# Service difficulty reports: N310NV, cancelled Mar 29, 2026

A list on [N310NV, cancelled Mar 29, 2026](https://openairdocs.org/deregistered/N310NV-2026-03-29.md).

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

- [SDR WX0A2025031432355](https://openairdocs.org/sdr/WX0A2025031432355.md): Girt Bar · fod · Mar 13, 2025 · N310NV · Airbus A319112 · Emergency Equipment
  > (AIRCRAFT NOT GROUNDED) L1 DOOR SLIDE WILL NOT ARM. / REMOVED DEBRIS FROM SLIDE ARMING MECHANISM AND PERFORMED FUNCTIONAL TEST W/GOOD RESULTS IAW AMM 52-10-00-720-005-A."
- [SDR WX0A2024042232016](https://openairdocs.org/sdr/WX0A2024042232016.md): O2 Generator · no test · Apr 18, 2024 · N310NV · Airbus A319112 · Passenger Oxygen System
  > PASSENGER CABIN, O2 CONTAINER OF SEAT 24ABC FAILED TO DEPLOY. O2 CONTAINER OF SEAT 24ABC REPLACED AND TESTED SERVICEABLE IAW AMM 35-21-41-400-001-A.
- [SDR WX0A2023091031838](https://openairdocs.org/sdr/WX0A2023091031838.md): Epsu · unknown · Sep 7, 2023 · N310NV · Airbus A319112 · Emergency Lighting
  > DURING WEEKLY CHECK, FOUND EPSU BATTERIES AT LOCATION 10WL, 11WL, 12WL, 13WL FAILED THE EPSU SYSTEM TEST / REMOVED AND REPLACED EPSU BATTERIES AT LOCATIONS 10WL, 11WL, 12WL AND 13WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CHECK OF BATTERIES OKAY
- [SDR WX0A2023013031716](https://openairdocs.org/sdr/WX0A2023013031716.md): Battery Pack · no test · Jan 28, 2023 · N310NV · Airbus A319112 · Emergency Lighting
  > EMER L EPSU BATTERY (11WL) NEEDS REPLACMENT DUE TO FAILED EPSU BATTERY TEST ON MCDU / REMOVED AND REPLACED BATTERY OF EPSU IAW AMM 33-51-38-020-053-A, 33-51-38-420-054-A AND 25-23-44 PB 401"
- [SDR WX0A2022081574208](https://openairdocs.org/sdr/WX0A2022081574208.md): Light · inoperative · Aug 14, 2022 · N310NV · Airbus A319112 · Flight Compartment Lighting
  > R2 DOOR EXIT LIGHT COVER MISSING / INSTALLED NEW LIGHT LENS ON R2 EMERGENCY EXIT LIGHT ASSY. REF. AMM 33-51-13, OPS. CK. GOOD."
- [SDR WX0A2022050774085](https://openairdocs.org/sdr/WX0A2022050774085.md): None · none · May 7, 2022 · N310NV · Airbus A319112 · Lighting System
  > LTPR:5001159485-0010 EPSU 12WL FOUND INOP. TO BE REPLACED IAW AMM 33-51-38 PB 401/ REV 34.//REM/INS OF EPSU 12WL PERFORMED IAW 33-51-38 PB 401 /REV 34. PERFORMED OPERATIONAL CHECK OF THE EPSU THRU BITE TEST IAW AMM 33-51-00-710-001/ REV 34."
- [SDR WX0A2022021173992](https://openairdocs.org/sdr/WX0A2022021173992.md): Epsu · none · Feb 8, 2022 · N310NV · Airbus A319112 · Lighting System
  > AIRCRAFT DUE EMERGENCY LIGHT BATTERY CAP CHECK / REMOVE AND REPLACED 4 EMERGENCY LIGHT BATTERIES 10-WL, 11-WL, 12-WL, AND 13-WL REF AMM 33-51-38."
- [SDR WX0A2022020473955](https://openairdocs.org/sdr/WX0A2022020473955.md): Megaphone · faulty · Feb 3, 2022 · N310NV · Airbus A319112 · Escape Slide
  > MEGAPHONE AT FA POSITION 4 (AIRCRAFT RIGHT) DOESN'T CLICK FOR PREFLIGHT. / REMOVED AND REPLACED INOP MEGAPHONE WITH REFERENCE TO ALLEGIANT AIR STANDARD INDUSTRY PRACTICES."
- [SDR WX0A2022013173949](https://openairdocs.org/sdr/WX0A2022013173949.md): Connector · dirty · Jan 31, 2022 · N310NV · Airbus A319112 · Emergency Lighting
  > CIDS1 EPSU SYS TEST 13 WL / REMOVED AND CLEANED CONNECTOR AT 13WL AND MESSAGE CLEARED FROM CIDS1; TEST OK REF TC 05-000-002 AND AMM 33-51-00. ALSO REF ESPM 20-55-40."
- [SDR WX0A2022010373916](https://openairdocs.org/sdr/WX0A2022010373916.md): Light · false indication · Dec 30, 2021 · N310NV · Airbus A319112 · Emergency Lighting
  > EMERGENCY EXIT OVERWING LIGHTS DID NOT FLASH ON WHEN NO SMOKING SWITCH WAS CYCLED PASSING THROUGH 10,000 FT PER FCOM PROCEDURE. / PERFORMED OPS TEST OF OVERWING EMERENCY EXIT LIGHTS IAW A319 AMM 33-51-15 PB 401. OPS CK GOOD. OK FOR SERVICE."
- [SDR WX0A2021092773843](https://openairdocs.org/sdr/WX0A2021092773843.md): Unknown · vibration · Sep 26, 2021 · N310NV · Airbus A319112 · Fuselage Structure (General)
  > (EMERGENCY DECLARED) RHYTHMIC VIBRATION FELT THROUGHOUT AIRFRAME DURING CLIMB WITHOUT CONFIGURATION CHANGES. F/CTL PAGE DISPLAYED ALL SURFACES STOWED. LAND LIGHTS RETRACTED. AUTO PILOT WAS ON. FLIGHT ATTENDANTS REPORTED STRANGER VIBRATION ON THE AFT SECTION. V
- [SDR WX0A2021053173727](https://openairdocs.org/sdr/WX0A2021053173727.md): Epsu · no test · May 28, 2021 · N310NV · Airbus A319112 · Emergency Lighting
  > EPSU BATTERY 11WL FAILED EPSU SYSTEM 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 WX0A2020101973590](https://openairdocs.org/sdr/WX0A2020101973590.md): Epsu · failed · Oct 16, 2020 · N310NV · Airbus A319112 · Emergency Lighting
  > DURING CABIN EMERGENCY LIGHTING CHECK, FOUND EPSU FIN 12WL BAD. R & R EPSU 12WL, REF AMM 33-51-38 PB 401. BITE CHECK OK.
- [SDR WX0A2020091173571](https://openairdocs.org/sdr/WX0A2020091173571.md): O-Ring · leaking · Sep 10, 2020 · N310NV · Airbus A319112 · Hydraulic System, Main
  > DURING FLIGHT WE HAD ECAM "HYD Y ENG 2 PUMP LO PR" FOLLOWED BY ECAM "HYD Y RSVR LO LVL, RAN ECAM + QRH PROCEDURES. FOUND HYDRAULIC LEAK AT YELLOW SYS PTU MANIFOLD FIN 3015GM. O-RING UNDER REDUCER REPLACED, REF AMM 29-13-15-400-001-A. YELLOW SYS SERVICED, RE
- [SDR WX0A2020061973515](https://openairdocs.org/sdr/WX0A2020061973515.md): Battery Pack · no test · Jun 17, 2020 · N310NV · Airbus A319112 · Emergency Lighting
  > EPSU BATTERY FIN# 10WL FAILED EPSU BAT CAP TEST. REPLACED EPSU BATTERY.
- [SDR WX0A2020032373491](https://openairdocs.org/sdr/WX0A2020032373491.md): Battery Pack · failed · Mar 22, 2020 · N310NV · Airbus A319112 · Emergency Lighting
  > EPSU FAILED EMERGENCY LIGHTING TEST / REPLACED EMERGENCY BATTER PACK "
- [SDR RJEY2019052800004](https://openairdocs.org/sdr/RJEY2019052800004.md): Fitting · not reported · May 14, 2019 · N310NV · Airbus A319111 · Fuselage Miscellaneous Structure
  > LT / RT TORSION BOX LOWER SIDESHELL S-15 REINFORCE FITTING.
- [SDR RJEY2019052800006](https://openairdocs.org/sdr/RJEY2019052800006.md): Floorbeam · corroded · May 4, 2019 · N310NV · Airbus A319111 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM LOC. AT LEVEL OF -Y189 APPROX BTW FR20 TO FR21 IN PASSENGER CABIN.
- [SDR RJEY2019052800005](https://openairdocs.org/sdr/RJEY2019052800005.md): Floorbeam · corroded · Apr 30, 2019 · N310NV · Airbus A319111 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM -Y1292 BTW FR16 AND FR20 FLOOR STRUCTURE PAX CABIN FWD GALLEY AREA.
- [SDR RJEY2019052800002](https://openairdocs.org/sdr/RJEY2019052800002.md): Floorbeam · corroded · Apr 30, 2019 · N310NV · Airbus A319111 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM -Y765 AT LEVEL OF FR20 FLOOR STRUCTURE PAX CABIN FWD GALLEY AREA.
- [SDR RJEY2019052800003](https://openairdocs.org/sdr/RJEY2019052800003.md): Skin Panel · worn · Apr 24, 2019 · N310NV · Airbus A319111 · Fuselage Main, Plate/Skin
  > WEAR IB EXTERNAL SKIN PANEL LOC. ON FR34 BTW STR 43L TO STR 43R.
- [SDR WX0A2018080273364](https://openairdocs.org/sdr/WX0A2018080273364.md): Apu · contaminated · Jul 27, 2018 · N310NV · Airbus A319112 · Airborne Auxiliary Power Unit (APU) System
  > DIRTY SOCK ODOR IN THE CABIN DURING DESCENT. FOUND AND CLEANED OIL FOUND IN THE APU COMPARTMENT AROUND INLET SEAL. OPEN.
- [SDR WX0A2018052173324](https://openairdocs.org/sdr/WX0A2018052173324.md): Plenum · contaminated · May 20, 2018 · N310NV · Airbus A319112 · APU Core Engine
  > BAD ODOR IN CABIN DURING DECENT. FOUND TRACES OF OIL IN THE APU INTAKE PLENUM. CLEANED THE PLENUM.
- [SDR WX0A2018031473313](https://openairdocs.org/sdr/WX0A2018031473313.md): Filter · contaminated · Mar 13, 2018 · N310NV · Airbus A319112 · Air Distribution System
  > DIRTY SOCK SMELL ON CLIMB OUT AND DESCENT/FOUND CONTAMINATED OZONE FILTER, R&R OZONE FILTER.
- [SDR WX0A2016042973149](https://openairdocs.org/sdr/WX0A2016042973149.md): Light · illuminated · Apr 24, 2016 · N310NV · Airbus A319112 · Emergency Lighting
  > EMERGENCY EXIT LIGHTING SYS STAYED ON DURING FLIGHT. EMER LIGHTS PUSHBUTTON ON FWD ATTENDANT PANEL ILLUMINATED.
- [SDR WX0A2016032373111](https://openairdocs.org/sdr/WX0A2016032373111.md): Selector Valve · faulty · Mar 20, 2016 · N310NV · Airbus A319112 · Landing Gear Brake System
  > ON ROLL OUT AFTER LANDING, AFTER ENGAGING MANUAL BRAKING, ALLOWED AUTO BRAKES LO TO SLOW ACFT TO 60 KTS. BRAKES STARTED SLIPPING AT APPROX 48 KTS GND SPEED DOWN TO ABOUT 15 KTS GND SPEED. R & R SELECTOR VLV ALT BRAKE IAW AMM 32-42-11*-PB 40. OPERATIONS CHEC
- [SDR WX0A2016022373093](https://openairdocs.org/sdr/WX0A2016022373093.md): Brake Sys · contaminated · Feb 22, 2016 · N310NV · Airbus A319112 · Landing Gear Brake System
  > DURING DECELERATION PASSING 70 - 60 KNOTS, WHEN TRANSITIONING TO PEDAL BRAKES, BOTH BRAKES GET VERY GRABBY. HAD TO TAP THE BRAKES A FEW TIMES TO LOOSEN THEM UP. WILL NOT BE ABLE TO DUPLICATE DURING SLOW TAXI CHECKS. REF LOG PAGE 635331 IAW MOC REQUEST PERFO
- [SDR WX0A2016010373059](https://openairdocs.org/sdr/WX0A2016010373059.md): Battery Pack · discharged · Dec 29, 2015 · N310NV · Airbus A319112 · Emergency Equipment
  > AFT FLIGHT ATTENDANTS EMER FLASHLIGHT INOPERATIVE. R & R BATTERY PACK IN FLIGHT ATTENDANTS FLASHLIGHT IAW AMM 25-65-00. OPERATIONS CHECKED GOOD.
- [SDR WX0A2015110472985](https://openairdocs.org/sdr/WX0A2015110472985.md): Warning System · false activation · Nov 2, 2015 · N310NV · Airbus A319112 · Smoke Detection
  > ON ECAM, SMOKE FWD CHARGE BOTTLE FAULT & AFT CHARGE BOTTLE FAULT. PERFORMED CARGO SMOKE TEST, FAULT CLEARED, NO FURTHER DEFECTS IAW AMM 26-16-00.
- [SDR WX0A2015061972670](https://openairdocs.org/sdr/WX0A2015061972670.md): Unknown · vibration · Jun 16, 2015 · N310NV · Airbus A319112 · Aircraft Structures
  > CLIMBING OUT OF ABOUT 20000 FEET, SPEED ABOUT 295 VTS, VS ABOUT 2000 FEET, WE EXPERIENCED SIGNIFICANT ACFT VIBRATION. VIBRATION WAS MORE PRONOUNCED IN AFT OF ACFT. ACCORDING TO AFT FA IT WAS INTENSITY OF VIBRATION THEY HAVE NEVER FELT BEFORE. WE WERE IN CLEA
- [SDR WX0A2015022372431](https://openairdocs.org/sdr/WX0A2015022372431.md): Megaphone · inoperative · Feb 20, 2015 · N310NV · Airbus A319112 · Emergency Equipment
  > FORWARD MEGA PHONE INOPERATIVE. REPLACED FWD MEGA PHONE AS REQUIRED. OPERATIONS CHECKED NORMAL IAW 25-60.
- [SDR WX0A2014120972293](https://openairdocs.org/sdr/WX0A2014120972293.md): Servo · out of limits · Dec 3, 2014 · N310NV · Airbus A319112 · Rudder Control System
  > SLIGHT YAW, JERKY, AT CRUISE 370 & 390 FELT IN AFT CABIN WITH SMOOTH AIR. UNABLE TO DISCONNECT AUTOPILOT DUE TO RVSM AIRSPACE. COULD NOT COMPLY WITH STEP 4 OF VIBRATION REPORT. FOUND RUDDER SERVO CONTROL 2025GM, BLUE SYSTEM, TO BE OUT OF LIMITS, SEE LP 5735
- [SDR WX0A2014120272290](https://openairdocs.org/sdr/WX0A2014120272290.md): Unknown · vibration · Nov 30, 2014 · N310NV · Airbus A319112 · Aircraft Structures
  > EXCESSIVE AIRFRAME VIBRATION CLIMBING FROM 26500 ' TO 32500 ' VIBRATION REPORTED GREATER IN THE TAIL OF THE ACFT. DID NOT HEAR VIBRATION. VIBRATION WAS IN A SIDE TO SIDE MOTION, YAW. ACFT WEIGHT 138,000 LBS, AIR SPEED 290 KNOTS, 7.4 MOCK. NR 1 ENG N1 89.3,

## 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 = 'N310NV' AND deregistration_id = 'N310NV-2026-03-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N310NV-2026-03-29/reports

---
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