N206WN

Part: SLIDE — LOOSE (ZONE 800) · airframe 64,727 hrs · 38,569 cycles

FWD ENTRY DOOR SLIDE LOOSE. REATTACHED FWD ENTRY DOOR SLIDE I.A.W. 25-66-01.

Part: ENGINE — FAULTED (NR 2) · airframe 64,514 hrs · 38,438 cycles

AFTER START OF NR 2 ENG; SOURCE OFF LIGHT ILLUMINATED AND FUEL FLOW WENT TO ZERO, HAD WHITE FLASHING BOX AROUND EGT, AND SHUT NR 2 ENG DOWN. C/W EEC BITE IAW FIM 73-00 TASK 801. NO FAULTS FOUND FOR NR 2 ENG. C/W ENG IDLE RUN WITH CREW IAW AMM 71-00-00 RAN ENG FOR 5 MINS ENG RUN SUCCESSFUL WITH NO FAULTS NOTED. ACFT OK FOR SERVICE. WORK ORDER 107675. C/W EEC BITE IAW FIM 73-00 TASK 801. NO FAULTS FOUND FOR NR 2 ENG. C/W ENG IDLE RUN WITH CREW IAW AMM 71-00-00 ; RAN ENG FOR 5 MINS; ENG RUN SUCCESSFUL WITH NO FAULTS NOTED. ACFT OK FOR SERVICE.

Part: HOOK — LOOSE (GIRT BAR) · airframe 64,284 hrs · 38,268 cycles

FWD SERVICE DOOR RT GIRT BAR HOLDER REPORTED LOOSE BY FA. ADJUSTED GIRT BAR HOOK IAW SIP.

Part: GIRT BAR — STUCK (ZONE 800) · airframe 64,202 hrs · 38,216 cycles

CREW REPORTS R1 DOOR GIRT BAR STUCK IN SLIDE PACK.<[01] FREED R1 DOOR GIRT BAR AND CHECKED FIT IN FLOOR FITTINGS. NO ISSUES NOTED REF AMM 25-66-00.

Part: COVER — LOOSE (ZONE 200) · airframe 63,796 hrs · 37,965 cycles

FWD ENTRY EMERG. EXIT LIGHT COVER CAME OFF. REMOVED AND REPLACED FWD ENTRY EMERG. EXIT LIGHT ASSY PER AMM 33-25-00.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 63,708 hrs · 37,905 cycles

AFT ENTRY EMER LIGHT INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-06-960-804-NG.

Part: SIGN — DETACHED (ZONE 200) · airframe 63,693 hrs · 37,898 cycles

EXIT PLACARD CAPT SIDE OVER WING KNEE-LEVEL SIGN FELL OFF. INSTALLED NEW LH SIDE OVERWING EXIT SIGN IAW AMM 33-51-01.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 62,546 hrs · 37,203 cycles

AFT CENTER EMERGENCY EXIT LIGHT INOP<[01] REMOVED AND REPLACED AFT EMERGENCY EXIT LIGHT POWER SUPPLY M1672 REF AMM 33-51-06. OPS TEST GOOD.

Part: RELAY — FAULTED (ZONE 100) · airframe 62,254 hrs · 37,040 cycles

MULTIPLE CAUTION/FAILURE LIGHTS ON TAKEOFF(EMER LIGHTS NOT ARMED;BOTH WING TO BODY OVERHEAT; ALL MCP LIGHTS FLASHING; ENG#1 AND #2 OVERHEAT LIGHTS; ALL IRS LIGHTS; FIRE WARNING FAULT LIGHT; #1 AND #2 MULTIPLE CAUTION/FAILURE LIGHTS ON TAKEOFF (EMER LIGHTS NOT ARMEDBOTH WING TO BODY OVERHEAT ALL MCP LIGHTS FLASHING ENG#1 AND #2 OVERHEAT LIGHTS ALL IRS LIGHTS FIRE WARNING FAULT LIGHT #1 AND #2 SQUIB LIGHTS ON.)<[01] TROUBLESHOT CAUTION AND FAILURE LIGHTS USING WDM 33-18-37/51 AND FOUND R33 RELAY TO BE IN COMMON WITH ALL FAULTED LIGHTS. INSPECTED ALL FAULT AFFECTED LIGHTS FOR ANY FOD/DEBRIS AND WIRING ISSUES WITH NO DEFECTS NOTED. REMOVED AND REPLACED R33 RELAY IAW SWPM 20-81-22. PERFORMED MASTER DIM AND TEST OPERATIONAL TEST IAW AMM 33-18-00. NO DEFECTS NOTED; CAN NO LONGER DUPLICATE ISSUE.

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 61,640 hrs · 36,656 cycles

CRACK LEADING EDGE RIB LOCATED LE STA 151.75 AT LT HORIZONTAL STABILIZER 2024-691873<[01] REPLACED NEW LEADING EDGE RIB AND FASTENERS LOCATED LE STA 151.75 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG#186A1001; SHEET:10; REV:A. SEE INDIVIDUAL SING OFF BELOW;[02] REPLACED NEW LEADING EDGE RIB AND FASTENERS LOCATED LE STA 151.75 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DWG#186A1001; SHEET:10; REV:A. SEE INDIVIDUAL SING OFF BELOW

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 61,640 hrs · 36,656 cycles

CRACK SUPPORT ANGLE LOCATED STA188 TO STA203.8 WEATHER RADAR AREA AT FWD OF NOSE WHEEL WELL 2024-691870<[01] REPLACED SUPPORT ANGLE LOCATED STA188 TO STA203.8 WEATHER RADAR AREA AT FWD OF NOSE WHEEL WELL IAW B737-700 SRM 51-40-02-0G AND DWG 141A9194 SHEET 4 REV D. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED COMPLETE TASK

Part: SUPPORT BRACKET — CRACKED (ZONE 300) · airframe 61,640 hrs · 36,656 cycles

CRACK SUPPORT BRACKET LOCATED FRONT SPAR SUPPORT FITTING RT APROX AT STA 1016 AT VERTICAL STABILIZER 2024-691834<[01] REPLACED SUPPORT BRACKET LOCATED FRONT SPAR SUPPORT FITTING RT APROX AT STA 1016 AT VERTICAL STABILIZER IAW B737 700 SRM 51-40-02-0G AND DWG 176A3101 SHEET 4 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT BRACKET LOCATED FRONT SPAR SUPPORT FITTING RT APROX AT STA 1016 AT VERTICAL STABILIZER IAW B737 700 SRM 51-40-02-0G AND DWG 176A3101 SHEET 4 REV-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 61,640 hrs · 36,656 cycles

CRACK ANGLE LOCATED STA947.5 AND LBL10 AT AFT CARGO COMPARTMENT 2024-691800<[01] REPLACED ANGLE LOCATED STA947.5 AND LBL10 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G AND DWG 149A8103 SHEET 7 REV A.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE LOCATED STA947.5 AND LBL10 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G AND DWG 149A8103 SHEET 7 REV A.SEE INDIVIDUAL SIGN OFF BELOW.

Part: WEB — CORRODED (ZN 100 FUS LOWER) · airframe 61,640 hrs · 36,656 cycles

CORROSION SHIELD WEB LOCATED BETWEEN STA767 TO STA794.3 AND RBL22 WL156 AT AFT CARGO COMPARTMENT 2024-691813<[01] REPLACED SHIELD WEB LOCATED BETWEEN STA767 TO STA794.3 AND RBL22 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G AND DWG 146A0081 SHEET 25 REV A.SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED COMPLETE TASK RII

Part: SUPPORT CHANNEL — CRACKED (ZONE 100) · airframe 61,640 hrs · 36,656 cycles

CRACK CHANNEL SUPPORT LOCATED STA727 AND RBL6 AT AFT CARGO COMPARTMENT REPLACED CHANNEL SUPPORT LOCATED STA727 AND RBL6 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02-0G-0; DWG 144A2600 SHEET 566 REV - AND EVALUATED CHANNEL SUPPORT LOCATED STA727 AND RBL6 AT AFT CARGO COMPARTMENT NO DAMAGE IS ALLOWED AT THESE LOCATONS IAW B737-700 SRM 53-40-08-1A-3 FIG: 102 AND MEASURES OF CRACK IS: L= 0.760? TOOL USED CALIPER P/N: 500-196-30; S/N:A21033522; DUE DATE: 22-DEC-24;[02] CORRECTED STEP 1<BR>REPLACED CHANNEL SUPPORT LOCATED STA727 AND RBL6 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0;SRM 51-10-02 0G-0 ITEM 9;DWG 144A2600 SHEET 566 REV - AND EVALUATED CHANNEL SUPPORT LOCATED STA727 AND RBL6 AT AFT CARGO COMPARTMENT NO DAMAGE IS ALLOWED AT THESE LOCATONS IAW SRM 53-40-08-1A-3 FIG: 102

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 61,640 hrs · 36,656 cycles

CRACK ON SUPPORT ANGLE LOCATED CEILING AREA BTW BS 727A TO BS 727B LBL 52 AT AFT CARGO COMPARTMENT 2024-691801<[01] FABRICATED NEW SUPPORT ANGLE LOCATED CEILING AREA BTW BS 727A TO BS 747 LBL 52 AT AFT CARGO COMPARTMENT IAW B737-700 DWG 149A9A91 SHEET 6 REV-C;[02] CORRECTED STEP 1.FABRICATED NEW SUPPORT ANGLE LOCATED CEILING AREA BTW BS 727A TO BS 747 LBL 52 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 149A9491 SHEET 6 REV-C SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 1.FABRICATED NEW SUPPORT ANGLE LOCATED CEILING AREA BTW BS 727A TO BS 747 LBL 52 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 149A9491 SHEET 6 REV-C SEE INDIVIDUAL SIGN OFF BELOW. AS RII

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 61,640 hrs · 36,656 cycles

CRACK SHIELD WEB BETWEEN BS 492 TO BS 500A LEVEL STRINGER 26R AT FWD CARGO COMPARTMENT 2024-691805<[01] REPLACED NEW SHIELD WEB BETWEEN BS 492 TO BS 500A LEVEL STRINGER 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G AND DWG 143A0080 SHEET 19 REV -. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED NEW SHIELD WEB BETWEEN BS 492 TO BS 500A LEVEL STRINGER 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G AND DWG 143A0080 SHEET 19 REV -. SEE INDIVIDUAL SIGN-OFF BELOW.<BR><BR>RII

Part: SUPPORT — CRACKED (ZONE 100) · airframe 61,640 hrs · 36,656 cycles

CRACK ANGLE - SUPPORT LOCATED STA887 AND RBL56 CEILING AREA AT AFT CARGO COMPARTMENT. REPLACED ANGLE SUPPORT LOCATED STA 887 AND RBL 56 CEILING AREA AT AFT CARGO COMPARTMENT IAW SRM 51-40-02-0G AND DWG 149A9490 SHEET 20 REV -.

Part: ANGLE — CRACKED (ZONE 100) · airframe 61,640 hrs · 36,656 cycles

CRACK ANGLE LOCATED STA867 AND LBL10 AT AFT CARGO COMPARTMENT 2024-691806<[01] REPLACED ANGLE LOCATED STA867 AND LBL 10 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8102; SHEET 17; REV -.;[02] CORRECTED STEP 1.<BR>REPLACED ANGLE LOCATED STA867 AND LBL 10 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 149A8102; SHEET 17; REV -.;[03] REPLACED ANGLE LOCATED STA867 AND LBL 10 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 149A8102; SHEET 17; REV -.

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 61,640 hrs · 36,656 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN STA927 TO STA947.5 AND RBL21 AT AFT CARGO COMPARTMENT 2024-691802<[01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN STA927 TO STA947.5 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 147A7500 SHEET 18 REV -.SEE INDIVIDUAL SIGN OFF BELLOW;[02] CORRECTED STEP 1: REPLACED WEB - INTERCOSTAL LOCATED BETWEEN STA927 TO STA947.5 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 147A7500 SHEET 18; 19 AND 20 REV -.SEE INDIVIDUAL SIGN OFF BELLOW;[03] CORRECTIVE ACTION STEP 2 CERTIFIED

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 61,640 hrs · 36,656 cycles

CRACK SUPPORT ANGLE ON FRAME BS 867 BETWEEN STRINGER 2R TO STRINGER 3R AT PASSENGER CABIN 2024-691797<[01] REMOVED AND REINSTALLED NEW SUPPORT ANGLE AND APPLIED PROTECTIVE TREATMENT ON FRAME BS 867 BETWEEN STRINGER 2R TO STRINGER 3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; SRM 51-20-01 AND DWG 146A7901 SHEET 58 REV - MEASURE OF CRACK ARE: L:0.160 TOOL USED CALIPER P/N: 500-196-30; S/N:B23353457; DUE DATE: 09-MAR-25;[02] REMOVED AND REINSTALLED NEW SUPPORT ANGLE AND APPLIED PROTECTIVE TREATMENT ON FRAME BS 867 BETWEEN STRINGER 2R TO STRINGER 3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; SRM 51-20-01 AND DWG 146A7901 SHEET 58 REV - MEASURE OF CRACK ARE: L:0.160 TOOL USED CALIPER P/N: 500-196-30; S/N:B23353457; DUE DATE: 09-MAR-25. JOB COMPLETED.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 61,640 hrs · 36,656 cycles

CRACK ON SUPPORT ANGLE LOCATED CEILING AREA BS 927 RBL 36 AT AFT CARGO COMPARTMENT 2024-691803 CRACK ON SUPPORT ANGLE LOCATED CEILING AREA BS 927 RBL 46 AT AFT CARGO COMPARTMENT<[01] REPLACED SUPPORT ANGLE LOCATED CEILING AREA BS 927 RBL 36 AT AFT CARGO COMPARTMENT IAW B737 700 51-40-02-0G AND DWG 149A9490 SHEET 23 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1.<BR>REPLACED SUPPORT ANGLE LOCATED CEILING AREA BS 927 RBL 36 AT AFT CARGO COMPARTMENT IAW B737 700 51-40-02-0G; DWG 149A9490 SHEET 23 REV A AND DWG 149A8110 SHEET 13 REV B. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED SUPPORT ANGLE LOCATED CEILING AREA BS 927 RBL 36 AT AFT CARGO COMPARTMENT IAW B737 700 51-40-02-0G; DWG 149A9490 SHEET 23 REV A AND DWG 149A8110 SHEET 13 REV B. SEE INDIVIDUAL SIGN OFF BELOW

Part: ANGLE — CRACKED (ZONE 100) · airframe 61,640 hrs · 36,656 cycles

CRACK ANGLE - CLIP ON FWD FACE FRAME BS 500B AND STRINGER 26L FWD CARGO COMPARTMENT 2024-691772<[01] REPLACED ANGLE - CLIP ON FWD FACE FRAME BS 500B AND STRINGER 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG 143A7505 SHEET 5 REV-. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE - CLIP ON FWD FACE FRAME BS 500B AND STRINGER 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 DWG 143A7505 SHEET 5 REV-. SEE INDIVIDUAL SIGN OFF BELOW

Part: ANGLE — CRACKED (ZONE 100) · airframe 61,640 hrs · 36,656 cycles

CRACK ANGLE - CLIP ON AFT FACE FRAME BS 500B AND STRINGER 26L FWD CARGO COMPARTMENT 2024-691773<[01] REPLACED ANGLE - CLIP ON AFT FACE FRAME BS 500B AND STRINGER 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7502 SHEET 37 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE - CLIP ON AFT FACE FRAME BS 500B AND STRINGER 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7502 SHEET 37 REV-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 61,640 hrs · 36,656 cycles

CRACK SUPPORT ANGLE BS 663.75 AND LBL 42 WL 170 AT CENTER SECTION 2024-691733<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 9;[02] PERFORMED PERMANENT REPAIR ON BS 663.75 AND LBL 42 WL 170 AT CENTER SECTION IN ACCORDANCE WITH B737-700 SRM 57-10-10-2R-5 REPAIR 5.SEE INDIVIDUAL SING OFF BELOW;[03] CORRECTED STEP 2: PERFORMED PERMANENT REPAIR ON BS 663.75 AND LBL 42 WL 170 AT CENTER SECTION IN ACCORDANCE WITH B737-700 SRM 57-10-10-2R-5 REPAIR 5.SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR ON BS 663.75 AND LBL 42 WL 170 AT CENTER SECTION IN ACCORDANCE WITH B737-700 SRM 57-10-10-2R-5 REPAIR 5.SEE INDIVIDUAL SIGN OFF BELOW.<BR>AS RII

Part: STRINGER — CRACKED (ZN 500 LEFT WING) · airframe 61,640 hrs · 36,656 cycles

CRACK STRINGER 8 INTERNAL AREA FUEL TANK LOC. BTW RIB 19 AND RIB 20 UPPER SKIN LOWER SURFACE AFT AREA AT LT WING 2024-691730<[01] TOOL USED ON STEP 2: EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:200048001; DUE DATE:28-MAY-25;[02] REPAIRED STRINGER 8 INTERNAL AREA FUEL TANK LOCATED BETWEEN RIB 19 AND RIB 20 UPPER SKI LOWER SURFACE AFT AREA AT LT WING IN ACCORDANCE WITH EA 24-157-03169-WIP1 AND EA 24-157-03169 SUMMARY; SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPAIRED STRINGER 8 INTERNAL AREA FUEL TANK LOCATED BETWEEN RIB 19 AND RIB 20 UPPER SKI LOWER SURFACE AFT AREA AT LT WING IN ACCORDANCE WITH EA 24-157-03169-WIP1 AND EA 24-157-03169 SUMMARY; SEE INDIVIDUAL SIGN OFF BELOW. JOB COMPLETED. CERTIFIED AS RII.

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 61,640 hrs · 36,656 cycles

EMERGENCY EXIT LIGHT LOCATED BTW STA 639 AND STA 663.75 EXTERIOR FUSELAGE LT SIDE FAILS TEST IAW STEP 60 PER SWA TASK TTG8Q00WCEC4. 2024-691718<[01] REPLACED EMERGENCY POWER SUPPLY BATTERY PACK AT STA 603 M1668 UPPER FUSELAGE I.A.W. B737-700 33-51-06-960-805 THEN PERFORMED EMERGENCY LIGHT TEST AND TEST IS OK. SEE INDIVIDUAL SIGN OFF STEP BELOW;[02] REPLACED EMERGENCY POWER SUPPLY BATTERY PACK AT STA 603 M1668 UPPER FUSELAGE I.A.W. B737-700 33-51-06-960-805 THEN PERFORMED EMERGENCY LIGHT TEST AND TEST IS OK. SEE INDIVIDUAL SIGN OFF STEP BELOW

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 61,640 hrs · 36,656 cycles

DO NOT TURN ON POSITION EMERGENCY EXIT LIGHT LOCATED DOORWAY HEATER PANEL AFT ENTRY 2024-691723<[01] REPLACED BATTERY PACK ON POSITION EMERGENCY EXIT LIGHT LOCATED DOORWAY HEATER PANEL AFT ENTRY I.A.W B737-700 AMM 33-51-06-960-805.TEST IS OK.SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED BATTERY PACK ON POSITION EMERGENCY EXIT LIGHT LOCATED DOORWAY HEATER PANEL AFT ENTRY I.A.W B737-700 AMM 33-51-06-960-805.TEST IS OK.SEE INDIVIDUAL SIGN OFFS BELOW.

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 61,640 hrs · 36,656 cycles

DO NOT TURN ON POSITION EMERGENCY EXIT LIGHT LOCATE DOORWAY HEATER PANEL FWD SERVICE GALLEY DOOR 2024-691722<[01] REPLACED EMERGENCY POWER SUPPLY BATTERY PACK AT STA 322 M1674 UPPER FUSELAGE I.A.W. B737-700 33-51-06-960-805 THEN PERFORMED EMERGENCY LIGHT TEST AND TEST IS OK. SEE INDIVIDUAL SIGN OFF STEP BELOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: BATTERY PACK — FAILED (ZN 200 FUS TOP) · airframe 61,640 hrs · 36,656 cycles

EMERGENCY EXIT LIGHT LOCATED BTW STA 344 AND STA 360 STR 14L AND STR 15L EXTERIOR FUSELAGE FAILS TEST IAW STEP 60 PER SWA TASK TTG8Q00WCEC4. 2024-691714<[01] CLOSED THE ACCESS PANEL IN THE FWD LOWERED CEILING PANEL IAW B737-700 AMM:33-51-06-960-805 STEP 4.F.(1) AND (4);[02] CORRECTED STEP 1 ENTER IN ERROR;[03] REPLACED EMERGENCY POWER SUPPLY BATTERY PACK AT STA 322 M1675 UPPER FUSELAGE I.A.W. B737-700 33-51-06-960-805 THEN PERFORMED EMERGENCY LIGHT TEST AND TEST IS OK. SEE INDIVIDUAL SIGN OFF STEP BELOW;[04] REPLACED EMERGENCY POWER SUPPLY BATTERY PACK AT STA 322 M1675 UPPER FUSELAGE I.A.W. B737-700 33-51-06-960-805 THEN PERFORMED EMERGENCY LIGHT TEST AND TEST IS OK. SEE INDIVIDUAL SIGN OFF STEP BELOW

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 61,640 hrs · 36,656 cycles

EMERGENCY EXIT LIGHT LOCATED BTW STA 986.5 AND STA 1006 STR 13R EXTERIOR FUSELAGE FAILS TEST STEP 60 PER SWA TASK TTG8Q00WCEC4. 2024-691720<[01] REPLACED BATTERY PACK LOCATED BTW STA 986.5 AND STA 1006 STR 13R I.A.W B737-700 AMM 33-51-06-960-805.TEST IS OK. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED BATTERY PACK LOCATED BTW STA 986.5 AND STA 1006 STR 13R I.A.W B737-700 AMM 33-51-06-960-805.TEST IS OK.<BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ACCESS PANEL — WORN (ZONE 100) · airframe 61,640 hrs · 36,656 cycles

WEAR PLATE ON ACCESS PANEL 192CR OF BODY FAIRING AT LOWER FUSELAGE 2024-691628<[01] REPLACED PLATE ON ACCESS PANEL 192CR OF BODY FAIRING AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02-0G-0; SRM 51-40-04 AND DWG 14947231 SHEET 20 REV A AND MEASURES OF WEAR IS: D: 0.040? <BR><BR>APPLIED TORQUE 22.5 INCH.LB<BR>TOOL USED: TORQUE P/N: QD1R50; S/N: 0716079441 ; DUE DATE: 12-OCT-25<BR><BR>DIGITAL CALIPER P/N: 2340A11; S/N: B17119057; DUE DATE: 17-OCT-25.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 61,640 hrs · 36,656 cycles

CRACK SERVICE DOOR SCUFF PLATE AT FWD GALLEY AREA 2024-691627<[01] TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A23272235; DUE DATE: 03-JAN-25.;[02] TOOL USED ON STEP 4 RADIOMETER P/N XRP-3000 S/N 1998072 DUE DATE 23-JAN-25;[03] REPAIRED CENTER SCUFF PLATE OF SERVICE DOOR AT FWD GALLEY AREA I. A. W. BOEING 737-700 SRM TASK 53-10-15-2R-2; REPAIR 2; PARAGRAPH 4. B; STEPS (3) TO (6) AND (8); FIGURE 203 AND BAC 5975. SEE INDIVIDUAL SIGNOFF BELOW.;[04] TASK COMPLETED.

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 61,640 hrs · 36,656 cycles

CRACK SUPPORT ANGLE LOCATED STA695 AND BL0 CENTER SECTION 2024-691555<[01] REPLACED SUPPORT ANGLE LOCATED STA695 AND BL0 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV A. AND DWG 273A9112 SHEET 27; REV- SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 61,640 hrs · 36,656 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND BL0 CENTER SECTION 2024-691553<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N 386115K71 S/N AE-40585 DUE DATE 26 JUL 25.;[02] INSTALLED NEW ANGLE FLOOR STRUCTURE LOCATED STA695 AND BL0 CENTER SECTION IAW B737-700 SRM 51-40-02-0G-0 AND DWG 273A9110 SHEET 202 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[03] INSTALLED NEW ANGLE FLOOR STRUCTURE LOCATED STA695 AND BL0 CENTER SECTION IAW B737-700 SRM 51-40-02-0G-0 AND DWG 273A9110 SHEET 202 REV - SEE INDIVIDUAL SIGN OFF BELOW. CERTIFIED AS RII.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 61,640 hrs · 36,656 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-691587<[01] TOOL USED: DIGITAL CALIPER P/N: 500-196-30 S/N: A23048253 DUE DATE: 05-JUN-25.;[02] TOOL USED ON STEP 4 RADIOMETER P/N XRP-3000 S/N 1753759 DUE DATE 07- DEC-24;[03] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDING WITH BOEING 737-700 SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) AND (4) TO (7); REFER TO BAC 5975. SEE INDIVIDUAL SIGNOFF BELOW.;[04] JOB TASK COMPLETED.

Part: ANGLE — CRACKED (ZONE 100) · airframe 61,640 hrs · 36,656 cycles

CRACK GUSSET LOCATE STA 500D AT LEVEL STR 19L FWD CARGO COMPARTMENT 2024-691496<[01] REPLACED GUSSET ANGLE LOCATE STA 500D AT LEVEL STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 174 REV - . SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED GUSSET ANGLE LOCATE STA 500D AT LEVEL STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 174 REV - . SEE INDIVIDUAL SIGN OFF BELOW. CERTIFIED AS RII.

Part: SKIN — CRACKED (ZN 500 LEFT WING) · airframe 61,640 hrs · 36,656 cycles

CRACK LOWER SURFACE OF LEADING EDGE SLAT 3 NOSE SKIN AT ACTUATOR LOC. AROUND FASTENER AT LT WING 2024-691459<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 11-MAR-25;[02] PERFORMED REPAIR PART [1]DOUBLER [2]FILLER AND FASTENERS AT LOWER SURFACE OF LEADING EDGE SLAT 3 NOSE SKIN LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-40-05; B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1 FIGURE 202 SHEET 3.SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2.<BR>PERFORMED PERMANENT REPAIR LOC ON LOWER SURFACE OF LEADING EDGE SLAT 3 NOSE SKIN LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-40-05; B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1 FIGURE 202 SHEET 3.SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR LOC ON LOWER SURFACE OF LEADING EDGE SLAT 3 NOSE SKIN LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-40-05; B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1 FIGURE 202 SHEET 3.SEE INDIVIDUAL SIGN OFF BELOW.;[05] CERTIFIED COMPLETE TASK

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 61,398 hrs · 36,514 cycles

RAMP REPORTS AFT CARGO FLOOR PANEL HAS A CRACK<[01] OK TO CONTINUE PER <BR>MEL 25-16-01. SP1B MDDR# 207033;[02] REMOVED AND REPLACED AFT CARGO PIT FLOOR BOARD PER MM 25-52-01

Part: SEAT BACK — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 58,221 hrs · 34,535 cycles

ROW 12 DEF SEAT BACKS WILL NOT STAY UPRIGHT<[01] TIGHTENED AT HINGE ASSY BOLTS AT ROW 12DEF IAW AMM 25-22-00

Part: ENCLOSURE — CRACKED (DOOR SLIDE) · airframe 58,041 hrs · 34,431 cycles

AFT ENTRY DOOR FWD ISOLATOR CRACKED<[01] R&R AFT ENTRY DOOR FWD EMER. SLIDE ISOLATOR IAW AMM 52-13-31.

Part: HANDLE — BROKEN (ZN 800 DOOR) · airframe 56,638 hrs · 33,530 cycles

FORWARD SERVICE DOOR ASSIST HANDLE BROKEN<[01] INSTALLED NEW SERVICE DOOR ASSIST HANDLE NUT PER MM 52-41-31

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,205 hrs · 33,238 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1669 FOR RH EMERGENCY EXIT AND AISLE LIGHTS FAILED CAPACITY CHECK<[01] REMOVED AND REPLACED M1669 BATTERY PACK FOR THE RH EMERGENCY EXIT AND AISLE LIGHTS PER 33-51-06

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 55,781 hrs · 32,970 cycles

INOP EMERGENCY EXIT LIGHT EXTERIOR AFT POSITION RH AT TAIL CONE (1 EA) 2022-639066 / [01] PERFORMED TROUBLESHOOTING ON INOP EMERGENCY EXIT LIGHT EXTERIOR AFT POSITION RH AT TAIL CONE I.A.W B737-700 FIM 33-50 TASK 801 STEP 801.A THRU 801.E(1) AND FOUND WIRING W4142-0451-18 TO GROUND GD3810-DC AND INSTALLED CORRECTLY PIN IAW B737-700 WDM 33-51-14 AND SWPM 20-90-15.SEE INDIVIDUAL SIGNOFFS BELOW.;[02] PERFORMED TROUBLESHOOTING ON INOP EMERGENCY EXIT LIGHT EXTERIOR AFT POSITION RH AT TAIL CONE I.A.W B737-700 FIM 33-50 TASK 801 STEP 801.A THRU 801.E(1) AND FOUND WIRING W4142-0451-18 TO GROUND GD3810-DC AND INSTALLED CORRECTLY PIN IAW B737-700 WDM 33-51-14 AND SWPM 20-90-15.SEE INDIVIDUAL SIGNOFFS BELOW. COMPLETED

Part: ACCESS PANEL — CRACKED (FWD CARGO) · airframe 55,781 hrs · 32,970 cycles

CRACKED ACCESS PANEL 123YCC IN THE FWD CARGO BAY. FABRICATED A NEW CEILING PANEL 123YCC IAW AMM 25-52-01-201-801, AND DRAWING 453A1210, REV M.

Part: ANGLE — CRACKED (BS 460 S28R) · airframe 55,781 hrs · 32,970 cycles

CRACKED ANGLE, BS460, S28R IN THE FWD CARGO BAY. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A8131, SHEET 2, REV-.

Part: FILLER — CORRODED (BS 480 S28L-R) · airframe 55,781 hrs · 32,970 cycles

CORROSION FILLER ON EXISTING REPAIR LOCATED BS 480 AND BETWEEN STR28L TO STR28R AT WL 148.5 AT FWD CARGO COMPARTMENT.REMOVED AND REPLACED EXSISTING REPAIR LOCATED BS440 TO BS500 AND BETWEEN STR28L TO STR28R AT WL 148.5 AT FWD CARGO COMPARTMENT I.A.W EA 22-153-03583-WIP1 AND EA 22-153-03583 SUMMARY. SEE INDIVIDUAL STEP SIGNOFFS BELLOW;[04] CORRECTED STEP 3. REMOVED AND REPLACED EXSISTING REPAIR LOCATED BS440 TO BS500 AND BETWEEN STR27L TO STR27R AT WL 148.5 AT FWD CARGO COMPARTMENT I.A.W EA 22-153-03583-WIP1 AND EA 22-153-03583 SUMMARY. CERTIFIED RII MAJOR REPAIR PERFORMED.

Part: ACCESS PANEL — CRACKED (FWD CARGO BAY) · airframe 55,781 hrs · 32,970 cycles

CRACKED ACCESS PANEL 123YAC IN THE FWD CARGO BAY. FABRICATED A NEW CEILING ACCESS PANEL IAW AMM 25-52-01-201-801, AND DRAWING 453A1210-12, REV M.

Part: SUPPORT ANGLE — ELONGATED (BS 500D S26L-R) · airframe 55,781 hrs · 32,970 cycles

ELONGATED HOLE, ON SUPPORT ANGLE, BS 500D, S26L - S26R, IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902-162, REV -.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 55,781 hrs · 32,970 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975 .

Part: PLATE — CRACKED (LT WING) · airframe 55,781 hrs · 32,970 cycles

CRACK ON CORRUGATE PLATE LOCATED AT LEVEL ORSS 244 TRAILING EDGE LT WING 2022-638928 / [01] REPLACED CORRUGATE PLATE LOC. AT LEVEL ORSS244 TRAILING EDGE LT WING I.A.W. B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 30 REV. A DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700 57-51-02 CRACK LENGTH 0.792? TOOL USED CALIPER P/N: 500-193-30 S/N: 0039394 DUE DATE: 02-OCT-23. <BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED CORRUGATE PLATE LOC. AT LEVEL ORSS244 TRAILING EDGE LT WING I.A.W. B737-700 SRM 51-40-02 AND DWG 115A2001 SHEET 30 REV. A DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700 57-51-02 CRACK LENGTH 0.792? TOOL USED CALIPER P/N: 500-193-30 S/N: 0039394 DUE DATE: 02-OCT-23. <BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: PLATE — CRACKED (RT WING) · airframe 55,781 hrs · 32,970 cycles

CRACK ON CORRUGATE PLATE LOCATED AT LEVEL ORSS 244 TRAILING EDGE AT RT WING 2022-638949 / [01] REPLACED CORRUGATE PLATE LOCATED AT LEVEL ORSS 244 TRAILING EDGE AT RT WING AND FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 115A2001 REV. A. DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM. IAW B737-700 SRM-57-51-02 CRACK LENGTH IS 0.766? TOOL USED. CALIPER P/N: 500-197-30; S/N: A18109027; DUE DATE 24/JUN/23. SEE INDIVIDUAL SIGNOFFS BELOW;[02] TASK CARD COMPLETED

Part: RAIL — WORN (AFT CARGO) · airframe 55,781 hrs · 32,970 cycles

WEAR ON BILGE AREA RAIL LOC BS787 PLUS 8 INCH AND RBL8.10 AT AFT CARGO COMPARTMENT. PERFORMED REPAIR ON BILGE AREA LOC.ON BS787 PLUS 8 INCH AND RBL 8.10 AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM SRM 53-00-53-2R-2 REPAIR 2. <BR>SEE INDIVIDUAL SIGN-OFF BELOW;[04] PERFORMED REPAIR IAW SRM SRM 53-00-53-2R-2, REPAIR 2.

Part: PLATE — CRACKED (RT WING) · airframe 55,781 hrs · 32,970 cycles

CRACK ON CORRUGATE PLATE LOCATED AT LEVEL ORSS 261 TRAILING EDGE AT RT WING 2022-638948 / [01] REPLACED CORRUGATE PLATE LOCATED AT LEVEL ORSS 261 TRAILING EDGE AT RT WING I.A.W B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700 57-53-02 CRACK LENGTH L= 0.418 INCH TOOL USED: DIGITAL CALIPER P/N:DIGITAL150 S/N: 76210621217 DUE DATE: FEB-15-2023;[02] REPLACED CORRUGATE PLATE LOCATED AT LEVEL ORSS 261 TRAILING EDGE AT RT WING I.A.W B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700 57-53-02 CRACK LENGTH L= 0.418 INCH TOOL USED: DIGITAL CALIPER P/N:DIGITAL150 S/N: 76210621217 DUE DATE: FEB-15-2023

Part: SUPPORT BRACKET — BROKEN (LT WING) · airframe 55,781 hrs · 32,970 cycles

BROKEN SUPPORT BRACKET LOWER AFT STRUT BOX OUTBOARD SIDE ON ENGINE 1. REPLACED THE SUPPORT BRACKET IAW SRM 51-40-05 AND DWG 311A2683. REV -.

Part: TRAY — CRACKED (CABIN SEAT) · airframe 55,781 hrs · 32,970 cycles

CRACKED EMERGENCY EXIT SEAT FOODTRAY TABLE LATCH. FAULT WILL BE FIXED IAW TTG8Q00G4A95.

Part: TRAY — CRACKED (SEAT 11B) · airframe 55,781 hrs · 32,970 cycles

CRACK EMERGENCY EXIT SEAT FOODTRAY TABLE LATCH ON SEAT 11B. REPLACED THE SEAT FOODTRAY TABLE LATCH IAW CMM 25-21-42, REV 5, PAGE 10022, ITEM 10B, FIGURE 8.

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 55,781 hrs · 32,970 cycles

CRACK BS 540 LT SIDE BRACKET AT AIR CONDITIONING BAY. REPLACED THE BRACKET IAW SRM 51-40-02 AND 51-10-02 ITEM 9.

Part: BATTERY — DISCHARGED (MEGAPHONE) · airframe 55,781 hrs · 32,970 cycles

WORN OUT MEGAPHONE BATTERY IN THE AFT GALLEY. REPLACED THE MEGAPHONE BATTERY IAW AMM 25-64-00-900-804.

Part: BATTERY — DISCHARGED (MEGAPHONE) · airframe 55,781 hrs · 32,970 cycles

WORN OUT MEGAPHONE BATTERY IN FWD GALLEY. REPLACED THE MEGAPHONE BATTERY IAW AMM 25-64-00-900-804,

Part: ANGLE — CRACKED (BS 663) · airframe 55,781 hrs · 32,970 cycles

CRACK BS 663.75 RBL 41 AND WL 171 ANGLE AT AIR CONDITIONING BAY. REPLACED ANGLE IAW SRM 51-40-02, SRM 51-10-02 ITEM 9 AND DWG 111A1000 REV -.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 55,781 hrs · 32,970 cycles

ELONGATED HOLE ON FLOOR PANEL 120BF IN THE FWD CARGO BAY. FABRICATED A NEW FLOOR PANEL IAW SRM 51-40-05, SRM 51-20-01, AND DWG 453A1610, SHEET 7, REV C.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 55,781 hrs · 32,970 cycles

ELONGATED HOLE ON FLOOR PANEL 120AF IN THE FWD CARGO BAY. FABRICATED A NEW FLOOR PANEL IAW AMM 25-52-01-201-801, DWG 453A1610, SHEET 9, REV F.

Part: FLOOR PANEL — DAMAGED (FWD CARGO BAY) · airframe 55,781 hrs · 32,970 cycles

ELONGATED HOLE ON FLOOR PANEL 120CF IN THE FWD CARGO BAY. FABRICATED A NEW FLOOR PANEL IAW SRM 51-40-05, SRM 51-20-01, AND DWG 453A1610, SHEET 23, REV C.

Part: INTERCOSTAL — CRACKED (BS 847-867 LBL25) · airframe 55,781 hrs · 32,970 cycles

CRACKED INTERCOSTAL LOCATED BS 847 TO BS 867 UPPER POSITION AT LEVEL LBL 24.75 AFT CARGO COMPARTMENT. REPLACED WEB-INTERCOSTAL IAW SRM 51-40-02 AND SRM 51-10-02, ITEM 9, AND DWG 149A8100, SHEET 1, REV-.

Part: SUPPORT FITTING — DAMAGED (BS 1016 BL0) · airframe 55,781 hrs · 32,970 cycles

ELONGATED HOLES ON SUPPORT FITTING LOCATED ON BS 1016 BL 0. REPLACED THE SUPPORT FITTING IAW SRM 51-10-02, AND 51-40-02.

Part: BRACKET — CORRODED (ZN 600 RIGHT WIN) · airframe 55,781 hrs · 32,970 cycles

CORROSION WEB LOCATED OUTBOARD LEADING EDGE OFSS396 AT RT WING 2022-638857 / [01] REPLACED BRACKET ASSY OF FUEL QTY INDICATORS IAW B737-700 AMM 28-41-61-401-NG AND PERFORMED OPERATIONAL TEST OF FUEL QTY INDICATORS.TEST IS OK<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 55,781 hrs · 32,970 cycles

CRACKED SURGE TANK ACCESS DOOR 633BB ON DUCT, RT WING. REPLACED THE ACCESS PANEL IAW AMM 28-13-31-400-801.

Part: BRACKET — CRACKED (BS 460 S10L) · airframe 55,781 hrs · 32,970 cycles

CRACK UPPER BRACKET, STRINGER 10L, BS 460. REPLACED THE BRACKET IAW SRM 51-40-02, AND 51-10-02, ITEM 9.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 55,781 hrs · 32,970 cycles

CRACK INDICATION FOUND ON LT HORIZONTAL STAB LOWER IN-SPAR SKIN AT HSS 193.90, RIB, 25 INCH FROM FRONT SPAR. CRACK LENGTH 0.750 INCH. PERFORMED REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT HSS 193.90 RIB; 25.00 INCH FROM FRONT SPAR; INBD SIDE OF RIB IAW EA 22-155-03506 WIP1 AND EA COVER 22-155-03506.

Part: FLOOR SUPPORT — CRACKED (BS 294-312 RBL15) · airframe 55,781 hrs · 32,970 cycles

CRACKED FLOOR SUPPORT, BETWEEN BS 294.5 - 312, RBL 15 IN THE FWD GALLEY. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A5400 REV A.

Part: STRUCTURE — CORRODED (BS 947-986) · airframe 55,781 hrs · 32,970 cycles

CORROSION INNER STRUCTURE BETWEEN BS 947.5 - 986.5, RBL 51, WL 208.1 IN THE AFT GALLEY. REPLACED THE INNER STRUCTURE AND FASTENERS IAW SRM 51-40-02-0G-0, SRM-51-10-02, ITEM 9, AND DWG 147A8501, SHEET 93 REV A. 147A0060 SHEET 64 REV- AND DWG 147A0000, SHEET 45 REV-A.

Part: FLOOR SUPPORT — CRACKED (BS 328-344 LBL46) · airframe 55,781 hrs · 32,970 cycles

CRACKED FLOOR STRUCTUREBETWEEN BS 328 - 344, LBL 46. FWD GALLEY. REPLACED IAW 51-10-02, ITEM 9, AND SRM 51-40-02.

Part: STRAP — CORRODED (BS 1016) · airframe 55,781 hrs · 32,970 cycles

CORROSION STRAP BS 1016 RBL 3 WL 208.1 AT AFT GALLEY AREA 2022-638762 / [01] REPLACED STRAP BS 1016 RBL 3 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DRAWING# 147A5730 SHEET 23 REV. C. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED STRAP BS 1016 RBL 3 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DRAWING# 147A5730 SHEET 23 REV. C. Ï¿½TEM RII SEE INDIVIDUAL SIGN-OFF BELOW

Part: WEB — CORRODED (BS 1016 LBL 17) · airframe 55,781 hrs · 32,970 cycles

CORRODED WEB, BS 1016 + 13, LBL 17, WL 208.1, IN THE AFT GALLEY. EDDY CURRENT INSPECTION COMPLIED WITH. REPLACED THE WEB IAW SRM 51-40-02, AND DWG 147A5600 REV B.

Part: LIGHT — DETERIORATED (ZN 200 FUS TOP) · airframe 55,781 hrs · 32,970 cycles

DETERIORATED PHOTOLUMINESCENT FLOOR LIGHT. REPLACED FLOOR LIGHT IAW DWG 33500007, REV 2, AND SOPM 20-50-12, REV 55.

Part: FLOOR SUPPORT — CRACKED (BS 277-294 BL 0) · airframe 55,781 hrs · 32,970 cycles

CRACKED FLOOR SUPPORT BETWEEN BS 277 - 294.5 BL 0, IN THE FWD GALLEY. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02, ITEM 9, AND DRAWING 141A5400 REV -.

Part: FLOORBEAM — CORRODED (BS 986 LBL 43) · airframe 55,781 hrs · 32,970 cycles

CORROSION FLOOR EAM BS 986.5 LBL 43; WL 208.1 AT AFT GALLEY AREA 2022-638753 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N: 130060401 DUE DATE: 26-JAN-23;[02] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X11290U021704 DUE DATE 01-FEB-23.;[03] REPAIRED FLOOR BEAM BS 986.5 LBL 43; WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM-53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4 FIG. 205 SEE INDIVIDUAL SIGN-OFF BELOW;[04] CERTIFIED RII MAJOR REPAIR PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FLOOR SUPPORT — CRACKED (BS 344-366) · airframe 55,781 hrs · 32,970 cycles

CRACKED INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 TO BS 366 LBL 12 AT FWD GALLEY AREA. REPLACED WITH A NEW INTERCOSTAL AND FASTENERS. LOCATED AT FLOOR STRUCTURE BTW BS344 TO BS360 AND LBL12 IAW SRM 51-40-02 AND DWG 141A5400, REV A.

Part: FLOOR SUPPORT — CRACKED (BS 312-328 LBL46) · airframe 55,781 hrs · 32,970 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 TO BS 328 LBL 46 AT FWD GALLEY. REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE IAW SRM 51-40-02, AND DWG 141A5400, REV -.

Part: FLOOR SUPPORT — CRACKED (BS 344-366 BL0) · airframe 55,781 hrs · 32,970 cycles

CRACKED INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 344 TO BS 366 BL 0. REPLACED THE INTERCOSTAL FLOOR STRUCTURE AND FASTENERS LOCATED BETWEEN BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW SRM 51-40-02, AND DWG 141A5400, SHEET 32, REV-.

Part: FLOORBEAM — CORRODED (BS 986 RGL 43) · airframe 55,781 hrs · 32,970 cycles

CORRODED FLOORBEAM, BS 986.5, RBL 43, WL 208.1, IN THE AFT GALLEY. REPAIRED THE FLOORBEAM IAW SRM-53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4, FIG. 205.

Part: STRAP — CORRODED (BS 1016) · airframe 55,781 hrs · 32,970 cycles

CORROSION STRAP BS 1016 PLUS 13 INCH RBL 18 WL 208.1 AT AFT GALLEY AREA 2022-638763 / [01] REPLACED STRAP BS 1016 PLUS 13 INCH RBL 18 WL 208.1 AT AFT GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 147A5730 SHEET 23 REV. C. SEE INDIVIDUAL SING-OFF BELOW;[02] REPLACED STRAP BS 1016 PLUS 13 INCH RBL 18 WL 208.1 AT AFT GALLEY AREA AND FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 147A5730 SHEET 23 REV. C. Ï¿½TEM RII SEE INDIVIDUAL SING-OFF BELOW

Part: FLOOR SUPPORT — CRACKED (BS 312-328 RLB13) · airframe 55,781 hrs · 32,970 cycles

CRACKED FLOOR SUPPORT, BETWEEN BS 312 - 328, RBL 13. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 141A5400, REV- .

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 55,781 hrs · 32,970 cycles

CRACK ON HOLES LOCATED ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: STRAP — CORRODED (BS 1016) · airframe 55,781 hrs · 32,970 cycles

CORROSION STRAP BS 1016 PLUS 8 INCH LBL 3; WL 208.1 AT AFT GALLEY AREA 2022-638761 / [01] REPLACED STRAP BS 1016 PLUS 8 INCH LBL 3; WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #147A5600 SHEET 32 REV. B. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED STRAP BS 1016 PLUS 8 INCH LBL 3; WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #147A5600 SHEET 32 REV. B. Ï¿½TEM RII SEE INDIVIDUAL SIGN-OFF BELOW

Part: ANGLE — CRACKED (BS 291-294 RBL53) · airframe 55,781 hrs · 32,970 cycles

CRACKED ANGLE BETWEEN BS 291.5 - 294.5, RBL 53. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 141A8310 SHEET 25, REV-.

Part: STRUCTURE — CRACKED (BS 303) · airframe 55,781 hrs · 32,970 cycles

CRACK INNER CHORD BS 303.9 LBL 57 WL 208.1 AT FWD GALLEY AREA. REPLACED INNER CHORD AND FASTENERS BTW BS 270 - 360, LBL 57, WL 208.1 IAW SRM 51-40-02. DWG 141A8110 REV A, SHEET 9, AND DWG 140A9810, SHEET 48, REV-.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 55,781 hrs · 32,970 cycles

CRACKED ACCESS PANEL 661CB TRAILING EDGE HOLES RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.

Part: TIE CLIP — CRACKED (BS 277 S10R) · airframe 55,781 hrs · 32,970 cycles

CRACK TIE CLIP BS 277 STR 10R AT PASSENGER CABIN. REPLACED TIE CLIP IAW SRM 51-40-02 AND DRAWING 141A1110, REV.

Part: FRAME — CRACKED (BS 312 S5L) · airframe 55,781 hrs · 32,970 cycles

CRACKED FRAME ON BS 312, S5L IN THE FWD GALLEY AND LAVATORY. REPAIRED THE FRAME IAW EA M-22-153-01244.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 55,781 hrs · 32,970 cycles

BROKEN EMERGENCY EXIT LIGHT LENS ON SIDEWALL 242YAW AT PASSENGER CABIN 2022-638732 / [01] REPLACED EMERGENCY EXIT LIGHT LENS ON SIDEWALL 242YAW AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-01-960-802 STEP 3.C (10).;[02] REPLACED EMERGENCY EXIT LIGHT LENS ON SIDEWALL 242YAW AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-01-960-802 STEP 3.C (10).

Part: FLOORBEAM — CRACKED (BS 294 RBL 52) · airframe 55,781 hrs · 32,970 cycles

CRACK FLOOR BEAM BS 294.5 AT LEVEL RBL 52 AT FWD GALLEY AREA. FLOORBEAM REPAIRED ON FAULT TTG8Q00G0KBJ.

Part: FLOORBEAM — CORRODED (BS 294, LBL 1) · airframe 55,781 hrs · 32,970 cycles

CORROSION FLOOR BEAM BS 294.5 LBL 1; WL 208.1 AT FWD GALLEY AREA 2022-638699 / [01] TOOL USED: CALIPER; PN: 500-197-30; SN: A21143495; DUE DATE: 29-JUN-23.;[02] FLOOR BEAM BS 294.5 LBL 1 WL 208.1 AT FWD GALLEY AREA WAS REPAIRED ON FAULT TTG8Q00G0KBJ. <BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] FLOOR BEAM BS 294.5 LBL 1 WL 208.1 AT FWD GALLEY AREA WAS REPAIRED ON FAULT TTG8Q00G0KBJ. RII;SEE INDIVIDUAL SIGN-OFF BELOW.

Part: ANGLE — CRACKED (BS 695 RBL 24) · airframe 55,781 hrs · 32,970 cycles

CRACK ANGLE BS 695, RBL 24. REPLACED ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 111A6000, SHEET 236, REV-.

Part: FLOORBEAM — CORRODED (BS 294 RBL 11) · airframe 55,781 hrs · 32,970 cycles

CORRODED FLOORBEAM, BS 294.5, RBL 11, WL 208.1, IN THE FWD GALLEY. THE FLOORBEAM WAS REPAIRED ON FAULT TTG8Q00G0KBJ.

Part: WEB — CRACKED (RT NACELLE) · airframe 55,781 hrs · 32,970 cycles

CRACK WEB OUTBOARD FAN COWL, INTERNAL AREA ON ENGINE 2. REPLACED THE WEB AND FASTENER IAW CMM 71-13-30.

Part: SUPPORT ANGLE — CORRODED (BS 294 RBL 11) · airframe 55,781 hrs · 32,970 cycles

CORRODED SUPPORT ANGLE, BS 294.5 + 3, RBL 11, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, AND DWG 141A5400, SHEET 8 REV-.

Part: FLOORBEAM — CORRODED (BS 294 RBL7) · airframe 55,781 hrs · 32,970 cycles

CORROSION FLOOR BEAM BS 294.5 RBL 7; WL 208.1 AT FWD GALLEY AREA 2022-638700 / [01] TOOL USED: CALIPER; PN: 500-197-30; SN: A21143495; DUE DATE: 29-JUN-23.;[02] TOOL USED: RADIUS GAUGE; PN: 2204A3; SN: AE-408658; DUE DATE: 05-JUN-23.;[03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112031023 DUE DATE: 01-FEB-23. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 112820025 DUE DATE: 01-FEB-23.;[04] EDDY CURRENT EQUIPMENT USED; PN: NORTEC 600D ; SN: 190023010 ; DUE DATE: 14-FEB-23.;[05] PERFORMED REPAIR ON FLOOR BEAM 29.5 RBL 7; WL 208.1 AT FWD GALLEY AREA I.A.W. B737-700 SRM-53-10-51-2R-16 REPAIR 16. <BR>SEE INDIVIDUAL SIGN-OFF BELOW;[06] PERFORMED REPAIR ON FLOOR BEAM 29.5 RBL 7; WL 208.1 AT FWD GALLEY AREA I.A.W. B737-700 SRM-53-10-51-2R-16 REPAIR 16. RII ;SEE INDIVIDUAL SIGN-OFF BELOW.

Part: FLOORBEAM — CORRODED (BS 294 RBL 14) · airframe 55,781 hrs · 32,970 cycles

CORROSION FOUND ON FLOORBEAM, BS 294.5, RBL 14, WL 208.1 IN THE FWD GALLEY. THE FLOORBEAM WAS REPAIR ON FAULT TTG8Q00G0KBJ.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 54,896 hrs · 32,362 cycles

FWD GALLEY ENTRY EMERGENCY SLIDE DISLODGED AND HANGING ON FLOOR / [01] ADJUSTED FWD GALLEY SERVICE DOOR ESCAPE SLIDE PER 25-66-01.

Part: LIGHT — INOPERATIVE · airframe 53,249 hrs · 31,301 cycles

L 1 DOOR EMERGENCY LIGHT INOP ; / [01] RELAMPED PER AMM 33-51-04. OPS CKS GOOD

Part: NONE — LOOSE (CABIN) · airframe 52,887 hrs · 31,090 cycles

SUPPLEMENTAL INFORMATION: F/O SIDE EXIT EMERGENCY EXIT SIGN R2 FELL OFF. NEED PERMANENT ATTACHMENT. ; / [01] REATTACHED THE R2 DOOR LOWER EMERGENCY LIGHT LENS IAW EA M-21-133-0072. OK TO CONTINUE PER TLD.

Part: BULB — BURNED (CABIN) · airframe 52,876 hrs · 31,083 cycles

1EA BULB BURNT OUT IN LOWER RIGHT OVERWING EMERGENCY EXIT SIGN. ; / [01] RELAMPED BURNED OUT BULB IN LOWER RIGHT OVERWING EXIT SIGN AND PERFORMED GOOD INSTALLATION TEST. ALL WORK PERFORMED PER AMM 33-51-01-960-801; [02] VERIFIED CORRECTIVE ACTION STEP 1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,876 hrs · 31,083 cycles

EMERGENCY EXIT LIGHT L751 AT R/H OVER WING DOOR INOP. ; EMERGENCY EXIT LIGHT L751 AT RH OVER WING DOOR INOP. / [01] RELAMPED EMERGENCY EXIT LIGHT AT L751 AT R/H OVERWING DOOR AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-01-960-801; [02] VERIFIED CORRECTIVE ACTIONS STEP 1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,876 hrs · 31,083 cycles

AFT SERVICE DOOR SLIDE LIGHT IS INOP. / [01] RELAMPED AFT SERVICE DOOR SLIDE LIGHT AND PERFORMED GOOD INSTALLATION TEST PER AMM 33-51-04-960-801; [02] VERIFIED CORRECTIVE ACTIONS STEP 1.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

AFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED. WELDED CRACK ON ACB; AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4) FLURESCENT DYE PENETRANT INSPECTED REPAIRED AREA IN ACCORDANCE WITH SOPM 20-20-02 METHOD C. NO CRACKS NOTED. SANDED REPAIR WELD SMOOTH PER SRM 53-60-15-2R PARA 4.B.(5); [05] VERIFIED CORRECTIVE ACTION STEP 4. TREATED; PRIMED AND APPLIED A COAT OF STRIPPABLE PARTING AGENT TO ALL FAYING SURFACES OF THE CORNER SCUFF PLATE AND FUSELAGE SKIN/REPAIR PARTS IAW SRM 53-60-15-2R-1 PARA 4.B. (6-8). INSTALLED ACB; AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1 PARA 4.B.

Part: ANGLE — CRACKED (HORIZONTAL STAB) · airframe 52,876 hrs · 31,083 cycles

LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 120.30 4TH VERTICAL STIFFENER IS CRACKED. ; / [01] CUT AND REMOVED DAMAGE FROM 4TH VERTICAL STIFFENER AND WEB ON HORIZONTAL STAB. RIB AT STAB STA. 120.30; [02] CORRECTED CORRECTIVE ACTION 1. WORK ACCOMPLISHED IAW SRM 55-10-09-2R4.; [03] CERTIFIED CORRECTION.; [04] VERIFIED CORRECTIVE ACTION 1-2 FOR DAMAGE REMOVAL ON LH HORIZ STAB RIB; [05] EDDY CURRENT INSPECTED DAMAGE TRIM OUT AND SURROUNDING AREA IN ACCORDANCE WITH 737 NDT MANUAL PART 6; 51-00-00 PROCEDURE 23. NO CRACKS FOUND. EDDY CURRENT INSPECTED OPEN HOLES COMMON TO THE REPAIR AREA IN ACCORDANCE WITH 737 NDT MANUAL PART 6; 51-00-00 PROCEDURE 16. NO CRACKS FOUND.<BR><BR>TOOL I.D. ATS729 (OLYMPUS NORTEC 500)<BR>S.N. N500X10629S091205<BR><BR>TOOL I.D. ATS2407 (OLYMPUS MINIMITE ROTARY SCANNER)<BR>S.N. MM15391DD064104; [06] FABRICATED REPAIR ANGLE FROM BAC1490-2793#7075T62;.063'; LOT#1464923-1; REPAIR 'T' FROM 60-5872#7075T76511;.063';LOT#1463116-1;SHIMS FROM 7075T6;.063' LOT#1351319-2 IAW SRM 55-10=09-2R-4; PARA 4.;

Part: RAIL — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON CARGO TRACK AT BS 772, LBL 3, WL 157. FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED BY TRIMMING OUT AN AREA L=3.26' X W= .9' IAW SRM 53-00-53-2R-2, REPAIR 2. HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT IAW NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND. FABRICATED, LOCATED, AND DRILLED NEW SPLICE AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 53-00-53-2R-2, PAR 4, FIG 203, DETAIL F. APPLIED PRIMER ON SPLICE REPAIR IAW SRM 53-00-53-2R-2, PAR 4. FIG 203, DETAIL F. INSTALLED SPLICE REPAIR IAW SRM 53-00-53-2R-2, PAR 4, STEP Q, FIG 203, DETAIL F.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK WL 208 RBL 45 BS 727B-727C+5; BS 727C+9-727D+15; BS 727D+19-812; BS 817-887. [TTG8Q0093K44] REQUIRES RII BUY BACK ; / [01] WORK CARD TTG8Q0093K44 IS RII.; [02] COMPLETED ENTRY; [03] COMPLETE; [04] UPDATED WORK CARD; [05] COMPLETED; [06] CERTIFIED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS727B {TTG8Q0093H36} REQUIRES RII BUY BACK ; / [01] VERIFIED RII; [02] FINAL INSTALLATION OF SEAT TRACK IS RII FOR TTG8Q009H36.; [03] WORK CARD COMPLETED.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

FWD CARGO BAFFLE CRACKED AT BS 500 LBL 25 WL 156. NO LIMITS FOUNDED FOR CRACK IN SRM. REMOVED BAFFLE IAW SRM 51-40-02. FABRICATED BAFFLE, LOCATED, DRILLED, AND APPLIED CHEMICAL CONVERSION COATING IAW DWG 143A7510, REV B, AND SRM 51-40-05. APPLIED PRIMER IAW DWG 143A7510, REV B, AND AMM 51-21-72-370-804. INSTALLED BAFFLE IAW SRM 51-40-02, AND DWG 143A7505.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON PASSENGER CABIN SEAT TRACK WL 208 RBL 45 BS 727B-727C+5; BS 727C+9-727D+15; BS 727D+19-812; BS 817-887. [TTG8Q0093K44] REQUIRES RII BUY BACK ; / [01] WORK CARD TTG8Q0093K44 IS RII.; [02] COMPLETED ENTRY; [03] COMPLETE; [04] UPDATED WORK CARD; [05] COMPLETED; [06] CERTIFIED.

Part: NONE — CORRODED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CORROSION ON PRESSURE FLOOR AT STA 687+18 LBL 69. REMOVED DAMAGE ON PRESSURE FLOOR IAW SRM 51-10-02-0G-0. NO HAVE ALLOWABLE DAMAGE LIMITS. HFEC INSPECTED BLENDED AREA IAW NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.

Part: PANEL — CRACKED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

PANEL 191FR HAS SEVERAL CRACKED FASTENER HOLES. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-30-70-1A-1 PARA 4.B.(1).(A-C). UP SIZED FOUR FASTENER HOLES AND PREPPED FOR A SLURRY REPAIR WITH NO DISBOND OR CONTAMINATION NOTED. WORK PERFORMED IAW SRM 51-70-04-2R-9 PARA 4.A-C. INSTALLED REPAIR PLIES IAW SRM 51-70-04-2R-9 PARA 4.G-M. SKIN WAS REFINISHED ON FAULT TTG8Q0098X58.

Part: PANEL — CRACKED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

PANEL 191D HAS MULTIPLE CRACKED FASTENER HOLES ALONG R/H AND L/H EDGEBANDS. DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-30-70-1A-1 PAR 4B(1B). COMPLETED DAMAGE REMOVAL ON INNER SURFACE EDGEBAND IAW SRM 51-70-05-2R-6 PAR 4A-D. FABRICATED REPAIR PLIES IAW SRM 51-70-05-2R-6 PAR 4E-F. JOB COMPLETE PER SRM 51-70-05-2R-6.

Part: NONE — CORRODED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CORROSION ON PRESSURE FLOOR AT BS 687+18 RBL 67. REMOVED DAMAGE ON PRESSURE FLOOR IAW SRM 51-10-02-0G-0. REMOVED ONE FASTENER IAW SRM 51-40-02-0G-0, BLEND AREA IS 1'X1' AT BS 687+18 LBL 69 WL202. NO ALLOWABLE DAMAGE LIMITS. UT INSPECTED BLENDED AREA IAW NDTM PART 4 51-00-00 PROCEDURE 23. NO CRACKS NOTED. REPAIRED PRESSURE DECK FLOOR IAW EA 21-153-03444.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CORROSION ON FUSELAGE SKIN FROM STA 1016 TO STA 1088; RBL 15 TO LBL 15. REMOVED CORROSION. ACCOMPLISHED HFEC SURFACE SCAN IAW B737 NDTM PART 6 51-00-00 PROC 23; 51-00-00 PROC 16; 53-30-00 PROC PROC 3; AND PART 4 51-00-00 PROC 2. NO CRACKS NOTED. REPAIRED IAW EA 21-153-03421 REV A.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

STRINGER CLIP CRACKED BS 520 STR 26L. REMOVED STRINGER CLIP STR 26L BS 520 PER SRM 51-40-02. INSTALLED STRINGER CLIP IAW DWG 143A1215 REV-, AND SRM 51-40-02.

Part: BEAM — CRACKED (R1 DOOR) · airframe 52,875 hrs · 31,083 cycles

FWD GALLEY DOOR 4 BEAM IS CRACKED APPROXIMATELY 14 INCHES AFT OF INNER SKIN COMMON TO INBOARD FLANGE. FWD GALLEY DOOR 4 BEAM REMOVED AND REPLACED ON PO P1690269-1.

Part: BEAM — CRACKED (R1 DOOR) · airframe 52,875 hrs · 31,083 cycles

FWD GALLEY DOOR #5 BEAM IS CRACKED APPROXIMATELY 14 INCHES AFT OF INNER SKIN COMMON TO INBOARD FLANGE. FWD GALLEY DOOR #5 BEAM REMOVED AND REPLACED ON PO# P1690269-1.

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 52,876 hrs · 31,083 cycles

LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 120.30; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] CUT AND REMOVED DAMAGE FROM 3RD VERTICAL STIFFENER AND WEB ON R/H HORIZONTAL STAB. RIB AT STAB. STA. 120.30 IAW SRM 55-10-09-2R-4.;[06] FABRICATED REAIR'T' FROM 60-5872#7075T76511;.063';LOT#1463116-1; REPAIR ANGLE FROM BAC1490-2793#7075T62;.063';LOT#1464923-1; SHIMS FROM 7075T6;.063';LOT#1351319-2 IAW SRM55-10-09-2R-4;PARA 4.; [07] VERIFIED CORRECTIVE ACTION 6; [08] PERFORMED GVI IAW SRM 55-10-09-2R-4 PARA E. NO FURTHER DAMAGE NOTED; [09] APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO REPAIR PARTS IAW SRM 55-10-09-2R-4 PARA. 4.; [10] VERIFIED CHEMICAL CONVERSION COATING AND PRIMER APPLIED TO

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 52,876 hrs · 31,083 cycles

RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 2ND VERTICAL STIFFENER IS CRACKED. ; / [01] CUT AND REMOVED THE DAMAGE FROM THE VERTICAL STIFFENER OF THE RIB PER SRM 55-10-09-2R-4.; [12] INSTALLED REPAIR PARTS ON RIB ASSY. IAW SRM 55-10-09-2R-4 PARA. 4 AND FIG. 202.; [13] RII INSPECTED INSTALLATION OF REPAIR PARTS ON RIB ASSY. IAW SRM 55-10-09-2R-4.; [14] APPLIED FILLET SEAL AND FINISH TO REPAIR PARTS AND RIB ASSY. IAW SRM 55-10-09-2R-4 PARA. 4.; [15] VERIFIED CORRECTIVE ACTION STEP 14.

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 52,876 hrs · 31,083 cycles

SUPPLEMENTAL INFORMATION: RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] CUT AND REMOVED THE DAMAGE FROM THE VERTICAL STIFFENER AND WEB OF THE RIB PER SRM 55-10-09-2R-4.; [02] VERIFIED SRM 55-10-09-2R-4 IS APPLICABLE AND DAMAGE IS REMOVED; [03] HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16; NO CRACKS NOTED. <BR>EQUIP ID#: IS000450 S/N: N500D000M120071 EQUIP ID#: ATS2407 S/N: MM1591DD064104; [04] HFEC INSPECTED CUT OUT IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. <BR>EQUIP ID#: IS000450 S/N: N500D000M120071; [05] FABRICATED REPAIR PARTS -1 T SECTION FROM 60-5872#7075T76511 0.063' LOT#1463116-1;-2 ANGLE FROM BAC1490-2793#7075T62 0.063' LOT#1464923-1;-3 SHIM FROM 7075T6 0.016' LOT#1351319-2. APPLY A CHEMICAL CONVERSION COATING TO THE REPAIR PARTS. PER SRM55-10-09-2R-4.; [06] ACCOMPLISHED GVI; NO ADDITIONAL FAULTS NOTED; PER SRM 55-10-09-2R-4 REPAIR 4 STEP 4.E. <BR><BR>VERIFIED CORRECTIVE ACTION 5 (FAB OF PARTS); [07] APPLIED A CHEMICAL CONVERSION COATING AND PRIMER TO THE REPAIR PARTS AND THE BARE SURFACES AND CUT EDGES OF THE RIB. PER SRM 55-10-09-2R-4. O.K TO INSTALL [09] INSTALLED REPAIR PARTS PER SRM 55-10-09-2R-4 STEPS 4 M-P.; [10] RII INSPECTED REPAIR PARTS INSTALLED PER SRM 55-10-09-2R-4.; [11] APPLIED FILLET SEAL AND FINISH TO REPAIR PARTS AND RIB ASSY. IAW SRM 55-10=09=2R-4 PARA. 4

Part: SUPPORT — CORRODED (BS 727B-767) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON FLOOR TO SIDE WALL SUPPORT AT AFT CARGO BAY RBL 22 WL 153 BS 727B-767. ; / [01] REMOVED CORROSION FROM ACB R/H BS 727-767 FLOOR TO SIDEWALL SUPPORT AT BS747+5 MEASURRED 11'L X 2'W AND 0.017'DEEP ORIGINAL THICKNESS OF 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [02] REMOVED CORROSION FROM ACB R/H BS 727-767 FLOOR TO SIDEWALL SUPPORT AT BS747+5 MEASURRED 11'L X 2'W AND 0.017'DEEP ORIGINAL THICKNESS OF 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] FABRICATED NEW FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS 727B TO BS 767; RBL 22; WL 153 IAW SRM 51-40-05-0G-0; DWG 146A7500; ID:85; REV:A; BAC1496-377#7075T62; LOT#5093799-1; APPLIED CHEMICAL CONVERSION IAW AMM 51-21-41-370-802; OK TO APPLY PRIMER; [04] VERIFIED CORRECTIVE ACTION STEP 3. VERIFIED OK TO PRIMER.; [05] APPLIED PRIMER ON NEW FLOOR TO SIDEWALL SUPPORT IAW AMM 51-21-72-370-804; [06] VERIFIED CORRECTIVE ACTION STEP 5.; [07] VERIFIED FAULT COMPLETE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-25R RBL22 WL155. REPAIRED IAWSRM 53-00-03-2R-1 AND EA 21-153-03333.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON ATTACH ANGLE AT AFT CARGO BAY WL 150 RBL 7 BS 727D+6. THERE IS NO ALLOWABLE DAMAGE FOR ATTACH ANGLE. REMOVED ATTACH ANGLE IAW SRM 51-40-02-0G-0. FABRICATED ATTACH ANGLE IAW SRM 51-40-08 AND DWG 146A7734 SHT 2 REV A. APPLIED CHEMICAL CONVERSION AND PRIMER IAW SRM 51-20-01-0G-0. APPLIED CHEMICAL CONVERSION AND PRIMER AT AFT CARGO ANGLE IAW SRM 51-20-01-0G-0. INSTALLED NEW ANGLE IAW SRM 51-40-02 AND DWG 146A7730 REV:-.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 528,752 hrs · 31,083 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-26L WL153. MARKED ; / [01] EVALUATED CRACK MEASUREMENTS ON FCB STR 26L BS 536 ; STRINGER DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1 FIG 103; [21] REPAIRED STRINGER 26L; BETWEEN STA 500D-520; WL 153 I.A.W SRM 53-00-03-2R-1 REPAIR 1.; [22] CORRECTION FOR ITEM 21- REPAIRED STRINGER 26L; BETWEEN STA 500D-540; WL 153 I.A.W SRM 53-00-03-2R-1 REPAIR 1.; [23] VERIFIED INSTALLATION OF REPAIR PARTS FOR S-26L; BS 500D-540; WL 153; PER SRM 53-00-03-2R-1; REPAIR 1; [24] VERIFIED ALL WORK COMPLETE THIS TASK

Part: RAIL — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON CARGO TRACK AT RBL 8, WL 157, BS 772. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2, FIG 103, DETAIL E. INSTALLED A NEW CHANNEL FILLER AND NEW REPAIR CHANNEL SPLICES IAW SRM 53-00-53-2R-2, REPAIR 2, STEP 4 (P;Q R;S), AND DWG 146A7500 REV A.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CORROSION ON RAIL AT AFT CARGO BAY LBL 3 WL 153 BS 727E+3; WL 157 BS 772; WL 165 BS 867; WL 171 BS 907. ; / [01] REMOVED CORROSION FROM ACB RAIL BS 727E+3 LBL 3 WL 153 IN L= 2'; W=1' ; D= 0.019' FROM ORIGINAL THIKNESS 0.071' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG 103 DETAIL E.<BR><BR>TOOL USED ID : ATS2318 ; S/N : B19006095 ; DATE : 05/2021 ; DUE: 05/2022;17] INSTALLED NEW CHANNEL AND NEW SPLICES (TWO POSITIONS) AT ACB LBL3 WL 157 BTW BS 727D+12' TO BS 727E+10' FOR CHANNEL AND SPLICE BTW BS 727D+8' TO 727D+15' AND BTW BS 727E+7' TO 727E+14' IAW IAW SRM 53-00-53-2R-2 ; STEP 4(P;Q;R ;S) FIG. 203 ; DETAIL A.

Part: STRAP — CORRODED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CORROSION ON STRAP IN AFT CARGO BAY BS 804, RBL19, WL 158. REMOVED DAMAGE FROM STRAP, FOUND OUT OF LIMITS. REMOVED STRAP IAW SRM 51-40-02. LOCATED AND DRILLED A NEW STRAP IAW SRM 51-40-05-0G-0, AND DWG 146A8120 REV -. INSTALLED THE NEW STRAP IAW SRM 51-40-02, AND DWG 146A0081 REV C, AND DWG 146A8120 REV -.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,875 hrs · 310,833 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-26R WL153. MARKED ; / [01] EVALUATED CRACK MEASUREMENTS ON FCB STR 26R BS 536 ; STRINGER DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1 FIG 103; [18] REPAIRED STRINGER 26R; BETWEEN STA 500D - 540; WL 153. IAW SRM 53-00-53-2R-1; [19] VERIFIED CORRECTIVE ACTION STEPS 16 AND 18.; [20] VERIFIED CORRECTIVE ACTION STEPS 16 AND 18.; [21] COMPLETE; [22] COMPLETE

Part: ANGLE — CRACKED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CRACKED SUPPORT ANGLES AT AFT CARGO BAY BEHIND WATER SERVICE PANEL BS914; BS918 RBL10 WL169. ; / [01] REMOVED SUPPORT ANGLES AT AFT CARGO BAY BEHIND WATER SERVICE PANEL BS 914;AND BS 918 RBL 10 WL 169 IAW SRM 51-40-02.; [02] REMOVED SUPPORT ANGLES AT AFT CARGO BAY BEHIND WATER SERVICE PANEL BS 914;AND BS 918 RBL 10 WL 169 IAW SRM 51-40-02; [03] LOCATED AND DRILLED NEW SUPPORT ANGLES AT AFT CARGO BAY BEHIND WATER SERVICE PANEL PO#843612 IAW SRM 51-40-05; DWG 147A7221 REV -. OK TO INSTALL; [04] VERIFIED CORRECTIVE ACTION STEP 3. VERIFIED OK TO INSTALL.; [05] INSTALLED NEW SUPPORT ANGLES IN ACB BEHIND WATER SERVICE PANEL BS 914; BS918 RBL 10 IAW DWG 147A7221 REV -; SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25 WL155. ; / [01] REMOVED INTERCOSTAL ATTACH ANGLE AT FCB BS500C FWD SIDE LBL25 WL155 IAW SRM 51-40-02; [07] INSTALLED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25 WL155 IAW SRM 51-40-02-0G-0 AND DWG 143A7507 REV:B; [08] INSTALLED 4EA RIVETS COMMON TO THE INTERCOSTAL FWD SIDE; IAW SRM 51-40-02 AND DWG 143A7505 ID:0005 REV:B . 3EA MORE RIVETS NEEDS TO BE INSTALLED; [09] INSTALLED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25 WL155 IAW SRM 51-40-02-0G-0 AND DWG 143A7505 REV:B SHT:0005.

Part: TRACK — CRACKED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CRACK ON TRACK AT AFT CARGO BAY RBL 14 WL 152 BS 727E; BS 747; BS 767. ; / [01] EVALUATED ACB TRACK BS 727 TO 887 RBL 14 WL 152 DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. <BR><BR>REMOVED TRACK BS 727 TO 887 RBL 14 WL 152 IAW SRM 51-40-02; [02] EVALUATED ACB TRACK BS 727 TO 887 RBL 14 WL 152 DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [03] REMOVED TRACK BS 727 TO 887 RBL 14 WL 152 IAW SRM 51-40-02; [04] LOCATED AND DRILLED NEW TRACK PO#840759 AND FLOOR SPLICE P/N 146A7506-20 AT ACB BS 727 TO BS 887 RBL 14 IAW DWG 146A7500 REV A; SRM 51-40-05-0G-0; SRM 53-00-53-2R-3 REPAIR 3. INSTALLED NEW TRACK AT ACB BS 727 TO BS 887 WL 152 IAW SRM 51-40-02-0G-0 ANS DWG 146A7500 REV:A.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON ATTACH ANGLE AT WL 150, RBL 7, BS 727D+4. NO ALLOWABLE DAMAGE FOR ATTACH ANGLE. REMOVED ATTACH ANGLE IAW SRM 51-40-02-0G-0. FABRICATED ATTACH ANGLE IAW SRM 51-40-08, AND DWG 146A7734, SHT 2, REV A. APPLY CHEMICAL CONVERSION AND PRIMER IAW SRM 51-20-01-0G-0. INSTALLED A NEW ANGLE IAW SRM 51-40-02, AND DWG 146A7730 REV -.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CRACKED INTERCOSTAL ATTACH ANGLE IN THE FWD CARGO BAY BS 500C AFT SIDE LBL25, WL155. REMOVED THE INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED THE NEW INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-05, AND DWG 143A7502. INSTALLED THE INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02-0G, & DWG 143A7505 REV B.

Part: SUPPORT — CRACKED (BS 782) · airframe 52,875 hrs · 31,083 cycles

CRACK ON FLOOR TO SIDE WALL SUPPORT AT AFT CARGO BAY LBL 21 WL 155 BS 782. ; / [01] UPON FURTHER INVESTIGATION CRACK FOUND TO BE CORROSION ON ACB L/H BS 727-847 AT BS 782 MEASURED 3'L X 2'W AND 0.040' DEEP; 100% MATERIAL LOSS; PART FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2; [06] FABRICATED REPLACEMENT FLOOR TO SIDEWALL SUPPORT USING BAC1496-377#7075T62 LOT: 5093799-1 IAW SRM 51-40-05-0G-0; SRM 53-00-53-2R-5 SECTION 4. D-H AND DWG 146A7502 ID: 0027 REV:-. FABRICATED FLOOR TO SIDEWALL SUPPORT SPLICE REPAIR BS 747+10' USING BAC1496-377#7075T62 LOT: 5093799-1 IAW SRM 53-00-53-2R-5 SECTION 4. D-H; SRM 51-40-05 AND SRM 51-40-08. APPLIED CHEMICAL CONVERSION COATING TO SPLICE AND SIDEWALL SUPPORT IAW SOPM 20-41-02. OK TO APPLIED PRIMER TO SPLICE AND SIDEWALL SUPPORT; [07] VERIFIED CORRECTIVE ACTION STEP 6. OK TO PRIMER.; [08] OK TO INSTALL FLOOR TO SIDEWALL SUPPORT SPLICE REPAIR; [09] VERIFIED; [10] APPLIED PRIMER IAW SOPM 20-41-02 <BR><BR>OK TO INSTALL SPLICE; [11] VERIFIED; [12] VERIFIED CORRECTIVE ACTIONS 8-11.<BR><BR>PRIMER APPLIED TO REPAIR PARTS; OK TO INSTALL SPLICE REPAIR.; [13] INSTALLED FLOOR TO SIDEWALL SUPPORT SPLICE REPAIR IAW SRM 53-00-53-2R-5 AND SRM 51-40-02. INSTALLED NUT PLATES AT 13-NOV-2021 09:03 UTC IAW SRM51-40-10-2R-0; [14] VERIFIED CORRECTIVE ACTION STEP 13.

Part: RAIL — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON CARGO TRACK LBL 8, WL 157, BS 772. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; FIG 103 DETAIL E. TRIMMED OUT DAMAGE AREA IAW SRM 53-00-53-2R-2, FIGURE 202. FABRICATED, LOCATED, AND DRILLED THE NEW SPLICE AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 53-00-53-2R-2, PAR 4. FIG 203 DETAIL F. APPLIED PRIMER ON SPLICE REPAIR IAW SRM 53-00-53-2R-2, PAR 4. FIG 203 DETAIL F. INSTALLED SPLICE REPAIR IAW SRM 53-00-53-2R-2, PAR 4, STEP Q, FIG 203 DETAIL F.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 500B+2.5-500C+13.5, RBL 23, WL 157. REMOVED AND EVALUATED CORROSION. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. FABRICATED A NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05; 51-40-08 AND DWG 143A7501 AND APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW AMM 51-21-41-370-802, AMM 51-21-72-370-804. INSTALLED NUTPLATES IN 13EA. LOCATIONS ON REPLACEMENT FCB FLOOR TO SIDEWALL SUPPORT R/H FROM BS 500A-BS 500D IAW DWG 140N4500 REV:G AND DWG 143A7501 REV:-.

Part: FITTING — CORRODED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CORROSION ON WEB SUPPORT FITTING WL 151 RBL 20 BS 775. REMOVED CORROSION ON WEB SUPPORT FITTING AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1. LOCATED AND DRILLED NEW WEB SUPPORT FITTING IAW SRM 51-40-05-0G-0 AND DGW 146A0081. APPLIED CHEMICAL CONVERSION IAW AMM 51-21-41-370-802. INSTALLED NEW WEB SUPPORT FITTINGIAW DWG 146A0081 REV A.

Part: FITTING — CORRODED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CORROSION ON INTERCOSTAL SUPPORT FITTING AT AFT CARGO BAY BS944 LBL3 WL173. ; THERE IS NO ALLOWABLE DAMAGE FOR INTERCOSTAL SUPPORT FITTING. REMOVED INTERCOSTAL SUPPORT FITTING IAW SRM 51-40-02-0G-0. FORMED REPLACEMENT INTERCOSTAL SUPPORT FITTING IAW DWG 147A7580 REV E AND SRM 51-30-01-0G-0 SEC 8. LOCATED AND DRILLED NEW FITTING IAW SRM 51-40-05 AND DWG 147A7500. APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SOPM 20-43-03 AND SRM 51-21-72-370-804. INSTALLED INTERCOSTAL SUPPORT FITTING ACB BS944; LBL 3; WL 173 IAW SRM 51-40-02 AND DWG 147A7500.

Part: SUPPORT — CORRODED (BS 727A-807) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON FLOOR TO SIDE WALL SUPPORT AT AFT CARGO BAY LBL 21 WL 153 BS 727A-807. ; / [01] REMOVED CORROSION FROM ACB L/H FLOOR TO SIDWALL SUPPORT AT BS 727E+14' MEASURED 1.8'L X1'W AND 0.019' DEEP. ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2 WORK TO BE COMPLETED ON CUSTOMER CARD TTG8Q0094KP6; [02] REMOVED CORROSION FROM ACB L/H FLOOR TO SIDWALL SUPPORT AT BS 727E+14' MEASURED 1.8'L X1'W AND 0.019' DEEP. ORIGINAL THICKNESS OF 0.040' FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2 WORK TO BE COMPLETED ON CUSTOMER CARD TTG8Q0094KP6; [03] VERIFIED CORRECTIVE ACTIONS STEP 1.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON AFT SHIELD AT AFT CARGO BAY BS856 - BS867 RBL22 WL164. ; / [01] CORROSION ON AFT SHIELD AT ACB BS856-BS867; RBL22;WL164 NO ALLOWABLE DAMAGE IAW SRM 51-10-02-0G-0 GENERAL - INSPECTION AND REMOVAL OF DAMAGE (PAR.9. REPLACEMENT OF THE PART); [02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.; [03] REMOVED AFT SHIELD AT ACB BS 856-BS 867 RBL 22 WL 164 IAW SRM 51-40-02; [04] LOCATED AND DRILLED NEW ACB SHIELD PO#845151BS 856 - BS867 RBL 22 IAW SRM 51-40-05; DWG 146A0081 REV-.; [05] PART WILL BE INSTALLED ON CUSTOMER CARD TTG8Q004FDXV; [06] REMOVED AFT SHIELD IN ACB AT BS 856 - 867 RBL22 WL 164 ON CARD #TTG8Q004FDXV.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET WAS CRACKED BS 500D, S19L, WL 193. REMOVED GUSSET IAW SRM 51-40-02. LOCATED AND DRILLED NEW GUSSET IAW SRM 51-40-05 AND DWG 143A7902. INSTALLED NEW GUSSET IAW SRM 51-40-02 AND DWG 143A7902.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS807 RBL15 WL157. THERE IS NO ALLOWABLE DAMAGE FOR ATTACH ANGLE AT AFT CARGO BAY BS807 RBL15. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0. REMOVE STRINGER CLIP IAW SRM 51-40-02-0G-0. VERIFIED NO ALLOWABLE DAMAGE IN THE SRM FOR ATTACH ANGLE. MAY BE REPAIRED BY REPLACEMENT PER 51-10-02-0G-0. LOCATED AND DRILLED NEW CLIP P/N 146A1010-27 IAW SRM 51-40-05-0G-0 AND DWG 146A1263 REV. DRILLED STRINGER CLIP PER SRM 51-40-05 AND DWG 146A1263. INSTALLED STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1263 REV -.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION FOUND ON FWD SHIELD AT FWD CARGO BAY WL 153, RBL 25, BS 426-436. NO ALLOWABLE DAMAGE IAW SRM 51-10-02-0G-0 GENERAL. LOCATED AND DRILLED HOLES IN NEW FWD SHIELD IAW SRM 51-40-05-0G-0 GENERAL. FABRICATED THE NEW FWD SHIELD IAW SRM 51-40-02-0G-0, AND DWG'S 143A0080 REV - AND 143A0082 REV A. INSTALLED NUTPLATES ON FCB FWD SHIELD IAW SRM 51-40-02-0G-0 FASTENER INSTALL/REMOVAL AND DWG'S 143A0080 REV:- AND 143A0082 REV:A.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CORROSION FOUND ON FLOOR TO SIDEWALL SUPPORT IN THE FWD CARGO BAY BS 500+5-500C+13, LBL 23, WL 157. REMOVED AND EVALUATED CORROSION DAMAGE FOUND TO OUT OF LIMITS IAW SRM 53-00-53-1A-2. FABRICATED A NEW FLOOR TO SIDEWALL SUPPORT AND SPLICE. INSTALLED SPLICE TO FLOOR SIDEWALL SUPPORT IAW SRM 51-40-05-0G-0, SRM 51-40-08-0G-0, SRM 53-00-53-2R-5, AND DWG 143A7500 REV -.

Part: RAIL — CORRODED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CORROSION ON RAIL AT AFT CARGO BAY LBL 12 WL 157 BS 772. ; / [01] REMOVED CORROSION FROM ACB RAIL BS 772 LBL 12 WL 157 MATERIAL LOSS MORE THAN 20% FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; FIG 103 DETAIL E. <BR><BR> TOOL USED ID :ATS2318 ; S/N: B19006095 ; DATE : 05/2021 ; DUE : 05/2022 .[12] INSTALLED SPLICE REPAIR AT ACB LBL 12 WL 157 BS 772 IAW SRM 53-00-53-2R-2 ; PAR. 4. STEP Q ; FIG 203 DETAIL F.; [13] CERTIFIED ACTION 12; [14] VERIFIED CORRECTIVE ACTIONS STEP 12.; [15] FILL THE GAPS BETWEEN REPAIR AREA AND THE INITIAL PART AND APPLIED ONE LAYER CORROSION INHIBITING COMPOUND TO THE REPAIR AREA IAW SRM 53-00-53-2R-2.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED ; / [01] REMOVED GUSSET FROM FCB BS 500D; STR 19R IAW SRM 51-40-02.<BR><BR>PART HAS NO ALLOWABLE DAMGE LIMIT ON SRM REPAIR BY REPLACEMENT PER SRM 51-10-02.<BR><BR>LOCATED AND DRILLED NEW GUSSET BS 500D STR 19R PER SRM 51-40-05; DWG# 143A7902.; [02] REQUEST OK TO INSTALL.; [03] OK TO INSTALL GIVEN.; [04] INSTALLED FCB GUSSET BS 500D; STR 19R IAW SRM 51-40-02; DWG# 143A7902.; [05] VERIFIED INSTALLATION ON CORRECTIVE ACTION 4.; [06] ALL WORK ACCOMPLISHED.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CRACKED INTERCOSTAL ATTACH ANGLE IN FWD CARGO BAY BS 500A FWD SIDE LBL 25, WL 155. REMOVED INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED A NEW INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-05 AND DWG 143A7502. INSTALLED THE NEW INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02 AND DWG 143A7505.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CORROSION ON STRINGER SPLICE IN AFT CARGO BAY BS 796 RBL14 WL 153. REMOVED SPLICE BS 789 TO 799 RBL 14 WL 1.53 IAW SRM 51-40-02. REMOVED CORROSION ON STRINGER SPLICE, FOUND OUT OF LIMITS IAW SRM 53-00-03-1A-1, STEP 4A (1)(B). LOCATED AND DRILLED A NEW STRINGER SPLICE IAW SRM 51-40-05-0G-0 AND DWG 146A3230 REV A. APPLIED CHEMICAL CONVERSION IAW AMM 51-21-41-370-802. APPLIED PRIMER ON NEW STRINGER SPLICE IAW AMM 51-21-72-370-804 . INSTALLED NEW STRINGER SPLICE IAW SRM 51-40-02-0G-0 AND DWG 146A3230 REV:-.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CORROSION ON WEB SUPPORT AT AFT CARGO BAY WL 151 RBL 22 BS 770. REMOVED WED SUPPORT AT AFT CARGO BAY WL 151 RBL 22 BS 770 IAW SRM 51-40-02. REMOVED CORROSION ON WEB SUPPORT, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1;STEP 4H ;FIG 103. LOCATED AND DRILLED NEW WEB SUPPORT IAW SRM 51-40-05-0G-0 AND DWG 146A0081. INSTALLED NEW WEB SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 146A0081.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CRACKED INTERCOSTAL ATTACH ANGLE IN FWD CARGO BAY, BS 500B FWD SIDE RBL25, WL155. REMOVED INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED THE NEW INTERCOSTAL ATTACH IAW SRM 51-40-05, AND DWG 143A7502. INSTALLED THE NEW INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02, AND DWG 143A7505.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CORROSION ON CARGO TRACK RBL 3, WL 157, BS 772. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; FIG 103 DETAIL E. INSTALLED NEW CHANNEL FILLER AND NEW REPAIR CHANNEL SPLICES IAW SRM 53-00-53-2R-2 REPAIR 2 STEP 4(P;Q;R ;S) AND DWG 146A7500 REV A.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON FLOOR TO SIDE WALL SUPPORT AT FWD CARGO BAY WL 153 RBL 25 BS 402. ; / [01] REMOVED AND EVALUATED DAMAGE ON R/H FCB FLOOR TO SIDEWALL SUPPORT AT BS 402 RBL 25 WL 153; DAMAGE MEASURES 1.1' L; 0.9' W; 0.009' D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. PART TO BE REPAIRED BY REPLACEMENT. DIAL DEPTH GAUGE USED: ATS400.;[12] FABRICATED REPLACEMENT FCB FLOOR TO SIDEWALL SUPPORT R/H BS 396-420 OUT OF MATERIAL BAC1496-444 LOT#1467644-1 IAW SRM 51-40-05; 51-40-08; AND DWG#143A7500; [13] VERIFIED CORRECTIVE ACTION 12; JOB COMPLETE

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CORROSION ON WEB SUPPORT AT AFT CARGO BAY WL 151 RBL 22 BS 765. ; / [01] REMOVED WED SUPPORT AT AFT CARGO BAY WL 151 RBL 22 BS 765 IAW SRM 51-40-02; [02] REMOVED WED SUPPORT AT AFT CARGO BAY WL 151 RBL 22 BS 765 IAW SRM 51-40-02; [03] THIS PART WILL BE ACCOMPLISH ON CUSTOMER CARD NBR:TTG8Q0094KS7; [04] VERIFIED COMPLETE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,875 hrs · 31,083 cycles

CRACKED STRINGER AT AREA AFT OF FCB BS540 S-23R WL164. MARKED ; / [01] EVALUATED CRACK MEASUREMENTS ON FCB STR 23R BS 536 ; STRINGER DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1 FIG 103; [28] REPAIRED STRINGER 23R; BETWEEN STA 500D - 540; INSTALLED ALL FASTENERS I.A.W EA# 21-153-03354 REV:A.; [29] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 21-153-03354'; [30] VERIFIED CORRECTIVE ACTION STEP 24.

Part: SUPPORT — CORRODED (BS 840-883) · airframe 52,875 hrs · 31,083 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS870; BS883 RBL22 WL167. ; / [01] REMOVED CORROSION FROM ACB RH FLOOR TO SIDEWALL AT BS 870 MEASURED 1.5'L X 0.75'W AND 0.013 DEEP ORIGINAL THICKNESS OF 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [02] REMOVED CORROSION FROM ACB RH FLOOR TO SIDEWALL AT BS 870 MEASURED 1.5'L X 0.75'W AND 0.013 DEEP ORIGINAL THICKNESS OF 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] FABRICATED FROM ; NEW FLOOR TO SIDEWALL SUPPORT R/H AT AFT CARGO BAY BS 870 TO BS 883; RBL 22 ; WL 167 IAW SRM 51-40-05-0G-0 AND DWG 147A7501; ID 6; REV:A; BAC1496-377#7075T62; LOT #1467164-1; APPLIED CHEMICAL CONVERSION IAW AMM 51-21-41-370-802; OK TO PRIMER;

Part: ANGLE — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON ATTACH ANGEL AT AFT CARGO BAY WL 150 RBL 6 BS 745. ; / [01] THERE IS NO ALLOWABLE DAMAGE FOR ATTACH ANGLE AT AFT CARGO BAY B 745 RBL6. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0; [02] REMOVED ATTACH ANGLE IAW SRM 51-40-02-0G-0G; [03] VERIFIED NO ALLOWABLE DAMAGE IN THE SRM FOR ATTACH ANGLE. MAY BE REPAIRED BY REPLACEMENT PER 51-10-02-0G-0.; [04] LOCATED ABD DRILLED NEW ATTACH ANGLE IAW SRM 51-40-05-0G-0 AND DWG 146A7810 REV A; [05] VERIFIED CORRECTIVE ACTION 4; [06] REQUEST OK TO INSTALL ANGLE; [07] OKAY TO INSTALL; [08] INSTALLED ATTACH ANGLE IAW SRM 51-40-02 AND DWG 146A7810; [09] VERIFIED CORRECTIVE ACTIONS STEP 8.

Part: INTERCOSTAL — CORRODED (BS 770) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON INTERCOSTAL AT AFT CARGO BAY WL 151 RBL 6 BS 770. ; / [01] REMOVED CORROSION FROM ACB LWR AUX SILL WEB AT BS 770 RBL6 MEASURED 7'L X 4'W AND 0.005' DEEP ORIGINAL THICKNESS OF 0.036' FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1; [02] CAL ID <BR>DIAL DEPTH GAUGE <BR>ATS1225; [03] REMOVED CORROSION FROM ACB LWR AUX SILL WEB AT BS 770 RBL6 MEASURED 7'L X 4'W AND 0.005' DEEP ORIGINAL THICKNESS OF 0.036' FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1; [04] VERIFIED CORRECTIVE ACTION 1;2 AND 3.; [05] REMOVED INTERCOSTAL AT AFT CARGO BAY WL 151 RBL 6 BS 770 IAW SRM 51-40-02; [06] REMOVED INTERCOSTAL AT AFT CARGO BAY WL 151 RBL 6 BS 770 IAW SRM 51-40-02; [07] RECEIVED WEB FROM OUTSIDE SERVICES PART NUMBER HFAB53-WB-011 PO#845215. LOCATED AND DRILLED WEB AT BS STA 767 TO BS STA 787. IAW DWG# 146A8131 SHT 12 REV B AND SRM 51-40 -05.; [08] VERIFIED CORRECTIVE ACTION 7. OKAY TO TREAT AND PRIME.; [09] APPLIED CHEMICAL CONVERSION AND PRIMER IAW SRM 51-20-01-0G-0.; [10] VERIFIED CORRECTIVE ACTION 9; [11] REQUEST OK TO INSTALL.; [12] REQUEST OK TO INSTALL.; [13] OKAY TO INSTALL; [14] INSTALLED WEB AT ABC WL 151 RBL 6 BS 767 TO 787 IAW DWG: 146A8130 ID: 0012 REV:B AND SRM 51-40-02.; [15] INSTALLED WEB AT ABC WL 151 RBL 6 BS 767 TO 787 IAW DWG: 146A8130 ID: 0012 REV:B AND SRM 51-40-02; [16] VERIFIED CORRECTIVE ACTIONS STEP 14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK WL 208, RBL 25, BS 548-727A+7. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1; STEP 4A. REMOVED THE SEAT TRACK CROWN, SEAT TRACK FABRICATED IAW DWG 144A5350 SH. 1. LOCATED AND DRILLED THE NEW SEAT TRACK IAW SRM 51-40-05-0G-0 AND DWG 144A5300. INSTALLED THE NEW SEAT TRACK IAW SRM 51-40-04-0G-0, 51-40-02-0G-0, AND DWG 144A5300.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

RT OVERWING EMERGENCY EXIT CUTOUT STRUCTURE IS CORRODED ON THE LWR SILL BS 619 - 638, RBL71, WL221. REMOVED RT LOWER SILL FLAPPER AND LOWER SILL SUPPORT ANGLE IAW SRM 51-40-02-0G-0. REMOVED FASTENERS ON THE FWD, MID AND AFT SILL RETAINERS IAW SRM 51-40-02-0G-0. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS PER SRM 53-40-15-1A-1. APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO BLENDED AREAS IAW SRM 53-40-15-1A-1 STEPS 2.C.(2)(3). INSTALLED FASTENERS AND LOWER SILL SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 144A8201. REINSTALLED THE LOWER SILL FLAPPER IAW SRM 51-40-02-0G-0.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CRACKED FLOOR PANEL SUPPORT AT PASSENGER CABIN BS540 RBL1 WL208. ; / [01] REMOVED CRACKED FLOOR PANEL SUPPORT AT PASSENGER CABIN BS540 RBL1 WL208. IAW SRM 51-40-02.; [02] MATCH DRILLED AND INSTALLED NEW FLOOR PANEL SUPPORT AT PASSENGER CABIN BS540 RBL 1 WL208 IAW SRM 51-40-02 AND SRM 51-40-05 AND BOEING DWG 143A0060; [03] VERIFIED; [04] VERIFIED ACTION 2

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK WL 208, RBL 45, BS 727B-887. REMOVED CORROSION ON THE SEAT TRACK. FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1. REMOVED THE SEAT TRACK IAW SRM 51-40-02-0G-0. FABRICATED A NEW SEAT TRACK IAW DWG 144A5330. LOCATED AND DRILLED THE SEAT TRACK IAW SRM 51-40-05-0G-0 AND DWG 146A5300. INSTALLED THE NEW SEAT TRACK IAW SRM 51-40-02-0G-0 AND DWG 146A5300.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK WL 208 RBL 45 BS 500B+10-500D. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1. REMOVED THE SEAT TRACK IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW SEAT TRACK IAW DWG 143A5300 AND SRM 51-40-05, INSTALLED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK WL 208, RBL 45, BS 537-727B. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1. REMOVED SEAT TRACK IAW SRM 51-40-02 FABRICATED A NEW SEAT TRACK IAW DWG 144A5350 SH. 2. LOCATED AND DRILLED THE NEW SEAT TRACK IAW SRM 51-40-05-0G-0 AND DWG 144A5300. INSTALLED THE NEW SEAT TRACK IAW SRM 51-40-04-0G-0; 51-40-02-0G-0, AND DWG 144A5300.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK BS727B - 887. LBL25 WL208. REMOVED CORROSION ON PASSENGER CABIN SEAT TRACK REWORK AREA AT WELL 5'X.90' MAX. DEPTH OF REWORK .021' AND FOUND OUT LIMITS IAW SRM 53-00-52-1A-1. REMOVED PASSENGER CABIN SEAT TRACK FROM BS727B TO BS887; LBL25; WL208 PER SRM 51-40-02-0G-0.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CRACKED FLOOR PANEL SUPPORT AT PASSENGER CABIN BS540 LBL1 WL208. ; / [01] REMOVED CRACKED FLOOR PANEL SUPPORT AT PASSENGER CABIN BS540 LBL 1 WL208. IAW SRM 51-40-02; [02] MATCH DRILLED AND INSTALLED NEW FLOOR PANEL SUPPORT AT PASSENGER CABIN BS540 LBL 1 WL208 IAW SRM 51-40-02 AND SRM 51-40-05 AND BOEING DWG 143A0060; [03] VERIFIED; [04] VERIFIED ACTION 2

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK WL 208, RBL 25, BS 727B+4-875. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1. REMOVED THE CABIN SEAT TRACK IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW SEAT TRACK IAW DWG 146A5300 AND SRM 51-40-02. INSTALLED THE NEW SEAT TRACK IAW SRM 51-40-02-0G-0; 51-40-04-0G-0 AND DWG 146A5300.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON PASSENGER CABIN SEAT TRACK BS493 - BS500+10; BS500A+4 - BS500B+2; BS500B+15 - BS500C+9 LBL45 WL208. MARKED ; / [01] REMOVED CORROSION ON PASSENGER CABIN SEAT TRACK BS 493 TO BS 500+10; LBL 45; WL 208; REWORK AREA AT WELL 17'X.90' MAX. DEPTH OF REWORK .009'; REWORK AREA AT CROWN 4.1'X.40' MAX. DEPTH OF REWORK .023' AND FOUND OUT LIMITS IAW SRM 53-00-52-1A-1. MEASUREMENT TOOLS #1 ID:ATS1737 S/N: UNKNOWN; DATE 07/2021; DUE 07/2022; #2 ID:ATS1225 S/N: UNKNOWN; DATE 07/2021; DUE 07/2022.; [02] CERTIFIED ACTION 1; [03] VERIFIED CORRECTIVE ACTION 1; [04] REMOVED FLOOR PANELS 231VF; 231HF; 231JF; 231LF; 231MF IAW AMM 53-21-00-000-801; [05] REMOVED 1EA BOLT IN AFT PIVOT LINK AT BS 540 LBL45 WL206 IAW SRM 51-40-02-0G-0;[08] VERIFIED SEAT TRACK FABRICATION WITH BOEING DRAWING 143A5310; REFER TO ATS BUILD RECORDS ON CUSTOMER RO NO ATSHFAB-100-303 JOB NUMBER 538467.; [09] CERTIFIED STEP 7 AND 8; [10] VERIFIED CORRECTIVE ACTIONS STEP 7;8.; [11] LOCATED AND DRILLED NEW SEAT TRACK AT BS480-520 LBL 45 WL 208 IAW DWG 143A5300 AND SRM 51-40-05.; [12] VERIFIED CORRECTIVE ACTION STEP 11.; [13] OK TO INSTALL SEAT TRACK BS 480 TO 520 LBL 45 WL 208.; [14] VERIFIED IT IS OK TO INSTALL NEW SEAT TRACK AT BS 480 - BS 520; LBL 45; WL 208.; [15] PARTIAL INSTALLED CABIN SEAT TRACK BS 480 TO 520 LBL 45 WL 208 IAW B737 SRM 51-40-02-0G-0; SRM 51-40-04-0G-0 AND DRAWING 143A5300.;

Part: SEAT TRACK — CORRODED (BS 520-532) · airframe 52,876 hrs · 31,083 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK WL 208 RBL 25 BS 520-532. ; / [01] REMOVED CORROSION ON SEAT TRACK CROWN BS 532 ; WORK AREA 1.0' X 0.250'X 0.024 ; FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1; STEP 4A (2); TOOLS USED DEPTH GAGE ID: ATS400; S/N UNKNOWN ; DUE 08/22 ; DEPTH GAGE ID: ATS1737; S/N UNKNOWN ; DUE 07/2022; [02] CERTIFY; [03] REMOVED CORROSION ON SEAT TRACK CROWN BS 520 TO 532. DEEPEST BLENDOUT IS 1.0' X 0.250'X 0.024' ; FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1; STEP 4A (2); TOOLS USED DEPTH GAGE ID: ATS400; S/N UNKNOWN ; DUE 08/22 ; DEPTH GAGE ID: ATS1737; S/N UNKNOWN ; DUE 07/2022; [04] VERIFIED CORRECTIVE ACTION 1-3.<BR><BR>FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1; [05] REMOVED AND REPLACED SEAT TRACK AT BS 520-532 RBL 25 WL 208 IAW SRM 51-40-02-0G-O; SRM 51-40-04-0G-0; AND DWG 413A0060.; [06] VERIFIED CORRECTIVE ACTION STEP 5.; [07] TASK COMPLETE

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,876 hrs · 31,083 cycles

SUPPLEMENTAL INFORMATION: CORROSION ON PASSENGER CABIN SEAT TRACK WL 208 RBL 25 BS 481-489; BS 500+7-500A+2; BS 500A+15-500B+13; BS 500C+6-500D+10; BS 500D+15-520. ; / CORROSION DEFECT FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1VERIFIED SEAT TRACK FABRICATION IAW BOEING DRW 143A5310. REFER TO ATS BUILD RECORDS ON RO NO ATSHFAB-100-310 JOB # 524393 INSTALLED SCREWS IN SEAT TRACK FLANGES BOTH INBOARD AND OUTBOARD AT RBL 25 BS 480 TO 520 IAW SRM 51-40-02-0G-0 LOCATE AND DRILLED NEW SEAT SEATRACK BS 480 TO 520 RBL 25 WL 208 PER SRM 51-40-05-0G-0 INSTALLED NEW SEAT TRACK RBL 25 WL 208 BS 480 TO BS 520 PER SRM 51-40-02-0G-0 AND DRW # 143A5300 HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16, NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071 EQUIP ID#: ATS2407 S/N: MM1591DD064104 REINSTALLED FASTENERS IN SEAT TRACK BS 500C AND 500D RBL 25 WL 208 PER SRM 51-40-02-0G-0 PENDING ENGINEERING APPROVAL. VERIFIED INSTALLATION OF FASTENERS IN SEAT TRACK BS 500C AND 500D RBL 25 WL 209 PER SRM 51-40-02 PENDING ENGINEERING APPROVAL CORRECTION: FLOOR PANELS #231AAF AND 231RF ARE NOT EFFECTIVE FOR A 737-700 A/C. FLOOR PANELS ACTUALLY REMOVED WERE 231GF AND 231KF IAW SRM 51-40 02 INSTALLED FLOOR PANELS 231GF AND 231KF IAW AMM 53-21-00-400-801 PRIOR TO FLOOR PANEL INSTALLATION, VERIFIED INSTALLATION OF SEAT TRACK RBL 25 WL 208 BS 480 TO BS 520 PER SRM 51-40-02-0G-0 AND DRW # 143A5300

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,876 hrs · 31,083 cycles

EMERGENCY EXIT LIGHTS R/H GROUND ILLUMINATION LIGHT IS INOP. ; EMERGENCY EXIT LIGHTS RH GROND ILLMINATION LIGHT IS INOP. RE-LAMPED AND PERFORMED GOOD OPS TEST OF R/H GROUND ILLUMINATION LIGHT PER AMM 33-51-04-960-801. VERIFIED CORRECTIVE ACTIONS STEP 1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,876 hrs · 31,083 cycles

EMERGENCY EXIT LIGHTS AFT ENTRY DOOR SLIDE LIGHT IS INOP. / [01] RELAMPED EMERGENCY EXIT LIGHT AFT ENTRY DOOR LIGHT AND PERFORMED GOOD INSTALLATION TEST AS PER AMM. 33-51-04-960-801; [02] VERIFIED CORRECTIVE ACTION STEP 1.

Part: SEAT TRACK — OUT OF LIMITS (COCKPIT) · airframe 52,602 hrs · 30,916 cycles

F/O'S AFT I/B SEAT TRACK IS OUT OF LIMITS. / REMOVED AND REPLACED F/O'S AFT I/B SEAT TRACK PER AMM 25-11-11.

Part: SEAT TRACK — OUT OF LIMITS (COCKPIT) · airframe 52,602 hrs · 30,916 cycles

CAPT'S AFT I/B SEAT TRACK IS OUT OF LIMITS. / REMOVED AND REPLACED CAPT'S AFT I/B SEAT TRACK PER AMM 25-11-11.

Part: BATTERY — FAILED (CABIN) · airframe 50,561 hrs · 29,542 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 50,561 hrs · 29,542 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 50,561 hrs · 29,542 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 50,561 hrs · 29,542 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 50,561 hrs · 29,542 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PER MM.

Part: RETAINER — CRACKED (LT WING) · airframe 50,561 hrs · 29,542 cycles

LEFT WING UPPER FIXED TRAILING EDGE PANEL SEAL BRACKET CRACKED / R&R LEFT WING UPPER FIXED TRAILING EDGE PANEL SEAL BRACKET PER SRM 51-40-02 AND AMM 20-50-11

Part: BATTERY — FAILED (CABIN) · airframe 50,561 hrs · 29,542 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1674. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 50,561 hrs · 29,542 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PER MM.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 48,985 hrs · 28,533 cycles

RUDDER COUNTER BALANCE WEIGHT CORRODED / REMOVED AND INSTALLED SERVICEABLE RUDDER COUNTER BALANCE WEIGHT IAW CMM 55-40-09. REINSTALLED SURROUNDING PANELS AND RETAINERS IAW SRM 51-40-02. CLEARANCE CHECK OF WRAP AROUND SEALS ON RUDDER WEIGHT GOOD IAW M/M 27-21-11

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 48,985 hrs · 28,533 cycles

AFT CARGO COMPARTMENT LH #2 AND #3 CAP STRIPS HAVE CORROSION ON BACKSIDE. / LEFT SIDE #2 AND #3 CAP STRIP REMOVED AND REPLACED #2 P/N 453A2611-10 STATION 747 TO 772+5 CAP #3 P/N 453A2611-4 STATION 772+5 TO 847 PER SRM 51-40-02

Part: PLATE — CRACKED (L/H WING) · airframe 48,985 hrs · 28,533 cycles

REAR SPAR IB WIGGLE PLATE WBL 201 AT PANEL 551GB CRACKED. / REMOVED AND REPLACED REAR SPAR IB WIGGLE PLATE WBL 201 AT PANEL 551GB PER SRM 51-40-40; SEE WIP AND SUBTASK FOR INDIVIDUAL SIGNOFFS

Part: PANEL — ELONGATED (LT WING) · airframe 48,985 hrs · 28,533 cycles

LEFT WING LEADING EDGE PANEL 521QB HAS ELONGATED FASTENER HOLE. / REPAIRED FASTENER HOLE PER SRM 51-70-04 REPAIR 9. RESIN SEALED AREA PER SRM 51-70-08 AND RESTORED FINISH PER AMM 51-21-99.

Part: ANGLE — CRACKED (LT WING) · airframe 48,985 hrs · 28,533 cycles

LEFT WING; ANGLE ATTACHED TO THE INBD. DEFLECTION RIB IS CRACKED. MARKED / REMOVED AND REPLACED LEFT WING ANGLE ATTACHED INBOARD OF DEFLECTION RIB TO T/E SEAL RETAINERS PER SRM 51-40-02.

Part: SLAT TRACK — ELONGATED (L/H WING) · airframe 48,985 hrs · 28,533 cycles

LEFT WING. APROX. FSS 400. ELONGATED HOLE IN PANEL LANDING (AFT EDGE). JUST OUTBD OF #3 INBD SLAT TRACK. MARKED / REPAIRD PER EA. 1-757-15830

Part: SKIN — WORN (FUSELAGE) · airframe 48,984 hrs · 28,533 cycles

FUSELAGE UPPER CROWN SKIN WORN FROM DORSAL FIN SEAL BETWEEN BS 847 TO BS 847+3, STR 1R. REPAIRED SKIN PER EA.

Part: ANGLE — CRACKED (LH WING) · airframe 48,985 hrs · 28,533 cycles

LH WING IB UPPER WING PANEL (551AT) SUPPORT ANGLE CRACKED IB AND ABOVE #1 TANK AFT BOOST PUMP (MARKED) / REMOVED AND REPLACED ANGLE PER SRM 51-40-02

Part: RETAINER — CRACKED (LH WING) · airframe 48,985 hrs · 28,533 cycles

LH WING TE FLAP WELL AFT SEAL RETAINER CRACKED OB #3 FLAP TRACK (MARKED) / REMOVED & REPLACED SEAL RETAINER PER SRM 51-40-02.

Part: RETAINER — CRACKED (LH WING) · airframe 48,985 hrs · 28,533 cycles

LH WING TE FLAP WELL FWD SEAL RETAINER CRACKED OB #3 FLAP TRACK (MARKED) / REMOVED SEAL BRACKET; REPLACED CRACKED SEAL RETAINER; AND RE-INSTALLED SEAL BRACKET PER SRM 51-40-02.

Part: PANEL — CRACKED (LH WING) · airframe 48,985 hrs · 28,533 cycles

LEFT WING; LEADING EDGE PANELS 521DB HAS CRACKED CORNER. MARKED / REPAIRED DAMAGE IAW SRM 57-41-01-2R-1; SEE NON-ROUTINE FOR INDIVIDUAL SIGN OFFS.

Part: ACCESS DOOR — BROKEN (FUSELAGE) · airframe 48,985 hrs · 28,533 cycles

GROUND AIR ACCESS DOOR 191E HAS BROKEN HINGES. / REMOVED AND REPLACED DOOR ASSY PER SOPM 20-50-01

Part: PLATE — CRACKED (L/H WING) · airframe 48,985 hrs · 28,533 cycles

LH WING REAR SPAR LWR CHORD WAFFLE PLATE CRACKED IB OF #3 FLAP TRACK (MARKED) / REMOVED AND REPLACED LH WING REAR SPAR LWR CHORD WAFFLE PLATE IB OF #3 FLAP TRACK PER SRM 51-40-02.

Part: SKIN — CRACKED (LE SLAT) · airframe 48,984 hrs · 28,533 cycles

RT WING NR 8 SLAT LOWER LEADING EDGE SKIN ACTUATOR ATTACH POINT CRACKED AROUND FASTENER HOLE. R&R SKIN PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 47,995 hrs · 27,914 cycles

L1 DOOR SLIDE OUT OF ADJUST. R&R SLIDE IAW MT.

Part: SKIN — DAMAGED (LT WING SLAT) · airframe 46,680 hrs · 27,054 cycles

NR 3 L/E SLAT HAS A CREASE ON UPPER SURFACE AT OTBD AUX TRACK CUTOUT. R & R THE SLAT IAW MM.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 46,529 hrs · 26,958 cycles

FWD CARGO COMPARTMENT; FWD CORNER SECTION SCUFF PLATE IS CRACKED. / REMOVED AND REPLACED FWD SCUFF PLATE REF AMM 53-11-02.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 45,457 hrs · 26,283 cycles

R2 DOOR EMERGENCY LIGHT LENS MISSING. / INSTALLED LENS PER MM.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,418 hrs · 25,614 cycles

RIGHT OVERWING EXIT LIGHT INOPERATIVE. R & R THE FUSE IAW AMM.

Part: LIGHT — DELAMINATED (CABIN) · airframe 44,353 hrs · 25,568 cycles

RT CABIN FLOOR ESCAPE PATH LIGHTING STRIP DELAMINATED AT ROW 1. R&R LIGHT PER DWG.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 44,047 hrs · 25,383 cycles

UPPER RH SLIDER SEAL IS CRACKED AT THE FWD TRACK / REMOVED AND REPLACED SLIDING SEAL RH HORIZ STAB PER AMM 53-31-31

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 42,763 hrs · 24,614 cycles

LEFT CENTER EXIT SIGN LENS LOOSE. SECURED THE LENS IAW SIP.

Part: BAFFLE — CRACKED (AFT CARGO) · airframe 48,965 hrs · 28,524 cycles

FWD CARGO BAY; BAFFLE CRACKED AT BS 500 LBL 25 W/L 156 ; / [01] NOT FOUNDED LIMITS FOR CRACK ON SRM REPLACE PART FOR REPAIR IAW SRM 51-10-02; [02] REMOVED BAFFLE AT FCB BS.500 TO 500A LBL.25 WL 156 IAW SRM 51-40-02; [03] FABRICATED BAFFLE FROM MAT.7075-T6 .020' LOT. 1460998-1 LOCATED; DRILLED AND APPLIED CHEMICAL CONVERSION COATING IAW BOEING DWG 143A7510 REV:B AND SRM 51-40-05 OK TO PRIMER; [04] APPLIED PRIMER AT BAFFLE IAW BOEING DWG 143A7510 REV:B AND AMM 51-21-72-370-804; OK TO INSTALL; [05] APPLIED PRIMER AND INSTALL NUT PLATE AT BAFFLE IAW BOEING DWG 143A7510 REV:B AND AMM 51-21-72-370-804; OK TO INSTALL; [06] PRIOR TO PRIMER APPLICATION; VERIFIED FABRICATION OF BAFFLE AND APPLICATIONOF CHEMICAL CONVERSION COATING PER DWG 143A7510 AND SRM 51-40-05. OK GIVEN TO PRIMER. VERIFIED APPLICATION OF PRIMER PER DWG 143A7510 AND AMM 51-21-72-370-804. OK TO INSTALL.; [07] INSTALLED FCB BAFFLE BS 500-500A; LBL 25; WL 156 PER SRM 51-40-02; DWG# 143A7505.; [08] VERIFIED CORRECTIVE ACTIONS STEP 7.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,244 hrs · 24,306 cycles

R2 DOOR EXTERIOR EMERGENCY EGRESS LIGHT INOP. R&R LAMP IAW AMM AND WDM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,244 hrs · 24,306 cycles

R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY CHARGER IAW MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 42,244 hrs · 24,306 cycles

G1 GALLEY MOUNTED EMERGENCY LIGHT COVER BROKEN. R & R THE COVER IAW MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 42,244 hrs · 24,306 cycles

FORWARD LAVATORY MOUNTED EMERGENCY EXIT SIGN COVER BROKEN. R & R THE COVER IAW MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 42,244 hrs · 24,306 cycles

AFT LAVATORY MOUNTED EMERGENCY LIGHT COVER BROKEN. R & R THE COVER IAW MM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 42,244 hrs · 24,306 cycles

G4 GALLEY MOUNTED EMERGENCY EXIT LIGHT COVER BROKEN. R & R THE COVER IAW MM.

Part: ANGLE — CRACKED (FWD CARGO) · airframe 42,244 hrs · 24,306 cycles

ANGLE CRACKED AT BS 500C, WL 208. R & R THE ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME IAW EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 42,244 hrs · 24,306 cycles

LT WING FIXED UPPER TRAILING EDGE PANEL AT SAIL TAIL UPPER CENTER SUPPORT ANGLE CRACKED IN RADIUS. R&R ANGLE IAW SRM AND DWG.

Part: ATTACH FITTING — CORRODED (L1 DOOR) · airframe 42,244 hrs · 24,306 cycles

L1 DOOR EMERGENCY EVAC SLIDE FORWARD GIRT BAR ATTACH FITTING CORRODED AT FASTENER HOLES. R&R FITTING IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

FRAME CRACKED AT BS 500A, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

FRAME WEB CRACKED AT BS 787, STR 8L. REPAIRED FRAME WEB IAW EA.

Part: FRAME — CRACKED (BS 907) · airframe 42,244 hrs · 24,306 cycles

FUSELAGE FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

FRAME CRACKED AT BS 440, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

FORWARD CARGO COMPARTMENT STRINGER CLIP CRACKED AT BS 460, STR 28L. R&R CLIP IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

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

Part: ANGLE — CORRODED (BS 500A) · airframe 42,244 hrs · 24,306 cycles

ANGLE CORRODED AT BS 500A, STRINGER 26R. R & R THE ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

FORWARD CARGO COMPARTMENT LT Z-ANGLE CORRODED BETWEEN BS 500 TO BS 500D, STR 26L. R&R Z ANGLE IAW SRM.

Part: STRUCTURE — CRACKED (BS 540) · airframe 42,244 hrs · 24,306 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

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

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

AFT PIT LT Z ANGLE CORRODED BETWEEN BS 727E TO BS 747. R&R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

AFT PIT RT Z ANGLE CORRODED AT BS 727D+15. R&R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,244 hrs · 24,306 cycles

AFT PIT RT Z ANGLE CORRODED BETWEEN BS 747 TO BS 767. R&R Z ANGLE IAW SRM.

Part: SIGN — UNSECURE (CABIN) · airframe 42,099 hrs · 24,210 cycles

R1 DOOR LOWER EXIT SIGN POPPED OFF. SECURED SIGN PER SIP.

Part: SKIN — CRACKED (ACCESS PANEL) · airframe 41,609 hrs · 23,928 cycles

EXTERNAL ACCESS DOOR OPENING AT LOWER AFT CORNER CRACKED. REPAIRED CUTOUT IAW SRM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 39,841 hrs · 22,937 cycles

L1 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: COVER — MISSING (CABIN) · airframe 38,592 hrs · 22,208 cycles

AFT GALLEY EMER EXIT LIGHT COVER MISSING. INSTALLED COVER IAW SIP.

Part: LENS — BROKEN (CABIN) · airframe 38,026 hrs · 21,884 cycles

RIGHT OVERWING EMER EXIT SIGN LIGHT LENS BROKEN. R & R LENS IAW MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 37,984 hrs · 21,854 cycles

RIGHT WING OTBD AFT FLAP, INBD AFT CORNER DELAMINATED. REPAIRED AFT FLAP IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,984 hrs · 21,854 cycles

R1 DOOR EMER LIGHT INOPERATIVE. R & R LAMP IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 37,984 hrs · 21,854 cycles

BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R & R BATTERY IAW MM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 37,984 hrs · 21,854 cycles

RIGHT WING UPPER TE SHELF, BETWEEN NR 7 & 8 SPOILERS, AFT SUPPORT BRACKET CRACKED AT OTBD ATTACH FASTENER. R & R SUPPORT BRACKET IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,007 hrs · 21,300 cycles

LEFT OVERWING EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: BATTERY — FAILED (FLASHLIGHT) · airframe 36,435 hrs · 20,973 cycles

AFT EMER FLASHLIGHT FAILED TEST. R & R BATTERY IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

STRINGER CLIP CRACKED AT BS 460, STRINGER 19L. R & R CLIP PER SRM & DWG.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

STRINGER CRACKED AT BS 336.5, STRINGER 5R. R & R STRINGER IAW SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

STRINGER CRACKED AT BS 348.2, STRINGER 5R. REPAIRED STRINGER IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727B, LBL 46.5. REPAIRED FLANGE IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

LEFT FLIGHT DECK NR 1 WINDOW FRAME CRACKED ON INNER SURFACE F UPPER OTBD CORNER APPROX 100". REPAIRED FRAME IAW ACO.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727A+18, RBL 46.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727A, RBL 23.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727A+19, LBL 25.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727A+19, RBL 25.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727A+18, RBL 25.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727A+18, LBL 23.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727A+18, LBL 46.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727A+19, RBL 44.5. REPAIRED FLANGE IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 36,012 hrs · 20,735 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 33. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 36,012 hrs · 20,735 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 43. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727A+18, LBL 25.5. REPAIRED FLANGE IAW EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 36,012 hrs · 20,735 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727A+19, LBL 44.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727A+19, RBL 23.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727A+19, RBL 46.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 36,012 hrs · 20,735 cycles

MAIN CABIN FLOORBEAM SEAT TRACK FLANGE CRACKED AT BS 727A, LBL 44.5, HOLE D. REPAIRED FLANGE IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 36,012 hrs · 20,735 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 41. REPAIRED WEB IAW SRM.

Part: FITTING — LOOSE (R1 DOOR) · airframe 34,909 hrs · 20,108 cycles

R1 DOOR LOOSE AT UPPER RT CORNER. R & R LATCH FITTING IAW MM.

Part: TIRE — SEPARATED (LT MLG) · airframe 34,387 hrs · 19,793 cycles

AIR TURN BACK, DECLARED EMER. LOST NR 3 TIRE CAP & PRESS LOSS ON TAKEOFF DAMAGING SEVERAL COMPONENTS. R & R NR 3 MAIN WHEEL TIRE ASSEMBLY IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 33,523 hrs · 19,311 cycles

LEFT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY CHECK BETWEEN ROW 1 TO ROW 4. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 33,523 hrs · 19,311 cycles

AFT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED CAPACITY CHECK FAILED AT ROW 17. R & R BATTERY PACK IAW AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 32,891 hrs · 18,948 cycles

LEFT WING OTBD TE FLAP DELAMINATED. R & R FLAP IAW MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 32,882 hrs · 18,945 cycles

RIGHT MLG FWD TRUNNION FITTING LUG FACES CORRODED. R & R FITTING IAW EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 32,882 hrs · 18,945 cycles

LT MLG FWD TRUNNION FITTING LUG FACES CORRODED. R & R FITTING IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 31,680 hrs · 18,231 cycles

LT OVERWING EXIT LIGHT LENS BROKEN. R & R LT OVERWING EXIT LIGHT LENS IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 31,204 hrs · 17,956 cycles

LT EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK BETWEEN ROW 1 TO ROW 4. R & R BATTERY IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 30,501 hrs · 17,536 cycles

CENTER CABIN CEILING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN IAW SIP.

Part: LIGHT — BROKEN (CABIN) · airframe 30,413 hrs · 17,489 cycles

FORWARD ENTRY FLOOR EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R&R LIGHT ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,121 hrs · 16,753 cycles

EMERGENCY EXIT LIGHT AT AFT SIDE OF RIGHT OVERWING BULB INOP. RELAMPED LIGHT PER MM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 29,122 hrs · 16,753 cycles

FLOOR SUPPORT WEB CRACKED BETWEEN STA 328 TO STA 344, LBL 47. REMOVED AND REPLACED WEB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 29,122 hrs · 16,753 cycles

FLOOR SUPPORT WEB CRACKED BETWEEN STA 312 TO STA 328, RBL 30. REMOVED AND REPLACED WEB PER SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 29,122 hrs · 16,753 cycles

FLOOR SUPPORT WEB CRACKED BETWEEN STA 312 TO STA 328, LBL 47. REMOVED AND REPLACED WEB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 29,122 hrs · 16,753 cycles

RIGHT HORIZ STAB RIB AT STA 92.7 IS CRACKED AT FWD UPPER I/B CORNER. REPAIRED RIB IAW EA AND ER.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 29,122 hrs · 16,753 cycles

CORROSION AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 887-907, RBL 20. REMOVED AND REPLACED ZEE CHANNEL IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 29,122 hrs · 16,753 cycles

CORROSION AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BETWEEN BS 747 TO BS 767, RBL 20. REMOVED AND REPLACED SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 29,122 hrs · 16,753 cycles

RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 438 ON UPPER SURFACE. REMOVED AND REPLACED SUPPORT PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,122 hrs · 16,753 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR STAB STA 95.2 - 98.7. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,122 hrs · 16,753 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED I/B SIDE OF RIB STAB STA 184.70, 8.25-8.5" FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,122 hrs · 16,753 cycles

RIGHT HORIZ STAB LOWER SKIN CRACKED I/B SIDE OF RIB STAB STA 101.9, 18-19" FROM REAR SPAR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,122 hrs · 16,753 cycles

RIGHT HORIZONTAL STAB LOWER SKIN CRACKED AT REAR SPAR STAB STA 133 - 134.5. REPAIRED SKIN PER SRM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 29,122 hrs · 16,753 cycles

AFT CARGO BAY DOOR CUTOUT, FWD SCUFF PLATE, IS BROKEN AND CRACKED AT MULTIPLE LOCATIONS OF UPPER AND LOWER FLANGE. REPAIRED PLATE IAW EA.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 29,122 hrs · 16,753 cycles

LEFT HORIZ STAB RIB AT STAB STA 92.5 2ND AND 3RD VERTICAL STIFFENERS ARE CRACKED. REPAIRED STIFFENERS PER SRM AND AMM.

Part: WEB — CORRODED (FUSELAGE) · airframe 29,122 hrs · 16,753 cycles

CORROSION AFT CARGO BAY DOOR SURROUND SUB THRESHOLD WEB IS CORRODED ON UPPER SURFACE IN MULTIPLE LOCATIONS AT BODY STATION 794 TO 847. REMOVED AND REPLACED WEB SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 29,122 hrs · 16,753 cycles

CORROSION LEFT FLOOR TO SIDEWALL SUPPORT HAS CORROSION ON UPPER SURFACE AT NUT PLATE HOLES BETWEEN BS 500 AND BS 500C. REPAIRED SUPPORT PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,122 hrs · 16,753 cycles

LEFT HORIZONTAL STAB LOWER SKIN CRACKED I/B SIDE OF RIB STAB STA 129.5, 24.5-24.75" FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 29,122 hrs · 16,753 cycles

AFT CARGO BAY DOOR CUTOUT, AFT SCUFF PLATE, BROKEN AND CRACKED AT MULTIPLE LOCATIONS OF UPPER AND LOWER FLANGE. REPAIRED SCUFF PLATE PER EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 29,122 hrs · 16,753 cycles

RIGHT HORIZ STAB RIB AT STAB STA 92.5 (2ND, 3RD AND FOURTH) VERTICAL STIFFENERS CRACKED. REPAIRED STIFFENERS PER SRM.

Part: TEE FITTING — CRACKED (LT WING) · airframe 28,944 hrs · 16,643 cycles

LEFT WING, T-ANGLE BRACKET CRACKED OUT, JUST OUTBOARD OF NR 3 FLAP TRACK, WHERE THE STAND OFF ATTACHES (MARKED). REMOVED AND REPLACED T- ANGLE IAW SRM 51-10-02.

Part: LENS — LOOSE (R2 DOOR) · airframe 27,871 hrs · 16,026 cycles

R2 DOOR EMERGENCY EVAC SLIDE COVER LENS LOOSE. SECURED LENS PER M/M.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,871 hrs · 16,026 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 138.70. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 27,871 hrs · 16,026 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER M/M.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 27,871 hrs · 16,026 cycles

LEFT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 129.50. REPAIRED STABILIZER PER SRM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 27,871 hrs · 16,026 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT BAR STOW HOOK LOOSE. SECURED HOOK PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 26,722 hrs · 15,407 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN SURFACE CRACKED BETWEEN STA 97 TO STA 101. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,701 hrs · 14,839 cycles

L1 DOOR EXTERIOR EGRESS LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,701 hrs · 14,839 cycles

LT EGRESS FLOOR TRACK LIGHT INOP AT ROW 10. RELAMPED LIGHT IAW MM.

Part: LENS — MISSING (CABIN) · airframe 25,542 hrs · 14,743 cycles

FLOOR TRACK LIGHTING LENS MISSING AT 15 ABC. INSTALLED LENS PER M/M.

Part: COVER — MISSING (CABIN) · airframe 25,216 hrs · 14,553 cycles

EEPLS COVER MISSING AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 24,654 hrs · 14,233 cycles

LEFT EEPLS LOOSE AT ROW 1. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,922 hrs · 13,818 cycles

DURING SCHEDULED MV2 CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT INOP AT R1 DOOR. RELAMPED PER MM.

Part: LENS — BROKEN (CABIN) · airframe 22,056 hrs · 12,762 cycles

DURING SCHEDULED 6Y CHECK, FOUND LT EEPLS LENS BROKEN AT ROW 16. REMOVED AND REPLACED LENS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 22,056 hrs · 12,762 cycles

DURING SCHEDULED 6Y CHECK, FOUND EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 22,094 hrs · 12,789 cycles

L1 DOOR GIRT BAR DIFFICULT TO INSTALL. REPOSITIONED L1 DOOR GIRT BAR PER MT.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 22,094 hrs · 12,789 cycles

L1 DOOR GIRT BAR DIFFICULT TO INSTALL. REPOSITIONED L1 DOOR GIRT BAR PER MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 22,083 hrs · 12,781 cycles

DIFFICULT ATTACHING L1 DOOR SLIDE ASSY GIRT BAR. REPOSITIONED L1 DOOR SLIDE GIRT PER MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 22,056 hrs · 12,762 cycles

DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO COMPARTMENT Z-ANGLE CORRODED BETWEEN BS 767 TO BS 727E, LBL 22. REPAIRED Z-ANGLE PER SRM.

Part: LENS — OUT OF POSITION (CABIN) · airframe 22,055 hrs · 12,762 cycles

RT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. RE-INSTALLED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 20,912 hrs · 12,066 cycles

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

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 20,762 hrs · 11,984 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: LENS — BROKEN (CABIN) · airframe 20,762 hrs · 11,984 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 19,763 hrs · 11,393 cycles

LT EEPLS LOOSE AT ROW 1. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,635 hrs · 11,316 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS INOP. RELAMPED PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 19,420 hrs · 11,209 cycles

FWD BULKHEAD LOWER EMERGENCY LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 18,416 hrs · 10,625 cycles

FWD EEPLS LOOSE. SECURED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,942 hrs · 10,353 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP AT ROW 1. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,065 hrs · 9,810 cycles

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

Part: LENS — MISSING (CABIN) · airframe 16,415 hrs · 9,438 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 5. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,415 hrs · 9,438 cycles

DURING SCHEDULED MV2 CHECK, FOUND AFT EEPLS INOP. R&R EEPLS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 14,991 hrs · 8,594 cycles

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

Part: LENS — CRACKED (CABIN) · airframe 14,991 hrs · 8,594 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED BETWEEN ROW 22 TO ROW 8. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 12,625 hrs · 7,188 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — MISSING (CABIN) · airframe 12,487 hrs · 7,108 cycles

EEPLS LENS MISSING AT RT OVERWING EXIT. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 12,117 hrs · 6,593 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 11,283 hrs · 6,373 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 8,859 hrs · 4,900 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 5,780 hrs · 3,177 cycles

FOUND EEPLS LIGHT COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LIGHT COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,913 hrs · 2,683 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 4,906 hrs · 2,679 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 4,042 hrs · 2,204 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRACK LENS MISSING AT FWD END. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 3,093 hrs · 1,702 cycles

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