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 = '1900C' 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 = '1900C' 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 20010507CW019Stringer · corrodedINSPECTION REVEALED A .6 INCH SECTION OF FUSELAGE STRINGER 14L CORRODED AT APPROX F.S. 250 FUSELAGE SKIN WAS NOT DAMAGED.SDR 20010507CW016Door Frame · crackedDURING INSPECTION A CRACK WAS FOUND IN THE AIR-STAIR DOOR FRAME LOWER AFT AREA. CRACK ORIGINATED AT THE HING PIN RETAINER SCREWHOLE AND EXTENDED FORWARD APPROX. 10 INCHES THRU THE HINGE UPPER RIVET ROW. AFTER REMOVING THE HINGE, THE SKIN WAS FOUND CRACKED ALSDR 20010507CW015Bracket · corrodedINSPECTION DISCOVERED SIGNIFICANT CORROSION ON 2 RT ELEVATOR HINGE BRACKETS.SDR 20010507CW014Bracket · corrodedINSPECTION DISCOVERED SIGNIFICANT CORROSION ON 2 RT ELEVATOR HINGE BRACKETS.SDR 20010507CW008Floor Support · corroded4 FLOOR SUPPORT BRACKETS WERE FOUND WITH SIGNIFICANT CORROSION ON THE TOP SURFACE WHERE THEY ARE IN CONTACT WITH THE HONEYCOMB FLOOR PANEL.SDR 20010507CW007Floor Support · corroded4 FLOOR SUPPORT BRACKETS WERE FOUND WITH SIGNIFICANT CORROSION ON THE TOP SURFACE WHERE THEY ARE IN CONTACT WITH THE HONEYCOMB FLOOR PANEL.SDR 20010507CW006Bracket · wornINSPECTION FOUND ALL FLAP TRACK BRACKETS WORN BEYOND ACCEPTABLE LIMITS.SDR 20010507CW005Bracket · wornINSPECTION FOUND ALL FLAP TRACK BRACKETS WORN BEYOND ACCEPTABLE LIMITS.SDR CA010405005Hose · blown(CAN) PILOT REPORTED LT BRAKE DEICE FAIL LIGHT CAME ON IN FLIGHT. DEICE SYSTEM WAS TURNED OFF AND AIRCRAFT CONTINUED TO DESTINATION. UPON MAINTENANCE INVESTIGATION, THE FLEXIBLE BLEED AIR HOSE ASSY CARRYING HOT AIR TO BRAKE ASSY WAS FOUND BLOWN. THE LINE WAS RSDR 20010425CW015Oil Cooler · crackedFLIGHT CREW PERFORMED IN-FLIGHT SHUTDOWN OF THE NR 2 ENGINE ONE HALF HOUR PRIOR TO REACHING THE DESTINATION AIRPORT, DUE TO LOW ENGINE OIL PRESSURE INDICATION. UNEVENTFUL LANDING. A SUSPECTED OIL LEAK WAS REPAIRED AND THE AIRCRAFT DEPARTED AND AGAIN THE NR 2SDR 20010425AP004Blower · odorFLT 9323 - TPA-RSW - DURING FLIGHT, UNKNOWN SMELL IN THE COCKPIT. REMOVED AND REPLACED CONDENSOR BLOWER. (M)SDR 20010410AP029Blower · failedFLT 9323 - TPA/RSW - DURING FLIGHT, UNKNOWN ODOR IN THE COCKPIT. REMOVED AND REPLACED CONDENSER BLOWER. (M)SDR 20010410AP028Fire Loop · inoperativeFLT 9137 - FLL - AFTER TAKEOFF, LEFT ENGINE FIREWALL FUEL VALVE ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED FORWARD LEFT ENGINE FIRE LOOP. OPERATIONAL CHECK NORMAL. (M)SDR GLBA2001038Elevator · flutterPILOT REPORTED ELEVATOR FLUTTER ON DESCENT AND CLIMB. INSPECTED FLIGHT CONTROLS, PERFORMED TEST FLIGHT. COULD NOT DUPLICATE, OPS CHECKED GOOD. RETURNED TO SERVICE.SDR 20010315CW001Hinge Bracket · corrodedUPON INSPECTION OF RIGHT HAND OUTBOARD HORIZONTAL STABILATOR ELEVATOR HINGE BRACKET A BADLY EXFOLIATED BRACKET WAS FOUND. A FLEET INSPECTION REVEALED 4 OUT OF 5 AIRCRAFT HAD THE CORRODED BRACKET THAT NEEDED REPLACED.SDR 20010509CW007Hinge Bracket · corrodedUPON INSPECTION OF RIGHT HAND OUTBOARD HORIZONTAL STABILATOR ELEVATOR HINGE BRACKET, A BADLY EXFOLIATED BRACKET WAS FOUND.SDR 20010216SG006Squat Switch · out of adjFLT 9195 - FLL - ABORTED DEPARTURE DUE TO STALL AURAL WARNING SOUNDED CONTINUOUSLY DURING TAKEOFF ROLL ABOUT 90 KIAS. ADJUSTED LEFT SQUAT SWITCH. AIRCRAFT TEST FLIGHT SATISFACTORY. (M)SDR GLBA2001011Cowling · separatedRETURN TO BLOCK, RIGHT SIDE UPPER COWLING DERARTED FROM NACELLE ON T/O. INSPECTED COWLING FOR DAMAGE, RE-INSTALLED COWLING. RETURNED TO SERVICE.SDR 20010213CW013Engine · failedDURING TAKE OFF FROM ISP, PILOTS REPORTED HEARING A BANG AND OBSERVED SPARKS COMING FROM THE RIGHT ENGINE EXHAUST DUCT. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO GATE WITH NO FURTHER EVENT. PILOTS PERFORMED WALK AROUND INSPECTION AND DISCOVERED DENTS ANSDR 20010425CW012Engine · failedON RETURN LEG OF ROUND TRIP, PILOT NOTICED AN ORANGE FLASH FRO THE RIGHT HAND ENGINE. ENGINE ITT STARTED RISING AND THE POWER STARTED RISING AND THE POWER STARTED SURGING. THE ENGINE WAS SECURED AND FEATHERED 45 MINUTES OUT. MADE UNEVENTFUL LANDING. NO DETSDR 20010424CW005Nut · frettedDURING FLIGHT AT CRUISE, LOW FUEL PRESSURE AND LOW OIL PRESSURE WARNING LIGHTS CONFIRMED LOW OIL PRESSURE ON GAGE. OIL WAS NOTED COMING OUT OF EXHAUST. CREW SHUT DOWN ENGINE. DURING TEARDOWN, ACCESSORY GEARBOX COUPLING WAS FOUND SHEARED, SUGGESTED COUPLINGSDR 20010216SG005Bolt · looseFLT 9391 - EYW - DURING TAKEOFF, RIGHT FIREWALL FUEL VALVE T-HANDLE ILLUMINATED. ALL ENGINE INSTRUMENTS INDICATED NORMAL. TIGHTENED BOLT ON RIGHT EXHAUST FLEX HOSE FLANGE. ENGINE RUN CHECK NORMAL. (M)SDR 20010215CW005Door · crackedBOTTOM OF DOOR .5 INCH FROM HINGE ATTACH POINT 3.5IN CRACK.SDR 20010425CW013Fire Loop · chafedWITHIN MINUTES OF DEPARTURE, RIGHT ENGINE FIRE WARNING LIGHT CAME ON. PILOT REPORTED NO FLAMES, DID NOT USE EXTINGUISHER. SHUT DOWN RIGHT ENGINE. NO ABNORMAL ENGINE INSTRUMENTS. AIRCRAFT LAND OVER MAXIMUM LANDING WEIGHT. MAINTENANCE FOUND HEAVY CHAFED SPOSDR 20010216SG003Check Valve · malfunctionedFLT - 9195 - FPO-FLL, DURING DESCENT WITH POWER REDUCED BELOW APPROX 1000 LB TORQUE, STRONG FUEL SMELL ON FLIGHT DECK AND AT SEATS 1 AND 2. REMOVED AND REPLACED FUEL PURGE VALVES ON LEFT AND RIGHT ENGINES. (M)SDR 20010216SG002Engine · contaminatedFLT 9311 - MCO-FLL - DURING DESCENT, WHEN BRINGING TORQUE BELOW 1000 LB, FUEL SMELL ON FLIGHT DECK. CLEANED ENGINES. RAN AIRCRAFT ON GROUND WITH BLEEDS ON AND OFF. NO FUEL SMELL NOTED AT THIS TIME. (M)SDR 20010216SG004Unknown · odorFLT 9311 - MCO-FLL - DURING DESCENT, STRONG ODOR OF FUEL WHEN POWER REDUCED APPROXIMATELY 1000 LBS. INSPECTED AIRCRAFT AND PERFORMED GROUND RUN. NO DEFECTS NOTED. (M)SDR 20010208CW016Blower · shortedDURING CRUISE, SMELLED EXTREMELY STRONG ELECTRICAL ODOR. SMELL DISAPPEARED AFTER ONE MINUTE. REMOVED AND REPLACED AFT CABIN BLOWER ASSEMBLY. OPERATIONAL CHECK NORMAL.SDR GLBA9190Fuel Cap · leakingRETURN TO BLOCK - LEFT MAIN FUEL CAP LEAKING, REMOVED AND REINSTALLED FUEL CAP OPS CHECKED GOODSDR CA010206006Actuator · shorted(CAN) LANDING GEAR WOULD NOT RETRACT - POPPED CIRCUIT BREAKER - MOTOR FOUND SHORTED AND BURNT INTERNALLY.SDR 20010208CW015Wire · shortedSMOKE IN COCKPIT ORIGINATED NEAR CAPTAINS YOKE LIGHT SWITCH PANEL. TURNED BATTERY SWITCH OFF. SMOKE DISSIPATED. INSPECTED AREA BEHIND CAPTAINS YOKE. FOUND LOOSE WIRE BEHIND EDGE PANEL. SECURED WIRE. PERFORMED OPERATION OF YOKE LIGHT SWITCH. NO DEFECTS NSDR 20010123CW007Hinge · corrodedDURING SCHEDULED MAINTENANCE, LT HAND OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LT ELEVATOR OUTBOARD HINGE.SDR 20010123CW006Hinge · corrodedDURING SCHEDULED MAINTENANCE, RT HAND OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE.SDR 20010125SG006Control Cable · damagedFLT 9156 - FLL - SHORTLY AFTER TAKEOFF FROM FLL, THE LEFT PROPELLER BEGAN TO RETARD TOWARD FEATHER. AFTER APPROXIMATELY THIRTY SECONDS, PROPELLER WAS SPINNING IN FEATHER. REMOVED AND REPLACED LEFT ENGINE PROPELLER REVERSING LINKAGE PUSHPULL CONTROL CABLE. GSDR 20010215CW008Shutoff Valve · failedWHILE TROUBLE SHOOTING LEFT FIREWALL FUEL SHUT OFF VALVE TROUBLE, FOUND WIRE CORR. AT CONNECTOR A124P1 SOCKET NR1. THIS IS THE POWER WIRE TO THE SWITCH AT THE T HANDLE, REPAIRED WIRE AT SOCKET BY REPLACEMENT OF SOCKET. NOTE: THE SHUT OFF VALVE GETS POWER FRSDR 20010123CW005Bearing · failedDURING TAKEOFF ROLL, NR 4 WHEEL ASSEMBLY AND TIRE LOST DUE TO APPARENT BEARING FAILURE. PILOT REPORTED SLIGHT VIBRATION DURING TAKEOFF. APPLICABLE HARDWARE FOUND IN PLACE DURING AIRCRAFT INSPECTION. ALL OTHER WHEELS INSPECTED AND NO DAMAGE FOUND.SDR 20010112SG041Altimeter · malfunctionedCAPTAINS ALTIMETER STUCK AT 10,200 FEET, AIR TURN BACK. CAPTAINS ALTIMETER REMOVED AND REPLACED. SYSTEM TESTED OK. (M)SDR 20010112SG038Altimeter · failedCAPTAINS ALTIMETER FLAGGED AND ALTITUDE ALERTER FAILED AFTER TAKEOFF. RETURNED TO AIRPORT. CAPTAINS. CAPTAINS ALTIMETER WAS REMOVED AND REPLACED. TESTED OK. (M)SDR SJ3RR003569Blade · misoverhauledTHE OVERHAUL PERFORMED ON THIS BLADE WAS NOT TO HARTZEL SPECIFICATION, AND AS A RESULT, THE BLADE HAD SOME SIGNIFICANT PROBLEMS THAT COULD HAVE RESULTED IN SAFETY OF FLIGHT ISSUES. UNABLE TO DETERMINE WHERE THE OVERHAUL WAS PERFORMED. PLEASE REFERENCE HARTZESDR 20001219SH003Starter Gen · malfunctionedNR 1 GENERATOR DROPPED OFF-LINE. WOULD NOT RESET. ITT BEGAN TO RISE. POWER REDUCED, BUT WOULD NOT LOWER ITT. THEN FIRE HANDLE LIGHT ACTIVATED. SHUT DOWN ENGINE. TEAR DOWN WITH MFG''''S PMI PRESENT. MASSIVE FAILURE OF ARMATURE WINDINGS. STATOR GOUGED BYSDR 20010503CW001Spar Cap · corrodedFOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR. CORROSION WAS FOUND ON THE FORWARD FACE OF THE SPAR CAP AND WAS DISTRIBUTED ACROSS THE SPAR CAP. RECOMMEND THAT IMPROVED PAINT BE APPLIED TO THSDR 20001109SH019Bulkhead · crackedUPON INSPECTION OF THE INTERIOR SIDE WALL, A CRACK WAS FOUND. THE CRACK WAS LOCATED ON BULKHEAD 273 AT THE BEND ON THE BULKHEAD. THE CRACK WAS APPROXIMATELY ONE INCH IN LENGTH. REFER TO THE ATTACHED PICTURE. (X)SDR 20010112SG005Blower · inoperativeFLT 9399 - NAS/MIA - AFTER TAKEOFF, MOMENTARY BURNING SMELL AFTER BLEEDS ARE OPENED. REMOVED AND REPLACED AFT CABIN BLOWER. OPERATIONAL CHECK NORMAL. (M)SDR 20010112SG006Starter Gen · shortedFLT 9233 - FPO/FLL - AFTER TAKEOFF, LEFT DC GENERATOR LIGHT ILLUMINATED AND WOULD NOT RESET. LOST ELECTRICAL POWER TO NR 2 NAV, ADF, AND COMM HAD TO MANUALLY PUMP LANDING GEAR DOWN. REMOVED AND REPLACED LEFT DC STARTER GENERATOR AND RIGHT DC POWER PANEL 250 SDR NSVA20004Latch Handle · out of adjWHILE IN BOS PRIOR TO BOARDING PASSENGERS, THE CAPTAIN REPORTED TO DISPATCH THAT THE AIRSTAIR DOOR HANDLE APPEARED TO BE STIFF AND THOUGHT THAT A PASSENGER MAY HAVE TROUBLE OPENING THE DOOR IF NEED BE. MAINTENANCE INSTRUCTED THE CREW TO FLY THE AIRCRAFT TO HYSDR 20010601CW002Windshield · crackedWINDSHIELD CRACKED A FL20. THE FLIGHT CREW CANCELED THE INTENDED FLIGHT AND RETURNED TO ANCHORAGE, WITHOUT FURTHER PROBLEMS.SDR 20001229AP009Gyro · precessesNR 2 DIRECTIONAL GYRO PRECESSING CONSTANTLY. REMOVED AND REPLACED NR 2 DIRECTINAL GYRO. (M)SDR 20010601CW006Switch · disconnectedWHILE PERFORMING ENGINE FIRE EXTINGUISHER SYSTEM TEST IAW B1900C MM CAMP NR2 INSPECTION TEMP REVISION 26-1, FOUND NR 1 AND NR 2 ENGINE SQUIB POWER SWITCH DISCONNECTED FROM ANNUNCIATOR/ ACTUATOR ASSEMBLY. THIS A RECURRENT PROBLEM WITH THIS STYLE SWITCH ASSEMBLSDR 20001228AP001Fire Loop · shortedFLT 9141 - TPA-RSW - DURING FLIGHT, LEFT ENGINE FIRE INDICATION OCCURRED. PRECAUTIONARY SHUTDOWN AND DISCHARGE OF ENGINE FIRE BOTTLE CARRIED OUT. REMOVED AND REPLACED LEFT ENGINE FORWARD FIRE LOOP DUE TO SHORT. REPLACED LEFT ENGINE FIRE BOTTLE. (M)SDR NSVA20003Cable · brokenIN ACK AIRCRAFT WAS BOARDED BY CREW AND PASSENGERS. WHEN CREW CLOSED AIRSTAIR DOOR THEY NOTICED AN IRREGULARITY WITH THE HANDLE. CREW THEN TRIED TO OPEN DOOR AND IT WOULD NOT OPEN. OPENING THE DOOR FROM THE OUTSIDE WAS ATTEMPTED WITHOUT SUCCESS. PASSENGERS
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