# Service difficulty reports: N355NB

A list on [N355NB](https://openairdocs.org/aircraft/N355NB.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 3 · 144 reports

- [SDR DALA2026100705552](https://openairdocs.org/sdr/DALA2026100705552.md): Landing Gear · faulted · Oct 5, 2026 · N355NB · Airbus A319114 · Landing Gear Retraction/Extension System
  > ATB - DUE TO LANDING GEAR NOT RETRACTING, L/G SHOCK ABSORBER FAULT, L/G GEAR NOT UPLOCKED, AND L/G DOORS NOT CLOSED ECAM WARNINGS. MAINTENANCE STILL IN PROGRESS. (LP: 9539601, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026072804379](https://openairdocs.org/sdr/DALA2026072804379.md): Power Supply · faulted · Jul 25, 2026 · N355NB · Airbus A319114 · Emergency Lighting
  > DURING WC 3351-2991 FOUND EMERGENCY RT EPSU FAULTED. R & R EMERGENCY RT EPSU IAW AMM 33-51, OPS TEST OK. (LP: 8756474, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026070904018](https://openairdocs.org/sdr/DALA2026070904018.md): Sleeve · damaged · Jul 5, 2026 · N355NB · Airbus A319114 · Main Landing Gear Strut/Axle/Truck
  > NR 3 AND 4 MLG AXLE SLEEVE DAMAGED. R & R NR 3 & 4 MLG AXLE ADAPTER SLEEVES PER AMM 32-42. OK FOR SVC. (LP: 8924695, AIRCRAFTT WAS GROUNDED)
- [SDR DALA2026070603916](https://openairdocs.org/sdr/DALA2026070603916.md): Engine · no discrepancy · Jul 5, 2026 · N355NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > ATB, #2 ENG OVER LIMIT ON TAKEOFF. REMOVED CRANKPAD AND S17 BOROSCOPE PLUG ON NR 2 ENG PER A319 AMM 72-00. C/W OVERTEMP BSI ON #2 ENG PER A319 AMM 72-00 -00-200-003-A. NO DEFECTS NOTED. REINSTALLED CRANKPAD AND S17 BOROSCOPE PLUG ON #2 ENG PER A319 AMM 72-00.
- [SDR DALA2026061503563](https://openairdocs.org/sdr/DALA2026061503563.md): Unknown · odor · Jun 12, 2026 · N355NB · Airbus A319114 · Air Distribution System
  > FA REPORTED STRONG ELECTRICAL BURNING ODOR NEAR AFT GALLEY JUST AFTER STARTING BOTH ENGINES. ODOR DISSIPATED 5-10 MIN LATER. NO VISIBLE SMOKE OBSERVED. RETURNED TO GATE. INSPECTED COFFE MAKERS IN AFT GALLEY. NO DEFECTS NOTED. CHECKED AFT LAVS AND NO DEFECTS NO
- [SDR DALA2026052903250](https://openairdocs.org/sdr/DALA2026052903250.md): Warning Message · illuminated · May 27, 2026 · N355NB · Airbus A319114 · Communications System
  > REJECTED TAKEOFF AT APPROX.30 KTS DUE TO A COMMUNICATION ECAM. (F/O'S PTT SWITCH.) MAINTENANCE IN PROGRESS. (LP: 1616037) AIRCRAFT WAS GROUNDED
- [SDR DALA2026041602405](https://openairdocs.org/sdr/DALA2026041602405.md): Computer · faulty · Apr 14, 2026 · N355NB · Airbus A319114 · Flight Control System
  > ATO - AT THROTTLE UP DUE TO AN ELAC 2 PITCH FAULT. ENG 1 G HYD MON C/B WAS FOUND POPPED. REPLACED ELAC 2.
- [SDR DALA2026040902256](https://openairdocs.org/sdr/DALA2026040902256.md): Computer · faulty · Apr 7, 2026 · N355NB · Airbus A319114 · Flight Control System
  > ATO - AT THROTTLE UP DUE TO AN ELAC 2 PITCH FAULT. REPLACED ELAC 2. (LP: 8410558) AIRCRAFT WAS GROUNDED
- [SDR DALA2025090106451](https://openairdocs.org/sdr/DALA2025090106451.md): Floor Panel · delaminated · Aug 29, 2025 · N355NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 221PF IN FWD GALLEY. COMPLIED WITH 628267-14. (1171071).
- [SDR DALA2025090106447](https://openairdocs.org/sdr/DALA2025090106447.md): Frame · cracked · Aug 29, 2025 · N355NB · Airbus A319114 · Fuselage Main, Frame
  > FOUND CRACK AT FR20 RH, FASTENER HOLE #5. COMPLIED WITH ERA 583468-14AD. (1170469).
- [SDR DALA2025090106433](https://openairdocs.org/sdr/DALA2025090106433.md): Floor Support · corroded · Aug 29, 2025 · N355NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT Y1292-1162.5 AT FR67 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT Y1292-1162.5 LOC. BTW FR66 TO FR68 AT AFT GALLEY AREA IAW SRM 51-72-11. (1171104).
- [SDR DALA2025082906401](https://openairdocs.org/sdr/DALA2025082906401.md): Window Frame · cracked · Aug 29, 2025 · N355NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION WAS FOUND AT LH & RH (MIDDLE CENTER POST AND LOWER CORNER RADIUS AREA) FRONT WINDSHIELD FRAMING AND AT LH CONTINUITY FITTING. REPLACED PER ERA 627625-14. (1170092)
- [SDR DALA2025082906403](https://openairdocs.org/sdr/DALA2025082906403.md): Frame · cracked · Aug 28, 2025 · N355NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK INDICATION WAS FOUND ON FR20 RH, FASTENER HOLE 5. REPAIRED PER ERA 583468-14AD. (1169902)
- [SDR DALA2025082906402](https://openairdocs.org/sdr/DALA2025082906402.md): Floorbeam · corroded · Aug 28, 2025 · N355NB · Airbus A319114 · Fuselage Main, Floor Beam
  > ELONGATED HOLES (4EA) AND CORROSION SPOTS (4EA) WERE FOUND COMMON TO THE UPPER FLANGE OF CROSSBEAM AT FR67 AND BETWEEN Y1162.5 & Y1292.0. REPAIRED PER 628095-14. (1169101)
- [SDR DALA2025082906399](https://openairdocs.org/sdr/DALA2025082906399.md): Frame · gouged · Aug 28, 2025 · N355NB · Airbus A319114 · Fuselage Main, Frame
  > GOUGED FRAME 70 UPPER AREA RH SIDE AT AFT GALLEY AREA. COMPLIED WITH ERA 627820-14. (1169412).
- [SDR DALA2025082906397](https://openairdocs.org/sdr/DALA2025082906397.md): Fitting · cracked · Aug 28, 2025 · N355NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON LH CONTINUITY FITTING AT WINDSHIELD CENTER POST LO WER ATTACHMENT AREA. COMPLIED WITH ER/A 627696-14AD. (1169839).
- [SDR DALA2025082906396](https://openairdocs.org/sdr/DALA2025082906396.md): Window Post · cracked · Aug 28, 2025 · N355NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON LH WINDSHIELD CENTER POST LOWER ATTACHMENT AREA LOWER CORNER RADIUS. COMPLIED WITH ERA 627694-14AD. (1169533).
- [SDR DALA2025082806379](https://openairdocs.org/sdr/DALA2025082806379.md): Window Frame · cracked · Aug 27, 2025 · N355NB · Airbus A319114 · Fuselage Main, Structure
  > FOUND CRACK INDICATIONS AT LH & RH FRONT WINDSHIELD FRAMING. COMPLIED WITH ER/A 627696-14AD. (1167191).
- [SDR DALA2025082806377](https://openairdocs.org/sdr/DALA2025082806377.md): Floor Panel · delaminated · Aug 27, 2025 · N355NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 232DF IN PASSENGER CABIN. COMPLIED WITH ER/A 628113-14. (1167820).
- [SDR DALA2025082806376](https://openairdocs.org/sdr/DALA2025082806376.md): Window Frame · cracked · Aug 27, 2025 · N355NB · Airbus A319114 · Fuselage Main, Structure
  > FOUND CRACK INDICATIONS AT LH & RH FRONT WINDSHIELD FRAMING. COMPLIED WITH ER/A 627694-14AD. (1167118).
- [SDR DALA2025082706349](https://openairdocs.org/sdr/DALA2025082706349.md): Frame · gouged · Aug 27, 2025 · N355NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3155 GOUGE FRAME 70 UPPER AREA LH SIDE AT AFT GALLEY AREA. CORRECTIVE ACTION: COMPLIED WITH ERA 627820-14. (1166395)
- [SDR DALA2025082706347](https://openairdocs.org/sdr/DALA2025082706347.md): Structure · corroded · Aug 26, 2025 · N355NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3155 CORROSION UNDER WORK DECK GALLEY 1 AT PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WITH ER/A 627958-14. (1166080).
- [SDR DALA2025082706346](https://openairdocs.org/sdr/DALA2025082706346.md): Insert · corroded · Aug 26, 2025 · N355NB · Airbus A319114 · Fuselage Floor Panel
  > SHIP 3155 CORROSION FLOOR PANEL INSERT 261DF AT AFT GALLEY AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 627819-14. (1166054).
- [SDR DALA2025082506316](https://openairdocs.org/sdr/DALA2025082506316.md): Elec Connector · corroded · Aug 21, 2025 · N355NB · Airbus A319114 · Flight Control System Wiring
  > CORROSION ON ELECTRICAL CONNECTORS 7541VC AND 7543VC OF INTERCONNECTING STRUT ON LH WING. REPLACED ELECTRICAL CONNECTORS 7541VC AND 7543VC OF INTERCONNECTING STRUT ON LH WING AS PER AIRBUS ESPM 20-44-11. (1156567).
- [SDR DALA2025082506315](https://openairdocs.org/sdr/DALA2025082506315.md): Fairing · corroded · Aug 21, 2025 · N355NB · Airbus A319114 · Trailing Edge Flaps
  > CORROSION BONDING PLATE FLAP TRACK FAIRING 4 (533CB) ON LH WING. COMPLIED WITH ER/A 622998-14TR. (1156742).
- [SDR DALA2025082506314](https://openairdocs.org/sdr/DALA2025082506314.md): Fairing · corroded · Aug 21, 2025 · N355NB · Airbus A319114 · Trailing Edge Flaps
  > CORROSION BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. COMPLIED WITH ER/A 622998-14TR. (1156727).
- [SDR DALA2025082506313](https://openairdocs.org/sdr/DALA2025082506313.md): Seat Track · corroded · Aug 21, 2025 · N355NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK +Y1292 AT FR66 AT AFT GALLEY AREA. REPLACED SEAT TRACK Y1292 LOC. BTW FR64 TO FR66 IN AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1156676).
- [SDR DALA2025082206276](https://openairdocs.org/sdr/DALA2025082206276.md): Bonding Plate · corroded · Aug 21, 2025 · N355NB · Airbus A319114 · Wing Main, Frame Structure
  > CORROSION BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. REPLACED BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING AS PER ER/A 622998-14TR. (1156733)
- [SDR DALA2025082206275](https://openairdocs.org/sdr/DALA2025082206275.md): Floor Support · corroded · Aug 21, 2025 · N355NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORRODED FLOOR SUPPORT +Y1162.5 AT FR 68. REPLACED THE FLOOR SUPPORT, FR 68 TO 69 IAW SRM 51-42-11. (1156707)
- [SDR DALA2025082206277](https://openairdocs.org/sdr/DALA2025082206277.md): Insert · corroded · Aug 21, 2025 · N355NB · Airbus A319114 · Fuselage Floor Panel
  > CORRODED FLOOR PANEL INSERT 261PF AT AFT GALLEY AREA. COMPLIED WITH ER/A 627930-14. (1156589)
- [SDR DALA2025081106003](https://openairdocs.org/sdr/DALA2025081106003.md): Tee Angle · cracked · Aug 10, 2025 · N355NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CRACK ON TEE ANGLE, FR42 RH SIDE HYD BAY AREA LOWER FUSELAGE. REPLACED TEE ANGLE IAW CARD 5353-01006-03.
- [SDR DALA2025081306056](https://openairdocs.org/sdr/DALA2025081306056.md): Shear Tie · cracked · Aug 9, 2025 · N355NB · Airbus A319114 · Fuselage Internal Mounting Structure
  > CRACKS FR43 RH FRAME FOOT COUPLING. CORRECTIVE ACTION: REPAIRED PER AA WORK CARD 5311-01239-02B AND A319 SRM 53-11.
- [SDR DALA2025081306055](https://openairdocs.org/sdr/DALA2025081306055.md): Shear Tie · cracked · Aug 9, 2025 · N355NB · Airbus A319114 · Fuselage Internal Mounting Structure
  > CRACKS FR43 LH, FRAME FOOT COUPLING. C/W AA WORK CARD 5311-01239-02A AND PER A319 SRM 53-11.
- [SDR DALA2025080605902](https://openairdocs.org/sdr/DALA2025080605902.md): Skin · dented · Aug 5, 2025 · N355NB · Airbus A319114 · Leading Edge Devices
  > DENT LEADING EDGE INBOARD AREA SLAT 5 ON RH WING. REPAIRED LEADING EDGE INBOARD AREA SLAT 5 ON RH WING AS PER A319 SRM 57-40-00-300-106.
- [SDR DALA2025080505858](https://openairdocs.org/sdr/DALA2025080505858.md): Web · corroded · Aug 4, 2025 · N355NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION WEB FRAME 20 STR23L FWD GALLEY AREA. REPLACED WEB AND FASTENERS LOC. BETWEEN FR20 TO FR24 AND STR23L FORWARD GALLEY AREA AS PER A319 SRM 51-72-11, A319 SRM 51-42-11.
- [SDR DALA2025080505857](https://openairdocs.org/sdr/DALA2025080505857.md): Vertical Beam · cracked · Aug 4, 2025 · N355NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK ON UPPER EDGE OF Y0 VERTICAL BEAM. REPLACED Y0 VERTICAL BEAM AND FASTENERS LOCATED FR1 AS PER SRM 51-42-11, SRM 51-72-11.
- [SDR DALA2025080605904](https://openairdocs.org/sdr/DALA2025080605904.md): Bushing · worn · Aug 2, 2025 · N355NB · Airbus A319114 · Elevator Structure
  > WEAR FIXED BUSHINGS (2 EA) ON HINGE FITTING 5 LT ELEVATOR. REPAIRED LUG BORES AND REPLACED BUSHINGS (2 EA) ON HINGE FITTING #5 AT LH ELEVATOR AS PER A319 SRM 55-26-41-300-004.
- [SDR DALA2025080405834](https://openairdocs.org/sdr/DALA2025080405834.md): Stringer · corroded · Aug 2, 2025 · N355NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > SHIP 3155 CORROSION STRINGER 44 AND BETWEEN FR60 TO FR61 AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER 44 LOC BETWEEN FR 59 TO FR 64 AFT CARGO COMPARTMENT AS PER A319 SRM 51-72-11, A319 SRM 51-42-21. (1121659).
- [SDR DALA2025080405833](https://openairdocs.org/sdr/DALA2025080405833.md): Seat Track · corroded · Aug 1, 2025 · N355NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3155 CORROSION SEAT TRACK +Y1292 AT FR20 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292 AT FR20 FWD GALLEY AREA AS PER A319 SRM: 51-42-11 AND SRM:51-72-11. (1119276).
- [SDR DALA2025080105786](https://openairdocs.org/sdr/DALA2025080105786.md): Shear Tie · gouged · Jul 31, 2025 · N355NB · Airbus A319114 · Fuselage Internal Mounting Structure
  > GOUGE SHEAR TIE LOCATED FR30 AND BTW STR41R TO STR42R IN FWD CARGO COMPARTMENT. REPLACED SHEAR TIE AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11.
- [SDR DALA2025080105790](https://openairdocs.org/sdr/DALA2025080105790.md): Bushing · worn · Jul 30, 2025 · N355NB · Airbus A319114 · Elevator Structure
  > WEAR FIXED BUSHINGS (2 EA) ON HINGE FITTING 1 LH ELEVATOR. REPAIRED AND REPLACED BUSHINGS (2EA) ON HINGE FITTING NR 1 AT LH ELEVATOR AS PER A319 SRM 55-26-41-300-004.
- [SDR DALA2025080105789](https://openairdocs.org/sdr/DALA2025080105789.md): Bushing · worn · Jul 30, 2025 · N355NB · Airbus A319114 · Elevator Structure
  > WEAR FIXED BUSHINGS (2 EA) ON HINGE FITTING 3 LH ELEVATOR. REPAIRED AND REPLACED BUSHINGS (2EA) ON HINGE FITTING NR 3 AT LH ELEVATOR AS PER A319 SRM 55-26-41-300-004.
- [SDR DALA2025080105784](https://openairdocs.org/sdr/DALA2025080105784.md): Bushing · worn · Jul 30, 2025 · N355NB · Airbus A319114 · Elevator Structure
  > WEAR FIXED BUSHINGS (2 EA) ON HINGE FITTING 2 LH ELEVATOR. REPAIRED AND REPLACED BUSHINGS (2EA) ON HINGE FITTING #2 AT LH ELEVATOR AS PER A319 SRM 55-26-41-300-004.
- [SDR DALA2025073105743](https://openairdocs.org/sdr/DALA2025073105743.md): Mechanism · deteriorated · Jul 30, 2025 · N355NB · Airbus A319114 · Emergency Equipment
  > DETERIORATED PASSENGER CREW DOOR 832 FLEXIBLE CONTROL OF EMERGENCY ESCAPE SLIDE MECHANISM AT AFT GALLEY AREA. REPLACED PASSENGER CREW DOOR 832 FLEXIBLE CONTROL OF EMERGENCY ESCAPE SLIDE MECHANISM AT AFT GALLEY AREA AS PER A320 FAM AMM 52-13-22-000-001-A AND A
- [SDR DALA2025073105742](https://openairdocs.org/sdr/DALA2025073105742.md): Seat Track · corroded · Jul 30, 2025 · N355NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK -Y765 AND FR68 IN PASSENGER CABIN. FEPLACED THE SEAT TRACK IAW SRM 51-42-11 AND SRM 51-72-11.
- [SDR DALA2025073105741](https://openairdocs.org/sdr/DALA2025073105741.md): Web · corroded · Jul 30, 2025 · N355NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION WEB, FRAME 16, STR23L FWD GALLEY AREA. REPLACED WEB IAW SRM 51-42-11.
- [SDR DALA2025073105740](https://openairdocs.org/sdr/DALA2025073105740.md): Seat Track · corroded · Jul 30, 2025 · N355NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK -Y1292 AT FR20 FWD GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND SRM 51-42-11.
- [SDR DALA2025073105739](https://openairdocs.org/sdr/DALA2025073105739.md): Seat Track · corroded · Jul 30, 2025 · N355NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK +Y765 AT FR66 AT AFT GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND SRM 51-42-11.
- [SDR DALA2025073105738](https://openairdocs.org/sdr/DALA2025073105738.md): Floorbeam · corroded · Jul 30, 2025 · N355NB · Airbus A319114 · Fuselage Main, Floor Beam
  > CORRODED FLOORBEAM -Y1292 -1162, FR 67 RT AT AFT GALLEY AREA. REPAIRED THE FLOORBEAM IAW SRM 51-72-11 AND A319 SRM 51-42-11.
- [SDR DALA2025073105737](https://openairdocs.org/sdr/DALA2025073105737.md): Seat Track · corroded · Jul 30, 2025 · N355NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK -Y1162.5 LOC. AT LEVEL FR 68 RH AT AFT GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND SRM 51-42-11.

Next page: https://openairdocs.org/aircraft/N355NB/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 = 'N355NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N355NB/reports

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