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 = '525A' 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 = '525A' 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 TY2A2014070200620Unknown · unknownDURING DECENT FROM CRUISE ALTITUDE, CABIN STARTED CLIMBING AT 2800 FPM. INITIATED A STEEP DESCENT WHILE SELECTING LT, RT, AND EMERGENCY BLEED TO STOP CABIN FROM CLIMBING. CABIN ALTITUDE REACHED 14,000 FT BEFORE THE ACFT DID AND THE PASSENGER MASK DEPLOYED. SDR WI5R2014050200001Blade · detachedLT ENGINE HAD AN INTERMITTENT LOW RUMBLING NOISE AT GREATER THAN 80 PERCENT N1. DISASSEMBLY OF THE ENGINE HAS REVEALED IP ROTOR LIBERATED 1 OF THE 1ST STAGE BLADES.SDR FKEA2014042900001Precooler · rupturedDURING CLIMBOUT, ENROUTE, OPERATING UNDER A PART 91, THE PILOT NOTICED AN ITT SPLIT OF AROUND 70 DEGREES BETWEEN THE LT & RT ENGINES, LT BEING ABNORMALLY HIGH. THE PILOT RETARDED THE LT ENGINE AND SHUTDOWN. ACFT DIVERTED. EVIDENCE WAS FOUND OF AN OVERHEAT ISDR FKEA201404080123Controller · intermittentAIRCRAFT ENROUTE, DESCENDING FROM FL450 THROUGH FL280 WITH ENGINES AT FLIGHT IDLE. CABIN PRESSURE ROSE TO 15,000 FT WITH ASSOCIATED CABIN PRESSURE WARNING ANNUNCIATOR LIGHT, PAX O2 MASKS AUTOMATICALLY DEPLOYED. EMERGENCY DECLARED AND CREW INITIATED A RAPID DESSDR WI5R2014032800001Blade · missingDURING A BORESCOPE INSPECTION, A THIRD STAGE IP ROTOR BLADE WAS FOUND MISSING. SECONDARY DAMAGE WAS NOTED TO THE COMPRESSOR ROTOR. DISASSEMBLY CONFIRMED ONE BLADE ON THE THIRD STAGE IP ROTOR IS MISSING.SDR CA140306005Starter Gen · malfunctioned(CAN) DURING ENGINE START THE LT STARTER GENERATOR WOULD NOT DISENGAGE AFTER START CYCLE WAS COMPLETE, ON SHUTDOWN A RUMBLING NOISE WAS HEARD FROM ENGINE. THE STARTER GENERATOR WAS REMOVED AND FOUND THAT THE STARTER GENERATOR INPUT SHAFT WAS LOOSE IN THE STARTSDR CA140214003Brushes · worn(CAN) VAPOR CYCLE COMPRESSOR BRUSHES OVER WORN CAUSING THE MOTOR TO OVERHEAT WHICH IN TURN MELTED THE PLASTIC COVER, THIS CAUSED THE COOLING FAN BLADES TO CONTACT THE COVER AND BEND/TEAR. THE BRUSHES HAD 270.7 TT, INSPECTION CRITERIA IS TO INSPECT EVERY 300 HSDR 2014FA0000052Precooler · rupturedON ARRIVAL, SOME DISCOLORATION, MISSING PAINT WAS NOTED ON THE RT ENGINE PYLON. ON FURTHER INVESTIGATION IT WAS FOUND THAT THE PRE-COOLER HAD RUPTURED IN THE PYLON CAUSING SEVERE HEAT DAMAGE TO THE SURROUNDING STRUCTURE AND PYLON, FUSELAGE SKINS. IT WAS DETERSDR WI5R20131121001Blade · crackedDURING CHECK 4 MAINTENANCEON ENGINE, FAN ROTOR WAS REJECTED FOR SEVERAL CRACKS ON THE INNER FLOW PATH, POSSIBLY STEMMING FROM THE AFT FACE. ONE OF THE CRACKS HAS PROPAGATED INTO THE T/E OF THE BLADE. THE CRACKS APPEAR TO BE EVERY 3 TO 4 BLADES.SDR 2013FA0000664Precooler · splitPILOT REPORTED A HIGH ITT ON THE LT SIDE. DURING A POWER RUN TO CONFIRM TEMP SPLIT WITH BLEEDS ON THE TEMP WAS CLOSE TO THE LIMIT, BLEEDS OFF THE TEMP WAS SLIGHTLY LOWER. AFTER THE RUN, A VISUAL INSPECTION OF THE ACFT REVEALED A BURNED SPOT ON THE PYLON UPPESDR QREA2013111200001Uplock Hook · crackedHYDRAULIC ON AND GEAR UNLOCK LIGHT CAME ON DURING DECENT, FOLLOWED BY A THUMPING NOISE FROM THE LT GEAR. GEAR EXTENDED NORMALLY WITH 3 GREEN. LANDED AND CALL DOM. DOM ASKED THE PILOT TO LOOK AT THE UPLOCK HOOK ON THE LT GEAR. SHOWED UPLOCK HOOK CRACKED. FSDR W9BA2013080901Uplock Switch · intermittentPILOT REPORTED A "GEAR UNLOCK" ANNUNCIATOR MOMENTARILY ILLUMINATED DURING DESCENT. A HYD PRESSURE ANNUNCIATION ALSO ILLUMINATED AND EXTINGUISHED WHEN THE "GEAR UNLOCK" INDICATOR EXTINGUISHED. THE TECH TROUBLESHOT THE ISSUE TO A LT MLG UPLOCK SWITCH. SWITCH R SDR CA130711006Capacitor · overheated(CAN) WHEN CREW SELECTED GEAR DOWN, ONLY GOT RT GEAR TO INDICATE DOWN AND LOCKED, EMERGENCY EXTENSION CARRIED OUT WITH STILL ONLY RT GEAR INDICATION, DID NOT RECEIVE AN UNSAFE GEAR INDICATION. MAINTENANCE DETERMINED THERE WAS A FAULT WITH THE LANDING GEAR MONSDR CVGA201305002001Carbon Seal · leakingON FINAL APPROACH, RECEIVED A MASTER WARNING INDICATION AND "LOW OIL PRESSURE" ON THE RIGHT ENGINE. ENGINE WAS SHUTDOWN.SDR CVGA2013003028Uplock Hook · crackedGEAR UNLOCK LIGHT CAME ON INFLIGHT. CYCLED GEAR 3 TIMES WITH NO CHANGE. GEAR REMAINED DOWN FOR REMAINDER OF THE FLIGHT.SDR CNQR12172012585Oil System · low pressureLOSS OF OIL PRESSURE ON LEFT ENGINE AND HAD EXHAUST ODOR IN COCKPIT AND CABIN.SDR WI5R20121218Blade · brokenDURING A PRE-BUY BOROSCOPE INSPECTION, IT APPEARED THAT AN IP ROTOR BLADE HAD BROKEN OFF AND GONE THROUGH THE CORE OF THE ENGINE. THIS WAS CONFIRMED UPON DISASSEMBLY. BLADE ON THE 3RD STAGE OF THE IP ROTOR WAS MISSING.SDR WI5R201203010001Bolt · improper partDURING ON-WING REPLACEMENT OF A DIFFUSER ON ENGINE 216014, THE INCORRECT CONFIGURATION BOLT WAS FOUND INSTALLED IN THE SERVICE ISLAND OF THE DIFFUSER BEING REMOVED. INSTEAD OF THE PN MS9558-04, PLUG BOLT, THAT IS REQUIRED FOR THE THIS ENGINE, A PN 45947, SPECSDR 2011FA0000523Seal · looseACFT CLIMBED TO FL200 AND HEARD A LOUD POP AND A LOUD RUSH OF AIR COMING FROM MAIN CABIN DOOR. STARTED TO SEE A DROP IN CABIN PRESSURE, PILOTS THEN DESCENDED AND DIVERTED BACK TO ORIGINATING AIRPORT. PILOTS DID DECLARE AN EMERGENCY, ACFT LANDED WITH NO PROBLESDR 2011FA0000178Precooler · splitCREW REPORTED A 50 DEGREE TEMP SPLIT IN FLIGHT. FOUND THE RT PYLON PRE-COOLER SPLIT AT SEAMS. RESULTING IN BLEED AIR LEAK INSIDE THE PYLON WHICH CAUSED FAILED CONDUCTIVITY TEST RESULTS OF THE PYLON AND FUSELAGE SKINS.SDR 2010F00137Squat Switch · damaged(EBVR) PILOT REPORTED GEAR RETRACTION SEQUENCE COULD NOT BE COMPLETED. UPON RETURN TO MX FACILITY, IT WAS OBSERVED THAT THE ROLLER WHEEL AND ASSOC HARDWARE ON THE RT MLG SQUAT SWITCH WERE MISSING.SDR FCPR201000230Shutoff Valve · leaking(FCPR) LT HYD SHUTOFF VALVE LEAKING STATIC AND UNDER PRESSURE. OUTLET PORT FLANGE DEFORMED WITH EXTRUDED O-RING.SDR 2010FA0000390Diffuser · damagedCUSTOMER CALLED TO REPORT AN IFSD OF HIS ENGINE DURING AN ACFT FERRY FLIGHT. THE ACFT WAS GOING TO TROUBLESHOOT AN OIL SMELL IN THE CABIN COMPLAINT. ENGINE 216118 HAS 1223 HOURS REPORTED AT THIS TIME. A FIRE WARNING ANNUNCIATED AS THE AIRCRAFT WAS PASSING FSDR S30R1000022Precooler · rupturedTHE RT ENGINE BLEED AIR TO BYPASS AIR PRE COOLER RUPTURED IN FLIGHT CAUSING THE UPPER AND LOWER PYLON SKINS AS WELL AS THE ACFT SKIN TO BE COME EXPOSED TO HOT EXHAUST GASES WHICH SUBSEQUENTLY RESULTED IN WARPAGE OF THESE SKINS. PILOT REPORTED, HEARD A NOISE ASDR 2009FA0000911Wheel · misinstalledDURING TAKEOFF OF THE ACFT, WENT INTO A CLIMB IMMEDIATELY AFTER LIFTOFF. THE ACFT TRIED TO GO NOSE UP EXCESSIVELY AND THE PILOT HAD TO APPLY FWD PRESSURE TO THE CONTROL COLUMN TOO ARREST THE CLIMB AND CONTROL THE ACFT. A POST FLIGHT INSP FOUND THE POINTER FOSDR ZDVA424KOutflow Valve · malfunctionedCREW EXPERIENCED LOSS OF PRESSURIZATION/ERRATIC OPERATION, WAS ABLE TO CONTROL IN MANUAL MODE.SDR 2009FA0000270Seat Belt · misinstalledMAINTENANCE DISCOVERED THE INCORRECT PN SEAT BELT INSTALLED ON THE FWD RT SIDE FACING SEAT (BUCKLE OPENED LT TO RT). THE PN BELT INSTALLED IS 4799020-2 WHICH IS FOR THE AFT LT FACING TOILET SEAT. THIS ACFT WAS DELIVERED FROM THE FACTORY IN THIS CONFIGURATIONSDR 051108N425CS0Smoke Detector · contaminatedBAGGAGE SMOKE LIGHT INDICATION ON APPROACH. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINT PERSONNEL FOUND PAINT OVERSPRAY ON BAGGAGE SMOKE DETECTOR AND REPLACED WITH REPAIRED UNIT. AIRCRAFT RETURNED TO SERVICE.SDR 2007FA0001047Line · separatedFOUND FLAP RETRACT LINE SEPARATED FROM BACK OF B-NUT. SYSTEM FLUID WAS LOST. SUSPECT DEFECT WAS AT TIME OF MANUFACTURE. (K)SDR 2007FA0000565Valve · leakingPERFORMED AN EMERGENCY LANDING DUE TO LOSS OF HYDRAULIC PRESSURE. THE EMERGENCY BOTTLE WAS USED TO LOWER THE GEAR AND LAND WITHOUT INCIDENT. THE CAUSE HAS BEEN DETERMINED TO BE THE HYDRAULIC LOADING VALVE (PN 4134-4, SN 781) FAILING IN CLOSED POSITION, RESULSDR FCPR20060027Heater · burnedAFT TOILET RELIEF TUBE HEATER ELEMENT FAILED WITH EXTERNAL POWER APPLIED BURSTING INTO FLAMES. IPC REFERENCE 38-30-00 FIG 3 ITEM 16.SDR 2006FA0000411Lug · misdrilledAC WAS IN FOR A PHASE 1 AND 2 INSPECTION. A BROKEN BONDING STRAP AT THE UPPER LT SPEEDBRAKE DOOR NECESSITATED REMOVAL OF THE BOLT CONNECTING THE PUSH ROD TO THE UPPER DOOR LUG. DURING BOLT REMOVAL THE HELICOIL INSERT CAME OUT WITH THE BOLT AND WAS DEFORMED. SDR D942006F00000Squat Switch · failedCABIN WILL NOT PRESSURIZE IN FLIGHT. FOUND RT MAIN LANDING GEAR SQUAT SWITCH MALFUNCTION. NOTE: INFLIGHT, IN THE MALFUNCTION CONFIGURATION, THE CABIN ALTITUDE PRESSURE SWITCH WILL NOT ACTUATE. THE ONLY EXISTING SAFETY FEATURE IS THE MAXIMUM ALTITUDE SAFETY SDR 2006FA0000242Line · failedAIRCRAFT DEPARTED THE RUNWAY DURING LANDING ROLLOUT. FAILURE OF BOTH THE HYDRAULIC AND PNEUMATIC LINES TO THE LT MAIN LANDING GEAR BRAKE CAUSED THE AIRCRAFT TO SPIN INTO A GRASSY AREA ADJACENT TO THE RUNWAY. THE NOSE LANDING GEAR SHEARED OFF AND THE AIRCRAFTSDR AMCR200500009Fan · cloggedWHILE THE AIR CONDITIONER WAS RUNNING, THE CREW REPORTED INADEQUATE COOLING AND A FAINT ODOR OF SOMETHING BURNING. MAINTENANCE FOUND THE AFT EVAPORATOR FAN WAS BARELY RUNNING. AFTER REPLACING THE FAN, THE OLD FAN'S COVER WAS REMOVED AND A BIG PILE OF BRUSH DUSDR CNQ2004FAAAALine · brokenTHE AIRCRAFT WAS ON A FERRY FLIGHT WITH GEAR DOWN DUE TO A DAMAGED LANDING GEAR DOOR. UPON LANDING, THE AIRCRAFT HAD NO BRAKES AND HYDRAULIC FLUID WAS STREAMING FROM THE LT WHEEL WELL. DURING CLOSER INSPECTION IT WAS NOTED THAT THE HARD, BRAKE LINE IN THE LESDR 2004FA0000604Circuit Breaker · arcedTHE FOLLOWING SYS FAILED IN FLIGHT: NR 1 NAV/COMM/XPDR, CO-PILOTS AUDIO PANEL, RT PITOT HEAT, STANDBY HSI, NR 2 ATTITUDE/HEADING, AUTOPILOT DISENGAGED, LANDING GEAR HYDRAULIC, SYS PRESSURE, LANDING GEAR DOWN AND LOCK INDICATOR LIGHTS, FLIGHT CREW UTILIZED THESDR 2004FA0000345Piccolo Tube · brokenDURING THE PHASE 5 INSPECTION THE RT WING ANTI-ICE PICCOLO TUBE WAS FOUND BROKEN AT THE ANIT-ROTATION TAB. THE TUBE WORKED ITS WAY INBOARD APPROXIMATELY 4 INCHES. THE FLEX COUPLING KEPT IT FROM TRAVELING INBOARD ANY FURTHER. NEW PART WAS ORDERED AND INSTALLSDR 2004FA0000338Control Cable · brokenDURING ACCOMPLISHMENT OF THE AIRCRAFT'S FIRST PHASE 5 INSPECTION, FOUND ALL FOUR AILERON WING CABLES TO BE HEAVILY FLAT SPOTTED AT THE FAIRLEADS LOCATED AT WS 58.00, 103.43 AND 149.18. THE RT UPPER CABLE (P/N 6361002-7) HAD ONE BROKEN STRAND. THESE CABLES NOSDR AMCR200400001Connector · burnedLT WINGTIP STROBE ASSEMBLY WAS INSTALLED 13 HOURS PRIOR IAW SB525A-33-02. WHEN STROBE FAILURE WAS NOTED, FOUND CONNECTOR SEVERELY BURNED, WITH ONE PIN COMPLETELY BURNED AWAY (ON POWER SUPPLY SIDE). POWER SUPPLY FAILED ALSO (MFG:FLIGHT COMPONENTS AG). CHANGED SDR 200401Transponder · malfunctionedINSTALLED VARIOUS RADIOS IN THIS AIRCRAFT INCLUDING THE GTX 330 TRANSPONDER INTO THE LOWER SECTION OF THE CAPTAINS INSTRUMENT PANEL. MONTHS LATER, WHILE THE AIRCRAFT WAS UNDERGOING A PHASE 5 INSPECTION AT THE MFG, IT WAS DISCOVERED THAT THE NEWLY INSTALLED TRSDR E712004F00000Transducer · failedWHILE CLIMBING THROUGH FL180, PILOTS NOTICED A CONTINUAL DECLINE IN OIL PRESSURE ON THE LT ENGINE. PROCEDURE REQUIRED SHUTDOWN AND SECURING LT ENGINE IN FLIGHT. AT THAT TIME THE AIRCRAFT WAS 20 MIN FROM INTENDED DESTINATION. PILOTS MADE A NORMAL DESCENT TO SDR 2003FA0001152Screen · missingWHILE PERFORMING INSPECTION FOUND THAT IN-LINE HYDRAULIC FILTER SCREENS WERE NOT INSTALLED. THIS IS THE SECOND OF THESE TYPE NEW AIRCRAFT WE HAVE FOUND MISSING THESE FILTERS SCREENS. ORDERED FILTER SCREENS AND INSTALLED. NOTIFIED MANUFACTURER THAT THESE SCRSDR AP48200222808Inlet · crackedLEFT ENGINE INLET BARREL CRACKED AT 12 O'CLOCK POSITION FROM INLET RING RIVETS TO BARREL EDGE.SDR 2002F00980Nose Cowl · crackedAFTER FINDING THE SAME CRACK ON SERIAL NR 17 PERFORMED AN INSPECTION AND FOUND A CRACK ON THE INNER SIDE APPROXIMATELY 3 O'CLOCK POSITION OF THE RIGHT ENGINE INLET NOSE CAP. THE CRACK WAS APPROXIMATELY .75 OF AN INCH IN LENGTH RUNNING FROM THE EDGE OF THE MET
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