N7830A

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 65,799 hrs · 29,601 cycles

CRACK INDICATION ON HOLES A AND B POSITIONS ON SEAT TRACK AT BS 727B AND LBL 24.75 IN AFT PAX CABIN FLOOR STRUCTURE ; 2021-325973 / [01] TOOL USED PN NORTEC 500D; SN:N500X12101V022235; DUE DATE: 03-JUN-22; [02] TOOL USED: CALIPER; P/N: DIGITAL 150; S/N: AE-4125; DUE DATE: 21/MAY/22; [03] TOOL USED: CALIPER P/N: 500-464 S/N: 15045614 DUE DATE: JAN-22-2022 AND SMALL HOLE GAUGES P/N: 154-901 S/N: AE-407095 DUE DATE: JAN-16-2022; [04] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 210138203; DUE DATE: 05-MAR-22; [05] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN:210138203; DUE DATE: 05-MAR-22; [06] TOOL USED: CALIPER P/N: 54-100-00-2; S/N: 141233087; DUE DATE: 17-JUN-22; [07] PERFORMED PERMANENT REPAIR ON HOLES A AND B POSITIONS ON SEAT TRACK AT BS 727B AND LBL 24.75 IN AFT PAX CABIN FLOOR STRUCTURE IAW EA # 21-153-02197 AND 21-153-02197-WIP1; [08] PERFORMED PERMANENT REPAIR ON HOLES A AND B POSITIONS ON SEAT TRACK AT BS 727B AND LBL 24.75 IN AFT PAX CABIN FLOOR STRUCTURE IAW EA # 21-153-02197 AND 21-153-02197-WIP1 <BR>RII

Part: GLOWSTRIP — DETERIORATED (CABIN) · airframe 65,799 hrs · 29,601 cycles

DETERIORATED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (8 EA) ; 2021-325800 / [01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (8 EA) IWA B737-700 AMM 33-51-15-400-802; [02] VERIFIED STEP 1; [03] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (8 EA) IWA B737-700 AMM 33-51-15-400-802

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LGIHTS) · airframe 65,799 hrs · 29,601 cycles

INOP LOWERED CEILING PANEL BATTERY PACK LT SIDE AT FWD GALLEY AREA (1 EA) ; 2021-325912 / [01] REPLACED LOWERED CEILING PANEL BATTERY PACK LT SIDE AT FWD GALLEY AREA (1 EA) I.A.W. B737-700 AMM 33-51-06-960-805 TEST OK; [02] REPLACED LOWERED CEILING PANEL BATTERY PACK LT SIDE AT FWD GALLEY AREA (1 EA) I.A.W. B737-700 AMM 33-51-06-960-805 TEST OK

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 65,799 hrs · 29,601 cycles

CRACK ON AFT CORNER SCUFF PLATE ON AFT CARGO COMPARTMENT ; 2021-325901 / [01] TOOL USED: DIGITAL CALIPER P/N:500-197-30 S/N:A18229497 DUE DATE 27-JUL-21; [02] REPAIRED CORNER SCUFF PLATE AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.; [03] REPAIRED CORNER SCUFF PLATE AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.

Part: LINK — CRACKED (RAM AIR ACTUATOR) · airframe 65,799 hrs · 29,601 cycles

CRACK ON LINK ASSY LOCATED ON SHAFT ASSEMBLY OF THE RAM AIR INLET ACTUATOR LT SIDE ; 2021-325899 / [01] REPLACED LINK ASSY LOCATED ON SHAFT ASSEMBLY OF THE RAM AIR INLET ACTUATOR LT SIDE IAW DWG 213A3130-17 AND SRM 51-40-02-0G-0; [02] REPLACED LINK ASSY LOCATED ON SHAFT ASSEMBLY OF THE RAM AIR INLET ACTUATOR LT SIDE IAW DWG 213A3130-17 AND SRM 51-40-02-0G-0. COMPLETED

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 65,799 hrs · 29,601 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT ; 2021-325903 / [01] TOOL USED: DIGITAL CALIPER P/N;500-197-30 S/N;A18229497 DUE DATE 27-JUL-21; [02] REPAIRED CORNER SCUFF PLATE AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.; [03] REPAIRED CORNER SCUFF PLATE AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.

Part: LINK — CRACKED (RAM AIR ACTUATOR) · airframe 65,799 hrs · 29,601 cycles

CRACK ON LINK ASSY LOCATED AT SHAFT ASSEMBLY OF THE RAM AIR INLET ACTUATOR RT SIDE ; 2021-325900 / [01] REPLACED LINK ASSY LOCATED AT SHAFT ASSEMBLY OF THE RAM AIR INLET ACTUATOR RT SIDE IAW B737-700 SRM 51-40-02-0G-0; [02] REPLACED LINK ASSY LOCATED AT SHAFT ASSEMBLY OF THE RAM AIR INLET ACTUATOR RT SIDE IAW B737-700 SRM 51-40-02-0G-0

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 65,799 hrs · 29,601 cycles

CRACK FRONT SPAR SUPPORT ANGLE IFSS 120 APPROX WBL 94.24 AT LT WING ; 2021-325909 / [01] TOOLS USED: POWER PACK P/N: FMK0003223; S/N: PE0412/63335; DUE DATE: 23-AUG-21; MULTIMETER P/N: 2217-20; S/N: B83B914290479; DUE DATE:14-APR-22; THERMOMETER P/N: FLUKE63; S/N: 31330088; DUE DATE: 18-MAY-22.; [02] TOOL USED: CALIPER; PN: 500-464; SN:B16286923; DUE DATE: 14/SEP/21.; [03] REPLACED FRONT SPAR SUPPORT ANGLE IFSS 120 APPROX WBL 94.24 AT LT WIN I.A.W B737-700 SRM 51-10-02-0G-0; ITEM 9 AND DWG 116A3939 REV. B; [04] REPLACED FRONT SPAR SUPPORT ANGLE IFSS 120 APPROX WBL 94.24 AT LT WING I.A.W B737-700 SRM 51-10-02-0G-0; ITEM 9 AND DWG 116A3939 REV. B; [05] REPLACED FRONT SPAR SUPPORT ANGLE IFSS 120 APPROX WBL 94.24 AT LT WING I.A.W B737-700 SRM 51-10-02-0G-0; ITEM 9 AND DWG 116A3939 REV. B RII

Part: SUPPORT ANGLE — CRACKED (BS 807 S25R) · airframe 65,799 hrs · 29,601 cycles

CRACK ANGLE - SUPPORT LOCATED BS 807 AT LRVEL S-25R BELOW THRESHOLD AFT CARGO COMPARTMENT ; 2021-325889 / [01] REPLACED ANGLE-SUPPORT AND FASTENERS LOC.BS 807 AT LEVEL STR. 25R BELOW THRESHOLD AFT CARGO COMPARTMENT IAWB737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 DWG.# 146A8120; [02] TASK COMPLETED; VERIFIED AS RII.<BR><BR>REPLACED ANGLE-SUPPORT AND FASTENERS LOC.BS 807 AT LEVEL STR. 25R BELOW THRESHOLD AFT CARGO COMPARTMENT IAWB737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 DWG.# 146A8120 REV -

Part: SUPPORT — CORRODED (BS 727-847) · airframe 65,799 hrs · 29,601 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 847 STRINGER 25L WL 156 AT AFT CARGO COMPARTMENT. FABRICATED SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 847 STRINGER 25L WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM-51-10-02-0G-0 AND DRAWING # 146A7502-28 REV:-

Part: SUPPORT — CORRODED (BS 727-747) · airframe 65,799 hrs · 29,601 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 AND BS 747 AT LEVEL STRINGER 25R AND WL 156 AT AFT CARGO COMPARTMENT. FABRICATED SUPPORT ZEE LOC LOCATED BETWEEN BS 727 AND BS 747 AT LEVEL STRINGER 25R AND WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM-51-10-02-0G-0 AND DRAWING # 146A7502 REV:A..

Part: SUPPORT ANGLE — CRACKED (BS 827 S25R) · airframe 65,799 hrs · 29,601 cycles

CRACK ANGLE - SUPPORT LOCATED AT BS 827 AT LEVEL S-25R BELOW THRESHOLD AFT CARGO COMPARTMENT ; 2021-325888 / [01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 21-JAN-22; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 21-JAN-22;; [02] REPLACED ANGLE SUPPORT AND FASTENERS LOC. AT BS 827 AT LEVEL STR. 25R BELOW THRESHOLD AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 SRM 51-10-02 ITEM 9 DWG #146A8120 REV. E; [03] REPLACED ANGLE SUPPORT AND FASTENERS LOC. AT BS 827 AT LEVEL STR. 25R BELOW THRESHOLD AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 SRM 51-10-02 ITEM 9 DWG #146A8120 REV. E; [04] COMPLETED TASK RII

Part: BRACKET — BROKEN (BS 727 RBL 5) · airframe 65,799 hrs · 29,601 cycles

BROKEN BRACKET LOCATED AT FWD BULKHEAD BS 727 RBL5 AT AFT CARGO COMPARTMENT ; 2021-325890 / [01] REPLACED BRACKET LOCATED AT FWD BULKHEAD BS 727 RBL5 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02-0G-0-; ITEM 9 AND DWG 144A9401. REV: C; [02] REPLACED BRACKET LOCATED AT FWD BULKHEAD BS 727 RBL5 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02-0G-0-; ITEM 9 ; 51-40-02 AND DWG 144A2600 SHEET 62; REV -; [03] REPLACED BRACKET LOCATED AT FWD BULKHEAD BS 727 RBL5 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02-0G-0-; ITEM 9 ; 51-40-02 AND DWG 144A2600 SHEET 62; REV -

Part: ANGLE — CRACKED (BS 500C S25L) · airframe 65,799 hrs · 29,601 cycles

CRACK ANGLE - CLIP LOCATED ON BS 500C AT LEVEL STR 25L AT FWD CARGO COMPARTMEN ; 2021-325878 / [01] REPLACED ANGLE CLIP LOCATED ON BS 500C AT LEVEL STR 25L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 143A7505 REV:B; [02] REPLACED ANGLE CLIP LOCATED ON BS 500C AT LEVEL STR 25L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DWG 143A7505 REV:B; RII

Part: STUB FRAME — CRACKED (R1 DOOR) · airframe 65,799 hrs · 29,601 cycles

CRACK SERVICE DOOR CUT OUT STUD FRAME AT LEVEL STR17R AT FWD GALLEY AREA ; 2021-325852 / [01] TOOL USED PN/ NORTEC 600D; SN/ 210138003; DUE DATE/ 05MAR22; [02] SUMMARY EA 21-153-02088 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q005T64U.; [03] PERFORMED REPAIR ON SERVICE DOOR CUT OUT STUD FRAME AT LEVEL STR17R AT FWD GALLEY AREA IAW EA#21-153-02088 AND 21-153-02088-WIP1; [04] INSTALLED SCUFF PLATE FWD SERVICE DOOR I.A.W. B737-700 AMM-53-11-01-420-801 STEP 3 D (1) (P) AND (R); [05] OK TO INSTALL FLOOR-MOUNTED ESCAPE SLIDE BRACKET FWD SERVICE DOOR; [06] PERFORMED REPAIR ON SERVICE DOOR CUT OUT STUD FRAME AT LEVEL STR17R AT FWD GALLEY AREA IAW EA#21-153-02088 AND 21-153-02088-WIP1; [07] JOB CERTIFIED AS RII.

Part: STIFFENER — CORRODED (BS 1088) · airframe 65,799 hrs · 29,601 cycles

CORROSION STIFFENER ASSY LOC. BS1088 AND WL 224 APROX. ON APU COMPARTMENT ; 2021-325831 / [01] TOOL USED CALIPER; P/N: DIGITAL 150; S/N: AE-412601; DUE DATE 31-MAY-22; [02] TOOL USED: POWER PACK P/N PE1068 S/N PE0118-94826 DUE DATE: 23-FEB-22 FLUKE 566 S/N 31400105 DUE DATE: 13-JAN-23 MULTIMETER P/N FLUKE 87-5 S/N 31630287 DUE DATE: 08-AUG-21; [03] REPLACED STIFFENER LOC. BS1088 AND WL 224 APROX. ON APU COMPARTMENT IAW B737-700 SRM-51-40-00-02-0G-0 AND DWG-148A2410 REV: B; [04] REPLACED STIFFENER LOC. BS1088 AND WL 224 APROX. ON APU COMPARTMENT IAW B737-700 SRM-51-40-00-02-0G-0 AND DWG-148A2410 REV: B.. RII ITEM

Part: STRINGER — DENTED (BS 827 S15L) · airframe 65,799 hrs · 29,601 cycles

FOUND DENT ON FUSELAGE AT BS 827 +12; 1.75' ABOVE STR 15L. DENT MEASURES 3.25'L X 2.0'W X .065'D. W/Y=30.8. ; 2021-325836 / [01] TOOL USED P/N: NORTEC 500D; S/N: N500X1693P030456; DUE DATE: 30 NOV 21.; [02] TOOL USED: PN: MIZ-21C ; SN: 769680; DUE DATE: 26-FEB-22; [03] PERFORMED PERMANENT REPAIR ON FUSELAGE AT BS 827 +12; 1.75' ABOVE STR 15L IAW EA# 21-153-02158 AND EA # 21-153-02158-WIP1 . THIS REPAIR IS CATEGORY A AND NOT RE-INSPECTION REQUIRED; [04] PERFORMED PERMANENT REPAIR ON FUSELAGE AT BS 827 +12; 1.75' ABOVE STR 15L IAW EA# 21-153-02158 AND EA # 21-153-02158-WIP1 . THIS REPAIR IS CATEGORY A AND NOT RE-INSPECTION REQUIRED

Part: SCUFF PLATE — CRACKED (BS 540) · airframe 65,799 hrs · 29,601 cycles

CRACK FLOOR STRUCTURE PLATE LOCATED AT BS 540 BTW BL 0 AND LBL 24.75 AT PASSENGER CABIN ; 2021-325807 / [01] REPLACED FLOOR STRUCTURE PLATE AND FASTENERS LOCATED AT BS 540 BTW BL 0 AND LBL 24.75 AT PASSENGER CABIN IAW B 737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 DWG. # 143A0060 REV. -; [02] CERTIFIED RII WORK PERFORMED.

Part: SUPPORT BRACKET — CRACKED (BS 1021) · airframe 65,799 hrs · 29,601 cycles

CRACK SUPPORT BRACKET LOCATED ON BS 1021.27 AT LEVEL STR3L TO STR3R AT UPPER FUSELAGE (1 EA) ; 2021-325615 / [01] REPLACED NEW SUPPORT BRACKET AND FASTENERS LOCATED ON BS 1021.27 AT LEVEL STR 3L TO STR 3R AT UPPER FUSELAGE IAW SRM B737-700 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 176A3001 REV.E; [02] REPLACED NEW SUPPORT BRACKET AND FASTENERS LOCATED ON BS 1021.27 AT LEVEL STR 3L TO STR 3R AT UPPER FUSELAGE IAW SRM B737-700 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 176A3001 REV.E JOB COMPLETED RII

Part: ANGLE — DAMAGED (RT WING TE) · airframe 65,799 hrs · 29,601 cycles

ELONGATED HOLE TRAILING EDGE T-ANGLE LOCATED APPROX ORSS 254 AT RT WING ; 2021-325669 / [01] REPLACED T-ANGLE ON TRAILING EDGE LOCATED APPROX ORSS 254 AT RT WING IAW B737-700 SRM 52-10-02 ITEM 9; SRM 51-40-02; [02] REPLACED T-ANGLE ON TRAILING EDGE LOCATED APPROX ORSS 254 AT RT WING IAW B737-700 SRM 52-10-02 ITEM 9; SRM 51-40-02.

Part: PLATE — DAMAGED (RT WING TE) · airframe 65,799 hrs · 29,601 cycles

ELONGATED HOLE CORRUGATED PLATE TRAILING EDGE LOCATED APPROX ORSS 261 AT RT WING ; 2021-325666 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED APPROX ORSS 261 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2001 REV:B; [02] CERTIFIED WORK PERFORMED.

Part: PLATE — CRACKED (RT WING TE) · airframe 65,799 hrs · 29,601 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED APPROX ORSS 216 AT RT WING ; 2021-325667 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED APPROX ORSS 216 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 ;SRM 51-40-02 AND DRAWING #115A2001 REV:B; [02] CERTIFIED WORK PERFORMED.

Part: PLATE — CRACKED (LT WING) · airframe 65,799 hrs · 29,601 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED APPROX ORSS 261 AT LT WING ; 2021-325697 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED APPROX ORSS 261 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING # 115A2001 REV:B; [02] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED APPROX ORSS 261 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 ; 51-40-02 AND DRAWING # 115A2001 REV:B

Part: ANGLE — CRACKED (RT WING TE) · airframe 65,799 hrs · 29,601 cycles

CRACK ANGLE TRAILING EDGE SUPPORT LOCATED APPROX ORSS 284 AT RT WING ; 2021-325585 / [01] REPLACED ANGLE TRAILING EDGE SUPPORT LOCATED APPROX ORSS 284 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02; [02] TASK COMPLETED <BR><BR>REPLACED ANGLE TRAILING EDGE SUPPORT LOCATED APPROX ORSS 284 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02

Part: STRINGER — CRACKED (BS 540 S26L) · airframe 65,799 hrs · 29,601 cycles

CRACK STRINGER 26L LOCATED BS 540 FWD CARGO COMPARTMENT ; 2021-325606 / [01] TOOL USED P/N: 45 MG; S/N: 130060401; DUE DATE: 22 APR 22.; [02] TOOL USED P/N: NORTEC 500D; S/N: N500X12101V022240; DUE DATE: 01 DEC 21.; [03] TOOL USED: PRECISION RADIUS GAUGE; P/N: 2204A3; S/N: AE-408660; DUE DATE: 02-NOV-21; [04] PERFORMED PERMANENT REPAIR ON STRINGER 26L BETWEEN BS500D TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND NOT-REINSPECTION REQUIRED; [05] TASK COMPLETED; VERIFIED AS RII.<BR><BR>PERFORMED PERMANENT REPAIR ON STRINGER 26L BETWEEN BS500D TO BS540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 AND NOT-REINSPECTION REQUIRED

Part: ANGLE — CRACKED (RT WING TE) · airframe 65,799 hrs · 29,601 cycles

CRACK ANGLE TRAILING EDGE LOCATED AT ORSS 284 AT RT WING ; 2021-325583 / [01] REPLACED ANGLE AND FASTENERS TRAILING EDGE LOCATED AT ORSS 284 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; DWG# 115A6200 REV A.; [02] INSTALLED NEW ANGLE AND FASTENERS TRAILING EDGE LOCATED AT ORSS 284 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG# 115A6200 SHEET 7; REV A.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 65,799 hrs · 29,601 cycles

CRACK ON HORIZONTAL STABILIZER RIBS ON STA. 151.75 R/H SIDE ; 2021-325594 / [01] REPLACED RIB ON LEADING EDGE HORIZONTAL STABILIZER RIBS STA. 151.75 R/H SIDE IAW B737-700 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING #186A1001 REV:A; [02] TASK COMPLETED; VERIFIED AS RII.<BR><BR>REPLACED RIB ON LEADING EDGE HORIZONTAL STABILIZER STA. 151.75 R/H SIDE IAW B737-700 51-10-02 ITEM 9 AND 51-40-02 AND DRAWING #186A1001 REV:A

Part: ANGLE — CRACKED (L/H WING) · airframe 65,799 hrs · 29,601 cycles

CRACK ANGLE TRAILING EDGE LOCATED ON ORSS 268 AT LT WING. REPLACED ANGLE LOCATED TRAILING EDGE ON ORSS 268 AT LT WING IAW B737-700 SRM 51-10-02-0G ITEM 9.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 65,799 hrs · 29,601 cycles

CRACK ON HORIZONTAL STABILIZER LEADING ADGE RIBS (1E/A) STA. 105.26 R/H SIDE ; 2021-325590 / [01] REPLACED RIB LOC. ON LEADING EDGE HORIZONTAL STABILIZER STA. 105.26 IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING # 186A1001 REV. A; DRAWING # 186A1304 REV.; [02] REPLACED RIB LOC. ON LEADING EDGE HORIZONTAL STABILIZER STA. 105.26 IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING # 186A1001 REV. A; DRAWING # 186A1304 REV.

Part: SKIN — DENTED (BS 211) · airframe 65,799 hrs · 29,601 cycles

DENT ON EXTERNAL SKIN ON BS 211.8 PLUS 4 INCH AND 1 INCH ABOVE OF LAP JOINT ; 2021-325582 / [01] TOOL USED: P/N: NORTEC 500D; S/N: N500X1693P030457; DUE DATE: 02-JUN-22.; [02] EQUIPMENT P/N 45MG; S/N 130063701; DUE DATE: 11-MAY-22 WAS USED; [03] TOOL USED P/N : NORTEC 500D ; S/N:N500X12101V022237; DUE DATE : 24-AUG-21; [04] TOOL USED: P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 24-FEB-22; [05] SUMMARY EA 21-153-02104 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q005RPE3.; [06] PERFORMED REPAIR ON EXTERNAL SKIN ON BS 211.8 PLUS 4 INCH AND 1 INCH ABOVE OF LAP JOINT IAW EA # 21-153-02104 AND EA # 21-153-02104WIP1 AND NOT FURTHER ACTION OR RE-INSPECTION REQUIRED; [07] PERFORMED REPAIR ON EXTERNAL SKIN ON BTW BSTA 211.67 & BSTA 219.8 BTW S-21L & S-24L IAW EA # 21-153-02104 AND EA # 21-153-02104WIP1 AND NOT FURTHER ACTION OR RE-INSPECTION REQUIRED; [08] PERFORMED REPAIR ON EXTERNAL SKIN ON BTW BSTA 211.67 & BSTA 219.8 BTW S-21L & S-24L IAW EA # 21-153-02104 AND EA # 21-153-02104WIP1 AND NOT FURTHER ACTION OR RE-INSPECTION REQUIRED

Part: WEB — BROKEN (RT WING TE) · airframe 65,799 hrs · 29,601 cycles

BROKEN WEB TRAILING EDGE SUPPORT ACCESS PANEL LOCATED AT ORSS 287 AT RT WIN ; 2021-325581 / [01] REPLACED WEB (BEAM) AND FASTENERS ON TRAILING EDGE SUPPORT ACCESS PANEL LOCATED AT ORSS 287 AT RT WING IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 DWG # 115A3712 REV. -; [02] REPLACED WEB (BEAM) AND FASTENERS ON TRAILING EDGE SUPPORT ACCESS PANEL LOCATED AT ORSS 287 AT RT WING IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 DWG # 115A3712 REV. -

Part: SKIN — CRACKED (RT WING SLAT) · airframe 65,799 hrs · 29,601 cycles

CRACK LOWER SURFACE SLAT 6 LOCATED AT SS 202.45 RT WING. RAISED NEW FAULT TTG8Q005SM6L TO REPLACE SLAT #6 JOB COMPLETED.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 65,799 hrs · 29,601 cycles

CRACK INSPAR RIB 120.30 AT 28INCH OF FRONT SPAR LT HORIZONTAL STAB ; 2021-325546 / [01] EQUIPMENT P/N PHASEC 3D; S/N 587435\03; DUE DATE 02-DEC-21 WAS USED.; [02] TOOL USED RADIUS GAGE P/N: S167C S/N : AE-35947 DUE DATE 27/JAN/22; [03] TOOL USED: P/N: NORTEC 600 D; S/N: 190023010; DUE DATE: 01-DEC-21.; [04] PERFORMED PERMANENT REPAIR ON INSPAR RIB 120.30 AT 28INCH OF FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 THIS REPAIR IS CATEGORY A AND NOT RE-INSPECTION REQUIRED; [05] PERFORMED PERMANENT REPAIR ON INSPAR RIB 120.30 AT 28INCH OF FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5 THIS REPAIR IS CATEGORY A AND NOT RE-INSPECTION REQUIRED

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 65,799 hrs · 29,601 cycles

(CUSTOMER REQUEST) CRACK VAPOR VARRIER AT BS 663.75 AND RBL 15.54 AT MAIN WHEEL WELL COMPARTMENT ; 2021-325497 / [01] TOOL USED= CALIPER P/N:500-197-30; S/N:A18234376; DUE DATE: 30-JUL-21; [02] REPAIRED VAPOR BARRIER AT BS 663.75 AND RBL 15.54 AT MAIN WHEEL WELL COMPARTMENT AS PER B737-700 SRM 57-10-10-2R-2 REPAIR 2 PARAGRAPH 1.A; C; 2.C AND 6; [03] CERTIFIED WORK PERFORMED.; [04] CERTIFIED RII MAJOR REPAIR.

Part: HOOK — OUT OF ADJUST (L1 GIRT BAR) · airframe 64,781 hrs · 29,026 cycles

FWD CABIN DOOR ENTRY GIRT BAR WILL NOT STAY STOWED ON ON SIDE / ADJUSTED GIRT BAR STORAGE CLIP PER SIP OPS CK NORMAL

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 64,764 hrs · 29,015 cycles

FWD ENTRY DOOR ESCAPE SLIDE GIRTBAR WILLNOT STAY IN UNARMED BRACKETS / REPOSITIONED FWD ENTRY DOOR ESCAPE PER MT 725-61-06

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 64,550 hrs · 28,896 cycles

FWD SERVICE DOOR EMERGENCY EXIT LIGHT LENS MISSING DIRECTIONAL ARROW. REMOVED AND REPLACED FWD EMERGENCY EXIT LENS, REF MM 33-51-1.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 63,927 hrs · 28,507 cycles

TRANSFERED FROM NON-ROUTINE # G754086. L/H HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. / DMA 0285096 CLEARING # 57220 REPLACED L/H HORIZONTAL STAB SLIDING SEAL PER MM 53-31-31

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,134 hrs · 26,743 cycles

EMERGENCY LIGHT IS OUT. RELAMPED PER AMM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 61,134 hrs · 26,743 cycles

EMERGENCY EXIT LIGHT IS OUT. RECONNECTED CONNECTOR PER AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 61,134 hrs · 26,743 cycles

FWD EXIT SIGN LIGHT OUT. RELAMPED PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,134 hrs · 26,743 cycles

ROW 4L BULL NOSE LIGHT IS OUT. RELAMPED PER AMM.

Part: WIRE — BROKEN (COCKPIT) · airframe 61,134 hrs · 26,743 cycles

DOME LIGHT BROKEN WIRE. R&R LEFT DOME LIGHT ASSEMBLY PER AMM.

Part: SKIN — DELAMINATED (RT SPOILER) · airframe 61,134 hrs · 26,743 cycles

RT WING #11 SPOILER PANEL UPPER SURFACE DELAMINATED APPROX 19.25" FROM OUTBOARD END AND 18.5" FROM TRAILING EDGE. R&R #11 SPOILER IAW MM.

Part: SPOILER — DELAMINATED (R/H WING) · airframe 61,134 hrs · 26,743 cycles

REMOVE & REPLACE THE #11 SPOILER DUE TO DELAMINATION / REMOVED; REPLACED CHECK ADJUSTMENT AND FUNCTIONAL TESTED #11 SPOILER IAW MM 27-61-11-000-801 AND MM 27-61-11-400-801 FUCNTIONAL CHECK GOOD. (POS: #11; P/N OFF/ON: 113A4200-2; S/N OFF: 000225; S/N ON: 001022;)

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 61,134 hrs · 26,743 cycles

FCB FWD SCUFF PLATE CRACKED / REPAIRED FCB FWD SCUFF PLATE IAW EA 1-A53-2076 R11

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 61,134 hrs · 26,743 cycles

RT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY AT STA 101.90 #4 STIFFENER CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: PANEL — CRACKED (RH HOR STAB) · airframe 61,134 hrs · 26,743 cycles

R/H HORIZ STAB T/E PANEL 344CB HAS CRACK BETWEEN L/E AND O/B FASTENER HOLE / RECEIVED NEW R/H HORIZONTAL STAB T/E PANEL 344CB AND PANEL 344CB TO BE INSTALLED ON SWA CARD JPANEL-340-CLOSE

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,134 hrs · 26,743 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 500 TO BS 500A, RBL 24. R&R SHIELD SUPPORT PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 61,134 hrs · 26,743 cycles

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

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 61,134 hrs · 26,743 cycles

RT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 2 STA 101.90 #3 STIFFENER CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,134 hrs · 26,743 cycles

FORWARD CARGO BAY ON LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 400 TO BS. 500D, LBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 61,134 hrs · 26,743 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 61,134 hrs · 26,743 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS. 500D, STR. 22R. R&R GUSSET IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,134 hrs · 26,743 cycles

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

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 61,134 hrs · 26,743 cycles

AFT CABIN FLOOR PANEL 241ABF UPPER SURFACE PLIES DAMAGED BETWEEN BS. 887 TO BS. 1016. / REPAIRED FLOOR PANEL 241ABF IAW SRM AND DWG.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 61,134 hrs · 26,743 cycles

AFT CABIN FLOOR PANEL 241ADF UPPER SURFACE PLIES DAMAGED, BETWEEN BS. 887 TO BS. 1016. / REPAIRED FLOOR PANEL 241ADF IAW SRM.

Part: FLOOR PANEL — BROKEN (CABIN FLOOR) · airframe 61,134 hrs · 26,743 cycles

AFT CABIN FLOOR PANEL 242XF IS BROKEN / DUE TO THE EXTENT OF DAMAGE REPLACED AFT CABIN FLOOR PANEL 242XF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 220. 78570 8/14/19

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 61,134 hrs · 26,743 cycles

AFT CABIN FLOOR PANEL 242TF UPPER SURFACE PLIES DAMAGED BETWEEN BS. 887 TO BS. 1016. REPAIRED FLOOR PANEL 242TF IAW SRM.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 61,134 hrs · 26,743 cycles

AFT CABIN FLOOR PANEL 241XF UPPER SURFACE PLIES DAMAGED, BETWEEN BS. 887 TO BS. 1016. / REPAIRED FLOOR PANEL 241XF IAW SRM.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 61,134 hrs · 26,743 cycles

AFT CABIN FLOOR PANEL 241YF UPPER SURFACE PLIES DAMAGED BETWEEN BS. 887 TO BS. 1016. REPAIRED FLOOR PANEL IAW SRM.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 61,134 hrs · 26,743 cycles

AFT CABIN FLOOR PANEL 242VF UPPER SURFACE PLIES DAMAGED, BETWEEN BS. 887 TO BS. 1016. / REPAIRED FLOOR PANEL 242VF IAW SRM.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 61,134 hrs · 26,743 cycles

AFT CABIN FLOOR PANEL 241AEF UPPER SURFACE PLIES DAMAGED BETWEEN BS. 887 TO BS. 1016. REPAIRED FLOOR PANEL 241AEF IAW SRM.

Part: FLOOR PANEL — DAMAGED (AFT CABIN) · airframe 61,134 hrs · 26,743 cycles

AFT CABIN FLOOR PANEL 242UF UPPER SURFACE PLIES DAMAGED, BETWEEN BS. 887 TO BS. 1016. / REPAIRED FLOOR PANEL IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 61,134 hrs · 26,743 cycles

HORIZONTAL PRESSURE DECK WEB CRACKED AT BS. 663, RBL 41. REPAIRED WEB PER SRM.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 61,134 hrs · 26,743 cycles

VAPOR BARRIER CRACKED AT LOWER END AT BS. 663, RBL 10. REPAIRED VAPOR BARRIER PER SRM.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 60,538 hrs · 26,348 cycles

AFT GALLEY EMERGENCY LIGHT BROKEN CONNECTOR. R&R CONNECTOR PER SWPM & AMM.

Part: BULKHEAD — DENTED (BS 1016) · airframe 60,538 hrs · 26,348 cycles

AFT PRESSURE BULKHEAD DENT AT BS. 1016, BETWEEN LBL 30 AND LBL 40, 8" AFT OF THE "Y" CORD. / REPAIRED BULKHEAD PER SRM, ER, AND EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 59,446 hrs · 25,665 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD OUT FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 59,446 hrs · 25,665 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 59,446 hrs · 25,665 cycles

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

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 59,271 hrs · 25,536 cycles

FORWARD FLASHLIGHT RETENTION STRAPS BROKEN. R&R STRAP PER AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 59,271 hrs · 25,536 cycles

AFT FLASHLIGHT RETENTION STRAPS BROKEN. R&R STRAP PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 59,256 hrs · 25,527 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 59,256 hrs · 25,527 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 57,155 hrs · 24,223 cycles

L1 DOOR SLIDE OUT OF COVER POSITION. R&R SLIDE PACK IAW MT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,705 hrs · 23,940 cycles

RIGHT OVER DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,705 hrs · 23,940 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,607 hrs · 22,609 cycles

LIGHT CONNECTED TO M1674 EMERGENCY BATTERY CHARGER INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET PER SRM & DWG.

Part: DOUBLER — CRACKED (ECS BAY RH) · airframe 54,607 hrs · 22,609 cycles

RH; A/C EXHAUST DUCT; DOUBLER CRACKED. BS 663; WL 148; RBL 16 / REPLACED DOUBLER/SEAL RETAINER R/H B.S. 663 WL 148 RBL 16 7570349/NEW PER SRM 51-10-02-0G-0 9. SEAL RETAINER ASSY WILL BE INSTALLED ON NRC T686436.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

FORWARD CARGO BAY RT BAFFLE CRACKED BETWEEN BS 400 TO BS 420. R&R BAFFLE PER SRM & DWG.

Part: WEB — CRACKED (RT WING TE FLAP) · airframe 54,607 hrs · 22,609 cycles

RT WING UPPER TRAILING EDGE PANEL WEB CRACKED AT UPPER CORNER AT INBOARD AND OUTBOARD MAIN FLAP. R & R THE WEB IAW SRM.

Part: PANEL — CRACKED (RIGHT WING) · airframe 54,607 hrs · 22,609 cycles

RT WING PANEL 651FB I/B FAIRING IS CRACKED. / REMOVED AND REPLACED RT WING PANEL 651FB I/B FAIRING IAW SOPM 20-50-01

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 794, BETWEEN RBL 16 TO RBL 18. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

FORWARD CARGO BAY FLOOR TO BULKHEAD SUPPORT ANGLE BS 500D, BETWEEN RBL 15 TO LBL 15. R&R ANGLE PER SRM & DWG.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 54,607 hrs · 22,609 cycles

AFT CARGO BAY; DOOR CUTOUT; FWD. CORNER SCUFF PLATE CRACKED. / REPAIRED PER EA 1-A53-2076 REV 11 DATED 05/11/1999

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

FORWARD CARGO BAY BULKHEAD SIDEWALL SUPPORT CORRODED AT BS 500D, LBL 16. R&R SUPPORT PER SRM & DWG.

Part: SIDEWALL SUPPORT — CORRODED (BS 767-787) · airframe 54,607 hrs · 22,609 cycles

R/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 767 TO 787. R & R THE SIDEWALL SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 15. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727+4 TO BS 847. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FSD THRESHOLD) · airframe 54,607 hrs · 22,609 cycles

CORROSION ON THRESHOLD SUPPORT BS 315 RBL57 WL 209 / REMOVED CORRODED THRESHOLD SUPPORT; THEN INSTALLED NEW ON AT BS 315 RBL57 WL 209 I.A.W. SRM 51-40-02-0G-0. AND DWG 141A8310

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 420, RBL 15. R&R SUPPORT PER DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727B+11 TO BS 767. R&R SUPPORT PER SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

UPPER CHORD CORRODED AT BS 328, LBL 50. REPAIRED CHORD PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

AFT CARGO BAY FLOOR PANEL SUPPORT SPLICE STRIP CORRODED AT BS 887, BETWEEN BL 0 TO RBL 4. REPAIRED SPLICE STRIP PER SRM.

Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 54,607 hrs · 22,609 cycles

***CORROSION*** FORWARD CARGO BAY BULKHEAD SIDEWALL SUPPORT BS500D RBL16. / REMOVED AND REPLACED DAMAGED BULKHEAD ANGLE AT BS 500D; STR. 18R-26R PER SRM 51-40-02 AND DWG 143A9481

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

RT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 847 TO BS 867. R&R SUPPORT PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (BS 344-360) · airframe 54,607 hrs · 22,609 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, BL 0. R & R THE FLOOR SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D RBL 15. REPAIRED SUPPORT PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 495 TO BS 500A, RBL 15. R&R SUPPORT IAW DWG AND SRM.

Part: FLOOR PANEL — WARPED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

ACB; FLOOR PANEL 140AF; DENTED; AND WARP. / FABRICATED NEW ACB; FLOOR PANEL 140AF PER DRW PL 423A2610; LOCATED AND DRILLED PER SRM 51-40-02-0G-0; FIG.1. COUNTER SINK PER SRM 51-40-08-0G-0; APPLIED ALODINED PER AMM 51-21-41-370-802; APPLIED PRIMER PER AMM 51-21-72-370-804

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 54,607 hrs · 22,609 cycles

RIGHT WING L/E PANEL 621DB DELAMINATED AT CORNER. (MARKED) / RIGHT WING L/E PANEL 621DB DELAMINATION AT CORNER REPAIRED IAW SRM 51-70-05-2R-6 57443U 23JULY17

Part: SKIN — CRACKED (RT WING) · airframe 54,607 hrs · 22,609 cycles

RIGHT WING TRAILING EDGE PANEL 661AB OUTER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: FLOOR PANEL — WARPED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

ACB; FLOOR PANEL 140BF; DENTED; AND WARP. / FABRICATED NEW ACB FLOOR PANEL 140BF PER: DWG 453A2610; SRM 51-40-08-0G-0; AMM 51-21-41-370-802; AND AMM 51-21-82-370-804.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 54,607 hrs · 22,609 cycles

RT MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER CRACKED AT RBL 6. REPAIRED BARRIER IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 54,607 hrs · 22,609 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, LBL 32. R & R THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 54,607 hrs · 22,609 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294, BL 0. R & R THE FLOOR SUPPORT IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

CREASE BEAM WEB CORRODED BETWEEN BS 867 TO BS 887, LBL 65. R&R WEB IAW DWG.

Part: FLOOR PANEL — WARPED (FUSELAGE) · airframe 54,607 hrs · 22,609 cycles

ACB; FLOOR PANEL 140CF; DENTED; AND WARP. / FABRICATED; LOCATED & DRILLED NEW FLOOR PANEL 140CF DUE TO DENTED & WARP PER DWG # 453A2610; SRM 51-40-05-0G-0 & SRM 51-70-06-0G-0

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 54,607 hrs · 22,609 cycles

FWD CARGO BAY; FWD SCUFF PLATE IS CRACKED / FCB FWD CORNER SCUFF PLANTE REPAIRED PER SWA EA 1-A53-2076 REV 11 56708U 7AUG17

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 54,607 hrs · 22,609 cycles

LT MAIN WHEEL WELL SPAR PRESSURE WEB CRACKED AT STA 663, BETWEEN LBL 25 TO LBL 45. REPAIRED WEB PER ER & EA.

Part: LIMITER — LEAKING (FLAP HYD SYS) · airframe 54,467 hrs · 22,515 cycles

ON FIRST FLAP SELECTION DURING INITIAL APPROACH, COMPLETE LOSS OF SYSTEM B HYDRAULIC QUANTITY. EMERGENCY DECLARED. R & R FLOW LIMITER IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,084 hrs · 22,277 cycles

R1 DOOR EVAC SLIDE LIGHT INOP. RELAMPED PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 53,179 hrs · 21,696 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01673. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 53,179 hrs · 21,696 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,179 hrs · 21,696 cycles

LT WING OUTBOARD AFT FLAP INBOARD CORNER LOWER SURFACE DELAMINATED. R&R AFT FLAP IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 53,179 hrs · 21,696 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01668. R&R BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 53,179 hrs · 21,696 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01672. R&R BATTERY PER MM.

Part: FLANGE — CORRODED (NLG) · airframe 51,128 hrs · 20,498 cycles

LEFT NOSE GEAR AXLE SPACER FLANGE CORRODED AT THE 4 O'CLOCK AND 2 O'CLOCK POSITION. REPAIRED FLANGE IAW EA.

Part: FLANGE — CORRODED (NLG) · airframe 51,128 hrs · 20,498 cycles

RIGHT NOSE GEAR AXLE SPACER FLANGE CORRODED AT THE 10 O'CLOCK POSITION. REPAIRED THE FLANGE IAW EA.

Part: WIRE — DAMAGED (CABIN) · airframe 48,952 hrs · 19,216 cycles

COCKPIT EMER LIGHT INOPERATIVE. REPAIRED WIRE IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FORWARD CARGO BAY INTERCOSTAL UNDER LT FLOOR TO SIDEWALL SUPPORT CRACKED, BETWEEN BS 440 - 460. R & R INTERCOSTAL IAW SRM & DWG.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

UPPER FLANGE OF TRANSVERSE BEAM CORRODED, AT BS 344, BETWEEN LBL 6.75 TO LBL 8.25. REPAIRED FLANGE IAW SRM & EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FORWARD CARGO BAY INTERCOSTAL UNDER LT FLOOR TO SIDEWALL SUPPORT CRACKED, BETWEEN BS 400 - 420. R & R INTERCOSTAL IAW SRM & DWG.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

UPPER FLANGE OF TRANSVERSE BEAM CORRODED AT BS 328, BETWEEN RBL 9.4 TO RBL 12.3. REPAIRED FLANGE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FORWARD CARGO BAY INTERCOSTAL UNDER LT FLOOR TO SIDEWALL SUPPORT CRACKED, BETWEEN BS 500 - 500A. R & R INTERCOSTAL IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FLOORBEAM UPPER CHORD CORRODED AT BS 294.5, BETWEEN RBL 10 - 12.5. REPAIRED CHORD IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FORWARD CARGO BAY INTERCOSTAL UNDER LT FLOOR TO SIDEWALL SUPPORT CRACKED, BETWEEN BS 500A - 500B. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FORWARD CARGO BAY INTERCOSTAL UNDER LT FLOOR TO SIDEWALL SUPPORT CRACKED, BETWEEN BS 460 - 480 CRACKED. R & R INTERCOSTAL IAW SRM & DWG.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 48,952 hrs · 19,216 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70, VERTICAL STIFFENERS, THE SECOND & THIRD FROM THE FRONT. R & R STIFFENERS IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R CLIP IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW ER & EA.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

INTERCOSTAL ATTACH CLIP CORRODED, BETWEEN BS 787 - 807, STRINGER 16R. R & R CLIP IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW ER & EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

SUPPORT ANGLE CORRODED, BETWEEN BS 967 - 947.5, STRINGER 23R. R & R ANGLE IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

STRINGER CLIP CORRODED, BETWEEN BS 1006 - 986.5, STRINGER 27L. R & R CLIP IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

CREASE WEB CORRODED, BETWEEN BS 616 - 639, STRINGER 17L. REPAIRED WEB IAW ER & EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

STRINGER CLIP CORRODED, BETWEEN BS 1006 - 986.5, STRINGER 25L. R & R CLIP IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

CREASE WEB CORRODED, BETWEEN BS 639 - 663, STRINGER 17R. REPAIRED WEB IAW ER & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

CREASE WEB CORRODED, BETWEEN BS 616 - 639, STRINGER 17R. REPAIRED WEB IAW ER & EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

CREASE BEAM WEB CORRODED, BETWEEN BS 639 - 663, STRINGER 17L. REPAIRED WEB IAW ER & EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

STRINGER CLIP CORRODED, BETWEEN BS 951 - 947.5, STRINGER 18R. R & R CLIP IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

ANGLE SUPPORT CORRODED, BETWEEN BS 967 - 986.5, STRINGER 23R. R & R ANGLE IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW ER & EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

LONGITUDINAL FLOORBEAM VERTICAL WEB, CRACKED AT BS 727B, RBL 24.75. REPAIRED WEB IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW ER & EA.

Part: STRAP — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

AFT CARGO COMPARTMENT, INTERCOSTAL WEB STRAP CORRODED, BETWEEN BS 967 - 986.5, STRINGER 21R. R & R STRAP IAW SRM & DWG.

Part: SPACER — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

INTERCOSTAL TOP CHORD SPACER CORRODED, BETWEEN BS 328 - 344, LBL 11. REPAIRED SPACER IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

LEFT FWD CARGO COMPARTMENT, FLOOR TO SIDEWALL SUPPORT, CORRODED BETWEEN BS 500 TO 500D. REMOVED SUPPORT IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FRAME BRACKET CRACKED AT BS 727A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FRAME BRACKET CRACKED AT BS 360, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

LEFT NR 1 WINDOW FRAME CRACKED AT THE CORNER. REPAIRED FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FRAME BRACKET CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FRAME BRACKET CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 48,952 hrs · 19,216 cycles

LONGITUDINAL FLOORBEAM FLANGE CRACKED AT THE NR 8 FASTENER HOLE AT BS 727B, LBL 45. REPAIRED FLANGE IAW ER & EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 48,952 hrs · 19,216 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 36.5. REPAIRED WEB IAW SRM.