N228WN

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 64,528 hrs · 38,935 cycles

ALL ASSOCIATED LIGHTS WITH M1674 EMERGENCY BATTERY PACK INOP<[01] REMOVED AND REPLACED EMERGENCY BATTERY PACK POWER SUPPLY AND CHARGER M1674 PER AMM 33-51-06-960-806 AND TEST GOOD PER AMM 33-51-06-960-806;[02] VERIFIED CORRECTIVE ACTION

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 64,528 hrs · 38,935 cycles

ALL ASSOCIATED LIGHTS WITH EMERGENCY BATTERY PACK M1675 INOPERATIVE REMOVED AND REPLACED EMERGENCY BATTERY PACK POWER SUPPLY AND CHARGER M1675 PER AMM 33-51-06-960-806 AND TEST GOOD PER AMM 33-51-06-960-806;[02] VERIFIED CORRECTIVE ACTION

Part: LENS — BROKEN (ZONE 200) · airframe 64,528 hrs · 38,935 cycles

SIDEWALL PANEL 231YHW EMERGENCY EXIT LIGHT LENS BROKEN<[01] REMOVED AND REPLACED SIDEWALL PANEL 231YHW EMERGENCY EXIT LIGHT IAW AMM 33-51-01-960-802 <BR>OPT. CHECK: GOOD;[02] VERIFIED CORRECTIVE ACTION COMPLETE

Part: SKIN — CRACKED (ZONE 600) · airframe 64,528 hrs · 38,935 cycles

CRACKED FASTENER HOLE FOUND ON R/W FIXED L/E UPPER SURFACE; 5' I/B OF PYLON (MARKED LOCATION AND DIRECTION)<[01] REMOVED DAMAGE IN FASTENER HOLE FOUND ON R/W FIXED L/E UPPER SURFACE; 5' I/B OF PYLON IAW SRM 51-10-02-OG-0 AND SRM 57-41-01-2R-7.;[02] VERIFIED CORRECTIVE ACTION #1

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 64,528 hrs · 38,935 cycles

F/O'S SEAT TRACK'S WORN; CRACKED & CORRODED<[01] REOMVED AND REPLACED F/O'S SEAT TRACK'S PER AMM 25-11-11-400-801<BR>CAL:DATE:08/2024<BR>DUE:08/2025<BR>ID:ATS2328.;[02] COMPLETE.;[03] UPDATED MEASUREMENTS TABLE.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 64,528 hrs · 38,935 cycles

CAPTAIN'S SEAT TRACK'S WORN; CRACKED & CORRODED<[01] REMOVED AND REPLACED CAPTAIN'S SEAT TRACK'S PER AMM 25-11-11-400-801<BR>CAL:DATE:03/2025<BR>DUE:03/2026<BR>ID:ATS2842;[02] VERIFIED CORRECTIVE ACTION #1

Part: PANEL — DELAMINATED (ZONE 600) · airframe 64,528 hrs · 38,935 cycles

RIGHT WING L/E PANEL 621JB DELAMINATED AT CUTOUT FWD CORNERS. RIGHT WING L/E PANEL 621JB DELAMINATED AT CUTOUT FWD CORNERS; WAS REPAIRED IAW SRM 51-70-05-2R-6.

Part: PANEL — DELAMINATED (ZONE 500) · airframe 64,528 hrs · 38,935 cycles

LEFT ING L/E PANEL 521KB DELAMINATED AT CORNERS OF CUTOUT. LEFT WING L/E PANEL 521KB WITH DELAMINATIONS AT CORNERS OF CUTOUTS WAS REPAIRED PER SRM 51-70-05-2R-6.

Part: PANEL — DELAMINATED (ZONE 500) · airframe 64,528 hrs · 38,935 cycles

LEFT WING L/E PANEL 521DB DELAMINATED AT CUTOUT CORNERS. REPAIRED PER SRM 51-70-05-2R-6-A00737 REPAIR 6 - REPAIR OF DAMAGE TO THE EDGEBAND OF A HONEYCOMB PANEL.

Part: PANEL — DELAMINATED (ZONE 600) · airframe 64,528 hrs · 38,935 cycles

RIGHT WING L/E PANEL 621QB DELAMINATED AT FWD I/B CORNER. RIGHT WING L/E PANEL 621QB DELAMINATED AT FWD I/B CORNER; WAS REPAIRED IAW SRM 51-70-05-2R-6.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 64,528 hrs · 38,935 cycles

CRACKED FLOORBEAM AT PASSENGER COMPARTMENT BS 540 LBL 2 WL 208. REMOVED AND REPLACED FLOOR SUPPORT PANEL BREAK AT PASSENGER COMPARTMENT BS 540 LBL 2 WL 208 IAW SRM 51-40-02-0G-0 AND AIPC SWA D638A001-SWA-0102.

Part: SKIN — DELAMINATED (ZONE 600 FLAP) · airframe 64,528 hrs · 38,935 cycles

RIGHT WING INBD MAIN FLAP O/B T/E WEDGE IS DELAMINATED. REMOVED AND REPLACED THE RIGHT WING INBD MAIN FLAP O/B T/E WEDGE IAW SOPM 20-50-01.

Part: SPLICE STRAP — CORRODED (ZONE 100) · airframe 64,528 hrs · 38,935 cycles

CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS887 RBL11.5 WL168<[01] EVALUATED; REMOVED; LOCATED; DRILLED AND INSTALLED FLOOR SPLICE STRAP BS887 LBL 8 TO RBL 22 WL 168 IAW SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 AND DWG 149A8104 REV: B.;[02] COMPLETE;[03] COMPLETE

Part: SHIELD — CORRODED (ZONE 100) · airframe 64,528 hrs · 38,935 cycles

CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] EVALUATED; LOCATED AND DRILLED; REMOVED AND REPRACED AFT CARGO BAY NEW SHIELD BS767 TO BS794 RBL22 WL156 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A0081 REV: -;[02] CORRECTION ACTION.<BR><BR>EVALUATED; LOCATED AND DRILLED; REMOVED AND REPLACED AFT CARGO BAY NEW SHIELD BS767 TO BS794 RBL22 WL156 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A0081 REV: -;[03] COMPLETE;[04] COMPLETE

Part: SUPPORT — CORRODED (ZONE 100) · airframe 64,528 hrs · 38,935 cycles

CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] EVALUATED; REMOVED; LOCATED; DRILLED AND REPLACED AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE BS727 TO BS847 LBL22 WL156 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 146A7500 REV: A AND DWG 146A0067 REV: -.;[02] COMPLETE;[03] COMPLETE

Part: SUPPORT — CORRODED (ZONE 100) · airframe 64,528 hrs · 38,935 cycles

CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] EVALUATED; LOCATED AND DRILLED; REMOVED AND REPRACED AFT CARGO BAY NEW R/H FLOOR TO SIDEWALL SUPPORT PLATE BS727 TO BS767 RBL22 WL156 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A7500 REV: A.;[02] CORRECTION ACTION.<BR><BR>EVALUATED; LOCATED AND DRILLED; REMOVED AND REPLACED AFT CARGO BAY NEW R/H FLOOR TO SIDEWALL SUPPORT PLATE BS727 TO BS767 RBL22 WL156 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A7500 REV: A.;[03] COMPLETE;[04] COMPLETE

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 85,962 hrs · 38,913 cycles

R1 ESCAPE SLIDE EMERG LIGHT INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Part: LENS — CRACKED (ZONE 200) · airframe 62,307 hrs · 37,562 cycles

12 DEF TO 24 DEF EMERGENCY LIGHT LENS ARE CRACKED AND CRAZED MULTIPLE LOCATIONS<[01] REPLACED MULTIPLE LIGHT LENS IAW AMM 33-51-00.

Part: LENS — CRACKED (ZONE 200) · airframe 62,307 hrs · 37,562 cycles

12 ABC TO 24 ABC EMERGENCY LIGHT LENS ARE CRACKED AND CRAZED MULTIPLE LOCATIONS<[01] REPLACED MULTIPLE LIGHT LENS IAW AMM 33-51-00.

Part: GUARD — LOOSE (ZONE 200) · airframe 61,972 hrs · 37,356 cycles

AFT F/A EMERGENCY LIGHT SW GUARD IS LOOSE<[01] ADJUSTED SPRING ON GUARD REF AMM 25-25-11

Part: NUT PLATE — CRACKED (ZN 300 STABILIZE) · airframe 58,313 hrs · 35,117 cycles

CRACK NUTPLATE RAIL 2E/A LOCATED ON FRONT SPAR INTERNAL STRUCTURE LOWER CHORD BTW STAB STA 175.50 TO STAB STA 193.90 AT LT HORIZONTAL STABILIZER 2023-422644<[01] REPLACED NUTPLATE RAIL (2E/A) LOCATED ON FRONT SPAR INTERNAL STRUCTURE LOWER CHORD BTW STAB STA 175.50 TO STAB STA 193.90 AT LT HORIZONTAL STABILIZER I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 182A2401 SHEET 15 REV. F<BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] RII ITEM <BR>REPLACED NUTPLATE RAIL (2E/A) LOCATED ON FRONT SPAR INTERNAL STRUCTURE LOWER CHORD BTW STAB STA 175.50 TO STAB STA 193.90 AT LT HORIZONTAL STABILIZER I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 182A2401 SHEET 15 REV. F

Part: INTERCOSTAL — DAMAGED (ZN 100 FUS LOWER) · airframe 58,311 hrs · 35,116 cycles

AAI. FORWARD CARGO BAY INTERCOSTAL AT STA. 500 LBL 21 FORWARD FASTENER IS TOE NAILED AND HOLE IS NOT COMPLETELY FILLED. 2023-422641<[01] REPLACED FASTENERS ( 1 E/A) FORWARD CARGO BAY INTERCOSTAL AT STA. 500 LBL 21 IAW B737-700 SRM 51-40-02 AND DRAWING # 143A7505. REV: -. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: BRACKET — DAMAGED (ZN 600 RIGHT WIN) · airframe 58,313 hrs · 35,117 cycles

ELONGATED HOLE ON SUPPORT BRACKET LOCATED INBOARD LEADING EDGE AT INTERNAL CAVITY ACCESS PANEL 611AT RT WING 2023-422560<[01] REPLACED SUPPORT BRACKET LOCATED INBOARD LEADING EDGE AT INTERNAL CAVITY ACCESS PANEL 611AT RT WING IAW. B373-700 SRM 51-40-02-0G-0 AND DWG 212A1901 SHEET 3 REV-.;[02] CORRECTIVE ACTION CERTIFIED

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 58,313 hrs · 35,117 cycles

CRACK ANGLE LOCATED INBOARD AUXILIARY TRACK ON SLAT 8 AT RT WING 2023-422561<[01] REPLACED ANGLE LOCATED INBOARD AUXILIARY TRACK ON SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02. LENGTH OF CRACK:2.041?. TOOL USED CALIPER P/N: 500-752-20 S/N:B21015879 DUE DATE: 13-DEC-23;[02] TASK CARD COMPLETE.

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 58,313 hrs · 35,117 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED ORSS 270 TO ORSS 275 RT WING 2023-422520<[01] REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS 270 TO ORSS 275 RT WING AND FASTENERS IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG 115A2001 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK CARD COMPLETED

Part: ANGLE — DAMAGED (ZN 500 LEFT WING) · airframe 58,313 hrs · 35,117 cycles

ELONGATED HOLE ANGLE TRAILING EDGE LOCATED ON ORSS255 AT LT WING 2023-422507 IAW DWG NAME OF PART IS CLIP ASSY DWG114A5300 REV :A<[01] REPLACED ANGLE TRAILING EDGE LOCATED ON ORSS255 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A5300; SHEET 20; REV A;[02] REPLACED ANGLE (CILP ASSY IAW DWG )TRAILING EDGE LOCATED ON ORSS255 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A5300; SHEET 20; REV A

Part: PLATE — CRACKED (ZN 600 RIGHT WIN) · airframe 58,313 hrs · 35,117 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED ORSS 290 TO ORSS 299 RT WING 2023-422518<[01] REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS 290 TO ORSS 299 RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A3700 REV:-. LENGTH OF CRACK:0.807?. TOOL USED CALIPER P/N: 500-752-20 S/N:B21015879 DUE DATE: 13-DEC-23;[02] COMPLETED

Part: PANEL — BROKEN (ZN 500 LEFT WING) · airframe 58,313 hrs · 35,117 cycles

BROKEN ACCESS PANEL 551GB TRAILING EDGE ANGLE AT LT WING 2023-422541<[01] REPLACED ACCESS PANEL 551GB TRAILING EDGE ANGLE AT LT WING I.A.W SRM 51-40-02.;[02] REPLACED ACCESS PANEL 551GB TRAILING EDGE ANGLE AT LT WING I.A.W SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (ZN 600 RIGHT WIN) · airframe 58,313 hrs · 35,117 cycles

CRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 280 RT WING 2023-422516<[01] REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 280 RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A3700 REV.- SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 280 RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A3700 REV.- SEE INDIVIDUAL SIGN OFFS BELOW

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 58,313 hrs · 35,117 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS 273 FWD POSITION DEFLECTION CONTROL RIB RT WING 2023-422530PART INSTALLEDP/N: 115A2953-2 PO# 2022 196669<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 273 FWD POSITION DEFLECTION CONTROL RIB RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 115A2930 REV-.;[02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 273 FWD POSITION DEFLECTION CONTROL RIB RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 115A2930 REV-.

Part: FILLER — MISSING (ZN 100 FUS LOWER) · airframe 58,313 hrs · 35,117 cycles

MISSING FILLER STRUCTURE LOCATED BS727 LOWER STRUCTURE WING TO BODY FAIRING LOWER FUSELAGE 2 E/A 2023-422544<[01] REPLACED FILLER STRUCTURE LOCATED BS727 LOWER STRUCTURE WING TO BODY FAIRING LOWER FUSELAGE 2 E/A IAW B737-700 SRM 51-10-02 AND DWG AND DWG149A7519; SHEET 4 AND REV A AND BAC5010. SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1<BR>INSTALLED FILLER STRUCTURE LOCATED BS727 LOWER STRUCTURE WING TO BODY FAIRING LOWER FUSELAGE 2 E/A IAW B737-700 SRM 51-10-02 AND DWG AND DWG149A7519; SHEET 4 AND REV A AND BAC5010. SEE INDIVIDUAL SIGN-OFF BELOW;[03] CERTIFIED WORK PERFORMED <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: PLATE — CRACKED (ZN 500 LEFT WING) · airframe 58,313 hrs · 35,117 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 261 AT LT WING 2023-422505<[01] REPLACED CORRUGATED PLATE TRAILING EDGE AND FASTENERS LOCATED ON ORSS 261 AT LT WING IAW B737-700 SEM 51-40-02 AND DWG 115A2001 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1:<BR>REPLACED CORRUGATED PLATE TRAILING EDGE AND FASTENERS LOCATED ON ORSS 261 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CERTIFIED STEP 2 COMPLETED

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 58,313 hrs · 35,117 cycles

CRACK ANGLE TRAILING EDGE LOCATED IRSS140 AT LT WING 2023-422526 IAW DGW NAME PART IS CLIP ASSY 115A2000 REV-<[01] REPLACED ANGLE TRAILING EDGE LOCATED IRSS140 AT LT WING; MEASURE CRACK IS L=0.817? TOOL USED CALIPER P/N: 500-193-30; S/N: 0039393; DUE DATE: 02-OCT-23 IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2000 SHEET 21 REV -;[02] REPLACED ANGLE ( CLIP ASSY ) IAW DWG TRAILING EDGE LOCATED IRSS140 AT LT WING; MEASURE CRACK IS L=0.817? TOOL USED CALIPER P/N: 500-193-30; S/N: 0039393; DUE DATE: 02-OCT-23 IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2000 SHEET 21 REV -

Part: BRACKET — CRACKED (ZN 500 LEFT WING) · airframe 58,313 hrs · 35,117 cycles

CRACK TRAILING EDGE ON SUPPORT BRACKET LOCATED ORSS275 AT LT WING 2023-422506<[01] REPLACED SUPPORT BRACKET LOCATED ORSS275 AT LT WING I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9 ; DWG 115A3700 SHEET: 3 REV. B . SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED SUPPORT BRACKET LOCATED ORSS275 AT LT WING I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9 ; DWG 115A3700 SHEET: 3 REV. B . SEE INDIVIDUAL SIGNOFF BELOW.

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 58,313 hrs · 35,117 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS 273 AFT POSITION DEFLECTION CONTROL RIB RT WING 2023-422532<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 273 AFT POSITION DEFLECTION CONTROL RIB RT WING IAW SRM B737-700 51-40-02 SRM 51-10-02 PARAGRAPH 9;[02] STEP 1 CORRECTED REPLACED ANGLE TRAILING EDGE LOCATED ORSS 273 AFT POSITION DEFLECTION CONTROL RIB RT WING IAW SRM B737-700 51-40-02 SRM 51-10-02 PARAGRAPH 9 AND MEASURE CRACK L=0.800 IN TOOL USED CALIPER S/N= 0033174 P/N=700-113-10 DUE DATE=12-MAR-24;[03] JOB COMPLETED.

Part: ACCESS PANEL — CRACKED (ZN 500 LEFT WING) · airframe 58,313 hrs · 35,117 cycles

CRACK ACCESS PANEL 542BB SEAL SUPPORT PLATE LT WING 2023-422499<[01] REPLACED ACCESS PANEL 542BB SEAL SUPPORT PLATE LT WING I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG# 113A9350; SHEET 1; REV.F.;[02] REPLACED ACCESS PANEL 542BB SEAL SUPPORT PLATE LT WING I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG# 113A9350; SHEET 1; REV.F.

Part: ANGLE — CRACKED (ZN 800 DOOR) · airframe 58,313 hrs · 35,117 cycles

CRACK ANGLE ENTRY DOOR CUT OUT LOC BS 294.5 AND BTW STR 13 TO STR 14 FWD GALLEY AND LAV 2023-422454<[01] REPLACED ANGLE ENTRY DOOR CUT OUT LOC BS 294.5 AND BTW STR 13 TO STR 14 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETED <BR>REPLACED ANGLE ENTRY DOOR CUT OUT LOC BS 294.5 AND BTW STR 13 TO STR 14 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OFF BELOW

Part: ACCESS PANEL — CRACKED (ZN 600 RIGHT WIN) · airframe 58,313 hrs · 35,117 cycles

CRACK ACCESS PANEL 651GB TRAILING EDGE SUPPORT PLATE RT WING 2023-422502<[01] REPLACED ACCESS PANEL 651GB TRAILING EDGE SUPPORT PLATE AT RT WING I.A.W. B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700. CRACK LENGTH: 1.978?<BR><BR>TOOL USED CALIPER P/N: 4996A52 S/N: 200814522 DUE DATE: 16/MAR/24;[02] REPLACED ACCESS PANEL 651GB TRAILING EDGE SUPPORT PLATE AT RT WING I.A.W. B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE AND APPLICABLE REPAIR ON SRM B737-700. CRACK LENGTH: 1.978? <BR><BR>TOOL USED CALIPER P/N: 4996A52 S/N: 200814522 DUE DATE: 16/MAR/24

Part: BRACKET — DAMAGED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

ELONGATED HOLE BRACKET ON BS 1016 UPPER AREA AFT GALLEY AND LAV 2023-422464<[01] REPLACED BRACKET ON BS 1016 UPPER AREA AFT GALLEY AND LAV. IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 148A2230 REV. C. SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED BRACKET ON BS 1016 UPPER AREA AFT GALLEY AND LAV. IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 148A2230 REV. C. <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 58,313 hrs · 35,117 cycles

CRACK BRACKET CENTER SECTION LOCATED BS540 TO BS559 AT LEVEL LBL6 AT LOWER FUSELAGE 2023-422411<[01] REPLACED BRACKET CENTER SECTION LOCATED BS540 TO BS559 AT LEVEL LBL6 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 212A1101 SHEET 3 REV -;[02] REPLACED BRACKET CENTER SECTION LOCATED BS540 TO BS559 AT LEVEL LBL6 AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 212A1101 SHEET 3 REV -

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CORROSION ON FLOOR BEAM 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2023-422400<[01] TOOL USED: THICKNESS GAGE. P/N: 45MG; S/N: 130060401; DUE DATE: 20-MAR-24.;[02] TOOL USED: EDDY CURRENT EQUIPMENT. P/N: NORTEC 600D. S/N: 220273012. DUE DATE: 17-DEC-23.;[03] REPAIRED FLOOR BEAM 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM-53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4 FIG. 205. SEE INDIVIDUAL SIGN-OFF BELOW.;[04] REPAIRED FLOOR BEAM 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM-53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4 FIG. 205. SEE INDIVIDUAL SIGN-OFF BELOW.<BR>AS RII

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 58,313 hrs · 35,117 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023-422387<[01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A18229508; DUE DATE 30-OCT-23;[02] TOOL USED RADIOMETER PN.XRP-3000; SN. 1998072; DUE DATE. 15-OCT-23;[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] TASK COMPLETED.

Part: LIGHT — BROKEN (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

BROKEN EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY 1 2023-422419<[01] REPLACED EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY 1 I.A.W SOPM 20-50-01 REV. 38.;[02] REPLACED EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY 1 I.A.W SOPM 20-50-01 REV. 38.

Part: STRAP — CORRODED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CORROSION FLOOR STRUCTURE ON STRAP LOCATED BS1040 BETWEEN BL 0 TO RBL 43 WL 208.1 AT AFT GALLEY AREA 2023-422404<[01] REPLACED STRAP LOCATED BS1040 BETWEEN BL 0 TO RBL 43 WL 208.1 AT AFT GALLEY AREA AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 140A9870 SHEET: 5 REV: A SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED STRAP LOCATED BS1040 BETWEEN BL 0 TO RBL 43 WL 208.1 AT AFT GALLEY AREA AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 140A9870 SHEET: 5 REV: A SEE INDIVIDUAL SIGN OFF BELOW

Part: STRAP — CORRODED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CORROSION FLOOR STRUCTURE ON STRAP LOCATED BS1040 BETWEEN BL0 TO LBL 43 AND WL 208.1 AT AFT GALLEY AREA 2023-422406<[01] REPLACED STRAP LOCATED BS1040 BETWEEN BL0 TO LBL 43 AND WL 208.1 AT AFT GALLEY AREA AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 140A9870 SHEET: 5 REV: A SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED STRAP LOCATED BS1040 BETWEEN BL0 TO LBL 43 AND WL 208.1 AT AFT GALLEY AREA AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND DWG: 140A9870 SHEET: 5 REV: A SEE INDIVIDUAL SIGN OFF BELOW

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 58,313 hrs · 35,117 cycles

CRACK BRACKET CENTER SECTION LOCATED BS540 TO BS559 AT LEVEL RBL6 AT LOWER FUSELAGE 2023-422410<[01] REPLACED BRACKET CENTER SECTION LOCATED BS540 TO BS559 AT LEVEL RBL6 AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING 212A1101 SHEET 3 REV -;[02] REPLACED BRACKET CENTER SECTION LOCATED BS540 TO BS559 AT LEVEL RBL6 AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING 212A1101 SHEET 3 REV -

Part: STUB FRAME — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON STUB FRAME LOCATED BS 294.5 BTW STR 9R TO STR 11R CUTOUT AT FWD SERVICE DOOR 2023-422409<[01] REPLACED STUB FRAME LOC. BS 294.5 BTW STR 9R TO STR 11R CUTOUT AT FWD SERVICE DOOR IAW SRM B737-700 51-10-02. SRM 51-40-02; DRAWING: 141A8370 REV. D. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED STUB FRAME LOC. BS 294.5 BTW STR 9R TO STR 11R CUTOUT AT FWD SERVICE DOOR IAW SRM B737-700 51-10-02. SRM 51-40-02; DRAWING: 141A8370 REV. D.RII ; SEE INDIVIDUAL SIGN-OFF BELOW.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 58,313 hrs · 35,117 cycles

CRACK CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023-422386<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A21146102;DUE DATE:27-NOV-23.;[02] TOOL USED RADIOMETER P/N: XRP-3000; S/N: 1753759; DUE DATE: 14-OCT-23.;[03] 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.;[04] STEP 3 VERIFIED AND CORRECTIVE ACTION COMPLETED : 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.

Part: WEB — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA 2023-422310<[01] REPLACED WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW EA-23-153-02184-WIP5 <BR>SEE TTG8Q00LZECK; SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW EA-23-153-02184-WIP5 <BR>SEE TTG8Q00ME0P8; SEE INDIVIDUAL SIGN OFFS BELOW;[03] REPLACED WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW EA-23-153-02184-WIP5 <BR>SEE TTG8Q00ME0P8; SEE INDIVIDUAL SIGN OFFS BELOW<BR>CERTIFIED AS RII

Part: WEB — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON WEB LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 LBL 46 AT FWD GALLEY AREA 2023-422303<[01] REPLACED WEB AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS312 TO BS328 RBL34 AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV. -;[02] CORRECTED STEP 1:<BR>REPLACED WEB AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS312 TO BS328 LBL46 AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV. -<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED WEB AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS312 TO BS328 LBL46 AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV. - <BR>SEE INDIVIDUAL SIGN-OFF BELOW<BR>AS RII

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 LBL 31 AT FWD GALLEY AREA 2023-422295<[01] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 LBL 31 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 REV. A SEE INDIVIDUAL SIGNOFFS BELOW;[02] RII ITEM <BR>REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 LBL 31 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 REV. A SEE INDIVIDUAL SIGNOFFS BELOW

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 RBL 34 AT FWD GALLEY AREA 2023-422288<[01] REPLACED WEB AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS312 TO BS328 RBL34 AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV. -<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1:<BR>REPLACED WEB AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS312 TO BS328 RBL34 AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV. -<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: SKIN — CRACKED (ZN 300 STABILIZE) · airframe 58,313 hrs · 35,117 cycles

CRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 25.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.773 INCHES 2023-422271<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 60009161631; CAL DUE DATE: 31-JAN-24;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101U102020 DUE DATE: 30 AUG 23.;[03] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X11290U021704; DUE DATE: 12 MAR 24.;[04] PERFORMED REPAIR ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 25.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB IAW EA# 23-155-02228 WIP1 AND EA COVER # 23-155-02228 SEE INDIVIDUAL SIGN OFFS BELOW;[05] CORRECTED STEP 4 : PERFORMED REPAIR ON RH HORIZONTAL STABILIZER LOWER INSPAR SKIN AT STATION 193.90 RIB; 25.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB IAW EA# 23-155-02228 WIP1 AND EA COVER # 23-155-02228 SEE INDIVIDUAL SIGN OFFS BELOW;[06] PERFORMED REPAIR ON RH HORIZONTAL STABILIZER LOWER INSPAR SKIN AT STATION 193.90 RIB; 25.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB IAW EA# 23-155-02228 WIP1 AND EA COVER # 23-155-02228 SEE INDIVIDUAL SIGN OFFS BELOW;[07] CORRECTED STEP 6: PERFORMED REPAIR ON RH HORIZONTAL STABILIZER LOWER INSPAR SKIN AT STATION 193.90 RIB; 25.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB IAW EA# 23-155-02228 WIP1 AND EA COVER # 23-155-02228 SEE INDIVIDUAL SIGN OFFS BELOW ITEM RII

Part: WEB — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 34 AT FWD GALLEY AREA 2023-422312<[01] REPLACED INTERCOSTAL WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 34 AT FWD GALLEY AREA IAW B737-700 SRM-51-40-02 AND DWG-141A5400 REV:- SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED INTERCOSTAL WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 34 AT FWD GALLEY AREA IAW B737-700 SRM-51-40-02 AND DWG-141A5400 REV:- SEE INDIVIDUAL SIGN-OFF BELOW RII CERTIFIED

Part: WEB — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 52 AT FWD GALLEY AREA 2023-422313<[01] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 52 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 141A5400 REV: -. SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED AND CERTIFIED RII.

Part: FLOOR SUPPORT — CORRODED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CORROSION ON INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 WL 208.1 LBL13 AT FWD GALLEY AREA 2023-422314<[01] REPLACED INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 WL 208.1 LBL13 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG 141A5600 REV. N AND DWG 141A5400 REV. B;[02] CORRECTED STEP 1:<BR>REPLACED INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 WL 208.1 LBL13 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG 141A5600 REV. N AND DWG 141A5400 REV. B. SEE INDIVIDUAL SIGN OFFS BELOW;[03] CORRECTIVE ACTION STEP 2 CERTIFIED RII

Part: SKIN — CRACKED (ZN 300 STABILIZE) · airframe 58,313 hrs · 35,117 cycles

CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 18.00 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.692 INCHES 2023-422272<[01] TOOL USED P/N NORTEC 600D S/N 60009161631 DUE DATE 31/JAN/24;[02] PERFORMED REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION193.90 RIB MORE 18? FROM FRONT SPAR INBOARD SIDE OF RIB I.A.W. B737-00 SRM 55-10-01-2R-11 REPAIR 11 <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] PERFORMED REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION193.90 RIB MORE 18? FROM FRONT SPAR INBOARD SIDE OF RIB I.A.W. B737-00 SRM 55-10-01-2R-11 REPAIR 11 <BR><BR>SEE INDIVIDUAL SIGN-OFF BELOW<BR><BR>ITEM RII

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 17R FWD GALLEY AREA 2023-422372<[01] REPLACED SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 17R FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING # 141A8310 REV: -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1. REPLACED SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 17R FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DRAWING # 141A8310 REV: -. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 17R FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DRAWING # 141A8310 REV: -. SEE INDIVIDUAL SIGN OFF BELOW.<BR>CERTIFIED AS RII

Part: WEB — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON WEB LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL 46 AT FWD GALLEY AREA 2023-422307<[01] REPLACED AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS312 TO BS328 RBL34 AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV. -<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] CORRECTED STEP 1:<BR>REPLACED AND FASTENERS LOCATED ON FLOOR STRUCTURE BTW BS328 TO BS344 LBL46 AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV. -<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: WEB — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 12 AT FWD GALLEY AREA 2023-422311<[01] REPLACED WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 12 AT FWD GALLEY AREA IAW B737-700 SRM:51-10-02 Ï¿½TEM 9 AND DWG: 141A5400 SHEET 13 REV.?;[02] CORRECTED STEP 1.<BR>REPLACED WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 12 AT FWD GALLEY AREA IAW B737-700 SRM:51-10-02 Ï¿½TEM 9 AND DWG: 141A5400 SHEET 13 REV.? SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPLACED WEB LOCATED FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 12 AT FWD GALLEY AREA IAW B737-700 SRM:51-10-02 Ï¿½TEM 9 AND DWG: 141A5400 SHEET 13 REV.? SEE INDIVIDUAL SIGNOFFS BELOW.<BR>RII

Part: SKIN — CRACKED (ZN 300 STABILIZE) · airframe 58,313 hrs · 35,117 cycles

CRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.070 INCHES. 2023-422270<[01] REFER TO FAULT TTG8Q00LZ42S WHERE EA 23-155-02228 WAS ADDED AS A SUBTASK.;[02] REFER TO FAULT TTG8Q00LZ42S WHERE EA 23-155-02228 WAS ADDED AS A SUBTASK.

Part: STRUCTURE — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON INNER CHORD LOCATED BS 303.9 AT LEVEL STR 17L AT FWD GALLEY AREA 2023-422298<[01] REPLACED INNER CHORD LOCATED BS 277 TO BS 360 AT LEVEL STR 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG-141A8110 REV:- SEE INDIVIDUAL SIGN-OFF BELOW;[02] RII ITEM <BR>REPLACED INNER CHORD LOCATED BS 277 TO BS 360 AT LEVEL STR 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG-141A8110 REV:- SEE INDIVIDUAL SIGN-OFF BELOW

Part: BEAM — CORRODED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CORROSION ON EXISTING REPAIR LOCATED BS 344 LBL 7 WL 208.1 AT FWD GALLEY AREA 2023-422348<[01] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138203 AND DUE DATE: 09-JUN-24.;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X1693P030456; DUE DATE: 12 MAR 24.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[04] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X12101U102020 DUE DATE: 30 AUG 23.;[05] PERFORMED REPAIR ON FLOOR BEAM BS 344 BTW LBL20 AND RBL 10 AT FWD GALLEY AREA IAW EA-23-153-02184-WIP1; EA- 23-153-02184-WIP2; EA-23-153-02184-WIP3; EA-23-153-02184-WIP4; EA-23-153-02184-WIP5; AND SUMMARY EA-23-153-02184 SEE INDIVIDUAL SIGN OFFS BELOW.;[06] PERFORMED REPAIR ON FLOOR BEAM BS 344 BTW LBL20 AND RBL 10 AT FWD GALLEY AREA IAW EA-23-153-02184-WIP1; EA- 23-153-02184-WIP2; EA-23-153-02184-WIP3; EA-23-153-02184-WIP4; EA-23-153-02184-WIP5; AND SUMMARY EA-23-153-02184 SEE INDIVIDUAL SIGN OFFS BELOW.<BR>CERTIFIED AS RII

Part: STRINGER CLIP — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2023-422353<[01] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM-51-0-02 AND DWG-141A8380 REV: - SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM-51-0-02 AND DWG-141A8380 REV: - SEE INDIVIDUAL SIGN-OFF BELOW RII CERTIFIED

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 RBL 16 AT FWD GALLEY AREA 2023-422291<[01] REPLACED INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 RBL 16 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400; SHEET 45 AND REV: A SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 294.5 TO BS 312 RBL 16 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400; SHEET 45 AND REV: A; RII SEE INDIVIDUAL SIGN OFF BELOW

Part: BEAR STRAP — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON BEAR STRAP LOCATED BTW BS 303.9 TO BS 294 AT LEVEL STR 9R AT FWD GALLEY AREA 2023-422362<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 210138203 AND DUE DATE: 09-JUN-24.;[04] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[05] PERFORMED REPAIR ON BEAR STRAP LOC. BTW BS303.9 TO BS294 AT LEVEL STR 9R FWD GALLEY AREA I.A.W EA 23-153-02160-WIP1 AND EA SUMMARY 23-153-02160.SEE INDIVIDUAL STEP SIGN OFFS BELOW;[06] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA 2023-422296<[01] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG# 141A5400; SHEET 20; REV.-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK CARD COMPLETED <BR>REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG# 141A5400; SHEET 20; REV.-. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,313 hrs · 35,117 cycles

CRACK ANGLE BS 663.75 AND RBL 43 CENTER SECTION AT LOWER FUSELAGE 2023-422260<[01] FAULT RESOLVED ON TASK CARD TTG8Q00LYWBF WHERE ANGLE IS REPLACED;[02] FAULT RESOLVED ON TASK CARD TTG8Q00LYWBF WHERE ANGLE IS REPLACED

Part: LIGHT — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2023-422267<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802;[02] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802

Part: BEAM — CRACKED (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

CRACK INDICATION FOUND AT 141A6536-14 BEAM. #4 AT FWD SERVICE DOOR. CRACK LENGHT 0.800 INCH APPROX. (EO 5241-C-14093 OR 5241-C-14344 WILL BE ADDED TO THE REPAIR ORDER FOR REPAIR) 2023-422266<[01] REPLACED BEAM#4 LOCATED ON FWD SERVICE DOOR I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DWG# 141A6516; SHEET 92; REV.-. AND DWG# 141A6535; SHEET 3; REV.D. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED BEAM#4 LOCATED ON FWD SERVICE DOOR I.A.W B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DWG# 141A6516; SHEET 92; REV.-. AND DWG# 141A6535; SHEET 3; REV.D. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,313 hrs · 35,117 cycles

CRACK ON ANGLE BS 663.75 AND; RBL 6 AT CENTER SECTION LOWER FUSELAGE 2023-422258<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24.;[02] REPLACED ANGLE LOC. BS 663.75 AND; RBL 6 AT CENTER SECTION LOWER FUSELAGE IAW B737-700 SRM 51-40-02-0G-0 AND DWG: 111A1000 SHEET 180 REV. B; SEE INDIVIDUAL SIGN-OFF BELOW.;[03] REPLACED ANGLE LOC. BS 663.75 AND; RBL 6 AT CENTER SECTION LOWER FUSELAGE IAW B737-700 SRM 51-40-02-0G-0 AND DWG: 111A1000 SHEET 180 REV. B; RII SEE INDIVIDUAL SIGN-OFF BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,313 hrs · 35,117 cycles

CRACK ANGLE BS 663.75 AND LBL 43 CENTER SECTION AT LOWER FUSELAGE 2023-422264<[01] FAULT RESOLVED ON TASK CARD TTG8Q00LYWL WHERE ANGLE IS REPLACED;[02] CORRECTED STEP 1:<BR>FAULT RESOLVED ON TASK CARD TTG8Q00LYWL WHERE ANGLE IS REPLACED;[03] CORRECTED STEP 2:<BR>FAULT RESOLVED ON TASK CARD TTG8Q00LYWLN WHERE ANGLE IS REPLACED;[04] FAULT RESOLVED ON TASK CARD TTG8Q00LYWLN WHERE ANGLE IS REPLACED

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,313 hrs · 35,117 cycles

CRACK ANGLE BS 663.75 AND LBL 6 CENTER SECTION AT LOWER FUSELAGE 2023-422262<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24.;[02] REPLACED ANGLE LOCATED BS 663.75 AND LBL 6 CENTER SECTION AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02-0G-0 AND DWG: 111A1000 SHEET 171 REV. -; SEE INDIVIDUAL SIGN-OFF BELOW.;[03] TASK CARD COMPLETED <BR>REPLACED ANGLE LOCATED BS 663.75 AND LBL 6 CENTER SECTION AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02-0G-0 AND DWG: 111A1000 SHEET 171 REV. -; SEE INDIVIDUAL SIGN-OFF BELOW.<BR>RII

Part: BATTERY — INOPERATIVE (ZN 200 FUS TOP) · airframe 58,313 hrs · 35,117 cycles

INOP EMERGENCY DOOR BATTERY PACK RH AT PASSENGER CABIN (1 EA) 2023-422180<[01] REPLACED EMERGENCY DOOR BATTERY PACK RH AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 33-51-06-960-805. TEST IS OK. <BR>SEE INDIVIDUAL SIGNOFF BELOW.;[02] CERTIFIED WORK PERFORMED

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 58,313 hrs · 35,117 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 695 BL 0 LT SIDE AT CENTER SECTION 2023-422187CRACK ON SUPPORT ANGLE (BRACKET) LOCATED BS 695 BL 0 LT SIDE AT CENTER SECTION<[01] REPLACED SUPPORT ANGLE (BRACKET) LOCATED BS 695 BL 0 LT SIDE AT CENTER SECTION IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 273A9110 REV. A. SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED SUPPORT ANGLE (BRACKET) LOCATED BS 695 BL 0 LT SIDE AT CENTER SECTION IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 273A9110 REV. A. SEE INDIVIDUAL SIGN OFFS BELOW RII CERTIFIED

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 58,313 hrs · 35,117 cycles

CRACK ANGLE TRAILING EDGE ORSS 267 DEFLECTION CONTROL RIB LT WING 2023-422362<[01] REPLACED ANGLE TRAILING EDGE ORSS 267 DEFLECTION CONTROL RIB LT WING I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02 AND DWG 115A2930 SHEET 7 REV. - DUE TO NOT FOUND ALLOWABLE DAMAGE AND APLICABLE REPAIR ON SRM 57-51-02 <BR><BR>CRACK LENGTH 0.475? <BR><BR>TOOL USED CALIPER P/N 500-196-30 S/N A20231600 DUE DATE 12/SEP/23;[02] TASK COMPLETED

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 58,192 hrs · 35,036 cycles

FWD ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED GIRT ON FWD ENRTY DOOR REF AMM 25-66-01.

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 58,192 hrs · 35,036 cycles

FWD SERVICE DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED GIRT ON FWD SVC DOOR REF AMM 25-66-01.

Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 58,192 hrs · 35,036 cycles

AFT ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED GIRT BAR ON AFT ENTRY DOOR REF AMM 25-66-01

Part: LIGHT — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 57,966 hrs · 34,890 cycles

FORWARD SERVICE ENTRY DOOR EXIT LIGHT COVER NEEDS RESECURED<[01] RESECURED SCREW ON LIGHT COVER PER SIP

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 57,689 hrs · 34,719 cycles

SEVERAL EMERGENCY LIGHTS INOP AFT CABIN<[01] REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK M1672 REF AMM 33-51-06. OPS CHECK GOOD;[02] REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK M1672 REF AMM 33-51-06. OPS CHECK GOOD. FOR PARTS INFORMATION . PART # ON AD-D717-01-100SWA. BN 334086. PART # OF D717-01-100SWA. BN 354888.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 57,479 hrs · 34,582 cycles

ROW 16DEF; 18DEF EMERGENCY LIGHTS INOP ; AFT EMERGENCY EXIT SIGN LIGHT INOP ..<[01] R+R AFT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD

Part: GIRT BAR — UNSECURE (SERVICE DOOR) · airframe 57,081 hrs · 34,315 cycles

FWD SERVICE DOOR SLIDE GIRT BAR HANGING LOW.<[01] REPOSITIONED GURT BAR PER M/M 25-66-01.NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (AFT FUSELAGE) · airframe 55,626 hrs · 33,310 cycles

RH EXTERIOR AFT LOWER EMERGENCY LIGHT INOP. / [01] RELAMPED LH EXTERIOR AFT LOWER EMERG. LIGHT IAW AMM 33-51-04. OPS CHECK GOOD

Part: PANEL — ELONGATED (FUSELAGE) · airframe 55,257 hrs · 33,059 cycles

PANEL 193B HAS NUMEROUS ELONGATED COUNTERSINK HOLES / [01] REPLACED PANEL 193B PER SRM 51-40-02

Part: LIGHT — LOOSE (CABIN) · airframe 53,783 hrs · 32,131 cycles

PLASTIC EXIT SALIDA SIGN FELL OFF MID CABIN ; / [01] REPLACED MID CABIN CEILING EXIT SIGN LIGHT ASSY PER AMM 33-51-01

Part: ANGLE — ELONGATED (BS 857-867) · airframe 53,078 hrs · 31,709 cycles

ELONGATED HOLE FLOOR STRUCTURE ANGLE LOCATED BETWEEN BST 857 TO BST 867 STR 25 RH AT AFT CARGO COMPARTMENT ; 2021-392222 / REPLACED ANGLE LOCATED BETWEEN BST 857 TO BST 867 STR 25 RH AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 SRM 51-40-02 AND DWG 146A8123 .; [16] STEP 14 COMPLETED RII ITEM; [17] TASK COMPLETED RII

Part: ANGLE — DAMAGED (BS 787-792) · airframe 53,078 hrs · 31,709 cycles

ELONGATED HOLE FLOOR STRUCTURE ANGLE LOCATED BETWEEN BST 787 TO BST 792 STR 25R AT AFT CARGO COMPARTMENT ; 2021-392221 / [16] REPLACED ANGLE LOCATED BETWEEN BST 787 TO BST 792 STR 25R AT AFT CARGO COMPARTMENT B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG 146A8123; [17] STEP 15 COMPLETED RII ITEM; [18] TASK COMPLETED RII

Part: SUPPORT — CORRODED (BS 440-500C) · airframe 53,078 hrs · 31,709 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS440 TO BS500C LBL21.80 AND WL154.5 AT FWD CARGO COMPARTMENT ; 2021-392192 / [23] REPLACED SUPPORT ZEE LOC. BTW BS396 TO BS500D AT LEVEL STR 26L LBL21.80 AND WL154.5 ON FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DWG 143A7501 REV. A; [24] STEP 22 COMPLETED <BR>RII; [25] TASK CARD COMPLETED.

Part: FRAME — CRACKED (BS 312) · airframe 53,078 hrs · 31,709 cycles

CRACK FRAME LOCATED BS312 ENTRY DOOR CUT OUT AT PASSENGER CABIN ; 2021-392204 / [01] EVALUATED DAMAGE ON FRAME LOCATED BS312 ENTRY DOOR CUT OUT AT PASSENGER CABIN AND NO FOUND ALLOWABLE DAMAGE LIMITS ON SRM MUST BE REPAIRED MEASURE OF CRACK ARE: L: 0.283 INCH. TOOL USED DIGITAL CALIPER P/N: DIGITAL 150 S/N: AE-412610 DUE DATE: 21-MAY-22; [05] VERIFIED STEP 3 AND 4; [06] PERFORMED TRIM OUT OF DAMAGE PORTION ON REPAIR AREA FRAME LOCATED BS312 BTW S-4L AND S-5L ENTRY DOOR CUT OUT AT PASSENGER CABIN IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 FIGURE 202 TOOL USED CALIPER P/N: 500-752-20 S/N: B16101265 DUE DATE: 20APR22 RADIUS GAGE P/N: 2204A3 S/N: AE-408657 DUE DATE: 02NOV21; [07] PERFORMED BENT OF REPAIR ANGLE [1] IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 AND B737-700 SRM 51-30-01 MATERIAL USED ALUMINUM SHEET 7075T0-0.063 PO 2021 129486 TOOL USED RADIUS GAGE P/N: 2204A3 S/N: AE-408657 DUE DATE: 02NOV21; 12] HFEC INSPECTION DONE ON EDGES FRAME CUTOUT LOC. BS 312; FWD ENTRY DOOR CUTOUT IAW NDT MANUAL 51-00-00 PART6; PROCEDURE 23. CRACK INDICATION NOT FOUND. TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC500D; S/N: N500X1693P030456; CAL DUE DATE:30-NOV-21.;[23] INSTALLED REPAIR REPAIR ANGLE [1] AND FASTENER ON FRAME BS312 BTW S-4L AND S-5L ENTRY DOOR CUT OUT AT PASSENGER CABIN IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 AND B737-700 SRM 51-40-02;

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 53,078 hrs · 31,709 cycles

CORROSION SUPPORT ZEE LOCATED BS500A TO BS500D RBL21.80 AND WL154.5 AT FWD CARGO COMPARTMENT ; 2021-392193 / REPLACED SUPPORT ZEE LOCATED BS500A TO BS500D RBL21.80 AND WL154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ; SRM 5140-02 AND DWG DWG 143A7500 REV - MATERIAL USED BAC1496-444 PO 2019555053; [18] STEP 16 COMPLETED RII ITEM; [19] TASK COMPLETED RII

Part: WEB — CORRODED (BS 500-500A) · airframe 53,078 hrs · 31,709 cycles

CORROSION WEB - INTERCOSTAL LOCATED ON BS500 TO BS500A RBL21.8 AND WL154.5 AT FWD CARGO COMPARTMENT ; 2021-392194 / [07] INSTALLED NEW WEB - INTERCOSTAL AND FASTENERS LOCATED ON BS500 TO BS500A RBL21.8 AND WL154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080 REV-.; [08] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED ON BS500 TO BS500A RBL21.8 AND WL154.5 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A0080 REV-; [09] CERTIFIED STEP 7 & 8 RII.

Part: STRAP — CORRODED (BS 727D) · airframe 53,078 hrs · 31,709 cycles

CORROSION STRAP LOCATED BS727D BETWEEN LBL21 TO RBL21 AND WL154.5 AFT CARGO COMPARTMENT ; 2021-392180 / REPLACED STRAP LOCATED BS727D BETWEEN LBL21 TO RBL21 AND WL154.5 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02.RII <BR>TASK COMPLETED.

Part: SUPPORT — CORRODED (BS 727A-767) · airframe 53,078 hrs · 31,709 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS727A TO BS767 AND RBL21 WL154.5 AFT CARGO COMPARTMENT ; 2021-392159 / [17] REPLACED SUPPORT ZEE SECTION LOCATED ON BETWEEN BS 727+4 INCHS TO BS 767 AND RBL 21 WL 154.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A7500 REV A.; [18] STEP 16 COMPLETED RII ITEM; [19] CORRECTED STEP 7 STEP 6 CERTIFIED AS RII.; [20] STEP 17 COMPLETE RII

Part: ANGLE — CRACKED (BS 500C) · airframe 53,078 hrs · 31,709 cycles

CRACK ANGLE - CLIP LOCATED FWD FACE BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT ; 2021-392155 / [01] REMOVED ANGLE - CLIP LOCATED FWD FACE BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NOT FOUND MORE DAMAGE; LARGE OF CRACK IS:1.15 INCH TOOL USED DIGITAL CALIPER P/N:700-113-10 S/N:0033174 DUE DATE:08/JAN/22; DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700 ANGLE CLIP MUST BE REPLACED; [02] STEP 1 COMPLETED; [03] DRILLED NEW HOLES ON ANGLE - CLIP LOCATED FWD FACE BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT ON NEW HOLES ANGLE - CLIP LOCATED FWD FACE BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-20-01.; [04] OK TO INSTALL ANGLE - CLIP LOCATED FWD FACE BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT.; [05] COMPLETED STEP 3 AND 4<BR>RII; [06] INSTALLED ANGLE - CLIP LOCATED FWD FACE BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 SRM 51-40-02 AND DWG 143A7505 SHEET 5 REV B.; [07] REPLACED ANGLE - CLIP LOCATED FWD FACE BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 SRM 51-40-02 AND DWG 143A7505 SHEET 5 REV B.; [08] STEP 6 COMPLETED RII; [09] STEP 7 COMPLETED RII<BR>TASK CARD COMPLETED

Part: SUPPORT — CORRODED (BS 727C-807) · airframe 53,078 hrs · 31,709 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS727C TO BS807 AND LBL21 WL154.5 AFT CARGO COMPARTMENT ; 2021-392160 / [25] REPLACED SUPPORT ZEE LOCATED BETWEEN BS727 TO BS847 AND LBL21 WL154.5 AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 146A7500 SHEET 85 REV A:; [26] TASK CARD COMPLETE AND CERTIFIED AS RII.

Part: WEB — CRACKED (BS 927-947) · airframe 53,078 hrs · 31,709 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS927 TO BS947.5 AT LEVEL STR25R AFT CARGO COMPARTMENT ; 2021-392167 / [19] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED BTW BS 927 AND BS 947.5 AT STR 25R IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02 AND DWG 147A7500 REV -; RII

Part: WEB — CORRODED (BS 767-794) · airframe 53,078 hrs · 31,709 cycles

CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS767 TO BS794 AND RBL21 WL154.5 AFT CARGO COMPARTMENT ; 2021-392161 / REPLACED WEB-INTERCOSTAL LOCATED BETWEEN BS 767 TO BS 794 AND RBL21; WL154.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND IAW B737-700 SRM 51-40-02 AND DRAWING #146A0081 SHEET 34 REV -.; [14] CERTIFIED STEP 13 RII

Part: SUPPORT ANGLE — CRACKED (BS 867) · airframe 53,078 hrs · 31,709 cycles

CRACK ANGLE - SUPPORT LOCATED BS867 AT LEVEL STR26L AFT CARGO COMPARTMENT ; 2021-392163 / REPLACED ANGLE SUPPORT LOCATED BS867 AT LEVEL STR26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40- 02 AND B737-700 SRM 51-10-02 ITEM 9 DWG 149A8102 SHEET 17 REV. .

Part: GUSSET — CRACKED (BS 500D) · airframe 53,078 hrs · 31,709 cycles

CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT ; 2021-392156 / [01] EVALUATED DAMAGE ON GUSSET AND NOT FOUND ALLOWABLE DAMAGE LIMITS IN SRM B737-700; REMOVED GUSSET AND FASTENERS IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON COMMON AREA OF REMOVED PART AND NOT FOUND ANY DAMAGE; LENGTH OF CRACK IS 0.660 TOOL USED DIGITAL CALIPER P/N: DIGITAL 150; S/N: AE-412604; DUE DATE: 28/MAY/22; [02] STEP 1 COMPLETE; [03] DRILLED NEW GUSSET IAW B737-700 SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT ON NEW HOLES IAW 51-20-01; [04] OK TO INSTALL NEW GUSSET AND FASTENERS GRANTED; [05] STEP 3 AND STEP 4 COMPLETE..RII ITEM; [06] INSTALLED NEW GUSSET AND FASTENERS LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG:143A7902 SHEET:174 REV:-; [07] STEP 6 COMPLETE.RII; [08] REPLACED GUSSET AND FASTENERS LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG:143A7902 SHEET:174 REV:-; [09] VERIFIED STEP 8; RII

Part: GUSSET — CRACKED (BS 500D) · airframe 53,078 hrs · 31,709 cycles

CRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT ; 2021-392157 / [01] EVALUATED DAMAGE ON GUSSET AND NOT FOUND ALLOWABLE DAMAGE LIMITS IN SRM B737-700; REMOVED GUSSET AND FASTENERS IAW B737-700 SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON COMMON AREA OF REMOVED PART AND NOT FOUND ANY DAMAGE; LENGTH OF CRACK IS 0.348 TOOL USED DIGITAL CALIPER P/N: DIGITAL 150; S/N: AE-412604; DUE DATE: 28/MAY/22; [02] STEP 1 COMPLETE; [03] DRILLED NEW GUSSET IAW B737-700 SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT ON NEW HOLES IAW 51-20-01; [04] OK TO INSTALL NEW GUSSET AND FASTENERS GRANTED; [05] STEP 3 AND STEP 4 COMPLETE.. RII ITEM; [06] INSTALLED NEW GUSSET AND FASTENERS LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG:143A7902 SHEET:174 REV:-; [07] STEP 6 COMPLETE.RII; [08] REPLACED GUSSET AND FASTENERS LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG:143A7902 SHEET:174 REV:-; [09] VERIFIED STEP 8; RII

Part: ANGLE — ELONGATED (BS 847) · airframe 53,078 hrs · 31,709 cycles

ELONGATED HOLE ANGLE LOCATED BS847 AND RBL 21 AT AFT CARGO COMPARTMENT ; 2021-392173 / [14] REPLACED ANGLE AND FASTENERS LOCATED BS847 AND RBL 21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 DRAWING 146A8321 REV<BR>RII

Part: SUPPORT ANGLE — CRACKED (BS 540) · airframe 53,078 hrs · 31,709 cycles

CRACK SUPPORT ANGLE LOCATED BS540 BETWEEN BL0 TO RBL24 AT PASSENGER CABIN ; 2021-392083 / [10] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS540 BETWEEN BL0 TO RBL24 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 143A0060 SHEET 2 REV. B.; [11] COMPLETED TASK CARD WITH STEP 10 RII

Part: PLATE — CRACKED (BS 787-794 S25R) · airframe 53,078 hrs · 31,709 cycles

CRACK PLATE LOCATED BTW BS 787 TO BS 794 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT ; 2021-392097 / [01] REPLACED PLATE LOCATED BTW BS 787 TO BS 794 AT LEVEL STR 25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 TEM 9; [02] TASK COMPLETED RII ITEM

Part: STRINGER — CRACKED (BS 540 S25R) · airframe 53,078 hrs · 31,709 cycles

CRACK STRINGER 25R ; BS 540 FWD CARGO COMPARTMENT ; 2021-392103 / PERFORMED PERMANENT REPAIR ON STR 25R LOCATED BTW BS 500C + 4 INCH AND BS 540 IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 MATERIAL USED ALUMINUM SHEET P/N: 7075-T0/0.036Ï¿½ PO: 2021-131796 HEAT TREATED AND CONVERTED FROM 7075-T0 TO 7075T6 AND P/N: BAC1493-659, P/O: 2021 135314, P/N: BAC1493-249, P/O: 2021 147833.

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 53,078 hrs · 31,709 cycles

CRACK ANGLE LOCATED BS695 AND RBL24 AT CENTER WING BOX ; 2021-392080 / [15] REPLACED ANGLE LOCATED BS695 AND RBL24 AT CENTER WING BOX IAW B737-700 SRM 51-40-02 AND DWG 273A9110 SHEET 4 REV - AND DWG 111A6000 SHEET 2 REV. B. MATERIAL USED: BAC1490-2782; PO#2021-184600.; [16] TASK CARD COMPLETED <BR>RII

Part: BULKHEAD — CRACKED (AFT CARGO) · airframe 53,078 hrs · 31,709 cycles

CRACK BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT (1 EA) ; 2021-392093 / [01] FABRICATED BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING# 453A2510 REV ; MATERIAL USED: A60SG4W 60144; PO#2021-139302.; [02] FABRICATED BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING# 453A2510 REV ; MATERIAL USED: A60SG4W 60144; PO#2021-139302.

Part: STRINGER — CRACKED (BS 540 S25L) · airframe 53,078 hrs · 31,709 cycles

CRACK STRINGER 25L AT BS 540 FWD CARGO COMPARTMENT (1 EA) ; 2021-392102 / INSTALLED REPAIR PARTS STRINGER SECTION (1EA); ANGLE (2EA); CHANNEL (1EA); SHEAR TIE (1EA); TIE CLIP (1EA) AND FILLER (1EA) AND FASTENERS LOC. BTW BS500D BS540 AND BTW STR24L TO STR25L IAW B737-700 SRM,NG,NRC,2021-09-07 16:55:15,16Y,Y,MX,0,0,,CRACK STRINGER 25L AT BS 540 FWD CARGO COMPARTMENT (1 EA) ; 2021-392102"

Part: STRINGER — CRACKED (BS 540 S21R) · airframe 53,078 hrs · 31,709 cycles

CRACK STRINGER 21R ; BS 540 FWD CARGO COMPARTMENT ; 2021-392087 / [24] PERFORMED PERMANENT REPAIR ON STRINGER 21 RH BTW BS 500D MORE 3 INCH TO BST 540 FWD CARGO COMPARTMENT IAW B737-700,NG,NRC,2021-09-08 19:24:31,16Y,Y,MX,0,0,,CRACK STRINGER 21R ; BS 540 FWD CARGO COMPARTMENT ; 2021-392087"

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 53,078 hrs · 31,709 cycles

CRACK FLOOR PANEL 241BF AT PASSENGER CABIN ; 2021-392014 / REPAIRED FLOOR PANEL 241BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 53,078 hrs · 31,709 cycles

CRACK LEADING EDGE LOC ON RIB LE STA 105.26 AT LT HORIZONTAL STABILIZER ; 2021-391874 / [19] REPLACE RIB AND FASTENER LOC. ON LE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG:186A1001 SHEET:10 REV:A; RII.

Part: FLOOR PANEL — MISSING (CABIN) · airframe 53,078 hrs · 31,709 cycles

MISSING MATERIAL FLOOR PANEL 241DF AT PASSENGER CABIN ; 2021-392018 / REPAIRED FLOOR PANEL 241DF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 53,078 hrs · 31,709 cycles

MISSING MATERIAL FLOOR PANEL 231XF AT PASSENGER CABIN ; 2021-391970 / REPAIRED FLOOR PANEL 231XF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.

Part: FLOOR PANEL — MISSING (CABIN) · airframe 53,078 hrs · 31,709 cycles

MISSING MATERIAL FLOOR PANEL 241AF AT PASSENGER CABIN ; 2021-392013 / [24] REPAIRED FLOOR PANEL 241AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 53,078 hrs · 31,709 cycles

CRACK ACCESS PANEL 561BB TRAILING EDGE LOC. HOLES ATTACHED AERODYNAMIC SEAL AT LT WING ; 2021-391911 / [27] CORRECT STEP IS: REPAIRED ACCESS PANEL 561BB AT LT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9.; [28] REPAIRED ACCESS PANEL 561BB AT LT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9.

Part: FLAP — DELAMINATED (L/H WING) · airframe 53,078 hrs · 31,709 cycles

DELAMINATED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING ; 2021-391937 / [01] EVALUATED DELAMINATION ON IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING AND FOUND OUT OF LIMITS TO REPAIR AS PER B737-700 SRM 57-53-01-2R-7 REPAIR 7 TABLE 201 DAMAGE SIZE IS L=31.0 INCH W=9.0 INCH TOTAL AREA IS 279 SQUARE INCH. TOOL USED: CALIPER P/N:500-752-20 S/N:B21034751 DUE DATE: 11-AUG-22; [02] REPLACED I/B MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING IAW B737-700 SRM 51-40-02; [03] TASK COMPLETED

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 53,078 hrs · 31,709 cycles

CRACK ACCESS PANEL 661BB TRAILING EDGE LOC. HOLES ATTACH AERODYNAMIC SEAL AREA AT RT WING ; 2021-391916 / [25] REPAIRED ACCESS PANEL 661BB TRAILING EDGE LOC. HOLES ATTACHED AERODYNAMIC SEAL AREA AT RT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9.; [26] CORRECT STEP IS: REPAIRED ACCESS PANEL 661BB AT RT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9.; [27] REPAIRED ACCESS PANEL 661BB AT RT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 51,704 hrs · 30,875 cycles

CREW REPORTED FWD SVC. DOOR SLIDE FABRIC DRAGGING ON THE FLOOR. REPOSITIONED SLIDE ASSY REF. MM 25-66-01

Part: SUPPORT — CRACKED (LT W-B FAIRING) · airframe 50,678 hrs · 30,257 cycles

LEFT WING TO BODY FAIRING 194 GL FWD UPPER VERTICAL SUPPORT CRACKED. / REMOVED AND REPLACED VERTICAL SUPPORT PER SRM 51-40-02

Part: SKIN — DELAMINATED (LT WINGLET) · airframe 50,280 hrs · 29,994 cycles

L/H WINGLET UPPER SKIN DELAMINATED AT T/E WEDGE. LENGTH - 6.750'. DAMAGE BEYOND LIMITS PER AVIATION PARTNERS SUPPLEMENT DOC. # AP37.1-0632 / REF LP # 1247627 PER ACTION TAKEN EA # 20-157-00840.

Part: SKIN — DELAMINATED (LT WING) · airframe 50,280 hrs · 29,994 cycles

L/H WING LET LWR SKIN DELAMINATED AT T/E WEDGE. LENGTH = 6.900' DAMAGE BEYOND LIMITS PER AVIATION PARTNERS SUPPLEMENT DOC # AP37.1-0632 / DMA# 0454507 REMOVED AND REPLACED LH WINGLET PER AMM 57-21-21. CL# 40894 POS LH WING TAG 590695 P/N OFF 737-0010-33 S/N OFF N0156 P/N ON 737-0010-359 S/N ON C0643

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 49,585 hrs · 29,571 cycles

R1 DOOR SLIDE IN RED BAND. / R&R SLIDE PER AMM & MT.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 49,433 hrs · 29,462 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1670, M1673 AND M1675 IN CABIN. R & R THE BATTERY PACKS IAW AMM.

Part: FLAP TRACK — LOOSE (RT WING) · airframe 49,433 hrs · 29,462 cycles

RIGHT WING OUTBOARD AFT FLAP INBOARD TRACK LOOSE AT AFT ATTACH POINT. R & R THE FLAP TRACK IAW MM.

Part: FLAP TRACK — LOOSE (RT WING) · airframe 49,433 hrs · 29,462 cycles

RIGHT WING OUTBOARD AFT FLAP OUTBOARD TRACK LOOSE AT AFT ATTACH POINT. R & R THE FLAP TRACK IAW MM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 48,130 hrs · 28,586 cycles

R/H HORIZONTAL STABILIZER LEADING EDGE PANEL 341B, RIB AT LEADING EDGE CRACKED AT STA. 95.96, LOWER AFT EDGE. / REPAIRED RIB IAW SRM AND DWG.

Part: PANEL — CRACKED (RIGHT WING) · airframe 48,130 hrs · 28,586 cycles

PNL 621PB HAS CRACK AFT O/B T/E CORNER NEAR FASTENER HOLE / REPAIRED PNL 621PB AFT O/B T/E CORNER FASTNER HOLE I/A/W SRM 51-70-04-2R-9 REV 68; SRM 51-70-04-22-0 GENERAL REV 68; SRM 57-41-01-2R-6 REV 68; SRM 551-70-04-2R-3 REV 68.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 48,130 hrs · 28,586 cycles

AFT CARGO;FWD SCUFF PLATE HAS DAMEGE(CRACK) / AFT CARGO FWD CRACKED SCUFF PLATE REPAIRED ON WORK ORDER NO 39868-8300-0002 + EA 1-A53-2076 REV 11.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 48,130 hrs · 28,586 cycles

AFT CARGO; AFT SCUFF PLATE HAS DAMAGE(CRACK) / AFT CARGO AFT CRACKED SCUFF PLATE REPAIRED ON WO # 39868-8300-0001 & EA 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 48,130 hrs · 28,586 cycles

FWD CARGO;AFT SCUFF PLATE HAS DAMAGE (CRACK) / REPAIRED DAMAGE (CRACK) ON FWD CARGO; AFT SCUFF. PLATE IAW S/W EA 1A53-2076 REV:11.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 48,130 hrs · 28,586 cycles

L/H HORIZONTAL STABILIZER RIB 5 STIFFENER CRACKED NEAR THE LOWER END. / R&R STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 48,130 hrs · 28,586 cycles

L/H HORIZONTAL STABILIZER RIB 5 STIFFENER 2 CRACKED NEAR THE LOWER END. REPAIRED STIFFENER 2 IAW SRM & DWG.

Part: NONE — CRACKED (R/H WING) · airframe 48,130 hrs · 28,586 cycles

R/H WING AFT TRAILING EDGE CAVITY ABOVE #6 FLAP TRACK ASSY WIGGLE PLATE IS CRACKED / REMOVED AND REPLACED #6 FLAP TRACK ASSY WIGGLE PLATE AT R/H WING AFT TRAILING EDGE CAVITY IAW SRM 51-40-02-0G-0; BOEING DRAWING 115A2781 REV -. RESTORED FINISH ON AREA IAW AMM 51-21-72-370-801; AMM 51-21-41-701

Part: PANEL — CRACKED (RT WING TE) · airframe 48,130 hrs · 28,586 cycles

R/H WING TRAILING EDGE PANEL 661BB AFT EDGE INTERNAL SIDE OF FASTENER HOLES CRACKED. / REPAIRED PANEL 661BB IAW SRM.

Part: PANEL — CRACKED (RT WING TE) · airframe 48,130 hrs · 28,586 cycles

R/H WING TRAILING EDGE PANEL 661CB AFT EDGE INTERNAL SIDE OF FASTENER HOLES CRACKED. / REPAIRED PANEL 661CB IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 48,130 hrs · 28,586 cycles

L/H WING AFT TRAILING EDGE CAVITY ABOVE #3 FLAP TRACK ASSEMBLY WIGGLE PLATE ASSEMBLY CRACKED INBOARD SIDE CORNER. / R&R WIGGLE PLATE IAW SRM & DWG.

Part: PLATE — CRACKED (R/H WING) · airframe 48,130 hrs · 28,586 cycles

R/H WING AFT TRAILING EDGE CAVITY WIGGLE PLATE ABOVE BOTTOM ACCESS PNL 651GB IS CRACKED / R/H WING AFT TRAILING EDGE CAVITY WIGGLE PLATE ABOVE BOTTOM ACCESS PNL 651 GB WAS REMOVED DUE TO CRACK REPLACED VERIFIED P/N 115A2781-14 A TAG WN6612 LOCATED DRILLED AND INSTALLED AND REAPPLIED FINISHES IAW B 737 SRM 51-40-02 BOEING DRAWING 115A2001 REV A BOEING DRAWING 115A2781 REV B B 737 SRM 51-40-05 AMM 51-21-41 AMM 51-21-72 AND AMM 51-21-81

Part: BRACKET — CRACKED (LEFT WING) · airframe 48,130 hrs · 28,586 cycles

L/H WING AFT TRAILING EDGE CAVITY 9.50' INBD OF DEFLECTOR RIB BOTTOM CURVED BULB SEAL RETENTION BRACKET IS CRACKED ON FWD SIDE AS MARKED / REMOVED AND REPLACED RETENTION BRACKET FOR BOTTOM CURVED BULB SEAL AT L/H WING AFT TRAILING EDGE CAVITY; 9.50' INBD OF DEFLECTOR RIB IAW DRAWING 115A2930 REV- AND B737 SRM 51-40-02-0G-0

Part: PANEL — CRACKED (RT WING TE) · airframe 48,130 hrs · 28,586 cycles

R/H WING TRAILING EDGE PANEL 661AB AFT EDGE INTERNAL SIDE OF FASTENER HOLES CRACKED. / REPAIRED PANEL 661AB IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 48,130 hrs · 28,586 cycles

L/H WING AFT TRAILING EDGE CAVITY ABOVE BOTTOM ACCESS PANEL 551GB WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: NONE — CRACKED (RIGHT WING) · airframe 48,130 hrs · 28,586 cycles

R/H WING AFT TRAILING EDGE CAVITY INBD SIDE OF DEFLECTION RIB L BRACKET ON THE FWD SIDE OF STRUCTURE AS MARKED IS CRACKED / REMOVED DAMAGED SUPPORT CLIP @ R/H T/E DEFLECTION RIB IAW SRM 51-40-02-0G-0 AND INSTALLED NEW -2 SUPPORT CLIP @ R/H T/E DEFLECTION RIB IAW BOEING DWG 115A6200 REV:- A-TAG A13728

Part: PANEL — CRACKED (AILERON LH) · airframe 48,130 hrs · 28,586 cycles

LEFT AILERON HINGE PANEL 572BB HAS A CRACKED FASTENER HOLE / LOCATED AND DRILLED NEW L/H AILERON HINGE PANEL PART # 113A718043 ATG: 16432 IAW SRM 51-40-05-0G-0 AND INSTALLED IAW SRM AIPC 27-11-11-02 AND SRM 51-40-02-0G-0 AND AMM 27-11-00-210-802

Part: BRACKET — CRACKED (RIGHT WING) · airframe 48,130 hrs · 28,586 cycles

R/H WING AFT TRAILING EDGE CAVITY 9.50' INBD OF DEFLECTION RIB ASSY BOTTOM CURVED BULB SEAL RETENTION BRACKET ON FWD SIDE AS MARKED IS CRACKED / R/H WING AFT TRAILING EDGE CAVITY 9.50' INBD OF DEFLECTION RIB ASSY; REMOVE AND REPLACED SEAL RETENTION BRACKET ( FITTING) PN 115A2953-2 A-TAG A86357 IAW. AIPC 57-50-00-25; INSTALLED IAW. SRM. 51-40-02-0G0 AND BOEING DWG. 1152930- ID 0008 REV-

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 47,481 hrs · 28,173 cycles

EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK AT LOCATIONS M01668. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 47,481 hrs · 28,173 cycles

EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK AT LOCATIONS M01674. R&R BATTERY PACK PER AMM.

Part: HOOK — UNSECURE (R1 DOOR) · airframe 47,481 hrs · 28,173 cycles

R1 DOOR SLIDE COVER HOOK LOOSE. SECURED HOOK PER SRM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 47,481 hrs · 28,173 cycles

EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK AT LOCATIONS M01669. R&R BATTERY PACK PER AMM.

Part: PAN — CRACKED (L2 DOOR) · airframe 45,204 hrs · 26,710 cycles

AFT ENTRY DOOR LOWER PAN CRACKED AT AFT SUPPORT ANGLE RADIUS / R&R PAN AS PER AMM 52-13-31.

Part: LENS — FAULTY (CABIN) · airframe 45,196 hrs · 26,706 cycles

RT OVER WING ESCAPE HATCH THRESHOLD EMERGENCY EXIT LIGHT LENS FAULTY. R&R LENS PER AMM.

Part: LENS — FAULTY (CABIN) · airframe 45,196 hrs · 26,706 cycles

LT OVER WING ESCAPE HATCH THRESHOLD EMERGENCY EXIT LIGHT LENS FAULTY. R&R LENS PER AMM.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 44,841 hrs · 26,484 cycles

DIVERSION, AT FL 390, EXPERIENCED POSSIBLE COMPRESSOR STALL FOR NR 2 ENGINE. R&R NR 2 ENGINE PER MT.

Part: LENS — MISSING (CABIN) · airframe 44,108 hrs · 26,001 cycles

R1 DOOR EMERGENCY EXIT LIGHT MISSING ARROW. INSTALLED LIGHT LENS PER AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 43,005 hrs · 25,303 cycles

AFT GALLEY CABIN EMERGENCY LIGHT FAILED CAPACITY TEST. R & R THE BATTERY IAW AMM.

Part: HOLDER — LOOSE (R1 DOOR) · airframe 41,846 hrs · 24,580 cycles

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

Part: SLIDE — FAULTY (R1 DOOR) · airframe 41,479 hrs · 24,345 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOCK LATCH FAULTY. R&R SLIDE IAW AMM AND MT.

Part: CAP — BROKEN (R1 DOOR SLIDE) · airframe 41,479 hrs · 24,345 cycles

R1 DOOR SLIDE COVER BUMPER STRIP END CAP BROKEN. R & R THE END CAP IAW SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 41,479 hrs · 24,345 cycles

AFT ENTRY CEILING PANEL EMERGENCY LIGHT DAMAGED. R & R THE LIGHT IAW AMM.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 41,479 hrs · 24,345 cycles

SUPPLEMENTAL INFORMATION: INTERCOSTAL AT BS328 - BS344 LBL46 IS CRACKED / REMOVED AND REPLACED INTERCOSTAL AT BS 328 - BS 344 LBL46 IAW SRM 51-40-02-0G-0 AND DWG 141A5410 SH 16. 57232U 25AUG17.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 41,479 hrs · 24,345 cycles

SUPPLEMENTAL INFORMATION: PASSENGER CABIN FLOOR BOARD 241BF; BOTTOM SURFACE IS CRACKED AT EDGE OF BOARD / PASSENGER CABIN FLOOR BOARD 241BF; BOTTOM SURFACE EDGE CRACK WAS REPAIRED IAW SRM 53-00-50-2R-10.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 41,479 hrs · 24,345 cycles

SUPPLEMENTAL INFORMATION: FWD CABIN FLOOR PANEL 221BF LOWER SKIN IS DAMAGED AT I/B EDGE AT FWD AND AFT CORNERS. / REPAIRED DAMAGE AT I/B EDGE AT FWD AND AFT CORNERS OF FWD CABIN FLOOR PANEL 221BF IAW SRM 53-00-50-2R-9. 56749U 24AUG17

Part: WEB — CORRODED (CABIN) · airframe 41,479 hrs · 24,345 cycles

SUPPLEMENTAL INFORMATION: FLOOR WEB AT BS 1031 LBL 18; WL 208 IS CORRODED / REPAIRED CORROSION ON FLOOR WEB BS 1031 LBL 18 WL 208 IAW EA#1-753-316321R & ER#17-037741R.

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,479 hrs · 24,345 cycles

FLOOR STRAP CORRODED BETWEEN BS 1016 TO BS 1032, LBL 3. R&R STRAP IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,479 hrs · 24,345 cycles

FLOOR STRAP CORRODED AT BS 1030, RBL 3.5. R&R STRAP IAW SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,479 hrs · 24,345 cycles

FLOOR STRAP CORRODED AT BS 1031, RBL 18. R&R STRAP IAW SRM & DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,479 hrs · 24,345 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 120.30, 2ND VERTICAL STIFFENER FROM FORWARD AT LOWER RADIUS. REPAIRED RIB ASSEMBLY PER SRM.

Part: ANGLE — CRACKED (LEFT WING) · airframe 41,479 hrs · 24,345 cycles

SUPPLEMENTAL INFORMATION: LEFT WING UPPER TRAILING EDGE PANEL BETWEEN #5 AND #6 SPOILER PANELS CENTER AFT SEAL RETAINER ANGLE IS CRACKED / REMOVED AND REPLACED CRACKED AFT SEAL RETAINER (CENTER) ANGLE ON LEFT WING UPPER TRAILING EDGE PANEL BETWEEN #5 AND #6 SPOILER PANELS IAW SRM 51-40-02-0G-0

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,479 hrs · 24,345 cycles

AFT CARGO BAY, LAV BULKHEAD STANCHION LOWER END GUSSET CRACKED AT BS 867. R&R GUSSET IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,479 hrs · 24,345 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 767 TO 787, RBL 23. REPAIRED THE FLOOR SUPPORT IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 41,479 hrs · 24,345 cycles

FLOORBEAM CORRODED AT BS 328, RBL 39. REPAIRED THE FLOORBEAM IAW SRM.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 41,479 hrs · 24,345 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** RUDDER WEIGHT CORRODED / REMOVED AND REPLACED RUDDER WEIGHT IAW CMM 55-40-09 STEPS 2 C (2)(B) PG 301 AND 2C(3)(A) PG 703 AND SOPM 20-50-01 AND BAC 5009 PG 38

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,479 hrs · 24,345 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 120.30, 3RD VERTICAL STIFFENER FROM FORWARD AT LOWER RADIUS. REPAIRED RIB ASSEMBLY PER SRM.

Part: TRACK — CRACKED (AFT CARGO COMPT) · airframe 41,479 hrs · 24,345 cycles

SUPPLEMENTAL INFORMATION: CARGO TIE DOWN TRACK AT RBL 13 BS767 IS CRACKED IN THE RADIUS / REMOVED CARGO TIE DOWN TRACK AT RBL 13 BS 727-767; RECIEVED AND LOCATED AND DRILLED NEW TRACK IAW SRM 53-00-53-2R-3; FABRICATED TRACK SPLICE ANGLE; MADE FROM BAC 1509-100688 # 7050T76511; LOT # 1266842 AND INSTALLED CARGO TIE DOWN TRACK AT RBL 13 BS 727-767 IAW SRM 53-00-53-2R-3

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,479 hrs · 24,345 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 120.30, 4TH VERTICAL STIFFENER FROM FORWARD AT LOWER RADIUS. REPAIRED RIB ASSEMBLY PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,479 hrs · 24,345 cycles

RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727D TO BS 767. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,479 hrs · 24,345 cycles

AFT CARGO BAY, LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727E TO BS 787, LBL 25L. R&R SUPPORT IAW SRM.

Part: PANEL — BROKEN (LH OUTBD AFT FLA) · airframe 41,479 hrs · 24,345 cycles

LEFT O/B AFT FLAP I/B AND O/B CENTER TRACK CUTOUT LOWER PANELS ARE BROKEN / REMOVED AND REPLACED L/H O/B AFT FLAP I/B AND O/B CENTER TRACK CUTOUT BROKEN LOWER PANELS IAW SRM 51-40-02-0G-0 PAR 4. 57048U 24AUG17

Part: SHIELD — CORRODED (BS 767-794) · airframe 41,479 hrs · 24,345 cycles

AFT CARGO BAY SHIELD FORWARD OF THE CARGO DOOR CORRODED BETWEEN BS 767 TO 794, RBL 24. R & R SHIELD IAW SRM AND DWG.

Part: NONE — CORRODED (ASD THRESHOLD) · airframe 41,479 hrs · 24,345 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** AFT SERVICE DOOR MOPSILL HAS AREAS OF CORROSION / REMOVED & REPLACED CORRODED AFT SERVICE DOOR MOP SILL IAW SRM 51-40-02-0G-0; BOEING DWG # 147A8540; BOEING DWG # 147A0000; BOEING DWG # 147A8501.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,479 hrs · 24,345 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,479 hrs · 24,345 cycles

FORWARD CARGO BAY BULKHEAD GUSSET CRACKED AT BS 500D, STR 21L. R&R GUSSET IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,479 hrs · 24,345 cycles

FORWARD CARGO BAY RIGHT SHIELD CORRODED BETWEEN BS 492 TO BS 500A, RBL 25. R&R SHIELD PER SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,479 hrs · 24,345 cycles

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

Part: FAIRING — ELONGATED (LWR FUSELAGE) · airframe 41,479 hrs · 24,345 cycles

WTB PANEL # 194E HAS CHAFFING AND OVERSIZED HOLES ALONG AFT AFT EDGE OF PANEL ON INTERNAL SIDE / CHAFFING AND OVERSIZED HOLES ALONG AFT EDGE ON INTERNAL SIDE OF WTB PANEL # 194E WAS REPAIRED IAW SRM 51-70-05-2R-6 56563U

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 41,122 hrs · 24,137 cycles

R1 DOOR SLIDE INADVERTENTLY FELL FROM IT`S CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED THE SLIDE IAW MT.

Part: COVER — UNSECURE (CABIN) · airframe 39,650 hrs · 23,257 cycles

MID-CABIN CEILING EXIT LIGHT LENS COVER FELL OFF. REINSTALLED COVER IAW SIP.

Part: GLOWSTRIP — WORN (CABIN) · airframe 35,349 hrs · 20,769 cycles

FORWARD PHOTO LUMINESCENT STRIP WORN. REPAIRED STRIP IAW AMM.

Part: GLOWSTRIP — WORN (CABIN) · airframe 35,349 hrs · 20,769 cycles

AFT PHOTO LUMINESCENT STRIP WORN. REPAIRED STRIP IAW AMM.

Part: WEDGE — LOOSE (LE SLAT) · airframe 35,349 hrs · 20,769 cycles

LEFT WING NR 3 SLAT LOWER SURFACE OF TE WEDGE ON OTBD CORNER LOOSE. REPAIRED WEDGE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,349 hrs · 20,769 cycles

FLOORBOARD SUPPORT TRANSVERSE INTERCOSTAL CRACKED AT BS 540, LBL 24.45. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,349 hrs · 20,769 cycles

FLOORBOARD SUPPORT TRANSVERSE INTERCOSTAL CRACKED AT BS 540, RBL 24.45. R & R INTERCOSTAL IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,349 hrs · 20,769 cycles

LEFT NR 1 WINDOW FRAME CRACKED IN RADIUS OF THE UPPER OTBD CORNER. REPAIRED FRAME IAW ACO.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 32,472 hrs · 19,147 cycles

LEFT WING UPPER TE PANEL AFT SUPPORT BRACKET CRACKED BETWEEN NR 5 & 6 SPOILERS AT UPPER OTBD FASTENER. REPAIRED BRACKET IAW SRM & DWG.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 29,812 hrs · 17,654 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: SIGN — BROKEN (CABIN) · airframe 29,535 hrs · 17,493 cycles

OVERHEAD MIDDLE OF CABIN EMERGENCY EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: CONTROL VALVE — FAULTY (NR 1 ENGINE) · airframe 28,464 hrs · 16,823 cycles

AIR TURN BACK, DECLARED EMERGENCY AFTER TAKEOFF, TOWER REPORTED FROM GROUND VEHICLE CONTRAIL FROM LT ENGINE NR 1 CLIMBING THROUGH 12,000 FEET WE HAD A 600 POUND IMBALANCE. R &R HPT CLEARANCE CONTROL VALVE IAW MM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

INTERCOSTAL WEB AT FLOOR LEVEL CRACKED AT STATION 1016, LBL 35. R & R WEB IAW SRM & DRAWING.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

SEAT TRACK HOLES CRACKED AT STATION 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,423 hrs · 16,797 cycles

RT HORIZONTAL STABILIZER RIB STATION 92-70 SECOND FROM FWD VERTICAL STIFFENER CRACKED AT LOWER END. REPAIRED RIB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

SEAT TRACK HOLES CRACKED AT STATION 727B, RBL 27.75. REPAIRED FLANGES IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

INTERCOSTAL CRACKED AT STATION 321, LBL 46. R & R INTERCOSTAL IAW DRAWING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

INTERCOSTAL CRACKED AT STATION 354, LBL 11. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

FWD GALLEY DOOR THRESHOLD ATTACH ANGLE CORRODED. R & R ANGLE IAW SRM & DRAWING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

INTERCOSTAL CRACKED AT STATION 335, LBL 46. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

FLOOR BEAM CAP CORRODED AT STATION 344, BETWEEN BL 0 TO LBL 11. REPAIRED T CHORD IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

INTERCOSTAL CRACKED AT STATION 284, RBL 1. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

INTERCOSTAL CRACKED BETWEEN STATION 317 & 323, RBL 30. R & R INTERCOSTAL IAW DRAWING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

INTERCOSTAL CRACKED BETWEEN STATION 350 & 354, BL 0. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

INTERCOSTAL CRACKED BETWEEN STATION 301 TO STATION 307, RBL 15. R & R INTERCOSTAL IAW SRM & DRAWING.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 28,423 hrs · 16,797 cycles

VERTICAL PRESSURE WEB CRACKED AT STATION 663, LBL 32. REPAIRED WEB IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

FLOOR BOARD RAIL UPPER SURFACE CORRODED BETWEEN STATION 794 TO STATION 827, RBL 14. R & R SECTION IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

CREASE BEAM UPPER SURFACE CORRODED BETWEEN STATION 960 TO 986, RBL 52. R & R CREASE BEAM IAW SRM & DRAWING.

Part: STRAP — CORRODED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

FLOOR SUPPORT STRAP CORRODED AT STATION 767, BETWEEN RBL 0 TO RBL 14. R & R STRAP IAW SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 28,423 hrs · 16,797 cycles

AFT CARGO COMPARTMENT LOWER CARGO DOOR SILL WEB UPPER & LOWER SURFACE CORRODED BETWEEN STATION 794 TO 847, BETWEEN RBL 18 TO RBL 26. R & R SILL WEB IAW SRM & DRAWING.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,258 hrs · 16,706 cycles

SEAT TRACK CRACKED AT STATION 727B, RBL 45.5. REPAIRED SPLICE IAW EA.

Part: HMU — FAULTY (NR 2 ENGINE) · airframe 27,103 hrs · 16,017 cycles

AT 90 PERCENT N1 CLIMBING THROUGH 4,000' MSL W/ AUTO THROTTLES ENGAGED THE NR 2 ENGINE ROLLED BACK TO THE LOW 60 PERCENT N1 RANGE. R & R HMU IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 25,824 hrs · 15,263 cycles

EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST AT LOCATION M1669, M1672 AND M1675. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERIES AT LOCATION M1669, M1672 AND M1675PER AMM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 24,762 hrs · 14,609 cycles

EEPLS INOP BETWEEN ROW 12 TO ROW 15. CONNECTED CONNECTOR PER MM.

Part: LENS — MISSING (CABIN) · airframe 24,492 hrs · 14,427 cycles

FORWARD EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 24,345 hrs · 14,331 cycles

EMERGENCY TRACK LIGHT COVER LOOSE AT ROW 1. SECURED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 24,326 hrs · 14,320 cycles

EEPLS LOOSE AT ROW 1. SECURED EEPLS PER M/M.

Part: COVER — MISSING (CABIN) · airframe 24,071 hrs · 14,159 cycles

FWD EEPLS COVER MISSING. REMOVED AND REPLACED EEPLS IAW AMM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 23,997 hrs · 14,109 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE PER MT.

Part: LENS — LOOSE (CABIN) · airframe 23,867 hrs · 14,038 cycles

LEFT EEPLS LENS LOOSE AT ROW 2. SECURED LENS PER MM.

Part: LENS — DIRTY (CABIN) · airframe 23,664 hrs · 13,911 cycles

LEFT EEPLS DIRTY BETWEEN ROW 15 TO ROW 16L. CLEANED LENS PER M/M.

Part: BATTERY PACK — FAILED (CABIN) · airframe 23,664 hrs · 13,911 cycles

AFT EEPLS BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: COVER — CRACKED (CABIN) · airframe 23,664 hrs · 13,911 cycles

EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER M/M.

Part: LENS — BROKEN (CABIN) · airframe 23,443 hrs · 13,789 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER EA.

Part: LIGHT — LOOSE (CABIN) · airframe 23,327 hrs · 13,723 cycles

LEFT EMERGENCY EXIT FLOOR LIGHT LOOSE BETWEEN ROW 11 TO ROW 13. SECURED LIGHT ASSY PER MM.

Part: COVER — DAMAGED (CABIN) · airframe 22,612 hrs · 13,307 cycles

EMERGENCY EXIT FLOOR LIGHTING COVER DAMAGED. / R&R COVER IAW M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,554 hrs · 13,265 cycles

EMERGENCY FLOOR TRACK LIGHT AT ROW 5 INOP. RELAMPED LIGHT ASSY PER MM.

Part: COVER — BROKEN (CABIN) · airframe 22,336 hrs · 13,140 cycles

FLOOR TRACK LIGHTING COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER M/M

Part: COVER — MISSING (CABIN) · airframe 21,931 hrs · 12,929 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 14. INSTALLED COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 21,911 hrs · 12,917 cycles

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

Part: CAP — MISSING (CABIN) · airframe 21,816 hrs · 12,857 cycles

DURING SCHEDULED 6Y CHECK, FOUND FWD EEPLS MISSING AT END CAP. INSTALLED END CAP IAW MM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 22,033 hrs · 13,021 cycles

DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO COMPARTMENT VERTICAL WEB SUPPORT CORRODED AT BS 772, RBL 20. REMOVED AND REPLACED SUPPORT IAW DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,816 hrs · 12,857 cycles

DURING SCHEDULED 6Y CHECK FOUND, EEPLS INOP AT ROW 12 TO ROW 13. REMOVED AND REPLACED EEPLS IAW MM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 21,669 hrs · 12,764 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MAIN WHEEL WELL BULKHEAD WEB CRACKED AT BS 663. REPAIRED WEB.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 21,602 hrs · 12,728 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STA 184.7. REPAIRED SKIN PER SRM.

Part: COVER — MISSING (CABIN) · airframe 21,559 hrs · 12,770 cycles

EEPLS COVER MISSING AT ROW 1. INSTALLED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,142 hrs · 12,446 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 16. RELAMPED PER MM.

Part: COVER — CRACKED (CABIN) · airframe 19,885 hrs · 11,730 cycles

EMERGENCY LIGHT COVER AT ROW 5 CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 19,600 hrs · 11,569 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: COVER — CRACKED (CABIN) · airframe 19,105 hrs · 11,289 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,105 hrs · 11,289 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 1. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 18,204 hrs · 10,761 cycles

LT FWD EEPLS BROKEN. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,736 hrs · 9,900 cycles

EEPLS INOP AT ROW 2. REPAIRED EEPLS PER MM.

Part: HYDRAULIC LINE — LEAKING (MLG WW) · airframe 16,147 hrs · 9,540 cycles

AIR TURNBACK / DECLARED EMERGENCY. HYD A-SYS FLUID LOSS. REMOVED AND REPLACED LEAKY A-SYS SPOILER RETURN LINE PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 14,656 hrs · 8,653 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EVAC SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED HOOK FASTENERS PER SRM.

Part: COVER — BROKEN (CABIN) · airframe 14,656 hrs · 8,653 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 14,656 hrs · 8,653 cycles

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

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 13,653 hrs · 8,017 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: LENS — MISSING (CABIN) · airframe 12,928 hrs · 7,562 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SIGN — BROKEN (R2 DOOR) · airframe 12,791 hrs · 7,486 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 12,494 hrs · 7,309 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 12,494 hrs · 7,309 cycles

DURING SCHEDULED HC1 CHECK, RT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 1,223 hrs · 7,154 cycles

DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,906 hrs · 6,970 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRACK LIGHT INOP AT OVERWING EMERGENCY EXIT. REPAIRED LIGHT PER MM.

Part: COVER — LOOSE (CABIN) · airframe 11,826 hrs · 6,911 cycles

MID POSITION EMERGENCY EXIT LIGHT COVER LOOSE AT R2 DOOR. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 11,660 hrs · 6,804 cycles

L2 COCKPIT WINDOW ARCED. REMOVED AD REPLACED WINDOW PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 9,818 hrs · 5,669 cycles

R1 DOOR EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 7,505 hrs · 4,304 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 6,286 hrs · 3,601 cycles

EEPLS COVER LOOSE AT ROW 5 ABC. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 4,627 hrs · 2,651 cycles

DURING SCHEDULED MV1 CHECK, FOUND LEFT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 3,307 hrs · 1,900 cycles

EEPLS COVER LOOSE AT LT FWD CABIN. SECURED COVER PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 3,181 hrs · 1,832 cycles

R2 DOOR EMERGECNY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: COVER — BROKEN (CABIN) · airframe 2,361 hrs · 1,354 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,361 hrs · 1,354 cycles

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