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 aircraft_model_key = '425' 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 aircraft_model_key = '425' 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 2009FA0000549Skin · delaminatedLT NACELLE HAS SEVERAL AREAS OF DELAMINATION AND CORROSION OF OUTER SKIN. OBTAINED DER APPROVAL FOR REPAIRS OF AFFECTED AREAS.SDR 2009FA0000548Skin · delaminatedRT NACELLE HAS SEVERAL AREAS OF DELAMINATION AND CORROSION OF OUTER SKIN. OBTAINED DER APPROVAL FOR REPAIRS OF DELAMINATED AND CORRODED AREAS.SDR 2009FA0000546Spar Cap · damagedRT WING FWD SPAR CAP HAS A DOUBLE HOLE UNDER THE INBD ENGINE MOUNT SUPPORT. SUSPECT MIS-DRILLED DURING PRODUCTION. ENGINEERING DISPOSITION OBTAINED FOR REPAIR OF ELONGATED HOLE AREA.SDR 2009FA0000389Attach Angle · crackedLT INBD ENGINE NACELLE TO WING STRUCTURAL ATTACH POINT (ANGLE). CRACKED AT MID-POINT IN RADIUS. DISCOVERED DURING SID INSPECTION.SDR 2009FA0000384Trim System · out of rigFOUND ELEVATOR TRIM TAB HORN CONTACTING ELEVATOR SKIN AT 15 DEGREES TAB DOWN AND TRIM CABLE CAN NOT BE WRAPPED AT SERVO IAW MM. CALLED TECH SUPPORT, SENT AN E-MAIL STATING THAT THE RIGGING PROCEDURE FOR THE TRIM IS INCORRECT IN THE MM. MFG WILL CHANGE THE M/SDR 2009FA0000195Line · cutPERFORMED SUPPLEMENTAL INSP FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSP NR 57-10-14 CARRY-THRU FWD SPAR CAP FOUND MULTIPLE PNEUMATIC LINES SPLICED TOGETHER WITH STANDARD MIL-SPEC HOSE ON LT AND RT WINGS. LINES NOT AVAILABLE FROM MFGSDR 2009FA0000194Line · cutPERFORMED SUPPLEMENTAL INSP FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUP INSP NR 57-10-14 CARRY-THRU FWD SPAR CAP, FOUND MULTIPLE PNEUMATIC LINES SPLICED TOGETHER WITH STANDARD MIL-SPEC HOSE ON LT AND RT WINGS. LINES NOT AVAILABLE FROM MFG. FABRISDR 2009FA0000180Fitting · corrodedREPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THEIR SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND RT LOWER FWD FITTING CORRODED. REPLACED FITTING PN 0811350-10.SDR 2009FA0000179Fitting · corrodedREPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THEIR SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND LT LWR FWD FITTING CORRODED. REPLACED FITTING PN 0811350-10.SDR 2009FA0000178Torque Tube · corrodedREPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THE SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND RUDDER TORQUE TUBE RUSTED DURING SUPPLEMENTAL INSPECTION 27-20-04. REPLACED TORQUE TUBE PN 5833011-9.SDR 2009FA0000170Actuator · corrodedREPORTED DURING SUPPLEMENTAL INSPECTIONS FOR CONTINUED AIRWORTHINESS FOR THE AIRPLANE. DURING INSPECTION OF ELEVATOR TRIM TAB ACUTATOR IAW MM 27-30-02 FOUND BARREL CORRODED. REPLACED ACTUATOR WITH PN 5715160-8.SDR 2009FA0000169Actuator · corrodedREPORTED DURING SUPPLEMENTAL INSPECTIONS FOR CONTINUED AIRWORTHINESS FOR THE AIRPLANE. DURING INSPECTION OF ELEVATOR TRIM TAB ACUTATOR IAW MM 27-30-02 FOUND BARREL CORRODED. REPLACED ACTUATOR WITH PN 5715160-8.SDR 2009FA0000168Actuator · corrodedREPORTED DURING SUPPLEMENTAL INSPECTIONS FOR CONTINUED AIRWORTHINESS FOR THE AIRPLANE. DURING INSPECTION OF ELEVATOR TRIM TAB ACUTATOR IAW MM 27-30-02 FOUND BARREL CORRODED AND PITTED. REPLACED ACTUATOR WITH PN 5715160-8.SDR 2009FA0000165Hinge · corrodedREPORTED TO MFG DURING SUPPLEMENTAL INSPECTION FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSPECTION NR 52-10-01 CABIN DOOR RETENTION FOUND HARDWARE UNABLE TO REMOVE FROM UPPER CABIN DOOR DUE TO CORROSION. DRILLED OFF UPPER AND LOWER CASDR 2009FA0000164Hinge · corrodedPREVIOUSLY REPORTED TO MFG DURING SUPPLEMENTAL INSPECTION FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSPECTION NR 52-10-01 CABIN DOOR RETENTION FOUND HARDWARE UNABLE TO REMOVE FROM UPPER CABIN DOOR DUE TO CORROSION. DRILLED OFF UPPER ASDR 2009FA0000163Hinge · corrodedPREVIOUSLY REPORTED TO MFG DURING SUPPLEMENTAL INSPECTION FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING SUPPLEMENTAL INSPECTION NR 52-10-01 CABIN DOOR RETENTION FOUND HARDWARE UNABLE TO REMOVE FROM UPPER CABIN DOOR DUE TO CORROSION. DRILLED OFF UPPER ASDR 2009FA0000155Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND LT WING OTBD TRUSS ASSY PN 5951051-35 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000154Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND LT WING OTBD TRUSS ASSY PN 5951051-35 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000153Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND RT WING INBD TRUSS ASSY PN 5951051-38 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000152Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND LT WING INBD TRUSS ASSY PN 5951051-37 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000151Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND RT WING INBD TRUSS ASSY PN 5951051-38 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000150Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND LT WING INBD TRUSS ASSY PN 5951051-37 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000149Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND RT WING INBD TRUSS ASSY PN 5951051-38 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000148Truss · corrodedDURING SUPPLEMENTAL INSP 54-10-02 FOUND LT WING INBD TRUSS ASSLY PN 5951051-37 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000144Bellcrank · crackedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. NOSE GEAR STEERING BELLCRANK PN 5942001-1 FAILED VISUAL AND NDT INSPECTION IAW SUPPLEMENTAL INSPECTION 32-50-00. REPLACEDSDR 2009FA0000143Bellcrank · crackedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. NOSE GEAR STEERING BELLCRANK PN 5942001-1 FAILED VISUAL AND NDT INSPECTION IAW SUPPLEMENTAL INSPECTION 32-50-00. REPLACEDSDR 2009FA0000142Bellcrank · crackedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. NOSE GEAR STEERING BELLCRANK PN 5942001-1 FAILED VISUAL AND NDT INSPECTION IAW SUPPLEMENTAL INSPECTION 32-50-00. REPLACEDSDR 2009FA0000139Fork · crackedPREVIOUSLY REPORTED TO MFG INSTRUCTIONS STIPULATED IN SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. NOSE GEAR FORK FAILED NDT IAW SUPPLEMENTAL INSPECTION 32-20-02. REPLACED NOSE FORK ASSEMBLY PN 5842000-5.SDR 2009FA0000138Strut · crackedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. NOSE GEAR FORK FAILED NDT IAW SUPPLEMENTAL INSPECTION 32-20-02. REPLACED NOSE FORK ASSEMBLY PN 5842000-230.SDR 2009FA0000137Fork · crackedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. NOSE GEAR FORK FAILED NDT IAW SUPPLEMENTAL INSPECTION 32-20-02. REPLACED NOSE FORK ASSEMBLY PN 5842000-5.SDR 2009FA0000136Fork · crackedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. NOSE GEAR FORK FAILED NDT IAW SUPPLEMENTAL INSPECTION 32-20-02. REPLACED NOSE FORK ASSEMBLY PN 5842000-5.SDR 2009FA0000135Fork · crackedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. NOSE GEAR FORK FAILED NDT IAW SUPPLEMENTAL INSPECTION 32-20-02. REPLACED NOSE FORK ASSEMBLY PN 5842000-5.SDR 2009FA0000131Torque Tube · corrodedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THE SUPPLEMENTAL INSP DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND RUDDER TORQUE TUBE RUSTED DURING INSPECTION OF SUPPLEMENTAL INSPECTION 27-20-04. REPLACED TORQUE TUBE PN 5833011-9.SDR 2009FA0000130Torque Tube · corrodedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THE SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND RUDDER TORQUE TUBE RUSTED DURING INSPECTION OF SUPPLEMENTAL INSPECTION 27-20-04. REPLACED TORQUE TUBE PN 583301SDR 2009FA0000129Torque Tube · corrodedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THE SUPPLEMENTAL INSP DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND RUDDER TORQUE TUBE RUSTED DURING INSP OF SUPPLEMENTAL INSP 27-20-04. REPLACED TORQUE TUBE PN 5833011-9.SDR 2009FA0000128Mast · rustedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THE SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND RUDDER TORQUE TUBE RUSTED DURING INSPECTION OF SUPPLEMENTAL INSPECTION 27-20-04. REPLACED TORQUE TUBE PN 583301SDR 2009FA0000127Torque Tube · corrodedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THE SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND RUDDER TORQUE TUBE RUSTED DURING INSPECTION OF SUPPLEMENTAL INSPECTION 27-20-04. REPLACED TORQUE TUBE PN 583301SDR 2009FA0000126Torque Tube · corrodedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THE SUPPLEMENTAL INSP DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND RUDDER TORQUE TUBE RUSTED DURING INSP OF SUPPLEMENTAL INSP 27-20-04. REPLACED TORQUE TUBE PN 5833011-9.SDR 2009FA0000125Torque Tube · corrodedPREVIOUSLY REPORTED TO MFG IAW INSTRUCTIONS STIPULATED IN THE SUPPLEMENTAL INSP DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. FOUND RUDDER TORQUE TUBE RUSTED DURING INSPECTION OF SUPPLEMENTAL INSPECTION 27-20-04. REPLACED TORQUE TUBE PN 5833011-9.SDR 2009FA0000119Fitting · corrodedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE RT WING LWR FWD ATTACH FITTING PN0811350-10 FAILED NDT INSPECTION. REPLACED WING FITTING.SDR 2009FA0000118Fitting · misrepairedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE RT WING UPPER FWD ATTACH FITTING PN 0822550-30 HAD UNAPPROVED STEEL BUSHING UNABLE TO PERFORM NDT INSPECTION. REPLACED WING FITTINGSDR 2009FA0000117Attach Fitting · misrepairedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE RT WING LWR FWD ATTACH FITTING PN 0822550-50 HAD UNAPPROVED STEEL BUSHING INSTALLED UNABLE TO PERFORM NDT INSPECTION. REPLACED WINGSDR 2009FA0000115Attach Fitting · corrodedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE RT WING LWR AFT ATTACH FITTING PN 5011024-2 FAILED NDT INSPECTION. REPLACED WING FITTING.SDR 2009FA0000114Attach Fitting · corrodedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE RT WING LWR FWD ATTACH FITTING PN 0811350-10 FAILED NDT INSPECTION. REPLACED WING FITTING.SDR 2009FA0000113Attach Fitting · crackedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE LT WING LWR AFT ATTACH FITTING PN 5011024-2 FAILED NDT INSPECTION. REPLACED WING FITTING.SDR 2009FA0000112Attach Fitting · corrodedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE RT WING LWR AFT ATTACH FITTING PN 5011024-2 FAILED NDT INSPECTION. REPLACED WING FITTING.SDR 2009FA0000111Attach Fitting · corrodedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE RT WING LWR FWD ATTACH FITTING PN 0811350-10 FAILED NDT INSPECTION. REPLACED WING FITTING.SDR 2009FA0000110Attach Fitting · corrodedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSP DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE LT WING UPPER FWD ATTACH FITTING PN 5011023-2 FAILED NDT INSPECTION. REPLACED WING FITTING.SDR 2009FA0000109Attach Fitting · corrodedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE LT WING LWR AFT ATTACH FITTING PN 5011024-2 FAILED NDT INSPECTION. REPLACED WING FITTING.SDR 2009FA0000108Attach Fitting · corrodedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY SUPPLEMENTAL INSP DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE LT WING LOWER FWD ATTACH FITTING PN 0811350-10 FAILED NDT INSPECTION. REPLACED WING FITTING.
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