# Service difficulty reports: N361NB

A list on [N361NB](https://openairdocs.org/aircraft/N361NB.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 · 192 reports

- [SDR DALA2026100105457](https://openairdocs.org/sdr/DALA2026100105457.md): Light · missing · Sep 29, 2026 · N361NB · Airbus A319114 · Emergency Lighting
  > DURING CAV FOUND FLOOR PROZIMITY EMERGENCY ESCAPE PATH MARKING LIGHT LENS MISSING NEXT TO CLOSET 302. FWD TO MEL 33-50-03A. MEL PLACARD INSTALLED. MEL REMARKS C/W. NO "M" PROCEDURES. CONTACTED MCC. REQURES MPN BR9471-11 STOCK # 33-3300-3-0127. REF CMM 25-31-9
- [SDR DALA2026052703187](https://openairdocs.org/sdr/DALA2026052703187.md): Battery · overheated · May 23, 2026 · N361NB · Airbus A319114 · Standard Practices/Structures
  > AT CRUISE, FA HAD USE THE LITHUIUM CONTAINMENT BAG FOR AN OVERHEATING EXTERNAL BATTERY. FWD TO MCC PER NEF 25-32-13. ALL REMARK C/W SEE L//P 8936275. (LP: 8936274) AIRCRAFT WAS GROUNDED
- [SDR DALA2026053103307](https://openairdocs.org/sdr/DALA2026053103307.md): Window · blistered · May 16, 2026 · N361NB · Airbus A319114 · Flight Compartment Windows
  > FO MIDDLE WINDSCREEN DELAMINTING ATTHE BOTTOM. ABOUT HALF DOLLR SIZE AND GROWING. CANNOT TOUCH WINDSCREEN IN THAT AREA DO TO HEAT. PULLED\ C/B W13 PER MAINT CONTROL DIRECTION. PERFORMED SLIDING WINDOW INSPECTION PER A319 AMM 56-12. FOUND TO BE WITHIN DELAM LI
- [SDR DALA2026052203122](https://openairdocs.org/sdr/DALA2026052203122.md): Oven · odor · May 12, 2026 · N361NB · Airbus A319114 · Buffet/Galleys
  > SHIP 3161 DISC: OVEN -INCLUDES OVEN TIMERS DAMAGED. WHEN ON AND IN USE, THE OVEN HAS A STRONG BURNT PLASTIC SMELL. THE SMELL FILLS UP THE GALLEY. I DO NOW THINK THIS OVEN SHOULD BE USED AGAIN BEFORE IT'S FIXED. C/A: DISCUSSION SMELL WITH F/A AND CAPT. RAN OVEN
- [SDR DALA2026030801587](https://openairdocs.org/sdr/DALA2026030801587.md): Tailpipe · fire · Mar 3, 2026 · N361NB · Airbus A319114 · Engine Collector/Tailpipe/Nozzle
  > TAILPIPE FIRE ON ENG 2. INFORMATION WAS FORWARDED FROM ANOTHER CREW ALL START INDICATIONS ON ECAM NORMAL. PERFORMED FADEC 2A/B OP TEST PER A319 AMM-NO FAULTS NO LAST LEG FAULTS.RAN ENGINE 2 PER A319 AMM 71-00-00 NO DEFECTS. (LP: 8280298)
- [SDR DALA2026012600553](https://openairdocs.org/sdr/DALA2026012600553.md): Hmu · failed · Jan 22, 2026 · N361NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > OBSERVED LARGE FLAMES EXITING NR 2 ROTOR ON START. TOWER CAM VERIFIED. NO COCKPIT/ECAM INDICATIONS. SHUTDOWN NR 2 AND TOWED BACK IN. R & R NR 2 ENGINE HMU IAW AMM 73-21. PERFORMED ENGINE IDLE LEAK CHECK. LEAK CHECKS GOOD. (LP: 8056744)
- [SDR DALA2026011500360](https://openairdocs.org/sdr/DALA2026011500360.md): Repair · damaged · Jan 12, 2026 · N361NB · Airbus A319114 · Service Doors
  > ON R1 DOOR AFT LWR SHEET REPAIR FOUND ONE RIVET BUCKTAIL ISN'T CENTER AND OFF TO ONE SIDE. ALSO FOUND SEALANT MISSING FOR SEAL RETAINER. APPLIED SEALANT ON FWD CHANNEL CORNER ON FWD PAX DOOR PER A319 SRM 52-10. REMOVED TWO RIVETS WITH POOR QUALITY BUCKTAILS R
- [SDR DALA2026011200259](https://openairdocs.org/sdr/DALA2026011200259.md): Engine · fire · Jan 11, 2026 · N361NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > ON NR 2 ENGINE START, GROUND ADVISED FIRE & THAT THEY OBSERVED FLAMES COMING FROM THE ENGINE. T/S IAW TSM 72-00-00-810-801-A. NO DISCREPANCIES NOTED. NO 30-DAY HISTORY
- [SDR DALA2025123109530](https://openairdocs.org/sdr/DALA2025123109530.md): Door Frame · gouged · Dec 31, 2025 · N361NB · Airbus A319114 · Fuselage Main, Structure
  > GOUGE BETWEEN FASTENERS C & D OF FR 20R DOUBLE JOGGLE AFT OF R1 DOOR. REPAIRED PER ERA 631197-14. (1378104)
- [SDR DALA2025123109529](https://openairdocs.org/sdr/DALA2025123109529.md): Frame · cracked · Dec 31, 2025 · N361NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK INDICATION FOUND ON FRAME 20RH DOUBLE JOGGLE AREA HOLE 5. REPAIRED PER ER/A 630623-14AD. (1377940)
- [SDR DALA2025123109527](https://openairdocs.org/sdr/DALA2025123109527.md): Skin · nicked · Dec 31, 2025 · N361NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > NICK EXTERNAL SKIN LOCATED BTW FR 67 TO FR 68 AND BTW STR 26L TO STR 27L LOWER FUSELAGE. REPAIRED PER ERA 631213-14. (1377959)
- [SDR DALA2025123109525](https://openairdocs.org/sdr/DALA2025123109525.md): Support · corroded · Dec 31, 2025 · N361NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION LOWER SILL LOCATED BETWEEN FR68 AND STR23R AFT GALLEY AREA. REPLACED LOWER SILL (1E/A), LOWER CORNER (2E/A), BRACKETS (11E/A), DRAIN (2E/A), CENTER FITTING (1E/A), SPLICE (4E/A) GIRT BARFITTINGS (2EA). AND FASTENERS LOCATED BETWEEN FR66 TO FR68 AN
- [SDR DALA2025123109538](https://openairdocs.org/sdr/DALA2025123109538.md): Door Frame · cracked · Dec 30, 2025 · N361NB · Airbus A319114 · Fuselage Main, Structure
  > FWD FUSELAGE FR 20 RHS DOUBLE JOGGLE AREA HOLE C & D GOUGE. REPAIRED PER ER/A 631197-14. (1377595)
- [SDR DALA2025123109537](https://openairdocs.org/sdr/DALA2025123109537.md): Door Frame · cracked · Dec 30, 2025 · N361NB · Airbus A319114 · Fuselage Main, Structure
  > NOSE FWD FUSELAGE FR20RH AT DOOR STOP NR 7 LEVEL, DOUBLE JOGGLE AREA FASTENER HOLE 5 CRACK. REPAIRED PER ER/A 630623-14AD. (1377389)
- [SDR DALA2025123109536](https://openairdocs.org/sdr/DALA2025123109536.md): Structure · damaged · Dec 30, 2025 · N361NB · Airbus A319114 · Buffet/Galleys
  > CORROSION ON COMPARTMENTS 510, 511 AND 512 ON GALLEY 5 AFT GALLEY AREA. REPAIRED PER ER/A 630809-14. (1377077)
- [SDR DALA2025123109533](https://openairdocs.org/sdr/DALA2025123109533.md): Power Supply · faulted · Dec 30, 2025 · N361NB · Airbus A319114 · Emergency Lighting
  > UNIT FAULT EPSU 10WL. REPLACED EMERGENCY POWER SUPPLY UNIT (10WL)AS PER A320 FAM AMM 33-51-38-000-001-A AND A320 FAM AMM 33-51-38-400-001-A. (1377317)
- [SDR DALA2025123109532](https://openairdocs.org/sdr/DALA2025123109532.md): Frame · cracked · Dec 30, 2025 · N361NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 20 LH SIDE OPEN FASTENER HOLE H18 IN CROSSBE AM SPLICING AREA. REPAIRED PER ER/A 630734-14AD. (1377113)
- [SDR DALA2025123109531](https://openairdocs.org/sdr/DALA2025123109531.md): Frame · cracked · Dec 30, 2025 · N361NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 20 LH SIDE OPEN FASTENER HOLE H26 IN CROSSBEAM SPLICING AREA. REPAIRED PER ER/A 630734-14AD. (1377105)
- [SDR DALA2025123109528](https://openairdocs.org/sdr/DALA2025123109528.md): Floor Panel · delaminated · Dec 30, 2025 · N361NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 261DF IN PASSENGER CABIN. REPAIRED PER ER/A 630841-14. (1377632)
- [SDR DALA2025123109526](https://openairdocs.org/sdr/DALA2025123109526.md): Rib · gouged · Dec 30, 2025 · N361NB · Airbus A319114 · Trailing Edge Flaps
  > GOUGE INBOARD END RIB OF OB FLAP ON RH WING. REPAIRED PER ER/A 631149-14. (1377593)
- [SDR DALA2025123109524](https://openairdocs.org/sdr/DALA2025123109524.md): Skin · dented · Dec 30, 2025 · N361NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > DENTS ON SKIN LOCATED ON DOUBLER REPAIR BTW FR 6 TO FR 7 AT LATERAL LONGITUNAL LAP JOINT RH SIDE AT LOWER FUSELAGE. REPAIRED PER ER/A 630823-14. (1377088)
- [SDR DALA2025122909443](https://openairdocs.org/sdr/DALA2025122909443.md): Floor Panel · corroded · Dec 28, 2025 · N361NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 222EF IN PASSENGER CABIN. REPAIRED PER ER/A 630951-14. (1374034)
- [SDR DALA2025122909441](https://openairdocs.org/sdr/DALA2025122909441.md): Insert · corroded · Dec 28, 2025 · N361NB · Airbus A319114 · Fuselage Floor Panel
  > CORROSION INSERT FLOOR PANEL 221LF IN PASSENGER CABIN. REPAIRED PER ER/A 630951-14. (1374022)
- [SDR DALA2025122909440](https://openairdocs.org/sdr/DALA2025122909440.md): Floor Panel · delaminated · Dec 28, 2025 · N361NB · Airbus A319114 · Fuselage Floor Panel
  > DELAMINATED FLOOR PANEL 221DF IN PASSENGER CABIN. REPAIRED PER ER/A 630951-14. (1373982)
- [SDR DALA2025122909447](https://openairdocs.org/sdr/DALA2025122909447.md): Crossbeam · cracked · Dec 27, 2025 · N361NB · Airbus A319114 · Fuselage Main, Structure
  > FUSELAGE FRAMES CROSSBEAM JUNCTION AREA AT FR20 LH HOLES H18 & H26 CRACK. REPAIRED PER ERA 630734-14AD. (1371189)
- [SDR DALA2025122909445](https://openairdocs.org/sdr/DALA2025122909445.md): Post · corroded · Dec 27, 2025 · N361NB · Airbus A319114 · Fuselage Main, Structure
  > CORROSION ON AFT RH LATERAL POST LAV A. REPAIRED PER ER/A 630720-14. (1372197)
- [SDR DALA2025122909442](https://openairdocs.org/sdr/DALA2025122909442.md): Floor Panel · corroded · Dec 27, 2025 · N361NB · Airbus A319114 · Fuselage Floor Panel
  > CORROSION FUSELAGE PANEL INSTL-PASS COMPT FLOOR PANELS SEALING ANGLE. REPAIRED PER ER/A 631147-14. (1372047)
- [SDR DALA2025122909446](https://openairdocs.org/sdr/DALA2025122909446.md): Skin · dented · Dec 26, 2025 · N361NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > FWD FUSELAGE SKIN PANEL BTW FR6-8 RHS LATERAL STGR DENT ON PREVIOUS DOUBLER REPAIR. REPAIRED PER ERA 630823-14. (1371027)
- [SDR DALA2025122909444](https://openairdocs.org/sdr/DALA2025122909444.md): Slat Track · corroded · Dec 26, 2025 · N361NB · Airbus A319114 · Leading Edge Devices
  > CORROSION ON BOLT ON SLAT TRACK N1 RH WING. R/R BOLT ON SLAT TRACK N1 RH WING (1 EA) AS PER A320 FAM AIPC 27-84-61-01B. (1370951)
- [SDR DALA2025122209286](https://openairdocs.org/sdr/DALA2025122209286.md): Access Panel · damaged · Dec 21, 2025 · N361NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > IMPROPERLY HOLE ACCESS PANEL 192KB BELLY FAIRING AT LOWER FUSELAGE. COMPLIED WITH ER/A 592345-14. (1362569).
- [SDR DALA2025122209284](https://openairdocs.org/sdr/DALA2025122209284.md): Bonding Plate · debonded · Dec 20, 2025 · N361NB · Airbus A319114 · Trailing Edge Flaps
  > DEBONDED BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. COMPLIED WITH ER/A 622998-14TR. (1360175).
- [SDR DALA2025122209283](https://openairdocs.org/sdr/DALA2025122209283.md): Bonding Plate · debonded · Dec 20, 2025 · N361NB · Airbus A319114 · Trailing Edge Flaps
  > DEBONDED BONDING PLATE FLAP TRACK FAIRING 632CB ON RH WING. COMPLIED WITH ER/A 622998-14TR. (1360171)
- [SDR DALA2025122209282](https://openairdocs.org/sdr/DALA2025122209282.md): Bonding Plate · debonded · Dec 20, 2025 · N361NB · Airbus A319114 · Trailing Edge Flaps
  > DEBONDED BONDING PLATE FLAP TRACK FAIRING 4 (533CB) ON LT WING. COMPLIED WITH ER/A 622998-14TR. (1360147).
- [SDR DALA2025121909254](https://openairdocs.org/sdr/DALA2025121909254.md): Seat Track · corroded · Dec 18, 2025 · N361NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK -Y254, FR 67. REPLACED THE SEAT AND FASTENERS, BTW FR 66 - 68 IAW SRM 51-42-11, AND SRM 51-72-11. (1358084).
- [SDR DALA2025121809219](https://openairdocs.org/sdr/DALA2025121809219.md): Seat Track · corroded · Dec 17, 2025 · N361NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3161 CORROSION SEAT TRACK -Y464.8 AT FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y464.8 BTW FR68 TO FR70 AT AFT GALLEY AREA AND FASTENERS AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1356233).
- [SDR DALA2025121809218](https://openairdocs.org/sdr/DALA2025121809218.md): Web · corroded · Dec 17, 2025 · N361NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3161 CORROSION WEB LOCATED BETWEEN FR20 AND STR23R FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB LOCATED BETWEEN FR20 TO FR24 AND AT LEVEL STR23R FWD GALLEY AREA AS PER A319 SRM 51-72-11. (1356222).
- [SDR DALA2025121809217](https://openairdocs.org/sdr/DALA2025121809217.md): Skin · dented · Dec 17, 2025 · N361NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3161 DENTS ON SKIN LOCATED ON DOUBLER REPAIR BTW FR 29 TO FR 30 AND STR 4 1L TO STR 42L AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 555536-14AD. (1356218).
- [SDR DALA2025121809216](https://openairdocs.org/sdr/DALA2025121809216.md): Seat Track · corroded · Dec 17, 2025 · N361NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3161 CORROSION SEAT TRACK -Y1162.5 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y 1162.5 LOC. BTW FR 66 TO FR 68 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (1356214).
- [SDR DALA2025121809215](https://openairdocs.org/sdr/DALA2025121809215.md): Seat Track · corroded · Dec 17, 2025 · N361NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3161 CORROSION SEAT TRACK -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLE Y AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y 1162.5 LOC. BTW FR 68 TO FR 69 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (1356205).
- [SDR DALA2025121809214](https://openairdocs.org/sdr/DALA2025121809214.md): Seat Track · corroded · Dec 17, 2025 · N361NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3161 CORROSION SEAT TRACK -Y765 AT FR20 FWD GALLEY AREA. REPLACED SEAT TRACK -Y765 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (1356178).
- [SDR DALA2025121609156](https://openairdocs.org/sdr/DALA2025121609156.md): Stringer · corroded · Dec 16, 2025 · N361NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 41R LOC BTW FR63 TO FR64 IN AFT CARGO BAY. REPLACED STRINGER 41R IAW SRM 51-72-11 AND SRM 51-42-11. (1353612).
- [SDR DALA2025121609154](https://openairdocs.org/sdr/DALA2025121609154.md): Seat Track · corroded · Dec 15, 2025 · N361NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK -Y1292 AT FR66 AT AFT GALLEY AREA. REPLACED SEAT TRACK -Y1292, LOC. FROM FR64 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1351997).
- [SDR DALA2025121609153](https://openairdocs.org/sdr/DALA2025121609153.md): Seat Track · corroded · Dec 14, 2025 · N361NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FLOOR BEAM -Y765 AT FR68 AT AFT GALLEY AREA. REPLACED FLOOR BEAM -Y765 LOC. BTW FR67 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (1350495).
- [SDR DALA2025121609152](https://openairdocs.org/sdr/DALA2025121609152.md): Seat Track · corroded · Dec 14, 2025 · N361NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK +Y1292 LOCATED BTW FR 65 TO FR 66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292 FR 64 TO FR 66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1350491).
- [SDR DALA2025121609151](https://openairdocs.org/sdr/DALA2025121609151.md): Seat Track · corroded · Dec 13, 2025 · N361NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3161 CORROSION SEAT TRACK +Y765 AT FR20 FWD GALLEY AREA: CORRECTIVE ACTION: REPLACED FLOOR BEAM (SEAT TRACK) Y765 LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (1350466).
- [SDR DALA2025121209081](https://openairdocs.org/sdr/DALA2025121209081.md): Seat Track · corroded · Dec 11, 2025 · N361NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK -Y1292 AT FR20 FWD GALLEY AREA. REPLACED SEAT TRACK -Y1292 AND FASTENERS LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA. AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1347142).
- [SDR DALA2025121209080](https://openairdocs.org/sdr/DALA2025121209080.md): Shear Plate · corroded · Dec 11, 2025 · N361NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION SHEAR PLATE STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE AND FASTENERS LOC. STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72 -11. (1347132).
- [SDR DALA2025121209079](https://openairdocs.org/sdr/DALA2025121209079.md): Web · cracked · Dec 11, 2025 · N361NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CRACK WEB LOCATED FLOOR STRUCTURE AREA FROM FR68 TO FR69 AND STR23LH AT AFT GALLEY AREA. REPLACED WED LOCATED FLOOR STRUCTURE AREA FROM FR68 TO FR69 AND STR23LH AT AFT GALLEY AREA AS PER A319 SRM 51-42-11. (1347126).
- [SDR DALA2025121209078](https://openairdocs.org/sdr/DALA2025121209078.md): Shear Plate · corroded · Dec 11, 2025 · N361NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > CORROSION SHEAR PLATE STR 23 R LOCATED BTW FR 69 TO FR 70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SHEAR PLATE AND FASTENERS LOC. ON STR23 RH BTW FR69 TO FR70 AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72- 11. (1347119).
- [SDR DALA2025121209077](https://openairdocs.org/sdr/DALA2025121209077.md): Shear Plate · corroded · Dec 11, 2025 · N361NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION SHEAR PLATE STRINGER 23L BTW FR69 AND FR70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE AND FASTENERS LOC. STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA AS PER SRM 51-42-11 AND SRM 51-72 -11. (1347109).

Next page: https://openairdocs.org/aircraft/N361NB/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 = 'N361NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N361NB/reports

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