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 = '1900' 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 = '1900' 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 JIKA2024052901Hydraulic Line · chafedDURING LANDING, THE FLIGHT CREW ATTEMPTED TO LOWER THE GEAR NORMALLY. IT WAS OBSERVED THAT THERE WAS A LOW HYDRAULIC LIGHT FLICKER INDICATING A LOSS OF PRESSURE. THE FLIGHT CREW THEN EXTENDED THE LANDING GEAR THROUGH MANUAL EXTENSION AND LANDED THE AIRCRAFT SASDR JIKA2024021601Wire Harness · shortedWHEN THE FLIGHT CREW PLACED THE LANDING GEAR HANDLE IN THE DOWN POSITION THE CIRCUIT BREAKER POPPED AND CAUSED THE LANDING GEAR INDICATION LIGHTS TO COMPLETELY EXTINGUISH. THE PILOT RESET THE CIRCUIT BREAKER AND CYCLED THE LANDING GEAR HANDLE ONCE MORE, BUT THSDR JIKA2019101701Packing · leakingAPPROXIMATELY 1HR INTO FLIGHT, RIGHT ENGINE OIL PRESSURE DROPPED TO 40PSI ACCOMPANIED WITH LOW OIL PRESSURE WARNING ANNUNCIATOR LIGHT. CREW COMPLIED WITH CHECKLIST ACTION TO SECURE THE RIGHT ENGINE. THE FLIGHT WAS CONTINUED TO DESTINATION WITH SINGLE ENGINE ASDR JIKA2018100201Unknown · smokeTHE PILOT REPORTED THAT WHILE INFLIGHT THERE WAS SMOKE OR VAPOR COMING FROM UNDERNEATH THE PILOT AND CO-PILOTS SEATS, WHERE THE FLOOR VENTS ARE LOCATED. THE ENVIRONMENTAL BLEED AIR HAD BEEN TURNED ON AND THERE WAS NO SMELL ASSOCIATED WITH THE SMOKE OR VAPOR OBSDR JIKA2018100192701Circuit Breaker · defectiveDISCREPANCY: THE PILOT REPORTED ON APPROACH INTO KBUR, THE CREW SELECTED THE GEAR LEVER TO DOWN. THE THREE GREEN GEAR INDICATORS DID NOT ILLUMINATE. THE CREW ELECTED TO MANUALLY EXTEND THE GEAR AND THE THREE GREEN GEAR INDICATORS ILLUMINATED. THE AIRCRAFT LANDSDR JIKA2018060453002Filter · contaminatedTHE PILOT REPORTED DURING TAKEOFF, THAT THE RIGHT LOW PRESSURE FUEL PUMP FAIL INDICATION ILLUMINATED. THE PILOT ACTIVATED THE RIGHT BOOST PUMP. THE FUEL PUMP FAIL INDICATION EXTINGUISHED. THE PILOT DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. MAINTENANCSDR JIKA201806043001Filter · contaminatedTHE PILOT REPORTED AFTER TAKEOFF, THAT THE RIGHT LOW PRESSURE FUEL PUMP FAILED INDICATION ILLUMINATED. THE PILOT ACTIVATED THE RIGHT BOOST PUMP. THE FUEL PUMP FAILED INDICATION EXTINGUISHED. THE PILOT DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. MAINTENSDR JIKA2018032301Unknown · smokeTHE PILOT REPORTED DURING APPROACH, THERE WAS AN UNUSUAL ODOR FOLLOWED BY LIGHT SMOKE IN THE COCKPIT. THE PILOT FOLLOWED PROCEDURES AND TURNED THE BLEED SYSTEM TO THE OFF POSITION AND REPORTED THE SMOKE DISSIPATED. LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DSDR JIKA2016052301Fuel Cell · leakingEN-ROUTE THE PILOT REPORTED A STRONG FUEL ODOR FROM THE CABIN AREA. DEPRESSURIZED THE CABIN, USED OXYGEN & OPENED THE FRESH AIR VENTS, LANDED WITHOUT INCIDENT. INSPECTED THE ACFT, THE INSPECTION INCLUDED REMOVING THE CABIN FLOORBOARDS & INSPECTING FOR ANY SISDR JIKA201512081501Fuel Control · low pressureEN-ROUTE, THE PILOT REPORTED THAT THE RT ENG TORQUE STARTED TO DROP OFF. THE PILOT WAS ABLE TO MATCH TOQUE BY ADVANCING THE RT POWER LEVER. DURING APPROACH, THE RT ENG BEGAN TO SURGE. THE PILOT PERFORMED A PRECAUTIONARY IN FLIGHT SHUTDOWN OF THE RT ENG. DESDR CA141103001Engine · power loss(CAN) DURING THE CRUISE THE CAPTAIN NOTICED THE NR 1 ENGINE SHOWING 93% N1 MAX AND SHORTLY AFTER NOTICING THIS, THE LH GENERATOR FAILED. THE CREW THEN ATTEMPTED TO RESET THE GENERATOR BUT THE GENERATOR DID NOT COME BACK ONLINE. THE LH ENGINE OIL LOW ANNUNCIATOSDR GLBA2013021500177Bulb · inoperativePILOT REPORTED THAT THE EMERGENCY LIGHTS ON THE F/O'S SIDE DO NOT ILLUMINATE AND ARE ALSO INOPERATIVE IN INDIRECT LIGHT MODE. MX REPLACED THE BULBS AND SECURED WIRING, OPS CHECKED GOOD.SDR HSYA20110307001Torque Link · damagedRT MLG TORQUE LINK DISCONNECTED AT START OF ACFT TAXING FROM BLOCKS. UPON INSP, MX DISCOVERED INCORRECT WASHER INSTALLATION AT UPPER AND LOWER TORQUE LINK ATTACH POINT.SDR GUUA94055030609DSpar Cap · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT HORIZONTAL STABILIZER UPPER REAR SPAR CAP HAS EXFOLIATION. REPLACED RIGHT HORIZONTAL STABILIZER UPPER REAR SPAR CAP.SDR GUUA94055030609CHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR OTBD HINGE BRACKET HAS SURFACE CORROSION. REPLACED RT ELEVATOR OUTBOARD HINGE BRACKET.SDR GUUA94055030609BHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CENTER HINGE BRACKET.SDR GUUA93352011609ADoor · stiffDURING SCHEDULED ROUTINE MX, DISCOVERED RT FWD EMERGENCY EXIT HARD TO OPEN. LUBRICATED RT FWD EMERGENCY EXIT DOOR OUTSIDE HANDLE. OPS CHECK OK.SDR TAS07003Cap · crackedMLG ACTUATOR WAS RECEIVED DUE TO INDICATIONS FOUND IN THE END CAP DURING ULTRASONIC TESTING. ACTUATOR WENT THROUGH A PRELIMINARY INSPECTION AND A COMPLETE FUNCTIONAL TEST WITH NO EXTERNAL EVIDENCE OF LEAKING OR CRACKING. AFTER DISASSEMBLY, A CRACK IN THE INTSDR TIM2005F00003Skin · corrodedCORROSION FOUND ON LT AND RT ELEVATOR: AFT LOWER SPAR CAP LT SIDE, AFT LOWER SPAR CAP RT SIDE, LT OB HINGE, RT OB HINGE, RT CENTER HINGE, LT ELEVATOR TRIM TAB PUSH ROD, RT ELEVATOR TRIM TAB HORN. (K)SDR TIM2005F00002Skin · corrodedCORROSION FOUND ON SKIN FS243-FS273 AND STRINGERS 14L-15R. (K)SDR HSY2005F00001Sensor · defective(MRR NR 01-011405) LOSS OF NR 1 ENGINE OIL PRESSURE. LOOSE AND LEAKING OIL TEMPERATURE SENSOR. LOOSE BUT IN SERVICEABLE CONDITION. REMOVED TEMPERATURE SENSOR, INSPECTED, AND REINSTALLED. RAN ENGINE AND FOUND NO FURTHER DEFECTS. (NM05200502782) (K)SDR TIM2004F00000Tube · pin holeWHILE DOING A ROUTINE INSPECTION, IT WAS NOTICED HYDRAULIC FLUID ON THE LOWER PORTION OF THE LT IB WING. AFTER CLEANING THE AREA AND PERFORMING A RETRACTION TEST, IT WAS DETERMINED THAT THE RETRACTION TUBE HAD A PIN HOLE IN IT. COULD NOT GUESS ON THE PROBABLSDR GLBA2003072Pressure Switch · malfunctionedRIGHT EVIR ILLUM, ON T/O ROLL. CHECKED THE PRESSURE SOLENOID FOR OPERATION AND LEAKAGE AND RIGHT PROP PRESSURE SWITCH FOR PROPER OPERATION, BOTH GOOD. CHECKED RIGHT ENVIR TEMP AND PRESSURE, OPS CHECK GOOD.SDR GLBA2003070Filter · dirtyAIRCRAFT WILL NOT PRESSURIZE. CLEANED PRESSURE CONTROLLER FILTER, OPS CHECK GOOD.SDR GLBA2003071Switch · out of adjustAIRCRAFT RETURNS, FLAPS WILL NOT RETRACT. ADJUSTED FLAP SAFETY SWITCH, OPS CK GOOD.SDR TIM2002F00010Angle · brokenANGLE LOCATED ABOVE THE ICE DOOR HINGE. THIS ANGLE HOLDS THE LOWER FIRE SEAL BULK HEAD WHEN THIS ANGLE CRACKS, IT ALLOWS THE OUTSIDE COWL RIVETS TO WORK LOOSE, AND THIS CAUSES THE COWL SIDE SKIN TO CRACK.SDR AUS20020164Light · failed(AUS) RH MAIN LANDING GEAR POSITION LIGHT FAILED.SDR TIM2002F00009Bolt · corrodedBOLT PN 908200115, CONNECTING NOSE GEAR DRAG BRACE TO NOSE STRUT, AND BOLT PN 908200111 CONNECTING THE TWO DRAG BRACE HALVES WAS FOUND WITH PITTING TYPE CORROSION.SDR OYG2002F00000Cowling · crackedSEVERAL CRACKS WERE FOUND ON THE INSIDE OF THE AIR INLET COWL (HOT LIP) THESE CRACKS RUN HORIZONTALLY AND VERTICALLY ALONG THE WELD THE POSSIBLE CAUSE MIGHT BE THE HARMONICS OF THE VIBRATIONS FROM THE ENGINE AND PROPELLER. POSSIBLY GOING TO A THICKER GAUGE OFSDR TIM2002F00004Cable · brokenAIRSTAIR DOOR CABLE BROKE, ALLOWING ONE SIDE OF THE DOOR TO REMAIN UNLOCKED.SDR 2003F00020Angle · crackedGJT - LEFT ENGINE NACELLE LOWER AFT BULKHEAD HAS SEVERAL CRACKS. REPLACED THE LEFT ENGINE COWLING REINFORCEMENT ANGLE, THE ENGINE TRUSS BRACKET RECEPTACLE, AND THE UPPER AFT ANGLES. THE REPAIRS WERE COMPLETED 12-03-01 TAT 21, 140.9. (M)SDR 2003F00019Bracket · crackedGJT - LEFT ENGINE NACELLE LOWER AFT BULKHEAD HAS SEVERAL CRACKS. STRUCTURAL REPAIRS ARE IN PROGRESS. (M)SDR TIM2001F00011Wire · brokenTHE ICE VANE CONTROL WIRE NUMBER 20A20 BROKE AT THE TERMINAL END UNDER THE PANEL AT INST ZONE 245 CAUSING A SHORT WHICH CAUSED SMOKE IN THE COCKPIT.SDR TIM2001F00009Bulkhead · crackedTHE LEFT COWLING BULKHEAD AT STATION 238.18 THAT THE LOWER FRONT ENGINE COWLING ATTACHES TO WAS BROKEN OUT ON THE RIGHT LOWER SIDE. THE LOCATION IS WHERE ONE OF THE FOUR BOLTS SECURE THE COWL TO THE BULKHEAD. PICTURES INCLUDED.SDR 2001F00623Shaft · defectiveINSPECTION OF FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE RIGHT OUTBOARD FLAP CABLE DEFECTIVE. THE INNER SHAFT RETAINER WAS NOT ATTACHED TO THE FERRULE AS REQUIRED. (M)SDR TIM2001F00006B-Nut · looseOIL LINE TO THE TORQUE MANIFOLD, B-NUT CAME LOOSE, OIL PRESSURE FLUCTUATED AND ENGINE SHUT DOWN. AIRCRAFT LANDED. ENGINE WAS INSPECTED AS PER MM, LOW OIL PRESSURE PROCEDURE. NO DAMAGE FOUND - OIL SERVICED AND ENGINE TEST RUN PER P/W CHECK.SDR GUU2001F00008Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M)SDR GUU2001F00007Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS ON INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET. (M)SDR 2001F00089Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, LEFT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR CENTER HINGE BRACKET. (M)SDR 2001F00088Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M)SDR ME42001F00000Spring · brokenHARTZELL PROPELLER MODEL NUMBER HC-B4MP-3A/M10877K WITH SERIAL NUMBER FW778 WAS RECEIVED FOR HUB REPLACEMENT IAW AD NOTE 96-18-14. DURING THE DISASSEMBLY, THE SPRING, PN A3496, IN THE SPRING KIT ASSEMBLY WAS NOTED BROKEN. TALKING WITH THE FLIGHT CREW, THEY SSDR 20000925SH017Truss · crackedGJT - RIGHT ENGINE TRUSS MOUNT CRACKED NEAR WELD AT UPPER OUTBOARD ATTACH POINT. AREA ''A''. CRACKED AT TYPICAL LOCATION AS IDENTIFIED IN AD 95-02-18, BEECH SB NR 2255 R6. REMOVED AND REPLACED THE TRUSS ASSEMBLY. THE REPETATIVE INSPECTIONS REQUIRED BY ASDR 20000725AP006Bracket · corrodedDURING ROUTINE MAINTENANCE, RIGHT MIDDLE ELEVATOR ATTACH BRACKET HINGE CORRODED. REMOVED AND REPLACED MIDDLE ELEVATOR HINGE ATTACH BRACKET. (M)SDR MASA00018Bulb · unserviceableFLT 6202 - FLG-PHX - DURING STANDARD PRE-FLIGHT CHECK, THE CREW NOTED THE INSTRUMENT EMERGENCY LIGHT ON THE CAPTAINS SIDE WAS INOPERATIVE. THIS ITEM WAS DEFERRED PER MEL 3302 AND THE AIRCRAFT DEPARTED TO PHX. (M)SDR 20000725AP004Truss · crackedC-2 INSPECTION, RIGHT ENGINE TRUSS HAS A CRACK AT INBOARD COWLING ATTACH BRACKET. REMOVED AND REPLACED RIGHT ENGINE TRUSS. (M)SDR 98ZZZM612Switch · out of adjustFLT 9472 - TLH-TPA - GEAR WARNING HORN SOUNDS WITH GEAR UP AND FLAPS IN APPROACH POSITION. ADJUSTED APPROACH LIMITS SWITCH. OPERATIONAL CHECKS SATISFACTORY. (M)SDR 98ZZZM613Lever · out of adjustFLT 9483 - MIA-MCO - GEAR WARNING HORN SOUNDS WITH GEAR UP AND FLAPS MOVED INTO APPROACH. REPOSITIONED FLAP SELECTOR LEVER GUARD. OPERATIONAL CHECKS SATISFACTORY. (M)SDR 98ZZZX2865Acm · malfunctionedRSW/MIA - FLT 9283 - ON TAKEOFF, SMOKEY SMELL WHEN ACM IS SELECTED. SMELL DISSIPATED AFTER 30 SECONDS. RAN AIRCRAFT ENGINES WITH ACM RUNNING. COULD NOT DUPLICATE. (X)SDR 98ZZZX2261Bearing · failedTACHOMETER/GENERATOR WAS OVERHAULED 55.9 HOURS AGO. UNIT STOPPED WORKING. ON REMOVAL, FOUND DRIVE SHAFT SNAPPED IN TWO. ON DI SASSEMBLY, FOUND BOTH BEARINGS HAD FAILED. THESE BEARINGS HAVE NO IDENTIFYING MARKINGS ON THEM, ONLY ON THE SHIPPING TUBES IS THERESDR 98ZZZX2410Line · crackedEYW/MIA - FLT 5300 - LANDING GEAR DOES NOT RETRACT. REMOVED AND REPLACED RIGHT HAND 'UP' HYDRAULIC LINE. (X)
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