# Service difficulty reports: N351NB

A list on [N351NB](https://openairdocs.org/aircraft/N351NB.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 · 133 reports

- [SDR DALA2026072904389](https://openairdocs.org/sdr/DALA2026072904389.md): Apu · odor · Jul 29, 2026 · N351NB · Airbus A319114 · Airborne Auxiliary Power Unit (APU) System
  > CREW MENTIONED DIRTY SOCK SMELL THROUGHOUT ALL PHASES OF FLIGHT. TURN ON APU BLEED AND SMELLED FUMES AROUND MID CABIN. PERFORMED P TRAK INITIAL RUNS REF AMDS 0550-2001 RESULTS SENT TO MCC (A. HERMS 948587) C/W MSI LOG 1723981 STEP'S A-G RECORD'S SENT TO MCC S
- [SDR DALA2026071704208](https://openairdocs.org/sdr/DALA2026071704208.md): Selector Valve · faulted · Jul 16, 2026 · N351NB · Airbus A319114 · Landing Gear Brake System
  > DECLARED EMERGENCY DUE TO AN AUTO BRAKE FAULT WITH A NORMAL BRAKE SELECTOR VALVE (23GG) FAILURE MESSAGE. REPLACED BRAKE SELECTOR VALVE 23GG. (LP: 9080442, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026071404131](https://openairdocs.org/sdr/DALA2026071404131.md): Selector Valve · faulted · Jul 14, 2026 · N351NB · Airbus A319114 · Landing Gear Brake System
  > DECLARED EMERGENCY DUE TO AN AUTO BRAKE FAULT WITH A NORMAL BRAKE SELECTOR VALVE (23GG) FAILURE MESSAGE. REPLACED BRAKE SELECTOR VALVE 23GG. (LP: 9080424, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026042902703](https://openairdocs.org/sdr/DALA2026042902703.md): Battery · inoperative · Apr 25, 2026 · N351NB · Airbus A319114 · Emergency Lighting
  > RT OVERWING EMERGENCY LIGHTS INOP. FWD TO MEL AND PLAC IAW MEL 33-50-04A NEEDS EPSU. R & R RT OVERWING EPSU IAW AMM 31-51. OPS CHECK NORMAL. (LP: 8892318). AIRCRAFT WAS GROUNDED
- [SDR DALA2026042902702](https://openairdocs.org/sdr/DALA2026042902702.md): Elec Connector · disconnected · Apr 25, 2026 · N351NB · Airbus A319114 · Light System Wiring
  > OPS TEST OF EPSU FAULTS EPSU EXT LOAD AFT LT. FOUND CONNECTOR ON SLIDE DISCONNECTED. RECONNECTED IAW AMM 25-62. ONLY SLIDE COVER WAS REMOVED. NO RII STEPS TO C/W. R &R BATTERY ON EPSU (13WL) IAW AMM 33-51. (LP: 8892317). AIRCRAFT WS GROUNDED
- [SDR DALA2026042902699](https://openairdocs.org/sdr/DALA2026042902699.md): Power Supply · no test · Apr 25, 2026 · N351NB · Airbus A319114 · Emergency Lighting
  > DURING R1 DOOR SLIDE CHANGE, FAIL OPS TEST OF EPSU. R & R EPSU (11WL) IAW AMM 33-51, OPS CHKD FAILED. OP CHECKS GOOD IAW AMM 33-51. (LP: 8892316). AIRCRAFT WAS GROUNDED
- [SDR DALA2026040202138](https://openairdocs.org/sdr/DALA2026040202138.md): Packing · damaged · Apr 1, 2026 · N351NB · Airbus A319114 · Hydraulic System, Main
  > DIVERTED TO MIA DUE TO LOSS OF BLUE HYDRAULIC SYSTEM WITH HYD B RSVR LO LVL ECAM WARNING. FOUND DAMAGED PACKING AT FITTING IN THE BLUE SYSTEM PRESSURE LINE GOING TO THE SLATS WTB. (LP: 8323720) AIRCRAFT WAS GROUNDED
- [SDR DALA2026020600879](https://openairdocs.org/sdr/DALA2026020600879.md): Unknown · odor · Feb 4, 2026 · N351NB · Airbus A319114 · Air Distribution System
  > UPON TOUCH DOWN STRONG ODOR OF BURNED CRAYON, WAXY ODOR LASTED ABOUT 60 SECONDS AND DISAPPEARED. FA'S SMELLED IT AT BACK OF CABIN ODOR LASTED A FEW MINUTES. ENGINE BLEEDS OPEN PACKS ON APU BLEED OFF. PERFORMED AMM 05-50-00-810-831-A. NO ODORS PRESENT. OK FOR
- [SDR DALA2025102707835](https://openairdocs.org/sdr/DALA2025102707835.md): Microphone · inoperative · Oct 24, 2025 · N351NB · Airbus A319114 · Communications System
  > OBSERVER'S O2 MASK MICROPHONE INOPERATIVE. RESEATED MICROPHONE CONNECTOR ON OBSERVER O2 MASK OPS NORMAL. (7710498).
- [SDR DALA2025101307491](https://openairdocs.org/sdr/DALA2025101307491.md): Battery Pack · inoperative · Oct 10, 2025 · N351NB · Airbus A319114 · Emergency Lighting
  > PASSENGER CABIN EPSU 12WL FAILED AND BATTERY 11WL INOPERATIVE. REPLACED PAX CABIN EPSU 12WL IAW 319 AMM TASK 33-51-38-000-001-A AND 33-51-38-400-001-A. (1245409).
- [SDR DALA2025101007407](https://openairdocs.org/sdr/DALA2025101007407.md): Doubler · cracked · Oct 9, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > UPPER FUSELAGE L1 DOOR CUTOUT FR16 DOUBLE JOGGLE AREA IN THE OUTER FLANGE OF THE FRAME WITH CRACK AT DOOR STOP 7 LHS FASTENER HOLE LOCATIONS #7, #A & #C WITH CRACK. COMPLIED WITH ER/A 628831-14AD. (1243004).
- [SDR DALA2025101007406](https://openairdocs.org/sdr/DALA2025101007406.md): Doubler · cracked · Oct 9, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > UPPER FUSELAGE R1 DOOR CUTOUT FR20 DOUBLE JOGGLE AREA IN THE OUTER FLANGE OF THE FRAME WITH CRACK AT DOOR STOP 1 RHS FASTENER HOLE LOCATION #14 WITH CRACK. ER/A #628975-14AD. (1243972).
- [SDR DALA2025100907366](https://openairdocs.org/sdr/DALA2025100907366.md): Bushing · excess play · Oct 8, 2025 · N351NB · Airbus A319114 · Spoilers
  > RIGHT WING SPOILER 2 WITH EXCESSIVE PLAY. REPLACED SLEEVES, BEARINGS AND BUSHINGS AT RH WING SPOILER #2 IAW A319 CMM TASK 57-72-21-010-803-A01. (1241365).
- [SDR DALA2025100807335](https://openairdocs.org/sdr/DALA2025100807335.md): Door Frame · cracked · Oct 7, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > UPPER FUSELAGE L1 DOOR CUTOUT FR20 DOUBLE JOGGLE AREA IN THE OUTER FLANGE OF THE FRAME WITH CRACK AT DOOR STOP 1 LHS FASTENER HOLE LOCATION #9 WITH CRACK. COMPLIED WITH ER/A 628974-14AD. (1239330).
- [SDR DALA2025100807334](https://openairdocs.org/sdr/DALA2025100807334.md): Door Frame · cracked · Oct 7, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > UPPER FUSELAGE R1 DOOR CUTOUT FR16 DOUBLE JOGGLE AREA IN THE OUTER FLANGE OF THE FRAME WITH CRACK AT DOOR STOP 7 RHS FASTENER HOLE LOCATIONS #A & #C WITH CRACK. COMPLIED WITH ER/A 628832-14AD. (1239308).
- [SDR DALA2025100807333](https://openairdocs.org/sdr/DALA2025100807333.md): Crossbeam · damaged · Oct 7, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > FWD FUSELAGE CROSSBEAM SPLICING FR16, RH SIDE WERE FOUND HOLES H14 & H15 WITH DIAMETER GREATER THAN THE MAXIMUM STARTING HOLE DIAMETER FOR COLD EXPANSION. COMPLIED WITH ER/A 629070-14AD. (1239284).
- [SDR DALA2025100807332](https://openairdocs.org/sdr/DALA2025100807332.md): Crossbeam · damaged · Oct 7, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > FWD FUSELAGE CROSSBEAM SPLICING FR16, LH SIDE WERE FOUND HOLES H14 & H15 WITH DIAMETER GREATER THAN THE MAXIMUM STARTING HOLE DIAMETER FOR COLD EXPANSION. COMPLIED WITH ER/A 629071-14AD. (1239273).
- [SDR DALA2025100807331](https://openairdocs.org/sdr/DALA2025100807331.md): Door Frame · cracked · Oct 7, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > UPPER FUSELAGE, PAX CABIN, R/H FORWARD ENTRY DOOR, FR 16 DOOR STOP NR 1 WITH CRACK INDICATION AT FRAME AND INTERCOSTAL LAYERS AT THE LOWER INBOARD HOLE. COMPLIED WITH ER/A 628823-14AD. (1239733).
- [SDR DALA2025100707281](https://openairdocs.org/sdr/DALA2025100707281.md): Door Frame · cracked · Oct 6, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3151 CRACK FOUND AT FASTENER HOLES NR 7, A AND C, UPPER FUSELAGE, FRAME 16LT, DOUBLE JOGGLE AREA. COMPLIED WITH ER/A 628831-14AD. (1238454).
- [SDR DALA2025100707280](https://openairdocs.org/sdr/DALA2025100707280.md): Door Frame · cracked · Oct 6, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > FOUND CRACK AT FASTENER HOLES NR 7, A, C ON UPPER FUSELAGE, FRME 16LT, DOUBLE JOGGLE AREA. COMPLIED WITH ER/A 628831-14AD. (1238446).
- [SDR DALA2025100607268](https://openairdocs.org/sdr/DALA2025100607268.md): Bearing · worn · Oct 4, 2025 · N351NB · Airbus A319114 · Rudder Control System
  > EMPENNAGE RUDDER SERVO CONTROLS WITH PLAY OUT OF LIMITS. ACCOMPLISHED DELTA WC #2724-2010 AND REPLACED BEARINGS AND HARDWARE OF THE RUDDER SERVO CONTROLS SEE DELTA WC #2724-2013 AND PERFORMED CHECK OF THE RUDDER T/E PLAY IAW A319 AMM TASK 27 -24-00-200-002-A
- [SDR DALA2025100607267](https://openairdocs.org/sdr/DALA2025100607267.md): Seat Track · corroded · Oct 4, 2025 · N351NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > PAX CABIN AT FR64, Y-1292 SEAT TRACK OUTBOARD FLANGE WITH CORROSION. PERFORMED PERMANENT REPAIR AT PAX CABIN FR64, Y-1292 SET TRACK IAW A319 SRM TASK 53-41-15-300-003. (1234374).
- [SDR DALA2025100607266](https://openairdocs.org/sdr/DALA2025100607266.md): Pump · leaking · Oct 4, 2025 · N351NB · Airbus A319114 · Hydraulic Pump (Electric/Engine), Main
  > LOWER FUSELAGE BLUE ELECTRICAL PUMP HYD FLUID AND GREASE COME OUT THROUGH HOSE DRAIN. REPLACED BLUE ELECTRIC PUMP (2075 GJ) IAW A319 AMM TASK 29-12-51 -000-001-A AND TASK 29-12-51-400-001-A. (1234342).
- [SDR DALA2025100607265](https://openairdocs.org/sdr/DALA2025100607265.md): Web · corroded · Oct 4, 2025 · N351NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > UPPER FUSELAGE, PAX CABIN ON FR 68 AND ON STGR-23L(LEVEL) SILL WEB WITH CORROSION. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR AT AFT L/H PASSENGER CREW DOOR SILL BEAM BETWEEN FR68-190.5 MM AND FR68+63.5 MM, Y1242.5 IAW A319 SRM TASK 53-41-14-300-001. (12342
- [SDR DALA2025100607272](https://openairdocs.org/sdr/DALA2025100607272.md): Support Fitting · corroded · Oct 3, 2025 · N351NB · Airbus A319114 · Trailing Edge Flaps
  > LEFT WING INBD FLAP OUTBOARD MAIN SUPPORT FITTING BEARING CORROSION. REPAIRED PER ER/A 628976-14. (1232420)
- [SDR DALA2025100607271](https://openairdocs.org/sdr/DALA2025100607271.md): Flap Track · corroded · Oct 3, 2025 · N351NB · Airbus A319114 · Trailing Edge Flaps
  > RIGHT WING OB FLAP TRACK #3, INNER AND OUTER RIB 5, AT ECCENTRIC BEARING AREA CORROSION. REPAIRED PER ER/A 14-629082. (1232738)
- [SDR DALA2025100607270](https://openairdocs.org/sdr/DALA2025100607270.md): Fitting · cracked · Oct 3, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > FRAME AND INTERCOSTAL FITTING WERE FOUND WITH CRACK AT LEVEL OF STOP FITITNG 1, HOLE #3. COMPLIED WITH ER/A 628823-14AD. (1232396).
- [SDR DALA2025100607274](https://openairdocs.org/sdr/DALA2025100607274.md): Crossbeam · damaged · Oct 2, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > CROSSBEAM JUNCTION AT FR 16LHS HOLE # 14 AND #15 OVERSIZED. REPAIRED PER ER/A 14-629071. (1230830)
- [SDR DALA2025100607273](https://openairdocs.org/sdr/DALA2025100607273.md): Crossbeam · corroded · Oct 2, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > FRAME 16 RT CROSSBEAM SPLICE OVERSIZED HOLES. REPAIRED PER ER/A 14-629070. (1230336)
- [SDR DALA2025100307226](https://openairdocs.org/sdr/DALA2025100307226.md): Frame · cracked · Oct 2, 2025 · N351NB · Airbus A319114 · Fuselage Main, Frame
  > CRACKS INDICATIONS WERE FOUND AT HOLE #A AND #C FRAME LAYER ONLY. COMPLIED WITH ER/A 628832-14AD. (1230320).
- [SDR DALA2025100307223](https://openairdocs.org/sdr/DALA2025100307223.md): Door Frame · cracked · Oct 2, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > UPPER FUSELAGE, PAX CABIN, LT FORWARD ENTRY DOOR, FR 16 DOOR STOP 7 WITH CRACK INDICATION AT INTERCOSTAL LAYER IN UPPER INBOARD AND LOWER INBOARD HOLES. REPLACED INTERCOSTAL FR16 DOOR STOP 7 IAW SRM 51-72-11-911-001. (1230614).
- [SDR DALA2025100307221](https://openairdocs.org/sdr/DALA2025100307221.md): Bearing · excess play · Oct 2, 2025 · N351NB · Airbus A319114 · Spoilers
  > LEFT WING SPOILER 5 WITH EXCESSIVE PLAY. REPLACED BEARINGS SLEEVES AND BUSHINGS AT LT WING SPOILER 5 IAW CMM TASK 57-75-21-000-806-A01. (1230737).
- [SDR DALA2025100307220](https://openairdocs.org/sdr/DALA2025100307220.md): Bearing · excess play · Oct 2, 2025 · N351NB · Airbus A319114 · Spoilers
  > LEFT WING SPOILER 1 WITH EXCESSIVE PLAY. REPLACED BEARINGS SLEEVES AND BUSHINGS AT LT WING SPOILER NR 1 IAW CMM TASK 57-71-21-000-805-A01. (1230724).
- [SDR DALA2025100307219](https://openairdocs.org/sdr/DALA2025100307219.md): Bearing · excess play · Oct 2, 2025 · N351NB · Airbus A319114 · Spoilers
  > RIGHT WING SPOILER 3 WITH EXCESSIVE PLAY. REPLACED BEARINGS SLEEVES AND BUSHINGS AT R/H WING SPOILER #3 IAW A319 CMM TASK 57-73-21-000-803-A01. (130715).
- [SDR DALA2025100307218](https://openairdocs.org/sdr/DALA2025100307218.md): Bearing · excess play · Oct 2, 2025 · N351NB · Airbus A319114 · Spoilers
  > RIGHT WING SPOILER 5 WITH EXCESSIVE PLAY. REPLACED BEARINGS SLEEVES AND BUSHINGS AT RT WING SPOILER 5 IAW CMM TASK 57-75-21-000-806-A01. (1230692).
- [SDR DALA2025100307215](https://openairdocs.org/sdr/DALA2025100307215.md): Shear Plate · corroded · Oct 2, 2025 · N351NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, UNDER FLOOR COMPARTMENT BETWEEN FR69-FR70 STR 23R-24R SHEAR PLATE CORRODED AROUND ANCHOR NUTS. REPLACED SHEAR PLATE IAW A319 SRM 53-41-17-01A. (1230652).
- [SDR DALA2025100307214](https://openairdocs.org/sdr/DALA2025100307214.md): Seat Track · corroded · Oct 2, 2025 · N351NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE, PAX CABIN SEAT TRACK Y765 FROM FR65 TO FR66 WITH CORROSION. COMPLIED WITH ER/A 628887-14. (1230635).
- [SDR DALA2025100307213](https://openairdocs.org/sdr/DALA2025100307213.md): Seat Track · corroded · Oct 2, 2025 · N351NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE, PAX CABIN SEAT TRACK -Y1292 FROM FR65 TO FR66 WITH CORROSION. COMPLIED WITH ER/A 628887-14. (1230630).
- [SDR DALA2025100307212](https://openairdocs.org/sdr/DALA2025100307212.md): Seat Track · corroded · Oct 2, 2025 · N351NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE, PAX CABIN SEAT TRACK Y1292 FROM FR65 TO FR66 WITH CORROSION. COMPLIED WITH ER/A # 628887-14. (1230619).
- [SDR DALA2025100307229](https://openairdocs.org/sdr/DALA2025100307229.md): Bearing · excess play · Oct 2, 2025 · N351NB · Airbus A319114 · Spoilers
  > LEFT WING SPOILER 2 WITH EXCESSIVE PLAY. REPLACED BEARINGS SLEEVES AND BUSHINGS AT LT WING SPOILER NR 2 IAW CMM TASK 57-72-21-010-803-A01. (1230752).
- [SDR DALA2025100307228](https://openairdocs.org/sdr/DALA2025100307228.md): Bearing · excess play · Oct 2, 2025 · N351NB · Airbus A319114 · Drag Control Actuator
  > LEFT WING SPOILER 3 WITH EXCESSIVE PLAY. REPLACED BEARINGS SLEEVES AND BUSHINGS AT LT WING SPOILER NR 3 IAW CMM TASK 57-73-21-000-803-A01. (1230768).
- [SDR DALA2025100107141](https://openairdocs.org/sdr/DALA2025100107141.md): Door Frame · cracked · Sep 30, 2025 · N351NB · Airbus A319114 · Fuselage Main, Structure
  > FR 16 DOOR STOP #7 WITH CRACK INDICATION AT INTERCOSTAL LAYER IN UPPER INBOARD HOLE. REPLACED INTERCOSTAL IAW A319 SRM 51-72-11- 911-001. (1226685).
- [SDR DALA2025100107138](https://openairdocs.org/sdr/DALA2025100107138.md): Bearing · excess play · Sep 30, 2025 · N351NB · Airbus A319114 · Spoilers
  > SHIP 3151, RT WING SPOILER 1 WITH EXCESSIVE PLAY. REPLACED SLEEVES BEARINGS AND BUSHINGS AT RH WING SPOILER #1 IAW A319 CMM 57-71-21-000-805-A01. (1226911).
- [SDR DALA2025093007085](https://openairdocs.org/sdr/DALA2025093007085.md): Seat Track · corroded · Sep 29, 2025 · N351NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE, PAX CABIN SEAT TRACK -Y765 FROM FR65 TO FR66 WITH CORROSION. REPLACED SEAT TRACK AT -Y765, FROM FR65 TO FR66 IAW ER/A #628887-14. (1224708).
- [SDR DALA2025093007084](https://openairdocs.org/sdr/DALA2025093007084.md): Floor Support · corroded · Sep 29, 2025 · N351NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > UPPER FUSELAGE, PAX CABIN FROM 66 TO FR 68 AT -Y1162 FOOR SUPPORT WITH CORROSION. REPLACED THE FLOOR SUPPORT AT -Y1162, FROM FR66 TO FR68 IAW A319 SRM 51-72-11-911-001. (1224701).
- [SDR DALA2025093007083](https://openairdocs.org/sdr/DALA2025093007083.md): Flange · corroded · Sep 26, 2025 · N351NB · Airbus A319114 · Vertical Stabilizer Miscellaneous Structure
  > CORROSION AT VERTICAL FLANGE OUTBOARD SURFACES AND AROUND NUT PLATE HOLES. COMPLIED WITH ER/A 629280-14. (1219817).
- [SDR DALA2025092206923](https://openairdocs.org/sdr/DALA2025092206923.md): Seat Track · corroded · Sep 19, 2025 · N351NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE, PAX CABIN SEAT TRACK Y765 AT FR 20 WITH CORROSION. REPLACED PAX CABIN SEAT TRACK P/N: D5311281300251 BETWEEN FR16 AND FR20 AT Y765 IAW A319 SRM 51-72-11-911. (1207463).
- [SDR DALA2025091906889](https://openairdocs.org/sdr/DALA2025091906889.md): Bearing · excess play · Sep 18, 2025 · N351NB · Airbus A319114 · Trailing Edge Flap Control System
  > LEFT WING FLAP INTERCONNECTING STRUT, FWD BEARING WITH PLAY. REPLACED LT WING FLAP INTERCONNECTING STRUT RAD END IAW AMM TASK 27-51-44-960-001-A. (1205337).
- [SDR DALA2025091906888](https://openairdocs.org/sdr/DALA2025091906888.md): Bearing · excess play · Sep 18, 2025 · N351NB · Airbus A319114 · Trailing Edge Flap Control System
  > RIGHT WING FLAP INTERCONNECTING STRUT, FWD BEARING WITH PLAY. REPLACED R/H WING FLAP INTERCONNECTING STRUT RAD END IAWW A319 AMM TASK 27-51-44-960-001-A. (1205325).
- [SDR DALA2025091906885](https://openairdocs.org/sdr/DALA2025091906885.md): Seat Track · corroded · Sep 18, 2025 · N351NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE, PAX CABIN SEAT TRACK Y1292 AT FR16 AND FR 20 WITH CORROSION. REPLACED PAX CABIN SEAT TRACK BETWEEN FR16 AND FR20 AT Y1292 IAW A319 SRM 51-72-11-911. (1205452).

Next page: https://openairdocs.org/aircraft/N351NB/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 = 'N351NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N351NB/reports

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