# Service difficulty reports: N261NV

A list on [N261NV](https://openairdocs.org/aircraft/N261NV.md).

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

- [SDR WX0A2026101432975](https://openairdocs.org/sdr/WX0A2026101432975.md): Plate · corroded · Oct 13, 2026 · N261NV · Airbus A320214 · Fuselage Main, Structure
  > (AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 1000-0092: 404-11 FWD CARGO COMPARTMENT FIXED PARTITION, PLATE AT FR34 BTW STR 35R -38R FOUND CORRODED, FWD CARGO COMPARTMENT FIXED PARTITION, PLATE AT FR34 BTW STGR35RH-STGR38RH WAS REP
- [SDR WX0A2026102132982](https://openairdocs.org/sdr/WX0A2026102132982.md): Post · damaged · Oct 10, 2026 · N261NV · Airbus A320214 · Fuselage Main, Structure
  > (MAJOR REPAIR) (AIRCRAFT NOT GROUNDED) NRC 1000-0023: (274-11) AT FR24A, FWD CARGO BLKH POST AT Y254, VERTICAL MEMBER UPPER ATTACHMENT SECTION FOUND DAMAGED / AT FR24A, FWD CARGO BLKH POST AT Y254, VERTICAL MEMBER UPPER ATTACHMENT SECTION, PERMANENTLY REPAIRED
- [SDR WX0A2026100532971](https://openairdocs.org/sdr/WX0A2026100532971.md): Profile · corroded · Oct 3, 2026 · N261NV · Airbus A320214 · Fuselage Main, Structure
  > (AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 1000-0047: AFT CARGO COMPARTMENT, PROFILE BTW FR56 - FR58 AND AT STGR 38R FOUND CORRODED. / AFT CARGO COMPARTMENT, PROFILE BTW FR56 - FR58 AND AT STGR 38R REPLACED AS PER SRM 51-72-11 RE
- [SDR WX0A2026100232969](https://openairdocs.org/sdr/WX0A2026100232969.md): Beam · corroded · Oct 1, 2026 · N261NV · Airbus A320214 · Fuselage Main, Structure
  > (AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 1000-0049: BULK CARGO COMPARTMENT, SILL BEAM BTW FR60 - FR62 FOUND CORRODED. TO BE INVESTIGATED. / BULK CARGO COMPARTMENT, AFTER REMOVAL OF CORROSION ON 4X ANCHOR NUT AREA OF SILL BEAM BT
- [SDR WX0A2026100232968](https://openairdocs.org/sdr/WX0A2026100232968.md): Diaphragm · corroded · Sep 28, 2026 · N261NV · Airbus A320214 · Wing Miscellaneous Structure
  > (AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 5000-0026: 1711-45 L/H WING TRAILING EDGE DIAPHRAGM (RIBLET) AT RIB25 CORRODED. L/H WING TRAILING EDGE DIAPHRAGM (RIBLET) AT RIB25 REPLACED AS PER SRM 51-72-11-911-001 REV.159"
- [SDR WX0A2026092832965](https://openairdocs.org/sdr/WX0A2026092832965.md): Floor Support · corroded · Sep 28, 2026 · N261NV · Airbus A320214 · Fuselage Miscellaneous Structure
  > (AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT)NRC 2000-0043: 404-09 REAR FUSELAGE CABIN FLOOR STRUCTURE, SUPPORT BTW FR69 - FR70 AT STGR23RH FOUND CORRODED / REAR FUSELAGE CABIN FLOOR STRUCTURE, SUPPORT BTW FR69 - FR70 AT STGR23RH WAS REP
- [SDR WX0A2026092832964](https://openairdocs.org/sdr/WX0A2026092832964.md): Floor Support · corroded · Sep 28, 2026 · N261NV · Airbus A320214 · Fuselage Miscellaneous Structure
  > (AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 1000-0051: PASSENGER CABIN FLOOR STRUCTURE, FLOOR BEAM BTW FR12 - FR16 AND AT Y-81 FOUND CORRODED. TO BE INVESTIGATED. / PASSENGER CABIN FLOOR STRUCTURE, FLOOR BEAM BTW FR12 - FR16 AND AT
- [SDR WX0A2026092132956](https://openairdocs.org/sdr/WX0A2026092132956.md): Pin · missing · Sep 16, 2026 · N261NV · Airbus A320214 · Escape Slide
  > (AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 9000-0009: ON L2 PASSENGER DOOR, SAFETY PIN FOR DEACTIVATION OF ESCAPE SLIDE-RAFT MISSING. / ON L2 PASSENGER DOOR, SAFETY PIN FOR DEACTIVATION OF ESCAPE SLIDE-RAFT INSTALLED AS PER AMM /
- [SDR WX0A2026091832956](https://openairdocs.org/sdr/WX0A2026091832956.md): Safety Pin · missing · Sep 16, 2026 · N261NV · Airbus A320214 · Escape Slide
  > (AIRCRAFT NOT GROUNDED) (DEFECT DISCOVERED DURING AC HEAVY MX VISIT) NRC 9000-0009: ON L2 PASSENGER DOOR, SAFETY PIN FOR DEACTIVATION OF ESCAPE SLIDE-RAFT MISSING. / TROUBLESHOOTING INPROGRESS"
- [SDR WX0A2026032532763](https://openairdocs.org/sdr/WX0A2026032532763.md): Oil System · leaking · Mar 24, 2026 · N261NV · Airbus A320214 · Air Distribution System
  > (AIRCRAFT NOT GROUNDED) DIRTY SOCK ODOR DETECTED BY ALL 4 FLIGHT ATTENDANTS FROM ROW 23 TO AFT GALLEY. ODOR DISSIPATED AFTER 5-10 MINUTES. / C/W PHASE 1 OIL TYPE SMELL REF TC 21-000-001 GVI OF APU AND APU COMPARTMENT SHOWED NO EVIDENCE OF AN OIL LEAK. COULD NO
- [SDR WX0A2026031132752](https://openairdocs.org/sdr/WX0A2026031132752.md): Battery · inoperative · Mar 10, 2026 · N261NV · Airbus A320214 · Emergency Equipment
  > AFT CABIN MEGAPHONE INOPERATIVE. REMOVED AND REPLACED AFT CABIN MEGAPHONE BATTERIES REF AMM 25-65-51-920-001A. OPS CHECK GOOD.
- [SDR WX0A2025123132690](https://openairdocs.org/sdr/WX0A2025123132690.md): Switch · out of position · Dec 30, 2025 · N261NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) EMERGENCY EXIT LIGHTS IN CABIN WOULD NOT TURN OFF AIRBORNE, TRIED TO CYCLE OFF THEN ARM STILL STAYED ON IN CABIN / UPON FLT DK ENTRY NOTED NO SMOKING SIGN SWITCH IN THE ON POSITION AND NOT IN AUTO. REF CABIN EMER LIGHTING SCHEMATIC 33-5
- [SDR EE4Y2025103123400](https://openairdocs.org/sdr/EE4Y2025103123400.md): Spar · cracked · Oct 31, 2025 · N261NV · Airbus A320214 · Nacelle/Pylon, Frame/Spar/Rib
  > DURING ACCOMPLISHMENT OF ALLEGIANT TASK A32X-54-481-002, NACELLES/PYLON AFT FIXED FAIRING RHS UPPER SPAR AT SEALING RIB 15 O/B AREA WITH CRACK INDICATION.AFT FIXED FAIRING UPPER SPAR WAS REPARED FOLLOW REPAIR INSTRUCTIONS PER ALLEGIANT ENGINEERING ORDER A32X-
- [SDR EE4Y2025103123399](https://openairdocs.org/sdr/EE4Y2025103123399.md): Window Frame · cracked · Oct 31, 2025 · N261NV · Airbus A320214 · Fuselage Main, Structure
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-212-020, UPPER FUSELAGE COCKPIT LATERAL WINDOW FRAME AT FR4 RH VERTICAL STIFFENER WITH CRACK WAS FOUND.STIFFENER WAS REPAIRED FOLLOW REPAIR INSTRUCTIONS PER ALLEGIANT ENGINEERING ENGINEERING ORDER A32X-STR-53
- [SDR WX0A2025101732602](https://openairdocs.org/sdr/WX0A2025101732602.md): Battery Pack · not reported · Oct 15, 2025 · N261NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) EPSU BATTERIES REQUIRE REPLACEMENT. INSTALLED 10,11,12,13 WL (FIN) EPSU BATTERIES IN REF TO AMM 33-51-38-000-002-A"
- [SDR WX0A2025012732281](https://openairdocs.org/sdr/WX0A2025012732281.md): Slide · unwanted deploy · Jan 27, 2025 · N261NV · Airbus A320214 · Escape Slide
  > (AIRCRAFT NOT GROUNDED) R-2 DOOR SLIDE DEPLOYED / REFERENCE NR 3, NR 6 W/O 512619 R2 DOOR SLIDE R/R WORK COMPLETION. (RESOLVED ON W/O: 512619 TASKCARD: NR-00002) REMOVED R2 DOOR SLIDE IAW AMM 25-62-44-000-805-AITEM: 1REMOVED R2 DOOR SLIDE IAW AMM 25-62-44-000
- [SDR WX0A2024011731946](https://openairdocs.org/sdr/WX0A2024011731946.md): Epsu · faulted · Jan 16, 2024 · N261NV · Airbus A320214 · Emergency Lighting
  > BAT/EPSU (10WL) FWD L FAULT 335100 / REF. A320 TSM 33-51-00-810-829-A REMOVED AND REPLACED EPSU BATTERY AT POWER SUPPLY 10WL IAW A320 AMM 33-51-38-000-002-A AND 33-51-38-400-002-A OPS CHECK GOOD."
- [SDR WX0A2023121131911](https://openairdocs.org/sdr/WX0A2023121131911.md): Epsu · unknown · Dec 7, 2023 · N261NV · Airbus A320214 · Emergency Lighting
  > EPSU TEST SHOWS FAULT AT 12WL / REMOVED & REPLACED EPSU BATTERY AT 12WL REF AMM 33-51-38-000-002-A & 33-51-38-400-002-A. OPS CHECK GOOD"
- [SDR EE4Y2023112918887](https://openairdocs.org/sdr/EE4Y2023112918887.md): Frame · cracked · Nov 29, 2023 · N261NV · Airbus A320214 · Fuselage, Wing Attach Fittings
  > DURING ALLEGIANT TASK INSPECTION 534123-01-3-001 FUSELAGE INTERNAL STRUCTURE FR666 RH SIDEINNER CAP JOINT TO GUSSET PLATE AT STGR 15RH LEVEL. FOUND THE HIGHEST HOLE & THE LOWESTHOLE CRACKED. COOPESA PERFORMED REPAIR IN ACCORDANCE A320 SRM TASK 53-41-12-300-018
- [SDR EE4Y2023112918886](https://openairdocs.org/sdr/EE4Y2023112918886.md): Frame · cracked · Nov 29, 2023 · N261NV · Airbus A320214 · Fuselage Main, Frame
  > DURING ALLEGIANT TASK INSPECTION 534123-01-3-001 FUSELAGE INTERNAL STRUCTURE FR666 RH SIDE INNER CAP JOINT TO GUSSET PLATE AT STGR 16RH LEVEL. FOUND THE HIGHEST HOLE & THE LOWEST HOLE CRACKED. COOPESA PERFORMED REPAIR IN ACCORDANCE A319 SRM TASK 53-41-12-300-0
- [SDR WX0A2023102531873](https://openairdocs.org/sdr/WX0A2023102531873.md): Epsu · unknown · Oct 25, 2023 · N261NV · Airbus A320214 · Emergency Lighting
  > EPSU 11WL FAILED BATTERY CAP CHECK / REMOVED AND REPLACED 11WL EPSU IAW AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A. OPS CHECK GOOD."
- [SDR WX0A1900010074295](https://openairdocs.org/sdr/WX0A1900010074295.md): None · none · Oct 30, 2022 · N261NV · Airbus A320214 · Fuselage Structure (General)
  > REF WO465856-1 TC53-140-003, NOTED TOOLING MARK ON THE LH KEEL BEAM MLG DOOR FWD HINGE FITTING AFT LUG AFT FACE AT 3 O'CLOCK POSITION, MEASURING 0.200-IN L X 0.100-IN W X 0.015-IN D./REMOVED AND REPLACED LH MLG DOOR LOWER FWG HINGE FITTING IAW AIRBUS REPAIR IN
- [SDR WX0A2022050274077](https://openairdocs.org/sdr/WX0A2022050274077.md): Megaphone · none · Apr 30, 2022 · N261NV · Airbus A320214 · Escape Slide
  > FWD MEGAPHONE INOP / R&R FWD MEGAPHONE, OP CHECKED GOOD, REF AIRCRAFT LOPA"
- [SDR WX0A2022020473951](https://openairdocs.org/sdr/WX0A2022020473951.md): Connector · damaged · Feb 2, 2022 · N261NV · Airbus A320214 · Passenger/Crew Doors
  > FOUND L1 DOOR EMERGENCY CYLINDER ELECTRICAL CONNECTOR DAMAGED / REMOVED AND REPLACED L1 DOOR DAMPER ELECTRICAL CIRCULAR CONNECTOR. REF ESPM 20-44-10. OPS CHECK PER AMM 52-11-14-200-001-A. NO DEFECTS NOTED."
- [SDR WX0A2021092273840](https://openairdocs.org/sdr/WX0A2021092273840.md): Epsu · no test · Sep 20, 2021 · N261NV · Airbus A320214 · Emergency Lighting
  > CABIN EMERGENCY LIGHT (10WL) FAILED DURING EPSU TEST / CABIN EMERGENCY LIGHT (10WL) REPLACED IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHK GOOD."
- [SDR WX0A202107267797](https://openairdocs.org/sdr/WX0A202107267797.md): Connector · dirty · Jul 28, 2021 · N261NV · Airbus A320214 · Light System Wiring
  > CIDS1 EPSU SYS TEST 10WL / REMOVED AND CLEANED CONNECTOR AT 10WL AND MESSAGE CLEARED FROM CIDS1; TEST OK REF TC 05-000-002 AND AMM 33-51-00. ALSO REF ESPM 20-55-40."
- [SDR WX0A2020123073624](https://openairdocs.org/sdr/WX0A2020123073624.md): Cable · out of rig · Dec 29, 2020 · N261NV · Airbus A320214 · Service Doors
  > REF NR 00720779 FOUND R1 DOOR EMERGENCY CONTROL HANDLE FLEXIBLE CABLE OUT OF RIG AT J3 DIMENSION, PER AMM 52-11-22-820-001-A. RE-SECURED, RE-TORQUED AND SAFETIED CABLE HARDWARE, PER AMM 52-11-22-400-001-A. PERFORMED ADJUSTMENT OF THE ESCAPE SLIDE/RAFT GIRT B
- [SDR WX0A2020082873565](https://openairdocs.org/sdr/WX0A2020082873565.md): Battery Pack · no test · Aug 27, 2020 · N261NV · Airbus A320214 · Emergency Lighting
  > EMERGENCY BATTERY FIN 12WL FAILED MCDU BITE TEST / REMOVED AND REPLACED EMERGENCY EXIT BATTERY FIN 12WL IAW AMM 25-23-44-000-001-A OPS CHECK IAW AMM 33-51-00-710-001-A OK FOR CONTINUED SERVICE"
- [SDR WX0A073403](https://openairdocs.org/sdr/WX0A073403.md): Hydraulic Line · broken · Jul 1, 2019 · N261NV · Airbus A320214 · Hydraulic System, Main
  > (EMERGENCY DECLARED) ON DEPARTURE AFTER RETRACTION OF GEAR, RECIEVED HYD GREEN RSVR LO LVL FOLLOWED BY LG DOORS NOT CLOSED & GEAR NOT UPLOCKED / FOUND HOSE ASSY (2765GM) BROKEN AT LT MLG DOOR ACTUATOR; R&R WITH TEMP FLEX LINE."
- [SDR WX0A2018071373353](https://openairdocs.org/sdr/WX0A2018071373353.md): Relay · faulty · Jul 10, 2018 · N261NV · Airbus A320214 · Landing Gear Retraction/Extension System
  > (EMERGENCY DECLARED) GEAR WOULD NOT RETRACT AFTER TAKEOFF. R&R HYDRAULIC CONTROL RELAY.

## 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 = 'N261NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N261NV/reports

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