# Service difficulty reports: N352NB

A list on [N352NB](https://openairdocs.org/aircraft/N352NB.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 · 138 reports

- [SDR DALA2026040102119](https://openairdocs.org/sdr/DALA2026040102119.md): Skin · corroded · Mar 27, 2026 · N352NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > DURING M2 AND WHILE INSPECTING PER JIC 5320-6010-DE, CORROSION SPOTS FOUND ON FUSELAGE SKIN, INTERNAL SIDE BETWEEN STRGR 31L - STRGR 32L AND FR67 - FR69. AT REV A STAGE II DTE IS COMPLETE. STAGE III PENDING. C/A: *DTE* PER SECTION DTE I, THE REPAIR OF SECTION
- [SDR DALA2026032201926](https://openairdocs.org/sdr/DALA2026032201926.md): Unknown · odor · Mar 20, 2026 · N352NB · Airbus A319114 · Air Distribution System
  > SULPHUR, FOUL ODOR ON TAXI OUT. STRONG, ENTIRE CABIN. FELT IN THROAT, NO PERCEPTIBLE VISUAL CUES. LASTED 5-10 MINS. RAN FUMES QRH. SEEMED TO IMPROVE WITH AIR/COND FUMES SUSPECTED PROCEDURE. NO APU AND ON ENGINES PACK/BLEEDS FOR AT LEAST 10 MINS. CHEMICAL SMELL
- [SDR DALA2026021701070](https://openairdocs.org/sdr/DALA2026021701070.md): Inlet · contaminated · Feb 9, 2026 · N352NB · Airbus A319114 · APU Core Engine
  > DURING DESCENT AROUND 10,000 FT AN ODOR WAS NOTICE THAT SEEMED TO SMELL LIKE A MUSTY BURNING. IT WAS SHORT LIVED, BUT RETURNED ON THE GROUND. WORK CARRIED 0550-2002 WAS ACCOMPLISHED TO IDENTIFY ISSUE. HEAVY OIL SATURATION WAS FOUND IN APU INLET UP INSIDE ENTI
- [SDR DALA2025111808409](https://openairdocs.org/sdr/DALA2025111808409.md): Cids · faulted · Nov 17, 2025 · N352NB · Airbus A319114 · Emergency Lighting
  > AFT TO EXIT SIGNS/NO SMOKING SIGNS OFF AND ON BLINKING WHOLE FLIGHT INTERPHONE L1 TO L2 CUT OUT SAME WHITE UP AS PREVIOUS. PERFORMED FULL CIDS RESET PER A319 TSM 24-00. NO FAULTS AT THIS TIME. OK FOR SVC. (8014238).
- [SDR DALA2025100707282](https://openairdocs.org/sdr/DALA2025100707282.md): Outflow Valve · damaged · Oct 4, 2025 · N352NB · Airbus A319114 · Pressure Regulator/Outflow Valve
  > SHIP 3152 - ATB - DUE TO CAB PR SYS 2 FAULT ECAM WARNING FOLLOWED BY CAB PR SYS 1 2 FAULT ECAM WARNING. CORRECTIVE ACTION: FOUND BROKEN DRILL BIT BETWEEN OUTFLOW VALVE AND THE CUTOUT FRAME NOT ALLOWING THE OUTFLOW VALVE TO CLOSE PROPERLY. REMOVED FOD AND OUTFL
- [SDR DALA2025100307224](https://openairdocs.org/sdr/DALA2025100307224.md): Window Frame · cracked · Oct 2, 2025 · N352NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK FOUND ON WINDSHIELD FRAMES ON LH AND RH SIDES. COMPLIED WITH ER/A 628472-14. (1230870).
- [SDR DALA2025100307222](https://openairdocs.org/sdr/DALA2025100307222.md): Frame · cracked · Oct 2, 2025 · N352NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK INDICATION FOUND ON FRAME 16LH HOLE C. ON DOUBLE JOGGLE AREA. COMPLIED WITH ER/A 628459-14AD. (1230633).
- [SDR DALA2025100307217](https://openairdocs.org/sdr/DALA2025100307217.md): Window Frame · cracked · Oct 2, 2025 · N352NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA LOWER RADIO RT SIDE. COMPLIED WITH ER/A 628400-14AD. (1230996).
- [SDR DALA2025100307216](https://openairdocs.org/sdr/DALA2025100307216.md): Skin · corroded · Oct 2, 2025 · N352NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > CORROSION INTERNAL SKIN LOCATED BTW FR 67 TO FR 68 AND BTW STR 30L TO STR 31L IN AFT CARGO COMPARTMENT. COMPLIED WITH ER/A 628904-14. (1230844).
- [SDR DALA2025100307211](https://openairdocs.org/sdr/DALA2025100307211.md): Window Frame · cracked · Oct 2, 2025 · N352NB · Airbus A319114 · Fuselage Main, Structure
  > CRACKS FOUND ON LT WINDSHIELD, CENTER POST, LOWER ATTACHMENT AREA, UPPER RADIUS, FRONT WINDSHIELD FRAMING, RT WINDSHIELD, CENTER POST, LOWER ATTACHMENT AREA, LOWER RADIUS, FRONT WINDSHIELD FRAMING. COMPLIED WITH ER/A 628585-14AD. (1230430).
- [SDR DALA2025100207187](https://openairdocs.org/sdr/DALA2025100207187.md): Skin · corroded · Oct 1, 2025 · N352NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > CORROSION SPOTS FOUND ON FUSELAGE SKIN, INTERNAL SIDE BETWEEN STRGR 31L - STRGR 32L AND FR67 - FR69. COMPLIED WITH ER/A 628904-14. (1229384).
- [SDR DALA2025100207186](https://openairdocs.org/sdr/DALA2025100207186.md): Floor Panel · delaminated · Oct 1, 2025 · N352NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 231CF IN PASSENGER CABIN. COMPLIED WITH ER/A 628624-14. (1229123).
- [SDR DALA2025100207185](https://openairdocs.org/sdr/DALA2025100207185.md): Floor Panel · delaminated · Oct 1, 2025 · N352NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 231EF IN PASSENGER CABIN. COMPLIED WITH ER/A 628624-14. (1229113).
- [SDR DALA2025100207184](https://openairdocs.org/sdr/DALA2025100207184.md): Floor Panel · delaminated · Oct 1, 2025 · N352NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 231BF IN PASSENGER CABIN. COMPLIED WITH ER/A 628624-14. (1228110).
- [SDR DALA2025100207183](https://openairdocs.org/sdr/DALA2025100207183.md): Access Panel · deteriorated · Oct 1, 2025 · N352NB · Airbus A319114 · Aerodynamic Fairings
  > DETERIORATED ALUMINUM MESH ON ACCESS PANEL 191BB BELLY FAIRING. COMPLIED WITH ER/A 542077-14TR. (1229102).
- [SDR DALA2025100107143](https://openairdocs.org/sdr/DALA2025100107143.md): Door Frame · cracked · Sep 30, 2025 · N352NB · Airbus A319114 · Fuselage Main, Structure
  > DURING M2 AND WHILE ACCOMPLISHING EM 5311-1246-01A, A CRACK WAS FOUND IN HOLE #C OF FR16 LHS DBL JGL AREA. COMPLIED WITH ER/A 628459-14AD. (1226712).
- [SDR DALA2025100107140](https://openairdocs.org/sdr/DALA2025100107140.md): Frame · cracked · Sep 30, 2025 · N352NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK INDICATION FOUND ON FRAME 16RH HOLE C. ON DOUBLE JOGGLE AREA, CRACK DIRECTION AT 3 O CLOCK LOOKING FROM OUTSIDE THE AIRCRAFT. COMPLIED WHIT ER/A 628458-14AD. (1226864).
- [SDR DALA2025100107139](https://openairdocs.org/sdr/DALA2025100107139.md): Frame · cracked · Sep 30, 2025 · N352NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK INDICATION FOUND ON FRAME 16RH HOLE C. ON DOUBLE JOGGLE AREA. COMPLIED WHIT ER/A 628458-14AD. (1226841).
- [SDR DALA2025093007086](https://openairdocs.org/sdr/DALA2025093007086.md): Window Frame · cracked · Sep 29, 2025 · N352NB · Airbus A319114 · Fuselage Main, Structure
  > CRACKS FOUND IN LT AND RT FRONT WINDSHIELD FRAMES AT LWR CENTER NODE. COMPLIED WITH ER/A 628400-14. (1225292).
- [SDR DALA2025092907074](https://openairdocs.org/sdr/DALA2025092907074.md): Floor Panel · delaminated · Sep 28, 2025 · N352NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 231FF IN PASSENGER CABIN. COMPLIED WITH ER/A 628624-14. (1223263).
- [SDR DALA2025092907073](https://openairdocs.org/sdr/DALA2025092907073.md): Floor Panel · delaminated · Sep 28, 2025 · N352NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 232FF IN PASSENGER CABIN. COMPLIED WITH ER/A 628624-14. (1223255).
- [SDR DALA2025092907072](https://openairdocs.org/sdr/DALA2025092907072.md): Floor Panel · delaminated · Sep 28, 2025 · N352NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 221PF AT FWD GALLEY AREA. COMPLIED WITH ER/A 628624-14. (1223257).
- [SDR DALA2025092907071](https://openairdocs.org/sdr/DALA2025092907071.md): Floor Panel · delaminated · Sep 28, 2025 · N352NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 222EF AT FWD GALLEY AREA. COMPLIED WITH ER/A 628624-14. (1223246).
- [SDR DALA2025092907070](https://openairdocs.org/sdr/DALA2025092907070.md): Floor Panel · delaminated · Sep 28, 2025 · N352NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 222CF AT FWD GALLEY AREA. COMPLIED WITH ER/A 628624-14. (1223252).
- [SDR DALA2025092907069](https://openairdocs.org/sdr/DALA2025092907069.md): Floor Panel · delaminated · Sep 28, 2025 · N352NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 221EF AT FWD GALLEY AREA. COMPLIED WITH ER/A 628624-14. (1223219).
- [SDR DALA2025092907079](https://openairdocs.org/sdr/DALA2025092907079.md): Window Frame · cracked · Sep 26, 2025 · N352NB · Airbus A319114 · Fuselage Main, Structure
  > CRACKS FOUND IN LT AND RT FRONT WINDSHIELD FRAMES AT LWR CENTER NOD. COMPLIED WITH ER/A 628585-14AD. (1219746).
- [SDR DALA2025092607006](https://openairdocs.org/sdr/DALA2025092607006.md): Bonding Plate · corroded · Sep 25, 2025 · N352NB · Airbus A319114 · Wing Main, Frame Structure
  > CORRODED STATIC DISCHARGER PLATE-BONDING FLAP TRACK FAIRING 532CB ON LT WING. COMPLIED WITH ER/A 622998-14TR. (1217688).
- [SDR DALA2025092607005](https://openairdocs.org/sdr/DALA2025092607005.md): Bonding Plate · corroded · Sep 25, 2025 · N352NB · Airbus A319114 · Wing Main, Frame Structure
  > CORRODED BONDING PLATE FLAP TRACK FAIRING 631CB ON RT WING. COMPLIED WITH ER/A 622998-14TR. (1217597).
- [SDR DALA2025092607004](https://openairdocs.org/sdr/DALA2025092607004.md): Bonding Plate · corroded · Sep 25, 2025 · N352NB · Airbus A319114 · Wing Main, Frame Structure
  > CORRODED FLAP TRACK FAIRING 632CB BONDING PLATE ON RH WING. COMPLIED WITH ER/A 622998-14TR. (1217586).
- [SDR DALA2025092506987](https://openairdocs.org/sdr/DALA2025092506987.md): Door Frame · cracked · Sep 24, 2025 · N352NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK FOUND ON FASTENER HOLE AT THE DOUBLE JOGGLE AREA OF THE FR16RH AROUND THE PASSENGER SERVICE DOOR. COMPLIED WITH ER/A 628458-14AD. (1215573).
- [SDR DALA2025092506986](https://openairdocs.org/sdr/DALA2025092506986.md): Bonding Plate · corroded · Sep 24, 2025 · N352NB · Airbus A319114 · Trailing Edge Flaps
  > CORROSION BONDING PLATE FLAP TRACK FAIRING (533CB) ON LH WING. COMPLIED WITH ER/A 622998-14TR. (1216019).
- [SDR DALA2025092506985](https://openairdocs.org/sdr/DALA2025092506985.md): Bonding Plate · corroded · Sep 24, 2025 · N352NB · Airbus A319114 · Trailing Edge Flaps
  > CORROSION BONDING PLATE FLAP TRACK FAIRING 633CB ON RH WING. COMPLIED WITH ER/A 622998-14TR. (1216002).
- [SDR DALA2025092506983](https://openairdocs.org/sdr/DALA2025092506983.md): Crossbeam · cracked · Sep 23, 2025 · N352NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON CROSS BEAM IN PASSENGER CABIN, ON FR 16 L, HOLE H3. CORRECTIVE ACTION: COMPLIED WITH ER/A 628546-14AD. (1214415).
- [SDR DALA2025092506982](https://openairdocs.org/sdr/DALA2025092506982.md): Stringer · corroded · Sep 23, 2025 · N352NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 42R BTW FR 59 TO FR 60 AFT CARGO COMPARTMENT. REPLACED STRINGER 42R AND FASTENER LOC BTW FR59 TO FR64 AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1214470).
- [SDR DALA2025091906887](https://openairdocs.org/sdr/DALA2025091906887.md): Access Panel · cracked · Sep 18, 2025 · N352NB · Airbus A319114 · Aerodynamic Fairings
  > DELAMINATED ACCESS PANEL 191BB BELLY FAIRING AT LOWER FUSELAGE. COMPLIED WITH ER/A 542077-14TR. (1205793).
- [SDR DALA2025091906886](https://openairdocs.org/sdr/DALA2025091906886.md): Access Panel · cracked · Sep 18, 2025 · N352NB · Airbus A319114 · Vertical Stabilizer, Plate/Skin
  > CRACK ACCESS PANEL 322BL ON VERTICAL STABILIZER. COMPLIED WITH ER/A 628592-14. (1205816).
- [SDR DALA2025091906892](https://openairdocs.org/sdr/DALA2025091906892.md): Floor Panel · delaminated · Sep 18, 2025 · N352NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 261DF AT AFT GALLEY AREA. COMPLIED WITH ER/A 628697-14. (1205802).
- [SDR DALA2025091506789](https://openairdocs.org/sdr/DALA2025091506789.md): Skin · not reported · Sep 13, 2025 · N352NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BT W FR 5 TO FR 6 AT THE LAP SEAM AND 5 INCHES BELOW LH SIDE STRINGER L OWER FUSELAGE. COMPLIED WITH ER/A 574394-14. (1197223).
- [SDR DALA2025091106708](https://openairdocs.org/sdr/DALA2025091106708.md): Floor Support · corroded · Sep 10, 2025 · N352NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT +Y1162.5 LOCATED AT LEVEL FR68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT Y1162.5 AND FASTENERS LOCATED IN FR68 TO FR69 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72 -11. (1191865).
- [SDR DALA2025090806613](https://openairdocs.org/sdr/DALA2025090806613.md): Bearing · corroded · Sep 6, 2025 · N352NB · Airbus A319114 · Trailing Edge Flaps
  > CORROSION SPHERICAL BEARING OUTBOARD FLAP TRACK 3 LH WING. REPLACED SPHERICAL BEARINGS OUTBOARD FLAP TRACK 3 LH WING AS PER A320- FAM AMM 57-53-21-000-001-A AS PER A320-FAM AMM 57-53-21-400-001. (1185070).
- [SDR DALA2025090806609](https://openairdocs.org/sdr/DALA2025090806609.md): Seat Track · corroded · Sep 6, 2025 · N352NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK -Y765 LOCATED AT FR 20 AT FWD GALLEY AREA. REPLACED SEAT TRACK -Y765 LOCATED FR 12 TO FR 24 FWD GALLEY AREA AS PER A319 SRM 53-11-15-283-011, A319 SRM 51-42-11 AND A319 SRM 51-44 -11. (1185106).
- [SDR DALA2025090806608](https://openairdocs.org/sdr/DALA2025090806608.md): Seat Track · corroded · Sep 5, 2025 · N352NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK +Y1292 LOCATED AT FR 66 AT AFT GALLEY AREA. REPLACED NEW SEAT TRACK AND FASTENERS LOC ON Y1292 (FR64 TO FR66) AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1183374).
- [SDR DALA2025090806607](https://openairdocs.org/sdr/DALA2025090806607.md): Door Sill · corroded · Sep 5, 2025 · N352NB · Airbus A319114 · Fuselage Main, Structure
  > CORROSION LOWER SILL LOCATED ON HOLE AT FR 68 LH SIDE AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON LOWER SILL LOCATED AT FR 68 LH SIDE AT AFT GALLEY AREA AS PER A319 SRM 53-41-14-300-001. (1183368).
- [SDR DALA2025090506581](https://openairdocs.org/sdr/DALA2025090506581.md): Fastener · out of position · Sep 4, 2025 · N352NB · Airbus A319114 · Fuselage Main, Structure
  > FASTENER ON H18 HAS BEEN FOUND IN WRONG POSITION RH SIDE. REMOVED AND REINSTALLED FASTENER CORRECTLY HOLE #18 LOCATED CROSSBEAM FR20 RH SIDE AS PER AD 5311-01221-12. (1182249).
- [SDR DALA2025090506580](https://openairdocs.org/sdr/DALA2025090506580.md): Seat Track · corroded · Sep 4, 2025 · N352NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK -Y765 LOCATED AT FR 66 AT AFT GALLEY AREA. REPLACED SEAT TRACK -Y765 AND FASTENERS LOC BTW FR64 TO FR66 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72-11. (1182280).
- [SDR DALA2025090506579](https://openairdocs.org/sdr/DALA2025090506579.md): Bushing · excess play · Sep 4, 2025 · N352NB · Airbus A319114 · Passenger/Crew Doors
  > EXCESSIVE PLAY, PASSENGER CREW DOOR 841 UPPER AND LOWER BUSHING BETWEEN DOOR AND SUPPORT ARM AT FWD GALLEY AREA. REMOVED AND REPLACED BUSHINGS BETWEEN UPPER AND LOWER CONNECTION LINK AND SUPPORT ARM PASSENGER CREW DOOR 841 IAW FAM AMM 52-11-21-000-001-A,AS P
- [SDR DALA2025090506578](https://openairdocs.org/sdr/DALA2025090506578.md): Floor Support · corroded · Sep 4, 2025 · N352NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT Y160.5 AT LEVEL FR68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT Y160.5, HARD POINT (2EA) AND FASTENERS LOCATED BETWEEN FR 68 TO FR 70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AS PER A319 SRM 51-72-11. (1182265).
- [SDR DALA2025090506577](https://openairdocs.org/sdr/DALA2025090506577.md): Seat Track · corroded · Sep 4, 2025 · N352NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK -Y1292 LOCATED AT FR 66 AT AFT GALLEY AREA. REPLACED SEAT TRACK -Y1292 AND FASTENERS LOC BTW FR64 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1182258).
- [SDR DALA2025090506576](https://openairdocs.org/sdr/DALA2025090506576.md): Floor Support · corroded · Sep 4, 2025 · N352NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOORBEAM +Y765 LOCATED AT LEVEL FR68 AT AFT GALLEY AREA. REPLACED FLOORBEAM Y765 AND FASTENERS LOC BETWEEN FR67 TO FR70 AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1182208).
- [SDR DALA2025090506575](https://openairdocs.org/sdr/DALA2025090506575.md): Floorbeam · corroded · Sep 4, 2025 · N352NB · Airbus A319114 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM -Y254 LOCATED BTW FR 18 TO FR 20 AT FWD GALLEY A REA. REPLACED FLOOR BEAM -Y254 AND FASTENERS LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1182178).

Next page: https://openairdocs.org/aircraft/N352NB/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 = 'N352NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N352NB/reports

---
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