N8886A
Service difficulty reports · 112
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 = 'N8886A' 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 = 'N8886A' 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 REXA201100470Bulkhead · chafedREAR PRESSURE BULKHEAD CHAFED ON PREVIOUS REPAIRS 2 LOCATIONS ON LT SIDE AT LBL 18 AND LBL 27 ALL LOCATED 30 INCHES ABOVE THE FLOOR LEVEL. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.SDR REXA201100469Post · damagedFOUND FS 409.0+128 VERTICAL POST BL 0.00 LT & RT SIDES HAVE INDICATIONS NOTED APPROX .2 INCH IN LENGTH 60 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS BOTH FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06 AND BOMBARDIER REO 601R-53-41-889.SDR REXA201100468Post · damagedFOUND FS 409.0+128 VERTICAL POST RBL 18.0 OTBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 60 PERCENT FSH AT WL 69.0 AFT. FLANGE RADIUS FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06, 51-42-22, AND BOMBARDIER REO 601R-53-41-889.SDR REXA201100467Skin · dentedFUSELAGE SKIN IS DENTED AT FS 642 BETWEEN STR 21L & 22L. DENT MEASURES APPROX .650" DIA X .045"D. REPAIRED IAW BOMBARDIER REO 601R-53-61-4132.SDR REXA2011004645Floor Support · corrodedCARGO FLOOR SUPPORT BEAM CAP ANGLE HAS CORROSION AROUND FASTENER HOLES BETWEEN FS 589-FS 621, LBL 27. REPAIRED IAW SRM 51-42-34, 51-45-00,51-42-21, 5142-22, AND BOMBARDIER REO 601R53-61-3788 REV A.SDR REXA201100131Engine · malfunctionedCREW REPORTED SMOKE IN THE CABIN EMERGENCY DECLARED. T/S TO THE RIGHT ENGINE CAUSING THE SMOKE IN CABIN WITH EITHER LT OR RT PACKS RUNNING OFF RT ENGINE, A/C WAS FERRIED TO TYS FOR BOROSCOPE AND POSSIBLE ENGINE CHANGE.SDR REXA201100080Control Unit · malfunctionedSTAB TRIM RUNAWAY ON DEPARTURE. AIR RETURN TO JFK. QRH COMPLETED. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. PERFORMED OPS CHECK ON HSTCU. OPS CHECK GOOD. OK FOR SERVICE.SDR REXA201100041Carbon Seal · leakingON CLIMBOUT OF KDTW THE CAPTAIN SAW SMOKE COMING FROM A VENT. THIS WAS FOLLOWED BY A SMOKE TOILET CAUTION MESSAGE. THE FLIGHT CREW COMPLIED WITH THE QRH, DECLARED AN EMERGENCY AND REQUESTED TO RETURN TO KDTW. AN OTHERWISE UNEVENTFULL APPROACH AND LANDING WASDR REXA201000114Shutoff Valve · inoperativeREFUEL PANEL INOP. NOT READING CORRECTLY. REFUEL SOV INOP. OPERATIONAL CHECK OF FUEL SYSTEM GOOD IAW AMM 28-00-00. THIS CLEARS DM 27692.SDR REX2008F00018Control Panel · malfunctionedRUDDER TRIM RUNAWAY WITH FULL DEFLECTION TO THE LT ON CLIMBOUT. REMOVED AND REPLACED AILERON RUDDER TRIM CONTROL PANEL IAW AMM. (A)SDR REXA200500115Control System · malfunctionedFLAP FAIL MESSAGE. INSPECTED PER AD 98-20-01. NO DEFECTS NOTED. RESET FLAPS PER MANUFACTURES FAULT ISOLATION MANUAL (FILM). OPERATIONALLY CHECKS GOOD.SDR REXA04040Elt · failedELT FAILS G-SWITCH TEST. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207.
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