# Service difficulty reports: N338NV

A list on [N338NV](https://openairdocs.org/aircraft/N338NV.md).

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

- [SDR WX0A2026071732894](https://openairdocs.org/sdr/WX0A2026071732894.md): Engine · faulted · Jul 17, 2026 · N338NV · Airbus A319112 · Engine (Turbine/Turboprop)
  > (AIRCRAFT GROUNDED) (ENG SHUTDOWN EVENT) AT ABOUT 26000FT DURING A DECENT ENG 1 MADE A LOUD BANG AND SHUT ITSELF DOWN. UPON INSPECTION, DETERMINATION MADE FOR ENGINE REPLACEMENT. ASSIGNED W.O. 556297 FOR REPLACEMENT. REFER TO ALL NR'S ON WORK ORDER.
- [SDR WX0A2026021332732](https://openairdocs.org/sdr/WX0A2026021332732.md): Power Supply · no test · Feb 11, 2026 · N338NV · Airbus A319111 · Emergency Lighting
  > AIRCRAFT NOT GROUNDED. 10WL FAILED EPSU BATTERY CAPACITY TEST AND 11WL FAILED EPSU BATTERY TEST. R & R 10WL EPSU IAW AMM 33-51-38-000-001-A AND AMM 33-51-38-400-002-A. R & R 11WL EPSU IAW AMM 33-51-38-000-001-A AND AMM 33-51-38-400-002-A.
- [SDR WX0A2025092432579](https://openairdocs.org/sdr/WX0A2025092432579.md): Lens · broken · Sep 22, 2025 · N338NV · Airbus A319111 · Emergency Lighting
  > AIRCRAFT NOT GROUNDED, EXIT LIGHT COVER FROM L1 BROKEN. INSTALLED EXIT LIGHT LENS AT L1 DOOR IAW AMM 33-51-13-400-001-A. A/C OK FOR SERVICE.
- [SDR WX0A2025061332458](https://openairdocs.org/sdr/WX0A2025061332458.md): Slide · faulted · Jun 12, 2025 · N338NV · Airbus A319111 · Escape Slide
  > (AIRCRAFT NOT GROUNDED) LEFT OVERWING SLIDE NOT ARMED / REMOVED AND REINSTALLED LT OVER WING EXIT ROW DOOR TO RESET SLIDE IND. IAW AMM 52-21-11-04 CONF"
- [SDR WX0A2025061832466](https://openairdocs.org/sdr/WX0A2025061832466.md): Cooling Fan · odor · Jun 10, 2025 · N338NV · Airbus A319111 · Air Distribution Fan
  > (AIRCRAFT NOT GROUNDED) AFTER LANDING AFT FA'S REPORTED ""DIRTY SOCKS"" SMELL FOR LAST 15 MIN OF FLIGHT ON DESCENT / PERFORMED TC A32X-21-000-001, BEFORE PERFORMING ENGINE RUNS REACTICATED PACK 2 IAW AMM 21-51-00-400-002-A. WHILE AT THE GATE WITH APU BLEED AND
- [SDR WX0A2025060632448](https://openairdocs.org/sdr/WX0A2025060632448.md): Slide · inoperative · Jun 5, 2025 · N338NV · Airbus A319111 · Escape Slide
  > (AIRCRAFT NOT GROUNDED) FA ADVISES L1 DOOR SLIDE WILL NOT ARM / PERFOMED OPS CHECK SEVERAL TIMES IAW AMM 25-42-44-400-006-A NO FAULTS FOUND. NORMAL OPERATION VERIFIED."
- [SDR EE4Y2025060422450](https://openairdocs.org/sdr/EE4Y2025060422450.md): Fitting · cracked · Jun 4, 2025 · N338NV · Airbus A319112 · Fuselage Main, Structure
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD A32X-53-210-003, UPPER FUSELAGE COCKPIT WINDSHIELD CENTER POST LOWER ATTACHMENT AREA CONTINUITY FITTINGS WITH CRACK WERE FOUND. CONTINUITY FITTINGS WERE REPLACED PER ALLEGIANT EO # A32X-STR-53ERO-00285-R00.THIS
- [SDR EE4Y2025060422449](https://openairdocs.org/sdr/EE4Y2025060422449.md): Door Frame · cracked · Jun 4, 2025 · N338NV · Airbus A319112 · Fuselage Main, Structure
  > DURING ACCOMPLISHMENT OF THE ALLEGIANT INSPECTION PER WROK CARD A32X-53-260-002, UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR 66 LHS DOOR STOP FITTING # 2 LOWER I/B HOLE WITH CRACK INDICATION. PERFORMED REPAIR STOP FITTING HOLES OF LH AFT DOOR FR 66 FREEZE
- [SDR EE4Y2025060422448](https://openairdocs.org/sdr/EE4Y2025060422448.md): Door Frame · cracked · Jun 4, 2025 · N338NV · Airbus A319112 · Fuselage Main, Structure
  > DURING ALLEGIANT INSPECTION PER WORK CARD A32X-53-260-002, UPPER FUSELAGE AFT PAX CABIN/ENTRY DOOR FR66 LHS DOOR STOP FITTING # 1 LOWER I/B HOLE WITH CRACK INDICATION WAS FOUND.PERFORMED REPAIR STOP FITTING HOLES OF LHS AFT DOOR FR 66 - FREEZE PLUG AND OVERSIZ
- [SDR EE4Y2025060422447](https://openairdocs.org/sdr/EE4Y2025060422447.md): Door Frame · cracked · Jun 4, 2025 · N338NV · Airbus A319112 · Fuselage Main, Structure
  > DURING ALLEGIANT INSPECTION PER WORK CARD A32X-53-260-002, UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR66 RHS DOOR STOP FITTING # 1 LOWER I/B HOLE WITH CRACK INDICATION WAS FOUND.PERFORMED REPAIR STOP FITTING HOLES OF RHS AFT DOOR FR 66 FREEZE PLUG AND OVER
- [SDR EE4Y2025060422446](https://openairdocs.org/sdr/EE4Y2025060422446.md): Frame · cracked · Jun 4, 2025 · N338NV · Airbus A319112 · Fuselage Main, Frame
  > DURING ALLEGIANT INSPECTION PER EO # A32X-E5311-0018, UPPER FUSELAGE DOOR FR16 RH AT DOUBLE JOGGLE AREA IN THE OUTER FLANGE OF THE FRAME AFT ROW OF FASTENER TWO INCHES ABOVE OF THE STOP FITTING 7 FASTENER HOLE WITH CRACK INDICATION WAS FOUND.PERFORMED FASTENER
- [SDR WX0A2025032832369](https://openairdocs.org/sdr/WX0A2025032832369.md): Oxygen Bottle · faulted · Mar 27, 2025 · N338NV · Airbus A319111 · Passenger Oxygen System
  > (AIRCRAFT NOT GROUNDED) OXYGEN CONTAINER ROW 26ABC CAME DOWN AFTER TAKE OFF. / REMOVED AND REPLACED EMERGENCY O2 CONTAINER AT 26ABC IAW AMM 35-21-41-000/400-001-A. OPS CHECK GOOD. THIS CLEARS MEL 35-21-01A. MDDR# 209815. PLACARDS REMOVED."
- [SDR WX0A2025032432365](https://openairdocs.org/sdr/WX0A2025032432365.md): Light · inoperative · Mar 22, 2025 · N338NV · Airbus A319111 · Emergency Lighting
  > (AIRCRAFT NOT GROUNDED) EMERGENCY EXIT LIGHT ABOVE R1 DOOR INOP / REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD IAW AMM 33-51-11-04 CONF 00"
- [SDR WX0A2025012732287](https://openairdocs.org/sdr/WX0A2025012732287.md): Stowage Box · no test · Jan 26, 2025 · N338NV · Airbus A319111 · Crew Oxygen System
  > (AIRCRAFT NOT GROUNDED) F/O OXYGEN MASK NOT TESTING PROPERLY / REMOVED & REPLACED F/O'S MASK AND BOX REF AMM 35-12-41-400-001-A OPS AND LEAK OK"
- [SDR WX0A2024120432227](https://openairdocs.org/sdr/WX0A2024120432227.md): Skin · dented · Nov 29, 2024 · N338NV · Airbus A319111 · Fuselage Main, Frame
  > (AIRCRAFT NOT GROUNDED) (DISCREPANCY NOTED DURING AIRCRAFT HEAVY MX VISIT) PERMANENT REPAIR PER EA 79-2024-184 NEED ACCOMPLISHED. DENT FWD FUSE AT FR21 +300MM, BELOW STR 23L / PERMANENT REPAIR PER EA 79-2024-184 ACCOMPLISHED. DENT FWD FUES AT FR21+300 MM BELO
- [SDR WX0A2024022631967](https://openairdocs.org/sdr/WX0A2024022631967.md): Epsu · no test · Feb 22, 2024 · N338NV · Airbus A319111 · Emergency Lighting
  > DURING EPSU BATTERY CAPACITY TEST ALL FOUR BATTERIES FAILED. / REMOVED AND REPLACED EPSU BATTERIES (10WL, 11WL, 12WL, 13WL) REF AMM 33-51-38-000-002-A & 33-51-38-400-002-A. OPS TEST GOOD."
- [SDR WX0A2023121131916](https://openairdocs.org/sdr/WX0A2023121131916.md): Epsu · unknown · Dec 10, 2023 · N338NV · Airbus A319111 · Emergency Lighting
  > EPSU 11WL FAILED WEEKLY BITE CHECK / TROUBLESHOT PER TSM 33-51-00-810-834-A. REMOVED AND REPLACED 11WL BATTERY PER AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A. OPS CHECK GOOD"
- [SDR WX0A2023100431858](https://openairdocs.org/sdr/WX0A2023100431858.md): Epsu · unknown · Oct 3, 2023 · N338NV · Airbus A319111 · Emergency Lighting
  > FOUND FWD EMERGANCY LIGHTS OUT / REPLACED EMER BATTERY PACK, FWD FIN 10WL, OPS CHECK GOOD REF AMM 33-51-38-400-002A"
- [SDR WX0A2023083031826](https://openairdocs.org/sdr/WX0A2023083031826.md): Epsu · unknown · Aug 29, 2023 · N338NV · Airbus A319111 · Emergency Lighting
  > EPSU BATTERY 13WL AFT, FAILED CAP TEST PER T/C 335100-03-1 / REPLACED AFT EPSU BATTERY FIN 13WL IAW AMM 33-51-38-000-002A AND 33-51-38-400-002A. OPS CHECKS NORMAL."
- [SDR EE4Y2023062717942](https://openairdocs.org/sdr/EE4Y2023062717942.md): Frame · unknown · Jun 27, 2023 · N338NV · Airbus A319112 · Fuselage Structure (General)
  > DURING THE STRUCTURAL INSPECTION AS PER ALLEGIANT TASK: 534124-01-2-001 AN EXISTNG REPAIR WHICH INTERFERES WITH THE INSPECTION AND WITH A DEVIATION WAS FOUND. ALL DETAILS ABOUT EXISTING REPAIR WERE SENT TO AIRBUS ASKING ABOUT FORM APPROVAL TO COVER THE DEVIATI
- [SDR EE4Y2023031017394](https://openairdocs.org/sdr/EE4Y2023031017394.md): Beam · corroded · Mar 10, 2023 · N338NV · Airbus A319111 · Fuselage Structure (General)
  > DURING TH ESTRUCTURE INSPECTION WAS FOUND AT UPPER FUSELAGE FORWARD PAX CABIN AT FR 16, Y503.2 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM P/N: D5311282720200 FROM FR 12 TO FR 16 Y503.2 WAS REPLACED IAW A319 SRM 51-72-11-911-001. THE R
- [SDR EE4Y2023031017393](https://openairdocs.org/sdr/EE4Y2023031017393.md): None · corroded · Mar 10, 2023 · N338NV · Airbus A319111 · Fuselage Structure (General)
  > DURING TH ESTRUCTURE INSPECTION WAS AT UPPER FUSELAGE AFT PASSENGER CREW DOOR CUTOUT BETWEEN FR 66 AND FR 68 AT STRG 23R SILL BEAM WITH CORROSION. DUE TO THIS FACT SILL BEAM P/N D5348004320701 WAS REPLACED IAW A319 SRM 51-72-11-911-001 PARAGRAPH 2B. THE REPLAC
- [SDR EE4Y2023031017392](https://openairdocs.org/sdr/EE4Y2023031017392.md): Beam · corroded · Mar 10, 2023 · N338NV · Airbus A319111 · Fuselage Structure (General)
  > DURING TH ESTRUCTURE INSPECTION WAS AT UPPER FUSELAGE AFT PAX CABIN AT FR 68+80MM Y160.5 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM FROM FR 68 TO FR 70 Y160.5 WAS REPLACED IAW A319 SRM 51-72-11-911-001. THE REPLACE WAS HANDLED UNDER C
- [SDR EE4Y2023031017391](https://openairdocs.org/sdr/EE4Y2023031017391.md): Beam · corroded · Mar 10, 2023 · N338NV · Airbus A319111 · Fuselage Structure (General)
  > DURING TH ESTRUCTURE INSPECTION WAS FOUND IN THE UPPER FUSELAGE AFT PAX CABIN AT FR 68 Y765 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM P/N D5472192200000 WAS REPLACED IAW A319 SRM 51-72-11-911-001 PARAGRAPH 2. THE REPAIR WAS HANDLED
- [SDR EE4Y2023031017390](https://openairdocs.org/sdr/EE4Y2023031017390.md): Frame · none · Mar 10, 2023 · N338NV · Airbus A319111 · Fuselage Structure (General)
  > DURING TH ESTRUCTURE INSPECTION WAS FOUND IN THECCKPIT WINSHIEL SIDE POST FR 4LH UPPER ATTACHMENT FITTING AND FRAME SECTION WITH DOUBLE HOLE. DUE TO THIS FACT FITTING P/N D5311086620200 AND FRAME P/N D53111068202200 WERE REPLACED. THE REPAIR WAS HANDLED UNDER
- [SDR EE4Y2023100317401](https://openairdocs.org/sdr/EE4Y2023100317401.md): Skin Panel · dented · Mar 10, 2023 · N338NV · Airbus A319111 · Wing Structure
  > DESCRIPTION: DURING THE STRUCTURAL INSPECTION, IT WAS FOUND AT LH WING SLAT #1 FROM TRACK #2 100MM O/B AND 111MM FROM THE LOWER EDGE, EXTERNAL SKIN WITH DENT CORRECTIVE ACTION EVALUATED DENT AND IT WAS FOUND WITHIN LIMITS IAW A319 SRM 57-40-00-283-001 FIGUR
- [SDR EE4Y2023100317400](https://openairdocs.org/sdr/EE4Y2023100317400.md): Skin Panel · corroded · Mar 10, 2023 · N338NV · Airbus A319111 · Fuselage Structure (General)
  > DESCRIPTION: DURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD 200003-01-1-001_P1-OP-UP/0 PROCESS, COO FOUND AT EMPENNAGE, DORSAL FIN AREA WITH CORROSION BETWEEN THE SKIN AND CONNECTOR 7113VC. CORRECTIVE ACTION REPAIRED FUSELAGE SKIN SECTION FROM F
- [SDR EE4Y2023031017399](https://openairdocs.org/sdr/EE4Y2023031017399.md): Fitting · corroded · Mar 10, 2023 · N338NV · Airbus A319111 · Empennage Structure
  > DESCRIPTION: DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE ARM#7 WITH CORROSION. CORRECTIVE ACTION: REPLACED HINGE ARM BR7 IAW A319-SRM TASK 55-36-42-300-003. SEE COOPESA WORK ORDER A1M116
- [SDR EE4Y2023031017398](https://openairdocs.org/sdr/EE4Y2023031017398.md): Fitting · none · Mar 10, 2023 · N338NV · Airbus A319111 · Empennage Structure
  > DESCRIPTION: DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE #3 BEARING WITH PLAY. CORRECTIVE ACTION: REPLACED FORK AND END FITTING AT HINGE ARM BR3 IAW A319-SRM TASK 55-36-42-300-008. SEE
- [SDR EE4Y2023031017397](https://openairdocs.org/sdr/EE4Y2023031017397.md): Fitting · none · Mar 10, 2023 · N338NV · Airbus A319111 · Empennage Structure
  > DESCRIPTION: DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE #7 BEARING WITH PLAY. CORRECTIVE ACTION: REPLACED FORK AND END FITTING AT HINGE ARM BR7 IAW A319-SRM TASK 55-36-42-300-008. SEE
- [SDR EE4Y2023031017396](https://openairdocs.org/sdr/EE4Y2023031017396.md): Fitting · excess play · Mar 10, 2023 · N338NV · Airbus A319111 · Fuselage Main, Structure
  > DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE#5 BEARING WITH PLAY. REPLACED FORK AND END FITTING AT HINGE ARM BR5 IAW A319-SRM TASK 55-36-42-300-008. SEE COOPESA WORK ORDER A1M116 3-16
- [SDR EE4Y2023031017395](https://openairdocs.org/sdr/EE4Y2023031017395.md): Fitting · excess play · Mar 10, 2023 · N338NV · Airbus A319111 · Fuselage Main, Structure
  > DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE#4 BEARING WITH PLAY. REPLACED FORK AND END FITTING AT HINGE ARM BR4 IAW A319-SRM TASK 55-36-42-300-008. SEE COOPESA WORK ORDER A1M116 3-15
- [SDR WX0A2023010931694](https://openairdocs.org/sdr/WX0A2023010931694.md): Megaphone · no test · Jan 8, 2023 · N338NV · Airbus A319111 · Emergency Equipment
  > AFT MEGAPHONE FAILED PRE FLIGHT INSPECTION / REMOVED AND REPLACED MEGAPHONES PER LOPA ""A125000L03"" REV ""00"" AND PER AMM 25-65-51"
- [SDR WX0A2023010931693](https://openairdocs.org/sdr/WX0A2023010931693.md): Megaphone · none · Jan 8, 2023 · N338NV · Airbus A319111 · Emergency Equipment
  > FWD MEGAPHONE FAILED PRE FLIGHT INSPECTION / PERFORMED OPS CHECK ON MEGAPHONE ""FLASHING GREEN"" INDICATES GOOD BATTIERIES. OPS CHECK GOOD PER AMM 25-65-710-002"
- [SDR WX0A2022091674250](https://openairdocs.org/sdr/WX0A2022091674250.md): None · none · Sep 14, 2022 · N338NV · Airbus A300* · Emergency Locator Beacon
  > R2 DOOR SLIDE INADVERTENTLY DEPLOYED / REPLACED R2 SLIDE PER AMM 25-62-44-000-802-A. GOOD FOR SERVICE."
- [SDR WX0A2022090674232](https://openairdocs.org/sdr/WX0A2022090674232.md): Epsu · none · Sep 6, 2022 · N338NV · Airbus A319111 · Lighting System
  > EPSU BATTERY (10WL) FWD L FAILED WHEN PERFORMING TC CHECK BATTERY CAPACITY 335100-03-1-001. / R&R EPSU BATTERY (10WL) FWD L IAW TSM 33-51-00-810-822-A. OPS CHECK GOOD. NO DEFECTS NOTED."
- [SDR WX0A2022080874195](https://openairdocs.org/sdr/WX0A2022080874195.md): Megaphone · none · Aug 6, 2022 · N338NV · Airbus A319111 · Escape Slide
  > R2 MEGAPHONE INOP / R&R'D MEGAPHONE IN REF TO AMM 25-65-11. OPS CHECK GOOD."
- [SDR EE4Y2022063015861](https://openairdocs.org/sdr/EE4Y2022063015861.md): Frame · cracked · Jun 30, 2022 · N338NV · Airbus A319111 · Fuselage Structure (General)
  > DURING THE STRUCTURAL INSPECTION PER 531135-01-2-001 MPD, IT WAS FOUND LH WINDSHIELD SIDE POST UPPER ATTACHMENT AT FRAME 4 WITH A HOLE WITH CRACK INDICATION AND FITTING WITH A DOUBLE HOLE AND FRAME SECTION WITH TOOL MARK.. DUE TO THIS FACT DETAILS WERE SENT T
- [SDR WX0A2022012473935](https://openairdocs.org/sdr/WX0A2022012473935.md): Cover · missing · Jan 23, 2022 · N338NV · Airbus A319111 · Emergency Lighting
  > THE R/H FWD EMERGENCY EXIT WALL MOUNTED LIGHT COVER MISSING / REPLACED MISSING LENS COVER ON THE R/H FWD EMERGENCY EXIT WALL MOUNTED LIGHT IAW AMM 33-51-13"
- [SDR WX0A2021093073848](https://openairdocs.org/sdr/WX0A2021093073848.md): Battery Pack · faulted · Sep 27, 2021 · N338NV · Airbus A319111 · Emergency Lighting
  > WHEN POWER IS DISCONNECTED AND EMERGENCY LIGHTS ARE SUPPOSED TO TRIGGER ON, ONLY THE REAR CABIN EXIT SIGN AND OVERHEAD LIGHTS AT SEAT ROWS 19 AND 28 ILLUMINATE. ALL OTHER OVERHEAD LIGHTS ARE INOP, INCLUDING OVERWING EXIT SIGNS AND L1 & R1 EXIT SIGNS. / FOUND (
- [SDR WX0A2021092773844](https://openairdocs.org/sdr/WX0A2021092773844.md): Battery Pack · faulted · Sep 26, 2021 · N338NV · Airbus A319111 · Emergency Lighting
  > WHEN POWER IS DISCONNECTED AND EMERGENCY LIGHTS ARE SUPPOSED TO TRIGGER ON, ONLY THE REAR CABIN EXIT SIGN AND OVERHEAD LIGHTS AT SEAT ROWS 19 AND 28 ILLUMINATE. FOUND (10WL, 11WL AND 12WL) EPSU BATTERY TO BE FAULTING REPLACED ALL 3 BATTERY IAW AMM 33-51-38
- [SDR WX0A2021051773717](https://openairdocs.org/sdr/WX0A2021051773717.md): Battery Pack · no test · May 15, 2021 · N338NV · Airbus A319112 · Emergency Lighting
  > R/H OVER WING EMERGENCY POWER PACK BATTERY FAILS TEST. / REPLACED R/H EMERGENCY POWER PACK BATTERY AND PERFORMED OPS TEST PER AMM 33-51-38 P/B 401. OK FOR SERVICE."
- [SDR WX0A2020080373542](https://openairdocs.org/sdr/WX0A2020080373542.md): Battery Pack · no test · Jul 31, 2020 · N338NV · Airbus A319111 · Emergency Lighting
  > CABIN EMERGENCY BATTERY CLASS 1 FAULT AFT L (13WL) / REMOVED AND REPLACED AFT L EMERGENCY SUPPLY BATTERY UNIT IAW AMM 33-51-000-002-A AND 33-51-38-400-002-A. OPS CHECK GOOD"
- [SDR WX0A2020072473532](https://openairdocs.org/sdr/WX0A2020072473532.md): Controller · malfunctioned · Jul 23, 2020 · N338NV · Airbus A319111 · Cabin Pressure Controller
  > DESCENDING THROUGH APPROXIMATELY FL320 RECEIVED ECAM CAB PR EXCESS CAB ALT AND COMPLIED WITH THOSE PROCEDURE. CABIN PRESSURE GOT AS HIGH AS 12500 FT. MASK DID NOT DEPLOY. OTHER ECAM THAT FOLLOWED WERE CABPR LO DIFF PR, DOOR R AFT CABIN, AND CAB PR SAFETY VALV
- [SDR WX0A2019120273441](https://openairdocs.org/sdr/WX0A2019120273441.md): Battery Pack · inoperative · Dec 1, 2019 · N338NV · Airbus A319112 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST FOUND EMERGENCY BATTERY PACK 12WL INOP / "
- [SDR WX0A2019120273440](https://openairdocs.org/sdr/WX0A2019120273440.md): Battery Pack · inoperative · Nov 29, 2019 · N338NV · Airbus A319112 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST FOUND EMERGENCY LIGHT BATTERY PACK 11WL INOP. / "

## 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 = 'N338NV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N338NV/reports

---
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