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 = '182N' 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 = '182N' 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 2020FA0000520Pump · damagedTHE AIRCRAFT HAD A OIL LEAK. WE FOUND THE THREADS IN THE OIL PUMP HOUSING WERE GAULDED AND THE OIL FILTER ADAPTER THREADS WERE DAMAGED. MOST LIKELY FROM OVER TORQUE. THE PUMP BODY P/N 632563 WAS REPLACED AND AIR WOLF REMOTE OIL FILTER KIT INSTALLED.SDR KC2R1218201449609Impulse Coupling · crackedDURING A ROUTINE 500 HR INSPECTION OF THE MAGNETOS, FOUND BOTH IMPULSE COUPLINGS CRACKED AT HUB PLATE, NEAR FULL ADVANCE STOP NOTCH.SDR CA140321002Air Box · defective(CAN) CARBURETOR AIR BOX SEALING FACE PREVIOUSLY REPAIRED. FIT BETWEEN AIR BOX SEALING FACE & ENG LOWER COWLING INDUCTION AIR DUCT EXPANSION BOOT VERY POOR, ALLOWING UNFILTERED AIR TO ENTER ENG INDUCTION SYS.SDR CA140322002Feeder Cable · damaged(CAN) ENGINE STARTER POWER CABLE, WIRE NR D-PA8, WILL NOT ALLOW SUFFICIENT CURRENT FLOW TO CRANK ENGINE PROPERLY DUE TO CABLE STRANDS BROKEN IN TERMINAL END AT STARTER SOLENOID.SDR CA140322001Governor · leaking(CAN) PROPELLER GOVERNOR, CSU, FOUND TO BE LEAKING ENGINE OIL HEAVILY FROM THE CONTROL SHAFT.SDR CA140321013Brake Assy · misinstalled(CAN) VISUAL INSPECTION FOUND LT AND RT BRAKE INSTALLATION UNAPPROVED FOR USE ON INSTALLED WHEELS. ALSO FOUND BRAKES INSTALL BACKWARDS. ON AFT SIDE OF WHEEL.SDR CA140321012Bulkhead · cracked(CAN) FS 230.18 BULKHEAD FOUND BADLY CRACKED IN THE AREAS OF THE RUDDER TRAVEL STOPS. ALSO NOTED PREVIOUSLY STOP DRILLED CRACKING.SDR CA140321011Lead · misinstalled(CAN) DURING ENGINE MAGNETO TIMING/SYNCHRONIZATION, FOUND IGNITION SWITCH POSITIONS INCORRECT. TROUBLESHOOTING DETERMINED LT AND RT "P" LEADS REVERSED ON MAGNETOS.SDR CA140321010Mount · weak(CAN) ENGINE LOWER COWLING INDUCTION AIR DUCT CHAFED THOUGH BY ENGINE EXHAUST MUFFLER HEAT SHROUD. FOUND ENGINE RUBBER ISOLATION MOUNTS WEAK AND DAMAGED AND POOR CLEARANCE WITH MODIFIED ENGINE EXHAUST SYSTEM COMPONENTS.SDR CA140321009Extinguisher · misinstalledCABIN FIRE EXTINGUISHER FOUND TO BE POORLY SECURED TO CABIN FLOOR. PK STYLE SHEET METAL SCREWS FASTENING MOUNT TO LIGHT ALUMINUM FLOOR. WEEK INSTALLATION UNABLE TO WITHSTAND "G" LOADS IN ANY NORMAL AXIS.SDR CA140321008Sensor · malfunctioned(CAN) ENGINE TEMPERATURE MONITOR PROBES ON THE ODD CYLINDER BANK REVERSED CAUSING THE INCORRECT CYLINDER DATA TO BE DISPLAYED TO PILOT. ALSO, FOUND MAIN POWER AND LIGHTING DIMMER POWER NOT CIRCUIT PROTECTED AND HARD WIRED TO ACFT MAIN BUSS.SDR CA140321007Cylinder · corroded(CAN) HOT CYLINDER DIFFERENTIAL COMPRESSION CHECK CARRIED OUT AND FOUND ALL CYLINDER COMPRESSIONS WELL BELOW MINIMUM ALLOWABLE. VIDEOSCOPE INSPECTION CARRIED OUT, AND FOUND ALL CYLINDER INTERNAL WALLS HEAVILY CORRODED IN THE CHOKE PORTION OF EACH CYLINDER.SDR CA140321006Wire · misinstalled(CAN) ELT REMOTE POWER WIRING NOT CIRCUIT PROTECTED. FOUND POWER WIRE HARD WIRED TO CLOCK. CLOCK POWER CIRCUIT PROTECTION UNAPPROVED. FOUND CLOCK POWER FUSE WRAPPED IN ALUMINUM FOIL FROM A CIGARETTE PACKAGE.SDR CA140321005Fuse · misinstalled(CAN) EXTERNAL GROUND POWER CIRCUIT PROTECTION UNAPPROVED. FOUND PREVIOUSLY TRIPPED GLASS FUSE WRAPPED IN ALUMINUM FOIL FROM A CIGARETTE PACKAGE AND INSTALLED IN FUSE HOLDER.SDR CA140321004Horn · deformed(CAN) LT AND RT ELEVATOR HORN L/E DEFORMED AND COVERED IN A UNAPPROVED RUBBER L/E BOOT. VERY POOR HORIZONTAL STABILIZER TO ELEVATOR HORN CLEARANCE. WHEN UNAPPROVED RUBBER BOOTS REMOVED, FOUND SUBSTANTIAL SKIN DAMAGE. ELEVATOR BALANCE WITH UNAPPROVED BOOTS WISDR CA140321003Restraint · missing(CAN) LT AND RT CABIN DOOR RESTRAINTS BROKEN AND MISSING ALLOWING DOORS, REPEATEDLY CONTACT WING STRUTS. DAMAGE TO DOOR SKINS AND WING STRUTS OCCURRED.SDR CA130701017Bulkhead · cracked(CAN) FUSELAGE/EMPENAGE BULKHEAD ASSY AT STA 230.187" AFT OF DATUM FOUND BADLY CRACKED AT RUDDER STOPS. FOUND OTHER CRACKS PREVIOUSLY STOP DRILLED AND NOTED. ALSO NOTE AD 72-07-09, OVERDUE BY 71 HRS. WHICH REQUIRES AN INSPECTION OF THAT AREA.SDR 2009FA0000692Spar · corrodedFOUND THE REAR SPAR CARRY THROUGH TO AFT DOOR POST WITH 6 RIVET HEADS POPPED OFF. FOUND BOTH LT AND RT AFT FITTINGS, PN 07116069 AND -10 AS WELL AS 0422229-12 AND -23 CORRODED SO THAT THEY ARE IN 2 PIECES. THE REAR SPAR CARRY THROUGH HAS A 1 INCH CRACK AT THSDR 2008FA0000574Impulse Coupling · failedPILOT PERFORMED PRE-FLIGHT INSP DISCOVERED OIL ON FWD PORTION OF COWLING, SLIGHT OIL RESIDUE ON WINDSHIELD. MECHANIC REMOVED TOP COWLING TO INVESTIGATE, DISCOVERED MAGNETO HOUSING SHATTERED AT AREA IMMEDIATELY ADJACENT TO IMPULSE COUPLING. APPARENTLY IMPULSESDR CA060419005Cylinder Head · leakingLEAKAGE FOUND BETWEEN BARREL AND HEAD.SDR 2004FA0000758Bulkhead · crackedBULKHEAD FOUND CRACKED DURING ANNUAL INSPECTION AT RT RUDDER STOP BOLT. THIS BULKHEAD REQUIRES 1000 HR INSPECTIONS IAW AD72-07-09, WHICH WAS NOT DUE AT THIS TIME. SUSPECT WIND DAMAGE FROM REPEATEDLY STRIKING STOP. (SO05200410568)SDR 2003FA0000565Bulkhead · crackedTIME SINCE LAST AD REQUIRED INSPECTION 901.8. ORIGINALLY INSPECTED ON 9/19/74 WITH 1246 TT, FOUND OK. REINSPECTED AT 1502 AND 2334.58 TT AND FOUND, OK. ALSO INSPECTED AT 3345.1 AND FOUND AIRWORTHY. CURRENT INSPECTION REVEALED TWO SMALL CRACKS .1250 AND .25SDR CA020304004Bulkhead · cracked(CAN) SPINNER BULKHEAD FOUND MOUNTED BETWEEN PROP AND CRANKSHAFT FLANGE - BULKHEAD SUPPOSED TO BE MOUNTED ON REAR RACK OF CRANKSHAFT FLANGE. INCORRECT MOUNTING RESULTED IN CRACKED BULKHEAD AND PROP HUB DISTORTION LEADING TO FLUID LOSS.SDR 2001FA0000391Bulkhead · crackedIN COMPLYING WITH AD, (CRACKS AND LOOSE BOLTS IN FIN AND RUDDER) CRACKS WERE FOUND IN THE AREA IN THE AFT BULKHEAD BETWEEN THE RUDDER CABLE CUTOUT AND THE BULKHEAD FLANGE. 1 CRACK EACH SIDE, BULKHEAD WAS REPLACED.SDR CA000811004Crankshaft · separated(CAN) AIRCRAFT WAS IN A CRUISE ATTITUDE, IN PREPARATION TO DISEMBARK SKYDIVERS, WHEN PILOT NOTICED AN ENGINE VIBRATION FOLLOWED BY A BANG, ENGINE CAME TO A SUDDEN STOP. AIRCRAFT LANDED AT AIRPORT OF DEPARTURE WITHOUT FURTHER INCIDENT. UPON INSPECTION, FOUNSDR 20000427SH022Lock · missingWHILE PERFORMING THE APRIL, 2000 ANNUAL, FOUND THE MOUNT SAFETY LOCKS, PN 0851559, WERE MISSING ON ALL FOUR ENGINE MOUNTS, PN J6545-1. INSTEAD, THERE WAS AN EXTRA WASHER TO TAKE UP THE BOLT LENGTH. THE MOUNTS WERE INSTALLED 5-19-98. (X)SDR CA991103001Lifter · failed(CAN) HYDRAULIC LIFTERS FAILING TO KEEP CONTACT WITH CAMS. NEW P/N INSTALLED.SDR 98ZZZX3444Gasket · missingDURING ACCIDENT INVESTIGATION, OIL FILTER CAP WAS NOT ATTACHED TO FILLER TANK. CAP WAS FOUND IN ENGINE COMPARTMENT. THE CHAIN AND HOOK WERE AFFIXED TO CAP. THE GASKET UNDER SIDE OF CAP WAS MISSING. THE CAP WOULD NOT LOCK OR FIT SNUGGLY TO FILLER TANK. EVISDR 98ZZZX3152Line · leakingTHIS FUEL LINE, THAT ATTACHES TO THE FUEL SELECTOR VALVE COMING FROM LT TANK, WAS WORN IN TWO BY THE ELEVATOR CABLE. ACFT HAD UNDERGONE A REPAIR FOR A BADLY DAMAGED FIREWALL AND FLOORING AFTER A HARD LANDING APPROX 6 MONTHS AND 200 HRS BEFORE. AT THAT TIME, SDR 98ZZZX2599Throttle · sticksTHROTTLE WOULD STICK WIDE OPEN AT FULL POWER. UPON DISASSEMBLY OF CARBURETOR, DETERMINED THAT WEAR OF THE FULL OPEN STOPS ON THE CARBURETOR BODY AND THROTTLE STOP ARM, THE POWER ENRICHMENT LEVER OPERATES THE AIR METERING PIN WOULD TRAVEL PAST ITS DESIGN LIMITSDR 98ZZZX1476Plug · missingFOLLOWING TAKEOFF, ENGINE RUNNING ROUGH AND FIRE ERUPTED. AFTER LANDING, INSPECTION FOUND FIRE IN ENGINE COMPARTMENT DUE TO MISSING DRAIN PLUG FROM CARBURETOR BOWL. NO SAFETY WIRE EVIDENT.SDR 99ZZZX1061Camshaft · wornOVER THE LIFE OF THE ENGINE, THIS ENGINE HAS BEEN ON OIL ANALYSIS. THE TEST SHOWED A TREND OF HIGH AL AND FE STARTING AT 529 HOURS WITH THE RECOMMENDATION FOR RE-TEST IN 25 HOURS. THE TREND CONTINUED WITH NO DECREASE, BORESCOPES WERE USED TO DETECT.SDR 97ZZZX2119Bulkhead · crackedDURING ROUTINE INSPECTION, CRACKS DETECTED IN UPPER LEFT BULKHEAD FLANGE RADIUS ABOVE RUDDER STOP. SUBJECT IS COVERED BY CESSNA SL 72-3 AND AD 72-07-09. SUSPECT CAUSE IS YEARS OF RUDDER STOP CONTACT. SUBMITTER STATED THIS TYPE OF CRACK MAY BE ELIMINATED BY SDR AU960589Spar · corroded(AUS) LH WING CONTAINED SEVERE EXFOLIATION CORROSION IN THE UPPER FORWARD SPAR EXTRUSIONS, EXFOLIATION CORROSION AND CRACKING IN THE MAIN SPAR AND CORROSION IN THE INNER SPAR WEB - CORROSION APPEARS TO HAVE BEEN PREVIOUSLY TREATED WITH LPS TYPE COMPOUNDSDR 96ZZZX1256Bulkhead · crackedCRACK IN THE RT RUDDER CABLE CUT-OUT HOLE AT THE RT UPPER OUTBOARD RADIUS. ALSO, CRACK FROM RT RUDDER STOP BOLT HOLE UPWARD TO BULKHEAD BEND RADIUS, THEN ALONG BEND RADIUS FOR .3750 INCH. SUSPECT CAUSED BY RUDDER SLAMMING AGAINST STOPS IN GUSTY WIND. SUBMIT
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