# Service difficulty reports: N319NB

A list on [N319NB](https://openairdocs.org/aircraft/N319NB.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 6 · 283 reports

- [SDR DALA2026100305476](https://openairdocs.org/sdr/DALA2026100305476.md): Transmission · faulted · Oct 2, 2026 · N319NB · Airbus A319114 · Trailing Edge Flap Control System
  > DIV - TO AUS DUE TO F/CTL FLAPS FAULT. WTB RESET AND INSPECTED FLAP TRANSMISSION, NO TROUBLE FOUND. (LP: 9499366, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026052603148](https://openairdocs.org/sdr/DALA2026052603148.md): Glide Slope · faulted · May 24, 2026 · N319NB · Airbus A319114 · Glide Slope System
  > DIV - TO SAV DUE TO GLIDE SLOPE NOT CAPTURING DURING THE APPROACH TO ATL IN IFR CONDITIONS. COULD NOT DUPLICATE. SWAPPED MMR NR 1 AND NR 2. AIRCRAFT RETURNED TO SERVICE. (LP: 8881250) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026041602406](https://openairdocs.org/sdr/DALA2026041602406.md): Bleed Air Sys · warning message · Apr 15, 2026 · N319NB · Airbus A319114 · Pneumatic Distribution System
  > DIV - TO RDU DUE TO A RT WING BLEED LEAK MESSAGE WITH THE LT ENG BLEED SYSTEM ALREADY ON MEL AND THE CABIN PRESSURE CLIMBING. MASKS DID NOT DEPLOY. REPLACED LT AND RT EBAS TLT. (LP: 7729686) AIRCRAFT WAS GROUNDED
- [SDR DALA2025092506984](https://openairdocs.org/sdr/DALA2025092506984.md): Skin · ground damage · Sep 23, 2025 · N319NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > A GROUND VEHICLE HOSE CONTACTED THE AIRCRAFT ON THE FUSELAGE BETWEEN FR2 AND FR4, ABOVE Y330 RT. CORRECTIVE ACTION: COMPLIED WITH ER/A 628044-14. (1213648).
- [SDR DALA2025092506981](https://openairdocs.org/sdr/DALA2025092506981.md): Skin · ground damage · Sep 23, 2025 · N319NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > A GROUND VEHICLE HOSE CONTACTED THE AIRCRAFT ON THE FUSELAGE BETWEEN FR2 AND FR4, ABOVE Y330 RH. COMPLIED WITH ER/A 628044-14. (1213814).
- [SDR DALA2025092306957](https://openairdocs.org/sdr/DALA2025092306957.md): Skin · scratched · Sep 22, 2025 · N319NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > FOUND SCRATCHES AAFFECTING THE FUSELAGE SKIN PANEL BETWEEN FR 57 AND STR 26L-27L. COMPLIED WITH ER/A 629166-14AD. (1212433).
- [SDR DALA2025092306956](https://openairdocs.org/sdr/DALA2025092306956.md): Skin · scratched · Sep 22, 2025 · N319NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SCRATCH ON EXTERNAL SKIN LOCATED BTW FR 57 TO FR 58 AND STR 26L TO ST R 27L AT LOWER FUSELAGE. COMPLIED WITH ER/A 629166-14AD. (1212626).
- [SDR DALA2025092306955](https://openairdocs.org/sdr/DALA2025092306955.md): Cover · damaged · Sep 22, 2025 · N319NB · Airbus A319114 · Escape Slide
  > SLIDE COVER NEEDS TO BE REPLACED. REMOVE AND RE-INSTALL SLIDE COVER AND INSTALL AND REMOVE SAFETY LOCK P IN ON RESERVOIR ASSY OF ESCAPE SLIDE OF PASSENGER CREW DOOR 831, 832, 841 AND 842. (1212191).
- [SDR DALA2025082706351](https://openairdocs.org/sdr/DALA2025082706351.md): Plate · cracked · Aug 20, 2025 · N319NB · Airbus A319114 · Leading Edge Devices
  > SHIP 3119 FOUND PLATE CRACKED. CORRECTIVE ACTION: INSTALLED NEW SLAT TRACK CLOSING PLATE ON RIGHT INBOARD SLAT PER A319 AMM 27-84. ALL CHECKS OK. (7415292)
- [SDR DALA2025072805670](https://openairdocs.org/sdr/DALA2025072805670.md): Skin · damaged · Jul 27, 2025 · N319NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3119 FWD FUSELAGE DAMAGE FR 1-4. CORRECTIVE ACTION: COMPLIED WITH ER/A 628044-14. (1108228).
- [SDR DALA2025080405839](https://openairdocs.org/sdr/DALA2025080405839.md): Skin · ground damage · Jul 26, 2025 · N319NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3119 GROUND VEHICLE HOSE CONTACTED THE AIRCRAFT ON THE FUSELAGE BETWEEN FR 2-4 AND ABOVE Y=330 RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 628044-14. (1107429).
- [SDR DALA2025080405836](https://openairdocs.org/sdr/DALA2025080405836.md): Skin · dented · Jul 26, 2025 · N319NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3119 FOUND DENT ON THE CROWN SKIN AFT OF FR 53 BETWEEN STR 3L-4L. CORRECTIVE ACTION: COMPLIED WITH ER/A 626580-14. (1107420).
- [SDR DALA2025072405556](https://openairdocs.org/sdr/DALA2025072405556.md): Radome · damaged · Jul 24, 2025 · N319NB · Airbus A319114 · Aerodynamic Fairings
  > SHIP 3119 DAMAGE TO NOSE RADOME RIGHT SIDE. CORRECTIVE ACTION: R/R RADOME PER A320 AMM 53-15-11. (1102409)
- [SDR DALA2025072205520](https://openairdocs.org/sdr/DALA2025072205520.md): Panel · delaminated · Jul 22, 2025 · N319NB · Airbus A319114 · Horizontal Stabilizer, Plate/Skin
  > SHIP 3119 LEFT HORIZONTAL STAB UPPER PANEL 334BT DELAMINATED/SEPERATED. CORRECTIVE ACTION: R/R'D PANEL 334BT ON LEFT HORIZONTAL STAB IAW A319 AMM 55-10. (7455080).
- [SDR DALA2025070705065](https://openairdocs.org/sdr/DALA2025070705065.md): Controller · faulted · Jul 6, 2025 · N319NB · Airbus A319114 · Heating System
  > SHIP 3119 - ATO - DUE TO AFT CARGO HEAT MESSAGE AT THROTTLE UP. DEFERRED AFT CARGO HEAT PER MEL AND CONTINUE. REPLACED AFT CARGO HEAT CONTROLLER 10HV.
- [SDR DALA2025063004873](https://openairdocs.org/sdr/DALA2025063004873.md): Fairing · damaged · Jun 19, 2025 · N319NB · Airbus A319114 · Leading Edge Devices
  > SHIP 3119 RIGHT WING SLAT TRACK FAIRING RACKED AND PEELED BACK. CORRECTIVE ACTION: INSTALLED NEW SLAT CLOSING PLATE PER A319 AMM 27-84. (7441368)
- [SDR DALA2025040402558](https://openairdocs.org/sdr/DALA2025040402558.md): Pin · broken · Mar 31, 2025 · N319NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3119 DISC: L1 DOOR BOARDER DOOR PIN LEAGH FOR PIN IS BROKEN. C/A: FWD TO NEF 52-13-03 NO "M" PROCEDURE. DOOR 1L DISARM PIN LANYARD ALREADY ON NEF DEFERRAL, SEE LP 088291. (LP: 7209952)
- [SDR DALA2024051605290](https://openairdocs.org/sdr/DALA2024051605290.md): Frame · cracked · May 15, 2024 · N319NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3119 CRACK 2.0" LONG FOUND RUNNING THROUGH FASTENER HOLES #2, #6, AND #7, LHS FR35 BH AT LEVEL OF STR 30. CORRECTIVE ACTION: REPAIRED PER ER/A 612601-14. (0344527)
- [SDR DALA2024051605289](https://openairdocs.org/sdr/DALA2024051605289.md): Frame · cracked · May 15, 2024 · N319NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3119 CRACK 2.0" LONG FOUND RUNNING THROUGH FASTENER HOLES #2, #6, AND #7, LHS FR35 BH AT LEVEL OF STR 30. CORRECTIVE ACTION: REPAIRED PER ER/A 612601-14. (0344522)
- [SDR DALA2024051605288](https://openairdocs.org/sdr/DALA2024051605288.md): Frame · cracked · May 15, 2024 · N319NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3119 CRACK 2.0" LONG FOUND RUNNING THROUGH FASTENER HOLES #2,#6, AND #7, LHS FR35 BH AT LEVEL OF STR 30. CORRECTIVE ACTION: REPAIRED PER ER/A 612601-14. (0344509)
- [SDR DALA2024051305129](https://openairdocs.org/sdr/DALA2024051305129.md): Unknown · unknown · May 12, 2024 · N319NB · Airbus A319114 · Standard Practices/Structures
  > SHIP 3119 ON TAKE OFF PLACE PLANE PULLED TO THE RIGHT ON LANDING PLANE PULLS TO THE RIGHT. CORRECTIVE ACTION: PERFORMED STEERING CHECK AT GATE NO DEFECTS NOTED. TAXI A/C WITH NO STEERING FAULTS NOTED. PER A319 AMM 32-51-00. A/C OF FOR SERVICE. (5876236)
- [SDR DALA2024051005104](https://openairdocs.org/sdr/DALA2024051005104.md): Insert · misaligned · May 10, 2024 · N319NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3119 GUST LOCK ON DOOR 1L NOT OPERATING CORRECTLY VERY DIFFICULT TO UNLOCK IN IAH AND UPON ARRIVAL AT GATE IN LAX IT WILL NOT LOCK. CORRECTIVE ACTION: PERFORMED A GVI OF 1L DOOR GUST LOCK FOUND TEFLON INSERT MISALINGED, REALINGED TEFLON INSERT IN REF TO A
- [SDR DALA2024051005103](https://openairdocs.org/sdr/DALA2024051005103.md): Housing · corroded · May 9, 2024 · N319NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3119 CORROSION FOUND IN TRACK 2 BEARING HOUSING AT RIB 9 LEVEL ON RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 612951-14. (0334300)
- [SDR DALA2024040404063](https://openairdocs.org/sdr/DALA2024040404063.md): Girt Bar · obstructed · Apr 2, 2024 · N319NB · Airbus A319114 · Emergency Equipment
  > SHIP 3119 2L DOOR/ SLIDE WILL NOT ARM. CORRECTIVE ACTION: REMOVED FOD FROM GIRT BAR LOCKING MECHANISM PER A319 AMM 52-12. OK FOR SVC. (5352444)
- [SDR DALA2024021302016](https://openairdocs.org/sdr/DALA2024021302016.md): Sensor · faulted · Feb 10, 2024 · N319NB · Airbus A319114 · Power Lever
  > SHIP 3119 - ATO - AT 40KTS DUE TO A MOMENTARY #2 THRUST LEVER ANGLE SENSOR FAULT. CORRECTIVE ACTION: DEFERRED TLA SENSOR PER MEL 76-11-01. LATER REPLACED #2 THRUST CONTROL MODULE.
- [SDR DALA2023121210153](https://openairdocs.org/sdr/DALA2023121210153.md): Unknown · unknown · Dec 11, 2023 · N319NB · Airbus A319114 · Emergency Lighting
  > SHIP 3119 EPLS ROW'S 14-17 INOP. CORRECTIVE ACTION: REMOVED & REPLACED POWER (EPSU) FIN 12WL AS PER A320F AMM 33-51-38. OPS CHECK GOOD. A/C OK FOR SERVICE. (4334732)
- [SDR DALA2023112709739](https://openairdocs.org/sdr/DALA2023112709739.md): Unknown · unknown · Nov 24, 2023 · N319NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3119 DAMAGED SEAT TRACK Y1292 LOC. BTW FR64 TO FR66 AFT GALLEY AREA SEAT TRACK. CORRECTIVE ACTION: REPLACED PER ER/A 612734-14. (0080000)
- [SDR DALA2023112409674](https://openairdocs.org/sdr/DALA2023112409674.md): Unknown · unknown · Nov 23, 2023 · N319NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3119 CRACK INDICATION WAS FOUND ON FR16RH AT HOLE IDENTIFIED AS HOLE #6. CORRECTIVE ACTION: REPAIRED PER ER/A 563226-14AD. (0078980)
- [SDR DALA2023112409673](https://openairdocs.org/sdr/DALA2023112409673.md): Unknown · unknown · Nov 23, 2023 · N319NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3119 CRACK HAS BEEN NOTICED IN UPPER AREA OF FR20 LHS, EXISTING REPAIR ON HOLE 5. CORRECTIVE ACTION: REPAIRED PER ER/A 563224-14AD. (0078904)
- [SDR DALA2023112409672](https://openairdocs.org/sdr/DALA2023112409672.md): Unknown · unknown · Nov 23, 2023 · N319NB · Airbus A319114 · Fuselage Structure (General)
  > SHIP 3119 CRACK HAS BEEN NOTICED IN UPPER AREA OF FR20 LHS, EXISTING REPAIR ON HOLE 6. CORRECTIVE ACION: REPAIRED PER ER/A 563224-14AD. (0078632)
- [SDR DALA2023112409671](https://openairdocs.org/sdr/DALA2023112409671.md): Unknown · unknown · Nov 23, 2023 · N319NB · Airbus A319114 · Landing Gear Doors
  > SHIP 3119 WEAR FORWARD FITTING MAIN DOOR AT MAIN LANDING GEAR L/H SIDE. CORRECTIVE ACTION: REPLACED FORWARD FITTING MAIN DOOR AT MAIN LANDING GEAR L/H SIDE AS PER AIRBUS CMM 52-81-18. (0079084)
- [SDR DALA2023112409670](https://openairdocs.org/sdr/DALA2023112409670.md): Unknown · unknown · Nov 23, 2023 · N319NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3119 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA CONTINUITY FITTING LH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 612406-14AD. (0079068)
- [SDR DALA2023112409669](https://openairdocs.org/sdr/DALA2023112409669.md): Unknown · unknown · Nov 23, 2023 · N319NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3119 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT INTERNAL AREA FROM UPPER TENSION BOLT, RH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 612406-14AD. (0079050)
- [SDR DALA2023112409668](https://openairdocs.org/sdr/DALA2023112409668.md): Unknown · unknown · Nov 23, 2023 · N319NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3119 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT INTERNAL AREA, FROM UPPER TENSION BOLT, LH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 612406-14AD. (0079046)
- [SDR DALA2023112409667](https://openairdocs.org/sdr/DALA2023112409667.md): Unknown · unknown · Nov 23, 2023 · N319NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3119 CORROSION INTERNAL STRUCTURE WEB AND NUT PLATE LOC.AT STR 38L BTW FR 5 8 AND FR 59 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB AND NUT PLATE LOC.AT STR 38L BTW FR 58 AND FR 59 IN AFT CARGO COMPARTMENT AS PER A319 SRM5
- [SDR DALA2023112309663](https://openairdocs.org/sdr/DALA2023112309663.md): Unknown · unknown · Nov 23, 2023 · N319NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3119 CRACK INDICATION WAS FOUND ON FR16LH AT HOLE IDENTIFIED AS HOLE #6. CORRECTIVE ACTION: REPAIRED PER ER/A 563227-14AD. (0078062)
- [SDR DALA2023112709740](https://openairdocs.org/sdr/DALA2023112709740.md): Unknown · unknown · Nov 22, 2023 · N319NB · Airbus A319114 · Airborne Auxiliary Power Unit (APU) System
  > SHIP 3119 CORROSION ON ELECTRICAL CONNECTOR OF MANUAL DRIVE CWW EXTEND OF APU IN LET FLAPPER. CORRECTIVE ACTION: REPLACED APU AIR INTAKE FLAP ACTUATOR PER A320 FAM AMM 49-16-51-000-003-A AND A320 FAM AMM 49-16-51-400-003-A. (0076551)
- [SDR DALA2023112409675](https://openairdocs.org/sdr/DALA2023112409675.md): Unknown · unknown · Nov 22, 2023 · N319NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > SHIP 3119 CORROSION AIR INTAKE COWL ON ENG 2. CORRECTIVE ACTION: REPLACED AIR INTAKE COWL ON ENG 2 AS PER A320 FAM AMM 71-11-00- 000-040-A. (0076358)
- [SDR DALA2023112309665](https://openairdocs.org/sdr/DALA2023112309665.md): Unknown · unknown · Nov 22, 2023 · N319NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3119 CRACK INDICATION ON FRAME 16 RH SIDE CROSSBEAM SPLICING AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 612478-14AD. (0077687)
- [SDR DALA2023112309664](https://openairdocs.org/sdr/DALA2023112309664.md): Unknown · unknown · Nov 22, 2023 · N319NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3119 CRACK INDICATION ON FRAME 20 LH SIDE CROSSBEAM SPLICING AREA. CORRECTIVE ACTION: REPAIRED PER ERA 612506-14AD. (0077678)
- [SDR DALA2023112309662](https://openairdocs.org/sdr/DALA2023112309662.md): Unknown · unknown · Nov 22, 2023 · N319NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3119 CORROSION FLAP TRACK 3 BUSHING (2 EA) LOCATED ON FITTING ON LH WING. CORRECTIVE ACTION: REPLACED END STOP FITTING FLAP TRACK 3 ON LH WING AS PER A320 FAM AMM 27-54-46-000-001-A AND AMM 27-54-46-400-001-A. (0077178)
- [SDR DALA2023112309661](https://openairdocs.org/sdr/DALA2023112309661.md): Unknown · unknown · Nov 22, 2023 · N319NB · Airbus A319114 · Fuselage Main, Bulkhead
  > SHIP 3119 CRACK FRAME 35 STR 30 LH FWD FACE PRESSURE BULKHEAD IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A 612601-14AD. (0077732)
- [SDR DALA2023112209631](https://openairdocs.org/sdr/DALA2023112209631.md): Unknown · unknown · Nov 22, 2023 · N319NB · Airbus A319114 · Engine Cowling System
  > SHIP 3119 CRACK ON AIR INTAKE COWL AFT BULKHEAD LOC. AT 4 OCLOCK ON ENGINE 1. CORRECTIVE ACTION: REPAIRED PER ER/A 613867-14. (0076470)
- [SDR DALA2023112209633](https://openairdocs.org/sdr/DALA2023112209633.md): Unknown · unknown · Nov 21, 2023 · N319NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3119 CRACK INDICATION WAS FOUND ON FR16LH AT HOLE IDENTIFIED AS HOLE #6. CORRECTIVE ACTION: REPAIRED PER ERA 563227-14AD. (0075894)
- [SDR DALA2023112209630](https://openairdocs.org/sdr/DALA2023112209630.md): Unknown · unknown · Nov 21, 2023 · N319NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3119 DENT INTERNAL STRUCTURE DOOR AT LOWER FORWARD CORNER IN AFT CARGO COMP ARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A 613185-14. (0076074)
- [SDR DALA2023112209634](https://openairdocs.org/sdr/DALA2023112209634.md): Unknown · unknown · Nov 21, 2023 · N319NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3119 CRACK INDICATION WAS FOUND ON FR16RH AT HOLE IDENTIFIED AS HOLE #6. CORRECTIVE ACTION: REPAIRED PER ER/A 31-563226. (0075057)
- [SDR DALA2023112009551](https://openairdocs.org/sdr/DALA2023112009551.md): Unknown · unknown · Nov 19, 2023 · N319NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3119 FR35 PRESSURE BH ATTACHMENTS A CRACK 2.0" LONG WAS FOUND RUNNING THROUGH FASTENER HOLES #2, #6, AND #7 IN LHS FR35 BH AT LEVEL OF STR30. CORRECTIVE ACTION: COMPLIED WITH ERA 612601-31. (0073402)
- [SDR DALA2023112009545](https://openairdocs.org/sdr/DALA2023112009545.md): Unknown · unknown · Nov 19, 2023 · N319NB · Airbus A319114 · Nacelle/Pylon, Frame/Spar/Rib
  > SHIP 3119 GOUGE WEB UPPER SPAR LOC. BTW RIB8 AND RI9 OUTBOARD SIDE LH PYLON. CORRECTIVE ACTION: COMPLIED WITH ERA 612671-14 REV. ORIGINAL. (0072104)
- [SDR DALA2023112009550](https://openairdocs.org/sdr/DALA2023112009550.md): Unknown · unknown · Nov 18, 2023 · N319NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3119 CRACK INDICATIONS FOUND IN LH FRONT WINDSHIELD FRAME AT THE CENTER LWR NODE AREA IN UPPER TENSION BOLT ATTACH HOLE D1. CORRECTIVE ACTION: COMPLIED WITH ERA 612406-31. (0071632)
- [SDR DALA2023112009549](https://openairdocs.org/sdr/DALA2023112009549.md): Unknown · unknown · Nov 18, 2023 · N319NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3119 CRACK INDICATIONS FOUND IN LH FRONT WINDSHIELD FRAME AT THE CENTER LWR NODE AREA IN UPPER TENSION BOLT ATTACH HOLE D1. CORRECTIVE ACTION: COMPLIED WITH ERA 612406-31. (0071624)

Next page: https://openairdocs.org/aircraft/N319NB/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 = 'N319NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N319NB/reports

---
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