N221WN

Part: CHARGER — SMOKE (ZN 200 FUS TOP) · airframe 66,516 hrs · 39,497 cycles

THERE IS SMOKE COMING FROM FWD RT EMERGENCY LIGHTING CHARGER AND BATTERY PACK. REMOVED AND REPLACED FWD R/H CHARGER AND BATTERY PACK PER M/M 33-51-06

Part: BATTERY PACK — SMOKE (ZONE 200) · airframe 66,516 hrs · 39,497 cycles

THERE IS SMOKE COMING FROM FWD RT EMERGENCY LIGHTING CHARGER AND BATTERY PACK. REMOVED AND REPLACED FWD R/H CHARGER AND BATTERY PACK PER M/M 33-51-06.

Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 65,563 hrs · 38,921 cycles

FA REPORTS AFT SERVICE DOOR SLIDE PRESSURE OUT OF RANGE <[01]. 02 - INSPECTED PER [AMM 25-66-01-200-801-NG (ESCAPE SLIDE PACK INFLATION CYLINDER CHECK - PERMANENT)] FOUND AFT ENTER DOOR SLIDE TO BE WITHIN 1 NEEDLE WIDTH OF GREEN BAND AND IS WITHIN NORMAL RANGE.

Part: TRANSMISSION — FAULTY (ZONE 100) · airframe 65,433 hrs · 38,839 cycles

FLAP LOCKOUT ON APPROACH. <[01] SERVICED TRAILING EDGE FLAP TRANSMISSION #1 AND #8 IAW AMM 12-22-51 AND PERFORMED TRAILING EDGE FLAP SYSTEM OPERATIONAL CHECK IAW AMM 27-51-00 AND OPS CHECK GOOD.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 65,130 hrs · 38,662 cycles

(CUSTOMER REQUEST) CRACK ON LOWER CHORD ASSY BS 663 AND RBL 10 AT LOWER FUSELAGE 2025-224536<[01] TOOLS USED: POWER PACK P/N: PE1068 S/N: PE0118-94826 DUE DATE: 24-SEP-25. THERMOMETER P/N: FLUKE 566 S/N: 65900156WS DUE DATE: 23-OCT-25.;[02] REPLACED LOWER CHORD ASSY BS 663 AND RBL 10 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02-0G AND DWG 111A1000 SHEET 180 REV. B .SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2.REPLACED LOWER CHORD ASSY BS 663 AND RBL 15 TO LBL 15 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02-0G AND DWG 111A1000 SHEET 180 REV. B .SEE INDIVIDUAL SIGN OFF BELOW.;[04] COMPLETED TASK CERTIFIED

Part: RIB — CRACKED (ZONE 500) · airframe 65,130 hrs · 38,662 cycles

CRACK INSPAR RIB LOWER SIDE LOC. ON FRONT SPAR RIB 120.30 AT LT HORIZONTAL STABILIZER 2025-224531<[01] TOOL USED ON ITEM 3 AND 4: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 60007161486; DUE DATE: 06-SEP-25;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26. TEMPERATURE CONTROLLER: P/N: P3015GOES00000 S/N: 112820025 DUE DATE: 28-JAN-26.;[03] REJECTED STEP 9 DUE TO INCORRECT BEND PROCESS ON REPAIR ANGLE [2];[04] VERIFIED MINIMUM BENT RADIUS ON ANGLE LOWER SIDE LOC. ON FRONT SPAR RIB 120.30 AT LT HORIZONTAL STABILIZER IAW SRM B737-700 51-30-01 FIGURE 3 TABLE A; SHEET 1; TOOL USED: PRECISION RADIUS GAUGE P/N: S167C S/N: AE-28535 DUE DATE: 04-SEP-25;[05] RIIRJCT RESOLUTION<BR>VERIFIED MINIMUM BENT RADIUS ON ANGLE LOWER SIDE LOC. ON FRONT SPAR RIB 120.30 AT LT HORIZONTAL STABILIZER IAW SRM B737-700 51-30-01 FIGURE 3 TABLE A; SHEET 1; FOUND WITHIN TOLERANCE.;[06] TOOL USED: RADIOMETER/PHOTOMETER KIT; P/N XRP-3000; S/N: 1753759; DUE DATE: 30-JUN-25.;[07] REPAIRED INSPAR RIB LOWER SIDE LOC. ON FRONT SPAR RIB 120.30 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM: 55-10-09-2R-5 REPAIR 5. SEE INDIVIDUAL SIGN OFF BELOW.;[08] REPAIRED INSPAR RIB LOWER SIDE LOC. ON FRONT SPAR RIB 120.30 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM: 55-10-09-2R-5 REPAIR 5. SEE INDIVIDUAL SIGN OFF BELOW<BR>RII

Part: RIB — CRACKED (ZONE 300) · airframe 65,130 hrs · 38,662 cycles

CRACK INSPAR RIB LOWER SIDE LOC. ON FRONT SPAR RIB 120.30 AT LT HORIZONTAL STABILIZER 2025-224531<[01] TOOL USED ON ITEM 3 AND 4: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 60007161486; DUE DATE: 06-SEP-25;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26. TEMPERATURE CONTROLLER: P/N: P3015GOES00000 S/N: 112820025 DUE DATE: 28-JAN-26.;[03] REJECTED STEP 9 DUE TO INCORRECT BEND PROCESS ON REPAIR ANGLE [2];[04] VERIFIED MINIMUM BENT RADIUS ON ANGLE LOWER SIDE LOC. ON FRONT SPAR RIB 120.30 AT LT HORIZONTAL STABILIZER IAW SRM B737-700 51-30-01 FIGURE 3 TABLE A; SHEET 1; TOOL USED: PRECISION RADIUS GAUGE P/N: S167C S/N: AE-28535 DUE DATE: 04-SEP-25;[05] RIIRJCT RESOLUTION<BR>VERIFIED MINIMUM BENT RADIUS ON ANGLE LOWER SIDE LOC. ON FRONT SPAR RIB 120.30 AT LT HORIZONTAL STABILIZER IAW SRM B737-700 51-30-01 FIGURE 3 TABLE A; SHEET 1; FOUND WITHIN TOLERANCE.;[06] TOOL USED: RADIOMETER/PHOTOMETER KIT; P/N XRP-3000; S/N: 1753759; DUE DATE: 30-JUN-25.;[07] REPAIRED INSPAR RIB LOWER SIDE LOC. ON FRONT SPAR RIB 120.30 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM: 55-10-09-2R-5 REPAIR 5. SEE INDIVIDUAL SIGN OFF BELOW.;[08] REPAIRED INSPAR RIB LOWER SIDE LOC. ON FRONT SPAR RIB 120.30 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM: 55-10-09-2R-5 REPAIR 5. SEE INDIVIDUAL SIGN OFF BELOW<BR>RII

Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 65,130 hrs · 38,662 cycles

CRACK ACCESS PANEL 343AT ON PLATE AT RT HORIZONTAL STABILIZER 2025-224508<[01] REPLACED BLADE AY AT ACCESS PANEL 343AT LOCATED RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G;[02] REPLACED BLADE AY AT ACCESS PANEL 343AT LOCATED RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G

Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 65,130 hrs · 38,662 cycles

CRACK ACCESS PANEL 343AT ON PLATE AT RT HORIZONTAL STABILIZER 2025-224508<[01] REPLACED BLADE AY AT ACCESS PANEL 343AT LOCATED RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G;[02] REPLACED BLADE AY AT ACCESS PANEL 343AT LOCATED RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G

Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 65,130 hrs · 38,662 cycles

CRACK ACCESS PANEL 333AT ON PLATE AT LH HORIZONTAL STABILIZER 2025-224509<[01] REPLACED BLADE ASSY AT ACCESS PANEL 333AT LOCATED LH HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G;[02] REPLACED BLADE ASSY AT ACCESS PANEL 333AT LOCATED LH HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G

Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 65,130 hrs · 38,662 cycles

CRACK ACCESS PANEL 333AT ON PLATE AT LH HORIZONTAL STABILIZER 2025-224509<[01] REPLACED BLADE ASSY AT ACCESS PANEL 333AT LOCATED LH HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G;[02] REPLACED BLADE ASSY AT ACCESS PANEL 333AT LOCATED LH HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G

Part: SUPPORT ANGLE — CRACKED (ZONE 600) · airframe 65,130 hrs · 38,662 cycles

CRACK ON SUPPORT ANGLE LOCATED AUXILIARY TRACK INBOARD POSITION OF SLAT 8 AT RT WING 2025-224502<[01] REPLACED SKIN TAB SUPPORT ANGLE LOCATED ON AUXILIARY TRACK INBOARD POSITION OF SLAT 8 AT RT WING I.A.W. B737-700 CMM 57-43-01.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SKIN TAB SUPPORT ANGLE LOCATED ON AUXILIARY TRACK INBOARD POSITION OF SLAT 8 AT RT WING I.A.W. B737-700 CMM 57-43-01.<BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 65,130 hrs · 38,662 cycles

(CUSTOMER REQUEST) CRACK ON SUPPORT BRACKET LOCATED BS 663 AND RBL 45.6 TO RBL 54.21 VAPOR BARRIER 2025-224491<[01] TOOL USED TEMPERATURE CONTROLLED P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 28-JAN-26.;[02] REPLACED SUPPORT BRACKET LOCATED BS 663 AND RBL 45.6 TO RBL 54.21 VAPOR BARRIER IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING# 111A1001 REV:-; SEE INDIVIDUAL SIGNOFF BELOW.;[03] TASK COMPLETED

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 65,130 hrs · 38,662 cycles

CRACK ON SUPPORT ANGLE LOCATED BS294.5 AND STR13L AT PASSENGER CABIN 2025-224489<[01] REPLACED SUPPORT ANGLE LOCATED ON BS294.5 AND STR13L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1311; SHEET: 1 AND REV: C.<BR>SEE INDIVIDUAL SING-OFF BELOW.;[02] RII.<BR>REPLACED SUPPORT ANGLE LOCATED ON BS294.5 AND STR13L AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1311; SHEET: 1 AND REV: C.<BR>SEE INDIVIDUAL SING-OFF BELOW.

Part: LENS — BROKEN (ZONE 200) · airframe 65,130 hrs · 38,662 cycles

BROKEN EMERGENCY EXIT LENS ASSY ON SIDEWALL PANEL 231YHW AT PASSENGER CABIN (1 EA) 2025-224464<[01] REPLACED EMERGENCY EXIT LENS ASSY ON SIDEWALL PANEL 231YHW AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-01-960-801;[02] REPLACED EMERGENCY EXIT LENS ASSY ON SIDEWALL PANEL 231YHW AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-01-960-801

Part: SEAL — CRACKED (ZONE 300) · airframe 65,130 hrs · 38,662 cycles

CRACK SEAL - PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB 2025-224433<[01] REPLACED SEAL - PLATE LOCATED ON ACCESS PANEL 343AB AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02-OG.;[02] REPLACED SEAL - PLATE LOCATED ON ACCESS PANEL 343AB AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02-OG.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 65,130 hrs · 38,662 cycles

INOP EMERGENCY LIGHT ASSY ON OVERHEAD STOWAGE BIN ROW POSITION 11 AND 13 RH SIDE AT PASSENGER CABIN (2EA) 2025-224249<[01] REPLACED EMERGENCY LIGHT ASSY ON OVERHEAD STOWAGE BIN ROW POSITION 11 AND 13 RH SIDE AT PASSENGER CABIN (2EA) IAW B737-700 AMM 33-51-03-960-802. PERFORMED OPERATIONAL TEST. TEST IS OK.;[02] JOB COMPLETED

Part: WEB — CORRODED (ZONE 100) · airframe 65,130 hrs · 38,662 cycles

CORROSION SHIELD WEB LOCATED BTW BS492.4 TO BS500A RBL25 WL156 AT FWD CARGO COMPARTMENT 2025-224411<[01] TOOL USED ON STEP 3: ULTRASONIC EQUIPMENT P/N 45MG; S/N 130066701 DUE DATE 12-JUL-25;[02] REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS492.4 TO BS500A RBL25 WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080 SHEET 23 REV: ? SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS492.4 TO BS500A RBL25 WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080 SHEET 23 REV: ? <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SKIN — DEBONDED (ZONE 500 FLAP) · airframe 65,130 hrs · 38,662 cycles

CUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT LT WING 2025-224275<[01] TOOL USED CALIPER PN: 8647A42; SN: A22356048; DUE DATE: 25/JUL/25.;[02] TOOL USED: AUDIBLE BOND TESTER; P/N S-3; S/N: 064; CAL DUE DATE: 27-AUG-25;[03] TOOL USED ON STEP 18 ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 15-OCT-25;[04] PERFORMED INTERIM REPAIR ON OB AFT FLAP ON IB SIDE AT LT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. AND THE REPAIR REQUIRES TAP TEST INSPECTION EVERY 6;875 FC OR 30 MONTHS WHICHEVER COMES FIRST. SEE INDIVIDUAL SIGNOFF BELOW.;[05] PERFORMED INTERIM REPAIR ON OB AFT FLAP ON IB SIDE AT LT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. AND THE REPAIR REQUIRES TAP TEST INSPECTION EVERY 6;875 FC OR 30 MONTHS WHICHEVER COMES FIRST. SEE INDIVIDUAL SIGNOFF BELOW.;[06] CORRECTIVE ACTION 5 CORRECTED. PERFORMED INTERIM REPAIR ON OB AFT FLAP ON IB SIDE AT LT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. AND THE REPAIR REQUIRES TAP TEST INSPECTION EVERY 6;875 FC OR 30 MONTHS WHICHEVER COMES FIRST. SEE INDIVIDUAL SIGNOFF BELOW. RII ACCOMPLISHED

Part: SKIN — DEBONDED (ZONE 500 FLAP) · airframe 65,130 hrs · 38,662 cycles

CUSTOMER REQUEST - DEBONDED OB AFT FLAP ON IB SIDE AT LT WING 2025-224275<[01] TOOL USED CALIPER PN: 8647A42; SN: A22356048; DUE DATE: 25/JUL/25.;[02] TOOL USED: AUDIBLE BOND TESTER; P/N S-3; S/N: 064; CAL DUE DATE: 27-AUG-25;[03] TOOL USED ON STEP 18 ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 15-OCT-25;[04] PERFORMED INTERIM REPAIR ON OB AFT FLAP ON IB SIDE AT LT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. AND THE REPAIR REQUIRES TAP TEST INSPECTION EVERY 6;875 FC OR 30 MONTHS WHICHEVER COMES FIRST. SEE INDIVIDUAL SIGNOFF BELOW.;[05] PERFORMED INTERIM REPAIR ON OB AFT FLAP ON IB SIDE AT LT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. AND THE REPAIR REQUIRES TAP TEST INSPECTION EVERY 6;875 FC OR 30 MONTHS WHICHEVER COMES FIRST. SEE INDIVIDUAL SIGNOFF BELOW.;[06] CORRECTIVE ACTION 5 CORRECTED. PERFORMED INTERIM REPAIR ON OB AFT FLAP ON IB SIDE AT LT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. AND THE REPAIR REQUIRES TAP TEST INSPECTION EVERY 6;875 FC OR 30 MONTHS WHICHEVER COMES FIRST. SEE INDIVIDUAL SIGNOFF BELOW. RII ACCOMPLISHED

Part: RIB — CRACKED (ZONE 300) · airframe 65,130 hrs · 38,662 cycles

CRACK ON INSPAR RIB LOCATED STAB STA 120.30 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL STAB 2025-224224<[01] TOOL USED IN STEP 5: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 200053402 DUE DATE: 16-SEP-25. ELECTRONIC CALIPER P/N: 500-196-30 S/N: A23048253 DUE DATE: 05-JUN-25.;[02] TOOL USED IN STEP 6: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 200053402 DUE DATE: 16-SEP-25;[03] TOOL USED ON STEP 8 AND 9: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S/N: 210138103 DUE DATE: 28-JAN-26;[04] REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL STAB IAW SRM B737-700 55-10-09-2R-5 REPAIR 5; SEE INDIVIDUAL SIGNOFF BELOW.;[05] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNOFF BELOW.

Part: GUSSET — CRACKED (ZONE 100) · airframe 65,130 hrs · 38,662 cycles

CRACK GUSSET LOCATED BS 500D AND S-19L FWD CARGO COMPARTMENT 2025-224210<[01] REPLACED GUSSET LOCATED BS 500D AND S-19L FWD CARGO COMPARTMENT IAW B737-700 B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 174 REV: ?;[02] REPLACED GUSSET LOCATED BS 500D AND S-19L FWD CARGO COMPARTMENT IAW B737-700 B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 174 REV: ?

Part: RIB — CRACKED (ZONE 300) · airframe 65,130 hrs · 38,662 cycles

CRACK ON INSPAR RIB LOCATED STAB STA 120.30 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL STAB 2025-224224<[01] TOOL USED IN STEP 5: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 200053402 DUE DATE: 16-SEP-25. ELECTRONIC CALIPER P/N: 500-196-30 S/N: A23048253 DUE DATE: 05-JUN-25.;[02] TOOL USED IN STEP 6: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 200053402 DUE DATE: 16-SEP-25;[03] TOOL USED ON STEP 8 AND 9: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S/N: 210138103 DUE DATE: 28-JAN-26;[04] REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL STAB IAW SRM B737-700 55-10-09-2R-5 REPAIR 5; SEE INDIVIDUAL SIGNOFF BELOW.;[05] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGNOFF BELOW.

Part: GUSSET — CRACKED (ZONE 100) · airframe 65,130 hrs · 38,662 cycles

CRACK GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT 2025-224211<[01] REPLACED GUSSET AND FASTENERS LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; AND DWG 143A7902 SHEET:147 REV:- SEE INDIVIDUAL SIGNS OFF BELOW;[02] CORRECTED STEP 1: <BR>REPLACED GUSSET AND FASTENERS LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; AND DWG 143A7902 SHEET:174 REV:- SEE INDIVIDUAL SIGNS OFF BELOW;[03] REPLACED GUSSET AND FASTENERS LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; AND DWG 143A7902 SHEET:174 REV:- <BR>RII<BR>SEE INDIVIDUAL SIGNS OFF BELOW

Part: FRAME — CRACKED (ZONE 100) · airframe 65,130 hrs · 38,662 cycles

CRACK FRAME LOCATED BS259.5 BTW STR8R TO STR9R AT PASSENGER CABIN 2025-224171<[01] STEP 4 TOOL USED: EDDY CURRENT EQUIPMENT PN: NORTEC 600D SN: 210138003 DUE DATE: 11-JUN-25;[02] REPAIRED FRAME - WEB AT BSTA 259.5 - BTW WL 240 & WL 280 AND BTW RBL 20 AND RBL 50 IAW EA#25-153-00828-WIP1;25-153-00828-WIP2 AND SUMMARY EA#25-153-00828 SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPAIRED FRAME - WEB AT BSTA 259.5 - BTW WL 240 & WL 280 AND BTW RBL 20 AND RBL 50 IAW EA#25-153-00828-WIP1;25-153-00828-WIP2 AND SUMMARY EA#25-153-00828 SEE INDIVIDUAL SIGNOFF BELOW.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 65,130 hrs · 38,662 cycles

CRACK ANGLE LOCATED BS540 RBL1 AT CENTER WING BOX 2025-224187<[01] REPLACED BRAKE PANEL AND FASTENERS LOCATED BS 540 BETWEEN BL 0 AND RBL 24.75 AT PASSENGER CABIN. IAW B737-700 SRM: 51-40-02 AND DWG:143A0060;SHEET:44;REV:A SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 65,130 hrs · 38,662 cycles

CRACK ANGLE LOCATED BS540 LBL1 AT CENTER WING BOX 2025-224186<[01] REPLACED BRAKE PANEL AND FASTENERS LOC FLOOR STRUCTURE BS 540 BETWEEN BL O AND LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG: 143A0060; SHEET:44;REV:A. SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1: REPLACED ANGLE (BRAKE PANEL) AND FASTENERS LOC FLOOR STRUCTURE BS 540 BETWEEN BL O AND LBL 24.75 AT CENTER WING BOX PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG: 143A0060; SHEET:44;REV:A. SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED ANGLE (BRAKE PANEL) AND FASTENERS LOC FLOOR STRUCTURE BS 540 BETWEEN BL O AND LBL 24.75 AT CENTER WING BOX PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG: 143A0060; SHEET:44;REV:A. SEE INDIVIDUAL SIGN OFF BELOW

Part: LIGHT — BROKEN (ZONE 200) · airframe 65,130 hrs · 38,662 cycles

BROKEN FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) 2025-224172<[01] REPLACED FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) IAW B737-700 AMM 33-51-15-400-8020;[02] CORRECTED STEP 1 <BR>REPLACED FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) IAW B737-700 AMM 33-51-15-400-802;[03] CERTIFIED <BR>REPLACED FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) IAW B737-700 AMM 33-51-15-400-802

Part: ANGLE — CRACKED (ZONE 200) · airframe 65,130 hrs · 38,662 cycles

CRACK ANGLE LOCATED BS695 RBL24.75 AT CENTER WING BOX 2025-224192<[01] PERFORMED VISUAL INSPECTION ON ANGLE LOCATED BS695 RBL24.75 AT CENTER WING BOX AND NOT FOUND DAMAGE; ANGLE FOUND IN GOOD CONDITIONS IAW B737-700 SRM 51-10-02-0G.;[02] CORRECTED STEP 1.<BR>PERFORMED VISUAL INSPECTION ON ANGLE LOCATED BS695 RBL24.75 AT CENTER WING BOX AND NOT FOUND DAMAGE; ONLY MISSING PROTECTIVE TREATMENT ANGLE AND APPLIED PROTECTIVE TREATMENT IAW SRM B737-700 51-20-01;MATERIAL USED PRIMER+CURE SOLUTION; P/N: 10P4-2+EC-117S; P/O: 2024-272681/001 AND EXPIRE DATE: 30-MAY-26;[03] COMPLETED ACTION 2

Part: ACCESS PANEL — DELAMINATED (ZONE 100) · airframe 65,130 hrs · 38,662 cycles

DELAMINATED ACCESS PANEL 193CL AT LOWER FUSELAGE 2025-224103<[01] TOOL USED: CALIPER PN: 8647A42 SN: B22440130 DUE DATE: 20-SEP-25.;[02] TOOL USED: SCALE PN: 91847 SN: AE-409315 DUE DATE: 29-JUN-25.;[03] TOOL USED: HUMIDITY/TEMPERATURE CHART RECORDER P/N: TH800 ; S/N: 08193228 ; DUE DATE: 23-AUG-25;[04] TOOL USED: MULTIMETER P/N: FLUKE-289; S/N: 01180136; DUE DATE: 10-JUL-25.;[05] REPAIRED ACCESS PANEL 193CL IAW B737-700 SRM 51-70-04-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[06] REPAIRED ACCESS PANEL 193CL IAW B737-700 SRM 51-70-04-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 65,130 hrs · 38,662 cycles

(CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOC ON BS 663.75 ON RBL 34 AT MAIN WHEEL WHEEL COMPARTMENT 2025-224146<[01] TOOL USED: CALIPER P/N: 500-196-30; S/N: A23378547; DUE DATE: 16 SEP 25.;[02] TOOL USED: HOT HONDER P/N: HCS9000B; S/N: 18175469; DUE DATE: 14 AUG 25.;[03] TOOL USED: SCALE P/N: 91847; S/N:AE-409319; DUE DATE: 29-SEP-25.;[04] TOOL USED: SCALE P/N: 91847; S/N:AE-409313; DUE DATE: 29-JUN-25.;[05] ULTRASONIC EQUIPMENT USED P/N: EPOCH 650; S/N: 190984811; DUE DATE: 24-FEB-26;[06] REPAIRED VAPOR BARRIER LOC ON BS 663.75 ON RBL 34 AT MAIN WHEEL WHEEL COMPARTMENT AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGN OFFS BELOW;[07] TASK COMPLETED ; RII ITEM <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 64,924 hrs · 38,529 cycles

FOUND EMERGENCY LIGHTS AT ROWS 14CBA - 23CBA; AFT RH DOOR OH LIGHT & LH DOOR ESCAPE SLIDE LIGHT OUT <[01]. REPLACED BATTERY PACK EQUIP #M1673 IAW AMM 33-51-06. OPS CHECK GOOD.

Part: SLIDE — OUT OF POSITION (ZONE 800) · airframe 64,650 hrs · 38,361 cycles

CREW REQUEST AFT ENTRY DOOR SLIDE TO BE REPOSITIONED IN THE SLIDE COMPARTMENT.<[01] REPOSITIONED AE DOOR SLIDE INSIDE THE COMPARTMENT PER MT 725-61-06.

Part: LIGHT — MISSING (ZONE 200) · airframe 64,534 hrs · 38,279 cycles

EMERGENCY EXIT LENSE CAP MISSING OVERWING FO SIDE NEAR FLOOR<[01] REMOVED AND REPLACED LIGHT ASSY PER MM 33-51-01

Part: LENS — DETACHED (ZONE 200) · airframe 63,328 hrs · 37,536 cycles

PLASTIC EXIT SIGN COVER DETACHED MID CABIN<[01] SECURED LENS PER S.I.P.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 63,248 hrs · 37,485 cycles

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

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 63,248 hrs · 37,485 cycles

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

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 60,874 hrs · 36,056 cycles

TAIL LH UPPER FRONT SPAR SLIDING SEAL IS CRACKED. TAIL LH HORIZONTAL UPPER FRONT SPAR SLIDING SEAL IS CRACKED.<[01] REMOVED AND REPLACED SLIDING SEAL IAW AMM 53-31-31.

Part: SLIDE — DETACHED (ZN 800 DOOR) · airframe 60,874 hrs · 36,056 cycles

AFT SERVICE DOOR SLIDE VELCRO STRIPS ON THE GIRT ARE NOT ATTACHED TO VELCRO STRIPS ON THE BACKING PAN SHELF<[01] REPACKED AFT SERVICE DOOR EMERGENCY SLIDE. REF MT 725-61-06 (REM/INST - SLIDE REMOVAL AND INSTALLATION) [TTG8Q00PEV32] FOR WORK PERFORMED.

Part: BRACKET — ELONGATED (ZN 500 LEFT WING) · airframe 58,906 hrs · 34,822 cycles

ELONGATED HOLE ON SUPPORT BRACKET TRAILING EDGE AREA ORS 255 AT LT WING 2023-185590<[01] REPLACED SUPPORT BRACKET TRAILING EDGE AREA ORS 255 AT LT WING;[02] CORRECTED STEP 1 <BR>REPLACED SUPPORT BRACKET TRAILING EDGE AREA ORS 255 AT LT WING I.A.W SRM B737-700 51-40-02 AND DRAWING 115A5300 REV: A;[03] REPLACED SUPPORT BRACKET TRAILING EDGE AREA ORS 255 AT LT WING I.A.W SRM B737-700 51-40-02 AND DRAWING 115A5300 REV: A

Part: PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

DELAMINATED ACCESS PANEL 193CL ON BELLY FAIRING 2023-185577<[01] TOOL USED CALIPER P/N: 500-193-30; S/N: 0000288; DUE DATE: 27-DEC-23.;[02] TOOL USED: SCALE P/N:8340225441 DUE DATE:20-JUL-23;[03] TOOL USED: SCALE P/N:SPX621 S/N:8340225441 DUE DATE:20-JUL-23;[04] TOOL USED:HOT BONDER P/N:HCS9200B-AV S/N:18196021 DUE DATE: 24-JAN-24;[05] REPAIRED ACCESS PANEL 193CL ON BELLY FAIRING IAW B737-700 SRM 51-70-05-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] CORRECTIVE ACTION 2 AND 5 ENTERED AS IN ERROR. CORRECT CORRECTIVE ACTION IS :<BR>TOOL USED: SCALE P/N:SPX621 S/N:8340225441 DUE DATE:20-JUL-23 <BR><BR>REPAIRED ACCESS PANEL 193CL ON BELLY FAIRING IAW B737-700 SRM 51-70-05-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] JOB COMPLETED

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CORROSION ACCESS PANEL 193AL T-ANGLE AT LOWER FUSELAGE 2023-185576<[01] REPLACED T-ANGLE AND FASTENERS AT LOWER FUSELAGE LOCATED ON ACCESS PANEL 193AL IAW B737-700 SRM 51-40-02 AND DWG 149A7216 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED T-ANGLE AND FASTENERS AT LOWER FUSELAGE LOCATED ON ACCESS PANEL 193AL IAW B737-700 SRM 51-40-02 AND DWG 149A7216 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CRACK ON ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 25R AT FWD CARGO COMPARTMENT 2023-185524<[01] REPLACED ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 25R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #143A7505 REV. D. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE LOCATED FWD FACE BS 500C AT LEVEL STR 25R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #143A7505 REV. D.RII; SEE INDIVIDUAL SIGN OFF BELOW.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 58,906 hrs · 34,822 cycles

CRACK REAR SPAR CORRUGATED PLATE ORSS 241 AT LT WING 2023-185533<[01] REPLACED CORRUGATED PLATE LOC. REAR SPAR ORSS 241 AT LT WING AND FASTENERS IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2001 REV. A. SEE INDIVIDUAL SIGN OFFS BELOW;[02] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 58,906 hrs · 34,822 cycles

CRACK REAR SPAR CORRUGATED PLATE IRSS 216 AT RT WING 2023-185522<[01] REPLACED CORRUGATED PLATE LOCATED IRSS 216 AT RT WING AND FASTENERS IAW B737-700 SRM 51-40-05 AND DWG 115A2001 REV: . SEE INDIVIDUAL SIGN-OFF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN-OFF BELOW.

Part: BRACKET — CRACKED (ZN 600 RIGHT WIN) · airframe 58,906 hrs · 34,822 cycles

CRACK REAR SPAR BRACKET IRSS 211 AT RT WING 2023-185520<[01] REAPLACED BRACKET ON REAR SPAR IRSS 211 AT RT WING IAW B737-700 SRM 51-49-92 AND MEASURES OF CRACK ARE: L: 0.500 INCH TOOK MECHANICALLY TOOL USED CALIPER P/N : 500-750-20 S/N: B21015879 DUE DATE: 13-DEC -23.;[02] CORRECTED STEP 1 <BR>REAPLACED BRACKET ON REAR SPAR IRSS 211 AT RT WING IAW B737-700 SRM 51-40-02 AND MEASURES OF CRACK ARE: L: 0.500 INCH TOOK MECHANICALLY TOOL USED CALIPER P/N : 500-750-20 S/N: B21015879 DUE DATE: 13-DEC -23.;[03] CORRECTED STEP 1 <BR>REAPLACED BRACKET ON REAR SPAR IRSS 211 AT RT WING IAW B737-700 SRM 51-40-02 AND MEASURES OF CRACK ARE: L: 0.500 INCH TOOK MECHANICALLY TOOL USED CALIPER P/N : 500-750-20 S/N: B21015879 DUE DATE: 13-DEC -23.

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 58,906 hrs · 34,822 cycles

CRACK REAR SPAR CORRUGATED PLATE ORSS 261 AT LT WING 2023-185532<[01] REPLACED CORRUGATED PLATE LOCATED ORSS 261 AT LT<BR>WING AND FASTENERS IAW B737-700 SRM 51-40-05 AND DWG<BR>115A2001 REV: A. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: LIGHT — BROKEN (ZN 200 FUS TOP) · airframe 58,935 hrs · 34,847 cycles

BROKEN EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) 2023-185473<[01] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-802. STEP 3.C. ITEM (1) THRU (6). SE INDIVIDUAL SIGN BELOW;[02] CORRECTED STEP 1 REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-802. STEP 3.C. ITEM (1) THRU (6). SEE INDIVIDUAL SIGNOFFS BELOW;[03] REPLACED EMERGENCY EXIT LIGHT LENS LAVATORY B AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-802. STEP 3.C. ITEM (1) THRU (6). SEE INDIVIDUAL SIGNOFFS BELOW

Part: STUB FRAME — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK SERVICE DOOR CUT OUT STUB FRAME LOC. AT BS 294.5 AND BTW STR 8R AND STR 9R AT FWD GALLEY AREA 2023-185494<[01] REPLACED STUB FRAME AND FASTENERS LOCATED AT BS 294.5 AND BTW STR 5R AND STR 8R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8370 REV:D. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED STUB FRAME AND FASTENERS LOCATED AT BS 294.5 AND BTW STR 5R AND STR 8R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8370 REV:D. SEE INDIVIDUAL SIGN OFF BELOW.<BR>CERTIFIED AS RII

Part: LENS — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA (1 EA) 2023-185433<[01] REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA (1 EA) I.A.W B737-700 AMM 33-51-01-960-802 .<BR>SEE INDIVIDUAL SIGNOFF BELOW .;[02] TASK CARD COMPLETED

Part: STRAP — CORRODED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CORROSION STRAP LOCATED BS794 AT LEVEL STR25R AND WL 156 AFT CARGO COMPARTMENT 2023-185449<[01] REPLACED STRAP LOCATED BS794 AT LEVEL STR25R AND WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING # 146A8120 REV: -.;[02] CORRECTED STEP 1 <BR><BR>REPLACED STRAP LOCATED BS794 AT LEVEL STR25R AND WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING # 146A8120 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED STRAP LOCATED BS794 AT LEVEL STR25R AND WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING # 146A8120 REV: - SEE INDIVIDUAL SIGN-OFF BELOW RII CERTIFIED

Part: FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CRACK FRAME ON BS 947.5 AT LBL 8.1 AFT CARGO COMPARTMENT 2023-185388<[01] REPLACED FRAME LOCATED ON BS947.5 BTW STR23L TO STR23R AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 147A1047 SHEET 107 REV. - AND DWG 147A0040 SHEET 42 REV. A AND DWG 147A0002 SHEET 104 REV. - AND SHEET 115 REV. - AND DWG 147A7410 SHEET 1 REV. E. <BR>CRACK LENGTH: 0.385? TOOL USED CALIPER P/N: 8647A42 S/N: B22058409 DUE DATE: 27/AUG/23<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CORROSION SUPPORT ZEE LOCATED BS727 TO BS767 AT LEVEL STR25R AND WL155.75 AFT CARGO COMPARTMENT 2023-185416<[01] TOOL USED: ELECTRIC CALIPER P/N: 8647A42 S/N: B22058409 DUE DATE: 27-JAUG-2023;[02] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BS727 TO BS767 AT LEVEL STR25R AND WL155.75 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A7500 REV:A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BS727 TO BS767 AT LEVEL STR25R AND WL155.75 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A7500 REV:A. <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: INTERCOSTAL — CORRODED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CORROSION WEB - INTERCOSTAL LOCATED BS767 TO BS787 BETWEEN STR25R TO STR26R AND WL156 AFT CARGO COMPARTMENT 2023-185440<[01] TOOL USED: THICKNESS GAGE P/N:45MG; S/N: 221861811; DUE DATE: 08-NOV-23.;[02] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BS767 TO BS787 BETWEEN STR25R TO STR26R AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081 REV:A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BS767 TO BS787 BETWEEN STR25R TO STR26R AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 146A0081 REV:A; RII. SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CRACK BRACKET SUPPORT LOCATED BS947.5 AT LBL10 AT AFT CARGO COMPARTMENT 2023-185389<[01] REPLACED SUPPORT BRACKET LOCATED ON BS947.5 AT LBL10 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG# 149A8103; SHEET 7; REV.A. SEE INDIVIDUAL SIGN OFF BELLOW.;[02] CERTIFIED STEP 1 COMPLETED <BR>RII

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CORROSION SUPPORT ZEE LOCATED BS727 TO BS847 AT LEVEL STR25L AND WL156 AFT CARGO COMPARTMENT 2023-185417<[01] REPLACED SUPPORT ZEE LOC. BS727 TO BS847 AT LEVEL STR25L AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM-51-40-02 AND DWG-146A7500 REV: A SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: STRAP — CORRODED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CORROSION STRAP LOCATED BS847 AT LEVEL STR25R AND WL163 AFT CARGO COMPARTMENT 2023-185448<[01] TOOL USED ULTRASONIC THICKNESS GAGE PN 45MG SN 130066401 DUE DATE 21-SEP-23.;[02] REPLACED STRAP LOCATED BS767 TO BS867 AT LEVEL STR25R AND WL163 AFT CARGO COMPARTMENT IAW B737 SRM 51-10-02 ITEM 9 AND DRAWING # 146A8120 REV: -. SEE INDIVIDUAL SIGN OFF OF BELOW;[03] REPLACED STRAP LOCATED BS767 TO BS867 AT LEVEL STR25R AND WL163 AFT CARGO COMPARTMENT IAW B737 SRM 51-10-02 ITEM 9 AND DRAWING # 146A8120 REV: -. SEE INDIVIDUAL SIGN OFF OF BELOW RII Ï¿½TEM

Part: INTERCOSTAL — CORRODED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CORROSION WEB - INTERCOSTAL LOCATED BS767 TO BS787 AT LEVEL STR25R AND WL156 AFT CARGO COMPARTMENT 2023-185438<[01] REPLACED WEB - INTERCOSTAL LOCATED BS767 TO BS787 AT LEVEL STR25R AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-05; SRM 51-10-02 ITEM 9 AND DWG:146A0081 REV:A SEE INDIVIDUAL SIGN-OFF BELOW;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CRACK ANGLE - SUPPORT LOCATED BS907 TO BS927 AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT 2023-185387<[01] REPLACED ANGLE - SUPPORT LOCATED BS907 TO BS927 AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 24 REV - SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE - SUPPORT LOCATED BS907 TO BS927 AND BETWEEN STR25R TO STR27R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 147A7221 SHEET 24 REV - SEE INDIVIDUAL SIGN OFF BELOW

Part: STRAP — CORRODED (ZN 600 RIGHT WIN) · airframe 58,906 hrs · 34,822 cycles

CORROSION LEADING EDGE LOWER STRAP LOCATED OFSS 410 AT RT WING 2023-185369<[01] TOOL USED; CALIPER; PN: 700-113-10; SN: 0033170; DUE DATE: 24-OCT-23.;[02] TOOL USED; CALIPER; PN: 700-113-10; SN: 0033170; DUE DATE: 24-OCT-23.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138203; DUE DATE: 11-APR-23;[04] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138203; DUE DATE: 11-APR-23;[05] ULTRASONIC THICKNESS GAGE P/N:45MG; S/N: 130066701; DUE DATE: 08-APR-23.;[06] TOOL USED : ULTRASONIC EQUIPMENT P/N 45MG S/N 221860711 DUE DATE: NOV-07-23.;[07] REPAIRED LOWER STRAP LOCATED OFSS 410 AT RT WING I.A.W EA 23-157-01023-WIP1 AND EA SUMMARY 23-157-01023; SEE INDIVIDUAL STEP SIGN OFFS BELOW;[08] REPAIRED LOWER STRAP LOCATED OFSS 410 AT RT WING I.A.W EA 23-157-01023-WIP1 AND EA SUMMARY 23-157-01023; SEE INDIVIDUAL STEP SIGN OFFS BELOW. JOB COMPLETED.

Part: BEAM — CORRODED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CORROSION FLOOR BEAM BS 986.5 RBL 36 WL 208.1 AT AFT GALLEY AREA 2023-185359<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N:45MG; S/N:221859911 DUE DATE: 07-NOV-23.;[02] FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00JN2MM WHERE EA 23-153-00987 WAS ADDED AS A SUBTASK. SE INDIVISUAL SING-OFFS BELOW.;[03] CORRECTED ITEM 2: FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00JN2MM WHERE EA 23-153-00987 WAS ADDED AS A SUBTASK. SEE INDIVIDUAL SIGN-OFFS BELOW.;[04] FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00JN2MM WHERE EA 23-153-00987 WAS ADDED AS A SUBTASK. SEE INDIVIDUAL SIGN-OFFS BELOW.

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CRACK ANGLE - SUPPORT LOCATED BS727B AT LBL52 CEILING STRUCTURE AFT CARGO COMPARTMENT 2023-185372<[01] REPLACED SUPPORT ANGLE LOCATED BS727A TO BS 727E MORE 13 INCH AT LBL52 CEILING STRUCTURE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DRAWING #149A9490 REV: -. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT ANGLE LOCATED BS727A TO BS 727E MORE 13 INCH AT LBL52 CEILING STRUCTURE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DRAWING #149A9490 REV: -.ITEM RII SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK ON SUPPORT ANGLE CEILING AREA LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2023-185374<[01] REPLACED SUPPORT ANGLE CEILING AREA LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING# 146A7601 REV: A;[02] REPLACED SUPPORT ANGLE CEILING AREA LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING# 146A7601 REV: A

Part: BEAM — CORRODED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CORROSION ON FLOOR BEAM 986.5 AT LEVEL STR 17L WL 208.1 LBL 46 AT GALLEY AREA 2023-185347<[01] INITIAL MEASURES OF CORROSION ARE L= 1.167? W=1.020? TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N:A21042066 DUE DATE: 30-JUN-23.;[02] TOOL USED ULTRASONIC EQUIPMENT PN: 45MG; SN: 221861811; DUE DATE: 08 NOV 23;[03] TOOL USED: EDDY CURRENT EQUIPMENT. P/N: NORTEC 600D. S/N: 220272512. DUE DATE: 17-DEC-23.;[04] PERFORMED PERMANENT REPAIR LOCATED ON FLOOR BEAM 986.5 AT LEVEL STR 17L WL 208.1 BTW LBL 40 UP TO LBL 49 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. THIS REPAIR IS CATEGORY A NO FURTHER ACTIONS OR ADDITIONAL INSPECTIONS ARE REQUIRED. SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED PERMANENT REPAIR LOCATED ON FLOOR BEAM 986.5 AT LEVEL STR 17L WL 208.1 BTW LBL 40 UP TO LBL 49 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. THIS REPAIR IS CATEGORY A NO FURTHER ACTIONS OR ADDITIONAL INSPECTIONS ARE REQUIRED. SEE INDIVIDUAL SIGN OFF BELOW.<BR>CERTIFIED AS RII

Part: BEAM — CORRODED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CORROSION ON FLOOR BEAM 986.5 AT LEVEL STR 17R WL 208.1 RBL 46 AT GALLEY AREA 2023-185342<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N:45MG; S/N:221859911 DUE DATE: 07-NOV-23.;[02] TOOL USED: EDDY CURRENT EQUIPMENT. P/N: NORTEC 600D. S/N: 220272512. DUE DATE: 17-DEC-23.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138203; DUE DATE: 11-APR-23.;[04] PERFORMED PERMANENT REPAIR ON FLOOR BEAM 986.5 AT LEVEL STR 17R WL 208.1 RBL 46 AT GALLEY AREA IAW EA: 23-153-00987. SEE INDIVIDUAL SING-OFFS BELOW.;[05] CORRECTED ITEM 4: PERFORMED PERMANENT REPAIR ON FLOOR BEAM 986.5 BTW RBL 30.00 & RBL 50.00 AT WL 208.1 AFT GALLEY AREA IAW EA: 23-153-00987. SEE INDIVIDUAL SIGN-OFFS BELOW.;[06] PERFORMED PERMANENT REPAIR ON FLOOR BEAM 986.5 BTW RBL 30.00 & RBL 50.00 AT WL 208.1 AFT GALLEY AREA IAW EA: 23-153-00987. SEE INDIVIDUAL SIGN-OFFS BELOW. RII.

Part: ANGLE — CORRODED (ZN 500 LEFT WING) · airframe 58,906 hrs · 34,822 cycles

CORROSION ANGLE OUTBOARD TRAILING EDGE LOCATED BTW SPOILER 3 AND SPOILER 4 ORSS 354 LT WING 2023-185285<[01] REPLACED ANGLE OUTBOARD TRAILING EDGE LOCATED BTW SPOILER 3 AND SPOILER 4 ORSS 354 LT WING I.A.W B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG# 115A3500; SHEET 9; REV.-. DUE TO NOT FOUND ALLOWABLE DAMAGE AND APLICABLE REPAIR ON B737-700 SRM 57-51-02 TOOK MEASURE OF CORROSION ARE: L= 0.825?; W= 0.466?. TOOL USED DIGITAL CALIPER P/N: 500-752-20; S/N: B21015879 AND DUE DATE: 13/DEC/23.;[02] REPLACED ANGLE OUTBOARD TRAILING EDGE LOCATED BTW SPOILER 3 AND SPOILER 4 ORSS 354 LT WING I.A.W B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG# 115A3500; SHEET 9; REV.-. DUE TO NOT FOUND ALLOWABLE DAMAGE AND APLICABLE REPAIR ON B737-700 SRM 57-51-02 TOOK MEASURE OF CORROSION ARE: L= 0.825?; W= 0.466?. TOOL USED DIGITAL CALIPER P/N: 500-752-20; S/N: B21015879 AND DUE DATE: 13/DEC/23.

Part: INTERCOSTAL — CORRODED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CORROSION ON FLOOR STRUCTURE INTERCOSTAL BRAKE PANEL LOCATED BTW BS 312 TO BS 328 WL 208.1 RBL 10 AT FWD GALLEY AREA 2023-185317<[01] REPLACED FLOOR STRUCTURE INTERCOSTAL BRAKE PANEL LOCATED BTW BS 312 TO BS 328 WL 208.1 RBL 10 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 10 REV- .SEE INDIVIDUAL SIGN-OFF BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 58,906 hrs · 34,822 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 261 LT WING 2023-185292<[01] FAULT RESOLVER IN FAULT TTG8Q00JWHBK DUE TO DISCREPANCY IS DUPLICATED;[02] FAULT RESOLVER IN FAULT TTG8Q00JWHBK DUE TO DISCREPANCY IS DUPLICATED

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK ON WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 52 AT FWD GALLEY AREA 2023-185254<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 52 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 141A5400 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 52 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 141A5400 REV: - RII; SEE INDIVIDUAL SIGN-OFF BELOW

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK ON WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA 2023-185226<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 141A5400 REV-.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 141A5400 REV-.RII;SEE INDIVIDUAL SIGN OFF BELOW.

Part: PANEL — CRACKED (ZN 500 LEFT WING) · airframe 58,906 hrs · 34,822 cycles

CRACK ACCESS PANEL 561CB TRAILING EDGE AROUND HOLES LT WING 2023-185210<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189416 DUE DATE: 19-DEC-23;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 24/SEP/23;[03] TOOL USED: SCALE P/N: SPX621 S/N:8340225441 DUE DATE: 20-JUL-23.;[04] TOOL USED:HOT BONDER PN: HCS9200B-AV; SN: 18185781; DUE DATE: 24-JAN-24.;[05] REPAIRED ACCESS PANEL 561CB TRAILING EDGE LT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] REPAIRED ACCESS PANEL 561CB TRAILING EDGE LT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.

Part: PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 58,906 hrs · 34,822 cycles

CRACK ACCESS PANEL 661BB AROUND HOLE AT RT WING 2023-185257<[01] TOOL USED: CALIPER P/N:500-197-30; S/N:B2018941; DUE DATE:19-DEC-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 24/SEP/23.;[03] TOOL USED: SCALE P/N: SPX621 S/N:8340225441 DUE DATE: 20-JUL-23.;[04] TOOL USED: SCALE PN: SPX621; SN: 8340225441; DUE DATE: 20-JUL-23.;[05] REPAIRED ACCESS PANEL 661BB AROUND HOLE AT RT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] REPAIRED ACCESS PANEL 661BB AROUND HOLE AT RT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK ON WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 LBL 14 AT FWD GALLEY AREA 2023-185250<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 LBL 14 AT FWD GALLEY AREA IAW B737-700 SRM-51-40-02 AND DWG-141A5400 REV:- SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 LBL 14 AT FWD GALLEY AREA IAW B737-700 SRM-51-40-02 AND DWG-141A5400 REV:- SEE INDIVIDUAL SIGN-OFF BELOW AS RII

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK ON WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 33 AT FWD GALLEY AREA 2023-185253<[01] REPLACED WEB INTERCOSTAL AND FASTENERS ON FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 33 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG #141A5400 REV -;[02] REPLACED WEB INTERCOSTAL AND FASTENERS ON FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 33 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG #141A5400 REV - RII Ï¿½TEM

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK ON WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 277 TO BS 294.5 RBL 2 AT FWD GALLEY AREA 2023-185233<[01] REPLACED WEB INTERCOSTAL LOCATED ON FLOOR STRUCTURE LOCATED BTW BS 277 TO BS 294.5 RBL 2 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400; SHEET 20 AND REV - SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED WEB INTERCOSTAL LOCATED ON FLOOR STRUCTURE LOCATED BTW BS 277 TO BS 294.5 RBL 2 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400; SHEET 20 AND REV - RII;SEE INDIVIDUAL SIGN-OFF BELOW.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK ON WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 270 TO BS 277 RBL 3 AT FWD GALLEY AREA 2023-185229<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 270 TO BS 277 RBL 3 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 141A5210 REV: -;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 270 TO BS 277 RBL 3 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 141A5210 REV: - SEE INDIVIDUAL SIGN OFF BELOW;[03] RII ITEM <BR>REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 270 TO BS 277 RBL 3 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 141A5210 REV: - SEE INDIVIDUAL SIGN OFF BELOW<BR>TASKCARD COMPLETED;[04] RII ITEM <BR>REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 270 TO BS 277 RBL 3 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 141A5210 REV: - SEE INDIVIDUAL SIGN OFF BELOW <BR>TASKCARD COMPLETED

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK ON WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA 2023-185219<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02;51-40-02 AND DWG 141A5400 REV -.SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02;51-40-02 AND DWG 141A5400 REV -.RII;SEE INDIVIDUAL SIGN-OFF BELOW.

Part: PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 58,906 hrs · 34,822 cycles

CRACK ACCESS PANEL 661AB AROUND HOLE AT RT WING 2023-185259<[01] TOOL USED: CALIPER P/N:500-197-30; S/N:B20189416; DUE DATE:19-DEC-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 24/SEP/23;[03] TOOL USED: CALIPER P/N: 500-193-30 S/N: 0000288 DUE DATE: 27-DEC-23.;[04] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 24-JAN-24;[05] TOOL USED: SCALE P/N: SPX621 S/N:8340225441 DUE DATE: 20-JUL-23;[06] TOOL USED: MULTIMETER P/N: FLUKE 87-5 S/N: 98740068 DUE DATE: 16-DEC-23.;[07] REPAIRED ACCESS PANEL 661AB AT RT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] REPAIRED ACCESS PANEL 661AB AT RT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.

Part: PANEL — CRACKED (ZN 500 LEFT WING) · airframe 58,906 hrs · 34,822 cycles

CRACK ACCESS PANEL 561AB TRAILING EDGE AROUND HOLES LT WING 2023-185218<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189416 DUE DATE:19-DEC-23;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 24/SEP/23.;[03] TOOL USED: SCALE P/N: SPX621 S/N:8340225441 DUE DATE: 20-JUL-23.;[04] TOOL USED: SCALE PN: SPX621; SN: 8340225441; DUE DATE: 20-JUL-23;[05] TOOL USED:HOT BONDER PN: HCS9200B-AV; SN: 18185781; DUE DATE: 24-JAN-24.;[06] REPAIRED ACCESS PANEL 561AB TRAILING EDGE LT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] REPAIRED ACCESS PANEL 561AB TRAILING EDGE LT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.

Part: PANEL — CRACKED (ZN 500 LEFT WING) · airframe 58,906 hrs · 34,822 cycles

CRACK ACCESS PANEL 561BB TRAILING EDGE AROUND HOLES LT WING 2023-185220<[01] TOOL USED: CALIPER PN: 500-197-30; SN: B20189416; DUE DATE: 19-DEC-23;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 24/SEP/23.;[03] TOOL USED: SCALE P/N: SPX621 S/N:8340225441 DUE DATE: 20-JUL-23.;[04] REPAIRED ACCESS PANEL 561BB TRAILING EDGE LT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] JOB COMPLETED RII

Part: PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 58,906 hrs · 34,822 cycles

CRACK ACCESS PANEL 661CB HOLES AT RT WING 2023-185255<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:B20189416 DUE DATE:19-DEC-23;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 24/SEP/23.;[03] TOOL USED: SCALE P/N: SPX621 S/N:8340225441 DUE DATE: 20-JUL-23;[04] TOOL USED: SCALE PN: SPX621; SN: 8340225441; DUE DATE: 20-JUL-23;[05] TOOL USED:HOT BONDER PN: HCS9200B-AV; SN: 18185781; DUE DATE: 24-JAN-24;[06] REPAIRED ACCESS PANEL 661CB HOLES AT RT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] REPAIRED ACCESS PANEL 661CB HOLES AT RT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.

Part: TIE — CRACKED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-185225<[01] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV-;[02] CORRECTED STEP 1<BR>REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV- <BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV- <BR>SEE INDIVIDUAL SIGN-OFF BELOW RII Ï¿½TEM

Part: WEB — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK ON WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 RBL 32 AT FWD GALLEY AREA 2023-185236<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 RBL 32 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG #141A5410 REV:-<BR>SEE INDIVIDUAL SING BELOW;[02] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 RBL 32 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG #141A5410 REV:-<BR>SEE INDIVIDUAL SING-OFF BELOW;[03] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 RBL 32 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG #141A5410 REV:- <BR>SEE INDIVIDUAL SING-OFF BELOW RII Ï¿½TEM

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK ON INTERCOSTAL LOCATED BTW BS 303.9 TO BS 294.5 AT LEVEL STR 16L AT FWD GALLEY AREA 2023-185222<[01] REPLACED INTERCOSTAL; LOCATED BTW BS 303.9 TO BS 294.5 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02 AND DWG: 141A8180 REV: C. SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED INTERCOSTAL; LOCATED BTW BS 303.9 TO BS 294.5 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02 AND DWG: 141A8180 REV: C. SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII

Part: STUB FRAME — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK ON STUD FRAME LOCATED BS 294.5 AT LEVEL STR 17R RBL 54 FWD GALLEY AREA 2023-185243<[01] ET EQUIPMENT P/N: NORTEC 600D; S/N: 220272712; DUE DATE: 17-DEC-23;[02] ET EQUIPMENT P/N: NORTEC 600D; S/N: 220272712; DUE DATE: 17-DEC-23;[03] PERFORMED PERMANENT REPAIR ON STUD FRAME LOCATED BS 294.5 AT LEVEL STR 17R RBL 54 FWD GALLEY AREA IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7. SEE INDIVIDUAL SIGN-OFF BELOW.;[04] CERTIFIED AS RII <BR>PERFORMED PERMANENT REPAIR ON STUD FRAME LOCATED BS 294.5 AT LEVEL STR 17R RBL 54 FWD GALLEY AREA IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7. SEE INDIVIDUAL SIGN-OFF BELOW.

Part: INTERCOSTAL — CORRODED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CORROSION ON FLOOR STRUCTURE INTERCOSTAL BRAKE PANEL LOCATED BTW BS 294.5 TO BS 312 AT FWD GALLEY AREA 2023-185239<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN: 221861811; DUE DATE: 08-NOV-23;[02] REPLACED NEW INTERCOSTAL BRAKE PANEL LOCATED BTW BS 294.5 TO BS 312 AT FWD GALLEY AREA AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG 141A5400 REV - SHEET 8 SEE INDIVIDUAL SIGN OFF BELOW;[03] RII ITEM <BR>REPLACED NEW INTERCOSTAL BRAKE PANEL LOCATED BTW BS 294.5 TO BS 312 AT FWD GALLEY AREA AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG 141A5400 REV - SHEET 8 SEE INDIVIDUAL SIGN OFF BELOW<BR>TASKCARD COMPLETED

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 58,906 hrs · 34,822 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 17R FWD GALLEY AREA 2023-185241<[01] FAULT RESOLVED ON OTHER FAULT; SEE FAULT TTG8Q00JJ51Q;[02] FAULT RESOLVED ON OTHER FAULT; SEE FAULT TTG8Q00JJ51Q

Part: STRIP — BROKEN (ZN 200 FUS TOP) · airframe 58,908 hrs · 34,823 cycles

BROKEN STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (8 EA) 2023-185149<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (8 EA) I.A.W B737-700 AMM 33-51-15-400-802.;[02] CORRECTED STEP 1<BR>REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (8 EA) SEE JOB CARD 733-50-01 (TTG8Q003LXN1);[03] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (8 EA) SEE JOB CARD 733-50-01 (TTG8Q003LXN1)

Part: BEAR STRAP — CRACKED (ZN 200 FUS TOP) · airframe 58,908 hrs · 34,823 cycles

CRACK ON BEAR STRAP LOCATED BS 291.5 PLUS 4 INCHES BTW STR 9RTO STR 10R AT FWD GALLEY AREA 2023-185146< EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022237; DUE DATE: 26-JAN-23;[05] ET EQUIPMENT P/N: NORTEC 600D; S/N: 220272712; DUE DATE: 17-DEC-23;[06] TOOL USED: EDDY CURRENT EQUIPMENT. P/N: NORTEC 600D. S/N: 220272512. DUE DATE: 17-DEC-23.;[07] TOOL USED MICROMETER PN:293-344-30; SN: 71736459; DUE DATE: 29-NOV-23; SMALL HOLE GAUGE: PN: 154-901; SN: AE-411355; DUE DATE: 27-JAN:24.;[08] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138203; DUE DATE: 11-APR-23.;[09] TOOL USED MICROMETER PN:293-344-30; SN: 71736459; DUE DATE: 29-NOV-23;CALIPER PN: 500-197-30; SN: B20189362; DUE DATE: 27-DEC-23.;[10] TOOL USED MICROMETER PN:293-831-30; SN: 71150743; DUE DATE: 17-NOV-23;CALIPER PN: 500-197-30; SN: B20189362; DUE DATE: 27-DEC-23.;[11] PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BTW BSTA 277 & BSTA 320 AND S-6R & S-11R (FWD GALLEY DOORWAY) IAW B737-700 SRM 51-10-01-2R-6 REPAIR 6 PARAGRAPH 4 Ï¿½TEM M;N AND O; AND EA-23-153-00981 SEE INDIVIDUAL SIGNOFFS BELOW.;[12] PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BTW BSTA 277 & BSTA 320 AND S-6R & S-11R (FWD GALLEY DOORWAY) IAW B737-700 SRM 51-10-01-2R-6 REPAIR 6 PARAGRAPH 4 Ï¿½TEM M;N AND O; AND EA-23-153-00981 RII; SEE INDIVIDUAL SIGNOFFS BELOW.

Part: RIB — CRACKED (ZN 500 LEFT WING) · airframe 58,906 hrs · 34,822 cycles

CRACK ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 270 LT WING 2023-185161<[01] REPLACED ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 270 LT WING I.A.W B737-700 SRM 51-40-02 AND DWG#115A2930; SHEET 7; REV.-. TOOL USED DIGITAL CALIPER P/N: 500-720-20; S/N: B21015879 AND DUE DATE: 13/DEC/23;[02] TASK COMPLETED

Part: FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 58,906 hrs · 34,822 cycles

CRACK ON FRAME BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2023-185148<[01] REPAIRED FRAME ON BS 312 AND BETWEEN STR5L TO STR6L AT FWD GALLEY AREA IAW EA M-22-153-01244 SEE SUB TASK BAR CODE TTG8Q00JFQ50;[02] STEP 1 CORRECTED. REPAIRED FRAME ON BS 312 AND BETWEEN STR5L TO STR6L AT FWD GALLEY AREA IAW EA M-22-153-01244 SEE SUB TASK BAR CODE TTG8Q00JFQ50. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPAIRED FRAME ON BS 312 AND BETWEEN STR5L TO STR6L AT FWD GALLEY AREA IAW EA M-22-153-01244 SEE SUB TASK BAR CODE TTG8Q00JFQ50. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: WEB — CRACKED (ZN 500 LEFT WING) · airframe 58,906 hrs · 34,822 cycles

CRACK WEB TRAILING EDGE DEFLECTION CONTROL RIB ORSS 270 LT WING 2023-185162<[01] REPLACED WEB TRAILING EDGE DEFLECTION CONTROL RIB ORSS 270 LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 115A2512 REV: -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB TRAILING EDGE DEFLECTION CONTROL RIB ORSS 270 LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 115A2512 REV: -. SEE INDIVIDUAL SIGN OFF BELOW.AS RII. JOB COMPLETED.

Part: LIGHT — INOPERATIVE (ZN 800 DOOR) · airframe 58,752 hrs · 34,713 cycles

AFT R/H AFT SERVICE DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP<[01] RELAMP AFT R/H AFT SERVICE DOOR EMERGENCY LIGHT IAW AMM 33-51-04

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,107 hrs · 34,310 cycles

CRACK FOUND ON STA. 663 VERTICAL LEG OF ATTACH ANGLE COMMON TO DRAIN VALVE LOWER I/B NUTPLATE HOLE AT RBL 32 WL 193 / [01] VERIFIED CRACK FROM DRAIN CUTOUT TO INBD NUTPLATE HOLE ON LOWER ATTACH ANGLE VERTICAL LEG IAW B737 NDT PART 6 51-00-00 PROCEDURE 23. TOOL# 40083 DUE 14SEP23;[02] CUT AND REMOVED DAMAGED SECTION OF ANGLE IAW SRM 57-10-10-2R-6 SECTION 4.C. VERIFIED MATERIAL 7075-T6 .100' ATAG A39363 IAW SRM 57-10-10-2R-6 TABLE 201.;[03] VERIFIED STEP 2;[04] HFEC DAMAGE CUTOUT AND OPEN HOLES IN REPAIR AREA IAW B737 NDT PART 6 51-00-00 PROCEDURES 23 AND 16. NO DEFECTS NOTED. TOOL# 44291 DUE 03NOV23;[05] ACCOMPLISHED INSURANCE CUT; FABRICATED; LOCATED AND DRILLED REPAIR FILLER IAW SRM 57-10-10-2R-6 SECTION 4. D; AND F - J.;[06] VERIFIED STEP 5;[07] APPLIED CHEMICAL CONVERSION AND PRIMER IAW SRM 57-10-10-2R-6 SECTION 4. K AND L.;[08] VERIFIED STEP 7 C/W;[09] OK TO INSTALL REPAIR PARTS;[10] INSTALLED REPAIR PART IAW SRM 57-10-10-2R-6;[11] VERIFIED ITEM 10.;[12] VERIFIED ACTION 10;[13] APPLIED CIC TO REPAIRED AREA IAW SRM 57-10-10-2R-6;[14] VERIFIED JOB IS COMPLETE;[15] VERIFIED ITEMS 12-14.;[16] UPDATED MEASUREMENTS;[17] VERIFIED ITEM 16.<BR>AUDITED

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 58,107 hrs · 34,310 cycles

CRACK FOUND ON LOWER ATTACH ANGLE AT RBL 45 STA 663 (WL 193) / [01] VERIFIED ITEM 1 OF STEP 1;[02] VERIFIED ITEM 1 OF STEP 2;[03] VERIFIED STEP 6 AND 7;[04] UPDATED MEASUREMENTS;[05] UPDATED MEASUREMENTS;[06] LEAK CHECKED REPAIR AREA NO LEAK DETECTED I.A.W MM 28-11-00-400-801;[07] VERIFIED ITEM# 6. REPAIR BEEN COMPLETED ON N/R TTG8Q00G38ZT;[09] AUDIT C/W;[10] REPAIR BEEN COMPLETED ON EA# 22-157-03313

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 58,107 hrs · 34,310 cycles

CRACK FOUND ON UPPER ATTACH ANGLE AT RBL 40 STA 663 (WL 167) / [01] VERIFIED ITEM 1 OF STEP 1;[02] RECEIVED -1 REPLACEMENT ANGLE 2024-T3 .063' AND -2 SPLICE ANGLE 2024-T3 .071' FROM BACKSHOP ON W/O#'S 44275-6000-0001 AND 44275-6000-0002 IAW SRM 57-10-10-2R-5 TABLE 201.;[03] VERIFIED STEP 2 C/W;[04] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 16. NO DEFECTS NOTED. TOOL#31823; DUE 23DEC22;[05] ONE OPEN HOLE IS THE OVER SIZE FASTENER;[06] VERIFIED ITEM 2 OF STEP 2; ITEM 3 OF STEP 4 AND ITEM 6 OF STEP 11;[07] VERIFIED STEPS 12 AND 13 ARE COMPLETE;[08] AUDIT C/W

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 57,996 hrs · 34,228 cycles

FWD ENTRY DOOR GENT BAR WILL NOT STAY SEATED / [01] REMOVED DECREE FROM GIRT BAR LATCH PER SIP OPS CHECK GOOD

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 57,232 hrs · 33,718 cycles

AFT DOOR SLIDE FO SIDE PARTIALLY CAME OUT OF HOLDER. / [01] REINSTALLED GIRT BAR BACK IN TO THE SLIDE BRACKET REF 25-66-01

Part: FLAP — FAILED · airframe 56,863 hrs · 33,471 cycles

FLAP ASYMMETRY INDICATED UPON INITIAL MOVEMENT OF FLAP HANDLE FROM THE UP POSITION. FLAPS LOCKED OUT. / [01] R/R #6 AND #7 FLAP SKEW SENSORS PER AMM 27-59-01

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 56,748 hrs · 33,396 cycles

OVERWING EXIT SIGN FELL OFF / [01] RESECURED OVERWING EXIT SIGN COVER PER SIP

Part: SIGN — DETACHED (MID CABIN) · airframe 56,369 hrs · 33,146 cycles

EXIT SIGN IN OVERHEAD AT MID OF AIRCRAFT BACK SIDE FELL OFF / [01] RESECURED SIGN IN PLACE IAW AMM 33-51-01;OK FOR SERVICE

Part: FLAP — DELAMINATED (R/H WING) · airframe 56,102 hrs · 32,975 cycles

RT WING OUTBD AFT FLAP LOWER SKIN DELAMINATED AFT INBD CORNER MEASUING 7IN BY 9IN. / [01] REMOVED O/B AFT FLAP PER AMM 27-51-22.;[02] REMOVED AND REPLACED RT WING OUTBOARD AFT FLAP PER AMM 27-51-22

Part: STIFFENER — CRACKED (L/H MLG W/W) · airframe 56,102 hrs · 32,975 cycles

LEFT MLG CENTER DOOR LOWER FWD ATTACH POINT STIFFENER HAS A 1' CRACK / [01] OK TO CONTINUE CDL 32-10-03; CENTER/INNER DOOR REMOVED; REFERENCE LP 2008271

Part: PLATE — SHEARED (R/H WING) · airframe 56,102 hrs · 32,975 cycles

RT WING LOWER AFT SHELF PANEL 651GB FWD SUPPORT BRACKET(WIGGLE PLATE) HAS SHEARED FASTENERS. / [01] REMOVED AND REPLACED WIGGLE PLATE IAW SRM 51-40-02

Part: BATTERY PACK — POPPED (CABIN) · airframe 55,506 hrs · 32,621 cycles

SUPPLEMENTAL INFORMATION: RH AFT EMERGENCY LIGHT CB POPPED ; / [01] R&RED RH AFT EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK PER AMM 33-51-06.

Part: POWER SUPPLY — POPPED (CABIN) · airframe 55,506 hrs · 32,621 cycles

SUPPLEMENTAL INFORMATION: RH AFT EMERGENCY LIGHT CB POPPED ; / [01] R&RED RH AFT EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK PER AMM 33-51-06.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 54,968 hrs · 32,292 cycles

FORWARD SERVICE DOOR ESCAPE SLIDE DROPPED DOWN ; / [01] RE INSTALLED SLIDE PER MT-725-61-06

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 53,780 hrs · 31,610 cycles

OVERHEAD CENTER EMERGENCY EXIT LIGHT COVER FELL OFF ; / INSTALLED COVER PER MM 33-51-01

Part: SUPPORT — CRACKED (AFT CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK SUPPORT ZEE LOCATED BS747 AFT CARGO COMPARTMENT. FABRICATED SUPPORT ZEE LOC BS 727 TO BS 767 AT LEVEL STR 26R AT AFT CARGO COMPARTMENT IAW B737700 DWG 146A7502 REV.

Part: ANGLE — CRACKED (FWD CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK ANGLE AFT FACE BS500B AND STR 26L AT FWD CARGO COMPARTMENT. REPLACED ANGLE AFT FACE BS 500B AND STR 26L AT FWD CARGO COMPARTMENT IAW B737700 SRM 514002 SRM 511002 AND DRAWING #143A7505 SHEET 5 REV B MATERIAL PN:143A7502U155 P.O 2020 212944

Part: SUPPORT ANGLE — CRACKED (BS 867 LBL 10) · airframe 53,548 hrs · 31,478 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS 867 ATLEVEL OF LBL 10 AFT CARGO COMPARTMENT / REPLACE ANGLE-SUPPORT LOCATED ON BS 867 AT LEVEL OF 1BL 10 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 AND DWG 149A8102 REV. -

Part: WEB — CRACKED (AFT CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK WEB LOCATED ON BS 914 AT LEVEL OF RBL 8 AT AFT CARGO COMPARTMENT REPLACED WEB (STIFFENER) LOCATED ON BS 914 AT LEVEL OF RBL 8 AT AFT CARGO COMPARTMENT IAW B737700 SRM 514002 AND DWG 147A7221 SHEET 17 REV D. MATERIAL USED :ALLUMINIUM SHEET PN:7075T6 0.040' PO:2021 124744

Part: WEB — CRACKED (FWD CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK WEB. INTERCOSTAL LOCATED BETWEEN BS 400 AND BS 420 S-26L FWD CARGO COMPARTMENT. REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS 400 AND BS 420 S26L FWD CARGO COMPARTMENT IAW 737700 SRM 5140020G0 AND DWG 143A7505 REV B SHEET 2 PN 143A751033 PO: 2021 136981

Part: CHANNEL — CRACKED (AFT CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK CHANNEL SUPPORT LOCATED ON BS 727 BULKHEAD AFT CARGO COMPARTMENT / REPLACED CHANNEL SUPPORT LOCATED ON BS 727 BULKHEAD AFT CARGO COMPARTMENT I.A.W B737700 SRM 514002 AND DWG #144A2600 SHEET 566 REV

Part: SUPPORT ANGLE — CRACKED (FWD CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK ANGLE SUPPORT LOCATED AT BS 500D S-28R AFT FACE FWD CARGO COMPARTMENT. REPLACED ANGLE SUPPORT LOCATED AT BS 500D S28R AFT FACE FWD CARGO COMPARTMENT ASPER B737700 SRM 511002 ITEM 9 AND DWG # 143A9805 SHEET 11 REV AND DWG # 143A7902 SHEET 126 REV A ALUMINUM SHEET PO 2020 207070

Part: WEB — CORRODED (FWD CARGO) · airframe 53,548 hrs · 31,478 cycles

CORROSION WEB INTERCOSTAL LOCATED BETWEEN BS 489 AND BS 500A RBBL 21 WL 151 AT FWD CARGO COMPARTMENT. REPLACED WEB INTERCOSTAL LOCATED BETWEEN BST 489 AND BST 500A RBBL 21WL 151 AT FWD CARGO COMPARTMENT IAW SRM B737700 514002 AND DRAWING #143A0080 REV 23

Part: ANGLE — CRACKED (CABIN) · airframe 53,548 hrs · 31,478 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 695 AT RBL 24.5 AT PASSENGER CABIN (1 EA). REPLACED ANGLE FLOOR STRUCTURE LOCATED ON BS 695 AT RBL 24.5 AT PASSENGER CABIN (1 EA) I.A.W B737700 SRM 514002 AND DWG 111A6002 SHEET 36 REV. SRM 511002 ITEM 9.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCODANCE WITH BOEING 737700 SRM 5360152R1 REPAIR 1;PARAGRAPH 4.B;STEP (4) AND BAC 5975.

Part: FLOORBEAM — CRACKED (CABIN) · airframe 53,548 hrs · 31,478 cycles

CRACK INTERCOSTAL. WEB FLOOR STRUCTURE LOCATED BS 540 AT LBL 24.5 TO RBL 24.5 AT PASSENGER CABIN (2 EA). REPLACED INTERCOSTAL WEB FLOOR STRUCTURE LOCATED BS540 AT LBL 24.5 TO RBL 24.5 PASSENGER CABIN (2EA) IAW SRM B737700 514002 AND 511002 ITEM 9

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737700 SRM 5360152R1; REPAIR 1;PARAGRAPH 4.B; STEP (4) AND BAC 5975.

Part: INTERCOSTAL — CRACKED (BS 500D-520 S28R) · airframe 53,548 hrs · 31,478 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS 500D TO BS 520 STRINGER 28R FWD CARGO COMPARTMENT / REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS500D TO BS520 STRINGER 28R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #143A7902 REV A AND DRAWING #143A9803 SHEET 8 REV B

Part: FLOORBEAM — CRACKED (CABIN) · airframe 53,548 hrs · 31,478 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 695 AT RBL 24.5 AT PASSENGER CABIN (1 EA)

Part: STRINGER — CRACKED (FWD CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK STRINGER 26R AT BS 540 FWD CARGO COMPARTMENT. EVALUATED ALLOWABLE DAMAGE LIMITS OF STR-26R AND FOUND OUT OF LIMITS DUE TO CRACK IS NOT PERMITTED FABRICATE REPAIR PARTS OF MATERIAL ALUMINUM SHEET PN 70750.045' PO: 2021 113097 AND PN 7075 TO 0.050' PO 2021 121145 HEAT TREATED AND CONVERTED FROM TO TO CONDITION T6 AND PERFORMED PERMANENT REPAIR ON STR26R LOC BS540 TO BS500D +100' IAW B737700 SRM 5300032R1 REPAIR 1

Part: CARGO TRACK — CRACKED (BS 767 RBL13.84) · airframe 53,548 hrs · 31,478 cycles

CRACK FLOOR STRUCTURE CARGO TRACK LOCATED ON BS 767 AT LEVEL RBL 13.84 AT AFT CARGO COMPARTMENT / REPAIRED CARGO TRACK LOCATED ON BS 747+9' TO BS 767+9' IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 AND 51-40-02 RBL 13.84 AFT CARGO COMPARTMENT

Part: ANGLE — CRACKED (FWD CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK ANGLE LOCATED AT BS 500D AT LEVEL STRINGER 28L FWD CARGO COMPARTMENT. REPLACED ANGLE LOC AT BS 500D AT LEVEL STRINGER 28L FWD CARGO COMPARTMENT IAW B737700 SRM 511002 AND SRM 514002 DWG # 143A7902 REV A

Part: GUSSET — CRACKED (FWD CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK GUSSET LOCATED AT BS 500D STRINGER 19L FWD CARGO COMPARTMENT. REPLACED GUSSET LOC AT BS500D; STR19L AT FWD CARGO COMPARTMENT IAW B737700 SRM 514002 AND DWG 143A7902 REV A PN USED IS 143A94816 GUSSET PO #2020 215356

Part: SUPPORT ANGLE — CRACKED (FWD CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK ANGLE SUPPORT LOCATED BS 500A STRINGER 26L FWD FACE FWD CARGO COMPARTMENT REPLACED ANGLE. SUPPORT LOCATED BS 500A STRINGER 26L FWD FACE FWD CARGO COMPARTMENT IAW B737700 SRM 514002 B737700 SRM 511002 ITEM 9 AND B737700 DWG #143A7505 SHEET 7 REV. PART NUMBER USED:143A7502U159 P.O 2020 202445.

Part: GUSSET — CRACKED (FWD CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK GUSSET LOCATED AT BS 500D STRINGER 19R FWD CARGO COMPARTMENT. REPLACED GUSSET LOCATED AT BS 500D STRINGER 19R FWD CARGO COMPARTMENT IAW B737700 SRM 511002; ITEM 9 SRM 514002 AND DWG N. 143A7902; REV. SHEET 174

Part: SUPPORT ANGLE — CRACKED (FWD CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK ANGLE SUPPORT LOCATED BS500B FWD FACE STRINGER 26L FWD CARGO COMPARTMENT REPLACED ANGLE SUPPORT LOCATED BS 500B FWD FACE STRINGER 26L FWD AND B737700 DWG #143A7505 SHEET 5 REV. B PART NUMBER USED: 143A7502U159 P.O 2020 202445.

Part: WEB — CRACKED (FWD CARGO) · airframe 53,548 hrs · 31,478 cycles

CRACK WEB. INTERCOSTAL LOCATED BETWEEN BS 500B AND BS 500C STRINGER 26L FWD CARGO COMPARTMENT REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS500B AND BS500C STRINGER 26L FWD CARGO COMPARTMENT IAW B737700 SRM 511002 ITEM 9 AND SRM 514002 DRAWING #143A7505 SHEET 5 REV B MATERIAL USED PN 143A751011 PO 2021 137530

Part: SUPPORT ANGLE — CRACKED (VERTICAL STAB) · airframe 53,548 hrs · 31,478 cycles

CRACK FRONT SPAR SUPPORT ANGLE LOCATED AT BS 1016 BETWEEN STR 2R AND 2L EXTERNAL FUSELAGE AT VERTICAL STABILIZER. REPLACED FRONT SPAR SUPPORT ANGLE PN 176A3101U26 LOC AT BS 1016 BTW STR 2R AND STR 2L EXTERNAL FUSELAGE AT VERTICAL STABILIZER IAW B737700 SRM 514002 AND DWG 176A3101 REV

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 53,548 hrs · 31,478 cycles

CRACK LEADING EDGE RIB STA 151.75 AT RT HORIZONTAL STABILIZER / REPLACED LEADING EDGE RIB STA 151.75 AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 51-40-02 AND DWG-186A1001 REV B P/N USED 15186A1401Y2 RIB

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 53,548 hrs · 31,478 cycles

CRACK INSPAR RIB LOCATED AT STAB STA 120.30 AT 28 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER / PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED AT STAB STA 120.30 BTW 23.000 INCHES TO 29.800 INCHES FROM FRONT SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND B737-700 SRM 55-10-09-2R-5 REPAIR 5 FIGURE 204 DETAIL A CRACK LENGHT IS 0.490'

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 53,121 hrs · 31,218 cycles

EMERGENCY EXIT FWD SERVICE DOOR UNATTACHED. REINSTALLED EMERGENCY EXIT SIGN AT FWD SERVICE DOWN, IAW SIP. OPERATIONS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,569 hrs · 30,898 cycles

MID AISLE EMERGENCY LIGHT INOPERABLE. R & R EMERGENCY BATTERY POWER PACK, IAW AMM 33-51-06. OPERATIONS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 51,747 hrs · 30,389 cycles

SEVERAL EMERGENCY LIGHTS IN FWD GALLEY/L1 DOOR AREA INOP. REMOVED AND REPLACED LT FWD BATTERY PACK REFERENCE AMM CH 33-51-06. OPS CK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 50,689 hrs · 29,729 cycles

EXIT ROW OVERHEAD SIGN MISSING. R&R LENS PER AMM.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 48,864 hrs · 28,550 cycles

DIVERSION, NO.1 ENGINE APPEARED TO BE LOOSING OIL AT AN ABNORMALLY HIGH RATE. OIL QUANTITY GOT DOWN TO 40% BUT LOW OIL PRESSURE LIGHT DID NOT COME ON. / SERVICED ENGINE OIL PER AMM.

Part: WEB — CRACKED (LT MLG WW) · airframe 48,642 hrs · 28,402 cycles

VERTICAL SEAL WEB CRACKED AT BS. 663, LBL 47. R&R WEB PER SRM AND DWG.

Part: RETAINER — CRACKED (LT WING) · airframe 48,642 hrs · 28,402 cycles

BULB SEAL RETAINER IS CRACKED AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON. MARKED / REMOVED CHECKED BULB SEAL RETAINER AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON AND INSTALLED NEW BULB SEAL RETAINER P/N 115A2982-9 SAME LOCATION ABOVE IAW AIPC 57-50-00-25 AND SRM 51-40-02-0G-0.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 48,642 hrs · 28,402 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB AT LEADING EDGE STA. 114 CRACKED AT FASTENER HOLE. R&R RIB IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 48,642 hrs · 28,402 cycles

VERTICAL PRESSURE WEB CRACKED AT BS. 663, LBL 26. REPAIRED WEB PER EA & ER.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 48,642 hrs · 28,402 cycles

VERTICAL PRESSURE WEB CRACKED AT BS. 663, RBL 40. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 48,642 hrs · 28,402 cycles

HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS. 663 TO BS. 675, RBL 40. REPAIRED DECK IAW SRM.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 48,642 hrs · 28,402 cycles

PASSENGER CABIN SEAT TRACK MECHANICAL DAMAGED BETWEEN BS. 540 TO BS. 727B, LBL 24.5. REPAIRED SEAT TRACK IAW SRM & DWG.

Part: BEAM — CRACKED (R1 DOOR) · airframe 48,642 hrs · 28,402 cycles

R1 DOOR NR 4 LOWER BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. REINSTALLED #4 LOWER BEAM IAW AMM.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 48,642 hrs · 28,402 cycles

***CORROSION*** ON PASSENGER CABIN SEAT TRACK; IN MULTIPLE AREAS; AT B.S. 680-727B; L.B.L. 24.5; W.L. 208. / REPLACEMENT OF PASSENGER CABIN SEAT TRACK FROM B.S. 540- B.S. 727B; L.B.L 24.5; WL 208 TO BE ACCOMPLISHED ON CUSTOMER CARD T928070 INTERIOR 5079

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 48,642 hrs · 28,402 cycles

HORIZONTAL PRESSURE DECK CRACKED BETWEEN BS. 663 TO BS. 675, BETWEEN LBL 30 TO LBL 60. REPAIRED DECK IAW SRM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 48,642 hrs · 28,402 cycles

ACB AFT CORNER SCUFF PLATE IS CRACKED / RECEIVED NEW ACB AFT. CORNER SCUFF PLATE; WILL BE INSTALLED AT COSTOMER CARD # 753-721-00-01

Part: TIRE — SEPARATED (NLG) · airframe 48,329 hrs · 28,210 cycles

AIR TURNBACK/DECLARED EMERGENCY, RT NOSE TIRE TREAD CAME OFF AT ROTATION. R&R LT NOSE TIRE PER AMM.

Part: TIRE — SEPARATED (NLG) · airframe 48,329 hrs · 28,210 cycles

AIR TURNBACK/DECLARED EMERGENCY, RT NOSE TIRE TREAD CAME OFF AT ROTATION. R&R RT NOSE TIRE PER AMM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 47,763 hrs · 27,864 cycles

RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 47,763 hrs · 27,864 cycles

LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / REMOVED AND REPLACED LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31.

Part: WINDOW — ARCED (COCKPIT) · airframe 47,173 hrs · 27,495 cycles

R1 WINDOW ARCED ON DESCENT. R&R R1 WINDOW ASSEMBLY PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,398 hrs · 26,971 cycles

RT DOOR EMERGENCY EXIT UPPER SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — DEFECTIVE (R2 DOOR) · airframe 45,641 hrs · 26,483 cycles

R2 DOOR EMERGENCY EVAC SLIDE FAILED INSPECTION. R&R SLIDE PER MT.

Part: HOOK AND LOOP — BROKEN (EMERGENCY EXIT) · airframe 45,601 hrs · 26,460 cycles

LT OVERWING DOOR EMERGENCY EXIT STRAP COVER HOOK AND LOOP BROKEN. R&R HOOK AND LOOP PER CMM.

Part: MOTOR — FAILED (STAB TRIM) · airframe 43,495 hrs · 25,124 cycles

ELECTRIC STABILIZER TRIM FAILURE, BOTH YOKES. NO CIRCUIT BREAKERS TRIPPED. EMERGENCY DECLARED AND DIVERTED. R & R THE STAB TRIM MOTOR IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 43,421 hrs · 25,072 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 43,421 hrs · 25,072 cycles

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

Part: STRAP — BROKEN (FLASHLIGHT ASSY) · airframe 43,047 hrs · 24,837 cycles

AFT CABIN OUTBOARD EMERGENCY FLASHLIGHT STRAP BROKEN. R & R THE STRAP IAW SIP.

Part: HOLDER — LOOSE (GIRT BAR) · airframe 41,958 hrs · 24,189 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. ADJUSTED HOLDER PER MT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,819 hrs · 24,110 cycles

R1 DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: INTERCOSTAL — CRACKED (BS 500B-500C) · airframe 41,819 hrs · 24,110 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500B TO 500C, STRINGER 27L. R & R THE INTERCOSTAL IAW DWG & SRM.

Part: BRACKET — CRACKED (BS 947) · airframe 41,819 hrs · 24,110 cycles

AFT CARGO BAY FLOOR SUPPORT BRACKET CRACKED AT BS 947, LBL 11. R & R BRACKET IAW SRM AND DWG.

Part: ANGLE — CRACKED (BS 663) · airframe 41,819 hrs · 24,110 cycles

VERTICAL FLANGE OF ANGLE CRACKED AT BS 663, LBL 7.5 R & R THE ANGLE IAW SRM AND DWG.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 41,819 hrs · 24,110 cycles

LEFT WING OTBD TRAILING EDGE AFT FLAP DELAMINATED ON THE INBOARD LOWER SIDE. REPAIRED THE AFT FLAP IAW SRM.

Part: CREASE BEAM — CORRODED (BS 951-992) · airframe 41,819 hrs · 24,110 cycles

CREASE BEAM CORRODED BETWEEN BS 951 - 992. R & R THE CREASE BEAM IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (BS 322) · airframe 41,819 hrs · 24,110 cycles

CREASE BEAM CORRODED AT BS 322, RBL 60. R & R THE CREASE BEAM IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,819 hrs · 24,110 cycles

CABIN FLOOR INTERCOSTAL CRACKED AT STA 312 TO STA 320, RBL 31. R&R INTERCOSTAL SECTION PER SRM.

Part: STRIP — CRACKED (LT WING) · airframe 41,819 hrs · 24,110 cycles

LEFT WING INBD TRAILING EDGE LOWER SURFACE PANEL SUPPORT WAFFLE BOARD CRACKED. R&R STRIP IAW SRM & DWG.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 41,617 hrs · 23,991 cycles

LEFT AFT BATTERY FAILED CAPACITY CHECK. R & R THE BATTERY IAW AMM.

Part: BRACKET — BROKEN (L2 DOOR) · airframe 37,119 hrs · 21,405 cycles

L2 DOOR EMER EVAC SLIDE, FWD MOUNT BRACKET NUTPLATE BROKEN. R & R BRACKET ASSEMBLY IAW SRM.

Part: SIGN — CRACKED (CABIN) · airframe 37,003 hrs · 21,343 cycles

CENTER AISLE OVERHEAD EMER EXIT SIGN HOUSING CRACKED. R & R SIGN IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 35,703 hrs · 20,618 cycles

FORWARD EXIT SIGN LOOSE. R & R SIGN IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,666 hrs · 20,597 cycles

LEFT NR 1 WINDOW FRAME OTBD UPPER CORNER CRACKED. REPAIRED FRAME IAW ACO.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,666 hrs · 20,597 cycles

STIFFENER ON AFT SIDE OF FLOORBEAM CRACKED AT BS 727B, LBL 24.75. R & R STIFFENER IAW DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,666 hrs · 20,597 cycles

FORWARD SEAT TRACK, INBD FLANGE, AFT FASTENER CRACKED, BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,666 hrs · 20,597 cycles

FORWARD SEAT TRACK INBD FLANGE FWD FASTENER HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 35,666 hrs · 20,597 cycles

MAIN CABIN MAIN WWW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, LBL 33. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,666 hrs · 20,597 cycles

LEFT BULKHEAD CHORD SKIN CRACKED AT BS 540, STRINGER 22L, AFT FASTENER ROW 2ND FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: COVER — LOOSE (CABIN) · airframe 35,269 hrs · 20,379 cycles

L1 DOOR EMER LIGHT COVER LOOSE. R & R LIGHT ASSEMBLY IAW AMM.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 34,381 hrs · 19,877 cycles

RIGHT MLG FWD TRUNNION SUPPORT FITTING, UPPER OTBD LUG FACE CORRODED. REPAIRED LUG FACE IAW EA.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 34,381 hrs · 19,877 cycles

RIGHT MLG FWD TRUNNION SUPPORT FITTING, UPPER INBD LUG FACE CORRODED. REPAIRED LUG FACE IAW EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 34,381 hrs · 19,877 cycles

LEFT MLG FWD TRUNNION SUPPORT FITTING, UPPER INBD LUG FACE CORRODED. REPAIRED LUG FACE IAW EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 34,381 hrs · 19,877 cycles

LEFT MLG FWD TRUNNION SUPPORT FITTING, LOWER INBD LUG FACE CORRODED. REPAIRED LUG FACE IAW EA.

Part: COVER — MISSING (EXIT SIGN) · airframe 33,242 hrs · 19,229 cycles

RIGHT OVERWING LOWER EXIT SIGN COVER MISSING. INSTALLED SIGN IAW MM.

Part: RIVET — SHEARED (L1 DOOR) · airframe 31,450 hrs · 18,223 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT HOOK RIVET SHEARED. R & R RIVET IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,651 hrs · 16,611 cycles

AFT LT EXTERNAL EMERGENCY LIGHT INOP. RELAMPED PER AMM.

Part: NUT PLATE — BROKEN (BATTERY CHARGER) · airframe 28,651 hrs · 16,611 cycles

FWD LT EMERGENCY LIGHT BATTERY CHARGER BROKEN MOUNTING NUT PLATE. R&R BATTERY CHARGER IAW AMM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,651 hrs · 16,611 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT I/B SIDE OF RIB STAB STA 193.90 7.5". REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,651 hrs · 16,611 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT I/B SIDE OF RIB STAB BS 147.90 7.5"-8" FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 28,651 hrs · 16,611 cycles

RT NR 3 E-F WINDOW POST 2ND FROM BOTTOM FASTENER CRACKED. REPAIRED POST IAW ACO.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,651 hrs · 16,611 cycles

RT HORIZONTAL STAB LOWER SKIN CRACKED AT I/B SIDE OF RIB STAB BS 101.90 8"-9" FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,651 hrs · 16,611 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT REAR SPAR STAB BS 96-99. REPAIRED SKIN IAW SRM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 28,651 hrs · 16,611 cycles

LT NR 3 E-F WINDOW POST 2ND FROM BOTTOM FASTENER CRACKED. REPAIRED POST PER CUSTOMER CARD.

Part: PANEL — CORRODED (FUSELAGE) · airframe 28,651 hrs · 16,611 cycles

PANEL 120BF CORRODED ON UPPER SURFACE. R&R PANEL IAW SRM.

Part: PANEL — CORRODED (FUSELAGE) · airframe 28,651 hrs · 16,611 cycles

PANEL 140CF CORRODED ON UPPER SURFACE. R&R PANEL IAW SRM.

Part: BATTERY PACK — CRACKED (EMERGENCY LIGHT) · airframe 28,364 hrs · 16,444 cycles

FWD LEFT BATTERY PACK FAILED EMERGENCY LIGHTING BATTERY PACK CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: HOUSING — BROKEN (EXIT SIGN) · airframe 28,346 hrs · 16,436 cycles

MID CABIN OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED SIGN HOUSING PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 28,334 hrs · 16,430 cycles

CEILING EXIT SIGN BROKEN. SECURED SIGN IAW MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 26,020 hrs · 15,067 cycles

LEFT LOWER HORIZONTAL SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 26,020 hrs · 15,067 cycles

RIGHT LOWER HORIZONTAL SKIN CRACKED AT STA. 147.90. REPAIRED SKIN PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 24,901 hrs · 14,432 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT HOOK LOOSE. REMOVED AND REPLACED HOOK PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 24,901 hrs · 14,432 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER GIRT HOOK LOOSE. REMOVED AND REPLACED HOOK PER SRM.

Part: FAN — FAULTY (A/C BAY) · airframe 23,298 hrs · 13,497 cycles

FLIGHT ATTENDANT REPORTED ODOR AT ROW 10. TURNED OFF RECIRC FAN, ODOR DISSIPATED. REMOVED AND REPLACED RECIRC FAN PER MM.

Part: COVER — BROKEN (CABIN) · airframe 22,528 hrs · 13,065 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,973 hrs · 12,744 cycles

DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 772, RBL 3. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,973 hrs · 12,744 cycles

DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED BEAM IAW SRM AND EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,973 hrs · 12,744 cycles

DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 772, LBL 8. REPAIRED BEAM IAW SRM AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,785 hrs · 1,331 cycles

DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EEPLS LIGHT INOP. REMOVED AND REPLACED EEPLS PER MM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,852 hrs · 12,897 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX STIFFENER CRACKED AT BS 547.5, RBL 15. REMOVED AND REPLACED STIFFENER PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 21,661 hrs · 12,781 cycles

DURING SCHEDULED HC2 CHECK FOUND, RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 21,480 hrs · 12,452 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 20,925 hrs · 12,139 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 20,488 hrs · 11,907 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 21. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,233 hrs · 11,748 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS INOP AT ROW 12. RELAMPED PER MM.

Part: LENS — BROKEN (CABIN) · airframe 19,827 hrs · 11,505 cycles

DURING SCHEDULED MV3 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,467 hrs · 11,290 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP AT ROW 1. REMOVED AND REPLACED BULB PER MM.

Part: TAB — BROKEN (EXIT LIGHT) · airframe 19,459 hrs · 11,284 cycles

DURING SCHEDULED HC2 CHECK, FOUND FWD LT EMERGENCY EXIT BATTERY BASE UNIT FWD LOCKING TAB BROKEN. REMOVED AND REPLACED LIGHT BASE PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 19,459 hrs · 11,284 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — MISSING (CABIN) · airframe 19,176 hrs · 11,123 cycles

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

Part: LENS — MISSING (CABIN) · airframe 17,543 hrs · 10,196 cycles

DURING SCHEDULED SPV CHECK, FOUND EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.

Part: HOLDER — LOOSE (GIRT BAR) · airframe 16,404 hrs · 9,549 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACHMENT LOOSE. SECURED HOLDER PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 16,062 hrs · 9,332 cycles

R1 DOOR EVAC SLIDE GIRT BAR DIFFICULT TO SECURE. ADJUSTED SLIDE ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 16,033 hrs · 9,309 cycles

EEPLS LENS COVER MISSING AT ROW 2. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 16,000 hrs · 9,291 cycles

EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 14,874 hrs · 8,626 cycles

FWD EEPLS LOOSE. SECURED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 13,116 hrs · 7,560 cycles

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

Part: COVER — MISSING (CABIN) · airframe 12,646 hrs · 7,298 cycles

FOUND EMERGENCY EXIT LIGHT LENS COVER MISSING AT ROW 1. INSTALLED COVER PER MM.

Part: CAP — BROKEN (CABIN) · airframe 12,512 hrs · 7,213 cycles

DURING SCHEDULED HC1 CHECK, FOUND FWD EEPLS END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 11,874 hrs · 6,837 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 10,119 hrs · 5,762 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 9,867 hrs · 5,612 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 9,867 hrs · 5,612 cycles

RIGHT AFT CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: CAP — LOOSE (CABIN) · airframe 7,761 hrs · 4,361 cycles

EEPLS END CAP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,452 hrs · 4,180 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS LIGHT INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 6,026 hrs · 3,342 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS LENS MISSING. INSTALLED EEPLS LENS PER MM

Part: COVER — MISSING (CABIN) · airframe 4,910 hrs · 2,717 cycles

EELS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM.

Part: VALVE — FAULTY (FUEL SYSTEM) · airframe 3,963 hrs · 2,167 cycles

AT FL 390, RECEIVED FUEL IMBALANCE ALERT. LEFT TANK WAS 1000 LBS LESS THAN RIGHT TANK AND DECREASING RAPIDLY. REMOVED AND REPLACED FUEL CROSSFEED VALVE PER MM.

Part: HOOK — LOOSE (L1 DOOR SLIDE) · airframe 3,562 hrs · 1,950 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED GIRT BAR HOOKS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,111 hrs · 1,695 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT FWD CABIN EEPLS LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — LOOSE (CABIN) · airframe 2,839 hrs · 1,553 cycles

EEPLS COVER LOOSE AT ROW 14 DEF. SECURED EEPLS COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,743 hrs · 1,494 cycles

DURING SCHEDULED MV3 CHECK, FOUND FWD CABIN EEPLS STRIP INOP. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 2,394 hrs · 1,309 cycles

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