N315DN

Part: ENGINE — STALLED (NR 2) · airframe 23,496 hrs · 10,842 cycles

SHIP 3015 -ATB- RETURNED TO SLC DUE TO A #2 ENGINE STALL MESSAGE ACCOMPANIED BY A FADEC FAULT, LOUD POPS AND AIRCRAFT YAW. CORRECTIVE ACTION: PERFORMED BORESCOPE WITH NO DAMAGED NOTED. REPLACED T25 SENSOR AND ECU. PERFORMED HIGH POWER RUN, ALL PARAMETERS NORMAL. (LP 6488366)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 20,767 hrs · 9,725 cycles

SHIP 3015 CLIMBING THROUGH FLIGHT LEVEL 200 ON AP2 SLUTTER VIBRATION BEGAN. MILD FLUTTER CONTINUED THROUGH FL 260. NO INDICATIONS ON FLIGHT CONTROL PAGE. CLIMBING SPEED WAS 320KTS REDUCED TO 300 AND STILL FELT FLUTTER. CORRRECTIVE ACTION: R/R RT OB ELEVATOR SERVO CONTROL ACUATOR PER A321 AMM 27-34. OPS AND LEAK CHECK GOOD. (5523968)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 20,718 hrs · 9,707 cycles

SHIP 3015 CABIN PRESSURE DOOR LIGHTS REMAIN ILLUMINATED AFTER SHUTDOWN. CORRECTIVE ACTION: R/R CABIN PRESSURE DETECTION PRESSURE SWITCH PER A321 AMM 52-73-12 OPS CKS OK. (5523940)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 20,694 hrs · 9,698 cycles

SHIP 3015 REPAIR DOUBLER AT FWD ATG4 ANTENNA AREA, BETWEEN FR25 & FR26 NEEDS INSP. CORRECTIVE ACION: COMPLIED WITH ERA 604474-14AD. (0137106)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 20,271 hrs · 9,521 cycles

SHIP 3015 L1 DOOR DOES NOT SHOW CLOSED AFTER MULTIPLE ATTEMPTS. CORRECTIVE ACTION: FOUND LARGE FAKE FINGERNAIL IN DOOR LINKAGE. REMOVED. ALL OPS NORMAL NOW. (9188084)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 20,205 hrs · 9,488 cycles

SHIP 3015 AFTER GATE ARRIVAL PASSENGER REPORTED OXYGEN MASK AT DOOR 3L FELL DOWN. CORRECTIVE ACTION: RESECURED 3L DOOR PASSENGER EMERGENCY OXYGEN CONTAINER PER A321 AMM 25-21. OK FOR SERVICE. (9188050)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 17,906 hrs · 8,547 cycles

SHIP 3015 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE AT SEAT 17C. CORRECTIVE ACTION: INSTALL NEW ASSEMBLY. OK FOR SERVICE. (2679851)

Part: FITTING — CORRODED (FRM 66 S23L) · corrosion level 2 · airframe 17,160 hrs · 8,241 cycles

CORROSION FLOOR STRUCTURE CORNER FRAME 66 AT STRINGER 23LH AT AFT GALLEY AREA. REPLACED CORNER FRAME 66 AT STRINGER 23LH AT AFT GALLEY AREA ASPER A321 SRM 51-72-11 AND SRM 51-42-11 DUE TO NOT FOUND ALLOWABLE DAMAGE IN SRM MEASURES OF CORROSION ARE L=3.780 INCH, W=1.100 INCH.

Part: DOUBLER — CORRODED (FRM25-26 S43-44R) · airframe 17,160 hrs · 8,241 cycles

ELONGATED HOLE EXTERNAL SKIN DOUBLER REPAIR LOC. FR 25 TO FR 26 BTW STR 44 STR 43 R AT LOWER FUSELAGE. COMPLIED WITH ER/A 644474-14AD REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI 644474-14AD REV 1 IT HAS BEEN VALIDATED. PERFORMEDREPAIR INSTRUCTIONS EXTERNAL SKIN DOUBLER REPAIR LOC. FR 25 TO FR 26 BTW STR 44 STR 43 R AT LOWER FUSELAGE AS PER ER/A644474-14AD REV. ORIGINAL SECTION I HAS BEEN COMPLIED WITH.

Part: FITTING — CORRODED (FRM 68 S23R) · corrosion level 2 · airframe 17,160 hrs · 8,241 cycles

CORROSION FLOOR STRUCTURE CORNER FITTING ON FRAME 68 AT STRINGER 23RH AT AFT GALLEY AREA. REPLACED CORNER FITTING ON FRAME 68 AT STRINGER 23RH AT AFT GALLEY AREA AS PER A321 SRM 51-72-11 MEASURE OF CORROSION L= 1.022 IN W=0.665 IN.

Part: NONE — NONE (NONE) · airframe 17,175 hrs · 8,248 cycles

AMOC, ERA 604474-14AD. REPAIR AT EXTERNAL FUSELAGE SKIN, FR25-26 AND STRG43-44 REQUIRES AMOC FOR AD 2020-20-05. REVISE/UPDATE ERA 604474-14AD WITH AMOC TO AD 2020-20-05 RESULTS PRIOR TO 12,638 TOTAL FLIGHT CYCLES. ASSOCIATED ER/A 14-604474 ADDED FOR AC 3015. (LP# 2570680)

Part: NONE — NONE (NONE) · airframe 17,175 hrs · 8,248 cycles

DTE, ERA 604474-14AD, REPAIR AT EXTERNAL FUSELAGE SKIN, FR25-26 AND STRG43-44 REQUIRES DTE PRIOR TO 12/30/2023.REVISE/UPDATE ERA 604474-14AD WITH DTE RESULTS PRIOR TO 12/30/ 2023. ASSOCIATED ER/A 14-604474 ADDED FOR AC 3015. (LP# 2570671)

Part: SHEAR PLATE — CRACKED (FRMS 69-70) · airframe 17,160 hrs · 8,241 cycles

CRACK SHEAR PLATE BTW FR 69 TO FR 70 AT LEVEL FLOOR STRUCTURE AND AT L EVEL OF STR 23 R AT AFT GALLEY AREA. REPLACED SHEAR PLATE LOC BETWEEN FR 69 TO FR 70 AT LEVEL STR 23R FLOOR STRUCTURE AFT GALLEY AREA AS PER A321 SRM 51-72-11, SRM51 -42-11 AND DWG D53474180, RELEASE DATE 14-JUL-22, ISSUE Z. MEASURE OF CRACK IS L: 0.709 IN.

Part: FITTING — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 17,154 hrs · 8,238 cycles

CORROSION CENTER FITTING LOWER DOOR CUTOUT STR 23L AT AFT GALLEY AREA. REPLACED CENTER FITTING LOWER DOOR CUTOUT S23L AT AFT GALLEY AREA IAW SRM 51-72-11, AND DWG D53480505.

Part: STRUCTURE — CORRODED (FRM 66 S23R) · corrosion level 2 · airframe 17,154 hrs · 8,238 cycles

CORROSION FLOOR STRUCTURE CORNER FITTING FRAME 66 AND STRINGER 23RH AT AFT GALLEY AREA. REPLACED CORNER FITTING AND FASTENERS FRAME 66 AND STRINGER 23RH ON FLOOR STRUCTURE AT AFT GALLEY AREA AS PER A321 SRM 51-72-11AND DWG D53480505 RELEASE DATE 26/JAN/21 ISSUE: EV.

Part: SEAT TRACK — CORRODED (FRMS 20-23) · corrosion level 2 · airframe 17,154 hrs · 8,238 cycles

CORROSION SEAT TRACK -Y1292 BTW FR20 AND FR 23 FWD GALLEY AREA. REPLACED SEAT TRACK -Y1292 LOC. BTW FR 12 TO FR24 FWD GALLEY AREA AS PER A321 SRM 51-72-11-911-001 AND DWG D53135362 AND DWGD53212368 RELEASE DATE: 29-JAN-16 ISSUE: A00 AND RELEASE DATE: 14-MAY-15 ISSUE: C00. MEASURES OF CORROSION ARE L: 0.491 INW: 0.339 IN. TOOL USED DIGITAL CALIPER P/N: 500-197-30, S/N: 15120588, DUE DATE: 03/NOV/23. RII INSPECTION COMPLETE 0943462. (LP# 2539701)

Part: NONE — NONE · airframe 15,036 hrs · 7,322 cycles

EMERGENCY EXIT SIGNS INOPERATIVE. PERFORMED OPERATIONAL TEST OF THE EMERGENCY EXIT SIGNS PER A321 AMM 33-51-00-710-008 CKS NORMAL. (LP# 2197619)

Part: COMPUTER — FAILED (NR 2 MMR) · airframe 11,137 hrs · 5,547 cycles

ON DESCENT TO ATL, TOTAL FAILURE, FLIGHT PLAN DUMPED. UNABLE TO RELOAD ANYTHING, NO QRH PROCEDURE. PERFORMED RAW DATA ILS APPROACH TO ATL. CORRECTIVE ACITON: REMOVED AND REPLACED MMR2, PER A321 AMM 34-36. OPERATIONS CHECKS GOOD LAND CAT III TEST OK.

Part: FITTING — OUT OF TOLERANCE (R1 GIRT BAR) · airframe 10,631 hrs · 5,334 cycles

R1 DOOR FWD GIRT BAR FLOOR FITTING OUT OF CLEARANCE ON F2, PER AMM 52-11. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0223:5210-7089-RF/001 00202 ADJUSTED GIRT BAR FLOOR LATCH FITTING, PER AMM 52-11.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHT) · airframe 10,386 hrs · 5,222 cycles

EPSU 11WL EXT FAULTED BATTERY ON EMERGENCY LIGHT TEST. CORRECTIVE ACTION: RESET BATTERY PACK AND CYCLED AC PWR. ESPU SYS TEST OK.

Part: LIGHT — LOOSE (CABIN) · airframe 10,319 hrs · 5,198 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE, LOCATIONS: 31C. CORRECTIVE ACTION: SECURED LOOSE HARDWARE LIGHT OPS NML

Part: LIGHT — DETACHED (SEAT 37C) · airframe 10,319 hrs · 5,198 cycles

SEAT 37C LIGHT ON SEAT SIDE HANGING OFF. CORRECTIVE ACTION: RESECURED LIGHT AT 37C.

Part: LIGHT — DAMAGED (CABIN) · airframe 10,126 hrs · 5,105 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:37A, 37B AND 37C. CORRECTIVE ACTION: SECURED. OK FOR SERVICE

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 6,524 hrs · 3,517 cycles

AFT EMERGENCY LIGHTS INOP, REPLACED EMERGENCY BATTERYPACK 13WL

Part: SPAR — CRACKED (NR 2 NACELLE) · airframe 5,313 hrs · 2,977 cycles

#2 ENGINE PYLON- IB UPPER SPAR OF AFT FIXED FAIRING CRACKED, SEE NR FOR ADDITIONAL INFORMATION 068-0001:5450-01052-01B/001 00069 REPAIR OF AFT FIXED FAIRING WAS ACCOMPLISHED PER AA5450-01052-06B

Part: FAIRING — CRACKED (NR 1 NACELLE) · airframe 5,313 hrs · 2,977 cycles

#1 PYLON AFT. FIXED FAIRING CRACKED AT #15 RIB, SEE NR FOR ADDITIONAL INFORMATION 069-0001:5450-01052-01A/001 00043 REPAIR OF AFT FIXED FAIRING WAS ACCOMPLISHED PER AA5450-01052-06A

Part: LIGHT — UNSECURE (CABIN) · airframe 4,382 hrs · 2,550 cycles

EMERGENCY FLOOR LIGHTING DAMAGED AT SEAT 31C, RESECURED EMERGENCY EXIT.