N8416B
Service difficulty reports · 60
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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 = 'N8416B' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'N8416B' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR REXA201100303Fitting · chafedRT FWD OUTBOARD WING TO FUSELAGE FITTING IS CHAFED AT FWD CORNER .565" L X 0.170" W X 0.11D. REPAIRED IAW BOMBARDIER REO 601R-57-21-1433.SDR REXA201100301Structure · corrodedLBL 9 HAS CORROSION AROUND NUT PLATE HOLES BETWEEN FS 621 AND FS 574. REPAIRED IAW BOMBARDIER REO 601R-53-61-3780.SDR REXA201100300Floorbeam · corrodedLBL 27 FLOORBEAM HAS CORROSION AROUND NUT PLATE HOLES BETWEEN FS 621 AND FS 574. REPAIRED IAW BOMBARDIER REO 601R-53-61-3778.SDR REXA201100277Bulkhead · chafedFS 621 PRESSURE BULKHEAD FORWARD FACE HAS 6 CHAFED AREAS, 4 EACH HAVE BEEN PREVIOUSLY REPAIRED. ALL 36 INCHES ABOVE THE FLOOR. MATERIAL REMOVED: RBL36.2 - 0.010", RBL27.5 - 0.008", RBL18 - 0.003", LBL9.5 - 0.004", LBL18 - 0.009", AND LBL 27.5 - 0.007". REPSDR REXA201100093Flap · malfunctionedFLAPS FAIL AT 0, PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39, IAW AD2009-06-12 PARAGRAPH (H)(6)(I) AMOC DATED MARCH 27,2009 TR#27-012 PER AMOC DATED DEC 18 2009 & PA AD27-052G. THIS CLEARS DM#38354.SDR REXA201000224Skin · damagedLEFT OUTBOARD FLAP VANE HAD WEAR DAMAGE OUTBOARD OF THE WF = 282.5 FLAP HINGE ARM. THE DAMAGE WAS THE RESULT OF AN INCORRECT LENGTH FASTENER INSTALLED IN THE WING TRAILING EDGE STRUCTURE. THE FLAP VANE LEADING EDGE DAMAGE MEASURES 0.65 INCHES LONG BY 0.25 INSDR REXA200700066Engine · flamed outWHEN THE CREW REDUCED POWER TO DESCEND FROM FL300, THE RIGHT ENGINE FLAMED OUT. THE ENGINE OUT PROCEDURES OF THE QRH WERE PERFORMED AND THE ENGINE RESTARTED ON THE FIRST ATTEMPT. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WERE MADE. MAINTENANCE TROUBLESHOSDR REXA200600006Flap · malfunctionedFLAP FAIL AT 20 DEGREES ON APPROACH. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.SDR REXA05001Bpsu · failedFLAPS FAILED AT 30 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM WOULD NOT RESET. REPLACED RT BPSU (BRAKE POSITION SENSING UNIT) IAW AMM. (K)SDR REXA01001Control Unit · shortedDURING APPROACH TO MEMPHIS, THE L FIRE FAIL, L JETOVHT FAIL, APU FAIL, R FIRE FAIL, AND R JETOVHT FAIL CAUTION MESSAGES ILLUMINATED. APPROXIMATELY 20 SECONDS LATER, THE L JETOVHT WARNIGN MESSAGE ILLUMINATED INTERMITTENTLY, FOLLOWED BY THE L ENG FIRE AND APU F
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