N279NV

Part: SLIDE — UNWANTED DEPLOY (ZONE 800) · airframe 36,335 hrs · 23,647 cycles

(AIRCRAFT NOT GROUNDED) R1 DOOR SLIDE DEPLOYED. R & R R1 DOOR SLIDE IAW AMM 25-62-44-400-803-A"

Part: ELEC CONNECTOR — DISCONNECTED (ZONE 200) · airframe 35,755 hrs · 23,335 cycles

(AIRCRAFT NOT GROUNDED) DURING SERVICE CHECK, FOUND LOWER EMEGENCY LIGHT ON R2 DOOR INOP / FOUND ELECTRICAL CONNECTORS TO R2 DOOR WALL MOUNTED EMERGENCY EXIT MARKER NOT CONNECTED CONNECTED ELECTRICAL CONNECTORS TO R2 DOOR WALL MOUNTED EMERGENCY EXIT MARKER ASSEMBLY IAW A320 AMM 33-51-13-400-001-A OPS CHECK GOOD "

Part: OIL SYSTEM — LEAKING (APU) · airframe 35,697 hrs · 23,311 cycles

(AIRCRAFT NOT GROUNDED) DURING DESCENT ALL CREWMEMBERS DETECTED DIRTY SOCK ODORS. REF LP 1967836. REPLACED FCU PER AMM 49-32-11-000/400-003-A. LEAK CHECK GOOD. NO LEAKS NOTED AT THIS TIME. PER TC 21-000-001 LEVEL 2 DUE. (RESOLVED ON W/O: 525871 TASKCARD: NR-00001 ) W/O 21-000-002. RAN APU IAW AMM 49-00-00-710-010-A. DURING RUN FOUND OIL LEAKING IN THE INTERNAL SIDE OF THE INTAKE.PICTURES SUBMITTED TO TSR-1749. VIDEOS HAVE BEEN ALSO SUBMITTED ON TSR 1749. THIS MEL 49-10-01-A. PERFORMED APU CLEANING IAW AMM 49-00-00-100-003-A. PERFORMED LEAK CHECK, FOUND OIL COOLER LEAKING. REMOVED AND REPLACED APU OIL COOLER PER AMM 49-91-44-000-001A AND 49-91-44-400-001A. OPS/LEAK CHECK GOOD.

Part: LIGHT — NO TEST (ZONE 200) · airframe 35,661 hrs · 23,290 cycles

(AIRCRAFT NOT GROUNDED) TC 335100-03-1-001 CABIN EMERGENCY LIGHTING TEST FAILED. REMOVED AND REPLACED EPSU REF WO524847.

Part: FUEL CONTROL — LEAKING (APU) · airframe 35,632 hrs · 23,278 cycles

(AIRCRAFT NOT GROUNDED) FLIGHT ATTENDANT REPORTS DIRTY SOCK SMELL AT 18,000 FEET IN DECENT. / TC 21-000-001 ACCOMPLISHED, FOUND AND CLEANED OFF OIL AROUND INLET OF APU PLENUM AND EDGE OF INLET SCREEN. RAN BOTH PACK INDIVIDUALLY WITH APU, ENG 1, AND ENG 2 SEPARATELY, UNABLE TO DUPLICATE ODOR. (RESOLVED ON W/O: 525103 TASKCARD: NR-00001 ) C/W TC 21-000-002, NO EXTERNAL LEAKS FOUND, HAVE NOTED A LEAK FROM INLET OF THE APU AT THIS TIME. NO PARTS REPLACED AT THIS TIME. APU REMAINS ON DEFERRAL. C/W TC 21-000-003. APU FCU - FUEL CONTROL UNIT LEAKING. REMOVED AND REPLACED APU FCU (FUEL CONTROL UNIT) IAW AMM 49-32-11-000-003-A, 49-32-11-400-003-A, PASSED LEAK CHECK IAW 49-00-00-710-010.

Part: HINGE FITTING — DAMAGED (RT ELEVATOR) · airframe 35,332 hrs · 23,103 cycles

(AIRCRAFT GROUNDED) (DISCREPANCY NOTED DURING AIRCRAFT HEAVY MX VISIT) RH ELEV ATOR ASSY, HINGE FITTING #5 OUTB HOLE ELONGATED / RH EVEVATOR ASSY PIN: D5528000200334P S/N: JC7561, HINGE FITTING #5 OUTB HOLE PERMANENTLY REPAIRED AS PER SRM 55-26-41-300-004 REV.! 50. REPAIR CATEGORY B, SEE SRI 55-26-41-205-001 REV.150 FOR INSPECTION REQUIREMENTS, INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT: 6 YEARS, SUBSEQUENT INSPECTION AT INTERVALS OF: 6 YEARS, NDT INSPECTION TYPE: DETAILED INSPECTION, REMARK: MRBR TASK 55002-01-1. SEE TASK 552600-01-1-002 FOR RH ELEVATOR REMOVAL AND REINSTALLATION."

Part: HINGE FITTING — DAMAGED (RT ELEVATOR) · airframe 35,332 hrs · 23,103 cycles

(AIRCRAFT GROUNDED) (DISCREPANCY NOTED DURING AIRCRAFT HEAVY MX VISIT) RH ELEV ATOR ASSY, HINGE FITTING #2 !NB HOLES ELONGATED / RH EVEVATOR ASSY PIN: D5528000200334P SIN: IC756I, HINGE FITTING #2 INBD HOLE PERMANENTLY REPAIRED AS PER SRM 55-26-41-300-004 REV, I 50. REPAIR CATEGORY B, SEE SRI 55-26-4I-205-00I REV.I50 FOR INSPECTION REQUIREMENTS, INSPECTION THRESHOLD FROM COMPONENT FIRST FLIGHT: 6 YEARS, SUBSEQUENT INSPECTION AT INTERVALS OF: 6 YEARS, NOT INSPECTION TYPE: DETAILED INSPECTION, REMARK: MRBR TASK 55002-0I-L. SEE TASK CARD 552600-01-1-002 FOR RH ELEVATOR REMOVAL AND REINSTALLATION, "

Part: STRINGER — CORRODED (ZONE 100) · airframe 33,801 hrs · 22,428 cycles

DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 533152-01-7-001 ON STRINGER 41 LH AT FR33+230MM SPOT CORROSION WAS FOUND. THE STRINGER WAS REPAIRED FOLLOW THE REPAIR INSTRUCTIONS IAW A320 SRM 53-21-13-300-018 FIG 001. THIS IS A PERMANENT REPAIR CAT B AND MUST BE INSPECTED IAW A320 SRM 53-21-13-205-018 TABLE 1.THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1P182 ITEM 1-25.

Part: BATTERY — FAILED (ZONE 200) · airframe 33,801 hrs · 22,428 cycles

DURING EMERGENCY POWER SUPPLY CHECK IAW ALLEGIANT TASK 335100-03-1-001 AFT ENTRY AREA EPSU 13WL FAILED. THE EMERGENCY POWER SUPPLY UNIT 13WL WAS REPLACED IAW A320 AMM 33-51-38-000-001-A AND 33-51-38-400-001-A REV 44 DATE 05-01-2024, THE NEW PART PASS THE TEST. EPSU P/N ON 3214-31 S/N ON 946042.

Part: BULKHEAD — CORRODED (ZONE 100) · airframe 33,801 hrs · 22,428 cycles

DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 533152-01-7-001, FR 35 BULHEAD FWD FACE LOWER CHORD BETWEEN STGR 38 LH/43 RH WITH (2EA) SPOT CORROSION WAS FOUND.DUE THE DAMAGE IS BEYOND SRM LIMITS TO REPAIR AIRBUS WAS CONTACTED ASKING FOR REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND BOTH AFFECTED AREAS WERE REPAIRED IAW COOPESA ENGINEERING ORDER # COO-2024-20423-R00. THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1P182 ITEM 1-22.

Part: BATTERY — FAILED (ZONE 200) · airframe 33,801 hrs · 22,428 cycles

AIRCRAFT NOT GROUNDED) REF: NRI 2-10 - UPPER FUSELAGE AFT ENTRY AREA EPSU (13WL) BATTERY FAILED. REPLACED UPPER FUSELAGE AFT ENTRY AREA EPSU BATTERY (131WL), IAW AMM TASK 33-51-38-000-002-A AND 33-51-38-400-002-A, REV 44, DATED: 05/01/2024. A1P182 2-10.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 32,629 hrs · 21,919 cycles

DURING OPS CHECK ON EPSU FOUND 11WL AND 12WL FLAGGING FOR EXTERIOR EMERGANCY LIGHTS AND 11WL AND 12WL EPSU PANEL STILL OPEN / REMOVED AND REPLACED EMERGENCY OVERWING LIGHTBULBS AT 62WL AND 63WL REF AMM 33-51-15-000-001-A AND AMM 33-51-15-400-001-A.CLOSED EPSU PANELS 241KW AND 242KW REF AMM 25-23-44-400-001"

Part: EPSU — NOT ENTERED (NOT ENTERED) · airframe 30,990 hrs · 21,104 cycles

DURING WEEKLY CHECK FOUND EPSU 11WL FAILED / REMOVED, REPLACED AND OPS CHECKED 11WL PER AMM 33-51-38-000-001-A AND 33-51-38-400-001-A NO FURTHER DEFECTS NOTED"

Part: BATTERY — INOPERATIVE · airframe 30,668 hrs · 20,973 cycles

DURING OPS TEST OF THE EMERGENCY LIGHTS RECIEVED BAT/EPSU (13WL) AFT L CLASS 1 FAULT MESSAGE / R+R EPSU BATTERY AT 13WL IAW AMM 33-51-38-400-002-A OPS CHECK GOOD"

Part: BATTERY — INOPERATIVE · airframe 30,668 hrs · 20,973 cycles

DURING OPS TEST OF THE EMERGENCY LIGHTS RECIEVED BAT/EPSU (10WL) FWD L CLASS 1 FAULT MESSAGE / R+R EPSU BATTERY AT 10WL IAW 33-51-38-400-002-A OPS CHECK GOOD"

Part: BATTERY — INOPERATIVE · airframe 30,668 hrs · 20,973 cycles

DURING OPS TEST OF THE EMERGENCY LIGHTS RECIEVED BAT/EPSU (11WL) EMER L CLASS 1 FAULT MESSAGE / R/R EPSU 11WL BATTERY IAW AMM 33-51-38-000/400-002-A. CHECKS GOOD"

Part: EPSU — FAILED · airframe 29,748 hrs · 20,515 cycles

EPSU BATTERY EMER R(12WL) FAILED CAPACITY TEST / REMOVED AND REPLACED EPSU BATTERY EMER R(12WL) PER A320 AMM 33-51-38PB401. OPS CHECK GOOD."

Part: EPSU — FAILED INSP (12WL) · airframe 28,512 hrs · 19,930 cycles

DURING CABIN LIGHTING TEST FOUND EPSU BATTERY FAILED AT 12WL. / REPLACED EPSU BATTERY AT 12WL - REF AMM 33-51-28-000-002/400-002. OPS TEST GOOD."

Part: COMPUTER — FAULTED (NR 2 ELAC) · airframe 26,829 hrs · 19,086 cycles

(EMERGENCY DECLARED) F CONTROL ELAC 2 PITCH FAULT ECAM MESSAGE DEPARTING KVPS // CORRECTIVE ACTION PENDING"

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 25,875 hrs · 18,555 cycles

MID LEFT EPSU BATTERY FAULTED. REMOVED AND REPLACED MID LEFT EPSU BATTERY. OPERATIONS CHECK GOOD W/REF TO AMM 33-51-00 PB 001.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 25,875 hrs · 18,555 cycles

FWD EPSU BATTERY FAULTED. REMOVED AND REPLACED FWD EPSU BATTERY. OPERATIONS CHECK GOOD W/REF TO AMM 33-51-00 PB 001.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 25,875 hrs · 18,555 cycles

AFT EPSU BATTERY FAULTED. REMOVED AND REPLACED AFT EPSU BATTERY. OPERATIONS CHECK GOOD W/REF TO AMM 33-51-00 PB 001.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 23,925 hrs · 17,502 cycles

EXIT SIGN LOWER FELL OFF NEAR L1 DOOR / R/R EXIT LIGHT COVER PER AMM 33-51-13. NO OTHER DEFECTS NOTED AT THIS TIME."

Part: HMU — MALFUNCTIONED (NR 1 ENGINE)

(RESUBMITTED WITH FINAL CORRECTIVE ACTION - EMERGENCY DECLARED - IFSD) ECAM: ENG 1 COMPRESSOR VANE FAULT FOLLOWED BY ENG FAILURE. R&R DAMAGED HMU & J8 HARNESS"

Part: SLIDE — DEPLOYED (R2 DOOR)

R2 SLIDE DEPLOYED. R&R R2 DOOR SLIDE"

Part: SUPPORT — CORRODED (FWD CARGO BAY)

FWD CARGO COMPARTMENT AFT BULKHEAD LOWER PROFILE PANEL SUPPORT CORRODED/R&R FWD CARGO AFT BULKHEAD PROFILE"