N232WN

Part: STRINGER CLIP — CRACKED (ZN 100 FUS LOWER) · airframe 64,160 hrs · 38,524 cycles

CRACKED STRINGER CLIP AT PAX CABIN BS 727B, S7L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1102 REV -.

Part: STRAP — CORRODED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON STRAP AT MID CABIN BS 703, LBL 68, WL 203. REFER TO FAULT TTG8Q013SLHA. EA 25-153-01977.

Part: STRAP — CORRODED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON STRAP AT MID CABIN BS692 LBL68 WL203. REMOVED CORROSION ON STRAP BS 692, LBL 68, WL 203 AND ACCOMPLISHED REWORK OF STRAP IAW EA 25-153-01977.

Part: STRAP — CORRODED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON STRAP AT MID CABIN, BS 709, LBL 63, WL 203. REFER TO FAULT TTG8Q013SLHA WHERE EA 25-153-01977 WAS ADDED AS A SUBTASK.

Part: STRAP — CORRODED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON STRAP AT MID CABIN, BS 713, LBL 64 - LBL 67, WL 203. REFER TO FAULT TTG8Q013SLHA WHERE EA 25-153-01977 WAS ADDED AS A SUBTASK.

Part: STRAP — CORRODED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON STRAP AT MID CABIN BS718 RBL62 WL203. CORROSION ON STRAP AT MID CABIN BS718 RBL62 WL203 REPAIRED PER EA 25-153-01971-WIP1.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

CRACKED PANEL BREAK AT PASSENGER CABIN BS 540, LBL 1, WL 208. REPLACED PANEL BREAK PASSENGER CABIN BS540 LBL1 IAW SRM 51-40-02 AND DWG 143A0060 REV-.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

CRACKED PANEL BREAK AT PASSENGER CABIN BS 540, LBL 26, WL 208. REPLACED PANEL BREAK IAW SRM 51-40-02, AND BOEING DWG 143A0060 REV:-;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON AFT BULKHEAD SUPPORT BS 947; RBL 20; WL 160. REMOVED AND REPLACED AFT BULKHEAD SUPPORT STA 947. STR 25L-STR 25R IAW SRM 51-40-02; DWG 149A8117 REV:- AND DWG 149A8110 REV:A.

Part: SHIELD — CORRODED (ZONE 100) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON AFT CARGO COMPARTMENT FWD SHIELD BS 767-787, RBL 22, WL 156-157. INSTALLED NEW SHIELD IAW SRM 51-40-02, 51-40-05, AND DWG 146A8127 REV -.

Part: SHIELD — CORRODED (ZONE 100) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON FWD CARGO COMPARTMENT SHIELD BS 500+6, 500+10, RBL 22, WL 156. CORROSION FOUND TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2. REPAIR BY REPLACEMENT IAW SRM 51-10-02<BR>REMOVED DAMAGED SHIELD IAW SRM 51-40-02. INSTALLED A NEW SHIELD IAW SRM 51-40-02 AND DWG 143A0080 REV-.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BS 500A-500D; RBL 22; WL 157. REMOVED AND REPLACED SIDEWALL SUPPORT IAW SRM 51-4-02 AND DWG 143A7500 REV-.

Part: SHIELD — CORRODED (ZONE 100) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON AFT CARGO COMPARTMENT AFT SHIELD BS 847-867, RBL 22, WL 157. NO ALLOWABLE DAMAGE GIVEN FOR THIS PART IN SRM 53-00-53-1A-2. REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0, STEP 9. REMOVED DAMAGED SHIELD AND INSTALLED A NEW SHIELD IAW SRM 51-40-02 AND DWG 146A0081 REV -.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON AFT CARGO COMPARTMENT L/H FLOOR TO SIDEWALL SUPPORT BS 727+4 - 787+1-10, LBL 22, WL 156. REMOVED AND REPLACED AFT CARGO COMPARTMENT LT FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, DWG 146A7500 REV:B, DWG 146A7502 REV-, AND SRM 51-40-05-0G-0.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

MAIN CABIN SEAT TRACK LBL 45 AT STA 616+18 APPROX.; BS 663; BS 663+12 APPROX.; STA 685+12 APPROX. AND AT STA 727A+10 APPROX. WAS FOUND CORRODED ON CROWN. REMOVED CORROSION ON SEAT TRACK BS 540-727 LBL 45 FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02-0G-0 AND DWG 144A5300 REV E.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT STA 727+4-767 RBL 22; WL 156. REMOVED OLD AND INSTALLED NEW AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT BS A 727+4 - 767 RBL 22; WL 156 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0; BOEING DWG 146A7500 REV:A; BOEING DWG 146A7502 REV:-.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT BS 867+10, 867+15-16, RBL 22, WL 158. REMOVED AND REPLACED ON AFT CARGO COMPARTMENT R/H FLOOR SIDEWALL SUPPORT BS 867 TO 887 IAW SRM 51-40-02, AND 51-40-05 AND DWG 146A7500 REV A.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON FWD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT BS 400-500D, LBL 22, WL 157. SUPPORT HAS MISSING FASTENER AND IS NOT DRILLED AT BS 396, LBL 22, WL 157. DRILLED HOLE AND INSTALLED FASTENER IAW SRM 51-40-05, SRM 51-40-02, AND DWG 143A7500 REV-. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS 400-500D, LBL 22; WL 157 IAW SRM 51-40-02 AND DWG :143A7500 REV-.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

MAIN CABIN SEAT TRACK LBL 45 AT STA 540 AND STA 727+12 APPROX. WAS FOUND MECHANICAL DAMAGE ON CROWN. AND AT STA 559+10 APPROX. WAS FOUND CORROSION ON WELL. SEAT TRACK FOUND TO BE OUT OF LIMITS ON FAULT TTG8Q013QT63 AND WILL BE REPLACED ON TTG8Q013QT63.

Part: STRAP — CORRODED (ZONE 100) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON AFT CARGO COMPARTMENT FLOOR TIEDOWN STRAP STA 887; BETWEEN FLOOR PANELS 140CF-140DF. REMOVED AND REPLACED SPLICE / TEE ASSY IAW SRM 51-40-05 AND DWG 146A7500 REV A.

Part: SIDEWALL SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 64,160 hrs · 38,524 cycles

CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT STA 887+4-887+12; 907+2; RBL 22; WL 159. REMOVED AND REPLACED ON AFT CARGO COMPARTMENT R/H FLOOR TO SIDEWALL SUPPORT STA 867 TO 887 PER SRM 51-40-02; 51-40-05 AND BOEING DWG 147A7500REV -.

Part: PLATE — CRACKED (ZONE 600) · airframe 64,160 hrs · 38,524 cycles

RIGHT WING T/E WIGGLE PLATE AT ORSS 261 IS CRACKED.

Part: STRINGER — CRACKED (ZONE 100) · airframe 64,160 hrs · 38,524 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS535 S-23L WL164. REMOVED DAMAGED STRINGER S-23L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT STRINGER 23L BS 540-BS 500D+10 IAW SRM 53-00-03-2R-1; SRM 51-40-02 DWG143A3210 REV B.

Part: STRINGER — CRACKED (ZONE 100) · airframe 64,160 hrs · 38,524 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. REMOVED DAMAGED STRINGER S-26L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT STRINGER 26L BS 540-BS 500D+10 IAW SRM 53-00-03-2R-1; SRM 51-40-02 DWG143A3230 REV A.

Part: STRINGER — CRACKED (ZONE 100) · airframe 64,160 hrs · 38,524 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS 535, S-23L, WL164. REMOVED DAMAGED STRINGER S-23L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT STRINGER 23L BS 540-BS 500D+10 IAW SRM 53-00-03-2R-1; SRM 51-40-02 DWG143A3210 REV B.

Part: STRINGER SPLICE — CRACKED (ZN 100 FUS LOWER) · airframe 64,160 hrs · 38,524 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. REMOVED DAMAGED STRINGER S-26L BS 540 - BS500D+10; FABRICATED AND INSTALLED NEW STRINGER AND SPLICE AT STRINGER 26L BS 540-BS 500D+10 IAW SRM 53-00-03-2R-1; SRM 51-40-02 DWG143A3230 REV A.

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

CRACK FOUND ON STUB FRAME BS 294.5 +8.5'; ABOVE SEAL DEPRESSOR, BETWEEN S8R AND S9R; LENGTH 1.4'. REMOVED OLD FWD SERVICE DOOR STUB FRAME BS 294 +8.5' IAW SRM 51-40-02-0G-0 AND INSTALLED NEW FWD SERVICE DOOR STUB FRAME IAW SRM 51-40-02-0G-0 AND DWG 141A8370 REV. D.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 64,160 hrs · 38,524 cycles

FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED FWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE PER SRM 53-30-15-2R-1, SOPM 20-43-03, SOPM 20-41-02;

Part: RIB — CRACKED (ZONE 300) · airframe 64,160 hrs · 38,524 cycles

L/H HORIZONTAL STAB REMOVABLE L/E; 4TH RIB FROM I/B END IS CRACKED. REMOVED AND REPLACED 4TH RIB FROM I/B END OF L/H HORIZONTAL STAB. L/E IAW SRM 51-40-02-0G-0 PARA. 4.

Part: RIB — CRACKED (ZONE 300) · airframe 64,160 hrs · 38,524 cycles

L/H HORIZONTAL STAB REMOVABLE L/E; 5TH RIB FROM I/B END IS CRACKED. REMOVED AND REPLACED 5TH RIB FROM I/B END OF L/H HORIZONTAL STAB. L/E IAW SRM 51-40-02-0G-0 PARA. 4.

Part: ASSIST HANDLE — BROKEN (ZONE 800) · airframe 64,160 hrs · 38,524 cycles

AFT SERVICE DOOR SURROUND ASSIST HANDLE IS BROKEN.

Part: RIB — CRACKED (ZONE 300) · airframe 64,160 hrs · 38,524 cycles

L/H HORIZONTAL STAB REMOVABLE L/E; 3RD RIB FROM I/B END IS CRACKED. REMOVED AND REPLACED 3RD RIB FROM I/B END OF L/H HORIZONTAL STAB. L/E IAW SRM 51-40-02-0G-0 PARA. 4.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

PASSENGER CABIN FLOOR PANEL 241EF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241EF WITH AREAS OF DELAMINATION ON UPPER SKIN WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810-129.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

PASSENGER CABIN FLOOR PANEL 241AF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241AF WITH AREAS OF UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810-127.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

PASSENGER CABIN FLOOR PANEL 232SF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 232SF IAW SRM 53-00-50-2R-0 AND DWG 144A5810 SHEET 159.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

PASSENGER CABIN FLOOR PANEL 231XF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 231XF IAW SRM 53-00-50-2R-0 AND BOEING DRAWING 144A5810 SHEET 126.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

PASSENGER CABIN FLOOR PANEL 241FF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241FF WITH AREAS OF UPPER SKIN DELAMINATION WAS REPLACED BY FABRICATING A NEW BOARD IAW SRM 53-00-50-2R-0 AND DWG 144A5810-131.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

PASSENGER CABIN FLOOR PANEL 231YF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 231YF IAW SRM 53-00-50-2R-0 AND BOEING DRAWING 144A5810 SHEET 124..

Part: FLOOR PANEL — DELAMINATED (ZN 200 FUS TOP) · airframe 64,160 hrs · 38,524 cycles

PASSENGER CABIN FLOOR PANEL 242CF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 242CF WITH AREAS OF UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0125.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

PASSENGER CABIN FLOOR PANEL 241BF HAS AREAS OF DELAMINATION ON UPPER SKIN. FLOOR PANEL 241BF WITH AREAS OF UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810-189.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

PASSENGER CABIN FLOOR PANEL 242BF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATED NEW FLOOR PANEL 242BF IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0122.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 64,160 hrs · 38,524 cycles

PASSENGER CABIN FLOOR PANEL 242AF HAS AREAS OF DELAMINATION ON UPPER SKIN. FABRICATION OF NEW 242AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0-A00938, REPAIR GENERAL.

Part: RIB — CRACKED (ZONE 300) · airframe 64,160 hrs · 38,524 cycles

RIGHT HORIZONTAL STAB RIB 5 STIFFENER HAS CRACK ON LOWER RADIUS. REPAIRED RT HORIZONTAL STAB RIB 5, STAB STA 129.5 IAW SRM 51-40-2-0G-0 AND SRM 55-10-09-2R-4 REPAIR 4; FIG. 202; DETAIL.

Part: SKIN — PULLED (LT ENG INLET) · airframe 64,160 hrs · 38,524 cycles

L/H ENGINE INLET COWL BARREL SKIN HAS A PULLED THROUGH FASTENER AT 10:00 O'CLOCK POSITION.NR 1 ENGINE INLET COWL WAS REMOVED AND REPLACED ON CARD 7111-E-17062-NG. FAULT WAS ATTACHED TO R/O AND WILL BE CORRECTED WHEN INLET COWL GETS MODIFIED.

Part: LENS — DISPLACED (ZONE 200) · airframe 63,591 hrs · 38,181 cycles

RAMP REPORTS. EMERGENCY LIGHT LENSE DISPLACED AIRCRAFT LEFT AFT<[01] SECURED EMERGENCY LIGHT LENSE REF SIP

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 63,439 hrs · 38,091 cycles

EMERGENCY AREA LIGHT AMS AT 9ABC AND 18DEF INOP <[01]. 01 - REMOVED AND REPLACED EMERGENCY AREA LAMPS AT 9ABC AND 18DEF PER [AMM 33-51-03-960-801-NG (AREA LIGHT - LAMP REPLACEMENT - PERMANENT)].

Part: EDS — FAILED (NR 2 ENGINE) · airframe 63,011 hrs · 37,826 cycles

#2 ENGINE FAILED ON APPROACH TO RUNWAY 22@ HOU.<[01] PERFORMED FIM TASK 73-06 TASK 812 DUE TO LOSS OF THRUST ON #2 ENGINE FOUND INTERNAL EEC FAULT AND R/R #2 ENGINE EEC REF MM 73-21-60 OPS CHECK GOOD. ALSO VISUALLY INSPECTED FUEL PUMP DRIVE SHAFT REF MM 73-11-01 NO DEFCETS NOTED AND CHECKED WIRING BETWEEN #2 TRA RESOLVER AND #2 EEC REF WD 73-21-21 NO DEFECTS NOTED

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 62,328 hrs · 37,390 cycles

M1670 FAILED CAPACITY CHECK<[01] R/R M1670 BATTERY PACK PER AMM 33-51-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 62,328 hrs · 37,390 cycles

M1675 AND. M1674 FAILED CAPACITY CHECK<[01] R/R M1675 AND M1674 BATTERY. PACK PER AMM 33-51-06

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 62,328 hrs · 37,390 cycles

M1673 AND M1672 FAILED CAPACITY CHECK<[01] R/R M1673 AND M1672 BATTERY PACKS PER AMM 33-51-06

Part: MEGAPHONE — CRACKED (ZN 200 FUS TOP) · airframe 62,328 hrs · 37,390 cycles

FWD MEGAPHONE CRACKED<[01] R/R FWD MEGAPHONE IAW AMM 25-64-00.

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 62,328 hrs · 37,390 cycles

M1668 AND M1669 FAILED CAPACITY CHECK<[01] R/R M1668 AND M1669 BATTERY PACK PER AMM 33-51-06

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,796 hrs · 36,442 cycles

EMERGENCY LIGHT AT ROW 11DEF AND 22DEF INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BULBS AT ROWS 11DEF AND 22DEF IAW AMM 33-51-03. OPS CHECKED GOOD

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 60,458 hrs · 36,232 cycles

R/H AFT O/B TRAILING EDGE FLAP DISBONDED<[01] APPLIED PERMANENT REPAIR PER SRM 51-70-10.

Part: SLIDE — DISLODGED (AFT PAX DOOR) · airframe 60,436 hrs · 36,218 cycles

AFT ENTRY DOOR ESCAPE SLIDE DISLODGED (CAPT SIDE)<[01] ADJUSTED AND REINSTALLED AFT ENTRY DOOR SLIDE PER MM25-66-01.

Part: LENS — BROKEN (ZN 200 FUS TOP) · airframe 58,605 hrs · 35,096 cycles

LEFT OVERWING EXIT DOOR SIGN LENS BROKEN<[01] REPLACED EXIT SIGN ASSY BASE PER MM 33-51-01

Part: ACCESS PANEL — CORRODED (ZN 100 FUS LOWER) · airframe 57,989 hrs · 34,674 cycles

CORROSION ACCESS PANEL 193AR BODY FAIRING STRUCTURE AT LOWER FUSELAGE 2023-447823<[01] REPLACED FRAME LOC ON BODY FAIRING STRUCTURE AT LOWER FUSELAGE AND FASTENERS IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 149A7216 SHEET 7 REV-A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: ACCESS PANEL — CORRODED (ZN 100 FUS LOWER) · airframe 57,989 hrs · 34,674 cycles

CORROSION ACCESS PANEL 193AL BODY FAIRING STRUCURE AT LOWER FUSELAGE 2023-447822<[01] REPLACED FRAME LOC ON BODY FAIRING STRUCTURE AT LOWER FUSELAGE AND FASTENERS IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 149A7216 SHEET 7 REV-A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] COMPLETED JOB

Part: BRACKET — CRACKED (ZN 500 LEFT WING) · airframe 57,989 hrs · 34,674 cycles

CRACK ON BRACKET ASSY OF ACCESS PANEL I/B FIXED TRAILING<BR>EGDE AT LT WING 2023-447819<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 25-JAN-24;[02] REPLACED FASTENERS AND BRACKET ASSY OF ACCESS PANEL I/B FIXED TRAILING EGDE AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2511 SHEET 9 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED FASTENERS AND BRACKET ASSY OF ACCESS PANEL I/B FIXED TRAILING EGDE AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2511 SHEET 9 REV-. SEE INDIVIDUAL SIGN OFF BELOW

Part: ACCESS PANEL — BROKEN (ZN 500 LEFT WING) · airframe 57,989 hrs · 34,674 cycles

BROKEN ACCESS PANEL I/B FIXED TRAILING EGDE AT LT WING 2023-447802<[01] TOOL USED CALIPER PN: 500-197-30; SN: 15120589; DUE DATE: 13/FEB/24.;[02] TOOL USED HOT BONDER PN: HCS9000B; SN: 18175469; DUE DATE: 24/SEP/23.;[03] TOOL USED SCALE PN: CR5200; SN: 8343110765; DUE DATE: 20/FEB/24.;[04] TOOL USED: SCALE: P/N:CR5200 S/N:8343110809 DUE DATE:21-FEB-24.;[05] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 24-JAN-24.;[06] TOOL USED: HOT BONDER PN: HCS9000B-AV SN: 18185761 DUE DATE: 24/SEP/23.;[07] TOOL USED BONDMASTER EQUIPMENT PN: BONDMASTER 600M; SN:220052310; DUE DATE:31-OCT-23;[08] TOOL USED MULTIMETER PN: FLUKE 87; S/N: 37640208; DUE DATE: 24-FEB-24;[09] REPAIRED ACCESS PANEL I/B FIXED TRAILING EGDE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGN OFF BELOW.;[10] JOB TASK COMPLETED.

Part: HANDLE — WORN (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

WEAR ON EMERGENCY DOOR BOLT(1EA) AND NUT(1EA) THAT ATTACH INTERIOR HANDLE RH SIDE AT PASSENGER CABIN 2023-447794<[01] REPLACED ON EMERGENCY DOOR BOLT(1EA) AND NUT(1EA) THAT ATTACH INTERIOR HANDLE RH SIDE AT PASSENGER CABIN IAW SOPM 20-50-01 REV.38;[02] TASK CARD COMPLETED

Part: ACCESS PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 57,989 hrs · 34,674 cycles

DELAMINATED WING TO BODY FAIRING ACCESS PANEL 193B INTERNAL AREA AT MAIN WHEEL WELL COMPARTMENT 2023-447751<[01] TOOL USED= CALIPER P/N: 500-196-30; S/N:A20231600; DUE DATE: 12-SEP-23;[02] TOOL USED= HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 26-MAR-24;[03] TOOL USED= SCALE P/N: CR5200; S/N: 8342514563; DUE DATE. 20-FEB-24;[04] REPAIRED WING TO BODY FAIRING ACCESS PANEL 193B INTERNAL AREA AT MAIN WHEEL WELL COMPARTMENT AS PER B737-700 SRM 53-40-70-2R-1 REPAIR 1 . AND B737-700 SRM 51-70-04-2R-2 REPAIR 2. TOOL USED .CALIPER P/N: 500-196-30; S/N:A20231600; DUE DATE: 12-SEP-23. HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 26-MAR-24. SCALE P/N: CR5200; S/N: 8342514563; DUE DATE. 20-FEB-24. SEE INDIVIDUAL SIGN OFFS BELOW.;[05] REPAIRED WING TO BODY FAIRING ACCESS PANEL 193B INTERNAL AREA AT MAIN WHEEL WELL COMPARTMENT AS PER B737-700 SRM 53-40-70-2R-1 REPAIR 1 . AND B737-700 SRM 51-70-04-2R-2 REPAIR 2. TOOL USED .CALIPER P/N: 500-196-30; S/N:A20231600; DUE DATE: 12-SEP-23. HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 26-MAR-24. SCALE P/N: CR5200; S/N: 8342514563; DUE DATE. 20-FEB-24. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: LIGHT — BROKEN (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

BROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2023-447744<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) I.A.W AMM 33-51-15-400-802.;[02] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) I.A.W AMM 33-51-15-400-802

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 57,989 hrs · 34,674 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 289 AT LT WING 2023-447715<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 289 AT LT WING I.A.W. B737-700 SRM 51-40-02;[02] TASK CARD COMPLETED

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 57,989 hrs · 34,674 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 212 AT LT WING TASK CARD 2023-447712<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 212 AT LT WING I.A.W. B737-700 SRM 51-40-02;[02] TASK CARD COMPLETED

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 57,989 hrs · 34,674 cycles

CRACK TRAILING EDGE TEE ANGLE LOCATED ORSS 273 AT RT WING 2023-447668<[01] REPLACED TRAILING EDGE TEE ANGLE LOCATED ON ORSS273 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A3700 REV.- SHEET 41 DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B7377-700 57-51-02 <BR><BR>CRACK LENGTH: 1.956? <BR><BR>TOOL USED CALIPERP/N: 500-752-20 S/N: B21014901 DUE DATE: 20/SEP/23;[02] REPLACED TRAILING EDGE TEE ANGLE LOCATED ON ORSS273 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A3700 REV.- SHEET 41 DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B7377-700 57-51-02 <BR><BR>CRACK LENGTH: 1.956? <BR><BR>TOOL USED CALIPERP/N: 500-752-20 S/N: B21014901 DUE DATE: 20/SEP/23

Part: BEAM — CRACKED (ZN 600 RIGHT WIN) · airframe 57,989 hrs · 34,674 cycles

CRACK TRAILING EDGE BEAM ASSY LOCATED ORSS 275 AT RT WING 2023-447667<[01] REPLACED BEAM ASSY LOCATED ON TRAILING EDGE ORSS 275 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 115A3712; SHEET: 7; REV: A. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED BEAM ASSY LOCATED ON TRAILING EDGE ORSS 275 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 115A3712; SHEET: 7; REV: A. SEE INDIVIDUAL SIGN OFF BELOW

Part: FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 57,989 hrs · 34,674 cycles

CRACK FRAME ON BS 947.5 LBL 8.10 AFT CARGO COMPARTMENT 2023-447661<[01] REPLACED FRAME LOCATED ON BS 947.5 BTW STR 23L TO STR 23R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING: 147A1047 REV: -. SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK CARD COMPLETED <BR>REPLACED FRAME LOCATED ON BS 947.5 BTW STR 23L TO STR 23R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING: 147A1047 REV: -. SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII

Part: FAIRING — CRACKED (ZN 600 RIGHT WIN) · airframe 57,989 hrs · 34,674 cycles

CRACK FLAP TRACK FAIRING 7 INTERNAL AND EXTERNAL SKIN LOCATED AT 44IN FROM AFT EDGE AT RT WING (REFER TO FAULT TTG8Q00BE1UM) 2023-447704<[01] TOOL USED; CALIPER PN: 500-464; S/N: B17030933; DUE DATE: 17/OCT/2023.;[02] REPAIRED FLAP TRACK FAIRING 7 (643BB) INTERNAL AND EXTERNAL SKIN IAW EA # 23-157-02310. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] STEPS 1 AND 2 ENTERED IN ERROR; <BR><BR>CORRECT STEP: REPAIRED FLAP TRACK FAIRING 7 (643BB) INTERNAL AND EXTERNAL SKIN IAW EA # 23-157-02310. TOOL USED; CALIPER PN: 500-464; S/N: B17030933; DUE DATE: 17/OCT/23. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] CORRECTIVE ACTION COMPLETED: REPAIRED FLAP TRACK FAIRING 7 (643BB) INTERNAL AND EXTERNAL SKIN IAW EA # 23-157-02310. TOOL USED; CALIPER PN: 500-464; S/N: B17030933; DUE DATE: 17/OCT/23. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (ZN 400 NACELLE/P) · airframe 57,989 hrs · 34,674 cycles

CRACK ON ANGLE LOCATED 12 INCHES OF AFT EDGE AND 17 INCHES OF LOWER EDGE AT OUTBOARD FAN COWL 2023-447695<[01] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[02] PERFORMED HFEC AND CONFIRMED NO CRACK ON ANGLE LOCATED 12 INCHES OF AFT EDGE AND 17 INCHES OF LOWER EDGE AT OUTBOARD FAN COWL; RESTORED PROTECTIVE FINISH IAW B737-700 SRM 51-20-01. SEE INDIVIDUAL SIGN OFF BELOW.;[03] TASK CARD COMPLETED <BR>PERFORMED HFEC AND CONFIRMED NO CRACK ON ANGLE LOCATED 12 INCHES OF AFT EDGE AND 17 INCHES OF LOWER EDGE AT OUTBOARD FAN COWL; RESTORED PROTECTIVE FINISH IAW B737-700 SRM 51-20-01. SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 57,989 hrs · 34,674 cycles

CRACK ANGLE BS 867 LBL 12.5 WL 164 AFT CARGO COMPARTMENT 2023-447603<[01] REPLACED ANGLE LOCATED BS 867 LBL 12.5 WL 164 AFT CARGO COMPARTMENT. IAW. B737-700 SRM 51-40-02; DWG: 149A8102 SHEET:17 REV:- MEASURE OF CRACK L:1.000?. TOOL USED CALIPER P/N:700-113-10 SN:0023244 DUE DATE: 05-DEC-2023.;[02] REPLACED ANGLE LOCATED BS 867 LBL 12.5 WL 164 AFT CARGO COMPARTMENT. IAW. B737-700 SRM 51-40-02; DWG: 149A8102 SHEET:17 REV:- MEASURE OF CRACK L:1.000?. TOOL USED CALIPER P/N:700-113-10 SN:0023244 DUE DATE: 05-DEC-2023.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 57,989 hrs · 34,674 cycles

CRACK ANGLE BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R FWD POSITION AFT CARGO COMPARTMENT 2023-447604<[01] REPLACED ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R FWD POSITION AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV.- <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R FWD POSITION AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV.- RII CERTIFIED

Part: CARGO TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 57,989 hrs · 34,674 cycles

CRACK TRACK RBBL 13.84 BS 767 AFT CARGO COMPARTMENT 2023-447614<[01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN 220272712; DUE DATE 17-DEC-23;[02] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 220273012; CAL DUE DATE: 17-DEC-23.;[03] REPAIRED TRACK LOCATED ON RBBL 13.84 BS 767 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 AND B737-700 SRM 51-10-02.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[04] CORRECTED ITEM 3: REPAIRED TRACK LOCATED ON RBBL 13.84 BS 767 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ITEM 4 (P) FIGURE 203 SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPAIRED TRACK LOCATED ON RBBL 13.84 BS 767 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ITEM 4 (P) FIGURE 203 SEE INDIVIDUAL SIGN OFF BELOW.ITEM RII

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 57,989 hrs · 34,674 cycles

CORROSION LOWER SILL BTW BS 787 TO BS 847 RBL 24 WL 159 AFT CARGO COMPARTMENT 2023-447612<[01] EQUIPMENT P/N 45MG; S/N 221859911; DUE DATE 07-NOV-23 WAS USED;[02] REMOVED CORROSION AND EVALUATE REWORK LOWER SILL BTW BS 787 TO BS 847 RBL 24 WL 159 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-60-15-1A-1 ALLOWABLE DAMAGE 1 PARAGRAPH 4(G)(2)(B) FIGURE 103 DETAIL G AND FOUND WITHIN LIMITS SEE INDIVIDUAL SIGN OFF BELOW;[03] JOB COMPLETED

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 57,989 hrs · 34,674 cycles

CRACK ANGLE BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R AFT POSITION AFT CARGO COMPARTMENT 2023-447605<[01] REPLACED ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R AFT POSITION AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV.-<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED ANGLE LOCATED BTW BS907 TO BS927 AND STR25R TO STR27R AFT POSITION AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV.- RII CERTIFIED

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON SUPPORT ANGLE LOCATED CEILING AREA BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2023-447553<[01] REPLACED SUPPORT ANGLE LOCATED CEILING AREA BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM-51-40-02 AND DWG-146A7901 REV: -;[02] REPLACED SUPPORT ANGLE LOCATED CEILING AREA BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM-51-40-02 AND DWG-146A7901 REV: -

Part: FRAME — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON FRAME LOCATED BS 787 BTW STR 8R TO 9R AT PASSENGER CABIN 2023-447565<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512 AND DUE DATE: 17-DEC-23.;[02] PERFORMED HFEC ON AREA AND NOT FOUNS CRACK INDICATION; INSTALLED BRACKET AND FASTENER ON FRAME LOCATED BS787 BETWEEN STR 8R TO STR 9R I.A.W B737-700 SRM 51-40-02. AND DRAWING #146A1133REV: - .SEE INDIVIDUAL STEP SIGN OFFS BELOW;[03] CORRECTED STEP 2<BR>CORRECTED ITEM 1 PERFORMED HFEC INSPECTION ON AREA AND NOT FOUND CRACK INDICATION; INSTALLED BRACKET AND FASTENER ON FRAME LOCATED BS787 BETWEEN STR 8R TO STR 9R I.A.W B737-700 SRM 51-40-02. AND DRAWING #146A1133REV:- .SEE INDIVIDUAL STEP SIGN OFFS BELOW;[04] PERFORMED HFEC INSPECTION ON AREA AND NOT FOUND CRACK INDICATION; INSTALLED BRACKET AND FASTENER ON FRAME LOCATED BS787 BETWEEN STR 8R TO STR 9R I.A.W B737-700 SRM 51-40-02. AND DRAWING #146A1133REV:- .SEE INDIVIDUAL STEP SIGN OFFS BELOW ITEM RII

Part: LENS — BROKEN (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

BROKEN EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA 2023-447522<[01] REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(7)(10);[02] REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(7)(10). JOB COMPLETED.

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 57,989 hrs · 34,674 cycles

CRACK ANGLE - SUPPORT LOCATED BS727A TO BS727E AT LBL51 AFT CARGO COMPARTMENT 2023-447481<[01] REMOVED FASTENER COMMON TO ANGLE - SUPPORT LOCATED BS727A TO BS727E AT LBL51 AFT CARGO COMPARTMENT IAW B737-700 51-40-02 AND PERFORMED VISUAL INSPECCIÏ¿½N IAW B737-700 51-10-02 AND DAMAGE IS ONLY ON FASTENER; REPLACED FASTENERS IAW B737-700 51-40-02;[02] CORRECTED STEP 1.<BR>REMOVED FASTENER COMMON TO ANGLE - SUPPORT LOCATED BS727A TO BS727E AT LBL51 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECCIÏ¿½N IAW B737-700 SRM 51-10-02 AND DAMAGE IS ONLY ON FASTENER; FASTENER WAS REPLACED IAW B737-700 SRM 51-40-02;[03] CORRECTED STEP 1. <BR>REMOVED FASTENER COMMON TO ANGLE - SUPPORT LOCATED BS727A TO BS727E AT LBL51 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECCIÏ¿½N IAW B737-700 SRM 51-10-02 AND DAMAGE IS ONLY ON FASTENER AND WAS REPLACED IAW B737-700 SRM 51-40-02

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 LBL 27 AT FWD GALLEY AREA 2023-447485<[01] REPLACED WEB-INTERCOSTAL LOCATED FLOOR STRUCTURE BETWEEN BS294.5 TO BS312 AND LBL27 FWD GALLEY AREA IAW B737-700 SRM:51-40-02 AND DWG: 141A5400 REV.A. SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] CORRECTED STEP 1: REPLACED WEB-INTERCOSTAL LOCATED ON FLOOR STRUCTURE BETWEEN BS294.5 TO BS312 AND LBL27 FWD GALLEY AREA IAW B737-700 SRM:51-40-02 AND DWG: 141A5400 SHEET: 22; REV: A. SEE INDIVIDUAL SIGN-OFF BELOW.;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA 2023-447488<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED WEB AND FASTENER LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA I.A.W SRM B737-700 51-40-02 AND DRAWING 141A5400 REV:-;SEE INDIVIDUAL SIGN OFFS BELOW;[03] REPLACED WEB AND FASTENER LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA I.A.W SRM B737-700 51-40-02 AND DRAWING 141A5400 REV:-;SEE INDIVIDUAL SIGN OFFS BELOW<BR>RII CERTIFIED

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA 2023-447498<[01] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23;[02] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23;[03] REPAIRED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW SRM B737-700 53-10-51-2R-19 REPAIR 19 SEE INDIVIDUAL SIGNOFF BELOW.;[04] REPAIRED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-19 REPAIR 19 SEE INDIVIDUAL SIGN OFF BELOW.;[05] TASK CARD COMPLETED <BR>REPAIRED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-19 REPAIR 19 SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA 2023-447482<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA IAW B 737-700 51-40-02 AND DWG 141A5400 SHEET 44 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2.<BR>REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA IAW B 737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA IAW B 737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV - SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2023-447516<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 25 REV : SEE INDIVIDUAL SIGNOFF BELOW;[02] CORRECTIVE ACTION CERTIFIED RII

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 LBL 32 AT FWD GALLEY AREA 2023-447491<[01] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 LBL 32 AT FWD GALLEY AREA. IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET: 24 REV: A. SEE INDIVIDUAL SIGNOFF BELOW.;[02] TASK CARD COMPLETED <BR>REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 LBL 32 AT FWD GALLEY AREA. IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET: 24 REV: A. SEE INDIVIDUAL SIGNOFF BELOW.<BR>RII

Part: SUPPORT BRACKET — CORRODED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CORROSION ON SUPPORT BRACKET LOCATED BS 312 RBL 54 AT LEVEL STR 17L AT FWD GALLEY AREA 2023-447504<[01] REPLACED SUPPORT BRACKET LOCATED BS 312 RBL 54 AT LEVEL STR 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM B737-700 SRM 51-10-02. TOOK MEASURE OF CORROSION ARE: L= 0.625?; W= 0.550?; D= 0.035?. TOOL USED CALIPER P/N: 500-752-20; S/N:B21038258; DUE DATE: 20-SEP-23. EVALUATED CORROSION AND NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 53-10-15-1A-1. ALLOWABLE DAMAGE 1.;[02] CORRECTED STEP 1. REPLACED SUPPORT BRACKET LOCATED BS 312 LBL 54 AT LEVEL STR 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND SRM B737-700 SRM 51-10-02. TOOK MEASURE OF CORROSION ARE: L= 0.625?; W= 0.550?; D= 0.035?. TOOL USED CALIPER P/N: 500-752-20; S/N:B21038258; DUE DATE: 20-SEP-23. EVALUATED CORROSION AND NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM 53-10-15-1A-1. ALLOWABLE DAMAGE 1.;[03] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 LBL 12 AT FWD GALLEY AREA 2023-447497<[01] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23;[02] PERFORMED PERMANENT REPAIR ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 LBL 12 AT FWD GALLEY AREA I.A.W B737-700 SRM 53-10-51-2R-20 REPAIR 20; FIGURE 206; ALTERNATIVE 2; SHEET 1; AND INSTALLED WEB INTERCOSTAL I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG#141A5400; SHEET 94; REV.-. SEE INDIVIDUAL SIGN OFF BELOW.;[03] RII JOB COMPLETED

Part: SUPPORT ANGLE — CORRODED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CORROSION ON SUPPORT ANGLE LOCATED BTW BS 312 TO BS 344 AT LEVEL STR 17R RBL57 WL 208.1 AT FWD GALLEY AREA 2023-447502<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N:221861811 AND DUE DATE: 08-NOV-23.;[02] REPLACED NEW SUPPORT ANGLE LOCATED BTW BS 312 TO BS 344 AT LEVEL STR 17R RBL57 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET:23 SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED NEW SUPPORT ANGLE LOCATED BTW BS 312 TO BS 344 AT LEVEL STR 17R RBL57 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET:23 SEE INDIVIDUAL SIGN OFF BELOW

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA 2023-447483<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[03] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA I.A.W SRM B737-700 51-40-02 AND DRAWING 141A5400 REV:-;SEE INDIVIDUAL STEP SIGN OFFS BELOW;[04] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA I.A.W SRM B737-700 51-40-02 AND DRAWING 141A5400 REV:-;SEE INDIVIDUAL STEP SIGN OFFS BELOW<BR>RII CERTIFIED

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 RBL 15 AT FWD GALLEY AREA 2023-447486<[01] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022237; DUE DATE: 26-JAN-24.;[02] PERFORMED PERMANENT REPAIR ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 RBL 15 AT FWD I.A.W B737-700 SRM 53-10-51-2R-6 REPAIR 6; FIGURE 203; SHEET 5; AND SRM 51-40-02-0G-0. SEE INDIVIDUAL SIGN OFF BELOW.;[03] PERFORMED PERMANENT REPAIR ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 RBL 15 AT FWD I.A.W B737-700 SRM 53-10-51-2R-6 REPAIR 6; FIGURE 203; SHEET 5; AND SRM 51-40-02-0G-0. SEE INDIVIDUAL SIGN OFF BELOW.<BR>TASK COMPLETED RII

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 RBL 32 AT FWD GALLEY AREA 2023-447487<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 RBL 32 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -;[03] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 RBL 32 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -<BR>RII CERTIFIED

Part: ACCESS PANEL — CRACKED (ZN 500 LEFT WING) · airframe 57,989 hrs · 34,674 cycles

CRACK ACCESS PANEL 561AB TRAILING EDGE AT LT WING 2023-447443<[01] TOOL USED: CALIPER P/N: 500-193-30 S/N: 0000288 DUE DATE: 27/DEC/23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N:18185733 DUE DATE:23-JAN-24.;[03] TOOL USED: SCALE P/N: CR5200; S/N: 8343110809; DUE DATE:21-FEB-24.;[04] TOOL USED ULTRASONIC EQUIPMENT P/N: EPOCH 650; S/N: 201036102; CAL DUE DATE: 16/SEP/23;[05] TOOL USED: MULTIMETER P/N: FLUKE 179 S/N: 97220166 DUE DATE: 24-FEB-24.;[06] REPAIRED ACCESS PANEL 561AB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] STEP 6 VERIFIED AND CORRECTIVE ACTION COMPLETED : REPAIRED ACCESS PANEL 561AB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FRAME — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON FRAME LOCATED BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA 2023-447419<[01] MEASURE OF CRACK IS L:0.125 INCHES TOOL USED CALIPER P/N: 500-752-20 S/N:B21014945 DUE DATE: 08-NOV-23 AND EVALUATE CRACK IS NOT PERMITTED I.A.W SRM B737-700 53-00-07-1A-1 STEP 4.A(1); FRAME MUST BE REPAIRED.<BR>REPAIRED FRAME ON BS 312 AND BETWEEN STR5L TO STR6L FWD GALLEY AND LAV IAW EA M-22-153-01244 SEE SUB TASK BAR CODE TTG8Q00M70VK;[02] STEP 1 CORRECTED.<BR>REPAIRED FRAME ON BS 312 AND BETWEEN STR5L TO STR6L FWD GALLEY AREA IAW EA M-22-153-01244 SEE SUB TASK BAR CODE TTG8Q00M70VK SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPAIRED FRAME ON BS 312 AND BETWEEN STR5L TO STR6L FWD GALLEY AREA IAW EA M-22-153-01244 SEE SUB TASK BAR CODE TTG8Q00M70VK; SEE INDIVIDUAL SIGNOFFS BELOW. RII.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2023-447425<[01] REPLACED NEW INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-40-02 AND DWG # 141A8180 REV ?C? SEE INDIVIDUAL SING OFF BELLOW;[02] RII ITEM <BR>REPLACED NEW INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-40-02 AND DWG # 141A8180 REV ?C? SEE INDIVIDUAL SING OFF BELLOW

Part: ACCESS PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 57,989 hrs · 34,674 cycles

CRACK ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2023-447442<[01] TOOL USED: CALIPER P/N: 500-193-30 S/N: 0000288 DUE DATE: 27/DEC/23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N:18185733 DUE DATE:23-JAN-24.;[03] TOOL USED SCALE P/N:CR5200 S/N:8343110809 DUE DATE: 21-FEB-24.;[04] TOOL USED ULTRASONIC EQUIPMENT P/N: EPOCH 650; S/N: 201036102; CAL DUE DATE: 16/SEP/23;[05] TOOL USED: MULTIMETER P/N: FLUKE 179 S/N: 97220166 DUE DATE: 24-FEB-24.;[06] REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196127 DUE DATE: 22-JAN-24. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CORROSION ON FLOOR BEAM BS 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2023-447441<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 130060401 AND DUE DATE: 20-MAR-24.;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101U102020 DUE DATE: 30 AUG 23.;[03] PERFORMED PERMANENT REPAIR LOCATED FLOOR BEAM BS 986.5 AT LBL 43 AND WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 4 AND FIGURE 205. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[04] PERFORMED PERMANENT REPAIR LOCATED FLOOR BEAM BS 986.5 AT LBL 43 AND WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 4 AND FIGURE 205. RII SEE INDIVIDUAL SIGNOFFS BELOW.

Part: BRACKET — CRACKED (ZN 500 LEFT WING) · airframe 57,989 hrs · 34,674 cycles

CRACK SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS273 AT LT WING 2023-447423<[01] REPLACED SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS273 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2930; REV: ?.;[02] REPLACED SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS273 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2930; REV

Part: PANEL — CRACKED (ZN 500 LEFT WING) · airframe 57,989 hrs · 34,674 cycles

CRACK ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2023-447440<[01] TOOL USED: CALIPER P/N: 500-193-30 S/N: 0000288 DUE DATE: 27/DEC/23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N:18196021 DUE DATE:24-JAN-24.;[03] TOOL USED: SCALE P/N: CR5200; S/N: 8343110809; DUE DATE:21-FEB-24.;[04] TOOL USED SCALE P/N:CR5200 S/N:8343110809 DUE DATE: 21-FEB-24.;[05] TOOL USED ULTRASONIC EQUIPMENT P/N: EPOCH 650; S/N: 201036102; CAL DUE DATE: 16/SEP/23;[06] REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CORROSION ON EXISTING REPAIR LOCATED BS 986.5 BTW RBL 35 TO RBL 44 WL 208.1 AT AFT GALLEY AREA 2023-447444<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 130060401 AND DUE DATE: 20-MAR-24.;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[03] PERFORMED REPAIR ON FLOOR BEAM LOCATED BS 986.5 BTW RBL 35 TO RBL 44 WL 208.1 AT AFT GALLEY AREA I.A.W EA 23-153-02337-WIP1 AND EA 23-153-02337 SUMMARY. SEE INDIVIDUAL STEP SIGN OFFS BELOW;[04] PERFORMED REPAIR ON FLOOR BEAM LOCATED BS 986.5 BTW RBL 35 TO RBL 44 WL 208.1 AT AFT GALLEY AREA I.A.W EA 23-153-02337-WIP1 AND EA 23-153-02337 SUMMARY. SEE INDIVIDUAL STEP SIGN OFFS BELOW

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 57,989 hrs · 34,674 cycles

CRACK INSPAR RIB LOCATED STAB STA111.10 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL STAB 2023-447369<[01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138203; CAL DUE DATE: 09-JUN-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN -24.;[03] REPAIRED INSPAR RIB LOCATED STAB STA111.10 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4;[04] CORRECTED STEP 3.<BR>REPAIRED INSPAR RIB LOCATED STAB STA111.10 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN OFF BELOW;[05] CORRECTED STEP 3. <BR>REPAIRED INSPAR RIB LOCATED STAB STA111.10 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4. RII; SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 57,989 hrs · 34,674 cycles

CRACK SUPPORT ANGLE ON FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN 2023-447360<[01] REPLACED ANGLE - SUPPORT ANGLE ON FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN IAW B737 700 SRM 51-40-02 ; SRM 51-10-02 AND DWG 273A9110-6 REV:A AND MEASURES OF CRACK IS L: 1.593 INCH TOOK MECHANICALLY TOOL USED CALIPER P/N: 500-196-30 S/N:A20231707 DUE DATE: 06-SEP-23.SEE INDIVIDUAL SIGN OFF STEP BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED ANGLE - SUPPORT ANGLE ON FLOOR STRUCTURE LOCATED BS 695 RBL 24.75 AT PASSENGER CABIN IAW B737 700 SRM 51-40-02 ; SRM 51-10-02 AND DWG 273A9110 REV:A AND MEASURES OF CRACK IS L: 1.593 INCH TOOK MECHANICALLY TOOL USED CALIPER P/N: 500-196-30 S/N:A20231707 DUE DATE: 06-SEP-23.SEE INDIVIDUAL SIGN OFF STEP BELOW.;[03] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 57,989 hrs · 34,674 cycles

CRACK SUPPORT BRACKET BS 540 AND LBL 6 AT AIR CONDITIONING BAY 2023-447326<[01] REPLACED SUPPORT BRACKET LOCATED BS 540 AND LBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] COMPLETED

Part: PLATE — CORRODED (ZN 100 FUS LOWER) · airframe 57,989 hrs · 34,674 cycles

CORROSION COVER PLATE LOCATED BS400 TO BS420 AND BETWEEN STR27L TO STR28L AND WL149.5 LOWER FUSELAGE 2023-447319<[01] REPLACED COVER PLATE LOCATED BS400 TO BS420 AND BETWEEN STR27L TO STR28L AND WL149.5 LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SING-OFF BELOW;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PLATE — CORRODED (ZN 100 FUS LOWER) · airframe 57,989 hrs · 34,674 cycles

CORROSION COVER PLATE LOCATED BS440 TO BS460 AND BETWEEN STR27L TO STR28L AND WL149.5 LOWER FUSELAGE 2023-447320<[01] REPLACED COVER PLATE LOCATED BS440 TO BS460 AND BETWEEN STR27L TO STR28L AND WL149.5 LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SING-OFFS BELOW;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 56,157 hrs · 33,512 cycles

RT WING I/B MAIN FLAP DELAMINATED APPROX 11 FOR O/B EDGE. DAMAGE IS APPROX 11.5X5.7. PERFORMED TEMPORARY REPAIR OF RT WING INBD MAIN FLAP PER SRM 57-53-01-1A-1. PERFORMED INTERIM REPAIR OF RH WING INBD MAIN FLAP PER SRM 57-53-01-1A-1.

Part: HANDLE — LOOSE (L1 DOOR) · airframe 55,318 hrs · 32,967 cycles

INSIDE L1 DOOR ASSIST CLOSE HANDLE UPPER ATTACHMENT LOOSE. / [01] TIGHTENED INSIDE L1 DOOR ASSIST CLOSE HANDLE UPPER ATTACHMENT PER AMM-52-11-00;[02] INSPECTED

Part: LAMP — INOPERATIVE (PAX CABIN) · airframe 55,303 hrs · 32,957 cycles

20 ABC EMER LIGHT INOP / [01] RELAMPED 20ABC EMERGENCY LIGHT PER AMM 33-51-03. OPS CHECK NORMAL.

Part: TRANSMITTER — FAILED (E&E BAY) · airframe 54,982 hrs · 32,737 cycles

FLAP ASSEMETRY; RIGHT SIDE LOCKED OUT. F185 ATL-LGA DIVERTED INTO EWR._PERFORMED FSEU BITE FOUND MAINT MSG 27-52260; PER FIM 27-51 TASK 820; / R&RD R/H FLAP POSITION TRANSMITTER PER AMM 27-58-01; AND FLAP POSITION INDICATOR PER AMM 27-58-02; ALL OPS CHECKS NORMAL._BWI MX DROVE;

Part: TRANSMITTER — FAILED (E&E BAY) · airframe 54,983 hrs · 32,737 cycles

POSITIONED FLAP HANDLE TO 5; FLAPS FAILED TO EXTEND BEYOND 1; SPLIT NEEDLE INDICATION INDICATED. TRAILING EDGE FLAP LOCKOUT / [01] PERFORMED FSEU BITE FOUND MAINT MSG 27-52260; PER FIM 27-51 TASK 820; R&R?D R/H FLAP POSITION TRANSMITTER PER AMM 27-58-01; AND FLAP POSITION INDICATOR PER AMM 27-58-02; ALL OPS CHECKS NORMAL.

Part: ENGINE — FLAMED OUT · airframe 54,750 hrs · 32,579 cycles

DURING TAXI OUT ATC AND FLIGHT ATTENDANTS REPORTED FLAMES OUT OF THE BACK OF THE #1 ENGINE / [01] PERFORMED GVI OF #1 ENGINE INLET AND EXHAUST AREA; NO DEFECTS NOTED. PERFORMED #1 ENGINE START PROCEDURE; NO DEFECTS NOTED IAW AMM 71-00-00. A/C OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTEROR) · airframe 53,568 hrs · 31,817 cycles

LEFT NR 3 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS. OPS CHECK GOOD.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 53,478 hrs · 31,766 cycles

SUPPLEMENTAL INFORMATION: R1 DOOR SLIDE NEEDS REPACK / [01] REPACKED R1 DOOR SLIDE PER AMM 25-66-01 MT 725-61-06

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 53,478 hrs · 31,766 cycles

SUPPLEMENTAL INFORMATION: R2 DOOR SLIDE NEEDS REPACK / [01] REPACKED R2 DOOR SLIDE PER AMM 25-66-01 AND MT 725-61-06

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,002 hrs · 31,465 cycles

LEFT HAND LOWER EMERGENCY SLIDE LIGHT IS INOP. / [01] RE-LAMPED AND PERFORMED GOOD OPS TEST OF LEFT HAND LOWER EMERGENCY SLIDE LIGHT PER AMM 33-51-04-960-801.; [02] VERIFIED CORRECTIVE ACTIONS STEP 1.

Part: NONE — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

AFT CARGO BAY R/H SIDEWALL CAP STRIP CRACKED BS 790 STR 18 - STR 25 ; / [01] REPLACED CRACKED AFT CARGO BAY R/H SIDEWALL CAP STRIP AT BS 790; STR 18R - 25R WITH NEW PART S/N / LOT# 1421820-3 IAW AMM 25-52-06-400-801 PAR. 3.D. (9)<BR><BR>ATS SCREW GUN ATS2246 S/N 1703310 07/2022; [02] VERIFIED AFT CARGO BAY CAP STRIP AT BS 790 STR 18R - 25R INSTALLED PER AMM 25-52-06-400-801 PARA. 3.D.(9).

Part: NONE — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

AFT CARGO BAY FLOOR PNL 140CF CRACKED. CRACK FOUND L=1' X W=1 X D=.080'; NO CRACKS ALLOWED IAW SRM REPAIR BY REPLACEMENT. FABRICATED NEW ACB FLOOR PANEL 140CF IAW DWG 435A2610 AND SRM 51-40-05.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

FWD CARGO BAY AFT BULKHEAD GUSSET CRACKED AT BS 500D, S19R. REMOVED FWD CARGO BAY AFT BULKHEAD GUSSET IAW SRM 51-40-02-0G-0. REMOVED FWD CARGO BAY AFT BULKHEAD GUSSET IAW SRM 51-40-02-0G-0. LOCATED & DRILLED NEW PART IAW SRM 51-40-05-0G-0 & DWG 143A7902. INSTALLED FWD CARGO BAY AFT BULKHEAD GUSSET IAW 737 SRM51-40-02-0G-0 AND DWG 143A7902.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

FWD CARGO BAY AFT BULHEAD GUSSET CRACKED AT BS 500D STR 21L REMOVED FCB AFT BULKHEAD GUSSED IAW SRM 51-40-02. LOCATED AND DRILLED NEW GUSSET IAW SRM 51-40-02 AND DWG 143A481 ID:0003 REV -. INSTALLED FCB AFT BULKHEAD GUSSET IAW SRM 51-40-02 AND DWG 143A7902.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

FWD CARGO BAY AFT CORNER SCUFF PLATE CRACKED. WELDED CRACKS ON FCB; AFT CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1 PARA. 4.B. (2) & (4). FLUORESCENT DYE PENETRANT INSPECTED REPAIRED AREA IAW SOPM 20-20-02 METHOD C. NO CRACKS FOUND. SANDED WELD REPAIR AREA PER SRM 53-30-15-2R-1 PARA. 4.B. (5). APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO BARE METAL IAW SRM 53-30-15-2R-1, SOPM 20-43-03, & SPOM 20-41-02. INSTALLED FWD BAY AFT CORNER SUFF PLATE IAW SRM 53-30-15-2R-1.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

FWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED, WELDED CRACKS ON FCB; FWD CORNER SCUFF PLATE IAW SRM 53-30-15-2R-1 PARA. 4.B. (2) & (4). FLUORESCENT DYE PENETRANT INSPECTED REPAIR AREA IAW SOPM 20-20-02 METHOD C. NO CRACKS FOUND. SANDED WELD REPAIR AREA PER SRM 53-30-15-2R-1 PARA. 4.B. (5). APPLIED CHEMICAL CONVERSION COATING AND BMS-10 PRIMER TO BARE METAL IAW SRM 53-30-15-2R-1, SOPM 20-43-03, SPOM 20-41-02. INSTALLED FWD BAY FWD CORNER SUFF PLATE IAW SRM 53-30-15-2R-1.

Part: INTERCOSTAL — ELONGATED (FUSLELAGE) · airframe 53,002 hrs · 31,465 cycles

AFT CARGO RH FLOOR INTERCOSTAL HAS AN ELONGATED HOLE; BS 727A + 5; RBL 21; WL 156. REMOVED INTERCOSTAL IAW SRM 51-40-02. DID NOT FIND ALLOWABLE DAMAGE IN SRM. REPLACED PART FOR REPAIR IAW SRM 51-10-02. LOCATED AND DRILLED NEW PART IAW SRM 51-40-05-0G-0 AND DWG 146A7502. INSTALLED AFT CARGO R/H FLOOR INTERCOSTAL AT BS 727A TO BS 727B; RBL 21; WL 156 IAW SRM 51-40-02-0G-0 AND DWG 146A7500 ; ID 88; [07] VERIFIED AFT CARGO BAY R/H FLOOR INTERCOSTAL AT BS 727A TO BS 727B; RBL 21; WL 156 INSTALLED PER SRM 51-40-02-0G-0 AND DWG 146A7500 .

Part: SPLICE STRAP — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

UPON ACCOMPLISHING HFEC INSPECTION; FOUND 1 (EA) CRACK IN SEAT TRACK FASTENER HOLE AT BS 727B RBL 24.75 COMMON TO THE LWR STRAP. ; / [01] REMOVED AND REPLACED LWR SPLICE STRAP AT BS727B RBL 24.75 IAW SB 737-53-1296 FIG.7 & FIG11.; [02] REJECTION: INCORRECT ORIENTATION ON RADIUS FILLER; RAISED FAULT TTG8Q006UCGQ.; [03] UPDATED MEASUREMENT CHART.; [04] UPDATED PARTS.; [05] VERIFIED SPLICE STRAP REPLACED AT BS 727 RBL 24.75 PER 51-40-02 AND SB 737-53-1296.

Part: NONE — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY TENSION STRAP AT B.S..794 - 807+14; 827+7 AND 827+14; R.B.L. 20; W.L. 154. ; / [01] REMOVED CORROSION FROM ACB TENSION STRAP BS 827+14; RBL 20 IN AN AREA OF L=2.5 X W=2 X DEPTH= 0.025 FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 4(G).3 FIG103 DETAIL G.; [02] USED TOOL DEPTH GAUGE ID# ATS400 DUE 08/2022.; [03] PROCURED ; LOCATED AND DRILLED NEW TENSION STRAP ; BTW B/S 767+10' TO B/S 847+14' RBL 20 WL 154 LOT#1468918 IAW SRM 51-40-05 AND DWG 146A8120 REV:-. AND 146A 8130 REV:B AND OK TO INSTALL; [04] VERIFIED CORRECTIVE ACTION 1 AND 3.; [05] REMOVED TENSION STRAP ; BTW B/S 767+10' TO B/S 847+14' IAW SRM 51-40-02; [06] INSTALLED NEW TENSION STRAP BS 767+10' TO BS 847+14' RBL 20 WL 154 IAW DWG: 146A8120 ID:0034 REV:- ; DWG:146A0081 ID:0031 REV:- AND SRM 51-40-02; [07] INSTALLED NEW TENSION STRAP BS 767+10' TO BS 847+14' RBL 20 WL 154 IAW DWG: 146A8120 ID:0034 REV:- ; DWG:146A0081 ID:0031 REV:- AND SRM 51-40-02; [08] RII VERIFIED NEW STRAP INSTALLED IAW DWG: 146A8120 ID:0034 REV:- ; DWG:146A0081 ID:0031 REV:- AND SRM 51-40-02.; [09] VERIFIED ALL STEPS COMPLETE; JOB COMPLETE.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY SHIELD AT B.S. 767+3; 767+7; 767+11; 767+12; 767+15; 767+16 AND 767+19; R.B.L. 22; W.L. 154. ; / [01] CORROSION ON SHIELD ACB IT'S OUT OF LIMITS DUE TO NO ARE LIMITS GIVEN IN SRM. REPLACEMENT PAR PER SRM 51-10-02-0G-0 STEP 9.C. REMOVED ACB SHIELD AT BS794-787 RBL22. WL154 IAW SRM 51-40-02; [02] UPDATED MEASUREMENTS; [03] VERIFIED CORRECTIVE ACTION 1.; [04] LOCATED AND DRILLED NEW SHIELD SUPPORT AT BS 767+3;RBL 22; WL 154 IAW SRM 51-40-05-0G-0 AND DWG 146A0081; ID 31; [05] VERIFIED CORRECTIVE ACTION 4.; [06] REQUEST OK TO INSTALL.; [07] OKAY TO INSTALL NEW SHIELD SUPPORT IN THE AFT CARGO BAY AT BS 767-787 RBL 22 WL 154.; [08] INSTALLED NEW ACB SHIELD AT BS 767-787 RBL 22 WL 154 IAW DWG 146A0081 SHEET 34 AND SRM 51-40-02-0G; [09] VERIFIED INSTALLED NEW ACB SHIELD AT BS 767-787 RBL 22 WL 154 IAW DWG 146A0081 SHEET 34 AND SRM 51-40-02-0G.; [10] VERIFIED ALL STEPS COMPLETE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT B.S. 947; R.B.L. 23; W.L. 157. ; / [01] REMOVED CORRODED AFT CARGO BAY BULKHEAD CENTER PANEL LOWER SUPPORT AT BS 947.5 RBL 23 WL157. NO LIMITS FOUND IN SRM; REPAIR BY REPLACEMENT. IAW SRM 51-10-02-0G-0 PARAGRAPH 9 STEP C; SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW BRACKET ASSY SUPPORT PO#812692 IAW SRM 51-40-05-0G-0; DWG 149A8118 REV B <BR><BR>OK TO INSTALL; [03] OKAY TO INSTALL AFT CARGO BAY AFT BULKHEAD LOWER SUPPORT BRACKET P/N 149A8118-27 AT BS947; RBL 23.; [04] INSTALLED AFT CARGO BAY SUPPORT BRACKET AT BS 947.5 RBL 23 WL157 IAW SRM 51-40-02-0G-0; DWG 149A8118 REV B; 149A8110 REV B; [05] VERIFIED AFT CARGO BAY SUPPORT BRACKET AT BS 947.5 RBL 23 WL 157 INSTALLED PER SRM 51-40-02-0G-0; DWG 149A8118 REV B AND 149A8110 REV B.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

AFT CARGO BAY FORWARD BULKHEAD PANEL SUPPORT ATTACH BRACKET IS CRACKED AT BS 727, RBL 3, WL 160. INSTALLED A NEW ATTACH BRACKET IAW SRM 51-40-02 AND DWG 144A2600.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY SHIELD SUPPORT AT B.S. 847+1 AND 847+2; R.B.L. 22; W.L. 154. ; / [01] REMOVED AFT CARGO BAY AFT SHIELD IAW SRM 51-40-02-0G-0; [02] THERE ARE NO SRM ALLOWABLE DAMAGE FOR AFT CARGO BAY SHIELD. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9.C; [03] VERIFIED CORRECTIVE ACTION 1 AND 2.; [04] LOCATED AND DRILLED NEW SHIELD SUPPORT AT BS 847+1;RBL 22; WL 154 IAW SRM 51-40-05-0G-0 AND DWG 146A0081; ID 31; [05] VERIFIED CORRECTIVE ACTION 4.; [06] REQUESTING OK TO INSTALL NEW SHIELD SUPPORT AT BS 847-BS 867;RBL 22; WL 154; [07] OKAY TO INSTALL SHIELD SUPPORT AT BS 847 - BS 867 AND RBL 22; WL 154.; [08] INSTALLED SHIELD SUPPORT AT BS 847 - BS 867 AND RBL 22; WL 154. IAW SRM 51-40-02 AND DWG 146A0081 REV:-; [09] VERIFIED CORRECTIVE ACTION ENTRY 8.; [10] VERIFIED CARD COMPLETE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY INTERCOSTAL AT B.S..767+5; R.B.L. 20; W.L. 154. ; / [01] REMOVED DAMAGE FROM ACB INTERCOSTAL BS 767+5 RBL 20; MATERIAL LOSS MORE THAN 20% FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1.; [02] REMOVED INTERCOSTAL AT RBL 20 WL 154 BS 767 TO BS 787 IAW ARM 51-40-02-0G-0; LOCATED AND DRILLED NEW INTERCOSTAL P/N 146A8123U19 PO# 1466078 IAW SRM 51-40-05-0G-0; [03] VERIFIED CORRECTIVE ACTION 2.; [04] REQ. OK TO INSTALL INTERCOSTAL AT AFT CARGO BAY INTERCOSTAL AT B.S..767-787 R.B.L. 20; W.L. 154; [05] VERIFIED CORRECTIVE ACTION 4.; [06] INSTALLED INTERCOSTAL AT AFT CARGO BAY AT B.S..767-787 R.B.L. 20; W.L. 154 IAW SRM 51-40-020G-0 AND DWG 164A0081 REV.-; [07] VERIFIED CORRECTIVE ACTION ITEM 6.; [08] APPLIED CORROSION INHIBITING COMPOUND AT AFT CARGO BAY INTERCOSTAL AT B.S..767-787 R.B.L. 20; AND REWORK AREA IAW SOPM 20-41-05; [09] VERIFIED CORRECTIVE ACTION 8.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 887+9; 907+2; 907+6 AND 927+10; R.B.L. 22; W.L. 154. REMOVED ACB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02. REMOVED AND EVALUATED DAMAGE, LARGEST AREA OF REMOVED MATERIAL AT BS 947. DAMAGE MEASURES 1.33' L; 0.61' W; 0.006' D. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED ACB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02. DRILLED A NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05; 51-40-08 AND DWG 147A7501 REV A. APPLIED CHEMICAL CONVERSION COATING IAW SOPM 20-41-02. LOCATED AND DRILLED THE NEW FLOOR TO SIDEWALL SUPPORT1 IAW SRM 51-40-05; 51-40-08 AND DWG 147A7501 ID: 0006 REV:A.

Part: WEB — CORRODED (BS 794 RBL 22) · airframe 53,002 hrs · 31,465 cycles

CORROSION ON AFT CARGO BAY DOOR THRESHOLD SUBWEB AT B.S..794+3; R.B.L. 22; W.L. 154. ; / [01] REMOVED ACB DOOR THRESHOLD SUBWED AT B.S. 807-847 RBL 22 WL 154 IAW 51-40-02; [02] REMOVED ACB DOOR THRESHOLD SUBWED AT B.S. 807-847 RBL 22 WL 154 IAW 51-40-02; [03] REMOVED CORROSION FROM ACB DOOR THRESHOLD WEB AT BS 794+3 RBL 22 MEASURED 3'L X 2'W AND 0.020' DEEP ORIGINAL THICKNESS OF 0.045' FOUND OUT OF LIMITS PER SRM 53-60-15-1A-1; [04] REMOVED CORROSION FROM ACB DOOR THRESHOLD WEB AT BS 794+3 RBL 22 MEASURED 3'L X 2'W AND 0.020' DEEP ORIGINAL THICKNESS OF 0.045' FOUND OUT OF LIMITS PER SRM 53-60-15-1A-1; [05] VERIFIED DAMAGE OUT OF LIMITS PER SRM 53-60-15-1A-1; [06] UPDATED MEASUREMENTS; [07] LOCATED AND DRILLED NEW ACB SUBTHRESHOLD WEB PER SRM 51-40-05; SRM 51-40-08; DWG# 146A8123.; [08] VERIFIED CORRECTIVE ACTION 7.; [09] REQUEST OK TO INSTALL.; [10] CERTIFIED ACTION 9; [11] OK TO INSTALL GIVEN.; [12] APPLIED SEALANT AT 06:27 UTC 13OCT21 AND INSTALLED ALL TEMP AND PERMANENT FASTENERS IAW SRM 51-31-00-390-801 ; SRM 51-40-02; DWG 146A8340 ID 28 REV-; [13] VERIFIED CORRECTIVE ACTION ENTRY 12.; [14] INSTALLED REMAINING PERMANENT FASTENERS IN ACB CARGO BAY DOOR THRESHOLD SUBWED AT BS 794+3 RBL 22 WL 154 IAW SRM 51-40-02 0G-0 AND DWG 146A8340 REV:-; [15] RII INSPECTED ACTION 14; [16] INSPECTION COMPLETE

Part: SIDEWALL SUPPORT — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 747+16 AND 747+19; R.B.L. 22; W.L. 154. ; / [01] REMOVED AND EVALUATED MULTIPLE AREAS OF CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT R/H FROM BS 747+16 TO BS 747+19. LARGEST AREA OF MATERIAL REMOVED MEASURED 1.84' L; 1.25' W; 0.005' D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMAINDER OF WORK TO BE ACCOMPLISHED ON TASK TTG8Q006S5CK.; [02] VERIFIED CORRECTIVE ACTION STEP 1; [03] REMOVED AND EVALUATED MULTIPLE AREAS OF CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT R/H FROM BS 747+16 TO BS 747+19. LARGEST AREA OF MATERIAL REMOVED MEASURED 1.84' L; 1.25' W; 0.005' D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMAINDER OF WORK TO BE ACCOMPLISHED ON TASK TTG8Q006S5CK; [04] VERIFIED ACTION 3

Part: SIDEWALL SUPPORT — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S..727E+10; 727E+14; 727E+15; 727E+18; 727E+19; 747; 747+2; 747+5; 747+6 AND 747+10; R.B.L. 22; W.L. 154. ; / [01] REMOVED AND EVALUATED MULTIPLE AREAS OF CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT R/H FROM BS 727E+10 TO BS 747+10 RBL 22 WL 154. LARGEST AREA OF MATERIAL REMOVED MEASURES 2.4' L; 0.98' W; 0.18' D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMAINDER OF WORK TO BE ACCOMPLISHED ON TASK TTG8Q006S5CK.; [02] VERIFIED CORRECTIVE ACTION STEP 1; [03] REMOVED AND EVALUATED MULTIPLE AREAS OF CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT R/H FROM BS 727E+10 TO BS 747+10 RBL 22 WL 154. LARGEST AREA OF MATERIAL REMOVED MEASURES 2.4' L; 0.98' W; 0.18' D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMAINDER OF WORK TO BE ACCOMPLISHED ON TASK TTG8Q006S5CK; [04] VERIFIED ACTION 3

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S..727B+14; 727C+5; 727C+10; 727D+3; 727D+7; 727D+10; 727D+14; 727D+19; 727E+2 AND 727E+6; R.B.L. 22; W.L. 154. ; / [18] INSTALLED FLOOR TO SIDEWALL SUPPORT AT ACB B.S 727 TO B.S 767; R.B.L. 22 W.L. 154 PER SRM 51-40-02-0G-0 AND DWG 146A7500; 146A7502; AND 146A0061; [19] VERIFIED CORRECTIVE ACTION ENTRY 17.; [20] VERIFIED CARD COMPLETE

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S..727A+10; 727B+5; 727B+8; 727C+14; 727D+2; 727D+4; 727D+5; 727D+7; 727D+10 AND 727D+15; L.B.L. 22; W.L. 154. ; / [23] INSTALLED NEW FLOOR TO SIDEWALL SUPPORT LOCATED BTW B/S 727 TO B/S 847 LBL 22 WL 154 IAW SRM 51-40-02 AND DWG 146A7502 REV:-. AND 146A7500 REV:A; [24] VERIFIED CORRECTIVE ACTION ENTRY 23.; [25] VERIFIED CARD COMPLETE

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 767+3; 767+7; 767+10; 767+14; 787+6 AND 787+10; L.B.L. 22; W.L. 154. ; / [01] REMOVED AND EVALUATED MULTIPLE AREAS OF CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT L/H FROM BS 767+3 TO BS 787+10. LARGEST AREA OF MATERIAL REMOVED MEASURED 1.32' L; 1.15' W; 0.004' D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMAINDER OF WORK TO BE ACCOMPLISHED ON TASK TTG8Q006S5AU.; [02] VERIFIED CORRECTIVE ACTION STEP 1; [03] REMOVED AND EVALUATED MULTIPLE AREAS OF CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT L/H FROM BS 767+3 TO BS 787+10. LARGEST AREA OF MATERIAL REMOVED MEASURED 1.32' L; 1.15' W; 0.004' D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMAINDER OF WORK TO BE ACCOMPLISHED ON TASK TTG8Q006S5AU; [04] VERIFIED CORRECTIVE ACTION 3.; [05] VERIFIED FLOOR TO SIDEWALL SUPPORT WILL BE REPLACED ON TASK TTG8Q006S5AU

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

FWD CARGO INTERCOSTAL ATTACH ANGLE CRACKED BS 400 LBL 25 WL 155. REMOVED INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02 AND DWG 143A7505 REV.-B. LOCATED AND DRILLED NEW ATTACH ANGLE IAW SRM 51-40-02-0G0-0, AND DWG 143A7505 REV- B. INSTALLED FCB INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02 AND DWG 143A7505 ID:0002 REV B.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

CORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL24 WL156. EVALUATED DAMAGE ON SHIELD AND NO FOUND ALLOWABLE DAMAGE LIMITS IN SRM 51-10-02-0G-0 PARA 9. REMOVED SHIELD IAW SRM 51-40-02. LOCATED & DRILLED IAW SRM 51-40-05-0G-0 & DWG 143A0080. INSTALLED FCB AFT SHIELD IAW SRM 51-40-02-0G-0 AND DWG 143A0080 REV -.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500 -BS500B LBL24 WL156. ; / [24] INSTALLED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 396-500D LBL24 WL 156 IAW SRM 51-40-02 ;DWG 143A7500 REV:- AND DWG 143A7505 REV:D.; [25] VERIFIED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT INSTALLED AT BS 396-500D LBL 24 WL 156 PER SRM 51-40-02 ;DWG 143A7500 REV:- AND DWG 143A7505 REV:D.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

CORROSION ON FWD SHIELD AT FWD CARGO BAY BS420 - 440, RBL 23, WL 156. REMOVED SHIELD IAW SRM 51-40-02. LOCATED AND DRILLED THE SHIELD IAW SRM 51-40-05 AND DWG 143A0080. INSTALLED FWD SHIELD AT FCB BS.420 TO BS.440 RBL 23 WL 156 IAW SRM 51-40-02 AND BOEING DWG 143A0080- REV-.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

CRACKED STRINGER 26R, BS 540, WL 153. REMOVED FASTENERS FROM STRINGER IAW SRM 51-40-02-0G-0. EVALUATED CRACK AND FOUND OUT OF LIMITS IAW SRM 53-00-03-1A-1, PARA 4A(2)(A)1. FABRICATED, LOCATED & DRILLED A NEW STRINGER SECTION AND SPLICE IAW SRM 53-00-03-2R-1, FIG 205. APPLIED CHEMICAL CONVERSION COATING ON REPAIR PARTS IAW SRM 53-00-03-2R-1, PARA 4.I. APPLIED PRIMER ON REPAIR PARTS IAW SRM 53-00-03-2R-1. PERFORMED VISUAL INSPECTION, NO MORE DAMAGE FOUND IAW SRM 53-00-03-2R-1, REPAIR 1 STEP 4B(1). HFEC INSPECTED CUT EDGES IAW NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. INSTALLED THE NEW STRINGER SECTION AND SPLICE IAW SRM 53-00-03-2R-1, REPAIR 1, SOPM 20-50-19 AND DWG 143A3230 REV A.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A -BS500D RBL24 WL156. ; / [16] INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 500A-500D RBL 24 WL 156;IAW SRM 51-40-02 ;DWG 143A7500 REV:- AND DWG 143A7505 REV:D.; [17] VERIFIED INSTALLATION OF THE FLOOR TO SIDEWALL SUPPORT BS500500D RBL 24 WL156 PER SRM 51-40-02; DWG 143A7500 REV:- AND DWG 143A7505 REV:D.

Part: STRINGER — CRACKED (BS 540 S25R) · airframe 53,002 hrs · 31,465 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS 540, S25R, WL 156. EVALUATED CRACK AND FOUND OUT OF LIMITS IAW SRM 53-00-03-1A-1 PARAGRAPH 4A(2)(A)1. REMOVED FASTENERS FROM STRINGER 25 RT IAW SRM 51 40-02. REMOVED DAMAGE BY TRIMMING IAW SRM 51-10-02. LOCATED AND DRILLED A NEW SECTION OF STRINGER IAW SRM 51-40-05 AND 53-00-03-2R-1. STRINGER 25R REPAIRED IAW EA 21-153-02986 REV A.

Part: NONE — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS 454 - 476, RBL 28, WL 156. EVALUATED DAMAGE ON SUBTHRESHOLD WEB. ORIGINAL THICKNESS .045' DAMAGE REMOVED; .009' REMAINING THICKNESS .0036 L= 2' X W=1.2' DEPTH .009 DAMAGE EXCEED 10% OF ORIGINAL THICKNESS, FOUND TO BE OUT LIMITS IAW SRM 53-30-15-1A-1; 4.G.(12). REMOVED SUBTHRESHOLD WEB IAW SRM 51-40-02. LOCATED, DRILLED AND COUNTERSINK NEW SUBTHRESHOLD WEB IAW SRM 51-40-05-0G-0, SRM 51-40-08-0G-0 & DWG 143A8330. INSTALLED FCB SUBTHRESHOLD WEB IAW SRM 51-40-02-0G-0 PAR. 5 AND DWG 143A8330. INSTALLED FCB SUBTHRESHOLD WEB IAW SRM 51-40-02-0G-0 PAR. 5 & DWG 143A8330.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED ; / [01] REMOVED FCB AFT BULKHEAD SUPPORT GUSSET AT BS500D S-19L WL 193 PER SRM 51-40-02; [02] REMOVED FCB AFT BULKHEAD SUPPORT GUSSET AT BS500D S-19L WL 193 PER SRM 51-40-02; [03] NO ALLOWABLE DAMAGE FOUND IN SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0; PARA 9; STEP C; [04] LOCATED AND DRILLED NEW GUSSET IAW SRM 51-40-05; DWG 143A7902 REV-. OKAY TO INSTALL; [05] VERIFIED NEW GUSSET DRILLED; OK TO INSTALL PER SRM 51-40-05 AND DWG 143A7902.; [06] INSTALLED GUSSET AT BS 500D S-19L WL 193 IAW DWG 143A7902 REV -; SRM 51-40-02-0G-0 PARAGRAPH 4.; [07] VERIFIED CORRECTIVE ACTION ITEM 6.; [08] VERIFIED TASK IS COMPLETE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS494; BS500+6; BS500A+7; BS500A+16; BS500B+18; ; / [01] UPON FURTHER INVESTIGATION; FOUND CORROSION TO BE ON SEAT TRACK AT LBL 45.; [02] VERIFIED CORRECTIVE ACTION 1; [03] SEAT TRACK AT BS 480 - BS 520 LBL45 WL208 TO BE REPLACED ON CUSTOMER CARD#TTG8Q006RCWF; [04] VERIFIED CORRECTIVE ACTION 3.; [05] TO BE REPLACED ON CUSTOMER CARD#TTG8Q006RCWF COMPLETE

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

PANEL 191D HAS SEVERAL DELAMINATIONS TO OUTER SURFACE. IDENTIFIED PANEL IAW SRM 53-30-70-0I-1 FIG 2 TABLE 2 ITM 9. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-30-70-1A-1 PARA 4.A. DAMAGE IS TO BE REPAIRED IAW SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11 AS GIVEN IAW SRM 53-30-70-2R-1 PARA 4.B (2) TABLE 202. REMOVED DAMAGED SKIN AND PARTIAL DEPTH CORE IAW SRM 51-70-05-2R-2 PARA 4.A - 4.C. CLEANED; FABRICATED REPAIR PARTS, INSTALLED IAW SRM 51-70-05-2R-11 PAR 4B-E; SRM 51-70-05-2R-2 PAR 4F-G; AND SRM 51-70-14-2R-4 PAR 6D;H-I.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

CRACKED FLOOR SUPPORT AT BODY STATION 540+1; LBL 1; WL 208 ; / [01] REMOVED AND BEGAN INSTALLATION OF FLOOR SUPPORT AT BS 540+1 LBL1 WL208 IAW SRM 51-40-02 AND BOEING DWG 143A0060; [02] COMPLETED INSTALLATION OF FLOOR SUPPORT AT BS 540+1 LBL1 WL208 IAW SRM 51-40-02 AND BOEING DWG 143A0060<BR>MATCH DRILLED FLOOR BOARD HOLES IAW SRM 51-40-05; [03] VERIFIED; [04] VERIFIED CORRECTIVE ACTION ENTRIES 1. AND 2.

Part: ATTACH ANGLE — CRACKED (CENTER WING) · airframe 53,002 hrs · 31,465 cycles

B.S. 663 LOWER COMPOSITE BULK HEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 42; W.L. 163. ; / [01] REMOVED EXISTING SPLICE AND DAMAGE ANGLE AT R/H VAPOR BARRIER BS 663 WL 163 BNETWEEN RBL 65 TO RBL 18 IAW SRM 51-10-02 0G-0; [02] REMOVED EXISTING REPAIR ANGLE AT R/H VAPOR BARRIER BS 663 WL163 RBL 18 TO RBL 6 IAW SRM 51-40-02-0G-0; [03] VERIFIED CORRECTIVE ACTION 1 AND 2.; [04] FORMED AND HEAT TREATED NEW ANGLE IAW 111A1322 REV:B ON CUSTOMER RO NO 840092-SWA JOB NUMBER 543500; [05] LOCATED AND DRILLED NEW ANGLE AT B/S 663 BTW RBL6 - RBL 65 WL 163 IAW SRM 51 40-05 AND DWG 111A1000 REV:AND DWG 111A1000 REV:-. FORMED AND HEAT TREATED NEW ANGLE IAW 111A1322 REV B.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

CRACKED FLOOR SUPPORT AT BODY STATION 540+1; RBL 1; WL 208 ; / [01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 540+1 RBL 1 WL 208 IAW SRM 51-40-02 AND BOEING DWG 143A0060.; [02] MATCH DRILLED FLOOR BOARD HOLES IAW SRM 51-40-05.; [03] VERIFIED; [04] VERIFIED CORRECTIVE ACTION ENTRIES 1. AND 2.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 53,002 hrs · 31,465 cycles

CRACKED FLOOR SUPPORT AT BODY STATION 540+1; RBL 25; WL 208 ; / [01] REMOVED AND REPLACED FLOOR SUPPORT AT BS 540+1 RBL 25 WL 208 IAW SRM 51-40-02 AND BOEING DWG 143A0060 <BR>MATCH DRILLED FLOOR BOARD HOLES IAW SRM 51-40-05.; [02] VERIFIED; [03] VERIFIED CORRECTIVE ACTION ENTRY 1.

Part: GIRT BAR — OUT OF ADJUST (L2 ENTRY DOOR) · airframe 51,071 hrs · 30,326 cycles

AFT ENTRY DOOR SLIDE GIRT NEEDS ADJUSTMENT. INSTALLED AFT ENTRY DOOR SLIDE GIRT PER AMM 25-66-01.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 51,071 hrs · 30,326 cycles

LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED / R&R LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL PER MM 53-31-31

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,071 hrs · 30,326 cycles

LEFT EMER EXIT SIGNS; LT OVERWING LIGHT AND ISLE LIGHT AT 6ABC DIDN'T PASS CAPACITY TEST. R & R BATTERY PACK AND POWER SUPPLY AT M1668 PER AMM 33-51-06.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,071 hrs · 30,326 cycles

LEFT EMER EXIT SIGNS; LT OVERWING LIGHT AND ISLE LIGHT AT 6ABC DIDN'T PASS CAPACITY TEST. R & R BATTERY PACK AND POWER SUPPLY AT M1668 PER AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,621 hrs · 29,415 cycles

EMERGENCY BATTERY PACK AFT LT AND MIDDLE RT INOPERATIVE. REMOVED A DREPLACED AFT LT AND MIDDLE RT EMERGENCY BATTERY PACKS IAW AMM 33-51-06. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 49,498 hrs · 29,347 cycles

SEVERAL LH AFT CABIN EMERGENCY LIGHT'S OUT AND L-2 EXTERNAL EMERGENCY LIGHT OUT. / REMOVED & INSTALLED SERVICEABLE PACK CHARGER ASSY M1673. OPS CK GOOD PER MT 33-51-06

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 47,991 hrs · 28,390 cycles

R/H OVERWING EMERGENCY EXIT SIGN LIGHT COVER MISSING. / INSTALLED LENS PER AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 47,973 hrs · 28,378 cycles

L/H FLOOR TRACK LIGHTING AT ROW 8 AREA PULLED UP FROM FLOOR. / SECURED PHOTO LUMINESCENT STRIP IAW AMM.

Part: PLATE — CRACKED (R/H WING) · airframe 47,811 hrs · 28,275 cycles

R/H WING TRAILING EDGE CAVITY INBD WIGGLE PLATE ABOVE SAIL TAIL HAS FASTENERS SHEARED AND PLATE IS CRACKED / REMOVED AND REPLACED RH WING TRAILING EDGE CAVITY I/B WIGGLE PLATE P/N 115A2781-14 (7570259) WN6612 IAW B 737-700 AIPC 57-50-00-30 & SRM 51-40-02-0G-0

Part: BEAM — CRACKED (R1 DOOR) · airframe 47,811 hrs · 28,275 cycles

R1 DOOR UPPER DOOR BEAM #5 CRACKED IN UPPER FILLET AREA.BY FASTNER HOLE. R&R NR 5 BEAM IAW SRM AND DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 47,811 hrs · 28,275 cycles

R1 DOOR LOWER DOOR BEAM #4 CRACKED BY UPPER FASTNER IN FILLET AREA. R&R #4 BEAM IAW SRM AND DWG.

Part: PANEL — CRACKED (RIGHT WING) · airframe 47,811 hrs · 28,275 cycles

RIGHT WING TRAILING EDGE PANEL 661CB INTERNAL MATING SURFACE AFT FASTENER ROW HAS SEVERAL CRACKED HOLES / REPAIRED FASTENER HOLES ON PANEL 661CB I/A/W SRM 57-51-01-2R-1 REV. 68; SRM 51-70-04-2R-9 REV.68 AND AMM 51-21-99-300-802 REV. 69; AMM 51-21-81-370-802 REV. 69 A33188; A22759; A72331; A98284; A20068

Part: PLATE — CRACKED (R/H WING) · airframe 47,811 hrs · 28,275 cycles

R/H WING TRAILING EDGE CAVITY INBD WIGGLE PLATE ABOVE SAIL TAIL HAS FASTENERS SHEARED AND PLATE IS CRACKED / R/H TRAILING EDGE ACVITY I/B PLATE ABOVE SAIL TAIL REMOVED IAW B-737-700 SRM 51-40-02-0G-0 AND REPLACED NEW IAW -737-700 SRM 51-40-05-0G-0 & SRM 51-40-06-0G-0 & SRM 51-4-02-0G-0. A-TAG # WN8798

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 47,811 hrs · 28,275 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 4 (STAB STA 120.30) IS CRACKED AT 2ND VERTICAL STIFFENER. / REPAIRED STIFFENER IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 47,811 hrs · 28,275 cycles

R/H WING TRAILING EDGE CAVITY ABOVE #6 FLAP TRACK ASSEMBLY WIGGLE PLATE ASSEMBLY CRACKED AT INBOARD FASTENER LOCATION. R&R WIGGLE PLATE ASSEMBLY IAW SRM AND DWG.

Part: PANEL — CRACKED (RIGHT WING) · airframe 47,811 hrs · 28,275 cycles

RIGHT WING TRAILING EDGE PANEL 661BB INTERNAL MATING SURFACE AFT FASTENER ROW HAS SEVERAL CRACKED HOLES / REPAIRED DAMAGE TO FASTENER HOLES ON PANEL 661BB IAW SRM 57-51-01-2R-1 REV 68; SRM 51-70-04-2R-9 REV. 68; AMM 51-21-99-300-802 REV. 69; AMM 51-21-81-370-802 RE. 69 A33188; A22759; A72331; A20069; A98284

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 47,811 hrs · 28,275 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 4 (STAB STA 120.30) IS CRACKED AT 3RD VERTICAL STIFFENER. REPAIRED STIFFENER IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 47,811 hrs · 28,275 cycles

L/H WING AFT TRAILING EDGE CAVITY WIGGLE PLATE UNDER SAIL TAIL INBOARD SIDE, RIVETS SHEARED AND PLATE CRACKED. R&R WIGGLE PLATE IAW SRM & AMM.

Part: BRACKET — BROKEN (LEFT WING) · airframe 47,811 hrs · 28,275 cycles

L/H WING PANEL 551FB FWD BRACKET IS BROKEN OFF 27' FROM OTBD EDGE AS MARKED. / REMOVED BRACKET @ L/H WING PANEL 551FB FWD END 27 FROM OUTBOARD EDGE IAW SRM 51-40-02-0G-0 AND INSTALLED NEW BRACKET P/N 287A9152 A-TAG WN5864 AT L/H WING PANEL 551FB FWD END 27' FROM O/B EDGE IAW SRM 51-40-02-0G-0 PG 2 STEP 4B

Part: RETAINER — CRACKED (RIGHT WING) · airframe 47,811 hrs · 28,275 cycles

R/H WING TRAILING EDGE CAVITY 10' INBD OF DIFLECTOR RIB ASSY BULB SEAL RETAINER IS CRACKED OUTBD SIDE AT FASTENER HOLE / REMOVED CRACKED R/WING TRAILING EDGE FITTING AND BULB SEAL RETAINER 10' I/B DEFLECTOR RIB. VERIFIED NEW PART. P/N 115A2953-2 (A21612) IAW IPC 57-50-00-25 MATCH DRILLED NEW FITTING IAW 737-700 SRM 51-40-050G-0 AND INSTALLED IAW 737-700 SRM 51-40-02-0G-0

Part: SKIN — DENTED (BS 1016) · airframe 47,811 hrs · 28,275 cycles

SECTION 48 EXTERNAL SKIN HAS A DENT AT STA 1016 +4.5", 2.0" ABOVE S-14L. / REPAIRED SKIN PER ER AND SWA EA.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 47,811 hrs · 28,275 cycles

RIGHT WING TRAILING EDGE PANEL 651GB AFT BULB SEAL RETAINER IS CRACKED AT OUTBOARD END / REPLACED CRACKED BULB SEAL RETAINER ON PNL 651GB IAW SRM 51-40-02-0G-0. A TAG #WN8435

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,735 hrs · 28,227 cycles

LEFT FWD EMERGENCY BATTERY PACK DOES NOT LAST THE REQUIRED TEST TIME. R&R LEFT FWD EMERGENCY BATTERY PACK AND CHARGER PER AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 47,735 hrs · 28,227 cycles

AFT CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED. / REMOVED AND REPLACED SCUFF PLATE REF AMM 53-11-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,735 hrs · 28,227 cycles

RIGHT FWD EMERGENCY BATTERY PACK DOES NOT LAST THE REQUIRED TEST TIME. R&R RIGHT FWD EMERGENCY BATTERY PACK AND CHARGER PER AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,018 hrs · 27,718 cycles

R2 DOOR EMERGENCY EXIT LIGHTS INOP. R&R AFT RH BATTERY PACK IAW MM.

Part: HOOK — OUT OF ADJUST (R1 DOOR GIRT BAR) · airframe 46,352 hrs · 27,305 cycles

FORWARD SERVICE DOOR SLIDE GIRT BAR WILL NOT STAY IN THE DISARMED/STOWED POSIITON. ADJUSTED AFT BAR RETAINER HOOK ON FWD SERVICE DOOR AND VERIFIED SECURITY OF GIRT BAR WITH SLIDE DISARM REF AMM 25-66-01

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,294 hrs · 27,265 cycles

L/H SIDE EMERGENCY LIGHT BEHIND L2 DOOR INOP. RELAMPED LIGHT PER AMM.

Part: COVER — DISLODGED (EXIT SIGN) · airframe 44,209 hrs · 25,931 cycles

MID CABIN CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN DISLODGED. REINSTALLED COVER PER SIP.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 44,199 hrs · 25,924 cycles

LT PHOTOLUMINESCENT STRIP MISSING AT AISLE 1. INSTALLED STRIP PER DWG.

Part: LATCH — LOOSE (CABIN) · airframe 42,395 hrs · 24,762 cycles

AFT GALLEY FLASHLIGHT COMPARTMENT DOOR LATCH LOOSE. SECURED LATCH PER SIP.

Part: PANEL — CRACKED (LT WING) · airframe 41,297 hrs · 24,071 cycles

LEFT WING; LOWER LEADING EDGE PANEL 521ZB; CRACKED AT FOWARD OUTBOARD FASTENER HOLE. / REPAIRED AND RESTORED FINISH ON EDGE PANEL 521ZB OUTBOARD FASTENER HOLE IAW B737-700 AMM 51-21-99-300-801 REV 63; SRM 51-70-14-2R-REV62; SRM 51-70-04-2R-0 REV 62 SRM 57-41-01-2R-1 REV 62

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 41,297 hrs · 24,071 cycles

RIGHT WING SUPPORT ANGLE CRACKED AT DEFLECTOR RIB. R & R THE SUPPORT ANGLE IAW SRM AND DWG.

Part: PLATE — CRACKED (LT WING SKIN) · airframe 41,297 hrs · 24,071 cycles

LEFT WING LOWER TRAILING EDGE SKIN WIGGLE PLATE JUST OUTBOARD OF THE NR 3 FLAP TRACK CRACKED. R & R THE WIGGLE PLATE IAW SRM AND DWG.

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 41,297 hrs · 24,071 cycles

PASSENGER CABIN FLOOR PANEL BREAK CRACKED AT STA 540 BL 0 TO RBL 25 / STA 540 BETWEEN BL O AND RBL 25'; REMOVED AND REPLACED PANEL BREAK MPN 143A5240-36 SI # 75309009 ATAG VE0043; IAW BOEING DWG 143A0060 AND SRM 51-40-02-0G-0

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,297 hrs · 24,071 cycles

RIGHT STABILIZER LEADING EDGE RIB CRACKED AT BS 114.55 BETWEEN RADIS AND FASTENER HOLE. R & R THE RIB IAW DWG & SRM.

Part: RIB — ELONGATED (RT HORIZ STAB) · airframe 41,297 hrs · 24,071 cycles

REF. EA1-A55-3550 STEP 16. HORIZONTAL STAB. RIGHT SIDE LEADING EDGE RIB HAS ONE ELONGATED RIVET HOLE ON LOWER FLANGE. (AT STATION 133.15) / RH STAB HORIZONTAL LEADING EDGE RIB AT STA 133.15 REMOVED ON NON-ROUTINE X637200. RECIVED NEW RIB P/N 186A1307; SI# 7550164 A-TAG WN7783 LOCATED AND DRILLED NEW RIB AND INSTALLED NEW RIN IN RH STAB HORIZONTAL LEADING EDGE AT STA 133.15 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 186A1001 REV A

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 41,297 hrs · 24,071 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT HSS 216.83, UPPER AFT FASTENER HOLE. R & R THE RIB IAW SRM & DWG.

Part: FAIRING — CORRODED (LWR FUSELAGE) · airframe 41,297 hrs · 24,071 cycles

KEEL BEAM PANEL 192F HAS CORROSION AT BOTH DME ANTENNA MOUNT LOCATIONS / REPAIRE OF KEEL BEAM PANEL WAS ACCOMPLISHED ON BACK SHOP REPAIRE ORDER # 36442 1000 0004 PANEL #192F AND #36440-1000-0036

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 41,297 hrs · 24,071 cycles

FLOOR BOARD 241TF IS PUNCTURED [MARKED] / REPAIRED FLOORBOARD 241TF PUNCTURE I-A-W B737-700SRM 53-00-50-2R-4 REV 62 SRM 53-00-50-2R-0 REV 62

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,297 hrs · 24,071 cycles

SUPPLEMENTAL INFORMATION: PASSENGER CABIN SEAT TRACK LBL 45 BETWEEN STA 500B AND 520 GOUGED WITH MINOR CORROSION IN BASE AND CROWN AS MARKED / BLENDEDGAUGEAT PASSENGER CABIN SEAT TRACK LBL 45 STA 500B-520 AND FOUND DEPTH OF .030' LOSS; .020' ALLOWED FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1. CUT OUT DAMAGED SECTION OF SEAT TRACK AND SPLICED IN NEW IAW WA 1-A53-11779REV. I AND SRM 53-00-52-2R-4

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 41,297 hrs · 24,071 cycles

PASSENGER CABIN FWD WET AREA BETWEEN STA 312 AND 328 LBL 47 INTERCOASTAL IS CRACKED AS MARKED / AT PASSENGER CABIN; FWD WET AREA; BETWEEN STA 312 TO 328 LBL 47REMOVED + REPLACED INTERCOSTAL IAW- BOEING DWG 141A5400 REV:- AND B737-700 SRM 51-40-02-0G-0 PAR 7.D. AND FIG 12. PART A TAG # IS A82274

Part: TEE FITTING — CRACKED (BS 520) · airframe 41,297 hrs · 24,071 cycles

TEE CAP CRACKED AT BS 520, RBL 65. REPAIRED THE TEE CAP IAW EA.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 41,297 hrs · 24,071 cycles

PASSENGER CABIN FWD WET AREA BETWEEN STA 312 AND 328 RBL 31 INTERCOASTAL IS CRACKED AS MARKED / AT PASSENGER CABIN FWD WETAREA BETWEEN B.S.312 TO 328 RBL31 REMOVED AND REPLACED INTERCOSTAL I.A.W. BOEING DWG 141A541OU12;AND B737-700 S.R.M 51-40-02 PAR 7.FIG12; A-TAG # A82274

Part: FRAME ANGLE — CRACKED (BS 500B) · airframe 41,297 hrs · 24,071 cycles

FORWARD CARGO BAY LEFT FORWARD SIDE OF FRAME CRACKED AT BS 500B. R & R THE FRAME ANGLE IAW DWG AND SRM.

Part: WEB — CORRODED (FWD CARGO THRESH) · airframe 41,297 hrs · 24,071 cycles

FORWARD CARGO PIT LOWER SILL WEB STA 440 - 492 RBL 24 - RBL 29 HAS CORROSION ON UPPER AND LOWER SURFACES / BLEND CORROSION ON FWD PIT SILL WEB IAW SRM 53-30-15-1A-1; ORIGINAL THICKNESS .045; .007 MAT'L LOSS WITH .038 REMAINING OUT OF LIMITS VERIFIED NEW SILL WEB IAW 143A8330 ATAG OW0067 P/N 654A0003-58 LOCATED AND DRILLED NEW WEB IAW SRM 51-40-05-06 & BOEING DWG 143A8330 INSTALLED NEW WEB FWD CARGO IAW BOEING DWG 143A8330

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,297 hrs · 24,071 cycles

AFT CARGO BAY "Z" ANGLE CORRODED BETWEEN BS 727C TO BS 787, LBL 25. REPAIRED Z ANGLE IAW SRM.

Part: STIFFENER — CRACKED (RT WING) · airframe 41,297 hrs · 24,071 cycles

RIGHT WING TRAILING EDGE INBOARD OF INBOARD DEFLECTOR RIB UPPER FIXED PANEL MID TRIANGLE SHAPED STIFFENER CRACKED. R & R THE STIFFENER IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 41,297 hrs · 24,071 cycles

RT WING TRAILING EDGE INBOARD OF INBOARD DEFLECTOR RIB VERTICAL INTERCOSTAL ANGLE COMMON TO RIB CRACKED. R&R ANGLE IAW AMM & DWG.

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 41,297 hrs · 24,071 cycles

FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 36 TO RBL 43. R & R THE FLOORBEAM IAW SRM AND EA.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 41,297 hrs · 24,071 cycles

AFT CARGO COMPARTMENT; STA 947.5; AFT BULKHEAD LOWER ATTACH ANGLE RBL 9-14 HAS CORROSION. / REMOVED AND REPLACED AFT BULKHEAD LOWER ATTACH ANGLE AT RBL 9 - 14 DUE TO CORROSION ORIGINAL THICNKESS .090' MATERIAL REMAINING .060' MATERIAL IS OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED + REPLACED IAW SRM 51-40-02-0G-0 + IPC 53-11-51-01

Part: FRAME ANGLE — CRACKED (BS 500C) · airframe 41,297 hrs · 24,071 cycles

FORWARD CARGO BAY LEFT SIDE, FORWARD SIDE OF FRAME ANGLE CRACKED AT BS 500C. R & R THE FRAME ANGLE IAW DWG AND SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,297 hrs · 24,071 cycles

RT KEEL BEAM WEB ANGLE CRACKED AT BS 663. REPAIRED ANGLE IAW EA.

Part: WEB — CORRODED (BS 795-835) · airframe 41,297 hrs · 24,071 cycles

AFT CARGO DOOR THRESHOLD WEB CORRODED BETWEEN BS 795 & 835. REPAIRED THE WEB IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,297 hrs · 24,071 cycles

FORWARD CARGO PIT GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 41,297 hrs · 24,071 cycles

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

Part: ANGLE — CRACKED (BS 500B) · airframe 41,297 hrs · 24,071 cycles

FORWARD CARGO BAY, RT BAFFLE ANGLE ON THE FORWARD SIDE OF FRAME CRACKED AT BS 500B. R & R THE ANGLE IAW DWG & SRM.

Part: ANGLE — CORRODED (BS 500-500C) · airframe 41,297 hrs · 24,071 cycles

FORWARD CARGO BAY LT SIDE ANGLE CORRODED BETWEEN BS 500+5 TO 500C+11, LBL 21. REPAIRED THE ANGLE IAW SRM.

Part: ANGLE — CORRODED (FWD CARGO COMPT) · airframe 41,297 hrs · 24,071 cycles

FORWARD CARGO PIT STA 500D BULKHEAD LOWER ANGLE LBL 24 - RBL 24 HAS CORROSION ON UPPER SURFACE / REMOVED CORROSION AT STA 500D LBL 24 - RBL 24 ON ANGLE ASSY FOUND TO BE 100% OUT OF LIMITS IAW SRM 51-10-02-0G-0 & SRM 53-00-53-1A-2 VERIFIED P/N FOR NEW RAIL ASSY 143A9485-35/7530142 IAW SWA AIPC 53-11-01-43 INSTALLED NEW RAIL ASSY FWD PIT STA 500D LBL 24 - RBL 24 IAW SRM 51-40-02-0G-0 PG 3 STEP B.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 41,297 hrs · 24,071 cycles

AFT CARGO BAY STA767 PLUS 4' FLOOR PANEL SPLICE HAS CORROSION. / REMOVED CORROSION AT AFT CARGO BAY STA 767+4' FLOOR PANEL SPLICE IAW SRM 51-10-02-0G-0 FOUND TO 100% OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED AND REPLACED SPLICE PN: 146A9401-4 IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV A TAG A27911

Part: SHIELD — CORRODED (FWD CARGO THRESH) · airframe 41,297 hrs · 24,071 cycles

FORWARD CARGO PIT DOOR SURROUND AFT SHIELD STA 492 - 500A RBL 23 HAS CORROSION ON UPPER AND LOWER SURFACES / REMOVED CORROSION. EVALUATED DAMAGE AS OUT OF LIMITS. REMOVED SHIELD IAW SRM 51-40-02; SRM 51-40-05; AND DWG 143A0080 REV-

Part: CREASE BEAM — CORRODED (BS 956-992) · airframe 41,297 hrs · 24,071 cycles

AFT GALLEY R2 CUTOUT CREASE BEAM INBOARD CORRODED BETWEEN BS 956 TO 992. R & R THE CREASE BEAM IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,297 hrs · 24,071 cycles

AFT CARGO BAY "Z" ANGLE CORRODED BETWEEN BS 727C TO BS 787, RBL 25. REPAIRED Z ANGLE IAW SRM.

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 41,297 hrs · 24,071 cycles

CARGO TRACK CORRODED AT BS 942, LBL 3. R & R THE CARGO TRACK IAW SRM AND DWG.

Part: FRAME ANGLE — CRACKED (BS 500C) · airframe 41,297 hrs · 24,071 cycles

FORWARD CARGO BAY, LEFT SIDE, AFT OF FRAME ANGLE CRACKED AT BS 500C. R & R THE FRAME ANGLE IAW DWG AND SRM.

Part: CREASE BEAM — CRACKED (BS 302) · airframe 41,297 hrs · 24,071 cycles

L1 DOOR CUTOUT LT CREASE BEAM VERTICAL FLANGE WAS CRACKED AT BS 302. R & R THE CREASE BEAM IAW DWG AND SRM.

Part: WEB — CORRODED (BS 787) · airframe 41,297 hrs · 24,071 cycles

AFT CARGO BAY LONGITUDINAL WEB CORRODED AT BS 787, STRINGER 27R. R & R THE WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (WNG-BDY FAIRING) · airframe 41,297 hrs · 24,071 cycles

RIGHT WING INBOARD LEADING EDGE WING TO BODY FAIRING CURVED ANGLE CRACKED AT BS 500D. REPAIRED THE ANGLE IAW SRM.

Part: PANEL — DELAMINATED (LEFT WING) · airframe 41,297 hrs · 24,071 cycles

LEFT WING LEADING EDGE PANEL 521KB FORWARD EDGE MATING SURFACE HAS EROSION/DELAM AT 3 AREAS (MARKED) / REPAIRED LEFT WING L/E PANEL 521 KB FWD EDGE MATING SURFACE AS MARKED AND REPAIRED ALLUMINIUM FOIL I/A/W SRM 51-70-04-2R-6 REV 62 AND SRM 51-70-14-2R-3 REV 62

Part: LENS — LOOSE (CABIN) · airframe 40,123 hrs · 23,355 cycles

L2 DOOR EXIT LIGHT LENS LOOSE. R&R LIGHT ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 40,116 hrs · 23,349 cycles

LT OVERWING EXIT LIGHT INOP. R&R EXIT LIGHT BATTERY ASSY PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 38,165 hrs · 22,185 cycles

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

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 35,835 hrs · 20,833 cycles

AIR TURN BACK, LOUD BANG ON TAKEOFF, FOLLOWED BY LOUD AIR NOISE IN AIR. ALL OTHER INDICATIONS NORMAL. R & R NR 1 ENG ASSEMBLY IAW MT.

Part: HOUSING — BROKEN (CABIN) · airframe 35,009 hrs · 20,375 cycles

CENTER CABIN OVERWING EXIT LIGHT HOUSING BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,009 hrs · 20,375 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN, CRACKED AT STAB STATION 184.7, 9" FWD OF STAB REAR SPAR. REPAIRED SKIN IAW ACO & EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,009 hrs · 20,375 cycles

LEFT HORIZONTAL STABILIZER LOWER INSPAR SKIN, CRACKED AT STAB STATION 184.7 RIB, FROM REAR SPAR. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,009 hrs · 20,375 cycles

RIGHT HORIZONTAL STABILIZER, LOWER SKIN CRACKED AT STABILIZER STATION 138.7 24" AFT OF LE. REPAIRED SKIN IAW CCO.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,009 hrs · 20,375 cycles

LEFT HORIZONTAL STABILIZER INSPAR SKIN CRACKED AT STAB STATION 138.70 RIB, 17" FROM REAR SPAR. REPAIRED SKIN IAW ACCO.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,009 hrs · 20,375 cycles

RIGHT HORIZONTAL STAB LOWER IN SPAR SKIN CRACKED AT REAR SPAR, BETWEEN STAB STATION 92.7 & 101.9. REPAIRED SKIN IAW CCO.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,009 hrs · 20,375 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN, CRACKED AT STAB STATION 184.7, 9" FWD OF STAB REAR SPAR. REPAIRED SKIN IAW CCO & EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 35,009 hrs · 20,375 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 101.9, HORIZONTAL FLANGE AT AFT SPAR, CRACKED ON OUTBOARD SIDE. REPAIRED RIB IAW EA.

Part: ANGLE — CRACKED (RT HORIZ STAB) · airframe 35,009 hrs · 20,375 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT 2ND VERTICAL STIFFENER FROM AFT SPAR AT STATION 129.5. REPAIRED ANGLE IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 35,009 hrs · 20,375 cycles

LEFT HORIZONTAL STABILIZER STATION 120.30, 3RD RIB AFT CRACKED. REPAIRED RIB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,009 hrs · 20,375 cycles

LONGITUDINAL FLOORBEAM FLOOR SEAT TRACK, CRACKED AT BS 727B, RBL 24. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,009 hrs · 20,375 cycles

LONGITUDINAL FLOORBEAM FLOOR SEAT TRACK, CRACKED AT BS 727B, RBL 45. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,009 hrs · 20,375 cycles

LONGITUDINAL FLOORBEAM FLOOR SEAT TRACK, CRACKED AT BS 727B, LBL 24. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,009 hrs · 20,375 cycles

LONGITUDINAL FLOORBEAM FLOOR SEAT TRACK, CRACKED AT BS 727B, LBL 45. REPAIRED SEAT TRACK IAW EA.

Part: LIGHT — LOOSE (CABIN) · airframe 34,361 hrs · 19,974 cycles

RIGHT OVERWING EXIT LIGHT ASSEMBLY LOOSE. REPAIRED LIGHT ASSEMBLY IAW EA.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 34,069 hrs · 19,788 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING LUG FACE CORRODED. REPAIRED FITTING IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 28,524 hrs · 16,622 cycles

RT FLIGHT DECK WINDOW FRAME CRACKED. REPAIRED FRAME IAW SWA EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,524 hrs · 16,622 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 184.7, 9" FWD OF STAB REAR SPAR. REPAIRED SKIN IAW SRM.

Part: FITTING — CORRODED (L1 DOOR) · airframe 28,524 hrs · 16,622 cycles

L1 DOOR FWD GIRT BAR TIE DOWN FITTING CORRODED AT BS 312, LBL 54. R & R FITTING IAW SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 28,524 hrs · 16,622 cycles

AFT CARGO FLOOR SUPPORT STRAP CORRODED AT BS 772 BETWEEN LBL 8 TO RBL 21. R & R STRAP IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 28,524 hrs · 16,622 cycles

RT VERTICAL PRESS DECK WEB CRACKED AT BS 663, RBL 33. REPAIRED WEB IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,524 hrs · 16,622 cycles

INTERCOSTAL CRACKED BETWEEN BS 294 TO BS 312 RBL 15. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,524 hrs · 16,622 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328 RBL 30. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,524 hrs · 16,622 cycles

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

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 26,167 hrs · 15,245 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.70 2. REPAIRED SKIN PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 24,055 hrs · 14,032 cycles

CENTER EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT IAW AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 24,056 hrs · 14,032 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.7. REPAIRED RIB IAW ER & EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 24,056 hrs · 14,032 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.7 3RD VERT STIFFENER. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 24,056 hrs · 14,032 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT STA 129.50. REPAIRED RIB IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 24,056 hrs · 14,032 cycles

RIGHT HORIZONTAL STABILIZER INSPAR SKIN CRACKED BETWEEN STA 92.70 TO STA 101.90. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 24,056 hrs · 14,032 cycles

LEFT HORIZONTAL STABILIZER INSPAR SKIN CRACKED AT STA 138.70. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 24,056 hrs · 14,032 cycles

LEFT HORIZONTAL STABILIZER INSPAR SKIN CRACKED AT STA 184.70. REPAIRED SKIN IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 24,015 hrs · 14,008 cycles

RIGHT EMERGENCY BATTERY PACK FAILED LONG CHECK. REMOVED AND REPLACED BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 24,015 hrs · 14,008 cycles

LEFT EMERGENCY BATTERY PACK FAILED LONG CHECK. REMOVED AND REPLACED BATTERY PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 23,698 hrs · 13,846 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 22,735 hrs · 13,344 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 22,735 hrs · 13,344 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,404 hrs · 11,981 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERWING EEPLS INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 15,753 hrs · 9,304 cycles

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

Part: FITTING — LOOSE (GIRT BAR) · airframe 15,605 hrs · 9,220 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 15,605 hrs · 9,220 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: LENS — BROKEN (CABIN) · airframe 14,809 hrs · 8,754 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS BROKEN AT ROW 2. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,369 hrs · 8,497 cycles

DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 12,401 hrs · 7,305 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 12,401 hrs · 7,305 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 12,385 hrs · 7,293 cycles

RIGHT AFT EMERGENCY EXIT SIDEWALL SIGN COVER LOOSE. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 9,622 hrs · 5,635 cycles

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

Part: LENS — MISSING (CABIN) · airframe 9,473 hrs · 5,538 cycles

EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,452 hrs · 5,526 cycles

EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 9,425 hrs · 5,515 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 9,297 hrs · 5,443 cycles

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

Part: LENS — MISSING (CABIN) · airframe 9,296 hrs · 5,442 cycles

EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 9,296 hrs · 5,443 cycles

EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 9,215 hrs · 5,387 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STUCK WILL NOT LOCK. CLEANED GIRT BAR PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 7,477 hrs · 4,307 cycles

DURING SCHEDULED HC1 CHECK, FWD LT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 7,477 hrs · 4,307 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 7,477 hrs · 4,307 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 6,744 hrs · 3,861 cycles

EEPLS ASSY LOOSE AT ROW 3 ABC. SECURED EEPLS ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 6,540 hrs · 3,747 cycles

EEPLS ASSY LOOSE AT ROW 1 ABC. SECURED ASSY PER MM.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 5,000 hrs · 2,842 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS END CAP MISSING. INSTALLED END CAP PER MM.

Part: COVER — MISSING (CABIN) · airframe 4,966 hrs · 2,824 cycles

EEPLS COVER MISSING ROW 1 ABC. INSTALLED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 4,923 hrs · 2,795 cycles

EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM.

Part: FITTING — LOOSE (R1 DOOR) · airframe 1,813 hrs · 1,060 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 1,568 hrs · 887 cycles

EEPLS LIGHT COVER LOOSE AT ROW 1 ABC. SECURED EEPLS LIGHT COVER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 400 hrs · 206 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 280 hrs · 141 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.