# Service difficulty reports: N218NV

A list on [N218NV](https://openairdocs.org/aircraft/N218NV.md).

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

Page 1 of 2 · 53 reports

- [SDR WX0A2026072732901](https://openairdocs.org/sdr/WX0A2026072732901.md): A/C Pack · odor · Jul 27, 2026 · N218NV · Airbus A320214 · Cabin Cooling System
  > (AIRCRAFT NOT GROUNDED) VERY STRONG ODOR EVENT IN FLIGHT DECK BELOW 18,000 TO THE GATE. PERFORMED TC 21-000-001, SMELL ONLY REPRODUCED ON PACK 2, DEFERRED PACK 2 ON MEL 21-52-01C, MDDR 235500, INOP PLACARDS APPLIED.
- [SDR WX0A2026070832881](https://openairdocs.org/sdr/WX0A2026070832881.md): Battery Pack · no test · Jul 4, 2026 · N218NV · Airbus A320214 · Humidity Control System
  > (AIRCRAFT NOT GROUNDED) FWD LEFT & RIGHT EXIT SIGNS INOP / REPLACED EMERGENCY LIGHT BATTERY OPS GOOD IAW AMM 33-51-38-400-001-A"
- [SDR WX0A2026051132811](https://openairdocs.org/sdr/WX0A2026051132811.md): Bolt · loose · May 9, 2026 · N218NV · Airbus A320214 · Escape Slide
  > (AIRCRAFT NOT GROUNDED) RT SIDE MIDWING ESCAPE SLIDE BOLT IS LOOSE. FAR AFT BOTTOM FASTENER REINSTALLED IAW AMM 25-62-42-400-001-A, A/C OK FOR SERVICE"
- [SDR WX0A2026020232721](https://openairdocs.org/sdr/WX0A2026020232721.md): Spring · broken · Jan 29, 2026 · N218NV · Airbus A320214 · Emergency Equipment
  > AIRCRAFT NOT GROUNDED. WHILE REPLACING L2 DOOR SLIDE, FOUND L2 DOOR DAMPER CYLINDER STRIKER MECHANISM HAD BROKEN SPRING & PRESSURE GAUGE PLUG MISSING LIQUID LEAKED OUT. L2 DOOR DAMPER EMERGENCY CYLINDER INSTALLED IAW AMM 52-13-14-400-001-B, C/W AMM 52-11-14
- [SDR WX0A2026013032718](https://openairdocs.org/sdr/WX0A2026013032718.md): Slide · not reported · Jan 27, 2026 · N218NV · Airbus A320214 · Escape Slide
  > (AIRCRAFT NOT GROUNDED) R & R DOOR SLIDE 7502MM. REMOVED INEFFECTIVE SLIDE REF 25-62-44-000-002-A. INSTALLED NEW SLIDE IAW AMM 25-62-44-400-006-A UP TO 4A6 "
- [SDR WX0A2026012632713](https://openairdocs.org/sdr/WX0A2026012632713.md): Battery · inoperative · Jan 23, 2026 · N218NV · Airbus A320214 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) AFT FA FLASHLIGHT INOPERATIVE. R & R AFT FA FLASHLIGHT BATTERY IAW CMM 25-60-02, OPS CHECK GOOD"
- [SDR WX0A2025091032560](https://openairdocs.org/sdr/WX0A2025091032560.md): Battery · no test · Sep 8, 2025 · N218NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) BATTERY FAULT AFTER CAPACITY TEST. REMOVED AND REPLACED EPSU REF WO530669.
- [SDR WX0A2025032832368](https://openairdocs.org/sdr/WX0A2025032832368.md): Seal · damaged · Mar 26, 2025 · N218NV · Airbus A320214 · Emergency Exits
  > (AIRCRAFT NOT GROUNDED) HIGH SQUEAL PITCH AT EMERGENCY EXIT ROW A/C LEFT PASSING THROUGH 30,000 FEET / REMOVED LH EMERGENCY HATCHES PER AMM 52-21-11-000-001-A, FOUND LH AFT EMERGENCY DOOR SEAL DAMAGED, REMOVED AND REPLACED SEAL PER AMM 52-21-18-960-003-A, PRES
- [SDR WX0A2025032132361](https://openairdocs.org/sdr/WX0A2025032132361.md): Elec Connector · faulted · Mar 20, 2025 · N218NV · Airbus A320214 · Communications System
  > (AIRCRAFT NOT GROUNDED) CA AND OBSERVER OXYGEN MASKS MICROPHONE INOP. / DISCONNECTED AND RECONNECTED CONNECTOR PLUG ON CAPT'S O2 MASK STORAGE BOX AND CAPT'S OP CKS GOOD IAW AMM 23-51-00-710-004-A OCCUPANT MIC IS NOT CONNECTED PER AMM 23-51-00-710-004-A."
- [SDR WX0A2025012932289](https://openairdocs.org/sdr/WX0A2025012932289.md): Epsu · no test · Jan 28, 2025 · N218NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) EMERG LIGHT TEST FAILS EPSU BATTERY MID L / REMOVED AND REPLACED BATTS AT L MID (11WL) AND AFT L (13WL) AND BOTH POSITIONS BITE CK GOOD. SEE LOG PAGE 1897000 FOR FURTHER TROUBLESHOOTING REF AMM 33-51-38-000/400-002-A."
- [SDR WX0A2025012932288](https://openairdocs.org/sdr/WX0A2025012932288.md): Battery Pack · no test · Jan 28, 2025 · N218NV · Airbus A320214 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) EMERGENCY LIGHT TEST FAILED, EPSU UNIT MID RIGHT / REPLACED MID RIGHT EPSU BATTERY REF A320 AMM 33-51-38-000-002-A & 33-51-38-400-002-A. OPS CHECK GOOD AT THIS TIME. "
- [SDR WX0A2024111532217](https://openairdocs.org/sdr/WX0A2024111532217.md): Hydraulic System · leaking · Nov 5, 2024 · N218NV · Airbus A320214 · Hydraulic System, Main
  > (AIRCRAFT NOT GROUNDED) AFT FA REPORTED DIRTY SOCK SMELL IN THE AFT GALLEY AREA. OCCURED ABOUT 1:30 INTO FLIGHT WITH ABOUT 30-40 MIN LEFT. REPRTED SMELL CONTINUED DURING DESCENT AND ALSO AT GATE WITH APU BLEED ON. CABIN ODOR REPORT FILLED OUT. / IN RESPONSE TO
- [SDR DU4R2024091300046](https://openairdocs.org/sdr/DU4R2024091300046.md): Skin · corroded · Sep 13, 2024 · N218NV · Airbus A320214 · Wing, Plate/Skin
  > DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND LH WING, UPPER SURFACE HAS CORROSION, TOP SKIN PANEL 1, HAS PREVIOUS BLEND APPROX. 48 SQ. IN. AT RIB 9 & 18" INCHES AFT OF FWD SPAR. S/O 193151 NR-1021 HAECO 28256
- [SDR DU4R202409130045](https://openairdocs.org/sdr/DU4R202409130045.md): Fitting · gouged · Sep 13, 2024 · N218NV · Airbus A320214 · Spoilers
  > DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND #5 SPOILER ON RIGHT WING REAR SPAR O/B LUG IS GOUGED. S/O 193151 NR-00969 HAECO NR 28923
- [SDR DU4R202409110044](https://openairdocs.org/sdr/DU4R202409110044.md): Door Sill · corroded · Sep 11, 2024 · N218NV · Airbus A320214 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED INSPECTION. FOUND L-1 DOOR SILL CORRODED AT FWD GIRT BAR FITTING ATTACHMENT.
- [SDR DU4R202409030043](https://openairdocs.org/sdr/DU4R202409030043.md): Door Sill · corroded · Sep 3, 2024 · N218NV · Airbus A320214 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA, FOUND L/H AFT PASSENGER DOOR AFT LOWER CENTER SILL HAS CORROSION. S/O 193151 NR 28776
- [SDR DU4R202408080042](https://openairdocs.org/sdr/DU4R202408080042.md): Frame · cracked · Aug 8, 2024 · N218NV · Airbus A320214 · Fuselage Main, Frame
  > DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FL FOUND CRACK INDICATION IN OPEN HOLE #5 AT 9 O-CLOCK IN FRAME LAYER AT UPPER DOUBLE JOGGLE AREA FR 20 RH SIDE. S/O 193151 NR 28487
- [SDR DU4R202408080041](https://openairdocs.org/sdr/DU4R202408080041.md): Frame · cracked · Aug 8, 2024 · N218NV · Airbus A320214 · Fuselage Main, Frame
  > DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FL FOUND CRACK INDICATION IN OPEN HOLE #A AT 2 O-CLOCK IN FRAME LAYER AT UPPER DOUBLE JOGGLE AREA FR 20 LH SIDE. S/O 193151 NR 28489
- [SDR WX0A2024072932130](https://openairdocs.org/sdr/WX0A2024072932130.md): Seal · torn · Jun 28, 2024 · N218NV · Airbus A320214 · Service Doors
  > (AIRCRAFT NOT GROUNDED) PANEL 841CZ (R1 DOOR) SLIDE ARMING HANDLE CUTOUT SEAL TORN/MISSING / REMOVED AND REPLACED SLIDE ARMING CUTOUT SEAL/SIGHT CLASS ON 841CZ IAW A320 AMM 25-23-46-960-801-A"
- [SDR WX0A2024072932129](https://openairdocs.org/sdr/WX0A2024072932129.md): Seal · torn · Jun 28, 2024 · N218NV · Airbus A320214 · Passenger/Crew Doors
  > (AIRCRAFT NOT GROUNDED) PANEL 831CZ (L1 DOOR) SLIDE ARMING HANDLE CUTOUT SEAL TORN / REMOVED AND REPLACED SLIDE ARMING HANDLE CUTOUT SEAL/SIGHT GLASS IAW A320 AMM 25-23-46-960-801-A"
- [SDR WX0A2023011731701](https://openairdocs.org/sdr/WX0A2023011731701.md): Battery Pack · no test · Jan 16, 2023 · N218NV · Airbus A320214 · Emergency Lighting
  > EPSU BATTERIES AT FIN LOCATION 11WL, 12WL, AND 13WL FAILED DURING EPSU BATTERY CAPACITY TEST. REQUIRE REPLACEMENT. / REMOVED AND REPLACED EPSU BATTERIES AT FIN LOCATION 11WL, 12WL, AND 13WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CHECK GOOD."
- [SDR WX0A1900010074284](https://openairdocs.org/sdr/WX0A1900010074284.md): Actuator · faulted · Oct 16, 2022 · N218NV · Airbus A320214 · Trailing Edge Flap Control System
  > (EMERGENCY DECLARED) ON APPROACH FLT CNTL FLAPS FAULT RAN ECAM ATTEMPTED FLAP RESET BY SELECTING PREVIOUS POSSITION FLAP FAULT REMAINED. PERFORMED TSM 27-51-00-810-810-A, FLAP SYSTEM JAM, FOUND TRIPPED TORQUE LIMITER INDICATOR ON L/H WING OF ACTUATOR ASSY 1, P
- [SDR WX0A2022100374268](https://openairdocs.org/sdr/WX0A2022100374268.md): None · none · Oct 1, 2022 · N218NV · Airbus A320214 · Lighting System
  > EMERGENCY CEILING LIGHT AT 206WL INOP / REMOVED AND REPLACED LAMPS ON EMERGENCY CEILING LIGHT IAW AMM 33-51-11-000-001-A AND AMM 33-51-11-400-001-A. OPS CHECK GOOD."
- [SDR WX0A2022100374267](https://openairdocs.org/sdr/WX0A2022100374267.md): Epsu · none · Oct 1, 2022 · N218NV · Airbus A320214 · Lighting System
  > FWD 10 WL EPSU BATTERY FAILED BITE TEST / REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK GOOD."
- [SDR WX0A2022072974169](https://openairdocs.org/sdr/WX0A2022072974169.md): Cylinder · low pressure · Jul 29, 2022 · N218NV · Airbus A320214 · Passenger/Crew Doors
  > R1 DOOR EMER. OPERATION CYLINDER PRESSURE IS LOW. / SERVICED R1 DOOR EMERGENCY OPERATION CYLINDER IAW A320 AMM 52-10-00. NO LEAKS NOTED."
- [SDR WX0A2022051374087](https://openairdocs.org/sdr/WX0A2022051374087.md): None · none · May 9, 2022 · N218NV · Airbus A320214 · Emergency Lighting
  > NRC 7000-0008: SEVERAL EMERGENCY LIGHT BULB TO BE RELAMP. / ALL EMERGENCY LIGHT BULB INOP REPLACED AND TESTED SERVICEABLE IAW AMM 33-51-16-400-001-A"
- [SDR WX0A2022030974023](https://openairdocs.org/sdr/WX0A2022030974023.md): Sign · inoperative · Mar 8, 2022 · N218NV · Airbus A320214 · Emergency Lighting
  > CABIN WALL MOUNTED EMERGENCY EXIT MARKER ON L2 DOOR HAS MOST LIGHTS OUT, R/H OVERWING HAS 2 LIGHTS OUT AND FWD R1 DOOR HAS 2 LIGHTS OUT / REMOVED AND REPLACED BULBS IAW AMM 33-51-13 PB 401. OPS CHECK OF ALL LIGHTS GOOD."
- [SDR WX0A2021120273882](https://openairdocs.org/sdr/WX0A2021120273882.md): Connector · dirty · Nov 30, 2021 · N218NV · Airbus A320214 · Emergency Lighting
  > 11WL FAILS EMERG LIGHT TEST / REMOVED AND CLEANED CONNECTOR AT L MID BATT 11WL AND MESSAGE CLEARED FROM CIDS1; TEST OK REF TC 05-000-002 AND AMM 33-51-00. ALSO REF ESPM 20-55-40"
- [SDR WX0A2021102573858](https://openairdocs.org/sdr/WX0A2021102573858.md): Lamp · inoperative · Oct 25, 2021 · N218NV · Airbus A320214 · Emergency Lighting
  > MULTIPLE EMERGENCY EXIT SIGN LAMPS INOP AT RH OVERWING EXIT AND CENTER OVERHEAD SIGN / REPLACED MULTIPLE EMERGENCY EXIT SIGN LAMPS AT RH OVERWING EXIT AND CENTER OVERHEAD SIGN IAW AMM 33-51-11, OPS CHECK GOOD."
- [SDR WX0A1900010073857](https://openairdocs.org/sdr/WX0A1900010073857.md): Connector · contaminated · Oct 15, 2021 · N218NV · Airbus A320214 · Hydraulic Power System Wiring
  > DURING CRUISE GREEN HYD RSVR OVERHEAT FOLLOWED BY SYS LO PRESSURE. OVERHEAT OUT AFTER 25 MIN. \ FOUND CANNON PLUG CONTAMINATED @ ENG PUMP SOLENOID VALVE, CLEANED IAW ESPM 20-55-50. REMOVED AND REPLACED ENGINE 1 GREEN HYDRAULIC PUMP (1030GK) IAW AMM 29-11-51.
- [SDR WX0A2021101673852](https://openairdocs.org/sdr/WX0A2021101673852.md): Line · leaking · Oct 14, 2021 · N218NV · Airbus A320214 · Hydraulic System, Main
  > DURING CRUISE BEFORE TOP OF DESCENT YELLOW HYDRAULIC RESEVOIR LOST ALL FLUID. ECAM FOR HYD LO LVL ANF PRESSURE. FOLLOWED ECAM AND LANDED NORMALLY / REMOVED AND REPLACED YELLOW HYDRAULIC SYSTEM HCU PIPE ON ENG 2 IAW AMM 29-13-49 OP'S/LEAK CHECK GOOD A/C OKAY FO
- [SDR EE4Y2021060312856](https://openairdocs.org/sdr/EE4Y2021060312856.md): Door Frame · cracked · Jun 3, 2021 · N218NV · Airbus A320214 · Fuselage Main, Structure
  > DURING MAINTENANCE ACCOMPLISHMENT WERE FOUND A DENT WITH CRACK LOCATED AT FR24A BETWEEN STR35RH AND STR36RH, THE DAMAGE WAS FOUND OUT OF ALLOWABLE DAMAGE LIMITS AS PER A320 SRM, DUE TO THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FI
- [SDR EE4Y2021052412851](https://openairdocs.org/sdr/EE4Y2021052412851.md): Skin · damaged · Jun 2, 2021 · N218NV · Airbus A320214 · Fuselage Main, Plate/Skin
  > DURING MAINTENANCE ACCOMPLISHMENT WERE FOUND THE LOWER FUSELAGE AT FR24+385MM, BETWEEN STRG 42R AND STRG 43R SKIN WITH NICKS, THE DAMAGE REMOVAL WAS FOUND OUT OF ALLOWABLE DAMAGE LIMITS AS PER A320 SRM, DUE TO THIS FACT A REPAIR WAS PERFORMED AS PER A320 SRM T
- [SDR EE4Y2021052412814](https://openairdocs.org/sdr/EE4Y2021052412814.md): Skin · corroded · May 24, 2021 · N218NV · Airbus A320214 · Wing, Plate/Skin
  > DURING MAINTENANCE ACCOMPLISHMENT WERE FOUND CORROSION AT RH WING UPPER SKIN SURFACE AT TRAILING EDGE OVERHANG AND FRONT SPAR AREA, EVALUATED RH WING UPPER SKIN UPPER SURFACE FRONT SPAR AREA BETWEEN RIB 8 AND RIB 9 AND IT WAS FOUND OUT ALLOWABLE DAMAGE LIMITS
- [SDR EE4Y2021052412812](https://openairdocs.org/sdr/EE4Y2021052412812.md): Skin · dented · May 24, 2021 · N218NV · Airbus A320214 · Cargo/Baggage Doors
  > DURING MAINTENANCE ACCOMPLISHMENT WERE FOUND THE BULK CARGO DOOR SKIN WITH DENT LOCATED AT FR60+100 BETWEEN BEAMS 5 AND 6, THE DENT WAS FOUND OUT OF ALLOWABLE DAMAGE LIMITS AS PER A320 SRM, DUE TO THIS FACT A REPAIR WAS PERFORMED AS PER A320 SRM 52-33-00-300-0
- [SDR EE4Y2023031017358](https://openairdocs.org/sdr/EE4Y2023031017358.md): Skin · corroded · May 7, 2021 · N218NV · Airbus A320214 · Wing Structure
  > DURING THE INSPECTION PER TASK CARD ZL-500-03-1-002_P1-OP-UP/0, CORROSION WAS FOUND COMMON TO RIGHT WING UPPER SKIN FRONT SPAR AREA, BETWEEN RIB 7 AND RIB 8. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED AS PER AIRBUS DOSSIER# 80917709 AND APPROVED ON RDA
- [SDR EE4Y2023031017359](https://openairdocs.org/sdr/EE4Y2023031017359.md): Skin · corroded · May 6, 2021 · N218NV · Airbus A320214 · Wing Structure
  > DURING THE VISUAL INSPECTION PER ALLEGIANT TASK CARD ZL-500-03-1-002_P1-OP-UP/0, RIGHT WING UPPER SKIN LOWER SURFACE WAS FOUND CORRODED AT OVERHANG AREA RIB 7. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED AS PER AIRBUS DOSSIER# 80917709 AND APPROVED ON R
- [SDR WX0A2021032673670](https://openairdocs.org/sdr/WX0A2021032673670.md): Battery Pack · no test · Mar 25, 2021 · N218NV · Airbus A320214 · Emergency Lighting
  > DURING CHECK OF BATTERY CAPACITY, AFT BATTERY(13WL) FAILED / REMOVED AND REPLACED AFT BATTERY(13WL) PER AMM 33-51-38. OPS CHECK GOOD."
- [SDR WX0A2021032673669](https://openairdocs.org/sdr/WX0A2021032673669.md): Battery Pack · no test · Mar 25, 2021 · N218NV · Airbus A320214 · Emergency Lighting
  > DURING CHECK OF BATTERY CAPACITY, FWD BATTERY(10WL) FAILED / REMOVED AND REPLACED FWD BATTERY(10WL) PER AMM 33-51-38. OPS CHECK GOOD."
- [SDR WX0A2021032673668](https://openairdocs.org/sdr/WX0A2021032673668.md): Battery Pack · no test · Mar 25, 2021 · N218NV · Airbus A320214 · Emergency Lighting
  > DURING CHECK OF BATTERY CAPACITY, MID R/H BATTERY(12WL) FAILED / REMOVED AND REPLACED MID R/H BATTERY(12WL) PER AMM 33-51-38. OPS CHECK GOOD."
- [SDR WX0A2021032673667](https://openairdocs.org/sdr/WX0A2021032673667.md): Battery Pack · no test · Mar 25, 2021 · N218NV · Airbus A320214 · Emergency Lighting
  > DURING CHECK OF BATTERY CAPACITY, MID L/H BATTERY(11WL) FAILED / REMOVED AND REPLACED MID L/H BATTERY(11WL) PER AMM 33-51-38. OPS CHECK GOOD."
- [SDR WX0A2020120973616](https://openairdocs.org/sdr/WX0A2020120973616.md): Actuator · malfunctioned · Dec 7, 2020 · N218NV · Airbus A320214 · Trailing Edge Flap Actuator
  > F/CTL FLAPS FAULT ON ECAM WHEN FLAPS SELECT TO FLAP 2. PER TSM 27-51-00-810-810-A STEP 4A(5) REMOVED AND REPLACED FLAP ACTUATOR 1 ON LT WING, IAW AMM 27-54-49. OPERATIONS CHECK GOOD.
- [SDR WX0A2020072273531](https://openairdocs.org/sdr/WX0A2020072273531.md): Power Supply · malfunctioned · Jul 22, 2020 · N218NV · Airbus A320214 · Emergency Lighting
  > REF R OFFWING ESCAPE SLIDE R & R, UPON OPERATIONAL CHECK OF EMERGENCY LIGHTING SYS, RECEIVED EPSU INT LOAD AFT L MAINTENANCE MESSAGE / PER TSM 33-51-00-810-807-A, PERFORMED VISUAL CHECK OF CABIN EMERGENCY LIGHT SYSTEM, FOUND AFT LEFT CABIN DOOR OVERHEAD FWD LA
- [SDR WX0A2020040173497](https://openairdocs.org/sdr/WX0A2020040173497.md): Battery · discharged · Apr 1, 2020 · N218NV · Airbus A320214 · Emergency Lighting
  > EPSU BATTERY FIN# 10WL FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"
- [SDR WX0A2020040173496](https://openairdocs.org/sdr/WX0A2020040173496.md): Battery · discharged · Apr 1, 2020 · N218NV · Airbus A320214 · Emergency Lighting
  > EPSU BATTERY FIN# 11WL FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"
- [SDR WX0A2020040173495](https://openairdocs.org/sdr/WX0A2020040173495.md): Battery · discharged · Apr 1, 2020 · N218NV · Airbus A320214 · Emergency Lighting
  > EPSU BATTERY FIN# 13WL FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"
- [SDR WX0A2018101073370](https://openairdocs.org/sdr/WX0A2018101073370.md): Megaphone · inoperative · Oct 8, 2018 · N218NV · Airbus A320214 · Emergency Equipment
  > FLT ATT REPORTED THE MEGAPHONE WAS INOPERATIVE. R & R THE MEGAPHONE.
- [SDR WX0A073225](https://openairdocs.org/sdr/WX0A073225.md): Servo Valve · failed · Feb 2, 2017 · N218NV · Airbus A320214 · Landing Gear Steering System
  > DURING CRUISE, RECEIVED N/W STRG FAULT ON UPPER ECAM. RESET UNSUCCESSFUL. EMERGENCY DECLARED. REPLACED STEERING SERVO VALVE"
- [SDR WX0A2017020373226](https://openairdocs.org/sdr/WX0A2017020373226.md): Connector · contaminated · Feb 1, 2017 · N218NV · Airbus A320214 · Landing Gear System Wiring
  > EMERGENCY DECLARED, DURING CRUISE RECEIVED WHEEL NW STRG FAULT ON UPPER ECAM. UNABLE STEER AIRCRAFT WITH EITHER TILLER PER MAINTENANCE REQUEST. TROUBLE SHOT PER TSM, CLEANED WATER OFF SERVO CONNECTOR. FAULT CLEARED, OPS CHECK AND TAXI CHECK WITH CREW WAS SUCC
- [SDR WX0A2015082172828](https://openairdocs.org/sdr/WX0A2015082172828.md): Light · inoperative · Aug 21, 2015 · N218NV · Airbus A320214 · Emergency Lighting
  > EMERGENCY EXIT LIGHT LAMP BURNED. REPLACED LAMP IN EMER EXIT SIGNS AS REQUIRED IAW AMM 33-51-16 PB 401. OPERATIONS NORMAL.

Next page: https://openairdocs.org/aircraft/N218NV/reports.md?page=2

## 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 = 'N218NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N218NV/reports

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