# Service difficulty reports: N289NV

A list on [N289NV](https://openairdocs.org/aircraft/N289NV.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR WX0A2026080732915](https://openairdocs.org/sdr/WX0A2026080732915.md): Battery Pack · inoperative · Aug 5, 2026 · N289NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD FA FLASHLIGHT INOP. / REMOVED AND REPLACED BATTERY FOR FWD FA FLASHLIGHT IAW ALLEGIANT LOPA. OPS TEST GOOD. THIS CLEARS MEL 25-60-08-A, MDDR 236053. INOP PLACARD REMOVED. A/C OK FOR SERVICE."
- [SDR WX0A2026042732797](https://openairdocs.org/sdr/WX0A2026042732797.md): Landing Gear · faulted · Apr 24, 2026 · N289NV · Airbus A320214 · Landing Gear Retraction/Extension System
  > (AIRCRAFT NOT GROUNDED) (ATC DECLARED EMERGENCY) AFTER T/O L/G GEAR NOT UPLOCKED ECAM APPEARED AFTER THE LANDING GEAR HAMDLE WAS PUT IN THE UP POSITION. THE A/C WAS OVER 200KTS. PERFORMED TSM 32-31-00-810-808-A UP TO B3D1 OPS CHECK GOOD AT THIS TIME. RELAY 6
- [SDR WX0A2026022732741](https://openairdocs.org/sdr/WX0A2026022732741.md): Safety Valve · faulted · Feb 27, 2026 · N289NV · Airbus A320214 · Landing Gear Retraction/Extension System
  > (EMERGENCY DECLARED) (AIRCRAFT NOT GROUNDED) ON APPROCH, LANDING GEAR WOULD NOT COME DOWN. GOT ECAM L/G GEAR NOT DOWNLOCKED. DID A GRAVITY GEAR EXTENSION / REMOVED AND REPLACED L/G SAFETY VALVE, OPS CHECK GOOD. THIS CLOSES MEL 32-31-00A MDDR# 227361, (M) PROCE
- [SDR EE4Y2025070222618](https://openairdocs.org/sdr/EE4Y2025070222618.md): Frame · cracked · Jul 2, 2025 · N289NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-E5316-0003, UPPER FUSELAGE PASSENGER CABIN FR16 LH AT DOOR STOP FITTING LOCATION # 7 UPPER AND LOWER INBOARD OPEN HOLES WITH CRACK INDICATION WAS FOUND. PERFORMED FREEZE PLUG FASTENER HOLE REPAIR AT FR16 STOP FI
- [SDR EE4Y2025070222617](https://openairdocs.org/sdr/EE4Y2025070222617.md): Frame · cracked · Jul 2, 2025 · N289NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-E5316-0003, UPPER FUSELAGE PASSENGER CABIN FR 16 LHS AT DOOR STOP FITTING # 1 LOWER INBOARD OPEN HOLE WITH CRACK INDICATION. PÉRFORMED FREEZE PLUG FASTENER HOLE REPAIR FR16 LHS STOP FITTING # 1 LOWER INBD HOLE A
- [SDR EE4Y2025070222616](https://openairdocs.org/sdr/EE4Y2025070222616.md): Frame · cracked · Jul 2, 2025 · N289NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-003, UPPER FUSELAGE FR68 RHS AT DOOR STOP FITTING # 1 LOWER OUTBOARD FASTENER HOLE WITH CRACK INDICATION. PERFORMED FREEZE PLUG FASTENER HOLE REPAIR AND OVERSIZE BOLT INSTALLATION AT FR68 STOP FITTING # 1
- [SDR EE4Y2025070222615](https://openairdocs.org/sdr/EE4Y2025070222615.md): Frame · cracked · Jul 2, 2025 · N289NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-E5311-0018, UPPER FUSELAGE FR16 RHS DOUBLE JOGGLE UPPER AREA HOLES POSITIONS # 7, #A, #B AND #C WITH CRACK INDICATION WERE FOUND. PERFORMED TEMPORARY FASTENER HOLES # 7, #A, #B AND #C BUSHES REPAIR AT FR 16 RHS
- [SDR EE4Y2025070122614](https://openairdocs.org/sdr/EE4Y2025070122614.md): Frame · cracked · Jul 1, 2025 · N289NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ALLEGIANT ACCOMPLISHMENT OF THE TASK A32X-E5311-0019, UPPER FUSELAGE FR16 LH SIDE DOUBLE JOGGLE AREA HOLE POSITION # 7 WITH CRACK INDICATION WAS FOUND. PERFORMED NEXT NOMINAL FASTENER HOLE # 7 REPAIR AND ASSOCIATED HOLE # 8 SECOND OVERSIZE REPAIR IAW A3
- [SDR WX0A2025021732320](https://openairdocs.org/sdr/WX0A2025021732320.md): Latch · out of position · Feb 17, 2025 · N289NV · Airbus A320214 · Emergency Exits
  > (AIRCRAFT NOT GROUNDED) ROW 12 L OVERWING EXIT SLIDE NOT ARMED / DURING INSPECTION L OVERWING EMERGENCY HATCH FOUND LATCH PIN OF THE SLIDE RELEASE MECHANISM RETRACTED. PUT THE LATCH MECHANISM BACK IN THE ARMED POSTION PER AMM 52-21-11-400-001-A. A/C OK FOR SE
- [SDR WX0A2025021032310](https://openairdocs.org/sdr/WX0A2025021032310.md): Megaphone · intermittent · Feb 9, 2025 · N289NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD MEGAPHONE WORKS INTERMITENTLY / REMOVED AND REPLACED MEGAPHONE IAW AMM 25-65-51-710-002-A. OPS CHECK GOOD.
- [SDR WX0A2025012932292](https://openairdocs.org/sdr/WX0A2025012932292.md): Battery · no test · Jan 29, 2025 · N289NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) EPSU BATTERY 10WL FAILED BITE / (RESOLVED ON W/O: 512591 TASKCARD: NR-00005) REMOVED AND REPLACED EPSU BATTERY 10WL IAW AMM 33-51-38-400-002-A AND 33-51-38-000-002-A. OPS CHECKS GOOD. ITEM: 1REMOVED AND REPLACED EPSU BATTERY 10WL IAW A
- [SDR WX0A2024121632233](https://openairdocs.org/sdr/WX0A2024121632233.md): Compressor · leaking · Nov 25, 2024 · N289NV · Airbus A320214 · APU Core Engine
  > (AIRCRAFT NOT GROUNDED) DIRTY SOCK SMELL FILLED FLIGHT DECK WHEN OUTFLOW VALVE OPENED AROUND 3,000' / C/W ALLEGIANT AIR A320 TC 21-000-002. FOUND EVIDENCE OF WETTNESS IN LOAD COMPRESSOR WITH BORESCOPE. APU LOAD COMPRESSOR LEAK. REMOVED APU IAW AMM TASK 49-11
- [SDR WX0A2024111332214](https://openairdocs.org/sdr/WX0A2024111332214.md): Emer Light Sys · broken · Nov 12, 2024 · N289NV · Airbus A320214 · Exterior Lighting
  > (AIRCRAFT NOT GROUNDED) R1 LOWER EMERGENCY EXIT SIGN LENS BROKEN OFF WALL / R1 EMERGENCY EXIT SIGN RECONNECT AND REINSTALLED,OPS CHECK GOOD IAW A320 AMM 33-51-17"
- [SDR WX0A2024062132086](https://openairdocs.org/sdr/WX0A2024062132086.md): Slide Raft · faulty · Jun 18, 2024 · N289NV · Airbus A320214 · Escape Slide
  > (AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 2000-0066: R1 DOOR ESCAPE SLIDE FOUND FAULTY / R1 DOOR ESCAPE SLIDE REPLACED AS PER AMM 25-62-44-400-803-A. FOR THE OPERATIONAL TEST SEE AWS FOR DETAILS."
- [SDR WX0A2024061932081](https://openairdocs.org/sdr/WX0A2024061932081.md): Skin · corroded · May 31, 2024 · N289NV · Airbus A320214 · Wing, Plate/Skin
  > (AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 6000-0022: (1042-001A) RH WING TOP SKIN LOWER SURFACE AT OVERHANG TRAILING EDGE, CORROSION FOUND BETWEEN RIB 15 AND RIB16. / RH WING TOP SKIN PANEL #2 LOWER SURFACE TEOH AREA B
- [SDR WX0A2024061932080](https://openairdocs.org/sdr/WX0A2024061932080.md): Skin · corroded · May 31, 2024 · N289NV · Airbus A320214 · Wing, Plate/Skin
  > (AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 5000-0035: LH WING TRAILING EDGE OVERHANG, CORROSION FOUND AT UPPER SKIN LOWER SURFACE BETWEEN INBD OF RIB 14 AND RIB 16. / LH WING TOP SKIN PANEL #2 LOWER SURFACE TEOH AREA BT
- [SDR WX0A2024061932084](https://openairdocs.org/sdr/WX0A2024061932084.md): Skin · corroded · May 29, 2024 · N289NV · Airbus A320214 · Wing, Plate/Skin
  > (AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 6000-0005: 33284-001 RH WING TOP SKIN LOWER SURFACE AT OVERHANG TRAILING EDGE, CORROSION FOUND BETWEEN RIB16 AND RIB17 (WMRX 5855.60). / RH WING TOP SKIN PANEL #2 LOWER SURFACE
- [SDR WX0A2024061932083](https://openairdocs.org/sdr/WX0A2024061932083.md): Skin · damaged · May 29, 2024 · N289NV · Airbus A320214 · Fuselage Main, Plate/Skin
  > (AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 2000-0005: (S/M)34240-01 REAR FUSELAGE SKIN, AT L2 DOOR CUTOUT, UPPER FWD CORNER FOUND DAMAGED. / REAR FUSELAGE SKIN L2 DOOR CUTOUT UPPER FWD CORNER PERMANENTLY REPAIRED PER AI
- [SDR WX0A2024061932082](https://openairdocs.org/sdr/WX0A2024061932082.md): Skin · corroded · May 29, 2024 · N289NV · Airbus A320214 · Wing, Plate/Skin
  > (AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 5000-0023: 1711-15 LH WING TRAILING EDGE OVERHANG, CORROSION FOUND ON UPPER SKIN LOWER SURFACE BTW RIB 16 TO OUTBD OF RIB 17. / LH WING TOP SKIN PANEL #2 LOWER SURFACE TEOH ARE
- [SDR WX0A2024052232052](https://openairdocs.org/sdr/WX0A2024052232052.md): Deu · faulted · May 20, 2024 · N289NV · Airbus A320214 · Emergency Lighting
  > EPSU BITE TEST EPSU FWD L 10WL/DEU FAULT / REPLACED REF TC 23-73-47-400-001-A"
- [SDR WX0A2024052232051](https://openairdocs.org/sdr/WX0A2024052232051.md): Epsu · no test · May 20, 2024 · N289NV · Airbus A320214 · Emergency Lighting
  > EPSU BITE TEST EPSU FWD L 10WL/DEU.B FAULT / R&R EPSU IAW AMM REF 33-51-38-000-001-A & 33-51-38-400-001-A. OPS CHECK GOOD."
- [SDR WX0A2024011631942](https://openairdocs.org/sdr/WX0A2024011631942.md): Unknown · unknown · Jan 13, 2024 · N289NV · Airbus A320214 · Emergency Lighting
  > PERFORMED EPSU SYS TEST AND FOUND CLASS 1 FAULT FOR SPSU (10WL) FWD BATTERY / ALEX CAMPBELL INSTALLED EPSU IAW AMM 33-51-38-400-001-A UP TO STEP 4(E). KOLTON WHITMORE INSTALLED CEILING PANELS IAW AMM 25-23-42-400-001."
- [SDR WX0A2024011231940](https://openairdocs.org/sdr/WX0A2024011231940.md): Slide Raft · unknown · Jan 11, 2024 · N289NV · Airbus A320214 · Escape Slide
  > L1 DOOR WILL NOT ARM SLIDE. / INSTALLED NEW L1 DOOR ESCAPE-SLIDE RAFT PACK ASSY IAW AMM 25-62-44-400-007-A. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED AT THIS TIME. AIRCRAFT OKAY FOR SERVICE."
- [SDR EE4Y2023062717943](https://openairdocs.org/sdr/EE4Y2023062717943.md): Stringer · corroded · Jun 27, 2023 · N289NV · Airbus A320214 · Fuselage, Wing Attach Fittings
  > DURING INSPECTION TASK ZL-171-01-2-001 STRINGER 43 LEFT FLANGE UPPER CORROSION WAS FOUND.PERFORMED PERMANENT REPAIR AT STGR43L, BETWEEN FR64 AND FR66 I.A.W A320 SRM TASK 53-41-13-300-004 FIGURE 001 (SHEET 1), REV 144 DATED 02- 01-2023. THIS IS A MAJOR PERMANEN
- [SDR EE4Y2023062717944](https://openairdocs.org/sdr/EE4Y2023062717944.md): Rib · corroded · Jun 27, 2023 · N289NV · Airbus A320214 · Wing Structure
  > DURING THE INSPECTION ACCOMPLISHMENT PER ALLEGIANT WORK CARD Nº: ZL-575-01-1-001 IT WAS FOUND THE RIBLET J CORRODED. DUE TO THIS FACT IT WILL BE REPLACED BY NEW ONE, DUE TO FLY BY WIRE CABLES PASS THROUGH THE MENTIONED RIBLET J, DETAILS WERE SENT TO AIRBUS ASK
- [SDR WX0A2022101774280](https://openairdocs.org/sdr/WX0A2022101774280.md): None · none · Oct 15, 2022 · N289NV · Airbus A320214 · Lighting System
  > L1 LOWER EMERGENCY EXIT SIGN FELL OFF. / REPLACED L1 LOWER EMERGENCY EXIT SIGN IAW AMM 33-51-13-400-001-A."
- [SDR WX0A2022091674247](https://openairdocs.org/sdr/WX0A2022091674247.md): None · none · Sep 15, 2022 · N289NV · Airbus A320214 · Rudder, Spar/Rib
  > REF. W/O 463019-2 PERMANENT REPAIR OF RUDDER DAMAGE REQUIRES REPAIR/PERFORMED RUDDER SKIN REPAIR AROUND TRAILING EDGE SCREW LINE IN THE GFRP AREA UP TO STEP 2.A.2 H.13 SRM 55-41-13-300-025.COMPLETED RUDDER SKIN REPAIR AROUND TRIALING EDGE SCREW IN GFRP AREA FR
- [SDR WX0A2022081274204](https://openairdocs.org/sdr/WX0A2022081274204.md): Slide & Sleeve · inoperative · Aug 11, 2022 · N289NV · Airbus A320214 · Emergency Equipment
  > L2 SLIDE BLOWN / REINSTALLED SERVICEABLE SLIDE PER AMM 25-62-44 REPLACED DOOR ASSIST BOTTLE DIAPHRAGM AND SERVICED BOTTLE PER AMM 52-10-00.L2 DOOR SLIDE CHECKS NORMAL."
- [SDR WX0A2022072974173](https://openairdocs.org/sdr/WX0A2022072974173.md): Sign · missing · Jul 28, 2022 · N289NV · Airbus A320214 · Emergency Lighting
  > EXIT SIGN MISSING ROW 14 AIRCRAFT RIGHT / DETAILED VISUAL INSPECTION C/W AND PLACED CLEAR TAPE OVER EXPOSED AREA IAW EA 72-2022-138. 1 FC PERMANENT REPAIR TRACKED BY M313# 05330004/1."
- [SDR WX0A2022072274167](https://openairdocs.org/sdr/WX0A2022072274167.md): Light · inoperative · Jul 22, 2022 · N289NV · Airbus A320214 · Emergency Lighting
  > EMERGENCY LIGHTS AT LEFT AND RIGHT OVERWING EXITS ARE INOP / PERFORMED OPS CHECK OF EMERGENGY LIGHTS IAW AMM 33-51-00. REMOVED AND REPLACED OVERWING EXITS BATTERIES 12WL AND 11WL IAW AMM 33-51-38. OPS CHECK GOOD."
- [SDR WX0A2021121773895](https://openairdocs.org/sdr/WX0A2021121773895.md): Epsu · failed insp · Dec 15, 2021 · N289NV · Airbus A320214 · Emergency Lighting
  > 13WL EPSU BATTERY FAIL ON TEST / REMOVED AND REPLACED (13WL) EPSU BATTERIE IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A; OP'S CHECK GOOD"
- [SDR WX0A2021110573864](https://openairdocs.org/sdr/WX0A2021110573864.md): Epsu · no test · Nov 4, 2021 · N289NV · Airbus A320214 · Emergency Lighting
  > EPSU SYSTEM TEST REVEALED EPSU (10WL) FAILED. / REMOVED AND REPLACED EPSU (10WL) IAW AMM 33-51-38 PB 401. OPS CHECK GOOD."

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N289NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N289NV/reports

---
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