N7724A

Part: SLIDE — LOOSE (ZONE 800) · airframe 51,319 hrs · 27,769 cycles

L1 SLIDE UNSECURED FROM DOOR/HOUSING. RESECURED L1 SLIDE ASY IAW AMM 25-66-01. OK TO CONTINUE SERVICE.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 49,503 hrs · 26,699 cycles

EXIT SIGN ON DOOR R1 WILL NOT STAY ATTACHED<[01] REMOVED AND REPLACED EMERGENCY LIGHT HOUSING ASSY REF AMM 33-51-01

Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 49,183 hrs · 26,535 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. <[01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04.

Part: ENGINE — SMOKE (NR 2) · airframe 49,172 hrs · 26,529 cycles

#2 ENG OVERTEMP AT APPPROX 700FT. HEARD POPPING SOUND. RAN QRC/QRH ENGINE SEIZURE DUNE TO HIGH VIBRATION. LANDED AIRCRAFT. F/AS REPORTED BURNT SMELL IN CABIN. EVACUATED AIRCRAFT.<[01] COMPLIED WITH CONDITIONAL INSPECTION FOR THE REPORT OF SMOKE OR FUMES IN THE CABIN REF. AMM 05-51-56. REMOVED AND REPLACED #2 ENG. ON MXI TASK CARD 771-00-01 (TTG8Q00ZX80A).

Part: SEAL — CRACKED (ZONE 300) · airframe 48,568 hrs · 26,181 cycles

TAIL LH HORIZONTAL STABILIZER UPPER FRONT SPAR SLIDING SEAL IS CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-400-802-NG (STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL INSTALLATION - PERMANENT)] LEFT UPPER HORIZONTAL STABILIZER SLIDING SEAL.;[02] CORRECTED RII BLOCK TO STATE NO<BR>01 - REMOVED AND REPLACED PER [AMM 53-31-31-400-802-NG (STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL INSTALLATION - PERMANENT)]

Part: STRAP — DETACHED (ZONE 200) · airframe 48,567 hrs · 26,179 cycles

CREW REPORTS AFT FLASHLIGHT STRAP NOT ATTACHED CORRECTLY<[01] INSTALLED SCREW FOR FLASHLIGHT STRAP PER SIP

Part: LIGHT — MISSING (ZONE 200) · airframe 48,334 hrs · 26,046 cycles

PAX CABIN FWD SERVICE DOOR AREA ;EXIT LIGHT LENS WITH MISSING ARROW. 2024-763844<[01] REPLACED EXIT LIGHT ASSY FWD SERVICE DOOR I.A.W B737-700 AMM 33-51-01-960-802 TEST IS OK;[02] TASK COMPLETED

Part: WEB — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK WEB LOCATED BTW LBL6.13 TO LBL31.83 AT BS663 ON VAPOR BARRIER LT SIDE MAIN WHEEL WELL 2024-763790<[01] REPLACED WEB LOCATED BTW LBL6.13 TO LBL31.83 AT BS663 ON VAPOR BARRIER LT SIDE MAIN WHEEL WELL IAW B737-700 SRM DWG 111A1511 SHEET 25 REV - AND SRM 51-10-02.<BR>FOR INSTALLATION SEE: TTG8Q00XHUXW<BR>SEE INDIVIDUAL SIGNS OFF BELOW.;[02] REPLACED WEB LOCATED BTW LBL6.13 TO LBL31.83 AT BS663 ON VAPOR BARRIER LT SIDE MAIN WHEEL WELL IAW B737-700 SRM DWG 111A1511 SHEET 25 REV - AND SRM 51-10-02.<BR>FOR INSTALLATION SEE: TTG8Q00XHUXW<BR>SEE INDIVIDUAL SIGNS OFF BELOW.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CORROSION SUPPORT ZEE LBL 21 BETWEEN BS 747 TO BS 767 AT AFT CARGO COMPARTMENT 2024-763758<[01] TOOL USED ON STEP 3 UT EQUIPMENT. P/N: 45MG; S/N: 232017609; CAL DUE DATE: 08-OCT-25;[02] FAULT RESOLVED ON OTHER FAULT. SEE FAULT ID TTG8Q00XMBJZ<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] FAULT RESOLVED ON OTHER FAULT. SEE FAULT ID TTG8Q00XMBJZ<BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CORROSION SUPPORT ZEE RBL 21 BETWEEN BS 727D TO BS727E AT AFT CARGO COMPARTMENT 2024- 763760<[01] ON STEP 3: FAULT RESOLVED ON OTHER FAULT.

Part: ACCESS DOOR — DAMAGED (ZONE 100) · airframe 48,334 hrs · 26,046 cycles

ELONGATED HOLES ON GROUND SERVICE ACCESS DOOR 114AR LOWER FUSELAGE 2024-763752<[01] REPLACED GROUND SERVICE ACCESS DOOR 114AR LOWER FUSELAGE IAW B737-700 AMM 52-49-02-000-801 AND AMM 52-49-02-400-801 <BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED GROUND SERVICE ACCESS DOOR 114AR LOWER FUSELAGE IAW B737-700 AMM 52-49-02-000-801 AND AMM 52-49-02-400-801. VERIFIED

Part: SUPPORT — CORRODED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CORROSION SUPPORT ZEE RBL 21 BETWEEN BS 727C TO BS 727D AT AFT CARGO COMPARTMENT. FAULT RESOLVED ON OTHER FAULT.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CORROSION SUPPORT ZEE LBL21 BETWEEN BS 727D TO BS 727E AT AFT CARGO COMPARTMENT 2024-763757<[01] TOOL USED ON STEP 3 UT EQUIPMENT. P/N: 45MG; S/N: 232017609; CAL DUE DATE: 08-OCT-25;[02] FAULT RESOLVED ON OTHER FAULT. SEE FAULT ID TTG8Q00XMBJZ<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] FAULT RESOLVED ON OTHER FAULT. SEE FAULT ID TTG8Q00XMBJZ<BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK SUPPORT BRACKET AFT FACE BULKHEAD BS 727 LEVEL STRINGER 27R AT AFT CARGO COMPARTMENT 2024-763735<[01] REPLACED SUPPORT BRACKET LOC. AFT FACE BULKHEAD BS 727 LEVEL STRINGER 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 144A2600 SHEET 712 REV ?;LENGTH OF CRACK IS: 0.750? TOOL USED CALIPER P/N: 500-197?30;S/N: A22257522 DUE DATE: 29-AUG-25;[02] REPLACED SUPPORT BRACKET LOC. AFT FACE BULKHEAD BS 727 LEVEL STRINGER 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 144A2600 SHEET 712 REV ?;LENGTH OF CRACK IS: 0.750? TOOL USED CALIPER P/N: 500-197?30;S/N: A22257522 DUE DATE: 29-AUG-25

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 48,336 hrs · 26,047 cycles

CRACK SUPPORT ANGLE BS 867 BETWEEN STRINGER 2R TO STRINGER 3R AT PASSENGER CABIN 2024-763721<[01] REPLACED ANGLE AND FASTENERS LOCATED BS 867 BETWEEN STRINGER 2R TO STRINGER 3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A7901 SHEET 66; REV A.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE AND FASTENERS LOCATED BS 867 BETWEEN STRINGER 2R TO STRINGER 3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ; B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A7901 SHEET 66; REV A.<BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK SUPPORT ANGLE BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AT AFT CARGO COMPARTMENT 2024-763733<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N:A23325478; DUE DATE:07-JAN-25.;[02] REPLACED SUPPORT ANGLE AND FASTENERS BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AT AFT CARGO COMPARTMENT. I.A.W. B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #147A7221; SHEET 17; REV D.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED SUPPORT ANGLE AND FASTENERS BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AT AFT CARGO COMPARTMENT. I.A.W. B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DRAWING #147A7221; SHEET 17; REV D.<BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: GUSSET — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK GUSSET BS 500D AND STRINGER 19R AT FWD CARGO COMPARTMENT 2024-763726<[01] REPLACED GUSSET LOCATED BS 500D AND STRINGER 19R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 ;SHEET 209 ;REV -. SEE INDIVIDUAL SIGNS-OFF BELOW;[02] REPLACED GUSSET LOCATED BS 500D AND STRINGER 19R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 ;SHEET 209 ;REV -. SEE INDIVIDUAL SIGNS-OFF BELOW

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK SUPPORT ANGLE BS 867 AND STRINGER 26L AT AFT CARGO COMPARTMENT 2024-763734<[01] REPLACED SUPPORT ANGLE BS 867 AND STRINGER 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 149A8102 SHEET: 18 REV: - DWG: 149A8104 SHEET: 1 REV: B.<BR>TOOL USED: ELECTRONIC CALIPER P/N:500-196-30 S/N: A23325478 DUE DATE: 07/JAN/25.;[02] REPLACED SUPPORT ANGLE BS 867 AND STRINGER 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 149A8102 SHEET: 18 REV: - DWG: 149A8104 SHEET: 1 REV: B.<BR>TOOL USED: ELECTRONIC CALIPER P/N:500-196-30 S/N: A23325478 DUE DATE: 07/JAN/25.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CORROSION SUPPORT ZEE LBL 21 BETWEEN BS 727B TO BS 807 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LBL 21 BETWEEN BS 727 TO BS 847 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 146A7500 SHEET 137 REV -.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK SUPPORT BRACKET BS 947.5 AND STRINGER 26L AT AFT CARGO COMPARTMENT 2024-763732<[01] REPLACED SUPPORT BRACKET BS 947.5 AND STRINGER 26L AT AFT CARGO COMPARTMENT IAW SRM 737-700 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 149A8103 SHEET 7 REV A SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT BRACKET BS 947.5 AND STRINGER 26L AT AFT CARGO COMPARTMENT IAW SRM 737-700 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 149A8103 SHEET 7 REV A SEE INDIVIDUAL SIGN OFF BELOW<BR><BR>RII

Part: GUSSET — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK GUSSET BS 500D AND STRINGER 19L AT FWD CARGO COMPARTMENT 2024-763729<[01] REPLACED GUSSET LOC. BS 500D AND STRINGER 19L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV -.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED GUSSET LOC. BS 500D AND STRINGER 19L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV -.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK ANGLE - CLIP BS 400 AND STRINGER 26L FWD CARGO COMPARTMENT 2024-763727<[01] REPLACED ANGLE - CLIP BS 400 AND STRINGER 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DRAWING 143A7505 SHEET 81 REV -;[02] REPLACED ANGLE - CLIP BS 400 AND STRINGER 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DRAWING 143A7505 SHEET 81 REV -

Part: SUPPORT — CORRODED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CORROSION SUPPORT ZEE RBL 21 BETWEEN BS 727C TO BS 767 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE RBL 21 BETWEEN BS 727 TO BS 767 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG 146A7500; SHEET 137; REV -.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 48,336 hrs · 26,047 cycles

CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN 2024-763639<[01] REPLACED BRAKE PANEL LOCATED FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A0060 SHEET: 51 REV: - .;[02] CORRECTED STEP 1.<BR>REPLACED BRAKE PANEL LOCATED FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A0060 SHEET: 51 REV: - . <BR>SEE INDIVIDUAL SIGNS OFF BELOW.;[03] REPLACED BRAKE PANEL LOCATED FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A0060 SHEET: 51 REV: - . VERIFIED

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 48,336 hrs · 26,047 cycles

CRACK BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN 2024-763640<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A0060 SHEET: 51 REV: - SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED BRAKE PANEL FLOOR STRUCTURE BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A0060 SHEET: 51 REV: - VERIFIED

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 48,336 hrs · 26,047 cycles

CRACK LOWER SUPPORT ANGLE FLOOR STRUCTURE BS 695 AND RBL 24.75 AT CENTER SECTION 2024-763641<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 112820025 DUE DATE 22 JAN 25.;[02] REPLACED ANGLE LOCATED ON FLOOR STRUCTURES BS 695 AND RBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9;DWG 273A9110 SHEET 6 REV A;AND DWG 111A6000 SHEET 304 REV- SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED ANGLE LOCATED ON FLOOR STRUCTURES BS 695 AND RBL 24.75 AT CENTER SECTION IAW B737-700 SRM 51-40-02;SRM 51-10-02 ITEM 9;DWG 273A9110 SHEET 6 REV A;AND DWG 111A6000 SHEET 304 REV- SEE INDIVIDUAL SIGN OFF BELOW

Part: SEAL — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB 2024-763646<[01] REPLACED SEAL - PLATE LOC. ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW B737-700 SRM 51-40-02-0G-0 AND B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9.LENGTH OF CRACK IS: 2.000 INCH TOOL USED CALIPER P/N: 500-197?30;S/N: A22257522 DUE DATE: 29-AUG-25;[02] REPLACED SEAL - PLATE LOC. ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW B737-700 SRM 51-40-02-0G-0 AND B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9.LENGTH OF CRACK IS: 2.000 INCH TOOL USED CALIPER P/N: 500-197?30;S/N: A22257522 DUE DATE: 29-AUG-25

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2024-763622<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23399190; DUE DATE: 04-MAR-25.;[02] EQUIPMENT P/N XRP-3000; S/N 1998072; DUE DATE 23-JAN-25 WAS USED ON STEP 4;[03] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] TASK COMPLETED.

Part: DOUBLER — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK LOCATED ON EGPR SURROUND DOUBLER 2024-763604<[01] STEP 6. EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138103 AND DUE DATE: 10-JUN-25;[02] PERFORMED PERMANENT REPAIR LOCATED EXTERNAL GROUND ELECTRICAL POWER RECEPTACLE SURROUND DOUBLER BTW BS 227.8 TO BS 235.8 AND BTW STR 21R TO 24R AT LOWER FUSELAGE IAW B737-700 SRM 53-10-15-2R-4 REPAIR 4 ZONE 2 ALTERNATIVE 1 FIGURE 204 SHEET 1 AND 2. SEE INDIVIDUAL SIGN OFF BELOW.;[03] PERFORMED PERMANENT REPAIR LOCATED EXTERNAL GROUND ELECTRICAL POWER RECEPTACLE SURROUND DOUBLER BTW BS 227.8 TO BS 235.8 AND BTW STR 21R TO 24R AT LOWER FUSELAGE IAW B737-700 SRM 53-10-15-2R-4 REPAIR 4 ZONE 2 ALTERNATIVE 1 FIGURE 204 SHEET 1 AND 2. RII VERIFIED

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-763537<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23399190; DUE DATE: 04-MAR-25.;[02] EQUIPMENT P/N XRP-3000; S/N 1998072; DUE DATE 23-JAN-25 WAS USED ON STEP 4;[03] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-763540<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: B23399190; DUE DATE: 04-MAR-25.;[02] TOOL USED RADIOMETER PN. XRP-3000; SN. 1859843; DUE DATE. 10-MAR-25;[03] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] TASK COMPLETED.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-763535<[01] EQUIPMENT P/N XRP-3000; S/N 1998072; DUE DATE 23-JAN-25 WAS USED ON STEP 4;[02] REPAIRED CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[03] TASK COMPLETED.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK ON VAPOR BARRIER LOCATED BS663.75 LBL 34 APROX. MAIN WHEEL WELL 2024-763426<[01] REPLACED VAPOR BARRIER LOC. BS 663 BTW LBL5 TO LBL75 MAIN WHEEL WELL IAW B737-700 SRM 51-40-02-0G-0 AND DWG 111A1000 ;SHEET 259; REV A; DWG 111A1001 SHEET 444; REV A. DRILLED OF VAPOR BARRIER; REMOVAL AND INSTALLATION OF STRUCTURAL PARTS WAS DOCUMENTED ON TTG8Q00XHUXW;[02] CORRECTED STEP 1:REPLACED VAPOR BARRIER LOC. BS 663 BTW LBL5 TO LBL75 MAIN WHEEL WELL IAW B737-700 SRM 51-40-02-0G-0 AND DWG 111A1000 ;SHEET 259; REV A; DWG 111A1001 SHEET 444; REV A. LENGTH OF CRACK IS: 8.000? TOOL USED CALIPER P/N:500-193-30;S/N: 0037624 DUE DATE: 15-JAN-25.DRILLED OF VAPOR BARRIER; REMOVAL AND INSTALLATION OF STRUCTURAL PARTS WAS DOCUMENTED ON TTG8Q00XHUXW;[03] REPLACED VAPOR BARRIER LOC. BS 663 BTW LBL5 TO LBL75 MAIN WHEEL WELL IAW B737-700 SRM 51-40-02-0G-0 AND DWG 111A1000 ;SHEET 259; REV A; DWG 111A1001 SHEET 444; REV A. LENGTH OF CRACK IS: 8.000? TOOL USED CALIPER P/N:500-193-30;S/N: 0037624 DUE DATE: 15-JAN-25.DRILLED OF VAPOR BARRIER; REMOVAL AND INSTALLATION OF STRUCTURAL PARTS WAS DOCUMENTED ON TTG8Q00XHUXW

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 48,336 hrs · 26,047 cycles

DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT SIDE AT PASSENGER CABIN (10 EA) 2024-763453<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT SIDE AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802;[02] COMPLETED JOB

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT. FABRICATED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT. I.A.W. B737-700 AMM 25-52-01-201-801. STEP 1.F. AND DRAWING #453A1610; SHEET 29; REV B. AND APPLIED PROTECTIVE TREATMENT ON PANEL IAW SRM 51-20-01.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 48,336 hrs · 26,047 cycles

CRACK ON VAPOR BARRIER LOCATED BS663.75 RBL 34 APROX. MAIN WHEEL WELL 2024-763446<[01] TOOL USED ON STEP 11. ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190984811; CAL DUE DATE: 11-JAN-25;[02] REPAIRED VAPOR BARRIER LOCATED BS663.75 RBL 34 APROX. MAIN WHEEL WELL IAW B737-700 SRM 51-70-04-2R- 10 REPAIR 10. REFER INDIVIDUAL SIGNOFF BELOW;[03] REPAIRED VAPOR BARRIER LOCATED BS663.75 RBL 34 APROX. MAIN WHEEL WELL IAW B737-700 SRM 51-70-04-2R- 10 REPAIR 10. REFER INDIVIDUAL SIGNOFF BELOW. RII COMPLETED.

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 48,336 hrs · 26,047 cycles

DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT SIDE AT PASSENGER CABIN (10 EA) 2024-763449<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT SIDE AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802;[02] COMPLETED JOB

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 47,498 hrs · 25,564 cycles

EMERGENCY LIGHTS AT RT EMERGENCY DOOR EXIT INOP<[01] R/R BATTERY PACK M1669 IAW AMM 33-51-06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,023 hrs · 24,686 cycles

EXTERIOR EMERGENCY LIGHT BESIDE AFT SVC DOOR WILL NOT ILLUMINATE.<[01] RELAMPED PER AMM 33-51-00.

Part: GIRT BAR — LOOSE (FWD GALLEY DOOR) · airframe 45,587 hrs · 24,441 cycles

FWD GALLEY DOORGIRT BAR LOOSE.EASILY FALLS OFFDOOR WHEN STOWED IN BRACKETS ON GROUND<[01] ADJUSTED GIRT BAR RETAINER CLEAT PER AMM 25-66-01 AND SIP

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 45,430 hrs · 24,341 cycles

FORWARD ENTRY AND GALLEY EMERGENCY LIGHTS INOP.<[01] R/R CHARGER ASSEMBLY AND BATTERY PACK PER AMM 33-51-06.;[02] LOCATION M1674.

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 44,269 hrs · 23,680 cycles

R/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED<[01] R&R R/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL. IAW AMM 53-31-31

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 44,269 hrs · 23,680 cycles

L/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED<[01] R&R L/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL IAW AMM 53-31-31.

Part: SLIDE — LOW (ZN 200 FUS TOP) · airframe 43,077 hrs · 22,951 cycles

AFT GALLEY SERVICE DOOR SLIDE PRESSURE GAUGE READS LOW<[01] REMOVED AND REPLACED AFT GALLEY SERVICE DOOR ESCAPE SLIDE IN REF TO AMM 25-66-01. ACCOMPLISHED MT725-61-06

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 42,328 hrs · 22,503 cycles

AFT CARGO COMPARTMENT FWD CORNER SCUFF PLATE CRACKED<[01] RECEIVED AFT CARGO COMPT FWD CORNER SCUFF PLATE P/N: 146A8341-7; PO#1782375. REF TASK CARD: TTG8Q004ECQ5 FOR INSTALLATION;[02] VERIFIED STEP 1

Part: STIFFENER — CRACKED (BS 663) · airframe 42,328 hrs · 22,503 cycles

STIFFENER CRACKED AT CENTER WING LOWER FUSELAGE L/H SIDE VAPOR BARRIER BULKHEAD STA 663.75 @ LBL28 MKD DOT<[01] REMOVED FASTENERS FOR ACCESS STIFFENER DAMAGED AT L/H SIDE VAPOR BARRIER BULKHEAD STA; 663.75 LBL 28'. REF. SRM. 51-40-02;[02] OK TO INSTALL NEW STIFFNER;[03] INSTALLED STIFFENER AT CENTER WING LOWER FUSELAGE L/H SIDE VAPOR BARRIER BULKHEAD STA 663.75 AT LBL28 AS PER BOEING 737-700 SRM 51-40-02-OG-0;[04] VERIFIED STEP 3.

Part: CHANNEL — CRACKED (ZONE 100) · airframe 42,328 hrs · 22,503 cycles

AFT CARGO COMPARTMENT RH STA 747+6 Z-CHANNEL CRACKED<[01] CUT AND REMOVED DAMAGED SECTION OF ZEE-CHANNEL FROM STA 727C+11 TO 767 PER REF SRM 53-00-53-2R-5;[02] FABRICATED NEW ZEE CHANNEL SECTION FROM STA 727C+11 TO 767; AND NEW REPAIR SPLICE AT 727C+11 PER REF SRM 53-00-53-2R-5;[03] EDIT STEP #2: LOCATED AND DRILLED NEW ZEE CHANNEL SECTION FROM STA 727C+11 TO 767; AND NEW REPAIR SPLICE AT 727C+11 PER REF SRM 53-00-53-2R-5;[04] VERIFIED 1 AND 3;[05] OK TO TREAT AND PRIME REPAIR PIECES;[06] TREATED AND PRIMED NEW REPAIR PIECES PER REF AMM 51-21-41-370-804 AND 51-21-72-370-804;[07] VERIFIED 6. OK TO ASSEMBLE PARTS;[08] ASSEMBLED Z-CHANNEL AND REPAIR SPLICE PER REF SRM 53-00-53-2R-5.;[09] VERIFIED STEP 8;[10] ALL STEPS COMPLETED

Part: CHANNEL — CRACKED (ZONE 100) · airframe 42,328 hrs · 22,503 cycles

AFT CARGO LH STA 807 Z-CHANNEL CRACKED<[01] LOCTED AND DRILL 2EA NEW Z CHANNEL SECTIONS FROM STA 727E + 13 TO STA 847 PER REF SRM 51-40-05-0G-0;[02] FABRICATED NEW SPLICE BETWEEN STA 727 E TO STA 747 PER REF SRM 53-00-53-2R-5 REPAIR 5;[03] VERIFIED 1 AND 2. OK TO TREAT AND PRIME REPAIR PARTS;[04] TREATED AND PRIMED NEW REPAIR PIECES PER REF AMM 51-21-41-370-804 AND 51-21-72-370-804;[05] VERIFIED 4. OK TO ASSEMBLE PARTS;[06] LOCATED AND DRILLED 2EA NEW Z CHANNEL SECTIONS FROM STA 727 TO 727E + 13 AND FROM STA727 E +13 TO STA 847 PER REF SRM 51-40-05-0G-0;[07] VERIFIED STEP 6; CORRECTION FOR STEP 1;[08] OK TO ASSEMBLE PARTS - Z CHANNEL FROM 727 TO 727E+13;[09] ASSEMBLED PARTS Z CHANNEL SECTION 727 TO 727 E +13 AND SECTION 727 E +13 TO 847 WITH REPAIR SPLICE AT 727 E +13; PER REF SRM 53-00-53-2R-5.;[10] VERIFIED STEP 9

Part: PANEL — CRACKED (ZONE 100) · airframe 42,328 hrs · 22,503 cycles

FOUND AFT CARGO PANEL 142NW CRACKED. RECEIVED AFT CARGO PANEL . REFERENCE TASK CARD TTG8Q00G5USN FOR PANEL INSTALLATION.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 42,328 hrs · 22,503 cycles

'CORROSION' AFT CARGO COMPARTMENT STA 727B EXFOLIATED CORROSIN AFT CARGO LH STA 727B STR 25L -CHANNEL<[01] Z CHANNEL PN:(146A7502-29) REPLACED FROM STA 727 TO 847; FOR WORK ACCOMPLISHED REFERENCE TASK CARD #TTG8Q00H6RQJ;[02] VERIFIED STEP 1

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 42,328 hrs · 22,503 cycles

AFT CARGO COMPARTMENT AFT CORNER SCUFF PLATE CRACKE<[01] NEW CORNER SCUFF PLATE WILL BE INSTALL ON WORK CARD TTG8Q004ECQ5;[02] VERIFIED STEP 1

Part: PANEL — DAMAGED (ZONE 100) · airframe 42,328 hrs · 22,503 cycles

PANEL 661CB ELONGATED HOLES VARIOUS<[01] MEASUREMENTS;[02] REPAIRED AREAS AT PANEL#661CB (ELONGATED HOLES) AS PER BOEING737 SRM 51-70-04-2R-9. MATERIAL USED EY3804 PO#!800218PLUS BMS9-3-120TYD CL7.;[03] VERIFIED STEP# 1 AND 2;[04] LOCATED AND DRILLED FASTER HOLE SIZES FOR PANEL# 661CB AS PER B 737-700 SRM 51-40-05-0G-0.;[05] (FINAL) REPAIRED AREAS AT PANEL#661CB (ELONGATED HOLES) AS PER BOEING737 SRM 51-70-04-2R-9. MATERIAL USED EY3804 PO#!800218PLUS BMS9-3-120TYD CL7 ; LOCATED AND DRILLED FASTER HOLE SIZES FOR PANEL# 661CB AS PER B 737-700 SRM 51-40-05-0G-0.;[06] (CORRECTING STEP #5) (FINAL) REPAIRED AREAS AT PANEL#661CB (ELONGATED HOLES) AS PER BOEING737 SRM 51-70-04-2R-0. MATERIAL USED EY3804 PO#!800218 PLUS BMS9-3-120TYD CL7 ; LOCATED AND DRILLED FASTER HOLE SIZES FOR PANEL# 661CB AS PER B 737-700 SRM 51-40-05-0G-0.;[07] VERIFIED STEP #6.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 42,328 hrs · 22,503 cycles

CENTER WING REAR SPAR VAPOR WEB LEFT SIDE LWR AREA CRACKED<[01] MEASUREMENTS;[02] PERFORMED VISUAL INSPECTION ON L/H VAPOR BARRIER AND FOUND CRACK OF 11' PER B737 NDTM 51-05-01.;[03] PERFORMED STOP DRILL SIZE 0.25 DIAMETER AT THE END OF THE CRACK PER B737 SRM 57-10-10-2R-2 STEP 6.B;[04] PREPARED DAMAGED AREA ON L/H VAPOR BARRIER FOR REPAIR PER B737 SRM 51-70-04-2R-10 AND 51-70-04-2R-0 PARAGRAPH 4.E. REPAIRED L/H VAPOR BARRIER AT DAMAGED AREA PER B737 SRM 51-70-2R-10 AND SRM 51-70-04-2R-0. PERFORMED TAP TEST ON VAPOR BARRIER AND FOUND NO DELAMINATION AND NO COMPOSITE MATERIAL DAMAGE PER B737 NDTM 51-05-01.

Part: LIGHT — MISSING · airframe 39,574 hrs · 20,879 cycles

L2 DOOR EMERGENCY EXIT SIGN MISSING DIRECTION ARROW. / [01] REMOVED AND REPLACED L2 DOOR EMERGENCY EXIT SIGN LENS REF AMM 33-51-01.;[02] C/W

Part: GIRT BAR — MISSING (R1 DOOR) · airframe 39,283 hrs · 20,730 cycles

FWD SERVICE DOOR SLIDE GIRT BAR MISSING PLASTIC STOP ; / [01] INSTALLED PLASTIC STOP ON FWD SERVICE DOOR SLIDE GIRT BAR PER AMM 25-66-01

Part: ACCESS PANEL — BROKEN (HORIZONTAL STAB) · airframe 36,671 hrs · 19,328 cycles

BROKEN TRAILING EDGE BOLT ACCESS PANELS AT LT HORIZONTAL STABILIZER (265 EA) / REPLACED TRAILING EDGE BOLT ACCESS PANELS AT LT HORIZONTAL STABILIZER (265 E/A) IAW B737-700 SRM 51-40-02

Part: BRACKET — BROKEN (RT WING) · airframe 36,671 hrs · 19,328 cycles

BROKEN TRAILING EDGE LOWER INBOARD FIXED CLIP BRACKET AT RT WING / REPLACED BROKEN TRAILING EDGE LOWER INBOARD FIXED CLIP BRACKET AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE

Part: RETAINER — CRACKED (ELEVATOR) · airframe 36,671 hrs · 19,328 cycles

CRACK ELEVATOR PIN RETAINER ON THE ELEVATOR TAB CONTROL MECHANISM AT RT HORIZONTAL STABILIZER (1 EA) / REPLACED ELEVATOR PIN RETAINER ON THE ELEVATOR TAB CONTROL MECHANISM AT RT HORIZONTAL STABILIZER (1EA) IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 AIPC 31-34-09 NOTE E SHEET 004 REPLACED ELEVATOR P/N RETAINER DUE TO DAMAGE FOUND

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 36,671 hrs · 19,328 cycles

CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 847 TO BS 867; RBL 26 AT LEVEL STRINGER 25R AFT CARGO COMPARTMENT / REPLACED WEB-INTERCOSTAL (SHIELD) LOCATED BETWEEN BS 847 TO BS 867 RBL 26 AT LEVEL STRINGER 25R AFT CARGO COMPARTMENT WL 153.5 IAW B737-700 SRM 51-10 -02 ITEM 9; SRM 51-40-02 AND DRAWING # 146A0081 SHEET 25 REV A DUE TO NOT FOUND ALLOWABLE DAMAGE LIMITS IN B737-700 SRM

Part: BRACKET — BROKEN (KEELBEAM) · airframe 36,671 hrs · 19,328 cycles

BROKEN BRACKET KEEL BEAM LOCATED STA 556 AT LEVEL LBL 5 AT LOWER FUSELAGE / REPLACED BRACKET (FITTING) KEEL BEAM LOCATED STA 556 AT LEVEL LBL 5 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9

Part: WEB — CORRODED (ZONE 100) · airframe 36,671 hrs · 19,328 cycles

CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 767 TO BS 794; RBL26 AT LEVEL STRINGER 25R AFT CARGO COMPARTMENT WL 153.5 / REPLACED WEB INTERCOSTAL LOCATED BETWEEN BS 767 TO BS 794 RBL 26 AT LEVEL STRINGER 25R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG # 146A0081 REV A

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 36,671 hrs · 19,328 cycles

CRACK ACCESS PANEL 642BB LOCATED INTERNAL AERA RT WING / REPAIRED ACCESS PANEL 642BB LOCATED ON INTERNAL AREA AT RT WING ASPER B737-700 SRM 51-70-04-2R-2 REPAIR 2

Part: GUSSET — CRACKED (ZONE 100) · airframe 36,671 hrs · 19,328 cycles

CRACK GUSSET LOCATED BS 500D AT LEVEL STRINGER 19L FWD CARGO COMPATMENT / REPLACED GUSSET LOCBS 500D AT LEVEL STRINGER 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV.-

Part: STRINGER — CRACKED (ZONE 100) · airframe 36,671 hrs · 19,328 cycles

CRACK STRINGER 23L LOCATED BS 540 FWD CARGO COMPARTMENT / REPAIRED STRINGER 23L LOCATED BTW BS 500D AND BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. REPAIR PARTS INSTALLED ANGLE-3 (2EA) MATERIAL USED 7075/0.040' PO 2020 180353 CHANNEL-2 MATERIAL USED 7075/0.040' PO 2020-180353 STRINGER SECTION -7 MATERIAL USED 7075/0.036' PO 2020-194719

Part: SUPPORT — CORRODED (ZONE 100) · airframe 36,671 hrs · 19,328 cycles

CORROSION SUPPORT ZEE LOCATED BS 420 TO BS 440; RBL 25; STRINGER 26R AT FWD CARGO COMPARTMENT WL 153.5 / REPLACED SUPPORT ZEE LOCATED BS420 TO BS440; RBL 25 STRINGER 26R AT FWD CARGO COMPARTMENT WL 153.5 P/N 143A8126-21 IAW B737-700 SRM 51-40-02 AND DWG 143A00 80 REV - SHEET 29; BATCH NUMBER SW 2021000212

Part: GUSSET — CRACKED (ZONE 100) · airframe 36,671 hrs · 19,328 cycles

CRACK GUSSET LOCATED BS 500D AL LEVEL STRINGER 19R FWD CARGO COMPARTMENT / REPLACED GUSSET LOC BS 500D AT LEVEL STRINGE 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV .-

Part: SUPPORT — CORRODED (ZONE 100) · airframe 36,671 hrs · 19,328 cycles

CORROSION SUPPORT ZEE LOCATED BS 400 TO BS 420; RBL 25; AT LEVEL STRINGER 26R AT FWD CARGO COMPARTMENT WL 153.5 / REPLACED SUPPORT ZEE LOCATED BS 400 TO BS 420 RBL 25 AT LEVEL STRINGER 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG # 142A7500

Part: SUPPORT — CORRODED (ZONE 100) · airframe 36,671 hrs · 19,328 cycles

CORROSION SUPPORT ZEE LOCATED BS 492 TO BS500A AT LEVEL STRINGER 26R; RBL 25 AT FWD CARGO COMPARTMENT WL 153.5 / REPLACED SUPPORT ZEE LOC BS 492 TO BS 500D AT LEVEL STRINGER 26R; RBL 25 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 DRAWING # 143A0080 REV -

Part: WEB — CRACKED (ZONE 200) · airframe 36,671 hrs · 19,328 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED ON BS277 TO BS294.5 AT LEVEL BL O FWD GALLEY AND LAV (1 EA) / REPLACED WEB-INTERCOSTAL FLOOR STRUCTURE LOCATED ON BS277 TO BS 294..5 AT LEVEL BL0 FWD GALLEY AND LAV (1EA) IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 141A5400 SHEET 02 REV - AND DWG 141A5410 SHEET 3 REV A

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 36,671 hrs · 19,328 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS380 TO BS400 AT LEVEL BL0 AT FWD GALLEY AREA / REPLACED WEB-INTERCOSTAL ANGLE LOC ON FLOOR STRUCTURE BS380 TO BS400 AT LEVEL BLO AT FWD GALLEY AREA PN 143A5410-170 IAW B737-700 DWG #43A5400 SHEET 114 AND SRM 51-40-02

Part: WEB — CRACKED (ZONE 200) · airframe 36,671 hrs · 19,328 cycles

CRACK WEB LOCATED BTW BS 312 TO BS 328 AT LEVEL RBBL 30 AT FWD GALLEY AREA / REPLACED WEB LOC BTW BS 312 TO BS328 AT LEVEL RBBL30 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 SRM 51-40-02 AND DWG 141A5400 SHEET 39EV DWG 141A5410 SHEET 12 REV A

Part: WEB — CRACKED (ZONE 200) · airframe 36,671 hrs · 19,328 cycles

CRACK WEB LOCATED BTW BS 344 TO BS 360 AT BL 0 AT FWD GALLEY AREA / REPLACED WEB (INTERCOSTAL) LOCATED BTW BS 344 TO BS 360 AT BLO AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02 AND DWG # 141A5400 REV -

Part: LIGHT — CRACKED (CABIN) · airframe 36,671 hrs · 19,328 cycles

CRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT CENTER SECTION (5 EA) / REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT CENTER SECTION (5EA) IAW AMM 33-51- 15-400-802

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 36,671 hrs · 19,328 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED ON BS294.5 TO BS303.4 AT LEVEL STR16L FWD GALLEY AND LAV / REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED ON BS 294.5 TO BS 303.4 AT LEVEL STR 16L FWD GALLEY AND LAV P/N 141A8181V51 IAW B737-700 DWG #141A8180 SHEET 27 REV C SRM 51-40-02

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 36,671 hrs · 19,328 cycles

CRACK TIE CLIP LOCATED ON BS 277 AT LEVEL STR 10R AT PASSENGER CABIN / REPLACED TIE CLIP LOCATED ON BS277 AT LEVEL STR 10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02 AND DWG # 141A1110 REV - 141A8380 REV -

Part: SUPPORT ANGLE — CRACKED (VERTICAL STAB) · airframe 36,671 hrs · 19,328 cycles

CRACK LEADING EDGE ON SUPPORT ANGLE LOCATED INTERNAL AREA AT VERTICAL STABILIZER / REPLACED SUPPORT ANGLE LOC INTERNAL AREA AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DRAWING # 176A3101 REV -

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,671 hrs · 19,328 cycles

CORROSION FLOOR STRUCTURE INNER CHORD LOCATED BTW BS 967 TO BS 1006 AT LEVEL STR 17R AND RBBL 53 AT AFT GALLEY AREA / REPLACED INNER CHORD P/N 147A8540U8 AT SMR0 LOCATED BETWEEN BS887 TO BS1006 AT LEVEL STR 17R AND RBBL 53 AT AFT GALLEY AREA IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING #147A8501 REV A

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 36,671 hrs · 19,328 cycles

CRACK LEADING EDGE RIB LOCATED LE STA 114.55 RT HORIZONTAL STAB / REPLACED RIB LOC LE STA 114.55 RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 1186A1001 REV A

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,671 hrs · 19,328 cycles

CORROSION EXTERNAL SKIN AROUND CUT OUT WATER SERVICE _DOOR AT LOWER FUSELAGE / REMOVED CORROSION LOC EXTERNAL SKIN AROUND CUT OUT WATER SERVICE DOOR AT LOWER FUSELAGE EVALUATED REWORKED AREA AND FOUND WITHIN LIMIT IAW B737-700 SRM 53-00-01-1A-1 PAR 4B(2)(B) FIG 103 DETAIL D MEASURRED OF REWORKED AREA ARE L=13.949' W=11.561', MINIMUN REMAINING THICKNESS IS 0.058'

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,671 hrs · 19,328 cycles

CORROSION EXTERNAL SKIN BS 1016 BETWEEN STR 23R AND STR 24L AT LOWER FUSELAGE. REMOVED CORROSION LOC ON EXTERNAL SKIN BS 1016 BTW STR 23R AND STR 24L AT LOWER FUSELAGE EVALUATED REWORKED AREA AND FOUND WITHIN LIMITS IAW B737-700 P1 AND P3 SRM 53-00-01-1A-1 PAR 4B(2)(B) FIG 103 DETAIL C AND P2 AND P4 SRM 53-00-01-1A-1 PAR 4C(2) FIG 103 DETAIL C MEASURED OF REWORKED AREA P1: L= 97' W=1.960' P2: L=44.5' W=0.623' P3: L=3.800' W=0.393' P4: L=12.500' W=0.400' TOOL USED CALIPER P/N 500-193 S/N 1116081 DUE DATE 24SEP21 AND MRT P1: P1=0.063' P2=0.080' P3=0.071' P4=0.080'.

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,671 hrs · 19,328 cycles

CORROSION EXTERNAL SKIN TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,671 hrs · 19,328 cycles

SUPPLEMENTAL INFORMATION: CORROSION EXTERNAL SKIN AROUND DRAIN HOLE BTW BS 947 AND BS 967 AND BT W STR 26L AND 27L AT LOWER FUSELAGE / REMOVED CORROSION LOC ON EXTERNAL SKIN AROUND DRAIN HOLE BTW BS947 AND BS967 AND BTW STR26L AND 27L LOWER FUSELAGE, EVALUATED REWORKED AREA AND FOUND WITHIN LIMITS I.A.W. B737-700 SRM 53-00-01-1A-1PARAGRAPH 4.B, ITEM 2 FIG 103, DETAIL C ALLOWABLE ALLOWABLE DAMAGE 1, MEASURE REWORKED AREA L=3.295", W=3.136", TOOL USED CALIPER P/N: 500-464, S/N: B12030932 AND MINIMUM REMAINING THICKNESS

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,671 hrs · 19,328 cycles

CORROSION EXTERNAL SKIN AROUND SAFETY RELIEF VALVE CUT OUT BETWEEN BS 967 AND BS 987 AND BETWEEN STR 26R AND STR 27R AT LOWER FUSELAGE. REMOVED CORROSION LOC EXTERNAL SKIN AROUND SAFETY RELIEF VALVE CUT OUT BTW BS967 AND BS987 AND BTW STR26R AND STR27R AT LOWER FUSELAGE; EVALUATED REWORKED AREA AND FOUND WITHIN LIMITS I.A.W. B737-700 SRM 53-00-01-1A-1 PARAGRAPH 4B;ITEM 2 DETAIL C ALLOWABLE DAMAGE 1 MEASURE OF REWORKED AREA ARE: L=9.271'; W=5.428' TOOL USED CALIPER P/N: 500-197-30; S/N: A18229521 DUE DATE: 02 AUG 21 AND MINIMUM REMAINING THICKNESS ARE 0.057'

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,671 hrs · 19,328 cycles

CORROSION EXTERNAL SKIN AROUND DRAIN HOLE BTW BS 967 AND BS 987 AND BTW STR 26L AND STR 27L AT LOWER FUSELAGE / REMOVED CORROSION LOC AT EXTERNAL SKIN ARROUND DRAIN HOLE BTW STR26L AND STR27L AT LOWER FUSELAGE AND EVALUATED REWORKED AREA AND FOUND WITHIN LIMITS I.A.W. B737-700 SRM 53-00-01-2A-1 PARAGRAPH 4.B ITEM 2 FIG. 103 DETAIL C; MEASURE REWORKED AREA ARE: L=3.229'; W=2.482';

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 36,671 hrs · 19,328 cycles

CRACK VAPOR BARRIER LH SIDE AT MAIN WHEEL WELL COMPARTME / REPAIRED VAPOR BARRIER LH SIDE AT MAIN WHEEL WELL COMPARTMENT ASPER B737-700 SRM 51-70-04-2R-10 REPAIR 10 TOOL USED CALIPER PN 500-197-30 SN 15120589 DUE DATE 14SEP-21 HOT BONDER PN HCS9000B SN 15092096 DUE DATE 14-DEC-21 SCALE PN CL5000 SN AE-39089 DUE DATE 07-MAY-21 HOT BONDER PN HCS9200B SN 18175478 DUE DATE 07-JUL-21

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,671 hrs · 19,328 cycles

CORROSION EXTERNAL SKIN BS 887 BETWEEN STR 23R AND 23L AT LOWER FUSELAGE / REMOVED CRROSION LOC ON EXTERNAL SKIN P1 STA 886TO STA 887BTW STR23R TO STR23L.THE MEASURE OF REWORKED IS L=77' W=1.875' AND P2 STA 887 TO STA 888 BTW STA 23R TO STR23L. THE MEASURE OF REWORKED IS L=77' W= 1.967' TOOL USED CALIPER 700-113-10 SN 002865 DUE DATE 10OCT21 AND FOUND WITHIN LIMITS IAW B737-700 P1 SRM 53-00-01-1A-5 PARAGRAPH 4A ITEM 2 DETAIL C;E TABLE 101 AND P2 SRM 53-00-01-1A-1 PARAGRAPH 4B ITEM2 DETAIL C E AND MINIMUN REMAINING THICKNESS ARE P1 0.076' P2 0.054'

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,671 hrs · 19,328 cycles

CORROSION EXTERNAL SKIN AROUND CUT OUT POWERED OUTFLOW VALVE BETWEEN BS 967 AND BS 987 AND BETWEEN STR 23R AND STR 25R AT LOWER FUSELAGE. REMOVED CORROSION LOC ON EXTERNAL SKIN AROUND CUT OUT POWERED OUTFLOW VALVE BTW BS967 AND BS987 AND BTW STR 23R AND STR 25R AT LOWER FUSELAGE EVALUATED REWORKED AREA AND FOUND WITHIN LIMITS IAW B737-700 SRM 53-00-01-1A-1 PAR 4B(2)(B) FIG 103 DETAIL D AND FIG 104 MEASURE REWORKED AREA ARE P1: L=0.893' W= 0.815' P2: L=4.276' W=2.915' TOOL USED CALIPER P/N 500-752-10 S/N 15183542 DUE DATE 04-OCT-11 AND MINIMUN REMAINING THICKNESS IS 0.063'.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 36,671 hrs · 19,328 cycles

CRACK VAPOR BARRIER RT SIDE AT MAIN WHEEL WELL COMPARTME / REPAIRED VAPOR BARRIER RT SIDE AT MAIN WHEEL WELL COMPARTMENT AS PER B737-700SRM 51-70-04-2R REPAIR 10 TOOL USED CALIPER PN 500-197-30SN 15120589 DUE DATE 14-SEP-21 HOT BONDER PN HCS9000B SN 18175469 DUE DATE 08-JUL-21 SCALE PN CL5000 SN AE-39089 DUE DATE 07-MAY-21 HOT BONDER PN HCS9200B SN B175478 DUE DATE 07-JUL-21

Part: SKIN — CORRODED (FUSELAGE) · airframe 36,671 hrs · 19,328 cycles

SUPPLEMENTAL INFORMATION: CORROSION EXTERNAL SKIN WATER SERVICE DOOR 146AR AT LOWER FUSELAGE / REMOVED CORROSION LOC EXTERNAL SKIN WATER SERVICE DOOR 146AR AT LOWER FUSELAGE EVALUATED REWORKED AREA AND FOUND WITHIN LIMITS IAW B737-700 SRM 52-40-01-1A-5 PARAGRAPH 4A ITEM 2 DETAIL B MEASURED OF REWORKED AREA ARE P1: L=3.407' W=3.176' P2: L= 7.498' W=4.801' TOOL USED CALIPER P/N 500-197-30 S/N A18229521 DUE DATE 02-AUG-21 AND MINIMUM REMAINING THICKNESS IS P1=0.125' P2=0.116' NO FURTHER ACTION OR INSPECTION REQUIRED

Part: STRAP — CORRODED (FUSELAGE SKIN) · airframe 36,671 hrs · 19,328 cycles

CORROSION EXTERNAL SKIN STRAP BELOW TOILET SERVICE DOOR CUTOUT AT LOWER FUSELAGE.

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 36,671 hrs · 19,328 cycles

SUPPLEMENTAL INFORMATION: CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 18 INCH FROM REAR SPAR AT RT HORIZONTAL STABILIZER / PERFORMED PERMANENT REPAIR INPAR RIB STA STA 120.30 AND 18 INCH FROM REAR SPAR IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4 MATERIAL USED KIT T-SECTION PN 55100003-01 BATCH 2020002209

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 36,671 hrs · 19,328 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 17 INCH FROM FRONT SPAR AT RT HORIZONTAL STABILIZER.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 36,671 hrs · 19,328 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 9 INCH FROM REAR SPAR AT RT HORIZONTAL STABILIZER / PERFORMED PERMANENT REPAIR INSPAR RIB STAB STA 120.30 AND 9 INCHES FROM REAR SPAR AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 MATERIAL USED BAC1490-2734 PO 2015 503061 AND KIT T SECTION P/N 55100003-01 BATCH 2020002209

Part: SKIN — DENTED (ZONE 200) · airframe 36,671 hrs · 19,328 cycles

DENT EXTERNAL SKIN BS 992.8 MORE 10 INCH AND AT STR 15R AT UPPER FUSELAGE / REPAIRED EXTERNAL SKIN LOCATED BTW BS 992.8 AND BS 1016 BTW STR 13R AND STR 17R IAW EA # 53-0013-21 REV 0 AND 21-153-00187 REV IR. FOR REQUIREMENT INSPECTION SEE TLD # T080517

Part: RETAINER — CRACKED (NACELLE ACCESS) · airframe 36,671 hrs · 19,328 cycles

CRACK SEAL RETAINER ACCESS PANEL 441AR AND 441AL RT ENGINE / REPLACED SEAL RETAINERS ACCESS PANEL 441AR AND 441AL RT ENGINE IAW B737-700 SRM 51-40-02

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 36,478 hrs · 19,211 cycles

R2 DOOR SLIDE GIRT IS DRAGGING ON THE FLOOR. ADJUSTED Z FOLD, PER AMM 25-66-01.

Part: RIVET — LOOSE (R1 DOOR GIRT BAR) · airframe 35,855 hrs · 18,834 cycles

FWD SERVICE DOOR SLIDE BOX GIRT BAR STOW CLIP LOOSE ON LEFT SIDE. REMOVED AND REPLACED RIVETS IAW SRM 51-40-02.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 34,467 hrs · 17,990 cycles

L/H HORIZONTAL STABILIZER CRACKED ON LOWER #2 VERTICAL STIFFENER ON #4 INSPAR RIB AT STAB. STA. 120.30. / R&R #4 RIB PER SRM.

Part: RIB — DAMAGED (HORIZONTAL STAB) · airframe 34,467 hrs · 17,990 cycles

L/H HORIZ STAB #4 INSPAR RIB AT STAB STA 120.30 LOWER FLANGE I/B SIDE; 21ST FASTENER HOLE BACK FROM FWD STIFFENER IS OBLONG / R&R'D L/H STAB #4 RIB AT STATION 120.30 PER SRM 51-40-02 & 51-10-02.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 34,467 hrs · 17,990 cycles

L/H HORIZONTAL STABILIZER #4 INSPAR RIB AT STAB. STA. 120.30 LOWER FLANGE OF RIB JUST AFT OF 10TH FASTENER HOLE FROM AFT STIFFENER CRACKED. / R&R #4 RIB PER SRM.

Part: RIB — DAMAGED (HORIZONAL STAB) · airframe 34,467 hrs · 17,990 cycles

L/H HORIZ STAN #4 INSPAR RIB AT STAB STA 120.30 FWD STIFFENER LOWER FASTENER HOLE IS OBLONG / R&R'D L/H STAB #4 RIB AT STATION 120.30 PER SRM 51-40-02 & 51-10-02.

Part: RIB — DAMAGED (HORIZONTAL STAB) · airframe 34,467 hrs · 17,990 cycles

L/H HORIZ STAB #4 INSPAR RIB AT STAB STA 120.30 LOWER FLANGE I/B SIDE; 24TH FASTENER HOLE BACK FROM FWD STIFFENER IS OBLONG / R&R'D L/H STAB #4 RIB AT STATION 120.30 PER SRM 51-40-02 & 51-10-02

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 34,467 hrs · 17,990 cycles

L/H HORIZONTAL STABILIZER #4 INSPAR RIB AT STAB. STA. 120.30 LOWER FLANGE INBOARD SIDE, 10TH FASTENER HOLE FORWARD OF AT STIFFENER CRACKED. / R&R #4 RIB PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 34,467 hrs · 17,990 cycles

L/H HORIZONTAL STABILIZER CRACKED ON LOWER #3 VERTICAL STIFFENER ON #4 INSPAR RIB AT STAB. STA. 120.30. / R&R #4 RIB PER SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 34,467 hrs · 17,990 cycles

L/H HORIZONTAL STABILIZER #4 IN SPAR RIB AT STAB. STA. 120.30 LOWER FLANGE INBOARD SIDE, 19TH FASTENER HOLE BACK FROM FORWARD STIFFENER CRACKED. / R&R #4 RIB PER SRM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 34,228 hrs · 17,861 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 34,228 hrs · 17,861 cycles

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

Part: SEAL — CRACKED (LH HOR STAB) · airframe 34,223 hrs · 17,858 cycles

TAIL LEFT HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED. / R&R TAIL LEFT HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL REF AMM 53-31-31.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,706 hrs · 16,926 cycles

BULL NOSE LIGHT INOP. R&R LIGHT PER AMM.

Part: FUSE — BLOWN (EXIT LIGHT) · airframe 32,216 hrs · 16,636 cycles

R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. R&R FUSE PER AMM.

Part: GLOWSTRIP — DELAMINATED (CABIN) · airframe 32,216 hrs · 16,636 cycles

RT FORWARD PHOTO ILLUMINATION STRIP DELAMINATED. R&R STRIP PER DWG.

Part: SKIN — ELONGATED (AFT CARGO DOOR) · airframe 31,350 hrs · 16,125 cycles

AFT CARGO DOOR HANDLE HOUSING HAS 6EA DOOR SKIN FASTENER HOLES ELONGATED . / REMOVED AND REPLACED AFT CARGO DOOR PER AMM 52-31-00; TAG NO: 546439 PN ON: 146A6110-29 SN ON: 002266 PN OFF: SN OFF: 002818

Part: RIVET — MISSING (R1 DOOR) · airframe 31,350 hrs · 16,125 cycles

R1 DOOR ESCAPE SLIDE COMPARTMENT MISSING RIVET ON GIRT BAR LATCH. INSTALLED RIVET PER SRM.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 232FF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED FLOORBOARD PANEL 232FF IAW MM 53-21-00.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 232DF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED CABIN FLOOR PANEL 232CF PER AMM 53-21-00

Part: PANEL — CORRODED (NLG WHEEL WELL) · airframe 31,350 hrs · 16,125 cycles

NOSE WHEEL WELL PANEL: 114AC HAS MINOR CORROSION AROUND 18 EACH FASTENER HOLES ON THE UPPER MATING SURFACE. MARKED / REMOVED AND REPLACED PANEL 114AC PER REF AMM53-14-01.

Part: PANEL — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 232EF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED FLOORBOARD PANEL 232EF IAW MM 53-21-00.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 231UF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / R/R CABIN FLOOR PANEL 231UF PER AMM 53-21-00

Part: FLOOR PANEL — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 241NF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED FLOORBOARD PANEL 241NF IAW MM 53-21-00.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 231GF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED CABIN FLOOR PANEL 231GF PER AMM 53-21-00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 31,350 hrs · 16,125 cycles

LOWER PORTION OF NR 4 SEAT TRACK DAMAGED AT BS 663+10, RBL 45.5. R&R SEAT TRACK PER SRM AND DWG.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 231BF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED CABIN FLOOR PANEL 231BF PER AMM 53-21-00.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 231CF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED CABIN FLOOR PANEL 231CF PER AMM 53-21-00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 31,350 hrs · 16,125 cycles

UPPER PORTION OF NR 4 SEAT TRACK DAMAGED AT BS 663, RBL 45.5. R&R SEAT TRACK PER SRM AND DWG.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 231AF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED CABIN FLOOR PANEL 231AF PER AMM 53-21-00.

Part: PANEL — CORRODED (NLG WHEEL WELL) · airframe 31,350 hrs · 16,125 cycles

NOSE WHEEL WELL PANEL: 113BW HAS MINOR CORROSION AROUND 7 FASTENER HOLES ON THE MATING SURFACE. MARKED / REMOVED AND REPLACED PANEL 113BW PER REF AMM53-14-01.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 42,304 hrs · 24,971 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB PER SRM.

Part: PANEL — CORRODED (NLG WHEEL WELL) · airframe 31,350 hrs · 16,125 cycles

NOSE WHEEL WELL PANEL: 113AC HAS MINOR CORROSION AROUND 14 FASTENER HOLES ON THE MATING SURFACE. MARKED / REMOVED AND REPLACED PANEL 113AC PER REF AMM53-14-01.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 232EF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED FLOORBOARD PANEL 232EF IAW MM 53-21-00.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 231DF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED CABIN FLOOR PANEL 231DF PER AMM 53-21-00

Part: PANEL — CORRODED (NLG WHEEL WELL) · airframe 31,350 hrs · 16,125 cycles

NOSE WHEEL WELL PANEL: 114AC HAS CORROSION IN GOUGE ON THE UPPER MATING SURFACE CAUSED FROM COTTER PIN DEPRESSION. MARKED / REMOVED AND REPLACED PANEL 114AC PER REF AMM53-14-01.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 241UF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED FLOORBOARD PANEL 241UF IAW MM 53-21-00.

Part: FLOORBOARD — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 232CF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED FLOORBOARD PANEL 232CF IAW MM 53-21-00.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 241RF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED FLOORBOARD 241RF IAW MM 53-21-00.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 31,350 hrs · 16,125 cycles

UPPER PORTION OF NR 4 SEAT TRACK DAMAGED AT BS 700+6, RBL 45.5. R&R SEAT TRACK PER SRM AND DWG.

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 31,350 hrs · 16,125 cycles

CABIN FLOOR PANEL 241KF HAS FIBERGLASS PLIES PEELING UP IN SEVERAL AREAS THE ENTIRE LENGTH OF FLOOR PANEL. / REMOVED AND REPLACED FLOORBOARD PANEL 241KF IAW MM 53-21-00.

Part: BEAM — CRACKED (FSD) · airframe 31,350 hrs · 16,125 cycles

FWD SERVICE DOOR HAS AN HFEC INDICATION OF A .50 INCH LONG CRACK IN #5 BEAM ADJACENT TO INBD TORQUE BOX MOUNT BOLT (MARKED) / REMOVED AND REPLACED R1 (FWD GALLEY) DOOR PER AMM 52-41-00. (SEE SUB TASKS FOR INDIVIDUAL SIGN OFFS.) TAG NO: 384637 PN ON: 141A6516-20 SN ON: 002419 PN OFF: SN OFF: 002822

Part: PLATE — CRACKED (R/H WING) · airframe 31,350 hrs · 16,125 cycles

RT. WING WIGGLE PLATE CRACKED O/B OF PANEL #651DB. / REMOVED AND INSTALLED NEW WIGGLE PLATE PER. SRM 51-40-02

Part: BEAM — CRACKED (R1 DOOR) · airframe 42,304 hrs · 24,971 cycles

R1 DOOR NR 4 BEAM CRACKED ADJACENT TO INBOARD TORQUE BOX MOUNT BOLT. R&R R1 DOOR PER MM.

Part: BALANCE WEIGHT — CORRODED (R/H WING) · airframe 31,350 hrs · 16,125 cycles

RT. WING AILERON WEIGHTS HAVE SURFACE CORROSION LOCATED UNDER PANEL #671BB. (M) / INSPECTED AND FOUND 3 LOWER BALANCE WEIGHTS WITH SURFACE CORROSION (113A7183-5) AND 1 UPPER WEIGHT WITH SURFACE CORROSION (113A7183-6) . REMOVED AND INSTALLED NEW WEIGHTS WITH SAME PART NUMBERS AND VERIFIED ALL REPLACED WEIGHTS TO BE IN CORRECT WEIGHT RANGE PER. DRAWING PL 113A7183 INSTALLED WEIGHTS IN ORIGINAL POSITIONS PER. SRM 51-40-02 AND M.M. 20-50-11

Part: BEAM — CRACKED (R1 DOOR) · airframe 42,304 hrs · 24,971 cycles

R1 DOOR NR 5 BEAM CRACKED ADJACENT TO INBOARD TORQUE BOX MOUNT BOLT. R&R R1 DOOR PER MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 30,930 hrs · 15,874 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE UPPER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 30,930 hrs · 15,874 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE UPPER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,407 hrs · 15,543 cycles

RT EMERGENCY LIGHT INOP AT ROW 9. R&R BULB IAW AMM.

Part: STRIP — DELAMINATED (CABIN) · airframe 30,282 hrs · 15,465 cycles

RT FORWARD EGRESS STRIP DELAMINATED. R&R STRIP PER DWG.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 30,282 hrs · 15,465 cycles

RUDDER BALANCE WEIGHT CORRODED / REMOVED AND REPLACED PER CMM 55-40-09

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 28,525 hrs · 14,431 cycles

CABIN ALTITUDE WARNING HORN SOUNDED ALONG WITH CABIN ALTITUDE WARNING LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED. R & R THE EQUIPMENT COOLING OUTBOARD EXHAUST VALVE IAW MM.

Part: REGULATOR — FAILED (NR 1 ENGINE) · airframe 28,253 hrs · 14,262 cycles

DECLARED EMERGENCY, CABIN ALTITUDE WARNING HORN CAME ON AT FL 380. CABIN ALTITUDE WAS AT 10,000. INITIATED QRC. WENT TO MANUAL MODE. CABIN CONTINUED UP TO 11,000 FEET. INITIATED EMERGENCY DESCENT. R&R NR 1 HIGH STAGE REGULATORY PER AMM.

Part: REGULATOR — FAILED (NR 2 ENGINE) · airframe 28,253 hrs · 14,262 cycles

DECLARED EMERGENCY, CABIN ALTITUDE WARNING HORN CAME ON AT FL 380. CABIN ALTITUDE WAS AT 10,000. INITIATED QRC. WENT TO MANUAL MODE. CABIN CONTINUED UP TO 11,000 FEET. INITIATED EMERGENCY DESCENT. R&R NR 2 HIGH STAGE REGULATORY PER AMM.

Part: RELIEF VALVE — FAULTY (CABIN PRESSURE) · airframe 28,253 hrs · 14,262 cycles

DECLARED EMERGENCY, CABIN ALTITUDE WARNING HORN CAME ON AT FL 380. CABIN ALTITUDE WAS AT 10,000. INITIATED QRC. WENT TO MANUAL MODE. CABIN CONTINUED UP TO 11,000 FEET. INITIATED EMERGENCY DESCENT. R&R NR 1 POSITIVE PRESSURE SAFETY RELIEF VALVE PER AMM.

Part: RELIEF VALVE — FAULTY (CABIN PRESSURE) · airframe 28,253 hrs · 14,262 cycles

DECLARED EMERGENCY, CABIN ALTITUDE WARNING HORN CAME ON AT FL 380. CABIN ALTITUDE WAS AT 10,000. INITIATED QRC. WENT TO MANUAL MODE. CABIN CONTINUED UP TO 11,000 FEET. INITIATED EMERGENCY DESCENT. R&R NR 2 POSITIVE PRESSURE SAFETY RELIEF VALVE PER AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 28,177 hrs · 14,202 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY CHECK AT M01674. R & R THE BATTERY IAW AMM.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 28,177 hrs · 14,202 cycles

FUSELAGE FORWARD CARGO BAY FLOOR SUPPORT CRACKED AT BS 540. R & R THE FLOOR SUPPORT IAW SRM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 28,177 hrs · 14,202 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY CHECK AT M01672. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 28,177 hrs · 14,202 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY CHECK AT M01670. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 28,177 hrs · 14,202 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY CHECK AT M01669. R & R THE BATTERY IAW AMM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 26,965 hrs · 13,467 cycles

LT MAIN LANDING GEAR WHEEL WELL VAPOR WEB CRACKED AT BS 663, LBL 48.9. REPAIRED BARRIER PER SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 26,603 hrs · 13,240 cycles

L2 DOOR EMERGENCY SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 24,724 hrs · 12,191 cycles

AFT CARGO FLOORBEAM CORRODED AROUND NUTPLATE HOLES BETWEEN BS 793 TO BS 827, RBL 14. REPAIRED FLOORBEAM PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 24,724 hrs · 12,191 cycles

AFT CARGO WATER TANK SUPPORT POST ANGLE CRACKED AT BS 867, LBL 12. R&R ANGLE PER SRM AND DWG.

Part: FITTING — LOOSE (R1 DOOR) · airframe 23,727 hrs · 11,635 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CLIP LOOSE. SECURED CLIP IAW SIP.

Part: SLIDE — UNSERVICEABLE (R2 DOOR) · airframe 20,882 hrs · 10,058 cycles

R2 DOOR EMER EVAC SLIDE DATA PLACARD FRAYED. R & R SLIDE ASSEMBLY IAW MT.

Part: COVER — LOOSE (EXIT SIGN) · airframe 20,752 hrs · 9,989 cycles

R1 DOOR LOWER EMER EXIT SIGN COVER LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 19,516 hrs · 9,289 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 19,245 hrs · 9,151 cycles

R2 DOOR EMER ESCAPE SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW MT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 17,665 hrs · 8,235 cycles

FORWARD CEILING EMER LIGHT INOPERATIVE AT STATION 382. R & R BATTERY IAW MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 17,631 hrs · 8,216 cycles

R1 DOOR EVACUATION SLIDE LOOSE. REINSTALLED SLIDE IAW MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 16,936 hrs · 7,820 cycles

L1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: STRIP — DELAMINATED (CABIN) · airframe 16,506 hrs · 7,548 cycles

RIGHT EMER EGRESS LIGHT STRIP DELAMINATED AT ROW 1. R & R STRIP IAW MM.

Part: STRIP — DELAMINATED (CABIN) · airframe 16,506 hrs · 7,548 cycles

LEFT EMER EGRESS LIGHT STRIP DELAMINATED AT ROW 24. R & R STRIP IAW MM.

Part: LENS — MISSING (CABIN) · airframe 15,352 hrs · 6,899 cycles

LEFT OVERWING EMER EXIT LENS COVER MISSING. R & R LENS ASSEMBLY IAW MM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 13,127 hrs · 5,660 cycles

AFT CARGO BAY FLOOR PANEL NR 140AF CORRODED ALONG UPPER EDGES. R & R PANEL IAW MM & SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 13,127 hrs · 5,660 cycles

AFT CARGO BAY FLOOR PANEL NR 140BF CORRODED. R & R PANEL IAW SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 13,127 hrs · 5,660 cycles

FWD CARGO BAY FLOOR PANEL NR 120CF CORRODED ALONG UPPER EDGES. R&R PANEL IAW SRM.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 13,127 hrs · 5,660 cycles

L1 DOOR EMERGENCY EVAC SLIDE RETAINER CLIPS LOOSE. R&R CLIPS IAW SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 13,127 hrs · 5,660 cycles

SHEAR TIE CRACKED AT BS 807 BETWEEN STRINGER 27L & STRINGER 27R. REPAIRED SHEAR TIE IAW EA.