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 = '1900D' 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 = '1900D' 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 ERAA201307030045Line · leakingFUEL LEAK FROM RT NACELLE. R & R FUEL LINE BETWEEN FCU AND FUEL FLOW TRANSMITTER IAW MM 73-10-03. LEAK CHECKED GOOD.SDR 29GA94232070213AConnector · looseNOSE GEAR WOULD NOT INDICATE GREEN, MANUAL GEAR EXTENSION PERFORMED. RESECURED LOOSE CONNECTORS AT NOSE GEAR ACTUATOR AND REPLACED ANNUNCIATOR LAMPS OPS CHECK ALL INDICATIONS NORMAL. TEST FLIGHT SATISFACTORY.SDR GLBA2013070100267Relay · inoperativePILOT REPORTED THAT THE LANDING GEAR WOULD NOT EXTEND NORMALLY ON APPROACH, RAN CHECKLIST AND NOT HELP, MANUALLY PUMPED GEAR DOWN, ALL INDICATIONS NORMAL, AFTER LANDING FOUND LANDING GEAR RELAY CB POPPED. MX R & R TIME DELAY PCB, R & R GEAR MOTOR RELAY, R & RSDR GLBA2013070100266Motor · inoperativePILOT REPORTED THAT THE LANDING GEAR FAILED TO EXTEND WHEN GEAR HANDLE WAS SELECTED TO DOWN POSITION, NO INTRANSIT LIGHT INDICATION AND NO GREEN LIGHTS, RAN CHECKLIST AND MANUALLY EXTENDED GEAR. MX R & R THE POWER PACK MOTOR AND TIME DELAY PCB, OPS CHECKED GOSDR GLBA2013062800265Relay · malfunctionedLANDING GEAR WOULD NOT EXTEND NORMALLY ON APPROACH. RAN CHECKLISTS AND NO HELP, MANUALLY PUMPED GEAR DOWN. ALL INDICATIONS NORMAL. AFTER LANDING, FOUND LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED. R & R LANDING GEAR MOTOR RELAY IAW AIM 12-15.0. R & R LANDINSDR 29GA201307022530Skin · corrodedDURING SCHEDULED STRUCTURAL INSPECTION, DISCOVERED CORROSION ON EXTERIOR SKIN APPROXIMATELY BS 251 TO 258 STRINGERS 14-16L. REMOVED DAMAGED EXTRIOR SKIN AND INSTALLED COVER PATCH.SDR 29GA2013062842530Skin · corrodedDURING SCHEDULED STRUCTURAL INSPECTION, DISCOVERED CORROSION ON EXTERIOR SKIN APPROXIMATELY AT FS 348, STRINGER 15R. REMOVED DAMAGED EXTERIOR SKIN AND INSTALLED COVER PATCH.SDR ERAA201307040047Unknown · odorEXHAUST ODOR IN COCKPIT AFTER ROTATION, ODOR WENT AWAY AFTER TURNING BLOWERS OFF. COULD NOT DUPLICATE ON GROUND, OK FOR SERVICE.SDR GLBA2013062400264Motor · odorPILOT REPORTED THAT THEY SMELLED ELECTRICAL SMOKE IN THE AFT CABIN DURING SHUTDOWN. REPLACED THE FLAP MOTOR, SYS OPS CHECKED GOOD, NO BURNING ODOR NOTED.SDR ERAA201306250039B-Nut · looseODOR AFTER TAKE-OFF FROM ENVIRONMENTAL SYSTEM. FOUND B-NUT ON FUEL SUPPLY LINE TO FLOW DIVIDER LOOSE ON NR 2 ENGINE. TIGHTENED B-NUT TO FLOW DIVIDER AND SAFTIED IAW MM 73-10-04 PERFORMED HIGH POWER RUNS, LEAK AND OPS CHECK GOOD OK FOR SERVICE.SDR GLBA2013062100263Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE FUSELAGE FRAME FLANGE AT FS 183.25 AND STRINGER 2R, 1.5 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-047.SDR GLBA2013061800262Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE FUSELAGE FRAME ANGLE AT FS 150.00 & STRINGER 6L AT THE UPPER & LOWER A/S DOOR GAS STRUT MOUNT NUTPLATE AREA, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-046.SDR 29GA2013062193652Trim Panel · out of positionCABIN DOOR NOT LOCKING. FOUND TRIM INTERFERING WITH DOOR HANDLE, ADJUSTED TRIM PANEL AS REQUIRED, OPS CHECK GOOD.SDR GLBA2013061400259Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE HORIZONTAL STAB AFT SPAR WEB, .25 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-55-017. MAJOR REPAIR.SDR 29GA2013061895653Bulkhead · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION, DISCOVERED FWD PRESSURE BULKHEAD CRACKED APPROXIMATELY 4.5 INCHES AT RIGHT LOWER PANEL AT TOP OF STIFFENER. STOPPED DRILLED ENDS OF CRACK AT POINT DETERMINED BY EDDY CURRENT AND INSTALLED EXTERNAL DOUBLER REPAISDR 29GA2013061742302Actuator · out of rigNOSE GEAR LIGHT DID NOT ILLUMINATE ON APPROACH, PUMPED GEAR DOWN NOSE WHEEL INDICATION ILLUMINATED AT THAT TIME, SHOWN. RIGGED NOSE GEAR ACTUATOR OPERATIONAL CHECK GOOD.SDR GLBA2013061400260Door Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE CARGO DOOR FRAME IN THE BEND RADIUS AT FS 456.00 AND STRINGER 3L, 3.5" IN LENGTH. REPAIRED IAW EO 13-1900-53-045. MAJOR REPAIR.SDR GLBA2013061300258Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT FWD SPAR CAP ANGLE AT 2D FASTENER HOLE FROM TOP OF ANGLE AT VSS 5.00, 0.375" IN LENGTH. REPAIRED IAW EO 13-1900-55-016. MAJOR REPAIR.SDR GLBA2013061300613Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT FWD SPAR CAP ANGLE AT 2D FASTENER HOLE FROM TOP OF ANGLE AT VSS 5.00, 0.375" IN LENGTH. OPENSDR CA130701001Engine · power loss(CAN) THE PILOT ELECTED TO ABORT THE TAKEOFF DUE TO NP DROPS OFF FROM 1700 TO 1500 RPM.SDR 29GA94627061013AWire Harness · out of positionFLIGHT CONTROLS STICKING. FOUND FLIGHT CONTROL COLUMN CATCHING ON WIRE BUNDLE, REPAIRED DAMAGED EFIS WIRING AND RESECURED WIRING, OPERATED CONTROL WHEEL AND CONTROL COLUMN ENSURED NO INTERFERENCE WITH INSTRUMENT PANEL WIRING.SDR GLBA2013060600257Connector · unsecurePILOT REPORTED THAT THE AFX DISABLE ILLUMINATES WHEN AUTOFEATHER IS ON AND NEITHER ENGINE IS ARMED, TORQUES ARE MATCHED DURING DECENT-APPROACH. MX CLEANED AND RESECURED PCB CONNECTORS.SDR CA130606005Attach Angle · cracked(CAN) FOUND ONE AIRCRAFT WITH A CRACK IN THE H STAB ATTACH ANGLE, THE MAINTENANCE PROGRAM WAS AMENDED TO CARRY OUT A REPEAT OF HBC MSB 55-4114 EVEN THOUGH IT CALLED FOR A ONE TIME ONLY INSPECTION. WHEN CARRYING OUT THE BORESCOPE INSPECTION IT WAS OBSERVED SDR GLBA2013060400256Gearbox · failedDURING CLIMBOUT EXPERIENCED SMOKE IN THE CABIN, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE, FLAPS DID NOT EXTEND, SMOKE DISSAPATED AFTER FIVE MINUTES. R & R FLAP GEAR BOX MOTOR ASSY IAW MM 27-50-03, PN 100-524073-1. SN OFF 6245 ON 979. R & R RT INBD FLSDR CA130614004Engine · making metal(CAN) DURING FLIGHT, THE PILOT REPORTED VIBRATION ON NR 1 ENGINE WITH A RAISE OF TEMPERATURE. THE POWER WAS REDUCED AND SOON AFTER A NOISE WAS HEARD ACCOMPANIED BY RUMBLING. THE ENGINE WAS SHUTDOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. POST FLIGSDR CA140418002Bearing · spalled(CAN) CREW REPORTED THAT DURING FLIGHT, NG STARTED TO DETERIORATE, SLOW UN-COMMANDED DECELERATION, WHILE THE FUEL FLOW (WF) AND TEMPERATURE (ITT) STARTED TO CLIMB. A COMMANDED, IN-FLIGHT SHUTDOWN, WAS PERFORMED AFTER THE ENGINE TEMPERATURE REACHED 1027 DEGREESDR 2013FA0000313Autofeather Sys · inoperativeALL PRE-FLIGHT AND RUN-UP SYSTEM CHECKS HAD BEEN NORMAL, AND ALL SYSTEMS HAD BEEN OPERATING NORMALLY FOR ALL PREVIOUS LEGS OF THE FLIGHT. ON APPROACH REDUCED THE POWER TO APPROX 600 LBS OF TORQUE PER SIDE TO SLOW DOWN TO FOLLOW PRECEDING TRAFFIC. THE AUTOFEASDR EHAA20130530006Switch · looseON APPROACH, REDUCED POWER TO 600LBS., THE NR 2 ENGINE STARTED TO CYCLE IN AND OUT OF AUTOFEATHER AS IT WOULD DO WHEN TESTING THE AUTOFEATHER ON THE GROUND.SDR CA130603008Duct · cracked(CAN) FLIGHT CREW NOTED AIRCRAFT HAD DIFFICULTY REACHING MAX DIFF 4 PRESSURIZATION WAS FLUCTUATING. DURING TROUBLESHOOTING IT WAS NOTICED THAT A BLEED AIR PIPE IN LH WING HAD A LARGE CRACK AROUND THE WELDED - 4 FITTING ALLOWING BLEED AIR TO ESCAPE INTO WING. ESDR GLBA2013052900255Pressure Blkhd · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS IN THE FWD PRESSURE BULKHEAD, RT WEB AT FS 84.00, CRACKS AT THE INBD EDGE OF WEB ATTACHING FASTENERS, 2" IN LENGTH. REPAIRED IAW EO 13-1900-53-044. MAJOR REPAIR.SDR GLBA2013052900254Pressure Blkhd · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 7 CRACKS IN THE FWD PRESSURE BULKHEAD, LT WEB AT FS 84.00, CRACKS AT INBD EDGE OF WEB ATTACHING FASTENERS, 3.5" IN LENGTH. REPAIRED IAW EO 13-1900-53-044. MAJOR REPAIR.SDR 29GA2013061794232Downlock Switch · stickingNOSE GEAR DID NOT INDICATE DOWN AND LOCKED RECYCLED GEAR AND NORMAL DOWN AND LOCKED INDICATION SHOWN. REPLACED AND ADJUSTED NOSE GEAR DOWN LOCK SWITCH OPS CHECK GOOD.SDR GLBA2013052800253Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 IN THE BEND RADIUS, 1" LENGTH. REPAIRED IAW EO 13-1900-53-043. MAJOR REPAIR.SDR GLBA2013052800252Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS AT THE CARGO DOOR FUSELAGE FRAME AT FS 509 BETWEEN STRINGER 4L & 5L, LOCATED IN THE BEND RADIUS OF THE FRAME, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-042. MAJOR REPAIR.SDR 29GA94232052713Downlock Switch · out of adjustFLIGHT: 3561 OLF/BIL NOSE GEAR LIGHT WORKS INTERMITTENTLY. FOUND DOWNLOCK SWITCH OUT OF ADJUSTMENT, ADJUSTED SWITCH OPERATIONAL CHECK GOOD.SDR 2013F00119Downlock Switch · out of adjustNOSE GEAR LIGHT WORKS INTERMITTENTLY. FOUND DOWNLOCK SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH AND OPS CHECK GOOD.SDR ERAA20130038Sealant · defective"CABIN ALT.HIGH" LIGHT ON AT 20,000FT CONTINUED LOSS OF DIFF PRESSURE. AIR LEAK FOUND ALONG LOWER EDGE OF AIRSTAIR DOOR. SEALED ALONG EDGE OF FUSELAGE SKIN AT BOTTOM OF AIRSTAIR DOOR IAW BE1900D MAINTENANCE MANUAL 20-10-00 AND PRESSURE CHECKS GOOD ON GROUND SDR 29GA94752052213Cable · out of positionFLIGHT: 4082 PKB/CLE CABIN DOOR SNUBBER CABLE CAUGHT ON DOOR CAM. FOUND CABLE STUCK ON DOOR STOP, MOVED CABLE FREE OF DOOR STOP, OPERATIONAL CHECK SATISFACTORY.SDR 29GA201306210002Angle · corrodedDURING ROUTINE SCHEDULED MAINTENANCE, DISCOVERED RIGHT ANGLE ON VERTICAL AFT SPAR HAS CORROSION ABOVE AND BELOW UPPER RUDDER HINGE BRACKET. REMOVED CORROSION AND BLENDED AREA ON VERTICAL AFT SPAR RIGHT ANGLE AS REQUIRED AND INSTALLED WEB FLANGE STRAP.SDR EHAA20130521005Switch · looseRIGHT AUTOFEATHER ACTIVATED ON APPROACH WITH NORMAL POWER SETTING.SDR 2013F00123Switch · activatedRIGHT AUTOFEATHER ACTIVATED ON APPROACH WITH NORMAL POWER SETTINGS.SDR 29GA201306210003Angle · corrodedDURING ROUTINE SCHEDULE MAINTENANCE, DISCOVERED CORROSION ON THE VERTICAL STABILIZER AT STATION 70.0 AND 64.0. REMOVED CORROSION AND BLENDED AREA ON VERTICAL AFT SPAR RIGHT ANGLE AS REQUIRED.SDR 29GA201305220002Structure · corrodedDURING ROUTINE SCHEDULED MAINTENANCE, DISCOVERED CORROSION ON VERTICAL STABILIZER STATION 70.0 AND 64.0.SDR GLBA2013052000251Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT LOWER BELLY SKIN OVER THE WING SPAR AT FS 288, 2.25 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-041. MAJOR REPAIR.SDR 29GA94732051913Uplock Switch · inoperativeFLIGHT: 4082 PKB/CLE GEAR UNSAFE LIGHTS REMAINS ILLUMINATED WHEN LANDING GEAR IS RETRACTED, GEAR EXTENDED WITH NORMAL INDICATIONS THREE GREEN NOTED. REPLACED LEFT UPLOCK SWITCH, OPERATIONAL CHECKS GOOD.SDR CA130522002Shutoff Valve · failed(CAN) DURING MAINTENANCE, THE LT ENGINE WAS STARTED FOR A GROUND RUN. THE BLEED AIR FAIL ANNUNCIATOR FAILED TO EXTINGUISH ON BOTH THE LT AND RT SIDES. IT WAS ALSO NOTED THAT THE PNEUMATIC AND VACUUM GUAGES BOTH READ ZERO. SYS WAS TROUBLESHOT. THE LT PNEUMATSDR CA130521021Duct · cracked(CAN) WHILE TROUBLESHOOTING FOR A PNEUMATIC BLEED AIR PROBLEM, NOTED A LT BLEED AIR DUCT ASSY, PN 129-910033-15 CRACKED APPROXIMATELY 75 PERCENT OF THE WAY AROUND THE DUCT JUST AFT OF THE FLANGE THAT ATTACHES THE DUCT TO THE FIREWALL. PART REPLACED WITH NEW. SDR 29GA2013052200093Switch · out of adjustFLIGHT4078, LANDING GEAR WARNING HORN CAME ON WHEN ADVANCING POWER LEVERS THROUGH 500 LBS TORQUE. ADJUSTED LEFT AND RIGHT GEAR WARNING SWITCHES IN PEDESTAL OPS CHECKED GOOD. TEST FLIGHT SATISFACTORY.SDR GLBA2013051600250Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE SPAR CAP, RT VERT STAB, SECOND FASTENER DOWN FROM THE TOP, .375" IN LENGTH. REPAIRED IAW EO 13-1900-55-015. MAJOR REPAIR.SDR GLBA2013051600249Rib · chafedDURING A SCHEDULED ROUTINE INSPECTION FOUND CHAFED AREA ON THE LT RIB 1 AT JUNCTION WITH WING SPAR, FLANGE PORTION OF RIB 1 WORN DOWN TO DOUBLER FLANGE, 1.5"*.75" AREA. REPAIRED IAW EO 13-1900-57-011. MAJOR REPAIR.
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