# Service difficulty reports: N357NB

A list on [N357NB](https://openairdocs.org/aircraft/N357NB.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 · 181 reports

- [SDR DALA2026080704566](https://openairdocs.org/sdr/DALA2026080704566.md): Cover · detached · Aug 2, 2026 · N357NB · Airbus A319114 · Emergency Lighting
  > EES, OVERHEAD EMERGENCY LIGHT COVER AROUND AISLE 20 FELL OFF. INSTALLED LIGHT COVER AS NECESSARY. (LP: 8319084, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026070103871](https://openairdocs.org/sdr/DALA2026070103871.md): Computer · faulty · Jun 30, 2026 · N357NB · Airbus A319114 · Flight Management Computing Hardware System
  > REJECTED TAKE OFF AT LOW SPEED BELOW 50 KNOTS DUE TO FLIGHT CONTROL CAUTION MSG. BITE TEST SFCC 1 FAULTS SLTS SFCC 1. R & R IAW TSM 27-51 AND AMM 27-51 BITE TEST NO FAULTS NOTED RESET SYS IAW AMM 27-51 NO FAULTS NOTED OK FOR SVC. (LP: 8651838, AIRCRAFT WAS
- [SDR DALA2026060503397](https://openairdocs.org/sdr/DALA2026060503397.md): Unknown · odor · Jun 1, 2026 · N357NB · Airbus A319114 · Air Distribution System
  > PASSANGERS IN 15 D AND 15E REPORTED OCCASIONAL WHIFS OF BURNING OIL SMELL THAT THEY REPORTED AT TOP OF DESCENT TO THE FLIGHT ATTENDANT. I SPOKE TO THE PASSANGERS AND THEY SAID THEY HAD NO ILLNESS SYMPTOMS AND CONFIRMED INTERMITTANT WHIFFS. INSPECTED PSU PANEL
- [SDR DALA2026051903075](https://openairdocs.org/sdr/DALA2026051903075.md): Oven · odor · May 14, 2026 · N357NB · Airbus A319114 · Buffet/Galleys
  > FA SMELLED ELEC ODOR FROM FWD GALLEY OVEN. TURNED OFF OVEN AND ODOR CLEARED. C/A: VERIFIED THAT ODOR COMES FROM CLEANNG SOLUTION AFTER TURNING ON THE OVEN. CLEANED AND DRIED OUT THE SMELLING CLEANING SOLUTIONS THRO-OUT THE OVEN. RUN OVEN AT HIGH TEMP FOR 30 MI
- [SDR DALA2026040402154](https://openairdocs.org/sdr/DALA2026040402154.md): Tab · damaged · Mar 29, 2026 · N357NB · Airbus A319114 · Spoilers
  > DURING MTC FOUND ANTI ROTATION TAB ON SPOILER PANEL DAMAGED. INSPECTED & BLENDED DAMAGE IAW SRM 57-70. FOUND MAXIMUM ALLOWABLE DAMAGE OF 0.028 EXCEEDED. REMOVED NR 4 SPOILER IAW AMM 27-64. INSPECTED SPOILER PANEL MOUNTING BOLTS & VERIFIED 8130. INSTALLED NR 4
- [SDR DALA2026022301263](https://openairdocs.org/sdr/DALA2026022301263.md): Warning Message · illuminated · Feb 20, 2026 · N357NB · Airbus A319114 · Cabin Pressure Control System
  > DECLARED EMERGENCY DUE TO A CABIN DIFFERENTIAL PRESSURE LOW MESSAGE FOLLOWED BY A CABIN PRESSURE SAFETY VALVE OPEN MESSAGE. NO TROUBLE FOUND. ECS-19 REPORT GENERATED SHOWS THAT AIRCRAFT AND CABIN ALTITUDE WERE EQUAL AT MESSAGE OCCURRENCE. PASSENGER MASKS WER
- [SDR DALA2025121609158](https://openairdocs.org/sdr/DALA2025121609158.md): Oxygen Mask · unwanted deploy · Dec 16, 2025 · N357NB · Airbus A319114 · Passenger Oxygen System
  > OXYGEN PANEL MASK DEPLOYED. RESECURED COMPARTMENT AT LAV 202 IAW AMM 35-21. (1353632).
- [SDR DALA2025121209082](https://openairdocs.org/sdr/DALA2025121209082.md): Radome · delaminated · Dec 12, 2025 · N357NB · Airbus A319114 · Aerodynamic Fairings
  > DURING WALK AROUND, FOUND DELAMINATION TO RADOME. R & R RADOME IAW A319 AMM 53-15. (7892405).
- [SDR DALA2025091806854](https://openairdocs.org/sdr/DALA2025091806854.md): A/C Pack · failed · Sep 18, 2025 · N357NB · Airbus A319114 · Cabin Cooling System
  > DECLARED EMERGENCY DURING APPROACH INTO ATL DUE TO A DUAL PACK FAILURE AT FL200. LT ENGINE EIU FAULT LED TO THE LT PACK FAULT. THE RT PACK WAS ALREADY ON MEL FOR A PRIOR OVERHEAT MESSAGE. CORRECTIVE ACTION: DURING TS, LT ENGINE PYLON CONNECTOR 406VC1 WAS FOUND
- [SDR DALA2025091506783](https://openairdocs.org/sdr/DALA2025091506783.md): Circuit Breaker · tripped · Sep 14, 2025 · N357NB · Airbus A319114 · Electrical Power System Wiring
  > DURING FLIGHT OPERATIONAL TEST GOT CIRCUIT BREAKER H07 TRIPPED. REPLACED CIRCUIT BREAKER H07 ON OVERHEAD PANEL 49VU IAW AIRBUS ESPM 20-52 -22. (1198052).
- [SDR DALA2025091506788](https://openairdocs.org/sdr/DALA2025091506788.md): Support Fitting · corroded · Sep 13, 2025 · N357NB · Airbus A319114 · Trailing Edge Flaps
  > CORROSION ON FITTING SUPPORT THE SPHERICAL BEARING TRACK 2 INBD FLAP LT WING. COMPLIED WITH ER/A 628405-14. (1197264).
- [SDR DALA2025091506782](https://openairdocs.org/sdr/DALA2025091506782.md): Elec Connector · broken · Sep 13, 2025 · N357NB · Airbus A319114 · Light System Wiring
  > BROKEN BACKSHELL ON ELECTRICAL CONNECTOR 205WLA AT PASSENGER CABIN. REPLACED BACKSHELL ON ELECTRICAL CONNECTOR 205WL-A AT PASSENGER CABIN IAW FAM AWM 33-51-02 AND IAW AIRBUS ESPM20-44-11. (1197407).
- [SDR DALA2025091506781](https://openairdocs.org/sdr/DALA2025091506781.md): Window Post · cracked · Sep 13, 2025 · N357NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON RH WINDSHIELD CENTER POST UPPER ATTACHMENT AREA UPPER CORNER RADIUS. COMPLIED WITH ER/A 628084-14AD. (1197373).
- [SDR DALA2025091506780](https://openairdocs.org/sdr/DALA2025091506780.md): Window Post · cracked · Sep 13, 2025 · N357NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON RH CONTINUITY FITTING AT WINDSHIELD CENTER POST LO WER ATTACHMENT AREA. COMPLIED WITH ER/A 628127-14AD. (1197365).
- [SDR DALA2025091506779](https://openairdocs.org/sdr/DALA2025091506779.md): Window Post · cracked · Sep 13, 2025 · N357NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON RT WINDSHIELD CENTER POST UPPER ATTACHMENT AREA UPPER CORNER RADIUS. COMPLIED WITH ER/A 628084-14AD. (1197362).
- [SDR DALA2025091506778](https://openairdocs.org/sdr/DALA2025091506778.md): Window Post · cracked · Sep 13, 2025 · N357NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON RT WINDSHIELD CENTER POST LOWER ATTACHMENT AREA L OWER CORNER RADIUS. COMPLIED WITH ER/A 628084-14AD. (1197182).
- [SDR DALA2025091506777](https://openairdocs.org/sdr/DALA2025091506777.md): Window Post · cracked · Sep 13, 2025 · N357NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON LT WINDSHIELD CENTER POST LOWER ATTACHMENT AREA LOWER CORNER RADIUS. COMPLIED WITH ER/A 628084-14AD. (1197175).
- [SDR DALA2025091506776](https://openairdocs.org/sdr/DALA2025091506776.md): Window Post · cracked · Sep 13, 2025 · N357NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON LH WINDSHIELD CENTER POST UPPER ATTACHMENT AREA UPPER CORNER RADIUS. COMPLIED WITH ER/A 628084-14AD. (1197169).
- [SDR DALA2025091506786](https://openairdocs.org/sdr/DALA2025091506786.md): Retainer · corroded · Sep 12, 2025 · N357NB · Airbus A319114 · Buffet/Galleys
  > CORROSION ON TROLLEY RETAINER BLOCK COMPARTMENTS 110 AND 111 OF GALLEY 1 AT FWD GALLEY AREA. COMPLIED WITH ER/A 628362-14. (1195648).
- [SDR DALA2025091206729](https://openairdocs.org/sdr/DALA2025091206729.md): Skin · worn · Sep 12, 2025 · N357NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > WEAR EXTERNAL SKIN UPPER CUT OUT ON PASSENGER CREW DOOR L/H LOC. FR 66 TO FR 68 IN PASSENGER CABIN. COMPLIED WITH ER/A 628846-14. (1194627).
- [SDR DALA2025091206728](https://openairdocs.org/sdr/DALA2025091206728.md): Floor Panel · delaminated · Sep 12, 2025 · N357NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 222EF TA FWD GALLEY AREA. COMPLIED WITH ER/A 628477-14. (1194617).
- [SDR DALA2025091206727](https://openairdocs.org/sdr/DALA2025091206727.md): Skin · worn · Sep 12, 2025 · N357NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > WEAR ON EXTERNAL SKIN UPPER CUT OUT ON PASSENGER CREW DOOR R/H LOC. FR 66 TO FR 68 IN PASSENGER CABIN. COMPLIED WITH ER/A 628845-14. (1194664).
- [SDR DALA2025091206726](https://openairdocs.org/sdr/DALA2025091206726.md): Support · corroded · Sep 12, 2025 · N357NB · Airbus A319114 · Wing Miscellaneous Structure
  > CORROSION ON FITTING SUPPORT THE SPHERICAL BEARING TRACK 3 0/B FLAP RT WING. COMPLIED WITH ER/A 628388-14. (1194658).
- [SDR DALA2025091206725](https://openairdocs.org/sdr/DALA2025091206725.md): Support Fitting · corroded · Sep 12, 2025 · N357NB · Airbus A319114 · Wing Miscellaneous Structure
  > CORROSION ON FITTING SUPPORT THE SPHERICAL BEARING TRACK 3 O/B FLAP LH WING. COMPLIED WITH ER/A 628387-14. (1194652).
- [SDR DALA2025091206733](https://openairdocs.org/sdr/DALA2025091206733.md): Window Frame · cracked · Sep 11, 2025 · N357NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATIONS FOUND IN LT AND RT FRONT WINDSHIELDS AND CONTINUITY FITTINGS AS WELL AS HOLES D1 LT AND RT SIDES. COMPLIED WITH ER/A 628127-14. (1193607).
- [SDR DALA2025091206732](https://openairdocs.org/sdr/DALA2025091206732.md): Skin · worn · Sep 11, 2025 · N357NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > WEARS FOUND ON EXTERNAL FUSELAGE SKIN AT THE CIRCULAR ZONE OF THE UPPER FWD AND AFT CORNERS OF AFT PASSENGER DOOR CUTOUT, 1 WEAR AT FR66 RHS AND 1 WEAR AT FR68 LHS. COMPLIED WITH ER/A 628845-14. (1193783).
- [SDR DALA2025091206731](https://openairdocs.org/sdr/DALA2025091206731.md): Bearing · corroded · Sep 11, 2025 · N357NB · Airbus A319114 · Trailing Edge Flaps
  > CORROSION WAS FOUND AFFECTING INB'D AND OUTB'D ALUMINUM PLATES IN INNER AND OUTER RIB 5 ECCENTRIC BEARING LH WING OUTG'D FLAP TRACK 3. COMPLIED WITH ER/A 628388-14. (1193993).
- [SDR DALA2025091206730](https://openairdocs.org/sdr/DALA2025091206730.md): Bearing · corroded · Sep 11, 2025 · N357NB · Airbus A319114 · Trailing Edge Flaps
  > CORROSION WAS FOUND AFFECTING INB'D AND OUTB'D ALUMINUM PLATES IN INNER AND OUTER RIB 5 ECCENTRIC BEARING LH WING OUTG'D FLAP. COMPLIED WITH ER/A 628387-14. (1193865).
- [SDR DALA2025091106713](https://openairdocs.org/sdr/DALA2025091106713.md): Support Fitting · corroded · Sep 11, 2025 · N357NB · Airbus A319114 · Trailing Edge Flaps
  > CORROSION ON FITTING SUPPORT THE SPHERICAL BEARING TRACK 4 O/B FLAP RH WING. REPAIRED PER ER/A 628418-14. (1192970)
- [SDR DALA2025091106712](https://openairdocs.org/sdr/DALA2025091106712.md): Fitting · cracked · Sep 10, 2025 · N357NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3157 CRACK INDICATIONS FOUND IN LH AND RH FRONT WINDSHIELDS AND CONTINUITY FTGS AS WELL AS HOLES D1 LH AND RH SIDES. CORRECTIVE ACTION: COMPLIED WITH ER/A 628084-14. (1192691).
- [SDR DALA2025091106711](https://openairdocs.org/sdr/DALA2025091106711.md): Fitting · cracked · Sep 10, 2025 · N357NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATIONS FOUND IN LH AND RH FRONT WINDSHIELDS AND CONTINUITY FTGS AS WELL AS HOLES D1 LH AND RH SIDES. COMPLIED WITH ER/A 628084-14. (1192669)
- [SDR DALA2025091106710](https://openairdocs.org/sdr/DALA2025091106710.md): Frame · cracked · Sep 10, 2025 · N357NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 16 RH SIDE OPEN FASTENER HOLE H3 IN CROSSBEAM SPLICING AREA. COMPLIED WITH ER/A 628163-14AD. (1192537).
- [SDR DALA2025091106709](https://openairdocs.org/sdr/DALA2025091106709.md): Frame · cracked · Sep 10, 2025 · N357NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 16 RH SIDE OPEN FASTENER HOLE H2 IN CROSSBEAM SPLICING AREA. COMPLIED WITH ER/A 628163-14AD. (1192533).
- [SDR DALA2025091106707](https://openairdocs.org/sdr/DALA2025091106707.md): Bearing · corroded · Sep 9, 2025 · N357NB · Airbus A319114 · Trailing Edge Flaps
  > CORROSION FOUND AFFECTING INB'D AND OUTB'D AL PLATES AT TRACK #2 IN THE INNER AND OUT RIB 9 ECCENTRIC BEARING, LH WING,INB'D FLAP. COMPLIED WITH ER/A 628405-14. (1190565).
- [SDR DALA2025090906647](https://openairdocs.org/sdr/DALA2025090906647.md): Access Panel · punctured · Sep 8, 2025 · N357NB · Airbus A319114 · Fuselage Structure (General)
  > PUNCTURE ON ACCESS PANEL 192KB AT LOWER FUSELAGE. COMPLIED WITH ER/A 524189-14. (1188635).
- [SDR DALA2025090806614](https://openairdocs.org/sdr/DALA2025090806614.md): Skin · worn · Sep 7, 2025 · N357NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > WEAR ON EXTERNAL SKIN LOC FR34 AT LEVEL STR44 AT LOWER FUSELAGE. COMPLIED WITH ER/A 628714-14. (1187074).
- [SDR DALA2025090806612](https://openairdocs.org/sdr/DALA2025090806612.md): Skin · worn · Sep 5, 2025 · N357NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > WEAR FOUND ON EXTERNAL FUSELAGE SKIN AT LWER SKIN PANEL BETWEEN FR34 TO FR35 AND STGR 43LH TO 43RH. COMPLIED WITH ER/A 628714-14. (1183404).
- [SDR DALA2025090806616](https://openairdocs.org/sdr/DALA2025090806616.md): Floor Panel · delaminated · Sep 5, 2025 · N357NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL (261DF) AT AFT GALLEY AREA. COMPLIED WITH ER/A 624842-14. (1183420).
- [SDR DALA2025090406540](https://openairdocs.org/sdr/DALA2025090406540.md): Shear Tie · corroded · Sep 3, 2025 · N357NB · Airbus A319114 · Fuselage Internal Mounting Structure
  > SHIP 3157 CORROSION SHEAR TIE AT LEVEL OF FR 65 AND BTW STR 44 TO STR 43L IN AF T CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AT LEVEL OF FR 65 AND BTW STR 44 TO STR 43L IN AFT CARGO COMPARTMENT, AS PER A319 SRM 51-42-11 AND A319 SRM 51- 72-11. (1
- [SDR DALA2025090306530](https://openairdocs.org/sdr/DALA2025090306530.md): Bracket · cracked · Sep 2, 2025 · N357NB · Airbus A319114 · Wing, Attach Fittings
  > CRACK BRACKET TELESCOPIC DUCT OB FIXED LEADING EDGE IB SIDE LH WING. REPLACED BRACKET AND FASTENERS ON TELESCOPIC DUCT OB FIXED LEADING EDGE IB SIDE LH WING AS PER A319 SRM 51-72-11 AND A319 SRM51-42-11. (1178540).
- [SDR DALA2025090106452](https://openairdocs.org/sdr/DALA2025090106452.md): Elec Connector · worn · Aug 30, 2025 · N357NB · Airbus A319114 · Flight Control System Wiring
  > WORN ELECTRICAL CONNECTOR 7540VC ON I/B FLAP RT. REPLACED ELECTRICAL CONNECTOR 7540VC ON I/B FLAP RT IAW AIRBUS ESPM 20-44-11. (1172999).
- [SDR DALA2025090106448](https://openairdocs.org/sdr/DALA2025090106448.md): Frame · cracked · Aug 29, 2025 · N357NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 16 LH SIDE OPEN FASTENER HOLE H2 IN CROSSBEAM SPLICING AREA. COMPLIED WITH ER/A 628162-14AD. (1171545).
- [SDR DALA2025082906398](https://openairdocs.org/sdr/DALA2025082906398.md): Floorbeam · corroded · Aug 28, 2025 · N357NB · Airbus A319114 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM -Y1292-1162.5 LOCATED BETWEEN FR66 TO FR68 AT AFT GALLEY AREA. REPLACED FLOOR BEAM -Y1292 -Y1162.5 AND FASTENER LOCATED. BTW FR66 TO FR68 AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1169846).
- [SDR DALA2025082906405](https://openairdocs.org/sdr/DALA2025082906405.md): Elec Connector · corroded · Aug 28, 2025 · N357NB · Airbus A319114 · Flight Control System Wiring
  > CORROSION ELECTRICAL CONNECTORS SPOILER 2,3,4 AND 5 ACTUATOR OF ON LH WING. REPLACED ELECTRICAL CONNECTORS SPOILER #2, 3, 4 AND 5 ACTUATOR OF LH WING AS PER AIRBUS ESPM 20-44-11. (1169860).
- [SDR DALA2025082506321](https://openairdocs.org/sdr/DALA2025082506321.md): Floor Support · corroded · Aug 25, 2025 · N357NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT -Y1162.5 AT FR68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y1162.5 AND FASTENER LOCATED. BTW FR68 TO FR69 AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1162040).
- [SDR DALA2025082506320](https://openairdocs.org/sdr/DALA2025082506320.md): Seat Track · scratched · Aug 24, 2025 · N357NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SCRATCH (3 E/A) LOC. ON SEAT TRACK -Y1292 ZONE 240 BTW FR35 TO FR 47. REPLACED SEAT TRACK -Y1292 AND FASTENERS LOCATED BTW FR36 TO FR41 AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (1161994).
- [SDR DALA2025082506319](https://openairdocs.org/sdr/DALA2025082506319.md): Door Frame · cracked · Aug 24, 2025 · N357NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE 4 AT DOOR STOP FITTING 1 POSITION. PERFORMED PERMANENT REPAIR LOC. ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE 4 AT DOOR STOP FITTING 1 POSITION AS PER A319 SRM 53-41-12-300-11. (1161986).
- [SDR DALA2025082506318](https://openairdocs.org/sdr/DALA2025082506318.md): Floor Support · corroded · Aug 24, 2025 · N357NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT +Y1292-1162.5 LOCATED BETWEEN FR66 TO FR68 AT AF T GALLEY AREA. REPLACED FLOOR SUPPORT Y1292-1162 LOCATED BETWEEN FR66 TO FR68 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (1161967).
- [SDR DALA2025082506317](https://openairdocs.org/sdr/DALA2025082506317.md): Floor Support · corroded · Aug 24, 2025 · N357NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT -Y765 LOCATED BETWEEN FR67 TO FR68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y765 LOCATED BETWEEN FR66 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1161961).
- [SDR DALA2025091806846](https://openairdocs.org/sdr/DALA2025091806846.md): Counter · dented · Aug 21, 2025 · N357NB · Airbus A319114 · Buffet/Galleys
  > DENTS WORK DECK GALLEY 1 AT FWD GALLEY AREA. R & R FWD GALLEY WORK DECK REF A319 CMM 25-31-561. (1156491).

Next page: https://openairdocs.org/aircraft/N357NB/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 = 'N357NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N357NB/reports

---
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