N328NV
Registered owner: SUNRISE ASSET MANAGEMENT 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) (ATC DECLARED EMERGENCY) SIGNIFICANT ODOR PASSING THROUGH 16,00 ON DESCENT NORMAL AIR CONFIGURATION. USED CREW OXY AND PERFORMED ODOR QRH PROCEDURE. SMELL REMAINED PERSISTENT IN FLIGHT. SLIGHT DISSIPACTION ON GROUND. ACRID/MELTING PLASTIC SMELL NOTED BY CREW AT GATE IN FLIGHT DECK ONLY. / NOTE: NO ECAM FAILURES, NO CIRCUIT BREAKERS OPENED. INSP AEVC SYSTEM FOR ODORS, INSP SEPERATE SYSTEM BOXES INCLUDING THE FUSELAGE MOUNTED SYSTEM BOXES. FOUND RADAR RT HAS SIMULAR ODOR. (REF INBOUND DISCREPANCY LOG PAGE 2108101 RADAR ISSUE). REPLACED RT (1SQ1) PER AMM 34-41-33 AND EXTRACT FAN (18HQ) PER AMM 21-26-51. ALSO, OTHER SYSTEM CHECKS RELATED TO EVENT PERFORMED THIS MX VISIT.
(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING THE AC HEAVY MX VISIT) NRC 2000-0003: AFT LAVATORY TOILET CORRODED. AFT LAVATORY TOILET REPLACED IAW AMM 38-31-41-400-001. SEE AWS FOR DETAIL.
(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING THE AC HEAVY MX VISIT) NR-00058 CORROSION ON PROFILE LOCATED AT FR 59, BTW STGR 35LH - STGR 38LH, FT CARGO COMPARTMENT. REPLACED LOCATED AT FR 59, BTW STGR 35LH - STGR 38LH, FT CARGO COMPARTMENT AS PER SRM 51-72-11-911-001 REV 157.
DURING THE EXECUTION OF ALLEGIANT WORK CARD A32X-25-127-003_P1-OP-UP-LFNDT/001 AT THELOWER FUSELAGE, AVIONICS COMPARTMENT, ELECTRONICS RACK FIN 80VU RH LATERAL LOWER FITTING WITH ELONGATE HOLE. PER CUSTOMER EO A32X-STRG-25-EO-00203 REV 01 AND 2023-05-14, 80VU RACK ATTACHMENT-INSPECTION/REPAIR ACCOMPLISHED.
(AIRCRAFT NOT GROUNDED) FA REPORTS PREFLIGHT OF FWD MEGAPHONE WAS NEGATIVE. REPLACED BATTERIES FOR FOREWARD MEGASPHONE OP'S CK GOOD IAW AMM 25-65-51-02"
(AIRCRAFT NOT GROUNDED) EPSU (12WL)(13WL) FAILED DURING EPSU BAT CAP TEST. REMOVED AND REPLACED EPSU 12WL AND 13WL REF AMM 33-51-38-400/000-001-A"
(AIRCRAFT NOT GROUNDED) SMOKE: LAVATORY DET FAULT ECAM IN FLIGHT FA REPORTS AFY LAV DET INOP. / RESET LAV SMOKE DEU B IAW AMM 26-17-00-710-001. OPS CHECKS GOOD."
(AIRCRAFT NOT GROUNDED) FAILED EMG LIGHTS OPS TEST FOR POSITION 11WL / REMOVED AND REPLACE EPSU REF WO52565.
(AIRCRAFT NOT GROUNDED) EPSU FAILED TEST / REMOVED AND REPLACED EPSU REF WO521616. W0 521616 COMPLIED W/ AWR COMPLETED IAW GMM CH 2 SEC 6"
(AIRCRAFT NOT GROUNDED) DURING DESCENT AT 10,000 FT AT CHIME (10,000 CHIME) VARIOUS EXIT SIGN LIGHTS REMAIN ON, THIS TIME ROW 12/14 ""EXIT"" REMAIN ON, RECYCLED PER FCOM(PRO-NOR-SOP-18) THE EMERGENCY LIGHT SWITCH TO TURN THESE LIGHTS OFF. (2 FLIGHTS IN A ROW) / PERFORMED EPSU TEST IAW TSM 33-51-00-810-823-A, OPS TEST GOOD. ALSO PERFORMED VISUAL CHECK OF CABIN EMERGENCY LIGHT SYSTEM IAW AMM 33-51-00-710-009. ALL LIGHTS OPERATIONAL. NO DISCREPANCIES AT THIS TIME."
(AIRCRAFT NOT GROUNDED) EXIT EMERGENCY LIGHTS REMAIN ON WITH NO POWER ON THE AIRCRAFT & WITH EMERGENCY LIGHT SWITCH OFF (BATTERY OFF & NO MX SWITCH ON). PERFORMED OPS TEST OF CABIN EMERGENCY EXIT LIGHTING IAW AMM 33-51-11-710-050-A CHECKS GOOD. A/C OK FOR SERVICE.
EPSU BATTERY AFT L 13WL FAILED ON EPSU BAT CAP TEST / REMOVED AND REPLACED EPSU BATTERY 13WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A."
FWD MEGAPHONE DOES NOT EMIT SOUND / REMOVED AND REPLACED FWD MEGAPHONE IAW AMM 25-65-51-710-002, OPS CHECK GOOD"
DURING THE ACCOMPLISHMENT OF ALLEGIANT WORK CARD NO: 53-240-001 WHICH IS RELATED TO SB A320-53-1258 AND AD2020-02-20, 2 FASTENERS HOLES WERE FOUND CRACKED, AS REQUESTED IN THE FLOW CHART OF THE ISB 53-1258, WE PERFORMED THE REPAIR INSTRUCTIONS AS PER R.I R53370494 ISSUE C .AIRBUS WAS CPNTCTED FOR FURHTER INSTRUCTIONS.AIRBUS CONFIRM THAT SB A320 53-1251 MUST BE EMBODIMENT . DUE DEVIATION DURING SB EMBODIMENT NEW REQUEST WAS SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL.AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER DOSSIER 81337747. THIS REPAIR WAS PERFORMED FOLLOW THE REPAIR INSTRUCTIONS HEREIN COOPESA EO COO-EO-2024-19237-R00. THE REPAIR IS COVER BY COOPESA JOB A1P011 ITEM 2-19.
DURING MAINTENANCE AT COOPESA MRO CORROSION WAS REPORTED ON AFT CARGO COMPARTMENT SHEAR PLATES AT STGR-38RH AND FR52-FR60. COOPESA ASSESSED THE DAMAGE AND COORDINATED A REPAIR WITH AIRBUS VIA TECH REQUEST DOSSIER 81044409. AIRBUS ISSUED A REPAIR APPROVAL BY MEANS OF RDAF REF & ISSUE 81044409/004/2022#A AND BASED ON TD/81044409/009/2022#C. THE APPROVED REPAIR PROCEDURE IS CAPTURED IN COOPESA EO # COO-EO-2023-15305 R03.
DURING INSPECTION AT COOPESA MRO COORSION WAS REPORTED AT AFT CARGO COMPARTMENT STGR 42RH BETWEEN FR57-FR59 AND STGR43LH BETWEEN FR56-FR58 COOPESA ASSESSED THE DAMAGE AND COORDINATED A REPAIR WITH AIRBUS VIA TECH REQUEST DOSSIER # 810422127. AIRBUS ISSUED A REPAIR APPROVAL BY MEANS OF RDAF REF 81042127/004/2022#A AND BASED ON AIRBUS TD/81042127/008/2022# A INSTRUCTIONS. THE APPROVED REPAIR PROCEDURE IS CAPTURED IN COOPESA EO # COO-EO-2022-15280.
AFT CARGO COMPARTMENT FROM FR47/51 TO FR65 BETWEEN 38LH AND 38RH NUT PLATES RUSTY AT SEVERAL PLACES WAS FOUND.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND DAMAGE WAS REPAIRED IAW COOPESA EO COO-EO-2022-15305-R03 AND THE AIRBUS REPAIR INSTRUCTIONS TD/81044409/009/2022#C AND RDAF81044409/004/2022#A.
BATTERY/EPSU (13WL) AFT L FAILED / R&R EPSU BATTERY IAW AMM REF 33-51-38-000-002-A AND 33-51-38-400-002"
EMG LIGHT OPS TEST FAILED 12WL LOCATION. / REMOVED AND REPLACED BATTERY ON ESPU AT 12WL I.A.W MM 33-51-38-000-001-A AND MM 33-51-38-400-001-A. OPS CHECKED GOOD I.A.W MM 33-51-00-710-001-A."
EPSU 10WL BATTERY FAILED CAPACITY TEST / REMOVED AND REPLACED EPSU BATTERY AT 10WL IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK GOOD."
DURING THE STRUCTURAL INSPECTION PER ALLEGIANT MPD TASK CARD 574107-01-1- 001_P1-OP-UP-/010, IT WAS FOUND ON AFT CARGO COMPARTMENT, INTERCOSTALS WITH CORROSION. DUE TO THIS FACT, DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL UNDER AIRBUS DOSSIER 81044409 AND COOPESA'S ENGINEERING ORDER COO-EO-2022-15305 REV 03 .
DURING THE STRUCTURE INSPECTION PER ALLEGIANT TASK CARD 534147-01-2, IT WAS FOUND REAR FUSELAGE FROM FR68-150MM TO FR68+160MM , Y+1250 SILL WEB WITH CORROSIÃN WORK PERFORMED: PERFORMED PERMANENT REPAIR AT SILL WEB Y+1250 BETWEEN 220MM FWD OF FR68 AND FR 68 AND BETWEEN FR68 AND 150MM AFT OF FR 68 IAW SRM REPAIR TASK 53-41-14-300-001 FIGURE 001 REPAIR PRINCIPE 7 AND 8 , REPAIR CATEGORY A
DURING THE STRUCTURE INSPECTION PER ALLEGIANT TASK CARD 534107-01-1-001, IT WAS FOUND AFT COMPARTMENT BETWEEN FR64 AND FR65, STRG 42RH WITH CORROSION. WORK PERFORMED: PERFORMED PERMANENT REPAIR IN AFT CARGO COMPARTMENT BETWEEN FR64 AND FR6 STRG42 RH IAW SRM REPAIR TASK 53-41-13-300-004 FIGURE 001 SHEET1 (CATEGORY A)
DURING THE STRUCTURE INSPECTION PER ALLEGIANT EO E5331-0006/0007, IT WAS FOUND FASTENER WITH CRACK ON THE PRESS PNL FLEX BRKT AT FR 36 WORK PERFORMED: EO E5331-0006/0006 REV 03 AD 2018-06-04 INSPECTION AND REPAIR OF FR 35-FR36 PRESSURE PLATE ATTACHMENTS HOLES, ACCOMPLISHED. EO E5331-0007 REV 03 AD 2018-06-04 MODIFICATION OF FR35-FR36 PRESSURE PANEL ATTACHMENT HOLES ACCOMPLISHED.
DURING THE STRUCTURAL INSPECTION PER TASK Nº: 534107-01-1-001_P1-OP-UP/0 CPCP, IT WAS FOUND AT AFT CARGO COMPARTMENT FROM FR57 TO FR59 AT S-42RH AND BETWEEN 260MM AFT FR57 AND 200MM FWD FR57 AT S-43L WITH CORROSION. DUE TO THIS FACT, DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL.. AND FINAL APPROVAL AND FINAL APPROVAL UNDER AIRBUS DOSSIER 81042127 AND COOPESA'S ENGINEERING ORDER COO-EO-2022-15280 .
DURING THE STRUCTURAL INSPECTION PER TASK CARD Nº: 572066-01-1-002 MPD, IT WAS FOUND AT RH WING, T/E FALSE REAR SPAR OVERHANG AREA BETWEEN STA 3592 AND STA 4012 OVERHANG TOP SKIN LOWER SURFACE WITH CORROSION AND LIGHTNING STRIKE ON UPPER SURFACE. THE RESULTING BLEND OUT AFTER CORROSION REMOVAL WAS FOUND OUT OF THE SRM LIMITS. DUE TO THIS FACT, DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL AND FINAL APPROVAL UNDER AIRBUS DOSSIER 81037170 AND COOPESA'S ENGINEERING ORDER COO-EO-2022-15251 REV 01 .
DURING THE WORK CARD Nº: 53-120-003 INSPECTION ACCOMPLISHMENT WHICH IS RELATED TO AD 2018-14-09 / SB A320-53-1286 (R1), IT WAS FOUND ON CROSSBEAM SPLICING UPPER ROW AREA AT AFT LH SIDE HOLE IDENTIFY AS H3 WITH CRACK AT 12 O´CLOCK POSITION. DUE TO THIS FACT, DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL. AND FINAL APPROVAL AND FINAL APPROVAL UNDER AIRBUS DOSSIER 81039658 AND COOPESA'S ENGINEERING ORDER COO-EO-2022-15255 .
REF: NRI 1-51 - AFT CARGO COMPARTMENT FROM FR57 TO FR59 STRG 42RH WITH CORROSION./PERFORMED PERMANENT REPAIR AT AFT CARGO COMPARTMENT STGR 42RH BETWEEN FR57-FR59 AND STGR 47LH BTW FR56-FR58 IAW COOPESA EO# COO-EO-2022-15280-R00, REV00 DATED:03-28-2022 AND AIRBUS RDAF REF AND ISSUE: 81042127/004/2022#A DATED:03/28/2022, APPROVED BY ALLEGIANT UNDER ERO N.R5341-0096, REV.00 ERO REV DATE:04-08-2022, APPROVAL DATE:04-11-2022. THIS IS A MAJOR PRMANENT REPAIR CATEGORY B AND MUST BE INSPECTED AT 3 YEARS FROM TIME OF REPAIR EMBODIMENT, SUBSEQUENT INSPECTIONS AT 3 YEARS, INSPECTION METHOD DVI. COOPESA A1M098 1-51."
L2, R2, L1 DOOR ESCAPE CYLINDER PRESSURE LOW / SERVICED CYLINDERS TO PROPER PRESSURES IAW AMM 52-10-00-614-001-A"
EPSU(13WL) AFT L BATTERY FAILED EPSU CAP TEST / REMOVED FAILED EPSU AFT LEFT BATTERY IAW AMM 33-51-38-000-002-A AND INSTALLED NEW BATTERY IAW AMM 33-51-38-400-002-A, OPS CHECK GOOD"
FWD CABIN MEGAPHONE IS COMING APART AND HAS CORRODED BATTERY TRAY. / REMOVED AND REPLACED FWD CABIN MEGAPHONE PER AMM 25-65-51. OPS CHECK GOOD."
WAKING UP A/C NOTICED FWD EMERGENCY CABIN LIGHTS ON. / C/W OPS CHECK OF EMERGENCY POWER SUPPLY UNITS BY BITE CHECK REF A319 AMM 33-51-00-710-001A. EPSU BAT 10WL FAILED. REMOVED AND REPLACED EPSU BATTERY 10WL REF A319 AMM 33-51-38 PB401. OPS CHECK GOOD."
EMERGENCY LIGHTS CHECK FAULTS ESPU 11WL LOCATION. REPLACED BATTERY ON ESPU 11WL LOCATION, IAW MM 33-51-38-000-002-A AND MM 33-51-38-400-002-A. OPS CHECKED GOOD, IAW MM 33-51-00-710-001-A.
AFT MEGAPHONE INOP. R&R MEGAPHONE.
STRONG MUSTY ODOR DETECTED DURING DESCENT. R & R THE APU.
STRONG ODOR IN CABIN DURING DESCENT. FOUND YELLOW & BLUE HYDRAULIC SYSTEMS OVERSERVICED. HYDRAULIC SYSTEMS WERE SERVICED TO PROPER LEVEL..
FA REPORTED A DIRTY SOCK ODOR DURING FLIGHT. CLEANED THE APU AIR INTAKE AND REPLACED THE OZONE FILTERS.
MAIN CABIN FLOOR SUPPORT BETWEEN FRAMES 66 - 68, LBL 53 HAS CORROSION.
ROTTEN EGG-MANURE ODOR COMING FROM PACKS. R & R THE APU MOTOR.
DIRTY SOCK ODOR WHEN APU BLEED IS ON. FUEL CONTROL LEAKING, R & R THE APU FUEL CONTROL PACKING.