N279NV
Registered owner: ALLEGIANT AIR LLC, NV (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
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
(AIRCRAFT NOT GROUNDED) 13WL EPSU BATTERY REQUIRES REPLACEMENT FAILURE ON EPSU CAP TEST AND SYS TEST. REMOVED AND REPLACED EPSU 13WL BATTERY IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPERATIONAL TEST SATISFACTORY."
(AIRCRAFT NOT GROUNDED) R1 DOOR SLIDE DEPLOYED. R & R R1 DOOR SLIDE IAW AMM 25-62-44-400-803-A"
(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 "
(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.
(AIRCRAFT NOT GROUNDED) TC 335100-03-1-001 CABIN EMERGENCY LIGHTING TEST FAILED. REMOVED AND REPLACED EPSU REF WO524847.
(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.
(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, "
(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."
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.
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.
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.
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.
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"
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"
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"
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"
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"
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."
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."
(EMERGENCY DECLARED) F CONTROL ELAC 2 PITCH FAULT ECAM MESSAGE DEPARTING KVPS // CORRECTIVE ACTION PENDING"
FWD EPSU BATTERY FAULTED. REMOVED AND REPLACED FWD EPSU BATTERY. OPERATIONS CHECK GOOD W/REF TO AMM 33-51-00 PB 001.
MID LEFT EPSU BATTERY FAULTED. REMOVED AND REPLACED MID LEFT EPSU BATTERY. OPERATIONS CHECK GOOD W/REF TO AMM 33-51-00 PB 001.
AFT EPSU BATTERY FAULTED. REMOVED AND REPLACED AFT EPSU BATTERY. OPERATIONS CHECK GOOD W/REF TO AMM 33-51-00 PB 001.
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."
(RESUBMITTED WITH FINAL CORRECTIVE ACTION - EMERGENCY DECLARED - IFSD) ECAM: ENG 1 COMPRESSOR VANE FAULT FOLLOWED BY ENG FAILURE. R&R DAMAGED HMU & J8 HARNESS"
R2 SLIDE DEPLOYED. R&R R2 DOOR SLIDE"
FWD CARGO COMPARTMENT AFT BULKHEAD LOWER PROFILE PANEL SUPPORT CORRODED/R&R FWD CARGO AFT BULKHEAD PROFILE"