N749SW

Part: HANDLE — LOOSE (FWD PAX DOOR) · airframe 79,156 hrs · 46,447 cycles

FORWARD ENTRY DOOR HANDLE CAM PLATE IS LOOSE. RETORQUED FORWARD ENTRY DOOR HANDLE CAM PLATE IAW AMM 20-50-11.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 79,156 hrs · 46,447 cycles

LEFT HORIZONTAL STAB LOWER SLIDING SEAL CRACKED. REMOVED AND REPLACED LEFT HORIZONTAL STAB LOWER SLIDING SEAL IAW AMM 53-31-31. OPS CHECKED GOOD.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 79,156 hrs · 46,447 cycles

6 MID EMERGENCY LIGHTS FAILED TO OPERATE CORRECTLY. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS IN LOCATIONS M01668; M01669; M1670; AND M01675 REF AMM 33-51-06. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 79,120 hrs · 46,421 cycles

EMERGENCY LIGHTS OUT / [01] REPLACED ROW 17 CBA AND LH AFT GALLEY EMERGENCY BATTERY PACKS PER AMM 33-51-06. OPS CHECK GOOD

Part: PANEL — ELONGATED (WTB) · airframe 78,586 hrs · 46,076 cycles

WING TO BODY FAIRING PANEL 193B HAS SEVERAL ENLARGED HOLES. / [01] DRILLED NEW PANEL PER SRM 51-40-05;[02] R&R WING TO BODY FAIRING PANEL 193B IAW AMM 53-51-21.

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 77,797 hrs · 45,558 cycles

LIGHT ON EMERGENCY EXIT CAPTAIN SIDE IS INOP / [01] R&R LAMP ON EMERGENCY EXIT CAPTAIN SIE PER AMM 33-51-01. O.P.S CHECK GOOD.

Part: MOUNT — BROKEN (L2 DOOR SLIDE) · airframe 77,309 hrs · 45,233 cycles

L2 DOOR; FWD MOUNT FOR EVAC SLIDE HAS 1 EA. NUTPLATE BROKEN / [01] R & R L2 DOOR; FWD MOUNT FOR EVAC SLIDE NUTPLATE PER SRM 51-40-02

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 77,198 hrs · 45,161 cycles

L1 DOOR SLIDE FELL OUT OF CONTAINER WHILE OPENING DOOR / [01] REINSTALLED L1 DOOR SLIDE REF AMM 25-66-00

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 76,954 hrs · 45,019 cycles

OUTBOARD FLAP ON CAPTAINS SIDE UPPER LAYER DELAMINATED / [01] INSPECTION C/W CORRECTIVE ACTION STEPS 1 AND 2.;[02] INSPECTION C/W CORRECTIVE ACTION STEPS 1 AND 2.

Part: SLIDE — OUT OF POSITION (FWD SERVICE DOOR) · airframe 76,893 hrs · 44,984 cycles

SLIDE COMING OUT OF BOTTOM RIGHT HAND CLAM SHELL ON FWD GALLEY SERVICE DOOR / [01] FOUND VELCRO FLAP COVER FOR MANUAL ACTIVATION TUCKED UNDER OUTER COVER. REPOSITIONED FLAP COVER AND ATTACHED TO GIRT BAR WITHOUT THE OPENING OF THE SLIDE. PER SIP. OK FOR SERVICE.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 75,776 hrs · 44,311 cycles

194E PANEL HOLES ; THE 194E PANEL HAS SEVERAL HOLES ELONGATED AND CRACKED. / [01] REMOVED AND REPLACED 194E PANEL PER AMM 53-51-21

Part: PANEL — ELONGATED (FUSELAGE) · airframe 75,776 hrs · 44,311 cycles

193D PANEL HOLES ; THE 193D PANEL HAS SEVERAL HOLES ELONGATED AND CRACKED. / [01] INSTALLED NEW 193D PANEL IAW AMM 53-51-21

Part: SKIN — CRACKED (FUSELAGE) · airframe 75,776 hrs · 44,311 cycles

FUSELAGE SKIN SUBSURFACE CRACK INDICATIONS AT BS 500D+8 TO 500D+11 ABOVE STR4L USING 737 NDT PART 6;53-30-25. CONFIRMED SUBSURFACE CRACK INDICATION USING OPTION 1&4 OF TTG8Q005VW3 ; FSELAGE SKIN SSRFACE CRACK INDICATIONS AT BS 500D+8 TO 500D+11 AOVE STR4L SING 737 NDT PART 6;53-30-25. CONFIRMED SSRFACE CRACK INDICATION SING OPTION 1 (737 NDT PART 6; 53-30-18) & OPTION 4 (737 NDT PART 4; 53-30-07TR 04-07) OF TTG8Q005VW3 /

Part: UNKNOWN — ODOR (CABIN) · airframe 75,519 hrs · 44,156 cycles

ELECTRICAL SMELL EMANATING FROM ROW 9/10 F/O SIDE. C/W SMOKE OR FUMES IN THE CABIN FAULT ISOLATION IAW FIM 21-00 TASK 806. NO DEFECTS NOTED. C/W ENG RUN AT GATE; NO FUMES NOTED. A/C OK FOR SERVICE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 75,157 hrs · 43,944 cycles

PASSENGER SIDEWALL EMERGENCY EXIT LIGHT LEFT SIDE INOP ; / [01] OK TO CONTINUE PER MEL 33-2-03 SP1<BR>AUTHORIZATION # 24155; [02] PERFORMED OPS CHECK PASSENGER SIDEWALL EMERGENCY EXIT LIGHT LH IAW AMM 33-14-00. OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (CABIN LIGHT) · airframe 75,157 hrs · 43,944 cycles

CAPTAIN SIDE PAX CABIN LIGHT ON OVERWING EXIT OUT. ; / [01] RELAMPED LEFT OVERWING EXIT DOOR LIGHT IAW AMM 33-51-04

Part: SUPPORT — CRACKED (BS 500B S26L) · airframe 74,742 hrs · 43,712 cycles

CRACK ANGLE - SUPPORT LOCATED BS500B FWD FACE AND STR26L FWD CARGO COMPARTMENT ; 2021-282491 / [01] TOOL USED CALIPER P/N:700-113-10; S/N:0023244; DUE DATE: 28-SEP-21; [02] REPLACED ANGLE SUPPORT AND FASTENERS LOCTED BS 500B FWD FACE AND STR. 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 TEM 9 SRM 51-40-02 DWG.#143A7505 REV.B; [03] REPLACED ANGLE SUPPORT AND FASTENERS LOCTED BS 500B FWD FACE AND STR. 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 TEM 9 SRM 51-40-02 DWG.#143A7505 REV.B RII

Part: WEB — CRACKED (BS 500-500A) · airframe 74,742 hrs · 43,712 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500 TO BS500A AND STR26L FWD CARGO COMPARTMENT ; 2021-282489 / [01] TOOL USED CALIPER P/N:700-113-10; S/N:0023244; DUE DATE: 28-SEP-21; [02] REPLACE WEB-INTERCOSTAL LOCATED BETWEEN BS500 TO BS500A AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND 51-40-02 AND DWG 143A7505; [03] REPLACE WEB-INTERCOSTAL LOCATED BETWEEN BS500 TO BS500A AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND 51-40-02 AND DWG 143A7505.. RII ITEM

Part: WEB — CRACKED (BS 500A-500B) · airframe 74,742 hrs · 43,712 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500A TO BS500B AND STR26R FWD CARGO COMPARTMENT ; 2021-282490 / [01] TOOL USED CALIPER P/N 700-113-10 S/N 0019289 DUE DATE 25-MAR-22; [02] TOOL USED PN/ NORTEC 600D; SN/ 200048001; DE DATE/ 24FEB22; [03] TOOL USED CALIPER P/N 700-113-10 S/N 0019289 DUE DATE 25-MAR-22 RADUS GAUG P/N S167C S/N AE-35947 DUE DATE 27-JAN 22; [04] REPLACED WEB-INTERCOSTAL LOCATED BTW BS 500A TO BS 500B AT LEVEL STR. 26R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7505 SHEET 6 REV D; [05] REPAIRED WEB-INTERCOSTAL LOCATED BTW BS 500A TO BS 500B AT LEVEL STR. 26R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-30-53-2R-1 REPAIR 1; [06] REPAIRED WEB-INTERCOSTAL LOCATED BTW BS 500A TO BS 500B AT LEVEL STR. 26R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 53-30-53-2R-1 REPAIR 1 (THIS REPAIR IS PERMANENT)<BR>RII

Part: TIE CLIP — CRACKED (BS 847) · airframe 74,742 hrs · 43,712 cycles

CRACK TIE CLIP LOCATED BS847 AND STR27L AT AFT CARGO COMPARTMENT ; 2021-282480 / [01] TOOL USED CALIPER P/N 700-113-10 S/N 0019289 DUE DATE 25-MAR-22; [02] REPLACED NEW TIE CLIP LOCATED BS847 AND STR27L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 AND DWG # 146A1281-19 REV A; [03] REPLACED NEW TIE CLIP LOCATED BS847 AND STR27L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 AND DWG # 146A1281-19 REV A.VERIFIED AS RII.

Part: WEB — CRACKED (BS 927-947) · airframe 74,742 hrs · 43,712 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS927 TO BS947.5 AND STR25R AFT CARGO COMPARTMENT ; 2021-282484 / [01] REPLACED WEB INTERCOSTAL LOCATED BETWEEN BS927 TO BS947.5 AND STR25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DWG 147A7500 SHEET 12; REV-; [02] REPLACED WEB INTERCOSTAL LOCATED BETWEEN BS927 TO BS947.5 AND STR25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DWG 147A7500 SHEET 12; REV-<BR>RII

Part: SUPPORT — CORRODED (BS 727-767) · airframe 74,742 hrs · 43,712 cycles

CORROSION SUPPORT ZEE LOCATED BS727 TO BS767 AND STR25R AFT CARGO COMPARTMENT ; 2021-282482 / [01] TOOL USED CALIPER P/;: 700-113-10 S/N:0033158 DUE DATE:14-JUL-21; [02] TOOL USED CALIPER P/;: 700-113-10 S/N:0033158 DUE DATE:14-JUL-21; [03] FABRICATED SUPPORT ZEE LOCATED BS727 TO BS767 AND STR25R AFT CARGO COMPARTMENT IAW DRAWING 146A7502 REV A; [04] FABRICATED SUPPORT ZEE LOCATED BS727 TO BS767 AND STR25R AFT CARGO COMPARTMENT IAW DRAWING 146A7502 REV A MATERIAL USED BAC1496-377 7075-T62 PO. 2021 134015.; [05] FABRICATED SUPPORT ZEE LOCATED BS727 TO BS767 AND STR25R AFT CARGO COMPARTMENT IAW DRAWING 146A7502 REV A AND B737-700 SRM 51-10-02 MATERIAL USED BAC1496-377 7075-T62 PO. 2021 134015.; [06] FABRICATED SUPPORT ZEE LOCATED BS727 TO BS767 AND STR25R AFT CARGO COMPARTMENT IAW DRAWING 146A7502 REV A AND B737-700 SRM 51-10-02 MATERIAL USED BAC1496-377 7075-T62 PO. 2021 134015. <BR><BR>RII

Part: TIE CLIP — CORRODED (BS 847 S25L) · airframe 74,742 hrs · 43,712 cycles

CORROSION TIE CLIP LOCATED BS847 AND STR25L AT AFT CARGO COMPARTMENT ; 2021-282486 / [01] TOOL USED CALIPER P/N 700-113-10 S/N 0019289 DUE DATE 25-MAR-22; [02] TOOL USED: PRECISION RADIUS GAUGE; P/N S167C; S/N AE-35943; DUE DATE 04-JAN-21; [03] TOOL USED P/N: NORTEC 500D S/N:N500X12101V022237; CAL DUE DATE:24-AUG-21; [04] REPLACED NEW TIE CLIP LOCATED BS847 AND STR25L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 AND DWG # 146A1281-19 REV A; [05] REPLACED NEW TIE CLIP LOCATED BS847 AND STR25L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 AND DWG # 146A1281-19 REV A; COMPLETED RII INSPECTION

Part: INTERCOSTAL — DAMAGED (BS 500C-500D) · airframe 74,742 hrs · 43,712 cycles

ELONGATED HOLE WEB - INTERCOSTAL LOCATED BETWEEN BS 500C TO BS 500D AT LEVEL STRINGER 26L AT FWD CARGO COMPARTMENT ; 2021-282477 / [01] TOOL USED P/N: NORTEC 600D; S/N2000053402; DUE DATE: 23-APR-22; [02] REPLACED WEB -INTERCOSTAL AND FASTENERS LOCATED BTW. BS 500C TO BS 500D AT LEVEL STR. 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 DWG # 143A7505 REV A.; [03] REPLACED WEB -INTERCOSTAL AND FASTENERS LOCATED BTW. BS 500C TO BS 500D AT LEVEL STR. 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 DWG # 143A7505 REV A. RII.

Part: WEB — CRACKED (BS 500B-500C) · airframe 74,742 hrs · 43,712 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS 500B TO BS 500C AT LEVEL STRINGER 26L AT FWD CARGO COMPARTMENT ; 2021-282478 / [01] TOOL USED CALIPER P/N 700-113-10 S/N 0013356 DUE DATE 01-APR-22; [02] TOOL USED P/N NORTEC600D; S/N 2000053402;DUE DATE: 23- APR-22; [03] REPLACED WEB-INTERCOSTAL LOCATED BTW. BS 500B TO 500C STR. 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 DWG # 143A7505 REV B; [04] REPLACED WEB-INTERCOSTAL LOCATED BTW. BS 500B TO 500C STR. 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 DWG # 143A7505 REV B.<BR>RII ITEM.

Part: WEB — CRACKED (BS 460-480) · airframe 74,742 hrs · 43,712 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS 460 TO BS 480 AT LEVEL STRINGER 26L AT FWD CARGO COMPARTMENT ; 2021-282479 / [01] TOOL USED CALIPER P/N 700-113-10 S/N 0023244 DUE DATE 28-SEP-21; [02] TOOL USED P/N:NORTEC 600D S/N: 60007161486 CAL DUE DATE: 30-NOV-21; [03] REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS 460 TO BS 480 AT LEVEL STRINGER 26L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 ;51-10-02 ITEM 9 AND DRAWING #143A7505 REV:-; [04] REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS 460 TO BS 480 AT LEVEL STRINGER 26L AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 ;51-10-02 ITEM 9 AND DRAWING #143A7505 REV:-<BR>RII ACCOMPLISHED

Part: SUPPORT BRACKET — CORRODED (BS 1088) · airframe 74,742 hrs · 43,712 cycles

CORROSION SUPPORT BRACKET (STIFFERNER) LOCATED BS1088 BETWEEN RBL11 TO LBL11 AND WL217 APPROX ON APU COMPARTMENT ; 2021-282400 / [01] TOOL USED: PRECISION RADIUS GAUGE PN:S167C SN:AE-27309 DUE DATE:05-AUG-21.; [02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820023; DUE DATE: 22-JAN-22.; [03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 22-JAN-22.; [04] TOOL USED: CALIPER; P/N: 700-113-10; S/N: 0019289; DUE DATE: 25/MAR/22.; [05] REPLACED SUPPORT BRACKET (STIFFERNER) LOCATED BS1088 BETWEEN RBL11 TO LBL11 AND WL217 APPROX ON APU COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING # 148A2410 REV :-; [06] REPLACED SUPPORT BRACKET (STIFFERNER) LOCATED BS1088 BETWEEN RBL11 TO LBL11 AND WL217 APPROX ON APU COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING # 148A2410 REV :-; [07] REPLACED SUPPORT BRACKET (STIFFERNER) LOCATED BS1088 BETWEEN RBL11 TO LBL11 AND WL217 APPROX ON APU COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING # 148A2410 REV :-

Part: BULKHEAD — CRACKED (AFT CARGO) · airframe 74,742 hrs · 43,712 cycles

CRACK BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT ; 2021-282363 / [01] FABRICATED BULKHEAD PANEL 141JW LOCATED AT AFT CARGO COMPARTMENT IAW DWG 453A2510-4 REV-A ; AND B737-700 AMM 25-52-01-201-801 MATERIAL P/N USED: A60SG4W P.O: 2021 149546.; [02] FABRICATED BULKHEAD PANEL 141JW LOCATED AT AFT CARGO COMPARTMENT IAW DWG 453A2510-4 REV - ; AND B737-700 AMM 25-52-01-201-801 MATERIAL P/N USED: A60SG4W P.O: 2021 149546.; [03] FABRICATED BULKHEAD PANEL 141JW LOCATED AT AFT CARGO COMPARTMENT IAW DWG 453A2510-4 REV - ; AND B737-700 AMM 25-52-01-201-801 MATERIAL P/N USED: A60SG4W P.O: 2021 149546.; [04] NO REQUIRED INDEPENDENT INSPECTOR

Part: PLATE — CRACKED (RT WING) · airframe 74,742 hrs · 43,712 cycles

CRACK CORRUGATED PLATE LOCATED BETWEEN WS204.25 TO WS228.25 AT RT WING ; 2021-282361 / [01] REPLACED CORRUGATED PLATE LOCATED BETWEEN WS204.25 TO WS228.25 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02; [02] REPLACED CORRUGATED PLATE LOCATED BETWEEN WS204.25 TO WS228.25 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 (UPDATED PART); [03] TOOL USED CALIPER P/N: 500-464 S/N: 15045614 DUE DATE: 22/JAN/22; [04] REPLACED CORRUGATED PLATE LOCATED BETWEEN WS204.25 TO WS228.25 AT RT WING IAW B737-700 SRM 51-10-02<BR>INSPECTED OK

Part: PLATE — CRACKED (RT WING) · airframe 74,742 hrs · 43,712 cycles

CRACK CORRUGATED PLATE LOCATED BETWEEN WS228.25 TO WS253.00 AT RT WING ; 2021-282360 / [01] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED BTW WS 228.25 TO 253.00MR/H WING IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02; [02] REPLACED CORRUGATED PLATE AND FASTENERS LOCATED BTW WS 228.25 TO 253.00 R/H WING IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02

Part: SCUFF PLATE — CRACKED (CARGO THRESHOLD) · airframe 74,742 hrs · 43,712 cycles

CRACK ON SCUFF PLATE FWD POSITION AFT CARGO COMPARTMENT ; 2021-282336 / [01] REPAIRED SCUFF PLATE FWD POSITION AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B AND BAC 5975.; [02] REPAIRED SCUFF PLATE FWD POSITION AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4.B AND BAC 5975.

Part: SUPPORT ANGLE — CRACKED (RT WING TE) · airframe 74,742 hrs · 43,712 cycles

CRACK TRAILING EDGE SUPPORT ANGLE LOCATED BETWEEN WS253.00 TO WS278.50 AT RT WING ; 2021-282358 / [01] REPLACED TRAILING EDGE SUPPORT ANGLE LOCATED BETWEEN W STA 253.00 TO W STA 278.50 I.W.A B737-700 SRM 51-10-02 ITEM 9; [02] 1. JUAN CORNEJO (TECHNICIAN); 23-JUN-2021 14:20 UTC <BR>REPLACED TRAILING EDGE SUPPORT ANGLE LOCATED BETWEEN W STA 253.00 TO W STA 278.50 I.W.A B737-700 SRM 51-10-02 ITEM 9.<BR><BR><BR>TASK CARD COMPLETE.

Part: PLATE — CRACKED (LT WING) · airframe 74,742 hrs · 43,712 cycles

CRACK REAR SPAR CORRUGATED PLATE LOCATED BTW WS 204.25 TO WS 228.25 AT LT WING ; 2021-282253 / [01] REPLACED CORRUGATED PLATE LOCATED BTW WS204.25 TO WS228.25 AT LT WING. IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02; [02] REPLACED CORRUGATED PLATE LOCATED BTW WS204.25 TO WS228.25 AT LT WING. IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 74,742 hrs · 43,712 cycles

CRACK SUPPORT ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 AT LT WING ; 2021-282257 / [01] REPLACED SUPPORT ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 AT LH WING I.A.W B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02; [02] REPLACED SUPPORT ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 AT LH WING I.A.W B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02; [03] REPLACED SUPPORT ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 AT LH WING I.A.W B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 (UPDATED MATERIAL); [04] REPLACED SUPPORT ANGLE TRAILING EDGE LOCATED BTW WS 253.00 TO WS 278.50 AT LH WING I.A.W B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 (UPDATED MATERIAL)

Part: PLATE — CRACKED (LT WING) · airframe 74,742 hrs · 43,712 cycles

CRACK REAR SPAR CORRUGATED PLATE LOCATED BTW WS 228.25 TO WS 253.00 AT LT WING ; 2021-282254 / [01] REPLACED REAR SPAR CORRUGATED PLATE LOCATED BTW WS 228.25 TO WS 253.00 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING # 115A2001 REV:B; [02] JOB COMPLETED.

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 74,742 hrs · 43,712 cycles

DEBONDED OB AFT FLAP UPPER SURFACE ON IB SIDE AT LT WING. ; 2021-282247 / [01] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18165044 DUE DATE:15-FEB-22; [02] TOOL USED:HOT BONDER P/N:HCS9000B-AV S/N:18164925 DUE DATE:19-NOV-21; [03] TOOL USED CALIPER P/N: 500-197-30 S/N:15120583 DUE DATE: 11-FEB-22; CALIPER P/N:500-464 S/N:15331932 DUE DATE:18-AUG-21; THICKNESS GAUGE P/N: PROSITECTOR 6000 NS3 S/N:767584 DUE DATE:18-SEP-21; [04] REPAIRED OB AFT FLAP UPPER SURFACE ON IB SIDE AT LT WING AS PER B737-700 SRM 57-53-01-2R-16 REPAIR 16.; [05] REPAIRED OB AFT FLAP UPPER SURFACE ON IB SIDE AT LT WING AS PER B737-700 SRM 57-53-01-2R-16 REPAIR 16.; [06] REPAIRED OB AFT FLAP UPPER SURFACE ON IB SIDE AT LT WING AS PER B737-700 SRM 57-53-01-2R-16 REPAIR 16.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 74,742 hrs · 43,712 cycles

BROKEN GALLEY 1 COVER LENS OF EMERGENCY EXIT LIGHT AT FWD GALLEY AREA (1 EA) ; 2021-282210 / [01] REPLACED GALLEY 1 COVER LENS OF EMERGENCY EXIT LIGHT AT FWD GALLEY AREA (1 EA) I.A.W B737-700 AMM-33-51-01-960-801 STEP 2. B(C); [02] REPLACED GALLEY 1 COVER LENS OF EMERGENCY EXIT LIGHT AT FWD GALLEY AREA (1 EA) I.A.W B737-700 AMM-33-51-01-960-802 STEP 3C(10).; [03] REPLACED GALLEY 1 COVER LENS OF EMERGENCY EXIT LIGHT AT FWD GALLEY AREA (1 EA) I.A.W B737-700 AMM-33-51-01-960-802 AND OPERATIONAL TEST ARE GOOD.AMM 33-51-00-710-801 AND AMM 33-51-00-720-801.; [04] REPLACED GALLEY 1 COVER LENS OF EMERGENCY EXIT LIGHT AT FWD GALLEY AREA (1 EA) I.A.W B737-700 AMM-33-51-01-960-802 AND OPERATIONAL TEST ARE GOOD.AMM 33-51-00-710-801 AND AMM 33-51-00-720-801.

Part: STRINGER — CRACKED (BS 540 S24R) · airframe 74,742 hrs · 43,712 cycles

CRACK STRINGER 24R LOCATED BS 540 FWD CARGO COMPARTMENT ; 2021-282245 / [01] TOOL USED: CALIPER; P/N: 700-113-10; S/N: 0019306; DUE DATE: 14-OCT-21.; [02] TOOL USED PN 45MG; SN: 130061901; DUE DATE: 11-MAY-22; [03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22. TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [04] PERFORMED REPAIR ON STRINGER 24R LOCATED BS500D TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A; NO FURTER ACTIONS OR RE-INSPECTION REQUIRED; [05] PERFORMED REPAIR ON STRINGER 24R LOCATED BS500D TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A; NO FURTER ACTIONS OR RE-INSPECTION REQUIRED<BR>RII

Part: STRINGER — CRACKED (BS 540 S26L) · airframe 74,742 hrs · 43,712 cycles

CRACK STRINGER 26L LOCATED BS 540 FWD CARGO COMPARTMENT ; 2021-282250 / [01] TOOL USED PN/ 25 DL PLUS; SN/ 071504410;DUE DATE/ 20NOV21; [02] TOOL USED P/N NORTEC500D S/N N500X11290U021704 DUE DATE: 08-OCT-21.; [03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820023; DUE DATE: 22-JAN-22.; [04] TOOL USED: BSCULA; P/N: SCA-301; S/N: AE-412128; DUE DATE: 25-FEB-22.; [05] PERFORMED REPAIR ON STRINGER 26L LOCATED BS 500D TO BS 540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A; NO FURTHER ACTION OR RE-INSPECTION REQUIRED; [06] MADE AND DRILLED REPAIR PARTS STRINGER SECTION; ANGLE 2 E/A; CHANEL AND IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 STEP 4.D;E;F;G;H; [07] PERFORMED REPAIR ON STRINGER 26L LOCATED BS 500D TO BS 540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A; NO FURTHER ACTION OR RE-INSPECTION REQUIRED. VERIFIED AS RII.

Part: STRINGER — CRACKED (BS 540 S26R) · airframe 74,742 hrs · 43,712 cycles

CRACK STRINGER 26R LOCATED BS 540 FWD CARGO COMPARTMENT ; 2021-282248 / [01] TOOL USED: CALIPER; P/N: 700-113-10; S/N: 0019306; DUE DATE: 14-OCT-21.; [02] TOOL USED PN 45MG; SN: 130061901; DUE DATE: 11-MAY-22; [03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22. TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 22-JAN-22.; [04] PERFORMED REPAIR ON STRINGER 26R LOCATED BS500D TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1THIS REPAIR IS CATEGORY A; NO FURTER ACTIONS OR RE-INSPECTION REQUIRED; [05] PERFORMED REPAIR ON STRINGER 26R LOCATED BS500D TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1THIS REPAIR IS CATEGORY A; NO FURTER ACTIONS OR RE-INSPECTION REQUIRED.. RII ITEM

Part: STRINGER — CRACKED (BS 540 S25R) · airframe 74,742 hrs · 43,712 cycles

CRACK STRINGER 25R LOCATED BS 540 FWD CARGO COMPARTMENT ; 2021-282246 / [01] TOOL USED PN/ 25DL PLUS; SN/ 071504410; DUE DATE/ 20NOV21; [02] TOOL USED CALIPER P/N 500-197-30 S/N A18135101 DUE DATE 04 JUL 21; [03] TOOL USED P/N NORTEC500D S/N N500X11290U021704 DUE DATE: 08-OCT-21.; [04] TOOL USED: RADIUS GAGE; P/N: 2204A3; S/N: AE-408651; DUE DATE: 02-FEB-22; [05] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-22; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820023; DUE DATE: 22-JAN-22.; [06] PERFORMED REPAIR ON STRINGER 25R LOCATED BS 500C TO BS 540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A; NO FURTHER ACTION OR RE-INSPECTION REQUIRED; [07] PERFORMED REPAIR ON STRINGER 25R LOCATED BS 500C TO BS 540 FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A; NO FURTHER ACTION OR RE-INSPECTION REQUIRED; RII INSPECTION DONE.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,742 hrs · 43,712 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 36 INCH FROM FRONT SPAR LT HORIZONTAL STAB ; 2021-282158 / [01] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22; [02] TOOL USED CALIPER P/N 700-113-10 S/N 0019288 DUE DATE 28-APR-22 RADIUS GAUGE P/N 2204A3 S/N AE-408651 DUE DATE 02-FEB-22; [03] TOOL USED. P/N: NORTEC 500D. S/N: N500X11290U021704. DUE DATE: 08-OCT-21.; [04] PERFORMED REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-5 REPAIR 5. PART USED: KIT T-SECTION P/N 55100003-1.; [05] PERFORMED REPAIR INSPAR RIB LOCATED STAB STA 120.30 AT 36 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-5 REPAIR 5. PART USED: KIT T-SECTION P/N 55100003-1. COMPLETED RII INSPECTION

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,742 hrs · 43,712 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 27 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER ; 2021-282152 / [01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138203; DUE DATE: 05-MAR-22; [02] TOOL USED CALIPER P/N 700-113-10 S/N 0019288 DUE DATE 28-APR-22 RADIUS GAUGE P/N 2204A3 S/N AE-408651 DUE DATE 02-FEB-22; [03] TOOL USED. P/N: NORTEC 500D. S/N: N500X11290U021704. DUE DATE: 08-OCT-21.; [04] PERFORMED REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 27 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-5 REPAIR 5. PART USED: KIT T-SECTION P/N 55100003-1.; [05] PERFORMED REPAIR INSPAR RIB LOCATED STAB STA 120.30 AT 27 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-5 REPAIR 5. PART USED: KIT T-SECTION P/N 55100003-1. COMPLETED RII INSPECTION

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,742 hrs · 43,712 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 19 INCH FROM FRONT SPAR LT HORIZONTAL STAB ; 2021-282156 / [01] TOOL USED: P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 05-MAR-22; [02] TOOL USED CALIPER P/N 700-113-10 S/N 0019289 DUE DATE 25-MAR-22; [03] PERFORMED REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4. PART USED: KIT T-SECTION P/N 55100003-1.; [04] PERFORMED REPAIR INSPAR RIB LOCATED STAB STA 120.30 AT 19 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4. PART USED: KIT T-SECTION P/N 55100003-1; COMPLETED RII INSPECTION

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 74,360 hrs · 43,489 cycles

FWD CARGO FLOOR AFT OF DOOR HAS 11 INCH CRACK. REPAIRED FWD CARGO FLOOR PANEL PER AMM 25-52-01

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 73,775 hrs · 43,158 cycles

GIRT BAR DIFFICULT TO STOW AT R1 DOOR. REPOSITIONED R1 DOOR ESCAPE SLIDE, PER MT#:725-61-06.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 73,645 hrs · 43,089 cycles

FORWARD ENTRY DOOR ESAPE SLIDE PARTIALLY DEPLOYED. REPOSITIONED FWD ENTRY DOOR SLIDE, IAW MT 725-61-06.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 73,561 hrs · 43,037 cycles

FWD SERVICE DOOR GIRT BAR NOT SEATING PROPERLY. ADJUSTED FWD SERVICE DOOR ESCAPPE SLIDE FLAP & GIRT BAR, IAW AMM 25-66-00. ACCOMPLISHED WITHOUT REMOVING SLIDE FROM POSITION.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 73,384 hrs · 42,937 cycles

ESCAPE SLIDE FRONT RIGHT (F/O SIDE) IS LOOSE. FWD SERVICE DOOR ESCAPE SLIDE INSTALLED CORRECTLY, PER AMM 25-66-01. A/C OK FOR SERVICE STS LINE MX Q6TR841X.

Part: SEAL — BENT (HORIZONTAL STAB) · airframe 72,388 hrs · 42,311 cycles

LEFT HORIZONTAL STAB FWD LOWER SLIDING SEAL UPPER EDGE BENT IN. / REMOVED AND REPLACED LEFT HORIZONTAL STAB FWD LOWER SLIDING SEAL PER AMM 53-31-31

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 72,226 hrs · 42,209 cycles

AFT LAV SMOKE DETECTOR SOUNDING BELOW 10;000 WITH NO APARENT SMOKE / REPLACED SMOKE DETECTOR PER AMM 26-14-01 OPS CHECK'S NORMAL

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 71,723 hrs · 41,906 cycles

AFT SERVICE DOOR EMER LIGHT LENS MISSING DIRECTIONAL ARROW. / INSTALLED NEW EMERG LIGHT LENS COVER PER AMM 35-51-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,686 hrs · 41,253 cycles

R2 DOOR EMERGENCY EXIT LIGHT INOP. / RELAMPED LIGHT PER AMM.

Part: SIGN — DETACHED (CABIN) · airframe 70,585 hrs · 41,184 cycles

AFT SERVICE ENTRANCE EXIT SIGN FELL DOWN. PERFORMED EA NO: 1-A33-0131. PERFORM PERMANENT REPAIR OR REPLACEMENT OF THE LENS ON OR BEFORE 30 FLIGHT CYCLES.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 70,585 hrs · 41,184 cycles

AFT SERVICE ENTRANCE EXIT SIGN FELL DOWN. / REPAIRED LENS PER EA.

Part: ANGLE — CRACKED (L/H WING) · airframe 70,573 hrs · 41,176 cycles

LEFT WING FIXED TE UPPER PANEL HAS AFT SUPPORT ANGLE CRACKED / REMOVED AND REPLACED PER SRM 51-40-02

Part: DOOR — CORRODED (LOWER EXT FUSELA) · airframe 69,844 hrs · 40,698 cycles

INNER SURFACE OF TOILET SERVICE DOOR IS CORRODED / REMOVED AND REPLACED CORRODED TOILET SERVICE DOOR PER AMM 52-49-07-000-801 AND AMM 52-49-07-400-801. BOND TEST OF JUMPER CHECKS GOOD AT .0005 OHMS 92982U 7/21/19

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY FORWARD CORNER SCUFF PLATE CRACKED. R&R SCUFF PLATE PER SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY SHIELD, FORWARD SIDE OF DOOR CORRODED BETWEEN BS. 767 TO BS. 794, RBL 20. R&R SHIELD IAW SRM AND DWG.

Part: RETAINER — CRACKED (WING CENTER SECT) · airframe 69,844 hrs · 40,698 cycles

REAR SPAR WING CENTER SECTION RH SEAL RETAINER ASSY IS CRACKED / REMOVED AND INSTALLED NEW RH SEAL RETAINER ASSY AT REAR SPAR WING CENTER SECTION ITEM #7570349 IAW SRM 51-40-02-0G-0 DWG #111A1515; DWG#111A1000; 57319U 07-15-19.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

FORWARD CARGO BAY AFT BULKHEAD SUPPORT GUSSET CRACKED AT BS. 500D, STR. 19R. R&R GUSSET PER SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

FORWARD CARGO BAY AFT BULKHEAD SUPPORT GUSSET CRACKED AT BS. 500D, STR. 19L. R&R GUSSET PER SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

STRINGER CORRODED AT BS. 382, STR. 25L. REPAIRED STRINGER IAW SRM AND EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

FRAME STRINGER SPLICE CORRODED AT BS. 360, STR. 25L. R&R SPLICE PER SRM & DWG.

Part: STRINGER — CORRODED (FWD CARGO BAY) · airframe 69,844 hrs · 40,698 cycles

***CORROSION*** BS 360 FRAME; STR 28R-27L IS CORRODED COMMON TO BUTT SPLICE STRAP. / CORROSION ON BS360 FRAME; STR 28R-27L COMMON TO BUTT SPLICE STRAP WAS REPAIRED IAW ATS ER 19-03959; REV IR DATED 23JUL19 AND EA 1-753-35296 REV IR

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY LOWER AFT CENTER BULKHEAD SUPPORT ANGLE CORRODED AT BS. 947, LBL 16. R&R ANGLE IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

FRAME CORRODED AT BS. 360, BETWEEN STR. 24L TO STR. 27L, COMMON TO THE AFT SIDE. REPAIRED FRAME IAW ER AND EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

OUTBOARD OF AFT CARGO BAY FLOOR INTERCOSTAL CORRODED AT BS. 794.37, STR. 27R. R&R INTERCOSTAL IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY STRINGER CLIP CORRODED AT BS. 987, STR. 27R. R&R STRINGER CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY STRINGER CLIP CORRODED AT BS. 987, STR. 24L. R&R CLIP IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY STRINGER CLIP CORRODED AT BS. 987, STR. 25L. R&R STRINGER CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY FRAME CORRODED AT BS. 947, BETWEEN BS. 24R TO STR. 24L, UNDER WATER TANK MOUNT. R&R FRAME IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY STRINGER CLIP CORRODED AT BS. 987+3, STR. 25L. R&R STRINGER CLIP IAW SRM AND DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY FRAME CORRODED AT BS. 967, BL 0. REPAIRED FRAME IAW ER AND EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY STRINGER CLIP CORRODED AT BS. 987+3, STR. 24L. R&R CLIP IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

STRINGER CORRODED AT BS. 374, STR. 26L. REPAIRED STRINGER IAW SRM, EA, AND ER.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

INTERNAL DOUBLER FOR TCAS ANTENNA CORRODED AT BS. 294.5+12.5, RBL 2. REPAIRED DOUBLER PER SRM & DWG.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 69,844 hrs · 40,698 cycles

L/H HORIZ STAB RIB AT STAB STA 120.3 3RD VERTICAL STIFFENER FROM FRONT IS CRACKED AT LOWER END. / TRIMMED CRACKOUT 0.350' X 0.334'; NDI NO DEFECTS NOTED; REPAIRED IAW SRM 55-10-09-2R-5; 3RD STIFFENER LH.H. STAB RIB STA 120.3

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

FORWARD CARGO BAY INTERCOSTAL ATTACH ANGLE CRACKED AT BS. 500C, RBL 25. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

FORWARD CARGO BAY AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE CORRODED AT BS. 500D, LBL 25. R&R ANGLE PER SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

FWD CARGO BAY INTERCOSTAL ATTACH ANGLE CRACKED AT BS. 500C, LBL25. R&R ATTACH ANGLE PER SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 69,844 hrs · 40,698 cycles

PASSENGER CABIN FLOOR PANEL 232RF IS DELAMINATING / DUE TO THE EXTENT OF DELAMINATION DAMAGE; FABRICATED NEW PASSENGER CABIN FLOOR PANEL 232RF USING BMS 4-17 TY6 LOT#1397799-1; INSTALLED INSERTS USING BMS 5-107 LOT#AK8KD4895K AND PART MARKED IAW SRM 53-00-50-2R-0 1A(NOTE); TABLE 204; 5S AND DWG 144A5810-4. 57066U 6/30/19

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

FORWARD CARGO BAY AFT BULKHEAD SUPPORT GUSSET CRACKED AT BS. 500D, STR. 19L. R&R GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (FWD CARGO RH) · airframe 69,844 hrs · 40,698 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / REMOVED AND REPLACED CRACKED GUSSET AT BS 500D S19R; WL193 I/A/W S.R.M. 51-40-02 AND DWG# 143A7902

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

FORWARD CARGO BAY AFT BULKHEAD SUPPORT GUSSET CRACKED AT BS. 500D, STR. 21L. R&R GUSSET IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

INBOARD SIDE OF STRINGER CLIP CORRODED AT BS. 787, STR. 27L. R&R STRINGER CLIP PER SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

OUTBOARD OF AFT CARGO BAY FLOOR INTERCOSTAL CORRODED AT BS. 787, STR. 27R. R&R INTERCOSTAL IAW SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY DOOR THRESHOLD STRAP CORRODED BETWEEN BS. 794 TO BS. 847, RBL 21. R&R THRESHOLD STRAP IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY FLOOR CARGO TRACK CORRODED AT BS. 847, RBL 14. R&R FLOOR TRACK IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY FLOOR STRAP CORRODED AT BS. 727D+5, BETWEEN RBL 21 TO LBL 21. R&R STRAP IAW SRM.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY FLOOR CHANNEL SUPPORT PLATE CORRODED BETWEEN BS. 727D TO BS. 767, LBL 21. R&R SUPPORT PLATE AW DWG & SRM.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 69,844 hrs · 40,698 cycles

AFT CARGO BAY FLOOR TRACK CRACKED BETWEEN BS. 727+4 TO BS. 887, RBL 14. R&R FLOOR TRACK IAW SRM AND DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

BULKHEAD HORIZONTAL STIFFENER CRACKED AT BS. 663, RBL 6. R&R STIFFENER PER SRM & DWG.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

VERTICAL STIFFENER FASTENER CRACKED AT BS. 663, RBL 6. R&R STIFFENER PER SRM & DWG.

Part: STRINGER — OUT OF TOLERANCE (AFT FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

AFT PRESSURE BULKHEAD FASTENER HOLE 5R AT STR-2R LARGER THAN TOLERANCE (REF 12107-53 STEP11.D.) / AFT PRESSURE BULKHEAD FASTENER HOLE 5R STRINGER 2 R/H REPAIRED PER CARD 12107-53 STEP 13A. 91195U 6-22-19

Part: BULKHEAD — OUT OF TOLERANCE (AFT FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

SI# 12107-53; STEP 11. F. FASTENER LOCATION 6R MEASURES .377; OUT OF TOLERANCE PER SI# 12107-53 / AFT PRESSURE BULKHEAD FASTENER HOLE 6R REPAIRED PER CARD 12107-53 STEP 13C. 91195U 6-22-19

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,844 hrs · 40,698 cycles

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

Part: FRAME — CRACKED (FUSELAGE FAIRING) · airframe 69,844 hrs · 40,698 cycles

CRACKED AROUND FASTENER ON WING TO BODY FAIRING PANEL VERTICAL SUPPORT AT BS. 500D, OUTBOARD OF STR. 19L. R&R FRAME IAW DWG AND SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 69,844 hrs · 40,698 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS. 665, RBL 41. REPAIRED DECK IAW SRM.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,844 hrs · 40,698 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS. 665, LBL 32. REPAIRED WEB IAW EA AND ER.

Part: BEAM — CRACKED (R1 DOOR) · airframe 69,844 hrs · 40,698 cycles

R1 DOOR #5 (UPPER) BEAM CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. REPAIRED BEAM ON WO.

Part: FLOOR PANEL — DENTED (COCKPIT) · airframe 69,844 hrs · 40,698 cycles

FLIGHT DECK FLOOR DENTED AT BS. 255, BETWEEN RBL 3 TO RBL 10. REPAIRED FLIGHT DECK FLOOR PER EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,844 hrs · 40,698 cycles

RT WING #5 SLAT NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 69,844 hrs · 40,698 cycles

LOWER COMPOSITE BULKHEAD CRACKED AT BS. 663, RBL 10. R&R BULKHEAD IAW SRM & DWG.

Part: LENS — OUT OF POSITION (CABIN) · airframe 69,844 hrs · 40,698 cycles

LT #6 OVERHEAD STOWBIN EMERGENCY LIGHT PROTRUDING FROM CUTOUT. R&R LENS IAW AMM.

Part: COVER — MISSING (R2 DOOR) · airframe 69,471 hrs · 40,453 cycles

R2 DOOR SLIDE MANUAL INFLATE HANDLE COVER MISSING. REPOSITIONED SLIDE COVER PER MT.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 68,862 hrs · 40,077 cycles

AFT CARGO FLOOR SUPPORT CRACKED AT BS 727E, RBL 13.8. R&R SUPPORT PER SRM.

Part: SCUFF PLATE — CORRODED (AFT CARGO THRESH) · airframe 68,862 hrs · 40,077 cycles

AFT CARGO COMPARTMENT AFT OF DOOR THRESHOLD SCUFF PLATE CORRODED / REMOVED AND REPLACED AFT CARGO COMPARTMENT AFT OF DOOR THRESHOLD SCUFF PLATE PER AMM 53-11-02

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 68,862 hrs · 40,077 cycles

AFT CARGO COMPARTMENT STA 947 FLOOR STRAP CORRODED / REMOVED AND REPLACED AFT CARGO COMPARTMENT STA 947 FLOOR STRAP PER AMM 25-52-10

Part: FITTING — CORRODED (RT M LG TRUNNION) · airframe 68,795 hrs · 40,030 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING INBOARD LOWER LUG INNER FACE CORRODED. REPAIRED FITTING PER SRM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,795 hrs · 40,030 cycles

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

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,795 hrs · 40,030 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING INBOARD LOW LUG INNER FACE CORRODED. REPAIRED FITTING PER SRM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,795 hrs · 40,030 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,795 hrs · 40,030 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG INNER FACE CORRODED. REPAIRED FITTING PER SRM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,795 hrs · 40,030 cycles

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

Part: VAPOR BARRIER — CRACKED (WHEEL WELL RH) · airframe 68,628 hrs · 39,924 cycles

FOUND 13' CRACK ON RH WHEEL WELL FWD UPPER BARRIER BETWEEN RBL 6.15 AND RBL 15.54 AND A 20' CRACK IN THE PACK BAY SIDE. TRANSFERRED FROM 0812282. / REPAIRED 5' SECTION OF CRACK PER SRM 51-70-04 REPAIR 10. APPLIED INTERIM REPAIR ON REMAINING 15' OF CRACK OER SRM 57-10-10-1A-2. INTERIM REPAIR APPLIED TO 8' SECTION ABOVE AND 7' SECTION BELOW THE PERMANENT REPAIR.

Part: BRACKET — CRACKED (LOWER EXT FUSELA) · airframe 66,666 hrs · 38,668 cycles

RT WING TO BODY BRACKET AT STA 663 AND WING ROOT CRACKED / REMOVED AND REPLACED RH WING TO BODY BRACKET I.A.W. SRM 51-40-02

Part: LENS — BROKEN (CABIN) · airframe 64,998 hrs · 37,612 cycles

LT EMERGENCY BULLNOSE LIGHT LENS BROKEN AT ROW 12. R&R LIGHT IAW AMM.

Part: BRACKET — CRACKED (VERTICAL STAB) · airframe 64,572 hrs · 37,338 cycles

SUPPLEMENTAL INFORMATION: SKATE ANGLE ATTACH BRACKET CRACKED; PANEL 324AR / REPLACED CRACKED SKATE ANGLE BRACKET ON PANEL 324AR PER SRM 51-40-02

Part: BRACKET — CRACKED (VERTICAL STAB) · airframe 64,572 hrs · 37,338 cycles

SUPPLEMENTAL INFORMATION: SKATE ANGLE ATTACH BRACKET CRACKED; PANEL 323CR / REMOVED AND REPLACED SKATE ATTACH BRACKET PER SRM 51-40-02

Part: HANDLE — LOOSE (R2 DOOR SLIDE) · airframe 63,397 hrs · 36,606 cycles

R2 DOOR SLIDE INFLATION HANDLE LOOSE. SECURED THE HANDLE IAW AMM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,290 hrs · 36,543 cycles

LEFT OVERWING FUSELAGE MOUNTED EMERGENCY EXIT LIGHT INOPERATIVEF. RESET POWER SUPPLY BATTERY IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 63,290 hrs · 36,543 cycles

R1 DOOR EMERGENCY LIGHT FAILED. R&R BATTERY PACK IAW AMM.

Part: STRIP — CRACKED (AFT CARGO BAY) · airframe 63,290 hrs · 36,543 cycles

AFT CARGO AFT L/H CAP STRIP IS CRACKED / REPLACED CRACKED CAP STRIP FOR AFT CARGO AFT L/H STRIP IAW BOEING P.L 453A2611

Part: INTERCOSTAL — CRACKED (LT MLG WW) · airframe 63,290 hrs · 36,543 cycles

LT MAIN LANDING GEAR WHEEL WELL AFT SIDE INTERCOSTAL WEB CRACKED AT BS 663, LBL 28.5. R&R WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (FWD CARGO BAY) · airframe 63,290 hrs · 36,543 cycles

FWD CARGO BAY L/H Z ANGLE BAFFLE CLIP CRACKED AT STA 500A FWD SIDE OF FRAME / REMOVED AND REPLACED BAFFLE CLIP AT FWD SIDE OF FRAM E STA 500A LH SIDE IAW SRM 51-40-02-0-0G-0 REV A ID 14 PN 143A7502U159

Part: ANGLE — MISSING (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

L1 CREASE BEAM LOWER SIDE ANGLE MISSING BETWEEN BS 270 TO BS 277. INSTALLED ANGLE IAW SRM AND DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 63,290 hrs · 36,543 cycles

RT WING OUTBOARD AFT FLAP INBOARD EDGE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

FLOORBEAM UPPER ''T'' CAP UNDER CREASE BEAM WEB CRACKED AT BS. 294, RBL 51. REPAIRED T CAP IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

FLIGHT DECK FIRST OFFICER SEAT, INBOARD FORWARD SEAT TRACK, FORWARD END OF VERTICAL WEB CRACKED. R&R SEAT TRACK IAW SRM.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 63,290 hrs · 36,543 cycles

RT AIR CONDITION PACK BAY ANGLE CRACKED AT BS 663, RBL 8. R&R ANGLE IAW EA.

Part: FITTING — CRACKED (LEFT WING) · airframe 63,290 hrs · 36,543 cycles

LEFT WING INBOARD OF DEFLECTOR RIB; FORWARD OF VERTICAL WEB; CURVED MIDSPAN GREEN ANGL IS CRACKED AT THE TOP. / REMOVED CRACKED FITTING AT LEFT WING INBOARD OF DEFLECTOR RIB; FORWARD OF VERTICAL WEB; IAW SRM 51-40-02-0G-00 DRILLED NEW FITTING IAW SRM SRM 51-40-05-0G-00 AND IPC 57-50-00-25. INSTALLED NEW FITTING IAW SRM 51-40-05-0G-00. AND IPC LLED NEW 57-50-00-25. RM 51-40-05-0G-00.

Part: DOUBLER — CRACKED (WHEEL WELL RH) · airframe 63,290 hrs · 36,543 cycles

RIGHT WHEEL WELL STATION 663; HORSESHOE ATTACH ANGLE ABOVE RIGHT A/C PACK EXHAUST IS CRACKED ON INBOARD FLANGE AS MARKED. / REMOVED DAMAGED HORSESHOE DOUBLER AND INSTALLED NEW HORSESHOE DOUBLER. RE-APPLIED CORROSION INHIBITING COMPOUND. R/H WHEEL WELL STA. 663 ABOVE RIGHT AC EXHAUST I.A.W. B737 SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; AMM 01-00-02-SWA-002; DWG. NO. 11A1515 SHT. 1. DOUBLER P/N: 111A1512-1 ATAG XM0247

Part: ANGLE — CRACKED (RIGHT WING) · airframe 63,290 hrs · 36,543 cycles

RIGHT WING TRAILING EDGE DEFLECTOR RIB MIDSPAN RIB CURVED ATTACH ANGLE CRACKED AT TOP . / REMOVED AND REPLACED RT. WING TRAILING EDGE DEFLECTOR RIB MID SPAN CURVED ATTACH ANGLE IAW SRM 51-40-02-0G-0 AND IPC 57-50-00-25 AND APPLIED C.I.C IAW AMM 51-21-91 ATS# A27219

Part: ANGLE — CRACKED (RIGHT WING) · airframe 63,290 hrs · 36,543 cycles

RIGHT WING DEFLECTOR RIB INBOARD ATTACH ANGLE CRACKED AT LOWER ATTACH POINT. / REMOVED AND REPLACED RT. WING INBOARD ATTACH ANGLE IAW SRM 51-40-02-0G-0 AND IPC 57-50-00-25 AND APPLIED C.I.C IAW AMM 51-21-91 ATS# A48108

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

R1 DOOR CUTOUT STUB FRAME CRACKED AT BS. 294, INBOARD FASTENER HOLE AT CREASE BEAM CHORD. REPAIRED STUB FRAME IAW SRM.

Part: SUPPORT STRAP — CORRODED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

R1 DOOR CREASE BEAM CHORD SUPPORT STRAP CORRODED BETWEEN BS 277 TO BS 301. R&R STRAP IAW DWG AND SRM.

Part: ANGLE — CRACKED (RIGHT WING) · airframe 63,290 hrs · 36,543 cycles

RIGHT WING LOWER PANEL 651DB ATTACH ANGLE BROKEN AT FORWARD ATTACH POINT. / REMOVED AND REPLACED CLIP PLN 115A 552-2 IAW B737-700 SRM 51-40-02-0G-0 STEP 7.D. AND DWGS 115A2001 REV-; 115A5552 REV A. ATAG A48565

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,290 hrs · 36,543 cycles

CABIN FLOOR PANEL 242AF HAS FASTENER INSERT PULLED THRU. MARKED. / CLEANED; PREPPED AND REPAIRED FASTENER HOLE AT FWD O/B EDGE ON FLOORBOARD 242AF AND REPLACE INSERT IAW B737 SRM 53-00-50-2R-1; PAR 3 (A-C;F;K1;L1;M1;N) REV 61

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,290 hrs · 36,543 cycles

CABIN FLOOR BOARD 221AF HAS SEVERAL CORRODED INSERTS AND AN AREA OF DELAMINATION. / CLEANED; PREPPED AND REPAIRED DAMAGE TO TOP SKIN PLIES AND REPLACED DAMAGED INSERTS ON FLOORBOARD 221 AF IAW B737 SRM 53-00-50-2R-1; PAR 3 (A-C; F; K1;L1;M1;N) REV 61

Part: FLOOR PANEL — FRAYED (CABIN) · airframe 63,290 hrs · 36,543 cycles

PASSENGER COMPARTMENT FLOOR BOARD 241EF HAS AREAS OF FRAYED LAMINATE. / PREPPED; CLEANED AND REPAIRED DAMAGE TO TOP SKIN AND DELAM AT AFT I/B EDGE IAW B737 SRM 53-00-50-2R-9; PAR 4 (A-C; E-K1; L1 M1;N) REV 61

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

R1 DOOR LOWER SILL CREASE BEAM ATTACH ANGLE CORRODED. R&R ANGLE IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

CREASE BEAM ANGLE CORRODED BETWEEN BS 695 TO BS 706, LBL 65. R&R CREASE BEAM IAW DWG.

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 63,290 hrs · 36,543 cycles

AFT CARGO COMPARTMENT CAPSTRIP MARKED #1 R/H IS CORRODED SEVERAL PLACES. / VERIFIED AFT CARGO CAPSTRIP NO. 1 R/H HAS CORROSION OVER 50% MATERIAL LOSS; THERE ARE NO ESTABLISHED LIMITS. CAP STRIP OUT OF LIMITS. REPLACED CORRODED CAP STRIP WITH NEW CAP STRIP. IAW DWG NO. 453A2600 REV B.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 63,290 hrs · 36,543 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140CF IS CORRODED AT EDGES SEVERAL PLACES. / REMOVED CORROSION AT AFT CARGO COMPARTMENT FLOOR PAN EL 140CF; VERIFIED MATERIAL LOSS ORIG 'T' 0.080'; RE MOVED 0.025'; REMAIN 0.055'; FOUND TO BE OUT OF LIMI TS; OBTAINED SMAL FOR P/N; 453A2610-2 PO#7252490-32; VERIFIED MATERIAL AS 2024T3 0.080' ATAG;A82803; FAB RICATED NEW FLOOR PANEL; TREATED AND PRIMED AS NECES SARY; IDENTIFED NEW PART PERFORMED FINAL VISUAL INSP ECTION; ACCOMPLISHED CONFORMITY INSPECTION IAW SRM 5 1-10-02-00-0; 53-00-53-1A-1; 51-20-01-06-0; 5.D; AMM 51-21-72-370-804; 5.E. AND BOEING DWG #453A2610 REV . D RSQM QC1-10-18

Part: ANGLE — CORRODED (FED THRESHOLD) · airframe 63,290 hrs · 36,543 cycles

L-1 DOOR LOWER SILL WEB CREASE BEAM ATTACH ANGLE CORROSION AROUND FASTENER HOLES / REMOVED CORROSION FROM L-1 DOOR LWR SILL CREASE BEAM ATTACH ANGLE. ATTACH ANGLE ORIGINAL THICKNESS IS .080'; REMOVED .067' MATERIAL LOSS; REMAINING THICKNESS .013'. L-1 CREASE BEAM ATTACH ANGLE OUT OF LIMITS. REMOVED CORRODED ATTACH ANGLE AND INSTALLED NEW ATTACH ANGLE. I.A.W BOEING DWG. NO.

Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

CABIN FLOOR BOARD 221EF HAS NUMEROUS DENTS AND AREAS OF DELAMINATION. / PREPPED; CLEANED AND REPAIRED MULTIPLE DENTS ON TOP SURFACE; DELAM AT FWD O/B CORNER AND PUNCTURES ON BOTTOM SURFACE ON FLOORBOARD 221EF IAW B737 SRM 53-00-50-2R-9; PAR 4 (A-K1; L1; M1) REV 61.

Part: FLOOR PANEL — FRAYED (CABIN) · airframe 63,290 hrs · 36,543 cycles

PASSENGER COMPARTMENT FLOOR BOARD 241FF HAS AREAS OF FRAYED LAMINATE. / PREPPED; CLEANED AND REPAIRED DAMAGE TO TOPSKIN ON FLOORBOARD 241FF IAW B737 SRM 53-00-50-2R-1 PAR 3 (A-C; E; F; K1; L1; M1;N) REV 61

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

INTERCOSTAL UPPER FLANGE CRACKED BETWEEN BS 344 TO BS 360, RBL 11. REPAIRED INTERCOSTAL PER SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 63,290 hrs · 36,543 cycles

AFT CARGO PI FWD CORNER SCUFF PLATE CRACKED / AFT CARGO PIT FWD CORNER SCUFF PLATE REPAIRED ON SHOP W/O 35611-1000-0002

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 63,290 hrs · 36,543 cycles

FLOOR SUPPORT CRACKED AT BS 312 TO 328, RBL 32. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 284) · airframe 63,290 hrs · 36,543 cycles

FUSELAGE FLOOR SUPPORT CRACKED AT BS 284, BL 0. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,290 hrs · 36,543 cycles

PASSENGER COMPARTMENT FLOOR PANEL 242TF HAS AREAS OF DELAMINATINO ON TOP. 1 PLY / REPAIRED PASSENGER COMPARTMENT FLOOR PANEL 242TF FOR SKIN INBOARD SIDE AS REQ IAW B737 SRM 53-00-50-2R-1 PAR 3 (A-C; E-F; K-M) REV 61 A38329; A76585; A37325; A30640; A34707

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

R1 DOOR CREASE BEAM THRESHOLD STRUCTURE CORRODED AROUND FASTENER HOLES. R&R CREASE BEAM IAW DWG AND SRM.

Part: THRESHOLD — CORRODED (FED THRESHOLD) · airframe 63,290 hrs · 36,543 cycles

L-1 DOOR THRESHOLD STRUCTURE HAS CORROSION AS MARKED; / REMOVED CORROSION FROM L-1 DOOR 2 STRUCTURE. Z STRUCTURAL ORIGINAL THICKNESS .050'; REMOVED MATERIAL LOSS .007'; REMAINING THICKNESS .043'. Z STRUCTURAL OUT OF LIMITS. REMOVED CORRODED Z STRUCTURAL AND INSTALLED NEW Z STRUCTURE. I.A.W. BOEING DWG. NO. 141A8110 REV. A; B737 SRM 51-40-02-0G-0; SRM 51-40-05-06-0

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, LBL 34. REPAIRED INTERCOSTAL IAW EA.

Part: PANEL — ELONGATED (LH PYLON) · airframe 63,290 hrs · 36,543 cycles

NO.1 ENGINE PYLON THUMBNAIL PANEL 431AT AFT ATTACH PIN PLATE HOLES; WORN AND ELONGATED BOTH LOCATIONS. / REMOVED AND REPLACED (2EA) PIN PLATES AT NO. 1 ENGIN E PYLON THUMBNAIL PANEL 431AT IAW B737 SRM 51-40-02 PARA 9.

Part: ANGLE — CRACKED (LEFT WING) · airframe 63,290 hrs · 36,543 cycles

LEFT WING FIXED TRAILING EDGE PANEL AFT OF NO. 1 PYLON; DEFLECTOR ATTACH ANGLE CRACKED AT OUTBOARD FASTENER ATTACH POINT. MARKED. / REMOVED & REPLACED L/H WING DEFLECTOR ATTACH ANGLE ON FIXED T/E PNL AFT OF #1 PYLON IAW B737-700 SRM 51-40-02 STEP 4B. PN 115A215607 ATAG #XM0232

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 63,290 hrs · 36,543 cycles

FLOOR SUPPORT CRACKED AT BS 312 TO 328, LBL 46. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

RT CREASE BEAM CORRODED BETWEEN BS 947 TO BS 980. R&R CREASE BEAM IAW DWG & SRM.

Part: BEAM — CORRODED (AED THRESHOLD) · airframe 63,290 hrs · 36,543 cycles

PASSENGER CABIN AFT ENTRY DOOR SILL INBD ATTACH POINT HAS CORROSION AS MARKED. / REMOVED CORROSION AT AFT ENTRY DOOR SILL INBD ATTACH POINT IAW SRM 53-70-15-1A-1 PAR 2A ORIG T .080 REM T .056 LOSS OF .024 FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1 FIG 103. REMOVED AND REPLACED CREASE BEAM I.A.W. SRM 51-40-02-0G-0 AND DWG 147A8501.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

INTERCOSTAL CRACKED AT BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,290 hrs · 36,543 cycles

PASSENGER COMPARTMENT FLOOR PANEL 242VF HAS AREAS OF DELAMINATINO ON TOP. / __REPAIRED PASSENGER COMPARTMENT FLOOR PANEL 242VF __TOP SKIN AS REQ IAW B737 SRM 53-00-50-2R-1 PAR 3 __(A-F); K-N) REV 61.A38329; A76585; A34707; __A78366;A16468

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 63,290 hrs · 36,543 cycles

PASSENGER COMPARTMENT FLOOR PANEL 242UF HAS AREAS OF DELAMINATINO ON TOP. / REPAIRED TOP SKIN OF PASSENGER COMPARTMENT FLOOR PANEL 242 OF PER IAW B737 SRM 55-00-50-2R-1 PAR 3 (A-F; K-M) REV 61 A30329; A76985

Part: RIB — CRACKED (LEFT WING) · airframe 63,290 hrs · 36,543 cycles

LEFT WING FIXED TRAILING EDGE PANEL AFT OF NO. 1 PYLON; DEFLECTOR RIB CRACKED AT LOWER FASTENER ATTACH POINT. MARKED. / REMOVED SEAL RETAINER FROM WEB ASSEMBLY AT LEFT WING FIXED TRAILING EDGE PANEL AFT OF NO. 1 PYLON; DEFLECTOR RIB. IAW SRM 51-40-02-0G-00. DRILLED NEW WEB ASSEMBLY IAW SRM 51-40-05-0G-00 AND IPC 57-56-00-25. INSTALLED SEAL RETAINER TO NEW WEB ASSEMBLY IW SRM 51-40-02-0G-00 AND IPC 57-50-00-25.

Part: FLOOR PANEL — FRAYED (CABIN) · airframe 63,290 hrs · 36,543 cycles

PASSENGER COMPARTMENT FLOOR PANEL 241XF HAS AREAS OF FRAYED TOP. / PREPPED; CLEANED AND REPAIRED DAMAGE TO TOPSKIN ON FLOORBOARD 241XF IAW B737 SRM 53-00-50-2R-1 PAR 3 (A-C; E; F; K1; L1; M1;N) REV 61

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

LT CREASE BEAM INBOARD CHORD CORRODED ON UPPER SURFACE BETWEEN BS 349 TO BS 357. R&R CREASE BEAM IAW DWG.

Part: PANEL — CORRODED (LOWER EXT FUSELA) · airframe 63,290 hrs · 36,543 cycles

FWD KEEL BEAM PANEL 192E; FWD PANEL SUPPORT STRUCTURE; HAS MULTIPLE WEAR MARKS AND CORROSION. / REMOVED CORROSION AND WEAR MARKS ON FWD KEEL BEAM SUPPORT STRUCTURE FOR PANEL 192E. VERIFIED MATERIAL LOSS. ORIGINAL THICKNESS .110; REMAINING .094 LOSS OF .016. OUT OF LIMITS IAW SRM 53-30-71-1A-1. REPAIRED IAW AAR EA 170215 IR AND SWA EA 1-A753-31316 REV IR.

Part: RAIL — CORRODED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT TIE DOWN RAIL CORRODED AT BS 934, RBL 13. R&R TIE DOWN RAIL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

AFT CARGO FLOOR SUPPORT CORRODED AT BS 727A+4, RBL 3. REPAIRED SUPPORT IAW SRM.

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 63,290 hrs · 36,543 cycles

AFT CARGO COMPARTMENT STA 887 LBL 9 TO RBL 21 FLOORBOARD SPLICE STRAP HAS CORROSION AT FASTNER HOLES. / REMOVED CORROSHION FROM FLOOR BOARD SPLICE STRAP STA 887 LBL 9 TO RBL 21. NO LIMITS FOUND FOR STRAP. FOUND STRAP OUT OF LIMITS. LOCATED AND DRILLED NEW SPLICE STRAP FOR FLOOR BOARDS AT STA 887 P/N 146A9401U39; A TAG WN7856. INSTALLED NEW FLOOR BOARD SPLICE STRAP IN AFT PIT AT STA 887 LBL 9 TO RBL 21 IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0; SRM 53-00-53-1A-2 DWG 149A8104; DWG 146A7500

Part: CARGO TRACK — CORRODED (BS 927-947) · airframe 63,290 hrs · 36,543 cycles

AFT CARGO BAY CARGO TRACK FASTENER HOLES CORRODED BETWEEN BS 927 TO 947, LBL 3. R & R THE CARGO TRACK IAW SRM & DWG.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 63,290 hrs · 36,543 cycles

AFT CARGO RT CARGO TIE DOWN CORRODED BETWEEN BS 787 TO BS 847. R&R TIE DOWN IAW EA & SRM.

Part: SCUFF PLATE — CRACKED (FED THRESHOLD) · airframe 63,290 hrs · 36,543 cycles

R-1 DOOR CENTER SCUFF PLATE CRACKED / R-1 DOOR CENTER SCUFF PLATE REPAIRED IAW EA 1-A53-2076 REV.11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT RAIL CORRODED AT BS 945, LBL 3. REPAIRED SUPPORT IAW SRM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

FORWARD PIT AFT BULKHEAD LOWER ATTACH ANGLE CORRODED AT BS 500D. R&R ANGLE IAW SRM AND DWG.

Part: SHIELD — CORRODED (AFT CARGO COMPT) · airframe 63,290 hrs · 36,543 cycles

AFT CARGO; RH STA 767 TO 787; SHIELD HAS MULTIPLE AREAS OF CORROSION / REMOVED CORROSION FROM SHIELD FROM ST 767 TO 787 ON R/H SIDE ORG THICKNESS .050'; REMAINING .033' LOSS .017'; FOUND SHIELD TO BE OUT OF LIMITS. REMOVED OUT OF LIMITS SHIELD. LOCATED AND DRILLED NEW SHIELD AND INSTALLED NEW SHIELD FROM STA 767 TO 787 IN RH SIDE OF AFT CARGO WET WITH SEALANT. APPLIED CIC TO SHIELD IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0; SRM 53-60-15-01-1; SRM 51-40-05-0G-0; DWG 146A0081 DWG 146A8320; AMM 51-21-91-620-802

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

FORWARD PIT LT Z-ANGLE CORRODED BETWEEN BS 500A TO BS 500D. R&R Z ANGLE IAW SRM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,290 hrs · 36,543 cycles

AFT CARGO LT "Z" CHANNEL CORRODED BETWEEN BS 727 TO BS 787. R&R "Z" CHANNEL IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,290 hrs · 36,543 cycles

RT WING NR 7 SLAT LOWER SURFACE OF LEADING EDGE NOSE SKIN AT ACTUATOR CRACKED. REPAIRED SKIN IAW SRM.

Part: COVER — LOOSE (CABIN) · airframe 62,625 hrs · 36,180 cycles

FORWARD EMERGENCY EXIT LIGHT COVER LOOSE. R&R LIGHT ASSEMBLY IAW AMM.

Part: STIFFENER — CRACKED (BS 663) · airframe 61,008 hrs · 35,220 cycles

STIFFENER EXTENSION CRACKED AT BS 663, RBL 25. R & R STIFFENER IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 60,850 hrs · 35,131 cycles

RIGHT EMERGENCY EXIT BULLNOSE LENS LOOSE AT ROW 2. SECURED LENS IAW SIP.

Part: SIGN — BROKEN (CABIN) · airframe 60,562 hrs · 34,957 cycles

RIGHT OVERWING EMERGENCY EXIT SIGN ON WALL BROKEN. R & R SIGN IAW MM.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 60,558 hrs · 34,954 cycles

RIGHT OVERWING EXIT SIGN BROKEN. R & R THE SIGN IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 60,562 hrs · 34,957 cycles

R2 DOOR EMERGENCY EXIT SIGN ON WALL BROKEN. R & R SIGN IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 60,562 hrs · 34,957 cycles

LEFT WING EMERGENCY EXIT SIGN ON WALL BROKEN. R & R SIGN IAW MM.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 60,558 hrs · 34,954 cycles

LEFT OVERWING EXIT SIGN BROKEN. R & R THE SIGN IAW MM.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 60,558 hrs · 34,954 cycles

R2 DOOR EXIT SIGN BROKEN. R & R IAW SIGN IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 59,721 hrs · 34,465 cycles

OVERWING CEILING EXIT SIGN LOOSE. R & R SIGN IAW AMM.

Part: LIGHT — MISSING (CABIN) · airframe 59,303 hrs · 34,210 cycles

AFT CEILING EMER EXIT LIGHT MISSING. INSTALLED LIGHT ASSEMBLY IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,674 hrs · 33,850 cycles

EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATION M1670. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,674 hrs · 33,850 cycles

EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATION M1669. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,674 hrs · 33,850 cycles

EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATION M1673. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 58,674 hrs · 33,850 cycles

EMERGENCY BATTERY FAILED CAPACITY CHECK AT LOCATION M1672. R & R BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,282 hrs · 33,609 cycles

LEFT EMER LIGHT INOPERATIVE AT SEAT ROW 24. RELAMPED LIGHT IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 56,790 hrs · 32,745 cycles

G1 GALLEY EMER EXIT LOCATOR LIGHT INOPERATIVE. R & R FUSE IAW CMM.

Part: LENS — MISSING (CABIN) · airframe 56,790 hrs · 32,745 cycles

LEFT EMER STOW BINS LIGHT LENS MISSING BETWEEN ROW 9 TO 20. INSTALLED LENS IAW AMM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

VERTICAL PRESS WEB CRACKED AT BS 663. REPAIRED WEB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 56,790 hrs · 32,745 cycles

LEFT HORIZONTAL STABILIZER RIB 92.7 CRACKED, 19" FROM FWD SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 56,790 hrs · 32,745 cycles

LEFT HORIZONTAL STABILIZER RIB 92.7, CRACKED 38.5" FROM FWD SPAR. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 56,790 hrs · 32,745 cycles

LEFT HORIZONTAL STABILIZER, RIB 92.7, CRACKED 29" FROM FWD SPAR. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 56,790 hrs · 32,745 cycles

LEFT HORIZONTAL STABILIZER RIB 92.7, CRACKED 10.5" FROM FWD SPAR. REPAIRED RIB IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 56,790 hrs · 32,745 cycles

LEFT WING OTBD AFT FLAP DELAMINATED. REPAIRED FLAP IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 56,790 hrs · 32,745 cycles

RIGHT HORIZONTAL STABILIZER INTERNAL RIB 129.5 VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW EA.

Part: WEB — CRACKED (LT MLG WW) · airframe 56,790 hrs · 32,745 cycles

LEFT WW WEB CRACKED BETWEEN UPPER & LOWER CHORD AFT SIDE. R & R WEB IAW DWG & SRM.

Part: WEB — CRACKED (RT MLG WW) · airframe 56,790 hrs · 32,745 cycles

RIGHT WW WEB CRACKED BETWEEN UPPER & LOWER CHORD AFT SIDE. R & R WEB IAW DWG & SRM.

Part: BULKHEAD — CORRODED (BS 1016) · airframe 56,790 hrs · 32,745 cycles

AFT PRESSURE BULKHEAD DOME CORRODED AT BS 1016, BL 0. REPAIRED DOME IAW EA.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 56,790 hrs · 32,745 cycles

CAPTAINS NR 1 WINDOW FRAME CRACKED, UPPER OTBD CORNER INNER SURFACE. REPAIRED FRAME IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

SEAT TRACK CRACKED AT STATION 727B, LBL 24. REPAIRED TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

SEAT TRACK CRACKED AT STATION 727B, RBL 24. REPAIRED TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

SEAT TRACK SUPPORT FITTING CRACKED AT BS 727B, LBL 45. R & R FITTING IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

SEAT TRACK CRACKED AT STATION 727B, LBL 45. REPAIRED TRACK IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: SKIN — CRACKED (LE SLAT) · airframe 56,790 hrs · 32,745 cycles

LEFT WING LE NR 2 SLAT, CRACKED IN BOTTOM SKIN SURFACE COMING FROM FASTENER HOLE FOR THE ACTUATOR MOUNT BRACKET ASSEMBLY. REPAIRED NR 2 SLAT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,790 hrs · 32,745 cycles

LEFT WING LE NR 3 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,790 hrs · 32,745 cycles

LEFT WING LE NR 1 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,790 hrs · 32,745 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,790 hrs · 32,745 cycles

RIGHT OVERWING ESCAPE PATH EMER LIGHT FWD OF AFT CARGO DOOR INOPERATIVE. REPAIRED LIGHT IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 56,705 hrs · 32,696 cycles

FORWARD CABIN LT EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,021 hrs · 31,201 cycles

RIGHT SKIN CRACKED AT BS 540. REPAIRED SKIN IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,021 hrs · 31,201 cycles

RIGHT SIDE LOWER BULKHEAD CHORD SKIN CRACKED AT BS 540 STRINGER 22R. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,021 hrs · 31,201 cycles

RIGHT LOWER BULKHEAD SKIN CRACKED AT BS 540, FOUND HOLES B & F CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,021 hrs · 31,201 cycles

RIGHT LOWER BULKHEAD SKIN CRACKED AT BS 540, FOUND HOLES G CRACKED. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,021 hrs · 31,201 cycles

LEFT SIDE LOWER BULKHEAD SKIN CRACKED AT BS 540 STRINGER 22L. REPAIRED SKIN IAW EA.

Part: WINDOW — BROKEN (COCKPIT) · airframe 51,665 hrs · 29,824 cycles

R2 WINDOW OUTER PANE BROKEN. R & R R2 WINDOW IAW MM.

Part: ELECTRONIC UNIT — FAULTY (TE FLAP) · airframe 51,586 hrs · 29,773 cycles

DECLARED EMERGENCY DURING LANDING TE FLAPS WOULD NOT EXCEED BEYOND 5. R & R FLAPS ELECTRONIC UNIT IAW MM.

Part: ENGINE — FAILED (NR 1) · airframe 51,340 hrs · 29,630 cycles

AIR TURN BACK, NR 1 ENGINE QUIT & ROLLED BACK AT 18,000. R & R NR 1 ENGINE IAW MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 50,522 hrs · 29,128 cycles

RT AFT INTERIOR OVERWING EMERGENCY EXIT SIGN ASSEMBLY INOPERATIVE. R&R SIGN ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 50,522 hrs · 29,128 cycles

RT FWD INTERIOR EMERGENCY EXIT SIGN OVERWING NR 2 LED INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

FLOOR BEAM UPPER AFT FLANGE CORRODED AT STATION 1016, BETWEEN LBL 5-LBL 12. REPAIRED BEAM IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

INTERCOSTAL CORRODED BETWEEN BL 1016 - BS 1026, LBL 18. R&R INTERCOSTAL IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

RT NR 1 FLIGHT DECK WINDOW FRAME CRACKED IN UPPER OTBD CORNER. REPAIRED FRAME IAW SWA EA.

Part: ANGLE — CORRODED (ENTRY DOOR) · airframe 50,470 hrs · 29,091 cycles

LT AFT ENTRY DOOR "Z" ANGLE CORRODED. REPAIRED Z ANGLE IAW SRM.

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

AFT PRESSURE BULKHEAD RADIAL STIFFENER FASTENER HOLES DAMAGED AT STATION 1016, BL 0. REPAIRED STIFFENER IAW EA.

Part: BELTFRAME — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

BELT FRAME CORRODED AT STATION 1006, BL 0. R&R FRAME IAW DRAWING.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

SUPPORT CORRODED BETWEEN STATION 1006 & STATION 1016, RBL 8, ON LOWER SIDE. R&R SUPPORT IAW SRM.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

AFT PRESSURE BULKHEAD RADIAL STIFFENER ATTACH CLIP CORRODED AT 5:30 POSITION. R&R CLIP IAW DRAWING & EA.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

STRINGER TIE CLIPS CORRODED AT STATION 1006, BETWEEN STRINGER 27L & STRINGER 27R. R&R CLIP IAW SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

INTERCOSTAL FITTING CORRODED BETWEEN STATION 1006 - STATION 1016, LBL 40. R&R FITTING IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

STRINGER CLIP CORRODED AT STATION 967, STRINGER 27R. R&R CLIP IAW SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

STRINGER CLIP CORRODED AT STATION 967, STRINGER 27L. R&R CLIP IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

PRESSURE WEB CORRODED AT BS 1016, BETWEEN 27.95 - LBL 41.95. R&R INTERCOSTAL IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

STRINGER CORRODED AT BS 993, STRINGER 26L.. REPAIRED STRINGER IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

STRINGER SPLICE CORRODED AT BS 887, RBL 4. R&R SPLICE IAW SRM.

Part: TIE DOWN — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

AFT LAVATORY AFT OTBD TIE DOWN FITTING CORRODED ON UPPER SURFACE. R&R TIE DOWN IAW SPM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

STRINGER SPLICE CORRODED AT BS 887, STRINGER 27L. REPAIRED SPLICE IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

SKIN CORRODED AT BS 727D+11, BL 0. REPAIRED SKIN IAW SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

SHEAR TIE CORRODED AT STATION 947, BETWEEN STRINGER 27L - STRINGER 27R. R&R SHEAR TIE IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

STRINGER CORRODED BETWEEN BS 996 - BS 1000, STRINGER 25R. REPAIRED STRINGER IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

FLOOR BEAM ON LOWER SURFACE CORRODED ON AFT FLANGE AT STATION 1016, BETWEEN LBL 7 - LBL 12. REPAIRED FLANGE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

RT MOISTURE WEB IN AFT GALLEY CORRODED AT AFT PRESSURE BULKHEAD SEAL ATTACHMENT AREA BETWEEN RBL 27-RBL 40. R&R WEB IAW DRAWING.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

LT FLOOR WEB CORRODED ON LOWER SURFACE AT STATION 1028, LBL 7. R&R SUPPORT IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

AFT CARGO BILGE AREA FRAME CORRODED ON FWD SIDE, STATION 907, BL 0. R&R FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

AFT CARGO BILGE AREA FRAME CORRODED AT BS 907 BETWEEN RBL 5 TO LBL 5. R&R FRAME IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

AFT CARGO BILGE AREA INTERCOSTAL CORRODED BETWEEN STATION 927 & STATION 947, RBL 3. REPAIRED INTERCOSTAL IAW SWA EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

FLOOR BEAM STRAP CORRODED BETWEEN STATION 1006-STATION 1016, LBL 3. REPAIRED FLOOR BEAM IAW SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 50,470 hrs · 29,091 cycles

RIGHT WING OTBD AFT FLAP DELAMINATED ON UPPER INBD SIDE. R & R AFT FLAP ASSY. IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

NR 7 FASTENER HOLE ON NR 3 COCKPIT WINDOW FRAME AFT CRACKED. REPAIRED FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

LEFT FLIGHT DECK WINDOW FRAME E-F POST CRACKED AT SECOND LOWER CORNER FASTENER. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,470 hrs · 29,091 cycles

RIGHT FLIGHT DECK WINDOW FRAME E-F POST CRACKED AT SECOND LOWER CORNER FASTENER. REPAIRED FRAME IAW ACO.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 50,470 hrs · 29,091 cycles

RIGHT MLG W/W VERTICAL BULKHEAD PRESSURE DECK CRACKED AT BS 663, RBL 40. REPAIRED BULKHEAD IAW SRM.

Part: SLIDE — OUT OF LIMITS (L1 DOOR) · airframe 46,167 hrs · 26,579 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF LIMITS. REMOVED AND REPLACED SLIDE IAW MT.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND EMERGENCY EXIT LIGHT INOP BETWEEN ROW 9 TO ROW 11. REMOVED AND REPLACED BATTERY PACK CHARGER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,755 hrs · 25,153 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT EEPLS INOP AT ROW 3. RELAMPED EEPLS IAW MM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER SPLICE CORRODED BETWEEN BS 277 TO BS 294, STR 23L. REMOVED AND REPLACED SPLICE IAW EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 277 TO BS 294, STR 23L. REMOVED AND REPLACED STRINGER IAW EA.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 24L. REMOVED AND REPLACED SPLICE IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND STUB FRAME CHORD CORRODED AT BS 320, STR 23L. REPAIRED CHORD PER SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME ANGLE CORRODED AT BS 360, STR 27L. REPAIRED ANGLE IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 351 TO BS 380, STR 28L. REPAIRED STRINGER PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME FITTING CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED FITTING IAW SRM AND DWG.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540+9, RBL 32.40. REMOVED AND REPLACED FITTING IAW SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540+9, LBL 15.04. REMOVED AND REPLACED FITTING IAW SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540+9, RBL 6.14. REMOVED AND REPLACED FITTING IAW SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540+9, LBL 40.87. REMOVED AND REPLACED FITTING IAW SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540+9, LBL 54.60. REMOVED AND REPLACED FITTING IAW SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540+9, RBL 40.87. REMOVED AND REPLACED FITTING IAW SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540+9, RBL 15.04. REMOVED AND REPLACED FITTING IAW SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540+9, LBL 6.14. REMOVED AND REPLACED FITTING IAW SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540+9, LBL 32.40. REMOVED AND REPLACED FITTING PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR CREASE BEAM INNER CHORD CORRODED AT BS 325. REPAIRED CHORD PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT FLOOR STRUCTURE FRAME CORRODED AT BS 270, BETWEEN LBL 10 TO RBL 10. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,732 hrs · 25,142 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME IAW EA.

Part: SIGN — LOOSE (CABIN) · airframe 42,522 hrs · 24,433 cycles

DURING SCHEDULED CV CHECK, FOUND RT AFT EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 37,104 hrs · 21,250 cycles

DURING SCHEDULED 10Y CHECK, FOUND LOWER FUSELAGE SKIN DOUBLER CORRODED FROM BS 504 TO BS 510, BL 0. REPAIRED DOUBLER PER SRM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 37,004 hrs · 21,188 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 37,004 hrs · 21,188 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,703 hrs · 20,987 cycles

DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT BULL NOSE LIGHT INOP AT ROW 13. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 36,293 hrs · 20,753 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 36,293 hrs · 20,753 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: LENS — BROKEN (CABIN) · airframe 36,223 hrs · 20,713 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,899 hrs · 20,512 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. RELAMPED PER MM.

Part: WIRE HARNESS — ARCED (COCKPIT) · airframe 32,093 hrs · 18,239 cycles

AIR TURNBACK/DECLARED EMERGENCY. FLIGHT DECK L2 WINDOW ARCED AT ROTATION. REMOVED AND REPLACED L2 WINDOW HEAT ELECTRIC HARNESS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 32,001 hrs · 18,179 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS) · airframe 30,733 hrs · 17,429 cycles

DURING SCHEDULED MV3 CHECK, FOUND LEFT AFT CABIN EMERGENCY EXIT BATTERY PACK CHARGER FAULTY. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,316 hrs · 17,188 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 986, LBL 32. REPAIRED FLOORBEAM CHORD PER SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,307 hrs · 17,183 cycles

DURING SCHEDULED 8Y CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FUSE — FAULTY (BATTERY CHARGER) · airframe 30,307 hrs · 17,183 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD CABIN EMERGENCY EXIT BATTERY CHARGER INOP. REMOVED AND REPLACED BATTERY CHARGER FUSES PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 28,718 hrs · 16,293 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 27,443 hrs · 15,550 cycles

DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 27,406 hrs · 15,814 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 6 DEF TO ROW 9 DEF. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,504 hrs · 15,024 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,327 hrs · 13,810 cycles

DURING SCHEDULED RON CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 23,557 hrs · 13,378 cycles

DECLARED EMERGENCY. CABIN ALTITUDE HORN SOUNDED ALONG WITH RAPID DECOMPRESSION & CABIN MASKS DROPPED. CABIN PRESSURE CONTROLLABLE IN ALTERNATE MODE. REMOVED AND REPLACED BOTH CABIN PRESSURE CONTROLLERS, CABIN AFT OUTFLOW VALVE & CABIN PRESSURIZATION CONTROL MODULE PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,044 hrs · 13,087 cycles

DURING SCHEDULED RON CHECK, FOUND LT FWD EMERGENCY EXIT BULLNOSE LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — DISCHARGED (L1 DOOR) · airframe 22,243 hrs · 12,611 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 21,234 hrs · 12,062 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 18,657 hrs · 10,622 cycles

FWD INBOARD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.

Part: COVER — MISSING (CABIN) · airframe 11,895 hrs · 6,851 cycles

EEPLS COVER MISSING AT ROW NR 20. INSTALLED COVER PER MM.

Part: COVER — BROKEN (FWD SVC DOOR) · airframe 10,844 hrs · 6,281 cycles

FWD SVC DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT COVER PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 8,405 hrs · 4,949 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,272 hrs · 4,870 cycles

DURING SCHEDULED CHECK, FOUND EEPLS COVER MISSING AT ROW 2 & EEPLS INOP AT ROW 1. RELAMPED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,076 hrs · 4,179 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP AT FWD CABIN. RELAMPED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 5,424 hrs · 3,217 cycles

EEPLS WHITE LENS MISSING NEAR FWD SECTION. REPLACED TRACK COVER PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 4,944 hrs · 2,946 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 4,610 hrs · 2,744 cycles

EEPLS LOOSE AT FWD SECTION. REMOVED AND REPLACED LIGHT STRIP AND COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,280 hrs · 1,372 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. R&R AFT ENTRY DOOR LIGHT BULB PER MM.