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 = '172N' 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 = '172N' 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 2011FA0000024Lifter · spalledACFT WAS IN FOR INSP AND THE MECHANIC CUT THE OIL FILTER OPEN TO CHECK FOR METAL, THERE WAS METAL IN THE OIL FILTER. THE ENGINE WAS SENT TO US FOR A METAL CONTAMINATION INSP, UPON OUR FINDINGS THERE WERE SEVERAL LIFTER BODIES THAT WERE BADLY SPALLED.SDR 2011FA0000022Lifter · spalledTHE ENGINE HAD A CYLINDER ISSUE, THE MECHANIC CHECKED THE ENGINE FOR METAL IN THE OIL FILTER. THE FILTER HAD METAL IN IT, THE ENGINE WAS SENT TO OUR FACILITY FOR A TEARDOWN INSP. UPON THE TEARDOWN INSP OUR FINDINGS WERE THAT: 4 LIFTERS WERE BADLY SPALLED WHICHSDR CA110125035Screw · loose(CAN) DURING INSPECTION OF CARB THROTTLE BODY SCREWS IAW SEB 07-11R, THROTTLE BODY SCREWS FOUND LOOSE. CARB REPLACED.SDR CA110125034Seal · leaking(CAN) OIL SEAL LEAKING OIL ON TO LANDING LIGHT.SDR CA110323008Magneto · failed(CAN) SHORTLY AFTER CONTROL SETUP FOR CRUISE CONDITION, ENG VIBRATION WAS DETECTED. THE PILOT ELECTED TO CARRY OUT A MAGNETO CHECK WHICH RESULTED IN A SUBSTANTIAL ENG RPM DROP WHEN THE NR RT MAGNETO WAS TESTED. THE PILOT ELECTED TO RETURN TO BASE. REMOVED TSDR BIGR12/15/10Control Cable · frayedDURING ANNUAL INSP THE LT AND RT AILERON CABLES (P/N MC0510105-262)WERE FOUND TO HAVE HALF OF THE WIRE STRANDS BROKEN AT A IDLER PULLEY INBD OF THE AILERON BELLCRANKS. BOTH CABLES WERE REPLACED AND ACFT WAS RERIGGED NO OTHER DEFECTS WERE NOTED.SDR CA101118002Heat Exchanger · cracked(CAN) LEAK DETECTED. UPON COMPLETION OF AD 90-03 R2 LEAK IDENTIFIED IN CABIN HEAT EXCHANGER. UNIT IS A FAA-STC AFTERMARKET EXHAUST INSTALLED PER STC SA01801AT. SIMILAR INSTALLATIONS CONTAINING THE SAME DESIGN ARE INSTALLED IN MANY OTHER MODEL AIRCRAFT. IT CONTSDR CA101109005Control Cable · separated(CAN) CARB HEAT CONTROL CABLE SEPARATED WHERE HANDLE ATTACHES TO INNER CABLE.SDR CA110125031Condenser · failed(CAN) RPM DROP ON RUNUP. TROUBLESHOT PROBLEM. CONDENSER U/S.SDR CA101013005Roll Pin · crackedDURING ANNUAL INSP, IT WAS NOTED THAT THE TIP OF A LANDING GEAR DOWN-STOP ROLL PIN HAD BEEN SHEARED OFF. UPON CLOSER INSP OF ALL REMAINING ROLL PINS IN THE UP AND DOWN STOP LATCH BLOCKS, IT WAS NOTED THAT ALL WERE CRACKED. REMOVAL OF THE PINS REVEALED MOST TOSDR CA110125030Support · cracked(CAN) MUFFLER SHROUD SUPPORT CRACKED AWAY FROM MUFFLER.SDR CA100924009Switch · failedDURING RUN-UP, AMPS FULL LOAD CHECK, SPARKS WERE SEEN FROM PILOTS SIDE WHEN LIGHTS SWITCHED ON. FAINT ODOR OF SMOKE AND NAV. LIGHT C/B POPPED. TURNED LIGHT SWITCH OFF. SPARKS SEEN FROM PARKING BRAKE AREA. ACFT RETURNED TO RAMP W/O FURTHER PROBLEMS. MX FOUNDSDR 2010FA0000927Dipstick · brokenBROKEN DIPSTICK .SDR PNYC675LDipstick · brokenDIPSTICK BRAKES OFF FROM CAP. DIPSTICK IS DRILLED FOR A PIN TO ATTACH IT TO THE CAP AND IT APPEARS TO BE OVER DRILLED CAUSING A WEAK SPOT. THE DIPSTICK FALLS DOWN INTO THE DIPSTICK TUBE AND MUST BE FISHED OUT WITH WITH SOME SORT OF GRABBING DEVICE. THIS IS THESDR CA110125033Magneto · contaminated(CAN) ENGINE ROUGH 1800-2000 RPM. OIL FOUND IN MAGNETO. MAGNETO SENT AWAY FOR REPAIR.SDR CA110125032Cylinder · misoverhauled(CAN) CYLINDER EXHAUST VALVE GUIDE EXCEEDS LIMITS AS PER SB 388C. CYLINDER`S OVERHAULED 400HR PRIOR AT PREVIOUS SB TIME. VALVE PLAY EXACTLY THE SAME AS PRIOR TO OVERHAUL. BELIEVE OVERHAUL COMPANY MISTAKENLY SENT CYLINDERS BACK WITHOUT OVERHAULING.SDR CA100621017Bearing · failedACFT PULLED OUT OF HANGAR FOR MORNING FLIGHT, WOULD NOT START - BATTERY DEAD. AME REMOVED BATTERY FOR CHARGING. CHECKED ELEC SYS, FOUND THAT THE ALTERNATOR BELT HAD FLIPPED OVER ON THE RING GEAR AND WHEN PROP WAS MOVED, ALTERNATOR PULLEY DID NOT MOVE. ALTERSDR CA100805010Bolt · sheared6 ON 8 BOLTS FOUND SHEARED ON CYLINDER NR 2.
SDR CA110125027Carburetor · loose(CAN) CARB SHAFT LOOSESDR CA110125028Bearing · loose(CAN) MAGNETO BEARING LOOSE.SDR CA100806003Points · separatedSCREW HOLDING POINT HALVES TOGETHER BACKED OUT CAUSING POINT HALVES TO SEPERATE AND FAIL.SDR CA100208007Breaker Points · worn(CAN) WHILE PERFORMING ROUTINGE INSP THE MAGNETO TO ENGINE TIMING WAS NOTED TO BE 5 DEGREES OFF. THE MAGNETO WAS REMOVED TO INSPECT AND ADJUST THE POINTS AND IT WAS FOUND THAT THE POINTS WERE JUST BARELY OPENING (WHICH MEANT THAT THE MAGNETO WAS CLOSE TO FAILISDR CA100127008Retaining Ring · cracked(CAN) LANDING LIGHT RETAINER RING CRACKED.SDR CA100115001Wire · burned(CAN) ON JANUARY 12, 2010, APPROX 19:20 LOCAL TIME, ACFT WAS CONDUCTING NIGHT TRAINING OPERATIONS WHEN A BURNING SMELL IN THE COCKPIT WAS NOTED AND THE LANDING LIGHT FAILED TO OPERATE. INSP COMPLETED BY MX, FOUND THAT THE LANDING LIGHT WIRING LOCATED IN THE LSDR CA100104003Coupling · failed(CAN) VACUUM PUMP COUPLING FAILED.SDR CA091214005Valve · leaking(CAN) ALTERNATE STATIC VALVE LEAKING.SDR CA091110002Magneto · faulty(CAN) DURING RUN-UP, ENG WOULD NOT RUN ON LT MAGNETO. MAGNETO REMOVED FROM ACFT. O/H MAGNETO INSTALLED ON ACFT AND GROUD RUNS CHECKED SERVICEABLE. FAULTY MAGNETO SENT FOR REPAIRS. CAUSE OF DEFECT UNKNOWN.SDR CA091102002Starter · failed(CAN) STARTER WILL NOT TURN ENG OVER.SDR CA091027006Cylinder Head · separated(CAN) THE LOWER SPARK PLUG (WITH HELI COIL AND GASKET STILL ATTACHED) SEPERATED FROM CYLINDER HEAD NR 4. CYLINDER HEAD NR 4 HAS MISSING THREADS AND PEICES OF HELI COIL STILL EMBEDDED IN REMAINING THREADS. IT APPEARS THAT THE HELI COIL INSERT BROKE APART AND TOSDR 2009FA0000977Condenser · failedCONDENSERS, LT AND RT FAILED INTERNALLY SO AS TO CAUSE PREMATURE WEAR AND BURNING OF POINTS. (K)SDR CA091021010Volt Regulator · failed(CAN) CREW REPORTED ALTERNATOR NOT CHARGING AFTER ENGINE START-UP. ENGINE SHUT DOWN. TROUBLESHOOTING INDICATED VOLTAGE REGULATOR AT FAULT. NEW REGULATOR INSTALLED AND GROUND RUNS CONFIRMED CHARGING SYSTEM FUNCTIONING CORRECTLY. (TC 20091021010)SDR CA091005012Vent Line · out of position(CAN) IT WAS PERIODICALLY NOTICED BY PILOTS THAT FUEL WAS VENTING OUT OF THE VENT LINE. SEVERAL ATTEMPTS WERE MADE TO PREVENT THESE OCCURENCES. THESE INCLUDED CHANGING THE CAPS AS WELL AS ADJUSTING ANGLE OF THE VENT LINE, AND REPLACING THE CHECK VALVE. AS AN ESDR CA091021003Connecting Rod · mismanufactured(CAN) THE BOLT HOLE DID NOT HAVE SUFFICIENT CHAMFER TO FULLY ACCEPT THE BOLT. THERE IS A SERVICE BULLETIN ADDRESSING THIS ISSUE FOR THE OLDER PART NUMBER CONNECTING RODS. THIS NEWER PART NUMBER ROD IS SUPPOSED TO HAVE THIS LARGER CHAMFER INCORPORATED. INSUFFISDR CA090914004Float · stuck(CAN) PILOT REPORTED ENGINE RUNNING ROUGH AND ON SHUT DOWN FUEL COMING FROM COWLING. INSPECTION REVEALED FUEL COMING FROM CARB INLET DUE TO STUCK FLOAT OR NEEDLE VALVE. CARB REPLACED AND AIRCRAFT RELEASE. (TC# 20090914004)SDR CA090902008Impulse Coupling · brokenDURING 500 HR INSP OF MAGNETO, PAWL PLATE WAS FOUND TO BE MISSING PIECES AT BOTH OF THE STOP LOCATIONS. ONE PIECE WAS FOUND ON THE LIP OF THE MAGNETO ADAPTER AND THE OTHER WAS RETIEVED WITH A MAGNET FROM THE BOTTOM OF THE ACCESSORY CASE.SDR CA090824009Piston · broken(CAN) COMPRESSION CHECK DURING INSP INDICATED LOW COMPRESSION, INSP REVEALED BROKEN PISTON RING LAND BETWEEN TOP 2 RINGS.SDR CA090730002Fairing · improper partPART DOES NOT HAVE PROPER CERTIFICATION.SDR CA090618002Bracket · loose(CAN) INSP REVEALED LOOSE BRACKET WITH LWR ATTACH RIVETS FOUND WITH RIVET HEAD MISSING.SDR 2009FA0000446Starter · crackedPILOT REPORTED ENGINE WOULD NOT START. INSPECTION REVEALED STARTER BENDIX HOUSING CRACKED CIRCUMFERENTIALLY AND LONGITUDINALLY. CAUSE UNKNOWN.SDR 2009FA0000453Bearing · failedLT OTBD AFT FLAP BEARING FAILURE. THIS CAUSED FLAP TO SEIZE ON OTBD TRACK ON FLAP RETRACTION, WHICH DISTORTED FLAP AND CAUSED RETRACTION CABLE TO BREAK. CAREFUL INSPECTION OF FLAP TRACKS FOR ABNORMAL WEAR AND INSPECTION OF ROLLERS COULD PREVENT RECURRENCE. SDR CA090407003Control Cable · broken(CAN) DURING PRE-FLIGHT CHECKS OF ACFT ON APRIL 5, 2009 AT 8195.2 TAT, THE PILOT REPORTED THAT THE CARBURETOR HEAT CONTROL KNOB CAN BE PULLED OUT OF THE PANEL. NOT CONNECTED. ACFT REMOVED FROM SERVICE. MX PERSONNEL INSPECTED AND FOUND THAT THE CARBURETOR HEASDR 2009FA0000245Tube · failedNOSE TUBE FAILED. TUBE SPLIT ON THE OUTSIDE DIAMETER OF TUBE. THIS TUBE INSTALLED 2-14-08. (K)SDR CA090407004Nut · separatedKNOB JAM NUT BECAME SEPARATED FROM ACTUATING KNOB.SDR CA090312001Spring · disconnected(CAN) ON FEB 13/2009 AT 14927.1 TAT, ACFT WAS REPORTED BY FLIGHT CREW TO HAVE AN EXCEPTIONALLY LOOSE RUDDER RETURN SPRING (LT SIDE). MX INVESTIGATION FOUND THE SPRING HAD BECOME DISCONNECTED. A NEW SPRING WAS INSTALLED AND RUDDER CONTROL SYS WAS FOUND TO BE SESDR CA090209006Roller · brokenLT FLAP OUTBOARD LOWER ROLLER BROKE COMPLETELY UP CAUSING THE FLAP TO SEIZE INTO THE FLAP TRACK DURING THE FLAPS BEING RETRACTED AFTER TAKEOFF. WITH THE FLAP SEIZE THE FLAP MOTOR CONTINUED TO PULL THE SLAVE FLAP UNTIL THE RETRACT CABLE SNAPPED IN FLIGHT. THE SDR CA090209003Control Cable · failedRT FLAP RETRACT CABLE P/N 0510105-94 FAILURE DURING FLAP RETRACTION JUST AFTER TAKEOFF. PILOT DISCOVERED DEFECT DURING FLIGHT VISUALLY AND DID NOT HEAR A FAILURE OF THE CABLE OCCUR IN THE CABIN. CABLE FAILURE CAUSED AIRCRAFT TO ROLL/TURN RIGHT IN FLIGHT DUE SDR CA090310001Carburetor · contaminated(CAN) IN CRUISE, AFTER GOING THROUGH SOME TURBULENCE, THE ENGINE LOST SOME POWER (MAX 2100 RPM), SO THEY RETURNED TO THE AIRPORT. MX RUN UP THE NEXT DAY CONFIRMED THE PROBLEM IN THAT THE ENGINE STARTED AND IDLED NORMALLY, IT WAS HARD TO GET PAST 1500 RPM. CARBSDR 2008FA0000722Carburetor · damagedPILOT WAS MAKING 3RD TOUCH AND GO, ON CLIMBOUT ENGINE STARTED VIBRATING EXCESSIVELY, POWER WAS REDUCED AT PATTERN ALTITUDE, MIXTURE ADJUSTED, SWITCHED MAGNETO'S FROM R TO L WITH NO CHANGE IN THE VIBRATION. AIRCRAFT LANDED AND SUBSEQUENT OPERATION WHILE TAXIINSDR 2008FA0000892Clevis Pin · missingCLEVIS PIN THAT SUPPORTS BACK OF PILOTS SEAT WORN OVER .2500 THRU. THIS PIN SLIDES IN A CURVED PORTION OF THE LOWER FRAME OF THE SEAT. PROBLEM PARTS ARE CLEVIS PINS THAT SUPPORT THE SEAT BACK ON NR (2), (BELLCRANK). THE BELLCRANK IS WELL WORN IN THE CURVED SDR CA080925002Spar · cracked(CAN) DURING THE 100 HRS/ANNUAL INSP, IT WAS DISCOVERED THAT THE HORIZONTAL STABILIZER FRONT SPAR ASSY (PN 0532001-98) AND THE RE-INFORCEMENT SPAR (PN 0531037-1) HAVE CRACKS AT 2 PLACES, ABOUT .5 INCH IN LENGTH, RADIATING FROM THE CENTER LIGHTENING HOLE BETWEE
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