# Service difficulty reports: N275NV A list on [N275NV](https://openairdocs.org/aircraft/N275NV.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR WX0A2025121932679](https://openairdocs.org/sdr/WX0A2025121932679.md): Flashlight · inoperative · Dec 18, 2025 · N275NV · Airbus A320214 · Emergency Equipment > (AIRCRAFT NOT GROUNDED) FWD FA FLASHLIGHT NOT FLASHING. REMOVED AND REPLACED FWD IB FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AND CRADLE ASSEMBLY PER CMM 20-60-02. OPS CHECK GOOD - [SDR WX0A2025040432375](https://openairdocs.org/sdr/WX0A2025040432375.md): Filter · odor · Apr 3, 2025 · N275NV · Airbus A320214 · Air Distribution System > (AIRCRAFT NOT GROUNDED) DIRTY SOCK ON DESCENT. CW TC 21-000-002. REPLACED RECIRC FILTER 4013HM IAW AMM 21-21-41-000-001-A. REMOVED AND REPLACED OZONE FILTER 100HM IAW A320 AMM 21-51-41-000-001-A AND 21-51-41-400-001-A. ACCOMPLISHED TC 21-000-003 ON WORK ORDE - [SDR WX0A2025011732267](https://openairdocs.org/sdr/WX0A2025011732267.md): Sensor · out of range · Jan 15, 2025 · N275NV · Airbus A320214 · Door Warning System > (AIRCRAFT NOT GROUNDED) DOOR L AFT EMER EXIT- CABIN IS NORMAL. / FOUND LEFT AFT EMERGENCY EXIT COVER FLAP TO BE LOOSE AND OUT SENSOR RANGE. ADJUSTED PROX SENSOR IAW AMM 52-71-13-400-001. OPS CHECK OF PROX SENSOR GOOD. NO ECAM MESSAGE. INSTALLED COVER FLAP IAW - [SDR WX0A2025010832260](https://openairdocs.org/sdr/WX0A2025010832260.md): Door Frame · cracked · Jan 6, 2025 · N275NV · Airbus A320214 · Fuselage Main, Structure > (AIRCRAFT GROUNDED) (DISCREPANCY NOTED DURING AIRCRAFT HEAVY MX VISIT) NRC 2000-0020: DURING ACCOMPLISHMENT OF EO E5316-0002 CRACK INDICATION FOUND AT FR 20 STOP FITTNG #1 LOWER INBOARD HOLE-FRAME WEB} / AT FR 20 RH SIDE AT STOP FITTING #1 LOWER INBD HOLE IN F - [SDR WX0A2025010632257](https://openairdocs.org/sdr/WX0A2025010632257.md): Door Frame · cracked · Dec 31, 2024 · N275NV · Airbus A320214 · Fuselage Main, Structure > (AIRCRAFT GROUNDED) (DISCREPANCY NOTED DURING AIRCRAFT HEAVY MX VISIT) DURING ACCOMPLISHMENT OF TC53-260-003 CRACK FOUND AT FR 68LH STOP FITTING #1 LOWER INBD HOLE. / L2 DOOR SURROUND FR 68, CRACK AT STOP FITTING #1 LOWER INBD HOLE PERMANENTLY REPAIRD AS PER S - [SDR WX0A2025010332255](https://openairdocs.org/sdr/WX0A2025010332255.md): Skin · damaged · Dec 23, 2024 · N275NV · Airbus A320214 · Fuselage Main, Plate/Skin > (AIRCRAFT GROUNDED) (DISCREPANCY NOTED DURING AIRCRAFT HEAVY MX VISIT) S/M ( I042-4) LOWER FUSELAGE, BTW FR3 I - FR32 AT STGR 37R, LIGHTNING STRIKE FOUND / LOWER FUSELAGE EXTERNAL SKFN BTW FR 31-32 AT STGR 37R FOUND OUT OF LIMITS AS PER SRM 53-21 -11 -283-018 - [SDR WX0A2024102332205](https://openairdocs.org/sdr/WX0A2024102332205.md): Engine · odor · Oct 21, 2024 · N275NV · Airbus A320214 · Engine (Turbine/Turboprop) > (AIRCRAFT NOT GROUNDED) DURING DESCENT WE GOT A FOUL SMELL ( MUSTY ODOR). ACCORDING TO THE FAS ITS STARTED RIGHT AFTER WE STARTED THE DESCENT AND IT LASTED TIL WE PARKED. IN THE FLIGHT DECK THE ODOR DISSIPATED AFTER A FEW MINUTES. APPARENTLY THE ODOR CAME ON - [SDR WX0A2024052032045](https://openairdocs.org/sdr/WX0A2024052032045.md): Slide Raft · faulted · May 16, 2024 · N275NV · Airbus A320214 · Escape Slide > NRC 7000-0011: EMERGENCY LIGHT EPSU SYSTEM TEST BITE RESULT SHOWS FAULT MSG""ESCAPE SLIDE LT/ EPSU(10WL)FWD L"". TO BE INVESTIGATED. / FWD LH PASSENGER DOOR SLIDE (7500MM) REPLACED AS PER AMM TASK 25-62-44-400-007-A. EPSU BITE TEST PERFORMED SERVICEABLE AS PER - [SDR WX0A2024052032046](https://openairdocs.org/sdr/WX0A2024052032046.md): Epsu · faulted · May 15, 2024 · N275NV · Airbus A320214 · Emergency Lighting > NRC 7000-0010: EMERGENCY LIGHT EPSU SYSTEM TEST BITE RESULT SHOWS FAULT MSG ""BAT / EPSU(12WL)EMER R"". / EPSU 12WL REPLACED AND TESTED SERVICEABLE IAW AMM 33-51-38-400-001-A." - [SDR WX0A2024051032039](https://openairdocs.org/sdr/WX0A2024051032039.md): Door Sill · corroded · May 8, 2024 · N275NV · Airbus A320214 · Fuselage Miscellaneous Structure > (DISCREPANCY NOTED DURING AIRCRAFT HEAVY MX) R1 DOOR SILL, UNDER FWD AND AFT GIRT BAR FITTINGS, CORROSION FOUND AROUND ALL FASTENERS ATTACHMENT HOLES, QTY 8X / R1 DOOR SILL, UNDER FWD AND AFT GIRT BAR FITTINGS ALL FASTENERS ATTACHMENTS HOLES (QTY.8) PERMANENTL - [SDR WX0A2024051432043](https://openairdocs.org/sdr/WX0A2024051432043.md): Fitting · corroded · Apr 24, 2024 · N275NV · Airbus A320214 · Emergency Equipment > DISCREPANCY NOTED DURING HEAVY MX VISIT) NRC 2000-0039: (34240-06)(S/M) R1 DOOR SILL, UNDER FWD AND AFT GIRT BAR FITTINGS, CORROSION FOUND AROUND ALL FASTENERS ATTACHMENT HOLES, QTY 8X / R1 DOOR SILL, UNDER FWD AND AFT GIRT BAR FITTINGS ALL FASTENERS ATTACHME - [SDR WX0A2024051432042](https://openairdocs.org/sdr/WX0A2024051432042.md): Door Sill · corroded · Apr 24, 2024 · N275NV · Airbus A320214 · Fuselage Miscellaneous Structure > DISCREPANCY NOTED DURING HEAVY MX VISIT) NRC 2000-0040: (34240-07)(S/M) L1 DOOR SILL, UNDER FWD AND AFT GIRT BAR FITTINGS, CORROSION FOUND AROUND ALL FASTENERS ATTACHMENT HOLES, QTY 8X, L1 DOOR SILL, UNDER FWD AND AFT GIRT BAR FITTINGS ALL FASTENERS ATTACHMENT - [SDR WX0A2024050632032](https://openairdocs.org/sdr/WX0A2024050632032.md): None · none · Apr 24, 2024 · N275NV · Airbus A320214 · Standard Practices/Structures > (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 1000-0039: 031-2 (SM) EXTERNAL FUSELAGE SKIN, UNRECORDED PREVIOUS DAMAGE FOUND BTW FRAME 61 TO FRAME 62 AND AREA OF STRINGER 35L. ( NEED TO BE INVESTIGATE). / EXTERNAL FUSELAGE SKIN, UNRECORDED PRE - [SDR WX0A2024050832036](https://openairdocs.org/sdr/WX0A2024050832036.md): Fairing · cracked · Apr 23, 2024 · N275NV · Airbus A320214 · Nacelle/Pylon, Main Frame > (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 4000-0011: REAR KEEL FAIRING CRACK ON R/H PYLON AFT LOWER FAIRING. / REAR KEEL FAIRING CRACK ON R/H PYLON AFT LOWER FAIRING REPAIRED IAW S.R.M. 54-56-11-283-013 PARA. (5) REV. 148. THIS REPAIR TASK I - [SDR WX0A2024050832035](https://openairdocs.org/sdr/WX0A2024050832035.md): Fairing · cracked · Apr 23, 2024 · N275NV · Airbus A320214 · Nacelle/Pylon, Main Frame > (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 4000-0010: REAR KEEL FAIRING CRACK ON L/H PYLON AFT LOWER FAIRING. / REAR KEEL FAIRING CRACK ON L/H PYLON AFT LOWER FAIRING REPAIRED IAW S.R.M. 54-56-11-283-013 PARA. (5) REV. 148. THIS REPAIR TASK I - [SDR WX0A2024050832034](https://openairdocs.org/sdr/WX0A2024050832034.md): Acoustic Panel · dented · Apr 23, 2024 · N275NV · Airbus A320214 · Nacelle/Pylon, Main Frame > (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 4000-0006: LOWER ACOUSTIC PANEL DENTED ON #2 ENG NOSE COWL. / LOWER ACOUSTIC PANEL DENT ON #2 ENG NOSE COWL LOCATED AT 6 O'CLOCK AND 3.550 IN FROM L/E WAS EVALUATED WITHIN REPAIRABLE LIMITS AS PER NSR - [SDR WX0A2023062831783](https://openairdocs.org/sdr/WX0A2023062831783.md): Slide · unknown · Jun 27, 2023 · N275NV · Airbus A320214 · Escape Slide > EMERGENCY LIGHTING TEST SHOWS FAULT: ESCAPE SLIDE LT/ EPSU(10WL) FWD L / R+R L1 DOOR ESCAPE RAFT-SLIDE IAW AMM 25-62-44-400-007-A, OPS CHECK GOOD" - [SDR WX0A2023050331761](https://openairdocs.org/sdr/WX0A2023050331761.md): Epsu · unknown · May 3, 2023 · N275NV · Airbus A320214 · Emergency Lighting > BAT/EPSU 10WL,11WL EMER LIGHT FAULT / R&R EPSU 10WL,11WL BATTERY PER TSM 33-51-00-810-855-A, IAW AMM 33-51-38-000-002-A" - [SDR WX0A2022083174223](https://openairdocs.org/sdr/WX0A2022083174223.md): Epsu · failed insp · Aug 30, 2022 · N275NV · Airbus A320214 · Emergency Lighting > EPSU BATTERY 13WL DID NOT PASS CHECK / REMOVED AND REPLACED ESPU BATTER AT 13WL, IAW AMM 33-51-38,OPS CHECK GOOD" - [SDR WX0A2022060374101](https://openairdocs.org/sdr/WX0A2022060374101.md): Epsu · inoperative · Jun 2, 2022 · N275NV · Airbus A320214 · Emergency Lighting > FOUND FIN #12WL BATTERY INOP / R & R FIN #12WL EPSU BATTERY IN REF TO AMM 33-51-38 PB401, OPS CHECK GOOD." - [SDR WX0A2022040674049](https://openairdocs.org/sdr/WX0A2022040674049.md): Epsu · none · Apr 5, 2022 · N275NV · Airbus A320214 · Lighting System > WHILE WORKING TC 335100-03-1, EPSU 11WL FAILED CAP BATTERY CHECK, EPSU REQUIRES REPLACEMENT. / REMOVED AND INSTALLED EPSU 11WL IAW AMM 33-51-38 OPS CHECK GOOD." - [SDR WX0A2021072373790](https://openairdocs.org/sdr/WX0A2021072373790.md): Hose · leaking · Jul 21, 2021 · N275NV · Airbus A320214 · Hydraulic System, Main > (EMERGENCY DECLARED) HYD G RSVR LO LVL ECAM AFTER LANDING GEAR EXTENDED. / REMOVED & REPLACED LEFT MLG DOOR ACTUATOR HYDRAULIC FLEX HOSE, IAW 32-31-39. LEAK CHECK GOOD. AIRCRAFT OK FOR SERVICE." - [SDR WX0A2021050373699](https://openairdocs.org/sdr/WX0A2021050373699.md): Battery · no test · Apr 30, 2021 · N275NV · Airbus A320214 · Emergency Equipment > #1 FA REPORTS, FWD MEGAPHONE WILL NOT TEST PROPERLY. / REMOVED AND REPLACED BATTERIES IN MEGAPHONE IAW AMM 25-65-51." - [SDR WX0A2021041673683](https://openairdocs.org/sdr/WX0A2021041673683.md): Battery Pack · no test · Apr 14, 2021 · N275NV · Airbus A320214 · Emergency Lighting > BATT CAP TEST FAILS 12WL R EMERG EXIT / FOUND BATTERY PACK DEAD AT 12WL-REMOVED AND REPLACED BATTERY PACK AND EPSU TEST OK REF AMM 33-51-38 PB 401." - [SDR WX0A2019120673444](https://openairdocs.org/sdr/WX0A2019120673444.md): Battery Pack · faulted · Dec 5, 2019 · N275NV · Airbus A320214 · Emergency Lighting > EPSU SYS TEST FAULTING BATT (10WL), AND BATT (13WL) / REPLACED BATTERY PACKS" ## 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 = 'N275NV' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N275NV/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.