N450WN

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,738 hrs · 36,638 cycles

EMERGENCY LIGHTS ALL FAIL TEST. SUSPECT LIGHTS WERE LEFT ON BY CLEANERS ON REMOTE PARKING WITH NO GPU. FOUND FWD RH (M1674) AND MID LH (M1668) BATTERIES UNABLE TO CHARGE AND PASS RUN TEST. R & R BATTERY PACKS M1674 AND 1668 PER AMM 33-51-00.

Part: DOUBLER — CRACKED (ZN 100 FUS LOWER) · airframe 61,509 hrs · 36,486 cycles

SUPPLEMENTAL INFORMATION: EGPR DOUBLER LOWER FORWAD FLANGE IS CRACKED AND REQUIRES PERMANENT REPAIR / [01] PAINT STRIP REPAIR AREA I.A.W MM51-21-11-701;[02] REMOVED EXTERNAL POWER RECEPTACLE ACCESS DOOR I.A.W MM 52-49-02-000-801;[03] REMOVED FASTENER TO GAIN ACCESS I.A.W SRM 51-40-02-0G-0;[04] CUTOUT DAMAGED AREA ON EGPR I.A.W SRM 53-10-15-1A-4;[05] HFEC CUTOUT ; OPEN HOLES; AND COUNTERSINKS IAW B737 NDT PART 6; 51-00-00 PROC 23 & PROC 16; 53-30-00 PROC 3. NO DEFECTS NOTED. TOOL#31823; DUE 23DEC22;[06] VERIFIED STEPS 1; 2; 3 & 4;[07] OK TO TREAT; PRIME AND PAINT;[08] INSTALLED FASTENERS REPAIR AREA IAW SRM 51-40-02-0G-0 AND DWG 141A3722-12;[09] VERIFIED ITEM 8<BR>OK TO INSTALL DOOR;[10] INSTALLED EXTERNAL POWER RECEPTACLE ACCESS DOOR IAW AMM 52-49-02-400-801;[11] PAINTED REPAIR AREA IAW AMM 51-21-00-71;[12] REAPIR BEEN C/W ON EA 22-153-03214-WIP1;[13] VERIFIED ITEM ITEMS 10; 11; AND 12<BR>NOTE: TREAT AND PRIME ACCOMPLISHED ON EA 22-153-03214-WIP1;[14] AUDIT CW

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

PANEL 193CR OUTER SKIN HAS A LARGE DISBOND IN CENTER OF PANEL. (MARKED) ; / [01] IDENTIFIED PANEL 193CR IAW SRM 53-40-70-0I-1 FIGURE 2 ITEM 9. <BR><BR>DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-40-1A-1 PARA 4.A.(6)(A).<BR><BR>DAMAGE WILL BE REPAIRED IAW SRM 51-70-05-2R-1 PER SRM 53-40-70-2R-1 PARA 4.B (1) TABLE 201.<BR><BR>REMOVED DELAMINATED SKINS ON OUTER SURFACE OF PANEL AND TAPER SANDED AREA (APPROX 5' X 15') IAW SRM 51-70-05-2R-1 PARA 4.A & 4.B. CORE IS IN GOOD CONDITION.; [02] UPON REMOVAL OF DAMAGE; FOUND DAMAGE TO EXTEND BEYOND ORIGINAL (5' X 15') TO A FINAL SIZE OF APPROX (12' X 18') TRIANGLUALR SHAPED. DISBOND EXTENDED UNDER REPAIR TO OUTER SURFACE (TTG8Q006WTSN). REMOVED COMPLETED REPAIR (TTG8Q006WTSN) TO OUTER SURFACE AND ALL DAMAGE ON OUTER SURFACE IAW SRM 51-70-05-2R-1 PARA 4.A & 4.B. CORE IS STILL IN GOOD CONDITION AS SIZE OF REPAIR HAS ONLY INCREASED. THIS REPAIR WILL NOW INCORPORATE CARD (TTG8Q006WTSN).; [03] UPDATED MEASUREMENTS ON CORRECTIVE ACTION LINE 1.; [04] VALIDATED APPLICABILITY OF REPAIR TO BE COMPLETED IAW SRM 51-70-05-2R-1.; [05] VERIFIED CORRECTIVE ACTION STEPS 1;2;3 AND 4.; [06] FABRICATED REPAIR PLIES USING BMS 8-79CL3ST120 LOT # 1472365-1 & BMS 8-79CL3ST1581 LOT # 1470662-1 IAW SRM 51-70-05-2R-1 PARA 4. C.; [07] INSTALLED REPAIR PLIES

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 58,641 hrs · 34,716 cycles

SUPPLEMENTAL INFORMATION: FWD ENTRY DOOR SLIDE GIRT BAR HARD TO RELEASE FROM FLOOR ATTACHMENTS ; / [01] REMOVED DEBRIS FROM FWD ENTRY DOOR GIRT BAR FLOOR ATTACH POINTS PER SIP AND LUBED LATCHES; [02] FAULT ENTERED IN ERROR TO WRONG A/C.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

PANEL 193CR HAS DELAMINATED FWD UPPER CORNER ; / [01] IDENTIFIED PANEL 193CR IAW SRM 53-40-70-0I-1 FIGURE 2 ITEM [9] AND TABLE 2 ITEM [9]. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-40-1A-1 PARA 4.B.(6).(A-B) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1 PARA 2.F. REMOVED AN APPROX. 1'X.25' AREA OF DELAMINATED BAGSIDE EDGEBAND PLIES LOCATED AT THE FWD UPPER CORNER TAPPER SANDED AREA AND CLEANED AREA IAW SRM 51-70-05-2R-6 PARA 4.A-D; [02] VALIDATED APPLICABILITY OF SRM 51-70-05-2R-6.; [03] VERIFIED CORRECTIVE ACTION 1 AND 2. OKAY TO PROCEED PER SRM 51-70-05-2R-6.; [04] FABRICATED REPAIR PLIES FROM BMS8-79 ST1581 LOT# 1464321-1; BMS5-129 GR05 LOT# 1467643-1 AND BMS8-79 ST120 LOT# 1466500-1; INSTALLED PLIES; VACUUM BAGGED REPAIR PLIES; VERIFIED 5X5 AND SET PLIES TO CURE USING HOTBONDER I/D: NCX000523; S/N: 11051262 IAW SRM 51-70-05-2R-6 PARA 4.E-G.; [05] CURED REPAIR PLIES & UNBAGGED IAW SRM 51-70-05-2R-6 PARA 4. G.; [06] LIGHTLY SANDED REPAIR PLIES IAW SRM 51-70-05-2R-6 PARA 4.I.; [07] VERIFIED CORRECTIVE ACTION STEPS 4;5 AND 6.; [08] TTU INSPECTED REPAIR AREA IN ACCORDANCE WITH 737 NDT MANUAL PART 4 51-00-02. NO DISBONDS NOTED<BR><BR>TOOL I.D. ATS2342 (OLYMPUS EPOCH 650)<BR>S.N.190848504; [09] COMPLETED REFINISH OF REPAIR AREA IAW SRM 51-70-05-2R-6 PARA 4.I.; [10] VERIFIED CORRECTIVE ACTION 9

Part: NONE — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

BS 270 UPPER CHORD LBL-11 TO RBL-11 IS CORRODED. ; / [01] REMOVED CORROSION ON UPPER CHORD B.S 270 LBL 11-RBL 11 WL 207.5;MATERIAL REMOVED 19'L X .900'W.PER SRM 53-10-51-1A-1FIG 104.; [02] VERIFIED CORRECTIVE ACTION STATEMENT 1; [03] UT INSPECTED BLENDED AREAS IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.036' ADJACENT TO 0.050'. <BR>EQUIP ID#: ATS2031 S/N: 170515011; [04] REMAINING THICKNESS IS 0.036';ORIGINAL THICKNESS 0.050' FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1FIG 105. REMOVED BRACKETS (2EA) AT B.S 270 LBL3&RBL3. REMOVED FASTENERS COMMON TO THE REPAIR B.S270 LBL10-RBL10 PER EA#M-21-153-00277.; [05] COMPLETED ALL REPAIR STEPS ON M-21-153-00277 (737-700 SWA LATERAL INTERCOSTAL REPAIR AT BS 270; LBL 10 TO RBL 10) TTG8Q006ZB9G; [06] VERIFIED DISCREPANCY ADDRESSED ON M-21-153-00277 (737-700 SWA LATERAL INTERCOSTAL REPAIR AT BS 270; LBL 10 TO RBL 10) TTG8Q006ZB9G

Part: NONE — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

BS 259 UPPER CHORD LBL-11 TO RBL-11 UPPER SURFACE IS CORRODED. ; / [01] REMOVED CORROSION ON UPPER CHORD B.S 259 LBL 11-RBL 11 WL 207.5;MATERIAL REMOVED 18'L X .800'W.PER SRM 53-10-51-1A-1FIG 103.; [02] VERIFIED CORRECTIVE ACTION STATEMENT 1; [03] UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.087' ADJACENT TO 0.1'. <BR>EQUIP ID#: ATS2031 S/N: 170515011; [04] VERIFIED ORIGINAL THICKNESS OF AFT CHORD BS 259 IS .094 PER DWG 141A7434 PROFILE DWG FOR EXTRUSION BAC1503-100146. AND USING MICROMETER ATS1672.; [05] VERIFIED CORRECTIVE ACTION STATEMENT 4; [06] UPDATED MEASUREMENT TABLE; [07] COMPLETED ALL REPAIR STEPS ON COSTUMER CARD TTG8Q0071SXD 21-153-03187-WIP1 BS 259 AFT FAIL SAFE CHORD BETWEEN LBL 10 AND RBL 10; AND LBL 11 INTERCOSTAL; [08] VERIFIED ALL STEPS OF COSTUMER CARD TTG8Q0071SXD 21-153-03187-WIP1 BS 259 AFT FAIL SAFE CHORD BETWEEN LBL 10 AND RBL 10; AND LBL 11 INTERCOSTAL ARE COMPLETE. AW ENG FINAL TO SIGN OFF.; [09] REPAIRED PER EA 21-153-03187

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION BS 259 - BS 270 VIEWING WINDOW SUPPORT IS CORRODED ON THE UPPER SURFACE. ; / [01] REMOVED CORROSION ON UPPER SURFACE VIEW WINDOW SUPPORT CHANNEL AT B.S 260-270 BL 0; MATERIAL REMOVED 6'L X 3'W PER SRM 53-10-51-1A-1; [02] VERIFIED CORRECTIVE ACTION STATEMENT 1; [03] UT INSPECTED BLENDED AREAS IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.35' ADJACENT TO 0.50'. <BR>EQUIP ID#: ATS2031 S/N: 170515011; [04] REMAINING THICKNESS IS 0.035';ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1 FIG 105. REMOVED VIEW WINDOW SUPPORT CHANNEL AT B.S 260-270 BL 0 WL207.5 PER SRM 51-40-02-0G-0.; [05] LOCATED AND DRILLED NEW WINDOW SUPPORT CHANNEL I.A.W BOEING DWG 141A5210 AND SRM 51-40-05-0G-0 OK TO INSTALL; [06] VERIFIED LOCATE AND DRILL OF THE NEW WINDOW SUPPORT BRACKET PER BOEING DWG 141A5210 AND SRM 51-40-05-0G-0. OK TO INSTALL; [07] INSTALLED NEW WINDOW SUPPORT BRACKET PER BOEING DWG 141A5210;SWA EA M-21-153-00277 REV A; ATTACHED TO COSTUMER CARD TTG8Q006ZB9G; [08] VERIFIED INSTALLATION OF THE VIEW WINDOW SUPPORT PER DWG 141A5210;SWA EA M-21-153-00277 REV A; ATTACHED TO COSTUMER CARD TTG8Q006ZB9G; [09] ADDED INSTALLED PART; [10] WORKSCOPE COMPLETE

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

FLOOR SUPPORT AT BS 259- BS 270 LBL-11 UPPER SURFACE IS CORRODED. ; / [01] REMOVED CORROSION ON FLOOR SUPPORT UPPER SURFACE AT B.S 260-270;MATERIAL REMOVED 7'L X.900'W PER SRM 53-10-51-1A-1 FIG 104; [02] VERIFIED CORRECTIVE ACTION STATEMENT 1; [03] UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.052'<BR>EQUIP ID#: ATS2031 S/N: 170515011; [04] REFER TO FAULT TTG8Q006WFJK WHERE EA 21-153-03187 WAS ADDED AS A SUBTASK; [05] RII STEPS VERIFIED AS REQUIRED; [06] VERIFIED FAULT TO BE ADDRESSED ON TTG8Q006WFJK AND EA 21-153-03187

Part: SEAT TRACK — CORRODED (CABIN) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON SEAT TRACK AT LOCATION BS706+6, RBL 25, WL 208. APPLIED CHEMICAL CONVERSION COATING ON SEAT TRACK AT BS706+6 RBL25 WL 208 IAW SRM 51-20-01-0G-0 UPDATED MEASUREMENT TABLE APPLIED PRIMER ON SEAT TRACK LOCATION BS 706+6 RBL 25 WL 208 PER SRM 51-20-01-0G-0. VERIFIED APPLICATION OF CHEMICAL CONVERSION COATING AND PRIMER ON SEAT TRACK LOCATION BS 706+6 RBL 25 WL 208 PER SRM 51-20-01-0G-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON SEAT TRACK LOCATION BS827 RBL 45 WL 208. APPLIED CHEMICAL CONVERSION COATING ON SEAT TRACK AT BS827 RBL 45 WL208 PER SRM 51-20-01-0G-0 UPDATED MEASUREMENT TABLE APPLIED PRIMER ON SEAT TRACK LOCATION BS 827 RBL 45 WL 208 PER SRM 51-20-01-0G-0.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON SUPPORT STIFFENER AT STA 721; LBL 68; WL 202. FOUND TO BE OUT OF LIMITS. DUE TO HAVING NO ALLOWABLE DAMAGE FOUND IN SRM. REPAIR BY REPLACEMENT. INSTALLED NEW STIFFENER AT BS 721 LBL 68 WL 202 IAW SRM 51-40-02-0G-0 AND DWG 144A7713 APPLIED FILLET SEAL IAW AMM 51-31-00-390-604 AND APPLIED CIC IAW AMM 51-21-91-620-802.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CRACKED ATTACH ANGLE AT STA 693; LBL 1 WL 207. ; / [01] UPDATED MEASUREMENT TABLE.; [02] VERIFIED FABRICATION OF NEW ANGLE PER DWG# 273A9112; [03] VERIFIED COMPLETION OF STEP 2.; [04] VERIFIED STEP 3.; [05] DISCREPANCY CORRECTION: CRACKED ATTACH ANGLE AT STA 693; RBL 1 WL 207 .; [06] STEP 1 AND 2 DISCRIPTION CORRECTION: ANGLE IS AT RBL1 NOT LBL1; [07] VERIFIED CORRECTIVE ACTION 5 AND 6; [08] VERIFIED STEP 4.; [09] VERIFIED STEP 5 COMPLETE.; [10] ALL INSPECTION STEPS COMPLETE.

Part: NONE — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

ACB FLOORBOARD STRIP BS 727D HAS AREAS OF CORROSION. ; / [01] CORROSION ON STRIP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED CORRECTIVE ACTION 1.; [03] RECEIVED NEW AFT CARGO BAY FLOORBOARD STRIP BS 727D INSTALL WELL BE WORK ON CARD # 5360-E-16462-NG ;TTG8Q004E0DV; [04] VERIFIED RECEIVED NEW AFT CARGO BAY FLOORBOARD STRIP BS 727D INSTALL WELL BE WORK ON CARD # 5360-E-16462-NG ;TTG8Q004E0DV

Part: BRACKET — CRACKED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CRACKED DUCT SUPPORT BRACKET AT STA 540+4; LBL 7; WL 166 ; / [01] UPDATED MEASUREMENTS; [02] REPLACED DUCT SUPPORT BRACKET AT STA 540+4 LBL 7 WL 166 <BR>PER SRM 51-40-02-0G-0; [03] VERIFIED REPLACEMENT OF THE PNEUMATIC DUCT SUPPORT BRACKET AT BS540+4 LBL7 WL166 PER

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CRACKED ATTACH ANGLE AT STA 693; RBL 1; WL 207 ; / [01] UPDATED MEASUREMENT TABLE; [02] VERIFIED FABRICATION OF NEW ANGLE PER DWG# 273A9112; [03] VERIFIED APPLICATION OF CHEMICAL CONVERSION COATING AND PRIMER TO ANGLE AND LOCATE AND DRILL PER SRM 51-40-05 AND DWG# 273A9110; OK TO INSTALL; [04] INSTALLED NEW ATTACH ANGLE AT BS 639 RBL 1 WL 207 PER SRM 51-40-02 AND DWG# 273A9110.; [05] INSTALLED NEW ATTACH ANGLE AT BS 693 RBL 1 WL 207 PER SRM 51-40-02 AND DWG# 273A9110.; [06] VERIFIED INSTALLATION OF NEW ATTACH ANGLE AT BS 693; RBL 1; WL 207; PER SRM 51-40-02 AND DWG 273A9110; [07] VERIFIED ALL WORK COMPLETE THIS TASK; [08] CORRECTION TO DISCREPANCY: CRACKED ATTACH ANGLE AT STA 693; LBL 1 WL 207. CORRECTIVE ACTIONS 4 AND 5 SHOULD READ: INSTALLED NEW ATTACH ANGLE AT BS 693 LBL 1 WL 207 PER SRM 51-40-02 AND DWG# 273A9110. STEP 1 DISCRIPTION SHOULD STATE: REMOVED CRACKED ATTACH ANGLE AT BS 693 LBL 1 WL 207 PER SRM 51-40-02.; [09] CORRECTION TO ACTION ITEM #6: VERIFIED INSTALLATION OF NEW ATTACH ANGLE AT BS 693; LBL 1; WL 207; PER SRM 51-40-02 AND DWG 273A9110

Part: SUPPORT — CORRODED (BS 867-887) · airframe 58,641 hrs · 34,716 cycles

ACB R/H FLOOR TO SIDEWALL SUPPORT BS 867 TO 887 HAS AREAS OF CORROSION ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 874 REMOVED 0.010' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [02] CORRECTION TO CORRECTIVE ACTION STEP 1 IT SHOULD HAVE STATED ' EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 874 REMOVED 0.010' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [03] VERIFIED CORRECTIVE ACTION 2.; [04] LOCATED AND DRILLED NEW R/H FLOOR TO SIDEWALL SUPPORT BS 867 TO 887 PER SRM 51-40-05-0G-0 AND DWG 146A7500; [05] VERIFIED CORRECTIVE ACTION 4.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON STIFFENER AT STA 693; RBL 64; WL 202. FOUND TO BE OUT OF LIMITS. DUE TO HAVING NO ALLOWABLE DAMAGE FOUND IN SRM. REPAIR BY REPLACEMENT. INSTALLED NEW STIFFENER AT BS693 RBL64 WL202 IAW EA 21-153-03268. CIC APPLIED IAW SOPM 20-41-05.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON SUPPORT STIFFENER AT STA 687; LBL 67; WL 202 ; / [01] FOUND TO BE OUT OF LIMITS. DUE TO HAVING NO ALLOWABLE DAMAGE FOUND IN SRM. REPAIR BY REPLACEMENT.; [02] REMOVED CORROSION ON STIFFENER AT BS 687 LBL67 WL 202 PER SRM 51-10-02. MAXIMUM MATERIAL REMOVED WAS 1'X1'X .008'. FOUND TO BE OUT OF LIMITS DUE TO HAVING NO ALLOWABLE DAMAGE FOUND IN SRM. REPAIR BY REPLACEMENT. DIAL DEPTH GAUGE ID:NCX000697 S/N:UNKNOWN.; [03] VERIFIED CORRECTIVE ACTION 2.; [04] UPDATED PARTS TABLE; [05] FABRICATED NEW STIFFENER AT BS 687; LBL 67; WL 202 FROM BAC1490-2824 7075T0 (LOT NUMBER 1473208-1) HEAT TREATED TO T62 CONDITION ON CUSTOMER RO NO. 843865-SWA; JOB NUMBER 544235 PER BOEING DWG 144A7713. LOCATED AND DRILLED NEW STIFFENER BS 687; LBL 67; WL 202 PER SRM 51-40-05-0G-0 AND BOEING DWG 144A7713. APPLIED CHEMICAL CONVERSION COATING TO NEW STIFFENER PER SRM 51-20-01-0G-0. OK TO APPLY PRIMER.; [06] VERIFIED ACTION 5; [07] PRIMED NEW SUPPORT STIFFENER AT BS 687; LBL 67; WL 202 PER BOEING DWG 144A7713 AND SRM 51-20-01-0G-0.; [08] VERIFIED CORRECTIVE ACTION ITEM 7.; [09] PARTIAL UPDATE OF STEP 1...OK TO INSTALL; [10] EDIT TO PARTIAL UPDATE OF STEP 1...OK TO INSTALL.; [11] CERTIFIED EDIT; [12] VERIFIED STEP 1; OK TO INSTALL STIFFNER; [13] PARTIAL UPDATE STEP 2; [14] REMOVED AND REPLACED STIFFENER AT BS 687; LBL 67; WL 202 I.A.W BOEING DWG 144A7730 AND SRM 51-40-02-0G-0; [15] VERIFIED CORRECTIVE ACTION STEP 14 COMPLETE.; [16] COMPLETE

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON STIFFENER AT STA 708; RBL 63 AND RBL 65; WL 202. ; / [01] FOUND TO BE OUT OF LIMITS DUE TO HAVING NO ALLOWABLE DAMAGE FOUND IN SRM. REPAIR BY REPLACEMENT.; [ [14] REMOVED AND REPLACED STIFFENER AT BS 708; RBL 63; WL 202 I.A.W BOEING DWG 144A7730 AND SRM 51-40-02-0G-0; [15] VERIFIED CORRECTIVE ACTION STEP 14.; [16] COMPLETE; [17] VERIFIED COMPLETE

Part: CARGO TRACK — CORRODED (BS 727-727A) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON TRACK AT AFT CARGO BAY BS727+17; BS727A; BS727A+10; BS727B; BS727B+3; BS727B+10; BS727C+3; BS727C+10. RBL13 WL156. ; / EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727+10? REMOVED 0.042' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.070' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [03] VERIFIED STEP 2.; [04] REMOVED R/H CARGO TRACK BS 727 TO 887 RBL 13 PER SRM 51-40-02-0G-0; [05] BEGAN DRILLING ACB R/H CARGO TRACK PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG 146A7500; [06] LOCATED AND DRILLED ACB R/H CARGO TRACK BS 727 TO 887 PER SRM 51-40-02-0G-0 ; SRM 51-40-05-0G-0 DWG 146A7500; [07] LOCATED AND DRILLED CARGO TIE DOWN TRACK SPLICE BS 747+10' RBL 13 USING SUPPLIED PART 146A7506-20 PER SRM 53-00-53-2R-3HFEC INSPECTED CUT OUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. <BR>EQUIP ID#: IS000450 S/N: N500D000M120071 APPLIED CHEMICAL CONVERSION COATING AND PRIMED TRIMMED EDGES PER SRM 53-00-53-2R-3 AMM 51-20-01 AND SOPM 20-41-02; OK TO INSTALL SEALED AND INSTALLED ACB TRACK BS727+4 TO BS887+5; RBL13; WL156 PER DWG 146A7500; SRM 51-40-02-0G-0; AMM51-31-00-390-801; CARGO TRACK SPLICE BS747+10; RBL13; WL156 PER SRM 53-00-53-2R-3;

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CRACKED FLOOR SUPPORT BS 312-328 RBL 30 WL 208 ; / [01] REMOVED CRACKED SUPPORT AND INSTALLED NEW SUPPORT IAW DWG 141A5400 SH 26 AND SRM 51-40-02; [02] VERIFIED CORRECTIVE ACTION 1.; [03] VERIFIED ALL STEPS COMPLETE.

Part: SUPPORT — CORRODED (BS 887-947) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS887 - BS947 RBL21 WL171. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 927 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [02] VERIFIED CORRECTIVE ACTION STEP 1.; [03] LOCATED AND DRILLED NEW R/H FLOOR TO SIDEWALL SUPPORT BS 887 TO 947 RBL21 WL171 PER SRM 51-40-05-0G-0 AND DWG 146A7500; [04] VERIFIED CORRECTIVE ACTION 3.

Part: SUPPORT — CORRODED (BS 727B-727C) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727B+10; BS727C+2.5; BS727D+10; BS727E+6.5; BS757 - BS767; BS767+5; BS787+14. LBL21 WL156. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 767 REMOVED 0.010' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [02] VERIFIED CORRECTIVE ACTION STEP 1.; [03] LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727 TO 847 LBL 21; WL 156 PER SRM 51-40-05-0G-0; AND DWG 146A7500; [04] VERIFIED CORRECTIVE ACTION 3.; [05] VERIFIED ALL STEPS COMPLETE.; [06] CORRECTION TO CORRECTIVE ACTION STEPS 1. IT SHOULD BE SRM 53-00-53-1A-2.

Part: CARGO TRACK — CORRODED (BS 787-802) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON TRACK AT AFT CARGO BAY BS787; BS795; BS799; BS802 RBL13 WL158. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 799 REMOVED 0.040' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.070' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN. CARGO TRACK WILL BE REPLACED FROM 727 TO 887 ON FAULT TTG8Q006TQL7; [02] VERIFIED CORRECTIVE ACTION 1.; [03] ALL INSPECTION STEPS COMPLETE

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

FSD THRESHOLD CRACKED AFT CORNER ; / [01] WELDED CRACK ON FSD SCUFF PLATE USING AMS 4954 TITANIUM FILLER ROD LOT # M798431 PER SRM 53-10-15-2R-2PARA 4.B. (3) AND (4)<BR>WELDING MACHINE E10583; S/N: KJ256554 12/2021; [02] VERIFIED CORRECTIVE ACTION 1.; [03] FLUORESCENT DYE PENETRANT INSPECTED REPAIRED AREA IN ACCORDANCE WITH SOPM 20-20-02 METHOD C.<BR>NO CRACKS NOTED.<BR><BR>TOOL I.D. ATS2504 (DLM-1000 RADIOMETER); [04] SANDED WELD REPAIR AREA PER SRM 53-10-15-2R-2 PARA 4.B.(6); [05] VERIFIED STEP 4.; [06] APPLIED PRIMER AND PARTING AGENT TO BACK OF THRESHOLD PER SRM 53-10-15-15-2R.; [07] ALL INSPECTION STEPS COMPLETE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON FED THRESHOLD SUPPORT BS 328-328+10 LBL 60 WL208 ; / [01] REMOVED CORROSION ON FED THRESHOLD SUPPORT BS 328-328+10 LBL 60 WL 208 PER SRM 51-10-02. MAXIMUM MATERIAL REMOVED WAS 1'X1'X.010'. ORIGINAL THICKNESS WAS .080'. FOUND TO BE OUT OF LIMITS PER SRM 53-10-15-1A-2. MICROMETER IDIS000461 SN:67126205.; [02] VERIFIED CORRECTIVE ACTION 1.; [03] VERIFIED LOCATED AND DRILLED NEW THRESHOLD ANGLE PER SRM 51-40-05 AND DWG#141A8110. AND GAVE OK TO INSTALL.PARTIAL WORK UPDATE FOR STEP 1.; [04] INSTALLED NEW FED THRESHOLD SUPPORT BS 328-328+10 LBL 60 WL 208 PER SRM 51-40-02 AND DWG#141A8110.; [05] INSTALLED NEW FED THRESHOLD SUPPORT BS 328-328+10 LBL 60 WL 208 PER SRM 51-40-02 AND DWG#141A8110.; [06] VERIFIED CORRECTIVE ACTION STEPS 4 AND 5.

Part: FRAME SPLICE — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON FRAME SPLICE AT AFT CARGO BAY BS787 RBL25 WL158. ; / [01] CORROSION ON SPLICE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED CORRECTIVE ACTION STEP 1.; [03] REMOVED ACB FRAME SPLICE BS787; RBL25; WL158. PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW ACB FRAME SPLICE BS787; RBL25; WL158. PER DWG 146A1262 AND SRM 51-40-05-0G-0. OK TO INSTALL.; [05] VERIFIED LOCATED AND DRILLED NEW ACB FRAME SPLICE BS787; RBL25; WL158. PER DWG 146A1262 AND SRM 51-40-05-0G-0. OK TO INSTALL.; [06] INSTALLED NEW ACB FRAME SPLICE BS787; RBL25; WL158. PER DWG 146A1262 AND SRM 51-40-02-0G-0.; [07] VERIFIED INSTALLED NEW ACB FRAME SPLICE BS787; RBL25; WL158. PER DWG 146A1262 AND SRM 51-40-02-0G-0.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT AFT CARGO BAY BS947 RBL20 WL180. ; / [01] CORROSION ON SUPPORT ANGLE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED CORRECTIVE ACTION 1.; [03] REMOVED SUPPORT PER SRM 51-40-02; [04] LOCATED AND DRILLED NEW AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS 947 RBL20 WL180 PER SRM 51-40-05-0G-0 AND DWG 149A8117; [05] VERIFIED CORRECTIVE ACTION STEP 4.; [06] OK TO INSTALL SUPPORT ANGLE; [07] VERIFIED STEP 6; OK TO INSTALL; [08] OK TO INSTALL CENTER AFT CARGO BULKHEAD SUPPORT ANGLE BS907; [09] INSTALLED CENTER AFT CARGO BULKHEAD SUPPORT ANGLE BS947 PER SRM 51-40-02-0G-0 AND DWG 149A8117; [10] VERIFIED STEP 9; [11] VERIFIED INSTALLATION OF THE AFT BULKHEAD FLOOR SUPPORT AT BS947 PER SRM 51-40-02-0G-0 AND DWG 149A8117; [12] WORKSCOPE COMPLETE ON REPLACEMENT OF THE BS947 AFT CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CRACKED FLOOR SUPPORT BS 344-360 RBL33 WL208 ; / [01] REMOVED CRACKED FLOOR SUPPORT AT BS 344-360 RBL 33 WL 208 IAW SRM 51-40-02. LOCATED AND DRILLED NEW FLOOR SUPPORT PER SRM 51-40-05 AND DWG 141A5400 ID:0033. REQUESTING OK TO INSTALL; [02] VERIFIED CORRECTIVE ACTION 1.; [03] INSTALLED NEW SUPPORT AT BS 344-360 RBL 33 WL 208 IAW DWG 141A5400 ID:0033 AND SRM 51-40-05.; [04] COMPLETE.; [05] VERIFIED CORRECTIVE ACTION STEP 3.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON AFT SHIELD AT AFT CARGO BAY BS847 - BS867 RBL21 WL164. ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED CORRECTIVE ACTION STEP 1.; [03] LOCATED AND DRILLED NEW ACB AFT SHIELD BS847-BS867; RBL21; WL164. PER DWG 146A0081; AND SRM 51-40-05-0G-0.; [04] VERIFIED LOCATED AND DRILLED NEW ACB AFT SHIELD BS847-BS867; RBL21; WL164. PER DWG 146A0081; AND SRM 51-40-05-0G-0.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS795 RBL6 WL152. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] REMOVED OLD INTERCOSTAL; RECEIVED NEW INTERCOSTAL; LOCATED DRILLED ALL PER SRM 51-40-02-0G-0; SRM 51-40-05; AND DWG 146A8130; OK TO INSTALL; [03] VERIFIED REMOVED OLD INTERCOSTAL; RECEIVED NEW INTERCOSTAL; LOCATED DRILLED ALL PER SRM 51-40-02-0G-0; SRM 51-40-05; AND DWG 146A8130; OK TO INSTALL; [04] INSTALLED NEW INTERCOSTAL AT ACB BS787 - BS807; RBL16; WL152 PER SRM 51-40-02-0G-0; SRM 51-40-02; AND DWG 146A8130; [05] INSTALLED NEW INTERCOSTAL AT ACB BS787 - BS807; RBL16; WL152 PER SRM 51-40-02; AND DWG 146A8130; [06] VERIFIED CORRECTIVE ACTION 5.; [07] VERIFIED INTERCOSTAL REPLACED. ALL WORK ACCOMPLISHED.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON FWD SHIELD ATTACH FITTING AT AFT CARGO BAY BS767 RBL23 WL157. ; / [01] CORROSION ON FITTING/GUSSET WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] REMOVED ACB GUSSET BS767; RBL23; WL157. PER SRM 51-40-02-0G-0; [03] LOCATED AND DRILLED NEW GUSSET BS767; RBL23; WL157. PER DWG 146A0081 AND SRM 51-40-05-0G-0. OK TO INSTALL.; [04] CERTIFY STEP'S 2 AND 3.; [05] VERIFIED LOCATED AND DRILLED NEW GUSSET BS767; RBL23; WL157. PER DWG 146A0081 AND SRM 51-40-05-0G-0. OK TO INSTALL.; [06] INSTALLED NEW GUSSET BS767; RBL23; WL157. PER DWG 146A0081; AND SRM 51-40-02-0G-0.; [07] VERIFIED INSTALLED NEW GUSSET BS767; RBL23; WL157. PER DWG 146A0081; AND SRM 51-40-02-0G-0.

Part: WEB — CORRODED (BS 799-839) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS799 - BS839 RBL26 WL158. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 800 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.045' FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING ATS TOOL ID ATS1225 S/N UNKNOWN.; [02] VERIFIED CORRECTIVE ACTION STEP 1; [03] LOCATED; DRILLED; AND INSTALLED NUTPLATES ON NEW ACB SUBTHRESHOLD WEB BS794-BS847; RBL26; WL158. PER DWG 146A8340; SRM 51-40-05-0G-0; AND SRM 51-40-02-0G-0; [04] VERIFIED CORRECTIVE ACTION 3.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CRACKED FLOOR SUPPORT BS 344-360 BL0 WL208 ; / [01] REMOVED CRACKED FLOOR SUPPORT AT BS 344-360 BL 0 WL 208 IAW SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-05 AND DWG 141A5400 ID:0032. REQUEST OK TO INSTALL.; [02] VERIFIED CORRECTIVE ACTION 1.; [03] INSTALLED NEW SUPPORT AT BS 34-360 BL 0 WL 208 IAW DWG 141A5400 ID:0032 AND SRM 51-40-05.; [04] COMPLETE; [05] VERIFIED CORRECTIVE ACTION STEP 3.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767 - BS787 RBL22 WL157. ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED CORRECTIVE ACTION STEP 1.; [03] LOCATED AND DRILLED NEW ACB FWD SHIELD BS767-BS792; RBL22; WL157 PER DWG 146A0081; AND SRM 51-40-05-0G-0.; [04] VERIFIED LOCATED AND DRILLED NEW ACB FWD SHIELD BS767-BS792; RBL22; WL157 PER DWG 146A0081; AND SRM 51-40-05-0G-0.; [05] VERIFIED COMPLETED

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS771 RBL6 WL154. ; / [01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] REMOVED OLD INTERCOSTAL PER SRM 51-40-02-0G-0; [03] VERIFIED EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [04] RECEIVED INTERCOSTAL FROM FORM AND HEAT TREAT PO#841173; [05] LOCATED AND DRILLED NEW INTERCOSTAL AT ACB BS767 - BS787 RBL6 WL154 PER SRM 51-40-05-0G-0 AND DWG 146A8130. APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO NEW INTERCOSTAL PER AMM 51-21-41-370-802; AMM 51-21-72-370-804. OK TO INSTALL; [06] VERIFIED CORRECTIVE ACTION STEPS 4 AND 5. OKAY TO INSTALL; [07] INSTALLED NEW INTERCOSTAL AT ACB BS767 - BS787; RBL16; WL154 PER SRM 51-40-02-0G-0 AND DWG 146A8130; [08] VERIFIED CORRECTIVE ACTION 7.; [09] VERIFIED REPLACEMENT OF INTERCOSTAL. ALL WORK ACCOMPLISHED.

Part: CARGO TRACK — CORRODED (BS 727A-727D) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON TRACK AT AFT CARGO BAY BS727A; BS727A+10; BS727D+6. LBL17 WL156. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727D+6? REMOVED 0.042' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.070' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [02] VERIFIED CORRECTIVE ACTION 1.; [03] REMOVED ACB TRACK BS 727 TO 867 LBL 17 PER SRM 51-40-02-06-0; [04] BEGAN DRILLING L/H ACB CARGO TRACK PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG 146A7500; [05] LOCATED AND DRILLED L/H AFT CARGO TIE DOWN TRACK BS 727 TO 867 PER SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 DWG 146A7500.; [06] VERIFIED LOCATE AND DRILL OF LH ACB TIE-DOWN TRACK; BS 727-867 PER SRM 51-40-02; SRM 51-40-05 AND DWG 146A7500; [07] OK TO INSTALL; [08] SEALED AND INSTALLED AFT CARGO BAY 727 TO 867 LBL 17 PER SRM 51-40-02-0G-0 AND DWG 146A7500; [09] VERIFIED INSTALLATION OF THE LBL17 CARGO TRACK FROM BS727-BS867 WL156 PER SRM 51-40-02-0G-0 AND DWG 146A7500; [10] WORKSCOPE COMPLETE

Part: SUPPORT — CORRODED (BS 727B) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727B+2.5; BS727B+18.5 RBL21 WL156. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727B+18.5' REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [02] VERIFIED CORRECTIVE ACTION STEP 1.; [03] LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727 TO 767 RBL 21 WL 156 PER SRM 51-40-05-0G-0; AND DWG 146A7500; [04] VERIFIED LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727 TO 767 RBL 21 WL 156 PER SRM 51-40-05-0G-0; AND DWG 146A7500; [05] CORRECTION TO CORRECTIVE ACTION STEPS 1. IT SHOULD BE SRM 53-00-53-1A-2.

Part: SUPPORT — CORRODED (BS 500A-500C) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT BS500A+7; BS500C+2; BS500C+6.5 RBL24 WL156. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 465 REMOVED 0.010' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [02] CORRECTION TO CORRECTIVE ACTION STEP 1. EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500C+2' REMOVED 0.010' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [03] VERIFIED ACTION 1;2; [04] FABRICATED NEW R/H FLOOR TO SIDEWALL SUPPORT BS 500A TO 500D RBL24 WL 156 FROM EXTRUSION BAC1496-444#7075T62 CLAD LOT# 1467644-1; AND LOCATED AND DRILLED PER SRM 51-40-02-0G-0; DWG 143A7500; AND DWG 143A7501; [05] APPLIED CHEMICAL CONVERSION COATING; PRIMER AND INSTALLED NUTPLATES PER SOPM 20-43-03; AMM 51-21-72-370-804; AND DWG 143A7501; [06] VERIFIED CORRECTIVE 4.; [07] VERIFIED ALL STEPS COMPLETE.; [08] CORRECTION TO CORRECTIVE ACTION STEPS 1 AND 2. IT SHOULD BE SRM 53-00-53-1A-2.

Part: SUPPORT — CORRODED (BS 400-500D) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS500D LBL24 WL156. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 470 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-2 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [02] VERIFIED ACTION 1; [03] FABRICATED AND LOCATED NEW L/H FLOOR TO SIDEWALL SUPPORT BS396 - 500D AND SPLICE REPAIR AT BS485 - BS495 FROM EXTRUSION BAC1496-444#7075 T62 CLAD LOT# 5098100-1 PER SRM 51-40-05-0G-0; SRM 53-00-53-2R-5; DWG 143A7501; DWG 143A7500 AND APPLIED CHEMICAL CONVERSION COATING TO SIDEWALL SUPPORT AND SPLICE REPAIR PER AMM 51-21-41-370-802; [04] CERTIFY STEP 3.; [05] VERIFIED CORRECTIVE ACTION ITEM 3.; [06] APPLIED PRIMER TO SIDEWALL SUPPORT PER AMM 51-21-72-370-804; [07] VERIFIED APPLIED PRIMER TO SIDEWALL SUPPORT PER AMM 51-21-72-370-804; [08] CORRECTION TO CORRECTIVE STEP 1. IT SHOULD BE SRM 53-00-53-1A-2.

Part: NONE — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON ASD MOPSILL INNER CHORD BS 947-992 RBL 49-56 WL 208 ; / [01] REMOVED CORROSION ON ASD MOPSILL INNER CHORD BS 947-992 RBL 49- RBL 56 WL 208 PER SRM 51-10-02. MAXIMUM MATERIAL REMOVED WAS 1'X1'X.013'. FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1[07] REMOVED ASD MOPSILL PER SRM 51-40-02-0G-0.; [08] LOCATED AND DRILLED NEW MOPSILL PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0 AND DWG 147A8540.; [09] VERIFIED CORRECTIVE ACTION 8.; [10] OK TO INSTALL MOPSILL AT ASD.; [11] VERIFIED ACTION 10; [12] INSTALLED ASD MOPSILL FROM BS 893-967 EXCEPT COMMON TO THE FRAME; AND INSTALLED O/B ROW FROM 967-986.50 RBL 56 WL 208 IAW SRM 51-40-02; BOEING DWG 147A8501.; [13] COMPLETED INSTALLATION OF ASD MOPSILL PER SRM 51-40-02-0G-0 AND BOEING DWG 147A8501.; [14] VERIFIED CORRECTIVE ACTION 13; [15] VERIFIED JOB COMPLETE; [16] UPDATED MEASUREMENT TABLE ITEM 14

Part: SHIELD — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL24 WL156. ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED ACTION 1; [03] LOCATED AND DRILLED SHIELD BS 500-500A RBL 24 WL 156 PER SRM 51-40-05 AND DWG 143A0080; [04] VERIFIED LOCATED AND DRILLED SHIELD BS 500-500A RBL 24 WL 156 PER SRM 51-40-05 AND DWG 143A0080

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED ; / [01] WELDED CRACKS ON AFT CARGO BAY; FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(2) AND (4)<BR>WELDING MACHINE CAL I.D. E10583; S/N: KJ256554; 12/2021; [02] VERIFIED CRACKS ON THE AFT CARGO DOOR FWD SCUFF PLATE ARE WELDED PER SRM 53-60-15-2R-1 PARA 4.B.(2) AND (4); [03] FLUORESCENT DYE PENETRANT INSPECTED REPAIRED AREAS IN ACCORDANCE WITH SOPM 20-20-02 METHOD C. NO CRACKS NOTED<BR><BR>TOOL I.D. ATS2504 (DLM-1000 RADIOMETER); [04] SANDED WELD REPAIR AREA PER SRM 53-60-15-2R-1 PARA 4.B.(5); [05] VERIFIED WELD AREA SANDED SMOOTH PER SRM 53-60-15-2R-1 PARA 4.B.(5); [06] ALL WORK COMPLETE; SCUFF PLATE WILL BE REINSTALLED ON FAULT TTG8Q004E0DV; [07] VERIFIED WELD REWORK ON THE AFT CARGO DOOR FWD SCUFF PLATE IS COMPLETE. SCUFF PLATE WILL BE REINSTALLED ON TTG8Q004E0DV

Part: WEB — CORRODED (BS 460-485) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS460 - BS485 RBL28 WL156. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 465 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.045' FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1 USING ATS TOOL ID ATS1225 S/N UNKNOWN; [02] VERIFIED ACTION 1; [03] BEGAN LOCATING; DRILLING; AND INSTALLING NUTPLATES ON FCB SUBTHRESHOLD WEB BS440-BS492; RBL28; WL156. PER DWG 143A8330; SRM 51-40-02-0G-0; AND SRM 51-40-05-0G-0.; [04] LOCATED; DRILLED; AND INSTALLED NUTPLATES ON NEW FCB SUBTHRESHOLD WEB BS440-BS492; RBL28; WL156. PER DWG 143A8330; SRM 51-40-05-0G-0; AND SRM 51-40-02-0G-0.; [05] VERIFIED CORRECTIVE ACTION ITEM 4.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON HORIZONTAL SHEAR WEB BS 1019-1022 RBL 4 WL 208 ; CORRECTION TO FALT DESCRIPTION: TTOCK LINE IS LBL. FALT DESCRIPTION SHOLD READ: CORROSION ON HORIZONTAL SHEAR WE BS 1019-1022 LBL 4 WL 208 / [01] CORRECTION TO FAULT DESCRIPTION: BUTTOCK LINE IS LBL. FAULT DESCRIPTION SHOULD READ: CORROSION ON HORIZONTAL SHEAR WEB BS 1019-1022 LBL 4 WL 208; [02] REMOVED CORROSION FROM HORIZONTAL SHEAR WEB BS 1019-1022 LBL 4 WL 208 IN AREA OF 0.5' BY 4.6' PER SRM 51-10-02-0G-0.; [03] VERIFIED CORRECTIVE ACTION 2.; [04] PERFORM UT INSPECTION TO DETERMINE REMAINING MATERIAL THICKNESS.; [05] UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; REMAINING THICKNESS IS 0.038' ADJACENT TO 0.04'. SEE ATTACHED GRID ON COVER SHEET<BR><BR>EQUIP ID#: ATS2031 S/N: 170515011; [06] HFEC INSPECTED IAW NDTM PART 6; 51-00-00 PROC 23. NO CRACKS FOUND. TOOL ID IS000450 N500; [07] VERIFIED ALL WORK COMPLETED; [08] COMPLETE; [09] ALL WORK STEPS COMPLETE.

Part: NONE — CORRODED · airframe 58,641 hrs · 34,716 cycles

CORROSION ON BS 986 BEAM UPPER CHORD BS 986 RBL 39-44 WL208 ; / [01] REMOVED CORROSION ON BS 986 BEAM UPPER CHORD BS 986 RBL 39-44 WL 208 IN AREA OF 1' BY 5' BY A MAXIMUM OF 0.057' PER SRM 51-10-02-0G-0 AND SRM 53-70-51-1A-1. OUT OF LIMITS PER SRM 53-70-51-1A-1.; [02] REMOVED CORROSION ON BS 986 BEAM UPPER CHORD BS 986 RBL 39-44 WL 208 IN AREA OF 1' BY 5' BY A MAXIMUM OF 0.057' PER SRM 51-10-02-0G-0 AND SRM 53-70-51-1A-1. OUT OF LIMITS PER SRM 53-70-51-1A-1. USED DIAL DEPTH GAUGE ID: NCX000697 S/N: UNKNOWN TRIMMED INTERCOSTAL I.A.W SRM 53-70-51-2R-4 STEP 4.F(3) REQUEST D.V.I; [25] FLAP PEENED THE CUT EDGE OF THE INTERCOSTAL I.A.W SRM 53-70-51-2R-4 STEP 4.F(5); [26] LOCATED AND DRILLED ITEM 8 CORNER FITTINGS(2EA) I.A.W SRM 53-70-51-2R-4 STEP 4.G-M FIGURE 207 SHEET 1-5; [27] OK TO INSTALL INTERCOSTAL.; [28] INSTALLED REPAIR PARTS BS986 RBL18-RBL50 ITEM 1 T-CHORD(1EA);ITEM 2 ANGLE(2EA);ITEM 3 ANGLE(2EA);ITEM 4 STRAP(2EA) ITEM 7 SHEAR TIE (1EA) I.A.W SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 2 PAR 4.N-O EXCEPT WHERE THE FASTENER ARE COMMON TO INTERCOSTAL ON RBL38. CORNER FITTINGS AND INTERCOSTAL BS 986-

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON INTERCOSTAL IN 2 LOCATIONS BS 956 RBL 18 WL 208 AND BS 956 RBL 23 WL 208 ; / [01] REMOVED CORROSION ON INTERCOSTAL IN 2 LOCATIONS BS 956 RBL 18 WL 208 IN AREA OF 0.8' BY 2.4' BY A MAXIMUM DEPTH OF 0.019' AND BS 956 RBL 23 WL 208 IN AREA OF 1.2' BY 1.8' BY A MAXIMUM DEPTH OF 0.020' PER SRM 51-10-02-0G-0 AND SRM 53-70-51-1A-1. OUT OF LIMITS PER SRM 53-70-51-1A-1.; [02] REMOVED CORROSION ON INTERCOSTAL IN 2 LOCATIONS BS 956 RBL 18 WL 208 IN AREA OF 0.8' BY 2.4' BY A MAXIMUM DEPTH OF 0.019' AND BS 956 RBL 23 WL 208 IN AREA OF 1.2' BY 1.8' BY A MAXIMUM DEPTH OF 0.020' PER SRM 51-10-02-0G-0 AND SRM 53-70-51-1A-1. OUT OF LIMITS PER SRM 53-70-51-1A-1. USED DIAL DEPTH GAUGE ID: NCX000697 S/N: UNKNOWN; [03] CERTIFIED CORRECTIVE ACTION #2; [04] VERIFIED CORRECTIVE ACTION 2.; [05] REMOVED DAMAGED INTERCOASTAL BS 956; RBL 7.9 - RBL 30; WL 208 PER SRM 51-40-02-0G-0.; [06] LOCATED AND DRILLED NEW INTERCOASTAL BS 956; RBL 7.9 - RBL 30; WL 208 PER SRM 51-40-05-0G-0 AND BOEING DWG 147A5760. OK TO INSTALL NEW INTERCOASTAL BS 956; RBL 7.9 - RBL 30; WL 208.; [07] VERIFIED CORRECTIVE ACTION 6 OKAY TO INSTALL; [08] INSTALLED NEW INTERCOASTAL BS 956; RBL 7.9 - RBL 30; WL 208 PER SRM 51-40-02-0G-0 AND BOEING DWG 147A5760.; [09] VERIFIED CORRECTIVE ACTION 8.; [10] INSPECTION STEPS COMPLETE.

Part: NONE — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON BS 986 BEAM UPPER CHORD BS 986 LBL 44 WL208 ; / [01] REMOVED CORROSION ON BS 986 BEAM UPPER CHORD BS 986 LBL 44 WL 208 IN AREA OF 1.1' BY 1.8' BY A MAXIMUM DEPTH OF 0.080' PER SRM 51-10-02-0G-0 AND SRM 53-70-51-1A-1. OUT OF LIMITS PER SRM 53-70-51-1A-1.[18] LOCATED AND DRILLED NEW ANGLE ITEM 5(4EA) OBTAINED FROM COSTUMER KIT BS986 SI 7530799 ALL I.A.W SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 2 PAR 4.G-M TABLE 201 OK TO INSTALL; [19] OK TO INSTALL ALL REMOVED PARTS FOR ACCESS COMMON TO REPAIR AREA.; [20] VERIFIED CORRECTIVE ACTION 17;18 AND 19.; [21] INSTALLED REPAIR PARTS BS986 LBL1-LBL50 ITEM 1 T-CHORD(1EA);ITEM 2 ANGLE(2EA);ITEM 3 ANGLE(2EA);ITEM 4 STRAP(2EA) ITEM 7 SHEAR TIE (1EA) I.A.W SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 2 PAR 4.N-O; [22] VERIFIED CORRECTIVE ACTION 21.; [23] VERIFY INSTALLATION ITEM 1-7; [24] VERIFIED STEPS 1-7 COMPLETE.; [25] ALL RII STEPS ARE COMPLETE.; [26] COMPLETED ALL REPAIR STEPS ON BS986 LBL1-LBL50 WL208 PER SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 2; [27] VERIFIED CORRECTIVE ACTION 26.; [28] UPDATED MEASUREMENT TABLE ITEM 14; [29] UPDATED MEASUREMENT TABLE ITEM 14

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON AFT BULKHEAD TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 500D RBL25 157. ; / [01] EVALUATED CORROSION; REMAINING THICKNESS LESS THAN 0.056' IN A AREA OF 1X1 FOUND TO BE OUT OF LIMITS PER SRM 53-30-08-1A-1 USING ATS TOOL ID ATS1225 S/N UNKNOWN.; [02] VERIFIED ACTION 1; [03] LOCATED AND DRILLED NEW FWD CARGO BAY R/H AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS 500D RBL25;WL157 PER SRM 51-40-05-0G-0; DWG 143A7902; AND 143A9481; [04] ADDED PART USE; [05] VERIFIED CORRECTIVE ACTION 3.; [06] VERIFIED ALL STEPS COMPLETE.

Part: NONE — CORRODED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON BS 967 BEAM UPPER CHORD IN 3 LOCATIONS BS967 RBL28 WL208; BS967 RBL42 WL208; AND BS967 RBL49 WL208 ; / [01] REMOVED CORROSION ON BS 967 BEAM UPPER CHORD IN 4 LOCATIONS: AT BS 967 RBL 49 WL 208 IN AN AREA OF 0.6' BY 0.7' BY A MAXIMUM DEPTH OF 0.009'; AT BS 967 RBL 47 WL 208 IN AN AREA OF 0.8' BY 1.1' BY A MAXIMUM DEPTH OF 0.034'; AT BS 967 RBL 40 WL 208 IN AN AREA OF 0.7' BY 0.8' BY A MAXIMUM DEPTH OF 0.008'; AND AT BS 967 RBL 28 WL 208 IN AN AREA OF 0.9' BY 0.9' BY A MAXIMUM DEPTH OF 0.020' PER SRM 51-10-02-0G-0 AND SRM 53-70-51-1A-1. OUT OF LIMITS PER SRM 53-70-51-1A-1.; [[06] REPAIRED DAMAGE ON BS 967 BEAM UPPER CHORD IN 3 LOCATIONS BS 967 RBL 28 WL 208; BS 967 RBL 42 WL 208; AND BS 967 RBL 49 WL 208 PER EA 21-153-03190 (N450WN - ATS (PAE) - REPAIR - BS 967 FLOOR BEAM REPAIR RBL 17 TO RBL 35 AND RBL 45 TO RBL 50) [TTG8Q0099EE6].; [07] VERIFIED CORRECTIVE ACTION 6; [08] UPDATED ITEM #14 P/N 147A5505-6; [09] MEASUREMENT TABLE UPDATED ITEM #14 P/N 147A5505-6

Part: NONE — CRACKED · airframe 58,641 hrs · 34,716 cycles

SUPPLEMENTAL INFORMATION: UPON COMPLETION OF HFEC INSPECTION; FOUND 1 INCH CRACK AT BS 666 RBL 40 WL 203 COMMON TO THE HORIZONTAL PRESSURE DECK / PERFORMED INSURANCE CUTDVIFABRICATED REPAIR PARTS DOUBLER(-1) FROM MATERIAL 2024 T3 CLAD 0.080' LOT.#1467098-1WEB (-3) FROM MAT 2024 T3 CLAD 0.063' LOT#1465400-1 STIFFENER (-2) 7EA FROM MAT. BAC1505-100052 7075 T6511 LOT#1465396-1 LOCATED DRILLEDAPPLIED CHEMICAL CONVERSION COATING AND PROTECTIVE TREATMENT IAW SRM 53-40-51-2R-2 PAR.4D(4)-4K. INSTALLED AND FILLET SEALED PARTS REMOVED FOR ACCESS TO REPAIR AREA 3 (EA) BRACKETS AND 1 (EA) SEAL IAW SRM 53-40-51-2R-2, SOPM 20-50-01 AND BOEING DWG 144A7700

Part: FLOORBEAM — CORRODED (BS 500D) · airframe 58,641 hrs · 34,716 cycles

CORROSION AT FWD CARGO BAY ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS500D LBL16;RBL13. WL156. ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT RBL 16 REMAINING THICKNESS LESS THAN 0.056' FOUND TO BE OUT OF LIMITS PER SRM 53-30-08-1A-1 USING ATS TOOL ID ATS1225 S/N UNKNOWN.; [02] CORRECTION TO CORRECTIVE ACTION STEP 1. EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT RBL 16 REMAINING THICKNESS LESS THAN 0.056' IN A AREA OF 1X1 FOUND TO BE OUT OF LIMITS PER SRM 53-30-08-1A-1 USING ATS TOOL ID ATS1225 S/N UNKNOWN.; [03] VERIFIED ACTION 1;2; [04] LOCATED AND DRILLED NEW FWD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS 500D LBL16; RBL13; WL156 PER SRM 51-40-05-0G-0; DWG 143A7902; AND 143A9481; [05] VERIFIED CORRECTIVE ACTION 4.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED ; / [01] REMOVED DAMAGED GUSSET; LOCATED;DRILLED AND OK TO INSTALL NEW GUSSET IAW SRM 51-40-02-0G-0 AND DWG 143A7902.; [02] OK TO INSTALL; [03] INSTALLED NEW SUPPORT GUSSET BS500D S-19L WL 193 IAW SRM 51-40-02-0G-0 AND DWG 143A7902.; [04] RII INSPECTED ACTION 3; [05] INSPECTION COMPLETE

Part: NONE — CRACKED (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CRACKED STRINGER CLIP AT FWD CARGO BAY BS500C S-19L WL193. ; / [01] CRACKED STRINGER CLIP WAS FOUND TO BE OUT OF LIMIT DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED ACTION 1; [03] REMOVED OLD STRINGER CLIP; LOCATED AND DRILLED NEW STRINGER CLIP PER SRM 51-40-05 AND DWG 143A1224; OK TO INSTALL; [04] VERIFIED REMOVED OLD STRINGER CLIP; LOCATED AND DRILLED NEW STRINGER CLIP PER SRM 51-40-05 AND DWG 143A1224; OK TO INSTALL; [05] INSTALLED NEW STRINGER CLIP PER SRM 51-40-02-0G-0 AND DWG 143A1224; [06] VERIFIED INSTALLED NEW STRINGER CLIP PER SRM 51-40-02-0G-0 AND DWG 143A1224

Part: STRIP — LOOSE (FUSELAGE) · airframe 58,641 hrs · 34,716 cycles

CORROSION ON FWD ANTENNA MOUNT AREA AND N/P STRIPS LOOSE ON 192F ; / [01] LOOSE NUTPLATE STRIPS WILL BE REINSTALLED ON CARD TTG8Q006VRM2.; [02] IDENTIFIED PART AND MATERIAL IAW SRM 51-70-14-0G-0 FIGURE 1; PAR 2.B AND TABLE 2.<BR>FOUND DAMAGE TO ALUMINUM FLAME-SPRAYED COATING TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 51-70-14-1A-0 PAR 2.B; TABLE 101 AND PAR 4.C (1).<BR>REPAIR WILL BE ACCOMPLISHED IAW SRM 51-70-14-2R-1 AS DIRECTED PER SRM 51-70-14-2R-0 PAR 2.C AND TABLE 201.;

Part: SIGN — LOOSE (OVERWING EXIT) · airframe 57,613 hrs · 34,093 cycles

CEILING OVERWING EXIT SIGN NOT SECURED. ; / SECURED CEING OVERWING EXIT SIGN PER AMM 33-51-01

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 56,665 hrs · 33,528 cycles

R2 DOOR EVACUATION SLIDE PARTIALLY HANGING OUT BOTTOM OF DOOR / REINSTALLED SLIDE IAW AMM 25-66-01 OPS GOOD; AFT OK FOR SERVICE

Part: SEAT TRACK — FAILED (COCKPIT) · airframe 56,304 hrs · 33,289 cycles

BOTH FIRST OFFICER SEAT TRACKS FAILED TASK CARD INSPECTION / R&R'D BOTH F/O'S SEAT AFT TRACKS PER MM 25-11-11.

Part: SEAT TRACK — FAILED (COCKPIT) · airframe 56,304 hrs · 33,289 cycles

BOTH CAPTAIN SEAT TRACKS FAILED TASK CARD INSPECTION / R&R'D BOTH CAPTAIN SEAT AFT TRACKS PER MM 25-11-11.

Part: BRACKET — CRACKED (WG-BDY FAIRING) · airframe 56,304 hrs · 33,289 cycles

RIGHT FWD UPPER WING TO BODY FAIRING 191AR; AFT LOWER SUPPORT BRACKET CRACKED. / REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02 AND SRM 51-10-02

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 56,304 hrs · 33,289 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01669. / R&R BATTERY PACK PER AMM.

Part: FITTING — CRACKED (NR 2 NACELLE) · airframe 56,304 hrs · 33,289 cycles

#2 ENGINE PYLON; LOWER AFT INBOARD INTERNAL PYLON FITTING HAS A 2 INCH CRACK. THE CRACK EXTENDS UNDER THE LOWER AFT OUTBOARD FITTING. / R&R'D #2 ENGINE PYLON; LOWER AFT PYLON FITTING REF AMM 54-52-04; SRM 51-10-02; AND SRM 51-40-02

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,827 hrs · 32,957 cycles

AFT ENTRY OUTSIDE EMERGENCY LIGHT INOP. / RELAMPED LIGHT IAW MM.

Part: PANEL — ELONGATED (LOWER EXT FUSELA) · airframe 55,311 hrs · 32,634 cycles

SERVERAL HOLES ON 193 PNL ARE ELONGATED. / DRILLED UP NEW PANEL REF B737 SRM 51-20-01 INSTALLED NEW PANEL REF B737 AMM 53-51-21 & EO WORK INSTRUCTIONS WIZARD # 14105

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,298 hrs · 32,627 cycles

R/H OVERWING EMERGENCY EXIT LIGHT INOP. / R&R SLIDE LIGHT LAMP PER AMM.

Part: CHANNEL — CRACKED (BS 918) · airframe 55,298 hrs · 32,627 cycles

CHANNEL CRACKED AT BS. 918, RBL 12. / R&R CHANNEL PER SRM AND DWG.

Part: CHANNEL — CRACKED (BS 914) · airframe 55,298 hrs · 32,627 cycles

CHANNEL CRACKED AT BS. 914, RBL 12. / R&R CHANNEL PER SRM AND DWG.

Part: ANGLE — CORRODED (AFT CARGO) · airframe 55,298 hrs · 32,627 cycles

***CORROSION*** WHILE WORKING CUSTOMER CARD T984889 FOUND ANGLE CORRODED BS 767-787 RBL 22 WL 158 / REMOVED AND REPLACED AFT CARGO BAY FWD ANGLE B/S 767-787 RBL 22 WL 158 IAW SRM 51-40-02 AND DWG 146A8123 REV -

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 55,298 hrs · 32,627 cycles

PASSENGER CABIN SEAT TRACK MECHANICALLY DAMAGED AT BS. 520, LBL 24.5. / REPAIRED SEAT TRACK IAW SRM AND DWG.

Part: FITTING — CORRODED (AFT FUSELAGE) · airframe 55,298 hrs · 32,627 cycles

***CORROSION*** ON WASTE DRAIN FITTING AT B.S. 997; STR.25L; W.L. 148. / NO ALLOWABLE LIMITS IN SRM. PART REPAIRED BY REPLACEMENT PER SRM 51-10-02. REMOVED AND REPLACED WASTE DRAIN FITTING BS 997 STR 25L WL 148 IAW SRM 51-40-02 AND DWG 147A7443.

Part: BRACKET — CRACKED (AFT CARGO) · airframe 55,298 hrs · 32,627 cycles

AFT CARGO BAY BULKHEAD SUPPORT BRACKET CRACKED BS 867 WL 160 LBL12 / REMOVED ACB BULKHEAD SUPPORT BRACKET CRACKED AT BS 867 WL 160 LBL 12. LOCATED AND DRILLED CLIP AND REINSTALLED NEW CLIP IAW SRM 51-40-02-0G-0; SRM 51-40-0G-0G-0; DWG 149A8102 ID:15 REV A 92954U 10/2/19 DWG 149A8104 REV

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 55,298 hrs · 32,627 cycles

PASSENGER CABIN SEAT TRACK MECHANICALLY DAMAGED AT BS. 520, LBL 45. / R&R SEAT TRACK IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 494 - 500A) · airframe 55,298 hrs · 32,627 cycles

FORWARD CARGO BAY AFT SHIELD CORRODED BETWEEN BS 494 - 500A, RBL 25. R&R SHIELD IAW SRM & DWG.

Part: RETAINER — CORRODED (CENTRE FUSELAGE) · airframe 55,298 hrs · 32,627 cycles

***CORROSION*** AREAS OF CORROSION ON FASTENERS ON LEFT OVERWING EXIT CUTOUT LOWER SEAL RETAINERS. / REMOVED AND REPLACED DAMAGED FASTENERS AND REPAIRED DAMAGED AREAS ON L/H OVERWING EXIT CUTOUT LOWER SEAL RETAINERS; AFT & CENTER IAW EA 19-05062 REV IR & EA -1753-35804 REV IR.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 55,298 hrs · 32,627 cycles

FLOOR SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO RBL 25. / R&R FLOOR SUPPORT PER SRM, DWG, AND MM.

Part: RETAINER — CORRODED (CENTRE FUSELAGE) · airframe 55,298 hrs · 32,627 cycles

***CORROSION*** AREAS OF CORROSION ON FASTENERS ON RIGHT OVERWING EXIT CUTOUT LOWER SEAL RETAINERS. / REMOVED AND REPLACED DAMAGED FASTENERS AND REPAIRED DAMAGED AREA ON R/H OVER USING EXIT CUTOUT LOWER SEAT RETAINER IAW EA 19-05068 REV IR. AND EA 1-753-35805. REV IR.

Part: SKIN — CORRODED (AFT FUSELAGE) · airframe 55,298 hrs · 32,627 cycles

***CORROSION*** MULTIPLE AREAS OF CORROSION ON FUSELAGE SKIN FROM BS 847 TO BS 1007; FROM S-2L TO S-2R; WL 306.5 / REPAIRED FUSELAGE SKIN B.S 847-1007 STR 2L- STR 2R W.L 306.5 IAW EA 1-753-35791 REV IR AND ATS ER 19-05054 REV IR

Part: SUPPORT — CORRODED (BS 727-847) · airframe 55,298 hrs · 32,627 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO 847, LBL 23. R&R SUPPORT IAW SRM & DWG.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 55,298 hrs · 32,627 cycles

AFT CARGO BAY FLOOR PNL T-STRAP HAS SPOTS OF CORROSION BS 772 W/L 158 RBL18-LBL18 / INSTALLED T-STRAP IN ACB AT BS 772; LBL 18 TO RBL 18 IAW B737 SRM 51-40-02.

Part: SUPPORT — CORRODED (BS 727C-767) · airframe 55,298 hrs · 32,627 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727C TO BS. 767, RBL 21. R&R SUPPORT IAW SRM & DWG.

Part: STUB FRAME — CRACKED · airframe 55,298 hrs · 32,627 cycles

UPPER FORWARD STUB FRAME CRACKED. / R&R STUB FRAME IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 767-787) · airframe 55,298 hrs · 32,627 cycles

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

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 55,298 hrs · 32,627 cycles

AFT CARGO BAY FLOOR PNL T-STRAP HAS SPOTS OF CORROSION BS 887 W/L 160 RBL18-LBL18 / REMOVED AND REPLACED NEW AFT CARGO BAY PNL T-STRAP BS 887 WL 160 RBL 18 - LBL 18 I.A.W SRM 51-40-02-0G-0; DWG 146A7500 ID:0061. REV:-; AND DWG 149A8104 ID:0001; REV:B

Part: SKATE ANGLE — CRACKED (BS 1106-1109) · airframe 55,298 hrs · 32,627 cycles

SKATE ANGLE CRACKED, BELOW VERTICAL FIN ON TOP OF FUSELAGE BETWEEN BS. 1106 TO BS. 1109, LBL 10. R&R SKATE ANGLE PER DWG, AMM, AND SRM.

Part: CAP — CRACKED (AFT CARGO COMPT) · airframe 55,298 hrs · 32,627 cycles

AFT CARGO BAY DOORWAY FWD NET HOLD DOWN CAP STRIP CRACKED / REMOVED AND REPLACED ACB DOORWAY CAP STRIP PER AMM 25-52-10-400-801. 92892U 10/12/19.

Part: WEB — CRACKED (AFT CARGO THRESH) · airframe 55,298 hrs · 32,627 cycles

ACB FWD DOOR SURROUND CLOSEOUT WEB IS CRACKED / REMOVED & REPLACED DOOR SURROUND IN ACB; FWD SURROUND IAW B737 SRM 51-40-02

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 55,298 hrs · 32,627 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED / ACCOMPLISHED REPAIR PER EA #1-A53-2076; REV 11

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,511 hrs · 32,122 cycles

EMERGENCY BATTERY PACK FAILED CAPACITANCE CHECK. R&R BATTERY PACK PER AMM.

Part: STIFFENER — CRACKED (RT WHEEL WELL) · airframe 54,504 hrs · 32,117 cycles

RT WHEEL WELL; RBL 24 VERTICAL STIFFENER CRACKED. / REMOVED AND REPLACED RT WHEEL WELL STIFFENER AT RBL 24 PER SRM 51-40-02

Part: STRINGER — CRACKED (RIGHT WING) · airframe 54,134 hrs · 31,880 cycles

ON THE RH WING JUST INBD OR PYLON FOUND AFT UPPER STRINGER CRACKED WS. 228.5 TO 204.5 / R&R STRINGER PER SRM 51-40-02.

Part: ACTUATOR — CRACKED (RT SPOILER) · airframe 53,391 hrs · 31,425 cycles

NR 12 GROUND SPOILER ACTUATOR CRACKED AND WAS LEAKING. R&R NR 12 GROUND SPOILER ACTUATOR PER AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 52,840 hrs · 31,087 cycles

L1 DOOR EVAC SLIDE FELL OUT OF CONTAINER, (DID NOT DEPLOY). R&R SLIDE ASSY PER MM.

Part: ENGINE — FOD (NR 1) · airframe 52,318 hrs · 30,748 cycles

NR 1 ENGINE VIBRATION WENT TO 5.0 IN CLIMB FROM FL340 TO FL360. RAN QRH AND REDUCED POWER TO 79% N1. ENGINE VIBRATION STABILIZED AT 3.9. FOUND FOD DAMAGE TO NR 1 ENGINE. R&R NR 1 ENGINE PER MT.

Part: SIGN — LOOSE (CABIN) · airframe 51,694 hrs · 30,336 cycles

MID CABIN CEILING EXIT SIGN LOOSE. SECURED SIGN PER SIP.

Part: LENS — MISSING (CABIN) · airframe 51,103 hrs · 29,945 cycles

R1 DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 51,103 hrs · 29,945 cycles

L1 DOOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW. INSTALLED LENS PER AMM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 50,269 hrs · 29,422 cycles

R1 DOOR SLIDE PRESSURE LOW. R & R THE SLIDE IAW AMM AND MT.

Part: ATTACH BRACKET — CRACKED (RT WHEEL WELL) · airframe 50,063 hrs · 29,290 cycles

RIGHT WING LANDING GEAR AREA UPPER WING PANEL FWD ATTACH BRACKET CRACKED ABOVE # 2 AFT BOOST PUMP / R/R BRACKET IAW SRM 51-40-02.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 50,063 hrs · 29,290 cycles

EMERGENCY LIGHTS BATTERY PACK M1675 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 50,063 hrs · 29,290 cycles

EMERGENCY LIGHTS BATTERY PACK M1670 FAILED A CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: SIGN — LOOSE (EMERGENCY LGIHTS) · airframe 49,855 hrs · 29,152 cycles

MID CABIN OVERHEAD OVERWING EXIT SIGN BROKEN LOOSE. REINSTALLED THE SIGN IAW MM.

Part: LIGHT — DETACHED (MID CABIN) · airframe 49,763 hrs · 29,097 cycles

MID CABIN EMERGENCY EXIT SIGN DETACHED ON LANDING. INSTALLED THE SIGN IAW AMM.

Part: ROPE — DISPLACED (CABIN) · airframe 48,844 hrs · 28,517 cycles

RT OVERWING EXIT ESCAPE ROPE DISPLACED. REPLACED ROPE IAW AMM.

Part: SEAT TRACK — CRACKED (FLIGHT DECK) · airframe 48,844 hrs · 28,517 cycles

COCKPIT FIRST OFFICER'S SEAT FWD INBD FLOOR TRACK IS CRACKED AT THE FWD END. / REMOVAL AND INSTALLED NEW FISRT OFFERS SEAT FWD INBD FLOOR TRACK IAW AMM 53-401-020-801 AND AMM 53-14-01-420-801 ATAG WN2793

Part: PLATE — CRACKED (LT WING) · airframe 48,844 hrs · 28,517 cycles

LEFT WING LOWER TRAILING EDGE; INBOARD OF #3 FLAP TRACK WAFFLE BOARD CRACKED AT FASTENER. / REMOVED AND REPLACED -3 WIGGLE PLATE ON LH WING LOWER TRAILING EDGE INBOARD OF #3 FLAP TRACK PER DWG 115A2001 REV A AND SRM 51-40-02-0G-0.

Part: ANGLE — CRACKED (LT WHEEL WELL) · airframe 48,844 hrs · 28,517 cycles

SWA TASK CARD # 14020-57; STEP 2D: L/H VERTICAL PRESSURE DECK WEB ATTACH ANGLE CRACKED AT INBOARD SIDE OF DRAIN HOLE. VERIFIED WITH HFEC. MARKED IN BLACK. 3 / REPAIRED L/H VERTICAL PRESSURE WEB ATTACH ANGLE AT I/B SIDE OF DRAIN HOLE AT BS 663; LBL 36; IAW EA# 170443 REV IR AND SWA EA# 1-757-14382 REV. IR.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 48,844 hrs · 28,517 cycles

AFT CARGO COMPARTMENT MOST FWD. R/H CAP STRIP CORRODED. / REMOVED AND REPLACED AFT CARGO MOST FWD R/H CAP STRIP IAW B737 SRM 51-40-02-0G-0 AND IPC 25-52-10-02

Part: PLATE — CRACKED (LT WING) · airframe 48,844 hrs · 28,517 cycles

LT WING LOWER TRAILING EDGE, ABOVE NR 3 FLAP TRACK WAFFLE BOARD CRACKED. R&R WIGGLE PLATE IAW DWG AND SRM.

Part: PLATE — CRACKED (LT WING) · airframe 48,844 hrs · 28,517 cycles

LT WING LOWER TRAILING EDGE, OUTBOARD OF NR 3 FLAP TRACK ORSS 261 WAFFLE BOARD CRACKED. R&R WIGGLE PLATE PER DWG AND SRM.

Part: PLATE — CRACKED (RT WING) · airframe 48,844 hrs · 28,517 cycles

RT WING LOWER TRAILING EDGE PANEL TO WING ATTACH WAFFLE PLATE CRACKED. R&R WAFFLE PLATE IAW SRM.

Part: RETAINER — CRACKED (RT WING) · airframe 48,844 hrs · 28,517 cycles

RIGHT WING; 10' INBOARD OF RIB DEFLECTOR; SEAL RETAINER IS CRACKED AT FASTENERS COMMON TO WEB. / REMOVED AND REPLACED WEB 10' INBD OF RIB DEFLECTOR REF DRW # 115A2930 REV- AND B737 SRM 51-40-02-0G-0 ATAG #S A31542; A07826

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 48,844 hrs · 28,517 cycles

LH HORIZONTAL STABILIZER FRONT SPAR UPPER SLIDING SEAL IS CRACKED AT CORNER PLATES. / REMOVED AND REPLACED LH HORIZ STAB FRONT APUR UPPER SLIDING SEAL IAW B737 AMM 53-31-31-400-802; AND AMM 53-31-31-000-802 ATAG: A11426; A48530; A31587

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 48,844 hrs · 28,517 cycles

RH HORIZONTAL STABILIZER FRONT SPAR UPPER SLIDING SEAL IS CRACKED AT CORNER PLATES. / REMOVED AND REPLACED RH STAB FRONT SPAR UPPER SLIDING SEAL IAW B737 AMM 53-31-400-802 AND AMM 53-31-31-000-802 ATAG: A29773

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 48,844 hrs · 28,517 cycles

_AFT CARGO DOOR FWD CORNER THRESHOLD CRACKED / ROUTED TO BACK SHOP AND REPAIRED ON WO# 36533-1600-0002 IAW SWA EA 1-A53-2076 REV 11

Part: ATTACH ANGLE — CRACKED (RT SPOILER) · airframe 48,844 hrs · 28,517 cycles

RT WING INBOARD OF NR 8 SPOILER ATTACH ANGLE COMMON TO RIB DEFLECTOR CRACKED. R&R ANGLE IAW SRM AND DWG.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 48,844 hrs · 28,517 cycles

__AFT CARGO DOOR AFT CORNER THRESHOLD CRACKED / ROUTED TO BACKSHOP FOR REPAIR WO # 36533-1600-0001 REPAIRED IAW SWA EA 1-A53-2076 REV 11

Part: PLATE — CRACKED (RT WING) · airframe 48,844 hrs · 28,517 cycles

RT WING LOWER TRAILING EDGE JUST OUTBOARD OF NR 6 FLAP TRACK PANEL TO WING ATTACH WAFFLE PLATE CRACKED. R&R WAFFLE PLATE IAW SRM AND DWG.

Part: PLATE — CRACKED (RT WING) · airframe 48,844 hrs · 28,517 cycles

RT WING LOWER TRAILING EDGE JUST INBOARD OF NR 6 FLAP TRACK PANEL TO WING ATTACH WAFFLE PLATE CRACKED. R&R WAFFLE PLATE IAW SRM AND DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 48,844 hrs · 28,517 cycles

RT WING CENTER SECTION REAR SPAR VERTICAL WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB IAW SRM.

Part: COVER — MISSING (CABIN) · airframe 48,413 hrs · 28,241 cycles

LT OVERWING EXIT DOOR LENS MISSING. INSTALLED COVER PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 48,222 hrs · 28,124 cycles

AFT GALLEY AREA EMERGENCY LIGHT FAILED CAPACITY FUNCTION CHECK. R&R BATTERY PACK PER AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 47,908 hrs · 27,943 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,756 hrs · 27,853 cycles

RT EXTERIOR LOWER FUSELAGE EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: FAN — OVERHEATED (E&E BAY) · airframe 47,602 hrs · 27,751 cycles

ELECTRICAL ODOR IN CABIN. R&R EQUIP COOLING EXHAUST NORMAL FAN PER MM.

Part: LENS — MISSING (EXIT SIGN) · airframe 44,520 hrs · 25,908 cycles

RT OVERWING EMERGENCY EXIT SIGN UPPER LENS MISSING AT ROW 12. INSTALLED LENS PER AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 42,488 hrs · 24,752 cycles

LEFT ABOVE EMER EXIT HATCH, EMER LIGHT INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,488 hrs · 24,752 cycles

RIGHT WING DOOR EMER EXIT LIGHT INOPERATIVE AT WING TO BODY FAIRING LOWER POSITION. R & R LIGHT IAW AMM.

Part: FITTING — CRACKED (TE FLAP) · airframe 42,488 hrs · 24,752 cycles

RIGHT WING INBD MID FLAP FITTING CRACKED. R & R FITTING IAW CMM & SRM.

Part: ELEVATOR — CRACKED (LEFT) · airframe 42,488 hrs · 24,752 cycles

LT LE ELEVATOR CRACKED. REPAIRED ELEVATOR IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

FORWARD CARGO COMPARTMENT WEB CRACKED, BETWEEN BS 400 - 420, STRINGER 26L. R & R WEB IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

INTERCOSTAL CRACKED AT BS 1016, BETWEEN LBL 20 - 30. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

PRESSURE BULKHEAD INTERCOSTAL CRACKED AT BS 1016, BETWEEN RBL 10 - 20. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

PRESSURE BULKHEAD INTERCOSTAL CRACKED AT BS 1016, BETWEEN BL 0 TO LBL 10. R & R INTERCOSTAL IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

TIE CLIP CRACKED AT BS 807, STRINGER 26R. R & R TIE CLIP IAW SRM & DWG.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 42,488 hrs · 24,752 cycles

LEFT HORIZONTAL STABILIZER, CRACKED ON INSPAR RIB VERTICAL STIFFENER, LOCATED AT STAB STATION 92.70, 20" FROM FRONT SPAR. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 42,488 hrs · 24,752 cycles

LEFT HORIZONTAL STABILIZER INSPAR RIB VERTICAL STIFFENER, CRACKED AT STAB STATION 92.70 & 29" FROM FRONT SPAR. REPAIRED STIFFENER IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

ANGLE CRACKED, BETWEEN BS 380 - 400, BL 0. R & R ANGLE IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

CHANNEL CRACKED AT BS 540, BETWEEN RBL 24.5 - 45.50. R & R CHANNEL IAW SRM & DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

AFT CARGO COMPARTMENT STRAP CORRODED AT BS 887, BETWEEN STRINGER 25R - 26L. R & R STRAP IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

ANGLE CRACKED, BETWEEN BS 500D - 520, BL 0. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

AFT CARGO COMPARTMENT, ANGLE CORRODED AT BS 947.5, BETWEEN STRINGER 25R TO 26L. R & R ANGLE IAW DWG & SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

BULKHEAD WEB CRACKED AT BS 663.75, LBL 17. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 42,488 hrs · 24,752 cycles

AFT FACE OF BULKHEAD AT MAIN WW VERTICAL ANGLE CRACKED AT BS 663.75, LBL 27. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

VERTICAL ANGLE CRACKED AT BS 663.75, RBL 27 AT AFT FACE BULKHEAD MAIN WW COMPARTMENT. R & R ANGLE IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

AFT CARGO COMPARTMENT FLOORBEAM INTERNAL STRUCTURE CORRODED AT BS 767+5, RBL 3. REPAIRED FLOORBEAM IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 500C, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

FLOOR STRUCTURE INNER CHORD CRACKED, BETWEEN BS 303.9, STRINGER 17L. R & R CHORD IAW SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

STRINGER CRACKED AT BS 540, STRINGER 23L. REPAIRED STRINGER IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 500B, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R GUSSET IAW SRM & DWG.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

FORWARD CARGO COMPARTMENT CHANNEL CRACKED AT BS 500A+5, STRINGER 26L. REPAIRED CHANNEL IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

FORWARD CARGO COMPARTMENT GUSSET, CRACKED AT BS 500D, STRINGER 19L. R & R GUSSET IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

FORWARD CARGO COMPARTMENT, WEB INTERCOSTAL CRACKED, BETWEEN BS 500 - 500A, STRINGER 26L. R & R INTERCOSTAL IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

FORWARD CARGO COMPARTMENT ANGLE, CRACKED AT BS 500A, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 500C, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 400, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

RIGHT AIR CONDITIONING BAY ON PNEUMATIC DUCT BRACKET, CRACKED AT BS 542. R & R BRACKET IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

FORWARD CARGO COMPARTMENT ANGLE CRACKED AT BS 500C, STRINGER 26R. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,488 hrs · 24,752 cycles

AFT CARGO COMPARTMENT CHANNEL SUPPORT, CRACKED AT BS 727, RBL 3. R & R SUPPORT IAW SRM & DWG.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 42,372 hrs · 24,690 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 41,973 hrs · 24,437 cycles

LEFT WING OTBD TE AFT FLAP INBD EDGE, LOWER CORNER DELAMINATED. R & R AFT FLAP IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,640 hrs · 24,244 cycles

LEFT OUTSIDE OVERWING EMER LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,034 hrs · 23,904 cycles

LEFT OVERWING EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 40,002 hrs · 23,311 cycles

L1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,707 hrs · 23,137 cycles

RIGHT EMER EXIT LIGHT FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 39,102 hrs · 22,792 cycles

LEFT OVERWING SIDE WALL EXIT LIGHT LENS BROKEN. R & R LENS IAW SIP.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 38,464 hrs · 22,409 cycles

L1 DOOR EMER EVAC SLIDE FELL OUT, DID NOT DEPLOY. R & R SLIDE MT.

Part: VALVE — MALFUNCTIONED (FUEL SYSTEM) · airframe 37,721 hrs · 22,004 cycles

FUEL CROSS FEED VLV CB TRIPPED. R & R FUEL CROSS FEED VLE ACTUATOR IAW MM.

Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 35,973 hrs · 20,971 cycles

FWD CABIN EMERGENCY FLASHLIGHT NOT CHARGING. R & R FLASHLIGHT IAW MM.

Part: FITTING — CRACKED (RT WING) · airframe 35,775 hrs · 20,850 cycles

RT WING INBD FIXED TE LOWER PANEL DEFLECTOR RIB CRACKED. R & R CLIP IAW SRM.

Part: RIB — CRACKED (LT WING) · airframe 35,775 hrs · 20,850 cycles

LT WING INBD FIXED TE LOWER PANEL DEFLECTOR RIB CRACKED. R & R RIB IAW SRM & DRAWING.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,775 hrs · 20,850 cycles

SEAT TRACK CRACKED AT STATION 727B, RBL 45.5. REPAIRED TRACK IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,775 hrs · 20,850 cycles

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

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 35,775 hrs · 20,850 cycles

FLOOR PANEL 242CF DELAMINATED. REPAIRED PANEL IAW SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,775 hrs · 20,850 cycles

RT LOWER BULKHEAD CHORD CRACKED AT BS 540, STRINGER 22R. REPAIRED CHORD IAW EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 35,775 hrs · 20,850 cycles

FLIGHT DECK LT NR 1 WINDOW FRAME UPPER OTBD CORNER CRACKED INTERNALLY & EXTERNALLY. REPAIRED DOUBLER IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,775 hrs · 20,850 cycles

RT HORIZONTAL STABILIZER AT RIB STATION 147.90 SKIN CRACKED. REPAIRED DOUBLER IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 35,775 hrs · 20,850 cycles

RT NR 3 FLIGHT DECK WINDOW FRAME CRACKED FWD POST SECOND FROM LOWER FASTENER HOLE. REPAIRED POST IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 35,775 hrs · 20,850 cycles

LT NR 3 WINDOW FWD POST SECOND FROM LOWER FASTENER HOLE CRACKED. REPAIRED POST IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,775 hrs · 20,850 cycles

LT HORIZONTAL STABILIZER SKIN CRACKED AT STATION 129.50. REPAIRED DOUBLER IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,775 hrs · 20,850 cycles

LT HORIZONTAL RIB STATION 147.90 SKIN CRACKED. REPAIRED DOUBLER IAW SRM.

Part: LENS — MISSING (CABIN) · airframe 35,775 hrs · 20,850 cycles

AFT GALLEY DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW AMM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 35,294 hrs · 20,574 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 34,514 hrs · 20,137 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 32,918 hrs · 19,190 cycles

EXTERNAL POWER DOOR CUTOUT, AFT LIP CRACKED OUT. INSTALLED PERMANENT REPAIR PER EA 1-A53-9269 AND TSR TRACKING 201300430.

Part: BATTERY — FAILED (CABIN) · airframe 32,918 hrs · 19,190 cycles

FORWARD RIGHT, AFT LEFT, AND LEFT OVERWING BATTERY PACKS FAILED TEST. REMOVED AND REPLACED BATTERIES PER M/M.

Part: LENS — LOOSE (EXIT SIGN) · airframe 32,809 hrs · 19,126 cycles

OVERWING EXIT SIGN ON RT WING WALL LOOSE LENS. RE-SECURED LIGHT LENS OVERWING EXIT SIGN ON RIGHT WING PER M/M.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 31,110 hrs · 18,074 cycles

L2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF HOLDER, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 30,282 hrs · 17,597 cycles

RT HORIZONTAL STAB LOWER SKIN CRACKED 79" OUTBOARD OF FUSELAGE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 30,282 hrs · 17,597 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED 96" OUTBOARD OF FUSELAGE. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 30,282 hrs · 17,597 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED 42" OUTBOARD OF FUSELAGE. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 29,999 hrs · 17,437 cycles

FWD EMERGENCY EXIT LIGHT LOOSE. RE-INSTALL LIGHT ASSY IAW MM.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 29,665 hrs · 17,237 cycles

OVERWING CEILING EMERGENCY EXIT SIGN IS LOOSE. SECURED SIGN IAW MM.

Part: COVER — MISSING (CABIN) · airframe 29,410 hrs · 17,092 cycles

EMERGENCY EXIT LIGHT COVER MISSING AT ROW 8. INSTALLED COVER PER MM.

Part: CHARGER — FAILED (CABIN) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT LAV EMERGENCY EXIT LIGHT FAILED TO ILLUMINATED DURING TEST. REMOVED AND REPLACED BATTERY CHARGER IAW MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR CUTOUT STUB FRAME CRACKED AT BS 294.5, RBL 54. REPAIRED FRAME IAW EA.

Part: LIGHT — CRACKED (CABIN) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS CRACKED BETWEEN BS 727C TO BS 807. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS CRACKED BETWEEN BS 807 TO BS 907. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS CRACKED BETWEEN BS 360 TO BS 420. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS CRACKED BETWEEN BS 706 TO BS 727C. REMOVED AND REPLACED EEPLS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 29,381 hrs · 17,075 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 29,381 hrs · 17,075 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT LOWER EEPLS INOP. REMOVED AND REPLACED BULB IAW MM.

Part: LIGHT — CRACKED (CABIN) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS CRACKED BETWEEN BS 597 TO BS 706. REMOVED AND REPLACED EEPLS PER MM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CLIP CRACKED AT BS 294.5, RBL 54. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD CARGO COMPARTMENT Z-ANGLE CORRODED AT BS 272C+10, STR 47L. REPAIRED Z-ANGLE IAW SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS CRACKED BETWEEN BS 500C TO BS 597. REMOVED AND REPLACED EEPLS PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO COMPARTMENT RT Z-ANGLE CORRODED BETWEEN BS 727D+4 TO BS 767. REPAIRED Z-ANGLE PER SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND EEPLS CRACKED BETWEEN BS 420 TO BS 500C. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND G4 GALLEY EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: ANGLE — PUNCTURED (FUSELAGE) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO COMPARTMENT RT FWD Z-ANGLE PUNCTURED AT BS 747. REMOVED AND REPLACED Z-ANGLE PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND R2 DOOR CREASE BEAM CORRODED BETWEEN BS 305 TO BS 325. REPAIRED BEAM IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR CREASE BEAM ANGLE CORRODED ON UPPER SURFACE. REMOVED AND REPLACED ANGLE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND R1 DOORWAY CREASE BEAM VERTICAL FLANGE CORRODED AT BS 312+8. REMOVED AND REPLACED BEAM IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,381 hrs · 17,075 cycles

DURING SCHEDULED 8Y CHECK, FOUND R2 DOOR CREASE BEAM CORRODED BETWEEN BS 947+10 TO BS 995. REMOVED AND REPLACED BEAM IAW SRM AND MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 28,804 hrs · 16,726 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,804 hrs · 16,726 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. RELAMPED PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,804 hrs · 16,726 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY LIGHT INOPERATIVE AT ROW 16. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,615 hrs · 16,049 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS INOP AT ROW 16. REMOVED AND REPLACED COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 16,049 hrs · 27,615 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: HOLDER — LOOSE (GIRT BAR) · airframe 26,825 hrs · 15,601 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. SECURED HOLDER ASSY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 26,593 hrs · 15,467 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 26,404 hrs · 15,365 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 13 TO ROW 23. REMOVED AND REPLACED COVER PER MM.

Part: LENS — CRACKED (CABIN) · airframe 26,404 hrs · 15,365 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LENS CRACKED BETWEEN ROW 3 TO ROW 9. REMOVED AND REPLACED COVER PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 25,945 hrs · 15,097 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EMERGENCY EXIT LIGHT WIRE LOOSE AT ROW 11. SECURED WIRE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 25,937 hrs · 15,090 cycles

FWD EEPLS LOOSE AT ROW 2. REPAIRED EEPLS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 25,931 hrs · 15,086 cycles

EEPLS COVER LOOSE. SECURED COVER PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 25,664 hrs · 14,915 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: COVER — MISSING (CABIN) · airframe 25,627 hrs · 14,893 cycles

FWD EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: HOLDER — LOOSE (GIRT BAR) · airframe 25,498 hrs · 14,809 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. SECURED HOLDER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 25,362 hrs · 14,721 cycles

LT EEPLS LOOSE AT ROW 1. SECURED LENS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 25,362 hrs · 14,721 cycles

FWD EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 25,142 hrs · 14,590 cycles

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

Part: COVER — MISSING (CABIN) · airframe 24,694 hrs · 14,331 cycles

EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 23,658 hrs · 13,726 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MT.

Part: LENS — MISSING (CABIN) · airframe 23,542 hrs · 13,664 cycles

RT OVERWING LOWER EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,250 hrs · 13,493 cycles

FWD EEPLS BULB INOP. REMOVED AND REPLACED BULB PER MM.

Part: COVER — CRACKED (CABIN) · airframe 23,068 hrs · 13,389 cycles

DURING SCHEDULED CV CHECK, FOUND FWD EEPLS COVERS CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 23,008 hrs · 13,353 cycles

EMERGENCY EXIT LIGHT COVER LOOSE AT EXIT ROW. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 22,719 hrs · 13,175 cycles

LT EEPLS LENS MISSING AT ROW 11. REMOVED AND REPLACED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 22,516 hrs · 13,059 cycles

DURING SCHEDULED 6Y CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 13 TO ROW 14. REMOVED AND REPLACED COVER PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 22,516 hrs · 13,059 cycles

DURING SCHEDULED 6Y CHECK, FOUND LT EEPLS LOOSE BETWEEN ROW 11 TO ROW 16. SECURED WIRE PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 22,516 hrs · 13,059 cycles

DURING SCHEDULED 6Y CHECK FOUND, SHEAR TIE CRACKED AT BS 540, RBL 14. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 22,516 hrs · 13,059 cycles

DURING SCHEDULED 6Y CHECK FOUND, SHEAR TIE CRACKED AT BS 540, LBL 14. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: LENS — BROKEN (CABIN) · airframe 22,223 hrs · 12,885 cycles

LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,131 hrs · 11,591 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP BETWEEN ROW 2 TO ROW 4. RELAMPED EMERGENCY LIGHT PER MM.

Part: COVER — WORN (CABIN) · airframe 19,810 hrs · 11,398 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS LIGHT COVER WORN AT ROW 6. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 19,810 hrs · 11,398 cycles

DURING SCHEDULED HC2 CHECK, RT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 19,810 hrs · 11,398 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 19,528 hrs · 11,217 cycles

L1 DOOR SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REINSTALLED SLIDE ASSY PER MT.

Part: LENS — BROKEN (CABIN) · airframe 18,971 hrs · 10,872 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 18,522 hrs · 10,597 cycles

FOUND R1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: ESCAPE ROPE — MISSING (CABIN) · airframe 17,413 hrs · 9,913 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY ESCAPE ROPE MISSING. INSTALLED ESCAPE ROPE PER MM.

Part: ESCAPE ROPE — MISSING (CABIN) · airframe 17,413 hrs · 9,913 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT OVERWING EMERGENCY ESCAPE ROPE MISSING. INSTALLED ESCAPE ROPE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 15,997 hrs · 9,097 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 13,811 hrs · 7,815 cycles

FLIGHT DECK R2 WINDOW ARCED. REMOVED AND REPLACED R2 WINDOW AND CONTROLLER PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 12,328 hrs · 6,956 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 2 ABC. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 10,813 hrs · 6,075 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 7,382 hrs · 4,073 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS TRACK COVERS CRACKED BETWEEN ROW 1 TO ROW 11. REMOVED AND REPLACED COVERS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 6,010 hrs · 3,324 cycles

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

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 5,989 hrs · 3,309 cycles

R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 5,956 hrs · 3,291 cycles

CABIN EEPLS LENS LOOSE AT FWD END. SECURED LENS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 4,406 hrs · 2,458 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD END OF EEPLS INOP. REMOVED AND REPLACED EEPLS BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 3,529 hrs · 1,968 cycles

R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.