N8509U
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
FWD L1 ENTRY DOOR EMERGENCY EXIT SLIDE NOT SECURE. RESECURED L1 FWD ENTRY DOOR SLIDE IAW AMM 25-66-01.
FORWARD ENTRY DOOR GIRT BAR REQUIRES ADJUSTMENT. BAR COMES OUT OF ITS HOLDER. REMOVED & INSTALLED THE GIRT BAR IAW AMM 25-66-02. FOUND RETENTION TO BE SATISFACTORY.
NOSE RADOME BOOT CRACKED. REPLACED NOSE RADOME BOOT IAW AMM 53-52-00.
LEFT WING LEADING EDGE; NR 3 SLAT TAI DUCT, OTBD SUPPORT STRUCTURE IS CORRODED. WING STATION OFSS 418. REPLACED TAI SUPPORT ASSY PER SRM 51-10-02.;[02] C/W INSPECTION AS REQUIRED
OVERWING FORWARD L/H AND R/H EMERGENCY ESCAPE HATCH LIGHTS INOPERATIVE. REMOVED AND REPLACED THE EMERGANCY LIGHT BATTERY PACK ON THE LT SIDE. OPS CHECKED GOOD IAW AMM 33-51-06.
AFT CARGO LEFT FLOOR TRANSITION ANGLE FROM BS 727I TO 787, DISBONDED NUTPLATES (QTY.10).<[01] INSTALLED BONDED NUTPLATES (QTY.10) ON AFT CARGO L/H FLOOR TRANSITION ANGLE FROM STA 727I TO STA 787 PER SRM 51-41-10.
AFT CARGO RT FLOOR TRANSITION ANGLE FROM STA 727J TO STA 767 DISBONDED NUTPLATES (QTY.6). INSTALLED BONDED NUTPLATES (QTY.6) ON AFT CARGO R/H FLOOR TRANSITION ANGLE FROM STA 727J TO STA 767 PER SRM 51-41-10.
#1 ENGINE I/B FAN COWL OIL ACCESS DOOR 414AR INNER SUPPORT ANGLE CRACKED. REMOVED AND REPLACED INNER SUPPORT ANGLE PER SRM 51-40-02.
SEAT TRACK NR 1 ATTACH ANGLE CRACKED ON INBD SIDE OF SEAT TRACK IN RADIUS AT BS 727B UNDER FLOORBOARD 241EF. REMOVED DAMAGED SPLICE STRAP AT BS 727B; LBL 45.5 PER SRM 51-40-02. LOCATED AND DRILLED NEW PART IAW SRM 51-40-05 AND INSTALLED NEW PART IAW SRM 51-40-02.
RIGHT VAPOR BARRIER ATTACH ANGLE BS 663 CRACKED AT FASTENER RBL 31. REMOVED DAMAGED SECTION OF RH STA 663 VAPOR BARRIER ATTACH ANGLE FROM RBL 31 TO RBL 65 PER SRM 57-10-10-2R-5;[02] RII. VERIFIED. REMOVED DAMAGED SECTION OF RH STA 663 VAPOR BARRIER ATTACH ANGLE FROM RBL 31 TO RBL 65 PER SRM 57-10-10-2R-5. FABRICATED, LOCATED, DRILLED, AND DEBURRED REPAIR ANGLE IAW SRM 57-10-10-2R-5.
SEAT TRACK NR 4 ATTACH BRACKET CRACKED AT BS 727B UNDER FLOORBOARD 242DF. REMOVED DAMAGED SPLICE STRAP AT BS 727B; RBL 45.5 IAW SRM 51-40-02. LOCATED AND DRILLED NEW PART IAW SRM 51-40-05.
FLASHLIGHT FWD FLIGHT ATTENDANT JUMP SEAT INOP. CHECKED BOTH FWD FLIGHT ATTENDANT SEAT FLASHLIGHTS; BOTH OPS CHECK GOOD. REINSTALLED IAW SIP.
2 AFT STATION EMERGENCY FLASHLIGHTS INOP. RESTEATED FLASHLIGHTS OPS CHECK GOOD ER AMM 25-64-00 MEL CLEARED.
FWD GALLEY EMERGENCY LIGHT BATTERY PACK CHARGER (M02816) OVERHEATING/SMOKING<[01] REMOVED AND REPLACED M02816 POWER SUPPLY CHARGER AND BATTERY PACK. DEEP CYCLE CHARGE AND EMERGENCY LIGHT OPS CHECK GOOD. REF: AMM 33-51-06
AFTER LANDING ATC REPORTED POSSIBLE SMOKE FROM LEFT MAIN LANDING GEAR. ARFF CAME TO THE A/C AND AFTER 10 MINUTES CLEARED US TO PARK AT THE GATE.MECHANIC ON SITE SUSPECTS DE-ICING FLUID IN THE BRAKES CAUSED THE SMOKE<[01] INSPECTED #1 BRAKE PER AMM 32-41-41. SUSPECT DEICING FLUID ON BRAKE CAUSED TEMPORARY SMOKE. COMPLIED WITH MPM 53.5.2 ALTERNATE BRAKE TEMP READING WERE NORMAL. ALSO ACCOMPLISHED TIRE PRESSURE CK PER AMM 12-15-51 ON #1 TIRE WAS NORMAL. NO FURTHER ACTION REQUIRED AT THIS TIME.
LIGHTBULB IN AFT SEATBELT SIGN NOT WORKING.<[01] RELAMPED IAW AMM 33-51-14.
EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK M2816 ARE INOP.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] 01 - REMOVED AND REPLACED BATTERY PACK; OP CK GOOD PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[03] INSPECTION COMPLETE ON CORRECTIVE ACTION #2 FOR REPLACEMENT OF BATTERY PACK AND SATISFACTORY OPS CHECK.
EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK M2335 ARE INOP.<[01] 01 - REMOVED AND REPLACED BATTERY PACK; OP CK GOOD PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR REPLACEMENT OF BATTERY PACK AND SATISFACTORY OPS CHECK.
EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK M1695 ARE INOP.<[01] 01 - REMOVED AND REPLACED BATTERY PACK; OP CK GOOD PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR REPLACEMENT OF BATTERY PACK AND SATISFACTORY OPS CHECK.
EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK M1671 ARE INOP.<[01] 01 - REMOVED AND REPLACED BATTERY PACK; OP CK GOOD PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR REPLACEMENT OF BATTERY PACK AND SATISFACTORY OPS CHECK.
EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK M1672 ARE INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK M1672 IAW AMM 33-51-06. OPS CHECK GOOD.;[02] INSPECTION C/W
EMERGENCY LIGHTS CONTROLLED BY BATTERY PACK M1670 ARE INOP.<[01] 01 - REMOVED AND REPLACED BATTERY PACK; OP CK GOOD PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR REPLACEMENT OF BATTERY PACK AND SATISFACTORY OPS CHECK.
FLOOR PANEL HOLE AT STA 947 LBL 4.5 & LBK 12 ON THE AFT FLANGE OF THE T REQUIRE RELOCATION DUE TO BEING IN THE RADIUS<[01] REPAIRED PANEL FASTENER HOLE AND INSTALLED INSERTS PER SRM 53-00?50-2R-1.;[02] REPAIRED PANEL FASTENER HOLE PER EA 24-153-03056-WIP2.;[03] VERIFIED WORK ACCOMPLISHED ON C/A #1 & C/A #2; REPAIRED PANEL FASTENER HOLE AND INSTALLED INSERTS PER SRM 53-00?50-2R-1 & REPAIRED PANEL FASTENER HOLE PER EA 24-153-03056-WIP2 (RII);[04] VERIFIED WORK ACCOMPLISHED ON C/A #1 & C/A #2; REPAIRED PANEL FASTENER HOLE AND INSTALLED INSERTS PER SRM 53-00?50-2R-1 & REPAIRED PANEL FASTENER HOLE PER EA 24-153-03056-WIP2 (RII) AND TTG8Q00X04HQ. SEE INDIVIDUAL SIGHN-OFFS FOR WORK ACCOMPLISHED.;[05] C/W INSP. FLOOR PANEL HOLE AT STA 947 LBL 4.5 & LBK 12 ON THE AFT FLANGE OF THE T REQUIRE RELOCATION DUE TO BEING IN THE RADIUS; VERIFIED WORK ACCOMPLISHED ON C/A #1 & C/A #2; REPAIRED PANEL FASTENER HOLE AND INSTALLED INSERTS PER SRM 53-00?50-2R-1 & REPAIRED PANEL FASTENER HOLE PER EA 24-153-03056-WIP2 (RII) AND TTG8Q00X04HQ. SEE INDIVIDUAL SIGHN-OFFS FOR WORK ACCOMPLISHED.
IN THE AFT CARGO BAY RIGHT HAND SIDE AFT OF THE DOOR; THE SHIELD ASSEMBLY FWD INBD SUPPORT/MOUNT ANGLE HAS AN ELONGATED HOLE WITH AN INDICATION OF A CRACK.<[01] REMOVED AFT CARGO BAY RIGHT HAND SIDE AFT OF THE DOOR; THE SHIELD ASSEMBLY SUPPORT ANGLE( P/N 146A8125-51) PER SRM 51-40-02.;[02] REFERENCE WORK PACKAGE LINE NUMBER 1492 ( TTG8Q00WJMPA ) FOR INSTALLATION AND PART REQUIREMENTS OF AFT CARGO; AFT SHIELD SUPPORT/MOUNT ANGLE AT STATION 847+6;[03] INSPECTION C/W
PASSENGER CABIN; FLOOR PANEL INTERCOSTAL (BREAK ASSY.)CRACKED AT STA.540 BL-0 TO RBL24<[01] REMOVED AND REPLACED R/H INTERCOSTAL PER SRM 51-40-02;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR INTERCOSTAL REPLACEMENT.
PASSENGER CABIN; FLOOR PANEL INTERCOSTAL (BREAK ASSY.) CRACKED AT STA.540 BL-0 TO LBL24<[01] REMOVED AND REPLACED L/H INTERCOSTAL PER SRM 51-40-02;[02] INSPECTION COMPLETE ON CORRECTIVE ACTION #1 FOR INTERCOSTAL REPLACEMENT.
CORROSION ON FLOOR INTERCOSTAL AT B/S 947 LBL51<[01] FOUND INTERCOSTAL TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. INTERCOSTAL TO BE REMOVED AND REPLACED ON [TTG8Q00WJ9TR].;[02] FOUND INTERCOSTAL TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. INTERCOSTAL TO BE REMOVED AND REPLACED ON [TTG8Q00WJ9TR].
FORWARD PASSENGER COMPARTMENT FLOOR STRUCTURE WET AREA UNDER FWD ENTRY DOOR THRESHOLD HAS MULTIPLE LARGE AREAS OF CORROSION ON CREASE BEAM. (MARKED)<[01] REMOVED CORROSION IAW SRM 51-10-02. CORROSION REMOVAL OUT OF ALLOWABLE LIMITS PER SRM 53-10-15-IA-1.;[02] REMOVED DAMAGED CREASE BEAM Z ANGLE IAW SRM 51-40-02.;[03] WORK ENTRY #2 ENTER IN ERROR. REMOVED DAMAGED CREASE BEAM ?L? ANGLE IAW SRM 51-40-02.;[04] LOCATED AND DRILLED CREASE BEAM ?L? ANGLE IAW SRM 51-40-02. OK TO INSTALL 'L' ANGLE.;[05] VERIFIED LOCATED AND DRILLED CREASE BEAM ?L? ANGLE IAW SRM 51-40-02. OK TO INSTALL 'L' ANGLE.;[06] REMOVED AND REPLACED CREASE BEAM ?L? ANGLE IAW SRM 51-40-02.
IN THE AFT CARGO BAY RIGHT HAND SIDED AFT OF THE DOOR; THE SHIELD ASSEMBLY FWD INBD SUPPORT/MOUNT ANGLE HAS AN ELONGATED HOLE. STATION 847+6 RBL15.<[01] LOCATED AND DRILLED SERVICEABLE ANGLE ASSEMBLY ( SHIELD ASSY. SUPPORT ) FOR THE AFT CARGO BAY DOOR SHIP AT STATION 847+6 IN REFERENCE TO SRM 51-40-05;[02] REMOVAL WAS ACCOMPLISHED ON CARD #TTG8Q00WTGVW;[03] VERIFIED LOCATED AND DRILLED PART; OK TO INSTALL REPAIR PART.;[04] REMOVED AND REPLACED AFT CARGO BAY AFT RIGHT SHIELD ASSEMBLY MOUNT/SUPPORT ANGLE IN REFERENCE TO SRM 51-40-02. SEE BARCODE TTG8Q00WTGVW FOR MOUNT/SUPPORT REMOVAL; SEE BARCODE TTG8Q00WTFXX FOR EA 24-153-03016-WIP1;[05] REMOVED AND REPLACED AFT CARGO BAY AFT RIGHT SHIELD ASSEMBLY MOUNT/SUPPORT ANGLE AT STATION 847+6 RBL15 IN REFERENCE TO SRM 51-40-02. SEE BARCODE TTG8Q00WTGVW FOR MOUNT/SUPPORT REMOVAL; SEE BARCODE TTG8Q00WTFXX FOR EA 24-153-03016-WIP1;[06] INSPECTION C/W CA #5;[07] PARTS UPDATE ONLY
'PASSENGER AREA STA947 LBL 24 INTERCOSTAL TOP SURFACE HAS CORROSION.<[01] FOUND INTERCOSTAL TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. INTERCOSTAL TO BE REMOVED AND REPLACED ON [TTG8Q00WJ9TR].
PASSENGER AREA STA 947; LBL 24 UNDER AFT LAV MOUNT HAS EVIDENT OF CORROSION.<[01] FOUND INTERCOSTAL TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. INTERCOSTAL TO BE REMOVED AND REPLACED ON [TTG8Q00WJ9TR].
PASSENGER AREA STA 949; LBL50 FLOOR SUPPORT UNDER LAV MOUNT HAS CORROSION .<[01] FOUND INTERCOSTAL TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. INTERCOSTAL TO BE REMOVED AND REPLACED ON [TTG8Q00WJ9TR].
SURFACE CORROSION FOUND ON CREASE BEAM ANGLE IN FWD PASSENGER CABIN FLOOR STRUCTURE WET AREA ON LEFT SIDE NEAR L1 ENTRY THRESHOLD; AT STA 294.5 +8'. (MARKED)<[01] REMOVED AND REPLACED CREASE BEAM ANGLE IN FWD PASSENGER CABIN FLOOR STRUCTURE WET AREA ON LEFT SIDE NEAR L1 ENTRY THRESHOLD; AT STA 294.5 +8' PER SRM 51-40-02. SEE TASK CARD TTG8Q00WJSU6 FOR ALL WORK ACCOMPLISHED.
.PASSENGER AREA STA 947;LBL16 FLOOR BEAM TOP CAP HAS CORROSION..<[01] CORROSION FOUND OUT OF LIMITS PER SRM 53-70-15-1A-1. REMOVED DAMAGED SECTION OF FLOOR BEAM TOP CAP PER SRM 53-70-51-2R-5;[02] FLAP PEENED THE CUT EDGES PER SRM 53-70-51-2R-5 LOCATED; DRILLED; DEBURED; TREATED AND PRIMED REPAIR PARTS; T-CHORD [1]; 2EA REPAIR ANGLES [2] AND 2EA REPAIR STRAPS [3]. ALL WORK DONE IAW SRM 53-70-51-2R-5.FABRICATED 3EA [4] FILLERS PER SRM 53-70-51-2R-5 AND TTG8Q00WV4YT<BR><BR>OK TO INSTALL.;[08] 7. TROY ROSSMAN (TECHNICIAN); 06-NOV-2024 16:25 UTC<BR>FABRICATED 3EA [4] FILLERS PER SRM 53-70-51-2R-5 AND TTG8Q00WV4YT TRIMMED FWD EDGE OF INTERCOSTAL AT STA. 947.5; LBL 24. FLAP PEENED TRIMMED EDGE; ALODINED AND PRIMED TRIMMED EDGE ALL IAW SRM 53-70-51-2R-5 REPAIR 5 INSTALLED FLOOR BEAM REPAIR SPLICE PER SRM 53-70-51-2R-5.;[12] 11. TROY ROSSMAN (TECHNICIAN); 08-NOV-2024 15:39 UTC<BR>INSTALLED FLOOR BEAM REPAIR SPLICE PER SRM 53-70-51-2R-5. RII;[13] INSTALLED REPAIR T- CAP PER SRM 53-70-51-2R-5.;[14] INSPECTED INSTALLATION OF REPAIR T- CAP PER SRM 53-70-51-2R-5. RII;[15] INSPECTED INSTALLED CABLE GUARD SUPPORT CLIP AT BS 947; LBL 3;[16] INSPECTED INSTALLED 2 ANGLE CLIPS AND SPACER TO COMPLETE INSTALLATION OF INTER COASTAL AT B/S 947-967 LBL-24.;[17] REPAIRED PER SRM 53-70-51-2R-5;[18] ALL INSP STEPS COMPLETE. SEE ABOVE CA FOR WORKED PERFORMED AND SIGNED FOR.;[19] ALL INSP RII STEPS COMPLETE. SEE ABOVE CA FOR WORKED PERFORMED AND SIGNED FOR
PASSSENGER AREA STA 984 ; LBL47 CREASE BEAM HAS CORROSION ON VERTICAL SURFACE .<[01] CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1. <BR><BR>Z ANGLE REMOVED PER SRM 51-40-02; FOR REPLACEMENT.;[02] VERIFIED OUT OF LIMITS CORROSION ON Z ANGLE PER SRM 53-70-15-1A-1.;[03] LOCATED AND DRILLED NEW Z ANGLE PER SRM 51-40-02>;[04] VERIFIED WORK SIGNED IN CA# 3 .......LOCATED AND DRILLED NEW Z ANGLE PER SRM 51-40-02 RII;[05] REMOVED FASTENERS AND HI-LOCKS IN MIDDLE OF DOOR THRESHOLD AND JUST FORWARD OF THRESHOLD IAW SRM 51-40-02 STILL REQUIRES MORE REMOVAL OF FASTENERS AND HI-LOCKS FOR THRESHOLD REMOVAL. THIS SHOULD BE STEP 3 AND TROY ROSSMAN SIGN OFF FOR LINE 4. ORIGINAL WRITE UP WAS SIGNED OFF ON WRONG CARD PER SAM T. 98405.;[06] OK TO INSTALL.;[07] 6. TROY ROSSMAN (TECHNICIAN); 08-NOV-2024 15:22 UTC<BR>OK TO INSTALL. CREASE BEAM (Z-ANGLE);[08] OK TO INSTALL CREASE BEAM ( Z- ANGLE);[09] 8. TROY ROSSMAN (TECHNICIAN); 08-NOV-2024 17:02 UTC<BR>OK TO INSTALL CREASE BEAM ( Z- ANGLE) INSPECTED.;[10] INSTALLED ALL FASTENERS COMMON TO HORIZONTAL FLANGE OF NEW CREASE BEAM ( Z-ANGLE) PER SRM 51-40-02.;[11] INSPECTED INSTALLED ALL FASTENERS COMMON TO HORIZONTAL FLANGE OF NEW CREASE BEAM ( Z-ANGLE) PER SRM 51-40-02. RII;[12] C/W INSPECTION;[13] C/W RII INSPECTION;[14] VERIFIED REPAIR AT 984; LBL 47 (Z-ANGLE) CREASE BEAM REPLACEMENT PER SRM 51-40-02.;[15] VERIFIED REPAIR AT 984; LBL 47 (Z-ANGLE) CREASE BEAM REPLACEMENT PER SRM 51-40-02. C/W RII INSPECTION.
AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.767-787. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR;[04] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR;[05] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR
AFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727F+20.MRKD<[01] WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT;[02] VERIFIED: WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT
AFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.747-767. MRKD<[01] WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT;[02] VERIFIED: WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT
AFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727J +2+2.5+6.5+10.5+12+14.5+18.5. MRKD<[01] WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT;[02] VERIFIED: WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT
AFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727I +8+10.5+14.5+16+18.5. MRKD<[01] WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT;[02] VERIFIED: WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT
AFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727H +6+9+13+16. MRKD<[01] WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT;[02] VERIFIED: WORK PERFORMED AND FINAL SIGN OFF ON TTG8Q00WHFVT
AFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLE STA.727E+20.MRKD<[01] REMOVED R/H TRANSITION ANGLE STA 727-767. IAW SRM 51-40-02.;[02] LOCATED AND DRILLED NEW TRANSITION ANGLE STA 727-767 IAW SRM 51-40-02.;[03] VERIFIED WORK PERFORMED ON CORRECTIVE ACTION #2;[04] R/R R/H TRANSITION ANGLE FROM STA 727 - STA 767 PER SRM 53-00-53-2R-5 AND SRM 51-40-02;[05] INSPECTED WORK PERFORMED IN C/A #4
AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.787-807. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON CARD TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR;[04] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR
AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.747-767. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR
AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727J +6+10=14.5. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR
AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727I +3+8+10.5+14.5+18.5. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR
FWD CARGO; AFT BULKHEAD TO FLOOR CORD HAS CORROSION BS 500I LBL 16<[01] BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMIT PER SRM 53-30-08-1A-1.;[02] REMOVED FWD CARGO; AFT BULKHEAD TO FLOOR CORD PER SRM 51-40-02.;[03] DRILLED NEW FWD CARGO; AFT BULKHEAD TO FLOOR CORD PER SRM 51-40-05.;[04] INSTALLED FWD CARGO; AFT BULKHEAD TO FLOOR CORD PER SRM 51-40-02.;[05] VERIFIED WORK PERFORMED.
FWD CARGO L/H TRANSITION ANGLE HAS CORROSION AT NUMERUS NUT PLATE HOLES BS 500A - 500H (SEE ATTACHED PICS)<[01] BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-2.;[02] REMOVED FWD CARGO L/H TRANSITION ANGLE BETWEEN STA 500-500I PER SRM 51-40-02.;[03] REMOVED AND REPLACED FWD CARGO L/H TRANSITION ANGLE FROM STA.492-500I PER SRM 51-40-02;[04] VERIFIED WORK SIGNED IN CA# 3 ........REMOVED AND REPLACED FWD CARGO L/H TRANSITION ANGLE FROM STA.492-500I PER SRM 51-40-02
AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLE STA.727F+16. MRKD<[01] UPDATED CORRODED ELEMENT PART NUMBER;[02] COMPLETED ON TTG8Q00WHFNR;[03] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR;[04] COMPLETE TRANSITION ANGLE WAS CHANGED ALL WORK ACCOMPLISHED WAS COMPLETED ON CARD TTG8Q00WHFNR
AFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES ON UNDERSIDE STA.767-794. MRKD<[01] BLENDED CORROSION AND FOUND TO BE OUT OF LIMIT IN REFERENCE TO SRM 53-00-53.;[02] REMOVED AFT CARGO R/H TRANSITION ANGLE STA.767-794 PER SRM 51-40-02.;[03] DRILLED NEW AFT CARGO R/H TRANSITION ANGLE STA.767 TO STA.794 PER SRM 51-40-05.;[04] INSPECTION C/W FOR CA 1;2; AND 3.<BR>OK TO INSTALL NEW PART.;[05] INSTALLED NEW AFT CARGO R/H TRANSITION ANGLE STA.767-794 PER SRM 51-40-02.;[06] BLENDED CORROSION AND FOUND TO BE OUT OF LIMIT PER SRM 53-00-53-1A-1.;[07] INSPECTION COMPLETE ON CORRECTIVE ACTION #5 FOR INSTALLATION OF AFT CARGO FWD SHIELD ASSEMBLY/ TRANSITION ANGLE. <BR><BR>INSPECTION VERIFIED THAT CORRECTIVE ACTION #6 CORRECTED THE REFERENCE USED IN CORRECTIVE ACTION #1 AS THE ORIGINAL WAS INCOMPLETE.
AFT CARGO R/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES UNDERSIDE STA.849-850. MRKD<[01] BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IN REFERENCE TO SRM 53-00-53;[02] REMOVED AFT CARGO RH TRANSITION ANGLE AT STA. 847 TO STA. 867 IN REFERENCE TO SRM 51-40-02;[03] UPDATED TOOL;[04] DRILLED NEW TRANSITION ANGLE FOR STATIONS 847 TO 867 IN REFERENCE TO SRM 51-40-05;[05] BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IN REFERENCE TO SRM 53-00-51-1A-2;[06] BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IN REFERENCE TO SRM 53-60-15-1A-1;[07] UPDATED CORRODED ELEMENT PART NUMBER;[08] R/R R/H TRANSITION ANGLE SHIELD PER SRM 53-60-15-1A-1 AND SRM 51-40-02;[09] CA #8 ENTERED INCORRECT REF.;[10] R/R R/H TRANSITION ANGLE SHIELD PER SRM 51-40-02;[11] 02 - INSPECTED PER [SRM 53-00-53-1A-2-B00297 (PERMANENT (NON-DENT DAMAGE TYPES))];[12] 02 - INSPECTED PER [SRM 53-00-53-1A-2-B00297 (PERMANENT (NON-DENT DAMAGE TYPES))] AND SRM 51-40-02
AFT CARGO L/H TRANSITION ANGLE HAS CORROSION AT N/P HOLES STA.727H +2;+6;+9++13+16+20. MRKD<[01] REMOVED L/H TRANSITION ANGLE PER SRM 51-40-02;[02] UPDATED MEASUREMENT PART NUMBER;[03] OK TO INSTALL L/H TRANSITION ANGLE;[04] R/R L/H TRANSITION ANGLE FROM STA 727 - STA 847 PER SRM 53-00-53-2R-5 AND SRM 51-40-02;[05] C/W INSPECTION;[06] C/W INSPECTION
FWD CARGO R/H TRANSITION ANGLE HAS CORROSION BS 492-500A<[01] REMOVED FWD CARGO R/H TRANSITION ANGLE (AFT DOOR CUTOUT SHIELD) BS 492-500A PER SRM 51-40-02.;[02] LOCATED AND DRILLED NEW R/H TRANSITION ANGLE (AFT DOOR CUTOUT SHIELD) BS 492-500A PER SRM 51-40-0 5;[03] INSPECTED CA#2 DRILLED NEW R/H TRANSITION ANGLE (AFT DOOR CUTOUT SHIELD) BS 492-500A;[04] INSTALLED SERVICEABLE RH TRANSITION ANGLE ( AFT DOOR COCONUT SHIELD ) AT BS 492-500A IN REFERENCE TO SRM 51-40-02;[05] INSTALLED SERVICEABLE RH TRANSITION ANGLE ( AFT DOOR CUT-OUT SHIELD ) AT BS 492-500A IN REFERENCE TO SRM 51-40-02;[06] FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1. REMOVED AND INSTALLED SERVICEABLE RH TRANSITION ANGLE ( AFT DOOR CUT-OUT SHIELD ) AT BS 492-500A IN REFERENCE TO SRM 51-40-02;[07] FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1. REMOVED AND INSTALLED SERVICEABLE RH TRANSITION ANGLE ( AFT DOOR CUT-OUT SHIELD ) AT BS 492-500A IN REFERENCE TO SRM 51-40-02;[08] INSPECTION COMPLETE ON CORRECTIVE ACTION #7 FOR INSTALLATION OF REPLACEMENT SHIELD ASSEMBLY AFT OF THE FORWARD CARGO ENTRY DOOR THRESHOLD.
AFT CORNER THRESHOLD OF FWD CARGO CRACKED.<[01] REPAIRED BY VENDOR AIRCRAFT DUCTING REPAIR INC. ON 23OCT2024 UNDER PO# P0058SQ5-1.;[02] INSTALLED REPAIRED SCUFF PLATE PER AMM 53-11-02.;[03] INSTALLED REPAIRED SCUFF PLATE PER AMM 53-11-02. INSPECTION C/W.
LH DEFLECTION RIB ANGLE ATTACH CLIP IS CRACKED (MPN 115A6260-1)<[01] LOCATED AND DRILLED FASTENER HOLES IN NEW ATTACH CLIP PER SRM 51-40-05.;[02] VERIFIED WORK SIGNED IN CA#1...............LOCATED AND DRILLED FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05;[03] ALL STEPS COMPLETE
FWD CORNER THRESHOLD ON FWD CARGO IS CRACKED.<[01] REPAIRED BY VENDOR AIRCRAFT DUCTING REPAIR INC. ON 23OCT2024 UNDER PO# P0058RXY-1;[02] INSTALLED REPAIRED SCUFF PLATE PER AMM 53-11-02.;[03] INSTALLED REPAIRED SCUFF PLATE PER AMM 53-11-02.INSPECTION C/W.
RIGHT WING INBD. TRAILING EDGE UPPER PANEL SUPPORT ANGLE CRACKED JUST INBD. OF THE DEFLECTION CONTROL RIB.<[01] LOCATED; DRILLED AND DEBURRED REPLACEMENT SUPPORT ANGLE PER SRM 51-40-05.;[02] VERIFIED WORK SIGNED IN CA#1. LOCATED; DRILLED AND DEBURRED REPLACEMENT SUPPORT ANGLE PER SRM 51-40-05;[03] C/W
LEFT WING INBD. TRAILING EDGE UPPER PANEL SUPPORT ANGLE CRACKED JUST INBD. OF THE DEFLECTION CONTROL RIB.<[01] LOCATED AND DRILLED FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05.;[02] VERIFIED WORK SIGNED IN CA#1.......LOCATED AND DRILLED FASTENER HOLES IN NEW SUPPORT ANGLE PER SRM 51-40-05;[03] ALL STEPS COMPLETE
L/H A/C BAY; STA. 663 ANGLE TO VAPOR BARRIER CRACKED AT FASTENER HOLE LBL-9<[01] REMOVED DAMAGED SECTION OF ANGLE PER SRM 57-10-102R-5 & SRM51-10-02.;[02] ACCOMPLISHED HFEC HOLE PROBE AND SURFACE INSPECTION OF REPAIR AREA PER NDT PART 6 50-00-00 PROC. 16 AND 51-00-00 PROC. 23 NO DEFECTS NOTED. C/W INSPECTION OF CORRECTIVE ACTION STEP # 1 .;[03] FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5. ALODINE REPAIR PARTS PER AMM 51-21-41. PRIMED REPAIR PARTS PER AMM 51-21-72.;[04] RII INSP C/W; FABRICATED REPAIR PARTS PER SRM 57-10-10-2R-5. ALODINE REPAIR PARTS PER AMM 51-21-41. PRIMED REPAIR PARTS PER AMM 51-21-72.;[05] OK TO INSTALL;[06] REPAIRED L/H STA 663 VAPOR BARRIER ATTACH ANGLE AT LBL 15 PER SRM 57-10-10-2R-5;[07] C/W STEP #6;[08] RII C/W INSPECTION AS REQUIRED
AIRCRAFT RIGHT LOWER EXIT SIGN IS LOOSE.<[01] RESECURED REF. AMM 33-51-03.
AFT GALLEY/ RIGHT FLASHLIGHT NOT CHARGING.<[01] REPLACED AFT GALLEY RIGHT FLASHLIGHT CHARGER IAW AMM 25-64-00
LIGHTED PLACARD BY AFT LEFT LAV DOOR MISSING ITS COVER<[01] REMOVED AND REPLACED AFT LAV EXIT SIGN ASSY IAW AMM 33-51-01. OPS CHECK GOOD
BATTERY PACK FOR R/H FWD AISLE EMERGENCY LIGHTS REQUIRES REPLACEMENT<[01] R/R BATTERY PACK FOR R/H FWD AISLE EMERGENCY LIGHTS IAW AMM 33-51-06
RIGHT HAND HORIZONTAL FWD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED RIGHT HAND HORIZONTAL FWD UPPER SLIDING SEAL IAW BOEING 737 AMM 53-31-31.
AFT LH EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED AFT LH EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06.OPS CHECK GOOD.
AFT ENTRY DOOR EXTERIOR SLIDE EMERGENCY LIGHT INOP<[01] RE-LAMPED AFT ENTRY DOOR EXTERIOR SLIDE EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.
F/A IN AFT GALLEY SMELLED A BURNING ODOR THAT CAME AND WENT AWAY 3 TIMES. NO SMOKE WITH SMELL NOTED ODOR CAME FROM SMALL VENT JUST ABOVE FLOOR LEVEL ON RT SIDE OF AFT GALLEY. PERFORMED CONDITIONAL INSPECTION SMOKE OR FUMES IN THE CABIN PER FIM 21-00 TASK 806 & AMM 05-51-56.
EMERGENCY EXIT LIGHT SIGN BY THE CAPTAINS SIDE AFT LAVATORY IS BLANK<[01] INSTALLED NEW EXIT LENS PER AMM 33-51-01.
FWD SERVICE DOOR ESCAPE SLIDE PRESSURE INDICATOR IN RED BAND. REMOVED AND REPLACED FWD SERVICE DOOR ESCAPE SLIDE IAW AMM 25-66-01 AND MT 725-61-06-FS.
FWD 3 RT EMERGENCY LIGHTS ON OVERHEAD BINS INOP / [01] REPLACED M1676 BATTERY/CHARGER ASSEMBLY AND TESTED PER AMM 33-51-06-960-806. AFTER 30 MINUTES CHARGING; NO LIGHTS; SLAVED BATTERY FROM M1675 (SEE DEFECT TTG8Q00FVHN7) TO CONFIRM LIGHTS WORK WITH KNOWN GOOD BATTERY.
SUPPLEMENTAL INFORMATION: FWD 3 RT EMERGENCY LIGHTS ON OVERHEAD BINS INOP / [01] REPLACED M1676 BATTERY/CHARGER ASSEMBLY AND TESTED PER AMM 33-51-06-960-806. AFTER 30 MINUTES CHARGING; NO LIGHTS; SLAVED BATTERY FROM M1675 (SEE DEFECT TTG8Q00FVHN7) TO CONFIRM LIGHTS WORK WITH KNOWN GOOD BATTERY.;[02] REMOVED AND REPLACED M1676 BATTERY PACK AND OPS CHECKED PER AMM 33-51-06-960-805 CHECKED GOOD;[03] INSPECTION COMPLETE
SUPPLEMENTAL INFORMATION: FWD ENTRY WAY EMERGENCY LIGHTS INOP / [01] REPLACED M1675 BATTERY/ CHARGER ASSEMBLY AND TESTED PER AMM 33-51-06-960-806; NO DEFECTS NOTED. REPLACED M2816 BATTERY/CHARGER ASSEMBLY AND TESTED PER AMM 33-51-06-960-806. AFTER 30 MINUTES CHARGING; NO LIGHTS; SLAVED BATTERY FROM M1675 (SEE DEFECT TTG8Q00FVHN7) TO CONFIRM LIGHTS WORK WITH KNOWN GOOD BATTERY.;[02] COMPLETED STEPS 1 AND 2;[03] REMOVED AND REPLACE M2816 BATTERY PACK AND OPS CHECKED PER AMM 33-51-06-960-805;[04] OPS CHECK FOR CORRECTIVE ACTION 3 CHECKED GOOD;[05] INSPECTION COMPLETE
BREAK PANEL IS CRACKED AT STA 540; BL0-RBL25; WL 208. / [01] REMOVED BREAK PANEL AT BS 540 BL0-RBL25 WL208 PER SRM 51-40-02-0G-0;[02] LOCATED AND DRILL BREAK PANEL AT BS 540 BL0-RBL25 WL 208 PER SRM 51-40-05-0G-0 AND IPC 53-42-11-66. OK TO INSTALL BREAK PANEL;[03] VERIFIED CORRECTIVE ACTION 2 AND OK TO INSTALL GIVEN. VERIFIED MEASUREMENT TABLE;[04] INSTALLED BREAK PANEL BS 540 BL0-RBL 25 WL 208 PER SRM 51-40-02-0G-0 AND IPC 53-42-11-66;[05] VERIFIED CORRECTIVE ACTION 4;[06] VERIFIED JOB COMPLETE
BREAK PANEL IS CRACKED AT STA 540; BL0-LBL25; WL 208. / [01] REMOVED BREAK PANEL AT BS 540 BL0-LBL 25 WL208 PER SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED BREAK PANEL BS 540 BL0-LBL25 WL 208 PER SRM 51-40-05-0G-0 AND IPC 53-42-11-66. OK TO INSTALL BREAK PANEL;[03] VERIFIED CORRECTIVE ACTION 2 AND OK TO INSTALL GIVEN. VERIFIED MEASUREMENT TABLE;[04] INSTALLED BREAK PANEL BS 540 BL0-LBL25 WL 208 PER SRM 51-40-02-0G-0;[05] INSTALLED BREAK PANEL BS 540 BL0-LBL25 WL 208 PER SRM 51-40-02-0G-0 AND IPC 53-42-11-66;[06] VERIFIED CORRECTIVE ACTION 5;[07] VERIFIED JOB COMPLETED
#2 ENGINE O/B FAN COWL OIL ACCESS DOOR CLOSE OUT SHIELD IS BROKEN PT# 314-2259-4 / [01] REMOVED #2 ENGINE O/B FAN COWL OIL ACCESS DOOR CLOSE OUT SHIELD IAW SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED #2 ENGINE I/B FAN COWL OIL ACCESS DOOR CLOSE OUT SHIELD P/N 314-2259-4 IAW CMM 71-13-30; SRM 51-40-02-0G-0.;[03] VERIFIED CORRECTIVE ACTION 2 INSTALLATION
#1 ENGINE I/B FAN COWL OIL ACCESS DOOR CLOSE OUT SHIELD IS BROKEN PT# 314-2259-4 / [01] REMOVED #1 ENGINE I/B FAN COWL OIL ACCESS DOOR CLOSE OUT SHIELD IAW SRM 51-40-02-0G-0;[02] REMOVED AND REPLACED #1 ENGINE I/B FAN COWL OIL ACCESS DOOR CLOSE OUT SHIELD P/N 314-2259-4 IAW CMM 71-13-30; SRM 51-40-02-0G-0.;[03] VERIFIED CORRECTIVE ACTION 2 INSTALLATION
LEFT WING T/E WIGGLE PLATE IS BROKEN AT ORSS 374. (MARKED) CORRECTION: RIGHT WING / [01] REMOVED RIGHT WING T/E BROKEN WIGGLE PLATE AT ORSS 374 IAW SRM 51-40-02-0G-0.;[02] INSTALLED RIGHT WING T/E WIGGLE PLATE AT ORSS 374 IAW SRM 51-40-02-0G-0 AND BOEING DWG 115A3700 OK TO CAP SEAL FASTENERS;[03] VERIFIED CORRECTIVE ACTION #2;[04] APPLIED CAP SEAL TO FASTENERS COMMON TO RIGHT WING T/E WIGGLE PLATE ORSS 374 IAW AMM 51-31-00-390-805;[05] VERIFIED CORRECTIVE ACTION #4
AFT CARGO BAY LAV TANK BULKHEAD LOWER BRACKET IS BROKEN BS867 LBL10 WL166 / [01] REMOVED OLD LAV TANK LOWER SUPPORT BRACKET BS 867 LBL 10 WL 166 PER SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW BRACKET PER SRM 51-40-05-0G-0; OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION #1 OK TO INSTALL;[03] INSTALLED LAV TANK BULKHEAD LOWER BRACKET ;BS 867; LBL 10; WL 166 PER SRM 51-40-02-0G-0; DWG 149A8104; DWG 149A8102.;[04] VERIFIED CORRECTIVE ACTION #3
AFT CARGO BAY CARGO FLOOR SPLICE STRAP HAS CORROSION AROUND FASTENER HOLE BS767+6 RBL2 WL156 / [01] UPDATED MEASUREMENT TABLE AND ATTACHED PHOTO;[02] CORROSION ON STRAP WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM;[03] VERIFIED CORRECTIVE ACTION STEP 2.;[04] RECEIVED NEW FLOOR SPLICE STRAP;[05] VERIFIED CORRECTIVE ACTION 4
FWD CARGO BAY SHIELD AFT OF DOOR HAS CORROSION AROUND NUT PLATE HOLE BS500+6 RBL23.5 WL156 / [01] UPDATED MEASUREMENT ABLE AND ATTACHED PHOTO;[02] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[03] VERIFIED CORRECTIVE ACTION 2.;[04] REMOVED DAMAGED FCB SHEILD AFT OF DOOR BS500-500A RBL23.5 WL 156 IAW SRM 51-40-02.;[05] LOCATED AND DRILLED NEW FCB AFT SHIELD; 495-500A; RBL23.5; IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0. AND OK TO INSTALL.;[06] VERIFIED CORRECTIVE ACTION #5 AND MEASUREMENT FIELD;[07] INSTALLED FCB AFT SHIELD; BS495-500A RBL 23.5; IAW SRM 51-40-02-0G-0; DWG 143A0080.;[08] VERIFIED CORRECTIVE ACTION #7;[09] VERIFIED CORRECTIVE ACTION #7
FWD CARGO BAR R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREA OF CORROSION AROUND NUT PLATE HOLES BS500A TO BS500I RBL24.5 WL156 / [01] UPDATED MEASUREMENT TABLE AND ATTACHED PHOTO;[02] VERIFIED APPLICABILITY OF SRM 53-00-53-1A-2. EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500A+7 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023;[03] VERIFIED CORRECTIVE ACTION 2.;[04] REMOVED FCB RH FLOOR TO SIDEWALL SUPPORT PLATE BS500A TO BS500I RBL24.5 WL156 IAW SRM 51-40-02.;[05] LOCATED AND DRILLED FCB RH FLOOR TO SIDEWALL SUPPORT BS 500A-500I; RBL 24; IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0. AND OK TO INSTALL.;[06] VERIFIED CORRECTIVE ACTION 5 OK TO INSTALL GIVEN;[07] INSTALLED FCB RH FLOOR TO SIDEWALL SUPPORT; BS500A-500I; RBL24; IAW SRM 51-40-02-0G-0; DWG 143A7500.;[08] RII VERIFIED CORRECTIVE ACTION ITEM 7.;[09] VERIFIED CORRECTIVE ACTION ITEM 7 AND MEASUREMENT FIELDS; CARD COMPLETE.
FWD CARGO BAY LOWER BULKHEAD SUPPORT HAS A AREA OF CORROSION AROUND FASTENER BS500I RBL8.5 WL156 / [01] UPDATED MEASUREMENT TABLE AND ATTACHED PHOTO;[02] VERIFIED APPLICABILITY OF SRM PER SRM 53-30-08-1A-1. REMOVED CORROSION IN A 1'X1' AREA; REMAINING THICKNESS IS LESS THAN 0.056' FOUND TO BE OUT OF LIMITS PER SRM 53-30-08-1A-1 USING ATS TOOL IDATS1225.;[03] VERIFIED CORRECTIVE ACTION 2;[04] REMOVED FCB LWR BLKHD SUPPORT @ BS500I RBL23-LBL23 WL156 IAW SRM 51-40-02.;[05] LOCATED AND DRILLED FCB LOWER BULKHEAD SUPPORT; BS 500I; IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0. AND OK TO INSTALL.;[06] VERIFIED CORRECTIVE ACTION 5 AND OK TO INSTALL GIVEN;[07] INSTALLED FCB LOWER BULKHEAD SUPPORT; BS 500I; IAW SRM 51-40-02-0G-0; DWG 143A7902; DWG 143A9481.;[08] UPDATED MEASUREMENT TABLE;[09] RII VERIFIED CORRECTIVE ACTION ITEM 7.;[10] VERIFIED CORRECTIVE ACTION ITEM 7-8; AND MEASUREMENT FIELDS; CARD COMPLETE.
AFT CARGO BAY SHIELD FWD OF CARGO DOOR HAS CORROSION AROUND NUT PLATE HOLE BS767+8 RBL22 WL156 / [01] UPDATED MEASUREMENT TABLE AND ATTACHED PHOTO;[02] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[03] VERIFIED CORRECTIVE ACTION STEP 2.;[04] REMOVED ACB FWD SHIELD AT BS767 -BS787+5' RBL22 WL156 PER SRM 51-40-02-0G-0;[05] LOCATED AND DRILLED ACB FWD SHIELD AT BS767 -BS787+5' RBL22 WL156 PER SRM 51-40-05-0G-0 AND DWG 146A0081;[06] VERIFIED CORRECTIVE ACTION 5.<BR>OK TO INSTALL;[07] INSTALLED NEW ACB FWD SHIELD AT BS767 -BS787+5' RBL22 WL156 PER SRM 51-40-02-0G-0 AND DWG 146A0081;[08] UPDATED MEASUREMENT TABLE STEP 14 CORRECTED PART NUMBER;[09] UPDATED MEASUREMENT TABLE;[10] RII VERIFIED CORRECTIVE ACTION ITEM 7.;[11] VERIFIED CORRECTIVE ACTION ITEM 7-9; AND MEASUREMENT FIELDS; CARD COMPLETE.
AFT CARGO BAY ATTACH ANGLE UNDER SHIELD HAS CORROSION AROUND NUT PLATE BS767+2 RBL20.5 WL156 / [01] UPDATED MEASUREMENT TABLE AND ATTACHED PHOTO;[02] CORROSION ON ANGLE WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM;[03] VERIFIED CORRECTIVE ACTION STEP 2.;[04] REMOVED ACB ATTACH ANGLE UNDER SHIELD AT BS767 -BS787+5' RBL20.5 WL156;[05] LOCATED AND DRILLED ACB ATTACH ANGLE UNDER SHIELD AT BS767 -BS787+5' RBL20.5 WL156 PER SRM 51-40-05-0G-0 AND DWG 146A8123. OK TO INSTALL;[06] VERIFIED CORRECTIVE ACTION 5. <BR>OK TO INSTALL;[07] INSTALLED NEW ACB ATTACH ANGLE UNDER SHIELD AT BS767 -BS78 RBL20.5 WL156 PER SRM 51-40-02-0G-0 AND DWG 146A8123.;[08] UPDATED STEP 19 ON MEASUREMENT TABLE;[09] UPDATED MEASUREMENT TABLE;[10] VERIFIED CORRECTIVE ACTION #7;[11] VERIFIED MEASUREMENT TABLE
AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS OF CORROSION AROUND NUT PLATE HOLES BS727H+16 TO BS767 RBL20 WL156 / [01] UPDATED MEASUREMENT TABLE AND ATTACHED PHOTO;[02] VERIFIED APPLICABILITY OF SRM 53-00-53-1A-2 AND SRM 53-00-53-2R-5. EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727J+6' REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023;[03] VERIFIED CORRECTIVE ACTION STEP 2.;[04] REMOVED SECTION OF DAMAGED ACB R\H FLOOR TO SIDEWALL SUPPORT BS727H+11' TO BS767' RBL20 WL156 PER SRM 51-40-02-0G-0;[05] FABRICATED; LOCATED; DRILLED AND DEBURRED; APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON NEW R\H FLOOR TO SIDEWALL SUPPORT SECTION FROM BS727H+11' TO BS767' RBL21 WL156 AND SPLICE AT BS727H+11'; EXTRUSION MATERIAL USED BAC1496-377#7075T62 CLAD; LOT# 1494598-1 PER SRM 53-00-53-2R-5 REP 5 PAR 4C-J AND EA M-22-153-01550; DWG 146A7500; 146A7502. OK TO INSTALL.;[06] VERIFIED CORRECTIVE ACTION 5.<BR>OK TO INSTALL;[07] INSTALLED ACB R\H FLOOR TO SIDEWALL SUPPORT BS727H+11' TO BS767' RBL20 WL156 PER SRM 53-00-53-2R-5 REP 5 EA M-22-153-01550; DWG 146A7500; 146A7502. SPLICE INSTALLED AT BS727H+11'.;[08] THE DAMAGE WAS REPAIRED PER SRM 53-00-53-2R-5 (REPAIR 5) AND EA M-22-153-01550.;[09] VERIFIED CORRECTIVE ACTION #7; 8<BR>VERIFIED MEASUREMENTS
AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS OF CORROSION AROUND NUT PLATE HOLES BS727H TO BS847 LBL22 WL156 / [01] ADDED PHOTO OF DAMAGE. VERIFIED APPLICABILITY OF SRM 53-00-53-1A-2 AND SRM 53-00-53-2R-5 .EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727J+4' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023;[02] VERIFIED CORRECTIVE ACTION STEP 1;[03] REMOVED AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE FROM BS 727G + 12 - BS 847; LBL 22; WL 156 IAW SRM 51-40-02-0G-0 AND SRM 53-00-53-2R-5 REPAIR 5;[04] FABRICATED AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATES 2(EA) AND SPLICE SIDEPLATES 2(EA); MADE FROM BAC1496-377#7075T62; LOT# 1494598-1; FROM BS 727G + 12 - BS 847; LBL 22; WL 156 IAW SRM 53-00-53-2R-5 REPAIR 5 PARG. 4 STEPS (D-H);[09] INSTALLED AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE FROM BS 727G + 12 - BS 847; LBL 22; WL 156 WITH SPLICEPLATES AT BS 727G +12 AND BS 747 +12 IAW SRM 51-40-02-0G-0; SRM 53-00-53-2R-5 REPAIR 5; DWG 146A7500 AND DWG 146A7502;[10] VERIFIED CORRECTIVE ACTION #9;[11] MEASUREMENT TABLE VERIFIED
R/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68 / REMOVED DAMAGED SECTION OF RH BS663 UPPER ATTACH ANGLE RBL8-RBL20 WL167.68 IAW SRM 57-10-10-2R-5.;[04] PERFORM AN OPEN HOLE HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION FOR ALL INITIAL FASTENER HOLES IN THE REPAIR AREA TO MAKE SURE THERE IS NO DAMAGE.;[05] PERFORM A DETAILED INSPECTION OF THE REPAIR AREA AND THE UNDERLYING STRUCTURE TO MAKE SURE THAT THERE IS NO DAMAGE WITHIN THE REPAIR AREA.;[06] RECEIVED REPAIR PARTS SPLICE ANGLE RO#887174-SWA-3 AND REPLACEMENT ANGLE RO#887174-SWA-1.;[07] VERIFIED CORRECIVE ACTION 1;2;3;5 AND 6;[08] HFEC INSPECTED OPEN HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16. <BR>NO CRACKS NOTED. <BR>EQUIP USED: <BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23 <BR>-MINIMITE ID: ATS1411 CAL DUE: 07/23;[09] LOCATED; DRILLED; TRIMMED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING AND PRIMERED REPAIR PARTS IAW SRM 57-10-10-2R-5. 0K TO INSTALL.;[10] VERIFIED CORRECTIVE ACTION 9. OK TO INSTALL.;[11] INSTALLED REPAIR PARTS FOR RH BS663 UPPER ATTACH ANGLE RBL8-RBL20 WL167.68 IAW SRM 57-10-10-2R-5.
FWD JUMP SEAT FA FLASHLIGHT DOES NOT TEST / [01] REPOSITION FWD FA FLASHLIGHT OPS CHECK GOOD PER AMM 25-64-00
PHOTOLUMINESCENT FLOOR LIGHTING INOP; FOR SIDE FROM ROW 1-2 / REMOVED RIGHT SIDE EMERGENCY TRACK LIGHTING FROM FWD GALLEY TO ROW 2 AND INSTALLED SERVICEABLE PHOTLUMINESCENT STRIP PER AMM 33-51-15
'EXIT-SALIDA' SIGN ON REAR SERVICE DOOR MISSING. / R&R AFT SERVICE DOOR EMERGENCY LIGHT FOR EXIT PER AMM 33-51-01
FWD CARGO CEILING PANEL 122ZFC HAS CRACK ALONG CONTOUR EDGE - 16'PERFORMED TIME LIMITED REPAIR REF EA 1-A25-3722 REV 4. PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING; EVERY 8 DAYS. ACCOMPLISH A PERMANENT REPAIR OR R&R DISCREPANT PANEL; WITHIN 730 DAYS.REPETITIVE ACTION REQUIRED PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIR AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. /
ONE AFT CABIN FLASH LIGHT INOP. OK TO CONT PER MEL 25-12-01 SP#1B TRACKING #106108 ( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ) / R/R FLASHLIGHT BATTERY PER MM:25-64-00. (CL#:85432)
FWD CARGO CEILING PANEL 122ZFC HAS CRACK ALONG CONTOUR EDGE - 16'PERFORMED TIME LIMITED REPAIR REF EA 1-A25-3722 REV 4. PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING; EVERY 8 DAYS. ACCOMPLISH A PERMANENT REPAIR OR R&R DISCREPANT PANEL; WITHIN 730 DAYS.REPETITIVE ACTION REQUIRED PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIR AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING. / A) REPETITIVE ACTION REQUIRED COMPLIED WITH; NO ADDITIONAL DAMAGE OR DETERIORATION NOTED. OK TO CONTINUE SERVICE IN ACCORDANCE WITH REFERENCE EA 1-A25-3722 REV 4
FWD CARGO CEILING PANEL 122ZFC HAS CRACK ALONG CONTOUR EDGE - 16' / PERFORMED TIME LIMITED REPAIR REF EA 1-A25-3722 REV 4. PERFORM A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA FOR ADDITIONAL DAMAGE AND REPAIR INTEGRITY. IF FURTHER DEFECTS ARE NOTED; CONTACT SERVICE ENGINEERING; EVERY 8 DAYS. ACCOMPLISH A PERMANENT REPAIR OR R&R DISCREPANT PANEL; WITHIN 730 DAYS.
AFT CARGO SIDEWALL PANEL 141FW HAS 2 - 2 INCH CRACKS ON BOTTOM EDGEPERFORMED TIME LIMITED REPAIR REF EA 1-A25-4142 REV 1 REPLACE DAMAGED PANEL OR ACCOMPLISH ALL EA 1-A25-3668 (WIZARD) / REPAIR-25EA-03644 (TRAX); WITHIN 30 DAYS.PERMANENT ACTION REQUIRED /
CREW REPORTED THE FWD EMERGENCY FLASHLIGHT NOT TESTING. R & R THE FWD FLASHLIGHT IAW AMM 25-64-00.
R1 DOOR GIRT BAR STOWAGE BRACKET LOOSE. SECURED BRACKET PER SIP.
GIRT BAR STUCK IN THE UP POSITION FWD. SERVICE DOOR. REMOVED GIRT BAR FROM UP POSITION IAW SIP. (CNTRCT AMT 3395336)
AFT GALLEY EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER AMM.
FORWARD FLIGHT ATTENDANT INBOARD FLASHLIGHT INDICATION INOP. R&R FLASHLIGHT ASSEMBLY PER MM.