N335NV
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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
34 reports on file, 2018-06-22 – 2026-07-05.
Part: SWITCH — FAULTED (ZONE 200) · airframe 52,770 hrs · 38,850 cycles
(AIRCRAFT NOT GROUNDED) NO SMOKING. EMERGENCY LIGHT ILLUMINATED IN AUTO POSITION. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH (4WL) IAW ESPM 20-45-21. OPS CHECK GOOD. "
Part: EPSU — INOPERATIVE (ZONE 200) · airframe 52,770 hrs · 38,850 cycles
(AIRCRAFT NOT GROUNDED) IN THE PASSANGER CABIN, EPSU 12WL FAILED BATTERY CAPACITY CHECK. / REMOVED AND REPLACED EPSU (12WL) IAW AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A OPS TEST GOOD NO FURTHER DEFECTS NOTED AT THIS TIME.
Part: EPSU — INOPERATIVE (ZONE 200) · airframe 52,770 hrs · 38,850 cycles
(AIRCRAFT NOT GROUNDED) IN THE PASSANGER CABIN, EPSU 11WL FAILED BATTERY CAPACITY CHECK / REMOVED AND REPLACED EPSU (11WL) IAW AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A OPS TEST GOOD NO FURTHER DEFECTS NOTED AT THIS TIME."
Part: STRINGER — CORRODED (ZONE 100) · airframe 52,748 hrs · 38,838 cycles
(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 9000-0007: (338-06) AFT CARGO FLOOR STRUCTURE, CORROSION FOUND ON STR 42R BTW FR 55 AND FR 59 / AFT CARGO STRUCTURE, STRINGER 42R BTW FR 54 AND FR 59 PERMANENTLY REPAIRED AS PER AIRBUS DOSSIER #80417492, AIRBUS TD/80417492/018/2018#A, AIRBUS DWG R53470620 ISSUE F AND ALLEGIANT ERO A32X-STR-53ERO-00607 REV.00. MINOR REPAIR CATEGORY A AS PER AIRBUS RDAF #80417492/045/2026#A. NO FURTHER ACTION REQUIRED."
Part: EPSU — NO TEST (ZONE 200) · airframe 52,748 hrs · 38,838 cycles
(AIRCRAFT NOT GROUNDED) DURING EPSU BITE TEST, BAT/EPSU(10WL)FWD L FAULT. / FWD L/H EPSU (10WL) REPLACED AND SERVICEABLE IAW AMM 33-51-38-400-002-A. EPSU BITE TEST COVERED ON T/C #335100-06-1-001."
Part: WEB — CORRODED (ZONE 200) · airframe 52,748 hrs · 38,838 cycles
(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING THE AC HEAVY MX VISIT) NRC 9000-0012: (S//M)(34240-02) PASSENGER CABIN FWD WET AREA, WEB BTW FR12 - FR16 AND AT Y1584 CORRODED, PASSENGER CABIN FWD WET AREA, WEB BTW FR12 - FR16 AND AT Y1584 WAS REPLACED IAW SRM 51-72-11-911-001, REV 158.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 52,748 hrs · 38,838 cycles
(AIRCRAFT NOT GROUNDED) PASSENGER CABIN FWD WET AREA, FLOOR SUPPORT BTW FR 12 - FR 24, Y-254 CORRODED. PASSENGER CABIN FWD WET AREA, FLOOR SUPPORT REPLACED IAW SRM 51-72-11-911-001 REV 158.
Part: LOCK NUT — CORRODED (ZONE 600 AILERON) · airframe 52,748 hrs · 38,838 cycles
(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING THE AC HEAVY MX VISIT) NRC 6000-0025: (37788-21) RH WING, AILERON BOX INBOARD ROD END LOCK NUT CORRODED / RH WING, AILERON BOX INBOARD ROD END LOCK NUT REPLACED IAW AMM 57-51-31-400-001-A, SUBTASK 57-51-31-420-052-E STEP: 17 - 18"
Part: PROFILE — CORRODED (ZONE 100) · airframe 52,748 hrs · 38,838 cycles
(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING THE AC HEAVY MX VISIT) NRC 9000-0008: (338-07) AFT CARGO, FLOOR STRUCTURE, CORROSION FOUND ON PROFILE AT FR 65 AND STR 38L / AFT CARGO, FLOOR STRUCTURE, PROFILE BTW FR63-65 AND STR 38L REPLACED AS PER SRM 51-72-11-911-001 REV. 158."
Part: BRACKET — DAMAGED (ZONE 100) · airframe 52,748 hrs · 38,838 cycles
(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING THE AC HEAVY MX VISIT) NRC 1000-0025: 35705-16, AFT CARGO COMPARTMENT, PROXIMITY SENSOR (32WV) BRACKET CORRODED, AFT CARGO COMPARTMENT, PROXIMITY SENSOR ( 32WV) BRACKET REPLACED AS PER SRM 51-72-11-911-001 REV 158.
Part: TIE DOWN — DAMAGED (ZONE 100) · airframe 52,748 hrs · 38,838 cycles
(AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING THE AC HEAVY MX VISIT) NRC 9000-0009: (338-09) FWD CARGO BAY, CORROSION FOUND ON TIEDOWN AT FR 28 AND STR41L / FWD CARGO BAY, TIE-DOWN WAS REPLACED AT FR 28 AND STR41L IAW SRM 51-42-11, SRM 51-72-11-911-001 REV 158 AND AMM 25-54-41-400-001-A REV 47A.
Part: PUMP — LOW PRESSURE (ZONE 400) · airframe 52,424 hrs · 38,669 cycles
(AIRCRAFT NOT GROUNDED) LOST GREEN SYSTEM HYDRAULIC FLUID AFTER TAKE OFF. ASSOCIATED MESSAGED ON ECAM: HYD. G ENG 1 PUMP LOW PRESS / HYD G SYS LOW PRESS/ HYD. G RESVR. LOW LEVEL / FOUND R/H MLG HYD LINE FROM MLG LOCK STAY ACTUATOR SEVERED. REMOVED + REPLACED R/H MLG LOCK STAY ACTUATOR OUTBOARD HYD LINE IAW AMM 32-11-21-000-001A + 32-11-21-400-001A. AND 32-11-22-04 CONF OO. OPS AND LEAK CHECK GOOD. NORMAL EXTENSION + RETRACTION FUNCTIONAL CHECK GOOD IAW AMM 32-31-00-720-002A"
Earlier reports · 2018–2025 · 22 reports
2025
Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 51,843 hrs · 38,339 cycles
(AIRCRAFT NOT GROUNDED) AFT MEGAPHONE INOPERATIVE. REMOVED & REPLACED AFT MEGAPHONE UNIT REF SIP. OPS CHECKED GOOD.
Part: LIGHT — MALFUNCTIONED (ZONE 200) · airframe 50,383 hrs · 37,566 cycles
(AIRCRAFT NOT GROUNDED) WHEN POWER WAS DISCONNECTED FROM GROUND CONNECTION, EMERGENCY LIGHT AND EXIT SIGNS DID NOT OPERATE AT L1, R1 OVERWING EXITS / PERFORMED OP'S CHECK OF EMERGENCY POWER SUPPLY UNITS REF. AMM 33-51-00-710-001-A, OP'S CHECK GOOD AT THIS TIME"
Part: BATTERY — NO TEST (ZONE 200) · airframe 50,356 hrs · 37,553 cycles
(AIRCRAFT NOT GROUNDED) EMERGENCY AND EXIT LIGHTS ARE INOP ON BATTERY POWER AT DOORS R1, L1, AND RIGHT OVERWING EXITS / PERFORMED CHARGE OF EPSU BATTS AND OPS CK OF EMERGENCY LIGHTS REF AMM 33-51-00-710-003-A AND AMM 33-51-00-710-008-A. OPS CK GOOD. NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE"
Part: OXYGEN BOX — BROKEN (ZONE 200) · airframe 49,978 hrs · 37,363 cycles
(AIRCRAFT GROUNDED) FOUND PASSENGER CABIN OXYGEN MASK CONTAINER BROKEN @18ABC / REMOVED AND REPLACED PAX 02 MODULE CONTAINER @18ABC IN REF TO AMM 35-21-41-04 CONF 00. THIS CLEARS MEL 35-21-01-A, MDDR 206114. NO (M). INOP PLACARDS REMOVED."
2024
Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 48,205 hrs · 36,459 cycles
DURING EPSU BAT CAP TEST, BATTERY AT POSITION 11WL FAILED / REMOVED AND REPLACED EPSU BATTERY AT POSITION 11WL WITH A SERVICABLE ONE REF AMMS 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CHECK GOOD, NO DEFECTS NOTED"
2023
Part: FRAME — CRACKED (ZONE 100) · airframe 47,688 hrs · 36,218 cycles
DURING THE AIRCRAFT INSPECTION AS PER ALLEGIANT EO E5311-0018 REV 00 HOLES AT RH FR16 (HOLE # B AND # C UPPER CORNER) WITH CRACKS AT THE FRAME ONLY WERE FOUND . DUE TO IN THE SRM IS NOT SPECIFIC REFERENCE TO REPAIR THE MENTIONED DAMAGE, AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS AND FINAL APPROVAL.THE DAMAGE WAS REPAIRED AND COVERED ON JOB A1N168 ITEM 2-39
Part: STRUT — UNKNOWN (ZONE 100) · airframe 47,688 hrs · 36,218 cycles
DURING ACCOMPLISHMENT OF THE ALLEGIANT EO # E5343-0001 REV01 FOR IMPLEMENTATION OF THE REQUIREMENTS OF AD2017-25-06 AND AIRBUS SB A320-53-1262 REV 01 CONFIGURATION 6. THE FITTING IDENTIFIED AS ITEM 16 WAS FOUND IN THE RIGHT SIDE. ALLEGIANT WAS CONTACTED FOR ENGINEERING SOLUTION FOR DEVIATION FOUND.ALLEGIANT PROVIDE EVA 5343-0003 TO COVER THIS DEVIATION. SEE COOPESA JOB A1N168 ITEM 9-1
Part: FRAME — CRACKED (ZONE 100) · airframe 47,688 hrs · 36,218 cycles
DURING THE AIRCRAFT INSPECTION AS PER ALLEGIANT EO E5311-0018 REV 00 HOLES AT RH FR16(HOLE # B AND # C UPPER CORNER) WITH CRACKS AT THE FRAME ONLY WERE FOUND . DUE TO IN THESRM IS NOT SPECIFIC REFERENCE TO REPAIR THE MENTIONED DAMAGE, AIRBUS WAS CONTACTEDREQUESTING REPAIR INSTRUCTIONS AND FINAL APPROVAL.THE DAMAGE WAS REPAIRED AND COVERED ONJOB A1N168 ITEM 2-40
Part: SKIN PANEL — CORRODED (ZONE 100) · airframe 47,688 hrs · 36,218 cycles
DURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD 05-000-002, AFT LAVATORY VENT OUTLETSKIN EXTERNAL EXISTING REPAIR IAW A320 SRM 53-41-11-300-004 WITH CORROSION WAS FOUND. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS AND FINALAPPROVAL,AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER DOSSIER 81285485. THE REPAIR WAS PERFORMED IN ACCORDANCE INSTRUCTIONS RECEIVED AND IT IS COVER UNDER COOPESA JOB A1N168 ITEM 1-22.
Part: EPSU — UNKNOWN (UNKNOWN) · airframe 47,545 hrs · 36,153 cycles
BAT/EPSU(12WL) EMER R CLASS 1 / R&R EPSU BATTERY AT 12WL IAW AMM REF 33-51-38-000-002-A AND 33-51-38-400-002-A.PERFORMED OPS CHECK,OPS CHECK GOOD"
Part: EPSU — UNKNOWN (UNKNOWN) · airframe 47,466 hrs · 36,113 cycles
OPERATIONAL TEST OF EPSU SYSTEM TEST AND FOUND FORWARD LEFT (FIN:10WL) BATTERY OF THE EPSU REQUIRED A REMOVAL AND REPLACE. / REMOVED AND REPLACED FORWARD LEFT BATTERY OF THE EMERGENCY POWER SUPPLY UNIT. IAW AMM 33-51-38-000-002-A AND IAW AMM 33-51-38-400-002-A. OPS CHECK GOOD."
2022
Part: REINFORCEMENT — CORRODED (ZONE 100) · airframe 46,220 hrs · 35,505 cycles
INTERGRANULAR CORROSION ON FRAME 65 REINFORCEMENT ANGLE BETWEEN STRINGER 39 AND STRINGER 44
Part: BATTERY — FAILED · airframe 46,037 hrs · 35,406 cycles
EMERGENCY LIGHT BATTERIES FAILED CAPACITY CHECK / R&R EMERGENCY LIGHTING BATTERIES IAW AMM 33-51-11. OPS CHECK GOOD AT THIS TIME"
Part: EPSU — INOPERATIVE · airframe 44,928 hrs · 34,847 cycles
EPSU BITE TEST FAULTED 11WL . / OPEN AFT CARGO AND PIN OVERWING SLIDE BOTTLE. RE-LAMPED L/H AFT BULBS AS REQUIRED,BITE TESTED EPSU EMERGENCY LIGHTING TEST OK .REMOVED PIN & STOWED AND CLOSED AFT CARGO I/A/W TSM 33-51-00-810-809-A & AMM 33-51-420-050-A."
Part: SLIDE — WILL NOT ARM · airframe 44,927 hrs · 34,845 cycles
RIGHT OVERWING EMERGENCY EXIT SLIDE NOT SHOWING ARMED. / FOUND REARM MECHANISAM OUT, REARMED IAW AMM 52-21-11-860-061-A OPS GOOD."
Part: SWITCH ACTUATOR — DEFECTIVE · airframe 44,927 hrs · 34,845 cycles
RIGHT OVERWING EMERGENCY EXIT SLIDE NOT SHOWING ARMED / REF NR00904147 FOR R/R PF ACTUATOR ASSEMBLY SWITCH. PERFORMED OPS CHECK IAW AMM 52-71-00-710-001-A. OPS CHECK GOOD."
Part: EPSU — FAULTED (13WL) · airframe 44,849 hrs · 34,809 cycles
DURING WEEKLY CHECK CIDS 1 EPSU SYS TEST BAT/ESPU (13WL) AFT L FAULT / REMOVED AND REPLACED 13WL BATTERY PER AMM 33-51-38 PB 401, FAULT CLEARED, NO DEFECTS NOTED AT THIS TIME."
2021
Part: MEGAPHONE — EXPIRED (AFT CABIN) · airframe 44,787 hrs · 34,781 cycles
AFT CABIN MEGAPHONE BATTERIES EXPIRE 12/31/2021 / REMOVED AND REPLACED AFT MEGAPHONE BATTERIES PER AMM 25-65-51, OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME."
2020
Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 42,167 hrs · 33,373 cycles
L/H OVERWING EPSU BATTERY (11WL) FAILED EPSU TEST. / REPLACED EPSU BATTERY"
2019
Part: CONVERTER — MALFUNCTIONED (AC BAY)
UPON DESCENT SMELLED DIRTY SOCK/MUSTY ODOR FROM FL310 DOWN TO MID 20'S/OZONE FILTERS CHANGE, OZONE CONVERTER CHANGED OP'S CHECK NO ODORS PRESENT.
2018
Part: FAN — MALFUNCTIONED (GALLEY) · airframe 38,447 hrs · 31,532 cycles
DURING APPROACH THE FA'S IN THE REAR OF THE CABIN SMELLED A CHEMICAL TYPE ODOR. APU WAS OFF. FOUND SOURCE TO BE AFT GALLEY LAV EXTRACT FAN. MX PLACED FAN ON MEL.
Part: UNKNOWN — ODOR (CABIN) · airframe 38,416 hrs · 31,518 cycles
FLT ATTS REPORTED A DIRTY SOCK ODOR DURING DESCENT. CLEANED APU BLEED AIR DUCT ELBOW AND LOAD CONTROL VALVE. R & R TH EOZONE AND RECIRCULATION FILTERS.