N382DN

Part: SKIN — HANDLER ERROR (FUSELAGE) · airframe 14,039 hrs · 6,060 cycles

AIRCRAFT 3082, DURING LAYOVER IN MSP, A CATERING TRUCK HAD CONTACTED THE AIRCRAFT AFT OF THE L4 DOOR. AFT FUSELAGE HAS 2 LARGE HOLES AFT OF DOOR 4L. CORRECTIVE ACTION: ACCOMPLISH TRIM OUT OF THE DAMAGED SKIN PER SRM 51-27-11 TO REMOVE ALL PUNCTURES, CRACKS, AND DENTS. ACCOMPLISH SURFACE HFEC INSPECTIONS OF THE SKIN INNER AND OUTER SURFACES. FABRICATE AND INSTALL REPLACEMENT SKIN, EXTERNAL REPAIR DOUBLER, STURCTUALL FILLER AND SKIN TRIM OUT FILLER PER ER/Z 615256-14. (LP 5103580)

Part: SKIN — GROUND DAMAGE (FUSELAGE) · airframe 14,583 hrs · 6,265 cycles

AIRCRAFT 3082, DURING LAYOVER IN MSP, A CATERING TRUCK HAD CONTACTED THE AIRCRAFT AFT OF THE L4 DOOR. THE FUSELAGE SKIN SUSTAINED A PUNCTURE BETWEEN FR 69-70 AND STR 34L 32L. THE FUSELAGE SKIN IS P/N D5348002324200. REMOVE ALL FASTENERS IN THE DAMAGE AREA. TRIM OUT OF THE DAMAGED SKIN. ACCOMPLISH SURFACE HFEC INSPECTIONS OF THE SKIN INNER AND OUTER SURFACES IN THE AREA OF THE TRIM OUT AND OF THE TRIMMED EDGES. ACCOMPLISH INTERNAL DVI OF THE FRAMES, FRAME SHEAR TIES, STRINGERS, STRINGER TIES AND ANY OTHER INTERNAL STRUCTURE IN THE AREA. INSTALL REPLACEMENT PARTS. FABRICATE ITEM 1 REPLACEMENT SKIN, FABRICATE ITEM 2 EXTERNAL REPAIR DOUBLER, FABRICATE ITEM 3 STRUCTURAL FILLER, AND FABRICATE ITEM 4 SKIN TRIM OUT FILLER. PER ER/A 615256-14. INSTALL THE SKIN TRIM OUT FILLER, REPAIR DOUBLER AND REPAIR TRIPLER.

Part: STRINGER — HANDLER ERROR (FUSELAGE) · airframe 14,039 hrs · 6,060 cycles

AIRCRAFT 3082, DURING LAYOVER IN MSP, A CATERING TRUCK HAD CONTACTED THE AIRCRAFT AFT OF THE L4 DOOR. STRINGER 26L DAMAGED BETWEEN FR 69 & FR 70. CORRECTIVE ACTION: ACCOMPLISH TRIM OUT OF THE DAMAGED SKIN PER SRM 51-27-11 TO REMOVE ALL PUNCTURES, CRACKS, AND DENTS. ACCOMPLISH SURFACE HFEC INSPECTIONS OF THE SKIN INNER AND OUTER SURFACES. FABRICATE AND INSTALL REPLACEMENT SKIN, EXTERNAL REPAIR DOUBLER, STURCTUALL FILLER AND SKIN TRIM OUT FILLER PER ER/Z 615256-14. (LP 0198769)

Part: DOOR — HANDLER ERROR (L4) · airframe 14,039 hrs · 6,060 cycles

AIRCRAFT 3082, DURING LAYOVER IN MSP, A CATERING TRUCK CONTACTED THE AIRCRAFT AFT OF THE L4 DOOR. THE UPPER AND LOWER FR69 SUSTAINED DAMAGE BETWEEN S-27L/S-28L AND S-29L/S-31L. CORRECTIVE ACTION: ACCOMPLISH TRIM OUT OF THE UPPER (LOCATION #1) AND LOWER (LOCATION #2) FR69 DAMAGE PER SRM 51-27-11 TO REMOVE ALL DENTS OR GOUGES. FABRICATE AND INSTALL ITEM 1 SPLICE, SIMILAR TO THE D53480092270 SPLICE. PER ER/A 615343-14. (LP 0198330)

Part: STRINGER — HANDLER ERROR (FUSELAGE) · airframe 14,039 hrs · 6,060 cycles

AIRCRAFT 3082, DURING LAYOVER IN MSP, A CATERING TRUCK HAD CONTACTED THE AIRCRAFT AFT OF THE L4 DOOR. STRINGER 28L DAMAGED BETWEEN FR 69 & FR 70. CORRECTIVE ACTION: ACCOMPLISH TRIM OUT OF THE DAMAGED SKIN PER SRM 51-27-11 TO REMOVE ALL PUNCTURES, CRACKS, AND DENTS. ACCOMPLISH SURFACE HFEC INSPECTIONS OF THE SKIN INNER AND OUTER SURFACES. FABRICATE AND INSTALL REPLACEMENT SKIN, EXTERNAL REPAIR DOUBLER, STURCTUALL FILLER AND SKIN TRIM OUT FILLER PER ER/Z 615256-14. (LP 0198760)

Part: STRINGER — HANDLER ERROR (FUSELAGE) · airframe 14,039 hrs · 6,060 cycles

AIRCRAFT 3082, DURING LAYOVER IN MSP, A CATERING TRUCK HAD CONTACTED THE AIRCRAFT AFT OF THE L4 DOOR. FR 70 BUTT SPLICE STRIP IS DEFORMED AT STR 27L & STR 29L. CORRECTIVE ACTION: ACCOMPLISH TRIM OUT OF THE DAMAGED SKIN PER SRM 51-27-11 TO REMOVE ALL PUNCTURES, CRACKS, AND DENTS. ACCOMPLISH SURFACE HFEC INSPECTIONS OF THE SKIN INNER AND OUTER SURFACES. FABRICATE AND INSTALL REPLACEMENT SKIN, EXTERNAL REPAIR DOUBLER, STURCTUALL FILLER AND SKIN TRIM OUT FILLER PER ER/Z 615256-14. (LP 0198774)

Part: STRINGER — DAMAGED (FRM 71-72 S27L) · airframe 14,039 hrs · 6,060 cycles

STRINGER 27L DAMAGED BETWEEN FR71 & FR72. CORRECTIVE ACTION: CUT STRINGER 27L APPROX 4" AFT OF FR72. REMOVED STR 27L UP TO FR70, 491345. PERFORMED HFEC INSPECTION OF CUT STRINGER PER A321 NTM 51-10-08, NO DEFECTS NOTED, QC5119. SPLICE FABRICATED ON RO #701997. DRILLED STRINGER & AFT SPLICE TO SIZE PER A321 SRM 53-13, 491375. TREATED & PRIMED SPLICE COUPLING. TREATED, PRIMED & TOPCOATED SPLICE COUPLING & CUT END OF STRINGER PER PS900-3-6, NO. 3, 491375. OK TO INSTALL STR 27L AND COUPLING AFT OF APB, QC2019. INSTALLED COUPLING AND NEW SECTION STRINGER 27L FROM APB (FR70) TO AFT OF FR72 IAW A321 SRM 53-00-13-300-001. (LP 0192521)

Part: SKIN — HANDLER ERROR · airframe 14,039 hrs · 6,060 cycles

AIRCRAFT 3082, DURING LAYOVER IN MSP, A CATERING TRUCK HAD CONTACTED THE AIRCRAFT AFT OF THE L4 DOOR. THE FUSELAGE SKIN SUSTAINED A LARGE PUNCTURE DAMAGE BETWEEN FR 71-72 AND STR 26L  28L AND INCLUDED SOME ADDITIONAL DENTING IN THE LOCAL AREA. THE FUSELAGE SKIN IS P/N D5357112821000. IT IS MADE FROM 0.126 2024-T42 CLAD SHEET AND IS 0.039 AND 0.079 LOCALLY IN THE AREA. THIS ERA WILL REPAIR THE AREA. CORRECTIVE ACTION: ACCOMPLISH TRIM OUT OF THE DAMAGED SKIN PER SRM 51-27-11 TO REMOVE ALL PUNCTURES, CRACKS, AND DENTS. FABRICATE THE DOUBLER/TRIPLER AND REPAIR PART(S) PER FIGURE 5. APPLY CHEMICAL CONVERSION COATING, PRIMER (MATERIAL NO. 04EAC2) AND TOPCOAT (MATERIAL NO. 04JME4 TO THE REPAIR PARTS. INSTALL THE REPAIR DOUBLER / TRIPLER AND ALL REPAIR PARTS PER FIGURE 5. (LP 0184832)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,239 hrs · 4,923 cycles

SHIP 3082 FR31 LEFT DAMAGED BETWEEN STRINGERS 44 AND 38L. CORRECTIVE ACTION: INSTALLED NEW FRAME PER A321 SRM 51-42. (2710911)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,239 hrs · 4,923 cycles

SHIP 3082 FR29 DAMAGED BETWEEN STRINGERS 44 AND 39L. CORRECTIVE ACTION: INSTALLED NEW FRAME PER A321 SRM 51-44. (2710936)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,239 hrs · 4,923 cycles

SHIP 3082 STRINGER 43L DAMAGED FWD OF FR29 TO AFT OF FR32. CORRECTIVE ACTION: REPLACED STRINGER PER A321 SRM 51-44. (2710931)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,239 hrs · 4,923 cycles

SHIP 3082 POST AT FR29 DAMAGED. CORRECTIVE ACTION: INSTALLEDCNEW POST PER A321 SRM 51-44. (2710935)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,239 hrs · 4,923 cycles

SHIP 3082 STRINGER 41L DAMAGED AFT OF FR28 TO FWD OF FR32. CORRECTIVE ACTION: REPLACED STRINGER PER A321 SRM 51-42. (2710919)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,239 hrs · 4,923 cycles

SHIP 3082 STRINGER 42L DAMAGED AFT OF FR28 TO FWD OF FR32. CORRECTIVE ACTION: REPLACED STRINGER PER A321 SRM 51-42. (2710926)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,239 hrs · 4,923 cycles

SHIP 3082 FR29 CROSS BEAM DAMAGED. CORRECTIVE ACTION: INSTALLED NEW CROSS BEAM PER A321 SRM 51-44. (2710929)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,239 hrs · 4,923 cycles

SHIP 3082 STRINGER 44 DOUBLER BETWEEN FR28 AND FR31 DAMAGED. CORRECTIVE ACTION: INSTALLED NEW DOUBLER PER A321 SRM 51-44. (2710933)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,239 hrs · 4,923 cycles

SHIP 3082 STRINGER 44 DAMAGED BEWTWEEN FR 28 AND JUST AFT OF FR 30. CORRECTIVE ACTION: REPLACED STRINGER PER A321 SRM 51-44. (2710934)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,239 hrs · 4,923 cycles

SHIP 3082 FUSELAGE SKIN DAMAGE APPROX FR29 TO FR31 S44 TO S41L. CORRECTIVE ACTION: REPLACED SKIN PER A321 SRM 51-42. (2710922)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,239 hrs · 4,923 cycles

SHIP 3082 STRINGER 40L DAMAGED AFT OF FR28 TO AFT OF FR31. CORRECTIVE ACTION: REPLACED STRINGER PER A321 SRM 51-42. (2710915)

Part: NONE — NONE · airframe 9,732 hrs · 4,281 cycles

EPSU FAULTED DURING TROUBLESHOOTING FIN 12WL. REPLACED EPSU 12WL WITH SERVICABLE FROM AMERICAN AIRLINES IAW A321 AMM 33-51 OPS CHECKS GOOD. (LP# 8929138)

Part: NONE — NONE · airframe 9,732 hrs · 4,281 cycles

FOUND MULTIPLE EXIT PATH LIGHTS INOP. REPAIRED WIRING AT ROW FWD OF MID LAV LH SIDE A321 ESPM 20-40 AND REPLACED EPSU 11WL IAW A321 AMM 33-51. OPS CHECKS GOOD MPN 3214-62-10 S/N ON 147937 S/N OFF 163241. (LP# 8929136)

Part: LIGHT — NOT SEATED · airframe 8,819 hrs · 3,915 cycles

EMERGENCY EXIT LIGHT DOES NOT WORK AT ROW# 33L. RECONNECTED EMERGENCY EXIT LIGHT AT SEAT ROW 33L. (LP# 2283359)

Part: NONE — NONE · airframe 8,505 hrs · 3,784 cycles

DURING TAXI OUT, STRONG BURNT RUBBER SMELL WAS REPORTED IN AFT GALLEY. TAXIED BACK TO GATE. SMOKE AND FUMES QUESTIONNAIRE COMPLETED. PERFORMED CARD 0550-2002 TYPE 9 CLASSIFICATION FOR RUBBER SMELL ONLY IN AFT GALLEY. PERFORMED EXT GVI NO ITEMS NOTED. FOLLOWED FLOW CHART FIGURE 4 PG 13 NO FINDINGS. PERFORMED ENGINE RUN ON #1 AND #2 INDEPENDENTLY. NO ODOR NOTED. (LP# 8564872)

Part: CONTROL VALVE — MALFUNCTIONED (PACK FLOW) · airframe 6,385 hrs · 2,815 cycles

SHIP 3082 - ATB - DUE TO EXCESSIVE CABIN ALTITUDE MESSAGE. #1 PACK UNABLE TO MAINTAIN PRESSURIZATION WITH #2 PACK ON MEL. NO MASK DEPLOYED. CORRECTIVE ACTION: REPLACED PACK #1 FLOW CONTROL VALVE AND #1 ACSC. REPLACED PACK #2 FLOW CONTROL VALVE. (LP# 7994658)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 5,739 hrs · 2,491 cycles

WORKING LOG PG. 6425050, DENT REPAIR. CUT OUT SKIN DAMAGE I.A.W.A321 SRM 53-11-11-300-041 FIG 003 WIP 881490, ACCOMPLISHED HFEC I.A.W. A321 NTM 51-10-08, NO CRACKS QC2070. FER A321 SRM 51-70-20-801 FIG 1 FLAGNOTE 3 EXISTING SKIN IS DETERMINED BY THE MILLED SKIN POCKET WHICH IS .056 THICK, FABRICATED DOUBLER FROM .063 2024-T3 AND DRILLED EXISTING FASTENERS, WIP M.FELLOWS672231. FINISHED DRILLING AND FABRICATING DOUBLER 881490. OK. TO TREAT AND PAINT QC2070. TREATED AND PRIMED DOUBLER AND FILLER 576315. OK. TO INSTALL QC2070. INSTALLED REPAIR DOUBLER AND FILLER PER A321 SRM 53-11- 11, NEEDS FINISH RESTORED AND TAG ID, 576315.QC2070. APPLIED TOP COAT TO INTERNAL AND EXTERNAL SIDES OF REPAIR PER A321 SRM 53- 11-11-300-041, APPLIED CORROSION PREVENTATIVE COMPOUND TO INSIDE OF REPAIR AREA, IDENTIFIED REPAIR PER ERA 584126-14 REV "O", DEFFERED TO MON PER A321 SRM 53-11-11-205-037 FOR ZONE 1 FOR INSPECTION AT 60,000FC/ 120,000FH WHICHEVER OCCURS FIRST, JOB COMPLETE. (LP# 1784368)

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 4,457 hrs · 1,944 cycles

ON SERVICE CHECK FOUND EPSU 15WL AND 13WL BATT FAIL. R & R BOTH EPSU BATTERY PACKS 13WL+15WL, PER A321 AMM 33-50. CHECKS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 3,868 hrs · 1,692 cycles

PILOT REPORT AFT CABIN EMERGENCY LIGHTS & SIGNS WON`T TEST. CORRECTIVE ACTION: T/S PER TSM R & R BATTERY PACK 13WC. PERFORMED MASTER RESET OF ALL A/C POWER SYSTEMS NOW OPERATIONS NORMAL. OK FOR CONTINUED SERVICE, REF A320 FAM AMM 33-51 & TSM 33-51.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 114 hrs · 42 cycles

EMERGENCY EXIT SIGNS INOPERATIVE, CONNECTOR ABOVE CEILING AT ROW 13, 2810VC DISCONNECTED, RESEATED SAME.