIED LEADING EDGE PANEL 521RB MATERIAL IAW SRM 57-41-01-OI-4; FIGURE 3; ITEM 2; TABLE 3. FOUND DAMAGED PANEL NOT TO BE WITHIN ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 TABLE 101. PARA 4.A.5. AND WILL REPAIRED IAW SRM 57-41-01-2R-1 PARA 4.E AND SRM 51-70-05-2R-6. REMOVED THE DAMAGE FROM THE INNER SURFACE; NO MOISTURE NOTED AND CLEANED PER SRM 51-70-05-2R-6 PARA 4.A-D.;[02] REMOVED 1EA BACKUP PLATE TO FACILITATE REPAIR IAW SRM 51-40-02-OG-0 PARA 4.E.<BR>REMOVED ENTIRE ALUMINUM FOIL TO FACILITATE REPAIR IAW SRM 51-70-14-2R-3 PARA 4.A.(2).E.;[03] VALIDATED APPLICABILITY OF SRM 51-70-05-2R-6.;[04] UPDATED MEASUREMENTS.;[05] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 1 THRU 4. OKAY TO PROCEED PER SRM 51-70-05-2R-6.;[06] CUT OUT REPAIR PLIES USING BMS 5-129TY2GR05 250DEG. LOT: 1491228-1; BMS 8-79CL3ST120 LOT: 1488453-1; BMS 8-79CL3ST1581 LOT:1486928-1<BR>ALSO; INSTALLED REPAIRS PLIES IAW SRM 51-70-05-2R-6 PARA 4.E.;[10] FABRICATED ALUMINUM FOIL USING BMS 8-289 LOT#1484605-1 INSTALLED USING BMS 5-128 LOT#JH1LAA7523 VACUUM BAGGED; LEAK CHECK GOOD USING VACUUM GAUGE ID: ATS2107 DUE: 09/2022 IAW SRM 51-70-14-2R-3 PARA 4.A.3-7;11(A-J).[12] REMOVED 1 EA. BACK PLATE TO FACILITATE REPAIR AND REINSTALLED 1 EA. BACK PLATE AFTER REPAIR PER. SRM 51-40-02-0G-0 PAR.4E AND PAR.4B.

Part: PANEL — DEBONDED (R/H WING) · airframe 59,194 hrs · 39,098 cycles

R/W L/E PANEL 621QB HAS DISBONDED CORNER / [01] REMOVED 1EA. BACKUP PLATE ACCORDING TO SRM 51-40-02; PARA. 4.E.<BR><BR>REMOVED UPPER SURFACE BONDED ALUMINUM FOIL TO FACILITATE EVALUATION ACCORDING TO SRM 51-70-14-2R-3; PARA. 4.A.(2).(B).;[02] IDENTIFIED PANEL 621QB MATERIAL ACCORDING TO SRM 57-41-01-0I-4; FIG. 3; TABLE 3; ITEM 2; AND FIG. 11; TABLE 10 .<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1; PARA'S 2.B AND 4.A.(5) & (6); AND FIG. 106.<BR><BR>AREAS TO BE REPAIRED ACCORDING TO SRM 51-70-05-2R-6; AS REQUIRED BY SRM 57-41-01-2R-1; PARA'S 2; 4.B; AND TABLE 202.<BR><BR>STRIPPED LOWER SURFACE PAINTS/PRIMERS; REMOVED ERODED PLIES TO A REGULAR SHAPE IN TWO AREAS; TAP TESTED AREAS (NO DISBONDS NOTED); REMOVED CONTAMINANTS FROM REPAIR AREA; ALL ACCORDING TO SRM 51-70-05-2R-6; PARA'S 4.A THRU 4.D.;[05] FABRICATED REPAIR PLIES USING BMS5-129TY2 GR05 LOT#1488462-1; BMS8-79CL3ST1581 LOT#1491918-1; AND BMS8-79CL3ST120 LOT#1493862-1 IAW SRM 51-70-05-2R-6 PAR.4 E;[06] INSTALLED REPAIR PLIES; VACUUM BAGGED; LEAK CHECK GOOD AND SET TO CURE USING HOTBONDER ID:ATS883 CAL DUE 10/2022 IAW SRM 51-70-05-2R-6 PARA 4E-G.;[10] FABRICATED FOIL REPAIR PLY FROM BMS8-289 LOT#1484605-1; INSTALLED FOIL USING BMS5-128 LOT#JH1LAA7523. VACUUM BAGGED; LEAK CHECKED GOOD USING VACUUM GAUGE ID:ATS2107 CAL DUE:09/2022. IAW SRM 51-70-14-2R-3 PAR.4 A(3-5A;11A-J);

Part: PANEL — DEBONDED (R/H WING) · airframe 59,194 hrs · 39,098 cycles

R/W L/E PANEL 621DB CORNERS ARE DISBONDED / [01] REMOVED 2EA. BACKUP PLATES ACCORDING TO SRM 51-40-02; PARA. 4.E.<BR><BR>REMOVED UPPER SURFACE BONDED ALUMINUM FOIL TO FACILITATE EVALUATION ACCORDING TO SRM 51-70-14-2R-3; PARA. 4.A.(2).(B).;[02] REMOVED LOWER SURFACE FINISHES TO FACILITATE EVALUATION ACCORDING TO AMM 51-21-99-300-802; PARA. 3.C.(3).(A) THRU (D).;[03] IDENTIFIED PANEL 621DB MATERIAL ACCORDING TO SRM 57-41-01-0I-4; FIG. 5; TABLE 5; ITEM 2; AND FIG. 19; TABLE 16.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1; PARA'S 2.B AND 4.A.(5) & (6); AND FIG. 106.<BR><BR>AREAS TO BE REPAIRED ACCORDING TO SRM 51-70-05-2R-6; AS REQUIRED BY SRM 57-41-01-2R-1; PARA'S 2; 4.B; AND TABLE 202.<BR><BR>REMOVED ERODED PLIES TO A REGULAR SHAPE IN TWO AREAS; TAP TESTED AREAS (NO DISBONDS NOTED); REMOVED CONTAMINANTS FROM REPAIR AREAS; ALL ACCORDING TO SRM 51-70-05-2R-6; PARA'S 4.A THRU 4.D.;[[11] FABRICATED FOIL REPAIR PLY FROM BMS8-289 LOT#1484605-1; INSTALLED FOIL USING BMS5-128 LOT#JH1LAA7523. VACUUM BAGGED; LEAK CHECKED GOOD USING VACUUM GAUGE ID:ATS2107 CAL DUE:09/2022. IAW SRM 51-70-14-2R-3 PAR.4 A(3-5A;11A-J);14] INSTALLED (2EA) BACK-UP PLATES IAW SRM 51-40-02-0G-0 PAR.4 B-C & BOEING DWG 116A9110-3<BR><BR>APPLIED; CURED; AND TESTED CONDUCTIVE COATING LOT#S22B211; RESISTIVITY CHECKED GOOD USING MULTIMETER ID:ATS1658 CAL DUE:03/2023 IAW AMM 51-21-71-370-801 PAR.3 D(1-4;7A);

Part: ATTACH ANGLE — CORRODED (FWD CARGO) · airframe 59,194 hrs · 39,098 cycles

CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT TO FRAME ATTACH ANGLE AT RBL 23 BS 400+19.(MARKED) / [01] THERE IS NO SRM ALLOWABLE DAMAGE FOR FCB FLOOR TO SIDEWALL SUPPORT TO FRAME ATTACH ANGLE. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED FCB FLOOR TO SIDWALL SUPPORT TO FRAME ATTACH ANGLE AT RBL23 BS 400+19 IAW SRM 51-40-02-0G-0;[03] RECEIVED NEW ATTACH ANGLE <BR>ITEM# : HFAB53-CL-012<BR>PO# : 871963/1<BR><BR>LOCATED; AND DRILLED NEW ATTACH ANGLE MATERIAL USING BAC1503-100593#7075-T73511 LOT# : 1494279-1 IAW SRM 51-40-05-0G-0 AND DWG 143A7500 ID:0018 REV:A;[04] VERIFIED CORRECTIVE ACTION 3;[05] VERIFIED MEASUREMENT TABLE;[06] ACCOMPLISHED BORIC ACID-SULFURIC ANODIZE ON NEW ANGLE (CLIP) ITEM : HFAB53-CL-011 LOT#: 1494790 P/O#: 872132/1 . APPLIED PRIMER IAW AMM 51-21-72-370-804;[07] OK TO INSTALL NEW ANGLE (CLIP);[08] VERIFIED CORRECTIVE ACTION ITEM 6-7; OK TO INSTALL.;[09] INSTALLED NEW ANGLE AT FCB RBL23 BS 400+19 IAW SRM 51-40-02-0G-0 AND DWG:143A7500 ID: 0013 REV:A.;[10] VERIFIED CORRECTIVE ACTION #9

Part: WEB — CORRODED (AFT CARGO) · airframe 59,194 hrs · 39,098 cycles

CORROSION ON AFT CARGO BAY THRESHOLD AT RBL 26 BS 807+1; BS 807+6; BS 827+4. / [01] REMOVED CORROSION AT ACB THRESHOLD RBL 26; <BR>BS 807+1; L=0.8' W=0.7' D=0.007'<BR>BS 807+6; L=0.6' W=0.5' D=0.011' <BR>BS 827+4; L=0.7' W=0.5' D=0.006'<BR> <BR>FOUND TO BE OUT OF LIMITS WITH REMAINING THICKNESS OF 0.034' OF ORIGINAL THICKNESS 0.045' IAW SRM 53-60-15-0I-1 AND SRM 53-60-15-1A-1 <BR><BR>TOOL USED DEPTH GAGE<BR>ID:ATS2473 <BR>S/N: UNKNOWN <BR>DUE DATE:07/2022;[02] VERIFIED CORRECTIVE ACTION ITEM 1. THRESHOLD WEB IS OUT OF LIMITS PER SRM 53-60-15-0I-1 AND SRM 53-60-15-1A-1.;[03] THRESHOLD WEB WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-40-02 PAR 9. <BR><BR>RECEIVED NEW WEB P/N:146A8123U25 ; LOT:1493804-1; P.O/N: 871289/1 AND LOCATED AND DRILLEW NEW WEB AT AFT CARGO BAY BTW BS 792 TO BS 849 ; RBL 20 TO RBL 28 IAW SRM 51-40-05.;[04] VERIFIED CORRECTIVE ACTION ITEM 3; MEASUREMENT FIELDS 19 AND 22 INCORRECT.;[05] FIXED MEASUREMENT CHART;[06] TASK CARD COMPLETE;[07] VERIFIED MEASUREMENT FIELDS; JOB COMPLETE.

Part: WEB — CRACKED (FUSELAGE) · airframe 59,194 hrs · 39,098 cycles

CRACK FOUND ON HORIZONTAL PRESSURE DECK; RBL 40; BS 663+2 AS MARKED. / [01] REMOVED THE ADJACENT STRUCTURE; FASTENERS COMMON TO THE DAMAGE WEB IAW SRM 51-40-02. CUTED AND REMOVED THE DAMAGE PART OF THE WEB PER SRM 53-40-51-2R-2.;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.;[03] HFEC INSPECTED CUT EDGE; AND ALL HOLES IN THE REPAIR AREA; PER NDTM PT 6 51-00-00 PROCEDURE 23 AND 16; NO CRACKS NOTED; EQUIP ID IS000680 04/2023<BR><BR>VISUALLY INSPECTED AT AND AROUND REPAIR AREA; NO DEFECTS NOTED;[04] LOCATED; DRILLED AND TRIMMED TO SIZE -1 DOUBLER MADE FROM 2024-T3 CLAD LOT# 1483761-1; -2 STIFFENERS (7EA); MADE FROM BAC1505-100052#7075-T6511 LOT# 1483757-1; AND -3 WEB MADE FROM 2024-T3 CLAD LOT# 1477768-1 PER SRM 53-40-51-2R-2 PARA. 4E-G (TABLE 201);

Part: SHIELD — CORRODED (AFT CARGO) · airframe 59,194 hrs · 39,098 cycles

CORROSION ON AFT CARGO BAY FWD SHIELD AT RBL 21 BS 767+2; BS 767+4. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPACEMENT IAW SRM 51-10-02-0G-0;[02] LOCATED AND DRILLED AFT CARGO BAY FWD NEW SHIELD AT RBL 21 WL 156 BS 767 TO BS 787+6 P/N 146A8127-1 LOT: 1482004 PO:856768/1 IAW SRM 51-40-05 AND DWG 146A8127 REV:C.;[03] VERIFIED CORRECTIVE ACTION 1 AND 2. NEW SHIELD WILL BE INSTALLED ON TTG8Q004E52Q;[04] VERIFIED MEASUREMENT TABLE

Part: SHIELD — CORRODED (FWD CARGO) · airframe 59,194 hrs · 39,098 cycles

CORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 24 BS 500+10; BS 500+18. / [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: 1484884/1 PO:860330/1 IAW SRM 51-40-05 AND DWG 143A8126 REV:A.;[03] SIGNED FOR PART USED.;[04] VERIFIED CORRECTIVE ACTION 1 AND 2. SHIELD WILL BE INSTALLED ON TTG8Q004EC7D;[05] VERIFIED CORRECTIVE ACTION 1; 2 AND THE MEASUREMENT TABLE. SHIELD WILL BE INSTALLED ON TTG8Q004EC7D

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 59,194 hrs · 39,098 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727E+10; BS 727E+14; BS 727E+18; BS 747+5; BS 747+10; BS 747+18. / [01] REMOVED CORROSION AT<BR>727E+10 0.012' ( THE DEEPEST DAMAGE)<BR>727E+14 0.010'<BR>727E+18 0.011'<BR>747+5 0.010'<BR>747+10 0.011'<BR>747+18 0.007'<BR>IAW SRM 51-10-02-0G-0G<BR><BR>CALIBRATION TOOL DEPTH GAUGE<BR>ID : ATS2472<BR>S/N : UNKNOWN<BR>DUE : 12/2022;[02] ORIGINAL MATERIAL THICKNESS : 0.040' THE DEEPEST DAMAGE AT 727E+10 : 0.012' REMAINING THICKNESS : 0.028' THE DAMAGE EXCEED 10% OF ORIGINAL MATERIAL THICKNESS. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2;[03] VERIFIED DAMAGE ON SIDEWALL SUPPORT IS OUT OF LIMITS PER SRM 53-00-53-1A-2.;[04] LOCATED; DRILLED; AND COUNTERSANK NEW FLOOR TO SIDEWALL SUPPORT MATERIAL USING BAC1496-377#7075T62 LOT#1490497-1 IAW SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 146A7502 ID:0002 REV:A;[05] APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01-0G-0; AND SOPM 20-41-02;[06] VERIFIED CORRECTIVE ACTIONS 4-5;[07] VERIFIED MEASUREMENT TABLE

Part: ATTACH ANGLE — CRACKED (AFT CARGO) · airframe 59,194 hrs · 39,098 cycles

CRACK ON AFT CARGO BAY AFT BULKHEAD SUPPORT LOWER ATTACH ANGLE AT LBL 10 BS 847+18. / [01] REMOVED AND REPLACED AFT CARGO BAY AFT BULKHEAD SUPPORT LOWER ATTACH ANGLE(SUPPORT BRACKET) AT LBL 10 BS 847+18; PN#149A8109-21 IAW SRM 51-40-02 AND IAW DWG#149A8102;[02] CRACKED ON AFT CARGO BAY AFT BULKHEAD SUPPORT LOWER ATTACH ANGLE(SUPPORT BRACKET) AT LBL 10 BS 847+18 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. PART IS TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PAR 9C;[03] VERIFIED CORRECTIVE ACTION 1-2;[04] UPDATED MEASUREMENTS

Part: STRINGER — CRACKED (FWD CARGO) · airframe 59,194 hrs · 39,098 cycles

CRACK ON FWD CARGO BAY BS 540 R/H STRINGER 25. / [01] PARTIAL UPDATE STEP 1-2;[02] EVALUATED CRACK AT STRINGER 25 R/H BS 540 STRINGER FOUND OUT OF LIMIT IAW SRM 53-00-03-1A-1 PARAGRAPH 4A(2)(A)1;[03] VERIFIED APPLICABILITY FOR STR 25 R/H IAW SRM 53-00-03-2R-1 <BR> PAR 4 ; FIG 206.<BR><BR>REMOVED FASTENERS BTW B/S 500D TO B/S 540 AND REMOVED DAMAGE BY TRIMMING OUT STRINGER SECTION BTW B/S 500D+12' AT STR 25 R/H IAW SRM 53-00-03-2R-1 <BR> PAR 4 ; FIG 206.;[04] PARTIAL UPDATE STEP 4-5.;[05] VERIFIED CORRECTIVE ACTION 2-3; AND UPDATED PARTIAL FOR FOR STEP 3.;[06] COMPLETED STEPS 6 AND 7.;[07] PARTIAL UPDATE STEP 8- SHEAR TIE REMOVAL;[08] RECEIVED NEW STRINGER SECTION P/N: HFAB53-STS-011 ; P.O/N: 871251/1 ; NEW J-ANGLE (2 EA) P/N:HFAB53-JA-011 ; LOT: 1493979-1 ; P.O/N:871249/1 ; NEW U-CHANEL P/N: HFAB53-UC-011 ; LOT : 1493980-1; P.O/N: 871252/1.<BR><BR>LOCATED AND DRILLED REPAIR PARTS AT FCB STR 25 R/H BTW BS 500D+6' TO BS 536 AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 53-00-03-2R-1 PAR 4 STEPS D - I FIG 206 AND EA NO.: 22-153-01692 REV. A. REQUEST OK TO PRIMER.16] INSTALLED REPAIR PARTS AT FCB STR 25 R/H BTW BS 500D+6' TO BS 536 IAW SRM 53-00-03-2R-1 PAR 4 ; FIG 206 AND EA NO.: 22-153-01692 REV. A.;[28] 'REPAIRED PER EA 22-153-01692.'

Part: STRINGER — CRACKED (FWD CARGO) · airframe 59,194 hrs · 39,098 cycles

CRACK ON FWD CARGO BAY BS 540 R/H STRINGER 27. / [01] EVALUATED CRACK AT STRINGER 27R/H B/S 540 WL 153. STRINGER FOUND OUT OF LIMIT IAW SRM 53-00-03-1A-1 PARAGRAPH 4A(2)(A)1;[02] VERIFIED APPLICABILITY FOR REPAIR ON STR 27 R/H B/S 540 IAW SRM 53-00-03-2R-1 PAR 4 ; FIG 205.;[03] PERFORMED CUT-OUT THE DAMAGE STRINGER 27 R/H LOCATED BTW B/S 500D-520 AND REMOVED FASTENER ON STRINGER SECTION BTW B/S 500D+10 TO B/S 540 IAW SRM 53-00-03-2R-1 REPAIR 1;[04] PARTIAL UPDATE STEP#1;[05] UPDATE CORRECTIVE ACTION #3:REMOVED FASTENERS BTW B/S 500D TO B/S 540 AND CUT AND REMOVED STRINGER SECTION AT B/S 500D+10' TO B/S 540 27R/H IAW SRM 53-00-03-2R-1 REPAIR 1;[06] VERIFIED CORRECTIVE ACTION 1; 2 AND 5.;[07] COMPLETED STEP 2.;[08] RECEIVED NEW STRINGER SECTION P/N: HFAB53-STR-011 ; LOT: 1493963 ; P.O/N: 871116/1 AND NEW HAT SECTION P/N:HFAB53-HS-011; LOT:1493936-1; P.O/N:871111/1.<BR><BR>LOCATED AND DRILLED NEW STRINGER SECTION AND HAT SECTION BTW BS 500D+3' TO BS 536 STR 27R/H AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 53-00-03-2R-1 REPAIR PAR 4 STEPS D-I FIG 205 ; REQUEST OK TO PRIMER ON REPAIR PARTS.;[14] INSTALL NEW REPAIR PARTS AT FCB BTW BS 500D+3' TO BS 536 STR 27R/H IAW SRM 53-00-03-2R-1 PAR 4 ; FIG 205;[15] INSTALLED NEW REPAIR PARTS AT FCB BTW BS 500D+3' TO BS 536 STR 27R/H IAW SRM 53-00-03-2R-1 PAR 4 ; FIG 205.;

Part: STRINGER — CRACKED (FWD CARGO) · airframe 59,194 hrs · 39,098 cycles

CRACK ON FWD CARGO BAY BS 540 R/H STRINGER 26. / [01] EVALUATED CRACK AT STRINGER 26R/H B/S 540 WL 153. STRINGER FOUND OUT OF LIMIT IAW SRM 53-00-03-1A-1 PARAGRAPH 4A(2)(A)1;[02] VERIFIED REPAIR APPLICABILITY FOR STR 26 R/H B/S 540 IAW SRM 53-00-03-2R-1 PAR 4 ; FIG 205.;[03] PERFORMED CUT-OUT THE DAMAGE STRINGER 26 R/H LOCATED BTW B/S 500D-520 AND REMOVED FASTENER ON STRINGER SECTION BTW B/S 500D+10 TO B/S 540 IAW SRM 53-00-03-2R-1 REPAIR 1;[04] PARTIAL UPDATE STEP#1 AND #2;[05] UPDATE CORRECTIVE ACTION #3:REMOVED FASTENERS BTW B/S 500D TO B/S 540 AND CUT AND REMOVED STRINGER SECTION AT B/S 500D+10' TO B/S 540 26R/H IAW SRM 53-00-03-2R-1 REPAIR 1;[06] VERIFIED CORRECTIVE ACTIONS 1; 2; AND 5.;[07] COMPLETED STEP 3.;[08] RECEIVED NEW STRINGER SECTION P/N: HFAB53-STR-011 ; LOT: 1493965-1 ; P.O/N: 871101/1 AND NEW HAT SECTION P/N:HFAB53-HS-011; LOT:1493919-1; P.O/N:871098/1.<BR><BR>LOCATED AND DRILLED NEW STRINGER SECTION AND HAT SECTION BTW BS 500D+4' TO BS 536 STR 26R/H AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 53-00-03-2R-1 REPAIR PAR 4 STEPS D-I FIG 205 ; REQUEST OK TO PRIMER ON REPAIR PARTS.;[15] INSTALLED REPAIR PARTS AT FCB BTW BS 500D+4' TO BS 536 STR 26R/H IAW SRM 53-00-03-2R-1 REPAIR PAR 4. FIG 205

Part: STRINGER — CRACKED (FUSELAGE) · airframe 59,194 hrs · 39,098 cycles

CRACK ON FWD CARGO BAY BS 540 L/H STRINGER 23. / [01] EVALUATED CRACK AT STRINGER 23 L/H B/S 540 STRINGER FOUND OUT OF LIMIT IAW SRM 53-00-03-1A-1 PARAGRAPH 4A(2)(A)1;[02] REMOVED FASTENERS BTW B/S 500D TO B/S 540 AND REMOVED DAMAGE BY TRIMMING OUT STRINGER SECTION BTW B/S 500D-520 STR 23L/H IAW SRM 51-10-02;[03] PARTIAL UPDATE STEP #1;[04] PARTIAL ; UPDATE STEP #2;[05] CERTIFIED PARTIAL STEP 2.;[06] UPDATE CORRECTIVE ACTION #2:REMOVED FASTENERS BTW B/S 500D TO B/S 540 AND CUT AND REMOVED STRINGER SECTION AT B/S 500D+10' TO B/S 540 23L/H IAW SRM 51-10-02;[07] UPDATED PARTIAL WORK FOR STEP 2 AND VERIFIED CORRECTIVE ACTIONS 1; 4; AND 6.;[08] COMPLETED STEP 3.;[09] STEP 3 COMPLETE;[10] FABRICATED OF THE STRINGER SECTION USING BAC5602 T62 7075 T 0.036' ITEM:HFAB53-STR-011 LOT: 1493964-1 AND HAT SECTION USING BAC5602 T6 7075T 0.040 ITEM:HFAB53-HS-011 LOT: 1493918-1 IAW SRM 53-00-03-2R-1 REPAIR 1 4.D-I;[11] FABRICATED OF THE STRINGER SECTION USING BAC5602 T62 7075 T 0.036' ITEM:HFAB53-STR-011 LOT: 1493964-1 AND HAT SECTION USING BAC5602 T6 7075T 0.040 ITEM:HFAB53-HS-011 LOT: 1493918-1 IAW SRM 53-00-03-2R-1 REPAIR 1 4.D-I;[21] INSTALLED REPAIR PATS AT STR 23L BS500D TO BS540 IAW IAW SRM 53-00-03-2R-1; EANO:22-153-01693 REV:A; BOEING DWG 143A0060 REV:- AND BOEING DWG 143A3210 REV:-;

Part: SUPPORT — CRACKED (AFT CARGO) · airframe 59,194 hrs · 39,098 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727B+2; BS 727C+6; BS 727C+10; BS 727C+14; BS 727D+7; BS 727D+13; BS 727D+16. / [01] VERIFY APPLICABILITY PER REF SRM 53-00-53-1A-2;[02] PROVIDED PARTIAL UPDATE FOR STEPS 1 - 7.;[03] PARTIAL UPDATE TO STEP TO STEP 8.;[04] REPLACEMENT OF AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT SECTION AT STA 727 - 847; LBL 21. FAULT RESOLVED ON FAULT TTG8Q00CUD69.;[05] VERIFIED CORRECTIVE ACTIONS STEP 4.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 59,194 hrs · 39,098 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727E+18; BS 747+8; BS 747+14; BS 747+18; BS 767+4; BS 767+8; BS 787+6; BS 787+10; BS 807+14. / [01] VERIFY APPLICABILITY PER REF SRM 53-00-53-1A-2;[02] PROVIDED PARTIAL UPDATES FOR STEPS 1 - 9.;[03] PARTIAL UPDATE TO STEP 10.;[04] LOCATED AND DRILLED NEW ACB FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727 TO 847 IAW SRM 51-40-05-0G-0; AND DWG 146A7502; FABRICATED SPLICE REPAIR BETWEEN BS 727E AND 747 IAW SRM 53-00-53-2R-5 REPAIR 5; APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01-0G-0. REQ. OK TO PRIMER.;[05] UPDATED STEP 10;[06] UPDATED PARTIAL WORK FOR STEP 10 AND CORRECTIVE ATION 3-5.;[07] OK TO INSTALL SPLICE REPAIR;[08] REQUEST OK TO INSTALL SPLICE REPAIR;[09] OK TO INSTALL SPLICE GRANTED.;[10] INSTALLED SPLICE REPAIR BETWEEN BS 727E + 10' IAW SRM 51-40-02 AND 53-00-53-2R-5;[11] VERIFIED CORRECTIVE ACTION #10;[12] APPLIED PRIMER TO FLOOR TO SIDEWALL SUPPORT AND SPLICE REPAIR IAW SRM 53-00-53-2R-5 REPAIR 5; SRM 51-20-01-0G-0;[13] VERIFIED CORRECTIVE ACTION ITEM 12; ALL STEPS COMPLETE JOB COMPLETE.;[14] MEASUREMENT FIELDS VERIFIED;[15] CERTIFIED

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 59,194 hrs · 39,098 cycles

CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 500A+10; BS 500A+14; BS 500B+6; BS 500B+10; BS 500B+18; BS 500C+10. / [01] SRM 53-00-53-1A-2 IS FOUND TO BE APPLICABLE FOR THIS REPAIR;[02] REMOVED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT RBL 24 BS 500A+10 L=1.6'XW=.7'XD=.002'; BS500A+14 L=1.7'XD=.9'XD=.001'; BS500B+6 L=1'XW=.7'XD=.003'; BS500B+10 L=1'XW=.9'XD=.002'; BS500B+18 L=.9'XW=.7'XD=.001'; BS500C L=1.1XW=.6'XD=.004'. FOUND TO BE IN LIMITS WITH REMAINING THICKNESS OF .036' OF ORIGINAL THICKNESS .040'. IAW SRM 53-30-53-0I-2 AND 53-00-53-1A-1.<BR><BR>DIAL DEPTH GAGE ID:ATS2473 S/N:UNKNOWN DUE: 07/2022;[03] VERIFIED;[04] REMOVED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT RBL 24 BS 500A+10 L=1.6'XW=.7'XD=.002'; BS500A+14 L=1.7'XD=.9'XD=.001'; BS500B+6 L=1'XW=.7'XD=.003'; BS500B+10 L=1'XW=.9'XD=.002'; BS500B+18 L=.9'XW=.7'XD=.001'; BS500C L=1.1XW=.6'XD=.006'. FOUND TO BE OUT OF LIMITS WITH REMAINING THICKNESS OF .034' OF ORIGINAL THICKNESS .040'. IAW SRM 53-30-53-0I-2 AND 53-00-53-1A-1.<BR><BR>DIAL DEPTH GAGE ID:ATS2473 S/N:UNKNOWN DUE: 07/2022;[07] FABRICATED REPLACMENT FCB R/H FLOOR TO SIDEWALL SUPPORT BS 500A-500D PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 143A7501 OUT OF BAC1496-444#7075T62 LOT:1485395-1;[08] FABRICATED REPLACMENT FCB R/H FLOOR TO SIDEWALL SUPPORT BS 500A-500D PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 143A7501 OUT OF BAC1496-444#7075T62 LOT:1485395-1

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 59,194 hrs · 39,098 cycles

CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 24 BS 500+10; BS 500A+6; BS 500B+6; BS 500B+18. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF FCB FLOOR TO SIDEWALL SUPPORT;LBL 24 WL 156 ; IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[02] FABRICATED REPLACEMENT FLOOR TO SIDEWALL SUPPORT USING BAC1496-444#7075T62 LOT:1485395-1 IAW SRM 51-40-05-0G-0; SRM 51-40-08; SRM 53-00-53-2R-5 SECTION 4.D-H AND DWG 143A7501 ID:0001 REV: B. FABRICATED FLOOR TO SIDEWALL SUPPORT SPLICE REPAIR BS 480+10' USING BAC1496-444#7075T62 LOT:1485395-1 IAW SRM 53-00-53-2R-5 SECTION 4.D-H; SRM 51-40-05. APPLIED CHEMICAL CONVERSION COATING TO SPLICE AND SIDEWALL SUPPORT IAW SOPM 20-41-02. OK APPLIED PRIMER TO SPLICE AND SIDEWALL SUPPORT.;[03] CORRECTIVE ACTION #2:FABRICATED ; LOCATED AND DRILLED REPLACEMENT FLOOR TO SIDEWALL SUPPORT USING BAC1496-444#7075T62 LOT:1485395-1 IAW SRM 51-40-05-0G-0; SRM 51-40-08; SRM 53-00-53-2R-6 AND DWG 143A7501 ID:0001 REV: B. FABRICATED FLOOR TO SIDEWALL SUPPORT SPLICE REPAIR AT B/S 480+10' USING BAC1496-444#7075T62 LOT:1485395-1 IAW SRM 53-00-53-2R-6 AND SRM 51-40-05. APPLIED CHEMICAL CONVERSION COATING TO SPLICE AND SIDEWALL SUPPORT IAW SOPM 20-41-02. OK APPLY PRIMER ON SPLICE AND SIDEWALL SUPPORT.[07] INSTALLED REPAIR SPLICE ON NEW FLOOR TO SIDEWALL SUPPORT LOCATED BTW BS 480 TO 500 LBL 24 WL 156 IAW SRM 51-40-02 AND SRM 53-00-53-2R-6 REPAIR 6;

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,194 hrs · 39,098 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT RBL 45 BS 787+10. / [01] REMOVED CORROSION FROM SEAT TRACK WITH A MAX. MATERIAL LOSS OF .042 IN THE BOTTOM OF WELL. USING TOOL ID # E9655 NO S/N CAL. DATE 03/2022 DUE 03/2023. FOUND TO BE OUT OF LIMITS IAW SRM CH 53-00-52-1A-1.;[02] VERIFIED CORRECTIVE ACTION #1;[03] REMOVED FLOOR PANELS 242GF; 242HF; 242JF; 242KF; 242LF; 242MF; 242NF; 242PF AND 242QF FOR ACCESS IAW AMM CH 53-21-00-000-801;[04] LOCATED AND DRILLED NEW SEAT TRACK IAW SRM CH 51-40-05 AND DRAWING #146A5350. ID #37 AND# 38. OK TO INSTALL;[05] REMOVED DAMAGED SEAT TRACK AT BS727B-887 RBL 45 IAW SRM CH 51-40-02.;[06] VERIFIED CORRECTIVE ACTIONS STEP 4;5 AND OK TO INSTALL GIVEN.;[07] INSTALLED SEAT TRACK AT BS 727B-887 RBL45 WL208 IAW SRM 51-40-02-0G-0; DWG 146A5300 SHT'S 36;37;38;[08] UPDATED PART REQUIREMENT;[09] VERIFIED CORRECTIVE ACTIONS 7-8;[10] EDIT TO CORRECTIVE ACTION 9; SHOULD HAVE BEEN DOCUMENTED AS:<BR><BR>VERIFIED CORRECTIVE ACTIONS 7-8; REINSTALLATION OF ACCESSED FLOOR PANELS WILL BE ACCOMPLISHED ON FAULT # TTG8Q00CXV8S;[11] VERIFIED MEASUREMENT TABLE

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,194 hrs · 39,098 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT RBL 45 BS 560+2; BS 580+1; BS 580+4; BS 640+8. / [01] REMOVED CORROSION FROM SEAT TRACK WITH A MAX MATERIAL LOSS OF .021 ON THE TOP OF THE TRACK. FOUND TO BE OUT OF LIMITS USING TOOL ID # ATS2677 NO S/N CAL DATE 11/21 DUE 11/22. IAW SRM CH 53-00-52-1A-1.;[02] VERIFIED CORRECTIVE ACTION 1;[03] REMOVED SEAT TRACK PASSENGER CABIN AT RBL 45 FROM BS 540 TO BS 727B IAW SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW SEAT TRACK PASSENGER CABIN AT RBL45 FROM BS 540 TO BS 727B IAW SRM 51-40-05-0G-0 AND DWG 143A5300;[05] VERIFIED RECEIPT OF ATSHFAB-100-313 SEAT TRACK AND CONFORMED FABRICATION TO BOEING DWG# 144A5350- REFERENCE JOB NUMBER #539867. VERIFIED CORRECTIVE ACTION 3 AND 4. PART MARK PER QCM 4.35.26 STILL REQUIRED.;[06] PART MARKED SEAT TRACK PER QCM 4.35.26 OK TO INSTALL;[07] STEP 1 COMPLETED; OK TO INSTALL GIVEN.;[08] INSTALLED NEW SEAT TRACK AT BS 540 TO BS 727B RBL 45 WL 208 IAW SRM 51-40-02 AND DWG # 144A5300;[09] REJECTED INSTALLATION OF SEAT TRACK DUE TO FASTENER AT BS 663+6 INSTALLED INCORRECTLY; SEE STEP 2 FOR REJECTION.;[10] REMOVED AND INSTALLED THE FASTENER AT BS 663+6' CORRECTLY IAW SRM 51-40-02-0G-0 AND DWG 144A5300.;[11] COMPLETED STEP 2 AND VERIFIED CORRECTIVE ACTION 10.;[12] VERIFIED MEASUREMENT TABLE

Part: THRESHOLD — CORRODED (FWD CARGO) · airframe 59,194 hrs · 39,098 cycles

CORROSION ON FWD CARGO BAY THRESHOLD AT RBL 28 BS 460+4. / [01] REMOVED CORROSION FROM FWD CARGO BAY THRESHOLD AT RBL 28; BS 460+4. IAW SRM 51-10-02-0G-0.;[02] REMOVED CORROSION DIMENSIONS: L = 3.3'; W = 1.1;[03] VERIFIED APPLICABILITY IAW SRM 53-30-15-1A-1 ALLOWABLE DAMAGE;[04] EVALUATED REWORKED AREA; ORIGINAL THICKNESS 0.045'; MAT. REMOVED: 0.012' REMAINING THICKNESS 0.033'; FOUND DAMAGE OUT OF LIMITS IAW SRM 53-30-15-1A-1 ALLOWABLE DAMAGE 1; FIG. 103; DETAIL D. TOOL DEPTH GAGE ID: ATS2677; S/N: UNKNOW; DUE: 11/2022.;[05] RECEIVED NEW THRESHOLD ITEM: 654A0003-58 LOT: 5099996-16. LOCATED AND DRILLED NEW THRESHOLD IAW SRM 51-40-05;[06] VERIFIED CORRECTIVE ACTION 5;[07] VERIFIED MEASUREMENT TABLE;[08] CERTIFY

Part: STIFFENER — CRACKED (CENTER WING) · airframe 59,194 hrs · 39,098 cycles

CRACKED L/H VAPOR BARRIER HORIZONTAL STIFFENER AT BS663 LBL9 WL156. MARKED / [01] REMOVED L/H VAPOR BARRIER HORIZONTAL STIFFENER AT BS663 LBL9 WL156. IAW SRM 51-40-02-0G-0;[02] LOCATED ND DRILLED NEW STIFFENER P/N 11A1301U5 PO#830094 IAW SRM 51-40-05-0G-0; REQ. OK TO INSTALL;[03] STIFFENER CRACK IS OUT OF LIMITS IAW SRM 57-10-10-1A-1;[04] VERIFIED CORRECTIVE ACTIONS 1-3; OK TO INSTALL;[05] INSTALLED NEW HORIZONTAL STIFFNER AT L/H VAPOR VARRIER BS 663 LBL 6 TO 31 IAW DWG 111A1000 REV.- AND SRM 51-40-02-0G-0. OK TO APPLY SEAL;[06] VERIFIED CORRECTIVE ACTION 5; OK TO SEAL;[07] APPLIED SEAL AT REPAIR AREA AND AT FASTENER REPAIR IAW AMM 51-31-00-390-812 AND AMM 51-31-00-390-805;[08] UPDATED PART INSTALLATION;[09] VERIFIED CORRECTIVE ACTION 7-8

Part: WEB — ELONGATED (L/H FUSELAGE) · airframe 58,348 hrs · 38,551 cycles

3 EA. AFT FASTENER HOLES ELONGATED ON L/H SUPPORT STRUCTURE WEB / [01] FABRICATED AND TRIMMED NEW STRUCTURE WEB OUT OF 2024-T3 0.040'<BR>DILLED AND INSTALLED PER SRM 51-40-05 AND 51-40-02

Part: BRACKET — CRACKED (L/H FUSELAGE) · airframe 58,348 hrs · 38,551 cycles

LH 193D FWD LOWER SUPPORT BRACKET FOUND CRACKED / [01] REMOVED BRACKET PER SRM 51-40-02.;[02] NEW BRACKET WAS FABRICATED PER EA 22-153-00512<BR>INSTALLED NEW BRACKET PER SRM 51-40-02-

Part: NONE — CRACKED (L/H FUSELAGE) · airframe 58,348 hrs · 38,551 cycles

LH 193D AFT SUPPORT BRACKET FOUND CRACKED / [01] REMOVED BRACKET PER SRM 51-40-02.;[02] FABRICATED NEW CLIP OUT OF BAC1505-100246 EXTRUSION T ANGLE; PARTIALLY INSTALLED NEW BRACKET PER SRM 51-40-02;[03] COMPLETED INSTALLATION OF T ANGLE BRACKET REF B737 SRM 51-40-02 AND BOEING DWG 149A7601 FOR FASTENER CALLOUT .

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,619 hrs · 38,116 cycles

LEFT EMERGENCY EXIT HATCH LIGHT INOP ; / [01] RELAMPED LEFT EMERGENCY EXIT HATCH LIGHT REF AMM 33-21-00.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 56,769 hrs · 37,589 cycles

FORWARD GALLEY MOUNTED EMERGENCY EXIT LIGHT COVER MISSING ; / [01] INSTALLED NEW EMERGENCY EXIT LIGHT COVER PER AMM 33-51-01

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 55,248 hrs · 36,747 cycles

CREW REPORTED FWD FA EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FWD FA FLASHLIGHT BATTERY PER AMM 25-64-00.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 54,381 hrs · 36,216 cycles

CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT / FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT REPAIRED BY WELDS IAW BOEING 737-700 SRM TASK 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4B STEP (4) AND BAC5975

Part: WEB — CRACKED (VERTICAL STAB) · airframe 54,381 hrs · 36,216 cycles

CRACK DORSAL FIN INTERNAL FWD WEB AT VERTICAL STABILIZER / REPLACED WEB LOC DORSAL FIN INTERNAL AREA AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 DWG # 174A1008 REV C

Part: SUPPORT — CORRODED (BS 727-767) · airframe 54,381 hrs · 36,216 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS767 AT LEVEL STR25R AND RBL 21.00 AFT CARGO COMPARTMENT / REPLACED SUPPORT ZEE LOCATED BETWEEN BS727 TO BS767 AT LEVEL STR 25R AND RBL 21.00 AFT CARGO COMPARTMENT IAW DWG 146A7502 SHEET 1 REV 'A' AND SRM B737-700 51-40-02 SRM 51-10-02 ITEM 9

Part: SUPPORT — CRACKED (BS 500-500D) · airframe 54,381 hrs · 36,216 cycles

CRACK SUPPORT ZEE LOCATED BS500 AT LEVEL STR26L AT FWD CARGO COMPARTMENT (1 EA) / REPLACED SUPPORT ZEE LOCATED BTW BS500 TO BS500D AT LEVEL STRG 26 AT FORWARD CARGO COMPARTMENT IAW B737- 700 SRM 53-00-53-2R-5 REPAIR 5 B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #143A7501 REV B

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 54,381 hrs · 36,216 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS727 TO BS827 AT LEVEL STR25L AND LBL 21.00 AFT CARGO COMPARTMENT REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 AT LEVEL STR25L AND LBL 21.00 AFT CARGO COMPARTMENT; WITH A REPAIR SPLICE LOCATED BETWEEN BS 727E AND BS 727F (BS727E+13') IAW B737700 SRM 5300532R5 REPAIR 5 FIGURE 202; B737700 SRM 514002; B737700 SRM 511002 ITEM 9 AND DRAWING 146A7502 REVISION A.

Part: WASHER — WORN (R1 DOOR GIRT BAR) · airframe 54,381 hrs · 36,216 cycles

WEAR ON GIRT BAR SCREW AND WASHER 8(EA) AT FWD GALLEY AREA / REPLACED GIRT BAR SCREW AND WASHER (8EA) AT FWD GALLEY AREA IAW SRM 51-10-02-0G-0 ITEM 9

Part: FITTING — WORN (R2 DOOR GIRT BAR) · airframe 54,381 hrs · 36,216 cycles

WEAR ON GIRT BAR FITTING SCREW AND WASHER 8(EA) AT AFT GALLEY AREA / REPLACED GIRT BAR FITTING SCREW AND WHASHER 8(EA) AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 54,381 hrs · 36,216 cycles

CORROSION CHANNEL SIDEPLATE LOCATED BS500 TO BS500A AT LEVEL STR26R AND WL156.5 FWD CARGO COMPARTMENT / REPLACED CHANNEL SIDEPLATE LOC BS500 TO BS500A AT LEVEL STR26R AND WL156.5 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG 143A0080 REV

Part: SKIN — DENTED (LT WING LE) · airframe 54,381 hrs · 36,216 cycles

DENT I/B FIXED LEADING EDGE UPPER SKIN LOCATED BTW KRAS 137.75 AND KRAS 150.75 AT LT WING (MEASURES OF DENT ARE: L=4.428 INCH W=2.847 INCH Y =0.162 INCH W/Y=17.57) / REPAIRED IB FIXED LEADING EDGE UPPER SKIN LOCATED BTW KRAS 137.75 AND KRAS 150.75 AT LT WING IAW B737-700 SRM 57-41-01-2R-4 REPAIR #4 THIS REPAIR IS CATEGORY 'A' PERMANENT AND NO FURTHER ACTION IS REQUIRED

Part: PLATE — WORN (R1 DOOR GIRT BAR) · airframe 54,381 hrs · 36,216 cycles

WEAR ON GIRT BAR ADAPTER PLATE4(EA) AT FWD GALLEY AREA / REPLACED GIRT BAR ADAPTER PLATE (4EA) AT FWD GALLEY AREA IAW SRM 51-10-02-0G-0 ITEM 9

Part: SCREW — WORN (R1 DOOR GIRT BAR) · airframe 54,381 hrs · 36,216 cycles

WEAR ON GIRT BAR SCREW AND WASHER 8(EA) AT FWD GALLEY AREA / REPLACED GIRT BAR SCREW AND WASHER (8EA) AT FWD GALLEY AREA IAW SRM 51-10-02-0G-0 ITEM 9

Part: STRINGER — CORRODED (BS 500A-500B) · airframe 54,381 hrs · 36,216 cycles

CORROSION STRINGER 28R LOCATED BS500A TO BS500B AND WL148.5 FWD CARGO COMPARTMENT / REPAIRED STR 28R FROM BS500A TO BS500B IAW EA # 53-05-52-20 REVISION 0 AND SWA EA N.20-153-01514 REV IR

Part: PLATE — WORN (R2 DOOR GIRT BAR) · airframe 54,381 hrs · 36,216 cycles

WEAR ON GIRT BAR FITTING PLATES AT AFT GALLEY AREA (4 EA) / REPLACED GIRT BAR FITTING PLATES AT AFT GALLEY AREA (4EA) IAW B737-700 AMM 2566-02-900-801

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 54,381 hrs · 36,216 cycles

CRACK TIE CLIP AT BS277 AND STR10R AT PASSENGER CABIN (1 EA). REPLACED TIE CLIP AT BS277 AND STR 10R AT PASSENGER CABIN (1EA) IAW B737700. SRM 511002 ITEM 9; DWG # 141A1110 SHEET 17 REV AND DWG # 141A8380 SHEET 14 REV

Part: SUPPORT ANGLE — CRACKED (BS 692) · airframe 54,381 hrs · 36,216 cycles

CRACK SUPPORT ANGLE LOCATED BS692 AT BL0 CENTER SECTION (2 EA) / REPLACED SUPPORT ANGLE 2E/A LOCATED BS692 AT BL0 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DWG 273A9110 SHEET 5 REV A

Part: LIGHT — CRACKED (CABIN) · airframe 54,381 hrs · 36,216 cycles

CRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING 6EA AT PASSENGER CABIN (6 EA) / REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING (6EA) AT PASSENGER CABIN IAW MT 733-50-01

Part: SCUFF PLATE — BROKEN (AFT CARGO) · airframe 54,381 hrs · 36,216 cycles

BROKEN CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT / REPAIRED BY WELD CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700 SRM TASK 53-60-15-2R-1; REPAIR 1 AND BAC 5975.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 54,381 hrs · 36,216 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT / FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT REPAIRED BY WELDS IN ACCORDANCE WITH BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B STEP (4)

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,381 hrs · 36,216 cycles

CRACK LEADING EDGE RIB STA 95.96 ACCESS PANEL 341 B RT HORIZONTAL STAB / REPLACED RIB LOC ON ACCESS PANEL 341B RT HORIZONTAL STAB STA 95.96 IAW SRM 51-40-02 B737-700 AND DWG 186A1001 REV A

Part: RIB — CRACKED (HORIZONTAL) · airframe 54,381 hrs · 36,216 cycles

CRACK LEADING EDGE RIB STA 105.26 ACCESS PANEL 341 B RT HORIZONTAL STAB / REPLACED RIB LOC ON ACCESS PANEL 341B RT HORIZONTAL STAB STA 105.26 IAW SRM 51-40-02 B737-700 AND DWG 186A1001 REV A

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 54,381 hrs · 36,216 cycles

CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT / REPAIRED BY WELD AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 54,381 hrs · 36,216 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT / REPAIRED BY WELDS AFT CORNER SCUFF PLATE AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B STEP (4)

Part: PANEL — ELONGATED · airframe 53,267 hrs · 35,503 cycles

PANEL 193B HAS NUMEROUS ELONGATED HOLES. / REPLACED PANEL 193B PER EO# 14108 AND SRM 51-40-02

Part: SLIDE — WORN (L2 DOOR) · airframe 53,257 hrs · 35,495 cycles

L2 DOOR EMERGENCY SLIDE GIRT WORN. / R&R SLIDE IAW MT.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 52,709 hrs · 35,147 cycles

EMERGENCY EXIT SIGN OVERWING EXIT DETACHED. REINSTALLED LENS COVER PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,408 hrs · 34,283 cycles

RT OVERWING EMERGENCY LIGHT INOP. R&R BULB PER AMM.

Part: LANYARD — BROKEN (EMERGENCY EXIT) · airframe 51,124 hrs · 34,101 cycles

LT EMERGENCY EXIT LOWER RED PULL HANDLE TRIM COVER LANYARD BROKEN. R&R LANYARD PER AMM.

Part: DOUBLER — CRACKED (LT MLG WW) · airframe 50,557 hrs · 33,737 cycles

LT WHEEL WELL THE CENTER WING REAR SPAR SEAL ASSEMBLY CRACKED AT LBL 15.54. R&R DOUBLER ASSEMBLY PER EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 50,476 hrs · 33,688 cycles

FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER AMM.

Part: BUTTON — BROKEN (CABIN) · airframe 49,818 hrs · 33,244 cycles

AFT ATTENDANT PANEL EMERGENCY LIGHT BUTTON BROKEN. RESEATED BUTTON PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,818 hrs · 33,244 cycles

EMERGENCY EXIT LIGHT ABOVE FLIGHT DECK DOOR BULBS INOP. R&R BULBS PER AMM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 49,818 hrs · 33,244 cycles

AFT ENTRY LOWERED CEILING EXIT SIGN, AFT LENS CRACKED. R&R SIGN ASSEMBLY IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 49,818 hrs · 33,244 cycles

EMERGENCY SIGN ASSEMBLY LENS STOPPER MISSING. R&R SIGN ASSEMBLY IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,818 hrs · 33,244 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520, STR 24R. R&R INTERCOSTAL PER SRM AND DWG.

Part: PANEL — CORRODED (SLAT) · airframe 49,818 hrs · 33,244 cycles

SUPPLEMENTAL INFORMATION: #7 SLAT COVE PANEL 624CB IS CORRODED / SLAT WAS REPLACED WITH SERVICEABLE UNITS WITH SERVICEABLE #7 SLAT COVE PANEL 624CB. REMOVAL AND REPLACEMENT OF #7 SLAT ACCOMPLISHED ON DEFECT NUMBER T857413

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 49,818 hrs · 33,244 cycles

FORWARD CARGO BAY BAFFLE CRACKED BETWEEN BS 400 TO BS 420, LBL 21. R&R BAFFLE PER SRM AND DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 49,818 hrs · 33,244 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB PER SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 49,818 hrs · 33,244 cycles

VERTICAL PRESSURE WEB TO BE CRACKED AT BS 663, LBL 34. REPAIRED WEB PER SRM.

Part: STIFFENER — CRACKED (AED) · airframe 49,818 hrs · 33,244 cycles

AED LOWER HINGE ACCESS COVER SUPPORT STIFFENER CRACKED. / REMOVED AND REPLACED AED LOWER HINGE ACCESS COVER SUPPORT STIFFENER PER SRM 51-10-02-0G-0

Part: BEAM — CRACKED (R1 DOOR) · airframe 49,818 hrs · 33,244 cycles

R1 DOOR NR 4 LOWER BEAM CRACKED IN THE RADIUS ON THE INBOARD SIDE. R&R LOWER BEAM IAW SRM.

Part: FLOOR PANEL — BROKEN (AFT CARGO) · airframe 49,818 hrs · 33,244 cycles

AFT CABIN FLOOR PANEL 241ADF AFT I/B CORNER IS BROKEN / REPAIRED BROKEN AFT I/B CORNER ON AFT CABIN FLOOR PANEL 241ADF IAW SRM 53-00-50-2R-9.

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 49,818 hrs · 33,244 cycles

WING TO BODY FAIRING #194AL HAS DELAMINATION; MARKED. / WING TO BODY FAIRING #194AL. DELAMINATION WAS REAPIRED IAW SRM 51-70-05-2R-1 56144U. 10/25/2018.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,818 hrs · 33,244 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,818 hrs · 33,244 cycles

AFT CARGO INTERCOSTAL COMMON TO FLOOR TO SIDEWALL SUPPORT CRACKED AT BS 947.5, RBL 20. R&R INTERCOSTAL IAW DWG & SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 49,818 hrs · 33,244 cycles

L1 DOOR MOPSILL CORRODED BETWEEN BS 303 TO BS 328, LBL 65. R&R MOPSILL PER SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 49,818 hrs · 33,244 cycles

AFT SHEAR WEB TENSION STRAP CORRODED AT BS 1026, RBL 3. R&R STRAP PER SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 49,818 hrs · 33,244 cycles

AFT CARGO BAY FWD SCUFF PLATE IS CRACKED / REPAIRED A.C.B. FWD SCUFF PLATE PER EA 1-A53-2076 REV 11

Part: SUPPORT BRACKET — DAMAGED (FUSELAGE) · airframe 49,818 hrs · 33,244 cycles

AFT CARGO BAY OUTBOARD ANGLED SUPPORT BRACKET DAMAGED AT BS 727D, STR 27. R&R BRACKET IAW SRM & DWG.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 49,818 hrs · 33,244 cycles

AFT CARGO BAY AFT SCUFF PLATE IS CRACKED / REPAIRED A.C.B. AFT SCUFF PLATE PER EA 1-A53-2076 REV 11

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 49,818 hrs · 33,244 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS 887, RBL 20. R&R SUPPORT PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 49,818 hrs · 33,244 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: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,818 hrs · 33,244 cycles

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

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 49,818 hrs · 33,244 cycles

***CORROSION*** AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 767-790; RBL 20 / REMOVED AND REPLACED SHIELD FLOOR TO SIDEWALL SUPPORT AT ACB BS 767 TO BS 790 RBL 20 IAW SRM 51-40-02-0G-0 AND DWG 146A0081 57049U 10NOV18

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,818 hrs · 33,244 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 49,818 hrs · 33,244 cycles

FORWARD CARGO BAY LT FLOOR-TO-SIDEWALL SUPPORT CORRODED BETWEEN BS 500+10 TO BS 500C+14, LBL 25. R&R SUPPORT PER SRM AND DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 49,818 hrs · 33,244 cycles

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

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 49,818 hrs · 33,244 cycles

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

Part: RETAINER — CRACKED (RT WING) · airframe 49,818 hrs · 33,244 cycles

RIGHT WING TRAILING EDGE FIXED PANEL AFT OF THE PYLON FOUND TO HAVE CRACKED SEAL RETAINER ANGLE. MARKED / REMOVED & REPLACED SEAL RETAINER ANGLE ON RIGHT WING TRAILING EDGE FIXED PANEL AFT OF THE PYLON IAW SRM 51-40-02-0G-0 PARA 4 & FIG 8; & IPC 57-50-00-25.

Part: PANEL SUPPORT — CORRODED (RT WING) · airframe 49,818 hrs · 33,244 cycles

***CORROSION*** FOUND IN MULTIPLE SPOTS ON RIGHT WING LOWER TRAILING EDGE PANEL SUPPORT BETWEEN #7 AND #8 FLAP TRACKS. MARKED / REMOVED AND REPLACED RIGHT WING LOWER T/E PANEL SUPPORT BETWEEN #7 AND #8 FLAP TRACKS IAW BOEING DWG 115A3711 AND SRM 51-40-02-0G-0 STEP 7. VERIFIED FASTENER CALLOUT WITH DWG 115A3711

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 49,818 hrs · 33,244 cycles

AFT CARGO BAY FLOOR PNL 140AF HAS CORROSION AROUND EDGES / FABRICATED NEW ACB FLOOR PANEL 140 AF FROM .090 CONOLITE; LOT #1355571-1 PER AMM 25-52-01-201-801 AND DWG 453A2610. INITIAL PANEL 140AF MADE FROM INCORRECT MATERIAL; PER DWG 453A2610 CORRECT MATERIAL IS .090 CONOLITE

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 49,818 hrs · 33,244 cycles

AFT CARGO BAY FLOOR PNL 140DF HAS CORROSION AROUND EDGES / FABRICATED NEW ACB FLOOR PANEL 140 DF FROM .090 CONOLITE; LOT #1355571-1 PER AMM 25-52-01-201-801 AND DWG 453A2610. INITIAL PANEL 140DF WAS MADE FROM INCORRECT MATERIAL; PER DWG 453A2610 THE CORRECT MATERIAL IS .090 CONOLITE

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 49,818 hrs · 33,244 cycles

FWD CARGO BAY FLOOR PNL120BF HAS CORROSION AROUND EDGES / FABRICATED NEW FCB FLOOR PANEL 120BF FROM .071 2024T3; LOT #1358971-1 PER ER 18-04888 REV IR AND SWA EA 1-753-33546 REV IR

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 49,818 hrs · 33,244 cycles

AFT CARGO BAY FLOOR PNL 140CF HAS CORROSION AROUND EDGES / FABRICATED NEW ACB FLOOR PANEL 140CF FROM .071 2024T3; LOT #1358971-1 PER ER 18-04888 REV IR AND SWA EA 1-753-33546 REV IR

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 49,818 hrs · 33,244 cycles

FWD CARGO BAY FLOOR PNL120AF HAS CORROSION AROUND EDGES / FABRICATED NEW FCB FLOOR PANEL 120AF FROM .090 CONOLITE; LOT #1355571-1 PER AMM 25-52-01-201-801 AND DWG 453A1610. INITIAL PANEL 120AF MADE FROM WRONG MATERIAL; DWG 453A1610 SPECIFIES .090 CONOLITE

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 49,818 hrs · 33,244 cycles

FWD CARGO BAY FLOOR PNL120CF HAS CORROSION AROUND EDGES / FABRICATED NEW FCB FLOOR PANEL 120CF FROM .090 CONOLITE; LOT #1355571-1 PER AMM 25-52-01-201-801 AND DWG 453A1610 NO CORROSION LIMITS GIVEN IN SRM FOR THIS PART; UPON FURTHER INVESTIGATION DWG 453A1610 SHOWS PANEL 120CF IS MADE FROM .090 CONOLITE

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 49,818 hrs · 33,244 cycles

AFT CARGO BAY FLOOR PNL 140BF HAS CORROSION AROUND EDGES / FABRICATED NEW ACB FLOOR PANEL 140BF FROM .090 CONOLITE; LOT #1355571-1 PER AMM 25-52-01-201-801 AND DWG 453A2610. INITIAL PANEL 140BF MADE FROM INCORRECT MATERIAL; PER DWG 453A2610 THE CORRECT MATERIAL IS .090 CONOLITE.

Part: SKIN — CRACKED (LE SLAT) · airframe 49,818 hrs · 33,244 cycles

RT WING LEADING EDGE NR 7 SLAT SKIN CRACKED AT ACTUATOR AROUND AFT OUTBOARD FASTENER HOLES. R&R NR 7 SLAT ASSEMBLY IAW AMM.

Part: SKIN — DAMAGED (FWD FUSELAGE) · airframe 49,818 hrs · 33,244 cycles

DEFECT TRANSFERRED FROM LOG PAGE 0298499: REFERENCE TSR 201808016 THE REPAIR AT BSTA 500A-500B S-4R REQUIRES A NEW CAT B REPAIR / REMOVED EXISTING REPAIR FROM BS 500A STR 4R AND REPLACED PER EA 1-753-33420 REV IR AND ATS ER 18-04419 REV IR

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,608 hrs · 33,111 cycles

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

Part: PANEL — CRACKED (LT ELEVATOR) · airframe 49,608 hrs · 33,111 cycles

LEFT ELEVATOR #4 BALANCE BAY FORWARD PANEL CRACKED AT FORWARD HINGE; INBOARD SIDE / R&R PANEL PER MM REF 27-31-41 AND SRM REF 51-40-02

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,608 hrs · 33,111 cycles

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

Part: STRAP — DAMAGED (R2 DOOR) · airframe 49,142 hrs · 32,807 cycles

R2 DOOR ARMED SLIDE STRAP MISSING SNAP. R&R STRAP ASSEMBLY PER MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 48,602 hrs · 32,469 cycles

L1 DOOR EMERGENCY SIGN MISSING RED ARROW. R&R LENS IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 48,602 hrs · 32,469 cycles

R1 DOOR EMERGENCY SIGN MISSING RED ARROW. R&R LENS PER AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,597 hrs · 31,859 cycles

LEFT OVERHEAD EMERGENCY LIGHT INOPERATIVE AT ROW 9. REPLACED THE LAMPS IAW AMM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 47,546 hrs · 31,821 cycles

RT WHEEL WELL VERTICAL WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB PER EA.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 45,525 hrs · 30,530 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 45,525 hrs · 30,530 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 45,525 hrs · 30,530 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R & R THE BATTERY IAW AMM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,307 hrs · 30,395 cycles

L2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY IAW MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,307 hrs · 30,395 cycles

L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 45,290 hrs · 30,382 cycles

L1 DOOR SLIDE OUT OF ADJUST. SECURED THE SLIDE ASSY IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,873 hrs · 30,131 cycles

RIGHT EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: FAN — FAILED (RECIRCULATION) · airframe 44,639 hrs · 29,993 cycles

SMOKE & FUMES REPORTED MID CABIN. DISPATCHED WITH GASPER FAN OFF. R & R THE RECIRCULATION FAN IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,438 hrs · 29,285 cycles

EMERGENCY LIGHT INOP AT BS 896, LBL 28. REPAIRED LIGHT PER ER & EA.

Part: FLASHLIGHT — LOOSE (CABIN) · airframe 43,438 hrs · 29,285 cycles

FORWARD WINDSCREEN FLASHLIGHT BASES LOOSE. SECURED BASE ASSEMBLY PER SOPM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

FORWARD CARGO BAY, FORWARD SCUFF PLATE CRACKED. R&R SCUFF PLATE IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

FORWARD CARGO BAY BULKHEAD SUPPORT BRACKET CRACKED AT BS 500D, STR 19L. R&R BRACKET IAW SRM.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

FORWARD CARGO BAY FLOOR BAFFLE CRACKED BETWEEN BS 500A TO BS 500B, RBL 23. R&R BAFFLE PER SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 43,438 hrs · 29,285 cycles

STRINGER TO FRAME GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

INTERCOSTAL TO FRAME ATTACH CLIP CRACKED AT BS 400, LBL 25. R & R CLIP IAW SRM.

Part: BAFFLE — CRACKED (BS 727A-727B) · airframe 43,438 hrs · 29,285 cycles

AFT CARGO BAY BAFFLE CRACKED BETWEEN BS 727A TO 727B, LBL 21. R & R BAFFLE IAW SRM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

FORWARD CARGO BAY BAFFLE ATTACH CLIP CRACKED AT BS 500C, RBL 23. R & R CLIP IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 500-500A) · airframe 43,438 hrs · 29,285 cycles

FORWARD CARGO BAY FLOOR SUPPORT CRACKED BETWEEN BS 500 TO 500A, LBL 23. R & R THE FLOOR SUPPORTA IAW SRM.

Part: BAFFLE — CRACKED (BS 400-420) · airframe 43,438 hrs · 29,285 cycles

FORWARD CARGO BAY BAFFLE CRACKED BETWEEN BS 400 TO 420, LBL 23. R & R THE BAFFLE IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

NR 2 ADF ANTENNA FOUND FUSELAGE SKIN CORRODED BETWEEN BS 727+12 TO BS 727B, BETWEEN STR 1 TO STR 2R. REPAIRED SKIN IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

LONGITUDINAL FLOORBEAM FLANGE CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW SRM.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 43,438 hrs · 29,285 cycles

FLOORBEAM FLANGE CRACKED AT BS 727B, RBL 45.5. REPAIRED THE FLOORBEAM FLANGE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (BS 947) · airframe 43,438 hrs · 29,285 cycles

AFT CARGO BAY LOWER BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, BETWEEN LBL 10 TO RBL 21. R & R THE ANGLE IAW SRM & DWG.

Part: SUPPORT — CORRODED (BS 847-867) · airframe 43,438 hrs · 29,285 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 847 & 867, RBL 21. R & R THE SUPPORT IAW SRM.

Part: WEB — CORRODED (BS 794-847) · airframe 43,438 hrs · 29,285 cycles

AFT CARGO BAY ON THRESHOLD WEB CORRODED BETWEEN BS 794 TO 847, BETWEEN RBL 20 TO 28. R & R THE WEB IAW SRM.

Part: CARGO TRACK — CRACKED (BS 727E-747) · airframe 43,438 hrs · 29,285 cycles

AFT CARGO BAY CARGO TRACK CRACKED BETWEEN BS 727E TO 747, RBL 13.5. R & R THE CARGO TRACK IAW SRM.

Part: ANGLE — CRACKED (BS 865) · airframe 43,438 hrs · 29,285 cycles

AFT CARGO BAY BOTTOM ATTACH ANGLE FOR BULKHEAD SUPPORT ANGLE CRACKED AT BS 865, LBL 10. R & R ANGLE IAW SRM.

Part: FITTING — CRACKED (BS 948) · airframe 43,438 hrs · 29,285 cycles

FITTING CRACKED AT BS 948, STRINGER 26L. R & R THE FITTING IAW SRM.

Part: FRAME — CRACKED (BS 440) · airframe 43,438 hrs · 29,285 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

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

Part: FRAME — CRACKED (BS 400) · airframe 43,438 hrs · 29,285 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

SKIN CRACKED AT BS 540, STR 22L. REPAIRED SKIN PER ER & EA.

Part: FRAME — CRACKED (BS 440) · airframe 43,438 hrs · 29,285 cycles

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

Part: FRAME — CRACKED (BS 827) · airframe 43,438 hrs · 29,285 cycles

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

Part: FRAME — CRACKED (BS 500C) · airframe 43,438 hrs · 29,285 cycles

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

Part: FRAME — CRACKED (BS 500A) · airframe 43,438 hrs · 29,285 cycles

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

Part: FRAME — CRACKED (BS 480) · airframe 43,438 hrs · 29,285 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

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

Part: FRAME — CRACKED (BS 400) · airframe 43,438 hrs · 29,285 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

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

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

FAIRING SUPPORT STRUCTURE CRACKED AT BS 727, RBL 10.5. R&R STRUCTURE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 907) · airframe 43,438 hrs · 29,285 cycles

FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME PER ER AND EA.

Part: FRAME — CRACKED (BS 480) · airframe 43,438 hrs · 29,285 cycles

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

Part: TEE FITTING — CORRODED (BS 992) · airframe 43,438 hrs · 29,285 cycles

L2 DOOR CUTOUT AFT FRAME TEE FITTING CORRODED AT BS 992.8, STRINGER 13L. R & R TEE FITTING IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 43,438 hrs · 29,285 cycles

STRINGER CLIP 8R CRACKED AT BS 360. R & R THE STRINGER CLIP IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 540 TO BS 559, STR 17R. REPAIRED WEB IAW ER AND EA.

Part: FLOOR SUPPORT — CRACKED (BS 380-400) · airframe 43,438 hrs · 29,285 cycles

FLOOR SUPPORT UPPER FLANGE CRACKED BETWEEN BS 380 TO 400, RBL 9. R & R THE FLOOR SUPPORT IAW DWG & SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

FORWARD CARGO BAY ON LOWER CURVED BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN STR 24R TO STR 26R. R&R ANGLE PER SRM.

Part: SUPPORT — CORRODED (BS 396-420) · airframe 43,438 hrs · 29,285 cycles

FORWARD CARGO BAY ON FLOOR TO SIDE WALL SUPPORT PLATE CORRODED BETWEEN BS 396 & 420, RBL 23. R & R THE SUPPORT IAW SRM.

Part: SUPPORT ANGLE — CORRODED (BS 500D) · airframe 43,438 hrs · 29,285 cycles

FORWARD CARGO BAY ON LOWER BULKHEAD SUPPORT ANGLE CORRODED AT BS. 500D, BETWEEN LBL 24 TO RBL 24. / R&R ANGLE PER DWG AND SRM.

Part: SUPPORT — CORRODED (BS 420-440) · airframe 43,438 hrs · 29,285 cycles

FORWARD CARGO BAY ON FLOOR TO SIDE WALL SUPPORT CORRODED BETWEEN BS 420 & 440, RBL 23. R & R THE SUPPORT IAW SRM.

Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 43,438 hrs · 29,285 cycles

FORWARD CARGO BAY FLOOR SUPPORT ATTACH ANGLE CRACKED AT BS 500C, STRINGER 26R. R & R THE ATTACH ANGLE IAW SRM.

Part: SHIELD — CORRODED (BS 492-500A) · airframe 43,438 hrs · 29,285 cycles

FORWARD CARGO BAY ON FLOOR TO SIDE WALL SUPPORT PLATE SHIELD CORRODED BETWEEN BS 492 TO 500A, RBL 23. R & R SHIELD IAW SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

FORWARD CARGO BAY ON FLOOR TO SIDE WALL SUPPORT PLATE CORRODED BETWEEN BS 396 TO BS 500D, LBL 23. R&R PLATE IAW SRM.

Part: ANGLE — CRACKED (BS 500C) · airframe 43,438 hrs · 29,285 cycles

INTERCOSTAL ANGLE CRACKED AT BS 500C, STRINGER 26L. R & R THE ANGLE IAW SRM.

Part: STRINGER CLIP — CORRODED (BS 716) · airframe 43,438 hrs · 29,285 cycles

STRINGER CLIP 15L CORRODED AT BS 716. R & R THE STRINGER CLIP SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

R2 DOOR SURROUNDING STRUCTURE FITTING CORRODED AT BS 986+7, STR 13R. R&R FITTING PER SRM & DWG.

Part: FITTING — CORRODED (BS 986) · airframe 43,438 hrs · 29,285 cycles

R2 DOOR FRAME SUPPORT WEB FITTING CORRODED AT BS 986+7, STRINGER 12R. R & R THE FITTING IAW SRM & DWG.

Part: FITTING — CORRODED (BS 986) · airframe 43,438 hrs · 29,285 cycles

R2 DOOR FITTING CORRODED AT BS 986+7, STRINGER 15R. R&R FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

STUB FRAME CRACKED AT BS 294, WL 208. R&R STUB FRAME PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 43,438 hrs · 29,285 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 &. 328, RBL 34. R & R FLOOR SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 43,438 hrs · 29,285 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, LBL 12. R & R THE FLOOR SUPPORT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 43,438 hrs · 29,285 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, RBL 1. R&R INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (BS 344-360) · airframe 43,438 hrs · 29,285 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO 360, LBL 1. R & R THE INTERCOSTAL IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 294-312) · airframe 43,438 hrs · 29,285 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 294 TO 312, RBL 16. R & R THE FLOOR SUPPORT IAW DWG & SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 43,438 hrs · 29,285 cycles

RT WING LEADING EDGE NR 8 SLAT NOSE SKIN CRACKED AT STA 451.97. REPAIRED SKIN PER SRM.