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 TIMA20260425001Blower Motor · inoperativeWAS IN CRUISE FROM MKG TO IND FOR ABOUT 5 MINUTES. BEGAN TO SMELL ODOR. GOT SLIGHTLY STRONGER WITHIN ABOUT 2 MINUTES. CHOSE TO DIVERT TO SBN. ON APPROACH/FINAL RADIOS CUT IN AND OUT.SDR TIMA20250603003Engine · power lossAFTER LEVELING OFF AT 14000' LEFT FUEL PRESSURE ANNUNCIATION CAME ON, STNADBY PUMP TURNED ON, FUEL PRESSURE ANNUMC REMAINED ON, FLOW DROPPED, ENGINE ROLLED BACK. PUSHED PROPS/POWER UP, LEFT ENGINE REMINED ROLLED BACK (11%) N1. SHUTDOWN ENGINE CUTOFF, FEATHEREDSDR TIMA20250215002Unknown · odorWHILE IN CRUISE FLIGHT AT 10,000FT PILOT BEGAN TO SMELL SOMETHING SUSPICIOUS. MOMENTS LATER THE PILOT EXPERIENCED A LEFT AC BUS FAILURE AND BEGAN TO SEE SMOKE COMING FROM UNDERNEATH THE CO-PILOTS SIDE OF THE AVIONICS PANEL. IMMEDIATELY PROCEEDED WITH THE MEMOSDR FXTA20231124001Relay · failedBATT TIE OPEN ANNUNCIATOR ILLUMINATED DURING FLIGHT.SDR TIMA20240724009Landing Gear · faultedDURING FLINAL APPROACH, ALL THREE BUSS TIE ANNUCIATOR LIGHTS ILLUMINATED INDICATING A FAILURE OF THE CENTER BUS. I VERIFIED THE STATUS OF THE ELECTRICAL SYSTEM AND CONFIRMED NO VOLTAGE ON THE CENTER BUS. I REFERRED TO THE QRH DUE TO THE LOSS OF THE CENTER BUSSSDR TIMA20240705007Engine · low torqueAFTER DESCENDING AND LEVELING OFF LEFT ENGINE TORQUE NOT RISING PROPERLY AND INCORRECT ENGINE CONTROL / FEEL, PILOT NOTICED IMPROPER POWER OUT OF LEFT ENGINE AND DECLARED EMERGENCY DUE TO PARITIAL POWER ON LEFT ENGINE. PILOT WAS CLEARD TO LAND. LANDED SAFELY ASDR TIMA2024071105007Engine · power lossAFTER DESCENDING AND LEVELING OFF LEFT ENGINE TORQUE NOT RISISNG PROPERLY AND INCORRECT ENGINE CONTROL/FEEL, PILOT NOTICED IMPROPER PWOER OUT OF LEFT ENGINE AND DECLARED EMERGENCY DUE TO PARITAL POWER ON LEFT ENGINE. PILOT WAS CLEARED TO LAND. LANDED SAFELY ANSDR 2024FA0000039Landing Gear · malfunctionedJUST BEFORE LANDING WE GOT LANDING GEAR RELAY MESSAGE, TURNO AROUND PERFORMED. NEXT LANDING TRY WAS SUCESSFUL. CORRECTIVE ACTION: CB RESET AND NLG LUBRICATED. ELECTRICAL CONECTRO WAS CLEANED IAW WIRING MANUAL 32-31-01-01.SDR 2022F00509Rib · crackedCRACKS IN LEFT HAND CENTER WING MAIN RIB, AT LEFT BUTTOCK LINE 29, RADIATING FROM FASTENER HOLES OF U-SHAPED STIFFENER CHANNEL FLANGES AT THE FOLLOWING LOCATIONS; BS 303 AFT FLANGE RADIATING BOTH INBOARD AND OUTBOARD FROM FASTENER HOLE AT LEFT BUTTOCK LINE 28.SDR 2022FA0000756Rib · crackedCRACKS IN LEFT HAND CENTER WING MAIN RIB, AT LEFT BUTTOCK LINE 29, RADIATING FROM FASTENER HOLES OF U-SHAPED STIFFENER CHANNEL FLANGES AT BS 303 AFT FLANGE RADIATING BOTH INBOARD AND OUTBOARD FROM FASTENER HOLE AT LEFT BUTTOCK LINE 28.3, WATER LINE 80.5. BS 30SDR 2022F00440Adapter · crackedDURING ROUTINE INSPECTION WHILE PERFORMING INSPECTION "I" CHECK PROCEDURE (5-00-I0) TABLE 1 ITEM 30. IT WAS DISCOVERED THAT THE ELEVATOR HORN TO ELEVATOR ATTACH BRACKET P/N:101-610017-1 WAS CRACKED 85% AROUND THE CIRCUMFERENCE OF THE BRACKET WITH THE CRACK TRASDR GRTA20220801001Skin · damagedLH ELEVATOR LIGHTNING STRIKE ON TRAILING EDGE APPROX 1.1" FROM ELEVATOR TRIM TAB AT DRAIN GROMMET. DAMAGE 0.7" X 0.6" THROUGH TOP AND BOTTOM SKIN. REPAIRED IAW TEXTRON REPAIR FR-UE-128-10858SDR 2022FA0000426Wire · out of positionLH ENGINE TORQUE INDICATION QITH CONTINUOUS OSCILATION. QRF TO SLLP. CORRECTIVE ACTION: REPOSITIONES ELECTRICAL LINE IAW WDM 77-12-01. IN OPERATIONAL TEST OK IAW AMM 72-00-00.SDR 2022FA0000289None · noneFORWARD DOOR WARNING INDICATOR LIGHT TUNED ON DURING CLIMB. CORRECTIVE ACTION: DOOR POSITION SWITCH WAS ADJUSTED/REGULATED. IN TEST OKSDR 2022FA0000757Rib · crackedCRACKS IN LEFT HAND CENTER WING MAIN RIB, AT LEFT BUTTOCK LINE 29, RADIATING FROM FASTENER HOLES OF U-SHAPED STIFFENER CHANNEL FORWARD AND AFT FLANGES AT FUSELAGE STATION 303 BOTH INBOARD AND OUTBOARD FROM FASTENER HOLE AT LEFT BUTTOCK LINE 28.3, WATER LINE 80SDR TIMA20220314003None · noneEXITING RUNWAY ONTO TAXIWAY AIRCRAFT ENCOUNTERED A PATCH OF ICE NEAR THE EDGE OF THE PAVEMENT SURFACE DURING LEFT HAND TURN. AS TURNING REQUIRED BRAKING ACTION TO COMPLETE, LEFT BRAKE WAS INEFFECTIVE. PLACED POWER LEVERS IN REVERSE AND DEPRESSED RIGHT BRAKE TOSDR 2021FA0000410Bleed Air Sys · dirtyENGINE #2 LOW POWER DURING TAKEOFF (TORQUE INDICATOR 600PSI). ABORTED TAKEOFF. CORRRECTIVE ACTION: BLEED AIR CLEANED IAW AMM 75-00-00. ENGINE RUNNUP OK.SDR GRTA20210420001Spar Cap · crackedAFT SPAR UPPER SPAR CAP CRACKED (FS 327.630) AT LBL 1.0 THRU LBL 5.0. JUST OB OF FLAP MOTOR/GEAR BOX.SDR GRTA20210414004Stringer · crackedSTRINGER 9R CRACKED AT LAST RIVET JUST AFT OF AFT PRESSURE BULKHEAD (APPROX FS 557.500)SDR GRTA20210414001Stringer · debondedSTRINGER 15R DISBONDED FROM SKIN BETWEEN FS 378.250 AND 393.250.SDR GRTA20210414003Pan · crackedEMERGENCY EXIT 4C WINDOW PAN CRACKED PART NUMBER 129-430043-3.SDR GRTA20210414002Pan · crackedEMERGENCY EXIT 6A WINDOW PAN CRACKED PART NUMBER 129-430043-3.SDR GRTA20201210002Skin · crackedBELLY SKIN CRACKED AT FS 288.25 JUST OUTBOARD OF STRINGER 15L APPROXIMATELY 1" AND 1.5". AFTER FURTHER INVESTIGATION, FOUND FRAME SHIM CORRODED. REPAIRED IAW BEECHCRAFT 1900 SRM 51-70-06.SDR TIMA2020090982003Governor · leakingLEVELED OFF IN CRUISE AT 14000' STARTED CRUISE CHECKS AND NOTICED OIL PRESS ON NR 2 ENGINE AT 60 PSI. PRESSURE EVENTUALLY DROPPED BELOW 60, SHUT DOWN ENGINE, MADE EMERGENCY LANDING IN BIL.SDR TIMA20200609002Control Rod · brokenDURING FLIGHT, PILOT EXPERIENCED LOSS OF RUDDER INPUT. LANDED SAFELY IN MOT. MAINTENANCE FOUND THE RUDDER CROSSOVER SHAFT WHICH CONNECTS PILOT WITH CO-PILOT PEDAL CONTROLS BROKEN.SDR CA190806006Bearing · damaged(CAN) DURING THE MANUFACTURERS SCHEDULED 5000HR/5 YEAR FLAP INSPECTION IT WAS FOUND THAT THE AIRCRAFT WAS NOT IN COMPLIANCE WITH AN AD THAT WAS SHOWING AS PREVIOUSLY COMPLIED WITH IN THE AIRCRAFT RECORDS. AD99-01-03 WAS SHOWING AS BEING PREVIOUSLY COMPLIED WITSDR CA190726009Control Head · failed(CAN) AT TOP OF CLIMB THE #2 COMM FAILED. THE CREW HAD CARRIED OUT SOME BASIC TROUBLESHOOTING AND DETERMINED THAT THE RADIO WAS, INDEED, U/S. THEY HAD INFORMED AIR TRAFFIC CONTROL AND DID A RETURN BACK TO AIRPORT OF ORIGIN WHERE THEY HAD LANDED SAFELY. MAINTENSDR CA190621007Torque Tube · cracked(CAN) DURING HEAVY CHECK 3RD PARTY MRO IDENTIFED RUDDER TORQUE SHAFT LOOSE AND A CIRCUMFERENTIAL CRACK.SDR CA190521005Diode · overheated(CAN) DURING LANDING CHECKS, UPON FINAL INTO XXXX, THE LANDING GEAR WAS SELECTED DOWN BY THE CREW, BUT DID NOT EXTEND. CREW HAD CARRIED OUT A `GO AROUND` AND REQUESTED A HOLD WITH CENTER. CREW HAD CARRIED OUT REQUIREMENTS OF THE APPLICABLE CHECKLIST WHERE THE SDR CA190513002Pressure Switch · leaking(CAN) AFTER DEPARTING OUT OF XXX WE HAD THE #2 ENGINE BOUNCING BETWEEN 4000-2500 TORQUE, AT 400 FEET WE BROUGHT POWER BACK TO CLIMB POWER AND THE TORQUE WAS STEADY, SO WE THOUGHT IT WAS JUST THE GAUGE. WHEN WE WERE CRUISING TO XXX AT 4500 FEET WE HAD A LOW OILSDR CA190501023Screw · damaged(CAN) UPON APPROCH INTO XXXX, FLIGHT CREW OF C-XXXX ATTEMPTED TO SELECT GEAR DOWN. `LANDING GEAR CONTROL` CIRCUIT BREAKER FOUND TO BE `POPPED`. BREAKER RESET & DOWN SELECTION RE-SELECTED. POSITIVE DOWN LOCK INDICATION FOR BOTH MAINS ACHIEVED, NEGATIVE INDICATISDR CA190501015Altimeter · failed(CAN) JUST AFTER TAKE OFF THE CAPTAIN`S ALTIMETER FAILED. THIS EVENT, IN TURN, CAUSED DISRUPTION OF OTHER ASSOCIATED EQUIPMENT SUCH AS THE ALTITUDE ALERTER, TCAS AND TRANSPONDER. (TC# 20190501015)SDR CA190514017Uplock Switch · faulty(CAN) GEAR FAILED TO RETRACT AFTER TAKE-OFF. FOUND RH MLG UPLOCK SWITCH TO BE AT FAULT. RH MLG UPLOCK SWITCH REPLACED AND RIGGED. (TC# 20190514017)SDR CA190415001Governor · weak(CAN) LEFT ENGINE AUTO FEATHER ENGAGED ON APPROACH PILOT REPORTED PROP FEATHERED FOR ABOUT 3 SEC WHEN POWER WAS REDUCED BEFORE SELECTING FLAP 35. IT CAUSED THE PLANE TO YAW QUITE A BIT CORRECTION P/N OS GOVERNOR 210961C (TC# 20190415001)SDR CA190417007Safety Switch · unserviceable(CAN) THIS GEAR SAFETY SWITCH (SQUAT SWITCH) HAS MULTIPLE SWITCH THROWS THAT CONTROL MULTIPLE SYSTEMS. ONE SWITCH THROW THAT CONTROLS THE OPERATION OF THE GROUND FINE SOLENOIDS SHORTED INTERNALLY WHICH MAKE THE GROUND FINE SOLENOID SYSTEM ALWAYS BEHAVE LIKE ITSDR CA190410015Actuator · malfunctioned(CAN) MAIN LANDING GEAR ACTUATOR 114-380041-15 S/N 0606A WAS INSTALLED ON 14 DEC 2018 AT 14,026.9HRS. THE ACTUATOR HAD A FORM ONE FOR THE OVERHAUL WHICH ALSO STATED AD2009-23-01 (ULTRASONIC INSPECTION) WAS CARRIED OUT AT THE OVERHAUL. WE RECEIVED AN EMAIL FROMSDR CA190403020Pushrod · worn(CAN) DURING INSPECTION IT WAS DISCOVERED THAT THERE WAS WEAR ON THE RH POWER LEVER PEDESTAL PUSH ROD. IT WAS DETERMINED TO ORIGINATE FROM INTERFERENCE WITH THE LH PROPELLER CONTROL. AFTER CONSULTATION WITH BEECHCRAFT IT WAS FOUND THAT THE DIAGRAM SHOWING INSTSDR CA190319008Connector · loose(CAN) AIRCRAFT LANDING GEAR WOULD NOT EXTEND. APPROACH WAS ABORTED AND FLIGHT CREW COMPLETED AN EMERGENCY EXTENSION. FOUND ELECTRICAL CONNECTOR ON THE LANDING GEAR CONTROL ASSEMBLY TO BE LOOSE. AFTER CONNECTOR TIGHTENED THE LANDING GEAR SYSTEM TESTED SERVICEABSDR CA190221008Shaft · deformed(CAN) DURING MAINTENANCE TO RECTIFY A FLAP MEL, IT WAS DISCOVERED THAT THE #4 FLAP SHAFT ASSEMBLY HAD BEEN TWISTED AND DEFORMED. THE SHAFT ASSEMBLY WAS ULTIMATELY REPLACED IAW MANUFACTURER`S INSTRUCTIONS AND SYSTEM OPERATION WAS CARRIED OUT WITH NO OTHER FAULTSDR CA190305016Relay · failed(CAN) JUST AFTER GROUND POWER WAS PUGGED IN, I OPENED THE DOOR TO COMMUNICATE THE FUEL LOAD TO THE FUELLER. I NOTICED THE PROP SMOKING NEAR THE SPINNER, JUST AFTER TALKING TO THE FUELLER. I CALL TO XXX TO TURN OFF THE PROP HEAT. HE SAID IT WAS OFF. I CALLED FOSDR CA181015014Buss Bar · corroded(CAN) DURING TROUBLE SHOOTING FOUND OUT THAT BUS BAR WAS CORRODED AND NOT MAKING PROPER CONTACTS WHEN GPU IS ATTACHED. BUS BAR WAS REPLACED ALONG WITH RECEPTACLE FOR FIX. SYSTEM CHECKED SERVICEABLE AND AIRCRAFT WAS RELEASED FOR SERVICE. (TC# 20181015014)SDR CA180707001Transducer · disconnected(CAN) ATTACH SCREWS P/N MS24693-S24 BECAME FREE OF WHEEL SPEED TRANSDUCER P/N 140-04715. TRANSDUCER WAS ABLE TO SHIFT INSIDE THE AXLE ALLOWING FOR THE TRANSDUCER TO LOOSE WHEEL SPEED INPUT, DUE TO SEPARATION FROM DRIVE HUBCAP P/N 114-810055-3. ONLY INDICATIOSDR GLBA2018032100704Cable · brokenMAINTENANCE REPORTED THAT THE FORWARD LOWER PASSENGER DOOR CABLE WAS BROKEN. MAINTENANCE REPLACED THE CABLE IAW MM 52-10-02 3A & B.SDR GLBA2018030800702Cable · frayedMAINTENANCE REPORTED THAT THE AIRSTAIR DOOR LOWER FORWARD HANDRAIL CABLE IS FRAYED. MAINTENANCE REMOVED AND REPLACED AIRSTAIR DOOR LOWER FORWARD HANDRAIL CABLE IAW MM 52-10-02.SDR CA180222015Landing Gear · damaged(CAN) DURING PUSH BACK IN YUL, DUE TO ICY CONDITION NOSE STEERING EXCEEDED NOSE GEAR STEERING LIMIT AND DAMAGE TO STEERING BUNGEE, SHIMMY DAMPER, GUIDE AND ALIGNMENT BRACKET. ALL THE DAMAGED PARTS HAVE BEEN REPLACED INCLUDING NOSE GEAR ASSEMBLY FOR FIX. (TC SDR GLBA2018020700701Mount · wornMAJOR REPAIR - RT INBD FLAP ACTUATOR FORWARD MOUNT WORN AT RT WS 53.94. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK. **SDR GLBA2018020700700Mount · wornMAJOR REPAIR - RT INBD FLAP ACTUATOR FORWARD MOUNT WORN AT RT WS 56.06. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK. **SDR 2018FA0000051Duct · damagedLEFT TEMPERATURE CONTROLLER SENSOR MOUNT BASE BROKE AT THE BLEED AIR DUCT ASSEMBLY CREATING A HOLE LARGE ENOUGH TO PROHIBIT CABIN PRESSURIZATION AND PROMPTING A LT ENVIR OFF LIGHT. PHOTOS AND DRAWING PROVIDED.SDR GLBA2018011100699Rudder Pedal · shearedPILOTS REPORTED THAT WHILE TAXING OFF THE RUNWAY, WHEN RIGHT RUDDER PRESSURE WAS APPLIED, THE CAPTAIN'S RIGHT RUDDER PEDAL ASSEMBLY SHEARED OFF, FLOPS LOOSE ON THE ASSEMBLY. R & R THE CAPTAIN'S RT RUDDER PEDAL AND ARM ASSEMBLY IAW MM 27-20-03-201. OPS CHECKSDR GLBA2017121800698Coupling · leakingCREW REPORTED THAT THERE WAS A HYDRAULIC LEAK IN THE RIGHT FRONT PART OF THE RIGHT WHEEL [WELL]. 6-7 INCH PUDDLE BUT COULD SEE NO ACTUAL DRIPS. MAINTENANCE TROUBLESHOT AND FOUND FUEL LEAKAGE AT THE RIGHT OUTBOARD WING VENT BOX TRANSFERRING TO WHEEL WELL THROUG
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