# Service difficulty reports: N346NB

A list on [N346NB](https://openairdocs.org/aircraft/N346NB.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 4 · 192 reports

- [SDR DALA2026072804378](https://openairdocs.org/sdr/DALA2026072804378.md): Unknown · odor · Jul 27, 2026 · N346NB · Airbus A319114 · Air Distribution System
  > ON TAXI OUT FLT ATTENDANTS REPORTED STRONG FUMES IN BACK OF AIRCRAFT. RETURNED TO GATE BOS. ODOR DISAPPEARED ON TAXI BACK. R & R RECIRC FILTERS PER A319 AMM 21-21 AS PERCAUTION WORKING IN CONJUCTION W/ LOG 1722110. W/C 0550-2002 AND W/C 2100-2007. C/W NO FURT
- [SDR DALA2026071004044](https://openairdocs.org/sdr/DALA2026071004044.md): Fairing · missing · Jul 2, 2026 · N346NB · Airbus A319114 · Engine Thrust Reverser
  > ENG 1 TOP OTBD LOCKOUT FAIRING MISSING. FWD TO CDL 78-00-11, M PROC C/W. REMOVED TOP OTBD THRUST REVERSER LOCKOUT FAIRING, PLACARDS INSTALLED, DISPATCH APPROVED, OK FOR SVC. INSTALLED NR 1 ENG TOP OTBD LOCKOUT FAIRING IAW AMM 78-30 -00. (LP: 8820078, AIRCRA
- [SDR DALA2026061103520](https://openairdocs.org/sdr/DALA2026061103520.md): Control Valve · contaminated · Jun 9, 2026 · N346NB · Airbus A319114 · APU Oil System
  > FO SMELLED WET SOCK SMELL ON TAXI - IN WHEN SWITCHING TO APU BLEED. SMELLED IN FLIGHT DECK ONLY NOT IN CABIN. REMOVED LOAD CTL VLV PER A319 AMM 49-51 INSP FOUND OIL CONTAMINATE. CLEANED AND REINSTALLED (KH 384158) PERFORMED LEVEL B DECONTAMINATION WITH REF TO
- [SDR DALA2026020600878](https://openairdocs.org/sdr/DALA2026020600878.md): None · none · Feb 4, 2026 · N346NB · Airbus A319114 · Standard Practices/Structures
  > ER/A 627460-14 HAS BEEN REVISED TO 'A'. FOLLOW ON ACTION IS REQU IRED. PERFORM SECTION IV THE SOONER OF EVERY 15000FC/30000FH AFTER SEC TION I. ASSOCIATED ER/A 14-627460 ADDED FOR AC 3146. (LP: 1435703)
- [SDR DALA2026020600877](https://openairdocs.org/sdr/DALA2026020600877.md): None · none · Feb 4, 2026 · N346NB · Airbus A319114 · Standard Practices/Structures
  > ER/A 627460-14 HAS BEEN REVISED TO 'A'. FOLLOW ON ACTION IS REQU IRED. PERFORM SECTION III WITHIN THE SOONER OF EVERY 10000FC/20000FH A FTER SECTION I. ASSOCIATED ER/A 14-627460 ADDED FOR AC 3146. (LP: 1435700)
- [SDR DALA2026020100735](https://openairdocs.org/sdr/DALA2026020100735.md): Flap Track · damaged · Jan 27, 2026 · N346NB · Airbus A319114 · Trailing Edge Flaps
  > DAMAGE TOLERANCE EVALUATION ( DTE) STAGE III APPROVAL REQUIRED FOR REPAIR ON THE LT OUTBOARD FLAP, TRACK 3, RIB 5 BORE PER ER/A 627489-14 REV A. SECTION I IS LIMITED TO 72000FC FROM SECTION I. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE ACFT FROM SER
- [SDR DALA2026020100734](https://openairdocs.org/sdr/DALA2026020100734.md): Skin · none · Jan 27, 2026 · N346NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > STAGE III DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR FUSELAGE SKIN REPAIR INSTALLED AT FR25 S-13R/14R PER ER/A 627770-14 R EV A. SECTION I IS LIMITED TO 64000FC FROM SECTION I. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. (LP: 1
- [SDR DALA2025112608645](https://openairdocs.org/sdr/DALA2025112608645.md): Rod End · excess play · Nov 26, 2025 · N346NB · Airbus A319114 · Aileron Control System
  > LEFT AILERON WITH PLAY AT PCA ROD ENDS. CORRECTIVE ACTION: R/R LT INBD AND LT OTBD SERVO CONTROL ACTUATORS PER WC 2714-4001. (7652718).
- [SDR DALA2025100907368](https://openairdocs.org/sdr/DALA2025100907368.md): Skin · ground damage · Oct 8, 2025 · N346NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > FOUND GROUND DAMAGE AT FR13 AND APPROXIMATELY 12 INCHES ABOVE LAP JOINT. COMPLIED WITH ER/A 628891-14. (1241211).
- [SDR DALA2025100907362](https://openairdocs.org/sdr/DALA2025100907362.md): Skin · punctured · Oct 8, 2025 · N346NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > FOUND PUNCTURE AT FR13 AND APPROXIMATELY 12 INCHES ABOVE LAP JOINT. COMPLIED WITH ER/A 628891-14. (1241292).
- [SDR DALA2025100707279](https://openairdocs.org/sdr/DALA2025100707279.md): Skin · ground damage · Oct 7, 2025 · N346NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > FOUND GROUND DAMAGE AT FR13 AND APPROXIMATELY 12 INCHES ABOVE LAP JOINT. COMPLIED WITH ER/A 628891-14. (1238415).
- [SDR DALA2025090106441](https://openairdocs.org/sdr/DALA2025090106441.md): Skin · damaged · Aug 30, 2025 · N346NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > FWD FUSELAGE SKIN DAMAGED LT SIDE BETWEEN FR 13 & F 14, 17.5' ABOVE SKIN BUTT JOINT. COMPLIED WITH ER/A 628891-14. (1172092).
- [SDR DALA2025090106440](https://openairdocs.org/sdr/DALA2025090106440.md): Skin · punctured · Aug 30, 2025 · N346NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > FOUND PUNCTURE FWD AND BELOW L1 DOOR. COMPLIED WITH ER/A 628891-14. (6798600)
- [SDR DALA2025081806181](https://openairdocs.org/sdr/DALA2025081806181.md): Intercostal · damaged · Aug 16, 2025 · N346NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > PAX CABIN, LT PASSENGER & CREW DOOR AT LEVEL OF STOP FITTING NR 1, AT FR 15 WAS FOUND INTERCOSTAL AND ANGLE WITH ELONGATED HOLES. PERFORMED REPAIR AT PAX CABIN LT PASSENGER / CREW DOOR AT FR 15 STOP FITTING #1 AND TEE IAW E/A 627852-14AD. (1147203)
- [SDR DALA2025081806180](https://openairdocs.org/sdr/DALA2025081806180.md): Skin · damaged · Aug 16, 2025 · N346NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE, EXTERNAL SKIN AREA UNDER ANTI-COLISION LIGHT BETWEEN FR 40 AND FR 41 AND BETWEEN STGR 1RH AND STGR 1LH, LEFT FWD SCREW HOLE WITH NICKS. PERFORMED REPAIR AT UPPER FUSELAGE, EXTERNAL SKIN AREA UNDE ANTI-COLISION LIGHT BETWEEN FR 40/41 BETWEEN S
- [SDR DALA2025081806179](https://openairdocs.org/sdr/DALA2025081806179.md): Skin · corroded · Aug 16, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > LEFT WING LOWER SKIN, PYLON AREA, FRONT SPAR BETWEEN RIB 7 AND RIB 8, CORROSION AROUND FASTENER HEAD HOLE. PERFORMED REPAIR AT LT WING BOTTOM SKIN, PYLON REINFORCING PLATE AT RIB 8 ANF STR5 IAW ER/A 627728-14AD. (1147031)
- [SDR DALA2025081806178](https://openairdocs.org/sdr/DALA2025081806178.md): Skin · corroded · Aug 16, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > RIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT WX3690.2 SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT WX3690.2 (AREA 1) I/A/W ER/A 627459-14AD. (1147233)
- [SDR DALA2025081806177](https://openairdocs.org/sdr/DALA2025081806177.md): Skin · corroded · Aug 16, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > RIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 8 +80MM SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 8+80MM (AREA 2) IAW ER/A 627459-14AD. (1147229)
- [SDR DALA2025081806176](https://openairdocs.org/sdr/DALA2025081806176.md): Skin · corroded · Aug 16, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > RIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 14 +390MM SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 14+440MM (AREA 7) I/A/W ER/A 627459-14AD. (1147220)
- [SDR DALA2025081806175](https://openairdocs.org/sdr/DALA2025081806175.md): Skin · corroded · Aug 15, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > RIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 17 +190MM SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 17+410MM (AREA 10) I/A/W ER/A 627459-14AD. (1145846)
- [SDR DALA2025081806174](https://openairdocs.org/sdr/DALA2025081806174.md): Skin · corroded · Aug 15, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > LEFT WING, TOP SKIN PANEL 2 LOWER SURFACE, TRAILING EDGE, OVERHANG AREA, WITH CORROSION AT RIB 11 + 115MM. PERFORMED REPAIR BY INSTALLED EXTERNAL REPAIR DOUBLER AT TOP SKIN PANEL 2, T/E OVERHANG AREA AT RIB 11+115MM (AREA 5) I/A/W ER/A 627460-14AD. (1145623)
- [SDR DALA2025081806173](https://openairdocs.org/sdr/DALA2025081806173.md): Skin · corroded · Aug 15, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > LEFT WING TOP SKIN PANEL 2 LOWER SURFACE, TRAILING EDGE, OVERHANG AREA AT RIB 11+490MM WITH CORROSION. PERFORMED REPAIR BY INSTALLED EXTERNAL REPAIR DOUBLER AT TOP SKIN PANEL 2, T/E OVERHANG AREA AT RIB 11+490MM (AREA 6) IAW ER/ A NO. 627460-14AD. (1145536)
- [SDR DALA2025081806172](https://openairdocs.org/sdr/DALA2025081806172.md): Skin · corroded · Aug 15, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > RIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 14 +45MM SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 14+45MM (AREA 6) I/A/W ER/A 627459-14AD. (1145496)
- [SDR DALA2025081806171](https://openairdocs.org/sdr/DALA2025081806171.md): Skin · corroded · Aug 15, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > RIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 17 SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 17MM (AREA 9) I/A/W ER/A 627459-14AD. (1145479)
- [SDR DALA2025081806170](https://openairdocs.org/sdr/DALA2025081806170.md): Skin · corroded · Aug 15, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > RIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 11 +140MM SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 11+140MM (AREA 4) I/A/W ER/A 627459-14AD. (1145475)
- [SDR DALA2025081806169](https://openairdocs.org/sdr/DALA2025081806169.md): Skin · corroded · Aug 15, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > RIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 11 +500MM SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB II + 500 (AREA 5) IAW ER/A NO. 627459-14AD. (1145453)
- [SDR DALA2025081806168](https://openairdocs.org/sdr/DALA2025081806168.md): Skin · corroded · Aug 15, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > RIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 16 +200MM SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 16+200M (AREA 8) IAW ER/A 627459-14AD. (1145364)
- [SDR DALA2025081506124](https://openairdocs.org/sdr/DALA2025081506124.md): Plate · corroded · Aug 14, 2025 · N346NB · Airbus A319114 · Wing, Nacelle/Pylon Attach Fittings
  > CORROSION WAS FOUND ON THE LT WING LOWER SURFACE PYLON REINFORCEMENT PLATE OTBD SIDE. COMPLIED WITH ER/A 627728-14. (1144222).
- [SDR DALA2025081506122](https://openairdocs.org/sdr/DALA2025081506122.md): Plate · corroded · Aug 14, 2025 · N346NB · Airbus A319114 · Wing, Nacelle/Pylon Attach Fittings
  > CORROSION WAS FOUND ON THE LT WING LOWER SURFACE PYLON REINFORCEMENT PLATE OTBD SIDE. COMPLIED WITH ER/A 627728-14. (1144192).
- [SDR DALA2025081506121](https://openairdocs.org/sdr/DALA2025081506121.md): Bushing · excess play · Aug 14, 2025 · N346NB · Airbus A319114 · Spoilers
  > LEFT WING NR 4 SPOILER WITH PLAY, IT HAS 1.22 MM. REPLACED BAEARINGS SLEEVES AND BUSHINGS AT LT WING SPOILER NR 4 AND CENTER HINGE BRACKET IAW CMM 57-72-21 AND SRM 57- 72-12. (1143283).
- [SDR DALA2025081506120](https://openairdocs.org/sdr/DALA2025081506120.md): Bushing · excess play · Aug 14, 2025 · N346NB · Airbus A319114 · Spoilers
  > RIGHT WING NR 3 SPOILER WITH PLAY. REPLACED BEARINGS SLEVES AND BUSHINGS AT RT WING SPOILER NR 3 CENTER HINGE BRACKET IAW CMM 57-72-21 AND SRM 57-72-12. (1143255).
- [SDR DALA2025081506119](https://openairdocs.org/sdr/DALA2025081506119.md): Bushing · excess play · Aug 14, 2025 · N346NB · Airbus A319114 · Spoilers
  > RIGHT WING NR 5 SPOILER WITH PLAY, IT HAS 1.15 MM. REPLACED BEARINGS SLEEVES AND BUSHINGS AT RT WING SPOILER NR 5 AND CENTER HINGE BRACKET IAW CMM 57-72-21 AND SRM 57-72- 12.
- [SDR DALA2025081506114](https://openairdocs.org/sdr/DALA2025081506114.md): Skin · corroded · Aug 14, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > LEFT WING TOP SKIN PANEL 2 LOWER SURFACE, TRAILING EDGE, OVERHANG AREA AT RIB 10 CORRODED. COMPLIED WITH ER/A 627460-14AD.
- [SDR DALA2025081506113](https://openairdocs.org/sdr/DALA2025081506113.md): Skin · corroded · Aug 14, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > LEFT WING TOP SKIN PANEL 2 LOWER SURFACE, TRAILING EDGE, OVERHANG AREA AT RIB 14 CORRODED. COMPLIED WITH ER/A 627460-14AD.
- [SDR DALA2025081506129](https://openairdocs.org/sdr/DALA2025081506129.md): Bushing · excess play · Aug 14, 2025 · N346NB · Airbus A319114 · Spoilers
  > LEFT WING NR 3 SPOILER WITH PLAY,IT HAS 1.77 MM. REPLACED BEARINGS SLEEVES AND BUSHINGS AT LH WING SPOILER #3 AND CENTER HINGE BRACKET IAW CMM 57-72-21 AND SRM 57-72- 12.
- [SDR DALA2025081506128](https://openairdocs.org/sdr/DALA2025081506128.md): Sleeve · excess play · Aug 14, 2025 · N346NB · Airbus A319114 · Spoilers
  > RIGHT WING NR 2 SPOILER WITH PLAY,IT HAS 1.50 MM. CORRECTIVE ACTION: REPLACED BEARINGS SLEEVES AND BUSHINGS AT RH WING SPOILER NR 2 AND CENTER HINGE BRACKET IAW A319 CMM 57-72-21 AND A319 SRM 57-72- 12.
- [SDR DALA2025081506127](https://openairdocs.org/sdr/DALA2025081506127.md): Bushing · excess play · Aug 14, 2025 · N346NB · Airbus A319114 · Ailerons
  > LEFT WING NR 2 SPOILER WITH PLAY, IT HAS 1.52 MM. REPLACED BAEARINGS SLEEVES AND BUSHINGS AT LT WING SPOILER NR 2 AND CENTER HINGE BRACKET IAW CMM 57-72-21 AND SRM 57- 72-12.
- [SDR DALA2025081406072](https://openairdocs.org/sdr/DALA2025081406072.md): Stringer · corroded · Aug 13, 2025 · N346NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > SHIP 3146 AFT LOWER REAR FUSELAGE, AFT CARGO COMPARTMENT BETWEEN FR59 AND FR60, STGR 33R WITH CORROSION. CORRECTIVE ACTION: REPLACED STRINGER 33R IAW A319 SRM 51-72-11-911- 001. (1141554).
- [SDR DALA2025081406089](https://openairdocs.org/sdr/DALA2025081406089.md): Skin · corroded · Aug 13, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3146 FOUND THE RH WING TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LOWER SURFACE WITH CORROSION. CORRECTIVE ACTION: COMPLIED WITH ER/A 627459-14. (1142290).
- [SDR DALA2025081406088](https://openairdocs.org/sdr/DALA2025081406088.md): Skin · corroded · Aug 13, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3146 RH WING TOP SKIN PANEL 2 WAS FOUND WITH CORROSION AT LOWER SURFACE TRAILING EDGE OVERHANG AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 627459-14. (1142287).
- [SDR DALA2025081406087](https://openairdocs.org/sdr/DALA2025081406087.md): Skin · corroded · Aug 13, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3146 CORROSION FOUND AT THE RH WING TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LOWER SURFACE. CORRECTIVE ACTION: COMPLIED WITH ER/A 627459-14. (1142277).
- [SDR DALA2025081406086](https://openairdocs.org/sdr/DALA2025081406086.md): Skin · corroded · Aug 13, 2025 · N346NB · Airbus A319114 · Wing Spar
  > SHIP 3146 TRAILING EDGE OVERHANG AREA AT LOWER SURFACE, RH WING TOP SKIN PANEL 2 WAS FOUND WITH CORROSION. CORRECTIVE ACTION: COMPLIED WITH ER/A 627459-14. (1142270).
- [SDR DALA2025081406085](https://openairdocs.org/sdr/DALA2025081406085.md): Skin · corroded · Aug 13, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3146 FOUND CORROSION AT THE RH WING TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LOWER SURFACE. CORRECTIVE ACTION: COMPLIED WITH ER/A 627459-14. (1142264).
- [SDR DALA2025081406084](https://openairdocs.org/sdr/DALA2025081406084.md): Skin · corroded · Aug 13, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3146 RH WING TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LOWER SURFACE CORRODED. CORRECTIVE ACTION COMPLIED WITH ER/A 627459-14. (1142256).
- [SDR DALA2025081406083](https://openairdocs.org/sdr/DALA2025081406083.md): Skin · corroded · Aug 13, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3146 RH WING TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LOWER SURFACE FOUND WITH CORROSION. CORRECTIVE ACTION: COMPLIED WITH ER/A 627459-14. (1142252).
- [SDR DALA2025081406071](https://openairdocs.org/sdr/DALA2025081406071.md): Skin · corroded · Aug 12, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3146 CORROSION FOUND ON LHWING TOP SKIN PANEL 2, TEOH, UPPER AN LOWER SURFACES. CORRECIVE ACTION: COMPLIED WITH ER/A 627460-14. (1140343).
- [SDR DALA2025081306069](https://openairdocs.org/sdr/DALA2025081306069.md): Doubler · cracked · Aug 12, 2025 · N346NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SERVICE PANEL CUTOUT, INTERNAL DOUBLER WITH CRACK INDICATION IN 1 (E.A.) OPEN HOLE DUE TO CORROSION AT FR65, STGR 39RH. REPLACED INTERNAL DOUBLER IAW A319 SRM 53-41-11-53A.
- [SDR DALA2025081306068](https://openairdocs.org/sdr/DALA2025081306068.md): Doubler · corroded · Aug 12, 2025 · N346NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > LOWER AFT FUSELAGE AT FR 65 BETWEEN STGR 38R AND STGR 40R, TOILET SERVICE PANEL INTERNAL DOUBLER WITH CORROSION. REPAIR PERFORMED WITH ORNRC 100-63.
- [SDR DALA2025081306062](https://openairdocs.org/sdr/DALA2025081306062.md): Skin · corroded · Aug 12, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > CORROSION FOUND ON LHWING TOP SKIN PANEL 2 TEOH, UPPER AN LOWER SURFACES. REPAIRED PER ER/A 31-627460.
- [SDR DALA2025081306061](https://openairdocs.org/sdr/DALA2025081306061.md): Skin · corroded · Aug 12, 2025 · N346NB · Airbus A319114 · Wing, Plate/Skin
  > CORROSION FOUND ON LH WING TOP SKIN PANEL 2 TEOH, UPPER AN LOWER SURFACES. REPAIRED PER ER/A 31-627460.

Next page: https://openairdocs.org/aircraft/N346NB/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 = 'N346NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N346NB/reports

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