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 = '150M' 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 = '150M' 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 CA090411001Bulkhead · cracked(CAN) PROPELLER BULKHEAD CRACKED.SDR CA090321002Valve Spring · unserviceable(CAN) INTERMITTENTLY ENGINE WOULD RUN ROUGH - CYLINDER LOW COMPRESSION. FOUND ONE OF THE LOCKS OUT OF POSITION RESULTING IN VALVE SEAT EXTENDING HIGHER AND RESULTING IN POSSIBLE CONTACT WITH ROCKER ARM. ROCKER ARM NO SIGNS OF DAMAGE NOTED. CYLINDER REPLACED SDR CA090329001Tube · defective(CAN) POTENTIAL RUBBER OR MFG DEFECT.SDR CA090401015Tube · defective(CAN) POTENTIAL RUBBER OR MANUFACTURING DEFECT.SDR CA090329004Tube · defective(CAN) POTENTIAL RUBBER OR MFG DEFECT.SDR CA090329002Tire · defective(CAN) POTENTIAL RUBBER OR MFG DEFECT.SDR CA090329003Tube · defective(CAN) POTENTIAL RUBBER OR MFG DEFECT.SDR CA081212011Switch · unserviceable(CAN) HAD STARTER FAILURES WHERE THEY SEIZED AND OVERHEATED. INVESTIGATION REVEALED THAT IF PILOT AGGRESSIVELY ROTATED KEY IN CLOCKWISE DIRECTION THAT KEY WOULD JAM AND LEAVE SWITCH IN THE START POSITION. THIS WOULD CAUSE THE STARTER TO REMAIN ENGAGED UNTIL SDR CA090406007Stiffener · cracked(CAN) SEAT RAIL SUPPORT STIFFENER CRACKED, PART REPLACED WITH NEW.SDR 2007FA0000361Coupling · wornALTERNATOR DRIVE COUPLING WAS WORN AND SEVERELY LOOSE WITH EXCESSIVE PLAY DUE TO SOFT, UNDERCUT BUSHINGS PN 632050. IN ADDITION, THE DRIVE HUB KEY WAY WAS SEVERELY WORN CAUSING EXCESSIVE PLAY OF THE HUB ON THE SHAFT. CONTINUED OPERATION WOULD RESULT IN DRIVESDR CA070114001Exhaust Valve · leaking(CAN) DURING ENGINE PERFORMANCE GROUND RUN AFTER INSPECTION, ENGINE WAS RUNNING ROUGH. ENGINE COMPRESSION CHECK CARRIED OUT AND CYLINDER NR 3 FAILED COMPRESSION CHECK AND AIR WAS LEAKING FROM THE EXHAUST. ROUGH RUNNING DURING TAKEOFF WAS ALSO REPORTED BY PILOSDR 2006FA0001077Cylinder · crackedOIL LEAK LEAD TO FINDING CYLINDER BARREL CRACKED, MID SECTION IN COOLING FINS, .7500 WAY AROUND BARREL. (K)SDR CA061219009Relay · stuck(CAN) POWER ON STARTER WITH WHEN MASTER SWITCH ON. FOUND MASTER RELAY STUCK IN POSITION. NEW RELAY S-1991-A1 INSTALLED.SDR 2006FA0000684Fitting · misinstalledON PREFLIGHT INSP, APPLIED A +/- 5 LB UP AND DOWN FORCE ON RT STABILIZER TIP, HEARD A GRUNTING SOUND. FURTHER INVESTIGATION REVEALED A SMALL RELATIVE MOTION BETWEEN STABILIZER AFT FITTING, 0432005-2, AND FUSELAGE. REMOVING NUT OPENED A 0.020 INCH AIR GAP SDR 2006FA0000685Fitting · looseON PREFLIGHT INSP, APPLIED A +/- 5 LB UP AND DOWN FORCE ON RT STABILIZER TIP AND HEARD A GRUNTING SOUND. FURTHER INVESTIGATION REVEALED A SMALL RELATIVE MOTION BETWEEN STABILIZER AFT FITTING, 0432005-2, AND FUSELAGE. REMOVING NUT, OPENED A 0.020 INCH AIR GASDR CA060707005Fitting · corroded(CAN) DURING 100 HOUR INSPECTION AME FOUND WHAT APPEARED TO BE A CRACK IN THE RADIUS OF THE LT FLANGE OF THE LT FITTING ATTACHING THE VERTICAL FIN TO THE HORIZONTAL STABILIZER. WHEN THE PART WAS REMOVED FROM THE AIRCRAFT THE LT FLANGE WAS FOUND TO BE BENT TOWSDR CA070207005Pump · failed(CAN) ON ADDING FULL POWER THE ENGINE STALLED AND STOPPED RUNNING. - FOUND TO BE THE ACCELERATOR PUMP WAS NOT WORKING PROPERLY. (TC NR 20070207005)SDR CA051222005Shaft · brokenELECTRICAL FAILURE ALTERNATOR REMOVED SHAFT FOUND BROKEN ALTERNATOR STILL TURNS NOT SEIZED. DRIVE GEAR AND CAM GEAR FOUND WORN DUE TO DRIVE GEAR BEING NOT ATTACHED TO THE ALTERNATOR. ALTERNATOR REPLACED CAM AND DRIVE GEAR, RETAINER AND BUSHINGS REPLACED.SDR CA050926002Rocker Boss · failed(CAN) ON INSPECTION, BRASS AND ALUMINUM PARTICLES FOUND IN FILTER. ROCKER BOSSES AND BUSHINGS FOUND WORN. THIS SHOWS UP AT ABOUT 200 HRS IN SERVICE AND HAS HAPPENED TO ALL CYLINDERS THAT ARE FACTORY NEW IN THE LAST COUPLE OF YEARS. ACCORDING TO THE FACTORY WESDR 2005FA0000609Mount · cracked100 HOUR INSPECTION, RT LOWER ENGINE MOUNT TUBE CRACKED. CRACK LOCATED WITHIN 1 INCH OF NOSE WHEEL STRUT SUPPORT CRACK, .7500 INCH IN LENGTH AROUND CIRCUMFERENCE OF TUBE. REPLACED MOUNT. (K)SDR RTE2005F00001Clutch · crackedDURING 100 HOUR INSPECTION ROUTINE MAINTENANCE OF THE STARTER DRIVE CLUTCH, INSTALLED UNDER STC NR SE995GL DATED 08 SEPT 86, FOUND BEARING RACE CRACKED AND SEVERAL ROLLERS LOOSE ENOUGH TO FALL OUT OF THE RACE. THIS ITEM REQUIRES DISASSEMBLY, CLEANING AND LUBRSDR CA050404003Magneto · failed(CAN) ON LANDING, ENGINE BECAME NOTICEABLY ROUGH. AFTER LANDING A MAGNETO CHECK WAS ACCOMPLISHED. THE MAG CHECK REVEALED THAT THE RT MAGNETO WAS NOT FIRING. UPON INSPECTION OF SAME IT WAS DISCOVERED THAT THE INTERNAL NYLON GEAR HAD FAILED (TEETH STRIPPED). SDR 2005FA0000177Magneto · brokenFLANGE BROKEN ON RT SIDE FOR SUPPORT OF MAG. FOUND ON ANNUAL INSP. 4001 MAG TT 394. (K)SDR CA041109004Control Cable · corroded(CAN) AILERON CONTROL CABLE FOUND CORRODED AT COPILOT FOOT AREA. THIS PROBLEM HAS BEEN NOTICED ON OTHER CESSNA 150. SUSPECT DIRT FROM SHOES CAUSING CORROSION. TO SEE THE CABLE YOU NEED TO REMOVE COVER (YOKE) AND MOVE AILERON TO TRAVEL LIMITS.SDR CA040830001Exhaust Valve · eroded(CAN) ENGINE PLACED ON (PISTON ENGINE ON CONDITION PROGRAM). DURING ON-CONDITION 100 HOUR INSPECTION, THE NR 2 CYLINDER COMPRESSION TEST WAS LOW AND LEAKING FROM VALVES. ON FURTHER INSPECTION, EXHAUST VALVE STEM WAS FOUND TO BE ERODED TO ABOUT HALF OF DIAMETESDR CA040610010Line · corroded(CAN) FUEL LINE ASSEMBLY LOCATION/LOCATED UNDER FLOOR AND UNDER CENTER CONSOLE. THIS LINE IS DIRECTLY FORWARD OF THE BELLY DRAIN. IT IS UP STREAM FROM THE GASCOLATOR AND DOWN STREAM OF THE FUEL SHUT-OFF. FUEL SMELL WAS DETECTED. FUEL STAINING WAS PRESENT. THSDR CA040520003Retaining Ring · dislodged(CAN) STARTER GEAR RETAINING RING (P/N 6401740) DISENGAGED FROM THE STARTER SHAFT AND LODGED IN THE STARTER GEAR NEEDLE BEARING (P/N 639788). THE NEEDLE BEARING FAILED WITH THE BEARING NEEDLES ENTERING THE ENGINE REAR CASE AND OIL SYSTEM. THE NEEDLES IN THE OSDR 2004FA0000362Bolt · corrodedWHEN PERFORMING MAINT. ON A/C, NOTED RUST ON HEADS OF MAIN SPAR WING ATTACHING BOLTS. REMOVED BOLTS FINDING THEM BADLY CORRODED AND RUSTED. INSPECTED FUSELAGE BEARING BORE AND SPAR BOAR AND INSTALLED NEW AN8-24A BOLTS. AGE AND ENVIRONMENT MAY BE PROBLEM, RECOMSDR CA040225015Bolt · broken(CAN) PROPELLER BOLTS WERE BEING INSTALLED AND TORQUED TO THE SPECIFIED VALUE OF 25 - 30 POUNDS FOOT. AS THE TORQUE WAS REACHING APPROXIMATELY 27 FOOT POUNDS, THE BOLT BROKE. THE BREAK WAS WHERE THE THREADS MEET THE GRIP. A SECOND BOLT WAS TORQUED AND IT BROKESDR CA040310008Bolt · sheared(CAN) UPON APPLICATION OF 27 FT/LBS TO 2 OF THE MOUNTING BOLTS AT THE THREADS FAILED. BOLTS FORWARDED TO COMPANY FOR EVALUATION.SDR CA040308001Bolt · broken(CAN) DURING INSTALLATION OF THE PROPELLER, WHEN TIGHTENING THE BOLTS TO THE SPECIFIC TORQUE OF 25-30 POUNDS FOOT. ONE OF THE BOLTS BROKE AT APPROXIMATELY 27 POUNDS FOOT. THE BOLT BROKE AT THE BASE OF THE THREADS NEAR THE START OF THE GRIP. A SECOND BOLT WASSDR 2004FA0000159Hinge Pin · brokenDURING A 100 HOUR INSPECTION, THIS BROKEN DOOR HINGE PIN WAS FOUND. FIND MANY OF THESE PINS BROKEN.(K) (NE01200402925)SDR 2003FA0001279Frame · crackedCRACKED FRAME AT TB/VERTICAL FIN SPAR JUNCTION. THIS IS THE SECOND SHIP WITH AN IDENTICAL CRACK THAT HAS BEEN SEEN IN THE LAST 90 DAYS. THE MFG SRM DETAILS THE REQUIRED REPAIRS. DETECTION IS POSSIBLE USING BRIGHT LIGHT AND MIRROR, OR BY DIRECT OBSERVATION. ASDR CA031119003Carburetor · iced(CAN) DEPARTING, CLIMBED UP TO CRUISING ALTITUDE OF 4,500 FT, STARTED DESCENT BY REDUCING POWER FROM 2,500 RPM TO APPROX 2,350 RPM. TEMP WAS -2 AND DEWPOINT -9 FOR 6,000 FT. GOT DOWN TO 3,500, LEVELED OFF, WENT TO ADD POWER FOR CRUISE, ENG SPUTTERED, WENT TO ISDR 2003FA0001098Rocker Boss · failedON APRIL 19, FLYING BACK TO LGU, THE ENGINE SUDDENLY BEGAN VIBRATING AND LOST A LOT OF POWER. COULD NOT MAINTAIN ALTITUDE, LANDED IN A FIELD. MECHANIC CAME AND FOUND THAT THE ROCKER BOSSES OF CYL NR 3 HAD FAILED. INSTALLED AN NEW CYLINDER ASSY AND FLEW IT BASDR CA030827002Exhaust Valve · eroded(CAN) DURING THE BOROSCOPE INSPECTION OF THE ON-CONDITION PROGRAM, SPECIAL EFFORT WAS MADE TO INSPECT THE EXHAUST VALVE AS WE HAD FOUND A PREVIOUS VALVE OF THE SAME PART NUMBER IN POOR CONDITION. THE NR 2 CYLINDER EXHAUST VALVE WAS FOUND SEVERELY ERODED 1/3 TSDR CA030703017Exhaust Valve · corroded(CAN) UPON INSTALLATION OF CYLINDERS AFTER OVERHAUL OF CRANKCASE THE EXHUAST VALVE IN ONE CYLINDER WAS NOTICED TO BE BADLY CORRODED AND ERODED AT THE NECK OF THE VALVE.ALL OTHER EXHAUST VALVES WERE INSPECTED SERVICEABLE AND THE ONE WILL BE REPLACED. IT SHOULDSDR CA030626009Cylinder Head · worn(CAN) ON INSPECTION FINE BRONZE PARTICLES FOUND IN OIL FILTER & SCREEN. FURTHER INVESTIGATION REVEALED ROCKER ARM BUSHINGS WORN. ALSO CYLINDER HEAD BOSSES WORN. THE ROCKER SHAFTS ON THESE NEW STYLE CYLINDERS ARE HELD IN PLACE WITH SET SCREWS WHICH SEEM TO LOOSSDR CA030702005Fitting · cracked(CAN) DURING PREFLIGHT INSPECTION PILOT NOTICED CRACK, PARALLEL ALONG 90 DEGREES ANGLE.SDR CA030627007Screw · loose(CAN) ROCKER SHAFT SET SCREW BECAME LOOSE AFTER 148.1 HRS OF OPERATION AND WORE THE ROCKER SHAFT BOSS IN CYLINDER HEAT MAKING THE CYLINDER UNSERVICEABLE.SDR CA030514012Starter · blocked(CAN) ON ENGINE START UP, PILOT NOTICED THAT THE PROP WAS NOT TURNING. AFTER INVESTIGATION WE DISCOVERED THAT THE STARTER WAS DEFECTIVE.SDR CA030423004Rib · cracked(CAN) LEADING EDGE RIB ASSEMBLIES ARE VERY DIFFICULT TO SEE.THE USE OF A MIRROR THROUGH THE HORIZONTAL SPAR AND RIB LIGHTNING HOLES IS THE ONLY WAY TO SEE THE CRACKS ALONG THE TABS.I HAVE INCLUDED TWO PHOTOS. ONE OF THE PHOTOS SHOWS A NEW PART AND WERE THE LOCSDR CA021119005Blade · improper part(CAN) PROPELLER HAD BEEN WELDED TO COVER UP DEFECTS. PROPELLER IS SCRAP. THIS IS A REOCCURRING PROBLEM.SDR CA021022004Fan · broken(CAN) ON VISUAL INSPECTION NOTICED COOLING FAN'S FINS BROKEN AND METAL STIFFENER BROKEN IN HALF, INSIDE THE ALTERNATOR CASE.SDR CQ92002F00000Metering Valve · scoredA/C WAS ON TRAINING FLIGHT, AT 4000 FT, INSTRUCTOR DEMONSTRATED LEANING PROCESS BY PULLING OUT MIXTURE CONTROL UNTIL ENGINE ROUGHNESS JUST OCCURRED. ENRICHENING MIXTURE HAD NO EFFECT, AND A EMERGENCY LANDING WAS MADE WITHOUT POWER. INITIAL INSP SHOWED THAT SDR CA020903004Hub · worn(CAN) IN FLIGHT ALTERNATOR FAILURE. DURING TROUBLESHOOTING, FOUND THE HUB COMPLETELY WORN OUT, THEREFORE THE GEAR COULD NO LONGER ROTATE THE ALTERNATOR.SDR 2002FA0001168Engine · malfunctionedAIRCRAFT LANDED ON THE ROADWAY BECAUSE PILOT STATED HE COULD NOT AMINTAIN ALTITUDE AT 1200 FT, THE ENGINE STARTED BACKFIRING AND SOUNDED LIKE IT WAS MISSING. ALL OTHER INSTRUMENTS APPEARED NORMAL, AND THE WEATHER WAS CLEAR AND 85 DEGREES. THIS WAS NOT THE SDR CA020812005Pin · missing(CAN) TWO PERMANENT PINS THAT HOLD THE SPUR GEAR TO THE ROTATING SHAFT OF THE TRIM TAB ACTUATOR HAD FALLEN OUT AND WENT MISSING. TRIM CONTROL WAS IMPOSSIBLE DUE TO SLIPPAGE OF THE SPUR GEAR IN THE SHAFT. ACTUATOR REPLACED WITH NEWLY OVERHAULED UNIT.SDR 2002FA0000884Bulkhead · crackedCRACKS THROUGH BULKHEAD. TIE DOWN PROBLEMS/ LANDINGS TAIL LOW. REPETITIVE TAIL LOW LANDINGS.SDR 2002FA0000495Bushing · failedEIGHT BUSHINGS FAILED WITHIN 15 HOURS OF OPERATION. THE PROBLEM WAS INDICATED BY BRASS METALIC DUST IN THE OIL FILTER. THIS LOOKED SIMILAR TO METALIC PAINT FLAKE SUSPENDED IN THE OIL. THE ROCKER ARMS WERE REMOVED AND BUSHING CLEARANCE WAS MEASURED. THE WEA
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