- Registered owner
- Allegiant Air LLC
- Location
- Las Vegas, NV
- Owner type
- LLC
- Serial number
- 7063
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 14, 2016
- Certificate issued
- March 30, 2023
- Expires
- March 31, 2030
- Mode S code
- A1836C
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B4/3 model are included below.
On this page
Airworthiness directives that may apply · 381
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1990 | 5 |
|---|---|
| 1991 | 1 |
| 1992 | 6 |
| 1993 | 10 |
| 1994 | 10 |
| 1995 | 4 |
| 1996 | 5 |
| 1997 | 9 |
| 1998 | 20 |
| 1999 | 14 |
| 2000 | 13 |
| 2001 | 8 |
| 2002 | 12 |
| 2003 | 3 |
| 2004 | 23 |
| 2005 | 20 |
| 2006 | 13 |
| 2007 | 16 |
| 2008 | 9 |
| 2009 | 13 |
| 2010 | 7 |
| 2011 | 12 |
| 2012 | 12 |
| 2013 | 17 |
| 2014 | 18 |
| 2015 | 23 |
| 2016 | 25 |
| 2017 | 24 |
| 2018 | 31 |
| 2019 | 23 |
| 2020 | 29 |
| 2021 | 16 |
| 2022 | 22 |
| 2023 | 19 |
| 2024 | 15 |
| 2025 | 21 |
| 2026 | 17 |
See all 545 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Airbus A320-214
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565SAIB NM-15-02Cabin Equipment/FurnishingsSAIB NM-14-21Communications: Honeywell RTA 44D VHF TransceiversSAIB NM-13-24Air Conditioning System: Air Distribution FanSAIB NM-13-03Hydraulic Power System: Power Transfer UnitSAIB NM-06-57Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.Engine · CFM International CFM56-5B4/3 series
SAIB NE-08-17R3Turbine Section - Propulsion Technology LLC Unapproved RepairSAIB NE-12-29Engine Fuel Distribution CFM56-5B LPTACC Fuel ManifoldHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N197NVMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Airbus A320-214 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EE4Y2026081724876Skin Panel · corrodedDURING 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 SESDR EE4Y2026081724875Skin Panel · corrodedDURING 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 SESDR WX0A2026070632873Engine · faulted(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.SDR EE4Y2025100723298Spar · crackedDURING 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 54-54-1SDR EE4Y2025100723297Spar · crackedDURING 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 54-54-1SDR WX0A1900010032340Reservoir · low(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 OPÏ¿½S CHECKS GOOD"SDR WX0A2024071032109Megaphone · intermittent(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.SDR WX0A2023120131902Epsu · unknownEPSU 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."SDR WX0A2023120131901Megaphone · unknownAFT MEGAPHONE INOP. / REMOVED & REPLACED AFT MEGAPHONE IAW AMM 25-65-51 PB 201 AND LOPAS DRAWING NUMBER A2250018L03. OPS CHECK GOOD."SDR WX0A2023041731754Epsu · unknownPERFORMED 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."
STCs that may be installed · 301
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 301 STCs