N8693A

Part: LENS — MISSING (ZONE 200) · airframe 30,913 hrs · 15,390 cycles

EXIT SIGN COVER AT FWD SERVICE DOOR MISSING. INSTALLED THE LENS IAW AMM 33-51-01.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 29,888 hrs · 14,887 cycles

FWD AND AFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHTS INOP. R&R FWD AND AFT FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT BATTERIES PER CMM 25-60-02.

Part: FLASHLIGHT — NO TEST (ZONE 200) · airframe 29,762 hrs · 14,814 cycles

OUTBOARD FLASHLIGHT WONT TEST. R & R THE BATTERY TO FWD OTBD FLASHLIGHT IAW SIP, OPS CHECKED GOOD.

Part: SILL DRAIN — ODOR (ZONE 200) · airframe 29,690 hrs · 14,777 cycles

TERRIBLE SMELL COMING FROM AFT GALLEY FLOOR DRAINS<[01] CLEANED AND FLUSHED AFT ENTRY AND AFT SERVICE DOOR SILL DRAINS REF AMM 38-31-00

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 29,542 hrs · 14,701 cycles

F/A FWD EMERGENCY FLASHLIGHT, LEFT SIDE WILL NOT TEST. R & R THE BATTERY IAW AMM 25-64-00.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 29,470 hrs · 14,662 cycles

EMERGENCY LIGHT RT BATTERY PACK AT BS 565 IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK AT BS 565 IAW MM 33-51-06. CABIN EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06.

Part: ATTACH ANGLE — CRACKED (ZONE 500) · airframe 29,470 hrs · 14,662 cycles

LEFT WING TRAILING EDGE; ATTACH ANGLE FROM DEFLECTION CONTROL RIB TO INTERCOSTAL WEB IS CRACKED. REMOVED CRACKED ANGLE PER SRM 51-40-02.;[02] ANGLE HAS BEEN REMOVED. LOCATED; DRILLED AND DEBURRED REPLACEMENT ANGLE PER SRM 51-40-05. INSTALLED REPLACEMENT ANGLE PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (ZONE 500) · airframe 29,470 hrs · 14,662 cycles

L/H WING TRAILING EDGE; INTERCOSTAL WEB INBD OF DEFLECTION CONTROL RIB IS CRACKED. REMOVED AND REPLACED INTERCOSTAL WEB PER SRM 51-40-02.

Part: ANGLE — CRACKED (ZONE 500) · airframe 29,470 hrs · 14,662 cycles

L/H WING TRAILING EDGE; ANGLE INBD OF INTERCOSTAL WEB AT DEFLECTION CONTROL RIB IS CRACKED. REMOVED CRACKED ANGLE INBD OF INTERCOSTAL WEB PER SRM 51-40-02. CRACKED ANGLE INBD OF INTERCOSTAL WEB HAS BEEN REMOVED. LOCATED; DRILLED AND DEBURRED REPLACEMENT ANGLE IAW SRM 51-40-05.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 29,470 hrs · 14,662 cycles

CRACK FOUND AT L/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE LBL 9. CUT OUT AND REMOVED BS 663 ATTACH ANGLE FROM APPROX LBL 18-LBL 5. ALL WORK DONE IAW SRM 57-10-10-2R-5.

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 29,470 hrs · 14,662 cycles

R/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT RBL 34. FABRICATED & MATCH DRILLED REPAIR PARTS PER SRM 57-10-10-2R-5. INITIAL AREA AND FASTENER HOLES REQUIRE NDT & GVI.;[03] PERFORMED NDT PER BOEING 51-00-00 PART 6. PROCEDURE 16 WITH NO DEFECT NOTED. PERFORMED GVI INSPECTION OF FASTENERS HOLES AND FOUND NO DEFECT. INSTALLED FASTENERS COMMON TO FUEL TANK PER SRM 51-40-02 & DWG 111A1000. REMOVED CRACKED PORTION OF ANGLE PER SRM 51-10-02. INSTALLED REMAINING REPAIR FASTENERS PER SRM 57-0-10-2R-5. C/W RII INSPECTION OF C/A #6;7;AND 8. VERIFIED DOME SEALED FASTENERS IAW AMM 51-31-00.

Part: PANEL — PULLED (ZONE 500) · airframe 29,470 hrs · 14,662 cycles

LH WING TRAILING EDGE PANEL 561BB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. ACCOMPLISHED REPAIR TO AREA REF SRM 51-70-04-2R-9 PER CORRECTIVE ACTIONS 1 AND 2. RESTORED FINISH TO AREA REF AMM 51-21-99..

Part: PANEL — PULLED (ZONE 500) · airframe 29,470 hrs · 14,662 cycles

LH WING TRAILING EDGE PANEL 561CB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. REMOVED DAMAGE AND ACCOMPLISHED REPAIR REF SRM 51-70-04-2R-9 SEE C/A 1-4. RESTORED FINISH TO REPAIR AREA REF AMM 51-21-99.

Part: PANEL — DAMAGED (ZONE 500) · airframe 29,470 hrs · 14,662 cycles

LH WING TRAILING EDGE PANEL 561AB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. REMOVED DAMAGE AND ACCOMPLISHED REPAIR REF SRM 51-70-04-2R-9 SEE C/A 1-4. RESTORED FINISH TO REPAIR AREA REF AMM 51-21-99.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 26,841 hrs · 13,223 cycles

FAS REPORT FWD ENTRY EMERG SLIDE GIRT BAR DIFFICULT TO ARM /INSERT INTO FLOOR RECEPTACLE<[01] ADJUSTED FWD ENTRY DOOR EMERGENCY SLIDE IAW AMM 25-66-01; OPS CHECK GOODS

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 26,745 hrs · 13,174 cycles

FWD GALLEY FLIGHT ATT FLASHLIGHT INOP FWD GALLEY FLIGHT ATT FLASHLIGHT INOP<

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,036 hrs · 12,784 cycles

CABIN EMERGENCY LIGHT BATTERY PACK M2335 INOP<[01] REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M2335 PER AMM 33-51-06. OPS CHECK GOOD;[02] VERIFIED. REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M2335 PER AMM 33-51-06. OPS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,036 hrs · 12,784 cycles

CABIN EMERGENCY LIGHT BATTERY PACK M1676 INOP<[01] REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M1676 PER AMM 33-51-06. OPS CHECK GOOD;[02] VERIFIED. REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M1676 PER AMM 33-51-06. OPS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,036 hrs · 12,784 cycles

CABIN EMERGENCY LIGHT BATTERY PACK M1694 INOP<[01] REPLACED CABIN EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY M1694 PER AMM 33-51-06. OPS CHECK GOOD;[02] VERIFIED. REPLACED CABIN EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY M1694 PER AMM 33-51-06. OPS CHECK GOOD

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,036 hrs · 12,784 cycles

CABIN EMERGENCY LIGHT BATTERY PACK M1675 INOP<[01] REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M1675 PER AMM 33-51-06. OPS CHECK GOOD;[02] VERIFIED. REPLACED CABIN EMERGENCY LIGHT BATTERY PACK M1675 PER AMM 33-51-06. OPS CHECK GOOD

Part: WEB — CRACKED (RT WING) · airframe 26,036 hrs · 12,784 cycles

R/H WING VERTICAL WEB LOCATED JUST INBOARD OF DEFLECTION RIB AT WS 278.5 IS CRACKED AT OUTBOARD HOLE.<[01] REMOVED CRACKED VERTICAL WEB PER SRM 51-40-02. DRILLED REPLACEMENT WEB PER SRM 51-40-05.;[02] 02 - INSPECTED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[03] OK TO INSTALL REPAIR PARTS.;[04] INSTALLED NEW R/H WING VERTICAL WEB LOCATED JUST INBOARD OF DEFLECTION RIB AT WS 278.5 PER SRM 51-40-02.;[05] C/W.

Part: FITTING — CRACKED (FWD CARGO) · airframe 26,036 hrs · 12,784 cycles

FWD CARGO AFT CORNER THRESHOLD FITTING IS CRACKED<[01] 01 - REMOVED AND REPLACED PER [AMM 53-11-02-401-NG (CARGO DOOR SCUFF PLATE - REMOVAL/INSTALLATION - PERMANENT)];[02] 02 - INSPECTED PER [AMM 53-11-02-401-NG (CARGO DOOR SCUFF PLATE - REMOVAL/INSTALLATION - PERMANENT)]

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 26,036 hrs · 12,784 cycles

L/H O/B AFT FLAP HAS DELAMINATION AT I/B LOWER CORNER LOWER SURFACE.<[01] REMOVED L/H O/B AFT FLAP ASSY. REF AMM 27-51-22;[02] INSTALLED L/H O/B AFT FLAP. REF AMM 27-51-22. PENDING ADJUSMENT CK.;[03] 02 - INSPECTED PER [AMM 27-51-22-401-NG (OUTBOARD AFT FLAP - REMOVAL/INSTALLATION - PERMANENT)];[04] REMOVED AND REPLACED L/H O/B AFT FLAP PER 27-51-22;[05] RII INSPECTED AS REQUIRED. CORRECTIVE ACTION #4

Part: FUEL PANEL — CORRODED (RT WING) · airframe 26,036 hrs · 12,784 cycles

FUELING STATION PANEL AT 621GB HAS SURFACE CORROSION.<[01] REMOVED AND REPLACED FUELING PANEL PER SOPM 20-50-01 AND MM 28-41-61;[02] VERIFIED. REMOVED AND REPLACED FUELING PANEL PER SOPM 20-50-01 AND MM 28-41-61;[03] WING REFUELING PANEL INDICATORS AND LIGHTS OPS CHECKED GOOD PER MM 28-21-00;[04] C/W STEP#1.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 26,036 hrs · 12,784 cycles

AFT R/H LAV; O/B AFT FLOOR MOUNT AT STA 947 HAS AREA OF SURFACE CORROSION IN FLOOR BEAM. REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. CUT AND REMOVED UPPER CHORD FLANGE OF STA. 947 FLOORBEAM FROM RBL 9' TO RBL 59' PER SRM 53-70-51-2R-5; ALTERNATIVE 2. C/W ALL STEPS REPAIRED PER SRM 53-70-51-2R-5; ALTERNATIVE 2 AND EA 24-153-01228-WIP1.

Part: FLOOR SUPPORT — CORRODED (BS 947-967 RBL24) · airframe 26,036 hrs · 12,784 cycles

INTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 24 HAS SURFACE CORROSION.<[01] REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] LOCATED AND DRILLED NEW INTERCOSTAL FROM STA. 947 TO STA. 967 AT RBL 24 PER SRM 51-40-05.;[03] VERIFIED2. RAJESH ALI (TECHNICIAN); 10-MAY-2024 06:21 UTC<BR>LOCATED AND DRILLED NEW INTERCOSTAL FROM STA. 947 TO STA. 967 AT RBL 24 PER SRM 51-40-05.;[04] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[05] C/W INSPECTION

Part: MOUNT — CORRODED (BS 947) · airframe 26,036 hrs · 12,784 cycles

AFT R/H LAV; O/B AFT MOUNT AT STA 947 HAS AREAS OF SURFACE CORROSION ON INTERCOSTAL. (MARKED)<[01] PRIOR TO BLENDING; DEPTH OF CORROSION IS .092'. REMAINING THICKNESS IS .108'. DAMAGE IS OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] LOCATED AND DRILLED NEW INTERCOSTAL BETWEEN STA. 947 TO STA. 967 AT RBL 50' PER SRM 51-40-05.;[03] VERIFIED1. RAJESH ALI (TECHNICIAN); 10-MAY-2024 06:32 UTC<BR>PRIOR TO BLENDING; DEPTH OF CORROSION IS .092'. REMAINING THICKNESS IS .108'. DAMAGE IS OUT OF LIMITS PER SRM 53-70-51-1A-1.;[04] VERIFIED2. RAJESH ALI (TECHNICIAN); 10-MAY-2024 06:33 UTC<BR>LOCATED AND DRILLED NEW INTERCOSTAL BETWEEN STA. 947 TO STA. 967 AT RBL 50' PER SRM 51-40-05.;[05] INSTALLED NEW INTERCOSTAL PER SRM 51-40-02.;[06] C/W INSPECTION;[07] C/W INSPECTION

Part: MOUNT — CORRODED (ZN 200 FUS TOP) · airframe 26,036 hrs · 12,784 cycles

AFT GALLEY L/H FWD FLOOR MOUNT HAS POSSIBLE LIGHT CORROSION PRESENT AROUND LOWER O/B EDGE. REMOVED DAMAGE PER SRM 51-10-02. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. MEASURES 0.010 DEEP. REMOVED L/H AFT SHEAR WEB PER SRM 51-40-02. LOCATED AND DRILLED NEW WEB PER SRM 51-40-05. TREATED AND PRIMED OPEN HOLES AND BARE METAL ON NEW WEB AND AIRCRAFT STRUCTURE PER SRM 51-20-01. INSTALLED NEW WEB, PRIMED ALL FASTENER HEADS, AND APPLIED FILLET SEAL PER SRM 51-40-02. LOCATED AND DRILLED NEW WEB PER SRM 51-40-05. TREATED AND PRIMED OPEN HOLES AND BARE METAL ON NEW WEB AND AIRCRAFT STRUCTURE PER SRM 51-20-01. INSTALLED NEW WEB; PRIMED ALL FASTENER HEADS; AND APPLIED FILLET SEAL PER SRM 51-40-02

Part: STRINGER CLIP — CRACKED (BS 500I S25R) · airframe 26,036 hrs · 12,784 cycles

FWD CARGO COMPARTMENT HAS A STRINGER CLIP THAT IS CRACKED AT FRAME RIVETS; STA 500I STR 25R.<[01] REMOVED RH SIDE PLATE BAFFLE AND BULKHEAD LOWER CHORD TO FOM PER SRM 51-40-02.;[02] REMOVED DAMAGED STRINGER CLIP ; LOCATED AND DRILLED NEW CLIP PER SRM 51-40-02.;[03] VERIFIED LOCATED AND DRILLED NEW CLIP<BR>LINE 2;[04] INSTALLED NEW CLIP PER SRM 51-40-02.;[05] 02 - INSPECTED PER SRM 51-40-02;[06] REMOVED RH SIDE PLATE BAFFLE AND BULKHEAD LOWER CHORD TO FOM PER SRM 51-40-02. REMOVED DAMAGED STRINGER CLIP ; LOCATED AND DRILLED NEW CLIP PER SRM 51-40-02. RESTORED AREA PER SRM 51-40-02.;[07] C/W INSPECTION;[08] C/W INSPECTION;[09] C/W INSPECTION OF STEP #1

Part: FLOORBEAM — CORRODED (BS 987) · airframe 26,036 hrs · 12,784 cycles

AFT GALLEY FLOOR STRUCTURE WET AREA AT STA 986.5 APPROXIMATELY 18' I/B OF AFT SERVICE DOOR OPENING HAS SMALL AREA OF SURFACE CORROSION ON FLOOR BEAM FASTENER HOLE. BLENDED LIGHT CORROSION PER SRM 51-10-02. REMAINING THICKNESS .140. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1. PERFORMED DETAILED INSPECTION OF THE ADJACENT STRUCTURE IN THE REPAIR, NO DAMAGE NOTED. PER SRM 53-70-51-2R-6.;[04] PERFORMED (HFEC) SURFACE INSPECTION PER NDT PART 6; 51-00-00; PROCEDURE 23. NO DEFECTS FOUND. PERFORMED OPEN HOLE HFEC INSPECTION PER 737 NDT PART 6; 51-00-00, PROCEDURE 16. NO DEFECTS FOUND. FLAP PEENED, TREATED, & PRIMED AREA PER SRM 53-70-51-2R-6; ALTERNATIVE 1. DRILLED; COUNTERSUNK; AND DEBURRED REPAIR HOLES IN 986.5 FLOORBEAM FORWARD FLANGE PER SRM 53-70-51-2R-6; ALTERNATIVE 1. FABRICATED; LOCATED; DRILLED; AND DEBURRED REPAIR STRAP PER SRM 53-70-51-2R-6; ALTERNATIVE 1. TREATED AND PRIMED REPAIR STRAP PER SRM 53-70-51-2R-6, ALTERNATIVE 1. INSPECTED C/A 5; 6; AND 7 PER SRM 53-70-51-2R-6; ALTERNATIVE 1. ACCOMPLISHED REPAIR OF 986.5 FLOORBEAM APPROX 18 " I/B OF AFT SERVICE DOOR OPENING PER SRM 53-70-51-2R-6; ALTERNATIVE 1. ACCOMPLISHED REPAIR OF 986.5 FLOORBEAM APPROXIMATELY 18" I/B OF AFT SERVICE DOOR OPENING PER SRM 53-70-51-2R-6; ALTERNATIVE 1.

Part: STRINGER CLIP — CRACKED (BS 500I S25L) · airframe 26,036 hrs · 12,784 cycles

FWD CARGO COMPARTMENT HAS A STRINGER CLIP THAT IS CRACKED AT FRAME RIVETS; STA 500I STR 25L.<[01] REMOVED DAMAGED STRINGER CLIP REF SRM 51-40-02.;[02] REMOVED L/H SIDE BAFFLE TO FOM REF SRM 51-40-02.;[03] LOCATED AND DRILLED NEW CLIP PER SRM 51-40-02.;[04] OK TO INSTALL STRINGER CLIP;[05] INSTALLED NEW CLIP AND ORIGINAL SIDE BAFFLE; RESTORED AREA. REF SRM 51-40-02.;[06] CW;[07] CORRECTIVE ACTION FOR PREVIOUS 'CW' SHOULD BE STATED AS UPDATED.;[08] INSPECTION COMPLETE ON CORRECTIVE ACTION #5 FOR STRINGER CLIP INSTALLATION.

Part: FLOOR SUPPORT — CORRODED (BS 987) · airframe 26,036 hrs · 12,784 cycles

AFT GALLEY FLOOR STRUCTURE SUPPORT ANGLE AT STA 986.5 +8' APPROXIMATELY 12' I/B OF AFT SERVICE DOOR OPENING HAS SMALL AREA OF SURFACE CORROSION ON FASTENER HOLE. REMOVED CORROSION PER SRM 53-70-51-1A-1. FOUND TO BE OUT OF LIMITS. BLENDED CORROSION ON AFT GALLEY STRUCTURE SUPPORT ANGLE PER SRM 51-10-02. REMAINING THICKNESS 0.035. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1. REMOVED SUPPORT ANGLE FOR REPLACEMENT PER SRM 51-40-02. VERIFIED OUT OF LIMITS PER SRM 53-70-51-1A-1. LOCATED, DRILLED, COUNTERSUNK, AND DEBURRED REPLACEMENT SUPPORT ANGLE PER SRM 51-40-05 AND SRM 51-40-08. LOCATED, DRILLED, COUNTERSUNK, AND DEBURRED REPLACEMENT SUPPORT ANGLE PER SRM 51-40-05 AND SRM 51-40-08. INSTALLED NEW SERVICEABLE AFT GALLEY FLOOR STRUCTURE SUPPORT ANGLE PER SRM 51-40-02. INSTALLED NEW SERVICEABLE AFT GALLEY FLOOR STRUCTURE SUPPORT ANGLE PER SRM 51-40-02.

Part: MOUNT — CORRODED (BS 947) · airframe 26,036 hrs · 12,784 cycles

AFT L/H LAV; O/B AFT FLOOR MOUNT AT STA 947 HAS AREAS OF SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-02. DAMAGE REMOVAL .041' OUT OF LIMITS PER SRM 53-70-51-1A-1 REMAINING THICKNESS ON 947.5 FLOORBEAM. REMOVED AFT L/H LAV; O/B AFT FLOOR MOUNT AT STA 947 IAW SRM 51-40-02. UPON FURTHER INSPECTION; FOUND AREA REPAIRABLE PER SRM 53-70-51-2R-8. ACCOMPLISHED BLENDOUT FOR SHIM PER SRM 53-70-51-2R-8. MAX MATERIAL REMAINING 0.136. MATERIAL REMOVAL IS WITHIN LIMITS PER SRM 53-70-51-2R-8. FLAP PEENED REMOVAL AREA PER SRM 53-70-51-2R-8 AND SOPM 20-10-03. FABRICATED, DRILLED, & DEBURRED 0.040. SHIM SRM 53-70-51-2R-8 ALTERNATIVE 3. FABRICATED, DRILLED, & DEBURRED 0.040? 7075-T6 SHIM PER SRM 53-70-51-2R-8 ALTERNATIVE 3. FABRICATED ON CA36 PER SRM 53-70-51-2R-8 ALTERNATIVE 3. INSTALLED REPAIR SHIM PER SRM 53-70-51-2R-8 ALTERNATIVE 3. REINSTALLED AFT L/H LAV, O/B AFT FLOOR MOUNT AT STA 947 IAW SRM 51-40-02. INSTALLED REPAIR SHIM PER SRM 53-70-51-2R-8 ALTERNATIVE 3. REINSTALLED AFT L/H LAV; O/B AFT FLOOR MOUNT AT STA 947 IAW SRM 51-40-02.

Part: MOUNT — CORRODED (BS 947) · airframe 26,036 hrs · 12,784 cycles

AFT R/H LAV; I/B AFT FLOOR MOUNT AT STA 947 HAS AREAS OF SURFACE CORROSION. (MARKED)<[01] REMOVED AFT R/H LAV; I/B AFT FLOOR MOUNT AT STA 947 IAW SRM 51-40-02;[02] REMOVED CORROSION ON FLOOR BEAM AT STA 947; RBL 24 PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. THIS REPAIR WILL BE ACCOMPLISHED ON FAULT #TTG8Q00T663C AND EA 24-153-01228.;[03] C/W INSPECTION

Part: ANGLE — CORRODED (BS 500E-500F) · airframe 26,036 hrs · 12,784 cycles

FWD CARGO STA 500E TO 500F AT TRANSITION ANGLE ON LEFT SIDE HAS CORROSION AROUND NUT PLATE HOLES. BLENDED AREAS; REMOVED .023' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR TTG8Q00T572F FROM BS 480 + 10 TO 500E + 10. RII - C/W INSPECTION.BLENDED AREAS; REMOVED .023' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR TTG8Q00T572F FROM STA. 480 + 10 TO 500E + 10.

Part: ANGLE — CORRODED (BS 727I-727J) · airframe 26,036 hrs · 12,784 cycles

AFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN AND AROUND NUT PLATE HOLES AT BS 727I TO 727J. REMOVED SURFACE CORROSION ON AFT CARGO RH TRANSITION ANGLE FROM STA 727I TO 727J. REMAINING THICKNESS IS 0.036. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.

Part: WEB — CORRODED (BS 767-787 S25R) · airframe 26,036 hrs · 12,784 cycles

AFT CARGO RIGHT INTERCOSTAL WEB AT STRINGER 25R BS 767 TO 787 HAS CORROSION IN AND AROUND NUT PLATE HOLES(MARKED).<[01] 01 - REMOVED AND REPLACED PER [SRM 51-10-02-0G-0-B00070 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)] REMOVED SURFACE CORROSION ON FASTENER HOLES PER SRM 51-10-02; FOUND TO BE OUT OF ALLOWABLE LIMITS. MATERIAL REMOVED .0085' AND REMAINING THICKNESS .0315'. NEW PART # 146A8127U12 WAS OBTAINED FROM STORES TO BE INSTALLED IAW SRM 51-40-02;[02] REMOVED SURFACE CORROSION ON FASTENER HOLES PER SRM 51-10-02; FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-60-15-1A-1 MATERIAL REMOVED .0085' AND REMAINING THICKNESS .0315'. NEW PART # 146A8127U12 WAS OBTAINED FROM STORES TO BE INSTALLED IAW SRM 51-40-02;[03] INSPECTION COMPLETE ON CORRECTIVE ACTION #2 FOR REMOVAL OF DAMAGE AND FINDING IT TO BE OUT OF LIMITS.;[04] CHANGED MEASUREMENT #17 PART NUMBER FROM 146A8127U12 TO 146A8127-12.;[05] INSTALLED SHIELD PART #146A8127-12 ASSY IAW SRM 51-40-02;[06] INSPECTION COMPLETE ON CORRECTIVE ACTION #5 FOR INSTALLATION OF SHIELD ASSEMBLY FWD OF AFT CARGO DOOR.

Part: WEB — CORRODED (AFT CARGO) · airframe 26,036 hrs · 12,784 cycles

AFT CARGO THRESHOLD WEB HAS CORROSION IN AND AROUND NUTPLATE HOLES AT NUMEROUS LOCATIONS. REMOVED SURFACE CORROSION AROUND DISCREPANT NUTPLATE HOLE LOCATIONS PER SRM 51-10-02; FOUND TO BE OUT OF ALLOWABLE LIMITS PER SRM 53-60-12-1A-1. MATERIAL REMOVED .010' AND REMAINING THICKNESS IS .030' THRESHOLD WEB REQUIRED TO BE REPLACED. REMOVED AFT CARGO THRESHOLD WEB PER SRM 51-40-02. LOCATED; DRILLED; AND COUNTERSUNK NEW AFT CARGO THRESHOLD WEB IAW SRM 51-40-05 AND SRM 51-40-08. TREATED AND PRIMED NEW HOLES IAW SRM 51-20-01. LOCATED; DRILLED; AND COUNTERSUNK NEW AFT CARGO THRESHOLD WEB IAW SRM 51-40-05 AND SRM 51-40-08. TREATED AND PRIMED NEW HOLES IAW SRM 51-20-01. INSTALLED NEW AFT CARGO THRESHOLD WEB IAW SRM 51-40-02. INSTALLED NEW AFT CARGO THRESHOLD WEB IAW SRM 51-40-02.

Part: RIB — WORN (RT WING TE) · airframe 26,036 hrs · 12,784 cycles

RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB IS WORN AT 2 FASTENER HOLES. TRIMMED OFF DAMAGED UPPER TAB FROM DEFLECTION CONTROL RIB IAW SRM 51-10-02 AND SRM 57-51-02-2R-3 REPAIR 3 STEP E. REPAIRED RIGHT WING TRAILING EDGE DEFLECTION RIB PER SRM 57-51-02-2R-3 AND SRM 57-51-02-2R-1.

Part: WEB — DAMAGED (FWD CARGO) · airframe 26,036 hrs · 12,784 cycles

FWD CARGO DOORWAY THRESHOLD WEB HAS NUMEROUS AREAS OF MISSING PRIMER.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-20-01-0G-0-B00331 (GENERAL - PROTECTIVE TREATMENT OF METALLIC AND COMPOSITE MATERIALS - AIRFRAME - PERMANENT)]PREPPED ;TREATED AND PRIMED THE AREA PER SRM 51-20-01.;[02] COMPLIED WITH INSPECTION.

Part: ANGLE — CORRODED (BS 500A-500B) · airframe 26,036 hrs · 12,784 cycles

FWD CARGO STA 500A TO 500B AT TRANSITION ANGLE ON LEFT SIDE HAS CORROSION AROUND NUT PLATE HOLES.<[01] BLENDED AREAS; REMOVED .008' MATERIAL. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] C/W INSPECTION CA #1.;[03] REMOVED AND REPLACED L/H TRANSITION ANGLE FROMSTA.480+10 TO STA. 500E+10; PER SRM. 53-00-53-2R-5-B00308;[04] REJECT: THE FAULT IS REJECTED FOR THE FOLLOWING REASONS : 1) REPAIR PARTS AND MATERIALS NOT ATTACHED TO NON-ROUTINE; 2) FABRICATION OF REPAIR PARTS IN STEP 1 WERE NOT INSPECTED BY QC PRIOR TO INSTALLATION; 3) NO OK TO INSTALL ; 4) EA M-22-153-01550 SUBTASK NOT COMPLETED; STEP 1 REFERENCES AN EA NOT ATTCHED TO FAULT.;[05] THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550'.;[06] RII: VERIFIED CORRECTION TO WORK ACCOMPLISHED IN C/A #3 AND C/A #5 FOR COMPLETION OF EA M-22-153-01550.;[07] RII INSPECTED AS REQUIRED.<BR>CORRECTIVE ACTIONS<BR>3&5;[08] THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550'.

Part: ANGLE — CORRODED (BS 727J-747) · airframe 26,036 hrs · 12,784 cycles

AFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN AND AROUND NUT PLATE HOLES AT BS 727J TO 747. REMOVED SURFACE CORROSION ON AFT CARGO RH TRANSITION ANGLE FROM STA 727J TO 747. REMAINING THICKNESS IS 0.032. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.

Part: ANGLE — CORRODED (BS 500B-500C) · airframe 26,036 hrs · 12,784 cycles

FWD CARGO STA 500B TO 500C AT TRANSITION ANGLE ON LEFT SIDE HAS CORROSION AROUND NUT PLATE HOLES.<[01] BLENDED AREAS; REMOVED .012' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00T572F FROM STA. 480 + 10 TO 500E + 10.;[02] RII - C/W INSPECTION. <BR>BLENDED AREAS; REMOVED .012' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00T572F FROM STA. 480 + 10 TO 500E + 10.

Part: ANGLE — CORRODED (BS 747-767) · airframe 26,036 hrs · 12,784 cycles

AFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN AND AROUND NUT PLATE HOLES AT BS 747 TO 767. REMOVED SURFACE CORROSION ON AFT CARGO RH TRANSITION ANGLE FROM STA 747 TO 767. REMAINING THICKNESS IS 0.035. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.

Part: WEDGE — DELAMINATED (RT NR 8 SLAT) · airframe 26,036 hrs · 12,784 cycles

#8 SLAT WEDGE UPPER O/B CORNER IS DELAMINATED.<[01] ACCOMPLISHED DAMAGE REMOVAL IAW SRM 51-70-10-2R-0; AND SRM 51-70-10-2R-4 REPAIR #4. OK TO INSTALL REPAIR PLIES.;[02] 02 - INSPECTED PER SRM 51-70-10-2R-0;[03] APPLIED REPAIR IAW SRM 51-70-10-2R-0; AND SRM 51-70-10-2R-4 REPAIR #4.;[04] 02 - INSPECTED PER [SRM 51-70-10-2R-4-B00746 (REPAIR 4 - REPAIRS TO LARGE DAMAGE - AIRFRAME - PERMANENT)];[05] REPAIRED DELAM AREA IAW SRM 51-70-10-2R-0; AND SRM 51-70-10-2R-4 REPAIR #4; RESTORED FINISH IAW AMM 51-21-99.;[06] INSPECTED WORK PERFORMED. REPAIRED DELAM AREA IAW SRM 51-70-10-2R-0; AND SRM 51-70-10-2R-4 REPAIR #4; RESTORED FINISH IAW AMM 51-21-99.

Part: ANGLE — CORRODED (BS 500D-500E) · airframe 26,036 hrs · 12,784 cycles

FWD CARGO STA 500D TO 500E AT TRANSITION ANGLE ON LEFT SIDE HAS CORROSION AROUND NUT PLATE HOLES.<[01] BLENDED AREAS; REMOVED .010' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00T572F FROM STA. 480 + 10 TO 500E + 10.;[02] RII - C/W INSPECTION.<BR>BLENDED AREAS; REMOVED .010' MATERIAL; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. THIS SECTION TO BE REPLACED ON NR# TTG8Q00T572F FROM STA. 480 + 10 TO 500E + 10.

Part: BUSHING — WORN (DOOR HANDLE) · airframe 26,036 hrs · 12,784 cycles

FWD SERVICE DOOR; INTERIOR DOOR HANDLE CAM BUSHINGS WORN<[01] FOUND HANDLE CAM ATTACHING HARDWARE LOOSE; SECURED HANDLE CAM ATTACHING HARDWARE PER M/M REF 52-41-11

Part: HANDLE — WORN (DOOR ASSIST) · airframe 26,036 hrs · 12,784 cycles

FWD SERVICE DOOR; DOOR ASSIST HANDLES WORN<[01] REMOVED AND REPLACED ASSIST HANDLES PER M/M REF 52-41-31;[02] VERIFIED REPLACEMENT OF ASSIST HANDLES PER MM 52-41-31

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,036 hrs · 12,784 cycles

CABIN EMERGENCY LIGHTS BATTERY PACK AT STA 727C L/H IS INOP<[01] REPLACED CABIN EMERGENCY LIGHT BATTERY PACK (M1670) AT STA 727C LH PER AMM 33-51-06. OPS CHECK GOOD;[02] VERIFIED. REPLACED CABIN EMERGENCY LIGHT BATTERY PACK (M1670) AT STA 727C LH PER AMM 33-51-06. OPS CHECK GOOD

Part: HANDLE — WORN (DOOR ASSIST) · airframe 26,036 hrs · 12,784 cycles

FWD ENTRY DOOR; DOOR ASSIST HANDLES WORN<[01] REMOVED AND REPLACED ASSIST HANDLES PER M/M REF 52-11-31;[02] VERIFIED REPLACEMENT OF ASSIST HANDLES PER M/M 52-11-31

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 26,009 hrs · 12,769 cycles

LH OVER WING AFT EMERGENCY LIGHT INOP<[01] RELAMPED LH OVER WING AFT EMERGENCY LIGHT REF AMM 33-51-04. OPS CHECK GOOD

Part: MEGAPHONE — MISSING (FWD CABIN) · airframe 25,789 hrs · 12,654 cycles

FWD MEGAPHONE MISSING<[01] INSTALLED FWD MEGAPHONE REF AMM 25-64-00

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,492 hrs · 12,505 cycles

AISLE EMERGENCY LIGHT ABOVE SEAT 21 FED INOP<[01] R&R EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06; OPS CHECK GOOD

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 25,300 hrs · 12,403 cycles

RIGHT WING O/B TE AFT FLAP LOWER SKIN IS DELAMINATED AT LOWER I/B CORNER MEASURING 10'X10'.<[01] C/W EA 24-127-00364 (COMPONENT - SWA - REPAIR - R/H O/B T/E AFT FLAP (PN: 113A3700-28; SN: 5952) LOWER SKIN DELAMINATION - TIME LIMITED) [TTG8Q00RF14V]

Part: CONTROLLER — MISSING (ZN 200 FUS TOP) · airframe 22,762 hrs · 10,937 cycles

OVERWING EXIT SIGN MISSING A COVER<[01] INSTALLED NEW COVER REF MM 33-51-03;[02] THIS WAS ENTERED ON WRONG A/C. DISCREPANCY WAS FOR A/C 8683. ITEM WAS CLOSED AND UNABLE TO CANCEL.

Part: FLASHLIGHT — FAILED (ZN 200 FUS TOP) · airframe 22,696 hrs · 10,895 cycles

CREW REPORTED AFT FA LEFT OUTBOARD FLASHLIGHT WILL NOT TEST<[01] OPS CHECK AFT FA LEFT OUTBOARD FLASHLIGHT. OPS CHECK GOOD REPLACED SEAL REF 25-64-00

Part: NONE — LOOSE (FWD SERVICE DOOR) · airframe 20,791 hrs · 9,806 cycles

FWD SERVICE DOOR HANDLE LOOSE / [01] RESECURED FWD GALLEY SERVICE DOOR HANDLE PER SIP

Part: LAMP — INOPERATIVE (PAX CABIN) · airframe 19,765 hrs · 9,211 cycles

EMERGENCY EXIT LIGHT AT AFT ENTRY CEILING (CENTER) HAS BULB OUT / [01] RE-LAMPED AND PERFORMED GOOD OPS TEST OF EMERGENCY EXIT LIGHT AT AFT ENTRY CEILING (CENTER) PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 19,765 hrs · 9,211 cycles

CRACKED FLOOR SUPPORT STA 540; BL0-RBL 25; WL 208. / [01] REMOVED FLOOR SUPPORT AT STA 540 BL0-RBL25 WL 208 IAW SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW FLOOR SUPPORT AT STA 540 BL0-RBL25 WL208 IAW SRM 51-40-05-0G-0. OK TO INSTALL.;[03] UPDATED MEASUREMENTS TABLE.;[04] VERIFIED CORRECTIVE ACTION 1-3 AND MEASUREMENT TABLE;[05] INSTALLED NEW FLOOR SUPPORT AT STA 540 BL0-RBL25 WL208 IAW SRM 51-40-02-0G-0.;[06] VERIFIED CORRECTIVE ACTION 5.;[07] JOB IS COMPLETE;[08] VERIFIED WORKSCOPE IS COMPLETE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 19,765 hrs · 9,211 cycles

CRACKED FLOOR SUPPORT STA 540; BL0-LBL 25; WL 208. / [01] REMOVED FLOOR SUPPORT AT STA 540 BL0 LBL25 WL 208 IAW SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW FLOOR SUPPORT AT STA 540 BL0-LBL25 WL 208 IAW SRM 51-40 -05-0G-0 . OK TO INSTALL.;[03] UPDATED MEASUREMENTS TABLE.;[04] VERIFIED CORRECTIVE ACTION 2; 3 AND MEASUREMENT TABLE;[05] INSTALLED NEW FLOOR SUPPORT AT STA 540 BL0-LBL25 WL 208 IAW SRM 51-40-02-0G-0.;[06] VERIFIED STEP 5.;[07] JOB IS COMPLETE.;[08] VERIFIED WORKSCOPE IS COMPLETE

Part: ANGLE — CORRODED (AFT CARGO) · airframe 19,765 hrs · 9,211 cycles

CORROSION ON AFT CARGO BAY INTERCOSTAL ANGLE BELOW SHIELD BS 767+5 RBL 22 WL 156<[01] EVALUATED CORROSION ON ANGLE BS 767+5 RBL 22 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION #1;[03] REMOVED ACB INTERCOSTAL ANGLE BELOW SHIELD BS 767-787; RBL 22; WL 156 IAW SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW AFT CARGO BAY INTERCOSTAL ANGLE BELOW SHIELD BS 767-787; RBL 22; WL 156 IAW SRM 51-40-05-0G-0 AND DWG 146A8123. INSTALLED NEW AFT CARGO BAY INTERCOSTAL ANGLE BELOW SHIELD BS 767-787; RBL 22; WL 156 IAW SRM 51-40-02-0G-0 AND DWG 146A8123.

Part: STRAP — CORRODED (AFT CARGO) · airframe 19,765 hrs · 9,211 cycles

CORROSION ON AFT CARGO BAY FLOOR STRAP BS 767+5 RBL 12 WL 156 / [01] EVALUATED CORROSION ON FLOOR STRAP BS 767+5 RBL 12 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION #1;[03] RECEIVED NEW AFT CARGO BAY FLOOR STRAP BS 767+5 RBL 12 WL 156 ON PO # 867103 INSTALL WELL BE ON CARD # TTG8Q00C7Z9K;[04] VERIFIED CORRECTIVE ACTION ENTRY 3.;[05] VERIFIED MEASUREMENTS

Part: SHIELD — CORRODED (AFT CARGO) · airframe 19,765 hrs · 9,211 cycles

CORROSION ON AFT CARGO BAY SHIELD BS 767+12 RBL 23 WL 156. EVALUATED CORROSION ON SHIELD BS 767+12 RBL 23 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM & REQUIRES REPLACEMENT IAW SRM 51-10-02-0G-0. REMOVED ACB SHIELD IAW SRM 51-40-02-0G-0. LOCATED & DRILLED NEW AFT CARGO BAY SHIELD IAW SRM 51-40-05-0G-0 & DWG 146A0081.

Part: PLATE — CORRODED (FWD CARGO) · airframe 19,765 hrs · 9,211 cycles

FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION BS 500A TO BS500I RBL23 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 500D+10 RBL 23 WL 156 IN NUMEROUS 1'X1' AREAS; FOUND 0.015 REMOVED FROM ORIG 0.040; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2678 DUE 04/2023;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. OUT OF LIMITS;[13] ' THE DAMAGE WAS REPAIRED PER 737-800 SRM 53-00-53-2R-5 (REPAIR 5) AND EA 22-153-01711'.;[14] VERIFIED CORRECTIVE ACTION ITEM 13; AND MEASUREMENT FIELDS; JOB COMPLETE

Part: STRAP — CORRODED (AFT CARGO) · airframe 19,765 hrs · 9,211 cycles

CORROSION ON AFT CARGO BAY FLOOR STRAP BS 887 RBL 6 WL 168 / [01] EVALUATED CORROSION ON FLOOR STRAP BS 887 RBL 6 WL 168; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION #1;[03] REMOVED ACB DAMAGED FLOOR STRAP BS 887; LOCATED AND DRILLED NEW FLOOR STRAP; IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0. AND OK TO INSTALL NEW FLOOR STRAP.;[04] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 3. OK TO INSTALL NEW ACB FLOOR STRAP GIVEN.;[05] INSTALLED ACB FLOOR STRAP; BS887; IAW SRM 51-40-02-0G-0; IPC 53-42-11-26.;[06] VERIFIED ORRECTIVE ACTION 5;[07] VERIFIED COMPLETE;[08] VERIFIED MEASURMENT TABLE;[09] CERTIFY

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 19,765 hrs · 9,211 cycles

CORROSION ON AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT BS 727F+16 TO BS 767 RBL 23 WL 156. REMOVED ACB FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0; SRM 53-00-53-2R-5. FABRICATED; LOCATED AND APPLIED CHEMICAL CONVERSION COATING TO ACB FLOOR TO SIDEWALL SUPPORT AND SPLICE REPAIR IAW SRM 51-40-05-0G AND DWG 146A7500; SRM 53-00-53-2R-5; AMM 51-21-41-370-802. APPLIED PRIMER TO SIDEWALL SUPPORT AND REPAIR PARTS PER AMM 51-21-72-370-804. APPLIED PRIMER TO ACB R/H FLOOR TO SIDEWALL SUPPORT AND REPAIR PARTS IAW AMM 51-21-72-370-804. INSTALLED ACB FLOOR TO SIDEWALL SUPPORT & SPLICE REPAIR IAW SRM 51-40-02-0G AND DWG 146A7500; SRM 53-00-53-2R-5.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 19,765 hrs · 9,211 cycles

CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT BS 727F+8 TO BS 847 LBL 23 WL 156 / [01] EVALUATED CORROSION AT ALL LOCATIONS OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 747+10 LBL 23 WL 156 IN NUMEROUS 1'X1' AREAS; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2678 DUE 04/2023;[02] VERIFIED CORRECTIVE ACTION #1;[03] REMOVED ACB LH FLOOR TO SIDEWALL SUPPORT BS 727+4 TO BS 847; LBL 23; WL 156 PER SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW ACB LH FLOOR TO SIDEWALL SUPPORT BS 727+4 TO BS 847; LBL 23; WL 156 PER DWG 146A7500 AND SRM 51-40-05-0G-0.;[05] VERIFIED CORRECTIVE ACTION ENTRY 4.;[06] OK TO INSTALL NEW ACB LH FLOOR TO SIDEWALL SUPPORT BS 727+4 TO BS 847; LBL 23; WL 156.;[07] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 6. OK TO INSTALL GIVEN.;[08] INSTALLED NEW ACB LH FLOOR TO SIDEWALL SUPPORT BS 727+4 TO BS 847; LBL 23; WL 156 PER DWG 146A7500 AND SRM 51-40-02-0G-0.;[09] VERIFIED CORRECTIVE ACTION 8;[10] VERIFIED ALL STEPS ACCOMPLISHED;[11] VERIFIED MEASUREMENT TABLE;[12] CERTIFY

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 19,765 hrs · 9,211 cycles

CORROSION ON AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT BS 727F+8 TO BS 847 LBL 23 WL 156 / [01] EVALUATED CORROSION AT ALL LOCATIONS OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE AT BS 747+10 LBL 23 WL 156 IN NUMEROUS 1'X1' AREAS; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2678 DUE 04/2023;[02] VERIFIED CORRECTIVE ACTION #1;[03] REMOVED ACB LH FLOOR TO SIDEWALL SUPPORT BS 727+4 TO BS 847; LBL 23; WL 156 PER SRM 51-40-02-0G-0.;[04] LOCATED AND DRILLED NEW ACB LH FLOOR TO SIDEWALL SUPPORT BS 727+4 TO BS 847; LBL 23; WL 156 PER DWG 146A7500 AND SRM 51-40-05-0G-0.;[05] VERIFIED CORRECTIVE ACTION ENTRY 4.;[06] OK TO INSTALL NEW ACB LH FLOOR TO SIDEWALL SUPPORT BS 727+4 TO BS 847; LBL 23; WL 156.;[07] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 6. OK TO INSTALL GIVEN.;[08] INSTALLED NEW ACB LH FLOOR TO SIDEWALL SUPPORT BS 727+4 TO BS 847; LBL 23; WL 156 PER DWG 146A7500 AND SRM 51-40-02-0G-0.;[09] VERIFIED CORRECTIVE ACTION 8;[10] VERIFIED ALL STEPS ACCOMPLISHED;[11] VERIFIED MEASUREMENT TABLE;[12] CERTIFY

Part: ATTACH ANGLE — CRACKED (CENTER WING) · airframe 19,765 hrs · 9,211 cycles

R/H BS663 UPPER ATTACH ANGLE IS CRACKED ON FWD SIDE OF VAPOR BARRIER RBL8 WL 167 / [01] VERIFIED APPLICABILITY OF SRM 57-10-10-2R-5 TO BE CORRECT AND UPDATED MEASUREMENT TABLE;[02] INSTALLED EWIS PROTECTION @ RH BS 663 UPPER ATTACH ANGLE RBL8- RBL20 WL167 ON FWD AND AFT SIDE OF VAPOR BARRIER IAW AMM 20-60-07-913-801.08] RECEIVED REPAIR PARTS; FILLER REPAIR ANGLE (1EA) RO. 871092-SWA MATERIAL USED 2024T42 CLAD LOT#14193330-1; DOUBLER SPLICE ANGLE (1EA) RO. 871093-SWA MATERIAL USED 2024T42 CLAD LOT#1398503-1. LOCATED;DRILLED AND APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON REPAIR PARTS AND REPAIR AREA; VERIFIED HEAT TREATMENT AND FABRICATION IAW BAC 5602;SRM 57-10-10-2R-5 AND DWG 111A1322.;[09] VERIFIED CORRECTIVED 8;[10] OK TO INSTALL;[11] OK TO INSTALL ANGLE.;[12] INSTALLED REPAIR PARTS; FILLER REPAIR ANGLE (1EA);DOUBLER SPLICE ANGLE (1EA) AT BS 663 RBL6-RBL23 IAW SRM 57-10-10-2R-5 PAR.4 L-N. BONDING TEST PASSED 0.53 MILLIOHMS TOOL USED E12275 DUE DATE 12/2022 IAW SWPM 20-20-00 PAR 15.;

Part: SUPPORT ANGLE — CORRODED (FWD CARGO) · airframe 19,765 hrs · 9,211 cycles

FWD CARGO BAY AFT LOWER BULKHEAD SUPPORT ANGLE HAS AREAS OF CORROSION BS500I RBL23 TO LBL23 WL156 / [01] EVALUATED CORROSION ON BULKHEAD SUPPORT ANGLE AT ALL LOCATIONS; FOUND THE DEEPEST LOCATION TO BE AT BS 500I RBL 23 WL 156 FOUND 0.021 REMOVED FROM ORIG 0.071 IN NUMEROUS 1'X1' AREAS; FOUND TO BE OUT OF LIMITS PER SRM 53-30-08-1A-1 USING DIAL DEPTH GAUGE ATS 2678 DUE 04/2023;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. OUT OF LIMITS;[03] REMOVED FWD CARGO BAY AFT LOWER BULKHEAD SUPPORT ANGLE BS 500I RBL23 TO LBL23 WL156 PER SRM 51-40-02-0G-0.;[04] LOCATED; DRILLED AND DEBURRED NEW BULKHEAD SUPPORT ANGLE BS 500I RBL23 TO LBL23 WL156 PER SRM 51-40-05-0G-0; AND DWG 143A7902.;[05] VERIFIED CORRECTIVE ACTION 4;[06] OK TO INSTALL;[07] OK TO INSTALL.;[08] UPDATED MEASUREMENT TABLE;[09] INSTALLED NEW FWD CARGO BAY AFT LOWER BULKHEAD SUPPORT ANGLE BS 500I RBL23 TO LBL23 WL156 IAW SRM 51-40-02-0G-0; AND DWG 143A7902.;[10] VERIFIED CORRECTIVE ACTION STEP 9.;[11] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.

Part: MEGAPHONE — INOPERATIVE (AFT GALLEY) · airframe 7,742 hrs · 17,096 cycles

MEGAPHONE LIGHT BLINKING/UNABLE TO SQUEEZE HANDLE TO TALK (AFT GALLEY) / R/R'D AFT MEGAPHONE OPS CK GOOD PER M/M 25-64-20

Part: BATTERY — FAILED (CABIN) · airframe 15,707 hrs · 7,023 cycles

ONE FLASHLIGHT UNDER FWD FA JUMPSEAT FLASHES RED WHEN TESTED OK TO CONT PER MEL 25-12-01 SP1B TK #106159 ( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ) / REMOVED AND REPLACED FWD FA'S FLASHLIGHT BATTERY IN REF TO AMM 25-64-00. FLASHLIGHT OC GOOD CLEARING #85488 TRACKING #106159

Part: SHUTTLE VALVE — FAULTY (RT MLG) · airframe 14,817 hrs · 6,575 cycles

WHEN TAXIING SLOWLY (1-2 KTS) AND TRYING TO STOP THE BRAKES 'RELEASE' SIMILAR TO ANTI-SKID CYCLING AND THE AIRCRAFT COASTS UNTIL YOU PRESS HARDER ON THE BRAKES. PERFORMED AACU BITE CHECK, PER AMM 32-42-00. FOUND FAULT A/B CONT. PERFORMED FIM TASK 32-42 TASK 807, FOUND AUTO BRAKE CONT MODULE OUT OF RESISTANCE RANGE. R & R AUTO BRAKE PRES CONT MODULE, PER AMM 32-42-81. OPERATIONS CHECK GOOD. WHILE PERFORMING T/S ALSO FOUND AUTO BRAKE SHUTTLE VALVE PRESS SWITCH BE 'STICKING' OPEN. R & R PRES ON SHUTTLE VALVE (RT), PER AMM 32-42-71 POS ONLY TAG 1020189 P/N OFF 78169-04 S/N OFF 1434A P/N ON 20102060-103S/N ON 2557.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 13,475 hrs · 5,898 cycles

RT HORIZ STAB FWD UPPER SLIDING SEAL CRACKED / R&R R/H HORIZONTAL STAB. FWD UPPER SLIDING SEAL REF AMM 53-31-31INSP P44

Part: FLASHLIGHT — INOPERATIVE (AFT GALLEY) · airframe 10,932 hrs · 4,747 cycles

AFT GALLEY FLASHLIGHT INOP. R & R FLASHLIGHT PER AMM.