N8547V

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 26,380 hrs · 13,321 cycles

EMERGENCY LIGHTS AT RH AFT OVERWING LOWER DOOR LIGHT; ROW17FED; 21FED, & 25FED DO NOT COME ON. REMOVED AND REPLACED IAW AMM 33-51-06-960-806-NG.

Part: HANDLE — LOOSE (ZONE 800) · airframe 26,379 hrs · 13,320 cycles

L2 DOOR ASSIST HANDLE NEEDS SECURING. SECURED L2 DOOR ASSIST HANDLE IAW AMM 52-13-31.

Part: HANDLE — LOOSE (ZONE 800) · airframe 26,379 hrs · 13,320 cycles

R1 DOOR ASSIST HANDLE NEEDS SECURING. SECURED R1 DOOR ASSIST HANDLE IAW 52-41-31-400-802, SUBTASK 52-41-31-020-008. VERIFIED SECURED R1 DOOR ASSIST HANDLE IAW 52-41-31-400-802, SUBTASK 52-41-31-020-008.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 23,863 hrs · 11,963 cycles

EMERGENCY LIGHT AFT AND L/H SIDE OUT<[01] REMOVED AND REPLACED UPPER AFT L/H BATTERY PACK ; OPS CHECK GOOD IAW AMM 33-51-06.

Part: LENS — MISSING (ZONE 200) · airframe 23,100 hrs · 11,551 cycles

CENTER EMER EXIT SIGN LENS MISSING<[01] INSTALLED MISSING LENS ON CENTER EMERGENCY EXIT SIGN PER AMM 33-51-01.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 21,658 hrs · 10,794 cycles

MID CABIN CEILING EMERGENCY EXIT LENSE MISSING. REPLACED OVERWING ?EMERGENCY EXIT? CEILING LENSE COVER AS PER AMM 33-51-01.

Part: SIGN — DISLODGED (EMERGENCY LIGHTS) · airframe 21,617 hrs · 10,774 cycles

OVERHEAD EMER SIGN CTR CABIN DISLODGED<[01] REINSTALLED EXIT SIGN IAW AMM 33-51-01

Part: COVER — BROKEN (ZN 200 FUS TOP) · airframe 21,028 hrs · 10,450 cycles

OVERHEAD EXIT SIGN MID CABIN (ROW15) BROKEN.<[01] INSTALLED LAMP COVER IAW AMM 33-51-01

Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 20,546 hrs · 10,188 cycles

ONE FWD FLASHLIGHT INOP<[01] REMOVED AND REPLACED BATTERIES IN FWD FLASHLIGHTS . BELOW F/A JUMP SEAT. I/A/W AMM 25-64-00. THIS CLEARS AUTHORIZATION #166032.

Part: COVER — MISSING (ZN 200 FUS TOP) · airframe 20,382 hrs · 10,089 cycles

OVERWING MISSING EXIT COVER<[01] INSTALLED MISSING EXIT COVER AS REQUIRED. WORK REF AMM 33-51-01

Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 20,034 hrs · 9,878 cycles

FLASHLIGHT IN FORWARD GALLEY INOP<[01] REPLACED FLASHLIGHT BATTERY IN FWD GALLEY. REF AMM 25-64-00.

Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 19,955 hrs · 9,833 cycles

SUPPLEMENTAL INFORMATION: 1 AFT EMERGENCY FLASHLIGHT INOP<[01] R AND R AT GALLEY EMERGENCY FLASHLIGHT LAW SIP

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 19,953 hrs · 9,831 cycles

CABIN EMERGENCY LIGHTS BATTERY PACK AT STA 500C+7 INOP<[01] REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERY PACK AT STATION 500C+7 PER AMM 33-51-06. OPERATIONAL CHECKS GOOD.;[02] INSPECTED A REQUIRED. CORRECTIVE ACTION #1

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 19,953 hrs · 9,831 cycles

FWD GALLEY EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT STA 310 AND STA 317 PER MM 33-51-06;[02] COMPLIED WITH INSPECTION; REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT STA 310 AND STA 317 PER MM 33-51-06;[03] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT STA 310 AND STA 317 PER MM 33-51-06.FWD GALLEY EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[04] C/W INSPECTION OF EMERGENCY EXIT LIGHT OPERATIONS PER AMM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 19,953 hrs · 9,831 cycles

EMERGENCY LIGHTS STA 952R AFT GALLEY BATTERY PACK INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT STA 952R PER MM 33-51-06;[02] C/W INSPECTION.;[03] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT STA 952R PER MM 33-51-06.AFT CABIN EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[04] C/W INSPECTION OF EMERGENCY EXIT LIGHT OPERATIONS PER AMM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 19,953 hrs · 9,831 cycles

EMERGENCY LIGHTS STA 727C L/H AFT CABIN BATTERY PACK INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT STA 727C L/H PER MM 33-51-06;[02] INSPECTED CA #1;[03] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT STA 727C L/H PER MM 33-51-06.CABIN EMERGENCY LIGHTS OPS CHECKED GOOD PER MM 33-51-06;[04] C/W INSPECTION OF EMERGENCY EXIT LIGHT OPERATIONS PER AMM 33-51-06.

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 19,953 hrs · 9,831 cycles

R/H HORIZONTAL STALIBIZER FWD UPPER SLIDING SEAL CRACKED AT AFT ATTACH POINT.<[01] SEAL REPLACED ON FAULT TTG8Q00MQEAH;[02] SEAL REPLACED ON FAULT TTG8Q00MQEAH

Part: BATTERY PACK — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 19,953 hrs · 9,831 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1694 MOUNT BRACKET IS MISSING THE AFT TWO BOLTS. M1694 IS LOCATED AT STATION 565 WL 213 LBL 68.<[01] INSTALLED THE M1694 STA 500C L/H EMERGENCY LIGHT POWER SUPPLY PER MM 33-51-06;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1

Part: PLATE — BROKEN (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

AFT CARGO FLOOR SPLICE PLATE AT 727I+6 BROKEN<[01] REMOVED AND REPLACED AFT CARGO FLOOR SPLICE PLATE ASSEMBLY AT STA. 727I+6' PER AMM 25-52-10.;[02] INSPECTION C/W REMOVED AND REPLACED AFT CARGO FLOOR SPLICE PLATE ASSEMBLY AT STA. 727I+6' PER AMM 25-52-10.

Part: ATTACH ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 19,953 hrs · 9,831 cycles

RT WING DEFLECTION CONTROL RIB TO UPPER T/E PANEL SUPPORT ANGLE ATTACH CLIP IS CRACKED.<[01] REMOVED DAMAGED CLIP FOR REPLACEMENT; LOCATED; AND DRILLED PER SRM 51-40-02 AND SRM 51-40-05.;[02] REMOVED AND REPLACED RT WING DEFLECTION CONTROL RIB TO UPPER T/E PANEL SUPPORT ANGLE ATTACH CLIP PER SRM 51-40-02.;[03] VERIFIED C/A #1 AND #2.

Part: SCUFF PLATE — DAMAGED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

AFT CARGO L/H FWD CORNER SCUFF PLATE IS BROKEN.PN-146A8341-9.<[01] REMOVED DAMAGED SCUFF PLATE PER AMM 53-11-02. SCUFF PLATE REPAIRED ON RO #P7564756. INSTALLED REPAIRED SCUFF PLATE PER AMM 53-11-02-420-801.;[02] VERIFIED C/A # ! : DAVID BELL (TECHNICIAN); 31-AUG-2023 21:58 UTC<BR>REMOVED DAMAGED SCUFF PLATE PER AMM 53-11-02. SCUFF PLATE REPAIRED ON RO #P7564756. INSTALLED REPAIRED SCUFF PLATE PER AMM 53-11-02-420-801.

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

AFT CARGO FLOOR ANGLE R/H UNDER TRANSITION ANGLE STA 767 HAS CORROSION AROUND HOLES.<[01] LOCATED AND DRILLED AFTE CARGO FLOOR ANGLE LOWER FASTERN HOLES IAW SRM 51-40-05.;[02] REMOVED AND REPLACED AFT CARGO FLOOR ANGLE R/H UNDER TRANSITION ANGLE STA 767- 787 PER SRM 51-40-02;[03] REMOVED CORROSION AFT CARGO FLOOR STRUCTURE R/H SHIELD SUPPORT ANGLE STA 767-787. ORIGINAL MATERIAL THICKNESS IS 0.050?; MATERIAL LOSS IS 0.009?; MAX ALLOWED IS 0.005?; REMAINING MATERIAL THICKNESS IS 0.041?. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2<BR>SEE CA #2 FOR REPLACEMENT;[04] INSPECTION C/W.

Part: SCUFF PLATE — DAMAGED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

AFT CARGO DOOR AFT CORNER SCUFF PLATE IS BROKEN.<[01] REMOVED AND REPLACED DAMAGED SCUFF PLATE PER AMM 53-11-02-420-801. OK TO INSTALL REPLACEMENT SCUFF PLATE WAS GIVEN ON FAULT #TTG8R007TZ9E; STEP 15.;[02] VERIFIED C/A # 1 : DAVID BELL (TECHNICIAN); 31-AUG-2023 21:05 UTC<BR>REMOVED AND REPLACED DAMAGED SCUFF PLATE PER AMM 53-11-02-420-801. OK TO INSTALL REPLACEMENT SCUFF PLATE WAS GIVEN ON FAULT #TTG8R007TZ9E; STEP 15.

Part: UNKNOWN — CORRODED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

FWD. CARGO BILGE; L/H T/A HAS LIGHT CORROSION FROM BS.500B-500C.<[01] BLENDED AND REMOVED CORROSION; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-1. .010' MATERIAL REMOVED.;[02] BLENDED AND REMOVED CORROSION; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. .010' MATERIAL REMOVED.;[03] FABRICATED REPAIR PARTS PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550.;[04] INSTALLED REPAIR PARTS PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550.;[05] C/W INSPECTION.;[06] RII; COMPLIED WITH INSPECTION FOR; INSTALLED REPAIR PARTS PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550.;[07] RII; COMPLIED WITH INSPECTION FOR; INSTALLED REPAIR PARTS PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550.

Part: STRUCTURE — CORRODED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

FWD. CARGO BILGE L/H T/A HAS LIGHT CORROSION FROM BS.500F-500G.

Part: STRUCTURE — CORRODED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

FWD. CARGO BILGE; L/H T/A HAS LIGHT CORROSION FROM BS.500C-500D.<[01] BLENDED AND REMOVED CORROSION; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-1. .010' MATERIAL REMOVED. THIS SECTION TO BE REPLACED ON NR# TTG8Q00MRD21.;[02] BLENDED AND REMOVED CORROSION; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. .010' MATERIAL REMOVED. THIS SECTION TO BE REPLACED ON NR# TTG8Q00MRD21.;[03] RII; COMPLIED WITH INSPECTION; BLENDED AND REMOVED CORROSION; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. .010' MATERIAL REMOVED. THIS SECTION TO BE REPLACED ON NR# TTG8Q00MRD21.

Part: SUPPORT BRACKET — DAMAGED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

BROKEN STRINGER CLIP SUPPORT BRACKET AT STA. 410 STRINGER 27L<[01] REPLACED WIRE SUPPORT ON STRINGER PER SWPM 20-10-12.;[02] C/W INSPECTION.

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

AFT CARGO FLOOR STRUCTURE R/H TRANSITION ANGLE STA 727C - 767 HAS CORROSION AROUND VARIOUS FASTENER HOLES. (MARKED)<[01] REMOVED LIGHT SURFACE CORROSION AT R/H TRANSITION ANGLE FROM STA. 727C-767 PER SRM 51-10-02; FOUND TO BE OUT OF LIMITS. MATERIAL REMOVED 0.007 AND REMAINING THICKNESS 0.033. PER SRM 53-00-53-1A-2.;[02] C/W INSP FOR CA 1;[03] REMOVED R/H TRANSITION ANGLE FROM STA. 727+4 TO 767 PER SRM 51-40-02;[04] DRILLED AND LOCATED R/H TRANSITION ANGLE FROM STA.727+4 TO 767 PER SRM 51-40-05.;[05] INSPECTED C/A 4. OK TO INSTALL R/H TRANSITION ANGLE FROM STA.727+4 TO 767;[06] INSTALLED R/H TRANSITION ANGLE FROM STA. 727+4 TO 767 PER SRM 51-40-02;[07] INSPECTED THE WORK ON C/A #6; NO DEFECTS NOTED.

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

AFT CARGO FLOOR STRUCTURE R/H TRANSITION ANGLE STA 767-787+6 HAS CORROSION AROUND VARIOUS FASTENER HOLES.<[01] REMOVED R/H AFT CARGO FLOOR STRUCTURE TRANSITION ANGLE FROM STA.767-787+6 PER SRM 51-40-02.;[02] REMOVED CORROSION AFT CARGO FLOOR STRUCTURE R/H SHIELD (TRANSITION ANGLE) STA 767-787+6 ORIGINAL MATERIAL THICKNESS IS 0.050?; MATERIAL LOSS IS 0.009?; MAX ALLOWED IS 0.005?; REMAINING MATERIAL THICKNESS IS 0.041?. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[03] REMOVED AND REPLACED AFT CARGO R/H SHIELD STA 767-787+6 PER SRM 51-40-02;[04] INSPECTION C/W.

Part: INTERCOSTAL — CORRODED (ZN 200 FUS TOP) · airframe 19,953 hrs · 9,831 cycles

PASSENGER CABIN FLOOR INTERCOSTAL CORRODED NEAR LAV MOUNT FITTING AT STA.947+2; LBL 50'. AREA MARKED.<[01] BLENDED CORROSION PER SRM 51-10-02. REMOVED .058' OF MATERIAL. REMAINING THICKNESS .092'. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] VERIFIED BLENDED CORROSION PER SRM 51-10-02. REMOVED .058' OF MATERIAL. REMAINING THICKNESS .092'. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1.;[03] REMOVED AND REPLACED INTERCOSTAL FROM STA. 947 TO STA. 967; LBL 50' PER SRM 51-40-02.;[04] INSTALLED 4EA. ADHESIVELY BONDED NUTPLATES ON INTERCOSTAL FROM STA. 947 TO STA. 967; LBL 50' PER SRM 51-40-10-2R-0. PUSH TEST -GOOD.;[05] RAJESH ALI (TECHNICIAN); 17-AUG-2023 10:20 UTC<BR>INSTALLED 4EA. ADHESIVELY BONDED NUTPLATES ON INTERCOSTAL FROM STA. 947 TO STA. 967; LBL 50' PER SRM 51-40-10-2R-0. PUSH TEST -GOOD.

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

WING CENTER SECTION FLOOR PANEL SUPPORT CRACKED AT STA 540 B.L 0 RIGHT 1.0<[01] REMOVED AND REPLACED PANEL BREAK PER SRM 51-40-02.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1;[03] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

WING CENTER SECTION FLOOR PANEL SUPPORT CRACKED AT STA 540 B.L.0 LEFT 1.0<[01] REMOVED AND REPLACED PANEL BREAK PER SRM 51-40-02.;[02] INSPECTED AS REQUIRED. CORRECTIVE ACTION #1

Part: INTERCOSTAL — CORRODED (ZN 200 FUS TOP) · airframe 19,953 hrs · 9,831 cycles

PASSENGER CABIN FLOOR INTERCOSTAL CORRODED NEAR LAV MOUNT FITTING AT STA.947+2; RBL 50'. REFERENCE TTG8Q00MPV7P FOR ORIGINAL DISCREPANCY.<[01] BLENDED CORROSION PER SRM 51-10-02. REMOVED .040 OF MATERIAL. REMAINING THICKNES IS .110'. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1;[02] VERIFIED BLENDED CORROSION PER SRM 51-10-02. REMOVED .040 OF MATERIAL. REMAINING THICKNES IS .110'. DAMAGE REMOVAL IS OUT OF LIMITS PER SRM 53-70-51-1A-1;[03] INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-40-02. INSTALLED 4 EA CLICK-BOND ADHESIVE NUT PLATES TO REPLACEMENT INTERCOSTAL ON 8/18/23 @ 1330 PER SRM 51-40-10.;[04] INSPECTED THE WORK PERFORMED ON C/A #3; NO DEFECTS NOTED.

Part: WEB — CORRODED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

AFT CARGO DOOR THRESHOLD WEB STA. 794-847 @ S-25R HAS CORROSION ON UPPER SURFACE.<[01] REMOVED AFT CARGO DOOR SILL WEB PER SRM 51-40-02;[02] DRILLED NEW AFT CARGO DOOR SILL WEB PER SRM 51-40-10;[03] INSTALLED NEW AFT CARGO DOOR LOWER SILL WEB PER SRM 51-40-02;[04] INSPECTION C/W.

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

AFT CARGO FLOOR STRUCTURE L/H TRANSITION ANGLE STA 727F-847 HAS CORROSION AROUND VARIOUS FASTENER HOLES. (MARKED)<[01] REMOVED LIGHT SURFACE CORROSION AT L/H TRANSITION ANGLE FROM STA. 727F-847 PER SRM 51-10-02; FOUND TO BE OUT OF LIMITS. MATERIAL REMOVED 0.010 AND REMAINING THICKNESS 0.030. PER SRM 53-00-53-1A-2.;[02] C/W INSP FOR CA 1;[03] REMOVED L/H TRANSITION ANGLE FROM STA. 727+4 TO 847 PER SRM 51-40-02.;[04] DRILLED AND LOCATED R/H TRANSITION ANGLE FROM STA.727+4 TO 847 PER SRM 51-40-05.;[05] DRILLED AND LOCATED L/H TRANSITION ANGLE FROM STA.727+4 TO 847 PER SRM 51-40-05.;[06] ITEM # 4 ENTERED IN ERROR.;[07] INSPECTED THE WORK PERFORMED ON C/A #3 AND #5; NO DEFECTS NOTED.;[08] OK TO INSTALL THE L/H TRANSITION ANGLE FROM STATION 727 +4' TO STATION 847.;[09] INSTALLED L/H TRANSITION ANGLE FROM STATION 727+4 TO STATION 847 PER SRM 51-40-02;[10] VERIFIED C/A # 9 : THINH PHAM (TECHNICIAN); 18-AUG-2023 06:38 UTC<BR>INSTALLED L/H TRANSITION ANGLE FROM STATION 727+4 TO STATION 847 PER SRM 51-40-02

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 19,953 hrs · 9,831 cycles

R/H HORIZONTAL STAB; UPPER FWD SLIDING SEAL CRACKED<[01] REMOVED AND REPLACED R/H HORIZONTAL STAB; UPPER FWD SLIDING SEAL PER AMM 53-31-31-000-802;[02] VERIFIED INSTALLATION OF R/H HORIZONTAL STAB; UPPER FWD SLIDING SEAL ONLY.;[03] R/R R/H STAB UPPER FWD SLIDING SEAL; OPS CHECK GOOD IAW AMM 53-31-31.;[04] COMPLIED WITH INSPECTION; R/R R/H STAB UPPER FWD SLIDING SEAL; OPS CHECK GOOD IAW AMM 53-31-31.

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 19,953 hrs · 9,831 cycles

FWD WET AREA; STA. 380-400 LBL 12; INTERCOSTAL CRACKED.<[01] REMOVED AND REPLACED INTERCOSTAL TOP L ANGLE (P/N 143A5410U174) AT STA 380 TO 400 LBL 12 IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZN 200 FUS TOP) · airframe 19,953 hrs · 9,831 cycles

PASSENGER CABIN FLOOR BEAM CORRODED AROUND AND UNDER LAV TIE DOWN FITTING BS947 LBL24.5.<OUT OF LIMITS PER SRM 53-70-51-1A-1;[03] CUT AND REMOVED DAMAGED FLANGES OF THE UPPER CHORD OF THE FLOOR BEAM AT STA. 947 FROM LBL 9' TO LBL 41.5' PER SRM 53-70-51-2R-5; ALTERNATIVE 2.;[04] INSPECTION C/W BUY BACK OF CUT FROM REMOVED DAMAGE FLAP PEENING OF THE CUT EDGES ON FLOOR BEAM PER SOPM 20-10-03. PRE DRILLED RIVET LAYOUT ON THE VERTICAL ANGLE OF T- CAP REPAIR PART AND PLUGGED RELOCATED BRACKET HOLE PER SRM 53-70-51-2R-5.;[08] FABRICATED REPAIR PARTS PER SRM 53-70-51-2R-5.;[09] FABRICATED REPAIR PARTS PER SRM 53-70-51-2R-5. (RII);[10] ALODINED AND PRIMED REPAIR AREA AND REPAIR PARTS IAW SRM 53-70-51-2R-5RELOCATED SUPPORT BRACKET ON THE REAR SIDE OF <BR>STA. 947; AT LBL 3.5' PER SRM 53-70-51-2R-5.;[13] INSPECTED C/A #12 RELOCATION OF SUPPORT BRACKET.INSTALLED REPAIR PARTS ON FLOORBEAM AT STA. 947 FROM LBL 15' TO LBL 47' PER SRM 53-70-51-2R-5; ALTERNATIVE 2.;[17] INSTALLED REPAIR PARTS ON FLOORBEAM AT STA. 947 FROM LBL 15' TO LBL 47' PER SRM 53-70-51-2R-5; ALTERNATIVE 2<BR>C/W INSPECTION INSTALLED REPAIR PARTS ON FLOORBEAM AT STA. 947 FROM LBL 2' TO LBL 15' PER SRM 53-70-51-2R-5; ALTERNATIVE 2. (RII);[21] RAJESH ALI (TECHNICIAN); 17-AUG-2023 09:42 UTC<BR>INSTALLED REPAIR PARTS ON FLOORBEAM AT STA. 947 FROM LBL 2' TO LBL 15' PER SRM 53-70-51-2R-5; ALTERNATIVE 2. (RII);[22] C/W;[23] VERIFIED ALL STEPS C/W

Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 19,953 hrs · 9,831 cycles

PASSENGER CABIN FLOOR Z' ANGLE @ R-2 DOOR AREA BS957-990 HAS SURFACE CORROSION IN AND AROUND N/P HOLES AND FASTENERS.<[01] REMOVED CORROSION PASSENGER CABIN FLOOR R-2 DOOR LWR MAIN SILL INNER CHORD (Z' ANGLE) AREA BS957-990 ORIGINAL MATERIAL THICKNESS IS 0.080? PER SRM 53-70-15-0I-1. MATERIAL LOSS IS 0.014?; MAX ALLOWED IS 0.008?; REMAINING THICKNESS IS 0.066?; FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1;[02] REMOVED R-2 DOOR LWR MAIN SILL INNER CHORD (Z ANGLE) PER SRM 51-40-02;[03] LOCATED AND DRILLED NEW R-2 DOOR LWR MAIN SILL INNER CHORD (Z' ANGLE) PER SRM 51-40-05;[04] INSPECTED C/A 3; OK TO INSTALL NEW R-2 DOOR LWR MAIN SILL INNER CHORD (Z' ANGLE);[05] INSTALLED MAJORITY OF RIVETS IN FLOOR 'Z' ANGLE PER SRM 51-40-02;[06] REMOVED AND REPLACED PASSENGER CABIN FLOOR 'Z ANGLE' AT R-2 DOOR AREA FROM STA. 887+7' TO STA. 1006; RBL 50' PER SRM 51-40-02. SEE INDIVIDUAL CORRECTIVE ACTIONS FOR WORK ACCOMPLISHED.;[07] C/W INSP. REMOVED AND REPLACED PASSENGER CABIN FLOOR 'Z ANGLE' AT R-2 DOOR AREA FROM STA. 887+7' TO STA. 1006; RBL 50' PER SRM 51-40-02. SEE INDIVIDUAL CORRECTIVE ACTIONS FOR WORK ACCOMPLISHED.

Part: MEGAPHONE — INOPERATIVE (ZN 200 FUS TOP) · airframe 18,341 hrs · 8,944 cycles

MEGA PHONE INOP<[01] R&R MEGA PHONE PER MM 25-64-00

Part: SIGN — DETACHED (CABIN) · airframe 17,969 hrs · 8,736 cycles

AFT FACING PIECE OF MID CABIN CEILING EXIT SIGN FELL OFF. REINSTALLED EXIT SIGN LENS PER AMM 33-51-01.

Part: SPLICE PLATE — MISSING (BS 792) · airframe 17,834 hrs · 8,662 cycles

AFT CARGO LEFT HAND CAP STRIP SPLICE PLATE(FORWARD OF STATION 792) MISSING. INSTALLED MISSING CAP STRIP SPLICE IN AFT CARGO LEFT HAND SIDE JUST FWD OF BS 792 IAW AMM 25-52-06 AND SRM 51-10-02.

Part: FLASHLIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 17,801 hrs · 8,640 cycles

FWD F/A FLASHLIGHT INOPERATIVE. REPLACED THE BATTERY & FLASHLIGHT AT FWD FA OTBD SEAT IAW AMM 25-64-00. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 17,801 hrs · 8,640 cycles

FWD F/A FLASHLIGHT INOPERATIVE. REPLACED THE BATTERY & FLASHLIGHT AT FWD FA OTBD SEAT IAW AMM 25-64-00. OPS CHECKED GOOD.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 17,801 hrs · 8,640 cycles

L1 DOOR SLIDE DISLODGED. REINSTALLED L1 DOOR SLIDE IAW AMM 25-66-01. AC OK FOR SERVICE.

Part: COVER — LOOSE (MID CABIN) · airframe 16,827 hrs · 8,070 cycles

MID-CABIN EXIT SIGN FASCIA LOOSE / [01] RE-INSTALLED LENS COVER PER S.I.P

Part: LENS — LOOSE (OVERWING) · airframe 15,974 hrs · 7,596 cycles

OVERWING EXIT CENTER CEILING OVERHEAD EXIT LIGHT ASSEMBLY-BOTH PLASTIC LENSES/COVERS HAVE FALLEN OUT. / [01] REINSTALLED BOTH LENSES/COVERS PER SIP.

Part: SIGN — FAILED (OVERWING EXIT) · airframe 15,867 hrs · 7,529 cycles

OVERWING EMERGENCY EXIT SIGN ON CEILING FELL OUT OVERWING EMERGENCY EXIT SIGN ON CEILING FELL OUT / [01] REPLACED EMERGENCY EXIT MARKER LENS ON CEILING MID CABIN REF AMM 33-51-01

Part: SIGN — OUT OF POSITION (PAX CABIN) · airframe 15,822 hrs · 7,501 cycles

MID CABIN OVERHEAD EXIT SIGN/PLACARD FELL OFF / [01] RESECURED OVERHEAD EXIT SIGN PER AMM 33-51-01. OK TO CONTINUE

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 15,658 hrs · 7,416 cycles

MID CABIN CEILING EXIT SIGN LENS FELL OFF / [01] INSTALLED FWD LENS ON MID CABIN EXILING EXIT SIGN IAW AMM 33-51-04

Part: NONE — FAILED (MID CABIN) · airframe 13,799 hrs · 6,388 cycles

THE FORWARD; PLASTIC COVER TO THE MID CABIN; CEILING EMERGENCY EXIT SIGN FELL OFF / RESECURED PLASTIC COVER PER SIP; NO DAMAGE FOUND

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 5,905 hrs · 12,853 cycles

LH AFT ENTRY EMER. SLIDE LIGHT INOP. / RELAMPED LH AFT ENTRY EMERGENCY SLIDE LIGHT IAW AMM 33-51-04.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 12,252 hrs · 5,577 cycles

EXIT SIGN IN AISLE FOR OVERWING EXIT FELL OFF / RESECURED CENTER AISLE EMERGENCY EXIT LENS COVER IAW AMM 33-51-03

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 12,083 hrs · 5,499 cycles

FWD CARGO PANEL 122ZFC HAS A 3' LONG CRACK 7' FROM FRONT EDGE OF PANELPERFORMED INTERIM REPAIR ON PANEL 122ZFC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPENT PANEL.REPETITIVE ACTION REQUIRED /

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 12,038 hrs · 5,477 cycles

FWD CARGO PANEL 122ZFC HAS A 3' LONG CRACK 7' FROM FRONT EDGE OF PANELPERFORMED INTERIM REPAIR ON PANEL 122ZFC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPENT PANEL.REPETITIVE ACTION REQUIRED /

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 12,038 hrs · 5,477 cycles

FWD CARGO PANEL 122ZFC HAS A 3' LONG CRACK 7' FROM FRONT EDGE OF PANELPERFORMED INTERIM REPAIR ON PANEL 122ZFC PER EA 1-A25-3722 REV 4. EVERY 8 DAYS PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. WITHIN 730 DAYS ACCOMPLISH A PERMANENT REPAIR OR R&R THE DISCREPENT PANEL.REPETITIVE ACTION REQUIRED /

Part: BATTERY — INOPERATIVE (FWD FLASHLIGHT) · airframe 11,937 hrs · 5,430 cycles

FWD EMERGENCY FLASHLIGHT BLINKS RED / R&R'D BATTERY IN REF TO A.M.M. TASK 25-64-00

Part: BATTERY — FAULTED (AFT FLASHLIGHT) · airframe 11,245 hrs · 5,079 cycles

NEED FLASHLIGHT REPLACED IN CABIN . R & R AFT INBOARD FLASHLIGHT BATTERY, IAW MM 25-64-00.

Part: FAIRING — CRACKED (NR 1 PYLON) · airframe 10,715 hrs · 4,796 cycles

#1 ENG PYLON AFT STRUT FAIRING (ZONE 434) AFT FITTING O/B AREA CRACKED THROUGH RADIUS - AS MARKED REMOVED AND REPLACED #1 ENG AFT STRUT FAIRING IAW AMM 54-52-04. REF OTHER-54EA-07715 #1 ENGINE PYLON AFT PYLON FAIRING ALTERNATE PART. THIS EC/TC ACCOMPLISHES THE INSTALLATION OF P/N 313A2060-957 AS A TIME LIMITED REPAIR FOR 365 DAYS. REMOVE AND REPLACE THE #1 ENGINE PYLON AFT FAIRING P/N 313A2060-957 W/ P/N 313A2060-73 (47962/68445)#1 ENG PN OFF:313A2060-73 PN ON: 313A2060-957PERMANENT ACTION REQUIREDREMOVE AND REPLACE THE #1 ENGINE PYLON AFT FAIRING P/N 313A2060-957 WITH P/N 313A2060-73 / (RESOLVED ON W/O: 708169 TASKCARD: N/R-00003 ) REMOVED #1 AFT PYLON FAIRING P/N P/N 313A2060-957; S/N 157709001INSTALLED AFT PYLON FAIRING P/N 313A2060-73; S/N NSN001. ALL WORK DONE IAW AMM 54-52-04TSR #20200014907 FOR EFFECTIVITY

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,489 hrs · 4,178 cycles

LEFT AFT OVERHEAD EMERGENCY EXIT LIGHT INOP / R&R LEFT AFT OVERHEAD ENERGENCY EXIT LIGHT IAW AMM 33-21-00. OPS CHECK GOOD.

Part: LENS — DETACHED (EXIT SIGN) · airframe 8,564 hrs · 3,743 cycles

MID CABIN OVERHEAD EMERGENCY EXIT SIGNS OUTER LENS DETACHED. INSTALLED LENS IAW SIP.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 8,459 hrs · 3,697 cycles

OVERWING EMERGENCY EXIT SIGN LENS CAME OFF. / SECURED LENS PER SIP.

Part: FLASHLIGHT — OUT OF ADJUST (CABIN) · airframe 3,248 hrs · 1,419 cycles

AFT EMERGENCY FLASHLIGHT FAILED TO TEST. ADJUSTED FLASHLIGHT PER MM.