N8684F

Part: LENS — DETACHED (ZONE 200) · airframe 32,090 hrs · 15,973 cycles

OVERWING EXIT LIGHT LENS FELL OFF. INSTALLED THE LENS IAW 33-51-01.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 31,054 hrs · 15,448 cycles

RIGHT AFT OVERWING EMERGENCY EXIT LIGHT LAMP OUT. RELAMPED RT AFT OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-04.

Part: TRANSMITTER — INOPERATIVE (TE FLAPS) · airframe 30,463 hrs · 15,135 cycles

TRAILING EDGE FLAP /DISAGREE /ASYMMETRY TRAILING EDGE FLAP DISAGREE / ASYMMETRY <1<[01] ALT FLAP SWITCH USED SWITCH TO DRIVE FLAPS DOWN ;SWITCH IN COCKPIT NOT SAFTY WIRED;[02] CREW REPORTS PSEU LIGHT ILLUMINATED ON LANDING ( FAULT CODES 32-62009;32-62010) ON APPROACH CREW SELECTED 5 . FLAPS ;CREW OBSERVED FLAP SPLIT;FOLLOWED QRH AND USED ALT FLAP SWITCH TO DRIVE FLAPS DOWN; (FLAP HANDLE IN UP POSTION SLATS IN @ 2 DEGREES );[03] FSEU BITE CURRENT LEG FAULT CODE 27-52259. INITIAL EVAL FOUND #5 FLAP TRANSMISSION TORQUE INDICATOR POPPED AS WELL AS ALL FLAP BALLSCREWS AND U-JOINTS DRY. DRAINED AND SERVICED ALL T/E FLAP TRANSMISSIONS EXCLUDING #8 IAW AMM 12-22-51. NOTED #2 FLAP TRANSMISSION FLUID CLOUDY AND OVER SERVICED. T/E FLAP DRIVE UNIT ALSO DRAINED AND SERVICED IAW AMM 12-22-51. LUBED FLAP BALLSCREWS AND U-JOINTS AS WELL AS FLAP ROLLERS AND LINKAGES IAW AMM 12-22-51. FLAP SYSTEM OPS CHECKS NORMAL IAW 27-51-00. FLAP POSITION VERIFICATION THROUGH ACMS CHECKS NORMAL WITH MARGIN SPLITS STAYING ABOVE 7.3 IAW AMM 27-58-01.;[04] DRAINED AND SERVICED #8 FLAP TRANSMISSION IAW AMM 12-22-51 LEAK CHECK GOOD;[05] ACCOMPLISHED FIM 27-51 TASK 813. LUBRICATED ALL 8 FLAP BALL <BR>SCREWS AND U-JOINTS REF AMM 12-22-51. DRAINED AND SERVICED <BR>ALL 8 FLAP TRANSMISSIONS REF AMM 12-22-51. PER MOC REQUEST REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER IAW AMM<BR>27-58-01 AND FLAP POSITION INDICATOR IAW AMM 27-58-02.

Part: TRANSMITTER — MALFUNCTIONED (ZONE 100) · airframe 30,336 hrs · 15,071 cycles

DURING APP AT MDW WHEN SELECTING FLAPS 5; WE GOT A SPLIT FLAP; RAN QRH PER OPPS T427 IS LAGGING ON AHM FSEU BITE FC 27-53279 CONFIRMED NO CB TRIPPED<[01] REMOVED AND REPLACED LT FLAP POSITION TRANSMITTER PER M/M 27-58-01

Part: FAIRING — DAMAGED (ZONE 600) · airframe 30,020 hrs · 14,905 cycles

#6 CANOE FAIRING HAS ELONGATED SEAL FASTENER HOLES.<[01] A NEW #6 CANOE FAIRING WAS ORDERED FOR A/C. NEW CANOE FAIRING WILL BE INSTALLED ON FAULT # TTG8Q00ZVLVW.;[02] C/W

Part: SEAL — CRACKED (ZONE 300) · airframe 30,020 hrs · 14,905 cycles

RT STAB UPPER FWD SLIDING SEAL ON FUSELAGE CRACKED.<[01] REMOVED RH HORIZONTAL UPPER FWD SLIDING SEAL PER AMM 53-31-31.;[02] REPLACED RH HORIZONTAL UPPER FWD SLIDING SEAL PER AMM 53-31-31.;[03] 02 - INSPECTED PER [AMM 53-31-31-401 CONFIG 2-NG (STABILIZER TO BODY FRONT SPAR SLIDING SEAL - REMOVAL/INSTALLATION - PERMANENT)]

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 30,020 hrs · 14,905 cycles

LEFT OVERWING EMERGENCY LIGHTS BATTERY PACK INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1694 AT STA 565L PER MM 33-51-06;[02] LEFT OVERWING EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[03] 02 - INSPECTED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 30,020 hrs · 14,905 cycles

RIGHT OVERWING EMERGENCY LIGHT BATTERY PACK M1695 AT STA 565R IS INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1695 AT STA 565R PER MM33-51-06;[02] RIGHT OVERWING EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[03] 02 - INSPECTED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 30,020 hrs · 14,905 cycles

EMERGENCY EXIT LIGHT EXTERNAL OF AFT R/H OVERWING EXIT WILL NOT ILLUMINATE.<[01] REMOVED AND REPLACED BATTERY PACK M1671 PER AMM 33-51-06. NO FAULTS NOTED.;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR BATTERY PACK REPLACEMENT.

Part: SUPPORT ANGLE — CRACKED (ZONE 600) · airframe 30,020 hrs · 14,905 cycles

R/H WING TRAILING EDGE UPPER SHELF PANEL SUPPORT ANGLE INBD OF DEFLECTION CONTROL RIB CRACKED<[01] LOCATED AND DRILLED NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05.;[02] INSPECTED LOCATION AND DRILLING OF NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05;[03] INSTALLED NEW SUPPORT ANGLE WITH FASTENERS PER SRM 51-40-02.;[04] VERIFIED WORK PERFORMED IN CORRECTIVE ACTION #3

Part: SUPPORT ANGLE — CRACKED (ZONE 600) · airframe 30,020 hrs · 14,905 cycles

R/H WING TRAILING EDGE UPPER SHELF PANEL SUPPORT ANGLE INBD OF DEFLECTION CONTROL RIB CRACKED<[01] LOCATED AND DRILLED NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05.;[02] INSPECTED LOCATION AND DRILLING OF NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05;[03] INSTALLED NEW SUPPORT ANGLE WITH FASTENERS PER SRM 51-40-02.;[04] VERIFIED WORK PERFORMED IN CORRECTIVE ACTION #3

Part: ANGLE — CRACKED (ZONE 600) · airframe 30,020 hrs · 14,905 cycles

R/H WING TRAILING EDGE UPPER SHELF PANEL SUPPORT ANGLE INBD OF DEFLECTION CONTROL RIB CRACKED<[01] LOCATED AND DRILLED NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05.;[02] INSPECTED LOCATION AND DRILLING OF NEW FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05;[03] INSTALLED NEW SUPPORT ANGLE WITH FASTENERS PER SRM 51-40-02.;[04] VERIFIED WORK PERFORMED IN CORRECTIVE ACTION #3

Part: ATTACH BRACKET — CRACKED (ZONE 600) · airframe 30,020 hrs · 14,905 cycles

RIGHT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR LOWER ATTACH POINT MOUNT IS CRACKED.<[01] INFO: WORK WITH FAULT ID TTG8Q00ZUZDG AS THIS IS WHERE THE OTHER HALF OF THE SAME BRACKET IS WRITTEN UP.;[02] REFERENCE TASK CARD LINE # 1177; R/H WING LOWER I/B FIXED TRAILING EDGE PANEL 651FB HAS BROKEN ATTACH ANGLE (MARKED). [TTG8Q00ZUZDG] FOR CORRECTIVE ACTION TAKEN.

Part: BRACKET — CRACKED (ZONE 600) · airframe 30,020 hrs · 14,905 cycles

RIGHT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR LOWER ATTACH POINT MOUNT IS CRACKED.<[01] INFO: WORK WITH FAULT ID TTG8Q00ZUZDG AS THIS IS WHERE THE OTHER HALF OF THE SAME BRACKET IS WRITTEN UP.;[02] REFERENCE TASK CARD LINE # 1177; R/H WING LOWER I/B FIXED TRAILING EDGE PANEL 651FB HAS BROKEN ATTACH ANGLE (MARKED). [TTG8Q00ZUZDG] FOR CORRECTIVE ACTION TAKEN.

Part: BRACKET — CRACKED (ZON E600) · airframe 30,020 hrs · 14,905 cycles

RIGHT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR LOWER ATTACH POINT MOUNT IS CRACKED.<[01] INFO: WORK WITH FAULT ID TTG8Q00ZUZDG AS THIS IS WHERE THE OTHER HALF OF THE SAME BRACKET IS WRITTEN UP.;[02] REFERENCE TASK CARD LINE # 1177; R/H WING LOWER I/B FIXED TRAILING EDGE PANEL 651FB HAS BROKEN ATTACH ANGLE (MARKED). [TTG8Q00ZUZDG] FOR CORRECTIVE ACTION TAKEN.

Part: BRACKET — CRACKED (ZONE 500) · airframe 30,020 hrs · 14,905 cycles

LT WING CONDUIT BRACKET ABOVE AND AFT OF MLG MAIN RETRACT ACTUATOR CRACKED. SEE ATTACHED PICS.<[01] REMOVED AND REPLACED CONDUIT BRACKET. IAW SRM 51-40-02;[02] 02 - INSPECTED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]

Part: SUPPORT BRACKET — CORRODED (ZONE 600) · airframe 30,020 hrs · 14,905 cycles

R/H WING L/E FUELING GAUGES SUPPORT BRACKET HAS SEVERAL AREAS OF SURFACE CORROSION. MRKD<[01] REMOVED AND REPLACED R/H WING L/E REFUELING GAUGES SUPPORT BRACKET (P15 PANEL) PER AMM 28-21-00.;[02] INSPECTION C/W C/A #1;[03] REQUIRES INSTALLATION TEST PER AMM 28-21-00.;[04] WING FUELING PANEL OPS CHECKED GOOD PER MM 28-21-51 AND MM 28-41-61;[05] WING FUELING PANEL OPS CHECKED GOOD

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 30,020 hrs · 14,905 cycles

BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT RBL 34<[01] REMOVED BS 63 R/H VAPOR BARRIER ANGLE PER SRM 51-40-02.;[02] MATCH DRILLED NEW ANGLE PER SRM 51-40-02. NEED OK TO INSTALL.;[03] C/W INSPECTION OF CA # 1-2. OK TO INSTALL;[04] INSTALLED FASTENERS COMMON TO FUEL TANK ON VAPOR BARRIER ATTACH ANGLE PER SRM 51-40-02 & DWG 111A1000.;[05] VERIFIED AND INSPECTED INSTALLATION OF FASTENERS COMMON TO THE FUEL TANK ON VAPOR BARRIER ATTACH ANGLE PER SRM 51-40-02 & DWG 111A1000.;[06] COMPLETED FASTENERS INSTALLATION COMMON TO VAPOR BARRIER ATTACH ANGLE PER SRM 51-40-02.;[07] C/W INSPECTION AS REQUIRED C/A # 6 - COMPLETED FASTENERS INSTALLATION COMMON TO VAPOR BARRIER ATTACH ANGLE PER SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 30,020 hrs · 14,905 cycles

BS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT RBL 34. REMOVED BS 63 R/H VAPOR BARRIER ANGLE PER SRM 51-40-02. MATCH DRILLED NEW ANGLE PER SRM 51-40-02. INSTALLED FASTENERS COMMON TO FUEL TANK ON VAPOR BARRIER ATTACH ANGLE PER SRM 51-40-02 & DWG 111A1000. COMPLETED FASTENERS INSTALLATION COMMON TO VAPOR BARRIER ATTACH ANGLE PER SRM 51-40-02.; REPLACED R/H BS 663 UPPER VAPOR BARRIER ATTACH ANGLE PER SRM 51-10-2 & DWG 111A1000.

Part: SIGN — BROKEN (ZONE 200) · airframe 28,931 hrs · 14,324 cycles

OVERHEAD EMERGENCY EXIT SIGN AT OVERNIGHT EXITS BROKEN.<[01] REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT SIGN ASSY AT OVERWING EXITS IAW AMM 33-51-01. OP CHECKS GOOD.

Part: COVER — MISSING (ZONE 200) · airframe 28,399 hrs · 14,028 cycles

CENTER AISLE FORWARD EXIT LOCATOR SIGN MISSING<[01] INSTALLED MISSING LENSE COVER PER SIP

Part: SIGN — BROKEN (ZONE 200) · airframe 28,272 hrs · 13,962 cycles

CENTER EMERGENCY EXIT SIGN BROKEN<[01] REPLACED CENTER EMER EXIT SIGN LENS PER M/M 33-51-01.

Part: COVER — DETACHED (ZONE 200) · airframe 27,819 hrs · 13,718 cycles

EMERGENCY EXIT LIGHT CEILING MOUNTED COVER FELL OFF<[01] REINSTALLED COVER PER SIP

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 27,580 hrs · 13,589 cycles

EMERGENCY EXIT ROW SIGN ON OVHD LENS FELL OFF<[01] REINSTALLED OVERWING EXIT SIGN LENS IAW AMM 33-51-01. A/C OK FOR SERVICE

Part: BRACKET — BROKEN (EMERGENCY LIGHT) · airframe 27,381 hrs · 13,482 cycles

MID CABIN EXIT SIGN BRACKET BROKEN<[01] RESECURED MID CABIN EXIT SIGN LENS PER MM 33-51-03; OPS CK GOOD

Part: LIGHT — BROKEN (FWD LAVATORY) · airframe 26,842 hrs · 13,196 cycles

FWD LAV A EXIT LIGHT IS BROKEN.<[01] REMOVED AND REPLACED FWD LAV A EXIT LIGHT PER SOPM 20-50-01.;[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOORBEAM — CORRODED (BS 947 RBL 23) · airframe 26,842 hrs · 13,196 cycles

CORROSION ON AFT WET AREA FLOOR BEAM AT BS 947; RBL 23; WL 208.<[01] REMOVED DAMAGED SECTION AND ACCOMPLISHED REPAIR OF FLOOR BEAM AT BS 947 RBL 8.5' TO RBL 41.7' WL 208; PER SRM 53-70-51-2R-5; REPAIR 5.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.

Part: WEB — CORRODED (BS 794-847) · airframe 26,842 hrs · 13,196 cycles

CORROSION AFT CARGO BAY SUB THRESHOLD WEB MULTIPLE AREAS AROUND NUT PLATE HOLES BS794 TO BS847 RBL 26 WL156<[01] REMOVED AFT CARGO BAY SUB THRESHOLD WEB; LOCATED; DRILLED AND INSTALLED NEW AFT CARGO BAY SUB THRESHOLD WEB IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A8340.;[02] VERIFIED CORRECTIVE ACTION 1

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 26,842 hrs · 13,196 cycles

PASSENGER CABIN FLOOR PANEL 242NF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 242NF PER AMM 53-21-00-000-801;[02] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242NF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[03] VERIFIED CORRECTIVE ACTION 2.;[04] REQUEST OK TO CLOSE;[05] GRANTED;[06] INSTALLED PANEL 242NF PER AMM 53-21-00-400-801;[07] CAL TOOL 35 IN-LB SCREW GUN<BR>ID: ATS3017<BR>DUE DATE: 03/2025;[08] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: NONE — NONE (NONE) · airframe 26,842 hrs · 13,196 cycles

REMOVE AND REINSTALL LEFT ELEVATOR FOR PAINT<[01] REMOVED AND REINSTALLED LH ELEVATOR IAW AMM 27-31-11-400-801. SEE PREVIOUS STEPS TO VERIFY.

Part: FLOOR SUPPORT — CRACKED (BS 380-400) · airframe 26,842 hrs · 13,196 cycles

PASSENGER CABIN FWD FLOOR SUPPORT IS CRACKED AT BS 380-400; LBL 52; WL 208.<[01] REMOVED AND REPLACED FLOOR SUPPORT TOP ANGLE AT STA 380-400; LBL 52; WL 208 PER SRM 51-40-02-0G-0; PARAGRAPHS 4 AND 7; REFERENCING BOEING DWG 142A5400; SHEET 183; REV - DATED 03/20/2013;[02] VERIFIED CORRECTIVE ACTION 1

Part: FLOOR SUPPORT — CRACKED (BS 380-400) · airframe 26,842 hrs · 13,196 cycles

PASSENGER CABIN FWD FLOOR SUPPORT IS CRACKED AT BS 380-400; LBL 13; WL 208.<[01] REMOVED AND REPLACE PASSENGER CABIN FWD FLOOR SUPPORT AT BS 380-400; LBL 13; WL 208 PER SRM 51-40-02; SRM 51-40-05; AND DWG#143A5400.;[02] VERIFIED CORRECTIVE ACTION 1

Part: BRACKET — CRACKED (SERVICE DOOR) · airframe 26,842 hrs · 13,196 cycles

BOTH BRACKETS CRACKED ON ASD PANEL 844DZ<[01] REPLACED BOTH FWD AND AFT BRACKETS ON ASD PANEL 844DZ PER SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.

Part: SIDEWALL SUPPORT — CORRODED (BS 727H-807) · airframe 26,842 hrs · 13,196 cycles

CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727H+21' TO BS807+3' LBL22 WL156<[01] REMOVED DAMAGED SECTION OF FLOOR TO SIDEWALL SUPPORT; LOCATED AND DRILLED NEW SIDEWALL SUPPORT PLATE AND REPAIR PARTS (BS727E+7.5'TO 847); REPAIR (2EA) SPLICES (2EA) LOCATED BS727E+7.5'AND BS727J+9'; INSTALLED FLOOR TO SIDEWALL SUPPORT PLATE SECTIONS AND REPAIR PARTS. IAW SRM 53-00-53-2R-5 REP. MATERIAL USED BAC1496-377 7075T62 CLAD.;[02] VERIFIED CORRECTIVE ACTION 1

Part: SIDEWALL SUPPORT — CORRODED (BS 500D-500I) · airframe 26,842 hrs · 13,196 cycles

CORROSION FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500D+6' TO BS500I LBL22 WL156<[01] ' THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550'.;[02] VERIFIED CORRECTIVE ACTION 1

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 26,842 hrs · 13,196 cycles

PASSENGER CABIN FLOOR PANEL 241GF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED FLOOR PANEL 241GF PER AMM 53-21-00-000-801;[02] REQUEST OK TO CLOSE;[03] INSTALLED PANEL 241GF PER AMM 53-21-00-400-801;[04] CAL TOOL 35 IN-LB SCREW GUN<BR>ID: ATS3017<BR>DUE DATE: 03/2025;[05] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 26,842 hrs · 13,196 cycles

PASSENGER CABIN FLOOR PANEL 241MF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 241MF PER AMM 53-21-00-000-801;[02] REQUEST OK TO CLOSE;[03] INSTALLED PANEL 241MF PER AMM 53-21-00-400-801;[04] INSTALLED PANEL 241MF PER AMM 53-21-00-400-801 <BR>CAL TOOL 35 IN-LB SCREW GUN<BR>ID: ATS3017<BR>DUE DATE: 03/2025;[05] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: SHIELD — CORRODED (BS 500) · airframe 26,842 hrs · 13,196 cycles

CORROSION FWD CARGO BAY AFT SHIELD BS500+1 TO BS500+19 RBL22 WL156 HAS MULTIPLE AREAS AROUND NUT PLATE HOLES<[01] REMOVED FWD CARGO BAY AFT SHIELD; LOCATED; DRILLED AND INSTALLED NEW FWD CARGO BAY AFT SHIELD IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 143A0080.;[02] VERIFIED CORRECTIVE ACTION 1

Part: SIDEWALL SUPPORT — CORRODED (BS 500A-500I) · airframe 26,842 hrs · 13,196 cycles

CORROSION FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS500A TO BS500I RBL22 WL156<[01] REMOVED FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE; LOCATED; DRILLED AND INSTALLED NEW FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 143A7500.;[02] VERIFIED CORRECTIVE ACTION 1

Part: SIDEWALL SUPPORT — CORRODED (BS 727B-767) · airframe 26,842 hrs · 13,196 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] REMOVED AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE; LOCATED; DRILLED AND INSTALLED NEW AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A7500.;[02] VERIFIED CORRECTIVE ACTION 1

Part: NONE — NONE (NONE) · airframe 26,842 hrs · 13,196 cycles

REMOVE AND REINSTALL RIGHT ELEVATOR FOR PAINT<[01] REMOVED AND REINSTALLED RH ELEVATOR IAW AMM 27-31-11-400-801. SEE PREVIOUS STEPS TO VERIFY.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 26,842 hrs · 13,196 cycles

PASSENGER CABIN FLOOR PANEL 231KF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 231KF PER AMM 53-21-00-000-801;[02] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 231KF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[03] VERIFIED CORRECTIVE ACTION ITEM 2.;[04] SELECTED PARTS REQUIREMENT;[05] REQUEST OK TO CLOSE;[06] INSTALLED PANEL 231KF PER AMM 53-21-00-400-801;[07] CAL TOOL 35 IN-LB SCREW GUN<BR>ID: ATS3017<BR>DUE DATE: 03/2025;[08] VERIFIED;[09] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 26,842 hrs · 13,196 cycles

PASSENGER CABIN FLOOR PANEL 242GF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 242GF PER AMM 53-21-00-000-801;[02] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242GF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[03] VERIFIED ITEM 2.;[04] REQUEST OK TO CLOSE;[05] OK TO CLOSE GRANTED;[06] INSTALLED PANEL 242GF PER AMM 53-21-00-400-801;[07] CAL TOOL 35 IN-LB SCREW GUN<BR>ID: ATS3017<BR>DUE DATE: 03/2025;[08] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: FLOOR SUPPORT — CRACKED (BS 380-400) · airframe 26,842 hrs · 13,196 cycles

PASSENGER CABIN FWD FLOOR SUPPORT IS CRACKED AT BS 380-400; LBL 1; WL 208.<[01] REMOVED AND REPLACED FLOOR SUPPORT TOP ANGLE AT STA 380-400; LBL 1; WL 208 PER SRM 51-40-02-0G-0; PARAGRAPHS 4 AND 7; REFERENCING BOEING DWG 143A5400; SHEET 154.;[02] VERIFIED CORRECTIVE ACTION 1

Part: SHIELD — CORRODED (BS 767-794) · airframe 26,842 hrs · 13,196 cycles

CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] REMOVED AFT CARGO BAY SHIELD FWD OF CARGO DOOR; LOCATED; DRILLED AND INSTALLED NEW AFT CARGO BAY SHIELD FWD OF CARGO DOOR IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A0081.;[02] VERIFIED CORRECTIVE ACTION 1

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 26,842 hrs · 13,196 cycles

PASSENGER CABIN FLOOR PANEL 242HF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 242HF PER AMM 53-21-00-000-801;[02] REQUEST OK TO CLOSE;[03] OK TO CLOSE GRANTED;[04] INSTALLED PANEL 242HF PER AMM 53-21-00-400-801;[05] CAL TOOL 35 IN-LB SCREW GUN<BR>ID: ATS3017<BR>DUE DATE: 03/2025;[06] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: STRAP — CORRODED (BS 727I) · airframe 26,842 hrs · 13,196 cycles

CORROSION ON AFT CARGO BAY FLOOR T STRAP BS 727I+5 RBL 16 TO LBL 16 WL 156<[01] RECEIVED NEW AFT CARGO BAY FLOOR T STRAP BS 727I+5 RBL 16 TO LBL 16 WL 156 ON PO # 968983 INSTALL WILL BE ON CARD # TTG8Q00S3YLY;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 26,842 hrs · 13,196 cycles

PASSENGER CABIN FLOOR PANEL 242MF IS DELAMINATED ON TOP SURFACE.<[01] REMOVED PANEL 242MF PER AMM 53-21-00-000-801;[02] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242MF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[03] VERIFIED CORRECTIVE ACTION 2.;[04] REQUEST OK TO CLOSE;[05] OK GRANTED;[06] INSTALLED PANEL 242MF PER AMM 53-21-00-400-801;[07] CAL TOOL 35 IN-LB SCREW GUN<BR>ID: ATS3017<BR>DUE DATE: 03/2025;[08] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 26,842 hrs · 13,196 cycles

R/H O/B AFT FLAP UPPER AND LOWER SKINS ARE DELAMINATED @ T/E I/B CORNER/<[01] REMOVED AND REPLACED R/H O/B AFT FLAP IAW AMM 27-51-22-400-801. WORK CARD COMPLETE

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 26,842 hrs · 13,196 cycles

L/H O/B AFT FLAP UPPER SKIN IS DELAMINATED AT AFT I/B CORNER. (MARKED)<[01] REMOVED AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22-400-801. WORK CARD COMPLETE

Part: GIRT BAR — LOOSE (FWD) · airframe 26,138 hrs · 12,812 cycles

FORWARD ENTREE DOOR GIRT BAR HOLDER IS LOOSE<[01] REPLACED BROKEN RIVET ON GIRT BAR HOLDER PER AMM 25-66-00 AND SRM 51-40-02

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 25,455 hrs · 12,432 cycles

EMERGENCY EXIT LIGHT BATTERY PACKS AT FWD RH DOOR; LH AISLE AT STA 500C+7; RH AISLE AT STA 500 C+7; AND AFT RH DOOR DISCHARGED.<[01] R&R EMERGENCY EXIT LIGHT BATTERY PACKS FOR FWD RH DOOR; LH AISLE AT STA 500C+7; RH AISLE AT STA 500 C+7; AND AFT RH DOOR; REF AMM 33-51-06. OPS CK GOOD.

Part: GIRT BAR — BROKEN (ZN 800 DOOR) · airframe 25,167 hrs · 12,265 cycles

FWD ENTRY DOOR GIRT BAR KNOB BROKEN<[01] REINSTALLED BAR LOCK ON FWD ENTRY SLIDE GIRT BAR PER AMM 25-66-01.

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 24,487 hrs · 11,893 cycles

FLOOR BOARD SUPPORT R/H PANEL BRAKE ASSY. CRACKED - LOCATED AT STA 540 (P/N 143A5240-36) (ZONE 126)<[01] REMOVED AND REPLACED R/H PANEL BRAKE ASSY AT STA.540 PER SRM 51-40-02.

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 24,487 hrs · 11,893 cycles

FLOOR BOARD SUPPORT L/H PANEL BRAKE ASSY. CRACKED - LOCATED AT STA 540 (P/N 143A5240-35) (ZONE 125)<[01] REMOVED AND REPLACED L/H PANEL BRAKE ASSY AT STA.540 PER SRM 51-40-02.

Part: SIGN — LOOSE (ZN 200 FUS TOP) · airframe 24,139 hrs · 11,693 cycles

EMER EXIT SIGN CENTER CABIN NEEDS RESECURED.<[01] RESECURED EMERG EXIT SIGN CENTER CABIN PER AMM 33-51-01.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 23,816 hrs · 11,502 cycles

L1 DOOR EMERGENCY LIGHTS INOP<[01] R&R EMERGENCY LIGHTS BATTERY CHARGER & BATTERY PACK REF MM 33-51-06 OPS CK GOOD

Part: CHARGER — INOPERATIVE (ZN 200 FUS TOP) · airframe 23,816 hrs · 11,502 cycles

L1 DOOR EMERGENCY LIGHTS INOP<[01] R&R EMERGENCY LIGHTS BATTERY CHARGER & BATTERY PACK REF MM 33-51-06 OPS CK GOOD

Part: SIGN — BROKEN (ZN 800 DOOR) · airframe 23,065 hrs · 11,080 cycles

R2 DOOR SIDE EMERGENCY SIGN BROKEN<[01] C/W EA M-21-133-00720 ITEM PLACED ON TLD PERMANENT REPAIR TO BE ACCOMPLISHED IN 30 CYCLES

Part: GIRT BAR — LOOSE (ZN 200 FUS TOP) · airframe 22,776 hrs · 10,915 cycles

FWD SERVICE DOOR GIRT BAR LOOSE.<[01] RESECURED FWD SERVICE DOOR GIRT BAR; IAW AMM 25-66-01.

Part: GIRT BAR — OUT OF ADJUST (SERVICE DOOR) · airframe 22,693 hrs · 10,861 cycles

FORWARD SERVICE DOOR GIRT BAR HOLDER HOOK (RT. SIDE) IS LOOSE<[01] INSTALLED RIVET ON FWD SERVICE DOOR GIRT BAR HOLDER (RT SIDE) PER SIP

Part: LENS — LOOSE (OVERWING EXIT) · airframe 22,550 hrs · 10,777 cycles

CREW REPORTED EMERGENCY EXIT SIGN AT OVERWING EXIT LENS LOOSE. RE-SECURED OVERWING EMERGENCY EXIT SIGN LENS REF 33-51-03

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 22,424 hrs · 10,713 cycles

RIGHT HORIZONTAL FWD UPPER SLIDING SEAL CRACKED. R & R RIGHT HORIZONTAL FWD UPPER SLIDING SEAL IAW MM 53-31-31

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 22,235 hrs · 10,601 cycles

LH ROW 15 TO ROW 27 EMERGENCY LIGHTS INOP / [01] REPLACED EMERGENCY LIGHT BATTERY PACK AT ROW 15 PER AMM 33-51-06 OPS CHECK GOOD. NO FURTHER DEFECTS

Part: ENGINE — OVERTEMP (ZN 400 NACELLE/P) · airframe 22,075 hrs · 10,515 cycles

ENGINE 1 FAIL; LOUD BANG; SEVERE DAMAGE; QRC/QRH PROCEDURES ALL COMPLIED WITH; OVERTEMP; N2 TO ZERO. / [01] R/R #1 ENG REF T/C 771-00-01

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 21,962 hrs · 10,448 cycles

MID CABIN EXIT SIGN MISSING FORWARD COVER / [01] INSTALLED LENS PER M/M 33-51-01

Part: NONE — OUT OF POSITION · airframe 21,746 hrs · 10,322 cycles

EMERGENCY EXIT SIGN LOCATED IN CEILING; CENTER AISLE; BY OVERWING EMERGENCY EXITS; FELL OFF / [01] RESECURED EMERGENCY EXIT LIGHT FACE ON FWD SIDE OF CEILING AT OVERWING EXIT PER AMM 33-51-01

Part: ANGLE — CORRODED (FWD FUSELAGE) · airframe 20,246 hrs · 9,455 cycles

DOT A-24-003 WIFI ADAPTER RING FORWARD BONDING STRAP ATTACH ANGLE CORRODED. / [01] EVALUATED ATTACH ANGLE FOUND 100% MATERIAL LOSE<BR>OUT OF LIMITS I.A.W SRM 51-10-02-0G-0;[02] REMOVED ATTACH ANGLE I.A.W SRM 51-40-02-0G-0;[03] VERIFIED MATERIAL FOR FABRICATION OF BRACKET AS 2024-0 .040<BR>I.A.W SAINT=GOBAIN DWG 5214-002 ANS SRM-5214-010<BR>A TAG #A11365;[04] VERIFIED STEPS 1 - 3; VERIFIED MATERIAL FOR FABRICATION OF BRACKET AS 2024-0 .040;[05] FABRICATED NEW BRACKET I.A.W SAAINT GOBAIN DWG 5214-010;[06] VERIFIED STEP 5;[07] OK GIVEN TO TREAT AND PRIME;[08] TREATED AND PRIMED BRACKET I.A.W MM 51-21-72-370-801;[09] VERIFIED ITEM 8<BR>OK TO INSTALL ATTACH ANGLE;[10] INSTALLED BRACKET AND EDGE SEALED BRACKET I.A.W SIAINT-GOBAIN SRM 5214-010;[11] VERIFIED STEP 10;[12] PERFORMED BONDING CHECK I/A/W SAINT-GOBAIN SRM 5214-010. CHECK GOOD<BR><BR>AAR TOOLS: 42387 DD:07/20/22;[13] VERIFIED STEPS 12.<BR>AUDIT C/W

Part: FLOOR SPLICE — CORRODED (AFT CARGO) · airframe 20,246 hrs · 9,455 cycles

A-061 DOT 022 A-061 DOT 021 AFT CARGO PIT FLOOR PNL BREAK AT STA 887 LBL 12 WL 155 CORRODED AT FASTENER HOLE / [01] REMOVED AFT CARGO PIT FLOOR PANEL BREAK ( SPLICE PLATE) IAW AMM 25-52-10-000-801.;[02] VERIFIED NEW PART AS 146A9401-21; IAW AIPC 53-42-11-26; ITEM # 675.. A-TAG #A72267.;[03] VERIFIED STEP 1 AND 2;[04] L9CATED AND DRILLED FASTENER HOLES IAW SRM 51-40-05-OG-0 .;[05] INSTALLED NUT PLATES IAW SRM 51-40-02-OG-0. NEED OK TO INSTALL.;[06] VERIFIED STEPS 4 AND 5<BR><BR>OK TO INSTALL;[07] INSTALLED REPLACEMENT FLOOR SPLICE AT STA 887; LBL12; IAW AMM 25-52-10-400-801.;[08] VERIFIED STEP 7;[09] AUDIT C/W

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 20,246 hrs · 9,455 cycles

AFT CARGO FLOOR PANEL 140CF HAS CORROSION ALONG EDGE A225-004 / [01] VERIFIED CORROSION IS OUT OF LIMITS DUE TO BEING GREATER THAN 20 SQ INCHES IAW SRM 53-00-53-1A-1;[02] VERIFIED MATERIAL TO BE 2024-T3 .071 IAW AMM25-52-01-201-801;[03] VERIFIED STEPS 1 & 2;[04] STARTED FABRICATING PANEL IAW AMM 25-52-01-201-801;[05] FABRICATED PANEL 140CF IAW AMM 25-52-01-201-801;[06] VERIFIED STEPS 4 & 5;[07] OK GIVEN TO TREAT AND PRIME;[08] FABRICATED NEW FLOOR PANEL 140CF IAW AMM 25-52-01-201-801;[09] VERIFIED STEP 8

Part: ANGLE — CRACKED (AFT CARGO) · airframe 20,246 hrs · 9,455 cycles

A-061 DOT 023 A-061 DOT 021 AFT CARGO PIT LOWER END OF VERTICAL BEAM FOR WASTE TANK CLOSE OUT AT STA 867 LBL 14 WL 155 ATTACH ANGLE CRACKED / [01] REMOVED CRACKED AFT CARGO LOWER VERTICAL BEAM WASTE TANK ATTACH ANGLE AT STA 867 LBL 14 AND REPLACED WITH NEW ATTACH ANGLE; P/N 149A8109-114 ATAG A108783; IAW SRM 51-40-02-0G-0 AND BOEING DWG 149A8102 ID15 REV A;[02] VERIFIED JOB IS COMPLETE

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 20,246 hrs · 9,455 cycles

AFT CARGO PIT LT Z ANGLE BETWEEN BS 727E - 807+10, LBL 23, WL 155 CORRODED ON UPPER SURFACE. REMOVED CORROSION FROM LH Z ANGLE, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. CUTOUT DAMAGE SECTION OF Z ANGLE AND REMOVED IAW SRM 53-00-53-2R-5. FABRICATED THE Z ANGLE REPAIR PARTS IAW SRM 53-00-53-2R-5 REPAIR 5. APPLIED ALODINE AND PRIMER REPAIR IAW SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804. INSTALLED Z ANGLE REPAIR IAW SRM 53-00-53-2R-5, REPAIR 5. APPLIED CIC TO UPPER AND LOWER SURFACES IAW AMM 51-21-1.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 20,246 hrs · 9,455 cycles

A-061 DOT 032 AFT CARGO PIT ATTACH ANGLE FOR FWD SHIELD STA 767 TO STA 767+15' RBL 23 WL 155 CORROSION AT NUTPLATE HOLES LOWER SURFACE / [01] REMOVED CORROSION FROM ATTACH ANGLE. ORIGINAL T=.050' LOSS OF .006' REMNING .044' FOUND TO BE UT OF LIMITS IAW SRM 53-60-15-1A-1. <BR>WORK PERFORMED BY DERNARD BEMKE 27266;[02] VERIFIED STEP 1;[03] ADDING TOOLING INFO TO STEP 1. AAR 32351 CAL DUE 10DEC22;[04] REMOVED AFT CARGO PIT ATTACH ANGLE FOR FWD SHIELD STA 767 TO STA 767+15 RBL 23 I/A/W B737-800 SRM 51-40-02-0G-0.;[05] VERIFIED ANGLE P/N 146A8125-53 TAG#FA3607 IAW DWG 146A8123 REV:-;[06] VERIFIED STEPS 4 & 5.;[07] STARTED TO DRILL HOLES ON NEW ANGLE IAW SRM 51-40-05-0G-0;[08] VERIFIED STEP 7 C/W;[09] CHANGED CORROSION LEVEL;[10] FINISHED LOCATED AND DRILL HOLES ON NEW ANGLE IAW SRM 51-40-05-0G-0;[11] VERIFIED STEP 10;[12] VERIFIED STEPS 7 -11;[13] OK GIVEN TO INSTALL REPAIR PARTS;[14] INSTALLED ATTACH ANGLE IAW SRM 51-40-02-0G-0 AND DWG 146A8123 REV:-;[15] VERIFED STEP 14 IS COMPLETE;[16] VERIFIED ITEMS 14 AND 15;[17] APPLIED CIC ON ATTACH ANGLE IAW AMM 51-21-91-620-802;[18] JOB COMPLETE; AUDIT C/W

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 20,246 hrs · 9,455 cycles

A-061 DOT 030 AFT CARGO PIT FLOOR PANEL BREAK AT STA 767+6' BL 0 TO RBL 23 WL 155 HAS CORROSION ON UPPER SURFACE / [01] VERIFY PART NO. FOR FLOOR SPLICE 146A9401-4 ATAG WN14921 IAW IPC53-42-11-26;[02] VERIFIED STEP 1;[03] REPLACE T SPLICE;[04] OK TO INSTALL;[05] INSTALLED FLOOR SPLICE T;[06] INSTALLED FLOOR SPLICE IAW AMM 25-52-10/401;[07] VERIFIED INSTALL<BR>AUDIT C/W

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 20,246 hrs · 9,455 cycles

AFT CARGO FLOOR PANEL 140DF HAS CORROSION ALONG EDGE A225-005 / [01] EVALUATED DAMAGE TO AFT CARGO FLOOR PANEL 140DF FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-1 PARA 5.A.(B) FIG. 102 SHT 1;[02] VERIFIED MATERIAL ID AS 2024-T3 .071' CLAD IAW B737-800 SRM 53-60-53-0I-1 TABLE 2 ITEM 1 ATAG: A115230;[03] VERIFIED ITEMS 1 AND 2;[04] BEGAN FABRICATING NEW FLOOR PANEL 140DF IAW B737-800 AMM 25-52-01-201-801; NOT COMPLETE;[05] COMPLETED FABRICATION OF NEW FLOOR PANEL 140DF IAW B737-800 AMM 25-52-01-201-801;[06] VERIFIED STEPS 4 & 5;[07] OK GIVEN TO TREAT AND ORIME;[08] APPLIED ALODINE IAW B737-800 AMM 51-21-41-370-802 AND APPLIED PRIMER IAW B737-800 AMM 51-21-72-370-804;[09] IDENTIFIED PANEL ON LOWER SUFACE IAW B737-800 AMM 25-52-01-201-801 FABRICATION COMPLETE;[10] VERIFIED STEPS 8-9

Part: BAFFLE — CORRODED (AFT CARGO BAY) · airframe 20,246 hrs · 9,455 cycles

A-061 DOT 033 AFT CARGO PIT BAFFLE UNDER R/H Z ANGLE BETWEEN STA 747 AND STA 767 RBL 23 WL 155 CORRODED AT NUTPLATES HOLES / [01] REMOVED DAMAGE PART IAW SRM 51-40-02-0G-0;[02] REMOVED CORROSION ON DAMAGE PARTS IAW SRM 51-10-02-0G-0 ITEM 15;[03] EVALUATED ALLOWABLE LIMITS: .040 ORIGINAL 'T' .025 REMAINING .015 LOSS FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 TOOL USED MICROMETER#AAR24510 DUE 01-25-23;[04] VERIFIED STEPS 1-3 ARE COMPLETE;[05] VERIFIED ITEMS 1 THROUGH 4;[06] ADDED P/N TO MEASUREMENTS TABLE;[07] VERIFIED NEW BAFFLE (SPLICE) P/N146A7505-12 WN 14818 IAW DWG 146A7500 REV:-;[08] VERIFIED STEPS 6 AND 7;[09] LOCATED AND DRILL HOLES ON NEW SPLICE IAW SRM 51-40-05-0G-0;[10] VERIFIED STEP 9.<BR>OK TO INSTALL REPLACEMENT PART.;[11] INSTALLED NEW SPLICE ( BAFFLE) IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV:-;[12] VERIFIED INSTALLATION OF PART IN STEP 11.<BR>OK TO CIC AREA.;[13] APPLIED CIC AREA IAW AMM 51-21-91-620-802;[14] VERIFIED STEP 13. <BR>VERIFIED REPLACEMENT OF SPLICE. <BR>AUDIT C/W.;[15] CHANGED CORROSION LEVEL

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 20,246 hrs · 9,455 cycles

AFT CARGO PIT FWD SHIELD BETWEEN STA 767+2' TO STA 767+10' RBL 23 WL 155 HAS CORROSION ON UPPER AND LOWER SURFACE / [01] REMOVED CORROSION ORIGINAL T= .050' LOSS OF .006' REMAING T= .044' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 TOOLING INFO AAR 35351 CAL DUE 10DEC22. WORK PERFORMED BY BERNARD BEMKE 27266;[02] VERIFIED STEP 1;[03] REMOVED FWD SHIELD IAW SRM 51-40-02-0G-0. WORK PERFORMED BY BERNARD BEMKE 27266;[04] RECEIVED AND VERIFIED REPLACEMENT SHIELD P/N: 146A8127-12 I/A/W BOING DWG NO. 146A0081.;[05] LOCATED AND DRILLED NEW SHIELD I/A/W BOEING DWG NO. 146A0081;[06] VERIFIED STEPS 4-5;[07] OK GIVEN TO INSTALL REPAIR PARTS;[08] INSTALLED FWD SHIELD IAW SRM 51-40-02-0G-0 AND DWG 146A0081 REV A;[09] VERIFIED STEP 8 IS COMPLETE;[10] VERIFIED ITEMS 8 AND 9<BR>OK TO CIC;[11] APPLIED CIC ON FWD SHIELD IAW AMM 51-21-91]620-802;[12] JOB COMPLETE; AUDIT C/W

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 20,246 hrs · 9,455 cycles

AFT CARGO FLOOR PANEL 140BF HAS CORROSION ALONG EDGE A225-002 / [01] FLOOR PANE DAMAGE OF #140BF EXCEEDS 20 MAX ALLOWABLE INCHES. FOUND TO BE OUT OF LIMITS IAW B-737 SRM 53-00-53-1A-1.;[02] MATERIAL VERIFIED AS .071' 2024-T3 IAW B-737 AMM 25-52-01-201-801. A-TAG A115230;[03] VERIFIED ITEMS 1 AND 2;[04] NEW PANEL 140BF FABRICATED IAW B-737 AMM 25-52-01-201-801.;[05] VERIFIED STEP 4;[06] OK GIVEN TO TREAT AND PRIME;[07] TREATED AND PRIMED IAW B-737 AMM 51-21-41 & AMM 51-21-72.;[08] NEW PANEL 140BF FABRICATED IAW B-737 AMM 25-52-01-201-801.;[09] JOB COMPLETE; AUDIT C/W

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 20,246 hrs · 9,455 cycles

AFT CARGO FLOOR PANEL 140AF HAS CORROSION ALONG EDGE A225-001 / [01] EVALUATED CORROSION ON FLOOR PNL 1401F HAVE MORE THAN 20' DAMGE TO PNL OUT OF LIMITS I.A.W 53-00-53-1A-1;[02] VERIFIED ITEM 1;[03] VERIFIED NEW MATERIAL FOR NEW PNL AS 2024-T3-0.071 <BR>ATAG# A118121 I.A.W MM 25-52-01-201-801;[04] VERIFIED ITEM 3;[05] FABRICATED NEW FLOOR PNL .<BR> DRILLED AND TRIMMED PNL I.A.W MM25-52-01-201-801 AND BOEING DWG 453A2610 REV:E;[06] VERIFIED STEP 5;[07] OK GIVEN TO TREAT AND PRIME;[08] ALODINED AND PRIMED LOWER SIDE OF FLOOR PNL.<BR>AND ALODINED UPPER SIDE OF FLOOR PNL I.A.W MM 25-52-01-201-801;[09] JOB COMPLETE; AUDIT C/W

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 20,246 hrs · 9,455 cycles

A-061 DOT 031 AFT CARGO PIT R/H Z ANGLE FROM STA 727G TO STA 747+15' RBL 23 WL 155 CORROSION ON UPPER SURFACE / [01] REMOVED CORROSION FROM RH ZEE ANGLE STA 727G-747+15 ORIINAL T= .045' LOSS OF .009' REM T= .036' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 TOOLING INFO AAR 41392 CAL DUE 08SEP22 WORK PERFORMED BY AUSTIN LANDIS 28323;[02] VERIFIED STEP 1;[03] CUT OUT DAMAGE Z ANGLE SECTION BETWEEN STA 727G TO 727F AND REMOVED IAW SRM 53-00-53-2R-5 REPAIR 5;[04] VERIFIED MATERIAL ID FOR Z ANGLE REPAIR PARTS BAC1496-377-7075 T6 TAG# A119065 IAW SRM 53-00-53-2R-5;[05] VERIFIED STEP 4 IS COMPLETE;[06] VERIFIED ITEMS 3 THROUGH 5;[07] STARTED TO FABRICATE Z ANGLE REPAIR PARTS IAW SRM 53-00-53-2R-5;[08] VERIFIED STEP 7;[09] FINISHED TO FABRICATE Z ANGLE REPAIR PARTS IAW SRM 53-00-53-2R-5 REPAIR 5;[10] VERIFIED STEP 9;[11] VERIFIED STEP 9-10 AND OK TO TREAT AND PRIME;[12] APPLIED ALODINE AND PRIMER TO Z ANGLE REPAIR PARTS IAW SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804;[13] CERTIFIED STEP 12;[14] VERIFIED STEPS 12-13;[15] OK GIVEN TO INSTALL Z ANGLE;[16] INSTALLED Z ANGLE REPAIR PARTS IAW SRM 53-00-53-2R-5 REPAIR 5;[17] VERIFIED STEP 16;[18] VERIFIED ITEM 16;[19] OK TO CIC UPPER AND LOWER SURFACES OF Z ANGLE .;[20] APPLIED CIC TO UPPER AND LOWER SEURFACES IAW AMM 51-21-1;[21] VERIFIED STEP 20;[22] C/W;[23] JOB COMPLETE; AUDIT C/W;[24] CHANGED CORROSION LEVEL

Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 20,246 hrs · 9,455 cycles

AFT CARGO FLOOR PANEL 140EF HAS CORROSION ALONG EDGE A225-003 / [01] EVALUATED DAMAGE TO AFT CARGO FLOOR PANEL 140EF FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-1 PARA 5.A.(B) FIG. 102 SHT 1;[02] VERIFIED ITEM 1;[03] VERIFIED MATERIAL TO FAB NEW PANEL AS 2024-T3 .071' ATAG A1181277 IAW AMM 25-52-01-201-801;[04] VERIFIED STEP 3;[05] COMPLETED FABRICATION OF PANEL 140EF IAW AMM 25-52-01-201-801.;[06] VERIFIED STEP 5<BR><BR>OK TO TREAT AND PRIME;[07] TREATED AND PRIMED PANEL IAW AMM 51-21-41; AMM 51-21-99;[08] FABRICATED REPLACEMENT PANEL 140EF IAW AMM 25-52-01-201-801.;[09] VERIFIED STEPS 7 & 8<BR>AUDIT CW

Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 20,246 hrs · 9,455 cycles

FWD CARGO METAL FLOOR PANEL 120DF HAS CORROSION AROUND EDGES. DOT 234/01 / [01] EVALUATED DAMAGE TO FWD CARGO FLOOR PANEL 120DF FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-53-1A-1 PARA 5.A.(B) FIG. 102 SHT 1;[02] VERIFIED STEP 1; OUT OF LIMITS;[03] VERIFIED MATERIAL ID FOR NEW PANEL AS 2024-T3 .071' CLAD ATAG: A118128 IAW B737-800 SRM 53-30-53-0I-1 TABLE 2 ITEM 1;[04] VERIFIED STEP 3;[05] BEGAN FABRICATION OF NEW FLOOR PANEL 120 DF IAW B737-800 AMM 25-52-01-201-801; NOT COMPLETED;[06] COMPLETED LOCATING AND DRILLING PANEL 120DF IAW B737 AMM 25-52-01-201-801; NEEDS TRIMMED AND COUNTERSUNK.;[07] VERIFIED STEP 6;[08] FINISHED FABRICATION OF PNL 120DF IAW AMM 25-52-01-201-801;[09] VERIFIED STEP 8;[10] VERIFIED STEPS 8 & 9;[11] OK GIVEN TO TREAT AND PRIME;[12] TREATED IAW AMM 51-21-41-370-801 AND PRIMED IAW AMM 51-21-72-370-804;[13] VERIFIED JOB IS COMPLETE;[14] VERIFIED 13

Part: ANGLE — CRACKED (RT AC BAY) · airframe 20,246 hrs · 9,455 cycles

RIGHT PACK BAY, HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT BS 663, RBL 10 FOUND CRACKED. REMOVED ALL FASTENERS IN REPAIR AREA IAW SRM 57-10-10-2R-5, FIG 202 SH 6. REMOVED DAMAGE IAW SRM 57-10-10-2R-5 FIG 202 SH 6. HFEC IAW NDT PART 6; 51-00-00 PROC 16. NO DEFECTS NOTED. LOCATED; DRILLED & TRIMMED THE REPLACEMENT ANGLE. LOCATED, DRILLED & TRIMMED SPLICE ANGLE IAW SRM 57-10-10-2R-5 FIG 202 SH 6. TREATED AND PRIMED REPAIR AND CUTOUT IAW SRM 57-10-10-2R-5 STEO 4F-4G. INSTALLED REPAIR IAW SRM 57-10-10-2R-5 STEP 4L(1)-4L(7).

Part: ANGLE — CRACKED (LH AC BAY) · airframe 20,246 hrs · 9,455 cycles

LEFT PACK BAY; HORIZONTAL ANGLE COMMON TO LOWER SIDE OF CENTER FUEL TANK AT BS 663, LBL 10 CRACKED. REMOVED DAMAGE IAW SRM 57-10-10-2R-5 FIG 202 SH 6. LOCATED, DRILLED & TRIMMED ANGLE IAW SRM 57-10-10-2R-5 FIG 202 SH 6. LOCATED, DRILLED & TRIMMED SPLICE ANGLE IAW SRM 57-10-10-2R-5 FIG 202 SH 6. TREATED & PRIMED REPAIR PARTS & CUTOUT IAW SRM 57-10-10-2R-5 STEO 4F-4G. INSTALLED REPAIR PARTS IAW SRM 57-10-10-2R-5 STEP 4L(1)-4L(7). BOND CHECK GOOD IAW SRM 57-10-10-2R-5 STEP 4M AND FIG 202 SH 6 FN 1. SEALED AND FILLET SEALED FASTENERS EXTERNALLY. SEALED FUEL TANK FASTENERS INTERNALLY IAW SRM 57-10-10-2R-5 STEP 4L(8). PERFORMED FUEL LEAK CHECK PER AMM 28-11-00/601. NO LEAKS NOTED.

Part: SIGN — LOOSE (L/H CABIN) · airframe 20,176 hrs · 9,416 cycles

OVERWING EXIT SIGN FELL OFF CAPTAINS SIDE / [01] INSTALLED OVERWING EXIT SIGN ON CEILING PER SIP CKS OK

Part: NONE — MISSING (FWD CABIN) · airframe 20,160 hrs · 9,407 cycles

FORWARD LENS COVER FOR CEILING EMERGENCY EXIT LIGHT MISSING / [01] REPLACED O/H EMERGENCY EXIT SIGN LENS IAW AMM 33-51-11. OPS CHK OK.

Part: LENS — MISSING (CABIN) · airframe 19,083 hrs · 8,817 cycles

EXIT SIGN LENSE COVER MISSING; SIDEWALL; AFT GALLEY CAPTAINS SIDE ; / [01] REPLACED LENS ASSAY PER AMM 33-51-01

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 8,209 hrs · 17,917 cycles

EXIT ROW SIGN COVER FELL OFF / RESECURED COVER PER SIP

Part: LIGHT — INTERMITTENT (CABIN) · airframe 8,075 hrs · 17,650 cycles

EXIT DOOR BULKHEAD LIGHT ABC ROW 14 FLICKERING ( CABIN INTERIOR ILLUM BOEING SKY INTERIOR PHOTOLUMINESCENT ) / R&R'D LIGHT ASSEMBLY IAW MM 33-51-04CLOSING# 90702

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 17,267 hrs · 7,870 cycles

EMERGENCY EXIT (AISLE) COVER LOOSE / INSTALLED EMERGENCY EXIT SIGN COVER IAW AMM 33-51-01 OPS CK OK

Part: SLIDE — DISPLACED (L1 DOOR) · airframe 14,407 hrs · 6,400 cycles

PORTION OF THE ESCAPE SLIDE IS COMING OUT THE BOTTOM OF THE L1 DOOR AND THE GIRT BAR WOULD NOT ENGAGE / C/W MT# 75-61-06 SLIDE REMOVAL AND INSTALLATION

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 14,169 hrs · 6,279 cycles

FA'S REPORT FWD ENTRY ESCAPE SLIDE RETENTION BAR VERY DIFFICULT TO GET INTO AND OUT OF FLOOR MOUNTED BRACKETS. / REPOSITION SLIDE OPS CK OK PER MT 725-61-05

Part: SLIDER — CRACKED (HORIZONTAL STAB) · airframe 13,609 hrs · 6,021 cycles

RH HORIZONTAL STAB; FWD UPPER L/E SLIDE CRACK / REMOVED AMD REPLACED SLIDER PER SRM 51-40-02. INSPECTOR H53

Part: HMU — FAULTY (NR 2 ENGINE) · airframe 12,474 hrs · 5,509 cycles

NR 2 ENGINE WOULD NOT MAKE TAKEOFF POWER. R&R HYDRO MECHANICAL UNIT PER AMM.

Part: SIGN — MISSING (CABIN) · airframe 12,262 hrs · 5,412 cycles

EMERGENCY EXIT SIGN AT AISLE EXIT AREA MISSING. REINSTALLED SIGN PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 7,414 hrs · 3,306 cycles

R2 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. R&R LAMP IAW AMM.

Part: LATCH — BROKEN (FLASHLIGHT) · airframe 6,783 hrs · 3,021 cycles

AFT GALLEY UNDER THE LT INSPECTION SLAT FLASHLIGHT LATCH BROKEN. R & R THE LATCH IAW SIP.

Part: LENS — LOOSE (EXIT SIGN) · airframe 6,004 hrs · 2,670 cycles

CEILING OVERWING EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: SWITCH — FAULTY (E&E BAY) · airframe 5,719 hrs · 2,539 cycles

AIR TURNBACK, ON TAKEOFF RAISED LANDING GEAR HANDLE TO UP POSITION. INDICATORS ON FRONT 3 RED/3 GREEN, PLACED HANDLE UP THEN PLACED HANDLE DOWN. R&R MANUAL EXTENSION ACCESS DOOR SWITCH PER AMM.