# Service difficulty reports: N292NV

A list on [N292NV](https://openairdocs.org/aircraft/N292NV.md).

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

- [SDR WX0A2026101232974](https://openairdocs.org/sdr/WX0A2026101232974.md): Engine · failed · Oct 12, 2026 · N292NV · Airbus A320214 · Engine (Turbine/Turboprop)
  > (AIRCRAFT GROUNDED) (EMERGENCY DECLARED) ENG 1 FAIL IN CRUISE. LOUD BANG, HIGH VIBRATION. RAN HIGH VIBRATION CHECKLIST IN QRH.ENGINE FAILED SHORTLY AFTER. REF AML 2202584 FOR REMOVAL AND INSTALLATION OF ENGINE NR 1. OPS AND LEAK CHECKS GOOD.
- [SDR WX0A2026082832934](https://openairdocs.org/sdr/WX0A2026082832934.md): Megaphone · inoperative · Aug 26, 2026 · N292NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) FWD FA MEGA PHONE NOT WORKING. REPLACED FWD FA MEGAPHONE PER LOPA WITH NEW. NO OTHER DEFECTS NOTED.
- [SDR WX0A2026081932926](https://openairdocs.org/sdr/WX0A2026081932926.md): Battery · discharged · Aug 17, 2026 · N292NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) AFT CENTER F/A STATION FLASHLIGHT LED NOT FLASHING, TAMPER SHIELD BROKEN / R/R BATTERY AND TAMPER SHIELD IAW CMM 25-60-02 OPS CHECK GOOD "
- [SDR WX0A2026050632805](https://openairdocs.org/sdr/WX0A2026050632805.md): Epsu · no test · May 3, 2026 · N292NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) DURING WEEKLY INSP (W/O 549885), FOUND EPSU SYS TEST FAILS, EPSU 11WL EMER L / PERFORMED TSM 33-51-00-810-822-A, OBSERVED DURING TEST ""RED EXTERIOR LIGHTS FAULT) "" ILLUMINATED. REPLACED EPSU BATTERY IAW AMM 33-51-38-000-002-A / AMM 33
- [SDR WX0A2026050432802](https://openairdocs.org/sdr/WX0A2026050432802.md): Epsu · faulted · May 3, 2026 · N292NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNED) DURING WEEKLY INSP (W/O 549885), FOUND EPSU SYS TEST FAILS, EPSU 11WL EMER LIGHT. PERFORMED TSM 33-51-00-810-822-A, OBSERVED DURING TEST RED EXTERIOR LIGHTS FAULT ILLUMINATED. REPLACED EPSU BATTERY IAW AMM 33-51-38-000-002-A / AMM 33-
- [SDR EE4Y2026042124346](https://openairdocs.org/sdr/EE4Y2026042124346.md): Angle · cracked · Apr 22, 2026 · N292NV · Airbus A320214 · Engine Thrust Reverser
  > DURING THE EXECUTION OF ALLEGIANT WORK CARD A32X-ZL-451-01-1-002_P1-OP-UP-ENG/007 IT WAS FOUND ENGINE #2, INBOARD THRUST REVERSER UPPER BLOCKER DOOR, INTERNAL FRONT LOWER ANGLE WITH CRACK. REPLACED ANGLE P/N 321-311-400-6 AT ENGINE#2 I/B T/R UPPER BLOCKER DO
- [SDR EE4Y2026042124345](https://openairdocs.org/sdr/EE4Y2026042124345.md): Fitting · cracked · Apr 22, 2026 · N292NV · Airbus A320214 · Engine Thrust Reverser
  > DURING THE EXECUTION OF ALLEGIANT WORK CARD A32X-ZL-451-01-1-002_P1-OP-UP-ENG/006 IT WAS FOUND ENGINE #2, OUTBOARD THRUST REVERSER UPPER BLOCKER DOOR, DEACTIVATION BOLT FITTING WITH CORROSION AND CRACKS. REPLACED LOCKOUT FITTING P/N 321-321-352-6 AT ENGINE
- [SDR EE4Y2026042124344](https://openairdocs.org/sdr/EE4Y2026042124344.md): Box Beam · cracked · Apr 22, 2026 · N292NV · Airbus A320214 · Fuselage Main, Structure
  > DURING THE EXECUTION OF ALLEGIANT WORK CARD A32X—53-240-001_P1-OP-UP-UF IT WAS FOUND AT THE UPPER FUSELAGE AT FR43 S15 AREA AND Y+1650.0 SIDE BOX BEAM, OPEN FASTENR HOLE WITH CRACK INDICATION. REPAIRED UPPER FUSELAGE AT FR 43,STR 15 LH AND Y+1650.0 SIDE BOX
- [SDR EE4Y2026042124343](https://openairdocs.org/sdr/EE4Y2026042124343.md): Box Beam · cracked · Apr 22, 2026 · N292NV · Airbus A320214 · Fuselage Main, Structure
  > DURING THE EXECUTION OF ALLEGIANT WORK CARD A32X—53-240-001_P1-OP-UP-UF IT WAS FOUND AT THE UPPER FUSELAGE AT FR43 S15 AREA AND Y-1650.0 SIDE BOX BEAM, OPEN FASTENR HOLE WITH CRACK INDICATION. REPAIRED UPPER FUSELAGE AT FR 43,STR 15 RH AND Y-1650.0 SIDE BOX
- [SDR WX0A2025041432385](https://openairdocs.org/sdr/WX0A2025041432385.md): Button · no test · Apr 11, 2025 · N292NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) EMERG BUTTON ON FAP NOT WORKING. NO AUDIBLE CHIMES WHEN PRESSED. / PERFORMED AMM 33-51-00-710-804-A OPERATIONAL CHECK OF MANUAL EMERGENCY LIGHTING ACTIVATION. NO DEFECTS. NO CHIMES ARE NORMAL OPERATION.
- [SDR WX0A2025010232252](https://openairdocs.org/sdr/WX0A2025010232252.md): Epsu · no test · Dec 28, 2024 · N292NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) BATTERY FAIL EPSU CHECK / R/R EPSU REF WO510177"
- [SDR WX0A2024090632165](https://openairdocs.org/sdr/WX0A2024090632165.md): Module · inoperative · Sep 1, 2024 · N292NV · Airbus A320214 · Passenger Oxygen System
  > (AIRCRAFT NOT GROUNDED) AFT GALLEY OXYGEN STORAGE MODULE INOP. / SWAPPED DAMAGED J-HOOK SUPPORTS WITH NEW PER CMM 35-22-25. REINSTALLED OXYGEN STORAGE MODULE (33WR) IAW AMM 35-21-41-400-001-A. OPS CHECK GOOD. THIS CLEARS MEL 35-21-01E, MDDR 200363. INOP PLACAR
- [SDR WX0A2024061932076](https://openairdocs.org/sdr/WX0A2024061932076.md): Megaphone · no test · Jun 17, 2024 · N292NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) REAR MEGAPHONE NO SIGNAL FEEDBACK / REMOVED & REPLACED AFT CABIN MEGAPHONE PER ALLEGIANT AIRLINES LOPA A2250013L03."
- [SDR WX0A2023071231792](https://openairdocs.org/sdr/WX0A2023071231792.md): Epsu · unknown · Jul 11, 2023 · N292NV · Airbus A320214 · Emergency Lighting
  > 10WL,11WL,13WL EPSU FAILED EMERGENCY LIGHT TEST. BOTH BATTERIES FAULT / REMOVED AND REPLACED EPSU BATTERIES (10WL,11WL, 13WL) IAW AMM 33-51-38-000-001A AND 33-51-38-400-001A OPS CHECK GOOD"
- [SDR WX0A2023061931778](https://openairdocs.org/sdr/WX0A2023061931778.md): Slide · unknown · Jun 17, 2023 · N292NV · Airbus A320214 · Escape Slide
  > R1 DOOR EMERGENCY SLIDE RAFT DEPLOYED / REMOVED AND REPLACED RIGHT HAND ESCAPE SLIDE RAFT PACK ASSEMBLY IAW AMM 25-62-44-000-804-A AND AMM 25-62-44-400-803-A AND LOPA A2250013L03"
- [SDR EE4Y2023042217636](https://openairdocs.org/sdr/EE4Y2023042217636.md): Stringer · corroded · Apr 22, 2023 · N292NV · Airbus A320214 · Fuselage Main, Longeron/Stringer
  > DURING ACCOMPLISHMENT ALLEGIANT TASK 532180-01-2-001 WAS FOUND A CORROSION ON LOWERFUSELAGE FWD CARGO COMPARTMENT AT FR33+230MM. PERMANENT REPAIR ON FWD CARGO COMPARTMENTSTGR 44LH OUTER FLANGE BETWEEN FR31-32 WAS PERFORMED IAW A320 SRM TASK 53-21-13-300-019 PA
- [SDR EE4Y2023042217635](https://openairdocs.org/sdr/EE4Y2023042217635.md): Stringer · corroded · Apr 22, 2023 · N292NV · Airbus A320214 · Fuselage Main, Longeron/Stringer
  > DURING ACCOMPLISHMENT ALLEGIANT TASK 532180-01-2-001 WAS FOUND A CORROSION ON LOWER FUSELAGE FWD CARGO COMPARTMENT AT FR31+280MM. PERMANENT REPAIR ON FWD CARGO COMPARTMENT STGR 44LH OUTER FLANGE BETWEEN FR31-32 WAS PERFORMED IAW A320 SRM TASK 53-21-13-300-019
- [SDR EE4Y2023042117634](https://openairdocs.org/sdr/EE4Y2023042117634.md): Reinforcement · corroded · Apr 21, 2023 · N292NV · Airbus A320214 · Fuselage Miscellaneous Structure
  > DURING THE AIRCRAFT INSPECTION, IT WAS FOUND CORROSION ON REINFORCEMENT CASE TRAIN DOUBLER NLG BETWEEN FR20 - FR21 AND Y175 AND Y-175. DUE TO THE DAMAGE IS BEYOND SRM ADL LIMITS, AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS AND FINAL APPROVAL.AIRBUS P
- [SDR EE4Y2023031017383](https://openairdocs.org/sdr/EE4Y2023031017383.md): Bracket · corroded · Mar 10, 2023 · N292NV · Airbus A320214 · Leading Edge Devices
  > DURING INSPECTION LEFT WING TRAILING EDGE CAVITY RIBS (3EA) BETWEEN WING RIB 15 AND 19 WITH CORROSION WAS FOUND. THE BRACKET P/N D5754042720000 WAS REPLACED IAW A320 SRM 51-72-11-911-001 REV 141 DATED 05/01/2022. THIS REPLACEMENT IS CAPTURED IN COOPESA NON RO
- [SDR EE4Y2023031017389](https://openairdocs.org/sdr/EE4Y2023031017389.md): Bracket · corroded · Mar 10, 2023 · N292NV · Airbus A320214 · Wing Structure
  > DURING TH ESTRUCTURE INSPECTION WAS FOUND IN THE RH WING FIXED T/E RIBS (3EA) WITH CORROSION BETWEEN WING RIBS 13-17. DUE TO THIS FACT THE BRACKETS P/N: D5754042720100 WERE REPLACED IAW A320 SRM 51-72-11-911-001 THE REPLACED WAS HANDLED UNDER COOPESA JOB: A1M
- [SDR EE4Y2023031017387](https://openairdocs.org/sdr/EE4Y2023031017387.md): Skin · corroded · Mar 10, 2023 · N292NV · Airbus A320214 · Wing Structure
  > DURING TH ESTRUCTURE INSPECTION WAS FOUND IN THE RH WING FIXED T/E AREA BETWEEN RIBS 14-16 OVERHANG WITH CORROSION. DUE TO THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL. AFTER AIRBUS EVALUATION REPAIR INSTRUCTIOINS WER
- [SDR EE4Y2023031017386](https://openairdocs.org/sdr/EE4Y2023031017386.md): Skin · corroded · Mar 10, 2023 · N292NV · Airbus A320214 · Wing Structure
  > DURING THE STRUCTURE INSPETION WAS FOUND IN THE LH WING TOP SKIN LOWER SURFACE OVERHANG AREA BETWEEN RIB 14 AND RIB 16 SKIN WITH CORROSION. DUE TO THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTUCTIONS AND FINAL APPROVAL. AFTER AIRBUS EVALUATION R
- [SDR WX0A2022091974252](https://openairdocs.org/sdr/WX0A2022091974252.md): Epsu · none · Sep 18, 2022 · N292NV · Airbus A320214 · Lighting System
  > EPSU BATTERY TEST FAILURE AT 12WL. / REMOVED AND REPLACED EPSU BATTERY AT 12WL IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. PERFORMED EPSU BITE CHECK, OPS CHECK GOOD IAW AMM 33-51-00-710-001."
- [SDR WX0A2022081274201](https://openairdocs.org/sdr/WX0A2022081274201.md): Light · inoperative · Aug 10, 2022 · N292NV · Airbus A320214 · Emergency Lighting
  > L1 DOOR EMERGANCY LIGHT COVER IS BROKEN / R&R L1 DOOR EMERGENCY LEN COVER IAW AMM 33-51-06 OPS CHKS GOOD"
- [SDR WX0A2022071874159](https://openairdocs.org/sdr/WX0A2022071874159.md): Epsu · failed · Jul 18, 2022 · N292NV · Airbus A320214 · Emergency Lighting
  > EPSU AT 12WL BAD / INSTALLED EPSU AT 12WL IAW AMM 33-51-38-400-001-A OPPS CK GOOD TEST GOOD"
- [SDR WX0A2022071174148](https://openairdocs.org/sdr/WX0A2022071174148.md): None · none · Jul 8, 2022 · N292NV · Airbus A320214 · Nose/Tail Landing Gear
  > (EMERGENCY DECLARED) AFTER TO NOSE LANDING GEAR DID NOT RETRACT. FOLLOWED ECAM ACTION. DID NOT FIXED THE PROBLEM. DID NOT EXCEED 220 KTS. FELT THE DRAG FROM A GEAR AND DOORS. FOLLOWED FCOM FOR OVERWEIGHT LANDING. TOUCHDOWN @100FT/MIN. LANDING WEIGHT 15
- [SDR EE4Y2022062015830](https://openairdocs.org/sdr/EE4Y2022062015830.md): Hinge Fitting · cracked · Jun 20, 2022 · N292NV · Airbus A319111 · Nose/Tail Landing Gear Attach Section
  > DURING THE STRUCTURAL INSPECTION PER TASK CARD Nº: 323300-05-2-001_P1-OP-CK/0, IT WAS FOUND AT LOWER FUSELAGE NLG LH DOOR HINGE FITTING UPPER SECTION CRACKED.. DUE TO THIS FACT THE HINGE P/N D5392538120000 WAS REPLACED I/A/W A320 SRM 51-72-11-911-001, AND AI
- [SDR EE4Y2022062015827](https://openairdocs.org/sdr/EE4Y2022062015827.md): Skin Panel · corroded · Jun 20, 2022 · N292NV · Airbus A319111 · Wing Spar
  > DURING THE STRUCTURAL INSPECTION PER TASK CARD Nº: 572062-01-1-001 MPD, IT WAS FOUND AT LH WING, T/E FALSE REAR SPAR OVERHANG AREA BETWEEN RIB 6 AND RIB 7 OVERHANG TOP SKIN LOWER SURFACE WITH CORROSION. THE RESULTING BLEND OUT AFTER CORROSION REMOVAL WAS FOUND
- [SDR EE4Y2022062015828](https://openairdocs.org/sdr/EE4Y2022062015828.md): Skin Panel · corroded · Jun 20, 2022 · N292NV · Airbus A319111 · Wing Spar
  > DURING THE STRUCTURAL INSPECTION PER TASK CARD Nº: 572062-01-1-002 MPD, IT WAS FOUND AT RH WING, T/E FALSE REAR SPAR OVERHANG AREA BETWEEN RIB 6 AND RIB 7, RIB 15, RIB 21 AND RIB 22 OVERHANG TOP SKIN LOWER SURFACE WITH CORROSION. THE RESULTING BLEND OUTS AFTER
- [SDR EE4Y2022062015829](https://openairdocs.org/sdr/EE4Y2022062015829.md): Skin · corroded · Jun 20, 2022 · N292NV · Airbus A319111 · Wing Structure
  > DURING THE INSPECTION ACCOMPLISHMENT PER ALLEGIANT WORK CARD Nº: ZL-575-01-1-001 IT WAS FOUND THE RIBLET E CORRODED. DUE TO THIS FACT IT WILL BE REPLACED BY NEW ONE, DUE TO FLY BY WIRE CABLES PASS THROUGH THE MENTIONED RIBLET E AND A HOLE COMMON TO THE REBLET
- [SDR WX0A2022012873940](https://openairdocs.org/sdr/WX0A2022012873940.md): Epsu · failed insp · Jan 26, 2022 · N292NV · Airbus A320214 · Emergency Lighting
  > CABIN EMERGENCY LIGHT TEST FAULTED EPSU(10WL) FWD L. / T/S EPSU (10WL) SELF TEST NO LIGHT SHOWN, REMOVED & REPLACED EPSU(10WL), OPS CHECK GOOD I/A/W AMM 33-51-38 PB 401."
- [SDR WX0A2022012873939](https://openairdocs.org/sdr/WX0A2022012873939.md): Epsu · failed insp · Jan 26, 2022 · N292NV · Airbus A320214 · Emergency Lighting
  > CABIN EMERGENCY LIGHT TEST FAULTED BAT/EPSU (13WL) AFT L. / T/S REPLACED BATTERY ON EPSU (13WL),NO HELP. REMOVED & REPLACED EPSU (13WL), OPS CHECK GOOD I/A/W AMM 33-51-38 PB 401."
- [SDR WX0A2022012873938](https://openairdocs.org/sdr/WX0A2022012873938.md): Epsu · failed insp · Jan 26, 2022 · N292NV · Airbus A320214 · Emergency Lighting
  > EMERGENCY BATTERY AT POSITION 11WL FAILED THE BATTERY CAPACITY CHECK / REMOVED AND REPLACED EMERGANCY LIGHT BATTERY AT LH OVER WING EXIT FIN 11WL RE AMM 33-51-38"
- [SDR WX0A2021073073801](https://openairdocs.org/sdr/WX0A2021073073801.md): Epsu · no test · Jul 31, 2021 · N292NV · Airbus A320214 · Emergency Lighting
  > EMERGENCY POWER SUPPLY (12WL) REQUIRES REPLACEMENT DUE TO BITE TEST FAULT / REMOVED AND REPLACED EMERGENCY POWER SUPPLY (12WL) BITE TEST GOOD REF AMM 33-51-38"
- [SDR WX0A2020082473561](https://openairdocs.org/sdr/WX0A2020082473561.md): Battery Pack · no test · Aug 23, 2020 · N292NV · Airbus A320214 · Emergency Lighting
  > DURING EPSU BATTERY TEST, FIN POSITION 10WL AND 13WL FAILED EPSU BATTERY CAPACITANCE TEST AND REQUIRES REPLACEMENT. / REMOVED/REPLACED (2EA) EPSU BATTERIES IAW A320 AMM 33-51-38-01A. BITE TEST PERFORMED SATISFACTORILY."

## 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 = 'N292NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N292NV/reports

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