N8608N

Part: ANGLE — CRACKED (ZONE 500) · airframe 42,858 hrs · 20,627 cycles

LEFT WING OTBD ANGLE UNDER UPPER INBD FIXED TRAILING EDGE PANEL CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-0G-0-B00069.

Part: LENS — WRONG PART (ZONE 200) · airframe 40,816 hrs · 19,544 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS DOESNT MATCH<[01] R&R L1 DOOR EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01

Part: LENS — WRONG PART (ZONE 200) · airframe 40,816 hrs · 19,544 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS DOESNT MATCH<[01] R&R R1 DOOR EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01

Part: HANDLE — OUT OF ADJUST (ZONE 800) · airframe 40,188 hrs · 19,212 cycles

CR RR R2 DOOR ASSIST HANDLE AIRFRAME SIDE NEEDS SECURED. <[01] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 25-21-420-801; [02] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 25-21-420-801; [03] SECURED R2 DOOR ASSIST HANDLE IAW B737-800 AMM 25-21-420-801.

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 40,188 hrs · 19,212 cycles

FORWARD RIGHT-HAND EMERGENCY LIGHTS INOP <[01]. REMOVED AND REPLACED FORWARD R/H BATTERY PACK M02816 AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-805.; [02] REMOVED AND REPLACED FORWARD R/H BATTERY PACK M02816 AND OPS CHECK GOOD IAW B737-800 AMM 33-51-06-960-80.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H CRACKED P/N 143A7502-154<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H P/N 143A7502-154 PO: 1112648.1 IAW DWG 143A7505 REV - AND B737-800 SRM 51-40-02;[02] VERIFIED REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H P/N 143A7502-154 PO: 1112648.1 IAW DWG 143A7505 REV - AND B737-800 SRM 51-40-02

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

FWD CARGO COMPARTMENT INTERCOSTAL CLIP STA 500H R/H CRACKED P/N#143A7502-158<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL CLIPS STA 500H R/H WITH NEW PN: 143A7502U158 PO: 1112667.1 AND PN:143A7502U154 PO: 1112648.1 IAW DWG 143A7505 REV - AND B737-800 SRM 51-40-02;[02] VERIFEID REMOVED AND REPLACED FWD CARGO COMPARTMENT INTERCOSTAL CLIPS STA 500H R/H WITH NEW PN: 143A7502U158 PO: 1112667.1 AND PN:143A7502U154 PO: 1112648.1 IAW DWG 143A7505 REV - AND B737-800 SRM 51-40-02

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

FWD CARGO COMPARTMENT R/H TRANSITION PANEL CORRODED AT FASTENER HOLES THROUGHOUT FROM STA 500C TO STA 500I<[01] EVALUATED FWD CARGO COMPARTMENT R/H TRANSITION PANEL FROM STA 500C TO STA 500I; ORIG. MAT. THK. 0.040'; MATERIAL REMOVED 100% AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 REMOVED AND FABRICATED NEW TRANSITION PANEL IAW B 737-800 SRM 53-00-53-2R-REPAIR 5 AND INSTALLED IAW B737-800 SRM 51-40-02; SRM 53-00-53-2R REPAIR 5.;[02] VERIFIED EVALUATED FWD CARGO COMPARTMENT R/H TRANSITION PANEL FROM STA 500C TO STA 500I; ORIG. MAT. THK. 0.040'; MATERIAL REMOVED 100% AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 REMOVED AND FABRICATED NEW TRANSITION PANEL IAW B 737-800 SRM 53-00-53-2R-REPAIR 5 AND INSTALLED IAW B737-800 SRM 51-40-02; SRM 53-00-53-2R REPAIR 5.;[03] VERIFIED EVALUATED FWD CARGO COMPARTMENT R/H TRANSITION PANEL FROM STA 500C TO STA 500I; ORIG. MAT. THK. 0.040'; MATERIAL REMOVED 100% AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 REMOVED AND FABRICATED NEW TRANSITION PANEL IAW B 737-800 SRM 53-00-53-2R-REPAIR 5 AND INSTALLED IAW B737-800 SRM 51-40-02; SRM 53-00-53-2R REPAIR 5.

Part: BAFFLE — CRACKED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

FWD CARGO COMPARTMENT INTERCOSTAL/BAFFLE STA 500F - STA 500G R/H CRACKED (DOT K570) <[01]. REMOVED AND REPLACED BAFFLE STA 500F IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A7510 REV: B AND REPAIRED IAW 51-70-13-2R-1.; [02] VERIFIED: REMOVED AND REPLACED BAFFLE STA 500F IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A7510 REV: B AND REPAIRED IAW 51-70-13-2R-1.; [03] VERIFIED: REMOVED AND REPLACED BAFFLE STA 500F IAW B737-800 SRM 51-40-02 AND BOEING DWG 143A7510 REV: B AND REPAIRED IAW 51-70-13-2R-1.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

FWD CARGO COMPARTMENT INTERCOSTAL STA 500D - STA 500E R/H CRACKED (DOT K569)<[01] REMOVED FWD CARGO COMPARTMENT INTERCOSTAL AT STA 500D - STA 500E R/H IAW B737-800 SRM 51-40-02; RECEIVED NEW PART P/N: 143A7510-22 BAFFLE ASSEMBLY; P.O: 1112649.1 IAW BAC DWG 143A7510 REV. B; LOCATED & DRILLED IAW B737-800 SRM 51-40-05 AND BAC DWG 143A7510 REV. B AND INSTALLED IAW B737-800 SRM 51-40-02 & BAC DWG 143A7510 REV. B.;[02] COMPLIED WITH FWD CARGO COMPARTMENT INTERCOSTAL STA 500D - STA 500E R/H CRACKED

Part: FRAME — CRACKED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

(CR - VERNON) FOUND FRAME CRACK AT STA 312 BETWEEN S-5L AND S-6L ABOVE L-1 DOOR<[01] REMOVED DAMAGE; FORMED; LOCATED; DRILLED; HFEC CUT OUT; OPEN HOLES AND FPI FORMED ANGLE; NO DEFECTS NOTED; ALODINED; PRIMED; INSTALLED REPAIR ANGLE; AND CIC REF B737-NG SRM 53-10-07-2R-1; THIS IS A CAT B REPAIR - THRESHOLD 50;000 CYC INSPECTION THRESHOLD; 12;000 CYC REPEAT HFEC FROM MANUFACTURED DATE.; [02] VERIFIED REMOVED DAMAGE; FORMED; LOCATED; DRILLED ANGLE; HFEC CUT OUT; OPEN HOLES AND FPI FORMED ANGLE; NO DEFECTS NOTED; ALODINE; PRIMED; INSTALLED REPAIR ANGLE; AND CIC REF B737-NG SRM 53-10-07-2R-1; THIS IS A CAT B REPAIR - THRESHOLD 50;000 CYC INSPECTION THRESHOLD; 12;000 CYC REPEAT HFEC FROM MANUFACTURED DATE; [03] VERIFIED REMOVED DAMAGE; FORMED; LOCATED; DRILLED ANGLE; HFEC CUT OUT; OPEN HOLES AND FPI FORMED ANGLE; NO DEFECTS NOTED; ALODINE; PRIMED; INSTALLED REPAIR ANGLE; AND CIC REF B737-NG SRM 53-10-07-2R-1; THIS IS A CAT B REPAIR - THRESHOLD 50;000 CYC INSPECTION THRESHOLD; 12;000 CYC REPEAT HFEC FROM MANUFACTURED DATE.

Part: SPLICE STRAP — CORRODED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

[DOT: B727] AFT CARGO FLOOR AT STA 847; RBL 19 HAS RAIL SPLICE STRAP CORRODED AS MARKED.<[01] REMOVED AND REPLACED NEW STRAP IAE B737-800 SRM 51-40-02 AAND BAC DWG 146A8120 REV A.;[02] VERIFIED REMOVED AND REPLACED NEW STRAP IAE B737-800 SRM 51-40-02 AAND BAC DWG 146A8120 REV A.;[03] VERIFIED REMOVED AND REPLACED NEW STRAP IAE B737-800 SRM 51-40-02 AAND BAC DWG 146A8120 REV A.

Part: TRANSITION PANEL — CORRODED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

[DOT: Z042] AFT CARGO FLOOR FROM FWD BULKHEAD TO STA 767; RIGHT TRANSITION PANEL CORRODED NUMEROUS PLACES AS MARKED. <[01] REMOVED CORROSION FROM R/H TRANSITION PANEL AT STA 727-STA767 ORIGINAL MATERIAL THICK .040 IAW BAC 1496-377. MATERIAL LOST FROM SAT 727-STA 727+10 .003 AND REMAINS THICK. .037 FOUND TO BE WITHIN LIMITS. ALODINED AND PRIMED IAW B737-800 SRM 51-20-01. FROM 727E+10-STA 767 MATERIAL LOST .020 AND REMAINING THICK. .020 FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 ; REMOVED TRANSITION PANEL FROM STA 727E+10 - STA767 AND REPAIRED IAW B737-800 SRM 53-00-53-2R-REPAIR 5 AND INSTALLED IAW B737-800 SRM 51-40-02 AND VBAC DWG 146A7500 REV:B.[03] VERIFIED REMOVED CORROSION FROM R/H TRANSITION PANEL AT STA 727-STA767 ORIGINAL MATERIAL THICK .040 IAW BAC 1496-377. MATERIAL LOST FROM SAT 727-STA 727+10 .003 AND REMAINS THICK. .037 FOUND TO BE WITHIN LIMITS. ALODINED AND PRIMED IAW B737-800 SRM 51-20-01. FROM 727E+10-STA 767 MATERIAL LOST .020 AND REMAINING THICK. .020 FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2 ; REMOVED TRANSITION PANEL FROM STA 727E+10 - STA767 AND REPAIRED IAW B737-800 SRM 53-00-53-2R-REPAIR 5 AND INSTALLED IAW B737-800 SRM 51-40-02 AND VBAC DWG 146A7500 REV:B.

Part: PANEL — CORRODED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

[DOT: Z041] AFT CARGO FLOOR BETWEEN STA 727C AND STA 807; LEFT TRANSITION PANEL CORRODED NUMEROUS PLACES AS MARKED. <FOUND TO BE OUT OF LIMITS ORGINAL MATERIAL IS 0.040IN AND THE MATERIAL REMOVED IS 0.007IN; THE NEW MATERIAL THICKNESS IS 0.033IN. FROM STA 737 TO STA 807 THE TRANSITION PANEL IS FOUND TO BE WITHIN LIMITS. THE ORGINAL MATERIAL IS 0.040IN; THE MATERIAL REMOVED IS 0.003IN AND THE NEW MATERIAL THICKNESS IS 0.037 IAW B737-800 SRM 53-00-53-1A-2. TOOL NUM: T8224L CAL DUE DATE: 02 DEC 25. REMOVED DAMAGED PART OF LEFT TRANSITION PANEL STA 727A TO STA 737 IAW B737-800 SRM 53-00-53-2R-5 AND SRM 51-40-02. APPLIED ALODINE IN LEFT TRANSITION PANEL STA 737 TO STA 807 IAW B737-800 SRM 51-20-01. APPLIED PRIMER IN LEFT TRANSITION PANEL STA 737 TO STA 807 IAW B737-800 SRM 51-20-01. RECEIVED NEW PART # BAC 1496-377 7075-T62 P.O # 1108010.1 PER B737-800 SRM 53-00-53-2R-5. FARBRICATED NEW L/H TRANSITION PANEL IAW B737-800 SRM 53-00-53-2R-5. PRIMED L/H TRANSITION PANEL IAW B737-800 SRM 53-00-53-2R-5. INSTALLED NEW L/H TRANSITION PANEL IAW B737-800 SRM 53-00-53-2R-5.

Part: ANGLE — CORRODED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

[DOT: B726] AFT CARGO FLOOR BETWEEN STA 767 AND STA 793; RIGHT SUPPORT Z-ANGLE CORRODED AS MARKED.<[01] REMOVED AND REPLACED &NBSP;&NBSP;&NBSP;&NBSP;&NBSP;AFT CARGO FLOOR BETWEEN STA 767 AND STA 793; RIGHT SUPPORT Z-ANGLE REQUIRES INSTALLATION WITH NEW PN:1468127U12 IAW B737-800 SRM 51-40-02 AND DWG 146A0081 REV: A;[02] VERIFIED REMOVED AND REPLACED AFT CARGO FLOOR BETWEEN STA 767 AND STA 793; RIGHT SUPPORT Z-ANGLE REQUIRES INSTALLATION WITH NEW PN:1468127U12 IAW B737-800 SRM 51-40-02 AND DWG 146A0081 REV: A;[03] VERIFIED REMOVED AND REPLACED AFT CARGO FLOOR BETWEEN STA 767 AND STA 793; RIGHT SUPPORT Z-ANGLE REQUIRES INSTALLATION WITH NEW PN:1468127U12 IAW B737-800 SRM 51-40-02 AND DWG 146A0081 REV: A

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 40,188 hrs · 19,212 cycles

MAIN CABIN FWD WET AREA INTERCOSTA AT STA.294.5-312 BL0 IS CORR0DED <[01]. REMOVED DAMAGE; ORIG. .063; MATERIAL LOSS .063; REMAINING 0.0; FOUND TO BE OUT OF LIMITS REF B737-NG SRM 53-10-51-1A-1 FIG 105 DETAIL A; REMOVED ALL FASTENERS COMMON TO INTERCOSTAL IAW B737-800 SRM 51-40-02; LOCATED AND DRILLED NEW INTERCOSTAL IAW B737-800 SRM 51-40-06 AND BOEING DWG 141A5600 REV: N. ; INSTALLED NEW INTERCOSTAL P/N 141A5690U1 P.O#0; AT STA.294.5-312 BL0; REF. B737-800 SRM 51-40-02; BOEING DWG 141A5600 REV: N.; [02] VERIFIED REMOVED DAMAGE; ORIG. .063; MATERIAL LOSS .063; REMAINING 0.0; FOUND TO BE OUT OF LIMITS REF B737-NG SRM 53-10-51-1A-1 FIG 105 DETAIL A; REMOVED ALL FASTENERS COMMON TO INTERCOSTAL IAW B737-800 SRM 51-40-02; LOCATED AND DRILLED NEW INTERCOSTAL IAW B737-800 SRM 51-40-06 AND BOEING DWG 141A5600 REV: N. ; INSTALLED NEW INTERCOSTAL P/N 141A5690U1 P.O#0; AT STA.294.5-312 BL0; REF. B737-800 SRM 51-40-02; BOEING DWG 141A5600 REV: N.;[03] VERIFIED REMOVED DAMAGE; ORIG. .063; MATERIAL LOSS .063; REMAINING 0.0; FOUND TO BE OUT OF LIMITS REF B737-NG SRM 53-10-51-1A-1 FIG 105 DETAIL A; REMOVED ALL FASTENERS COMMON TO INTERCOSTAL IAW B737-800 SRM 51-40-02; LOCATED AND DRILLED NEW INTERCOSTAL IAW B737-800 SRM 51-40-06 AND BOEING DWG 141A5600 REV: N. ; INSTALLED NEW INTERCOSTAL P/N 141A5690U1 P.O#0; AT STA.294.5-312 BL0; REF. B737-800 SRM 51-40-02; BOEING DWG 141A5600 REV: N.

Part: PANEL — CORRODED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

FWD PIT TRANSITON PANELS CORRODED AT FASTENER HOLES FROM STA 500C TO 500I <[01]. L/H TRANSITION PANEL FROM STA 500C TO STA 500I EVALUATED ORIG. MAT. THK. = 0.040'; RMV. MAT. = 0.040'; REM. MAT. THK.= 0.00' AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2; TOOL I.D T8224L; CAL. DUE DATE: 02/DEC/25. REMOVED; FABRICATED REPAIR PARTS USING BAC1496-444 7075-T6; PO: 1107340.1; APPLIED ALODINE; PRIMER; CIC; INSTALLED NUTPLATES AND INSTALLED TO AIRCRAFT IAW B737-800 SRM 53-00-53-2R-5. & BAC DWG 1496-444.;[02] VERIFIED L/H TRANSITION PANEL FROM STA 500C TO STA 500I EVALUATED ORIG. MAT. THK. = 0.040'; RMV. MAT. = 0.040'; REM. MAT. THK.= 0.00' AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2; TOOL I.D T8224L; CAL. DUE DATE: 02/DEC/25. REMOVED; FABRICATED REPAIR PARTS USING BAC1496-444 7075-T6; PO: 1107340.1; APPLIED ALODINE; PRIMER; CIC; INSTALLED NUTPLATES AND INSTALLED TO AIRCRAFT IAW B737-800 SRM 53-00-53-2R-5. & BAC DWG 1496-444.;[03] VERIFIED L/H TRANSITION PANEL FROM STA 500C TO STA 500I EVALUATED ORIG. MAT. THK. = 0.040'; RMV. MAT. = 0.040'; REM. MAT. THK.= 0.00' AND FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-2; TOOL I.D T8224L; CAL. DUE DATE: 02/DEC/25. REMOVED; FABRICATED REPAIR PARTS USING BAC1496-444 7075-T6; PO: 1107340.1; APPLIED ALODINE; PRIMER; CIC; INSTALLED NUTPLATES AND INSTALLED TO AIRCRAFT IAW B737-800 SRM 53-00-53-2R-5. & BAC DWG 1496-444.

Part: SEAL — CRACKED (ZONE 300) · airframe 40,188 hrs · 19,212 cycles

R-HORIZONTAL UPPER SLIDING SEAL CRACKED DOT# J149 <[01] REMOVED; LOCATED; DRILLED; AND INSTALLED NEW R/H HORIZONTAL UPPER SLIDING SEAL REF B737-NG AMM 53-31-31-400-802; [02] REMOVED; LOCATED; DRILLED; AND INSTALLED NEW R/H HORIZONTAL UPPER SLIDING SEAL REF B737-NG AMM 53-31-31-400-802.

Part: TAIL CONE — CRACKED (ZONE 600) · airframe 40,188 hrs · 19,212 cycles

R-WING FLAP FAIRING #6 AT TAILCONE IS CRACKED AND HAS A HOLE DOT# J148 <[01]. REPAIRED RH WING TAILCONE ON FLAP FAIRING #6 IAW 737-800 SRM 51-70-04-2R-1 REPAIR 1 AND APPLIED TOUCH UP PAINT IAW 737-800 AMM 51-21-99-300-802; [02] REPAIRED RH WING TAILCONE ON FLAP FAIRING #6 IAW 737-800 SRM 51-70-04-2R-1 REPAIR 1 AND APPLIED TOUCH UP PAINT IAW 737-800 AMM 51-21-99-300-802.

Part: SEAL — CRACKED (ZONE 300) · airframe 40,188 hrs · 19,212 cycles

L/H HORIZ. STAB TRAILING EDGE; UPPER BLADE SEAL DELAMINATED APPROX. EL STA. 155. <[01] REMOVED AND REPLACED BLADE SEAL P/N 185A1621-115 PO 1111955.1 REF BAC DWG 180A1659 REV A TOOL SCREW GUN T03835-203 DUE 03 JUN 25; [02] REMOVED AND REPLACED BLADE SEAL P/N 185A1621-115 PO 1111955.1 REF BAC DWG 180A1659 REV A TOOL SCREW GUN T03835-203 DUE 03 JUN 25.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-45. <[01] MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-45. EVALUATED DAMAGE AND FOUND OUT OF LIMITS IAW B737-800 SRM 53-10-51-1A-1 AND BOEING DWG 141A5770 REV:A; DAMAGE DEPTH: 0.044' ORIGINAL THICKNESS: 0.080'; REMOVED FLOOR SUPPORT IAW B737-800 SRM 51-40-02; RECEIVED NEW PART P/N: 141A5770U3 INTERCOSTAL; PO: 0 IAW B737-800 IPC 53-42-11-44; LOCATED & DRILLED IAW B737-800 SRM 51-40-05 & BAC DWG 141A5730 REV. A. AND INSTALLED IAW B737-800 SRM 51-40-02 & BAC DWG 141A5730 REV. A; [04] VERIFIED MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-45. EVALU

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 40,188 hrs · 19,212 cycles

AFT WET AREA BS 967 TO 987 LBL 15 +/- INTERCOSTAL CORRODED AS MARKED. <[01] REMOVED DAMGED ON LBL 15 +/- INTERCOSTAL STA 967-987 FOUND TO BE OUT OF LIMITS IAW B737-800 53-70-51-1A-1; BOEING DWG 147A5676 REV:M ORGINAL THICKNESS:.075 REMAINING THICKNESS .064 MATERIAL REMOVED: .11 MAXIUM ALLOWED MATERIAL REMOVED: 10% (.0075). REMOVED AND INSTALLED NEW INTERCOSTAL IAW B 737-800 SRM 51-40-02 AND BAC DWG 140A9872 REV: K.; [02] VERIFIED REMOVED DAMGED ON LBL 15 +/- INTERCOSTAL STA 967-987 FOUND TO BE OUT OF LIMITS IAW B737-800 53-70-51-1A-1; BOEING DWG 147A5676 REV:M ORGINAL THICKNESS:.075 REMAINING THICKNESS .064 MATERIAL REMOVED: .11 MAXIUM ALLOWED MATERIAL REMOVED: 10% (.0075). REMOVED AND INSTALLED NEW INTERCOSTAL IAW B 737-800 SRM 51-40-02 AND BAC DWG 140A9872 REV: K.

Part: WEB — CORRODED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

AFT WET AREA; BS 947 RBL 52 TO LBL 5 +/- FLOORBEAM T CAP CORRODED. WIDE SPREAD AND AS MARKED.<[01] REMOVED DAMAGE; ORIG. .180; MATERIAL LOSS .090. REMAINING .090; FOUND TO BE OUT OF LIMITS REF B737-NG SRM 53-70-51-1A-1 FIG 104 DETAIL C; ACCOMP. HFEC TRIMMED EDGES & ALL HOLES COMMON TO UPPER CHORD IN WEB. PER MX REQUEST; IAW B737 NDT MAN. 51-00-00 PROC 23 & 16; PT6.NO CRACK INDICATIONS FOUND. #T8257F . DUE 13 MAY 25.; MATERIAL I'D FOR -1 T-CHORD 53700002-001 PO 1111889.1; -2 ANGLES BAC1490-2885 7075-T62 CLAD PO 1099692.2; AND -3 STRAPS 7075-T6 .125 ALUMINUM SHEET CLAD PO 1106304.1 REF B737-NG SRM 53-70-51-2R-5 TABLE 201 AND SWA DWG 53700002 REV A; APPLIED ALODINE ON REPAIR PARTS -1 T-CHORD; -2 ANGLES; -3 STRAPS REF B737-NG SRM 53-70-51-2R-5; SRM 51-20-01. OK TO INSTALL REPAIR PARTS -1 T-CHORD; -2 ANGLES; -3 STRAPS; INSTALLED REPAIR PARTS -1 T-CHORD; -2 ANGLES; -3 STRAPS REF B737-NG SRM 53-70-51-2R-5; REMOVED AND INSTALLED INTERCOSTAL AND FLOOR SUPPORTS REQUIRED FOR REPAIR REF B737-NG SRM 51-40-02;[02] APPLIED PRIMER ON REPAIR PARTS -1 T-CHORD; -2 ANGLES; -3 STRAPS REF B737-NG SRM 53-70-51-2R-5; SOPM20-41-02. OK TO INSTALL REPAIR PARTS -1 T-CHORD; -2 ANGLES; -3 STRAPS; INSTALLED REPAIR PARTS -1 T-CHORD; -2 ANGLES; -3 STRAPS REF B737-NG SRM 53-70-51-2R-5; REMOVED AND INSTALLED INTERCOSTAL AND FLOOR SUPPORTS REQUIRED FOR REPAIR REF B737-NG SRM 51-40-02. VERIFIED WORK AND WORK STEPS.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,188 hrs · 19,212 cycles

AFT WET AREA; BS 995 LBL 38 +/- WEB CORRODED AT FASTENER. AS MARKED. <[01] REMOVED AND REPLACED FLOOR SUPPORT PN:147A5710U1 AT STA. 995 LBL 38. IAW B737-800 SRM 51-40-02 AND BOEING DWG. NO. 147A5700 REV:A; [02] REMOVED AND REPLACED FLOOR SUPPORT PN:147A5710U1 AT STA. 995 LBL 38. IAW B737-800 SRM 51-40-02 AND BOEING DWG. NO. 147A5700 REV:A.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

AFT WET AREA; BS 987 LBL 47 +/- FLOORBEAM T CAP CORRODED AT DOME NUT FASTENER. AS MARKED. <[01] REMOVED CORROSION FROM AFT WET AREA; BS 987 LBL 47 +/- FLOOR BEAM T CAP AT DOME NUT FASTENER IAW B 737-800 SRM 51-10-02; ORIGINAL MATERIAL THICK. 0.150 IAW BAC 1518-1211 MAXIMUM MATERIAL REMOVED .021 MATERIAL REMAINING 0.129 FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. ; CUT OUT DAMAGED IAW B737-NG SRM 53-70-51-2R-6.; ACCOMP. HFEC AREA & TRIM OUT IAW B737 NDT MAN. 51-00-00 PROC. 23; PT6. NO CRACK INDICATIONS FOUND. ; PERFORMED DVI AT THE REPAIR AREA IAW B737-NG SRM 53-70-51-2R-6; NO DEFECTS NOTED.; SHOT PEENED AREA IAW B737-NG SRM 53-70-51-2R-6 AND SRM 51-20-06-0G-0; FABRICATED; LOCATED; DRILLED AND INSTALLED REPAIR PARTS -1 STRAP; -2 ANGLE; AND -3 FILLER REF B737-NG SRM 53-70-51-2R-6.;;[02PERFORMED DVI AT THE REPAIR AREA IAW B737-NG SRM 53-70-51-2R-6; NO DEFECTS NOTED.;; SHOT PEENED AREA IAW B737-NG SRM 53-70-51-2R-6 AND SRM 51-20-06-0G-0; FABRICATED; LOCATED; DRILLED AND INSTALLED REPAIR PARTS -1 STRAP; -2 ANGLE; AND -3 FILLER REF B737-NG SRM 53-70-51-2R-6.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 40,188 hrs · 19,212 cycles

MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-24. MARKED <[01]. MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-24; EVALUATED DAMAGE AND FOUND OUT OF LIMITS IAW B737-800 SRM 53-10-51-1A-1 AND BOEING DWG 141A5770 REV:A; DAMAGE DEPTH: 0.044' ORIGINAL THICKNESS: 0.080'; REMOVED FLOOR SUPPORT IAW B737-800 SRM 51-40-02; RECEIVED NEW PART P/N: 141A5770U3 INTERCOSTAL; PO: 1112018.1 IAW B737-800 IPC 53-42-11-44; LOCATED & DRILLED IAW B737-800 SRM 51-40-05 & BAC DWG 141A5730 REV. A. AND INSTALLED IAW B737-800 SRM 51-40-02 & BAC DWG 141A5730 REV. A. [04] VERIFIED MAIN CABIN FWD WET AREA; FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344 APPROX. LBL-24; EVALUATED DAMAGE AND FOUND OUT OF LIMITS IAW B737-800 SRM 53-10-51-1A-1 AND BOEING DWG 141A5770 REV:A; DAMAGE DEPTH: 0.044' ORIGINAL THICKNESS: 0.080'; REMOVED FLOOR SUPPORT IAW B737-800 SRM 51-40-02; RECEIVED NEW PART P/N: 141A5770U3 INTERCOSTAL; PO: 1112018.1 IAW B737-800 IPC 53-42-11-44; LOCATED & DRILLED IAW B737-800 SRM 51-40-05 & BAC DWG 141A5730 REV. A. AND INSTALLED IAW B737-800 SRM 51-40-02 & BAC DWG 141A5730 REV. A & REV C.

Part: STRUCTURE — CRACKED (ZONE 200) · airframe 40,188 hrs · 19,212 cycles

STA540 R/H FLOORBOARD SUPPORT STRUCTURE CRACKED 2EA AREAS DOT T743 <[01]. REMOVED AND REPLACED PANEL BREAK#143A5240-64 PO#1111708.1 AT STA540 R/H IAW B737-800 SRM 51-40-02 AND BAC DWG#143A0060 REV.A; [02] REMOVED AND REPLACED PANEL BREAK#143A5240-64 PO#1111708.1 AT STA540 R/H IAW B737-800 SRM 51-40-02 AND BAC DWG#143A0060 REV.A. VERIFIED WORK AND WORK ENTRIES.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 40,188 hrs · 19,212 cycles

R/H AFT EMERGENCY LIGHTS ON R2 DOOR INOP <[01]. REMOVED AND REPLACED R/H AFT EMERGENCY BATTERY AND OPS CHECK GOOD IAW B737-800 AMM 33-51-00-710-801; [02] REMOVED AND REPLACED R/H AFT EMERGENCY BATTERY AND OPS CHECK GOOD IAW B737-800 AMM 33-51-00-710-801. VERIFIED WORK AND WORK ENTRIES.

Part: FLAP — DELAMINATED (ZONE 600) · airframe 40,188 hrs · 19,212 cycles

RIGHT WING OUTBOARD AFT FLAP INBOARD LOWER CORNER IS DELAMINATED <[01]. REMOVED AND REPLACED RIGHT WING OUTBOARD AFT FLAP IAW B737-800 AMM 27-51-22-401-NG.; [02] VERIFIED REMOVED AND REPLACED RIGHT WING OUTBOARD AFT FLAP IAW B737-800 AMM 27-51-22-401-NG.; [03] VERIFIED REMOVED AND REPLACED RIGHT WING OUTBOARD AFT FLAP IAW B737-800 AMM 27-51-22-401-NG.

Part: STAND OFF — CORRODED (ZONE 500) · airframe 40,188 hrs · 19,212 cycles

L/H WING FIXED L/E; 3 EACH STIAND OFFS FOR OVER HEAT DETECTOR CORRODED BETWEEN RIB #3 AND RIB #4. <[01] REMOVED AND REPLACED 3 EACH STAND OFFS # BACN10TL3A12 PO # 1111371.1 AT L/H WING FIXED L/E IAW B737-800 SRM 51-40-02 AND BAC DWG #116A2130 REV.- TOOL # T8866U. CAL.DUE.07/APR/25 (TORQUE WRENCH);[02] REMOVED AND REPLACED 3 EACH STAND OFFS # BACN10TL3A12 PO # 1111371.1 AT L/H WING FIXED L/E IAW B737-800 SRM 51-40-02 AND BAC DWG #116A2130 REV.- TOOL # T8866U CAL.DUE. 07/APR/25 (TORQUE WRENCH).

Part: SKIN — CRACKED (NR 2 FAN COWL) · airframe 37,369 hrs · 17,674 cycles

#2 ENGINE I/B FAN COWL IS CRACKED 17' LONG AT FWD LOWER FWD END.<[01] REMOVED AND REPLACED #2 ENGINE INBOARD FAN COWL REF. AMM 71-11-02. INSTALLED VORTEX CONTROL DEVICE REF. AMM 71-11-08.

Part: ACTUATOR — FAULTY (MLG UPLOCK) · airframe 37,164 hrs · 17,560 cycles

ON APPROACH LDG GEAR WAS LOWERED AND LT MAIN DISAGREED WITH HANDLE POSITION. NOSE & RT MAIN GREEN/ LEFT MAIN RED AND NO GREEN GEAR LT ON OVERHEAD FOR LT MAIN. RAN QRH FOR LANDING GEAR DISAGREE; PULLED MANUAL EXTENSION AND GOT GREEN LT ON LT MAIN AND OVERHEAD.<[01] OK TO CONTINUE PER MEL 32-16-01 SP#1;[02] REMOVED AND REPLACED L/H MLG UPLOCK ACTUATOR AS PER AMM 32-32-41. OPS CHECK GOOD!

Part: MEGAPHONE — INOPERATIVE (ZN 200 FUS TOP) · airframe 36,718 hrs · 17,297 cycles

FWD BULLHORN INOP<[01] R & R?D FWD GALLEY MEGAPHONE PER AMM 25-64-00.

Part: BATTERY — INOPERATIVE (ZN 200 FUS TOP) · airframe 33,832 hrs · 15,637 cycles

RIGHT SIDE PASSENGER EMERGENCY LIGHTS INOP<[01] T/S PER FIM 33-50 TASK 801; RR?D BATTER PACK AT ASSY# M1695 PER AMM 33-51-06. NO HELP. RETURNED BACK TO ORIGINAL CONFIGURATION. R/R EMERGENCY LIGHT BATTERY PACKS AT POS M1676 AND M1671 REF AMM 33-51-06. OPS CHECK NORMAL REF AMM 33-51-00. THIS CLEARS MEL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,579 hrs · 15,486 cycles

R/H AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP<[01] REMOVED AND REPLACED 2EA EMERGENCY LIGHT BATTERY PACKS PER AMM 33-51-06. OPERATIONAL CHECK NORMAL OF EMERGENCY LIGHTS PER AMM 33-51-00. REFERENCE CARD TTG8Q00HCN6F FOR PARTS INSTALLED.;[02] INSPECTED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,579 hrs · 15,486 cycles

R/H EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED 2EA EMERGENCY LIGHT BATTERY PACKS PER AMM 33-51-06. OPERATIONAL CHECK NORMAL OF EMERGENCY LIGHTS PER AMM 33-51-00.;[02] INSPECTED

Part: TRACK — CRACKED (HORIZONTAL STAB) · airframe 33,579 hrs · 15,486 cycles

R/T HORIZONTAL PANEL 343AT FWD TRACK IS CRACKED<[01] R&R TRACK PER SOPM 20-50-01;[02] INSPECTED WORK PERFORMED.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 33,579 hrs · 15,486 cycles

EVIDENCE OF CORROSION ON THE RUDDER BALANCE WEIGHT.<[01] REMOVED RUDDER WEIGHT PER CMM 55-40-09;[02] INSTALLED RUDDER WEIGHT PER CMM 55-40-09;[03] C/W INSPECTION.;[04] INSTALLED RUDDER WEIGHT PER CMM 55-40-09

Part: SUPPORT BEAM — CRACKED (LT WING) · airframe 33,579 hrs · 15,486 cycles

L/H WING FIXED TRAILING EDGE SUPPORT BEAM FWD FASTENER HOLE ADJACENT TO L/H DEFLECTION RIB HAS AN HFEC INDICATION OF A CRACK AT THE FWD SIDE OF THE HOLE SEE ATTACHED PICTURE<[01] REPAIR PER EA #23-157-00063 (N8608N - SWA - REPAIR - L/H WING TRAILING EDGE SUPPORT BEAM FASTENER HOLE CRACK ON PN 115A2179);[02] C/W INSPECTION.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 33,579 hrs · 15,486 cycles

CENTER CABIN STA. 540 RBL 1 FLOOR PANEL SUPPORT ANGLE IS CRACKED. MRKD<[01] REMOVED AND REPLACED SUPPORT PART SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 33,579 hrs · 15,486 cycles

CENTER CABIN STA. 540 LBL 1 FLOOR PANEL SUPPORT ANGLE IS CRACKED AT FASTENER HOLE. MRKD<[01] REMOVED AND REPLACED CABIN FLOOR SUPPORT PER SRM 51-40-02.

Part: PANEL — CRACKED (ZONE 100) · airframe 33,579 hrs · 15,486 cycles

FASTENER HOLE CRACKED ON PANEL 561CB<[01] REMOVED DAMAGE AND APPLIED REPAIR PER SRM 51-70-04-2R-9;[02] C/W INSPECTION.;[03] RESIN SWEEPED AND SANDED TO AERODYNAMIC SMOOTHNESS PER SRM 51-70-08;[04] C/W INSPECTION.;[05] PRIMED PER AMM 51-21-72 APPLIED TOPCOAT PER AMM 51-21-73;[06] C/W INSPECTION.

Part: PLATE — CRACKED (LT WING) · airframe 33,579 hrs · 15,486 cycles

L/H WING T/E WAFFLE PLATE IS CRACK AT APPROX. IRSS 220. MRKD<[01] REMOVED AND REPLACED WAFFLE PLATE IAW SRM 51-40-02.;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR: 1. JOSHUA PHIPPS (TECHNICIAN); 08-JAN-2023 04:43 UTC<BR>REMOVED AND REPLACED WAFFLE PLATE IAW SRM 51-40-02.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 30,469 hrs · 13,738 cycles

L2 EXTERIOR EMERGENCY LIGHT INOP ; / [01] RELAMPED L2 EXTERIOR EMERGENCY LIGHT PER AMM 33-51-04

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 29,563 hrs · 13,255 cycles

EMERGENCY LIGHTS INOP AFT OF 2ND OVER WING EXIT LT SIDE AND AFT OF WING TO BODY PNL'S LT SIDE / REMOVED AND REPLACED PACK CHARGER ASSY AND BATTERY PACK AT M1670 OPS CK'S GOOD REF AMM 33-51-06REF SA-M 326 A1073571P/N OFF/ON D717-02-030 S/N OFF 103651 S/N ON 25511P/N OFF/ON D717-01-100 S/N OFF 218913 S/N ON 220350

Part: NONE — INOPERATIVE (CABIN) · airframe 29,563 hrs · 13,255 cycles

EMERGENCY LIGHTS INOP AFT OF 2ND OVER WING EXIT LT SIDE AND AFT OF WING TO BODY PNL'S LT SIDE / REMOVED AND REPLACED PACK CHARGER ASSY AND BATTERY PACK AT M1670 OPS CK'S GOOD REF AMM 33-51-06REF SA-M 326 A1073571P/N OFF/ON D717-02-030 S/N OFF 103651 S/N ON 25511P/N OFF/ON D717-01-100 S/N OFF 218913 S/N ON 220350

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 28,094 hrs · 12,482 cycles

AFT RIGHT HAND (FO SIDE) LAV HAS INTERMITTENT SMOKE ALARM WITH NO PASSENGER IN LAV OR EVIDENCE OF SMOKE SEE AIRCRAFT LOGBOOK / REMOVED AND REPLACED AFT RIGHT LAV SMOKE DETECTOR IN REFERENCE TO AMM 26-14-01 OPS CHECK IS OK CLOSING # 87917

Part: PANEL — CRACKED (FUSELAGE) · airframe 27,553 hrs · 12,197 cycles

FWD CARGO PANEL 120ZAC HAS A CRACK 4.5' LONG 25' FROM LH EDGE OF PANEL PERFORMED INTERIM REPAIR ON PANEL 120ZAC PER EA 1-A25-3722 REV. 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPANT PANEL. REPETITIVE ACTION REQUIRED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,379 hrs · 12,102 cycles

FWD CABIN L/H AISLE EMERGENCY LIGHTS INOP / REMOVED AND REPLACED THE BATTERY PACK FOR THE POWER SUPPLY AT BS 500 C & 7; OPS CHECK GOOD PER AMM 33-51-06 (D62)

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 27,379 hrs · 12,102 cycles

FWD CARGO COMPARTMENT ; AFT CORNER SCUFF PLATE IS CRACKED. / R/R FWD CARGO AFT CORNER SCUFF PLATE IAW AMM 53-11-02SEE SA-M 326: A1304062

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 27,379 hrs · 12,102 cycles

FWD CARGO COMPARTMENT ; FWD CORNER SCUFF PLATE IS CRACKED. / R/R FWD CARGO FWD CORNER SCUFF PLATE IAW AMM 53-11-02 SEE SA-M 326: A1304063

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 27,379 hrs · 12,102 cycles

CABIN FLOORBOARDS 241 ZF; 242D;242E;242F DAMAGED BEYOND LIMITS / REPLACED AFT CABIN FLOORBOARDS 241ZF; 242D. 242E AND 242F. FLOORBOARD INSTALL ON SWA SAM 565S

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 27,379 hrs · 12,102 cycles

CORROSION ON TOP SURFACE OF INTERCOSTAL @ STA 947+2 AND RBL 50. / REMOVED AND REPLACED DAMAGED INTERCOSTAL 947 TO 967 RBL 50 PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 27,379 hrs · 12,102 cycles

CORROSION ON TOP SURFACE OF INTERCOSTAL @ STA 947+2 AND LBL 50. / REMOVED AND REPLACED INTERCOSTAL FROM STA 947 TO STA 967; LBL 50' PER SRM 51-40-02 AND EA 21-153-00093 PART 2. INTER COSTAL P/N 147A5660-21.SA-M 326 A1304011

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 27,379 hrs · 12,102 cycles

CORROSION ON TOP OF FLOOR BEAM @ STA 947 FROM RBL 49.5 TO LBL 52 IS OUT OF LIMITS / REMOVED AND REPLACED DAMAGED FLOOR BEA; UPPER HORIZONTAL LEG PER E.A. 21-153-0093 AND SRM 53-70-51-2R-5 SEE SA-M 326'S : A1304014;A1304015;A1304016;A1304017

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 27,379 hrs · 12,102 cycles

CORROSION ON TOP SURFACE OF INTERCOSTAL @ STA 947+2 AND LBL 25. / R/R INTERCOSTAL STA 947+2 LBL 25 IAW SRM 51-40-02 AND SRM 51-10-02. PART# REPALCED 147A5660V3.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,379 hrs · 12,102 cycles

FWD ENTRY DOOR CUT-OUT Z-ANGLE AND NUT-PLATE SUPPORT CORRODED FROM BS 303-348 / REMOVED + REPLACED FWD ENTRY DOOR CUTOOUT Z ANGLE IAW SRM 51-40-02 AND SRM 51-10-02SA-M 326 S/N A1304019

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,379 hrs · 12,102 cycles

FWD GALLEY FLOOR STRUCTURE STA. 274 TO 294 RBL. 1; INTERCOSTAL CRACKED AT FASTENER HOLE / REMOVED DAMAGED INETCOASTAL AND INSTALLED NEW INTERCOASTAL I/A/W SRM 51-40-02.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 27,379 hrs · 12,102 cycles

LT. HORIZ. STAB FWD UPPER SLIDING SEAL CRACKED. / R&R SLIDING SEAL ASSY IAW AMM 53-31-31SEE SA-M 326: A1304050

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 27,379 hrs · 12,102 cycles

FWD WET AREA FLOOR BOARDS DAMAGED FROM STA 2700-420 / FWD WET AREA FLOOR BOARDS (ZZ1AF-ZZICE-ZZ1DF-ZZ1EF-ZZ1FF; ZZ1GF; ZZZ AF - ZZZBF - ZZZCF - ZZZ DF) WERE R&R ON SA-M 565S TASK CARD PANEL SIGN OFF SHEET AND PER AMM 53-21-00; PANEL WERE ALL REPLACED WITH NEW PANELS

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 27,379 hrs · 12,102 cycles

RT STAB FWD UPPER SLIDING SEAL CRACKED. / R&R STAB FWD UPPER SLIDING SEAL ASSY IAW AMM 53-31-31SEE S-AM 326: A1304089

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 27,379 hrs · 12,102 cycles

BIN EMERGENCY EXIT LIGHT & BEZEL / LENS CRACKED AT 27 ABC / REPLACED LIGHT BEZEL/LENS PER AMM 33-51-03

Part: HOOK AND LOOP — DETACHED (L1 SLIDE COVER) · airframe 25,824 hrs · 11,318 cycles

FWD ENTRY DOOR SLIDE APPEARS TO BE IMPROPERLY RIGGED. REATTACHED THE HOOK AND LOOP ON THE SLIDE LOWER FLAP IAW MT 725-61-06. NO FAULTS NOTED.

Part: SPRING — BROKEN (FWD CARGO HANDLE) · airframe 25,628 hrs · 11,225 cycles

FWD. CARGO DOOR HANDLE RETURN SPRING BROKEN (RAMP REPORTS) ( FWD CARGO DOOR EXTERIOR HANDLE RECESS/HINGE SPRINGASSEMBLIES ) / CLEARING DMA LOG PAGE# 0428221REMOVED & REPLACED FWD CARGO DOOR HANDLE RETURN SPRING AS PER M/M 52-31-14 CL# 76792

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 23,217 hrs · 10,107 cycles

L/H EMERGENCY EXIT OVERWING FORWARD BROKEN OFF. R&R LIGHT LENS IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,148 hrs · 10,076 cycles

FORWARD CABIN EMERGENCY LIGHTS INOP AT LOCATION M1475. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,148 hrs · 10,076 cycles

FORWARD CABIN EMERGENCY LIGHTS INOP AT LOCATION M2816. R&R BATTERY PACK IAW AMM.

Part: STRINGER CLIP — MISSING (FUSELAGE) · airframe 23,148 hrs · 10,076 cycles

STRINGER CLIP MISSING AT BS. 727H, STR. 19L. R&R STRINGER CLIP PER SRM & DWG.

Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 23,188 hrs · 10,091 cycles

WING TO BODY PANEL 193CL FORWARD EDGE HAS SEVERAL LAYERS ERODED WITH DELAM / REPAIRED AND APPLIED RESTORATIVE FINISH ON WING TO BODY PANEL 193CL OF DAMAGE AT FORWARD EDGE OF ONE PLY OR LESS IAW B737-800 SRM 51-70-08-0G-0 REV 67 AND B737 AMM 51-21-99-300-801 REV 68. A38760; A86296; A56952

Part: SHEAR TIE — CRACKED (BS 847 S23L) · airframe 23,188 hrs · 10,091 cycles

SHEAR TIE CRACKED AT STA 847 BELOW S-23L / REMOVED DAMAGED SHEAR TIE; LOCATED; DRILLED; AND INSTALLED NEW SHEAR TIE REF B737 SRM 51-40-02; 51-40-03; DWG 146A3230 ID 0184 REV A. AT STA 847 BELOW S23L

Part: STRINGER — DAMAGED (BS 727I) · airframe 23,187 hrs · 10,090 cycles

STRINGER DAMAGED AT BS. 727I, STR. 25L. REPAIRED STRINGER PER EA.

Part: SKIN — DAMAGED (BS 727H-727J) · airframe 23,187 hrs · 10,090 cycles

SKIN DAMAGED BETWEEN BS. 727H-1.5 TO BS. 727J+6, BETWEEN STR. 23L TO STR. 25L. / REPAIR SKIN PER EA.

Part: STRINGER CLIP — DAMAGED (BS 727H) · airframe 23,187 hrs · 10,090 cycles

STRINGER CLIP DAMAGED AT BS. 727H, STR. 24L. / REPAIRED CLIP IAW EA.

Part: STRINGER — DAMAGED (BS 727H) · airframe 23,187 hrs · 10,090 cycles

STRINGER DAMAGED AT BS. 727H+6, STR. 18L. REPAIRED STRINGER PER EA.

Part: STRINGER CLIP — DAMAGED (BS 727I) · airframe 23,187 hrs · 10,090 cycles

STRINGER CLIP DAMAGED AT BS. 72I, STR. 25L. REPAIR CLIP IAW EA.

Part: STRINGER CLIP — DAMAGED (BS 727I) · airframe 23,187 hrs · 10,090 cycles

STRINGER CLIP DAMAGED AT BS. 727I, STR. 24L. / REPAIR CLIP PER EA.

Part: STRINGER CLIP — DAMAGED (BS 727J) · airframe 23,187 hrs · 10,090 cycles

STRINGER CLIP DAMAGED AT BS. 727J, STR. 25L. / REPAIRED CLIP IAW EA.

Part: SKIN — DAMAGED (BS 727H-727I) · airframe 23,187 hrs · 10,090 cycles

SKIN DAMAGED BETWEEN BS. 727H+5 TO BS. 727I+4, BETWEEN STR. 17L TO STR. 28L. / REPAIRED SKIN PER EA.

Part: STRINGER — DAMAGED (BS 727H-727I) · airframe 23,187 hrs · 10,090 cycles

STRINGER DAMAGED BETWEEN BS. 727H TO BS. 727I, STR. 20L. REPAIRED STRINGER PER EA.

Part: STRINGER CLIP — DAMAGED (BS 727I) · airframe 23,187 hrs · 10,090 cycles

STRINGER CLIP DAMAGED AT BS. 727I, STR. 18L. REPAIRED CLIP PER EA.

Part: STRINGER CLIP — DAMAGED (BS 727J) · airframe 23,187 hrs · 10,090 cycles

STRINGER CLIP DAMAGED AT BS. 727J, STR. 23L. / REPAIRED CLIP PER EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 23,148 hrs · 10,076 cycles

SHEAR TIE CRACKED AT BS. 847, STR 23L. R&R SHEAR TIE PER SRM & DWG.

Part: SKIN — BUCKLED (FUSELAGE) · airframe 23,187 hrs · 10,090 cycles

REF LP 1138480 - FGUESLAGE SKIN REPAIR FROM BS 727H - 727J AND BETWEEN STR23L-25L. REPAIR-53EA-07003 ( MX NOTE ) / REF NR X979661; R/R LEFTHAND SKIN PANEL 146A3201-32 ATAG # ZP0119 IAW SRM 51-40-05-0G-1; SRM 51-40-02-06-0 AND DRWG 146A3200 REV A

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 23,148 hrs · 10,076 cycles

SHEAR TIE DAMAGED AT BS. 867, BETWEEN STR. 25L TO STR. 26L. R&R SHEAR TIE PER SRM & DWG.

Part: STRAP — PULLED (R2 DOOR) · airframe 22,477 hrs · 9,779 cycles

R2 DOOR SAFETY STRAP PULLED OUT OF SIDEWALL. / INSTALLED PULLED SNAP IAW CMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,231 hrs · 9,221 cycles

EMERGENCY EXIT LIGHTS AT OVERWING EXITS INOP AT M1695. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,231 hrs · 9,221 cycles

EMERGENCY EXIT LIGHTS AT OVERWING EXITS INOP AT M1694. R&R BATTERY PACK IAW AMM.

Part: BAFFLE — CRACKED (FWD CARGO LH) · airframe 21,851 hrs · 9,492 cycles

FWD CARGO COMPARTMENT LH BAFFLE BS 500C-500D IS CRACKED / FWD CARGO L/H BAFFLE IS CRACKED AT B.S. 500C TO 500D. DRILLED AND REMOVED CRACKED BAFFLE I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW L/H BAFFLE I/A/W SRM 51-40-05-0G-0. INSTALLED NEW L/H BAFFLE AT STA 500C TO 500D I/A/W SRM 51-40-02-0G-0 ALSO BOEING DWG 143A7505 REV: . APPLIE C.I.C TO AREA I/A/W AMM 51-21-91-620-802.

Part: WEB — CRACKED (WHEEL WELL RH) · airframe 21,851 hrs · 9,492 cycles

CUSTOMER REQUEST-VB R/H STA 663 VAPOR WEB HAS 2 EACH PREVIOUS REPAIRS WITH CRACK EXTENDING BETWEEN REPAIRS. PERM. REPAIR REQUIRED. / REPAIRED R/H STA 663 VAPOR WEB IAW B737 SRM 57-10-10-2R-2 AND SRM 51-70-04-2R-10 PARA 4

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 21,231 hrs · 9,221 cycles

AFT CARGO ATTACH ANGLE CRACKED AT BS 727+6, BETWEEN LBL 20 TO RBL 20. R&R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (AFT CARGO COMPT) · airframe 21,851 hrs · 9,492 cycles

AFT CARGO; STA 867; LBL9; JUST BELOW CARGO FLOOR; ATTACH ANGLE CRACKED; COMMON TO VERTICAL BULKHEAD SUPPORT. / REMOVED AND REPLACED CRACKED ATTACH ANGLE; AFT CARGO; STA 867 LBL 8 WITH NEW PART P/N 149A8109U114 IAW SRM 51-40-02 AND DWG 149A8102 REV - ATAG ZP0073

Part: ANGLE — CRACKED (AFT CARGO COMPT) · airframe 21,851 hrs · 9,492 cycles

AFT CARGO; STA 727+6; LBL 20 TO RBL 20; FLOOR TO BULKHEAD SUPPORT ANGLE IS CRACKED. / REPLACED AFT CARGO; CRACKED SUPPORT ANGLE AT STA 727 +6 LBL 20 TO RBL 20 WITH NEW PART P/N 453A2611-25 IAW IPC 25-52-10-19 PART TO BE INSTALLED WITH FLOOR BOARD 140AF W/O 38868/1000/0016 ATAG # WN3970

Part: SPLICE PLATE — CORRODED (AFT CARGO) · airframe 21,851 hrs · 9,492 cycles

AFT CARGO FLOOR PANEL SPLICE PLATE CORRODED STA 767+5; RBL 18 TO LBL 18 / REMOVED AND INSTALLED AFT CARGO FLOOR PANEL SLICE PLATE AT STA 767 +5 RBL 18 TO LBL 18 P/N 146A9401-4 TAG # WN8493 IAW B737 DWG 146A7500 REV. - SRM 51-40-02-0G-0 AND APPLIED CIC IN PANEL AMM 51-21-91-620-802.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 21,231 hrs · 9,221 cycles

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

Part: SPLICE — CORRODED (AFT CARGO) · airframe 21,851 hrs · 9,492 cycles

AFT CARGO; STA 887; RBL 18 TO LBL 9; FLOOR PANEL SPLICE HAS CORROSION AROUND NUT PLATE HOLES / REPLACED AFT CARGO STA 887 FLOOR PANEL SPLICE P/N 146A9401-39 IAW B737 SRM 51-40-02; SRM 51-40-05 AND DWG 146A7500 REV:- ATAG: WN7408

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 21,231 hrs · 9,221 cycles

AFT CARGO ATTACH ANGLE CRACKED AT BS 867, LBL 9. R&R ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,231 hrs · 9,221 cycles

FORWARD CARGO COMP FLOOR STRUCTURE RT Z ANGLE CORRODED BETWEEN BS 500+14 TO BS 500E. REPAIRED Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FWD CARGO COMPT) · airframe 21,851 hrs · 9,492 cycles

FWD CARGO COMP FLOOR STRUCTURE;AFT BULKHEAD BOTTOM ANGLE CORROSION AROUND FASTNER HOLES STA.520 / THE FORWARD CARGO AFT BULKHEAD BOTTOM ANGLE 'RAIL ASSY' FOUND TO HAVE ALLOWABLE LIMITS ON SRM IAW B737 SRM 51-10-02-0G-0 PARAGRAPH 9. REMOVED AND INSTALLED A NEW FORWARD CARGO COMPARTMENT FLOOR STRUCTURE AFT BULKHEAD BOTTOM ANGLE 'RAIL ASSY' IAW B737 SRM 51-40-02-0G-0 AND BOEING DRAWING 143A9481 ATAG WN3051 P/N:143A9485-35

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 21,851 hrs · 9,492 cycles

AFT CARGO FLOOR PANEL 140EF HAS CORROSION ON O/B PERIMETER OF PANEL / AFT CARGO PANEL 140EF WAS OUT OF LIMITS RECEIVED NEW PANEL 453A2610-58. TO BE INSTALLED ON WORK CARD 422715 OUT OF LIMITS IAW SRM 53-00-53-1A-1 PANEL IAW IAW IPC 25-52-16-19 ATAG # WN4173

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 21,851 hrs · 9,492 cycles

AFT CARGO FLOOR PANEL 140EF HAS 1' CRACK 10' FROM FWD SIDE. / AFT CARGO FLOOR PANEL 140EF; HAS CRACK; OUT OF LIMITS IAW SRM 53-00-53-1A-1. REPLACED PANEL 140EF P/N 453A2610-58; 'A'TAG WN4173 ON NRC X888952

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 21,851 hrs · 9,492 cycles

AFT CARGO FLOOR PANEL 140BF HAS CORROSION ON O/B PERIMETER OF PANEL / AFT CARGO FLOOR PANEL # 140BF A-TAG # WN1365 PN # 453A2610-32 PN # 7253513 IAW IPC 25-52-10-19 ORIGINAL PANEL FOUND TO BE OUT OF LIMITS WITH MORE THAN 10 INCHES OF DAMAGE IAW SRM 53-00-53-1A-1 FIG 102. NEW PANEL TO BE INSTALLED ON W/O 422715

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 21,851 hrs · 9,492 cycles

AFT CARGO FLOOR PANEL 140CF HAS CORROSION ON O/B PERIMETER OF PANEL / PANEL 140CF WAS OUT OF LIMITS IAW SRM 53-00-53-1A-1 CORROSION THE LENGTH OF PANEL RECEIVED NEW PANEL TO REPLACE PANEL 140CF MATERIAL ID IS 453A2610-18 IAW IPC 25-52-10-19 ATAG WN0558 SI 7253512

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 21,851 hrs · 9,492 cycles

AFT CARGO FLOOR PANEL 140DF HAS CORROSION ON O/B AND AFT PERIMETER OF PANEL. / PANEL FOR AFT CARGO 140DF IS OUT OF LIMIT HAS CORROSION THE LENGTH OF PANEL OUT OG LIMITS IAW SRM 53-00-53-1A-1 MATERIAL ID FOR RECEIVED NEW IS 453A2610-20IAW IPC 25-52-10-19 PANEL INSTALLED ON CARD DOC SA-M 565S PG. 32 ITEM 1. ATAG NW9922

Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 21,851 hrs · 9,492 cycles

FWD CARGO COMP FLOOR STRUCTURE;RH Z-ANGLE CORROSION AROUND FASTNER HOLES STA.500+14'-500E / REMOVED Z ANGLE A500 TO 500E AND REPAIRED Z ANGLE IAW BOEING 737 SRM 53-00-53-2R-6 AND SPLICE IAW SRM 53-00-53-2R-5. P/N: 143A7501-158 TOOL AAR 36647 DUE 10 JUN 19

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 21,851 hrs · 9,492 cycles

AFT CARGO; AFT OF DOOR FLOOR PLATE IS CORRODED (AFT TIEDOWN PLATE) / RECEIVED NEW AFT CARGO DOOR FLOOR PLATE TIEDOWN REQ MATERIAL ID MATERIAL ID IS 453A2611-2 AIW IPC 25-52-10-04 TAG # A69675 PART TO BE INSTALLED ON CARD WO 422715

Part: ANGLE — CORRODED (FWD CARGO LH) · airframe 21,851 hrs · 9,492 cycles

FWD CARGO COMP FLOOR STRUCTURE;LH Z-ANGLE CORROSION AROUND FASTNER HOLES STA.500B+14'-500F / FWD CARGO L/H Z-ANGKE STA 500B+14-500F CORROSION FASTENER HOLES. BLENDED AND REMOVED CORROSION IAW AMM 51-00-53-201. 'OUT OF LIMITS' IAW SRM 53-00-53-1A-2 MAT THICKNESS .40 MAT REMOVED .012 REMAINING .028. REMOVED Z-ANGLE STA 500B TO STA 500I IAW SRM 51-40-02-0G-0. FABRICATED; TRIMMED; ALODINED PRIMED NEW SECTION OF Z-ANGLE STA 500B TO STA 500I IAW SRM 51-40-05-0G-0; BOEING DWG 143A7500 REV:-; AMM 51-21-41-370-802; AMM 51-21-72-370-804; INSTALLED NEW SECTION OF Z-ANGLE IAW SRM 51-40-02-0G-0 ALSO BOEING DWG 143A7500. APPLIED C.I.C IAW AMM 51-21-91-620-802 P/N 143A7501-81

Part: PLATE — CORRODED (AFT CARGO COMPT) · airframe 21,851 hrs · 9,492 cycles

AFT CARGO; FWD OF DOOR FLOOR PLATE IS CORRODED (FWD TIE DOWN PLATE) / REPLACED AFT CARGO; FWD OF DOOR FLOOR PLATE P/N 453A2611-1 ATAG 'A89367' IAW B737 AIPC 25-52-10-04. THE NEW PLATE WILL BE INSTALLED ON W/O TASK CARD PANEL SIGN OFF SHEET # 422715; THE REPLACEMENT OF THE PART WAS IAW B737 SRM 51-10-02-0G-0; PARAGRAPH 9. ATAG: A89367

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 21,851 hrs · 9,492 cycles

FWD CARGO FLOOR PANEL 120CF HAS CORROSION AROUND PERIMETER OF PANEL / VERIFIED NEW FWD CARGO FLOOR PANEL 120CF IAW IPC 25-52-10-17 FOUND FLOOR PANEL 120CF TO BE OUT OF LIMITS DUE TO CORROSION LENGTH OF OVER 10' IAW SRM 53-00-53-1A-1

Part: PANEL — CRACKED (LEFT WING) · airframe 21,851 hrs · 9,492 cycles

LH WING L/E PANEL 521JB IS CRACKED / REPAIRED AND APPLIED DECORATIVE FINISH TO L/H WING L/E PANEL 521JB OF LIGHT DISBOND OF EDGE STRIP (AS MARKED) IAW B737-800 SRM 57-41-01-2R-6 REV 65 AND B737 AMM 51-21-99-300-801 REV 67. A22088; A74378

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 21,851 hrs · 9,492 cycles

FWD CARGO FLOOR PANEL 120BF HAS CORROSION AROUND PERIMETER OF PANEL / DAMAGED AREA EXCEEDS LIMITS REPLACED PANEL 120BF P/N 453A1610-16 AS REQUIRED I.A.W. SRM 53-00-53-1A-1 I.P.C. 25-52-10-17

Part: BRACKET — BROKEN (LEFT WING) · airframe 21,851 hrs · 9,492 cycles

LH WING T/E PANEL 551FB HAS BROKEN OFF BRACKET / REMOVED AND REPLACED BROKEN BRACKET ON L/H WING PANEL 551FB IAW BOEING 737 SRM 51-40-02

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 21,851 hrs · 9,492 cycles

FWD CARGO FLOOR PANEL 120DF HAS CORROSION AROUND PERIMETER OF PANEL / DAMAGED AREA EXCEEDS LIMITS REPLACED PANEL 120DF P/N 453A1610-20 AS REQUIRED I.A.W. SRM 53-00-53-1A-1 I.P.PC. 25-52-10-17

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 21,851 hrs · 9,492 cycles

FWD CARGO FLOOR PANEL 120AF HAS CORROSION ON LH O/B SIDE. / DAMAGED AREA EXCEEDS LIMITS REPLACED PANEL 120AF P/N 453A1610-14 AS REQUIRED. I.A.W. SRM 53-00-53-1A-1 I.P.C. 25-52-10-17

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,231 hrs · 9,221 cycles

FORWARD CARGO COMP FLOOR STRUCTURE LT Z-ANGLE CORRODED BETWEEN BS 500B+14 TO BS 500F. R&R LT Z ANGLE IAW SRM AND DWG.

Part: RETAINER — CRACKED (LEFT WING) · airframe 19,863 hrs · 8,600 cycles

SEAL RETAINER AT THE TRAILING EDGE OF TJE L/H LOWER FIXED TRAILING EDGE PANEL 441GB IS CRACKED APPROX FIVE INCHES / REMOVED AND REPLACED THE TRAILING EDGE OF THE L/H LOWER TRAILING EDGE PANEL SEAL RETAINER. REF SRM 51-40-02 AND SIP

Part: LENS — CRACKED (CABIN) · airframe 17,639 hrs · 7,605 cycles

LT OVERHEAD BIN EMERGENCY LIGHT LENS CRACKED AT ROW 19. R&R COVER PER AMM.

Part: LENS — CRACKED (CABIN) · airframe 17,639 hrs · 7,605 cycles

RT OVERHEAD BIN EMERGENCY LIGHT LENS CRACKED AT ROW 10. R&R COVER PER AMM.

Part: SKIN — DELAMINATED (LT WING) · airframe 17,955 hrs · 7,752 cycles

L/H WING #1 SLAT T/E WEDGE LOWER SKIN O/B END DELAMINSTED 1.2' X 3.5' / REMOVED & REPLACED L/H WING #1 SLAT PER AMM 27-81-21. P/N OFF/ON 114A5010-207; S/N OFF 004404; S/N ON 005741

Part: PANEL — DELAMINATED (RT WING) · airframe 17,955 hrs · 7,752 cycles

#2 ENG STRUT PNL 441BR CORNERS HAVE DELAMINATION. LOWER AFT CORNER DAMAGE MEASURES 1.3 IN X 1.4 IN UPPER AFT CORNER MEASURES 2.9 IN X 2.3 IN. / REMOVED AND REPLACED PNL 441BR PER AMM 54-53-01 ROBBED FROM AIRCRAFT 283

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 16,096 hrs · 6,918 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM & SIP.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 12,908 hrs · 5,487 cycles

RIGHT WHEEL WELL VAPOR BARRIER CRACKED RBL 31.83. REPAIRED THE VAPOR BARRIER IAW EA.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 12,658 hrs · 5,374 cycles

LEFT EMERGENCY EXIT LIGHT LENS COVER MISSING AT ROW 27. INSTALLED THE COVER IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 11,028 hrs · 4,690 cycles

LEFT EMER AISLE LIGHT LENS COVER MISSING AT ROW 12. INSTALLED COVER IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 9,434 hrs · 4,004 cycles

LEFT CABIN OVERHEAD BIN, EMER LIGHT LENS CRACKED AT ROW 18. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 9,670 hrs · 4,099 cycles

LEFT OVERHEAD BIN, EMER LIGHT LENS CRACKED AT ROW 23. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 9,434 hrs · 4,004 cycles

LEFT EMER ESCAPE LIGHT LENS, CRACKED BETWEEN ROWS 5 - 16. R & R LENS IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 9,434 hrs · 4,004 cycles

LEFT CABIN OVERHEAD BIN, EMER LIGHT LENS CRACKED, BETWEEN ROWS 15 - 23. R & R LENS IAW AMM.

Part: LATCH — BROKEN (R1 DOOR) · airframe 6,444 hrs · 2,704 cycles

R1 DOOR EMER EVAC SLIDE LATCH BROKEN. REPAIRED LATCH IAW SIP.

Part: SIGN — UNSECURE (CABIN) · airframe 6,363 hrs · 2,668 cycles

R1 DOOR EMER EXIT SIGN FELL OFF. R & R LENS IAW SIP.

Part: LIGHT — BROKEN (CABIN) · airframe 5,614 hrs · 2,344 cycles

R1 DOOR EMER EXIT LIGHT THRESHOLD ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW SIP.

Part: COVER — BROKEN (CABIN) · airframe 3,588 hrs · 1,466 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. INSTALLED COVER IAW SIP.

Part: LENS — LOOSE (CABIN) · airframe 2,386 hrs · 960 cycles

R1 DOOR LOWER LIGHT EXIT LIGHT COVER LOOSE. R & R LENS IAW SIP.