N243NV
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.
15 reports on file, 2019-08-25 – 2024-09-06.
Part: DOOR SEAL — DAMAGED (ZONE 200) · airframe 57,335 hrs · 39,384 cycles
(AIRCRAFT NOT GROUNDED) LEAD FA REPORTS: ROW 12 A/C LEFT HUMMING NOISE FROM EMERGENCY LOWE DOOR / PERFORMED TSM 52-21-00-810-810-A. FOUND EMERGENCY HATCH SEAL ON LEFT HAND FWR SIDE DAMAGED. REMOVED AND REPLACED PER AMM 52-21-18-960-003A. OPS CHECK GOOD."
Part: UNKNOWN — ODOR (CABIN) · airframe 57,220 hrs · 39,326 cycles
(AIRCRAFT GROUNDED) (EMERGENCY DECLARED) FA AND PASSENGERS REPORTED ODOR IN AFT CABIN. COMPLIED WITH ELIMINATION OF ODOR/FUMES IN FLIGHT DECK/CABIN PROCEDURE. ODOR EVENT CONTINUED. PERFORMED INSPECTION OF ODOR EVENT PER TSM 05-50-00-810-831-A. PERFOR DECISION TABLE, REFERENCING TYPE 9 AND TYPE 10 CORRECTIVE ACTIONS. PERFORMED INSPECTION 9 AND 10. VERIFIED NO CB POPPED, INCLUDING FWD AND AFT GALLYS. INSPECTED ALL LIGHTS AND ELECTRICAL ITEMS IN MAIN CABIN, FWD AND AFT GALLEYS. CHECKED BOTH RECIRC FANS FOR SYSTEMS 1&2 IAW AMM 21-21-00-710-001-A. NO DEFECTS NOTED. A/C OK FOR SERVICE.
Earlier reports · 2019–2023 · 13 reports
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,871 hrs · 38,687 cycles
DURING EMERGENCY LT. OPS TEST MESSAGES EPSU INT LOAD FWD L AND EPSU INT LOAD AFT L APPEARED. / PERFORMED A320 TSM 33-51-00-810-807-A, FOUND MULTIPLE LAMPS OUT ON LH FWD & LH AFT EMERGENCY EXIT SIGNS. REMOVED & REPLACED MULTIPLE LAMPS ON LH FWD & LH AFT EMERGENCY EXIT SIGNS IAW A320 AMM 33-51-11-000/400-001-A OPS CHECK GOOD AT THIS TIME, NO MESSAGES PRESENT ON EPSU."
Part: FITTING — CRACKED (ZONE 200) · airframe 52,297 hrs · 36,929 cycles
DURING THE STRUCTURE INSPECTION PER ALLEGIANT WORK ORDER NUMBER 53-210-003 AND AYY EO E5311-0013 WE FOUND AT UPPER FUSELAGE, WINDSHIELD CENTER POST, LOWER ATTACHMENT, CONTINUITY FITTING RH / LH SIDE WITH CRACK. CORRECTIVE ACTION: PERFORMED REPLACEMENT OF THE LH AND RH CONTINUITY FITTINGS PER AIRBUS REPAIR INSTRUCTIONS R531-12919 ISSUE D DATED 09-24-2020 AND DOCUMENTED ON ENGINEERING ORDER ERO NUMBER R5311-0136 REV00 DATED 01-25-2022. THIS IS A PERMANENT REPAIR AND NO ADDITIONAL REQUIREMNENTS ERO R2311-0136 REV00 â N243NV AD 2020-17-03 REPAIR FOR CRACK DAMAGE TO WINDSHIELD FRAME CONTINUITY FITTINGS ACCOMPLISHED. SEE COOPESA WORK ORDER: A1M094, ITEM: 2-12.
Part: EPSU — NONE · airframe 54,130 hrs · 37,862 cycles
WHILE PERFORMING TASK CARD 33-51-00-710-003-A, EPSU AND BAT AFT FIN (13WL) FAILED. / REMOVED AND REPLACED EPSU AND BATTERY ON AFT FIN (13WL) IAW AMM 33-51-38-400-001-A. PERFORMED BITE TEST AND OPERATIONAL TEST GOOD."
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 54,066 hrs · 37,832 cycles
NRC 7000-0019: IN PASSENGER CABIN, ALL EMERGENCY LIGHT RELATED TO EPSU 10WL AND 12WL INOP ON BATTERY. / IN PASSENGER CABIN, EPSU 10WL AND 12WL REPLACED AND TESTED SERVICEABLE AS PER AMM 33-51-38-400-001-A"
2022
Part: NONE — NONE · airframe 53,308 hrs · 37,440 cycles
UPON REMOVAL OF THE R2 DOOR EMERGENCY ESCAPE SLIDE, THE SLIDE WAS DEPLOYED AND DISCHARGED THE EMERGENCY OPERATION CYLINDER / REPLACED THE DIAPHRAGM AND PACKINGS OF THE EMERGENCY OPERATION CYLINDER IAW AMM 52-10-00-610-001A AND SERVICED THE NITROGEN CHARGE IAW AMM 52-10-00-614-001, LEAK CHECK GOOD."
Part: FRAME — CRACKED (ZONE 200) · airframe 52,297 hrs · 36,929 cycles
DURING SPECIAL DETAILED INSPECTION ON SERVICE DOOR FRAME FR16 AS PER TASK CARD 531153-02-2-001 INSTRUCTIONS, IT WAS FOUND AT FWD SERVICE DOOR AREA, FR16 DOUBLE JOGGLE AREA, FASTENER HOLE âBâ WITH CRACK INDICATION. THE DAMAGE REPORTED WAS REPAIRED IAW TO AIRBUS REF. 81019156.
Part: BULB — INOPERATIVE (L1, R1) · airframe 52,224 hrs · 36,897 cycles
CABIN EMERGENCY EXIT LIGHT SIGN BULBS INOP AT L1 DOOR, R1 DOOR, MID CABIN AND AFT CABIN LOCATIONS / REMOVED AND REPLACED LIGHT BULBS AT EMERGENCY EXIT LIGHTED SIGNS L1 DOOR, R1 DOOR, MID CABIN AND AFT CABIN LOCATIONS PER AMM 33-51-11. OPS CHECK GOOD."
Part: SIGN — INOPERATIVE · airframe 52,224 hrs · 36,897 cycles
FWD CABIN L/H WALL MOUNTED EMERGENCY EXIT LIGHTED MARKER INOP / REMOVED AND REPLACED FWD CABIN L/H WALL MOUNTED EMERGENCY LIGHTED SIGN ASSY PER AMM 33-51-13. OPS CHECK GOOD."
Part: FITTING — CRACKED (ZONE 200) · airframe 52,297 hrs · 36,929 cycles
DURING SPECIAL DETAILED INSPECTION ON WINDSHIELD CENTRAL LOWER NODE WERE FOUND CONTINUITY FITTINGS WITH CRACKS. THE CRACK WAS REPAIRED IAW YO CONTINUITY FITTINGS REPLACEMENT AND REPAIR INSTRUCTIONS R53112919 ISSUE D.
2021
Part: WARNING LIGHT — FALSE ACTIVATION (ELECTRICAL BUSS) · airframe 51,420 hrs · 36,434 cycles
ELEC DC ESS BUS SHED ECAM FOUR TIMES IN FLIGHT. EMERGENCY CANCELLED AFTER COMPLETING ECAM, QRH, FCOM PROCEDURES. / PERFORMED ELEC DC ESS BUS SHED WARNING TEST PER TSM 24-60-00-810-801A. ALL INDICATIONS NORMAL. A/C OK FOR SERVICE."
2020
Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 49,291 hrs · 35,248 cycles
CIDS1 EPSU SYS TEST BAT/EPSU 12WL / REMOVED AND CLEANED CONNECTOR AT R MID BATT 12WL AND MESSAGE CLEARED FROM CIDS1; TEST OK REF TC 05-000-002 AND AMM 33-51-00. ALSO REF ESPM 20-55-40."
Part: SENSOR — FAULTY (NLG STEERING) · airframe 48,807 hrs · 34,979 cycles
(EMERGENCY DECLARED) WHEEL N/W STRG FAULT AIRBORNE. REPLACED N/W STEERING FDBK MONITORING SENSOR (4GC).
2019
Part: MEGAPHONE — INOPERATIVE (FWD CABIN)
FWD MEGAPHONE INOP. R&R MEGAPHONE.