N769SW

Part: SLIDE — OUT OF POSITION (ZN 800 DOOR) · airframe 78,365 hrs · 46,399 cycles

R1 DOOR SLIDE NOT SEEN IN WINDOW<[01] REMOVED AND REPLACED FS-ASSY PER MT 725-61-06 FS ;CK;S GOOD (76286)

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 78,301 hrs · 46,355 cycles

AFT SERVICE DOOR SLIDE MANUAL INFLATION HANDLE EXPOSED<[01] RESECURED COVER FLAP VELCRO ATTACHMENT TO OTHER SIDE OF VELCRO TO CONCEAL SLIDE MANUAL INFLATION HANDLE . REF SIP.

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 78,194 hrs · 46,288 cycles

FWD SERVICE DOOR SLIDE SLIPPING OUT OF POSITION<[01] REPOSITIONED FWD SVC. DOOR ESCAPE SLIDE PER M/T 725-61-06. CK OK @ THIS TIME.

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 78,195 hrs · 46,289 cycles

FORWARD RIGHT SIDE EMERGENCY EXIT SLIDE IS HANGING DOWN FROM BOTTOM.<[01] PERFORMED FORWARD SERVICE DOOR ESCAPE SLIDE REPACK PER MT 725-61-06-FS.

Part: SLIDE — OUT OF ADJUST (ZN 800 DOOR) · airframe 77,708 hrs · 45,975 cycles

CREW REPORTS THAT FWD SERVICE DOOR ESCAPE SLIDE PRESSURE GAUGE IS DIFFICULT TO READ DUE TO SITTING LOW IN INSPECTION WINDOW<[01] VERIFIED SLIDE ASSY IS CORRECT AND SERVICEABLE INSTALLED PART NUMBER. ADJUSTED SLIDE IN CONTAINER PER AMM 25-66-01 AND MT 725-61-06. SLIDE PRESSURE GAUGE IS IN VIEWABLE POSITION AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 77,241 hrs · 45,673 cycles

EMERGENCY LIGHTS AT 3DEF; 5DEF; EXTERIOR SERV DOOR LIGHT; AND OVER DOOR EXIT SIGN INOP<[01] REMOVED AND INSTALLED NEW BATTERY PACK IAW AMM 33-51-06.OPS CHECKS GOOD. OK FOR SERVICE.

Part: SLIDE — OUT OF ADJUST (ZN 900 LAV/GALLE) · airframe 76,451 hrs · 45,170 cycles

FWD SERVICE DOOR SLIDE HAS DROPPED 4 INCHES<[01] REF AMM 25-66-01 REPACKED SLIDE AS REQUIRED. OK FOR SERVICE

Part: SLIDE — OUT OF ADJUST (ZN 900 LAV/GALLE) · airframe 76,451 hrs · 45,170 cycles

MOC REQUEST -REPOSTION FWD SEV DOOR SLIDE<[01] RE-POSITIONED FWD SEV DOOR SLIDE;CK;S GOOD REF AMM 25-66-01 (69675)

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 76,147 hrs · 44,976 cycles

FLOOR BEAM INTERCOSTAL IS CRACKED BETWEEN STA 312-328 AT LBL 45<[01] R & R INTERCOSTAL PER SRM 51-10-02 & SRM 51-40-02.;[02] C/W INSPECTION PER SRM 51-10-02 & SRM 51-40-02

Part: LIGHT — FAILED (ZN 200 FUS TOP) · airframe 76,147 hrs · 44,976 cycles

FWD L/H AND MID R/H EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS M1675 AND M1669 REFERENCING AMM 33-51-06. OPS CHECK GOOD

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 76,147 hrs · 44,976 cycles

FWD L/H; AND MID R/H EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST.<[01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS M1675 AND M1669 REFERENCING AMM 33-51-06. OPS CHECK GOOD.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 76,147 hrs · 44,976 cycles

FLOOR BEAM INTERCOSTAL IS CRACKED BETWEEN STA 328-344 AT LBL 45<[01] R & R INTERCOSTAL PER SRM 51-10-02 & 51-40-02.;[02] C/W INSPECTION PER SRM 51-10-02 & SRM 51-40-02

Part: HANDLE — CRACKED (R/H OVERWING) · airframe 75,445 hrs · 44,510 cycles

RIGHT OVERWING EMERGENCY EXIT HANDLE IS CRACKED. / [01] REMOVED AND REPLACED RIGHT OVERWING HANDLE PER AMM 52-22-51. OPS CK OK

Part: PLATE — CRACKED (AFT CARGO) · airframe 74,146 hrs · 43,614 cycles

AFT CARGO BAY AFT ANCHOR PLATE CRACKED / [01] REMOVED AND REPLACED ACB AFT ANCHOR PLATE IAW AMM 25-52-10-400-801 STEPS 3.F.(10);[02] VERIFIED CORRECTIVE ACTION #1

Part: ANGLE — CRACKED (L/H MLG W/W) · airframe 74,146 hrs · 43,614 cycles

L/H MWW ATTACH CLIP 149A7692-15 CRACKED BS 727 LBL 19 WL 145 L/H MWW SUPPORT RING CLIP IS CRACKED BS 727 LBL 20.5 W/L 148. P/N 149A7678-7 / [01] UPDATED MEASUREMENTS;[02] ATTACH CLIP HAS NO LIMITS FOR A CRACK. PART FOUND TO BE OUT OF LIMITS IAW SRM 53-40-71-1A-1; SRM 51-10-02;[03] FORMED REPLACEMENT PART FROM 2024TO #0.050 SH-C LOT#1292371 IAW PL 149A7692 REV C; DWG 149A7692 ID:0007 REV-;[04] VERIFIED CORRECTIVE ACTION STEP 1-3.;[05] RECEIVED NEW ANGLE P/N:HFAB53-AN-002 ; LOT:1488687-1; P.O/N:864396/1.<BR><BR>LOCATED AND DRILLED AT L/H MWW BS 727 LBL19 WL 145 AND APPLIED CHEMICAL CONVERSION COATING ON NEW ANGLE IAW SRM 51-40-05. REQUEST OK TO PRIMER.;[06] VERIFIED CORRECTIVE ACTION #5;[07] APPLIED PRIMER ON NEW ANGLE IAW SOPM 20-41-02. REQUEST OK TO APPLY ENAMEL.;[08] VERIFIED CORRECTIVE ACTION #7;[09] APPLIED ENAMEL ON NEW ANGLE IAW SOPM 20-41-04. REQUEST OK TO INSTALL.;[10] OK TO INSTALL SUPPORT ANGLE.;[11] INSTALLED NEW CLIP IAW SRM 51-40-02-0G-0 AND DWG 149A7610 REV.-;[12] VERIFIED CORRECTIVE ACTION 11.;[13] WORKSCOPE COMPLETE.

Part: PANEL — DELAMINATED · airframe 74,146 hrs · 43,614 cycles

PANEL 193AR HAS 2 DELAMINATED AREAS ON OUTER SURFACE SKIN AS NOTED ON FAULT TTG8Q00BMNQU / [01] IDENTIFIED PANEL 193AR MATERIAL IAW SRM 53-40-70-0I-1 TABLE 2 FIGURE 2 ITEM 18. DELAMINATED SKIN AT DISCREPANT LOCATIONS OVER HONEYCOMB CORE EXCEED ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PARAGRAPH 4.A(6). DAMAGE IS REPAIRABLE PER SRM 51-70-05-2R-1 AS DIRECTED BY SRM 53-40-70-2R-1 <BR><BR>REMOVED 2 AREAS OF DAMAGE ON OUTER SURFACE OF PANEL 193AR; ONE AREA WAS A DETERIORATED PREVIOUS REPAIR. AREAS MEASURE 4.5' X 2.5' AND 5.5' X 2.5'. NO CONTAMINATION NOTED; AND CLEANED REPAIR AREAS IAW SRM 51-70-05-2R-1 PARAGRAPH 4.A-B.;[02] VALIDATED REPAIR PER SRM 51-70-50-2R-1;[03] VERIFIED CORRECTIVE ACTIONS 1 AND 2<BR><BR>VALIDATED REPAIR PER SRM 51-70-50-2R-1;[04] FABRICATED REPAIR PLIES FROM BMS 8-79ST1581 LOT#1482269-1 AND ADHESIVE BMS 5-129GR5 LOT#1483751-1; INSTALLED; VACUUM BAGGED; LEAK CHECK GOOD; CURED WITH HOTBONDER ID:NCX000526 S/N:12051216; UNBAGGED IAW SRM 51-70-05-2R-1 PARA 4C-E.;[05] INSPECTED AND VERIFIED CORRECTIVE ACTION 4. POST REPAIR UT INSPECTED PER 737NDT PART 4 51-00-02. NO DEFECTS FOUND. TOOL E650 ATS2342.;[06] APPLIED AND CURED BMS 10-21 TY III LOT#S21H278 CONDUCTIVE COATING USING THERMOMETER ID:ATS2208 S/N:43300740WS; CONDUCTIVITY TESTED GOOD USING MULTIMETER ID:ATS1658 S/N:43000350 IAW AMM 51-21-71-370-801 PAR 3D(1-4;7A).;[07] COMPLETED REFINISH OF PANEL'S TOOLSIDE IAW SRM 51-70-05-2R-2 PARAGRAPH 4.K.;[08] FINAL INSPECTION. JOB COMPLETE PER SRM 51-70-05-2R-1.

Part: SUPPORT RING — CRACKED (L/H MLG W/W) · airframe 74,146 hrs · 43,614 cycles

L/H MWW SUPPORT RING CLIP IS CRACKED BS 727; LBL 20.5; W/L 148. P/N 149A7678-7 / [01] REMOVED CLIP AT L/H MWW SUPPORT BS 727; LBL 20.5; W/L 148. IAW SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW CLIP P/N 149A7678U9 PO# 864333 IAW SRM 51-40-05-0G-0 AND DWG 149A7610 REV.-;[03] VERIFIED CORRECTIVE ACTION 2;[04] REQ. OK TO INSTALL CLIP;[05] OK TO INSTALL CLIP PN 149A7678-7;[06] INSTALLED NEW CLIP AT BS 727 LBL 20.5 W/L 148 IAW SRM 51-40-02-0G-0 AND DWG 149A7610 REV.-;[07] VERIFIED CORRECTIVE ACTION 6.;[08] VERIFIED WORKSCOPE IS COMPLETE.

Part: FLAP — DELAMINATED (R/H WING) · airframe 74,146 hrs · 43,614 cycles

R/W O/B AFT FLAP I/B END UPPER SURFACE IS DELAMINATED / [01] REMOVED R/W O/B AFT FLAP IAW AMM 27-51-22-000-801 STEPS 2.D.;[02] VERIFIED;[03] ACCOMPLISHED PARTS REMOVAL TABLE;[04] R/W O/B AFT FLAP I/B END UPPER SURFACE DELAMINATED AREA WAS REPAIRED ON ATS WORK ORDER #548603; CUSTOMER PO<BR>#P2796377-1;[05] OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION 3 AND 4. <BR>OK TO INSTALL;[07] INSTALLED R/W O/B AFT FLAP IAW AMM 27-51-22-420-002 STEP 3.F.(4)(A)-(D)(E)1)-6);[08] VERIFIED;[09] INSTALLED RIGHT WING OUTBOARD AFT FLAP IAW AMM 27-51-22-400-801 STEPS 3. F. (4) (5). TORQUE AND SAFETY VERIFIED<BR>CAL ID ATS2687<BR>S/N 1021903746<BR>CAL DUE 11/2022<BR><BR>CAL ID ATS1731<BR>S/N 1505093<BR>CAL DUE 11/2022;[10] VERIFIED;[11] VERIFIED CORRECTIVE ACTION #9;[12] ADJUSTED RIGHT WING OUTBOARD AFT FLAP IAW AMM 27-51-22-400-801 STEPS 3. G. ADJUSTMENT CHECK GOOD.;[13] VERIFIED;[14] REMOVED RIG PINS AND PUT AIRCRAFT BACK TO USUAL CONDITION IAW AMM 27-51-22-400-801;[15] VERIFIED;[16] VERIFIED CORRECTIVE ACTION 12;[17] VERIFIED CORRECTIVE ACTION 14

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 74,146 hrs · 43,614 cycles

AFT CARGO DOOR; FWD SCUFF PLATE IS CRACKED / [01] WELDED 1EA CRACKED AREA ON ACB; FWD CORNER SCUFF PLATE USING ER4043 ALUMINUM FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4)<BR>WELDING MACHINE CAL ID E10583; S/N; KJ256554;[02] VERIFIED WELD PER SRM 53-60-15-2R-1.;[03] PT INSPECTED WELD IAW SOPM 20-20-02.<BR>NO CRACKS NOTED <BR>EQUIP USED: RADIOMETER ID: ATS2561-1;2;3;[04] SANDED WELD REPAIR AREA SMOOTH PER SRM 53-60-15-2R-1 PARA 4.B.(5);[05] VERIFIED SMOOTH PER SRM 53-60-15-2R-1; JOB COMPLETE.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON ACB FLOOR SUPPORT AT STA 727A+10; 727B+10; 727D+4 ; RBL 14; WL 156. / RBL 14; WL 156 FOUND TO OUT OF LIMITS WITH REMAINING OF .053' OF ORIGINAL THICKNESS .063'. IAW SRM 53-60-53-0I-2; SRM 53-00-53-1A-2 AND BAC1509-100146<BR><BR>DEPTH GAUGE USED ID:ATS2473 DUE:07:2022;[02] VERIFIED CORRECTIVE ACTION 1;[03] REMOVED DAMAGED TIE DOWN TRACK AT BS 727 TO SLICE AT BS 747+9'; RBL 14; WL 156 IAW SRM 51-40-02;[ REMOVED CARGO TRACK AT BS 747+9 TO BS 887 ; RBL 14; WL 156 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED TRACK ASSY PN 146A7501-25 COMMON TO FRAMES AND BAFFLE FROM BS727 TO BS887 IAW SRM 51-40-05; DWG 146A7500; DWG 146A7501. LOCATED AND DRILLED TRACK ASSY PN 146A7501-25 COMMON TO FRAMES AND BAFFLE FROM BS727 TO BS 747 AND BS 767 TO BS 887;RBL 14; WL156 IAW SRM 51-40-05; DWG 146A7500; DWG 146A7501;ID: 27;REV:A;OK TO INSTALL NEW CARGO TRACK ON ACB BS 727 TO BS 747 AND BS 787 TO BS 887 ; RBL 14; WL 156 INSTALLED NEW TRACK ASSY ACB FROM BS727 TO BS 747 AND BS 767 TO BS 887;RBL 14; WL156 IAW SRM 51-40-02-0G-0; DWG 146A7500;ID:0027;REV:A; DWG 146A7501;ID:0027;REV: LOCATED AND DRILLED SPLICE BETWEEN BS 747 TO BS 767; RBL 14; WL 156 IAW SRM 53-00-53-2R-3; OK TO INSTALL SPLICE; LOCATED AND DRILLED SPLICE P/N 146A7506-20 BETWEEN BS 747 TO BS 767; RBL 14; WL 156 IAW SRM 53-00-53-2R-3; OK TO INSTALL SPLICE; INSTALLED SPLICE BETWEEN BS 747 TO BS 767 ; RBL 14; WL 156 IAW SRM 53-00-53-2R-3;

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON FWD CARGO BAY DOOR CUTOUT AFT SHIELD AT STA 500+10; WL 156; RBL 24. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED;[03] RECEIVED NEW SHIELD P/N:143A8126U31 ; LOT:1484884-1 AND LOCATED AND DRILLED AT FCB BETWEEN BS 492 TO 500A R/H WL 156 ; RBL 24 IAW SRM 51-40-05 AND DWG: 143A0080 ID:0029 REV:-.;[04] VERIFIED RECEIVED NEW SHIELD P/N:143A8126U31 ; LOT:1484884-1 AND LOCATED AND DRILLED AT FCB BETWEEN BS 492 TO 500A R/H WL 156 ; RBL 24 IAW SRM 51-40-05 AND DWG: 143A0080 ID:0029 REV:-.;[05] FIXED MEASUREMENT 22 TO MINOR.;[06] VERIFIED CARD COMPLETE

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON ACB FLOOR SUPPORT AT STA 767+5; RBL 2; WL 156. / [01] REMOVED CORROSION ON ACB FLOOR SUPPORT BS767+5; RBL 2; WL 156 IN AREA OF L=1.3'XW=.9'XD=.008' FOUND TO BE OUT OF LIMITS WITH REMAINING THICKNESS OF .055' OF ORIGINAL THICKNESS OF .063' IAW SRM 53-60-53-0I-2; SRM 53-00-53-1A-2 AND BAC1509-100146 <BR><BR>DEPTH GAUGE USED: ID:ATS2473 DUE:07/2022;[02] VERIFIED CORRECTIVE ACTION 1;[03] SRM 53-00-53-2R-2 IS FOUND TO BE APPLICABLE FOR THIS REPAIR;[04] SRM 53-00-53-2R-2 IS FOUND TO BE APPLICABLE FOR THIS REPAIR;[05] PERFORMED DAMAGE CUT OUT ON ACB FLOOR SUPPORT BS BS 767+5; RBL2; WL 156 IAW SRM 53-00-53-2R-2 STEPS 4.D.(B);[06] VERIFIED CORRECTIVE ACTION 5.;[07] ACCOMPLISHED HFEC INSPECTION OF DAMAGE CUT OUT IAW NDTM D6-37239 PART 6; 51-00-00 PROC 23. NO CRACKS FOUND. TOOL I.D. IS000450 500D;[08] STATUS CUTOUT DIMENSIONS: L=3'; W=1'; AT BS 767+5; RBL 2; WL 156 IAW SRM 53-00-53-2R-2; DETAIL F.;[09] LOCATED AND DRILLED NEW REPAIR CHANNEL FROM 7075-T6511; LOT. 1487793-1; PO # 863363/1; APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 53-00-53-2R-2; STEP 4D(B) N AND O; OK TO INSTALL REPAIR CHANNEL.;[10] VERIFIED CORRECTIVE ACTIONS #8 AND #9;[11] UPDATED MEASUREMENTS;[12] INSTALLED REPAIR AT ACB FLOOR SUPPORT RBL 2; BETWEEN BS 767-787 IAW SRM 53-00-53-2R-2;[13] REPAIR CHANNEL LOT NUMBER # FROM OUTSIDE SERVICES IS 1480675-1;[14] VERIFIED CORRECTIVE ACTION ENTRY 11-13.;[15] VERIFIED TASK COMPLETE

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON ACB FLOOR SUPPORT AT STA 767+5; LBL 2; WL 156. / [01] REMOVED CORROSION ON ACB FLOOR SUPPORT BS767+5; LBL 2; WL 156 IN AREA OF L=1.1'XW=.9'XD=.012' FOUND TO BE OUT OF LIMITS WITH REMAINING THICKNESS OF .051' OF ORIGINAL THICKNESS OF .063' IAW SRM 53-60-53-0I-2; SRM 53-00-53-1A-2 AND BAC1509-100146 <BR><BR>DEPTH GAUGE USED: ID:ATS2473 DUE:07/2022;[02] VERIFIED CORRECTIVE ACTION 1;[03] SRM 53-00-53-2R-2 IS FOUND TO BE APPLICABLE FOR THIS REPAIR;[04] PERFORMED DAMAGE CUT OUT ON ACB FLOOR SUPPORT BS BS 767+5; LBL 2; WL 156 IAW SRM 53-00-53-2R-2 STEPS 4.D.(B);[05] VERIFIED CORRECTIVE ACTION 5.;[06] ACCOMPLISHED HFEC INSPECTION OF DAMAGE CUT OUT IAW NDTM D6-37239 PART 6; 51-00-00 PROC 23. NO CRACKS FOUND. TOOL I.D. IS000450 500D;[07] STATUS CUTOUT DIMENSION L: 3' W: 1' AT ACB BS.767+5 LBL.2 WL.156 IWA SRM 53-00-53-2R-2 DETAIL F;[08] LOCATED AND DRILLED NEW REPAIR CHANNEL FROM 7075-T76511 LOT:1487793-1 PO NUMBER:863363/1; APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 53-00-53-2R-2 STEPS 4.D.(B) N AND O; OK TO INSTALL REPAIR CHANNEL;[09] VERIFIED CORRECTIVE ACTIONS #7 AND #8;[10] INSTALLED NUT PLATES; INSTALLED NEW REPAIR AND APPLIED CIC AT BS.767+5' LBL.2' WL.156 IAW SRM 53-00-53-2R-2 STEPS 4.D.(B) P AND Q (1)(2)(3) 4 S;[11] VERIFIED CORRECTIVE ACTION #10;[12] TASK COMPLETE;[13] CORRECTION- VERIFIED CORRECTIVE ACTION 4.

Part: SUPPORT — CRACKED (FWD CARGO BAY) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON FWD CARGO BAY AFT BULKHEAD SUPPORT AT STA 500D; RBL 18 TO LBL 18; WL 156. / [01] THERE IS NO SRM ALLOWABLE DAMAGE FOR FCB AFT BULKHEAD SUPPORT. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED ACTION 1;[03] REMOVED CORROSION AT STA 500D<BR><BR>LBL 1 0.005'<BR>LBL 2 0.003'<BR>LBL 9 0.004'<BR>LBL 17 0.003'<BR>LBL 18 0.004'<BR>RBL 1 0.003'<BR>RBL 2 0.003'<BR>RBL 9 0.004'<BR>RBL 14 0.005'<BR>RBL 18 0.006'<BR><BR>ORIGINAL MATERIAL THICKNESS : 0.071 ; THE DEEPEST DAMAGE : 0.006'. DAMAGE DOES NOT EXCEED 10% OF ORIG. MATERIAL THICKNESS. FOUND TO BE WITHIN LIMIT<BR><BR>CALIBRATION TOOL DEPTH GAUGE<BR>ID : ATS1225<BR>S/N : UNKNOWN<BR>DUE : 07/2022;[04] INSPECTED ACTION 3;[05] APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01-0G-0 AND SOPM 20-41-02;[06] INSPECTION COMPLETE;[07] UPDATED MEASUREMENTS

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON ACB R/H FLOOR TO SIDEWALL FROM STA 867+7; TO STA 927+17; RBL 22; WL 165 TO WL 178. / [01] REMOVED CORROSION FROM ACB R/H FLOOR TO SIDEWALL SUPPORT AT BS867+7 MEASURED 1.2'L X 0.6'W AND 0.001'DEEP ORIGINAL THICKNESS OF 0.040' FOUND IN LIMITS PER SRM 53-00-53-1A-2<BR><BR>REMOVED CORROSION FROM ACB R/H FLOOR TO SIDEWALL SUPPORT AT BS867+12 MEASURED 1.6'L X 0.8'W AND 0.0065'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2<BR><BR>REMOVED CORROSION FROM ACB R/H FLOOR TO SIDEWALL SUPPORT AT BS867+15 MEASURED 1.7'L X 0.8'W AND 0.017'DEEP ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2<BR><BR>CAL ID DIAL DEPTH GAUGE <BR>ATS400<BR>S/N UNKNOWN<BR>DUE 08/2022;[02] UPDATED MEASURMENTS;[03] VERIFIED CORRECTIVE ACTION #1;[04] FABRICATED REPLACEMENT ACB R/H FLOOR TO SIDEWALL SUPPORT BS867-947 OUT OF BAC1496-377#7075T62 LOT#1477731-1 PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; DWG 147A7501 AND DWG 146A7502;[05] VERIFIED CORRECTIVE ACTION #4;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON ACB R/H FLOOR TO SIDEWALL SUPPORT BS 867 TO BS 947 RBL 22;WL 165 IAW SRM 51-20-01` AND AMM 51-21-72-370-804.;[07] VERIFIED CORRECTIVE ACTION 6

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON AFT CARGO BAY DOOR CUTOUT AFT SHIELD FROM STA 847 TO STA 867; RBL 22; WL 164. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED;[03] RECEIVED NEW SHIELD ITEM: 146A8127Y5 LOT: 1481640-1 PO/NUMBER: 856196. LOCATED AND DRILL NEW SHIELD IAW SRM 51-40-02; SRM 51-40-05 AND DWG 146A8127 ID:0002 REV:B;[04] VERIFIED CORRECTIVE ACTION #3.;[05] FIXED MEASUREMENT 22 TO MINOR.;[06] SIGNED FOR PART;[07] VERIFIED CARD COMPLETE.;[08] CORRECTED MEASUREMENT SECTION 22;[09] CERTIFY MEASUREMENT SECTION 22 CORRECTED

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON FWD CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT AT STA 500A+5 TO STA 500C+15; RBL 24; WL 156. / [01] VERIFIED APPLICABILITY FOR ALLOWABLA DAMAGE LIMITS OF FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 500A+5 TO 500C+15 ;RBL 24 ;WL 156.IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[02] REMOVED CORROSION ON FWD CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT ( BTW STA 500A+5'500C+15';RBL 24 ;WL 156;IAW SRM 51-10-02 PARAGRAPH 15); EVALUATED ALL REWORKED AREAS;THE DEPPEST AREA BS 500A+5 RBL 24 WL 156; DIMENSION:L=2'X W=1'X DEPTH=0.011';ORIGINAL THICKNESS 0.040 REMAINING THICKNESS 0.029; FOUND TO BE OUT OF LIMITS ALLOWABLE DAMAGE LIMITS;IAW SRM 53-00-53-1A-2;ALLOWABLE DAMAGE 2 FIGURE#103 ;DEATIL 'E';TOOL USED MICROMETER ID ATS400 S/N UNKNOWN;DUE 08/2022;[03] VERIFIED ACTION 1;2;[04] FABRICATED LOCATED AND DRILLED ON FWD CARGO COMPARTMENT R/H NEW FLOOR TO SIDEWALL SUPPORT BS 500A TO BS 500D RBL 24 WL 156;MATERIAL USED BAC1496-444#7075T62;EXTRUSION;LOT#1485395-1;IAW SRM 51-40-05 AND DWG 143A7501 REV:A.APPLY CHEMICAL CONVERSION COATING AND PRIMER.;[05] INSPECTED ACTION 4;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER FWD CARGO COMPARTMENT R/H NEW FLOOR TO SIDEWALL BS 500A TO BS 500D RBL 24 WL 156 IAW SRM 51-20-01 AND AMM 51-21-72-370-804.;[07] VERIFIED CORRECTIVE ACTION ENTRY 6. CARD COMPLETE.

Part: STRAP — CORRODED (FWD CARGO BAY) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON FWD CARGO BAY TENSION STRAP AT STA 440+4 TO STA 480+5 RBL 22; WL 156. / [01] REMOVED CORROSION AT<BR><BR>STA 440+4 0.005'<BR>STA 440+9 0.006'<BR>STA 440+13 0.004'<BR>STA 440+17 0.003'<BR>STA 460+1 0.002'<BR>STA 460+5 0.002'<BR>STA 460+9 0.003'<BR>STA 460+13 0.015'<BR>STA 480+5 0.018'<BR><BR>ORIGINAL MATERIAL THICKNESS : 0.100'; REMAINING THICKNESS : 0.082'. DAMAGE EXCEED MAX ALLOWABLE DAMAGE.<BR>FOUND TO BE OUT OF LIMIT IAW SRM 53-30-15-1A-1<BR><BR>CALIBRATION TOOL DEPTH GAUGE<BR>ID : ATS1225<BR>S/N : UNKNOWN<BR>DUE : 07/2022;[02] VERIFIED ACTION 1;[03] REMOVED ON FWD CARGO BAY TENSION STRAP RBL 22; WL 156. BTW B/S 420 TO B/S 500A IAW SRM 51-40-02;[04] LOCATED AND DRILLED NEW TENSION STRAP LOT# 7530294 RBL 22; WL 156. BTW B/S 420 TO B/S 500A IAW SRM 51-40-05 AND DWG 143A8120 REV:A ; DWG 143A8330 REV:A;[05] OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION 4.<BR>OK TO INSTALL;[07] INSTALLED ON FWD CARGO BAY TENSION STRAP AT BS 420 T0 BS 500A; RBL 22; WL 156 IAW SRM 51-40-02-0G-0 AND DWG 143A8120 REV:A ; DWG 143A8330 REV:A;[08] VERIFIED CORRECTIVE ACTION 7

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON FWD CARGO BAY DOOR CUT-OUT FWD SHIELD FROM STA 420+5 TO STA 440; RBL 24; WL 156. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED;[03] RECEIVED NEW SHIELD P/N:143A8126U21ATSMRO ; LOT:1481125-1 AND LOCATED AND DRILLED AT FCB STA 420+5' TO STA 440 RBL 24 ; WL 156 IAW SRM 51-40-05 AND DWG:143A0080 ID:0013 REV:A.;[04] FIXED MEASUREMENT 22 TO MINOR.;[05] ADDED PART;[06] VERIFIED CORRECTIVE ACTION #3

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON ACB FLOOR SUPPORT AT STA927; LBL 2; WL 179. / [01] REMOVED CORROSION ON ACB FLOOR SUPPORT BS927; LBL 2; WL 179 IN AREA OF L=2'XW=2'XD=.006' REMAINING THICKNESS OF .074' OF ORIGINAL THICKNESS OF .080'; FOUND TO BE IN LIMITS IAW SRM 53-70-53-0I-2; SRM 53-00-53-1A-2 AND BAC1520-1397.;[02] REMOVED CORROSION ON ACB FLOOR SUPPORT BS927; LBL 2; WL 179 IN AREA OF L=2'XW=2'XD=.006' REMAINING THICKNESS OF .064' OF ORIGINAL THICKNESS OF .070'; FOUND TO BE IN LIMITS IAW SRM 53-70-53-0I-2; SRM 53-00-53-1A-2 AND BAC1520-1397.<BR>DIAL DEPTH GAUGE USED ID:ATS2473 DUE:07/2022;[03] REMOVED CORROSION ON ACB FLOOR SUPPORT BS927; LBL 2; WL 179 IN AREA OF L=2'XW=2'XD=.010' REMAINING THICKNESS OF .070' OF ORIGINAL THICKNESS OF .080'; FOUND TO BE OUT OF LIMITS IAW SRM 53-70-53-0I-2; SRM 53-00-53-1A-2 AND BAC1520-1397.<BR>PIN POINT MIC USED USED ID:ATS1671 DUE:10/2022;[04] VERIFIED CORRECTIVE ACTION 3;[05] REMOVED ACB FLOOR SUPPORT BS887-947.5 LBL2 WL179 IAW SRM 51-40-02-0G-0.;[06] LOCATED AND DRILLED NEW ACB FLOOR SUPPORT BS887-947.5 LBL2 WL179 P/N 147A7501-13 IAW SRM 51-40-05-0G-0 AND DRAWING#147A7501.<BR>OK TO INSTALL.;[07] VERIFIED CORRECTIVE ACTION #6;[08] INSTALLED FLOOR SUPPORT LBL 2 FROM BS 887 TO BS 947 PER SRM 51-40-02 AND DWG#147A7500;[09] VERIFIED INSTALLATION OF FLOOR SUPPORT LBL 2 FROM BS 887 TO BS 947 PER SRM 51-40-02 AND DWG#147A7500.;[10] ADDED PARTS;[11] VERIFIED ALL WORK ACCOMPLISHED

Part: ANGLE — CORRODED (FUSELAGE) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON ATTACH ANGLE AT STA 787+2; RBL 24; WL 156. / [01] REMOVED CORROSION ON ATTACH ANGLE AT STA 787+2; RBL 24; WL 156.; DIMENSIONS L:0.400' W :0.320' DEPTH : 0.045' ORIGINAL MATERIAL 0.063' TOOL USED : MICROMETER ID:ATS 601 DATE DUE: 05/2022 IAW SRM 51-10-02 PARAGRAPH 15.<BR> VERIFIED FOR ALLOWABLE DAMAGE LIMITS ON SRM AND NOT FOUND; ANGLE MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED ANGLE LOCATED BTW B/S 794.37 TO B/S 787 RBL24 WL 156 IAW SRM 51-40-02;[03] VERIFIED CORRECTIVE ACTION 1 AND 2.;[04] LOCATED AND DRILLED NEW ANGLE P/N 146A8323-10 IAW SRM 51-40-05-0G AND DWG. 146A8320; REV C;[05] LOCATED AND DRILLED NEW ANGLE P/N 146A8323-10 IAW SRM 51-40-05-0G AND DWG. 146A8320; REV C OK TO INSTALL.;[06] VERIFIED CORRECTIVE ACTION 5. OK TO INSTALL ANGLE.;[07] INSTALLED NEW ANGLE P/N 146A8323-10 IAW SRM 51-40-02-0G-0 AND DWG. 146A8320. REV C; SHEET 8; ON ACB; BS 787+2; RBL 156.;[08] VERIFIED CORRECTIVE ACTION 7.;[09] WORKSCOPE COMPLETE.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT FROM STA 727+4 TO STA 847; LBL 24; WL 156 TO WL 160. / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT BS 727+4 TO BS 847 LBL 24 WL 156;TO WL 160 IAW SRM 53-00-53-1A-2 ALLOWABLE DAMACE 2.;[04] FABRIACATED LOCATED AND DRILLED ON AFT CARGO BAY L/H NEW FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 847;LBL 24 WL 156 TO 160 MATERIAL USED BAC 1496-377#7075T62 LOT#1484618-1;AND SPLICE BTW BS 727'E' TO 747;LBL 24 WL 156 TO 160;MATERIAL USED BAC1496-377#7075T62 LOT#1484618-1;IAW SRM 51-40-05 ;SRM 53-00-53-2R-6 REPAIR 6 AND DWG 146A7502 REV:A.;[05] OK TO TREAT AND PRIME;[06] VERIFIED CORRECTIVE ACTION 4 AND 5. OK TO TREAT AND PRIME.;[07] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON AFT CARGO BAY L/H NEW FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 847 LBL 24 WL 156 TO 160 IAW SRM 51-20-01 AND AMM 51-21-72-370-804;OK TO INSTALL SPLICE.;[08] VERIFIED CORRECTIVE ACTION 7. OK TO INSTALL SPLICE;[09] INSTALLED SPLICE ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT BTW 727 'E' TO BS 747;LBL 24 WL 156 TO WL 160 IAW SRM53-00-53-2R-6 REPAIR 6 AND SRM 51-40-02;[10] VERIFIED CORRECTIVE ACTION 9.;[11] VERIFIED JOB COMPLETE

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT FROM STA 420+4 TO STA 500C+14; LBL 24; WL 156. / [01] REMOVED CORROSION ON FCB L/H FLOOR TO SIDEWALL SUPPORT BTW BS 480+7' TO 500D REWORKED AREA BTW BS 500B TO 500C' IN L=1' X W=1' X D= .002' FROM ORIGINAL THICKNESS OF .040' FOUND TO BE IN LIMITS <BR>USED TOOL :<BR>ID:ATS2503; S/N:A19335646 ; DATE:04/2021 ; DUE: 04/2022<BR>REMOVED CORROSION ON FCB L/H FLOOR TO SIDEWALL SUPPORT BTW BS 396 TO 480+7' REWORKED AREA BS 440+13' IN L=1' X W=1' X D= .010' FROM ORIGINAL THICKNESS OF .040' FOUND TO BE OUT OF LIMITS WILL BE REPAIRED BY SRM 53-00-53-2R-6.<BR>USED TOOL :<BR>ID:ATS2503; S/N:A19335646 ; DATE:04/2021 ; DUE: 04/2022 <BR>IAW SRM 53-00-53-1A-2 PAR. 4A. FIG 103 DETAIL E.<BR>REQUEST OK TO TREAT AND PRIME SECTION BS 396 TO 480+7' #1; FWD HALF OUT OF LIMITS; AFT HALF IN LIMITS;[03] FABRICATED NEW SECTION FLOOR SIDEWALL SUPPORT L/H FCB FROM P/N: BAC1496-444#7075T6 LOT: 1485395-1 BETWEEN BS 369 TO BS 480+7' IAW SRM 53-00-53-2R-6. REQUEST TREAT AND PRIMEFABRICATED SPLICE P/N: BAC1496-444#7075T6 LOT: 1485395-1 ON FLOOR TO SIDEWALL SUPPORT BETWEEN BS 480 TO BS 500 L/H IAW SRM 53-00-53-2R-6. REQUEST TREAT AND PRIME..APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON FLOOR SIDEWALL SUPPORT AND SPLICE BS 396 TO 500D IAW SRM 51-20-01 AND SOPM 20-41-02. ] INSTALLED SPLICE TO FLOOR TO SIDEWALL SUPPORT ON FCB BETWEEN BS 480 TO BS 500 L/H IAW SRM 53-00-53-2R-6 FIG 202 AND 51-40-02.; FIXED MEASUREMENTS 22 TO MINOR;

Part: WEB — CORRODED (FWD CARGO BAY) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON FWD CARGO BAY SUB THRESHOLD WEB AT STA 440+14 TO STA 460+19; WL 156; RBL 28 TO RBL 29. / [01] REMOVED CORROSION AT<BR><BR>STA 440+14 0.003'<BR>STA 440+15 0.001'<BR>STA 440+16 0.002'<BR>STA 460 0.006'<BR>STA 460+3 0.002'<BR>STA 460+5 0.002'<BR>STA 460+5 0.001'<BR>STA 460+6 0.001'<BR>STA 460+9 0.002'<BR>STA 460+13 0.003'<BR>STA 460+17 0.002'<BR>STA 460=18 0.002'<BR><BR>ORIGINAL MATERIAL THICKNESS : 0.045'; REMAINING MATERIAL THICKNESS : 0.039' AT STA 460.<BR><BR>DAMAGE EXCEED MAX ALLOWABLE DAMAGE.<BR>FOUND TO BE OUT OF LIMIT<BR><BR>CALIBRATION TOOL DEPTH GAUGE<BR>ID : ATS1225<BR>S/N : UNKNOWN<BR>DUE : 07/2022;[02] REMOVED CORROSION AT<BR><BR>STA 440+14 0.003'<BR>STA 440+15 0.001'<BR>STA 440+16 0.002'<BR>STA 460 0.006'<BR>STA 460+3 0.002'<BR>STA 460+5 0.002'<BR>STA 460+5 0.001'<BR>STA 460+6 0.001'<BR>STA 460+9 0.002'<BR>STA 460+13 0.003'<BR>STA 460+17 0.002'<BR>STA 460=18 0.002'<BR><BR>ORIGINAL MATERIAL THICKNESS : 0.045'; REMAINING MATERIAL THICKNESS : 0.039' AT STA 460.<BR><BR>DAMAGE EXCEED MAX ALLOWABLE DAMAGE.<BR>FOUND TO BE OUT OF LIMIT IAW SRM 53-30-15-1A-1<BR><BR>CALIBRATION TOOL DEPTH GAUGE<BR>ID : ATS1225<BR>S/N : UNKNOWN<BR>DUE : 07/2022;[03] VERIFIED ACTION 1;2;[04] LOCATED; DRILLED; AND COUNTERSUNK REPLACEMENT WEB PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; AND DWG 143A8330; SHT 21. APPLIED CHEMICAL CONVERSION COATING PER AMM 51-21-41-370-802. INSTALLED NUT PLATES PER SRM 51-40-02-0G-0 AND DWG 143A8300; SHT 21.

Part: STRINGER CLIP — CORRODED · airframe 74,146 hrs · 43,614 cycles

CORROSION ON STRINGER CLIP AT STA 787+1; RBL 14 WL 154. / [01] ENTERED MEASUREMENTS;[02] B737-700 SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS EVALUATION.<BR>NO ALLOWABLE DAMAGE FOR THIS PART FOUND IN B737-700 SRM. REPAIR BY REPLACEMENT IAW SRM 51-10-02.<BR>REMOVED DAMAGED PART IAW SRM 51-40-02.<BR>RECEIVED NEW CLIP PN 146A1010-27 FROM STORES REF PO 854889.<BR>LOCATED AND DRILLED NEW CLIP IAW SRM 51-40-05 AND DWG 146A1262.<BR>OK TO INSTALL.;[03] VERIFIED CORRECTIVE ACTION #2;[04] INSTALLED NEW STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1262 REV:-;[05] REJECTION TO ITEM 4 AT STEP 1.;[06] INSTALLED NEW STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1262 REV:- AND DWG 146A1263 REV: A;[07] CHANGED STEP FROM COMPLETE TO PARTIAL;[08] VERIFIED CORRECTIVE ACTION #6;[09] JOB COMPLETE

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON AFT CARGO BAY DOOR CUTOUT FWD SHIELD FROM STA 767+3 TO STA 767+9; WL 156; RBL 25. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] VERIFIED;[03] RECEIVED NEW SHIELD ITEM: 146A8127U1 LOT: 1474614-1. LOCATED AND DRILL NEW SHIELD IAW SRM 51-40-02; SRM 51-40-05 AND DWG 146A8127 ID: 0001 REV:C;[04] VERIFIED RECEIVED NEW SHIELD ITEM: 146A8127U1 LOT: 1474614-1. LOCATED AND DRILL NEW SHIELD IAW SRM 51-40-02; SRM 51-40-05 AND DWG 146A8127 ID: 0001 REV:C.;[05] FIXED MEASUREMENT 22 TO MINOR.;[06] JOB COMPLETE

Part: SUPPORT ANGLE — CRACKED (CABIN) · airframe 74,146 hrs · 43,614 cycles

CRACKED SUPPORT ANGLE AT MID PASSENGER CABIN BS691 RBL1. / [01] REMOVED DAMAGED BRACKET AT BS 691 RBL1 PER SRM 51-40-02;[02] CRACKED SUPPORT ANGLE AT BS691 RBL1 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS REPLAREABLE BY REPLACEMENT OF PART PER SRM 51-10-02-0G-0 STEP 9-C;[03] FABRICATED SUPPORT BRACKET P/N 237A9112-48 AND APPLIED CHEMICAL CONVERSION COATING PER DRAWING # 273A9111 SHT 8 REV A AND SRM 51-20-01-0G-0 ;SRM 51-40-05;[04] MATERIAL ID FOR BRACKET BAC1490-2883 7075-T73 .050 LOT#1482272-1; PO#857528-SWA;[05] INSPECTED ACTION 1-4;[06] APPLIED PRIMER TO REPLACEMENT SUPPORT ANGLE PER DRAWING # 273A9111 SHT 8 REV A AND SRM 51-20-01-0G-0; OK TO INSTALL;[07] INSPECTED ACTION 6; OK TO INSTALL;[08] INSTALLED SUPPORT ANGLE AT MID PASSENGER CABIN BS691; RBL1 PER SRM 51-40-02-0G-0 AND BOEING DRAWING #273A9111;[09] VERIFIED FASTENER INSTALLATION;[10] VERIFIED FASTENER INSTALLATION

Part: SEAT TRACK — CORRODED (CABIN FLOOR) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 45 BS 480+6; BS 500+7; BS 500A+7; BS 500A+18; BS 500C+9. / [01] SEAT TRACK TO BE WORKED ON CARD #TTG8Q00BKCK4;[02] UPDATED MEASUREMENT TABLE;[03] VERIFIED CORRECITVE ACTION 1 AND 2;[04] AMT ACTION IS COMPLETE

Part: SUPPORT ANGLE — CRACKED (CABIN) · airframe 74,146 hrs · 43,614 cycles

CRACKED SUPPORT ANGLE AT MID PASSENGER CABIN BS692 RBL24. / [01] REMOVED DAMAGED BRACKET AT BS692 RBL 24 PER SRM 51-40-02;[02] CRACKED SUPPORT ANGLE AT BS692 RBL24 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS REPLAREABLE BY REPLACEMENT OF PART PER SRM 51-10-02-0G-0 STEP 9-C;[03] FABRICATED SUPPORT BRACKET P/N 237A9112-45 AND APPLIED CHEMICAL CONVERSION COATING PER DRAWING # 273A9110 SHT 5 REV A AND SRM 51-20-01-0G-0 ;SRM 51-40-05;[04] MATERIAL ID FOR BRACKET BAC1490-2782 7075-T73 .050 LOT#1482272-1; PO#857530-SWA;[05] INSPECTED ACTION 1-4;[06] APPLIED PRIMER TO REPLACEMENT SUPPORT ANGLE PER DRAWING # 273A9110 SHT 5 REV A AND SRM 51-20-01-0G-0; OK TO INSTALL;[07] INSPECTED ACTION 6; OK TO INSTALL;[08] INSTALLED SUPPORT ANGLE AT BS692 RBL24 IAW RSM CH 51-40-02 AND DRAWING #273A9112.;[09] VERIFIED FASTENER INSTALLATION;[10] VERIFIED FASTENER INSTALLATION

Part: BRACKET — CRACKED (L/H WING) · airframe 74,146 hrs · 43,614 cycles

CRACK ON LEFT WING T/E BULB SEAL RETAINER SUPPORT AT ORSS 261; 3'BELOW FROM UPPER PANEL; 20' FWD FROM T/E.(ACCESS FROM 551GB) / [01] REMOVED L. WING T/E BULB SEAL SUPPORT PANEL AND BRACKET IAW SRM 51-40-04 AND AMM 20-50-01 AND LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-05;[02] INSTALLED NEW BRACKET TO L. WING T/E BULB SEAL PANEL IAW SRM 51-40-05-0G-0 AND INSTALLED L.WING T/E PANEL IAW AMM 20-50-01;[03] CERTIFIED ACTION 1 AND 2;[04] VERIFIED CORRECTIVE ACTION #2

Part: SEAT TRACK — CORRODED (CABIN FLOOR) · airframe 74,146 hrs · 43,614 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT RBL 25 BS 660+15. / [01] REMOVED CORROSION FROM SEAT TRACK WITH A MAX MATERIAL LOSS OF .037 ON THE TOP OF THE WELL. FOUND TO BE OUT OF LIMITS USING TOOL ID # ATS1225 S/N UNK CAL. DATE 07/2021 DUE 07/2022.;[02] REMOVED CORROSION FROM SEAT TRACK WITH A MAX MATERIAL LOSS OF .037 ON THE TOP OF THE WELL. FOUND TO BE OUT OF LIMITS USING TOOL ID # ATS1225 S/N UNK CAL. DATE 07/2021 DUE 07/2022. IAW SRM CH 53-00-52-1A-1;>CORROSION REMOVAL FOUND TO BE OUT OF LIMITS.;[04] REMOVED DAMAGED SEAT TRACK FROM BS727B THROUGH 887 RBL 25 LOCATED AND DRILLED NEW TRACK. IAW SRM CH 51-40-02. OK TO INSTALL.;[05] REMOVED DAMAGED SEAT TRACK FROM BS727B THROUGH 887 RBL 25 LOCATED AND DRILLED NEW TRACK. IAW SRM CH 51-40-02. SRM CH 51-40-05. OK TO INSTALL.;[06] RECEIVED SEAT TRACK FABRICATED IAW BOEING DRAWING # 144A5350 REFER TO ATS BUILD RECORD 533670.;[07] VERIFIED CORRECTIVE ACTION #5; 6;[08] RECEIVED SEAT TRACK FABRICATED IAW BOEING DRAWING # 144A5350 REFER TO ATS BUILD RECORD 533670.<BR>REMOVED DAMAGED SEAT TRACK FROM BS540 THROUGH 727B RBL 25 LOCATED AND DRILLED NEW TRACK. IAW SRM CH 51-40-02. SRM CH 51-40-05. OK TO INSTALL.;[09] VERIFIED CORRECTIVE ACTION #8; CORRECTED STATION NUMBERS;[10] INSTALLED SEAT TRACK AT RBL 25 BS 540 THROUGH 727B IAW SRM CH 51-40-02 AND DRAWING # 144A5300 SHT 1;[11] INSTALLED SEAT TRACK AT RBL 25 BS 540 THROUGH 727B IAW SRM CH 51-40-02 AND DRAWING # 144A5300 SHT 1 USING TOOL ID # E11969 S/N SP02F31939 CAL DATE 12/2021 DUE 12/2022

Part: BARRIER — CRACKED (L/H MLG) · airframe 74,146 hrs · 43,614 cycles

CRACK IN LEFT HAND VAPOR BARRIER AT B.S. 663; L.B.L. 8; W.L. 150. / [38] INSTALLED L/H VAPOR BARRIER BS 663 IAW SRM 51-40-02-0G-0 AND DWG 111A1000 REV-B AND 111A1001 REV-B AND 111A7000 REV-A. REQ OK TO INSTALL STEPS 4; 12 AND 13;[39] OK TO INSTALL EXHAUST PNL NGS STEP 17;[40] OK TO INSTALL ITEMS IN STEP 4;12;13; AND 17;[41] INSTALLED L/H VAPOR BARRIER BS 663 IAW SRM 51-40-02-0G-0 AND DWG 111A1000 REV-B AND DWG 111A1001 REV-B AND DWG 144A7100 RE.-;[42] UPDATED STEPS 4;12; 13; AND 16;[43] UPDATED STEP 17;[44] REQ. OK TO INSTALL ITEMS IN STEP 14 ND 15;[45] STEPS 14 AND 15 UPDATED.;[46] UPDATED STEP 17;[47] VERIFIED CORRECTIVE ACTION 41.;[48] APPLIED CAP SEAL AT FSTENERS AFT SIDE L/H VAPOR BARRIER BS 663 IAW AMM 51-31-00-390-805;[49] UPDATED STEP 2;3 AND 4;[50] UPDATED STEP 14 AND 15;[51] COMPLETED STEPS 14 AND 15 AND APPLIED CAP SEAL AT FASTENERS REFER ITEM 48;[52] VERIFIED STEPS 14 AND 15 (CORRECTIVE ACTION 50 AND 51;[53] OPENED STEPS 2; 3 AND 4 TO ALLOW Q/C BUY OFF OF STEPS;[54] STEPS 2-4 COMPLETE;[55] VERIFIED VAPOR BARRIER INSTALLATION ON CORRECTIVE ACTION 41.;[56] L/H BS663 VAPOR BARRIER REPLACEMENT IS COMPLETE.

Part: SENSOR — MALFUNCTIONED (LE FLAP SYSTEM) · airframe 72,493 hrs · 42,634 cycles

AFTER T/O FLAPS RETRACTED NORMALLY; PASSING 6000 AMBER LIGHT FLAP TRANSIT LT ILLUMINATE AND. #4 FLAP INDICATOR ILLUMINATED AMBER ON OVERHEAD PANEL. AIRSPEED WAS 250 AND HIT 25O DURING TROUBLESHOOTING ; THEN DECREASED TO 210. LIGHTS CAME AND WENT W/FLAPS. UP. NORMAL INDICATIONS W/FLAPS EXTENDED. NO ROLL NOTED. AMBER LTS ILLUMINATED AFTER LANDING W/FLAPS UP. / [01] BITE OF FSEU SHOWS FAULT MSG 27-81222. PERFORMED FIM 27-88 TASK 805. FOUND NO FAULTS WITH AIRCRAFT SIDE WIRING. REPLACED K-FLAP #4 RETRACT SENSOR S174 IAW M/M 27-88-11.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 71,655 hrs · 42,161 cycles

FWD SERVICE DOOR; LOWER EMER. EXIT LIGHT LENS MISSING DIRECTIONAL ARROW / REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-51-01

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 71,655 hrs · 42,161 cycles

LEFT OVERWING EMER EXIT LIGHT LOWER LIGHT LENS MISSING DIRECTIONAL ARROW / REMOVED AND REPLACED SIGN IAW AMM 33-51-01; INSPECTED

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 71,655 hrs · 42,161 cycles

FWD ENTRY DOOR; LOWER EMER. EXIT LIGHT LENS MISSING DIRECTIONAL ARROW / REMOVED AND REPLACED LENS COVER IAW AMM 33-51-01; INSPECTED

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 71,655 hrs · 42,161 cycles

RIGHT OVERWING EMER EXIT LIGHT LOWER LIGHT LENS MISSING DIRECTIONAL ARROW / REMOVED AND REPLACED COVER IAW AMM 33-51-01; INSPECTED

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 70,812 hrs · 41,681 cycles

RH FWD UPPER HORIZONTAL STABILIZER SLIDING SEAL CRACKED / R&R'D RH FWD UPPER HORIZONTAL STABILIZER SLIDING SEAL PER AMM 53-31-31.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 70,812 hrs · 41,681 cycles

LH FWD UPPER HORIZONTAL STABILIZER SLIDING SEAL CRACKED. / R&R LH FWD UPPER HORIZONTAL STABILIZER SLIDING SEAL PER MM REF 53-31-31

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 69,225 hrs · 40,698 cycles

CRACK CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT / REPAIRED CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW B737-700 EA 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (FWD GALLEY) · airframe 69,225 hrs · 40,698 cycles

CRACK SERVICE DOOR SCUFF PLATE AT FWD GALLEY AREA / PERFORMED PERMANENT REPAIR SCUFF PLATE SERVICE DOOR AT FWD GALLEY AREA IAW EA #1-A53-2076 REV.II

Part: ANGLE — CRACKED (RT MLG WW) · airframe 69,225 hrs · 40,698 cycles

CRACK BODY STATION 663.75 ANGLE RBL 6.15 TO RBL 31.83 AT MAIN WHEEL WE LL COMPARTME / REPLACED BODY STATION 663.75 ANGLE RBL 6.15 TO RBL 31.83 AT MAIN WHEEL WELL IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #111A1001 SHEET 153 REV B

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 69,225 hrs · 40,698 cycles

INOP EMERGENCY LIGHT BATTERY PACK M1668 LOCATED EMERGENCY EXIT DOORLH SIDE AT PASSENGER CABIN / REPLACED BATTERY PACK M1668 LOCATED EMERGENCY EXIT DOOR LH SIDE AT PASSENGER CABIN ; AND TEST IS OK IAW B737-700 AMM 33-51-06-960-805.

Part: LENS — BROKEN (CABIN) · airframe 69,225 hrs · 40,698 cycles

BROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA / REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA IAW AMM 33-51-01-960-802 OPERATIONAL TEST IS OK

Part: SKIN — BROKEN (BS 1016) · airframe 69,225 hrs · 40,698 cycles

BROKEN DRAIN EXTERNAL SKIN LOCATED BS 1016 LOWER FUSELAGE EXTERIOR ( 3 EA) / REPLACED DRAIN EXTERNAL SKIN LOCATED BS1016 LOWER FUSELAGE EXTERIOR (3EA) IAW B737-700 SRM 51-40-02 AND DWG: 148A3322 REV:-

Part: STRUCTURE — DENTED (COCKPIT) · airframe 69,225 hrs · 40,698 cycles

DENTS ON FLOOR STRUCTURE BETWEEN BS 251.6 TO BS 259.5 FROM LBL 5 TO LBL 15 AT COCKPIT / REPAIRED FLOOR STRUCTURE BETWEEN BS 251.6 TO BS 259.5 FROM LBL 5 TO LBL 15 AT COCKPIT I.A.W EA #1 A53-33179 REV IR

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CRACK SUPPORT ANGLE BS 320 AT LEVEL STR20L AT EQUIPMENT ELECTRONIC COMP (1 EA) / REPLACED SUPPORT ANGLE LOC ON BS320 AT LEVEL STR20L AT EQUIPMENT ELECTRONIC COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DRAWING 141A8140 REV:-

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

HOLE FRAME ON BS 1016 DIAMETER OF HOLE 8R AT STRG 3R IS OUT OF TOLERANCES REQUIRED IN SI CARD Ï¿½ 12107 -53 STEP 24.F AT BS 1016 PRESSURE BULKHEAD AT AFT GALLEY AREA / PERFORMED REPAIR ON HOLE 8R AT STR 3R IAW SI 12107-53 STEP 25 ITEM C TO ITEM D PAGE 50 TO PAGE 51

Part: BRACKET — RUSTED (R1 DOOR) · airframe 69,225 hrs · 40,698 cycles

RUST ON HARDWARE AND PLATE ASSY ADAPTER FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKE AT AT FWD GALLEY AREA / REPLACED HARDWARE AND PLATE ASSY ADAPTER FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKET AT FWD GALLEY AREA AND PERFORMED A GENERAL VISUAL INSPECTION AND NOT FOUND CORROSION IAW B737-700 AMM 25-66-02-400-801 STEP 3D(1)(A) AND 30(1)(B)

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

DIAMETER OF HOLE 9L AT STRG 3L IS OUT TOLERANCES REQUIRED IN SI CARD #12107-53 STEP 29D AT BS 1016 PRESSURE BULKHEAD / PERFORMED REPAIR ON HOLE 9L AT STR 3L IAW SI 12107-53 STEP 3L ITEM A TO ITEM B PAGE 60 TO PAGE 61

Part: BRACKET — RUSTED (R2 DOOR) · airframe 69,225 hrs · 40,698 cycles

RUST HARDWARE AND PLATE ASSY ADAPTER FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKET AT AFT GALLEY AND LAV / REPLACED HARDWARE AND PLATE ASSY ADAPTER FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKET AT AFT GALLEY AND LAV IAW BOEING 737-700 AMM 25-66- 02-400-801 STEP 3.D(1)(A)(B) AND PERFORMED VISUAL INSPECTION AND NO FOUND CORROSION ON MAIFING PARTS

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

HOLE FRAME ON BS 1016 DIAMETER OF HOLE 7R AT STRG 3R IS OUT OF TOLERANCES REQUIRED IN SI CARD Ï¿½ 12107- 53 STEP 24.D AT BS 1016 PRESSURE BULKHEAD AT AFT GALLEY AREA / PERFORMED REPAIR ON HOLE 7R AT STR 3R IAW SI 12107-53 STEP 25; ITEM A TO ITEM B PAGE 50

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

DIAMETER OF HOLE 9R AT STRG 3R IS OUT OF TOLERANCES REQUIRED IN SI CARD #12107-53 STEP 36D AT BS 1016 PRESSURE BULKHEAD / PERFORMED REPAIR ON HOLE 9R AT STR 3R IAW SI 12107-53 STEP 38 ITEM A TO ITEM B PAGE 69

Part: BRACKET — RUSTED (L2 DOOR) · airframe 69,225 hrs · 40,698 cycles

RUST HARDWARE AND PLATE ASSY ADAPTER FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKET AT AFT GALLEY AND LAV / REPLACED HARDWARE AND PLATE ASSY ADAPTER FLOOR DOOR MOUNTED EVACUATION SLIDE BRACKET AT AFT GALLEY AND LAV IAW BOEING 737-700 AMM 25-66- 02-400-801 STEP 3.D(1)(A)(B) AND PERFORMED VISUAL INSPECTION AND NO FOUND CORROSION ON MAIFING PARTS

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

DIAMETER OF HOLE 6R AT STRG 2R IS OUT OF TOLERANCES REQUIRED IN SI CARD #12107-53 STEP 11F AT BS 1016 PRESSURE BULKHEAD / PERFORMED REPAIRED ON HOLE 6R AT STR 2R IAW SI 12107-53 STEP 13 ITEM A TO ITEM B PAGE 25 TO PAGE 26

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CORROSION WEB - INTERCOSTAL BTW BS747 TO BS767 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT / REPLACED WEB-INTERCOSTAL BTW BS 747 TO BS 767 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02; 51-10-02 ITEM 9 AND DRAWING 146A7502 REV.A

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

DIAMETER OF HOLE FRAME ON BS 1016 DIAMETER OF HOLE 7L AT STRG 3L IS OUT OF TOLERAN CES REQUIRED IN SI CARD #12107-53 STEP 19.D AT BS 1016 PRESSURE BULKHE AD. / PERFORMED REPAIR ON HOLE 7L AT STR 3L IAW SI 12107-53 STEP 20 ITEM A TO ITEM B PAGE 39

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

DIAMETER OF HOLE FRAME ON BS 1016 DIAMETER OF HOLE 8L AT STR 3L IS OUT OF TOLERAN CES REQUIRED IN SI CARD #12107-53 STEP 19.F AT BS 1016 PRESSURE BULKHE AD. / PERFORMED REPAIR ON HOLE 8L AT STR 3L IAW SI 12107-53 STEP 20 ITEM C TO ITEM D PAGE 39 AND PAG 40

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

DIAMETER OF HOLE 5R AT STRG 2R IS OUT OF TOLERANCES REQUIRED IN SI CARD #12107-53 STEP 11.D AT BS 1016 PRESURE BULKHEAD / PERFORMED REPAIR ON HOLE SR AT STR 2R IAW SI 12107-53 STEP 13 ITEM A TO ITEM B PAGE 25

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

DIAMETER OF HOLE 6L AT STRG 2L IS OUT OF TOLERANCES REQUIRED IN SI CARD Ï¿½12107-53 STEP 3.F AT BS 1016 PRESSURE BULKHEAD / PERFORMED REPAIR ON HOLE 6L AT STR 2L IAW SI 12107-53 STEP 5 ITEM C TO ITEM D PAGE 11 TO PAGE 12

Part: HANDLE — DETERIORATED (ENTRY DOOR) · airframe 69,225 hrs · 40,698 cycles

DETERIORATED ENTRY DOOR LINING PANEL ASSIST HANDLE AT FWD GALLEY AREA (1 EA) / REPLACED ENTRY DOOR LINING PANEL ASSIST HANDLE AT FWD GALLEY AREA (1EA) IAW B737-700 AMM 52-11-31-400- 802 STEP 3G(2)

Part: SEAT TRACK — WORN (COCKPIT) · airframe 69,225 hrs · 40,698 cycles

WEAR ON CAPTAIN SEAT AND F/O SEAT TRACKS AT COCKPIT / REMOVED AND REPLACED CAPTAIN AND F/O SEAT TRACKS (8EA) AT COCKPIT IAW AMM 25-11-01-000-801 AND AMM 25-11-400-801.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

DIAMETER OF HOLE 5L AT STRG 2L IS OUT OF TOLERANCES REQUIRED IN SI CARD Ï¿½12107-53 STEP 3.D AT BS 1016 PRESSURE BULKHEAD / PERFORMED REPAIR ON HOLE 5L AT STR 2L IAW SI 12107-53 STEP 5 ; ITEM A TO ITEM B PAGE 11.

Part: STRAP — CORRODED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CORROSION STRAP LOCATED BETWEEN BS 727D TO BS 727E STR 25L / STR 25R WL 155.5 AT AFT CARGO COMPARTMENT / REPLACED STRAP LOCATED BETWEEN BS 727D TO BS 727E STR 25L / STR 25R WL 155.5 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02 AND DWG 146A7500 REV E

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 STR 25L AND WL155.5 AT AFT CARGO COMPARTMENT / REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 STR 25L AND WL 155.5 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02 ; SRM B737-700 51-10-02 PARAGRAPH 9 AND DRAWING 146A7500 REV -

Part: STRAP — CORRODED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CORROSION STRAP LOCATED BETWEEN BS 767 TO BS 787 STR25 L / STR 25R WL 155.5 AT AFT CARGO COMPARTMENT / REPLACED STRAP LOCATED BETWEEN BS 767 TO BS 787 STR25 L / STR 25R WL 155.5 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02 AND DWG 146A7500 REV B

Part: WEDGE — DENTED (TE FLAP) · airframe 69,225 hrs · 40,698 cycles

DENT IB MAIN FLAP WEDGE PANEL LOWER SURFACE (REFER TO DEFECT C976750) AT LT WING / REPAIRED IN MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT ASPER B737-700 SRM 51-70-10-2R-4 TOOL USED CALIPER P/N 700-113-10 S/N 0023216 DUE DATE 25-JUN-20 DENT GAUGE P/N P6KIT PREMIUM S/N 410042 DUE DATE 26-NOV-20 SCALE P/N CL5000 S/N AE-39882 DUE DATE 14-JUN-20;HOT BONDER P/N HCS980013 S/N 15102320 DUE DATE 14-JUN-20 ; COATING THICKNESS P/N PROSITEC TOM 6000N53 S/N 767584 DUE DATE 16-JUL-20

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 STR 25R AND WL155.5 AT AFT CARGO COMPARTMENT / REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 STR 25R AND WL 155.5 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG 146A7502 REV A; AND DWG 146A7500 REV.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CRACK SUPPORT ANGLE BS 328 AT LEVEL STR 20L AT EQUIPMENT ELECTRONIC COMP (1 EA) / REPLACED SUPPORT ANGLE LOC ON BS 328 AT LVEL STR20L AT EQUIPMENT ELECTRONIC COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DRAWING 141A8140 REV:

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CRACK ON FRAME LOCATED BS440 BETWEEN STR8R TO STR9R AT FWD GALLEY AREA / PERFORMED REPAIR ON FRAME LOCATED BS 440 BETWEEN STR 8R TO STR 9R FWD GALLEY AREA I.A.W EA 1-A53-12114 REV 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CRACK FRAME BS 827 BETWEEN STR 8L AND 9L AT PASSENGER CABIN / PERFORMED REPAIR ON FRAME BS827 BETWEEN STR 8L AND 5-9L AT PASSENGER CABIN I.A.W EA NO.1-A53-12114 REV 4.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CRACK INNER CHORD LOCATED BS 303.9 AT LEVEL STRINGER 17L AT FWD GALLEY AREA / REPLACED INNER CHORD LOCATED BS 277 TO BS 360 STR 17L AT FWD GALLEY AREA IAW SRM B737-700 51-40-02; SRM B737-700 51-10-02 PARAGRAPH 9 AND DRAWING #141A8110 REV -

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 69,225 hrs · 40,698 cycles

CRACK FLOOR PANEL 211AF AT COCKPIT (1 EA) / REPLACED FLOOR PANEL 211AF AT COCKPIT (1EA) IAW SRM B737-700 51-10-02 ITEM 9

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CRACK FRAME BS 727D BETWEEN S-8L AND S- 9L AT PASSENGER CABIN / PERFORMED REPAIR ON FRAME BS 7270 BETWEEN 5-8L AND 5-9L AT PASSENGER CABIN I.A.W EA NO.1-A53-12114 REV 4.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CORROSION BRACKET BETWEEN BS 500 TO BS 500A AND STR 28L TO STR 28R AT FWD CARGO COMPARTMENT (1 EA) / REPLACED BRACKET BETWEEN BS500 TO BS500A AND STR28L TO STR28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 DRAWING #143A3230 REV 'A'

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CRACK FRAME BS827 BETWEEN S-8R AND S-9R AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME BS 827 BETWEEN STR 8R AND STR 9R AT PASSENGER CABIN IAW B737-700 SRM 53-00-07-2R-1 REPAIR 1 FIGURE 201 SHEET 1; NO FURTHER ACTION OF INSPECTION REQUIRED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CRACK FRAME BS 867 BETWEEN S-8L AND S-9L AT PASSENGER CABIN / PERFORMED REPAIR ON FRAME BS 867 BETWEEN 5-8L AND 5-9L AT PASSENGER CABIN I.A.W EA NO.1-A53-12114 REV 4.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CRACK ANGLE - SUPPORT LOCATED BS 807 AND STRINGER 25R AT AFT CARGO COMPARTMENT / REPLACED ANGLE - SUPPORT LOC. BS807 AND STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DRAWING #146A8120 REV B.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,225 hrs · 40,698 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER / INSTALLED REPAIR ON INSPAR RIB LOCATED STAB. STA 120.30 AT 36 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 55-10-09-2R-5 REPAIR 5 FIGURE 204 (SHEET 1)

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 69,225 hrs · 40,698 cycles

CRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH AT PASSENGER CABIN (5 EA) / REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LH AT PASSENGER CABIN (5EA) IAW B737-700 AMM 33-51-15-400-802 AND DWG 33500007 REV 2

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 69,225 hrs · 40,698 cycles

CRACK TIE CLIP LOCATED AT BS277 AT LEVEL STR10R CENTER SECTION. REPLACED TIE CLIP LOCATED AT BS2277 AT LEVEL STR10 CENTER SECTION IAW B737700 SRM 514002 AND DRAWING 141A1110 REV.H

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 69,225 hrs · 40,698 cycles

CRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RH AT PASSENGER CABIN (5 EA) / REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY RH A LIGHTING RH AT PASSENGER CABIN (5EA) IAW B737-700 AM 33-51-15-400-802 AND DWG 33500007 REV 2

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,225 hrs · 40,698 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER / REPAIRED INSPAR RIB LOC. STAB STA 120.30 AT 19 INCHES FROM FRONT SPAR AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CRACK FRAME ON BS 360 AT LEVEL STR8R AT FWD GALLEY AREA / PERFORMED PERMANENT REPAIR ON FRAME BS 360 AT LEVEL STR 8R AT FWD GALLEY AREA IAW B737-700 SRM 53-00-07- 2R-1 REPAIR 1 FIGURE 201 SHEET 2; NO FURTHER ACTION OF INSPECTION REQUIRED.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,225 hrs · 40,698 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER / REPAIRED INSPAR RIB LOC. STAB. STA 120.30 AT 28INCHES FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4

Part: SCUFF PLATE — CRACKED (FWD GALLEY) · airframe 69,225 hrs · 40,698 cycles

CRACK CENTER SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA / REPLACED CENTR SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 SRM 51-16-02 ITEM 9

Part: SEAL PLATE — CANNING (HORIZONTAL STAB) · airframe 69,225 hrs · 40,698 cycles

CRACK SEAL - PLATE ACCESS PANEL 343AT AT RT HORIZONTAL STAB / REPLACED SEAL PLATE LOC ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW SRM B737-700 51-40-02 AND 51-10-02 ITEM 9

Part: CLAMP — BROKEN (CABIN) · airframe 69,225 hrs · 40,698 cycles

BROKEN FLOOR STRUCTURE CLAMP BETWEEN BS 616 TO BS 663 AND LBL 24.82 AND RBL 24.82 AT PASSENGER CABIN (3 EA) / REPLACED CLAMP BETWEEN BS616 TO BS663 AND LBL 24.82 AND RBL AT PASSENGER CABIN (3EA) IAW SWPM 20-10-11 U001

Part: SEAL PLATE — CRACKED (HORIZONTAL STAB) · airframe 69,225 hrs · 40,698 cycles

CRACK SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB (2 EA) / REPLACED SEAL PLATE (2EA) LOC ON ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW SRM B737-700 51-40-02 AND 51-10-02 ITEM 9

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CRACK GUSSET BS 500D AND STR 19R FWD CARGO COMPARTMENT (1 EA) / REPLACED GUSSET LOCATED BS 500D AND STR19R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 PARAGRAPH 9 SRM 51-40-02 AND DRAWING 143A7902 REV:E

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CRACK GUSSET AT BS 500D AND STR 19L FWD CARGO COMPARTMENT (1 EA) / REPLACED GUSSET LOCATED BS 500D AND STR 19L FWD CRGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING NÏ¿½143A7902 SHEET 21; REV:E.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,225 hrs · 40,698 cycles

CRACK ANGLE LOCATED BS 400 AND STR 26L FWD CARGO COMPARTMENT (1 EA) . / REPLACED ANGLE LOCATED BS 400 AND STR 26L FWD CARGO COMPARTMENT (1E/A) I.A.W. B737-700 SRM 51-10-02 ITEM 9

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 69,225 hrs · 40,698 cycles

CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT (1 EA) / REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW EA # 1-A53-2076 REV 11

Part: SCUFF PLATE — ELONGATED (FWD CARGO) · airframe 69,225 hrs · 40,698 cycles

ELONGATED HOLE AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT (1 EA) / REPLACED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT (1E/A) IAW SRM B737-700 51-10-02 ITEM 9

Part: SKIN — CRACKED (LE SLAT) · airframe 69,225 hrs · 40,698 cycles

CRACK LOWER SURFACE SLAT 1 ON SKIN LOCATED SLAT STATION 451.97 LT WING / REPAIRED LOWER SURFACE SLAT NO.1 SKIN LOCATED STA 451.97 LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 69,225 hrs · 40,698 cycles

CRACK VAPOR VARRIER BS 663 AT LBL 10 AT MAIN WHEEL WELL COMPARTME / REPAIRED CAPOR VARRIER BS663 AT LBL 10 AT MAIN WHEEL WELL COMPARTMENT . ASPER B737-700 SRM 51-70-04-2R-10 REPAIR 10 TOOL USED: CALIPER P/N 700-113-10 S/N 0033178 DUE DATE: 05-MAY-20 HOT BONDER P/N HCS9200 S/N 15102320 DUE DATE 14-JUN-20 DUE DATE 14-JUN-20; SCALE P/N CL5000 S/N AE-39882 DUE DATE 05-NOV-20

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 69,225 hrs · 40,698 cycles

CRACK VAPOR VARRIER BS 663 AT RBL 10 AT MAIN WHEEL WELL COMPARTME / REPAIRED VAPOR VARRIER BS663 AT RBL 10 AT MAIN WHEEL WELL COMPARTMENT ASPER B737-700 SRM 51-70-04-2R-10 REPAIR 10 TOOL USED. CALIPER P/N 500-197-30 S/N A18135096 DUE DATE 06-APR-20.HOT BONDER P/N HCS9200B S/N 16122983 DUE DATE 27-NOV-20; SCALE P/N CL5000 S/N AE-39882 DUE DATE 05-NOV-20.

Part: SKIN — CRACKED (LT NR 3 SLAT) · airframe 69,225 hrs · 40,698 cycles

CRACK LOWER SURFACE SLAT 3 ON SKIN LOCATED SLAT STATION 202.45 LT WING / REPLACED SLAT 3 LT WING AND STEPS ARE DOCUMENTED ON NRC # L164736

Part: STIFFENER — DAMAGED (BS 907) · airframe 69,225 hrs · 40,698 cycles

ELONGATED HOLE WASTE TANK INTERNAL STRUCTURE VERTICAL STIFFENER BS907 AT AFT CARGO COMPARTMENT (1 EA) / REPLACED WASTE TANK INTERNAL STRUCTURE VERTICAL STIFFENER BS907 AT AFT CARGO COMPARTMENT (1E/A) STANCHION ASSY IAW B737-700 SRM 51-10-02 ITEM 9

Part: STRAP — UNSECURE (L1 DOOR) · airframe 68,658 hrs · 40,325 cycles

L1 DOOR EMERGENCY SLIDE MAY NEED ADJUSTMENT. / SECURED VELCRO COVER STRAP PER AMM.

Part: RETAINING CLIP — LOOSE (L2 DOOR) · airframe 68,076 hrs · 39,946 cycles

AFT ENTRY GIRT BAR BRACKET LOOSE. / TIGHTEN AFT CLIP IAW SIP.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,802 hrs · 39,780 cycles

LEFT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG OUTER FACE CORRODED. REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,802 hrs · 39,780 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTER FACE CORRODED. / REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,802 hrs · 39,780 cycles

L/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG OUTER FACT CORRODED. / REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,802 hrs · 39,780 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER OUTBOARD LUG OUTER FACE CORRODED. REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,802 hrs · 39,780 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTER FACE CORRODED. REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,802 hrs · 39,780 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD LUG OUTER FACE CORRODED. / REPAIRED LUG PER EA.

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,802 hrs · 39,780 cycles

R/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG OUTER FACE CORRODED. REPAIRED LUG PER EA.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 67,335 hrs · 39,471 cycles

AFT CARGO COMPARTMENT FLOOR PANEL (140BF) 6.75 IN LONG CRACK. / CLOSING DMA PAGE: 0131071 R/R (140BF) FLOOR PANEL PER AMM 25-52-10 CL #83699

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 67,066 hrs · 39,289 cycles

FORWARD ENTRY RT AISLE PHOTOLUMINESCENT LIGHT STRIP LOOSE. SECURED PHOTOLUMINESCENT STRIP PER CMM.

Part: HANDLE — UNSECURE (DOOR SLIDE) · airframe 66,200 hrs · 38,743 cycles

AFT GALLEY SERVICE DOOR ESCAPE SLIDE PULL HANDLE HANGING DOWN RESECURED PULL HANDLE IAW AMM 25-66-01. A/C OK FOR SERVICE.

Part: BATTERY — FAILED (CABIN) · airframe 65,934 hrs · 38,580 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 65,934 hrs · 38,580 cycles

LT WING OUTBOARD TRAILING EDGE FLAP INBOARD LOWER CORNER DELAMINATED. R&R FLAP ASSEMBLY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 65,934 hrs · 38,580 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 65,934 hrs · 38,580 cycles

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

Part: RETAINER — CRACKED (LEFT WING) · airframe 65,934 hrs · 38,580 cycles

LEFT WING#1 PYLON TRAILING EDGE SMALL BLUB SEAL RETAINER UNDER FIXED TRAILING EDGE PANEL CRACKED ON UPPER FASTENER. / REMOVED AND REPLACED SEAL RETAINER IAW SRM 51-40-02

Part: COVER — MISSING (EXIT SIGN) · airframe 65,211 hrs · 38,131 cycles

RT SIDE EMERGENCY EXIT SIGN PLASTIC COVER OVER MISSING. INSTALLED COVER PER SIP.

Part: CONTROL LEVER — LACK OF LUBE (COCKPIT) · airframe 65,154 hrs · 38,094 cycles

DURING GEAR EXTENSION ALL GREEN AND RED LANDING GEAR INDICATING LIGHT ILLUMINATED. CONDITION CLEANED AFTER CYCLING. C/W LD4 GEAR LEVER CLEAN AND LUBE PER FIM TASK. OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,109 hrs · 38,060 cycles

RT AFT OVERWING EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 63,963 hrs · 37,334 cycles

L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: COVER — BROKEN (CABIN) · airframe 63,934 hrs · 37,315 cycles

AFT FLIGHT ATTENDANT PANEL EMERGENCY LIGHT SWITCH COVER SPRING BROKEN. R&R COVER IAW CMM.

Part: STIFFENER — CRACKED (LT WHEEL WELL) · airframe 63,934 hrs · 37,315 cycles

L/H W/W; STA 663 LBL 26 STIFFNER CRACKED O/B OF RAM AIR EXHAUST DUCT / REMOVED AND REPLACED PER SRM 51-40-02

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,631 hrs · 37,119 cycles

RT AFT WING SLIDE EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,631 hrs · 37,119 cycles

LT EMERGENCY LIGHT INOP AT ROW 14. RELAMPED LIGHT PER AMM.

Part: PROXIMITY SENSOR — FAULTY (LE SLAT) · airframe 63,349 hrs · 36,940 cycles

DIVERSION, LEADING EDGE TRANSIT LIGHT ILLUMINATED & REMAINED ILLUMINATED AT FLAPS IS. R&R NR 8 SLAT INBOARD PROXIMITY SENSOR IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,161 hrs · 36,818 cycles

EMERGENCY LIGHT INOP AT M1669. R&R BATTERY PER AMM.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 63,161 hrs · 36,818 cycles

FWD CARGO BAY BS 500C AFT SIDE OF FRAME LBL 21 WL 156 BAFFLE CLIP IS CRACKED / REMOVED AND REPLACED FWD CARGO BAY B.S 500C AFT SIDE OF FRAM LBL21 WL156 CLIP ASSY HFAB53-CL-101/NEW P.O 686487-SWA PER SRM 51-40-02-0G-0 SRM 51-40-05 AND DWG 143A7502

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 63,161 hrs · 36,818 cycles

FWD CARGO BAY BS 500C FWD SIDE OF FRAME LBL 21 WL 156 BAFFLE CLIP IS CRACKED / REMOVED AND REPLACED FWD CARGO BAY CLIP ASSY B.S 500C FWD SIDE OF FRAME LBL 21; WL 156. HFAB53.CL.010 P.O. 686522-SWA PER SRM 51-40-02-0G-0 SRM 51-40-05 AND DWG 143A7502

Part: BAFFLE — ELONGATED (FWD CARGO BAY) · airframe 63,161 hrs · 36,818 cycles

FWD CARGO BAY BS 500B-500C LBL 21 WL 156 BAFFLE HAS ELONGATED HOLE / REMOVED AND REPLACED FWD CARGO BAFFLE ASSY B.S. 500B-500C LBL21 WL156 WITH 7075-T6 .020 CLAD LOT# 1293090 PER SRM 51-40-02-0G-0 SRM 51-40-05 AND DWG 143A7510

Part: NONE — ELONGATED (FWD CARGO LH) · airframe 63,161 hrs · 36,818 cycles

FCB; BS 440; LBL 21; AFT BAFFLE CLIP HAS ELONGATED FASTENER HOLE. / REMOVED DAMAGED BAFFLE CLIP BS 440; LBL 21 PER SRM 51-40-02-0G-0. FORMED BAFFLE CLIP; LOCATED; DRILLED AND INSTALLED PER SRM 51-40-02-0G-0 AND PER DWG 143A7505.

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

FORWARD BAFFLE CLIP CRACKED AT BS 460, LBL 21. R&R BAFFLE CLIP PER SRM AND DWG.

Part: STRIP — BROKEN (AFT CARGO COMPT) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO BAY R/H FLOOR CAP STRIP FWD OF DOOR IS BROKEN / REPLACED AFT CARGO BAY RIGHT HAND FLOOR CAP STRIP FWD OF DOOR FOR A NEW CAPSTRIP 453A2611-11 PER SRM 51-10-02-0G-0 SECTION #9 93046U 05MAY18

Part: FITTING — CRACKED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

FORWARD CARGO BAY BAFFLE CLIP CRACKED AT BS 500A, LBL 21. R&R BAFFLE CLIP PER DWG & SRM.

Part: INTERCOSTAL — ELONGATED (AFT CARGO COMPT) · airframe 63,161 hrs · 36,818 cycles

WHILE WORKING; NOTED INTERCOSTAL; BS 857 TO 867; RBL 18; HAS ELONGATED FASTENER HOLES COMMON TO SHIELD. / REMOVED INTERCOSTAL PER SRM 51-40-02-0G-0. RECEIVED NEW INTERCOSTAL FROM O.S.S. PO # 685311-SWA; LOCATED; DRILLED; APPLIED CHEMICAL CONVERSION COATING; PRIMED AND INSTALLED AT BS 857-867 RBL 18 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; SRM 51-20-01-0G-0; DWG # 146A0081. FASTENERS COMMON TO INBD SILL REINFORCEMENT STRAP AND AFT SHIELD BS 847-867 TO BE INSTALLED ON NRC #S T777094; T777196. INTERCOSTAL FORMED FROM 7075-T0 .045' LOT # 891881. DWG 146A8123.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 63,161 hrs · 36,818 cycles

LT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 120.3, 3RD VERTICAL STIFFENER. REPAIRED RIB IAW SRM.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

FORWARD CARGO BAY BAFFLE CRACKED BETWEEN BS 500 TO BS 500A, LBL 21. R&R BAFFLE PER DWG AND SRM.

Part: RAIL — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO BAY SUPPORT RAIL CORRODED AT BS 767+6", LBL 8.1. REPAIRED RAIL IAW SRM AND EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 63,161 hrs · 36,818 cycles

LT HORIZONTAL STABILIZER RIB AT STAB STA 120.30, 2ND VERTICAL STIFFENER CRACKED. REPAIRED RIB PER SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

RT BULKHEAD SUPPORT LOWER ANGLE CORRODED AT BS 947. R&R ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

AFT LOWER CENTER BULK SUPPORT ANGLE CORRODED AT BS 947. REPAIRED ANGLE PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO BAY INTERCOSTAL WEB CORRODED BETWEEN BS 847 TO BS 847+9, RBL 18. R&R INTERCOSTAL PER SRM & DWG.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 63,161 hrs · 36,818 cycles

PANEL 193CR HAS DELAMINATED DENT ON EXTERIOR SURFACE / REPAIRED DELAMINATED DENT ON EXTERIOR SURFACE OF PANEL 193CR IAW SRM 51-70-05-2R-2

Part: STRAP — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO DOOR CUTOUT INBOARD SILL REINFORCEMENT STRAP CORRODED BETWEEN BS 787+6 TO BS 847, RBL 18. R&R STRAP PER SRM AND DWG.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO BAY FLOOR BEAM UPPER FLANGE CORRODED BETWEEN BS 787+6 TO BS 847, RBL 13.84. REPAIRED TIE DOWN PER SRM AND DWG.

Part: BRACKET — CRACKED (BS 867) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO BAY BRACKET CRACKED AT BS 867, LBL 11. R & R THE BRACKET IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 767) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO BAY UPPER FLOOR SUPPORT FLANGE CORRODED BETWEEN BS 767 TO 767+10, RBL 21. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO BAY, ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 807, LBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO BAY FLOORBEAM SPLICE CORRODED BETWEEN BS 767-8 TO BS 767+10, RBL 9. REPAIRED SPLICE IAW EA.

Part: FLOOR SUPPORT — CORRODED (BS 787-847) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO BAY UPPER FLOOR SUPPORT FLANGE CORRODED BETWEEN BS 787+6 TO 847, RBL 18. R & R THE FLOOR SUPPORT SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 767+5, RBL 22. R&R SUPPORT ASSEMBLY PER SRM & DWG.

Part: FRAME — CORRODED (AFT CARGO BAY) · airframe 63,161 hrs · 36,818 cycles

***CORROSION*** ACB; STA 787; ON UPPER FLANGE OF FRAME BELOW FLOOR SUPPORT; RBL4; APPROX.. WL 154. / REMOVED CORROSION ON STA 787 FRAME 1' X .4' ALONG EDGE OF INNER CHORD. ORIGINAL THICKNESS OF .063 WITH .059 MATERIAL REMAING AS PER SRM 53-00-07-1A-1. REPAIRED FRAME ON UPPER FLANGE STA 787 RBL 4 APPROX WL 154 AS PER ER 18-02560 REV IR & EA 1-753-32700 REV IR

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 941, RBL 22. R&R SUPPORT PER SRM AND DWG.

Part: WEB — CORRODED (BS 767) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO BAY WEB CORRODED BETWEEN BS 767 TO 767+5", RBL 7.5. R & R THE WEB IAW DWG AND SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO DOOR CUTOUT, THRESHOLD SILL WEB CORRODED BETWEEN BS 787+6 TO BS 847, BETWEEN RBL 19 TO RBL 27. R&R WEB PER SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 767+6, LBL 12. REPAIRED FLOOR BEAM IAW SRM, ER, AND EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

FORWARD CARGO BAY ON THRESHOLD SUB WEB CORRODED. R&R WEB PER SRM.

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,161 hrs · 36,818 cycles

FCB FLOOR TO SIDEWALL TRIM STRIP #3 L/H HAS CORROSION / NO ALLOWABLE DAMAGE FOUND IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARAGRAPH 9.A. 92954U 4/26/18. PART 453 A1611-10 WILL BE INSTALLED ON CARD: J PANEL-121-CLOSE 92954U 4/26/18

Part: NONE — CORRODED (MAIN CABIN) · airframe 63,161 hrs · 36,818 cycles

CORROSION ON ASD MOPSILL BS 917-986 NUMEROUS AREAS RBL52 / REMOVED CORRODED AFT SERVICE DOOR MOPSILL BS 917-1006 RBL52. INSTALLED NEW MOPSILL IAW SRM 51-40-02 AND DWG 147A8501

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

FORWARD CARGO BAY ON AFT BULKHEAD CENTER PANEL LOWER SUPPORT ANGLE CORRODED AT UPPER SURFACE. R&R ANGLE PER SRM AND DWG.

Part: SERVICE DOOR — CORRODED (LWR FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

CORROSION ON LAV SERVICE DOOR INTERIOR AND EXTERIOR SIDE / CORROSION ON LAV SERVICE DOOR SKIN FOUND TO BE OUT OF LIMITS; CAN'T MAINTAIN 20X MINIMUM DAMAGE FROM HOLES PER SRM 52-40-01-1A-4. 4.B (1). REMOVED AND INSTALLED NEW DOOR ASSEMBLY PER AIPC 52-49-07-01; AMM 52-49-07-000-801; AND AMM 52-49-07-400-801. 57546U 03MAY18

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

L2 DOOR MOPSILL CORRODED BETWEEN BS 945 TO BS 980, LBL 52. INSTALLED MOPSILL IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A+4 TO BS 500C, LBL 20. R&R SUPPORT PER SRM & DWG.

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,161 hrs · 36,818 cycles

FCB FLOOR TO SIDEWALL TRIM STRIP #2 L/H HAS CORROSION / NO ALLOWABLE DAMAGE FOUND IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0 PG. 9.A. NEW PART WILL BE INSTALLED ON CARD NO: J PANEL-121-CLOSE 92854U 4/26/18

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 63,161 hrs · 36,818 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS. 664, LBL 32. R&R DECK IAW ER AND EA.

Part: SUPPORT — CORRODED (BS 500C) · airframe 63,161 hrs · 36,818 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED AT BS. 500C+17, RBL 20. R & R THE SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 494-500A) · airframe 63,161 hrs · 36,818 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 494 TO 500A, RBL 20. R & R THE SUPPORT IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

UPPER CHORD CORRODED AT BS 986, BETWEEN RBL 20 TO RBL 47. REPAIRED BEAM PER EA.

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 63,161 hrs · 36,818 cycles

***CORROSION*** IN FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT B.S. 400-420; RBL 20. / REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT IN FWD CARGO BAY BS 400-420; RBL 20 PER SRM 51-40-02; DWG 143A2505

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

LT SIDE OUTBOARD OF KEEL BEAM ANGLE CRACKED AT BS 663. REPAIRED ANGLE PER ER & EA.

Part: RETAINER SEAL — CRACKED (RT WING) · airframe 63,161 hrs · 36,818 cycles

RT WING UPPER AFT T/E PANEL JUST AFT OF #2 PYLON HORIZ. SEAL RETAINER IS CRACKED. / REMOVED AND REPLACED SEAL RETAINER ON R/H WING UPPER AFT T/E PANEL JUST AFT OF #2 PYLON HORIZONTAL PER SRM 51-40-02 STEP 4 AND SOPM 205001. 55875U 04/23/2018

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

INTERCOSTAL CORRODED BETWEEN BS 294 TO BS 312, LBL 208. R&R INTERCOSTAL IAW SRM AND DWG.

Part: RETAINER SEAL — CRACKED (LT WING) · airframe 63,161 hrs · 36,818 cycles

LT WING UPPER T/E PANEL JUST AFT OF #1 PYLON VERT. SEAL RETAINER IS CRACKED. / REMOVED AND REPLACED LT WING UPPER T/E PANEL JUST AFT OF #1 PYLON VERT. SEAL RETAINER PER SRM 51-40-02-0G-0; AND IPC 57-50-00-25A AND SOPM 20-50-01.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 63,161 hrs · 36,818 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, LBL 13. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 63,161 hrs · 36,818 cycles

FCB; FWD. CORNER SCUFF PLATE CRACKED. / ACCOMPLISHED REPAIR TO FWD CARGO BAY FWD CORNER SCUFF PLATE PER EA 1-A53-2076 REV 11.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 63,161 hrs · 36,818 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 328 TO 344, LBL 45. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: BEAM — CORRODED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

BEAM UPPER CHORD CORRODED AT BS 312, LBL 13. REPAIRED CHORD IAW ER AND EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

SUPPORT CRACKED BETWEEN BS 294 TO BS 312, LBL 25. REPAIRED INTERCOSTAL PER ER & EA.

Part: ANGLE — CRACKED (LT WING) · airframe 63,161 hrs · 36,818 cycles

LEFT WING UPPER TRAILING EDGE PANEL JUST AFT OF THE NR 1 PYLON OUTBOARD ANGLE FOR TRANSVERSE WEB CRACKED. R & R THE ANGLE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 63,161 hrs · 36,818 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294, BL 0. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 63,161 hrs · 36,818 cycles

FLOORBEAM UPPER TEE FOUND CORRODED AT BS 328, BETWEEN RBL 35 TO RBL 50. R & R THE FLOORBEAM TEE IAW EA.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 63,161 hrs · 36,818 cycles

RT FORWARD SIDE OUTBOARD OF KEELBEAM ANGLE CRACKED AT BS 663. REPAIRED ANGLE IAW ER AND EA.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 63,161 hrs · 36,818 cycles

RIGHT WING NR 6 SLAT, NOSE SKIN CRACKED ON LOWER SURFACE AT ACTUATOR RIB. REPAIRED THE SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,714 hrs · 36,538 cycles

RT EMERGENCY EXIT DOOR SIDEWALL ILLUMINATION LIGHT INOP AT ROW 12. RELAMPED LIGHT PER AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 62,462 hrs · 36,375 cycles

L1 DOOR ESCAPE SLIDE GIRT BAR FLAP OUT OF ADJUST. READJUSTED SLIDE ASSEMBLY IAW MT.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 62,149 hrs · 36,188 cycles

R2 DOOR EXIT LIGHT LENS MISSING. INSTALLED THELENS IAW MM.

Part: SKIN — CORRODED (BS 500-500A) · airframe 61,551 hrs · 35,809 cycles

FORWARD CARGO BAY BILGE SKIN CHANNEL CORRODED BETWEEN BS 500 TO 500A, BETWEEN LBL 3 TO RBL 3. R & R THE SKIN CHANNEL IAW SRM.

Part: COVER — LOOSE (LIGHT SWITCH) · airframe 60,793 hrs · 35,346 cycles

AFT GALLEY EMERGENCY EXIT LIGHT SWITCH COVER LOOSE. SECURED THE COVER IAW SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 60,117 hrs · 34,938 cycles

EMERGENCY BATTERY PACK FAILED TIME TEST AT LOCATION M01672. R&R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 60,117 hrs · 34,938 cycles

EMERGENCY BATTERY PACK FAILED TIME TEST AT LOCATION M01669. R&R BATTERY PACK IAW MM.

Part: FRAME — CRACKED (APU DOOR) · airframe 57,298 hrs · 33,271 cycles

APU DOOR FORWARD OUTBOARD LT FRAME CRACKED. R&R DOOR IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,298 hrs · 33,271 cycles

OVERWING ESCAPE HATCH CEILING EXIT LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 57,298 hrs · 33,271 cycles

R1 DOOR EXIT INDICATOR LIGHT INOP. R&R FUSE IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,298 hrs · 33,271 cycles

LT OVERWING HATCH EXIT INDICATOR LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,298 hrs · 33,271 cycles

LT OVERWING ESCAPE LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,298 hrs · 33,271 cycles

L1 DOOR OVERHEAD EXIT SIGN INOP. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,298 hrs · 33,271 cycles

RT EMERGENCY AISLE LIGHT INOP BETWEEN ROW 3 TO ROW 6. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,298 hrs · 33,271 cycles

LT EMERGENCY AISLE LIGHT INOP AT ROW 7. R&R BATTERY PACK IAW AMM.

Part: SKIN — CRACKED (FLAP FAIRING) · airframe 57,298 hrs · 33,271 cycles

RIGHT WING NR 6 AFT FLAP TRACK FAIRING CRACKED ON INSIDE SKIN APPROXIMATELY 47" AFT OF FORWARD EDGE. REPAIRED FAIRING IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 57,298 hrs · 33,271 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN LBL 25 TO LBL 25.5. REPAIRED WEB IAW ER & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,298 hrs · 33,271 cycles

LOWER FRAME CRACKED AT BS 727, WL 200. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,298 hrs · 33,271 cycles

RIGHT LOWER FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED WEB IAW EA.

Part: STRAP — FRAYED (EMERGENCY EXIT) · airframe 57,298 hrs · 33,271 cycles

RIGHT EMERGENCY EXIT HATCH, RED NYLON ASSIST STRAP FRAYED. R & R STRAP IAW SRM.

Part: STRAP — FRAYED (EMERGENCY EXIT) · airframe 57,298 hrs · 33,271 cycles

LEFT EMERGENCY EXIT HATCH, RED NYLON ASSIST STRAP FRAYED. R & R STRAP IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,516 hrs · 32,241 cycles

LEFT EMER BULLNOSE EXIT LIGHT BULB INOPERATIVE AT ROW 14. INSTALLED BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,516 hrs · 32,241 cycles

RIGHT DOOR EMER EXIT LIGHT BULB INOPERATIVE. R & R BULB IAW AMM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 55,516 hrs · 32,241 cycles

LEFT NR 3 WINDOW POST NR 3 HOLE FROM BOTTOM CRACKED. REPAIRED WINDOW POST IAW EA.

Part: FLAP — DELAMINATED (RT WING) · airframe 55,516 hrs · 32,241 cycles

RIGHT WING OTBD AFT FLAP INBD AFT CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,516 hrs · 32,241 cycles

LEFT WING OTBD AFT FLAP, INBD AFT CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 53,440 hrs · 31,039 cycles

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

Part: SLIDE — LOOSE (R2 DOOR) · airframe 52,809 hrs · 30,679 cycles

R2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 52,809 hrs · 30,679 cycles

CENTER CEILING EMER LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,700 hrs · 30,047 cycles

LEFT OVERWING EMER EXIT DOOR LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 51,480 hrs · 29,913 cycles

AFT GALLEY OVERHEAD EMER EXIT SIGN LOOSE. SECURED SIGN ASSEMBLY IAW SIP.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,515 hrs · 29,351 cycles

SEAT TRACK ATTACH FLANGE CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 50,515 hrs · 29,351 cycles

RIGHT MLG WW UPPER PRESS DECK CRACKED AT BS 665, RBL 41. REPAIRED DECK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,515 hrs · 29,351 cycles

SEAT TRACK ATTACH FLANGE CRACKED AT BS 727B, LBL 45.50. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,515 hrs · 29,351 cycles

SEAT TRACK ATTACH FLANGE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 50,515 hrs · 29,351 cycles

LEFT WING INBD TE CAVITY CURVED SEAL RETAINER SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 50,515 hrs · 29,351 cycles

RIGHT MLG WW UPPER PRESS DECK CRACKED AT BS 665, RBL 41. REPAIRED DECK IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,515 hrs · 29,351 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STATION 92.70 CRACKED AT 2ND FROM FWD VERTICAL STIFFENER. REPAIRED RIB IAW SRM.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 50,515 hrs · 29,351 cycles

RIGHT WING INBD TE LOWER SURFACE PANEL SUPPORT FITTING CRACKED. REPAIRED FITTING IAW SRM & DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 50,515 hrs · 29,351 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STATION 92.70 CRACKED AT 3RD FROM FWD VERTICAL STIFFENER. REPAIRED RIB IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 50,515 hrs · 29,351 cycles

RIGHT WING INBD TE CAVITY CURVED SEAL RETAINER ANGLE CRACKED AT FWD SIDE OF UPPER SURFACE PANEL VERTICAL WEB. REPAIRED ANGLE IAW SRM & DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,515 hrs · 29,351 cycles

LEFT HORIZONTAL STABILIZER RIB 129.5 CRACKED 1 INCH ABOVE LOWER FLANGE IN VERTICAL STIFFENER 17.5 INCHES AFT OF FRONT LOWER SPAR CHORD. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,515 hrs · 29,351 cycles

LEFT HORIZONTAL STABILIZER RIB 129.5 CRACKED 1 INCH ABOVE LWR FLANGE IN VERTICAL STIFFENER 34 INCHES AFT OF FRONT LWR SPAR CHORD. REPAIRED RIB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,515 hrs · 29,351 cycles

LOWER FUSELAGE BELLY DRAINS 3 & 4 FROM THE FRONT CRACKED. R & R SKIN IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,515 hrs · 29,351 cycles

RIGHT WING LE NR 8 SLAT LOWER NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,491 hrs · 28,780 cycles

AFT EMERGENCY EXIT BATTERIES FAILED CAPACITY TEST. R & R BATTERY PACKS IAW WDM.

Part: BATTERY — FAILED (CABIN) · airframe 49,491 hrs · 28,780 cycles

MID CABIN EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. R & R BATTERIES IAW MM.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 49,491 hrs · 28,780 cycles

RT WING UPPER FIXED TE PANEL ABOVE DEFLECTION ROLLERS SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: COVER — DAMAGED (CABIN) · airframe 47,279 hrs · 27,491 cycles

RT EEPLS COVER DAMAGED AT ROW 1. R&R EEPLS IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,279 hrs · 27,491 cycles

FWD LT BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK IAW MM.

Part: COVER — OUT OF POSITION (L2 DOOR) · airframe 47,279 hrs · 27,491 cycles

L2 DOOR EMERGENCY EVAC SLIDE COVER OUT OF POSITION. REPOSITIONED COVER IAW M/M.

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,279 hrs · 27,491 cycles

MID-CABIN RT BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,761 hrs · 25,368 cycles

EXTERIOR EMERGENCY LIGHT AFT OF L1 DOOR INOP. RELAMPED LIGHT IAW AMM.

Part: SKIN — DAMAGED (KRUEGER FLAP) · airframe 50,514 hrs · 29,351 cycles

RIGHT WING NR 3 INBD FIXED LE KRUEGER FLAP DAMAGED ON FAIRING FACING PANEL. R & R SKIN IAW SRM & DWG.

Part: SKIN — DAMAGED (KRUEGER FLAP) · airframe 50,514 hrs · 29,351 cycles

RIGHT WING NR 3 INBD FIXED LE KRUEGER FLAP DAMAGED ON FAIRING FACING PANEL. R & R SKIN IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

FRAME CRACKED AT BS 294.5, STR 17R. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

CREASE BEAM ANGLE CRACKED AT BS 294.5, RBL 55. REMOVED AND REPLACED ANGLE IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

SKIN CORRODED AT BS 797, RBL 14. REPAIRED SKIN IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

CREASE BEAM INNER CHORD CORRODED AT BS 311, RBL 55. REMOVED AND REPLACED BEAM IAW SRM, DWG, AND MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

FLOORBEAM IS CORRODED AT BS 328, LBL 33. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

FLOOR SUPPORT BEAM CORRODED AT BS 268.25, BETWEEN LBL 10 TO RBL 12. REMOVED AND REPLACED BEAM IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

FRAME CRACKED AT BS 480, STR 4H. REPAIRED FRAME IAW EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

CREASE BEAM INNER CHORD SUPPORT ANGLE CORRODED BETWEEN BS 314 TO BS 343, LBL 53. REMOVED AND REPLACED SUPPORT IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

FRAME CRACKED AT BS 787, BETWEEN STR 8R AND STR 9R. REPAIRED FRAME IAW EA AND SOPM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

FLOOR BEAM T-CAP CORRODED AT BS 987, LBL 5. REPAIRED T-CAP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

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

Part: WEB — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

WEB IS CRACKED AT BS 520, 28R. REMOVED AND REPLACED WEB IAW SRM & DWG.

Part: WEB — CRACKED (L1 DOOR) · airframe 43,762 hrs · 25,368 cycles

L1 DOOR HORIZONTAL WEB CRACKED AT BS 360, STR 15L. REPAIRED WEB PER EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

WEB CRACKED AT BS 520, RBL 22. REMOVED AND REPLACED WEB IAW DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 43,762 hrs · 25,368 cycles

WEB CRACKED AT BS 520, LBL 2. REMOVED AND REPLACED WEB IAW DWG.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 43,762 hrs · 25,368 cycles

CAPTAINS NR 1 WINDOW FRAME UPPER O/B CORNER CRACKED. REMOVED AND REPLACED FRAME IAW SRM & BOEING DWG.

Part: LENS — BROKEN (CABIN) · airframe 39,862 hrs · 23,105 cycles

FWD EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,697 hrs · 22,950 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,697 hrs · 22,950 cycles

DURING SCHEDULED HC2 CHECK, LT AFT EEPLS FAILED DURATION TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CABLE — LOOSE (L2 DOOR) · airframe 38,594 hrs · 22,383 cycles

L2 DOOR EMERGENCY EVAC SLIDE CABLE LOOSE. SECURED CABLE PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,424 hrs · 22,274 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,424 hrs · 22,274 cycles

DURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: GASPER FAN — FAULTY (AC BAY) · airframe 38,424 hrs · 22,274 cycles

CREW SMELLED HOT PLASTIC/ELECTRICAL ODOR. REMOVED AND REPLACED GASPER FAN PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 37,960 hrs · 21,999 cycles

EEPLS BROKEN AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 36,664 hrs · 21,234 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CABIN EEPLS DELAMINATED. REMOVED AND REMOVED EEPLS PER MM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 36,664 hrs · 21,234 cycles

DURING SCHEDULED 10Y CHECK, FOUND MID CABIN EEPLS DELAMINATED. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 36,664 hrs · 21,234 cycles

DURING SCHEDULED 10Y CHECK, FOUND FWD CABIN EEPLS DELAMINATED. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 36,664 hrs · 21,234 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,664 hrs · 21,234 cycles

DURING SCHEDULED 10Y CHECK, FOUND R2 DOOR UPPER EMERGENCY EXIT LIGHT LAMP INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 36,664 hrs · 21,234 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 36,526 hrs · 21,152 cycles

FWD GALLEY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 36,374 hrs · 21,068 cycles

R1 DOOR EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: ATTACH FITTING — BROKEN (LE SLAT) · airframe 36,217 hrs · 20,968 cycles

DURING SCHEDULED HC2 CHECK, FOUND NR 7 L/E SLAT INBOARD ATTACH LUG BROKEN. REMOVED AND REPLACED SLAT PER MM.

Part: COVER — BROKEN (CABIN) · airframe 35,569 hrs · 20,584 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LAMP ASSY PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,391 hrs · 20,466 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,391 hrs · 20,466 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,636 hrs · 20,014 cycles

DURING SCHEDULED MV3 CHECK, FOUND MLG FWD UPPER BULKHEAD WEB CRACKED AT BS 663.75, RBL 42. REPAIRED WEB PER SWA EA.

Part: BULKHEAD — CRACKED (BS 663) · airframe 34,636 hrs · 20,014 cycles

DURING SCHEDULED MV3 CHECK, FOUND MLG FWD UPPER BULKHEAD WEB CRACKED AT BS 663.75, RBL 42. REPAIRED WEB PER EA.

Part: SLIDE — OUT OF LIMITS (R2 DOOR) · airframe 33,976 hrs · 19,621 cycles

R2 DOOR EMERGENCY EVAC SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: SIGN — DAMAGED (CABIN) · airframe 30,249 hrs · 17,338 cycles

DURING SCHEDULED 8Y CHECK, FOUND G-4 GALLEY EMERGENCY EXIT SIGN DAMAGED. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,249 hrs · 17,338 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, LBL 22 TO RBL 4. REPAIRED FLOORBEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 30,249 hrs · 17,338 cycles

DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CORRODED AT BS 312, STR 17R. REMOVED AND REPLACED CREASE BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,249 hrs · 17,338 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, RBL 4 TO LBL 0. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 30,249 hrs · 17,338 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 344, RBL 2. REPAIRED FLOORBEAM PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,487 hrs · 16,884 cycles

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

Part: SKIN — CRACKED (HORIZ STAB) · airframe 29,487 hrs · 16,884 cycles

DURING SCHEDULED HC1 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 21,881 hrs · 12,560 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,283 hrs · 13,838 cycles

DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 4 DEF. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 23,387 hrs · 13,329 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 6 ABC TO 8 ABC. REMOVED AND REPLACCED PHOTOLUMINESCENT STRIP PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 23,387 hrs · 13,329 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 9 DEF TO 10 DEF. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,909 hrs · 13,072 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,487 hrs · 12,830 cycles

FWD CABIN RIGHT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 21,886 hrs · 12,492 cycles

EEPLS STRIP BROKEN BETWEEN ROW 1 TO ROW 5. REMOVED AND REPLACED STRIP PER MM.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 20,837 hrs · 11,882 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 20,696 hrs · 11,803 cycles

R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED R1 WINDOW AND HEAT CONTROLLER IAW MM.

Part: LIGHT — LOOSE (CABIN) · airframe 20,663 hrs · 11,781 cycles

EEPLS STRIP COVER LOOSE AT ROW 8 ABC. REMOVED AND REPLACED EEPLS STRIP SECTION PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 19,992 hrs · 11,375 cycles

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

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 18,114 hrs · 10,320 cycles

DURING SCHEDULED 5Y CHECK, FOUND RIGHT WING INBOARD AFT T/E FLAP LOWER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.

Part: COFFEEMAKER — FAULTY (AFT GALLEY) · airframe 14,631 hrs · 8,329 cycles

STRONG ELECTRICAL SMELL FROM AFT COFFEEMAKER IN FLIGHT. WHEN CB PULLED SMELL WENT AWAY. REMOVED AND REPLACED BOTH AFT COFFEEMAKERS PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 13,789 hrs · 7,861 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 12,543 hrs · 7,191 cycles

DURING SCHEDULED C3 CHECK, FOUND 4 EA SECTIONS OF PHOTOLUMINESCENT EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM.

Part: GIRT BAR — DAMAGED (SERVICE DOOR) · airframe 11,030 hrs · 6,349 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT BAR WILL NOT STOW PROPERLY. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 10,188 hrs · 5,891 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 5,436 hrs · 3,146 cycles

DURING SCHEDULED PM CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 3,063 hrs · 1,796 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS FLOOR TRACKS CRACKED AT ROWS 1 & 11. REMOVED AND REPLACED TRACK COVERS PER MM.