# Service difficulty reports: N353NB

A list on [N353NB](https://openairdocs.org/aircraft/N353NB.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 · 157 reports

- [SDR DALA2026101005578](https://openairdocs.org/sdr/DALA2026101005578.md): Engine · bird ingestion · Oct 8, 2026 · N353NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > ON T/O ROLL POSSIBLE BIRD INGESTION ON RT ENGINE. HIGH VIBRATION MESSAGE ON ROTATION & CLIMB. N1 AS HIGH AS 9.0 IN CRUISE N1 VIB AROUND 5.2. PERFORM BIRD STRIKE INSPECTION IAW AMM 72-00-00-200-001-001-A. FOUND NR 2 ENGINE WITH FAN BLADE DAMAGE. INSTALLED PE
- [SDR DALA2026091705194](https://openairdocs.org/sdr/DALA2026091705194.md): Structure · damaged · Sep 15, 2026 · N353NB · Airbus A319114 · Passenger/Crew Doors
  > DURING GVI OF FR68 LH AFT PASSENGER DOOR INNER CAP AND FLANGE, A REPAIR PART WAS IDENTIFIED. PER ER/A 605954-14AD REV A, SRM 53- 41-12-300-011 WAS ACCOMPLISHED WITHOUT DEVIATION. DUE TO LOCATION OF GUSSET ON TOP OF REPAIR PART FLANGE, UNABLE TO PERFO COMPLETED
- [SDR DALA2026061503564](https://openairdocs.org/sdr/DALA2026061503564.md): Computer · faulted · Jun 13, 2026 · N353NB · Airbus A319114 · Flight Control System
  > BOTH ENGINES RUNNING, REJECTED TAKEOFF DUE TO ELAC 1 PITCH FAULT MESSAGE AT 10 KNOTS. DUE TO HISTORY - APPLING ELAC 1 TO MEL & PLAC PER A319/320/321 MEL 27-93-01. M PROC C/W, MCC NOTIFIED. (LP: 8778668, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026050102766](https://openairdocs.org/sdr/DALA2026050102766.md): Computer · faulted · Apr 30, 2026 · N353NB · Airbus A319114 · Flight Control System
  > ATO - AT APPROXIMATELY 10KTS DUE TO F/CTL ELAC 1 PITCH FAULT. ELAC 1 PLACED ON MEL AND CONTINUED. LATER REPLACED ELAC 1. (LP 8038066 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026030401478](https://openairdocs.org/sdr/DALA2026030401478.md): Fan · faulted · Feb 16, 2026 · N353NB · Airbus A319114 · Air Distribution Fan
  > VENT AVIONICS SYS FAULT DISPLAYED. WARM ELECTRICAL ODOR IS PRESENT. R & R AEVC IAW AMM 21-26. STILL REQ OPS CHK. OPS TEST OF AEVC FAULTED 21-26-51 EXTRACT FAN 18HQ AND 21-26-55 ISOLATION VALVE 24HQ. R & R EXTRACT FAN 18HQ IAW AMM 21-26. AEVC TESTED GOOD,
- [SDR DALA2025111208292](https://openairdocs.org/sdr/DALA2025111208292.md): Skin · damaged · Nov 11, 2025 · N353NB · Airbus A319114 · Wing, Plate/Skin
  > ELONGATED HOLE FUEL TANK CUT OUT LOWER SURFACE LOC. BTW RIB17/18 (1E/A) ON RT WING. PERFORMED PERMANENT REPAIR ON FUEL TANK CUT OUT LOWER SURFACE AS PER A319 SRM 57-21 -11-300-002. (1299055).
- [SDR DALA2025111208290](https://openairdocs.org/sdr/DALA2025111208290.md): Elec Connector · broken · Nov 11, 2025 · N353NB · Airbus A319114 · Flight Control System Wiring
  > BROKEN ELECTRICAL CONNECTOR (31CE10A) LOC. ON SPOILER ACTUATOR 5 RH WING. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTOR (31CE10A) LOC. ON SPOILER ACTUATOR #5 RH WING AS PER AIRBUS ESPM 20-44-11. (1299225).
- [SDR DALA2025111208284](https://openairdocs.org/sdr/DALA2025111208284.md): Frame · cracked · Nov 11, 2025 · N353NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK FOUND ON THE HORIZONTAL FLEANGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1299202).
- [SDR DALA2025111208283](https://openairdocs.org/sdr/DALA2025111208283.md): Skin · dented · Nov 11, 2025 · N353NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > DENTS ON EXISTING REPAIR EXTERNAL SKIN LOCATED BTW FR 62 TO FR 64 AND BTW STR 36R TO STR 41R AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 503435-14AD. (1299184).
- [SDR DALA2025111208282](https://openairdocs.org/sdr/DALA2025111208282.md): Window Post · cracked · Nov 11, 2025 · N353NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK FOUND AT RH WINDSHIELD CENTER POST LOWER ATTACHMENT AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 584325-14AD. (1299124).
- [SDR DALA2025111108234](https://openairdocs.org/sdr/DALA2025111108234.md): Skin · ground damage · Nov 11, 2025 · N353NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > CATERING TRUCK DAMAGED SKIN LOCATED BETWEEN FR 62-64 AND BETWEEN S 37-41R. CORRECTIVE ACTION: COMPLIED WITH ER/A 503435-14AD (1298120).
- [SDR DALA2025111108239](https://openairdocs.org/sdr/DALA2025111108239.md): Frame · cracked · Nov 10, 2025 · N353NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK FOUND ON THE HORIZONTAL FALNGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1297446).
- [SDR DALA2025111108238](https://openairdocs.org/sdr/DALA2025111108238.md): Frame · cracked · Nov 10, 2025 · N353NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK FOUND ON THE HORIZONTAL FALNGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1297432).
- [SDR DALA2025111108237](https://openairdocs.org/sdr/DALA2025111108237.md): Frame · cracked · Nov 10, 2025 · N353NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK FOUND ON THE HORIZONTAL FALNGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1297420).
- [SDR DALA2025111108236](https://openairdocs.org/sdr/DALA2025111108236.md): Frame · cracked · Nov 10, 2025 · N353NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK FOUND ON THE HORIZONTAL FALNGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1297300).
- [SDR DALA2025111108235](https://openairdocs.org/sdr/DALA2025111108235.md): Frame · cracked · Nov 10, 2025 · N353NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK FOUND ON THE HORIZONTAL FLANGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1297285).
- [SDR DALA2025111108233](https://openairdocs.org/sdr/DALA2025111108233.md): Frame · cracked · Nov 10, 2025 · N353NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK FOUND ON THE HORIZONTAL FALNGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. CORRECTIVE ACTION: COMPLIED WITH ER/A 605954-14AD. (1297278).
- [SDR DALA2025111108232](https://openairdocs.org/sdr/DALA2025111108232.md): Frame · cracked · Nov 10, 2025 · N353NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK FOUND ON THE HORIZONTAL FLANGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1297326).
- [SDR DALA2025111108229](https://openairdocs.org/sdr/DALA2025111108229.md): Plate · cracked · Nov 10, 2025 · N353NB · Airbus A319114 · Passenger/Crew Doors
  > CRACK FOUND AFFECTING THE UPPER PLATE OF LT PAX/CREW DOOR 831 CREW DOOR 831 IN PASSENGER CABIN. COMPLIED WITH ER/A 630181-14. (1297839).
- [SDR DALA2025111108227](https://openairdocs.org/sdr/DALA2025111108227.md): Window Frame · cracked · Nov 10, 2025 · N353NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK FOUND AT RH WINDSHIELD CENTER POST LOWER ATTACHMENT AREA. COMPLIED QITH ER/A 629316-14AD. (1297842).
- [SDR DALA2025111008208](https://openairdocs.org/sdr/DALA2025111008208.md): Access Panel · eroded · Nov 10, 2025 · N353NB · Airbus A319114 · Aerodynamic Fairings
  > EROSION ACCESS PANEL 191DB AT LOWER FUSELAGE. COMPLIED WITH ER/A 629770-14. (1296589).
- [SDR DALA2025111008207](https://openairdocs.org/sdr/DALA2025111008207.md): Door Frame · cracked · Nov 10, 2025 · N353NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON FRAME 20 LH DOUBLE JOGGLE AREA HOLE 6 DOOR STOP FITTING 7. CORRECTIVE ACTION: COMPLIED WITH ER/A 629422-14AD. (1296575).
- [SDR DALA2025111008210](https://openairdocs.org/sdr/DALA2025111008210.md): Window Post · cracked · Nov 9, 2025 · N353NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK FOUND AT RT WINDSHIELD CENTER POST LOWER ATTACHMENT AREA. COMPLIED WITH ER/A 584325-14AD. (1295928).
- [SDR DALA2025111008209](https://openairdocs.org/sdr/DALA2025111008209.md): Window Post · cracked · Nov 9, 2025 · N353NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK FOUND AT RT WINDSHIELD CENTER POST LOWER ATTACHMENT AREA. COMPLIED WITH ER/A 629316-14AD. (1295911).
- [SDR DALA2025111008206](https://openairdocs.org/sdr/DALA2025111008206.md): Elec Connector · corroded · Nov 9, 2025 · N353NB · Airbus A319114 · Flight Control System Wiring
  > CORROSION ON ELECTRICAL CONNECTOR 16CA LOCATED ARTIFICIAL FEEL AND RUD DER TRAVEL LIMITING AT VERTICAL STABILIZER. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTOR (16CA-A) AS PER AIRBUS ESPM 20-44- 11. (1295830).
- [SDR DALA2025111008205](https://openairdocs.org/sdr/DALA2025111008205.md): Post · corroded · Nov 9, 2025 · N353NB · Airbus A319114 · Fuselage Main, Structure
  > CORROSION ON LATERAL POST AFT RH SIDE AT LAV A. COMPLIED WITH ER/A 629473-14. (1295785)
- [SDR DALA2025111008204](https://openairdocs.org/sdr/DALA2025111008204.md): Elec Connector · corroded · Nov 9, 2025 · N353NB · Airbus A319114 · Flight Control System Wiring
  > CORROSION ELECTRICAL CONNECTOR ON IB ELEVATOR SERVO CONTROL ACTUATOR (1E/A) AND OB ELEVATOR SERVO CONTROL ACTUATOR (2E/A) ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTORS (34CE3-C) (34CE3-A) (34CE1-C) AS PER AIRBUS ESPM 20-44-11.
- [SDR DALA2025111008202](https://openairdocs.org/sdr/DALA2025111008202.md): Floorbeam · cracked · Nov 9, 2025 · N353NB · Airbus A319114 · Fuselage Main, Floor Beam
  > CRACK INDICATION FOUND IN FASTENER HOLE H3, LOCATED AT FR16RH CROSSBEA M SPLICING AREA. FWD FUSELAGE PASSENGER CABIN. COMPLIED WITH ER/A 629518-14AD. (1295791).
- [SDR DALA2025111008201](https://openairdocs.org/sdr/DALA2025111008201.md): Floorbeam · cracked · Nov 9, 2025 · N353NB · Airbus A319114 · Fuselage Main, Floor Beam
  > CRACK INDICATION FOUND IN FASTENER HOLE H2, LOCATED AT FR16RH CROSSBEAM SPLICING AREA. FWD FUSELAGE PASSENGER CABIN. COMPLIED WITH ERA 629518-14AD. (1295790).
- [SDR DALA2025111008200](https://openairdocs.org/sdr/DALA2025111008200.md): Crossbeam · cracked · Nov 9, 2025 · N353NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION FOUND IN FASTENER HOLE H1, LOCATED AT FR16RH CROSSBEAM SPLICING AREA. FWD FUSELAGE PASSENGER CABIN. COMPLIED WITH ER/A 629518-14AD. (1295786).
- [SDR DALA2025111008198](https://openairdocs.org/sdr/DALA2025111008198.md): Web · cracked · Nov 9, 2025 · N353NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CRACK WEB LOC. FR 52 LH AT BELLY FAIRING. CORRECTIVE ACTION: COMPLIED WITH ER/A 629731-14. (1295808).
- [SDR DALA2025111008197](https://openairdocs.org/sdr/DALA2025111008197.md): Skin · dented · Nov 9, 2025 · N353NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > DENT EXTERNAL SKIN LOCATED FR 3 AND 17 INCHES BELOW -Y675 LOWER FUSELAGE. COMPLIED WITH ER/A 629682-14. (1295801).
- [SDR DALA2025111008196](https://openairdocs.org/sdr/DALA2025111008196.md): Bushing · worn · Nov 9, 2025 · N353NB · Airbus A319114 · Fuselage, Door Hinge
  > WEAR ON FIXED FLANGED BUSHING OF FWD LUG ON RH KEEL BEAM MLG DOOR HING E FITTING FWD SIDE. COMPLIED WITH ER/A 629519-14AD. (1295862).
- [SDR DALA2025111008195](https://openairdocs.org/sdr/DALA2025111008195.md): Bushing · worn · Nov 9, 2025 · N353NB · Airbus A319114 · Fuselage, Door Hinge
  > WEAR ON FIXED FLANGED BUSHING OF FWD LUG ON LH KEEL BEAM MLG DOOR HING E FITTING FWD SIDE. COMPLIED WITH ER/A 629573-14AD. (1295792).
- [SDR DALA2025111008194](https://openairdocs.org/sdr/DALA2025111008194.md): Flap Track · corroded · Nov 9, 2025 · N353NB · Airbus A319114 · Trailing Edge Flaps
  > CORROSION ON OTBD FLAP BEARING HOUSING AT TRACK 3 LT WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 629676-14. (1295851).
- [SDR DALA2025111008211](https://openairdocs.org/sdr/DALA2025111008211.md): Door Frame · cracked · Nov 8, 2025 · N353NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION AT HOLE #6 AT THE DOUBLE JOGGLE AREA OF THE FR20LH AROUND THE PASSENGER SERVICE DOOR. COMPLIED WITH ER/A 629422-14AD. (1293811).
- [SDR DALA2025111008193](https://openairdocs.org/sdr/DALA2025111008193.md): Floor Panel · delaminated · Nov 8, 2025 · N353NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED TOP LAYER FLOOR PANEL 211GF IN COCKPIT. COMPLIED WITH ER/A 629679-14. (1294723).
- [SDR DALA2025111008192](https://openairdocs.org/sdr/DALA2025111008192.md): Floor Panel · delaminated · Nov 8, 2025 · N353NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED TOP LAYER FLOOR PANEL 212GF IN COCKPIT. COMPLIED WITH ER/A 629679-14. (1294717).
- [SDR DALA2025111008191](https://openairdocs.org/sdr/DALA2025111008191.md): Floor Panel · delaminated · Nov 8, 2025 · N353NB · Airbus A319114 · Fuselage Floor Panel
  > SHIP 3153 DELAMINATED TOP LAYER FLOOR PANEL 231CF IN PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WITH ER/A 629679-14. (1294714).
- [SDR DALA2025111008212](https://openairdocs.org/sdr/DALA2025111008212.md): Hinge Fitting · corroded · Nov 7, 2025 · N353NB · Airbus A319114 · Fuselage, Door Hinge
  > FUSELAGE MLG DOOR KEEL BEAM RH FWD HINGE FITTING WEAR AND CORROSION. CORRECTIVE ACTION: REPAIRED PER ERA 629519-14AD. (1292906)
- [SDR DALA2025110708126](https://openairdocs.org/sdr/DALA2025110708126.md): Keelbeam · corroded · Nov 6, 2025 · N353NB · Airbus A319114 · Fuselage Main, Keel
  > SHIP 3153 WEAR AND CORROSION FUSELAGE MLG DOOR KEEL BEAM LH FWD HINGE FITTING. CORRECTIVE ACTION: REPAIRED PER ERA 629573-14AD. (1291431)
- [SDR DALA2025110708121](https://openairdocs.org/sdr/DALA2025110708121.md): Power Supply · faulted · Nov 6, 2025 · N353NB · Airbus A319114 · Emergency Lighting
  > SHIP 3153 EMERGENCY POWER SUPPLY UNIT FAULT 11WL. CORRECTIVE ACTION: R/R EPSU 11WL ON UNSERVICEABLE CONDITION AS PER A320 FAM AMM 33-51-38-000-001-A. (1291827).
- [SDR DALA2025110708120](https://openairdocs.org/sdr/DALA2025110708120.md): Power Supply · faulted · Nov 6, 2025 · N353NB · Airbus A319114 · Emergency Lighting
  > SHIP 3153 EMERGENCY POWER SUPPLY UNIT FAULT 12WL. CORRECTIVE ACTION: R/R EPSU AS PER A320 FAM AMM 33-51-38-000-001-A. (1291831).
- [SDR DALA2025110508071](https://openairdocs.org/sdr/DALA2025110508071.md): Flap Track · corroded · Nov 4, 2025 · N353NB · Airbus A319114 · Trailing Edge Flaps
  > CORROSION ON LT WING OTBD FLAP TRACK NR 3, INNER AND OUTER RIB 5, AT ECCENTRIC BEARING. REPAIRED PER ERA 629676-14. (1287999)
- [SDR DALA2025110508070](https://openairdocs.org/sdr/DALA2025110508070.md): Skin · worn · Nov 4, 2025 · N353NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > WEAR ON EXTERNAL SKIN LOC. BTW FR73 TO FR74 AND STR17/18 LH ON TAIL. CORRECTIVE ACTION: COMPLIED WITH ER/A 630030-14. (1288502).
- [SDR DALA2025110308005](https://openairdocs.org/sdr/DALA2025110308005.md): Stringer · worn · Nov 2, 2025 · N353NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > WEAR ON STRINGER 39R LOCATED BTW FR 47 / 51 TO FR 52 IN AFT CARGO COMPARTMENT. REPLACED STRINGER AND FASTENERS LOC.STR39 R/H BTW FR 47 / 51 TO FR 54 IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM51-72-11. (1283932).
- [SDR DALA2025110308002](https://openairdocs.org/sdr/DALA2025110308002.md): Pin · broken · Oct 31, 2025 · N353NB · Airbus A319114 · Equipment/Furnishings Wiring
  > SHIP 3153 BROKEN PIN ON CONECTOR ON OFFWING SLIDE LH. CORRECTIVE ACTION: R/R OFFWING ESCAPE SLIDE LH SIDE IAW AMDS CARD 2562-4001. (1282257).
- [SDR DALA2025102707830](https://openairdocs.org/sdr/DALA2025102707830.md): Seat Track · corroded · Oct 24, 2025 · N353NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK +Y1292 LOCATED FROM FR12 TO FR24 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292 LOCATED FROM FR12 TO FR24 AT GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (1269662).
- [SDR DALA2025102407776](https://openairdocs.org/sdr/DALA2025102407776.md): Seat Track · corroded · Oct 23, 2025 · N353NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK -Y765 LOCATED FROM FR12 TO FR24 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y765 LOCATED FROM FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 A319 SRM 51-72-11. (1267628).
- [SDR DALA2025102307753](https://openairdocs.org/sdr/DALA2025102307753.md): Track · corroded · Oct 22, 2025 · N353NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3153 CORROSION ON FLAP BEARING TRACK 3 ON O/B FLAP L/H WING (1 E/A). CORRECTIVE ACTION: REPLACED FLAP BEARING TRACK #3 ON O/B FLAP L/H WING (1 E/A) AS PER A320 FAM AMM 57-52-21-000-001-A AND A320 FAM AMM 57-52-21- 400-001-A. (1266205).

Next page: https://openairdocs.org/aircraft/N353NB/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 = 'N353NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N353NB/reports

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