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 = '8KCAB' 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 = '8KCAB' 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 2000ZZZX622Strut · corrodedDURING ANNUAL INSPECTION, FOUND RT WING FORWARD LIFT STRUT, LOWER MOUNT AREA (ON STRUT) SEVERELY CORRODED (EXFOLIATION) AND CRACKED APPROXIMATELY 3 INCHES LONG FROM MOUNT BOLT HOLE UPWARD. AREA IS HIDDEN UNDER FAIRING. SPECIFIC CAUSE IS UNKNOWN. REPLACED PASDR 2000ZZZX371Baffle · looseAIRCRAFT WAS WRITTEN UP FOR HAVING A ROLL TENDENCY. INVESTIGATION BY MAINTENANCE FOUND INTERNAL BAFFLING ON LEFT FUEL TANK HAD COME LOOSE CAUSING TANK HAD COME LOOSE CAUSING TANK TO BUDGE INCREASING THE CAMBER ON THAT WING. FURTHER INSPECTION OF RT TANK FOUNSDR 99ZZZX4214Mount · failedENGINE MOUNT TUBE WAS FOUND BROKEN IN TWO WHERE IT CROSSES ABOVE MAGNETOS CAUSING EXCESSIVE FLEXING OF ENGINE IN MOUNT. AIRCRAFT WAS USED AS AN AEROBATIC TRAINER.SDR CA990531018Coil · broken(CAN) GOVERNOR OUTPUT PRESSURE LOW. REMOVED OLD SPRING AND FOUND IT TO BE BROKEN INTO THREE PIECES.SDR 99ZZZX958Line · separatedDURING AEROBATIC MANEUVERING, THE RT BRAKE FLUID LINE CAME LOOSE FROM THE PLASTIC T-FITTING ON THE BRAKE FLUID RESERVOIR. SUFFICIENT FLUID REMAINED IN THE BRAKE CYLINDER TO PROVIDE NORMAL BRAKING DURING LANDING. THE BRAKE SYSTEM (AS DELIVERED) USES PLASTIC TSDR 98ZZZX4768Dipstick · looseDIPSTICK VIBRATED LOOSE DURING SUSTAINED INVERTED FLIGHT AND 4 QUARTS OF OIL WERE LOST. ENGINE HAD OPERATED NORMALLY FOR 30 MINUTES OF AEROBATIC FLIGHT AND 30 MINUTES OF NORMAL FLIGHT BEFORE LOOSENING. ENGINE MANUFACTURER AND AIRCRAFT BUILDER DO NOT PROVIDE SDR 99ZZZX171Rod · crackedROD HAS A LINEAR INDICATION APPROXIMATLEY 1.75 INCHES LONG.SDR 98ZZZX2290Tank · leakLEFT FUEL TANK WAS LEAKING OUT OF FILLER NECK AREA. FOUND TANK BAFFLE BROKEN LOOSE IN TANK WHICH CAUSED CRACK AND LEAK AT FILLER NECK. TANK REPAIRED/REPLACED. SUBMITTER STATED THIS IS SECOND OCCURRENCE FOR THIS OPERATOR OF 2 8KCAB AIRCRAFT.SDR CA980610014Diaphragm · failed(CAN) DURING THE ENGINE RUN-UP PREPARATORY TO THE ANNUAL INSPECTION, THE ENGINE WAS RUNNING VERY ROUGH WITH BLADE SMOKE COMING FROM THE EXHAUST. INSPECTION REVEALED THE RUBBER DIAPHRAGM IN THE FUEL FLOW DIVIDER HAD DRIED OUT, DISINTEGRATED AND PLUGGED THE FUESDR 98ZZZX2454Rib · defectiveRIVETS PULLED AT BUTT RIB LT AND RT WING ON TOP SKIN. RIVETS PULLED THROUGH RIB NOT SKIN. AMERICAN CHAMPION CHANGED RIB THICKNESS AND FASTENER TYPE AND SPACING 1.5 YEARS AGO. UNKNOWN NUMBER OF WINGS OUT THERE WITH THIS PROBLEM. NEED SL OR AD.SDR 98ZZZX2453Rib · defectiveRIVETS PULLED AT BUTT RIB LT AND RT WING ON TOP SKIN. RIVETS PULLED THROUGH RIB NOT SKIN. AMERICAN CHAMPION CHANGED RIB THICKNESS AND FASTENER TYPE AND SPACING 1.5 YEARS AGO. UNKNOWN NUMBER OF WINGS OUT THERE WITH THIS PROBLEM. NEED SL OR AD.SDR 98ZZZX1606Battery · crackedBATTERY CASE CRACKED ON BOTH SIDES OF CELL BELOW POSITIVE POST. CRACKS STARTED FROM FACTORY SEAM DOWN ALMOST TO BOTTOM. CRACKS APPEAR EQUAL ON BOTH SIDES. LESS THAN 20 HOURS SINCE NEW. POSSIBLE INTERNAL SHORT CAUSED EXPLOSION.SDR 98ZZZX1630U-Bolt · brokenUPON LANDING, PILOT NOTED RIGHT MAIN LANDING GEAR WHEEL AND GEAR LEG MOVING BACK AND FORTH APPROXIMATELY 12 INCHES. FOUND BROKEN U-BOLT WHERE THE LANDING GEAR LEG COMES OUT OF THE FUSELAGE. U-BOLT BROKEN AT THE REAR.SDR 98ZZZX1423Fuel Line · leakingPILOT REPORTED ODOR OF FUEL IN THE COCKPIT. INSPECTION REVEALED FUEL SEEPAGE WHERE THE TUBE ASSEMBLY CONNECTS TO THE TEE AT THE HEADER TANK INLET (THIS IS THE TUBE ASSY FROM THE LEFT WING TANK). THE FLARE WAS FOUND TO HAVE AN OUTSIDE DIAMETER LARGER THAN THESDR 98ZZZX1315Fuel Line · leakingPILOT REPORTED ODOR OF FUEL IN THE COCKPIT. INSPECTION REVEALED FUEL SEEPAGE WHERE THE TUBE ASSEMBLY CONNECTS TO THE TEE AT THE HEADER TANK INLET (THIS IS THE TUBE ASSY FROM THE LEFT WING TANK). THE FLARE WAS FOUND TO HAVE AN OUTSIDE DIAMETER LARGER THAN THESDR 97ZZZX4500Spar · crackedDURING ANNUAL INSPECTION, PERFORMED WING SPAR INSPECTION PER AMERICAN CHAMPION SL 406 FOR WOOD SPARS: AC-43-16 ALERT NR 226 MAY97: FOUND EXTENSIVE COMPRESSION CRACKS AT FRONT, REAR AT BOTTOM OF BOTH WING SPARS. AIRCRAFT USED FOR AEROBATIC FLIGHT. AD 87-18SDR 97ZZZX2958Fitting · seepOWNER COMPLAINED OF FUEL SMELL IN THE COCKPIT. FOUND A SEEP ON THE EXIT FITTING, TOP OF HEADER TANK, UNDER DASH GOING TO THE FIREWALL SOV. THIS TANK IS SUPPLIED BY BOTH WING TANKS. FITTING IS A COMPRESSION TYPE, NOT AN AN-FLARE. MECHANIC WENT TO SNUG IT SDR AU970761Fitting · cracked(AUS) WING STRUT ATTACHMENT FITTING CRACKED - FOUND DURING MAGNETIC PARTICLE INSPECTION IAW AD/CHA22/2 - CRACK ORIGINATED FROM AIRCRAFT TIEDOWN ATTACHMENTSDR 97ZZZX2070Rib · crackedUPON INSPECTION FOR RECOVER PROCESS, FOUND BRACKET P/N 2-1992 AND RIB P/N 3-446 CRACKED AT SPAR ATTACH. SL 404 COVERS THIS SUBJECT FOR '7' SERIES AIRCRAFT WITH 1,000 'PLUS' HOURS, BUT DOES NOT INCLUDE '8' SERIES AIRCRAFT, THIS CONDITION FOUND ON BOTH AILERONSSDR 97ZZZX2059Bracket · crackedUPON INSPECTION FOR RECOVER PROCESS, FOUND BRACKET P/N 2-1992 AND RIB P/N 3-446 WERE CRACKED AT SPAR ATTACH. SL 404 COVERS THIS SUBJECT FOR '7' SERIES AIRCRAFT WITH 1,000 'PLUS' HOURS, BUT DOES NOT INCLUDE '8' SERIES AIRPLANES. THIS CONDITION FOUND ON BOTH ASDR 97ZZZX4530Fuel Vent · obstructedAIRCRAFT EXPERIENCED ENGINE FAILURE DURING AEROBATIC FLIGHT. PILOT ATTEMPTED TO RESTART ENGINE WITH NO SUCCESS. AIRCRAFT LANDED ON ROAD, LOST DIRECTIONAL CONTROL, AND IMPACTED A FENCE PARALLELING THE ROAD. SUBSTANTIAL DAMAGE WAS DONE. INVESTIGATION WAS DONSDR 97ZZZX179Pedal · failedTHE OPERATOR REPORTS A THIRD FAILURE OF THE LEFT FORWARD RUDDER PEDAL AT THE LOWER LEFT HAND CORNER AT 65 HOURS TIMES IN SERVICE. THIS FIRST AND S ECOND FAILURE OCCURRED AT 147 AND 86 HOURS RESPECTIVELY. PART TOTAL TIME AVERAGE = 93 HOURS.SDR 97ZZZX2582Gasket · deterioratedUPON ANNUAL INSPECTION, THE INDUCTION AIR FILTER GASKET WAS FOUND DETERIORATED, LOOSE ON FILTER ASSY. BRACKET AD 96-09-06 DOES NOT COVER THIS ASSY MODEL. SUGGEST INCLUDING MODEL IN AD AND/OR INSPECTING ALL BRACKET AIR FILTER ASSEMBLIES FOR AD 96-09-06 CONDITSDR 96ZZZX4032Strut Fitting · crackedINSPECTED THE LIFT STRUT FITTINGS (PN 3-1632-1 AND PN 316322) IAW AD 96-03-11 PER AMERICAN CHAMPION SERVICE LETTER NR 408. FOUND TWO OF THE FOUR FITTINGS CRACKED AT THE RADIUS AS SHOWN IN THE ILLUSTRATION. INSTALLED THE NEW STYLE FITTINGS (PN 3-1691) PER AMESDR 96ZZZX4031Strut Fitting · crackedINSPECTED THE LIFT STRUT FITTINGS (PN 3-1632-1 AND PN 316322) IAW AD 96-03-11 PER AMERICAN CHAMPION SERVICE LETTER NR 408. FOUND TWO OF THE FOUR FITTINGS CRACKED AT THE RADIUS AS SHOWN IN THE ILLUSTRATION. INSTALLED THE NEW STYLE FITTINGS (PN 3-1691) PER AMESDR EY2R9600824Blade · corrodedBLADE, SN E83260, FOUND CORRODED.SDR EY2R9600823Blade · corrodedBLADE, SN E84429, FOUND CORRODED.SDR CA960527007Spar · cracked(CAN)THE REAR SPAR EXHIBITS SIGNS OF WOOD COMPRESSION FAILURE AT THE 46 INCH LOCATION OUTBOARD FROM THE ROOT.SDR AU960505Fitting · cracked(AUS) WING STRUT FITTINGS (4OFF) PNO 3-1632-1 AND PNO 3-1632-2 CRACKED IN THE CORNER OF THE RECTANGULAR HOLLOW SECTIONS - FOUND DURINGINSPECTION IAW AD/CHA/25 AND SL408 - AIRCRAFT HAS ONLY 103 HOURS TIME SINCE NEW WITH 20 HOURS OF AEROBATIC TIMESDR AU960491Fitting · cracked(AUS) BOTH FORWARD WING STRUT FITTINGS PNO 3-1362-1 AND PNO 3-1632-2 CRACKED - ALL FOUR FORWARD AND REAR FITTING PIECES CRACKED - FOUND DURING DYE PENETRANT INSPECTIONSDR AU960439Fitting · worn(AUS) WING STRUT ATTACHMENT FITTINGS (4OFF) FOUND WITH CHAFE MARKS - ALSO TWO OF THE FITTINGS HAVE SEVERAL BOLT HOLES NOT DEBURRED -FOUND DURING INSPECTION IAW AD/CHA/25 AMDT 1SDR 96ZZZX2174Pedal · failedINSTALLED THE 4TH RUDDER PEDAL. THIRTY-FIVE HOURS TACH TIME ON THE THIRD RUDDER PEDAL BEFORE FAILURE.SDR 96ZZZX1986Rudder Pedal · failedSUBMITTER STATES THIS IS THE THIRD FAILURE OF THE NEW STYLE RUDDER PEDALS FROM AMERICAN CHAMPION AIRCRAFT. IT IS THE THIRD BROKEN RUDDER PEDAL IN 298.0 HRS.SDR 96ZZZX2022Tank · baffle brokenWITH LEFT TANK FULL, FUEL GAUGE READ 'ZERO' GALLONS. REMOVED SENDER AND CHECKED, OPERATION NORMAL. FOUND FUEL TANK BAFFLE BROKEN OFF AND LAYING ON BOTTOM OF TANK. SENDER PROBLEM TRACED TO FLOAT BEING CAUGHT ON LOOSE BAFFLE LAYING IN TANK. (REMOVED TANK FORSDR AU960019Trim Tab · distorted(AUS) ELEVATOR TRIM TAB DAMAGED AT INBOARD END - LOWER TRIM CABLE TURNBUCKLE SEPARATED AT TURN BARREL - RIVETS ATTACHING TRIM TAB TO TAB HINGE REPLACED APPROXIMATELY 700 HOURS PREVIOUSLY - RIVET TAILS HAD WORKED EXTENSIVELY AND WERE NOT HOLDING THE STRUCTURETSDR 96ZZZX355Support Strap · crackedFACTORY EXCHANGE FORWARD PILOT SEAT PREVIOUSLY INSTALLED 11-03-89 IAW AD 89-18-06, FOUND SEVERELY BENT, STRETCHED, AND CRACKED SUPPORT WEB STRIPS. SUBMITTER STATED WITH HIGH G-LOAD FACTORS, SUGGEST RE-ENGINEERING OF SUPPORT SYSTEM.SDR 96ZZZX195Servo Injector · seal failedWHILE IN LEVEL FLIGHT AT AN ALTITUDE OF 4,500 FEET MSL, ENGINE DEVELOPED A ROUGH RUNNING CONDITION AND THEN QUIT. UPON INSPECTION OF SERVO INJECTOR, FOUND A SEAL IN THE DIAPHRAGM HOUSING HAD BECOME DEFECTIVE.SDR 95ZZZX7010Window · departedRIGHT REAR WINDOW DEPARTED AIRCRAFT DURING FLIGHT. LEADING EDGE OF WINDOW IS HELD DOWN BY A METAL STRIP WITH 3 SCREWS. WINDOW AND NEW SEAL INSTALLED. OPERATOR SUGGESTS USE OF SEALANT BETWEEN FRAME AND WINDOW ON LEADING EDGE WILL PREVENT AIRFLOW FROM PEELINGSDR 95ZZZX6161Blade · seal failedPROPELLER WAS INSIDE OF OVERHAUL TIMES. IT WAS LEAKING GREASE. AFTER DISASSEMBLY, THE TEFLON TAPE AROUND THE SHANK THAT THE BLADE SEAL RIDES ON HAD FALLEN OFF; THUS, CAUSING THE LEAK. ALSO, THE BLADE SEAL HAD STARTED CUTTING INTO THE BLADE SHANK. ALSO, NOTSDR 95ZZZX6160Blade · seal failedPROPELLER WAS INSIDE OF OVERHAUL TIMES. IT WAS LEAKING GREASE. AFTER DISASSEMBLY, THE TEFLON TAPE AROUND THE SHANK THAT THE BLADE SEAL RIDES ON HAD FALLEN OFF; THUS, CAUSING THE LEAK. ALSO, THE BLADE SEAL HAD STARTED CUTTING INTO THE BLADE SHANK. ALSO, NOTSDR 95ZZZX3859Alternator · wire burnedALTERNATOR SHORTED INTERNALLY IN-FLIGHT CAUSING SMOKE IN COCKPIT. PILOT MADE EMERGENCY LANDING. INSPECTED AIRCRAFT, FOUND ALTERNATOR OUTPUT TERMINAL SHORTED TO GROUND. THERE IS NO CIRCUIT PROTECTION ON ALTERNATOR OUTPUT CIRCUIT. THIS CAUSED WIRING TO BURN SDR 95ZZZX4352Pedal · brokePEDAL BROKE IN TWO WITH NORMAL PRESSURE APPLIED. FACTORY PARTS DEPARTMENT REPORTS THIS IS SECOND ONE THAT HAS BROKEN. REPLACED WITH NEW FACTORY PART. TOTAL TIME OF AIRCRAFT 143.8 HOURS SINCE NEW.SDR 95ZZZX966Switch · miswiredAMERICAN CHAMPION AIRCRAFT, SUPER DECATHLON, FEB 94 MODEL. LEFT AND RIGHT MAGNETO WIRES FOUND INSTALLED ON INCORRECT SWITCH IN COCKPIT. LEFT WIRE FOUND LOOSE ON SWITCH. A/C TT 27.0 HRS.SDR 96ZZZX5031Crankshaft · corrodedDURING OVERHAUL INSPECTION OF CRACKSHAFT, SOME CORROSION PITTING WAS NOTED ON OUTSIDE DIAMETER OF SEVERAL BEARING JOURNALS. INSPECTION OF FRONT MAIN INSIDE DIAMETER REVEALED AN AREA OF APROXIMATELY 20 CORROSION PITS. PITS WERE APPROXIMATELY .010 INCH DEEP ANSDR 95ZZZX825Flex Tube · misinstalledDURING ENGINE MAINTENANCE, NOTED THAT UPON REINSTALLING THE LOWER ENGINE COWL THAT THE FLEX TUBE CAN BECOME FOLDED AND BLOCK AIR FLOW TO THAT AIR SCOOP BOX AND FUEL INJECTOR. SUBMITTER RECOMMENDS REMOVAL OF AIR FILTER TO INSPECT FOR THIS CONDITION AFTER EACH
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