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 = '182S' 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 = '182S' 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 2020FA0000029Hose · crackedSEVERAL MONTHS AGO I HAD A STRONG SMELL OF GAS IN THE CABIN, IT WAS TRACED DOWN TO A CRACKED "RUBBER" HOSE BETWEEN THE WING TANK AND THE TUBE DOWN TO THE ENGINE. AT THE TIME I ASKED THE MECHANIC IF IT SHOULD BE REPORTED AND THE OTHER SIDE OF THE PLANE CHECKED,SDR 2018FA0000207Housing · damagedAIR FILTER HOUSING PN 07506212 DAMAGED AT THE OUTLET. SUSPECT DAMAGE WAS CAUSED BY OVER TIGHTENING OF THE CLAMP THAT SECURES THE RUBBER COUPLING TO THE DUCT. METAL TAPE WAS WRAPPED AROUND THE OUTLET PORTION OF THE HOUSING IN AN ATTEMPT TO REPAIR THE CRACKED SDR 2017FA0000243Bearing · failedAFTER REMOVAL OF THE CYLINDER, FOUND THAT THE CRANKSHAFT MAIN BEARINGS FROM THE NR 6 CYLINDER WERE CRUSHED AND PARTS OF THEM MISSING, LATER FOUND THE REMAINING PIECES OF BEARING MATERIAL AND PIECES OF THE CONNECTING ROD END CAP, NUTS AND BOLTS IN THE OIL SUMP.SDR 2015FA0000366Support · crackedSUPPORTS FOR THE ACFT BATTERY ARE CRACKED AT 3 OF THE 4 CORNERS. IT APPEARS THAT THE STRESS OF THE BATTERY HOLD DOWN HARDWARE, WEIGHT OF THE BATTERY AND THE ACFT OPERATIONAL LOADS MAY HAVE CAUSED THE CRACKS. RECOMMEND THICKER MATERIAL FOR THE SUPPORTS.SDR 2014FA0000622Attach Fitting · brokenDURING ANNUAL INSPECTION, FOUND NOSE GEAR LOWER ATTACHMENT CAST FITTING TO AIRCRAFT FUSELAGE HAD TWO HORIZONTAL ATTACHMENT EARS CRACKED. AFTER REMOVING THE BOLT FROM EACH FITTING EAR, THE EARS CAME OFF, THE EARS APPEAR TO HAVE SNAPPED OFF FROMT THE CAST FITTISDR 2014FA0000099Nut · backed outDURING 50 HOUR INSPECTION. ATTEMPTED TO CONNECT EXTERNAL POWER AND FOUND TOP SMALL CONTROL PIN, LAYING IN BOTTOM OF RECEPTACLE. ATTACHING NUT WAS FOUND IN THE BOTTOM OF THE RELAY BOX. WIRE WAS FLOATING LOOSE IN BOX. APPARENTLY, NUT BACKED OFF DUE TO POSSISDR JRUR201312050013Exhaust Valve · out of toleranceDURING PERFORMANCE OF SB 388C, FOUND NR 2 CYLINDER EXHAUST VALVE TO GUIDE CLEARANCE MEASURED .032". EXCEEDS THE MAXIMUM ALLOWABLE CLEARANCE OF .030". NR 2 CYLINDER OVERHAULED 502.1 HOURS AGO. MAINTENANCE INSTALLED A NEW, EXHAUST VALVE GUIDE DURING OVERHAULSDR 2013FA0000445Selector Switch · failedACFT HAD PREVIOUS FORCED LANDING RESULTING IN PROP STRIKE CAUSED BY FUEL STARVATION. HAVE BEEN TROUBLESHOOTING A FUEL FEEDING ISSUE SINCE THE ACFT ARRIVED. THE ACFT FEEDS RANDOMLY FROM EITHER TANK WHEN BOTH SELECTED. DURING TROUBLESHOOTING AT ANNUAL, DISCOVSDR CA130729016Indication Sys · malfunctioned(CAN) TRIM INDICATOR PIN CAN BE DISLODGED FROM ITS FULL RT POSITION BY OVERTURNING TRIM WHEEL. RESULTANT INDICATION ERROR WHEN RETURNED TO NEUTRAL, EVIDENT BY POSITION OF RUDDER PEDALS AND CONTROL SURFACE.SDR CA120306009Exhaust Valve · seized(CAN) AFTER LEVELING OFF AT 4000` ENGINE WAS RUNNING FINE FOR ABOUT A MINUTE. SUDDENLY THERE WAS A SMALL VIBRATION THAT LASTED ABOUT 30 SECONDS THEN IT TURNED INTO A LARGE VIBRATION THAT GOT WORSE. PILOT REQUESTED IMMEDIATE LANDING AND REDUCED POWER WHICH CASDR 2012FA0000186Hub · crackedLIQUID PENETRANT INDICATION ON THE EXTERNAL SOCKET ON NR 2 BLADE AT 4 O`CLOCK. THIS IS NOT A RADIAL INDICATION. THIS CRACK INDICATION WAS DISCOVERED DURING O/H. THE PART IS UNAIRWORTHY. HUB WAS SENT TO MFG FOR DESTRUCTIVE TESTING.SDR 2011FA0000669Connecting Rod · failedINSTALLED CRANKSHAFT KIT 05K23580 TO C/W AD 06-02-09 CRANKSHAFT RETIREMENT. KIT INCLUDES NEW CRANK, NEW BEARINGS, ROD BOLTS AND NUTS. NEW PISTON RINGS, SEAL AND GASKET SET. ENGINE TEST RAN AND TEST FLOWN. ENGINE RAN FOR APPROX 40 HRS OF TROUBLE FREE OPERATSDR 2011FA0000366Screw · loosePIC WAS FORCED TO LAND USING ELEVATOR PITCH CONTROL DUE TO ELEVATOR JAMMING AFTER CONTROL COLUMN INTERNAL SLIDE ATTACH SCREW CAME LOOSE. ACFT RECORDS SHOW THAT SB98-27-04, DATED JUNE 1, 1998, SPECIFICALLY PERTAINS TO AN INSPECTION OF THIS SCREW, AND WAS ALLEGESDR CA100809026Exhaust Valve · stuckACFT DEPARTED FOR LOCAL FLIGHT OVER CITY, ON TAKEOFF EVERYTHING NORMAL, IN CLIMB ENGINE STARTED TO RUN ROUGH. PILOT LEVELED OUT AT 1000 FT AND RETURNED TO AIRPORT. LANDED WITH OUT ANY PROBLEMS. ACFT WAS RUN UP NEXT MORNING STILL RUNNING ROUGH AND MIXTURE WAS SDR JRUR20101216715HPDoubler · cracked(JRUR) A 1.25 INCH LONG CRACK WAS DISCOVERED IN THE FIREWALL FWD DOUBLER (PN 0753600-24). THE CRACK WAS LOCATED ON THE LOWER LT QUADRANT OF THE FWD FIREWALL DOUBLER. THE CRACKED LOCATION CAN BE FOUND BY LOCATING THE "BRACKET-PARKING BRAKE CONTROL" AFT OF THE SDR 2010FA0000149Support Bracket · crackedDURING ANNUAL INSPECTION BOTH AIRCRAFT BATTERY SHELF/TRAY LEFT & RIGHT SUPPORT BRACKETS P/N 0712059-1 FOUND CRACKED IN FWD & AFT ENDS (TOTAL OF 4 CRACKS). EACH CRACK STARTED AT ENDS OF SUPPORTS IN 90 DEGREE BEND RADIUS AND PROPAGATED TOWARD THE CENTER OF EACHSDR 2009FA0001016Valve · stuckON START UP AND TAXI OUT OF THE ACFT, THE EXHAUST AND INTAKE VALVES STUCK. THIS CAUSED BOTH PUSH RODS TO BEND. AND THE LIFTER PLUNGER WAS LOCKED UP UPON FURTHER INSP. THE ENG WAS USING W100 OIL AND HAD ONLY 634.8 HOURS SINCE NEW.SDR 2009FA0001015Valve · stuckON START UP AND TAXI OUT OF THE ACFT, EXHAUST AND INTAKE VALVES STUCK. THIS CAUSED BOTH PUSH RODS TO BEND. AND LIFTER PLUNGER WAS LOCKED UP UPON FURTHER INSP. ENG WAS USING W100 OIL AND HAD ONLY 634.8 HOURS SINCE NEW.SDR CA090218002Wire · damaged(CAN) DURING MASTER SWITCH SELECTION TO ON, NO POWER WAS OBSERVED ANYWHERE IN ACFT. TROUBLESHOT A FEW TIMES, EVERY TIME, WHEN MX TRIED TO DUPLICATE SNAG, UNABLE TO FAULT. FINALLY, WAS ABLE TO FAULT, FOUND THAT BUSS (BUS) TIE STRAP FROM ALTERNATOR CONTACTOR (SSDR 2008FA0000688Pump · crackedPUMP HOUSING CRACKED ALONG SEAM. POSSIBLE WEAK SPOT UPON MANUFACTURING. (K)SDR 2007FA0000900Control Cable · wornCONTROL CABLE, (P/N 0510105-189), FOUND WORN TO REPLACE LIMITS IAW AC43.13-1A, CABLE INSPECTION. CABLE WAS WORN DUE TO CONSTANT CONTACT WITH MICARDA GUARD PLATE OVER FUEL LINES AT FUEL SELECTOR AREA JUST FORWARD OF FRONT SEATS. THE CABLES ARE IN CONSTANT CONSDR 2007FA0000937Control Cable · wornLT AND RT ELEVATOR CONTROL CABLES, ( P/N 0510105-189), FOUND WORN TO REPLACEMENT LIMITS IAW CABLE WEAR INSPECTION GUIDELINES IN AC43.13-1A. CABLE WAS WORN DUE TO CONSTANT CONTACT WITH THE MICARDA PLATES OVER THE FUEL LINES AT FUEL SELECTOR AREA JUST FORWARD OSDR 2007FA0000492Bellcrank · brokenDURING ANNUAL INSPECTION, IT WAS NOTED THAT THE (BELLCRANK ASSY) ON THE FLAP FEEDBACK LEVER, BEHIND THE INSTRUMENT PANEL, WAS BROKEN IN TWO, IT CONSIST OF A PLASTIC BLOCK WITH A SLOT IN IT WHICH MOVES THE MICROSWITCH ASSY TO ACTIVATE, OR DEACTIVATE THE FLAP DRSDR 2007FA0000491Servo · bindingPILOT/OWNER REPORTED TO MX THAT ON APPROACH AFTER DISENGAGING AUTOPILOT, AILERONS WERE DIFFICULT TO MOVE. NO WINDS AND STABLE APPROACH MINIMIZED PROBLEM. MX NOTED AILERONS WERE EXTREMELY DIFFICULT TO MOVE, AND FURTHER MOVEMENT COULD HAVE CAUSED EVEN GREATER DISDR 2006FA0001069Exhaust Valve · stuckSTUCK EXHAUST VALVES ON NR 3 CYLINDER FOUND DURING PHASE 2 INSPECTION.SDR 2006FA0001037Exhaust Valve · stuckDURING A PHASE 2 INSPECTION, CYLINDER NR 5 WAS FOUND TO HAVE LOW COMPRESSION (5/80) WITH A STRONG LEAK PASSED THE EXHAUST VALVE. SUBSEQUENT INSPECTION FOLLOWING THE INSTRUCTIONS FOUND IN SB 388C REVEALED THE CYLINDER DID NOT MEET THE MEASUREMENT CRITERIA FOR TSDR 2006FA0001060Lifter · brokenLIFTER BROKE. (K)SDR AU510001735Screw · defective(AUS) CONTROL COLUMN/ELEVATOR BELLCRANK TORQUE TUBE SUPPORT SCREWS PNO MS35206-228 (2OFF3) DEFECTIVE. SCREWS APPEAR TO HAVE BEEN OVERTORQUED DURING ASSEMBLY. (OTHER CAUSE: MANUFACTURING QUALITY CONTROL ISSUE ) (CASA NR 510001735)SDR AU510001734Fitting · faulty(AUS) LT FORWARD DOORPOST WING STRUT ATTACHMENT FITTING MISSING 2 RIVETS PN MS20470AD6. FITTING AND SURROUNDING STRUCTURE SHOW EVIDENCE OF REWORK DURING MFG.(MANUFACTURING QUALITY CONTROL ISSUE ) (CASA NR 510001734)SDR 2005FA0000894Placard · reversedDURING INITIAL AUSTRALIAN CERTIFICATE OF AIRWORTHINESS INSPECTION, LT & RT CABIN DOOR HANDLE ESCUTCHEON/PLACARDS FOUND TO BE TRANSPOSED. THIS MEANS THAT INTERIOR DOOR HANDLE OPERATION INSTRUCTION IS IN REVERSE SENSE & EXIT HANDLE CANNOT BE OPERATED PER THE INSDR 2005FA0000893Placard · reversedDURING INITIAL AUSTRALIAN CERTIFICATE OF AIRWORTHINESS INSPECTION, LT & RT CABIN DOOR HANDLE ESCUTCHEON/PLACARDS FOUND TO BE TRANSPOSED. THIS MEANS THAT INTERIOR DOOR HANDLE OPERATION INSTRUCTION IS IN REVERSE SENSE & EXIT HANDLE CANNOT BE OPERATED PER THE INSDR CA050407008Brushes · loose(CAN) STARTER FAILED. BRUSHES WERE LOOSE UPON EXAMINATION AND WINDINGS BURNT. SUSPECT THE BRUSHES WERE LOOSE TO START WITH.SDR 2005FA0000158Alternator · failedPILOT DECLARED EMERGENCY, TOTAL ELECTRICAL FAILURE. DIAGNOSTIC INSPECTION REVEALED ALTERNATOR FAILURE. PILOT FAILED TO SEE WARNING LIGHT; DISCHARGE ON AMMETER AND LOW VOLT READING ON VOLT METER. (GL11200505028) (K)SDR CA041012006Switch · overheated(CAN) SWITCH WAS HOT TO THE TOUCH DURING GROUND FUNCTIONAL TEST. SWITCH DID NOT TRIP. SWITCH WENT OPEN CIRCUIT AFTER COUPLE MINUTES.SDR RG42004F00000Attach Bracket · crackedPART FOUND CRACKED DURING 100 HR INSPECTION. CRACK LOCATED AT LOWER LT CORNER OF PART, LT BRACKET. RECOMMEND PART OF STRONGER MATERIAL OR DIFFERENT DESIGN. OBTAINING ENGINEERING APPROVAL FRO MFG TO INSTALL HEAVIER DESIGNED PART, VIA FIELD APPROVAL. (FIRST SDR 2004FA0000816Stiffener · cracked2 INCH LONG CRACK IN LT AREA OF FIREWALL STIFFENER IN AREA OF THE PARKING BRAKE BRACKET MOUNTING. BELIEVED TO BE CAUSED BY FLEXING OF FIREWALL BY APPLICATION OF PARKING BRAKE. THIS IS THE SECOND AC IN FLEET WITH THIS PROBLEM. THIS AREA NEEDS ADDITIONAL REINSDR AUS20040434Support Bracket · cracked(AUS) BATTERY SUPPORT BRACKETS CRACKED.SDR 2004FA0000656Support · crackedOB BATTERY SUPPORT ANGLE CRACKED AT BOTH ENDS. THIS IS THE THIRD INSTANCE IN FLEET. THE BATTERY SUPPORT STRUCTURE NEEDS TO STRENGTHENED WITH ADDITIONAL STRUCTURE TO PREVENT THIS. (NM01200410074)SDR 2004FA0000306Bearing · missingDURING THE ANNUAL INSPECTION, IT WAS DETERMINED THAT THE BEARING FOR THE CO-PILOT RT RUDDER BAR TO BRAKE BELLCRANK WAS MISSING. THE FACTORY TORQUE SEAL ON THE ATTACHING HARDWARE WAS UNDISTURBED.SDR X072004F00000Actuator · inoperativePILOTS FOUND AILERON SYSTEM ROUGH ON PREFLIGHT. MECHANICS IN CHECKING OUT CAUSE, FOUND AILERON SYSTEM TO LOCKUP AND WOULD NOT FREE UP UNTIL SERVO WAS REMOVED. APPEARS BEARING IN GEAR BOX IS SLOPPY AND GEAR WILL BIND UP WHEN TURNED.SDR 2003FA0000631Check Valve · loosePILOT REPORTED RIGHT VACUUM PUMP WARNING LIGHT WAS ON. DURING TROUBLESHOOTING, DISCONNECTED HOSE FROM RIGHT SIDE OF CHECK VALVE MANIFOLD TO CONNECT TEST KIT AND DISCOVERED TWO MISSING RIVETS, TWO RIVETS ABOUT TO FALL OUT AND TWO LOOSE RIVETS ALL ON THE RIGHTSDR AUS20030530Line · cracked(AUS) STAINLESS STEEL FUEL PIPE LOCATED BETWEEN FUEL FILTER BOWL AND BOWL DRAIN VALVE CRACKED BENEATH (B) NUT FERRULE AT DRAIN VALVE END.SDR CA030427001Lock · collapsed(CAN) PILOT WAS PRACTICING A FORCED LANDING AND WAS ON FINAL APPROACH WITH FULL FLAPS, NO POWER AND A LOT OF TRIM TO PRODUCE A 70KT GLIDE. AS FULL THROTTLE WAS APPLIED AND ABORTED LANDING AT 500 FT, THERECLINABLE SEAT BACK COLLAPSED. THE PILOT MANAGED TO USE TSDR 2003FA0000506Strut · defectiveTHE DIAMETER OF THE OLOE TUBE IS .0012 INCHES SMALLER THAN THE BORE OF THE FORK. THE FORK WAS HELD ON ONLY BY THE NR5 BOLT. THE OLEO TUBE HAS AN UNUSUAL WEAR PATTERN OF CIRCUMFERENTIAL WEAR AND RIDGES. IT IS BELIEVED THAT THIS OLEO WAS DEFECTIVE FROM THE MASDR CA030414006Bulkhead · cracked(CAN) FUSELAGE SKIN PANEL UNDER REFUELING STEPS NOTED HAVING A BULGE AREA AROUND MOUNTING BOLT. SKIN MOVEMENT ALSO WAS EVIDENT WHEN WEIGHT WAS APPLIED TO THE STEP. DETAIL INSPECTION OF AREA FOUND BOTH THE FUSELAGE SKIN AND BULKHEAD WHERE THE STEP IS MOUNTED SDR CA030414005Skin · cracked(CAN) FUSELAGE SKIN PANEL UNDER REFUELING STEPS NOTED HAVING A BULGE AREA AROUND MOUNTING BOLT. SKIN MOVEMENT ALSO WAS EVIDENT WHEN WEIGHT WAS APPLIED TO THE STEP. DETAIL INSPECTION OF AREA FOUND BOTH THE FUSELAGE SKIN AND BULKHEAD WHERE THE STEPS ARE MOUNTESDR CA030414004Skin · cracked(CAN) FUSELAGE SKIN PANEL UNDER REFUELING STEP NOTED HAVING A BULGE AREA UNDER TOP REAR MOUNTING BOLT AREA. SKIN MOVEMENT ALSO WAS EVIDENT WHEN WEIGHT WAS APPLIED TO THE STEP. DETAIL INSPECTION OF AREA FOUND BOTH THE FUSELAGE SKIN AND BULKHEAD WHERE THE STEP SDR WDA2003F00000Fork · inoperativeDURING AN ANNUAL INSPECTION, WE REMOVED THE NOSE WHEEL PANT TOP ATTACHING BOLT AND THE LOWER FORK WITH THE TIRE ON IT FELL OFF OF THE STRUT ASSEMBLY. WE CALLED MFG TO VERIFY THAT FORK IS PRESSED ON THE STRUT ASSEMBLY. MFG REQUESTED THE FORK ASSEMBLY FOR FURTSDR 2003FA0000113Battery · corrodedSERIES 2000 AND 3000 BATTERY CORRODED FROM GASING BATTERY DISCOLORED SYTRAFOAM CASE, ALSO CAUSED DAMAGED TO ELT PLASTIC COVER. DISCOVERED AT ANNUAL INSPECTION. SUGGEST MORE FREQUENT INSPECTION.SDR LC12003F00000Rib · crackedDURING COMPLIANCE WITH SB FOR ELEVATOR RIVET INSTALLATION, THE ELEVATOR TOP, BOTTOM, AND TIP SKINS WERE CRACKED AND THE TIPS COULD BE FLEXED EASILY UP AND DOWN. AFTER REMOVING THE PLASTIC TIPS TO ACCOMPLISH THE SERVICE BULLETIN, IT WAS NOTED THAT THE ELEVATOR
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