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 BSAASDR0720Eva Tube · damagedDURING CLIMB TO ALTITUDE, THE RT BLEED AIR FAIL ANNUNCIATOR LIGHT CAME ON AT 12,500FT. CREW FOLLOWED CHECKLIST PROCEDURES, SHUT OFF BLEED ON RIGHT SIDE AND RETURNED TO STATION, LIGHT WENT OUT AT 8,000FT DURING RETURN TO STATION. INITIALLY DEFERRED RT BLEED SSDR BSAASDR0719Tube · splitDURING CLIMB TO ALTITUDE, THE RT BLEED AIR FAIL ANNUNCIATOR LIGHT CAME ON AT 16,800FT. CREW FOLLOWED CHECKLIST PROCEDURES, SHUT OFF BLEED ON RIGHT SIDE AND RETURNED TO STATION, LIGHT WENT OUT AT 7,000FT DURING RETURN TO STATION. INITIALLY DEFERRED THE RT BLESDR GUUA06027001Switch · failedON APPROACH LANDING GEAR SELECTED DOWN GEAR HORN CANNOT BE SILENCED. CLEANED LANDING GEAR SILENCE BUTTON. OPS CHECK SATISFACTORY.SDR NSVA20070148Spring · brokenBOTH THROTTLE LEVERS ARE LOOSE. REMOVED LT AND RT POWER LEVERS IAW BEECH 1900D MM 76-10-00, FOUND RT AND LT POWER LEVER ARM ASSY WORN AND GUILD PINS WORN IN POWER LEVERS. P.O.O. AND ONE RETURN SPRING BROKEN. INSTALLED NEW RT AND LT POWER LEVERS IAW BEECH 19SDR GUUA95253053107APressure Panel · crackedDURING INSP DISCOVERED CRACKED CEILING IN NOSE WHEEL WELL AT FS 89 WL 100.00 AT CENTER BUTT LINE. REMOVED DAMAGED AREA AND INSTALLED SHIM AND EXTERNAL REINFORCEMENT DOUBLER REPAIR.SDR BSAASDR0717Tube · damagedTHE RIGHT BLEED AIR FAIL LIGHT CAME ON. CREW WAS CLOSEST TO DESTINATION, AND LANDED WITHOUT INCIDENT. FOUND & REPLACED DAMAGED EVA TUBING UNDER RT WING PANEL 611 NEAR NACELLE. SYSTEM OPS CHECK & LEAK CHECK GOOD.SDR NSVA20070145Warning Light · unknownNO PUSH TO EXTINGUISH LIGHT DURING AMP TEST ON RIGHT SIDE. REMOVED AND REPLACED RIGHT ENG. FIRE BOTTLE AND SQUIB ASSY. REMOVED AND REPLACED RIGHT FIRE "T" HANDLE ASSY. OPS CHECK GOOD IAW COLGAN WORK CARD NR 26-20-05 AND MM CH 26-00-00.SDR BSAASDR0716Diode · intermittentTHE LANDING GEAR CONTROL CIRCUIT BREAKER TRIPPED WHEN GEAR DOWN WAS SELECTED. CREW EXTENDED GEAR BY MANUALLY PUMPING GEAR DOWN. REPLACED DIODES FOR THE LANDING GEAR SELECT SOLENOID, MULTIPLE GEAR SWINGS AND OPERATIONAL CHECK FLIGHT WERE BOTH GOOD.SDR GUUA05300702Wire · chafedFLIGHT: 9216 PNS/TPA - DURING APPROACH, WHEN LANDING GEAR SELECTED DOWN GEAR EXTENDED NORMALLY, BUT NO 3 GREEN LIGHTS. FOUND CIRCUIT BREAKER FOR GEAR INDICATION POPPED. RESET CIRCUIT BREAKER GREEN LIGHTS ILLUMINATED. REPAIRED CHAFED WIRES G25A22, D40A22, D3SDR GUUA05300701Relay · shortedFLIGHT: 9151 PNS/TPA DURING APPROACH LANDING GEAR WARNING HORN SILENCE BUTTON CAUSES GEAR WARNING LIGHTS TO EXTINGUISH. REPLACED NUMBER 8 RELAY CARD MODULE. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK NORMAL.SDR GUUA95253052907ABulkhead · crackedDURING INSP DISCOVERED RT FWD PRESSURE BULKHEAD CRACKED 2.5 INCHES HORIZONTALLY AND 1.0 INCH VERTICALLY AT STA 89.00. STOP DRILLED CRACKS AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR GUUA05280701Elevator · stuckELEVATOR CONTROL STUCK ON APPROACH / BINDING --- ACCESSED & INSPECTED BELLCRANKS, PULLEYS, PULLET GUIDES, CABLE RUNS, CABLE PASS THROUGHS. NO DEFECTS NOTED. ELEVATORS HAVE FREE UNOBSTRUCTED TRAVELS. TEST FLIGHT SATISFACTORY.SDR GUUA05280702Control Quadrant · stuckELEVATOR CONTROL STUCK ON APPROACH / BINDING, ACCESSED AND INSPECTED BELLCRANKS, PULLEYS, PULLET GUIDES, CABLE RUNS, CABLE PASS THROUGH. NO DEFECTS NOTED. ELEVATORS HAVE FREE UNOBSTRUCTED TRAVELS. TEST FLIGHT SATISFACTORY.SDR NSVA20070140Fitting · looseRT ENG OIL PRESS FLUCTUATED BETWEEN 65-70 THEN DROPPED BELOW 60 PSI WITH LOW OIL PRESS LIGHT ILLUMINATED. INFLIGHT SHUTDOWN. TIGHTENED OIL COOLER RETURN LINE FITTING IAW BE1900 MM 71-00-00, GROUND RAN AIRCRAFT 20 MIN IAW CRUISE CONFIGURATION, ALL ENGINE PARSDR GUUA05270701Oil System · low pressureFLIGHT: 9297 EYW/FLL DURING FINAL INTO FLL, THE NR 2 ENGINE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED. SECURED THE NR 2 ENGINE. CONTINUED TO FLL LANDED WITHOUT INCIDENT. SERVICED NR 2 ENGINE OIL SYSTEM. REMOVED NR 2 ENGINE STARTER GENERATOR INSPECTED AREA FSDR AMWA84889BCPower Unit · wornAFTER TAKEOFF, BATTERY CHARGE ANNUN ILLUM. AC CONTINUED TO LIT AND LANDED WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUN ILLUM IS CONSIDERED A NUISANCE WRITEUP AND A DISTRACTION TO THE PILOT. REMOVED AND REPLACED DC POWER PANEL.SDR GUUA05250701Actuator · bypassingFLIGHT: 9173 EYW/FLL AFTER TAKEOFF LANDING GEAR CIRCIUT BREAKER POPPED WHEN LANDING GEAR HANDLE WAS SELECTED TO THE UP POSITION. RAN ORH RESET CIRCUIT BREAKER. REPLACED THE RIGHT MAIN LANDING GEAR ACTUATOR. OPERATIONAL CHECK NORMAL.SDR NSVA20070139Switch · out of adjustMAIN CABIN DOOR LIGHT ILLUMINATED ON PUSHBACK. ADJUSTED AIRSTAIR DOOR LATCH PRESSURE LOCK SWITCH IAW BMM 52-70-02. OPERATIONAL CHECK SAT.
SDR NSVA20070137Fuel Control · malfunctionedABORTED TAKEOFF DUE TO POWER LOSS ON LT ENG. AT APPROX 40 KNOTS, LT ENG APPEARED TO ROLLBACK TO IDLE. INSPECTED NR 1 ENGINE FUEL CONTROL LINKAGES, GROUND RAN AIRCRAFT IAW PW MM 71-00-00, COULD NOT DUPLICATE DISCREPANCY, OPS CHECK GOOD AT THIS TIME.SDR NSVA20070133Flap System · malfunctionedFLAPS WOULD NOT RETRACT AFTER LANDING. MAINTENANCE RETURNED FLAPS TO FULL UP POSITION AND OPENED MEL.SDR BSAASDR0715Warning System · malfunctionedON DESCENT THE RT BLEED FAIL ANNUNCIATOR ILLUMINATED. THE CREW LANDED WITH NO FURTHER INCIDENT. EXTENSIVE TROUBLESHOOTING WAS COMPLETED WITH NO DEFECTS FOUND & MULTIPLE GROUND RUNS WERE COMPLETED, BUT COULD NOT DUPLICATE THE PROBLEM.SDR GUUA05200702Switch · out of adjustFLIGHT: 9267 EYW/MIA DURING APPROACH LANDING GEAR HORN AND LIGHT ANNUNCIATED AT ABOUT 75 PERCENT N1 OR ABOUT 500LBS OF TORQUE. SYSTEM WORKS BUT AT A LOWER VALUE THAN NORMAL. ADJUSTED PEDESTAL SWITCHES OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.SDR GUUA05200701Wire Harness · damagedFLIGHT: 9300 FPO/FLL DURING APPROACH, LANDING GEAR DOWN NO NOSE GEAR LIGHT INDICATION. CONTINUED TO FLL LANDED WITHOUT INCIDENT. FOUND BAD WIRE ON NOSE DOWNLOCK HARNESS REPLACED NOSE GEAR DOWNLOCK SWITCH AND HARNESS ASSEMBLY. OPERATIONAL CHECK NORMAL.SDR AMWA84785BCBattery · weakDURING FLT, THE BATTERY CHARGE ANNUN ILLUMINATED. ACFT LANDED WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUN WRITEUP IS A NUISANCE A SEVERE DISTRACTION TO THE PILOTS. REMOVED AND REPLACED BATTERY.SDR CA070523002Blower · seized(CAN) WHILE ENROUTE, THE AC CABIN AND COCKPIT FILLED UP WITH SMOKE FROM WHAT SMELLED ELECTRICAL IN NATURE. OXYGEN WAS USED AND THE AC FINISHED ITS TRIP AND LANDED (DESTINATION WAS CLOSER THAN TO TURN AROUND). MAINT WAS CALLED AND AN AC WAS DISPATCHED TO CONTINSDR GUUA05180702Skin · corrodedAT SCHEDULED INSPECTION DISCOVERED BELLY SKIN CORROSION AT FS 250.00 AT STRINGER 14L. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 51-70-06.SDR GUUA05180701Connector · looseFLIGHT:9167 PBI/TLH - AFTER TAKEOFF LANDING GEAR DID NOT RETRACT. RETURNED TO PBI, SELECTED GEAR DOWN LEFT MAIN GEAR WOULD NOT GIVE A SAFE DOWN LOCKED INDICATION. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. RESECURED MAIN LANDING GEAR LEFT ANDSDR BSAASDR0714Fire Loop · false indicationRIGHT FIRE LOOP ANNUNCIATOR ILLUMINATED WHEN VECTORED TO FINAL (DESCENT) INTO BOSTON. CREW LANDED WITHOUT INCIDENT. THE RIGHT FORWARD ENGINE FIRE LOOP WAS REMOVED AND REPLACED, AND AN OPERATIONAL CHECK ON THE SYSTEM WAS PERFORMED.SDR CA070515008Governor · out of rig(CAN) ON NUMEROUS LANDINGS THE AC YAWED HARD TO THE LT. AFTER RIGGING THE SNAG WOULD GO AWAY FOR NUMEROUS LANDINGS THEN YAW AGAIN TO THE LT. MAINT REPLACED THE LT PROP GOVERNOR AND RETURNED THE ACFT TO SERVICE. TO DATE THE SNAG HAS NOT RE-OCCURED. (TC NR 20070SDR NSVA20070129Fire Loop · defectiveT-HANDLE AND FIRE EXTINGUISHER DISCHARGE LIGHTS DO NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED LT ENG AFT FIRE LOOP, OPS CK GOOD IAW 26-10-01 P/N 244-09015 S/N 034119.
SDR GUUA05150701Bushing · frozenAT SCHEDULED FLEET CAMPAIGN INSPECTION: LEFT EMERGENCY EXIT DOOR INTERNAL BEARING BUSHING AT HANDLE FROZEN. REPLACED BUSHING.SDR GUUA05170701Bolt · crackedAT SCHEDULED INSPECTION DISCOVERED LEFT MAIN LANDING GEAR UPPER DRAG BRACE BOLT TO BE CRACKED IN TWO. CHECKED RIGHT DRAG BRACE UPPER BOLT AND DETERMINED IT ALSO TO BE CRACKED. REPLACED LEFT AND RIGHT DRAG BRACE ASSEMBLIES UPPER BOLTS.SDR BSAASDR0713Wire Harness · groundedDURING DESCENT MASTER CAUTION AND LEFT FIRE WALL FUEL VALVE LIGHT FLICKERED. CREW LANDED WITHOUT INCIDENT. AFTER LANDING LEFT FIRE LOOP WOULD NOT TEST. FOUND FIRE LOOP GROUNDING AT THE FIREWALL WIRE HARNESS FEED THRU. WIRE HARNESS FEED THRU WAS ADJUSTED TOSDR GUUA05140701Unknown · odorFLIGHT: 9133 JAX/TPA - AFTER TAKEOFF WITH BOTH BLEED AIR VALVES OPEN AND HEAT APPPLIED IN THE MANUAL MODE BURNED ODOR PERSISTS. ODOR WENT AWAY WHEN BLEED AIR VALVES WERE CLOSED. RAN ENGINES WITH BLEED VALVES OPEN FOR SEVERAL MINUTES COULD NOT DUPLICATE PROBLSDR GUUA05130701Annunciator · malfunctionedFLIGHT: 9232 TPA/EYW - DURING APPROACH, TWO ATTEMPTS TO GET THE NOSE GEAR DOWN AND LOCKED ON SECOND ATTEMPT IT TOOK TWO MINUTES TO LOCK. REPLACED NOSE GEAR ANNUNCIATOR ASSEMBLY. OPERATIONAL CHECK NORMAL.SDR GLBA20060946Wire · damagedABORTED TAKEOFF, DURING TAKEOFF ROLL PILOTS REPORTED THAT A LT DC GENERATOR ANNUNCIATOR ILLUMINATED. MAINTENANCE REPAIRED A WIRE AT THE LT STARTER GENERATOR. REFERENCE MFG 1900D 24-00-00. OPERATIONAL CHECK OF THE SYSTEM WAS GOOD.SDR BSAASDR0712Switch · inoperativeDURING APPROACH WHEN CREW SELECTED GEAR DOWN THE LANDING GEAR RELAY CONTROL CB TRIPPED WHEN THE GEAR WAS HALFWAY DOWN. CREW ABORTED THE APPROACH AND MANUALLY EXTENDED THE GEAR. CREW LANDED WITH NO FURTHER INCIDENT. ALL WIRING & COMPONENTS IN THE LANDING GEASDR GUUA05110702Uplock Switch · failedDURING APPROACH LANDING GEAR WOULD NOT EXTEND NORMALLY. MANUAL EXTENSION GOT SAFE FOR LT AND RT MAINS. LANDED WITHOUT A LOCKED NOSE GEAR. SHUTDOWN RT ENGINE AT 1,000 FEET AND LT ENGINE PRIOR TO TOUCHDOWN. REPLACED LT MAIN LANDING GEAR UP LOCK SWITCH AND SERVISDR AMWA84592Brake · bindingDURING ROLLING TAKEOFF, CAPT HAD EXCESSIVE BRAKE DRAG AND ABORTED TAKEOFF. RETURNED TO GATE W/O FURTHER INCIDENT. ADJUSTED PARKING BRAKE HANDLE AND VALVES.SDR GUUA05110701Control Handle · failedFLIGHT: 9181 PNS/FLL - DURING APPROACH, NOSE GEAR WOULD NOT EXTEND AND CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER NOSE GEAR EXTENDED BUT CIRCUIT BREAKER POPPED AGAIN. REPLACED LANDING GEAR CONTROL HANDLE. OPERATIONAL CHECK NORMAL.SDR BSAASDR0711Landing Gear · failedDURING APPROACH, WHEN CREW SELECTED GEAR DOWN, THE LANDING GEAR CONTROL RELAY CIRCUIT BREAKER TRIPPED HALFWAY THROUGH THE GEAR EXTENSION. CREW ABORTED LANDING, PERFORMED MANUAL EXTENSION AND LANDED WITH NO FURTHER INCIDENT. THE GEAR CB WAS RESET, AND THE GEASDR GUUA05100702Coupling · dirtyEMERGENCY EXIT 6A INOPERATIVE, UNABLE TO OPEN. CLEANED AND LUBRICATED COUPLING ATTACHED TO EXTERIOR HANDLE.SDR GUUA05100701Unknown · unknownFLIGHT: 9257 EYW/FLL - DURING FLIGHT, LANDING GEAR ANNUNCIATOR CIRCUIT BREAKER POPPED THEN AGAIN WHEN LANDING GEAR EXTENDED. CHECKED WIRES FOR CHAFING, NO DEFECTS NOTED. OPERATIONAL CHECK NORMAL.SDR AMWA06033FStiffener · corrodedBIO CORROSION DAMAGE IN LT MAIN TANK NACELLE. RIB REPAIR WS 124. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-3SDR AMWA06033EFrame · chafedAT MULTIPLE FUSELAGE STATIONS FRICTION CHAFING HAS OCCURED, THE DEPTH OF THE CHAFFING RANGES FROM .019 TO .030. REPAIRED IAW ENGINEERING AUTHENTICATION REPAIR DRAWING 1900D142-6 REVASDR AMWA06033DSkin · chafedFRICTION CHAFFING OCCURED DURING ENGINE OPERATION RESULTING IN WORN SEGMENTS ON THE LT ENGINE UPPER AFT NACELLE ALONG ENTIRE LENGHT & SHAPE OF NACELLE. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-1 REV 1R.SDR AMWA06033CSkin · chafedFRICTION CHAFFING OCCURED DURING ENGINE OPERATION RESULTING IN WORN SEGMENTS ON THE RT ENGINE UPPER AFT NACELLE ALONG ENTIRE LENGTH & SHAPE OF NACELLE. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-1 REV 1R.SDR AMWA06033BSpar Cap · corrodedBIO - CORROSION DAMAGE RT LOWER SPAR CAP AT WS 124. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-7 REV 1R.SDR AMWA06033ASpar Cap · corrodedBIO - CORROSION RT LOWER SPAR CAP AT WS 124. REPAIRED IAW ENGINEERING AUTHORIZATION REPAIR DWG 1900D142-7 REV 1R.SDR AMWA84517Annunciator · wornUPON DEPART GEAR RETRACTED NORMALLY. NO PROBLEMS UNTIL GEAR EXTENSION. COULD NOT DETERMINE IF GEAR WAS COMPLETELY DOWN. FLEW BY TOWER AND THEY SAID IT APPEARED ONE OF THE GEAR WAS NOT COMPLETELY DOWN. PERFORMED MANUAL EXTENSION, BURNED OFF ADDITIONAL FUEL
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