N197NV
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
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.
10 reports on file, 2023-04-16 – 2026-08-17.
Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 21,622 hrs · 8,439 cycles
DURING ACCOMPLISHMENT AS PER ALLEGIANT WORK CARD A32X-ZL-500-02-1-002 GENERAL VISUAL INSPECTION OF WING LOWER SURFACE INCLUDING UPPER AND LOWER SURFACES OF SLATS AND FLAPS (EWIS) RELATED TO MPD TASK ZL-500-02, IT WAS FOUND AT RH WING AT MLG SKIN DOUBLER O/B SECTION AND THE BOTTOM SKIN PANEL 2 LOWER SURFACE BETWEEN RIB 6 AND RIB 7, STRINGER 11 WITH CORROSION. CORRECTIVE ACTION: REPAIRED R/H WING BETWEEN RIB 6 AND 7, ON STGR 11 BOTTOM SKIN LOWER SURFACE, IAW COOPESA EO N° COO-EO-2026-24860-R00 DATED 08-11-2026, AND AIRBUS RDAF N° 81852989-004-2026#A DATED 08-13-2026. CONTROLLED BY ALLEGIANT IN ERO N° A32X-STR-57ERO-00648 REV 00 DATED 08-14-2026. THIS IS A MAJOR REPAIR CATEGORY "B" WITH INSPECTION REQUIRED. CONTROLLED UNDER COOPESA JOB: A1R148, NRI 6-2.
Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 21,622 hrs · 8,439 cycles
DURING ACCOMPLISHMENT AS PER ALLEGIANT WORK CARD A32X-ZL-500-02-1-002 GENERAL VISUAL INSPECTION OF WING LOWER SURFACE INCLUDING UPPER AND LOWER SURFACES OF SLATS AND FLAPS (EWIS) RELATED TO MPD TASK ZL-500-02, IT WAS FOUND AT RT WING AT MLG SKIN DOUBLER O/B SECTION AND THE BOTTOM SKIN PANEL 2 LOWER SURFACE BETWEEN RIB 6 AND RIB 7, STRINGER 11 WITH CORROSION. CORRECTIVE ACTION: REPAIRED R/H WING AT MLG SKIN DOUBLER O/B SECTION, IAW COOPESA EO N° COO-EO-2026-24861-R00 DATED 08-11-2026. AND AIRBUS RDAF REF N° 81851859-005-2026#A DATED 08-13-2026, CONTROLLED BY ALLEGIANT IN ERO N° A32X-STR-57ERO-00647-R00 DATED 08-14-2026. THIS IS A MAJOR REPAIR CATEGORY "B" WITH INSPECTION REQUIRED. CONTROLED UNDER COOPESA JOB A1R148, NRI 6-1.
Part: ENGINE — FAULTED (NR 2) · airframe 21,470 hrs · 8,364 cycles
(AIRCRAFT GROUNDED) (ENG SHUTDOWN EVENT) ENG 2 EGT OVER LIMIT / (FOLLOWUP - DI CLOSED) ENG 2 EGT OVER ALLOWED LIMIT. REMOVED #2 ENGINE PN CFM56-5B 4/3 SN 573435 IAW AMM 71-00-00-000-042-A. REPLACED WITH #2 ENG CFM56-5B 4/3 SN 779491 IAW AMM 71-00-00-400-042-A. PERFORMED OPS CHECKS AND LEAK CHECKS AND ENG RUNS IAW AMM 71-00-710-009-B ALL OPERATION CHECKS, LEAK CHEKS & ENG RUNS GOOD AT THIS TIME"
Part: SPAR — CRACKED (ZONE 500) · airframe 19,723 hrs · 7,447 cycles
DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-54-471-002, LH ENGINE PYLON AFT FIXED FAIRING UPPER SPAR WITH CRACK AT RIB 15 WAS FOUND.PERFORMED REPAIR IN ACCORDANCE WITH REPAIR INSTRUCTION R54512052 ISSUE F FIG 201 AND DIAGRAM A SRM PERMANENT REPAIR 54-54-12-300-003 AND ENGINEERING REPAIR ORDER ERO # A32X-STR-54ERO-00395-R00.THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q179 ITEM 4-33
Part: SPAR — CRACKED (ZONE 600) · airframe 19,723 hrs · 7,447 cycles
DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-54-481-002, RH ENGINE PYLON AFT FIXED FAIRING UPPER SPAR WITH CRACK AT RIB 15 WAS FOUND.PERFORMED REPAIR IN ACCORDANCE WITH REPAIR INSTRUCTION PER R54512052 ISSUE F (FIG 201 AND DIAG SRM PERMANENT REPAIR 54-54-12-300-003 AND ENGINEER REPAIR ORDER ERO A32X-STR-54ERO-00396-R00. THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q179 ITEM 4-30.
Part: RESERVOIR — LOW (ZONE 100) · airframe 18,263 hrs · 6,710 cycles
(EMERGENCY DECLARED)(AIRCRAFT NOT GROUNDED) HYD Y RSVR LO LVL / REMOVED AND REPLACED RT PYLON YELOW SYSTEM PRESSURE LINE AND CASE DRAIN LINES PER AMM. LEAK AND OPÿ½S CHECKS GOOD"
Part: MEGAPHONE — INTERMITTENT (FWD CABIN) · airframe 17,006 hrs · 6,181 cycles
(AIRCRAFT NOT GROUNDED) FWD CABIN ATTENDANT MEGAPHONE WORKING INTERMITTENTLY. REMOVED AND REPLACED CABIN ATTENDENT MEGAPHONE PER AMM 25-65-51-010-050-A AND 25-65-51-410-050-A, INSTALLED IN ORIGINAL POS NOTED IN LOPA A2250018L03.
Part: EPSU — UNKNOWN (UNKNOWN) · airframe 15,427 hrs · 5,536 cycles
EPSU BATTERY (13WL) AFT L INOP / REMOVED AND REPLACED AFT L (13WL) EPSU BATTERY. IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK GOOD."
Part: MEGAPHONE — UNKNOWN (UNKNOWN) · airframe 15,427 hrs · 5,536 cycles
AFT MEGAPHONE INOP. / REMOVED & REPLACED AFT MEGAPHONE IAW AMM 25-65-51 PB 201 AND LOPAS DRAWING NUMBER A2250018L03. OPS CHECK GOOD."
Part: EPSU — UNKNOWN · airframe 14,026 hrs · 4,904 cycles
PERFORMED EPSU TEST SHOWED FAULT FOR BAT/EPSU (11WL) EMER L. / REMOVED AND REPLACED EPSU (11WL) IAW A320 AMM 33-51-38 PB 401, OPS TEST GOOD."