N295NV
Registered owner: BANK OF UTAH TRUSTEE, UT (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) (DEFECT DISCOVERED DURING THE AC HEAVY MX VISIT) NRC 6000-0017: 33284-017. RT WING TRAILING EDGE, RIBLET BETWEEN RIB 21 AND RIB 22 (OUTBRD OF SPOILER #5 ACTUATOR) CORRODED / RT WING TRAILING EDGE , RIBLET BETWEEN RIB 21 AND RIB 22 (OUTBRD OF SPOILER#5 ACTUATOR) REPLCED AS PER SRM 51-72-11-911-001 RV.157.PN: D5754171120100 PO:4393031.C/W.
(AIRCRAFT NOT GROUNDED) (EMERGENCY DECLARED) AIR ENG 1 BLEED FAULT, ENG BLEED RESET UNSUCCESSFUL. FOLLOWING TSM 36-11-00-810-809-A, ACCOMPLISHED LEAK CHECKS OF SENSE LINES 3, 4, AND 2 IAW AMM 36-11-00-720-010, AMM 36-11-00-720-011 AMM 36-11-00-720-09, NO DEFECTS NOTED. REMOVED AND REPLACED PRV CONTROL SOLENOID IAW AMM 36-11-55-000-001-A AND 36-11-55-400-001-A.
(AIRCRAFT NOT GROUNDED) DURING CRUISE, FL 340, AFT FA'S REPORTED SOUR MILK SMELL AT LEAST 4 TIMES DURING CRZ. W/ EYE IRRIATITION. LOCATION L2 DOOR / REF WO# 526976 NRC 22814-1 FOR REPLACEMENT OF APU FUEL CONTROL UNIT DUE TO PHASE 2 ODOR EVENT TASK CARD. NO FURTHER LEAKS NOTED. PERFORMED GVI OF ENG FOR OIL LEAKS NO SIGNIFICANT LEAKS FOUND IAW AMM 12-13-79-610-002-A. NOTICED OIL CAP O-RING SLIGHLY WORN & LOOSE. REPLACED O-RING IAW AMM 79-11-10-300-003-A. A/C OK FOR SERVICE. OIL CONSUMPTION WITHIN LIMITS IAW AMM 72-00-00-200-008-A.
(AIRCRAFT NOT GROUNDED) FLIGHT ATTENDANT REPORTS EXIT SIGN OVERWING LEFT DID NOT ILLUMINATE WHEN LANDING. / PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-16-400-001-A."
(AIRCRAFT NOT GROUNDED) DURING WEEKLY CHECK, FOUND OVERHEAD EMERGENCY LIGHT BETWEEN ROWS 26-27 INOP. / PERFORMED WIRE CHECKS OF LIGHT 206WL PER AWM 33-51-02. CONFIREMED CONTINUITY FROM PIN 3 TO ESPU PIN E. WHILE CHECKING FOR GROUND AT PIN 1 OF LIGHT, READING WAS INTERMITTENT. FOUND GROUND AT 7262VN LOOSE. TIGHTENED AS REQUIRED OPS CHECK OF LIGHT GOOD REF AMM 33-51-20-710-001A. THIS CLEARS MEL 33-50-02B DMI# 203914. INOP PLACARDS REMOVED.
(AIRCRAFT NOT GROUNDED) CAB PR SAFETY VALVE OPEN ECAM, AP8.1PSI AT 37,000FT / PERFORMED OPS TEST IAW AMM 31-60-00-860-001A. OPS CHECK GOOD. NO OTHER DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE. PER TSM 21-31--00-040-005A. "
DURING ALLEGIANT INSPECTION AS PER TASK ZL-471-01-4001 ON BOTTOM SKIN REINFORCEMENT PLATE AND SKIN CLOSE TO LH PYLON AREA TWO SMALL AREAS WITH CORROSION WERE FOUND. THIS KIND OF DAMAGE IS NOT COVERED BY SRM MANUAL , DAMAGES DETAILS WERE SENT TO AIRBUS ASKING FOR PERMANENT REPAIR INSTRUCTIONS. AIRBUS PROVIDED RESPONSE WITH REPAIR INSTRUCTIONS. THE REPAIR WAS SUCCESFULLY PERFORMED AND COVERED WITH COOPESA EO COO-EO-2024-20443-R00 REV 00.THIS REPAIR IS CONSIDERED MAJOR AND PERMANENT AND WAS DOCUMENTED UNDER COOPESA JOB A1P200 ITEM 4-17.
DURING ALLEGIANT INSPECTION AS PER TASK ZL-471-01-4002 ON BOTTOM SKIN REINFORCEMENT PLATE AND SKIN CLOSE TO RH PYLON AREA TWO SMALL AREAS WITH CORROSION WERE FOUND. THIS KIND OF DAMAGE IS NOT COVERED BY SRM MANUAL , DAMAGES DETAILS WERE SENT TO AIRBUS ASKING FOR PERMANENT REPAIR INSTRUCTIONS. AIRBUS PROVIDED RESPONSE WITH REPAIR INSTRUCTIONS. THE REPAIR WAS SUCCESFULLY PERFORMED AND COVERED WITH COOPESA EO COO-EO-2024-20441-R00 REV 00. THIS REPAIR IS CONSIDERED MAJOR AND PERMANENT AND WAS DOCUMENTED UNDER COOPESA JOB A1P200 ITEM 4-16.
(AIRCRAFT NOT GROUNDED) REF: NRI 5-13 - M313 SUBMITTED FOR. ENGINE #1, LEFT WING, BOTTOM SKIN LOWER SURFACE, AT RIB 7 AND STRINGER 6. / PERFORMED BLEND OUT & INSTALLED OVERSIZE HI-LOK I.A.W. AIRBUS RDAF REF. & ISSUE: 81434230/2024#A WITH NRI 4-17.
(AIRCRAFT NOT GROUNDED) REF: NRI 5-14 - M313 SUBMITTED FOR. ENGINE #1, LEFT WING, BOTTOM SKIN PYLON REINFORCING PLATE, LOWER SURFACE, AT RIB 8 AND STRINGER 5. / PERFORMED BLEND OUT & INSTALLED OVERSIZE HI-LOK I.A.W. AIRBUS RDAF REF. & ISSUE: 81434230/004/2024#A WITH NRI 4-17.
(AIRCRAFT NOT GROUNDED) DURING TC 335100-03-1-001 RECEIVED EPSU (12WL) BATTERY FAULT / REMOVED AND REPLACED EPSU BATTERY (12WL) PER AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPERATIONAL CHECK SATISFACTORY."
EMER LIGHT TEST FAILED FOR EPSU BATTERY (10WL) / R/R EPSU BATTERY IAW AMM 33-51-38-400-002-A. OPS CHECK GOOD.
BAT/EPSU(13WL)AFT L / R&R EPSU BATTERY,FIN LOCATION 13WL AFT IAW AMM REF 33-51-38-000-002-A AND 33-51-38-400-002-A.OPS CHECK PERFORMED,OPS CHECK GOOD."
AFT MEGAPHONE INOP. / REPLACED AFT MEGAPHONE IAW LOPA DRAWING NO A2250007L01."
DURING BATTERY CHECK IAW ALLEGIANT TASK 335100-03-1-001 RH EMERGENCY EXIT EPSU BATTERY FAILED. DUE THIS CONDITION THE RH EMERGENCY EXIT EPSU BATTERY WAS REPALCED IAW A320 AMM TASK 33-51-38-000-002-A AND 33-51-38-400-002-A REV 39 DATED 02-01-2023. AFTER THE SYSTEM TEST WAS FOUND OK. THIS WORK IS COVERED BY COOPESA JOB A1N117 ITEM 2-13.
DURING ALLEGIANT TASK 534195-01-2-001 ON PASS CABIN FROM FR67+380MM TO FR68+100MM AND Y-1230 MM SILL WEB WITH CORROSION WAS FOUND. COOPESA PERFORMED REPAIR ON RH AFT PASS CREW DOOR SILL BEAM IN ACCORDANCE A320 SRM TASK 53-41-14-300-001 PARAG 2A FIG 001 SHEETS 3 REPAIR PRINCIPLE # 5. THIS REPAIR IS COVER WITH COOPESA JOB A1N117 ITEM 2-35.
DURING ALLEGIANT TASK 532180-01-2-001 FWD CARGO COMPARTMENT STRINGER 43RH WITH CORROSION WAS FOUND. COOPESA PERFORMED REPAIR IN ACCORDANCE A320 SRM TASK 53-21-13-300-018 PARAG 2A FIG 001 SHEETS 3,4 AND 5. THIS REPAIR IS COVER WITH COOPESA JOB A1N117 ITEM 1-34.
DURING ALLEGIANT TASK 534143-01-3-001 ON PASS CABIN FROM FR66+40MM TO FR66+150MM AND Y+1420 MM SILL WEB WITH CORROSION WAS FOUND. COOPESA PERFORMED REPAIR ON LH AFT PASS CREWDOOR SILL BEAM IN ACCORDANCE A320 SRM TASK 53-41-14-300-001 PARAG 2A FIG 001 SHEETS7 REPAIR PRINCIPLE # 11. THIS REPAIR IS COVER WITH COOPESA JOB A1N117 ITEM 2-40
DURING ALLEGIANT TASK 534195-01-2-001 ON PASS CABIN FROM FR67+450MM TO FR68+150MM AND Y+1230 MM SILL WEB WITH CORROSION WAS FOUND. COOPESA PERFORMED REPAIR ON LH AFT PASS CREW DOOR SILL BEAM IN ACCORDANCE A320 SRM TASK 53-41-14-300-001 PARAG 2A FIG 001 SHEETS 3REPAIR PRINCIPLE # 5. THIS REPAIR IS COVER WITH COOPESA JOB A1N117 ITEM 2-38
DURING THE AIRCRAFT INSPECTION AS PER ALLEGIANT TASK , IT WAS FOUND CORROSION ON REINFORCEMENT CASE TRAIN DOUBLERNLG BETWEEN FR20 - FR21 AND Y175 AND Y-175. DUE TO THE DAMAGE IS BEYOND SRM ADL LIMITS,AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS AND FINAL APPROVAL .AIRBUS PROVIDEDREPAIR INSTRUCTIONS UNDER TD TD/81250072/014/2023#A AND RDAF 81250072/005/2023#A .THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1N117 ( ITEM 1-82).
EPSU BATTERY AT 11WL FAILED OPS CHECK PERFORMED AS PER WEEKLY CHECK. / REMOVED AND REPLACED EPSU BATTERY AT 11WL IAW A320 AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CHECK GOOD, OK FOR SERVICE."
FWD MEGAPHONE INOP. / REPLACED FWD MEGAPHONE IAW LOPA DRAWING NO A2250013L03."
L1 DOOR OVERHEAD EMER LIGHT COVER BROKEN. REMOVED AND REMOVED EMER LIGHT ASSY IAW AMM 33-51-11-000-001 AND 33-51-11-400-001, OPS CHECK GOOD AT THIS TIME.
DURING OPERATIONAL TEST OF THE EMERGENCY LIGHT BAT/EPSU FWD L FAILED (10WL). / REMOVED AND REPLACED FWD L EPSU BATTERY FIN 10WL IAW AMM 33-51-38-00-002-A AND 33-51-38-400-002-A. OPS CHECK GOOD AT THIS TIME IAW AMM 33-51-00-710-001-A."
BAT/EPSU (12WL) EMER R FAULT ON EPSU TEST. / REMOVED AND REPLACED 12WL EPSU BATTERY PER AMM 33-51-38. OPS TESTS GOOD, NO FURTHER FAULTS."
BAT/EPSU (13WL) AFT L FAULT ON EPSU TEST. / REMOVED AND REPLACE 13WL EPSU BATTERY PER AMM 33-51-38. OPS TESTS GOOD, NO FURTHER FAULTS."
EMERGENCY LIGHT SECOND FROM AFT INOP. / TIGHTENED THE GROUND ON EMERGENCY LIGHT IAW ESPM 20-44-10."