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 jasc_code = '3600' 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 jasc_code = '3600' 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 TSAA0436037Regulator · failedNR 2 ENGINE BLEED GIVES NO DUCT PRESSURE WITH ISOLATION VALVE IN AUTO OR CLOSED. RETURNED TO DEPARTURE AIRPORT, EXECUTED LOW SINK RATE LANDING. REMOVED AND REPLACED NR 2 ENGINE BLEED AIR REGULATOR IAW AMM 36-11-03-4. ENGINE NR 2 BLEED SYSTEM OPS CHECKS NORMASDR 03FDEA02175Pressure Switch · failedRECEIVED NR 1 MANIFOLD FAIL ALERT AT FL350. COULD NOT MAINTAIN CABIN PRESSURE. RAN RED TABS AND DIVERTED TO DEN. FOUND LEFT WING PRESSURE SWITCH FAULT BALL NO LEAKS NOTED. PERFORMED DECAY CHECK PER MD-10 MM 36-00-01-5 DECAY CHECK WITHIN LIMITS. REMOVED ANSDR IXXA0300072OPrecooler · crackedDURING CLIMB FROM KGSO TO KTOL NR 2 ENGINE PNEUMATIC SYSTEM OVERHEATS WITH LOW OR HIGH STAGE BLEED WITH CLIMB POWER SET AND LT PACK AT MIN FLOW. CREW RETURNED TO KGSO AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 PRECOOLER CONTROL VALVE SDR USAASA03063Check Valve · failedAT APPROX FL260, DURING DESCENT, NR 2 ENG STALLED & LOST POWER. FELT A VIBRATION AS N1 DECREASED FROM 90 TO 50 PERCENT. THROTTLE PULL BACK STOPPED VIBRATION. COMMAND INDICATED APPROX 40 PERCENT, BUT ENGINE THRUST INDICATED 20 PERCENT. THROTTLE ADVANCED SLOWSDR 2003F00306Gasket · wornCREW REPORTED NR 3 STRUT OVERHEAT LIGHT CAME ON IMMEDIATELY AFTER LIFT OFF. CAPTAIN FOLLOWED AMERIJET NORMAL PROCEDURES AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND LEAK AT 13TH STAGE INBOARD DUCT. REMOVED AND REPLACED GASKETS. IN ADDITION, OFUNDSDR AMTA200300546Pilot Valve · failedRIGHT ENGINE HIGH STAGE EICAS MESSAGE. REMOVED AND REPLACED HIGH STAGE PILOT PER FIM 36-10-00-1 FIG 111. OPS CHECKS GOOD. REF MM 36-11-08-4. (M)SDR 200301Regulator · bindingDURING CRUISE FLIGHT, PILOT NOTICED A BURN ODOR IN COCKPIT. PILOT THEN NOTED THAT DOOR POST TRIM PANEL WAS DISCOLORED. RETURNED TO AIRPORT AND NOTIFIED MECHANIC. MECHANIC FOUND THE PRESSURE REGULATOR TO BE FAULTY. FURTHER INVESTIGATION LED TO REPLACEMENT OSDR SIMA200300601Connector · dirtyDFW - FLT 3873 - SHORTLY AFTER TAKEOFF CREW REPORTED A NR 1 BLEED LEAK WARNING. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS RETURNED TO DFW AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. A LEAK CHECK ON THE BLEED DUCTS FOUSDR VNAA0211030Bleed Valve · failedDURING TAKE OFF, THE CREW RECEIVED A BLEED SHUT OFF VALVE CAS MESSAGE AND ABORTED TAKE OFF. WHILE THE AIRCRAFT WAS CLEARING THE RUNWAY THE MESSAGE CLEARED. THE CREW WAS THEN NOTIFIED THAT THERE WAS TWO PASSENGERS THAT WERE ON THE WRONG FLIGHT AND WANTED TO GSDR VNAA0211029Bleed Valve · failedDURING TAKE OFF, THE CREW RECEIVED A BLEED SHUT OFF VALVE CAS MESSAGE AND ABORTED TAKE OFF. AFTER THE AIRCRAFT CLEARED THE RUNWAY, THE CREW CYCLED THE BLEED VALVE AND THE MESSAGE CLEARED. FLIGHT 9424 WAS THEN CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND FLIGHT 9SDR CA021117001Duct · chafed(CAN) IN HANGAR, AT ENGINE INSTALLATION DURING RE CONNECTION OF THE INTERMEDIATE PRESSURE, (IP) DUCT INSIDE THE PYLON NR 3 AREA IT WAS NOTICED THAT THE FLEXIBLE SECTION OF THE PIPE SECTION FOR THE ANTI-ICE TAP-OFF OF THE IP DUCT WAS CHAFED THROUGH. DAMAGE OCCSDR FL3A200200389Check Valve · inoperativeDURING CLIMB OUT, THE FLIGHT CREW NOTED AN ILLUMINATED WING/BODY OVERHEAT LIGHT WHICH WOULD NOT EXTINGUISH WHEN QUICK REFERENCE HANDBOOK ITEMS WERE ACCOMPLISHED. THE AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT.MAINTENANCE REMOVED AND REPLACED THE START MANIFOLSDR DL733021289Seal · tornAFTER LEVELING AT FL350 MASTER CAUTION W/OVERHEAD ON THE MASTER CAUTION PANEL ILL. PASS. O2 LIGHT ON THEOVERHEAD WASILL. CABIN ALT. WAS AT 15,000FEET. FA CONFIRMED MASKS HAD DROPPED. AUTO FAIL LIGHT WAS ILL. BUT NO ALT. ALERT HORN HADSOUNDED. ALT. CONT. SDR C2XA02CL204Line · brokenCLE FLIGHT#3296 THE CREW REPORTED AFTER TAKEOFF THEY RECEIVED A #1 BLEED LEAK MESSAGE ON THE EICAS AND THE OVERHEAD PANEL.THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE #1 ENGINE DIRRERENTIAL PRESSURE SESDR VJ32002F00077Pump · failedDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.SDR VJ32002F00076Pump · failedDURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. SUSPECT PROBABLE CAUSE IS HEAT AND VANES WEARING ON THIS DRY AIR PUMP.SDR WVE2002F00017Duct · damagedDURING 300 HOUR INSPECTION, THE UPPER COWLING WAS REMOVED FOR MINOR INSPECTION. DAMAGE WAS NOTED TO THE UPPER BYPASS DUCT. DURING FURTHER INVESTIGATION, DAMAGE WAS ALSO NOTED ON THE RIGHT AND LEFT INNER CORE COWLS. TO BE EVALUATED BY MFG.SDR VJ32002F00049Pump · failedDURING GROUND RUN UP, OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT 800 RPM. RAN AIRCRAFT UP TO 1600 RPM BEFORE PRESSURE READ 4.5. CHECKED PRESSURE SYSTEM FOR LEAKS AND CHECKED REGULATOR ALL CHECKED WELL.SDR ASOA02324Wire · brokenDURING CLIMB OUT, AT APPROXIMATELY 19,000 FEET, CAPTAIN REPORTED THAT DUCT LEAK WARNING WAS RECEIVED WITH CORRESPONDING LEFT DUCT LEAK LIGHT ILLUMINATING. CAPTAIN RAN CHECKLIST. WITH APU BLEED CLOSED THE WARNING INDICATION WENT OUT BRIEFLY THEN RETURNED. WSDR VJ32002F00045Pump · failedIN FLIGHT THE INSTRUMENT VACUUM SYSTEM FAIL. THE AIRCRAFT RETURNED TO MAINTENANCE AND AN INSPECTION OF THE SYSTEM FOUNDED THAT THE ROTOR HAD FROZEN UP AND THE SHAFT HAD SHEARED. PUMP WAS REMOVED AND A NEW PUMP INSTALLED. OPERATIONAL CHECK OF THE SYSTEM CHESDR VJ32002F00038Pump · failedIN FLIGHT, THE INSTRUMENT VACUUM SYSTEM FAILED. THE AIRCRAFT RETURNED TO MAINTENANCE AND AN INSPECTION OF THE SYSTEM FOUNDED THAT THE ROTOR HAD FROZEN UP AND THE SHAFT HAD SHEARED. PUMP WAS REMOVED AND A NEW PUMP INSTALLED. OPERATIONAL CHECK OF THE SYSTEM CSDR VJ32002F00032Pump · shearedMETAL SHAFT SHEARED IN PUMP. REMOVED AND INSTALLED NEW PUMP, SYSTEM OPERATIONAL CHECKED NORMAL. PUMP SENT IN FOR WARRANTY.SDR DLM88020498Clamp · looseTAIL COMPT HIGH WARNING DURING CLIMBOUT CA FOUND RT CROSSBLEED VALVE CLAMP LEAKING TIGHTENED CLAMPLK CKS GOOD.SDR VJ32002F00028Pump · inoperativeLOW OUT PUT FROM PUMP TO AIRCRAFT, REMOVED PUMP AND INSTALLED NEW PUMP OPERATION WAS NORMAL. PUMP SENT IN FOR WARRANTY.SDR WVE2002F00008Sleeve · missingAIRCRAFT ARRIVED FOR 600/1200 INSPECTION WITH FAIL SAFE SLEEVE MISSING FROM BLEED AIR MANIFOLD, PN 6019060-8 AS SHOWN IN IPC 36-10-09. PROBABLE CAUSE: MECHANIC FAILED TO INSTALL SLEEVE, POSSIBLY DUE TO ERROR IN THE PROCEDURE FOR BLEED AIR COUPLING INSTALLATISDR 2002FA0000473Pump · inoperativeLOW OUT PUT FROM PUMP TO AIRCRAFT, REMOVED PUMP AND INSTALLED NEW PUMP, OPERATION WAS NORMAL. PUMP SENT IN FOR WARRANTY.SDR 2002FA0000478Pump · damagedMETAL SHAFT SHEARED IN PUMP. REMOVED AND INSTALLED NEW PUMP, SYSTEM OPERATIONAL CHECKED NORMAL. PUMP SENT IN FOR WARRANTY.SDR C1HA200293003Flow Valve · inoperativeDuring climbout, unable to pressurize cabin above 1 PSI diff. Action Taken: Removed and replaced right flow control valve. Ops and leak check good on ground IAW MM 36-10-02.SDR ZKG2002F00001Cooler · crackedPRECOOLER CRACKED ON RIGHT ENGINE INBOARD AFT. THIS IS THE 2ND AC WITH THE SAME TROUBLE IN LESS THAN ONE WEEK.SDR 2002F00378Pilot Valve · inoperativeDURNG TAXI, LEFT DUCT PRESSURE FLUCTUATES. AIRCRAFT RETURNED TO GATES. MAINTENANCE REPLACED THE HIGH STAGE PILOT. (M)SDR 2002F00380Shutoff Valve · inoperativeDURING CRUISE EICAS MESSAGE LEFT ENGINE HIGH STAGE DISPLAYED, L HIGH STAGE LGT ILLUMINATED, DUCT PRESSURE NORMAL. AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED HPSOV PER MM 36-11-07. (M)SDR AALA20020061Duct · defectiveBOS - FLT 1229 - BOS-ORD - AFTER TAKEOFF, TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED. LANDED BOS WITHOUT INCIDENT. REPLACED RUPTURED DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR VNAA0112017Bleed Valve · failedDURING TAKE OFF THE CREW RECEIVED A BLEED VALVE SHUTOFF FAIL MESSAGE AND ABORTED TAKE OFF. THE CREW CALLED MAINTENANCE CONTROL AND RESET THE SYSTEM. FLIGHT 4062 WAS CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS.SDR VNAA0108020Valve · failedDURING CLIMB THE LEFT BLEED VALVE NEVER OPENED. AFTER TROUBLESHOOTING WITH MAINTENANCE CONTROL THE CREW WAS ASKED TO RETURN TO PIT. UPON ARRIVAL AT PIT, MAINTENANCE INSPECTED AND REPLACED THE FLOW CONTROL SHUT OFF VALVE IN ACCORDANCE WITH DORNIER MAINTENANCESDR C2XA01CL193Hose · blownCLE FLIGHT#3860 THE CREW SHUT DOWN THE #1 ENGINE ON LANDING INTO CLEVELAND DUE TO A #1 ENGINE BLEED LEAK WARNING AND PRESSURIZATION PROBLEM.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE BLEED DUCT HOSE HAD BLOWN OFF BETWEEN TSDR COMA0160423Valve · leakingR/H 14TH STAGE DUCT WARNING MESSAGE AND ANTI-ICE DUCT WARNING.FOUND 14TH STAGE BLEED VALVE LEAKING, REMOVED AND REINISTALLED VALVE.SDR DL738010957Controller · failedIRR/ NBR 1 ENG BLEED TRIP OFF LIGHT ILLUMINATED AS A/C LEVELED OF FL350. REPLACED BLEED AIR CONTROLLERSDR AALA20011198ClampDFW - FLT 552 - EN ROUTE DFW-PIT, DETECTED TAIL HIGH TEMPERATURE LIGHT ILLUMINATE IN COCKPIT. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. RE-SECURED CLAMP AT LEFT SIDE ACY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA20011182Sensor · defectiveDFW - FLT 1612 - EN ROUTE DFW-LIT, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED TAIL COMPARTMENT HIGH TEMPERATURE SENSORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA20011183Clamp · defectiveLAX - FLT 335 - EN ROUTE LAX-SJD - SHORTLY AFTER TAKEOFF TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. RETURNED LAX AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE AUGMENTATION VALVE CLAMP. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERSDR SIMA200114809O-Ring · wornORD - FLT 4112 - CREW REPORTED ENGINE TWO BLEED LEAK LIGHT CAME ON AFTER TAKEOFF. CREW RETURNED AIRCRAFT TO ORD. MAINTENANCE REPLACED O-RINGS AT COUPLING UNDER AFT PASSENGER SEAT NEAR THE LAVATORY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SDR AALA20011125ClampDFW - FLT 1580 - EN ROUTE DFW-DCA, TAIL HIGH TEMP LIGHT ILLUMINATED. RETURNED DFW LANDED WITHOUT INCIDENT. REPOSITIONED CLAMP ON LEFT PACK ANTI-ICE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AAL20011035DuctORD - FLT 1666 - EN ROUTE ORD-ALB, TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED DURING CLIMB-OUT AT 24,000 FEET. RETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED UPPER RETURN SYSTEM AIR CONDITIONING DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR DL76L010540Engine · malfunctionedON T/O GOT RT HP BLEED AND FOLLOWED POM. RETURNED TO CVG. REPLACED NBR 2 ENG HPSO VALVE PER MM 36-11-07-4-03 NO FURTHER FAULTS.SDR DHL2001366008Control Box · failedDURING BEFORE T/O CHECKLIST, PRESSED MWP RECALL BUTTON. PNEU LIGHT ILLUMINATED WITH NO CHIME, ALL SYS NORMAL. REMOVED AND REPLACED PRESS SEQ BOX IAW 21-31-00, OPS NORMAL.SDR DHL2001366007Controller · malfunctionedRETURNED TO BLOCK ON TAXI OUT. PNEUMATIC LIGHT ON MWP AND CHIME SOUNDED. ALL SYSTEMS APPEAR NORMAL. LIGHT WOULD NOT EXTINGUISH. SWAPPED PNEUMATIC CONTROLLERS FOR TROUBLESHOOTING. PERFORMED BITE CHECK. BOTH CHECK NORMAL IAW 36-10-01.SDR 2001UALA00082Smoke · detectedSMOKE IN THE COCKPIT. *S/D* THREE WIRE SOCKETS IN CONNECTOR D96 BROKE OFF AND SHORTED TOGETHER. REPLACED THE SOCKETS.SDR C2XA00CL099Duct · crackedCLE: CREW REPORTED NR 1 BLEED LEAK INDICATION AFTER TAKEOFF IN CLEVELAND. A/C RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND THE BLEED DUCT CRACKED ON LEFT SIDE IN THE AFT AVIONICS COMPARTMENT. DUCT WAS REPLACED IAW 36-12-02 & 36-11-09.SDR VNAA0011006Bleed Valve · failedDAY - FLT 4026 - AFTER TAKING THE RUNWAY AND AS POWER WAS ADVANCED THE PUT BLEED SHUTOFF VALVE FAILED. MAINTENANCE REPLACED THE RIGHT LP BLEED VALVE. THE AIRCRAFT DEPARTED WITH FURTHER INCIDENTS. (M)SDR HALA0000341Controller · failedPDX - FLT 25 - NR 3 MANIFOLD FAIL LIGHT CAME ON DURING FLIGHT. FOLLOWED CHECKLIST AND TURNED OFF NR 3 PNEU AND NR 3 PACK. PRESSURIZED PNEU SYSTEM 3. INSPECTED ALL DUCTING FOR LEAKS. NONE FOUND. INSPECTED WIRING TO DETECTORS IN WING, RES SWITCH AND LOOPS.
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