N214WN

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 67,712 hrs · 40,393 cycles

AFT R2 DOOR SLIDE GIRT HANGING DOWN EXCESSIVELY. AFT SIDE HOOK AND LOOP STRIP EXPOSED. SECURED AFT R2 DOOR EMERGENCY SLIDE GIRT IN REF TO SIP.

Part: COVER — DETACHED (ZONE 200) · airframe 67,490 hrs · 40,249 cycles

MID CABIN EXIT SIGN COVER FELL DOWN. SECURED EXIT SIGN COVER IAW SIP.

Part: SEAL — CRACKED (ZONE 300) · airframe 66,633 hrs · 39,720 cycles

RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDER SEAL CRACKED. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER UPPER SLIDER SEAL IAW AMM 53-31-31

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 65,995 hrs · 39,334 cycles

L2 EXTERIOR EMERGENCY LIGHT INOP<[01] REPLACED L2 EXTERIOR EMERGENCY LAMP REF AMM 33-51-04. OPS CHECK GOOD.

Part: BULB — BURNED OUT (ZONE 200) · airframe 65,362 hrs · 38,965 cycles

BURNED ENTRY DOOR EMERGENCY LIGHT BULB ON EXTERIOR FUSELAGE AT AFT GALLEY AREA 2024-780560<[01] REPLACED ENTRY DOOR EMERGENCY LIGHT BULB ON EXTERIOR FUSELAGE AT AFT GALLEY AREA IAW B737-700 AMM 33-51-04-960-801.;[02] TASK CARD COMPLETED <BR>REPLACED ENTRY DOOR EMERGENCY LIGHT BULB ON EXTERIOR FUSELAGE AT AFT GALLEY AREA IAW B737-700 AMM 33-51-04-960-801.

Part: LIGHT — DETACHED (ZONE 200) · airframe 65,362 hrs · 38,965 cycles

MISSING EMERGENCY EXIT LIGHT (2EA) FOUND DISCONNECTED AND REMOVED FROM EYE END TERMINALS BY UNDOCUMENTED MAINTENANCE ON ROW 12ABC AND 9ABC AT PASSENGER CABIN 2024-780549<[01] REMOVED AND RE-INSTALLED EMERGENCY Ï¿½REA LIGHT ROW 12ABC AND 9ABC LIGHT ASSEMBLY AT PASSENGER CABIN I.A.W B737-700 AMM 33-51-03-960-802. PERFORMED TEST OF THE EMERGENCY LIGHT. TEST IS OK. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: PLATE — CRACKED (ZONE 500) · airframe 65,362 hrs · 38,965 cycles

CRACK CORRUGATED PLATE AT OFS 353 BTW SPOILER 3 AND 4 LT WING 2024-780547<[01] REPLACED CURRUGATED PLATE LOC OFS 353 BTW SPOILER 3 AND 4 LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 STEP 9. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: BEAM — CRACKED (ZONE 200) · airframe 65,362 hrs · 38,965 cycles

CRACK INDICATION FOUND LOC. STA 663.75 LBL 45.5 I/B SIDE LOWER CHORD LONGITUDINAL BEAM AT 10 OCLOCK. 2024-780492 <[01]. TOOL USED ON STEP 2. ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25; [02] ON STEP 4: TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030456 DUE DATE: 14 APR 25.; [03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 04 FEB 25; P/N P3015GOES00000 S/N 142811019 DUE DATE 04 FEB 25.; [04] REPAIRED LOWER CHORD LONGITUDINAL BEAM BTW BSTA 660 AND BSTA 680 LBL 45.51 IAW EA-25-153-00187-WIP1; EA-25-153-00187-WIP2; AND EA-25-153-00187 SUMMARY; SEE INDIVIDUAL SIGN OFFS BELOW.; [05] REPAIRED LOWER CHORD LONGITUDINAL BEAM BTW BSTA 660 AND BSTA 680 LBL 45.51 IAW EA-25-153-00187-WIP1; EA-25-153-00187-WIP2; AND EA-25-153-00187 SUMMARY; SEE INDIVIDUAL SIGN OFFS BELOW. RII.

Part: STRINGER — CRACKED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

CRACK STRINGER 25L LOCATED STA540 FWD CARGO COMPARTMENT 2024-780465 <[01] TOOL USED P/N: 45MG; S/N: 130066401; CAL DUE: 21-OCT-25.;[02] TOOL USED ON STEP 8: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 60007161486 ; DUE DATE:06-SEP-25;[03] REPAIRED STRINGER 25L LOCATED BS 540 TO BS 500D IAW B737-700 SRM B737-700 SRM 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A. NOT FURTHER ACTIONS OR INSPECTION REQUIRED. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] CORRECTED STEP3: REPAIRED STRINGER 25L LOCATED BS 540 TO BS 500D IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A. NOT FURTHER ACTIONS OR INSPECTION REQUIRED. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] RII ITEM. REPAIRED STRINGER 25L LOCATED BS 540 TO BS 500D IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A. NOT FURTHER ACTIONS OR INSPECTION REQUIRED. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

CRACK ANGLE WEATHER RADAR SUPPORT STRUCTURE LOCATED BETWEEN STA188 TO STA203.8 AND RBL5 AT FWD OF NOSE WHEEL WELL 2024-780466<[01] REPLACED NEW ANGLE WEATHER RADAR SUPPORT STRUCTURE AND FASTENERS LOCATED BETWEEN STA188 TO STA203.8 AND RBL5 AT FWD OF NOSE WHEEL WELL. IAW B737-700 SRM 51-40-02; IAW B737-700 DWG NO:141A9194 SHEET: 4 REV: D; IAW B737-700 SRM 51-10-02 STEP 9. REV C. SEE INDIVIDUAL SIGN OFF BELOW;[02] COMPLETED TASK CERTIFIED

Part: STRINGER — CRACKED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

CRACK STRINGER 26L LOCATED STA540 FWD CARGO COMPARTMENT 2024-780464 <[01] TOOL USED P/N: 45MG; S/N: 130066401; CAL DUE: 21-OCT-25.;[02] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 60009161631 DUE DATE: 11-MAR-25;[03] REPAIRED STRINGER 26L LOCATED BS 540 TO BS 500D IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A. NOT FURTHER ACTIONS OR INSPECTION REQUIRED. SEE INDIVIDUAL SIGN-OFF BELOW.;[04] RII ITEM <BR>REPAIRED STRINGER 26L LOCATED BS 540 TO BS 500D IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 THIS REPAIR IS CATEGORY A. NOT FURTHER ACTIONS OR INSPECTION REQUIRED. SEE INDIVIDUAL SIGN-OFF BELOW.

Part: RIB — CRACKED (ZONE 300) · airframe 65,362 hrs · 38,965 cycles

CRACK LEADING EDGE RIB ACCESS PANEL 331B LE STA 161.04 AT LT HORIZONTAL STABILIZER 2024-780414<[01] REPLACED LEADING EDGE RIB ACCESS PANEL 331B LE STA 161.04 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; AND DWG 186A1001 SHEET 11 REV A.;[02] CORRECTIVE STEP 1<BR>REPLACED LEADING EDGE RIB ACCESS PANEL 331B LE STA 161.04 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; AND DWG 186A1001 SHEET 11 REV A.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] TASK COMPLETED; SEE INDIVIDUAL SIGN-OFF BELOW

Part: BRACKET — CRACKED (ZONE 600) · airframe 65,362 hrs · 38,965 cycles

CRACK SUPPORT BRACKET INBOARD FRONT SPAR IFSS 151 AT RT WING 2024-780410<[01] REPLACED SUPPORT BRACKET LOCATED INBOARD FRONT SPAR IFSS 151 AT RT WING IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGNS OF BELOW.;[02] REPLACED SUPPORT BRACKET LOCATED INBOARD FRONT SPAR IFSS 151 AT RT WING IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGNS OF BELOW. AS RII.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

CRACK SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND LBL 6 AT AIR CONDITIONING BAY 2024-780405<[01] REPLACED SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND LBL 6 AT AIR CONDITIONING BAY I.A.W B737-700 SRM 51-40-02-0G-0 AND AMM 20-50-11-910-801.<BR><BR>SEE INDIVIDUAL SIGN OFF BELLOW;[02] REPLACED SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND LBL 6 AT AIR CONDITIONING BAY I.A.W B737-700 SRM 51-40-02-0G-0 AND AMM 20-50-11-910-801.

Part: RIB — CRACKED (ZONE 300) · airframe 65,362 hrs · 38,965 cycles

CRACK LEADING EDGE RIB ACCESS PANEL 331B LE STA 151.75 AT LT HORIZONTAL STABILIZER 2024-780411<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25.;[02] REPLACED RIB LOCATED LEADING EDGE ACCESS PANEL 331B LE STA 151.75 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 186A1001 SHEET:10 REV:A SEE INDIVIDUAL SIGNS OFF BELOW;[03] TASK CARD COMPLETE. <BR><BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: STRINGER — CRACKED (ZONE 600) · airframe 65,362 hrs · 38,965 cycles

CRACK STRINGER 8 INTERNAL AREA FUEL TANK LOC. BTW RIB 19 AND RIB 20 UPPER SKIN LOWER SURFACE AFT AREA AT RT WING 2024-780408 <[01]. TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25.;[02] REPAIRED STRINGER 8 INTERNAL AREA FUEL TANK LOC. BTW RIB 19 AND RIB 20 WSTA 564.5 TO WSTA 591.5 AND SKIN ATTACHMENT FLANGE IAW EA-25-157-00126 WIP1 AND EA-25-157-00126 SUMMARY; SEE INDIVIDUAL SIGN OFF BELOW;[03] REPAIRED STRINGER 8 INTERNAL AREA FUEL TANK LOC. BTW RIB 19 AND RIB 20 WSTA 564.5 TO WSTA 591.5 AND SKIN ATTACHMENT FLANGE IAW EA-25-157-00126 WIP1 AND EA-25-157-00126 SUMMARY; SEE INDIVIDUAL SIGN OFF BELOW.

Part: SKIN PANEL — CRACKED (ZONE 300) · airframe 65,362 hrs · 38,965 cycles

CRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 1.25 INCH. APPROX. 2024-780403 <[01]. ON STEP 4; TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 210138103; DUE DATE: 10-JUN-25;[02] ON STEP 5; TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 210138103; DUE DATE: 10-JUN-25;[03] ULTRASONIC EQUIPMENT USED P/N: 45 MG; S/N: 130063701; DUE DATE: 08-OCT-25; [04] PERFORMED REPAIR ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. I.A.W. SRM 55-10-01-2R-11. REPAIR 11. SEE INDIVIDUAL SIGN-OFF BELOW.; [05] TASK COMPLETED; RII. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: TIE CLIP — COLLAPSED (ZONE 200) · airframe 65,362 hrs · 38,965 cycles

CRACK TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN 2024-780336 <[01]. REPLACED TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN IAW B737-700 SRM: 51-40-02 AND SRM 51-10-02 STEP 9; AND DWG: 141A8380 SHEET:15. REV:-; SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED; RII. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 65,362 hrs · 38,965 cycles

CRACK WEB INTERCOSTAL LOCATED BETWEEN BS 294.5 AND BS 303.9 AND STRINGER 16L AT FWD GALLEY AREA 2024-780350<[01]. INSTALLED NEW WEB INTERCOSTAL; STRAP 1(E/A) ANGLE 1(E/A) AND FASTENERS. LOCATED BETWEEN BS 294.5 AND BS 303.9 AND STRINGER 16L AT FWD GALLEY AREA IAW B737-700 SRM: 51-40-02 AND SRM 51-10-02 STEP 9; DWG: 141A8180 SHEET 27 REV. C. SEE INDIVIDUAL SIGN OFF BELOW; [02] CORRECTIVE ACTION 1: REPLACED WEB INTERCOSTAL AND FASTENERS. LOCATED BETWEEN BS 294.5 AND BS 303.9 AND STRINGER 16L AT FWD GALLEY AREA IAW B737-700 SRM: 51-40-02 AND SRM 51-10-02 STEP 9; DWG: 141A8180 SHEET 27 REV. C. SEE INDIVIDUAL SIGN OFF BELOW; [03] TASK COMPLETED; RII. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (ZONE 200) · airframe 65,362 hrs · 38,965 cycles

CRACK ANGLE LOCATED STA294.5 AND STR13L AT PASSENGER CABIN 2024-780338 <[01]. REPLACED ANGLE AND FASTENERS LOCATED STA294.5 AND STR13L AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A1311 SHEET 1 REV C. SEE INDIVIDUAL SIGN OFF BELOW; [02] TASK COMPLETED; RII SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 200) · airframe 65,362 hrs · 38,965 cycles

CRACK ANGLE LOCATED STA294.5 AND STR17R AT FWD GALLEY AREA 2024-780353 <[01] REPLACED ANGLE AND FASTENERS LOCATED STA294.5 AND STR17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 STEP 9 AND SRM 51-40-02; AND DWG:141A8310;SHEET:25; REV: ; SEE INDIVIDUAL SIGN OFF BELOW; [02] REPLACED ANGLE AND FASTENERS LOCATED STA294.5 AND STR17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 STEP 9 AND SRM 51-40-02; AND DWG:141A8310;SHEET:25; REV: ; SEE INDIVIDUAL SIGN OFF BELOW. CERTIFIED RII.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

CRACK ANGLE - SUPPORT BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRNGER 27R AFT CARGO COMPARTMENT 2024-780306 <[01] REPLACED ANGLE - SUPPORT LOCATED BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRNGER 27R AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02; DWG NO: DWG NO:147A7221 SHEET: 24 REV:-; IAW B737-700 SRM 51-10-02 STEP 9; [02] CORRECTED STEP 1. REPLACED ANGLE - SUPPORT LOCATED BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRNGER 27R AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02; DWG NO: DWG NO:147A7221 SHEET: 24 REV:-; IAW B737-700 SRM 51-10-02 STEP 9; SEE INDIVIDUAL SIGNOFF BELOW.;[03] TASK CARD COMPLETE. SEE INDIVIDUAL SIGN OFF BELOW.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 65,362 hrs · 38,965 cycles

CRACK WEB - INTERCOSTAL BETWEEN BS 927 TO BS 947.5 AND STRINGER 25R AFT CARGO COMPARTMENT 2024-780305<[01]. REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 927 TO BS 947.5 AND STRINGER 25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 147A7500 SHEET: 24 AND SHEET: 25 REV - SEE INDIVIDUAL SING OFF BELOW;[02] COMPLETED TASK CERTIFIED.

Part: SUPPORT — ELONGATED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

ELONGATED HOLE ON SUPPORT ZEE LOCATED BETWEEN STA500 TO STA500A AFT CARGO COMPARTMENT 2024-780276 ELONGATED HOLE ON SUPPORT ZEE LOCATED BETWEEN STA500 TO STA500A AND LBL22 FWD CARGO COMPARTMENT<[01] REPLACED SUPPORT ZEE (1E/A) AND STRAP SPLICE (1E/A) LOCATED BETWEEN STA520 TO STA480 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02-0G-0. ITEM 9 AND DWG 143A7500 SHEET:58 REV:- AND DWG 143A7501 SHEET:1 REV:B SEE INDIVIDUAL SIGN OFF BELOW; [02] REPLACED SUPPORT ZEE (1E/A) AND STRAP SPLICE (1E/A) LOCATED BETWEEN STA520 TO STA480 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02-0G-0. ITEM 9 AND DWG 143A7500 SHEET:58 REV:- AND DWG 143A7501 SHEET:1 REV:B SEE INDIVIDUAL SIGN OFF BELOW; [03] CORRECTED STEP 2. REPLACED SUPPORT ZEE (1E/A) AND STRAP SPLICE (1E/A) LOCATED BETWEEN STA520 TO STA480 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02-0G-0. ITEM 9 AND DWG 143A7500 SHEET:58 REV:- AND DWG 143A7501 SHEET:1 REV:B SEE INDIVIDUAL SIGN OFF BELOW RII.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN STA500 TO STA500A AND LBL22 FWD CARGO COMPARTMENT 2024-780277<[01]. REPLACED WEB - INTERCOSTAL LOCATED BETWEEN STA500 TO STA500A AND LBL22 FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 37 REV -. SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED WORK PERFORMED. SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

CRACK ANGLE - CLIP LOCATED STA400 AND STR26R FWD CARGO COMPARTMENT 2024-780271<[01] REPLACED ANGLE-CLIP AND FASTENERS LOC ON STA400 AND STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 STEP 9 AND SRM 51-40-02 AND DWG 143A7505 SHEET 2 REV B. SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW.

Part: PRESSURE WEB — CRACKED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

CRACK INDICATION FOUND ON HORIZONTAL PRESSURE WEB UPPER SURFACE BTW STA 663 TO STA 675; AT LEVEL LBL 30. CRACK LENGTH = 0.695 INCHES APPROX. 2024-780281<[01] ON STEP 5: TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030456 DUE DATE: 14 APR 25.; [02] TOOL USED ON STEP 6: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 28-MAY-25; [03] PERFORMED PERMANENT REPAIR ON PRESSURE DECK WEB LOCTED BTW BS 663 TO BS 675 BTW LBL 24 TO LBL 60 IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2. SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR ON PRESSURE DECK WEB LOCTED BTW BS 663 TO BS 675 BTW LBL 24 TO LBL 60 IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2. SEE INDIVIDUAL SIGN OFF BELOW.;[05] CORRECTED ITEM 4 <BR>PERFORMED PERMANENT REPAIR ON PRESSURE DECK WEB LOCTED BTW BS 663 TO BS 675 BTW LBL 24 TO LBL 60 IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2. SEE INDIVIDUAL SIGN OFF BELOW. AS RII.

Part: PANEL — CRACKED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

CRACK ON HOLES ACCESS PANEL 191CL BODY FAIRING AT FUSELAGE EXTERIOR 2024-780250 <[01] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 16122983 DUE DATE: 15-FEB-25;[02] UT EQUIPMENT USED P/N: EPOCH 600; S/N: 120357005; DUE DATE: 10-JUN-25;[03] REPAIRED ACCESS PANEL 191CL BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW.; [04] REPAIRED ACCESS PANEL 191CL BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW.

Part: PANEL — CRACKED (ZONE 200) · airframe 65,362 hrs · 38,965 cycles

CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 AND LBL 24.75 AT PASSENGER CABIN 2024-780225<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 AND LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 143A0060; SHEET:44;REV:A SEE INDIVIDUAL SIGN OFFS BELOW;[02]. REPLACED BRAKE PANEL FLOOR STRUCTURES BS 540 BETWEEN BL 0 AND LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM51 10 02 AND DOWN 143A0060 SHT44 REV A. SEE INDIVIDUALS SIGNOFFS.

Part: LIGHT — BROKEN (ZONE 200) · airframe 65,362 hrs · 38,965 cycles

BROKEN FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA) 2024-780243<[01] INSTALLED FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802;[02] CORRECTED STEP 1. REPLACED FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802;[03] REPLACED FLOOR PROXIMITY LIGHTING PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802.

Part: ANGLE — CRACKED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

CRACK ANGLE - CLIP LOCATED STA400 AND STR26L FWD CARGO COMPARTMENT 2024-780136<[01] REPLACED ANGLE - CLIP LOCATED STA400 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 51-40-02 AND DWG 143A7505 SHEET 2 REV: B SEE INDIVIDUAL SIGN OFF BELOW; [02] REPLACED ANGLE - CLIP LOCATED STA400 AND STR26L FWD CARGO COMPARTMENT IAW B737-700 51-40-02 AND DWG 143A7505 SHEET 2 REV: B SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

CRACK ANGLE - CLIP LOCATED STA500C AND STR26R FWD CARGO COMPARTMENT 2024-780168<[01] REPLACED ANGLE - CLIP LOCATED ON STA500C AND STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A7505 SHEET: 6 REV D;

Part: GUSSET — CRACKED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

CRACK GUSSET LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT 2024-780157 <[01]. REPLACED NEW 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] TASK CARD COMPLETE AND CERTIFIED AS RII. SEE INDIVIDUAL SIGN OFF BELOW.

Part: GUSSET — CRACKED (ZONE 100) · airframe 65,362 hrs · 38,965 cycles

CRACK GUSSET LOCATED STA500D AND STR19L FWD CARGO COMPARTMENT 2024-780148<[01] REPLACED GUSSET AND FASTENER LOCATED STA500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 SHEET 174 REV: ? SEE INDIVIDUAL SIGN OFFS BELOW;[02] TASK COMPLETED. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: PANEL — CRACKED (ZONE 200) · airframe 65,362 hrs · 38,965 cycles

CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 AND RBL 24.75 AT PASSENGER CABIN 2024-780232 <[01]. REPLACED BRAKE PANEL (INTERCOSTAL) 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] REPLACED BRAKE PANEL (INTERCOSTAL) 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.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 65,362 hrs · 38,965 cycles

CRACK SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND BL 0 AT PASSENGER CABIN 2024-780190<[01]. STEP 1. EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 240494307 AND DUE DATE: 27-AUG-25.;[02] PERFORMED NDT INSPECTION AND NOT CRACK FOUND IAW 737 NDT MANUAL PART 6 SECTION 51-00-00 AND NO MAINTENANCE ACTION REQUIRED SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED ITEM 2 : PERFORMED VISUAL INSPECTION ON SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND BL 0 AT PASSENGER CABIN AND NOT FOUND DAMAGE IAW B737-700 SRM 51-10-02 AND PERFORMED NDT INSPECTION AND NOT CRACK FOUND IAW 737 NDT MANUAL PART 6 SECTION 51-00-00 AND NO MAINTENANCE ACTION REQUIRED SEE INDIVIDUAL SIGN OFF BELOW.;[04] CORRECTIVE ACTION STEP 3 CERTIFIED.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 65,362 hrs · 38,965 cycles

CRACK LOWER SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND LBL 24.75 AT PASSENGER CABIN 2024-780204 <[01]. TOOL USED: TEMPE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE 23 JAN 25.;[02] INSTALLED NEW SUPPORT ANGLE AND FASTENERS. LOCATED BS 695 AND LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM: 51-40-02 AND SRM 51-10-02 STEP 9. DWG: 111A6000 ;SHEET:244 ;REV:- SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTIVED ACTION 2. REPLACED SUPPORT ANGLE AND FASTENERS. LOCATED BS 695 AND LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM: 51-40-02 AND SRM 51-10-02 STEP 9. DWG: 111A6000 ;SHEET:244 ;REV:- SEE INDIVIDUAL SIGN OFF BELOW.;[04] TASK COMPLETED; RII. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ACCESS PANEL — CRACKED (ZONE 600) · airframe 65,362 hrs · 38,965 cycles

CRACK ON HOLES ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2024-780050<[01] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 16122983 DUE DATE: 15-FEB-25;[02] TOOL USED: HOT BONDER PN: HCS9200B SN: 16122983 DUE DATE: 15/FEB/25.;[03] TOOL USED: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 600; S/N:120357005; DUE DATE: 10-JUN-25.;[04] TOOL USED: HUMIDITY/TEMPERATURE CHART RECORDER P/N: TH8P3; S/N: 19104817 ; DUE DATE: 21-MAR-25;[05] TOOL USED: MULTIMETER P/N: FLUKE 87; S/N: 42180179; DUE DATE: 26-MAR-25;[06] REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 65,021 hrs · 38,764 cycles

MID CABIN RIGHT SIDE 3 AISLE AND OVERWING EMERGENCY EXIT LIGHTS INOP<[01] T/S PER FIM 33-50 TASK 801; REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK (M1669) PER AMM 33-51-06. ALL E-LIGHTS OPS CHECK GOOD.

Part: COVER — DETACHED (ZONE 200) · airframe 64,589 hrs · 38,501 cycles

EXIT ROW SIGN AT MID CABIN FELL OFF THE CEILING<[01] REINSTALLED COVER PER AMM 33-51-03.

Part: HANDLE — LOOSE (MEGAPHONE) · airframe 63,683 hrs · 37,938 cycles

CREW REPORTS MEGAPHONE HANDLE IS LOOSE<[01] R & R MEGAPHONE IAW SIP OPS CHECKS GOOD

Part: COUNTER — SMOKE (COCKPIT) · airframe 62,626 hrs · 37,288 cycles

FO TRIP COUNTER HAD SMOKE COMING FROM LIGHT<[01] INSPECTED YOKE AREA; NO DAMAGE FOUND<BR>R/R TRIP COUNTER PER AMM 33-11-00

Part: FAIRING — DELAMINATED (ZN 100 FUS LOWER) · airframe 60,732 hrs · 36,120 cycles

FAIRING 194CR REQUIRE REPLACEMENT REF FAULT TTG8Q00M0RW FOR 194CR<[01] REMOVED AND REPLACED FAIRING PANEL ASSY 194CR IAW AMM 53-51-21.

Part: FAIRING — DELAMINATED (ZN 100 FUS LOWER) · airframe 60,732 hrs · 36,120 cycles

FAIRING 194FR REQUIRE REPLACEMENT REF TTG8Q00M0SWV FOR 194FR<[01] REPLACED 194FR PANEL PER AMM 53-51-21.

Part: FAIRING — DELAMINATED (ZN 100 FUS LOWER) · airframe 60,732 hrs · 36,120 cycles

FAIRING 194GR REQUIRE REPLACEMENT REF. TTG8Q00M0S0K FOR 194GR<[01] REMOVED AND REPLACED WING TO BODY FAIRING IAW AMM 53-51-21

Part: PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 60,500 hrs · 35,969 cycles

FOUND DELAMINATION ON PANEL 194CR<[01] COMPLIED WITH EA 23-153-02086.;[02] C/W

Part: PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 60,500 hrs · 35,969 cycles

FOUND DELAMINATION ON PANEL 194GR<[01] SEE TASK 23-153-02086 FOR WORK PERFORMED.

Part: PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 60,500 hrs · 35,969 cycles

FOUND DELAMINATION ON PANEL 194FR<[01] SEE TASK 23-153-02086 FOR WORK PERFORMED.

Part: SLIDE — INOPERATIVE (ZN 800 DOOR) · airframe 60,165 hrs · 35,752 cycles

L1 DOOR PRESSURE INDICATOR IN RED<[01] REPLACED FWD ENTRY DOOR SLIDE AMM 25-66-01 AND MT 725-61-01FE

Part: HANDLE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 60,150 hrs · 35,739 cycles

PASSENGER CABIN- AFT SERVICE DOOR INSIDE DOOR HANDLE SHAFT COVER NOT SECURE.<[01] RE-SECURED PASSENGER CABIN- AFT SERVICE DOOR INSIDE DOOR HANDLE SHAFT COVER REF AMM 52-41-31.

Part: FITTING — LOOSE (ZN 800 DOOR) · airframe 59,300 hrs · 35,194 cycles

CUSTOMER REQUEST: L1 DOOR GIRT BAR FITTING LOOSE<[01] L1 DOOR GIRT BAR FITTING TIGHTENED;[02] ADD TO STEP #1<BR>REFERENCE B737-700 AMM 25-66-01-000-804.;[03] VERIFIED STEPS 1 AND 2

Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 59,300 hrs · 35,194 cycles

AFT WINDSCREEN I/B FLASHLIGHT INOP<[01] REPLACED FLASHLIGHT BATTERY FOR PROPER FUNCTION AS PER AMM 25-64-00-900-806.;[02] VERIFIED STEP 1

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 59,300 hrs · 35,194 cycles

PASSENGER CABIN OVERHEAD BIN EMERGENCY LIGHT AT ROW 9ABC INOP.<[01] RELAMPED PASSENGER CABIN OVERHEAD BIN EMERGENCY LIGHT AT ROW 9ABC AS PER REF B737 AMM 33-51-03-960-801. TEST OK.;[02] VERIFIED STEP 1.

Part: LIGHT — INOPERATIVE (ZN 800 DOOR) · airframe 59,300 hrs · 35,194 cycles

L2 DOOR EXTERIOR EMERGENCY LIGHT INOP.<[01] RELAMPED L2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.

Part: COWLING — ELONGATED (ZN 400 NACELLE/P) · airframe 59,300 hrs · 35,194 cycles

# 2 ENGINE NOSE COWL INLET SKIN ATTACH STRAP HAS ELONGATED FASTENER HOLE AT 9 O'CLOCK POSITION AND 6' AFT OF FORWARD EDGE OF STRAP. (51-022)<[01] #2 ENG INLET COWL TO BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1

Part: COWLING — ELONGATED (ZN 400 NACELLE/P) · airframe 59,300 hrs · 35,194 cycles

# 2 ENGINE NOSE COWL INLET SKIN HAS ELONGATED FASTENER HOLE AT 9 O'CLOCK POSITION AND 7.5' AFT OF FORWARD EDGE OF SKIN.(51-021)<[01] #2 ENG INLET COWL TO BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1

Part: FAIRING — ELONGATED (ZN 600 RIGHT WIN) · airframe 59,300 hrs · 35,194 cycles

FOUND ELONGATED HOLES ON SUPPORT FAIRING 642BB MIDDLE SEAL SECTION R/H SIDE<[01] PREPARED FOR REPAIR FAIRING 642 BB; AS PER B737 SRM 51-70-06-2R-9;[02] VERIFIED STEP 1.;[03] REPAIRED FAIRING 642BB AS PER B737 SRM 51-70-06-2R-9 MATERIAL USED PO.1800218 AND PO.1690463;[04] VERIFIED STEP 3. OK TO APPLY TOP COAT.;[05] APPLIED TOP COAT TO SUPPORT FAIRING 642BB MIDDLE SEAL SECTION ON R/H SIDE PER AMM 51-21-73-370-803;[06] VERIFIED STEP 5.

Part: BRACKET — CRACKED (ZN 500 LEFT WING) · airframe 59,300 hrs · 35,194 cycles

LEFT WING T/E ABOVE ACCESS PANEL 551GB SUPPORT BRACKET CRACK<[01] REMOVED BRACKET TO GAIN ACCESS TO THE CRACKED BRACKET SUPPORT PER SRM 51-40-02-0G-0;[02] REMOVED CRACKED SUPPORT BRACKET PER SRM 51-40-02-0G-0;[03] VERIFIED STEPS 1 AND 2;[04] INSTALLED NEW BRACKET PART # 115A2350-1 PER SRM 51-40-02-0G-0;[05] VERIFIED STEP 4;[06] OK TO RE-INSTALL BRACKET;[07] REINSTALLED BRACKET PREVIOUSLY REMOVED FOR ACCESS AT LEFT WING T/E PER REF SRM 51-40-02-0G-0;[08] REMOVED AND REPLACED BRACKET AT LEFT WING T/E PER REF SRM 51-40-02-0G-0;[09] VERIFIED STEP 8

Part: PLATE — CORRODED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

EVIDENCE OF CORROSION ON LOWER FUSELAGE NO. 2 VHF ANTENNA MOUNTING PLATE<[01] REMOVED LOWER FUSELAGE NO. 2 VHF ANTENNA MOUNTING PLATE PER REF. SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.;[03] LOCATED AND DRILL NEW LOWER FUSELAGE NO. 2 VHF ANTENNA MOUNTING PLATE PER REF. SRM 51-40-05-0G-0.;[04] VERIFIED STEP 3 ; OK TO TREAT AND PRIME.;[05] TREATED LOWER FUSELAGE SKIN PER REF. AMM 51-21-41-370-802 AND TREATED AND PRIMED NO. 2 VHF ANTENNA MOUNTING PLATE HOLES PER REF. AMM 51-21-41-370-802 AND AMM 51-21-72-370-804.;[06] VERIFIED STEP 5 ; OK TO INSTALL #2 VHF ANTENNA MOUNTING PLATE.;[07] INSTALLED NO. 2 VHF ANTENNA MOUNTING PLATE PER REF. SRM 51-40-02-0G-0 AND DRAWING 146A7730.;[08] VERIFIED STEP 7.;[09] FINAL: REMOVED AND REINSTALLED NEW NO. 2 VHF ANTENNA MOUNTING PLATE PER REF. SRM 51-40-02-0G-0 AND DRAWING 146A7730.;[10] STEP 9 VERIFIED AS FINAL.

Part: DOOR — OUT OF ADJUST (ZN 800 DOOR) · airframe 59,300 hrs · 35,194 cycles

CUSTOMER REQUEST....L1 DOOR NEEDS RIG CHECK DOESN'T CLOSE EVENLY.<[01] ACCOMPLISHED L1 DOOR ADJUSTMENTS AS PER AMM 52-11-00-820-801 STEPS 2.H.(1) UP TO 2.H.(9). AND CHECKED SKIN CLEARANCE AND FLUSHNESS OK. ACCOMPLISHED FORWARD ENTRY DOOR SYSTEM TEST AS PER AMM 52-11-00-700-804<BR>TOOL USED: B/C 172991 DUE DATE: 25-JUL-23<BR>TOOL USED: B/C 10198 DUE DATE: 31-OCT-23;[02] VERIFIED STEP #1.-

Part: PANEL — CRACKED (ZN 300 STABILIZE) · airframe 59,300 hrs · 35,194 cycles

VERTICAL FIN ACCESS PANEL 323BL SKIN SURFACE CRACKED.<[01] CUT OUT DAMAGE AREA AS MARKED ON TOP SURFACE OF ACCESS PANEL 323BL; NO CORE DAMAGE. PERFORMED DRY OUT; FOUND NO WATER REPAIR SIZE 1' DIA. PREPARED AREA FOR REPAIR ASPER B737 SRM 51-70-04-2R-1;[02] VERIFIED STEP 1. OK TO INSTALL REPAIR.;[03] REPAIRED DAMAGE AREA AS MARKED ON TOP SURFACE OF VERTICAL FIN ACCESS PANEL 323BL AS PER B737 SRM 51-70-04-2R-1. MATERIALS USED PO#1800218 AND PO#1690463;[04] PERFORMED TAP TEST ON REPAIRED AREA. FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION 5;[05] VERIFIED STEPS 3 AND 4. OK TO TOPCOAT.;[06] PREPARED AND APPLIED TOPCOAT AT VERTICAL FIN ACCESS PANEL 323BL SKIN SURFACE IN REFERENCE WITH B737-700 AMM 51-21-73-370-803;[07] VERIFIED STEP SIX.

Part: THRESHOLD — CRACKED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

ITEM CABIN PASSENGER FLOOR STRUCTURE STA 303.9 LEFT WL 208.1 THRESHOLD INNER CORD HAS A CRACK<[01] REMOVED INNER CORD FROM STA. 277 TO 360 LBL 60' WL 208.1 AT CABIN PASSENGER FLOOR REF. B 737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] LATE ENTRY INSTALLED EWIS PROTECTION FROM STA 277 TO 360 LBL 60 WL 208.1 REF B 737 AMM 20-60-07-913-801;[04] LOCATED A DRILLED NEW INNER CORD PART # 654A0004 REFERENCE B737-700 SRM 51-40-05-0G-0;[05] VERIFIED STEP 3 AND 4<BR>OK TO TREAT AND PRIME;[06] TREATED AND PRIMER HOLES AT INNER CORD REF. B737-700 AMM 51-21-72-370-804;[07] VERIFIED STEP 6;[08] OK TO INSTALL INNER CORD;[09] MIXED SEALANT BMS 5-95 AT 06:00 PM 01-18-2023 SQUEEZE OUT AT 02:00 AM 02-22-2023;[10] PARTIALLY INSTALLED 80% FASTENERS AT LEFT INNER CORD STA.277 TO 360 REF B737-700 SRM 51-40-02-0G-0;[11] VERIFIED STEP 9 AND 10;[12] COMPLETED FASTENERS INSTALLATION AT LEFT INNER CORD STA. 277 TO 360 REF. B737-700 SRM 51-40-02 AND DWG # 141A8110;[13] VERIFIED STEP 12.;[14] REMOVED EWIS PROTECTION AT CABIN PASSENGER FLOOR STRUCTURE LEFT INNER CORD STA. 277 TO 360 REF. B737-700 AMM 20-60-07-913-801;[15] VERIFIED STEP 14;[16] REMOVED AND REPLACED LEFT INNER CORD AT CABIN PASSENGER FLOOR STA.277 TO 360 REF B737-700 SRM 51-40-02-0G-0 DWG # 141A8110;[17] VERIFIED STEP 16

Part: CHANNEL — CORRODED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

FWD CARGO FLOOR SUPPORT 24' LEFT OF CENTER LINE 'Z' CHANNEL AT B/S 420-440 HAS LIGHT CORROSION AROUND NUT PLATE HOLES<[01] FWD CARGO L/H Z CHANNEL STA 400-STA 500D WILL BE REPLACED. FOR WORK ACCOMPLISHED REF TASKCARD#TTG8Q00H5X7Q;[02] VERIFIED CORRECT NONROUTINE #

Part: CHANNEL — CORRODED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

FWD CARGO FLOOR SUPPORT 24' LEFT OF CENTER LINE 'Z' CHANNEL AT B/S 440-460 HAS LIGHT CORROSION AROUND NUT PLATE HOLES.<[01] FWD CARGO L/H Z CHANNEL STA 400-STA 500D WILL BE REPLACED. FOR WORK ACCOMPLISHED REF TASKCARD#TTG8Q00H5X7Q;[02] VERIFIED CORRECT NONROUTINE #

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

FWD CARGO FLOOR SUPPORT 24' LEFT OF CENTER LINE 'Z' CHANNEL AT B/S 500A-500B HAS LIGHT CORROSION AROUND NUT PLATE HOLES.<[01] FWD CARGO L/H Z CHANNEL STA 400-STA 500D WILL BE REPLACED. FOR WORK ACCOMPLISHED REF TASKCARD#TTG8Q00H5X7Q;[02] VERIFIED CORRECT NONROUTINE #

Part: CHANNEL — CORRODED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

FWD CARGO FLOOR SUPPORT 24' LEFT OF CENTER LINE 'Z' CHANNEL AT B/S 460-480 HAS LIGHT CORROSION AROUND NUT PLATE HOLES<[01] FOUND EXFOLIATED CORROSION AND CRACK AT FWD CARGO FLOOR SUPPORT Z CHANNEL LBL 24 PER REF SRM 51-10-02-0G-0;[02] LOCATED AND DRILLED NEW Z-CHANNEL FROM STA 400 TO STA 500D LBL 24 PER REF SRM 51-40-05-0G-0 MATERIAL USED (BAC1496-444 7075-T6) PO:1800018;[03] VERIFIED STEP 1 AND 2 EXFOLIATED CORROSION; LOCATED AND DRILLED. OK TO TREAT AND PRIME NEW Z CHANNEL.;[04] TREATED AND PRIMED NEW FWD CARGO L/H ZEE-CHANNEL STA 400-STA 500D PER REF AMM 51-21-72-370-804 AND AMM 51-21-41-370-802;[05] FOUND EXFOLIATED CORROSION AND CRACK AT FWD CARGO FLOOR SUPPORT Z CHANNEL LBL 24 PER REF SRM 51-10-02-0G-0<BR>LOCATED AND DRILLED NEW Z-CHANNEL FROM STA 400 TO STA 500D LBL 24 PER REF SRM 51-40-05-0G-0 MATERIAL USED (BAC1496-444 7075-T6) PO:1800018<BR>TREATED AND PRIMED NEW FWD CARGO L/H ZEE-CHANNEL STA 400-STA 500D PER REF AMM 51-21-72-370-804 AND AMM 51-21-41-370-802;[06] JOB IS COMPLETE;[07] VERIFIED STEP # 4 TREAT AND PRIME.

Part: CHANNEL — CORRODED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

FWD CARGO FLOOR SUPPORT 24' LEFT OF CENTER LINE 'Z' CHANNEL AT B/S 400-420 HAS LIGHT CORROSION AROUND NUT PLATE HOLES.<[01] FWD CARGO L/H Z CHANNEL STA 400-STA 500D WILL BE REPLACED. FOR WORK ACCOMPLISHED REF TASKCARD#TTG8Q00H5X7Q;[02] VERIFIED CORRECT NONROUTINE #

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

FWD CARGO FLOOR SUPPORT 24' LEFT OF CENTER LINE 'Z' CHANNEL AT B/S 500B-500C HAS LIGHT CORROSION AROUND NUT PLATE HOLES<[01] FWD CARGO L/H Z CHANNEL STA 400-STA 500D WILL BE REPLACED. FOR WORK ACCOMPLISHED REF TASKCARD#TTG8Q00H5X7Q;[02] VERIFIED CORRECT NONROUTINE #

Part: WEDGE — LOOSE (ZN 500 LEFT WING) · airframe 59,300 hrs · 35,194 cycles

LEFT MAIN FLAP O/B T/E AREA COMPOSITE LOWER EDGE SECTION LOOSE DOT 48 EVALAUTED AREA O/B T/E LOWER SKIN SECTION DELAMINATED<[01] PERFORMED VISUAL INPECTION AND TAP TEST AT L\W MAIN FLAP O\B T\E WEDGE ON LOWER SURFACE FOUND DELAMINATION SIZE 30'X9.5' PER B737 NTM 51-05-01;[02] VERIFIED STEP 1;[03] REMOVED LT WING MAIN FLAP O/B T/E WEDGE PER SRM 51-40-02-0G-0.;[04] VERIFIED STEP 3;[05] OK TO INSTALL LT WING MAIN FLAP O/B T/E WEDGE;[06] PARTIALLY INSTALLED SERVICEABLE LT MAIN FLAP O/B T/E WEDGE PER SRM 51-40-02-0G-0.;[07] (FINAL): REMOVED AND REPLACED LEFT MAIN FLAP O/B T/E WEDGE AS PER SRM 51-40-02-0G-0.;[08] VERIFIED STEPS 6 AND 7

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

CABIN FLOOR SUPPORT BETWEEN STA312-328 LBL 45.5 INTERCOSTAL CRACKED<[01] REMOVED CABIN FLOOR SUPPORT BETWEEN STA312-328 LBL 45.5 INTERCOSTAL CRACKED IN REF SRM 51-40-02-0G-0 AND FOUND OUT OF LIMITS IN REF SRM 51-10-02-0G-0;[02] LATE ENTRY :<BR>INSTALLED EWIS PROTECTION AT CABIN FLOOR SUPPORT BETWEEN STA312-328 LBL 45.5 IN REF AMM 20-60-07-913-801;[03] LOCATED AND DRILLED NEW INTERCOSTAL IN REF SRM 51-40-05-0G-0;[04] VERIFIED STEPS:1 AND 2;[05] VERIFIED STEP 3. <BR>OK TO TREAT AND PRIME.;[06] TREATED AND APPLIED PRIMER AT NEW HOLES AT INTERCOSTAL IN REF SRM 51-20-01-0G-0;[07] VERIFIED STEP 6. <BR>OK TO INSTALL NEW INTERCOSTAL.;[08] INSTALLED CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN STA312-328 LBL 45.5 INTERCOSTAL IN REF SRM 51-40-02-0G-0;[09] REMOVED EWIS PROTECTION AT CABIN FLOOR SUPPORT BETWEEN STA312-328 LBL 45.5 IN REF AMM 20-60-07-913-801;[10] REMOVED CABIN FLOOR SUPPORT BETWEEN STA312-328 LBL 45.5 INTERCOSTAL IN REF SRM 51-40-02-0G-0 AND FOUND OUT OF LIMITS IN REF SRM 51-10-02-0G-0; LOCATED AND DRILLED NEW INTERCOSTAL IN REF SRM 51-40-05-0G-0 AND INSTALLED CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN STA312-328 LBL 45.5 INTERCOSTAL IN REF SRM 51-40-02-0G-0;[11] VERIFIED STEPS:8;9 AND 10.

Part: STRUCTURE — CRACKED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

CABIN PASSENGER FLOOR STRUCTURE STA303.9 LEFT WL208 THRESHOLD INNER CORD HAS CRACK<[01] INSTALLED EWIS PROTECTION AT CABIN PASSENGER FLOOR STRUCTURE STA. 303.9 LEFT WL 208 THRESHOLD INNER CORD REF B 737-700 AMM 20-60-07-913-801;[02] REMOVED FASTENERS FOR ACCESS REPAIR AT STA. 303.9 LEFT WL 208 REF B737-700 SRM 51-40-02-0G-0;[03] CUT OUT DAMAGED AREA AT STA. 303.9 LEFT WL 208 CABIN PASSENGER FLOOR STRUCTURE THRESHOLD INNER CORD REF B737-700 SRM 53-10-15-2R-8 FIG.202 SHEET 1;[04] VERIFIED; STEPS # 1 THRU 3.;[05] PERFORMED HFEC ROTO INSP ON FASTENER OPEN HOLES; IAW B 737 NDT PART 6 51-00-00 PROCE 16. TOOL NORTEC 600. BC 172389. CALIB DUE 3-25-23. NO CRACKS FOUND.;[06] PERFORMED HFEC COUNTERSUNK INSP ON FASTENER OPEN HOLES; IAW B 737 NDT PART 6 53-30-00 PROCE 3. TOOL NORTEC 600. BC 172389. CALIB DUE 3-25-23. NO CRACKS FOUND.;[07] PERFORMED HFEC INSP ON CUTOUT AREA; IAW B 737 NDT PART 6 51-00-00 PROCE 23. TOOL NORTEC 600. BC 172389. CALIB DUE 3-25-23. NO CRACKS FOUND.;[08] TRIMMED 0.040' INSURANCE CUT ALONG THE EDGE OF THE TRIM REF. B737-700 SRM 53-10-15-2R-8 REPAIR 8;[09] FABRICATED (2) ANGLES REPAIRS 7075-0 0.063' REF B737-700 SRM 53-10-15-2R-8;[10] VERIFIED STEPS 8 AND 9;[11] CLEANED AND REMOVED EWIS PROTECTION AT LI DOOR CUT OUT STA 303.9 PER AMM 20-60-07-913-801;[12] INNER CORD WIIL BE REPLACE ON TTG8Q00H8411;[13] VERIFIED STEP 11 AND 12<BR><BR>COMPLETE REPLCE WILL BE PERFORM ON TTG8Q00H8411

Part: PANEL — CRACKED (ZN 500 LEFT WING) · airframe 59,300 hrs · 35,194 cycles

L/H WING FUEL ACCESS PANEL 532RB PLATE LOWER SURFACE CRACKED. (18-093)<[01] RECEIVED L/H WING NEW FUEL ACCESS PANEL #532RB WILL BE INSTALLED T/C TTG8Q00GDEB6;[02] VERIFIED STEP 1.

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

CABIN FLOOR SUPPORT INTERCOSTAL IS CRACKED BETWEEN 328-344 47' LEFT OF CENTER LINE<[01] REMOVED DAMAGED CABIN FLOOR SUPPORT INTERCOSTAL PER REF 51-40-02-0G-0.;[02] INSTALLED EWIS PROTECTION AT FWD CABIN STA 328-344 47' LEFT OF CENTER LINE PER REF AMM 20-60-07-913-801.;[03] VERIFIED STEPS 1 AND 2;[04] OK TO LOCATE AND DRILL HOLES;[05] LOCATED AND DRILLED NEW INTERCOSTAL PER REF SRM 51-40-05-0G-0;[06] VERIFIED STEP 5;[07] OK TO TREAT AND PRIME HOLES;[08] TREATED AND PRIMED PER REF AMM 51-21-41-370-803;[09] VERIFIED STEP 8;[10] OK TO INSTALL INTERCOSTAL;[11] INSTALLED NEW INTERCOSTAL PER REF SRM 51-40-02-0G-0 AND DWG 141A5400;[12] REMOVED AND REPLACED NEW INTERCOSTAL AT MAIN CABIN STA 328-344 47'LEFT OF CENTER LINE PER REF SRM 51-40-02-0G-0 AND DWG 141A5400.;[13] VERIFIED STEPS 11 AND 12

Part: STRIP — ELONGATED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

AFT CARGO R/H FLOORS CAP STRIPS; HOLES ELONGATED<[01] RECEIVED NEW AFT CARGO R/H FLOORS CAP STRIPS; P/ 453A2611-11; -13;-9 AND- 1; NEW CAP STRIPS TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004G38U;[02] VERIFIED STEP 1

Part: STRIP — ELONGATED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

L/H AFT CARGO FLOORS CAP STRIPS WITH HOLES ELONGATED<[01] RECEIVED NEW AFT CARGO.; L/H FLOORS CAP STRIPS; P/N 453A2611-8;-10;-13; AND-2; NEW CAP STRIPS TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q004G38U;[02] VERIFIED STEP 1

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

FWD CABIN FLOOR SUPPORT INTERCOSTAL IS CRACKED BETWEEN 344-360 AT CENTER LINE<[01] REMOVED FWD CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN 344-360 AT CENTER LINE IN REF SRM 51-40-02-0G-0; FOUND OUT OF LIMITS IN REF SRM 51-10-02-0G-0;[02] LATE ENTRY :<BR>INSTALLED EWIS PROTECTION AT FWD CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN 344-360 AT CENTER LINE IN REF AMM 20-60-07-913-801;[03] VERIFIED STEPS:1 AND 2.;[04] LOCATED AND DRILLED NEW INTERCOSTAL AT FWD CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN 344-360 AT CENTER LINE IN REF SRM 51-40-05-0G-0;[05] VERIFIED STEP 4. <BR>OK TO TREAT AND PRIME;[06] TREATED AND APPLIED PRIMER AT NEW HOLES AT INTERCOSTAL IN REF SRM 51-20-01-0G-0;[07] VERIFIED STEP 6. <BR>OK TO INSTALL NEW INTERCOSTAL.;[08] INSTALLED FWD CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN 344-360 AT CENTER LINE IN REF SRM 51-40-02-0G-0;;[09] REMOVED EWIS PROTECTION AT FWD CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN 344-360 AT CENTER LINE IN REF AMM 20-60-07-913-801;[10] REMOVED FWD CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN 344-360 AT CENTER LINE IN REF SRM 51-40-02-0G-0; FOUND OUT OF LIMITS IN REF SRM 51-10-02-0G-0; LOCATED AND DRILLED NEW INTERCOSTAL AT FWD CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN 344-360 AT CENTER LINE IN REF SRM 51-40-05-0G-0 AND INSTALLED FWD CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN 344-360 AT CENTER LINE IN REF SRM 51-40-02-0G-0;;[11] VERIFIED STEPS:8;9 AND 10.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

CABIN FLOOR SUPPORT BETWEEN 294.5 - 312 10 INCHES LEFT OF CENTER LINE IS CORRODED<[01] INSTALLED EWIS PROTECTION AT CABIN FLOOR SUPPORT BETWEEN 294.5 - 312 10 INCHES LEFT OF CENTER LINE IN REF AMM 20-60-07-913-801;[18] VERIFIED STEPS 16 AND 17;[19] REMOVED AND REPLACED INTERCOSTAL AT CABIN FLOOR SUPPORT BETWEEN STA. 294.5 TO 312 LBL 10' REF. B737-700 DWG #141A5600 SRM 51-40-02-0G-0;[20] VERIFIED STEP 19

Part: BRACKET — CRACKED (ZN 500 LEFT WING) · airframe 59,300 hrs · 35,194 cycles

LEFT WING T/E BY DEFLECTOR PANEL SUPPORT BRACKET CRACKED DOT 39<[01] REMOVED SUPPORT BRACKET AT L/W T/E BY DEFLECTOR IN REF 51-40-02-0G-0;[02] LOCATED AND DRILLED SUPPORT BRACKET AT R/W T/E BY DEFLECTOR IN REF SRM 51-40-05-0G-0;[03] CORRECTION TO STEP #2:<BR>LOCATED AND DRILLED NEW SUPPORT BRACKET AT R/W T/E BY DEFLECTOR IN REF SRM 51-40-05-0G-0.;[04] VERIFIED STEPS 1; 2 AND 3. OK TO INSTALL NEW SUPPORT BRACKET.;[05] INSTALLED NEW SUPPORT BRACKET AT L/W T/E BY DEFLECTOR PANEL IN REF SRM 51-40-02-0G-0;[06] VERIFIED STEP 5.

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

CABIN FLOOR SUPPORT INTERCOSTAL IS CRACKED BETWEEN 288-294.5 ON CENTER LINE<[01] REMOVED INTERCOSTAL CRACKED AT MAIN CABIN STA 288 TO STA 294.5 BL 0 PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] OK TO LOCATE AND DRILL HOLES;[04] LOCATE AND DRILLED NEW INTERCOSTAL AT MAIN CABIN STA 288 TO STA 294.5 BL 0 PER REF. SRM 51-40-05-0G-0;[05] VERIFIED STEP 4;[06] OK TO TREAT AND PRIME HOLES;[07] TREATED AND PRIMED PER REF SRM 51-20-01-0G-0;[08] VERIFIED STEP 7;[09] OK TO INSTALL INTERCOSTAL;[10] INSTALLED NEW INTERCOSTAL SAT 288-294.5 ON CENTER LINE PER REF SRM 51-40-02-0G-2;[11] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN FLOOR SUPPORT BETWEEN STA 288-294.5 BL 0 PER SRM 51-40-02-0G-0 AND DWG 141A5400;[12] FOD AND EWIS PROTECTION WAS INSTALL AND WILL REMOVE ON TTG8Q00H2GL3;[13] VERIFIED STEPS 11 AND 12;[14] VERIFIED STEP 10

Part: BEAM — CORRODED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

FLOOR BEAM 986.5 IS CORRODED ON TOP CAP 6 INCHES INBOARD OF R-2 DOOR SILL<[01] FOUND EXFOLIATE CORROSION AROUND FASTENER HOLE; OUT OF LIMITS PER SRM;53-70-51-1A-1;[02] REMOVED INTERCOSTAL BETWEEN STA. 986.5 AND STA. 1006 AND RBL 38; AND ATTACH ANGLES; PER REF SRM 51-40-02-0G-0[12] LOCATED AND DRILLED; NEW T CHORD P/N 53100011-002 PO# 1792296 REF. EA NO. 13-01967;[13] CORRECTION STEP 12; ENTER IN ERROR.;[14] AFT CABIN FLOOR BEAM 986.5 REPAIR AREA; FOUND HOLES STANDARD SIZE AND DRILLED TO THE NEXT OVERSIZE AS PER SRM 51-40-05-0G-0 AND SRM 53-70-51-2R-4 REPAIR 4.;[15] AFT CABIN FLOOR BEAM 986.5 REPAIR AREA; FOUND ANGLE @ STA 967 & STA 986 WITH NO DISCREPANCIES NOTED AND DOES NOT INTERFERE WITH THE REPAIR AS PER SRM 53-70-51-2R-4 REPAIR 4;[30] INSTALLED REPLACEMENT REPAIR PARTS ON FLOOR BEAM STA 986.5 FROM RBL 27 TO RBL 52 PER RE EA 1-753-22432 REV - AND ATS ER 13-01967;[31] APPLIED FILLET SEAL ON REPAIR AND INTERNAL GAPS; PER REF SRM 51-20-05-0G-0 AND APPLIED PRIMER TO THE FASTENERS HEADS PER REF SOPM 20-41-02;[32] VERIFIED STEP 30 AND 31 INSTALLATION OF REPAIR PARTS; SEALANT AND PRIMER APPLICATION.

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

FWD CABIN FLOOR SUPPORT INTERCOSTAL IS CRACKED BETWEEN 344-360 12 INCHES LEFT OF CENTER LINE<[01] PLACED EWIS PROTECTION FROM STA 344-360.12 PER REF AMM 20-60-07-913-801;[02] REMOVED FOR ACCESS INTERCOSTAL STA 344-360 BL 0 PER REF SRM 51-40-02-0G-0;[03] REMOVED FWD MAIN CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN 344- 360 RBL 11.1 PER REF SRM 51-40-02-0G-0;[04] VERIFIED STEPS 1; 2 AND 3;[05] LOCATED AND DRILLED NEW INTERCOSTAL PER SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0.;[06] VERIFIED STEP 5;[07] OK TO TREAT AND PRIME DRILLED AREA.;[08] TREATED AND PRIMED DRILLED AREA PER AMM 51-21-41-370-803 AND AMM 51-21-72-370-804.;[09] VERIFIED STEP # 8;[10] OK TO INSTALL NEW INTERCOSTAL.;[11] INSTALLED NEW INTERCOSTAL AT MAIN CABIN FLOOR SUPPPORT BETTWEEN STA 344 TO 360 LBL 11 PER SRM 51-40-02-0G-0 AND DWG 141A5400;[12] VERIFIED STEP # 11 INTERCOSTAL INSTALLATION.;[13] OK TO REINSTALL INTERCOSTALL REMOVED ON STEP 2;[14] REINSTALLED INTERCOSTAL BETWEEN STA 344-360 BL 0 PER SRM 51-40-02-0G-0 AND DWG 141A5400;[15] VERIFIED STEP 14;[16] REMOVED PROTECTION OF THE EWIS AT FWD CABIN STA 344- 360 12 INCHES PER REF AMM 20-60-07-913-801.;[17] VERIFIED STEP 16;[18] REMOVED AND REPLACED NEW INTERCOSTAL AT FWD CABIN STA 344-360 LBL 11 PER REF SRM 51-40-02-0G-0 AND DWG 141A5400.;[19] VERIFIED STEP 18

Part: FLOOR PANEL — PEELING (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

AFT CABIN FLOOR PANEL 241UF UPPER SKIN SURFACE PEELING. (18-043)<[01] PREPARED FLOOR PANEL #241UF AT DAMAGED AREA FOR REPAIR PER B737 SRM 53-00-50-2R-1;[02] VERIFIED STEP # 1;[03] OK TO INSTALL REPAIR.;[04] REPAIRED FLOOR PANEL #241UF AT DAMAGED AREA PER B737 SRM 53-00-50-2R-1. MATERIALS USED RESIN P/O#1778544; CLOTH P/O#1690463;[05] VERIFIED STEP 4;[06] TASK C/W

Part: FLOOR PANEL — PEELING (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

AFT CABIN FLOOR PANEL 241WF UPPER SKIN SURFACE PEELING. (18-041)<[01] REPAIRED DISCREPANCY ON MAIN CABIN FLOOR PANEL 241WF ON NON ROUTINE #8706529 COPY ATTACHED;[02] CORRECTION STEP 1 REPAIRED DISCREPANCY ON MAIN CABIN FLOOR PANEL 241WF ON CUSTOMER BAR CODE TTG8Q00H2540;[03] REPAIRED DISCREPANCY ON MAIN CABIN FLOOR PANEL 241WF ON CUSTOMER BAR CODE TTG8Q00H2540

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

AFT CABIN FLOOR PANEL 241WF CRACKED AROUND FASTENER HOLE. (18-042)<[01] REPAIRED DISCREPANCY ON MAIN CABIN FLOOR PANEL 241WF ON NON ROUTINE #8706529 COPY ATTACHED;[02] CORRECTION STEP 1 REPAIRED DISCREPANCY ON MAIN CABIN FLOOR PANEL 241WF ON CUSTOMER BAR CODE TTG8Q00H2540;[03] REPAIRED DISCREPANCY ON MAIN CABIN FLOOR PANEL 241WF ON CUSTOMER BAR CODE TTG8Q00H2540

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

FWD CARGO CO MPARTMENT PANEL 121YBC CRACKED<[01] RECEIVED NEW FWD CARGO COMPARTMENT CEILING. SHROUD PANEL P/N 221-11048-1A; NEW PANEL TO BE INSTALLED ON CUSTOMER BAR CODE TTG8Q00GDE6Z.;[02] VERIFIED STEP 1.

Part: FLOOR PANEL — PEELING (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

AFT CABIN FLOOR 242QF UPPER SKIN SURFACE PEELING.(18-046)<[01] REPAIRED DAMAGED AREA AS MARKED ON TOP SURFACE OF MAIN CABIN FLOOR PANEL #242QF AS PER B737 SRM 51-70-04-2R-1 MATERIAL USED PO#1778544 PO#1690463;[02] VERIFIED STEP 1.

Part: FLOOR PANEL — PEELING (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

AFT CABIN FLOOR PANEL 241WF UPPER SKIN SURFACE PEELING. (18-041)<[01] MEASUREMENTS;[02] REPAIRED ALL DAMAGES AS MARKED ON TOP SURFACE OF MAIN CABIN FLOOR PANEL 241WF AS PER B737 SRM 51-70-04-2R-1. MATERIALS USED PO#1800218 AND PO#1690463;[03] PERFORMED TAP TEST ON REPAIRED AREAS. FOUND NO DELAMINATION AS PER B737 SRM 51-05-01 SECTION 5;[04] VERIFIED STEPS 1 - 3.

Part: FITTING — CRACKED (ZN 600 RIGHT WIN) · airframe 59,300 hrs · 35,194 cycles

R/W REAR SPAR T/E DEFLECTION CONTROL RIB PANEL VERTICAL BULB SEAL FITTING CRACKED INB MKD DOT<[01] REMOVED BUILD SEAL FITTING AT R/W REAR SPAR T/E DEFLECTION CONTROL IN REF SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED HOLES AT BULB SEAL FITTING R/W REAR SPAR T/E DEFLECTION CONTROL RIB PANEL VERTICAL IN REF SRM 51-40-05 0G-0;[03] VERIFIED STEPS #1 AND #3.<BR> OK TO TREAT AND PRIME DRILLED HOLES.;[04] APPLIED TREATED PRIME HOLES AT BULB SEAL FITTING IN REF AMM 51-21-72-370-804;[05] VERIFIED STEP #4. <BR> OK TO INSTALL NEW REPLACEMENT FITTING.;[06] INSTALLED BULB SEAL FITTING AT R/W REAR SPAR T/E DEFLECTION CONTROL RID PANEL VERTICAL IN REF SRM 51-40-02-0G-0;[07] REMOVED AND REPLACE BULB SEAL FITTING AT T/E DEFLECTION CONTRO RIB PANEL PER SRM 51-40-02-0G-0;[08] VERIFIED STEPS 6 AND 7.

Part: WEB — CRACKED (ZN 300 STABILIZE) · airframe 59,300 hrs · 35,194 cycles

CRACK ON HORIZONTAL PRESSURE DECK WEB AT STA 663; RBL 42; LENGTH 0.500'. CRACK ON HORIONTAL PRESSURE DECK WEB AT STA 663 RBL 42 LENGTH 0.500&#34;<[01] FOR ACCESS TO PRESSURE DECK WEB REPAIR; INSTALLED EWIS PROTECTION TO ADJACENT AREA AT STA 663.75 AND STA 675 FROM RBL 38 TO RBL 60 REF. 737-AMM 20-60-07-913-801;[02] FOR ACCESS TO PRESSURE DECK WEB REPAIR; REMOVE FASTENERS FROM STA 663.75 AND STA 675 FROM RBL 30 TO RBL 60; REMOVE RETAINER; PLATE; ANGLES AND SUPPORT FLOOR REF.737-SRM 53-40-51-2R-2;12] LATE ENTRY; WERE FABRICATED THE REPAIR PARTS AT RBL 38 TO RBL 60 BETWEEN STA 663.75 STA 675 REF. SRM 51-30-01;[13] LATE ENTRY; FABRICATED THE REPAIR PARTS AT RBL 38 TO RBL 60 BETWEEN STA 663.75 STA 675 REF. SRM 53-40-51-2R-2 REPAIR 2 PAR.4 LETTER E;[14] VERIFIED STEPS:10;11;12 AND 13. FABRICATED AND INSTALLED REPAIR PARTS AT HORIZONTAL PRESSURE DECK WEB LOCATED ON STA 663 RBL 42 PER SRM 53-40-51-2R-2.;[36] VERIFIED STEP 35

Part: BRACKET — CRACKED (ZN 500 LEFT WING) · airframe 59,300 hrs · 35,194 cycles

L/H WING L/E #1 SLAT I/B AUXILIARY TRACK LOWER I/B BRACKET CRACKED. (18-006)<[01] REMOVER BRACKET AT L/H WING L/E #1 SLAT I/B AUXILIARY TRACK LOWER I/B PER REF SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1;[03] OK TO INSTALL NEW BRACKET.;[04] REPLACED L/H WING L/E #1 SLAT I/B AUXILIARY TRACK LOWER I/B BRACKET AS PER SRM 51-40-02-0G-0;[05] VERIFIED STEP 4 INSTALLATION OF BRACKET.

Part: FLOOR PANEL — PEELING (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

CABIN FLOOR PANEL 241DF TOP SURFACE SEVERAL AREAS COMPOSITE PEELING<[01] REPAIRED DAMAGED AREA AT UPPER SURFACE ON ACCESS FLOOR PANEL 241 DF. REF B737 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3. MATERIAL USED GLASS FABRIC PLIES PO#: 1690463 AND RESIN PO#: 1778544.;[02] VERIFIED STEP # 1;[03] VERIFIED STEP # 1; REPAIR IS COMPLETE.

Part: FLAP — CRACKED (ZN 500 LEFT WING) · airframe 59,300 hrs · 35,194 cycles

L/W KRUEGER FLAP NO-1 O/B HINGE # 2 RIB FITTING CRACKED @ LOWER L/E MKD DOT<[01] REMOVED L/E FLAP #1 IN REF. AMM 27-81-11-000-801;[02] L/E FLAP #1 P/N 114A1110-7 S/N ASTA-246;[03] VERIFIED STEPS 1 AND 2 REMOVAL OF FLAP AND P/N; S/N.;[04] OK TO INSTALL KRUEGER FLAP;[05] LATE ENTRY: <BR>PARTIALLY RE-INSTALLED REPLACEMENT L/W KRUEGER FLAP #1 PER AMM 27-81-11-400-801 UP TO AND INCLUDING STEP H. (2) (C). PENDING HARDWARE REPLACEMENT AND TORQUE.;[06] VERIFIED STEP 5;[07] ACCOMPLISHED TORQUE OF HINGES 1 & 4 (B/C 164345. DUE 10/28/23); HINGES 2 & 3 (B/C 175290. DUE 3/10/23) PER REF. B737 AMM 27-81-11-400-801. BONDING METER B/C 160450. DUE 12/06/23;[08] VERIFIED STEP 7;[09] FINALIZED INSTALLATION OF L/W KRUEGER FLAP #1 REF B737 AMM 27-81-11-400-801. PERFORMED OPS CHECKS. CHECKS GOOD;[10] REMOVED AND REPLACED L/W KRUEGER FLAP #1 REF B737 AMM 27-81-11-000-801 (REMOVAL) AND AMM 27-81-11-400-801 (INSTALLATION). PERFORMED ADJUSTMENTS AND OPS CHECK. CHECK GOOD;[11] VERIFIED STEPS 9 AND 10

Part: FLOOR PANEL — DELAMINATED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

CABIN FLOOR PANEL 242CF LEFT FWD CORNER INTERNAL AREA COMPOSITE PANEL DELAMINATED<[01] REMOVED DELAMINATED FACESHEET PLIES AND PREPARED DAMAGED AREA TO APPLY THE GLASS FABRIC REPAIR PLIES; NO WATER NOTE ON REPAIR AREA; AT ACCESS FLOOR PANEL 242CF. REF B737 SRM 53-00-50-2R-9 PARAGRAPH 5.;[02] VERIFIED STEP 1<BR>OK TO APPLY REPAIR;[03] APPLIED THE GLASS FABRIC REPAIR AT DAMAGED AREA ON ACCESS FLOOR PANEL 242CF. REF B737 SRM 53-00-50-2R-9 PARAGRAPH 5. MATERIAL USED GLASS FABRIC PLIES PO#:1690463 AND RESIN PO#:1778544;[04] VERIFIED STEP 3;[05] STEP 2 IS RII

Part: SPAR — CRACKED (ZN 600 RIGHT WIN) · airframe 59,300 hrs · 35,194 cycles

R/W FRONT SPAR INFERNAL UPPER CHORD FWD TIE-DOWN CLIP CRACKED ABOVE ACCESS PANEL621EB DEFUELING STATION MKD DOT<[01] REMOVED ACCESS PANEL # 621FB GAINED ACCESS TO REPAIR REF B 737-700 SRM 51-40-01;[02] PARTIAL REMOVED FASTENERS AT R/W UPPER CHORD FWD TIE DOWN ABOVE ACCESS PANEL 621EB REF B737-700 SRM 57-40-01;[03] REMOVED NOSE BEAM F/P AT R/W T/E SS 150.81 AND SS 48.97 IN REF SRM 51-40-02-0G-0;[04] LOCATED AND DRILED NEW NOSE BEAM P/N 116A5640Y18 REF. B737-700 SRM 51-40-05-0G-0;[13] PARTIALLY INSTALLED FASTENERS. 70% AT NOSE BEAM R/W FRONT SPAR ABOVE ACCESS PANEL 621 REF. B737-700SRM 51-40-02-0G-0;[14] COMPLETED INSTALLATION OF NOSE BEAM R/W FRONT SPAR ABOVE ACCESS PANEL 621EB 100% FASTENERS INSTALLED PER REF 51-40-02-0G-0 AND DWG 116A5640.;[21] (FINAL) REMOVED ACCESS PANEL # 621FB TO GAIN ACCESS TO NOSE BEAM REPLACEMENT; LOCATED; DRILLED; TREATED; PRIMED AND TOPCOAT NEW NOSE BEAM (P/N 116A5640Y18). INSTALLED NEW NOSE BEAM AND APPLIED CIC AND INSTALLED ACCESS PANEL # 621FB.;[22] VERIFIED STEPS 20 AND 21

Part: PANEL — CRACKED (ZN 800 DOOR) · airframe 59,300 hrs · 35,194 cycles

FWD GALLEY SERVICE DOOR FWD (SURROUND STRUCTURE) PANEL CRACKED BEHIND ELECTRIC OUTLET<[01] PAINTED FWD GALLEY SERVICE DOOR FWD SURROUND STRUCTURE PANEL BEHIND OUTLET ASPER B737-700 AMM 25-00-00-370-801;[02] PAINTED AND REPAIRED FWD GALLEY SERVICE DOOR FWD SURROUND STRUCTURE PANEL BEHIND OUTLET ASPER B737-700 AMM 25-00-00-370-801 -25-00-00-300-802;[03] VERIFIED STEPS 1 AND 2.

Part: PANEL — ELONGATED (ZN 600 RIGHT WIN) · airframe 59,300 hrs · 35,194 cycles

ACCESS PANEL 651ET COMPSITE AREA HAS ENLOGATED HOLES<[01] PREPARED FOR REPAIR PANEL651 ET; AS PER B737 SRM. 51-70-06-2R-7;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED PANEL 651ET; AS PER B737 SRM 51-70-06-2R-7 MATERIAL USED PO.1800218 AND PO.1690463;[04] VERIFIED STEP 3. OK TO APPLY TOP COAT.;[05] PREPARED AND APPLIED TOPCOAT AT ACCESS PANEL 651ET IN REFERENCE WITH B737-700 AMM 51-21-73-370-803.;[06] VERIFIED AND INSPECTED STEP #5.

Part: COWLING — PULLED (ZN 400 NACELLE/P) · airframe 59,300 hrs · 35,194 cycles

RH INLET COWL OUTER LIP SKIN AT 5 O'CLOCK TO 7 O'CLOCK HAS SEVERAL FASTENERS PULLED IN (14 EA)<[01] #2 ENG INLET COWL TO BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1

Part: COWLING — PULLED (ZN 400 NACELLE/P) · airframe 59,300 hrs · 35,194 cycles

RH INLET COWL OUTER LIP SKIN AT 2 O'CLOCK HAS THREE FASTENERS PULLED IN.<[01] #2 ENG INLET COWL TO BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1

Part: COWLING — PULLED (ZN 400 NACELLE/P) · airframe 59,300 hrs · 35,194 cycles

RH INLET COWL OUTER LIP SKIN AT 11 O'CLOCK HAS TWO FASTENERS PULLED IN.<[01] #2 ENG INLET COWL TO BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1

Part: COWLING — PULLED (ZN 100 FUS LOWER) · airframe 59,300 hrs · 35,194 cycles

RH INLET COWL OUTER LIP SKIN AT 4 O'CLOCK HAS TWO FASTENERS PULLED IN.<[01] #2 ENG INLET COWL WILL BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1

Part: HANDLE — LOOSE · airframe 58,566 hrs · 34,715 cycles

FWD GALLEY SERVICE DOOR HANDLE LOOSE / [01] RESECURED FWD SERVICE DOOR HANDLE IAW AMM 20-50-11

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 58,481 hrs · 34,667 cycles

DOT A-24-5 CENTER CABIN FLOOR BOARD PANEL 231XF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE. / [01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. FABRIC (A10269); RESIN (A141867).<BR><BR>REQUESTING OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 150 DEGREES (OVEN B0-06 EXP 11-8-22). TAP TEST GOOD.;[04] REPAIRED CENTER CABIN FLOOR BOARD PANEL 231XF UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3-4

Part: NONE — PULLED (FUSELAGE) · airframe 58,481 hrs · 34,667 cycles

DOT A-24-3 CENTER CABIN FLOOR BOARD PANEL 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE. / [01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE LENGTH OF BOARD. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. RESIN (A141927); POTTING COMPOUND (E125915); FABRIC (A10269).<BR><BR>REQUEST OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 250 DEGREES (OVEN B0-06 EXP 11-8-22). TAP TEST GOOD.;[04] REPAIRED CENTER CABIN FLOOR BOARD PANEL 242AF UPPER SURFACE ALONG LENGTH OF BOARD IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEP 3-4

Part: PANEL — PULLED (FUSELAGE) · airframe 58,481 hrs · 34,667 cycles

DOT A-24-7 CENTER CABIN FLOOR BOARD PANEL 232RF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE. / [01] EVALUATED AND FOUND MULTIPLE AREAS OF PULLED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3A;C;E;F<BR>VERIFIED REPAIR MATERIALS AS GLASS--(A10269); RESIN--(A141927) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEPS 3K;L;M. TAP TEST GOOD. OVEN B0-06 DUE 11-8-22;[04] REPAIRED DAMAGE TO UPPER SURFACE OF FLOOR BOARD IAW SRM 53-0-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 58,481 hrs · 34,667 cycles

DOT A-24-4 CENTER CABIN FLOOR BOARD PANEL 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE. / [01] EVALUATED DAMAGE; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD; NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A; B; C; E; F; AND J. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201 RESIN EPOCAST 50A; (A141867); FIBERGLASS CLOTH BMS 9-3 (A10269). <BR><BR>REQUIRES OKAY TO BOND REPAIR PLIES.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS K; L; M; AND N. OVEN B0-06 CAL DUE 11/8/22. TAP TEST GOOD.;[04] REPAIRED CENTER CABIN FLOOR BOARD PANEL 241AF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 REPAIR 1.;[05] VERIFIED STEPS 3-4

Part: FLOOR PANEL — PULLED (FUSELAGE) · airframe 58,481 hrs · 34,667 cycles

DOT A-24-6 CENTER CABIN FLOOR BOARD PANEL 241BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE. / [01] EVALUATED PANEL 241BF AND FOUND PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3A;C;E&F.VERIFIED MATERIALS AS: BMS 8-201(A141867); BMS 9-3(A10269). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201.NEED OK TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES. IAW B737-700 SRM 53-0050-2R-1 PAR 3K-M. AAR OVEN BO-06 150DEG.;[04] REPAIRED DAMAGED PLIES ON UPPER SURFACE ON PANEL 241BF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4

Part: PANEL — PULLED (FUSELAGE) · airframe 58,481 hrs · 34,667 cycles

DOT A-24-8 CENTER CABIN FLOOR BOARD PANEL 231YF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE. / [01] EVALUATED AND FOUND MULTIPLE AREAS OF PULLED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3A;C;E;F<BR>VERIFIED REPAIR MATERIALS AS GLASS--(A10269); RESIN--(A141927) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEPS 3K;L;M. TAP TEST GOOD. OVEN B0-06 DUE 11-8-22;[04] REPAIRED DAMAGE TO UPPER SURFACE OF FLOOR BOARD IAW SRM 53-0-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD;[05] VERIFIED STEPS 3-4

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,377 hrs · 33,902 cycles

AFT ENTRY DOOR EXTERNAL EMERGENCY LIGHT INOP / [01] RELAMPED AFT ENTRY EXTERIOR EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,067 hrs · 33,716 cycles

SKIN CORROSION AT STA 847 STRINGER 25L SKIN CORROSION AT STA 847 STRINGER 25 LEFT / [01] REMOVED CORROSION PER EA 22-153-00959-WIP1;[02] CORRECTED POTENTIAL CORROSION LEVEL ()

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,067 hrs · 33,716 cycles

SKIN CORROSION AT STATION 867 STRINGER 25LEFT SKIN CORROSION STATION 867 STRINGER 25 LEFT / [01] REMOVED CORROSION PER EA 22-153-00959-WIP1;[02] REMOVED CORROSION PER EA 22-153-00959-WIP1;[03] CORRECTED POTENTIAL CORROSION LEVEL ()

Part: DUMP VALVE — CORRODED (FUSELAGE) · airframe 57,067 hrs · 33,716 cycles

CORROSION ON AFT LAV DUMP VALVE PAN ASSY / [01] REMOVED & REPLACED AFT LAV DUMP VALVE PAN ASSY REF SRM 51-40-02;[02] CORRECTED POTENTIAL CORROSION LEVEL ();[03] REPAIR ACCOMPLISHED ON EA-153-00959-W1P1.;[04] COMPLIED WITH;[05] REPAIR WAS COMPLETED IAW EA 22-153-00959-WIP1;[06] REPAIR WAS COMPLETED IAW EA 22-153-00959-WIP1;[07] C/W;[08] REPAIR WAS COMPLETED IAW EA 22-153-00959-WIP1

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,067 hrs · 33,716 cycles

EVIDENCE OF CORROSION AT LAV DUMP VALVE PAN EXTERIOR DOOR FRAME. / [01] CORRECTED POTENTIAL CORROSION LEVEL ();[02] REPAIR ACCOMPLISHED ON EA-153-0095-W1P1.;[03] REPAIR WAS COMPLETED IAW EA 22-153-00959-WIP1;[04] REPAIR WAS COMPLETED IAW EA 22-153-00959-WIP1;[05] REPAIR WAS COMPLETED IAW EA 22-153-00959-WIP1;[06] C/W

Part: LIGHT — INOPERATIVE · airframe 56,975 hrs · 33,659 cycles

RT O/W EXIT SIDEWALL LT INOP / [01] OK TO CONTINUE PER MEL33-2-03 SP1B. AUTH53950;[02] RELAMPED RT OVERWIND EXIT SIDEWALL LIGHT PER AMM 33-21-00. OPS CHECK GOOD. REF LP 1844922

Part: SLIDE — DISLODGED (L2 DOOR) · airframe 56,848 hrs · 33,584 cycles

AFT ENTRY DOOR SLIDE COVER BECAME DISLODGED / [01] RE-SECURED AFT ENTRY DOOR SLIDE PER AMM 25-66-01. OPS CHECK GOOD.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 56,848 hrs · 33,584 cycles

AFT ENTRY DOOR SLIDE LOOSE / [01] PER MOC <BR>REPACKED AFT ENTRY DOOR SLIDE PER MM 25-66-01 OPS CHECK GOOD

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 55,317 hrs · 32,659 cycles

LT WING O/B AFT FLAP IS DELAMINATES ON THE I/B LOWER CORNER. ; / [01] REMOVED AND REINSTALLED LT WING O/B AFT FLAP IAW AMM 27-51-22-000-801 AND AMM 27-51-22-400-801 ADJUSTMENT AND OPERATIONAL CHECK IS GOOD; [02] INSPECTED OUTBOARD AFT FLAP INSTALLATION<BR>INSTALLATION AND ADJUSTMENT/OPS CHECK GOOD.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 54,166 hrs · 31,994 cycles

OVER WING EMERGENCY EXIT LIGHT REMAIN ILLUMINATED WHEN SWITCH IN ARMED POSITION / FOUND LEFT HAND EMERGENCY EXIT POWER SUPPLY POPPING BREAKER; R&R'D M1668 POWER SUPPLY AND BATTERY PACK PER MM 33-51-06. OPS CHECK GOOD.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHT) · airframe 54,166 hrs · 31,994 cycles

OVER WING EMERGENCY EXIT LIGHT REMAIN ILLUMINATED WHEN SWITCH IN ARMED POSITION / FOUND LEFT HAND EMERGENCY EXIT POWER SUPPLY POPPING BREAKER; R&R'D M1668 POWER SUPPLY AND BATTERY PACK PER MM 33-51-06. OPS CHECK GOOD.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 54,023 hrs · 31,914 cycles

WHEN GIVING OK TO CLOSE FOUND CRACKED BULKHEAD SUPPORT ATTACH ANGLE AT AFT CARGO BAY BS947 LBL11 WL 179. REMOVED AND REPLACED BULKHEAD SUPPORT ATTACH ANGLE AT ACB BS 947 LBL 11 WL179 IAW SRM 51-40-02-OG-0 AND DWG #149A8103 84632U 12MAR21

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,023 hrs · 31,914 cycles

EMERGENCY EXIT LIGHT L1358 AFT OF R/H OWE (INSIDE CABIN) HAS BULBS INOP. / RELAMPED EMERGENCY EXIT LIGHT L1358 AFT OF R/H OWE (INSIDE CABIN) AND PERFORMED GOOD FUNCTIONAL TEST IAW AMM 33-51-01-960-801 STEPS 2.B.(1)(A)4);(C);(2) AND (4).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,023 hrs · 31,914 cycles

EMERGENCY EXIT LIGHTS (2 EACH) L751 ABOVE R/H OWE ARE INOP. / RE-LAMPED EMERGENCY EXIT LIGHTS L751 ABOVE R/H OWE AND PERFORMED GOOD FUNCTIONAL TEST IAW AMM 33-51-01-960-801 STEP 2.B.(1)(A)(3); (C); (2) AND (4).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,023 hrs · 31,914 cycles

EMERGENCY EXIT LIGHT L1190 AFT OF AFT ENTRY DOOR (INSIDE CABIN) HAS BULBS INOP. / RE-LAMPED EMERGENCY EXIT LIGHT L1190 AFT OF AFT ENTRY DOOR (INSIDE CABIN) AND PERFORMED GOOD FUNCTIONAL TEST IAW AMM 33-51-01-960-801 STEPS 2.B.(1)(A)4);(C);(2) AND (4).

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,023 hrs · 31,914 cycles

EMERGENCY EXIT LIGHT L1189 FORWARD OF L/H OWE (INSIDE CABIN) HAS BULBS INOP. / RELAMPED EMERGENCY EXIT LIGHT L1189 FORWARD OF L/H OWE (INSIDE CABIN) AND PERFORMED GOOD FUNCTIONAL TEST IAW AMM 33-51-01-960-801 STEPS 2.B.(1)(A)4); (C);(2) AND (4).

Part: GUSSET — CRACKED (FWD CARGO) · airframe 54,023 hrs · 31,914 cycles

FORWARD CARGO BAY GUSSET IS CRACKED AT BS540 S-19L WL 190 / REMOVED AND REPLACED FWD CARGO BAY GUSSET AT BS 540 STR. 19L. WL. 190. I.A.W SRM 51-40-02-0G-0 AND DRAWING # 143A7902. GUSSET WAS EVALUATED AND FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE LIMITS FOUND ON SRM FOR CRACK I.A.W SRM 53-30-08-1A-1 PART REPAIRABLE BY REPLACEMENT.

Part: GUSSET — CRACKED (FWD CARGO) · airframe 54,023 hrs · 31,914 cycles

FORWARD CARGO BAY GUSSET IS CRACKED AT BS 540 S-19R WL 190 / REMOVED AND REPLACED FCB GUSSET AT BS 540 S-19L WL 190 I.A.W SRM. 51-40-02-0G-0 AND BOEING DWG # 143A7902

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 54,023 hrs · 31,914 cycles

BS 663 LH VAPOR BARRIER VERTICAL STIFFENER CRACKED; LBL 30; LWR RADIUS; MARKED / REMOVED AND REPLACED BS 663 L/H VAPOR BARRIER VERTICAL STIFFENER; LBL 30 IAW SRM 51-40-02-0G-0 AND DWG # 111A1000

Part: RETAINER — CORRODED (RT OVERWING SEAL) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** CORROSION ON R/H OVERWING EXIT CUTOUT SEAL RETAINER AT LOWER FWD CORNER; BS 619 COMMON TO LOWER SILL WEB; WL220; RBL71 / REMOVED AND REPLACED SEAL RETAINER AT R/H OVERWING EXIT CUTOUT LOWER FWD CORNER PER SRM 51-40-02 AND DWG 144A8803

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** AROUND PERIPHERY OF AFT CARGO BAY FLOOR PANEL 140CF. / FABRICATED NEW ACB FLOOR PANEL 140CF FROM 080 2024T3; LOT# 1449888-1 PER AMM 25-52-01-201-801 AND DWG 453A2610

Part: SHIELD — CORRODED (FWD CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 494-500A; R.B.L. 24; W.L. 154. / REMOVED AND REPLACED ON FCB NEW SHIELD BS 494 - 500A RBL 24 ITEM 7531855 PO# 813074. LOCATED AND DRILLED IAW SRM 51-40-02 SRM 51-40-03 AND DWG 143A0080

Part: WEB — CORRODED (AFT CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON AFT CARGO BAY THRESHOLD SUB WEB AT B.S. 794-847; R.B.L. 27; W.L. 154. / REMOVED AND REPLACED ON AFT CARGO BAY THRESHOLD SUB WEB AT BS 794-847 RBL 27. WL154 IAW SRM 51-40-02 AND DWG 146A8340 88920U 06MAR21

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR PANEL SUPPORT AT B.S. 772; L.B.L. 24 - R.B.L. 24; W.L. 154. / RECEIVED NEW / SERVICABLE AFT CARGO BAY FLOOR PANEL SUPPORT AT B.S. 772; L.B.L 24 - R.B.L. 24; W.L 154 TO BE INSTALLED ON JPANEL-141-CLOSE. 57609U 09MAR21

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON AFT CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT B.S. 947; L.B.L. 10 - R.B.L. 21; W.L. 154. / CORROSION ON ACB AFT BULKHEAD CENTER PANEL LOWER SUPPORT ANGLE @ BS 947-LBL10-RBL21 WL154. FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM NEED TO REMOVE AND REPLACE IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED LOWER BULKHEAD SUPPORT ANGLE PN #149A8118U30; PO #807682 IAW SRM 51-40-02 AND IAW DWG #149A8117

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,023 hrs · 31,914 cycles

CORROSION ON AFT CARGO BAY SHIELD SUPPORT AT B.S. 767-794; R.B.L. 24; W.L. 154. / NO LIMITS ALLOWED; PART MUST BE REPLACED. REMOVED AND REPLACED PART PER SRM 51-10-02; SRM 51-40-02-OG-0 AND BOEING DRAWING #146A0081. 57006U 05MAR21

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,023 hrs · 31,914 cycles

CORROSION ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 400-500D; L.B.L. 24; W.L. 154. / REMOVED AND INSTALLED ON FCB FLOOR TO SIDEWALL SUPPORT AT BS 400-500D LBL 24 IAW SRM 53-00-53-2R-6; DWG 143A7501 SRM 51-40-05 AMM 51-21-41-370 AND SRM 51-40-02 AND DWG 143A7500 80641U 04MAR21

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON AFT CARGO BAY SHIELD SUPPORT AT B.S. 847-867; R.B.L. 24; W.L. 154. / REMOVED AND REPLACED ON AFT CARGO BAY SHIELD SUPPORT AT BS. 847-867; R.B.L. 24 W.L 154 IAW. SRM 51-40-02 AND DWG 146A0081 R.O. 889204 04MAR21

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 727-767; R.B.L. 24; W.L. 154. / REMOVED CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 727-767 RBL 24 WL 154 MAX. MAT. LOSS 4.' X 2.' MORE THAN 50% MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ACB FLOOR TO SIDEWALL SUPPORT BS727-767 RBL 24 WL 154 I.A.W SRM 53-00-53-1A-2; SRM 51-40-02-OG-0 AND BOEING DWG #146A7500

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 887-947; R.B.L. 24; W.L. 154. / REMOVED AND REPLACED ACB FLOOR TO SIDEWALL SUPPORT AT BS 887 - 947 RBL 24; WL.154 P/N 147A7501-17 IAW SRM 51-40-02 AND DWG 147A7500 RO. 889204 05MAR21

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON AFT CARGO BAY CARGO TRACK AT B.S. 787-887; R.B.L. 14; W.L. 154. / REMOVED CORROSION AT ACB CARGO TRACK BS 787 - 887 RBL 14 WL 154; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; REMOVED AND REPLACED ACB CARGO TRACK SECTION BETWEEN BS 747 + 10 TO BS 887 RBL 14 WL 154 PER SRM 51-40-02 AND DWG 146A7501

Part: PLATE — CRACKED (HORIZONTAL STAB) · airframe 54,023 hrs · 31,914 cycles

LEFTT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE IS CRACKED. / REMOVED AND INSTALLED NEW L/T HAND HORIZONTAL STAB FORWARD UPPER SLIDE SEAL PLATE IAW AMM 53-31-31-000-802 AND AMM 53-31-31-400-802. 57015U 02MAR21

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 867-887; R.B.L. 24; W.L. 154. / REMOVED AND REPLACED ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT BS 867 - 887 RBL 24 WL 154 IAW. SRM 51-40-02 AND DWG 146A7500 82920U 04MAR21

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 420-440; R.B.L. 24; W.L. 154. / REMOVED AND REPLACED ON FCB FLOOR TO SIDEWALL SUPPORT AT BS 420-440 RBL24 ITEM 7530143 PO #806970 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 143A0080 80644U 04MAR21

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 500A-500D; R.B.L. 24; W.L. 154. / REMOVED AND REPLACED ON FCB NEW FLOOR TO SIDEWALL SUPPORT AT BS 500A-500D RBL 24 ITEM 7535472 PO# 813032 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 143A7500 80641U 02MAR21

Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 54,023 hrs · 31,914 cycles

LEFT HORIZONTAL STABILIZER; LOWER SKIN CRACKED AT STAB STA- 194; 17 INCHES AFT OF FRONT SPAR; CRACK IS .75' IN LENGTH. MARKED. / REPAIRED LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 194 PER SRM 55-10-01-22-11. REMOVABLE COMPONENT: P/N:186A1000-41; S/N:IC0581

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR PANEL SUPPORT AT B.S. 887; L.B.L. 10 - R.B.L. 21; W.L. 154. / REMOVED AND REPLACED PANEL SUPPORT AT B.S.887 LBL10 RBL21 WL154 IAW SOPM 20-50-01 56334U 09MAR21 LEAD 67 09MAR21 INSP 86 09MAR21

Part: PLATE — CRACKED (HORIZONTAL STAB) · airframe 54,023 hrs · 31,914 cycles

RIGHT HAND HORIZONTAL STABILIZER FORWARD UPPER SLIDE SEAL PLATE IS CRACKED. / REMOVED AND INSTALLED NEW R/H HORIZONTAL STAB FORWARD UPPER SLIDE SEAL PLATE IAW AMM 53-31-31-000-802 AND AMM 53-31-31-400-802 57015U 02MAR21

Part: FLOORBEAM — CRACKED (CABIN) · airframe 54,023 hrs · 31,914 cycles

PASSENGER CABIN FLOOR PANEL SUPPORT IS CRACKED AT B.S. 540; L.B.L. 24.5 - L.B.L. 45; W.L. 208.1. / REMOVED AND REPLACED PASSENGER CABIN FLOOR PANEL SUPPORT AT BS540 LBL.24.5 TO LBL 45 WL. 208.1 I.A.W SRM 51-40-02-OG-0 AND 51-40-05-OG-0 DRAWING #143A0060; PART WAS EVALUATED PASSENGER CABIN FLOOR PANEL SUPPORT AND NO FOUND ALLOWABLE DAMAGE.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON FORWARD CARGO BAY AFT BULKHEAD LEFT PANEL LOWER SUPPORT AT B.S. 500D; L.B.L. 27; W.L. 154. / REMOVED AND INSTALLED ON FCB AFT BULKHEAD LEFT PANEL SUPPORT AT BS 500D S - 19L - S - 26L ITEM 7530854 LOCATED AND DRILLED IAW SRM 51-40-02; SRM 51-40-05 AND DWG 143A7902 80641U 05MAR21

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 400-420; R.B.L. 24; W.L. 154. / REMOVED CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT AT BS 400-420; RBL 24 WL154; MAX MAT REMOVED IS MORE THAN 50%; FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED FCB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02 AND DWG #143A7500

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT B.S. 500D; L.B.L. 24 - R.B.L. 24; W.L. 154. / REMOVED AND REPLACED ON FCB AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT BS 500D LBL 24 - RBL 24 ITEM 7530142 PO# 803907 LOCATED AND DRILLED IAW SRM 51-40-05; SRM 51-40-02 AND DWG 143A7902 80641U 04MAR21

Part: FLOORBEAM — CORRODED (AFT CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR PANEL SUPPORT AT B.S. 727D+5; L.B.L. 24 - R.B.L. 24; W.L. 154. / RECIEVED NEW/SERVICABLE AFT CARGO BAY FLOOR PANEL SUPPORT AT B.S. 727D+5; L.B.L.29-R.B.L.24; W.L.159 TO BE INSTALLED ON JPANEL-141-CLOSE. 57609U 09MAR21

Part: WEB — CORRODED (FWD CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON FORWARD CARGO BAY THRESHOLD SUB WEB UPPER SURFACE AT B.S. 440-494; R.B.L. 27; W.L. 154. / REMOVED MULTIPLE AREAS OF CORROSION ON FCB SUB THRESHOLD WEB UPPER SURFACE AT BS 440-494; RBL 27 WL 154 IAW SRM 51-10-02. CORROSION REMOVED FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 50% MATERIAL LOSS IAW SRM 53-30-15-1A-1 ALLOWABLE DAMAGE 1. REMOVED AND REPLACED NEW SUB THRESHOLD WEB PER #143A8122-10; PO #805652 IAW SRM 51-40-02 AND IAW DWG #143A8330 AND IAW DWG #143A8122

Part: FLOORBEAM — CRACKED (PAX CABIN) · airframe 54,023 hrs · 31,914 cycles

PASSENGER CABIN FLOOR PANEL SUPPORT IS CRACKED AT B.S. 540; R.B.L. 24.5 - R.B.L. 45; W.L. 208.1. / REMOVED AND REPLACED PASSENGER CABIN FLOOR PANEL SUPPORT AT BS 540 RBL 24.5 TO RBL 45 WL 208.1 I.A.W SRM 51-40-02-OG-0 AND 51-40-05-OG-0 DRAWING #143A0600; PASSENGER CABIN FLOOR PANEL SUPPORT WAS EVALUATED AND NO FOUND ALLOWABLE DAMAGE FOR CRACK.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 54,023 hrs · 31,914 cycles

CORROSION ON FORWARD CARGO BAY AFT BULKHEAD RIGHT PANEL LOWER SUPPORT AT B.S. 500D; R.B.L. 27; W.L. 154. / REMOVED AND INSTALLED ON FCB AFT BULKHEAD RIGHT PANEL LOWER SUPPORT AT BS 500D S-19R S-27R ITEM 7530202 LOCATED AND DRILLED SRM 51-40-05; SRM 51-40-02 AND DWG 143A7902 80641U 05MAR21

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 54,023 hrs · 31,914 cycles

***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 727-847; L.B.L. 24; W.L. 154. / REMOVED AND REPLACED ACB FLOOR TO SIDEWALL SUPPORT AT BS 727-BS 847 LBL 27 WL 154 IAW SRM 51-40-02-OG-0 DWG 146A7500

Part: BEAM — CRACKED (R1 DOOR) · airframe 54,023 hrs · 31,914 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #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 / RECEIVED NEW SERVICEABLE FORWARD SERVICE DOOR. DOOR WILL BE INSTALLED ON CUSTOMER CARD# 14079. (POS:FSD; TAG NO:743121; P/N OFF:141A6516-18; S/N OFF:001726; P/N ON:141A6516-18M; S/N ON:002054)

Part: ANGLE — CRACKED (CENTER WING) · airframe 54,023 hrs · 31,914 cycles

BS663 LBL6 BULKHEAD UPPER ATTACH ANGLE COMMON TO THE CENTER TANK IS CRACKED / REPAIRED BULKHEAD UPPER ATTACH ANGLE COMMON TO THE CENTER TANK AT BS 663 LBL 5 TO LBL 18 IAW SRM 57-10-10-2R-5 REPAIR 5

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 54,023 hrs · 31,914 cycles

DURING COMPLETION OF CCN 15021; INTERNAL INSPECTION OF R1 BEAR STRAP; FOUND .300' CRACK ON FWD SIDE OF FASTENER LOCATED AT BS 294 THREE INCHES BELOW S-8R. ENGINEERING DISPOSITION REQUIRED. / REPAIRED CRACKED AT THE BEAR STRAP AT BS294; 3' BELOW S-8R PER 737-700 SRM 53-10-01-2R-6 (REPAIR 6) AND ESR #21-01354

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 54,023 hrs · 31,914 cycles

RH HORZ STAB INSPAR RIB ASSY 5 (STA 129.50) STIFFENER #3 IS CRACKED. TRIMED OUT THE DAMAGE PART OF R/H HORIZ STAB INSPAR RIB ASSY 5 (STA 129.50) STIFFENER #3 AND INSTALLED REPAIR PARTS IAW SRM 5310092R4 88920U 25FEB21

Part: ANGLE — CRACKED (L1 DOOR FRAME) · airframe 54,023 hrs · 31,914 cycles

FWD ENTRY DOOR AFT FRAME; SWITCH CONTACT ANGLE CRACKED / REMOVED & INSTALLED NEW FWD ENTRY DOOR TARGET ATTACH ANGLE PER SRM 51-40-02-0G-0; BOEING DRAWING 141A6101 & BOEING SERVICE BULLETIN 737-52-1159 STEP 5.

Part: PRESSURE DECK — DENTED (COCKPIT) · airframe 54,023 hrs · 31,914 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / REPAIRED DENTED FLIGHT DECK FLOOR AT BS 255 RBL 4 - LBL 14; WL 207.54 PER SWA EA 1-A53-33179 PAR 1 AND ESR NO. 21-01412

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,289 hrs · 31,474 cycles

MUPLTIPLE EMERGENCY LIGHTS OUT IN FWD GALLEY. R & R M1674 EMERGENCY LIGHT BATTERY PACK, IAW AMM 33-51-06.

Part: PANEL — CRACKED (LT MLG WW) · airframe 52,430 hrs · 30,933 cycles

L/H MLG WHEEL WELL HAS A 9' CRACK JUST OUTBOARD OF 'A' SYSTEM RETURN FILTER. / ACCOMPLISHED INTERIM REPAIR IAW SRM 57-10-10-1A-2.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 52,408 hrs · 30,916 cycles

CORROSION ON LOWER SUPPORT ANGLE BS BETWEEN BS 967 AND 986 WL 207.8 APPROX. RBL 46 JUST BELOW INNER CHORD (MOPSILL) / REMOVED CORROSION ON LOWER SUPPORT ANGLE AT STA 967 AND 986 WL 207.8 RBL 46 JUST BELOW INNER CHORD; CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1 STEP 4E(2)(A) DETAIL D. LOCATED AND DRILLED NEW SUPPORT ANGLE PART# 147A8530Y12 PO# 792824. INSTALLATION ACCOMPLISHED ON N259262

Part: STRUCTURE — CORRODED (R2 DOOR) · airframe 52,408 hrs · 30,916 cycles

** CORROSION ** R-2 INNER CHORD IS CORRODED; BS 967-987; WL 208; RBL 52 / REMOVED CORROSION ON R2 INNER CHORD; CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15-1A-1. REMOVED R2 INNER CHORD IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW INNER CHORD IAW SRM 51-40-05-0G-0. INSTALLED NEW INNER CHORD PART # 7530246 PO # 778976 IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A8501

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 52,408 hrs · 30,916 cycles

***CORROSION*** ON 986 FLOOR BEAM AFT FLANGE STA986; WL208; RBL22 / REMOVED CORROSION ON FLOOR BEAM AFT FLANGE AT STA. 986; WL 208; RBL 22 CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1. REMOVED EXISTING REPAIR 4 EA REPAIR ANGLES; 2 EA REPAIR STRAPS IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW REPAIR PARTS IAW SRM 53-70-51-2R-4 AND 51-40-05-0G-0 INSTALLED NEW REPAIR IAW SRM 53-70-51-2R-4 AND BOEING DWG 147A8501 2 EA ANGLES BAC 1490-2811 #7075T6 LOT# 5040890. 2EA ANGLE LOT# 5086355-1 2EA STRAP LOT# 5087742-6

Part: TERMINAL — BROKEN (FIRE LOOP) · airframe 52,376 hrs · 30,899 cycles

#1 ENG B FIRE LOOP INOP / DMA# 0088295 FOUND BROKEN TERMINAL END ON LOWER FAR LOOP ' B' CHANNEL REPAIRED TERMINAL END PER S.W.P.M 20-10-13 OPS CHKS GOOD PER M/M 26-11-02 CL# 37204

Part: SEAT TRACK — OUT OF LIMITS (COCKPIT) · airframe 52,024 hrs · 30,700 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 52,024 hrs · 30,700 cycles

AFT ENTRY DOOR SLIDE NEEDS TO BE REPACKED. INSTALLED AFT ENTRY DOOR SLIDE PER MT#725-61-06 AND AMM 25-66-01

Part: BATTERY — FAILED (CABIN) · airframe 52,024 hrs · 30,700 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1668 AND M1672. R&R EMERGENCY LIGHT BATTERIES AT LOCATIONS M1668 AND M1672 PER MM 33-51-06

Part: BRACKET — BROKEN (KEELBEAM) · airframe 52,024 hrs · 30,700 cycles

KEEL BEAM PANEL 192E LEFT FWD BRACKET BROKEN / REMOVED AND REPLACED BRACKET PER SRM 51-40-02

Part: SEAT TRACK — OUT OF LIMITS (COCKPIT) · airframe 52,024 hrs · 30,700 cycles

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

Part: FAIRING — ELONGATED (LWR FUSELAGE) · airframe 50,024 hrs · 29,448 cycles

FUSELAGE FAIRING PANEL 193 B HOLES ELONGATED AND OVER SIZED (SCREWS PULLING THRU PANEL) / INSTALLED 193B PANEL IAW DCR#39874 & AMM 53-51-21.

Part: SUPPORT BRACKET — CRACKED (AC BAY/FWD CARGO) · airframe 49,925 hrs · 29,381 cycles

AIR CONDITIONING DISTRIBUTION BAY IN FORWARD CARGO COMPART. AT BS540 CEILING FLOOR BOARD SUPPORT BRACKET RIGHT OF CENTER IS CRACKED / REMOVED AND REPLACED BS540 CEILING FLOOR BOARD SUPPORT BRACKET RIGHT OF CENTER PER SRM 51-10-02 AND SRM 51-40-02.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 49,925 hrs · 29,381 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01675. / R&R BATTERY PER AMM.

Part: LIGHT — DEBONDED (ROW 9) · airframe 48,812 hrs · 28,690 cycles

L/H EMERGENCY LIGHT DEBONDED ON THE STOW BIN BULLNOSE AT ROW 9. / REPAIRED LIGHT IAW SOPM AND DWG.

Part: DOUBLER — CRACKED (WHEEL WELL RH) · airframe 48,812 hrs · 28,690 cycles

DOUBLER WAS FOUND TO BE CRACKED ON FWD SIDE OF R/H BS 663 VAPOR BARRIER / FORMED NEW DOUBLER FROM 2024T3 #0.040' CLAD LOT #1375050-5 PER DWG 111A1511 AND 65-88700; LOCATED AND DRILLED IAW SRM 51-40-05; CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01 AND INSTALLED NEW DOUBLER BS 663 RBL 6 TO RBL 31 IAW SRM 51-40-02 AND DWG 111A1008 REV F AND DWG 111A1001 REV - 89004U 27MAR19

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 48,812 hrs · 28,690 cycles

CABIN FLOOR PANEL 231LF HAD STRAND DAMAGED ON UPPER SURFACE. REPAIRED FLOOR PANEL 231LF IAW SRM. (BETWEEN BS. 420 TO BS. 537.45)

Part: SKIN — DENTED (BS 927) · airframe 48,812 hrs · 28,690 cycles

SKIN DENTED AT BS. 927, BETWEEN STR. 23R. TO STR. 24R. REPAIRED SKIN IAW EA AND ER.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 48,812 hrs · 28,690 cycles

L ANGLE ATTACHED TO SEAT TRACK 206 MECHANICALLY DAMAGED BETWEEN BS 500D TO BS 520, LBL 45. R&R L-ANGLE IAW DWG & SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 48,812 hrs · 28,690 cycles

L/H HORIZONTAL STABILIZER RIB AT STAB. STA. 120.3, SECOND FROM FRONT VERTICAL STIFFENER, CRACKED AT THE LOWER END. / REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 48,812 hrs · 28,690 cycles

L/H HORIZONTAL STABILIZER RIB AT STAB. STA. 120.3, FOURTH FROM FRONT VERTICAL STIFFENER, CRACKED AT THE LOWER END. REPAIRED RIB IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 48,812 hrs · 28,690 cycles

VAPOR BARRIER CRACKED AT BS. 663, RBL 8. REPAIRED BARRIER IAW EA AND ER.

Part: RIB — CRACKED (HORIZONAL STAB) · airframe 48,812 hrs · 28,690 cycles

L/H HORIZONTAL STABILIZER RIB, AT STAB. STA. 120.3, THIRD FROM FRONT VERTICAL STIFFENER, CRACKED AT THE LOWER END. / REPAIRED RIB IAW SRM.

Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 48,812 hrs · 28,690 cycles

COCKPIT FLOOR DENTED AT BS. 256, BETWEEN RBL 4 TO LBL 14. / REPAIRED FLOOR IAW EA AND ER.

Part: SCUFF PLATE — CRACKED (CARGO BAY) · airframe 48,812 hrs · 28,690 cycles

FORWARD CARGO DOOR CUT OUT AFT SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: PLATE — CRACKED (L/H WING) · airframe 48,812 hrs · 28,690 cycles

L/W T/E ORSS 261 LOWER CORRUGATED PLATE IS LOOSE AND CRACKED. / REMOVED WIGGLE PLATE IAW SRM 51-40-02-0G-0 109C 03/23/2019 INSTALLED WIGGLE PLATE IAW SRM 51-40-02-0G-0 STEP 4; AND BOEING DWG 115A2001 57028U 6APR19

Part: SCUFF PLATE — CRACKED (CARGO BAY) · airframe 48,812 hrs · 28,690 cycles

FORWARD CARGO DOOR CUT OUT FORWARD SCUFF PLATE CRACKED. / REPAIRED SCUFF PLATE IAW EA.

Part: RETAINER — CRACKED (LEFT WING) · airframe 48,812 hrs · 28,690 cycles

L/W T/E ORSS 271 UPPER BULB SEAL RETAINER IS CRACKED / REMOVED AND REPLACED L/W T/E UPPER BULB SEAL RETAINER LOCATED AT ORSS 271 IAW SRM 51-40-02-0G-0 57055U 04/01/2019

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,812 hrs · 28,690 cycles

R/H EXTERIOR OVERWING ESCAPE LIGHT INOP. / R&R CHARGER ASSEMBLY IAW AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO DOOR) · airframe 48,812 hrs · 28,690 cycles

AFT CARGO BAY DOOR CUT OUT FORWARD SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SCUFF PLATE — CRACKED (AFT CARGO DOOR) · airframe 48,812 hrs · 28,690 cycles

AFT CARGO BAY DOOR CUT OUT AFT SCUFF PLATE CRACKED. / REPAIRED SCUFF PLATE IAW EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,812 hrs · 28,690 cycles

R/H EXTERIOR OVERWING ESCAPE LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,812 hrs · 28,690 cycles

L/H EMERGENCY EXIT LIGHTS ON STOW BIN INOP BETWEEN ROW 9 TO ROW 11. R&R BATTERY PACK IAW AMM.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,812 hrs · 28,690 cycles

L/H EMERGENCY EXIT LIGHTS ON STOW BIN INOP BETWEEN ROW 9 TO ROW 11. / R&R BATTERY PACK CHARGER ASSEMBLY IAW AMM.

Part: SKIN — DENTED (AFT FUSELAGE) · airframe 48,812 hrs · 28,690 cycles

MOD TYPE: 6 NBR 22971 REV: POS: SKIN DENT STA 1035; 2 INCHES ABOVE STR 15L DIMENSIONS 2 INCHES LENGTH 6 INCHES WIDTH .215 INCHES DEEP PER SRM 53-00-01-1A-1- 4.C.3.B DENT FOUND TO BE WITHIN LIMITS. RE-INSPECT FOR CORROSION AND CRACK AT EACH 5000 FLT CYCLE INTERVALS / CAT A REPAIR INSTALLED PER E.A. 1-753-34496 REV IR (ATS ER 19-02410 REV IR)

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 47,962 hrs · 28,129 cycles

RUDDER COUNTERBALANCE WEIGHT IS CORRODED . / REMOVED AND REPLACED RUDDER BALANCE ARM WEIGHT PER CMM 55-40-09

Part: RIB — CRACKED (LT WING) · airframe 46,947 hrs · 27,444 cycles

LT WING DEFLECTION CONTROL RIB UPPER MOUNT TAB CRACKED. REPAIRED RIB PER SRM.

Part: LENS — OUT OF POSITION (EXIT SIGN) · airframe 45,330 hrs · 26,431 cycles

FORWARD ENTRY EMERGENCY EXIT SIGN LIGHT ARROW OUT OF POSITION. R&R LENS PER AMM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,329 hrs · 25,787 cycles

FUSELAGE CREASED AT BS 380+6, STR 9L. REPAIRED SKIN PER SRM.

Part: SIGN — UNSECURE (CABIN) · airframe 43,769 hrs · 25,444 cycles

MID-CABIN OVERHEAD EMERGENCY LIGHT SIGN FELL OFF. REINSTALLED SIGN PER SIP.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 43,686 hrs · 25,391 cycles

RIGHT EMERGENCY EXIT BULLNOSE LIGHT INOPERATIVE AT ROW 3. CONNECTED A WIRE IAW WDM.

Part: SIGN — LOOSE (CABIN) · airframe 43,551 hrs · 25,309 cycles

CEILING OVERWING EXIT SIGN LOOSE. SECURED SIGN PER AMM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 42,024 hrs · 24,412 cycles

LEFT WING INBOARD TRAILING EDGE OUTBOARD AFT FLAP DELAMINATED ON UPPER SKIN. REPAIRED THE FLAP IAW SRM.

Part: ANGLE — CRACKED (BS 500C) · airframe 42,024 hrs · 24,412 cycles

FORWARD CARGO BAY ANGLE CRACKED AT BS 500C, BETWEEN STRINGERS 25 - 26L. R & R THE ANGLE IAW SRM AND DWG.

Part: SUPPORT — CRACKED (BS 747) · airframe 42,024 hrs · 24,412 cycles

AFT CARGO BAY CARGO TRACK SUPPORT CRACKED AT BS 747, BETWEEN STRINGERS 26 TO 27R. / REPAIRED TRACK SUPPORT IAW SRM.

Part: STIFFENER — CRACKED (BS 540) · airframe 42,024 hrs · 24,412 cycles

FLOORBEAM STIFFENER CRACKED AT BS 540, LBL 2. R & R STIFFENER IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 747-767) · airframe 42,024 hrs · 24,412 cycles

AFT CARGO BAY SUPPORT ZEE CORRODED BETWEEN BS 747 TO 767, STRINGER 25R. R & R THE SUPPORT IAW SRM AND DWG.

Part: SKIN SPLICE — CRACKED (BS 540) · airframe 42,024 hrs · 24,412 cycles

FUSELAGE SKIN SPLICE CRACKED AT BS 540, STRINGER 22L. REPAIRED THE SPLICE IAW EA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,024 hrs · 24,412 cycles

FORWARD CARGO COMPARTMENT ANGLE SUPPORT CRACKED AT BS 500B, BETWEEN STR 26L TO STR 25L. R&R SUPPORT IAW SRM AND DWG.

Part: LENS — BROKEN (CABIN) · airframe 42,024 hrs · 24,412 cycles

AFT GALLEY AREA EMERGENCY EXIT LENS BROKEN. R&R LENS IAW AMM.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 42,024 hrs · 24,412 cycles

FORWARD CARGO COMPARTMENT ANGLE SUPPORT CRACKED AT BS 500C, BETWEEN STR 26L TO STR 25L. R&R SUPPORT IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 42,024 hrs · 24,412 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED ON STA 95.96, ACCESS PANEL 341B. R&R RIB IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 42,024 hrs · 24,412 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE PANEL RIB CRACKED ON HSS 78.29. R & R THE RIB IAW SRM AND DWG.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 41,850 hrs · 24,311 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R & R BATTERY IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 41,850 hrs · 24,311 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R & R THE BATTERY PACK IAW AMM.

Part: POWER SUPPLY — NO TEST (CABIN) · airframe 41,850 hrs · 24,311 cycles

EMERGENCY LIGHT POWER SUPPLY BASE UNIT AT MO1669 FAILED TO TEST. R&R POWER SUPPLY IAW AMM.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,754 hrs · 24,260 cycles

LEFT OVERWING EMERGENCY EXIT DOOR WINDOW LIGHT INOPERATIVE. R & R THE BALLAST ASSEMBLY IAW MM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 41,002 hrs · 23,828 cycles

FORWARD RIGHT WHEEL WELL VAPOR BARRIER CRACKED. REPAIRED BARRIER PER SRM.

Part: ACTUATOR — TRIPPED (FUEL SYSTEM) · airframe 35,798 hrs · 20,835 cycles

TRIPPED CROSS FEED VLV CB INFLIGHT. R & R CROSS FEED VLV ACTUATOR IAW AMM.

Part: FLOOR PANEL — CORRODED (COCKPIT) · airframe 35,750 hrs · 20,809 cycles

COCKPIT FLOOR PANEL 211AF CUT OUT INTERFACE UPPER SURFACES CORRODED BETWEEN BS 260 - 270, BETWEEN LBL 11 TO RBL 11. REPAIRED PANEL IAW SRM & EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 35,750 hrs · 20,809 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 166.30 AT STIFFENER. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 35,750 hrs · 20,809 cycles

LEFT HORIZONTAL STABILIZER RIB STABILIZER STATION 129.5, 3RD VERTICAL STIFFENER FROM FRONT CRACKED. REPAIRED RIB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,750 hrs · 20,809 cycles

FORWARD SEAT TRACK BOTH INBD & OTBD FLANGE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,750 hrs · 20,809 cycles

SEAT TRACK & FLOOR STRUCTURE CRACKED AT BS 727B, RBL 24.75, AFT TRACK OTBD HOLE IN FLANGE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,750 hrs · 20,809 cycles

SEAT TRACK FLOOR STRUCTURE CRACKED AT BS 727B, LBL 24.75, FWD TRACK OUTER FLANGE & AFT HOLE ON INBD FLANGE OF FWD TRACK. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,750 hrs · 20,809 cycles

SEAT TRACK FLOOR STRUCTURE CRACKED AT BS 727B, RBL 45.5, IN FWD TRACK INBD FLANGE AFT HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,750 hrs · 20,809 cycles

FORWARD SEAT TRACK & FLOOR STRUCTURE CRACKED AT BS 727B, RBL 24.75, FWD HOLES OF BOTH INNER & OUTER FLANGE. REPAIRED SEAT TRACK IAW EA.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 35,750 hrs · 20,809 cycles

LEFT MAIN WW BULKHEAD WEB CRACKED AT BS 663, LBL 44. R & R WEB IAW SRM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 35,577 hrs · 20,712 cycles

L1 DOOR EMER EVAC SLIDE LIGHT INOPERATIVE. FOUND LIGHT DISCONNECTED. CONNECTED LIGHT IAW AMM.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 35,288 hrs · 20,548 cycles

L1 DOOR SKIN DAMAGED BETWEEN BS 376 - 378, BETWEEN STRINGER 15L - 16L. REPAIRED SKIN IAW EA.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 35,146 hrs · 20,459 cycles

RIGHT WW FWD BULKHEAD VAPOR BARRIER CRACKED. REPAIRED BARRIER IAW EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 30,554 hrs · 17,820 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. READJUSTED SLIDE IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 28,870 hrs · 16,839 cycles

MID CABIN EMERGENCY EXIT LENS LOOSE FROM OVERHEAD LIGHT ASSY. SECURED LENS PER AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 28,748 hrs · 16,762 cycles

LEFT AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — DIRTY (CABIN) · airframe 28,747 hrs · 16,760 cycles

EMERGENCY EXIT LIGHT DIRTY JUST FWD OF AFT CARGO BAY. CLEANED LENS PER SOPM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 28,747 hrs · 16,760 cycles

FORWARD CARGO LT FLOOR TO SIDEWALL CORRODED BETWEEN BS 453 TO BS 475. REMOVED AND REPLACED SUPPORT PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 28,747 hrs · 16,760 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 767 - BS 792, RBL 22. REMOVED AND REPLACED PLATE IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 28,747 hrs · 16,760 cycles

AFT CARGO BAY ON CARGO TIE DOWN TRACK CORRODED BETWEEN BS 792 TO BS 847, RBL. REMOVED AND REPLACED TRACK SECTION IAW SRM AND EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 28,747 hrs · 16,760 cycles

AFT CARGO BAY ON SUB-THRESHOLD WEB CORRODED BETWEEN BS 792 TO BS 847, BETWEEN RBL 20 TO RBL 28. REMOVED AND REPLACED WEB PER SRM AND DWG.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 28,747 hrs · 16,760 cycles

PASSENGER CABIN FLOOR PANEL 241ADF AFT O/B CORNER BROKEN. REPAIRED PANEL IAW SRM.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 28,747 hrs · 16,760 cycles

PASSENGER CABIN FLOOR PANEL 222DF O/B EDGE LOWER SURFACE BROKEN. REPAIRED PANEL IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,747 hrs · 16,760 cycles

FLOORBEAM CORRODED AT BS 986.5, RBL 44. REPAIRED BEAM IAW ER.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 28,747 hrs · 16,760 cycles

CAPTAINS NR 1 WINDOW FRAME CRACKED AT OUTBOARD UPPER CORNER. REPAIRED FRAME IAW ER AND EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,747 hrs · 16,760 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED I/B SIDE OF RIB STAB STA 101.90 17.5 - 18.5 FROM REAR SPAR. REPAIRED SKIN IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,747 hrs · 16,760 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STAB STA 92.70 1ST 2ND AND 3RD VERTICAL STIFFENERS FROM FWD END CRACKED. REPAIRED RIB PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,747 hrs · 16,760 cycles

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

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,747 hrs · 16,760 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STAB STA 157.10 3RD VERTICAL STIFFENER FROM FWD END CRACKED. REPAIRED RIB IAW EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,747 hrs · 16,760 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED I/B SIDE OF RIB AT STAB STA 166.30. REPAIRED SKIN IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 28,747 hrs · 16,760 cycles

LEFT HORIZONTAL STABILIZER RIB AT STA 92.70 2ND AND 3RD VERTICAL STIFFENERS FROM FWD EDGE CRACKED. REPAIRED RIB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 28,747 hrs · 16,760 cycles

VERTICAL WEB CRACKED AT BS 663, WL 196, RBL. 43.5. REPAIRED VERTICAL WEB PER SRM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 28,355 hrs · 16,533 cycles

RIGHT WING UPPER TRAILING EDGE PANEL BETWEEN SPOILER 7 AND 8, SUPPORT BRACKET CRACKED. REMOVED AND REPLACED SUPPORT BRACKET PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 28,355 hrs · 16,533 cycles

EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY ASSY'S PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 28,355 hrs · 16,533 cycles

LEFT OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 28,355 hrs · 16,533 cycles

R1 DOOR SLIDE OUT OF ADJUST. REPOSTIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 28,291 hrs · 16,495 cycles

EMERGENCY LIGHT ABOVE EXIT ON CAPTAIN SIDE EMERGENCY EXIT DOOR INOP. RELAMPED PER MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 27,952 hrs · 16,276 cycles

LEFT HORZ LOWER IN SPAR SKIN IS CRACKED 9" FWD OF AFT SPAR I/B OF RIB AT STATION 147.90 AND MEASURES 1" LONG. REPAIRED PER SRM 55-10-01-2R-11 THIS IS A CATEGORY B REPAIR. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 27,952 hrs · 16,276 cycles

LEFT HORZ, LOWER IN SPAR SKIN IS CRACKED 16.5" FWD OF AFT SPAR I/B OF RIB AT STATION 147.90 AND MEASURES 1.5" LONG. REPAIRED PER SRM 55-10-01-2R-11 REPAIR 11. THIS REPAIR IS A CATEGORY B REPAIR. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 27,952 hrs · 16,276 cycles

LEFT HORZ, LOWER IN SPAR SKIN IS CRACKED 10" FWD OF AFT SPAR I/B OF STATION 101.90 RIB AND MEASURES 1.5" IN LENGTH. REPAIRED PER SRM 55-10-01-2R-11 REPAIR 11. THIS IS A CATEGORY B REPAIR FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 27,952 hrs · 16,276 cycles

RIGHT HORIZ LOWER INSPAR SKIN IS CRACKED 10.5" FWD OF AFT SPAR I/B SIDE OF RIB AT STATION 101.90 AND MEASURES 1" LONG. REPAIRED PER SRM 55-10-01-2R-11 REPAIR 11 THIS REPAIR IS A CATEGORY B REPAIR.

Part: WINDOW — CRACKED (COCKPIT) · airframe 27,952 hrs · 16,276 cycles

WINDOW L1 CRACKED DURING FLT-GOT ARCHING JUST BEFORE WINDOW CRACKED OUTER PANE. REPLACED CAPTS L1 WINDOW AND WINDOW HEAT CONTROLLER AND OPS & LEAK CHECKS GOOD PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,261 hrs · 14,759 cycles

FWD EMERGENCY LIGHT INOPERATIVE. REPAIRED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,261 hrs · 14,759 cycles

FORWARD EMERGENCY EXIT FLOOR LIGHT INOP. RELAMPED LIGHT IPER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,261 hrs · 14,759 cycles

EEPLS INOP BETWEEN ROW 1 TO ROW 2. RELAMPED EEPLS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,588 hrs · 14,373 cycles

FLOOR PATH EMERGENCY EXIT LIGHT INOP AT OVERWING EXIT. RELAMPED LIGHT PER MM.

Part: CAP — OUT OF POSITION (CABIN) · airframe 24,507 hrs · 14,327 cycles

EMERGENCY EXIT LIGHT WIRE EXPOSED WIRE AT ROW 11. INSTALLED END CAP IAW MM.

Part: LENS — MISSING (CABIN) · airframe 23,019 hrs · 13,439 cycles

EMERGENCY EXIT LIGHT LENS MISSING AT ROW 13. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,889 hrs · 13,363 cycles

DURINGS SCHEDULED CV CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT ASSY PER MM.

Part: COVER — LOOSE (CABIN) · airframe 21,900 hrs · 12,769 cycles

DURING SCHEDULED MV2 CHECK FOUND, EEPLS FLOOR TRACK COVER LOOSE AT ROW 12ABC. R/R PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 21,702 hrs · 12,658 cycles

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

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,623 hrs · 12,608 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX HORIZONTAL STIFFENER CRACKED AT BS 550, LBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,623 hrs · 12,608 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX HORIZONTAL STIFFENER CRACKED AT BS 550, LBL 14.5. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,623 hrs · 12,608 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX HORIZONTAL STIFFENER CRACKED AT BS 550, LBL 6.75. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,623 hrs · 12,608 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX HORIZONTAL STIFFENER CRACKED AT BS 550, RBL 6.75. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,623 hrs · 12,608 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX HORIZONTAL STIFFENER CRACKED AT BS 550, RBL 31.5. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 21,623 hrs · 12,608 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX HORIZONTAL STIFFENER CRACKED AT BS 550, RBL 14.5. REMOVED AND REPLACED STIFFENER PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,623 hrs · 12,608 cycles

DURING SCHEDULED 6Y CHECK, FWD LT EMERGENCY EXIT LIGHT BATTERY PACK FAILED. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,623 hrs · 12,608 cycles

DURING SCHEDULED 6Y CHECK, LT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK FAILED. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,623 hrs · 12,608 cycles

DURING SCHEDULED 6Y CHECK, AFT RT EMERGENCY EXIT LIGHT BATTERY PACK FAILED. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — LOOSE (CABIN) · airframe 21,579 hrs · 12,581 cycles

FWD EEPLS LENS LOOSE. REMOVED AND REPLACED LENS PER MM.

Part: TRIM PANEL — BROKEN (CABIN) · airframe 21,470 hrs · 12,512 cycles

ROW 1 ABC EMERGENCY LIGHT TRIM BROKEN. REPLACED TRIM & LIGHT ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 18,168 hrs · 10,568 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED AT ROW 11-12. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 16,091 hrs · 9,265 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS CRACKED BETWEEN ROW 12 TO ROW 20. INSTALLED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 16,091 hrs · 9,265 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER MISSING AT ROW 4. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 16,034 hrs · 9,230 cycles

EEPLS TRACK MISSING. INSTALLED COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 15,099 hrs · 8,684 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 14,877 hrs · 8,558 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 14,877 hrs · 8,558 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 13,593 hrs · 7,808 cycles

EEPLS TRACK CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 13,593 hrs · 7,808 cycles

EGRESS LIGHT TRACK COVER CRACKED AT ROW 11. REPLACED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 12,450 hrs · 7,088 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 12,450 hrs · 7,088 cycles

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

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 12,450 hrs · 7,088 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 9,270 hrs · 5,182 cycles

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

Part: CAP — MISSING (CABIN) · airframe 8,536 hrs · 4,783 cycles

EEPLS END CAP MISSING AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 7,371 hrs · 4,122 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 11 ABC. REMOVED AND REPLACED COVER PER MM.

Part: LENS — BROKEN (EMERGENCY LIGHTS) · airframe 6,523 hrs · 3,664 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 3,791 hrs · 2,094 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT LENS MISSING AT ROW 1 ABC. INSTALLED EEPLS LIGHT LENS PER MM.

Part: LENS — CRACKED (MID CABIN) · airframe 678 hrs · 381 cycles

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