N7835A

Part: SLIDE — DISLODGED (ZONE 800) · airframe 65,581 hrs · 35,014 cycles

FWD ENTRY SLIDE FALLING OUT OF CASE. REPOSITIONED L1 DOOR SLIDE AS REQUIRED PER TASK CARD 725-61-06. AIRCRAFT OK FOR SERVICE.

Part: HANDLE — LOOSE (ZONE 800) · airframe 65,549 hrs · 34,991 cycles

FWD ENTRY DOOR UPPER ASSIST HANDLE LOOSE. RESECURED FWD ENTRY DOOR UPPER ASSIST HANDLE IAW AMM 20-50-11.

Part: FUSE — INOPERATIVE (ZONE 200) · airframe 65,200 hrs · 34,769 cycles

SIDEWALL LIGHTS AT ROWS 13 14 &15 DEF DO NOT ILLUMINATE. REMOVED AND REPLACED WINDOW LIGHT FUSE IAW AMM 33-21-00. OPS CHECK GOOD.

Part: SKIN — CORRODED (ZONE 100) · airframe 64,328 hrs · 34,217 cycles

CORROSION ON SKIN UNDER WASTE PAN STA 847 TO STA 867 BETWEEN STR23L TO STR 25L<[01] REPAIRED PER EA 25-153-01658 WITH AN INSPECTION THRESHOLD DEFINED IN 25-153-01658-DT;[02] VERIFIED <BR>REPAIRED PER EA 25-153-01658 WITH AN INSPECTION THRESHOLD DEFINED IN 25-153-01658-DT

Part: SERVICE PANEL — CORRODED (ZONE 100) · airframe 64,328 hrs · 34,217 cycles

POSSIBLE CORROSION AT STA 850 AT THE WASTE TANK SERVICE PANEL ALONG STRINGER 25L.<[01] REMOVED AND REPLACED WASTE TANK SERVICE PAN ASSY IAW B737 SRM 51-40-02 AND BOEING DWG#DWG 146A7400-16#B ID:22;[02] 02 - INSPECTED PER B737 SRM 51-40-02 AND BOEING DWG# 146A7400-16#B.;[03] 02 -RII INSPECTED PER B737 SRM 51-40-02 AND BOEING DWG# 146A7400-16#B.;[04] 02 - INSPECTED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]

Part: SLIDE — OUT OF POSITION (ZONE 800) · airframe 64,209 hrs · 34,148 cycles

PAX CABIN LEFT AND RIGTH AFT DOORS SLIDE COVER RUBBING AGAINST TO SCUFF PLATE WHEN THE DOOR IS GOING TO CLOSE POSITION 2025-298158<[01] INSTALLED CORRECTLY LEFT AND RIGTH AFT DOORS SLIDE COVER IAW MT 725-61-06-EA-SW AND MT 725-61-06-SA-SW;[02] INSTALLED CORRECTLY LEFT AND RIGTH AFT DOORS SLIDE COVER IAW MT 725-61-06-EA-SW AND MT 725-61-06-SA-SW

Part: ANGLE — CRACKED (ZONE 300) · airframe 64,212 hrs · 34,149 cycles

CRACK ON CLOSURE ANGLE EXISTING REPAIR LOCATED AT BS1104 MORE 6 INCH AND BTW STR2L TO STR3L AT UPPER FUSELAGE. REPAIRED CLOSURE ANGLE LOCATED BETWEEN BS1104 MORE 6 INCH AND BS1156 AND BTW STR2L TO STR3L AT UPPER FUSELAGE IAW B737-700 SRM 53-80-71-2R-6 REPAIR 6.

Part: ANGLE — CRACKED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CRACK BILGE AREA ANGLE ON BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT 2025-298069<[01] REPLACED ANGLE BILGE AREA BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DWG 143A7902 SHET 126 REV A. SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED ANGLE BILGE AREA BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DWG 143A7902 SHET 126 REV A. SEE INDIVIDUAL SIGNOFF BELOW.

Part: SKIN — CRACKED (ZONE 300) · airframe 64,212 hrs · 34,149 cycles

CRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.980 INCHES 2025-298037<[01] TOOL USED ON STEP 3: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 22-JAN-26.;[02] EQUIPMENT P/N PHASEC 3D; S/N 800YBRK; DUE DATE 16-JUL-25 WAS USED ON STEP 6;[03] PERFORMED REPAIR ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL LOCATED AT STAB 193.90 RIB; 17.5 INCHES FROM FRONT SPAR I.A.W. B737-700 SRM: 55-10-01-2R-11. REPAIR 11. SEE INDIVIDUAL SIGNS OFF BELOW;[04] CERTIFIED ACTION 3; COMPLETED <BR>RII

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CORROSION BILGE AREA SHEAR PLATE BTW BS 492 TO BS 500A AT LEVEL STR 26R AND RBL 21 AT FWD CARGO COMPARTMENT. REPLACED SHEAR PLATE BTW BS 492 TO BS 500A AT LEVEL STR 26R AND RBL 21 AT FWD CARGO AND NEW FASTENERS IAW B737-700 SRM 51-40-02-0G-0 AND DWG 143A0080 SHEET:23 REV:-.

Part: WEB — CRACKED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CRACK FLOOR STRUCTURE WEB BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT. REPLACED FLOOR STRUCTURE WEB BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT AFT CARGO COMPARTMENTAND FASTENERS IAW SRM 51-40-02-0G-0 AND DWG 147A7500 SHEET: 25 REV:- .

Part: ANGLE — CRACKED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CRACK BILGE AREA ANGLE BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT. IAW B737-700 SRM:51-40-02 AND DWG 147A7221 SHEET: 24 REV -.

Part: STRINGER — CRACKED (ZONE 600) · airframe 64,212 hrs · 34,149 cycles

CRACK STRINGER 9 INTERNAL AREA FUEL TANK LOC. BTW RIB 21 AND RIB 22 UPPER SKIN LOWER SURFACE AFT AREA AT RT WING. REPAIRED UPR STRINGER U9 - WSTA 617.0 TO WSTA 643.5 AND SKIN ATTACHMENT FLANGE IAW EA# 25-157-01182 WIP1 AND EA # 25-157-01182;

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CRACK SUPPORT ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DRAWING 146A7901 SHEET:66 REV A; AND MEASURE OF CRACK IS: 0.917 INCH TOOK MECHANICALLY .

Part: CARGO TRACK — CRACKED (ZONE 200) · airframe 64,212 hrs · 34,149 cycles

CRACK FLOOR STRUCTURE CARGO TRACK LBL 17 AT LEVEL BS 767 AT AFT CARGO COMPARTMENT. PERFORMED REPAIR ON FLOOR STRUCTURE CARGO TRACK LBL 17 AT LEVEL BS 767 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3. CIC ON REPAIR AREA MUST BE APPLIED WITH TTG8Q00577WT CORROSION PREVENTION ON AFT CARGO FLOOR STRUCTURE.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CORROSION SUPPORT ZEE BTW BS 747 TO BS 847 AT LEVEL STR 25L AND LBL 20 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BTW BS 747 TO BS 847 AT LEVEL STR 25L AND LBL 20 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02; SRM 53-00-53-2R-5 REPAIR 5 AND DWG: 146A7500; SHEET: 85; REV A.

Part: PLATE — CORRODED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CORROSION FLOOR STRUCTURE PLATE LOCATED ON BS 887 BTW STR 25R AND STR 26L AT WL 154 AT AFT CARGO COMPARTMENT. REPLACED FLOOR STRUCTURE PLATE LOCATED ON BS 887 BTW STR 25R AND STR 26L AT WL 154 AT AFT CARGO COMPARTMENT. IAW B737-700 AMM 51-40-02;DWG NO: 146A7500 SHEET: 85 REV: A. IAW B737-700 SRM 51-10-02 STEP 9 ITEM A.

Part: ANGLE — CRACKED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CRACK BILGE AREA ANGLE LOCATED ON BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED ON BS 867 AT LEVEL STR 26L IAW B737-700 SRM 51-40-02; 51-10-02 AND DWG# 149A8102; SHEET 17; REV: - .

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CORROSION FLOOR STRUCTURE SHEAR PLATE BTW BS 767 TO BS 792 AT LEVEL STR 25R AND RBL 21 AT AFT CARGO COMPARTMENT. REPLACED FLOOR STRUCTURE SHEAR PLATE BTW BS 767 TO BS 792 AT LEVEL STR 25R AND RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 146A0081 SHEET:25 REV:A .

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CORROSION FLOOR STRUCTURE ANGLE BTW BS 767 TO BS 792 AT LEVEL STR 25R AND RB 21 AT AFT CARGO COMPARTMENT. REPLACED FLOOR STRUCTURE ANGLE BTW BS 767 TO BS 792 AT LEVEL STR 25R AND RBL 31 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING 146A0081 SHEET: 25 REV A ; AND DWG 146A8123 SHEET: 16 REV .

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CRACK SUPPORT BRACKET ON FWD FACE BULKHEAD BS 663.75 AND RBL 50 AT LOWER FUSELAGE. REPLACED SUPPORT BRACKET ON FWD FACE BULKHEAD BS 663.75 AND RBL 50 AT LOWER FUSELAGE IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING# 111A1001 SHEET: 270 REV:-.

Part: FLOOR PANEL — DAMAGED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

ELONGATED HOLES ON FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT. REPLACED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9. FOR INSTALLATION SEE TTG8Q00ZL2JM.

Part: RIB — CRACKED (ZONE 300) · airframe 64,212 hrs · 34,149 cycles

CRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA 114.55 AT LT HORIZONTAL STABILIZER. REMOVED AND REINSTALLED RIB LOCATED ON STA 114.55 AT LT HORIZONTAL STABILIZER LEADING EDGE ACCESS PANEL 331B IAW B737-700 SRM 51-40-02 AND DWG: 186A1001 SHEET: 10 REV A.

Part: FLOOR PANEL — DAMAGED (ZONE 10) · airframe 64,212 hrs · 34,149 cycles

ELONGATED HOLES ON FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT. REPLACED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT 51-10-02 ITEM 9.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 64,212 hrs · 34,149 cycles

CRACK BRAKE PANEL FLOOR STRUCTURE LOCATED STA 540 AND BTW BL 0 TO RBL 24.5 AT PASSENGER CABIN 2025-297851<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA 540 AND BTW BL 0 TO RBL 24.5 AT PASSENGER CABIN AND FASTENERS IAW B737-700 SRM 51-40-02-0G-0 AND DWG 143A0060 SHEET:44 REV:A . SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA 540 AND BTW BL 0 TO RBL 24.5 AT PASSENGER CABIN AND FASTENERS IAW B737-700 SRM 51-40-02-0G-0 AND DWG 143A0060 SHEET:44 REV:A . SEE INDIVIDUAL SIGN OFFS BELOW

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 64,212 hrs · 34,149 cycles

CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 FROM LBL45.5 TO LBL64 AT PASSENGER CABIN 2025-297850<[01] REPLACED PLATE OF BRAKE PANEL FLOOR STRUCTURE BS 540 FROM LBL45.5 TO LBL64 AT PASSENGER CABIN IAW SRM B737-700 51-10-02 ITEM 9 AND DWG 143A5240; SHEET: 12 ; REV: ? AND 143A5240 SHEET: 21 REV: ? AND DWG 143A0060 SHEET: 44 REV: A SEE INDIVIDUAL SIGNOFF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGNOFF BELOW.

Part: WEB — CRACKED (ZONE 200) · airframe 64,212 hrs · 34,149 cycles

CRACK ON FRAME WEB BS 259.5 BETWEEN STRINGER 8R TO STRINGER 9R AT PASSENGER CABIN 2025-297867<[01] TOOL USED P/N: NORTEC 500D; S/N: N500X12101V022235; CAL DUE: 07-OCT-25.;[02] REPAIRED FRAME WEB AT BSTA 259.5 - BTW WL 240 & WL 280 AND BTW RBL 20 AND RBL 50 IAW EA#25-153-01189-WIP1 AND EA#25-153-01189 SEE INDIVIDUAL SIGN OFF BELOW.;[03] JOB COMPLETED AND CERTIFIED RII

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 64,212 hrs · 34,149 cycles

CRACK WEB INTERCOSTAL BETWEEN BS 294.5 TO BS 303.9 AND STRINGER 16L AT PASSENGER CABIN 2025-297871<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 29-JAN-26.;[02] REPAIRED WEB INTERCOSTAL BETWEEN BS 294.5 TO BS 303.9 AND STRINGER 16L AT PASSENGER CABIN IAW EA-25-153-01143- WIP1 AND EA-25-153-01143 SUMMARY SEE INDIVIDUAL SIGN OFFS BELOW.;[03] TASK COMPLETED;[04] TASK COMPLETED <BR>RII

Part: TIE CLIP — CRACKED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CRACK TIE CLIP ON BS 277 AND STRINGER 10R PASSENGER CABIN 2025-297872<[01] REPLACED TIE CLIP LOCATED STA277 AND STRINGER 10R PASSENGER CABIN IAW B737-700 SRM: 51-40-02<BR>AND DWG: 141A8380 ;SHEET:14. REV:- ; AND DWG:141A1110 SHEET:18; REV:-; SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED ACTION 1; COMPLETED <BR>RII

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 64,212 hrs · 34,149 cycles

CRACK BRAKE PANEL FLOOR STRUCTURE LOCATED STA 540 AND BTW BL 0 TO LBL 24.5 AT PASSENGER CABIN 2025-297852<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA 540 AND BTW BL 0 TO LBL 24.5 AT PASSENGER CABIN IAW B737-700 SRM: 51-40-02 AND DWG: 143A0060; SHEET:44;REV:A<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTED STEP 1<BR>REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA 540 AND BTW BL 0 TO LBL 24.5 AT PASSENGER CABIN IAW B737-700 SRM: 51-40-02-0G-0 AND DWG: 143A0060; SHEET:44;REV:A<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[03] TASK CARD COMPLETED <BR>REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA 540 AND BTW BL 0 TO LBL 24.5 AT PASSENGER CABIN IAW B737-700 SRM: 51-40-02-0G-0 AND DWG: 143A0060; SHEET:44;REV:A<BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: GUSSET — CRACKED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CRACK GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT 2025-297787<[01] REPLACED GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 174 REV: ?;[02] REPLACED GUSSET LOCATED BS500D AND S-19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 174 REV: ? CERTIFIED AS RII.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CRACK ANGLE - SUPPORT LOCATED BS 500B FWD SIDE AND S-26L FWD CARGO COMPARTMENT 2025-297785<[01] REPLACED ANGLE - SUPPORT LOCATED BS 500B FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DWG 143A7505 SHET 5 REV B. SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED ANGLE - SUPPORT LOCATED BS 500B FWD SIDE AND S-26L FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9 AND DWG 143A7505 SHET 5 REV B. SEE INDIVIDUAL SIGNOFF BELOW.

Part: GUSSET — CRACKED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CRACK GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT 2025-297786<[01] REPLACED GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 174 REV: ?;[02] CORRECTED STEP 1 <BR>REPLACED GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 174 REV: ? SEE INDIVIDUAL SIGN OFF;[03] REPLACED GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 174 REV: ? SEE INDIVIDUAL SIGN OFF<BR>AS RII

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 64,212 hrs · 34,149 cycles

INOP BATTERY PACK EMERGENCY EXIT DOOR LT SIDE PASSENGER CABIN (1EA) 2025-297813<[01] REPLACED BATTERY PACK EMERGENCY EXIT DOOR LT SIDE PASSENGER CABIN (1EA) IAW BOEING 737-700 AMM 33-51-06-960-805.;[02] REPLACED BATTERY PACK EMERGENCY EXIT DOOR LT SIDE PASSENGER CABIN (1EA) IAW BOEING 737-700 AMM 33-51-06-960-805. ACCOMPLISHED THE EMERGENCY LIGHT TEST; THE RESULTS IS PASSED;[03] CORRECTED STEP 1 AND 2<BR>REPLACED BATTERY PACK EMERGENCY EXIT DOOR LT SIDE PASSENGER CABIN (1EA) IAW BOEING 737-700 AMM 33-51-06-960-805. ACCOMPLISHED THE EMERGENCY LIGHT TEST; THE RESULTS IS PASSED;[04] TASK COMPLETED

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 64,212 hrs · 34,149 cycles

INOP BATTERY PACK EMERGENCY EXIT DOOR RT SIDE PASSENGER CABIN (1EA) 2025-297814<[01] REPLACED BATTERY PACK EMERGENCY EXIT DOOR RT SIDE PASSENGER CABIN (1EA) IAW BOEING 737-700 AMM 33-51-06-960-805.;[02] REPLACED BATTERY PACK EMERGENCY EXIT DOOR RT SIDE PASSENGER CABIN (1EA) IAW BOEING 737-700 AMM 33-51-06-960-805.ACCOMPLISHED THE EMERGENCY LIGHT TEST; THE RESULTS IS PASSED;[03] TASK COMPLETED

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CRACK ANGLE - SUPPORT LOCATED BS 500C AFT SIDE AND S-26L FWD CARGO COMPARTMENT 2025-297783<[01] REPLACED ANGLE - SUPPORT LOCATED BS 500C AFT SIDE AND S-26L FWD CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 143A7505 SHEET: 9 REV: A. SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED ANGLE - SUPPORT LOCATED BS 500C AFT SIDE AND S-26L FWD CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 143A7505 SHEET: 9 REV: A. SEE INDIVIDUAL SIGNOFFS BELOW

Part: RIB — CRACKED (ZONE 300) · airframe 64,212 hrs · 34,149 cycles

CRACK ON RIB ACCESS PANEL 341B LOCATED LE STA 86.66 AT RT HORIZONTAL STABILIZER 2025-297817<[01] REPLACED RIB ACCESS PANEL 341B LOCATED LE STA 86.66 AT RT HORIZONTAL STABILIZER AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 186A1001 SHEET: 19 REV: - . SEE INDIVIDUAL SIGNOFFS BELOW;[02] CERTIFIED CORRECTIVE ACTION STEP 1

Part: LENS — BROKEN (ZONE 200) · airframe 64,212 hrs · 34,149 cycles

BROKEN EMERGENCY EXIT LENS ASSY LOWERED CEILING AT AFT GALLEY AREA (1 EA) 2025-297758<[01] REPLACED EMERGENCY EXIT LENS ASSY LOWERED CEILING AT AFT GALLEY AREA (1 EA) IAW BOEING 737-700 AMM 33-51-01-960-802.;[02] TASK COMPLETED

Part: LIGHT — BROKEN (ZONE 200) · airframe 64,212 hrs · 34,149 cycles

BROKEN FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) 2025-297797<[01] FAULT RAISED IN ERROR AND IS BEING CLOSED SEE TTG8Q001SMQ2;[02] FAULT RAISED IN ERROR AND IS BEING CLOSED SEE TTG8Q001SMQ2

Part: ANGLE — CRACKED (ZONE 100) · airframe 64,212 hrs · 34,149 cycles

CRACK ANGLE - SUPPORT LOCATED BS 500C FWD SIDE AND S-26L FWD CARGO COMPARTMENT 2025-297784<[01] REPLACED NEW ANGLE AND FASTENERS LOCATED BS 500C FWD SIDE AND S-26L FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 DWG NO: 143A7505 SHEET: 5 REV:B. IAW B737-700 SRM 51-10-02 ITEM:9 .SEE INDIVIDUAL SIGN OFFS BELOW.;[02] COMPLETED TASK CERTIFIED

Part: RIB — CRACKED (ZONE 300) · airframe 64,212 hrs · 34,149 cycles

CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 28 INCH FROM FRONT SPAR LT HORIZONTAL STAB 2025-297763<[01] ON STEPS 3 AND 4; TOOL USED P/N: NORTEC 500D; S/N: N500X12101V022235; CAL DUE: 07-OCT-25.;[02] TOOL USED: ET EQUIPMENT; P/N: NORTEC600D; S/N: 240497907; CAL DUE DATE: 27-AUG-25;[03] REPAIRED INSPAR RIB LOCATED STAB STA 129.50 AND 28 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW SRM B737-700 55-10-09-2R-4 REPAIR 4; SEE INDIVIDUAL SIGNOFF BELOW.;[04] REPAIRED INSPAR RIB LOCATED STAB STA 129.50 AND 28 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW SRM B737-700 55-10-09-2R-4 REPAIR 4; SEE INDIVIDUAL SIGNOFF BELOW. ITEM RII

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 64,212 hrs · 34,149 cycles

INOP POWER SUPPLY DOOR EMERGENCY EXIT RT SIDE (1EA) 2025-297732<[01] REPLACED POWER SUPPLY DOOR EMERGENCY EXIT RT SIDE (1EA) IAW BOEING 737-700 AMM 33-51-06-960-805.;[02] CORRECTED STEP 1 <BR>REPLACED POWER SUPPLY DOOR EMERGENCY EXIT RT SIDE (1EA) IAW BOEING 737-700 AMM 33-51-06-960-805. ACCOMPLISHED THE EMERGENCY LIGHT TEST; THE RESULTS IS PASSED;[03] TASK COMPLETED

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 64,212 hrs · 34,149 cycles

INOP BASE EMERGENCY EXIT ASSY ON SIDEWALL PANEL 231YHW AT PASSENGER CABIN 2025-297707<[01] REPLACED EMERGENCY EXIT ASSY ON SIDEWALL PANEL 231YHW AT PASSENGER CABIN IAW BOEING 737-700 AMM 33-51-01-960-802.;[02] CORRECTED STEP 1<BR>REPLACED BASE EMERGENCY EXIT ASSY ON SIDEWALL PANEL 231YHW AT PASSENGER CABIN IAW BOEING 737-700 AMM 33-51-01-960-802.;[03] TASK COMPLETED

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 62,270 hrs · 32,959 cycles

8DEF EMERGENCY AREA LIGHT INOP<[01] RAR 8DEF EMERGENCY AREA LIGHT LAMP REF AMM 33-51-03.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 61,594 hrs · 32,548 cycles

L1 DOOR SLIDE DISLODGED<[01] RESECURED SLIDE PER AMM 25-66-01

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 57,926 hrs · 30,275 cycles

L2 DOOR SLIDE SKIRT RUBS ON SCUFF PLATE WHEN CLOSING DOOR.<[01] READJUSTED L-2 DOOR SLIDE GIRT Z-FOLD TO LIFT THE GIRT ABOVE THE DOOR FRAME AND PREVENT INTERFERENCE. OPERATED DOOR; GIRT NO LONGER INTERFERES WITH SCUFF PLATE. REF B 737 AMM 25-66-01-400-803.;[02] VERIFIED READJUSTMENT OF L-2 SLIDE GIRT BAR; OK.

Part: SKIRT — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

R2 DOOR SLIDE SKIRT RUBS ON SCUFF PLATE WHEN CLOSING DOOR.<[01] READJUSTED R-2 DOOR SLIDE GIRT Z-FOLD TO LIFT THE GIRT ABOVE THE DOOR FRAME AND PREVENT INTERFERENCE. OPERATED DOOR; GIRT NO LONGER INTERFERES WITH SCUFF PLATE. REF B 737 AMM 25-66-01-400-803.;[02] VERIFIED READJUSTMENT OF SLIDE GIRT Z FOLD.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

EMERGENCY LIGHTS INOP AT FOLLOW LOCATIONS: R1 DOOR LWR; OH BINS 6-11-13 RH 14-17 LH; RH EMERG EXIT<[01] BATTERY PACKS WERE REPLACED AT LOCATIONS M1670; M1669; M1674 & M1668 ON TTG8Q00L2DJ0 AS PER AMM REF 33-51-06-960-806. LIGHTS TESTED NORMAL.;[02] VERIFIED BATTERY PACK REPLACEMENT ON TTG8Q00L2DJ0.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

SEVERAL PASSENGER INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERATIVE.<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT POSITIONS M1668; M1669; M1674; M1670 AS PER AMM REF 33-51-06-960-805. PERFORMED OPERATIONAL TEST AS PER AMM REF 33-51-00-710-801. TESTED NORMAL.;[02] VERIFIED STEP 1.

Part: SUPPORT — CRACKED (ZN 500 LEFT WING) · airframe 57,926 hrs · 30,275 cycles

LH FWD OVERWING ACCESS PANEL 195AL SUPPORT STRUCTURE CRACK.<[01] REMOVED LH FWD OVERWING ACCESS PANEL 195AL SUPPORT STRUCTURE; LOCATED AND DRILLED NEW FRAME SUPPORT TREATED AND PRIMED HOLES; INSTALLED NEW FRAME SUPPORT. REF B737 SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AMM 51-21-72-370-804; AMM 51-21-41-370-802;[02] VERIFIED ENTRY #1 AS WORK ACCOMPLISHED

Part: LENS — DEFECTIVE (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

EMERGENCY LIGHT LENSE DEFECTIVE AT SEAT ROWS: 2DEF AND 6ABC. EMERGENCY LIGHT LENSE DEFECTIVE AT SEAT ROW 6 ABC<[01] REMOVED AND REPLACED EMERGENCY LIGHT LENS AT 6ABC PER B737 AMM-33-51-03-960-801;[02] VERIFIED LENS REPLACEMENT.

Part: FAIRING — CRACKED (ZN 400 NACELLE/P) · airframe 57,926 hrs · 30,275 cycles

#2 FLAP FAIRING # 543BB FWD EDGE SMALL CRACK.<[01] OK TO APPLY REPAIR.;[02] APPLIED REPAIR AT #2 FLAP FAIRING 543BB ON FWD EDGE PER B737 SRM 51-70-04-2R-0 PARAGRAPH 4.L.7 MATERIAL USED RESIN EY3804 PO#1800550 AND FIBERGLASS PO#1738579;[03] VERIFIED ALL STEPS

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 57,926 hrs · 30,275 cycles

LH HORIZONTAL STAB RIB #4 STIFFENER 2 LOWER FLANGE CRACK.<[01] REPAIRED LEFT HORIZONTAL STAB. #4 FOUND CRACKED AT STIFFENER #2 AS PER SRM 55-10-09-2R-5 REPAIR 5;[02] CORRECTION. REPAIRED LEFT HORIZONTAL STAB. RIB #4 FOUND CRACKED AT STIFFENER #2 AS PER SRM 55-10-09-2R-5 REPAIR 5;[03] RII -- VERIFIED LH HORIZONTAL STAB RIB # 4 REPAIR.

Part: FRAME — CRACKED (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

PASSENGER CABIN FUSELAGE FRAME 312 ABOVE L1 DOOR CRACK.<[01] ACCOMPLISHED REPAIR IN THE ITEM TTG8Q00KU1UT;[02] VERIFIED REPAIR WAS ACCOMPLISHED ON TTG8Q00KU1UT.

Part: MOUNT — BROKEN (ZN 800 DOOR) · airframe 57,926 hrs · 30,275 cycles

R-1 DOOR AFT DOOR SLIDE MOUNT BRACKET SHOCK MOUNT BROKEN<[01] REMOVED AND REPLACED R-1 DOOR AFT DOOR SLIDE MOUNT BRACKET SHOCKMOUNT PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED SHOCKMOUNT REPLACEMENT.<BR>OK TO INSTALL PLATE.;[03] INSTALLED R-1 DOOR AFT DOOR SLIDE MOUNT BRACKET SHOCK MOUNT AS PER B737-700 SRM 51-40-02-0G-0.;[04] VERIFIED INSTALLATION OF BRACKET PLATE.

Part: CHANNEL — CORRODED (ZN 100 FUS LOWER) · airframe 57,926 hrs · 30,275 cycles

FWD CARGO RIGHT 'Z' CHANNEL AT 500B-500D HAS LIGHT CORROSION AROUND NUT PLATES<[01] OK TO APPLY ALODINE AND PRIMER AND TOP COAT.;[02] TREATED; PRIMED AND TOP COAT APPLIED AT FWD CARGO COMP. FIGHT 'Z' CHANNEL FR0M STA 500B THRU STA 500D PER B737-700 SRM 51-20-01-0G-0; AMM 51-21-72-370-804 AND 51-21-73-370-804;[03] RII. VERIFIED STEPS FOR Z CHANNEL REPAIR.

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 57,926 hrs · 30,275 cycles

CORROSION FOUND AFT CARGO DOOR CUTOUT FWD SHIELD FROM STA 767 TO STA 787 RBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] REMOVED CORROSION AT AFT CARGO DOOR CUTOUT FWD SHIELD FROM STA 767 TO STA 787 RBL 21 WL 155.5 AS PER SRM 51-10-2-0G-0.<BR>PERFORMED BY O.P 4041. ORIGINAL THICKNESS 0.050'; MATERIAL LOST 0.026'; MATERIAL REMAINING 0.024'. FOUND OUT OF LIMITS AS PER SRM 53-60-15-1A-1. INSTALLED NEW AFT CARGO DOOR CUTOUT FWD SHIELD PER B 737-700 SRM 51-40-02-0G-0 AND DWG 146A0081.;[02] VERIFIED AND INSPECTED. REMOVED CORROSION AT AFT CARGO DOOR CUTOUT FWD SHIELD FROM STA 767 TO STA 787 RBL 21 WL 155.5 AS PER SRM 51-10-2-0G-0.<BR>PERFORMED BY O.P 4041. ORIGINAL THICKNESS 0.050'; MATERIAL LOST 0.026'; MATERIAL REMAINING 0.024'. FOUND OUT OF LIMITS AS PER SRM 53-60-15-1A-1. INSTALLED NEW AFT CARGO DOOR CUTOUT FWD SHIELD PER B 737-700 SRM 51-40-02-0G-0 AND DWG 146A0081.

Part: CHANNEL — CORRODED (ZN 100 FUS LOWER) · airframe 57,926 hrs · 30,275 cycles

CORROSION FOUND AFT CARGO RH 'Z' CHANNEL FROM STA 727 TO STA 767 RBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] REMOVED CORROSION AT AFT CARGO RH 'Z' CHANNEL FROM STA 727 TO STA 767 RBL 21 WL 155.5 AS PER SRM 51-10-02-0G-0. ORIGINAL TICKNESS 0.040'; MATERIAL LOST 0.014'; MATERIAL REMAINING 0.026'. FOUND OUT OF LIMITS AS PER SRM 53-00-53-1A-2. INSTALLED NEW AFT CARGO R/H 'Z' CHANNEL PER B 737-700 SRM 51-40-02-0G-0 AND DWG 146A7502.;[02] VERIFIED AND INSPECTED REMOVED CORROSION AT AFT CARGO RH 'Z' CHANNEL FROM STA 727 TO STA 767 RBL 21 WL 155.5 AS PER SRM 51-10-02-0G-0. ORIGINAL TICKNESS 0.040'; MATERIAL LOST 0.014'; MATERIAL REMAINING 0.026'. FOUND OUT OF LIMITS AS PER SRM 53-00-53-1A-2. INSTALLED NEW AFT CARGO R/H 'Z' CHANNEL PER B 737-700 SRM 51-40-02-0G-0 AND DWG 146A7502.

Part: STRAP — CORRODED (ZN 100 FUS LOWER) · airframe 57,926 hrs · 30,275 cycles

CORROSION FOUND AFT CARGO FLOOR STRAP AT STA 767 + 5 FROM LBL 6 TO RBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] REMOVED CORROSION FROM AFT CARGO FLOOR STRAP AND FOUND TO BE OUT OF LIMITS PER B737 SRM 53-00-53-1A-2 TOOL B/C: 172991 DUE DATE: 25-JUL-23; AND RECIEVED NEW AFT CARGO STRAP PART#: 146A9401-4 PO# 1792296; APPLIED TOPCOAT. REF B737 AMM 51-21-73-370-803<BR>REF TASK TTG8Q00J729ZFOR INSTALLATION;[02] VERIFIED STEP 1

Part: FLOORBEAM — CORRODED (ZN 100 FUS LOWER) · airframe 57,926 hrs · 30,275 cycles

*CORROSION* AFT CABIN FLOOR BEAM STA 986.5 BETWEEN RBL 39 AND RBL 44 WL 208.1 HAS CORROSION AROUND FASTENER HOLES AS MARKED. 124-051<[01] REPAIR AFT CABIN FLOOR BEAM STA 986.5 BETWEEN RBL 39 AND RBL 44 WL 208.1 ACCOMPLISHED ON THE ITEM TTG8Q00KJ1J7;[02] CORRECTION. REPAIR AFT CABIN FLOOR BEAM STA 986.5 BETWEEN RBL 39 AND RBL 44 WL 208.1 AS PER EA 23-153-01453; ACCOMPLISHED ON THE ITEM TTG8Q00KUXWV;[03] VERIFIED STEP 2.

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN FLOOR STRUCTURE BETWEEN STA 380 AND STA 400 LBL 13; INTERCOSTAL UPPER SUPPORT ANGLE CRACKED AT FASTENERS HOLES.<[01] REMOVED AND REPLACED INTERCOSTAL UPPER SUPPORT ANGLE AT MAIN CABIN FLOOR STRUCTURE BETWEEN STA 380 AND STA 400 LBL13 PER B737-700 SRM 51-40-02-0G-0 AND DRWG #143A5400 SH 38.;[02] VERIFIED RII STEPS.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

PASSENGER CABIN FLOOR INTERCOSTAL BETWEEN STA 312 AND STA 328 LBL 46 WL 208.1 HAS A CRACK AROUND FASTENER HOLE.<[01] OK TO INSTALL NEW INTERCOSTAL.;[02] REMOVED AND REPLACED CABIN FLOOR INTERCOSTAL BETWEEN STA 312 AND STA 328 LBL 46 WL 208.1 AS PER B737-700 SRM 51-40-02-0G-0.;[03] CORRECTING STEP 2: REMOVED AND REPLACED CABIN FLOOR INTERCOSTAL BETWEEN STA 312 AND STA 328 LBL 46 WL 208.1 AS PER B737-700 SRM 51-40-02-0G-0 AND DRWG #141A5400 SH 26.;[04] RII. VERIFIED INSTALLATION STEPS.

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN FLOOR STRUCTURE BETWEEN STA 380 AND STA 400 RBL 9; INTERCOSTAL UPPER SUPPORT ANGLE CRACKED AT FASTENERS HOLES.<[01] RII; VERIFIED INSTALLATION STEPS.

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN FLOOR STRUCTURE BETWEEN STA 380 AND STA 400 BL 0; INTERCOSTAL UPPER SUPPORT ANGLE CRACKED AT FASTENERS HOLES.<[01] REMOVED AND REPLACED INTERCOSTAL UPPER SUPPORT ANGLE AT MAIN CABIN FLOOR STRUCTURE BETWEEN STA 380 AND STA 400 BL0 PER B737-700 SRM 51-40-02-0G-0 AND DRWG #143A5400 SH 65 & 66.;[02] VERIFIED RII STEPS.

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

PASSENGER CABIN FLOOR STRUCTURE AT STA 695 BL 0 WL 204 ANGLE SUPPORT CRACK.<[01] ACCOMPLISHED HEAT TREAT ON ANGLE BY AAR FORM OP 84 AND SERVICEABLE TAG #407960;[02] OK TO APPLY ALODINE AND PRIMER.;[03] REPLACED FABRICATED BRACKET AT CABIN FLOOR STRUCTURE STA 695; BL0 WL 204 AS PER SRM 51-40-02-0G-0 AND DWG 2739110;[04] VERIFIED BRACKET REPLACEMENT.

Part: ATTACH ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

AFT CABIN INERCOSTAL BETWEEN STA 927 AND STA 947.5 AT RBL 0 WL 208.1 UPPER ATTACHED ANGLE IS CRACKED AS MARKED. 124-056<[01] REMOVED AND REPLACED AFT CABIN INTERCOASTAL BETWEEN STA 927 AND STA 947.5 AT RBL 0 WL 208.1 AS PER B 737-700 SRM 51-40-02-0G-0.;[02] VERIFIED AND INSPECTD REMOVED AND REPLACED AFT CABIN INTERCOASTAL BETWEEN STA 927 AND STA 947.5 AT RBL 0 WL 208.1 AS PER B 737-700 SRM 51-40-02-0G-0.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

PASSENGER CABIN FLOOR INTERCOSTAL BETWEEN STA 312 AND STA 328 RBL 30 WL 208.1 HAS A CRACK AROUND FASTENER HOLE.<[01] OK TO INSTALL NEW INTERCOSTAL.;[02] REMOVED AND REPLACE PASSENGER CABIN FLOOR INTERCOSTAL BETWEEN STA 312 AND STA 328 RBL 30 WL 208.1 PER B737-700 SRM 51-40-02-0G-0.;[03] CORRECTING STEP 2: REMOVED AND REPLACE PASSENGER CABIN FLOOR INTERCOSTAL BETWEEN STA 312 AND STA 328 RBL 30 WL 208.1 PER B737-700 SRM 51-40-02-0G-0 AND DRWG# 141A5400 SHEET 39.;[04] RII. VERIFIED INSTALLATION STEPS.

Part: FLOORBEAM — CRACKED (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

SUSPECT CRACK AT PASSENGER CABIN FWD SIDE OF FLOOR BEAM STA 294.5 RBL 51 WL 208.1 HAS A CRACK.<[01] ACCOMPLISHED DVI ON ADJACENT STRUCTURE AREAS; NO CRACKS; NO CORROSIONS OR OTHER DAMAGES NOTED. REF B737-7 SRM 53-10-51-2R-16 STEP 4.C.(4);[02] OK TO APPLY ALODINE AND PRIMER TO REPAIR PARTS AND TO THE CUTTED T CHORD.;[03] VERIFIED; ALODINE AND PRIMER APPLIED.;[04] RII. OK TO INSTALL REPAIR PARTS.;[05] REPAIRED FLOOR BEAM AT STA 294.5 FROM RBL25 TO THE END OF THE CHORD PER B737-700 SRM 53-10-51-2R-16 REP.16 FIG.202 DETAIL G.;[06] VERIFIED STEP 5. COMPLETION OF REPAIR PARTS AT FLOOR BEAM.;[07] VERIFIED STEPS ACCOMPLISHED.<BR>REMOVED AND REPLACED FLOOR BEAM AT STA 294.5 RBL 51.;[08] VERIFIED

Part: FLOORBEAM — CORRODED (ZN 100 FUS LOWER) · airframe 57,926 hrs · 30,275 cycles

*CORROSION* AFT CABIN FLOOR BEAM STA 986.5 BETWEEN LBL 35 AND LBL 44 WL 208.1 HAS CORROSION AROUND FASTENER HOLES AS MARKED. 124-047<[01] CORRECTION ON TABLE STEP 17 REMAINING THICKNESS IS 0.121;[02] VERIFIED CORRECTION;[03] REPAIR AFT CABIN FLOOR BEAM STA 986.5 BETWEEN LBL 35 AND LBL 44 WL 208.1 WAS ACCOMPLISHED ON THE ITEM TTG8Q00KUXWV;[04] CORRECTION. REPAIR AFT CABIN FLOOR BEAM STA 986.5 BETWEEN LBL 35 AND LBL 44 WL 208.1 AS PER EA 23-153-01453; WAS ACCOMPLISHED ON THE ITEM TTG8Q00KUXWV;[05] CORRECTION. REPAIR ACCOMPLISHED EA 23-153-01453. REF FAULT TTG8Q00KJ1J7;[06] VERIFIED STEPS 4 AND 5.

Part: FLOOR SUPPORT — CRACKED (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

PASSENGER CABIN FLOOR INTERCOSTAL BETWEEN STA 277 AND STA 294.5 BL 0 WL 208.1 HAS A CRACK AROUND FASTENER HOLE.<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN FWD WET AREA BETW. STA 277 THRU STA 294.5 BL 0 PER B737-700 SRM 51-40-02-0G-0 AND DRAWING #141A5400;[02] VERIFIED INSTALLATION OF INTERCOSTAL AT MAIN CABIN FWD WET AREA BETW. STA 277 THRU STA 294.5 BL 0

Part: FLOOR PANEL — DAMAGED (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN AFT WET AREA FLOOR PANEL # 241ADF HAS A PREVIOUS REPAIR AT TOP SKIN<[01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL #241ADF BY OUTSIDE VENDOR (AERO MARINE) WITH P.O. #2017549.THIS PANEL WILL BE INSTALL ON FAULT #TTG8Q00J71MC;[02] VERIFIED FABRICATION OF FLOOR PANEL # 241ADF BY OUTSIDE VENDOR UNDER P.O. #2017549. FAA 8130-3 # 04272023412-1 ATTACHED.

Part: STRAP — CORRODED (ZN 100 FUS LOWER) · airframe 57,926 hrs · 30,275 cycles

*CORROSION* AFT CABIN FLOOR WEB STRAP AT STA 1016+12 RBL 17 WL 208;1 AS MARKED. 124-042<[01] REMOVED CORROSION AT AFT CABIN FLOOR WEB STRAP AT STA 1016+12 RBL 17 WL 208.1. ORIGINAL THICKNESS 0.071'. MATERIAL LOSS 0.021'. REMAINING MATERIAL 0.050'; FOUND OUT OF LIMITS. REPLACED AS PER SRM 51-40-02-0G-0 AND DWG 147A5730;[02] VERIFIED AFT CABIN FLOOR WEB STRAP REPLACEMENT.

Part: FLOOR PANEL — PEELING (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN CENTER FLOOR PANEL #231UF TOP SKIN PEELING OFF SEVERAL AREAS<[01] VERIFIED STEPS.

Part: FLOOR PANEL — PEELING (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN FWD WET AREA FLOOR PANEL #221A TOP SKIN PEELING OFF SEVERAL AREAS<[01] REPLACED MAIN CABIN FWD WET AREA LEFT SIDE FLOOR PANEL #221A REF. B737-700 AMM 53-21-00-400-801. THIS PANEL WILL BE INSTALL ON FAULT #TTG8Q00KH44V;[02] VERIFIED REPLACEMENT OF PANEL # 221A AND TTG8Q00KH44V

Part: FLOOR PANEL — PEELING (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN CENTER FLOOR PANEL #242AF TOP SKIN PEELING OFF SEVERAL AREAS<[01] APPLIED GLASS FABRIC REPAIR PLIES AT DAMAGED AREA ON MAIN CABIN CENTER FLOOR PANEL #242AF. REF B737 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3. MATERIAL USED GLASS FABRIC PLIES PO#: 1738579 AND RESIN EPOCAST 50A PO#:1799598.;[02] VERIFIED REPAIR STEPS.

Part: FLOOR PANEL — PEELING (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN CENTER FLOOR PANEL #231DF TOP SKIN PEELING OFF SEVERAL AREAS<[01] VERIFIED STEPS.

Part: FLOOR PANEL — PEELING (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN CENTER FLOOR PANEL #231KF TOP SKIN PEELING OFF SEVERAL AREAS<[01] VERIFIED STEPS.

Part: FLOOR PANEL — PEELING (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN CENTER FLOOR PANEL #242CF TOP SKIN PEELING OFF SEVERAL AREAS<[01] 'LATE ENTRY' REMOVED MAIN CABIN CENTER AREA FLOOR PANEL #242CF FOR COMPOSITE REPAIR PER B737-700 AMM 53-00-50-2R-0 (PERFORMED BY RHR 19811);[02] MAIN CABIN FLOOR PANEL #242CF WILL BE INSTALL ON FAULT #TTG8Q00J71L1;[03] CORRECTION ON STEP #1 - CABIN FLOOR PANEL #242CF WAS REMOVED ON FAULT #TTG8Q00J71L0

Part: FLOOR PANEL — PEELING (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN CENTER FLOOR PANEL #241KF TOP SKIN PEELING OFF SEVERAL AREAS<[01] VERIFIED STEPS.

Part: FLOOR PANEL — PEELING (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN CENTER FLOOR PANEL #231GF TOP SKIN PEELING OFF SEVERAL AREAS<[01] VERIFIED STEPS.

Part: FLOOR PANEL — PEELING (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN CENTER FLOOR PANEL #231ZF TOP SKIN PEELING OFF SEVERA AREAS<[01] REPAIRED DAMAGE AREAS AS MARKED WITH A PERMANENT REPAIR ON TOP SURFACE OF MAIN CABIN FLOOR PANEL #231ZF AS PER B737 SRM 53-00-50-2R-1. MATERIALS USED PO#1738579 AND PO#1799598 AND PERFORMED TAP TEST ON REPAIRED AREA OF TOP SURFACE OF MAIN CABIN FLOOR PANEL #231ZF; FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION 5;[02] VERIFIED STEP 1.

Part: FLOOR PANEL — PEELING (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

MAIN CABIN CENTER FLOOR PANEL #241AF TOP SKIN PEELING OFF SEVERAL AREAS<[01] APPLIED REPAIR IN DAMAGED AREA AT FLOOR PANEL 241AF AS PER B737 SRM 53-00-50-2R-1; MATERIAL USED RESIN PO#1799598 AND CLOTH PO#1738579;[02] VERIFIED STEP 1.

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 57,926 hrs · 30,275 cycles

LEFT HORIZONTAL STABILIZER RIB #4 CRACKED AT STIFFENER #4 LOWER SECTION<[01] MIXED SEALANT PS870B2 ON REPAIR PARTS AT 9:30PM 04/22/2023 .SQUEEZE OUT TIME 11:30PM 04/22/2023 AND INSTALLED FASTENERS ON REPAIR PARTS AT L/H HORIZONTAL STAB RIB #4 AS PER REF B/737-700 SRM 55-10-09-2R-4 REPAIR 4 AND SRM 51-40-02-0G-0.;[02] RII -- VERIFIED STEP 1.;[03] REPAIRED LEFT HORIZONTAL STAB. RIB #4 CRACKED AT STIFFENER #4 AS PER SRM 55-10-09-2R-4 REPAIR 4;[04] RII -- VERIFIED LH HORIZONTAL STAB RIB # 4 REPAIR.

Part: BRACKET — ELONGATED (ZN 100 FUS LOWER) · airframe 57,926 hrs · 30,275 cycles

FWD CARGO COMP. LOWER BRACKET TO ATTACH SIDEWALL STRUCTURE WITH ELONGATED HOLE<[1] REPLACED FWD CARGO COMP. FWD LOWER BRACKET TO ATTACH SIDEWALL ACCESS PANEL 122BW REF. B737-700 AMM 25-52-06-400-801. THIS BRACKET WILL BE INSTALL ON FAULT #TTG8Q00J7277;[2] VERIFIED STEP 1.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 57,926 hrs · 30,275 cycles

LEFT VAPOR BARRIER UPPER ANGLE CRACKED AT FASTENER HOLE LBL 2' CORRECTION ON ORIGINAL WRITE UP LEFT VAPOR BARRIER UPPER ANGLE CRACKED AT FASTENER HOLE LBL 6'<[01] OK TO APPLY ALODINE AND PRIMER COAT TO REPAIR PARTS.;[02] TREATED WITH ALODINE AND PRIMER REPAIR PARTS AS PER 737-700 SRM 51-20-01-0G-0 AND 51-21-72-370-804;[03] VERIFIED ALODINE AND PRIMER APPLICATION.;[04] OK TO INSTALL REPAIR PARTS; FILLER AND ANGLE.;[05] OK TO APPLY CUP SEAL TO FASTENER HEADS.;[06] REPAIRED DAMAGE AT VAPOR BARRIER UPPER ATTACH ANGLE STA 663 LBL 6 AS PER B 737-700 SRM 57-10-10-2R-5 FIG 202 DETAIL B SHEET 4;[07] VERFIED WORK ACCOMPLISHED AND DOCUMENTATION;[08] RII. VERIFIED WORK STEPS PROCESS.;[09] VERIFIED COMPLETE WORK PERFORMED

Part: PANEL — CORRODED (ZN 600 RIGHT WIN) · airframe 57,926 hrs · 30,275 cycles

RT WING L/E FUELING STATION AT 621GB DOOR - P-15 PANEL HAS SURFACE CORROSION AROUND I/B AND O/B GAUGES. 124-011<[01] FAULT WAS RESOLVED ON ANOTHER FAULT. FAULT NUMBER TTG8Q00KFP2Q;;[02] VERIFIED TTG8Q00KFP2Q

Part: HANDLE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 57,926 hrs · 30,275 cycles

FWD ENTRY DOOR LINER LOWER ASSIST HANDLE NUT IS CRACKED<[01] REMOVED AND REPLACED FWD ENTRY DOOR LINER LOWER ASSIST HANDLE NUT REF BOEING 737 AMM 52-11-31-400-802;[02] VERIFIED STEP 1.

Part: BRACKET — ELONGATED (ZN 500 LEFT WING) · airframe 57,926 hrs · 30,275 cycles

LEFT WING L/E ANTI-ICE DUCT SUPPORT BRACKET HAS ELONGATED HOLES JUST UNDER ACCESS PANEL 511AT. (DOT #28-1)<[01] REMOVED AND REPLACED LEFT WING L/E ANTI-ICE DUCT SUPPORT BRACKET JUST UNDER ACCESS PANEL 511AT. IN REF SOPM 20-50-01;[02] VERIFIED STEP 1.

Part: DOOR — CRACKED (ZN 400 NACELLE/P) · airframe 57,926 hrs · 30,275 cycles

R/H MAIN LANDING GEAR CENTER DOOR CRACKED.<[01] PARTS TRANSACTION FOR ROUTING OUT FOR REPAIR;[02] REMOVED AND REPLACED R/H MAIN LANDING GEAR DOOR ASSEMBLY. REF:B-737 AMM 32-13-11-000-803 AND AMM 32-13-11-420-803.;[03] VERIFIED REMOVED AND REPLACED R/H MAIN LANDING GEAR DOOR ASSEMBLY. REF:B-737 AMM 32-13-11-000-803 AND AMM 32-13-11-420-803.CHECKED NORMAL NO ADJUSTMENTS MADE.;[04] ALL STEPS COMPLETED.

Part: FITTING — DAMAGED (ZN 500 LEFT WING) · airframe 57,926 hrs · 30,275 cycles

L/W REAR SPAR FIXED T/E PANEL 551GB INB AFT SUPPORT STRUT LOWER ATTACHED FITTING HAS ELONGATED HOLE MKD DOT<[01] REMOVED AND REPLACED FITTING AT 551-GB. PANEL. USED REF. SRM-51-40-02-0G-0.;[02] VERIFIED FITTING REPLACEMENT.

Part: SLAT — CRACKED (ZN 500 LEFT WING) · airframe 57,926 hrs · 30,275 cycles

L/W NO-1 SLAT NOSE L/E SKIN CRACKED @ ACTUATOR RIB ATTACHED POINT OUB MKD DOT<[01] ACCOMPLISHED PART TRANSACTION.;[02] REMOVED AND REPLACED L/W #1 SLAT ASSY IN REFERENCE AMM 27-81-000-801 AND AMM 27-81-21-400-801.;[03] RII -- VERIFIED L/W #1 SLAT ASSY REPLACEMENT.

Part: PANEL — DELAMINATED (ZN 600 RIGHT WIN) · airframe 57,926 hrs · 30,275 cycles

LOWER RT WING TO BODY FAIRING PANEL 192BR DELAMINATED<[01] REMOVED AND REAPPLIED GLASS FABRIC PLIES; PRIMED AND TOPCOATED PANEL 192BR. REF B737 SRM 53-40-70-2R-1 AND SRM 51-70-04-2R-1 REPAIR 1 PARAGRAPH 4; AMM 51-21-72-370-804; AMM 51-21-73-370-803<BR>MATERIAL USED DRY GRAPHI PO#: 1755421; GLASS FRABRIC PLIES PO#:1738579 AND RESIN EY3804AB PO#:1800550.;[02] VERIFIED AND INSPECTED REMOVED AND REAPPLIED GLASS FABRIC PLIES; PRIMED AND TOPCOATED PANEL 192BR. REF B737 SRM 53-40-70-2R-1 AND SRM 51-70-04-2R-1 REPAIR 1 PARAGRAPH 4; AMM 51-21-72-370-804; AMM 51-21-73-370-803<BR>MATERIAL USED DRY GRAPHI PO#: 1755421; GLASS FRABRIC PLIES PO#:1738579 AND RESIN EY3804AB PO#:1800550.

Part: FAIRING — PEELING (ZN 100 FUS LOWER) · airframe 57,926 hrs · 30,275 cycles

R/H WING TOBODY FAIRING 192BR FWD END EXTERIOR SKIN PEELING MKD DOT<[01] DUPLICATE ITEM - THIS FAULT WILL BE ACCOMPLISHED ON FAULT #TTG8Q00KFNWQ;[02] VERIFIED DUPLICATED.

Part: FITTING — ELONGATED (ZN 500 LEFT WING) · airframe 57,926 hrs · 30,275 cycles

L/W REAR SPAR FIXED T/E PANEL 551GB INB FWD SUPPORT STRUT UPPER ATTACHED FITTING HAS ELONGATED HOLE MKD DOT<[01] REMOVED AND REPLACED SUPPORT STRUT AT PANEL # 551-GB. REF. SRM- 51-40-02-0G-0.;[02] INSPECTED REPLACEMENT OF BEAM FITTING.

Part: FILLER — MISSING (ZN 100 FUS LOWER) · airframe 57,427 hrs · 29,960 cycles

EXTERNAL POWER RECEPTACLE DOOR CUTOUT EXISTING CENTER LOWER REPAIR DOUBLER HAS MISSING MATERIAL.<[01] REMOVED AND REPLACED FILLER #13 FROM PREVIOUS REPAIR IAW SRM 53-10-15-2R-4

Part: RAIL — OUT OF ADJUST (GALLEY) · airframe 57,221 hrs · 29,821 cycles

GALLEY G4 TRASH COMPARTMENT OTBD FLOOR SLIDE RAIL NOT SECURE. SECURED GALLEY G4 TRASH COMPARTMENT OTBD FLOOR SLIDE RAIL PER SIP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,221 hrs · 29,821 cycles

L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT; EMERGENCY BATTERY POWER SUPPLY AND BATTERY PER AMM 35-51-06.

Part: SLIDE — OUT OF POSITION (FWD ENTRY DOOR) · airframe 55,950 hrs · 28,980 cycles

FWD ENTRY DOOR SLIDE LOOSE FROM COMPARTMENT / [01] SLIDE WAS NOT FULLY REMOVED; RESECURED SLIDE PER AMM 25-66-01

Part: PANEL — ELONGATED (FUSELAGE) · airframe 54,248 hrs · 27,899 cycles

193D PANEL HAS TWO EACH ELONGATED FASTENER HOLES AT AFT SIDE / [01] INSTALLED 193D PANEL PER AMM 53-51-21.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 54,248 hrs · 27,899 cycles

193E PANEL HAS TWO EACH ELONGATED FASTENER HOLES AT FWD END ; 194E PANEL HAS TWO EACH ELONGATED FASTENER HOLES AT FWD END / [01] INSTALLED NEW PANEL PER AMM 53-51-21

Part: COVER — LOOSE (CABIN) · airframe 53,792 hrs · 27,621 cycles

FIRST OFFICER SIDE OVER WING EXIT SIGN COVER CAME OFF. ; / [01] REINSTALL EMERGENCY.EXIT SIGN COVER PER MM 33-51-01

Part: LIGHT — INOPERATIVE · airframe 53,686 hrs · 27,552 cycles

LH EMERGENCY EXTERNAL EXIT LIGHT INOP ; / [01] REMOVED AND REPLACED LH EMERGENCY EXIT OVER WING LIGHT PER AMM 33-51-04. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (EXIT DOOR) · airframe 53,215 hrs · 27,280 cycles

EMERGENCY EXIT DOOR LIGHT INOP (SIDEWALL LIGHT) ; / [01] OK TO CONTINUE PER MEL 33-2-03 SP#1B. AUTH# 28531; [02] RELAMPED SIDEWALL LT REF AMM 33-21-00.

Part: SUPPORT — CORRODED (BS 727-767) · airframe 52,122 hrs · 26,630 cycles

CORROSION SUPPORT ZEE LOCATED BS727 TO BS767 AT LEVEL STR25R AND WL156.5 AT AFT CARGO COMPARTMENT / FABRICATED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL S-25R AND WL 156.5 AT AFT CARGO COMPARTMENT IAW B737-700 DRAWING 146A7502 SHEET 26 REV- REMOVAL AND INSTALL DOCUMENTED ON WORK INSTRUCTION N. 5366-E-16462-NG MATERIAL USED BAC1496-377 PO#2021-134015 AND FABRICATION SRM B737-700 51-10-02 STEP 9

Part: BAFFLE — CRACKED (BS 500-500A S26L) · airframe 52,122 hrs · 26,630 cycles

CRACK WEB BAFLE LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT AND ANGLES (2 E/A) / REPLACED WEB BAFLE AND ANGLES (CLIPS) 2EA LOC. BTW BS 500 TO BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING #143A7505 REV.-

Part: SKIN — DENTED (BS 827 S24L) · airframe 52,122 hrs · 26,630 cycles

HAS A DENT ON FUSELAGE SKIN LOCATED AT BST 827 AND 1 INCH ABOVE STRINGER 24 LH. THE DENT MEASURES ARE W:0.971; L:1.086; Y:0.024 AND W/Y 40 / REPAIRED FUSELAGE SKIN BETWEEN BST 807 TO BS 847 AND BETWEEN STRINGER 23L TO STRINGER 25L IAW SW EA # 21-153-01289 REV IR AND AEROMAN EA # 53-0230 -21 REVISION #0 FOR INSPECTION REQUIREMENT SEE TLD# T080561

Part: BRACKET — CRACKED (BS 947.5 S26L) · airframe 52,122 hrs · 26,630 cycles

CRACK BRACKET LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT / REPLACED BRACKET LOCATED BS 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02;.PART NUMBER USED #149A8113U6 P.O 2021- 147735

Part: WEB — CRACKED (BS 847-867) · airframe 52,122 hrs · 26,630 cycles

CRACK WEB - INTERCOSTAL LOCATED BS847 TO BS867 AT LEVEL STR25R AFT CARGO COMPARTMENT / REPLACED WEB-INTERCOSTAL LOCATED BTW BS 847 TO BS 867 AT LEVEL STR 25R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #146A0081 SHEET 25 REV. A.

Part: ANGLE — CRACKED (BS 727B-727D) · airframe 52,122 hrs · 26,630 cycles

CRACK ANGLE CEILING STRUCTURE LOCATED BS727B TO BS727D AND LBL 50 AT AFT CARGO COMPARTMENT / REPLACED ANGLE CEILING STRUCTURE LOCATED BS 727B TO BS 7270 AND LBL 50 AT AFT CARGO COMPARTMENT IO.A.E B737-700 SRM 51-10-02 ITEM 9 51-40-02. AND DWG:149A9490. REV:-

Part: SUPPORT — CRACKED (BS 767-787) · airframe 52,122 hrs · 26,630 cycles

CRACK SUPPORT ZEE LOCATED BS767 TO BS787 AT LEVEL STR 25L AFT CARGO COMPARTMENT / FABRICATED SUPPORT ZEE LOCATED BS 787 TO BS 747 AT LEVEL STR 25L AFT CARGO COMPARTMENT IAW B737- 700 DWG #146A7502 REV - REMOVAL AND INSTALL DOCUMENTED ON WORK INSTRUCTION # 5360-E-16462-NG

Part: ANGLE — CRACKED (BS 540) · airframe 52,122 hrs · 26,630 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BS540 AND BETWEEN RBL 24 TO LBL 24 CENTER SECTION (2 EA) / REPLACED ANGLE ON FLOOR STRUCTURE LOCATE BS 540 AND BTW RBL 24 TO LBL 24 CENTER SECTION 2 E/A IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9

Part: SUPPORT ANGLE — CRACKED (BS 695) · airframe 52,122 hrs · 26,630 cycles

CRACK SUPPORT ANGLE LOCATED BS695 AND BL0 CENTER SECTION / REPLACED SUPPORT ANGLE LOCATED BS 695 AND BL0 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9 SRM B737-700 51-40-02 AND DRAWING #273A9111 SHEET 8 REV A MATERIAL USED EXTRUSION P/N BAC 1490-2883 PO 2020-195975

Part: ANGLE — CRACKED (BS 400 S26R) · airframe 52,122 hrs · 26,630 cycles

CRACK ANGLE LOCATED BS400 AND S-26R FWD CARGO COMPARTMENT / REPLACED ANGLE LOCATED BS 400 AND STR -26R FWD CARGO COMPARTMENT DUE TO CRACK NOT ALLOWABLE DAMAGE PART NUMBER USED #143A7502U154 P.O 2020- 194108 IAW B737-700 SRM 51-10-02;51-40-02 AND DWG 143A7505 SHEET 2 REV.B

Part: STRINGER — CRACKED (BS 540 S23L) · airframe 52,122 hrs · 26,630 cycles

CRACK STRINGER 23L LOCATED BS 540 FWD CARGO COMPARTMENT / PERFORMED PERMANENT REPAIR ON STRINGER 23L LOCATED BTW BS500D TO BS540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206 MATERIAL USED BAC-1498-157-7075 T6 PO 2020-189930 BAC-1493-659 PO 2021-135083 AND ALUMINUM SHEET 7075 T6 0.040 PO 2020-189926

Part: NUT PLATE — BROKEN (FUSELAGE SKIN) · airframe 52,122 hrs · 26,630 cycles

BROKEN SKIN NUT PLATES BETWEEN BST 680 TO BST 696 AND BETWEEN STR 1 TO STR 2R AT UPPER FUSELAGE (2 EA) / PERFORMED REPAIR ON SKIN NUTPLATES BETWEEN BST 680 TO BST 696 AND BETWEEN STR 1 T OSTR 2R AT UPPER FUSELAGE IAW B737-700 53-40-01-2R-1 REPAIR 1. MATERIAL USED ALLUMINUM SHEET PN:2024T3.040' PO: 2021 129458

Part: ANGLE — CRACKED (ACCESS PANEL) · airframe 52,122 hrs · 26,630 cycles

CRACK ANGLE ACCESS PANEL 323BL INTERNAL AREA AT LEVEL BS1016 AT VERTICAL STABILIZER / REPLACED ANGLE ACCESS PANEL 323BL INTERNAL AREA AT LEVEL BS1016 AT VERTICAL STABILER IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9

Part: ANGLE — CRACKED (BS 400 S26L) · airframe 52,122 hrs · 26,630 cycles

CRACK ANGLE LOCATED BS400 AND S-26L FWD CARGO COMPARTMENT / REPLACED ANGLE LOCATED BS 400 AND STR -26R FWD CARGO COMPARTMENT DUE TO CRACK NOT ALLOWABLE DAMAGE PART NUMBER USED 143A7502U155 P.O 2020- 212944 IAW B737-700 SRM 51-40-02;51-10-02 ITEM 9 AND DWG 143A7505 SHEET 2 REV.B

Part: INTERCOSTAL — CRACKED (BS 847-867) · airframe 52,122 hrs · 26,630 cycles

CRACK INTERNAL STRUCTURE INTERCOSTAL WEB LOCATED BETWEEN BST 847 TO BST 867 AT AFT CARGO COMPARTMENT / CRACK INTERNAL STRUCTURE INTERCOSTAL WEB LOCATED BETWEEN BST 847 TO BST 867 AT AFT CARGO COMPARTMENT REPAIRED IAW SW EA #21-153-01384 REV IR AND AEROMAN EA #53-0261-21 REVISION #0 FOR INSPECTION REQUIREMENT SEE TLD #T080562 PERMANENT REPAIR LIMIT: REMOVED THE REPAIRED INTERCOSTAL ASSY AND REPLACE WITH A NEW PN 149A8105-3 INTERCOSTAL ASSY PER PRODUCTION DWG / SRM REQUIREMENTS SEE EA 21-153-0138A FOR DETAILS OF THE EXISTING

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 52,122 hrs · 26,630 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 27 INCHES FROM FRONT SPAR AT RT HORIZONTAL STABILIZER / PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED STAB STA 120.30 AND 27 INCHES FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10- 09-2R-5 FIG 204 MATERIAL USED KIT T-SECTION P/N 55100003-01 BATCH SW2021600734 ANGLE P/N BAC1490 -2738 PO 2017-503185

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 52,122 hrs · 26,630 cycles

CRACK INSPAR RIB LOCATED STAB STA120.30 AND 27 INCHES FROM FRONT SPAR LT HORIZONTAL STAB / PERFORMED PERMANENT REPAIR ON T-SECTION LOCATED AT 27' FROM FRONT SPAR OF INSPAR RIB AT STAB STA 120.30 AT LH HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4; STEP 4.B.(2) AND SRM 51-40-02. MATERIAL USED:KIT T-SECTION P/N:55100003 BATCH:SW2021000734

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 52,122 hrs · 26,630 cycles

CRACK LEADING EDGE PANEL AT RIB LE STA 105.26 AT LT HORIZONTAL STABILIZER / REPLACED RIB LOC LEADING EDGE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND DRAWING #186A1001 REV 'B' PN USED 186A1352-7 PO #2021-145767

Part: PRESSURE DECK — CRACKED (BS 663-675) · airframe 52,122 hrs · 26,630 cycles

CRACK INDICATION ON WEB HORIZONTAL PRESSURE WEB DECK LOCATED BETWEEN STA 663 TO STA 675 AND RBL 40 AT PASSENGER CABIN. (LENGTH OF CRACK 0.500 INCH) / REPAIRED HORIZONTAL PRESSURE DECK WEB LOCATED BETWEEN BS 663 TO BS 675 AND RBL 30 TO RBL 60. T PASSENGER CABIN IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 MATERIAL USED: PN:BAC1505-100052 PO:2021129586 AND P/N:2024T3-063 PO:2020-213292

Part: VAPOR BARRIER — CRACKED (R/H MLG W/W) · airframe 52,122 hrs · 26,630 cycles

CRACK BODY STATION 663.75 VAPOR BARRIER APROX RBL 49 AT MAIN WHEEL WELL COMPARTME / REPAIRED VAPOR BARRIER AT MAIN WHEEL WELL COMPART MENT ASPER B737-700 SRM 51-70-04-2R-10 REPAIR 10. TOOL USED CALIPER P/N:500-197-30;S/N:15121550;DUE DATE 24-MAY-21;HOT BONDER P/N:HCS9200B S/N:18185733 DUE DATE:11 DEC 21 SCALE P/N:SCA-301; S/N:AE-412134 DUE DATE:24 FEB 22; HOT BONDER P/N:HCS9000B; S/N:15092096; DUE DATE:14 DEC 21.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 52,122 hrs · 26,630 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 36 INCHES FROM FRONT SPAR AT RT HORIZONTAL STABILIZER / PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED STAB STA 120.30 AND 36' FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 FIG 204 MATERIAL USED KIT T-SECTION P/N 55100003-01 BATCH SW2021000734 ANGLE P/N BAC1490-2738 PO 2017- 50-3185

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 52,122 hrs · 26,630 cycles

CRACK LEADING EDGE PANEL ON LE STA 95.96 AT LT HORIZONTAL STABILIZER / REPLACED LEADING EDGE PANEL RIB CHORD ON LE STA 95.96 AT LT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING 186A1001 REV. A

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 52,122 hrs · 26,630 cycles

DEBONDED OB AFT FLAP SKIN T/E ON INBOARD EDGE AT LT WING / REPAIRED O/B AFT FLAP SKIN T/E ON INBOARD EDGE AT LT WING ASPER B737-700 SRM 57-53-01-2R-16 REP 16 AND B737-700 SRM 51-70-10-2R-0 REPAIR GENERAL.TOOL USED CALIPER P/N 500-197-30 S/N A18135103 DUE DATE 14JUN21. HOTBONDER P/N HCS9200B S/N 15102320 DUE DATE 19NOV21 SEE TLD T080556 FOR RE-INSPECTION REQUIREMENTS

Part: SKIN — DEBONDED (RT WING SLAT) · airframe 52,122 hrs · 26,630 cycles

DEBONDED SLAT 8 EXISTING REPAIR ON T/E OUTBOARD EDGE AT RT WING / REPLACED SLAT 8 AT RT WING IAW B737-700 AMM 27-81-21 AND INSTALLATION IS DOCUMENT DEFECT # L206230

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,040 hrs · 25,349 cycles

FWD ENTRY DOOR EMERGENCY LIGHTS INOP / REMOVED AND REPLACED BATTERY PACK EMERGENCY LIGHTS OPS CHECK GOOD REF. AMM 33-51-00

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 48,292 hrs · 24,241 cycles

L1 DOOR SLIDE PARTIALLY OUT OF PACK. / REPACKED SLIDE PER MT.

Part: PANEL — ELONGATED (LOWER EXT FUSELA) · airframe 48,018 hrs · 24,074 cycles

WING TO BODY FAIRING PANEL 193B HAS ENLARGED FASTNER HOLES AT LOCATIONS 2;17;32;34 & 36 MOD / REMOVED AND REPLACED WING TO BODY FAIRING PANEL 193B PER M/M 53-51-21

Part: GUARD — MISSING (SWITCH) · airframe 47,625 hrs · 23,811 cycles

AFT ATTENDANT PANEL EMERGENCY LIGHT BUTTON MISSING GUARD. INSTALLED GUARD IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,625 hrs · 23,811 cycles

EMERGENCY EXIT LIGHTS FROM MID CABIN AFT INOP LOCATION M1672. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,625 hrs · 23,811 cycles

FORWARD EMERGENCY AISLE LIGHTS INOPERATIVE. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,625 hrs · 23,811 cycles

EMERGENCY EXIT LIGHTS FROM MID CABIN AFT INOP LOCATION M1673. R&R BATTERY PACK PER AMM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 47,625 hrs · 23,811 cycles

FWD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / RECIEVED REPLACEMENT FWD CARGO BAY AFT CORNER SCUFF PLATE SI # 7530065. LOCATED AND DRILLED NEW SCUFF PLATE IAW SRM 51-40-05 83802U 26JUL19

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 47,625 hrs · 23,811 cycles

FWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / RECIEVED REPLACEMENT FWD. CARGO BAY FWD. CORNER SCUFF PLATE WITH SI # 7530406; LOCATED AND DRILL NEW SCUFF PLATE I.A.W / SRM 51-40-05

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 47,625 hrs · 23,811 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / RECIEVED REPLACEMENT AFT CARGO BAY FWD CORNER SCUFF PLATE SI # 7530659. LOCATED AND DRILLED NEW SCUFF PLATE IAW SRM 51-40-05 82802U 26JUL19

Part: NONE — CRACKED (AFT CARGO BAY) · airframe 47,625 hrs · 23,811 cycles

ACB AT BS927 TO 947 RBL21 BUFFLE IS CRACKED / REMOVED AND REPLACED BUFFLE AT ACB BS927 TO BS947 RBL21 P/N 147A7500Y22 PO#747059 IAW SRM 51-40-02 AND DWG 147A7500 REV - 89004U 09JUL19

Part: INSERT — DAMAGED (FLOOR PANEL) · airframe 47,625 hrs · 23,811 cycles

PASSENGER CABIN FLOOR PANEL 242UF HAD MULTIPLE DAMAGED INSERTS. R&R INSERTS IAW SRM.

Part: INSERT — DAMAGED (FLOOR PANEL) · airframe 47,625 hrs · 23,811 cycles

PASSENGER CABIN FLOOR PANEL 241ADF HAD DAMAGED INSERT. R&R INSERT IAW SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

DRAIN HOLE CRACKED AT BS. 663, LBL 31. REPAIRED DRAIN HOLE IAW EA AND ER.

Part: PANEL — DELAMINATED (RT HORIZ STAB) · airframe 47,625 hrs · 23,811 cycles

RIGHT HORIZ. STAB PANEL 343BB HAS AREA OF DELAMINATION ON FWD O/B CORNER / RIGHT HORIZONTAL STAB PANEL 242BB AREA OF DELAMINATION ON FWD OUTBOARD CORNER REPAIRED IAW SRM 51-70-05-2R-6 PER SRM 55-10-01-2R-9

Part: SUPPORT BRACKET — CRACKED (AFT SERVICE DOOR) · airframe 47,625 hrs · 23,811 cycles

AFT SERVICE DOOR LOWER HINGE ACCESS COVER HAS 2EA CRACKED SUPPORT BRACKETS. / REMOVED & REPLACED AFT SERVICE DOOR LOWER HINGE ACCESS COVER PANEL BRACKETS PER SRM 51-40-02-0G-0D STEP 4. FIGURE 8 & BOEING DRAWING 411A2119.

Part: PANEL — CORRODED (LOWER EXT FUSELA) · airframe 47,625 hrs · 23,811 cycles

WATER SERVICE PANEL 146AR HAS BUBBLING PAINT ON THE EXTERNAL SKIN (POSSIBLE CORROSION) / ACCOMPLISHED DETAILED DAMAGE REMOVAL; INSPECTION AND REPAIR INSTRUCTIONS TO WATER SERVICE DOOR 146AR IAW EA 1-752-2591 REV IR AND ATS ER 19-04209 REV IR

Part: CHANNEL — BENT (AFT CARGO COMPT) · airframe 47,625 hrs · 23,811 cycles

BENT ACB FLOOR SUPPORT STA 727E-747 RBL 3 WL 157 / REPAIRED AFT CARGO BAY; FLOOR SUPPORT CHANNEL AT BS 727E-747 RBL 3 WL 157 I.A.W SRM 53-00-53-2R-4 88302U 12JUN19

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS. 787+7 TO BS. 847, RBL 22. R&R THRESHOLD WEB IAW SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 767 TO BS. 787+7, RBL 22. R&R SHIELD IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

AFT CARGO BAY ON R/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 767, RBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

AFT CARGO BAY BULKHEAD SUPPORT ANGLE BRACKET CRACKED AT BS. 847+18, LBL 10. R&R BRACKET IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

AFT CARGO BAY ON LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 787, LBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: CARGO TRACK — CRACKED (BS 727-887) · airframe 47,625 hrs · 23,811 cycles

AFT CARGO BAY FLOOR TRACK CRACKED IN RADIUS OF MOUNTING TAB BETWEEN BS. 727+4 TO BS. 887, RBL 14. / R&R TIE DOWN TRACK IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

AFT CARGO BAY BULKHEAD TO FLOOR SUPPORT CORRODED AT BS. 947, BETWEEN LBL 10 TO RBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED AT BS. 500D, BETWEEN LBL 21 TO RBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: PANEL — CORRODED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

FORWARD CARGO BAY AFT BULKHEAD LEFT PANEL LOWER SUPPORT CORRODED AT BS. 500D, LBL 23. R&R PANEL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 420 TO BS. 440, RBL 21. R&R WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FWD CARGO RH) · airframe 47,625 hrs · 23,811 cycles

***CORROSION*** ON FORWARD CARGO BAY AFT BULKHEAD RIGHT PANEL LOWER SUPPORT AT B.S. 500D; R.B.L. 23; W.L. 155. / REMOVED AND REPLACED R/H LOWER SUPPORT PANEL FCB AT BS500D IAW SRM 51-40-02-0G-0 AND DWG 143A9481 - 143A7902 59205U 15JUL19

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 494 TO BS. 500A, RBL 21. R&R SUPPORT (SHIELD) IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

FORWARD CARGO BAY SUB WEB THRESHOLD CORRODED BETWEEN BS. 440 TO BS. 494, RBL 25. R&R SUB THRESHOLD WEB IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 400 TO BS. 500D, LBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 500A TO BS. 500D, RBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

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

Part: STRIP — BROKEN (RIGHT WING) · airframe 47,625 hrs · 23,811 cycles

RIGHT WING TRAILING EDGE WIGGLE STRIP IS BROKEN AT ORSS 261. / REMOVED AND REPLACED RIGHT WING TRAILING EDGE WIGGLE STRIP AT ORSS 261 P/N 115A2781-14 IAW SRM 51-40-02 AND AIPC 57-50-00-30. 88920U 28JUN19.

Part: WEB — DENTED (FUSELAGE) · airframe 47,625 hrs · 23,811 cycles

FLIGHT DECK FLOOR DENTED AT BS. 255, BETWEEN RBL 3 TO LBL 20. REPAIRED WEB IAW EA.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 47,359 hrs · 23,632 cycles

RT OVERWING EMERGENCY EXIT SIGN FELL OFF MOUNT. SECURED LENS SIGN PER MM.

Part: COVER — LOOSE (CABIN) · airframe 46,405 hrs · 23,045 cycles

LT OVERWING EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,276 hrs · 22,961 cycles

R1 DOOR EXTERNAL EMERGENCY LIGHT INOP DURING TEST. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,276 hrs · 22,961 cycles

FIRST BULLNOSE EMERGENCY LIGHT INOP DURING TEST. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,276 hrs · 22,961 cycles

R1 LOWER EXIT SIGN INOP DURING TEST. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,276 hrs · 22,961 cycles

FORWARD CEILING LIGHT INOP DURING TEST. R&R BATTERY PACK IAW AMM.

Part: LANDING — BROKEN (LWR FUSELAGE) · airframe 45,582 hrs · 22,516 cycles

A/C EXTERNAL POWER DOOR CUT OUT HAS A PIECE BROKEN OFF AND BENT SECTIONS NEAR MIDDLE DOOR LATCH PAD. / REPAIRED ELECTRICAL GROUND POWER RECEPTACLE LANDING IAW SRM 53-10-15-2R-4 REPAIR 4

Part: FAIRING — ELONGATED (RT WING) · airframe 45,582 hrs · 22,516 cycles

#6 FLAP SUPPORT FAIRING TAILCONE HAS LOOSE FASTERNERS AND ELONGATED HOLES. FIVE FASTERNERS HAVE BROKEN NUTPLATES / REMOVED & REPLACED #6 FLAP SUPPORT FAIRING TAILCONE; IAW SRM 51-40-02 & REMOVED & REPLACED ALL BROKEN NUTPLATES; (6EA); IAW SRM 51-40-02. APPLIED AERODYNAMIC SMOOTHING SEALANT; IAW SOPM 20-50-11. PAINTED TAILCONE WING GRAY 707 TO MATCH FAIRING IAW AMM 51-21-73

Part: BEAM — CRACKED (R1 DOOR) · airframe 44,250 hrs · 21,654 cycles

R1 DOOR CRACKED IN DOOR BEAM. R&R DOOR PER DWG.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 43,078 hrs · 20,936 cycles

L1 DOOR THRESHOLD EMERGENCY EXIT LIGHT LENS CRACKED. R & R THE LENS IAW AMM.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 43,078 hrs · 20,936 cycles

R2 DOOR THRESHOLD EMERGENCY EXIT LIGHT LENS CRACKED. R & R THE LENS IAW AMM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 42,820 hrs · 20,789 cycles

LT WHEEL WELL VAPOR BARRIER CRACKED. REPAIRED BARRIER PER SRM.

Part: COVER — MISSING (CABIN) · airframe 42,278 hrs · 20,429 cycles

RT OVERWING FORWARD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED COVER PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,012 hrs · 20,260 cycles

SKIN CRACKED AT BS 234.5, STR S22R. REPAIRED SKIN IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,604 hrs · 20,011 cycles

LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT BULB INOP. R&R BULB PER MM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 40,860 hrs · 19,550 cycles

MID CABIN FLOOR PANEL 241CF FWD OTBD CORNER IS CRUSHED / DELAMINATED. / REPAIRED MID CABIN FLOOR PANEL 241CF FWD OTBD CORNER I/A/W SRM 53-00-50-2R-4 REV 61 AND SRM 53-00-50-2R-0 REV 61

Part: VAPOR BARRIER — CRACKED (LT AC BAY) · airframe 40,860 hrs · 19,550 cycles

LEFT AC BAY AFT 663 BULKHEAD HAS 10 INCH CRACK IN COMPOSITE. / REPAIRED L/H AC BAY AFT 663 BULKHEAD IAW B737-700 SRM 57-10-10-2R-2 PARA 6 TABLE 215 REV 61

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 40,860 hrs · 19,550 cycles

PASS. CABIN FLOOR; UPR FLANGE OF INTERCOSTAL CRACKED AT BS 285; RBL 1. / REMOVED CRACKED PASS CABIN FLOOR; UPR FLANGE OF INTERCOSTAL AT BS 285 RBL 1 AND REPLACED IT WITH NEW PART P/N 141 AB 410V3 IAW DWG 141A5410 REV A AND SRM 1-40-02

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 40,860 hrs · 19,550 cycles

PASS. CABIN FLOOR; UPR FLANGE OF INTERCOSTAL HAS SEVERAL CRACKS AT FASTENER HOLES BETWEEN BS 380 AND BS 400; BL0. / REMOVED AND REPLACED UPPER FLANGE OF INTERCOSTAL BS 380 - 400 BL0 IAW SRM 51-40-02 AND DWG 143A5400 REV:D

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,860 hrs · 19,550 cycles

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

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 40,860 hrs · 19,550 cycles

MID CABIN LATERAL FLOOR SUPPORT HAT CHANNEL IS CRACKED BS 537; BL 0 - RBL 25. / REMOVED CRACKED MID CABIN LATERAL FLOOR SUPPORT HAT CHANNEL BS 537; BL0 - RBL25 AND REPLACED IT WITH NEW PART P/N: 143A5240 - 36 IAW DWG 143A0060 REV A; SRM 51-40-02 AND SRM 51-40-05. ATAG #WN9532

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 40,860 hrs · 19,550 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140AF HAS CORROSION ALONG EDGES (MARKED) / AFT CARGO FLOOR PNL 140AF HAS CORROSION. RECEIVED NEW PNL P/N 453A2610-34 'A' TAG WN2616 I/A/W BOEING DWG 453A2610 REV B.

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 40,860 hrs · 19,550 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140CF HAS CORROSION ALONG EDGES OF PANEL (MARKED) / AFT CARGO FLOOR PNL 140CF HAS CORROSION ALONG EDGES. NEW PNL P/N 453A2610-18 RECEIVED ON DEFECT NO. X575374.

Part: CHANNEL — CRACKED (MAIN CABIN) · airframe 40,860 hrs · 19,550 cycles

MID CABIN LATERAL FLOOR SUPPORT HAT CHANNEL IS CRACKED BS 537; BL 0 - LBL 25. / REMOVED CRACKED MID CABIN LATERAL FLOOR SUPPORT HAT CHANNEL BS 537; BL0 - LBL 25 AND REPLACED IT WITH P/N 143A5240-35 IAW DWG 143A0060 SRM 31-40-02 AND SRM 51-40-05

Part: FLOOR PANEL — CRACKED (FUSLAGE) · airframe 40,860 hrs · 19,550 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140CF HAS DENT WITH CRACK 34' FROM AFT EDGE / AFT CARGO FLOOR PNL 140CF HAS DENT AND CRACK. NEW PNL 140CF; P/N 453A2610-18 RECEIVED 'A' TAG WN9320 I/A/W BOEING DWG 453A2610 REV K.

Part: INTERCOSTAL — CRACKED (MAIN CABIN) · airframe 40,860 hrs · 19,550 cycles

PASS. COMPT FLOOR; UPR FLANGE OF INTERCOSTAL HAS SEVERAL CRACKS AT FASTENER HOLE AT BS 500D+3; BL 0. / REMOVED & REPLACED INTERCOSTAL AT STATION 500D+3 BL0 IAW BOEING DWG # 143A5400 REV -

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 40,860 hrs · 19,550 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140BF HAS CORROSION ALONG EDGES (MARKED) / AFT CARGO FLOOR PNL 140BF HAS CORROSION ALONG EDGES.NEW PNL 140BF P/N 453A2610-32. RECEIVED 'A' TAG WN7211 I/A/W BOEING DWG 453A2610 REV K.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 40,860 hrs · 19,550 cycles

LT WING TRAILING EDGE PANEL SUPPORT BRACKET INBOARD OF FLAP DEFLECTION CONTROL RIB CRACKED. R&R BRACKET IAW IPC AND SRM.

Part: FLOOR PANEL — CORRODED (FWD CARGO COMPT) · airframe 40,860 hrs · 19,550 cycles

FWD PIT FLOORBOARD 120 CF HAS CORROSION / REMOVED & REPLACED FWD PIT FLOORBOARD 120CF IAW BOEING DWG 453A610-32 REV T; 453A100 REV C & SRM 51-40-02-0G-0 & AMM 51-21-41-370-802; 51-21-72-370-804.

Part: PLATE — CRACKED (LT WING) · airframe 40,860 hrs · 19,550 cycles

LT WING TRAILING EDGE WAFFLE PLATE INBOARD OF PYLON SAIL TAIL CRACKED. R&R WAFFLE PLATE IAW SRM AND DWG.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 40,860 hrs · 19,550 cycles

LT WING TRAILING EDGE SEAL SUPPORT BRACKET ABOVE PYLON SAIL TAIL CRACKED. R&R BRACKET IAW IPC AND SRM.

Part: RIB — CRACKED (RIGHT WING) · airframe 40,860 hrs · 19,550 cycles

R/H WING T/E SPAR AT 7' INBD OF THE DEFLECTOR RIB SEAL RETAINER FWD SIDE IS CRACKED / RH WING T/E SPAR AT 7' INBD OF THE DEFLECTOR RIB SEAL RETAINER FWD SIDE IS CRACKED - REMOVED CRACKED DEFLECTOR RIB AND REPLACED WITH NEW RIB IAW SRM 51-40-02-0G-0 AND BOEING DWG # 115A2930 REV A

Part: FITTING — BROKEN (LOWER EXT FUSELA) · airframe 40,860 hrs · 19,550 cycles

FWD KEEL BEAM CNTR ACCESS PANEL FWD LH ATTACH POINT ANGLE IS BROKEN OFF / REMOVED AND REPLACED FWD KEEL BEAM CNTR ACCESS PANEL FWD L/H ATTACH FITTING IAW SRM 51-40-02 A55686

Part: FAIRING — DELAMINATED (LOWER EXT FUSELA) · airframe 40,860 hrs · 19,550 cycles

LEFT SIDE LOWER BODY FAIRING #192AL; HAS 1' DELAM ON EXTERIOR SKIN. 9.5' FORWARD OF AFT EDGE AND 3.25' OUTBOARD OF INBOARD EDGE. / REPAIRED LEFT SIDE LOWER BODY FAIRING # 192AL EXTERIOR AFT INBOARD SKIN AS REQ IAW B737-700 SRM 51-70-04-2R-1 REPAIR 1 PAR 4 (A-G) REV 61. RESTORED FINISH IAW B737 AMM 51-21-99-300-801 PAR 2 E. 6 REV 62

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 40,860 hrs · 19,550 cycles

LT WING TRAILING EDGE SEAL SUPPORT BRACKET INBOARD OF FLAP DEFLECTION CONTROL RIB CRACKED. R&R BRACKET IAW IPC AND SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 40,860 hrs · 19,550 cycles

AFT PIT FWD CORNER SCUFF PLATE CRACKED / REPAIRED AFT PIT FWD CORNER SCUFF PLATE ACCOMPLISHED ON W/O 35788-1600-0001 IAW EA 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 40,860 hrs · 19,550 cycles

FWD PIT AFT CORNER SCUFF PLATE CRACKED / REPAIR ON FWD PIT AFT CORNER SCUFF PLATE ACCOMPLISHED ON W/O 35788-1400-0001 IAW EA # 1-A53-2076 REV 11

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 40,631 hrs · 19,407 cycles

RIGHT OVERWING EXIT SIGN LENS MISSING. R & R THE SIGN IAW MM.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 39,487 hrs · 18,723 cycles

RIGHT OVERWING EXIT SIGN COVER DETACHED. SECURED THE SIGN IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,066 hrs · 17,872 cycles

RIGHT BULLNOSE EMERGENCY LIGHT INOPERATIVE AT ROW 8. REPLACED THE LAMPS IAW AMM.

Part: SWITCH — OUT OF ADJUST (COCKPIT) · airframe 36,496 hrs · 16,943 cycles

AIR TURN BACK, DURING CLIMB OUT, GEAR HANDLE WAS RAISED, BUT GEAR REMAINED DOWN & LOCKED. CYCLED GEAR. R & R S1186 SWITCH IAW SAM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,211 hrs · 16,778 cycles

EMERGENCY EXIT NOT ARMED LIGHT ON P5 BULB INOPERATIVE. RELAMPED BULB IAW AMM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 36,211 hrs · 16,778 cycles

RIGHT EMER EXIT LIGHTS INOPERATIVE, BETWEEN ROWS 5 ABC & 8 ABC. REPAIRED BATTERY PACK M1674 CONNECTOR IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,211 hrs · 16,778 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 7 ABC. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,211 hrs · 16,778 cycles

AFT ENTRY CEILING EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,211 hrs · 16,778 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 8 ABC. RELAMPED IAW MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 36,211 hrs · 16,778 cycles

L2 DOOR SLIDE, OUT OF ADJUSTMENT. REPOSITIONED SLIDE IAW MM.

Part: RETAINING CLIP — BROKEN (CABIN) · airframe 36,211 hrs · 16,778 cycles

LEFT OVERWING EXIT LIGHT LENS RETAINER CLIP BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: RETAINER — BROKEN (CABIN) · airframe 36,211 hrs · 16,778 cycles

FORWARD CLOSE OUT CEILING PANEL EXIT LIGHT LENS RETAINER BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: RETAINING CLIP — BROKEN (CABIN) · airframe 36,211 hrs · 16,778 cycles

RIGHT OVERWING EXIT LIGHT LENS RETAINER CLIP BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,211 hrs · 16,778 cycles

INTERCOSTAL CORRODED, BETWEEN BS 747 - 767, STRINGER 25R. R & R INTERCOSTAL IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,211 hrs · 16,778 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 767 - 727, BETWEEN STRINGER 25R - 26R. REPAIRED SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,211 hrs · 16,778 cycles

AFT CARGO COMPARTMENT, FLOOR CROSS SUPPORT MEMBER CORRODED AT BS 887, BETWEEN STRINGER 25R TO 26L. R & R IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 36,211 hrs · 16,778 cycles

INTERCOSTAL CORRODED, BETWEEN BS 727A - 727B, BETWEEN STRINGER 25R - 26R. R & R INTERCOSTAL IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,211 hrs · 16,778 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 827 - 727, STRINGER 25L - 26L. R & R SUPPORT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,211 hrs · 16,778 cycles

FUSELAGE SKIN CRACKED AT STATION 540, STRINGER 22L. REPAIRED SKIN IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 36,211 hrs · 16,778 cycles

LEFT NR 3 COCKPIT WINDOW POST CRACKED. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 36,211 hrs · 16,778 cycles

RIGHT NR 3 COCKPIT WINDOW POST CRACKED. REPAIRED POST IAW ACO.

Part: SKIN — CRACKED (FLAP FAIRING) · airframe 36,211 hrs · 16,778 cycles

RIGHT WING FLAP FAIRING 642BB, INNER SKIN CRACKED, JUST FWD OF 4TH DRAIN HOLE FROM LE. REPAIRED SKIN IAW AMM & SRM.