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 = '172M' 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 = '172M' 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 CA981022005Bracket · damaged(CAN) HORIZONTAL MOVEMENT OF RUDDER WAS POSSIBLE WITH LIGHT PRESSURE. MOST NOTABLE AT LOWER HINGE. HINGE BRACKETS UPPER AND LOWER AT CENTER AND LOWER POSITIONS HAD ELONGATED BOLT HOLES. CAUSE NOT DETERMINED.SDR AU981249Switch · failed(AUS) FLAP POSITION SWITCH FAULTY. SWITCH WOULD NOT RETURN TO THE NEUTRAL POSITION. PART TC: 6,825.SDR CA981007003Pump · failed(CAN) AFTER INSTALLATION OF THE DRY AIR PUMP AND GROUND TEST, THE PUMP FAILED WITHIN ONE HOUR. CARBON VANES APPEAR TO HAVE STUCK IN THE CENTER HUB, ONLY ONE OR TWO VANES CAN BE HEARD WHEN THE PUMP IS ROTATED BY HAND.SDR CA981013014Pump · failed(CAN) ON DESCENT, REDUCTION OF 300-500 RPM WAS FOLLOWED 20 SECONDS LATER BY THE ENGINE SEIZING. AIRCRAFT LANDED SAFELY. POST-FLIGHT INSPECTION FOUND THE OIL PUMP HAD FAILED. THE ENGINE WAS A WRITE OFF; BROKEN AND SEIZED RODS, BROKEN CRANKCASE, ETC.SDR AU981165Crankshaft · corroded(AUS) CRANKSHAFT INTERNAL INSPECTION FOUND THAT THE CRANKSHAFT WAS CORRODED BEYOND LIMITS. FOUND DURING INSPECTION IAW AD/LYC/102AMDT 1.SDR AU981164Valve · missing(AUS) ENGINE OIL COOLER THERMOSTATIC BYPASS VALVE NOT FITTED TO THE ENGINE WITH THE HOLE BLANKED OFF BY A PLUG. FOUND DURING INSPECTION IAW AD/LYC/78 AMDT 5.SDR 98ZZZX3693Battery · brokenAT PRE-FLIGHT, OWNER FOUND CONTENTS OF ONE BATTERY CELL IN BAGGAGE AREA CARPET. FOUND ELT CASING CRACKED AND PIECES BROKEN AWAY IN BAGGAGE AREA. ELT BATTERY EXPLODED INSIDE UNIT.SDR 98ZZZX3450Battery · destroyedAT PRE-FLIGHT FOUND CONTENTS OF ONE BATTERY CELL ON AREA CARPET. FOUND ELT CASING CRACKED AND PIECES BROKEN AWAY IN BAGGAGE AREA.SDR 98ZZZX3608Wire · chafedALTERNATOR OUTPUT AND FIELD WIRES CHAFED AGAINST BAFFLE BEHIND ALTERNATOR. FIELD AND OUTPUT SHORTED TOGETHER CAUSING ALTERNATOR RUNAWAY. VOLTAGE RUINED MANY ELECTRICAL COMPONENTS. POTENTIAL FIRE. MASTER SWITCH WOULD NOT SHUT OFF RUNAWAY. SUBMITTER SUGGESTSDR 98ZZZX3560Cylinder · mismanufacturedENGINE L-34695-27A O/H BY TEXTRON LYC 11-8-97. INSTALLED 2-20-98. FOLLOWING TEST FLIGHT AND BREAK-IN, ACFT RELEASED FOR FLIGHT TRAINING. AT ENG SMOH 16.8 HRS ON TAKEOFF, A LOSS OF RPM AND DEGRADED CLIMB PERFORMANCE REQUIRED IMMEDIATE RETURN. SUBMITTER STATSDR 98ZZZX3559Cylinder · mismanufacturedENGINE L-34695-27A O/H BY TEXTRON LYC 11-8-97. INSTALLED 2-20-98. FOLLOWING TEST FLIGHT AND BREAK-IN, ACFT RELEASED FOR FLIGHT TRAINING. AT ENG SMOH 16.8 HRS ON TAKEOFF, A LOSS OF RPM AND DEGRADED CLIMB PERFORMANCE REQUIRED IMMEDIATE RETURN. SUBMITTER STASDR 98ZZZX3558Cylinder · mismanufacturedENGINE L-34695-27A O/H BY TEXTRON LYC 11-8-97. INSTALLED 2-20-98. FOLLOWING TEST FLIGHT AND BREAK-IN, ACFT RELEASED FOR FLIGHT TRAINING. AT ENG SMOH 16.8 HRS ON TAKEOFF, A LOSS OF RPM AND DEGRADED CLIMB PERFORMANCE REQUIRED IMMEDIATE RETURN. SUBMITTER STASDR AU981129Valve · missing(AUS) ENGINE OIL SYSTEM THERMAL BYPASS VALVE MISSING. VALVE BODY WAS FITTED TO THE OIL FILTER ADAPTER AS A PLUG. FOUND DURING INSPECTION IAW AD/LYC/78 AMDT 5.SDR AU981128Control Cable · corroded(AUS) FLIGHT CONTROL CABLES CORRODED AND WORN. SUBMITTER SUSPECTS CORROSION (RUST) IS A DIRECT RESULT OF THE RECENT STRIP AND RE-PAINT OF THE AIRCRAFT DUE TO CONTAMINATION BY THE PAINT STRIPPING CHEMICALS.SDR AU981127Spar · corroded(AUS) WING CENTER SECTION CARRY THROUGH SPAR CORRODED AND RIVET HEAD MISSING. RIVET HEAD HAD BEEN MISSING PRIOR TO RECENT RE-PAINT.SDR CA980825021Mount · cracked(CAN) DURING INSPECTION, A CRACK WAS FOUND ON THE ENGINE MOUNT WELD AT THE LEFT INBOARD SIDE OF THE LOWER CROSS BRACE.SDR AU980963Bolt · cracked(AUS) LEFT MAIN LANDING GEAR RETAINING BOLT CRACKED. FOUND USING MAGNETIC PARTICLE INSPECTION FOLLOWING FAILURE OF THE SIMILIAR BOLT ON THE RIGHT MAIN LANDING GEAR. SEE MDR 98/0962.SDR AU980962Bolt · sheared(AUS) RIGHT MAIN LANDING GEAR RETAINING BOLT FAILED. INVESTIGATION FOUND THAT THE BOLT HAD BEEN BROKEN FOR SOME TIME. RIGHT MLG LEG COLLAPSED.SDR 98ZZZX3244Seat Belt · malfunctionedTHIS BELT WAS INSTALLED IN BACK SEAT OF AIRCRAFT. A 200 PLUS POUND PERSON PUT ON SEAT BELT, AND WHILE MOVING AROUND, BELT WOULD LOOSEN UP NUMEROUS TIMES. NO CURLING EFFECT ON BELT. P/N LL01-AL24AB40AA-001.SDR 98ZZZX3415Camshaft · corrodedCORROSION PITS BEHIND EXPANSION PLATE IN CRANKSHAFT. PITS ALONG EDGE BETWEEN EXPANSION PLATE AND ID OF CRANKSHAFT. MISTAKENLY C/W AD 98-02-08. CORROSION PITS NOTED, BUT NO CRACKS.SDR CA980811007Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE WAS FOUND.SDR CA981202004Nozzle · separated(CAN) ENGINE POWER COULD NOT BE REDUCED BELOW 2300 RPM, THE THROTTLE APPEARED TO BE STUCK. ON THE ADVISE OF THE TOWER AND GROUND STAFF, THE PILOT SET UP AN APPROACH AND ONCE LANDING WAS ASSURED THE ENGINE WAS SHUT OFF BY SETTING THE MIXTURE TO IDLE CUTOFF. THSDR CA980706002Lock Tab · failed(CAN) PILOT WAS UNABLE TO SHUT DOWN THE ENGINE. INSPECTION OF THE CARBURETOR FOUND THE LONG LOK TAB WASHERS ON THE SAFETY SCREWS, THAT SECURE THE FLOAT BOWL TO THE CARBURETOR BODY, HAD FAILED ALLOWING THE MIXTURE VALVE TO SEPARATE FROM ITS RECEPTACLE. SUBMITSDR CA980615002Crankshaft · worn(CAN) CRANKSHAFT INSPECTED AS PRE FAA AD 98-02-08. NUMEROUS CORROSION PITTING FOUND EXCEEDING THE MAXIMUM INTERNAL DIMENSIONAL LIMITS. CRANKSHAFT SCRAPPED.SDR CA980616008Seal · broke(CAN) SEAL ON THE AIR BOX ASSEMBLY BROKE OFF AND WAS INGESTED INTO THE CARBURETOR. THE ENGINE WOULD NOT RUN ABOVE IDLE.SDR 98ZZZX2183Connect Rod · looseENGINE EXPERIENCED HIGH OIL TEMPERATURE 60 HOURS AFTER INSTALLING FACTORY OVERHAULED ENGINE. THERE WAS NOISE WHEN TURNING THE PROPELLER AFTER ENGINE SHUT DOWN. FACTORY SERVICE REP PULLED NR 3 AND NR 4 CYLINDERS AND FOUND THAT NR 3 AND NR 4 CONNECTING RODS HASDR AU980784Bolt · sheared(AUS) RIGHT MAIN LANDING GEAR ATTACHMENT BOLT SHEARED. MLG STRUT ROTATED IN ITS HOUSING AND THEN COLLAPSED. BOLT SHEARED DURING LANDING WHEN THE AIRCRAFT STRUCK A PILE OF GRAVEL. SUSPECT BOLT HAD ALREADY BEEN DAMAGED ALLOWING IT TO EASILY SHEAR WITHOUT CAUSISDR 98ZZZX3561Cylinder · mismanufacturedENGINE L-34695-27A O/H BY TEXTRON LYC 11-8-97. INSTALLED 2-20-98. FOLLOWING TEST FLIGHT AND BREAK-IN, ACFT RELEASED FOR FLIGHT TRAINING. AT ENG SMOH 16.8 HRS ON TAKEOFF, A LOSS OF RPM AND DEGRADED CLIMB PERFORMANCE REQUIRED IMMEDIATE RETURN. SUBMITTER STATSDR 98ZZZX1979Coil · openDURING A ROUTINE 500-HOUR INSPECTION ON THE MAGNETOS, FOUND THE COIL SECONDARY RESISTANCE OUT OF LIMITS: THE CIRCUIT WAS OPEN.SDR 98ZZZX1924Clamp · chafedTHE RUBBER CUSHION CLAMP THAT SUPPORTS THE WIRE BUNDLE TO THE ALTERNATOR WAS CHAFED BY THE STEEL BRAIDING ON THE WIRE WEARING THROUGH CAUSING AN ELECTRICAL SHORT MELTING TIE INSULATION. UPON FURTHER INVESTIGATION, THE OTHER TWO CLAMPS ON SAME WIRE WERE CHAFEDSDR CA980421021Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE AND CORROSION WAS FOUND ON THE LEADING EDGE AND THE FACE OF THE PROPELLER BLADES.SDR CA980529012Regulator · failed(CAN) ELECTRICAL FAILURE. REPLACED.SDR AU980375Propeller · damaged(AUS) PROPELLER CONTACTED GROUND SERVICING EQUIPMENT. PROPELLER WRITTEN OFF AND ENGINE CRANKCASE CRACKED.SDR CA980313006Wheel · failed(CAN) WHEEL FLANGE BOLTS PULLED FROM THEIR SOCKETS JAMMING WHEEL CAUSING DAMAGE. REPLACED.SDR 98ZZZX1013Wheel · crackedINSPECTION FOUND WHEEL CRACKED IN THE TYPICAL LOCATION. CRACKS EMANATING FROM EDGE OF FLANGE HOLES.SDR AU980034Switch · faulty(AUS) FLAP SWITCH FAULTY. FLAP SWITCH INTERNAL SPRING FAILS TO RETURN SWITCH TO NEUTRAL POSITION.SDR 98ZZZX975Throttle Control · failedPILOT REPORTED A SNAP OR SOMETHING GAVE AS HE ADVANCED THROTTLE ON GROUND. ENGINE RPM STAYED AT 1,100 RPM. INVESTIGATION REVEALED THAT CABLE OUTER HOUSING SLIPPED OUT OF METAL RETAINER AT CLAMP NEAR CARBURETOR. OUTER HOUSING APPARENTLY SHRUNK FROM HEAT. RESDR 98ZZZX553Alternator · failedALTERNATOR WAS OVERHAULED BY ELECTROSYSTEMS, INC. AFTER FAILURE, UNIT WAS OPENED AND ONE BRUSH WAS FOUND WORN COMPLETELY DOWN TO WIRE INSERT. SLIP RING WAS GROOVED DUE TO CONTACT WITH INSERT. ALTERNATOR HAD ONLY 341.8 HOURS SINCE OVERHAUL AND ONLY 8 MONTHS.SDR 98ZZZX99Coil · crackedDURING 500-HOUR INSPECTION, (PULLED AT 452.2 HOURS TSO), BOTH COILS IN TCM 2000 SERIES MAGNETO WERE FOUND CRACKED. COILS HAD THE FOLLOWING MARKINGS: 38/95 AND 8-9, 35/75 AND 10-10. MAGNETO WAS OVERHAULED BY ELECTROSYSTEMS, INC., FOR LYCOMING. ENGINE OVERHASDR CA971208001Crankcase · cracked(CAN) DURING INSPECTION, OIL WAS NOTICED AT LOWER SIDE OF NR 2 AND NR 4 CYLINDERS, ENGINE WAS WASHED DOWN AND A GROUND RUN-UP WAS CARRIED OUT. AN OIL LEAK WAS FOUND AT THE NR 2 CYLINDER DRAIN TUBE/LINE. LINE WAS REPLACED AND GROUND RUN WAS CARRIED OUT SERVICESDR 97ZZZX4714Fuel Tank · chafedAFTER REMOVING RIGHT FUEL TANK TO CHECK FOR LEAK, FOUND WEAR ON BOTTOM OF TANK INDENTED WITH RIVET HEAD MARKS. THE TANK RESTS ON A REINFORCEMENT PLATE THAT IS RIVETED TO STIFFENERS. USING A UNIVERSAL TYPE RIVET HEAD, A RUBBER CHAFE STRIP IS LAID OVER THE RIVSDR 97ZZZX4272Landing Light · deterioratedLANDING LIGHT REPLACED FOR BROKEN ELEMENT. THIS LAMP, AS WELL AS THE 4509 AND THE 4596, HAVE DETERIORATED TO THE POINT THE AVERAGE LIFE IS 50 HOURS TACH TIME.SDR 97ZZZX4270Control Cable · frayedLEFT PRIMARY AILERON CABLE WAS FOUND FRAYED DURING ROUTINE INSPECTION. SEVERAL HARD TO SEE AREAS OF CABLE WERE FRAYED (TOTAL TIME ON CABLE 4,101.1 HOURS. SUBMITTER RECOMMENDED CABLES BE REPLACED ON A TIME CHANGE BASIS, CABLE PN 0510105-224.SDR CA970610002Pitot Tubing · chafed(CAN) PITOT TUBE FROM THE PITOT MAST TO THE WING ROOT FOUND TO BE CHAFED AND LEAKING.SDR CA970609019Connecting Rod · broken(CAN) JUST AFTER CLIMB TO CRUISE ALTITUDE WHEN POWER WAS REDUCED A VIBRATION DEVELOPED AND A POWER LOSS WAS EXPERIENCED. THE PILOT NOTED HIGH OIL TEMPERATURE AND A LOSS OF OIL PRESSURE. AN EMERGENCY LANDING WAS CARRIED OUT IN A NEARBY FIELD. POST FLIGHT INSPECSDR CA970530005Blade · spray cut(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. LEADING EDGES OF PROPELLER BLADES FOUND WITH SPRAY CUTS.SDR 97ZZZX2623Air Filter · wrong partDURING ANNUAL INSPECTION, BRACKETT AIR FILTER ASSY WAS FOUND LOOSE ON THE AIRBOX. UPON REMOVAL, IT WAS FOUND TO BE THE INCORRECT ASSEMBLY FOR THE AIRCRAFT MODEL. THE MODEL 172M USES ASSEMBLY NR BA 5110, A BA 5710A WAS INSTALLED. THE CAMLOCK STUDS ON THE BA SDR AU970535Bulkhead · cracked(AUS) LOWER AFT DOORPOST BULKHEAD CRACKED - FOUND DURING INSPECTION IAW CESSNA SEB 97-1SDR 97ZZZX2795Seat Rail · wornREPLACED ALL SEAT RAILS AND ROLLERS ON SEATS. 529.4 HOURS LATER OF OPERATION, THE FOURTH HOLE AFT WAS FOUND OUT OF LIMITS PER AD 87-20-03R2. AD 87-20-03R2 STATES FIRST INSPECTION DUE 1,000 HOURS AFTER NEW RAILS INSTALLED. RECOMMEND REDUCING FIRST INSPECTIONSDR 97ZZZX2658Flap Track · corrodedSEVERE CORROSION AND WEAR FOUND ON TRACK DURING ANNUAL INSPECTION. TRACK AND ROLLERS SHOWED NO SIGNS OF RECENT LUBRICATION. TRACK IS AVAILABLE FOR INSPECTION.
Back to Cessna 172M