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 = '152' 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 = '152' 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 CA981230025Caliper Housing · cracked(CAN) CRACK FOUND ON THE CALIPER HOUSING IN THE PIN LUG AREA.SDR 99ZZZX635Crankcase · crackedDURING 50 HOUR INSPECTION, AN APPARENT OIL LEAK WAS FOUND ON THE TOP LEFT OF ENGINE CASE. PERFORMED DYE PENETRANT TEST. FOUND CRACK IN CASE ABOVE NR 2 CYLINDER ALONG THE EXHAUST LIFTER BOSS. CRACK WAS APPROXIMATELY 4 INCHES LONG. NO APPARENT REASON FOR DEFSDR CA981130023Disc · misdrilled(CAN) BRAKE DISC FOUND WORN. SUBMITTER STATED PART DRILLED TO RECEIVE A .3125 INCH BOLT, BUT NORMAL BOLT IS .25 INCH.SDR CA981130022Control Unit · worn(CAN) CARBURETOR HEAT CONTROL WIRE FOUND WORN AT THE OUTLET OF CASING NEAR THE CARBURETOR BOX ARM. THIS ONLY DETECTED WITH CARBURETOR HEAT FULLY OPENED.SDR CA981130021Power Lever · misinstalled(CAN) NO FRICTION LOCK ON THROTTLE. WHEN THROTTLE REMOVED, IT WAS FOUND TO BE IMPROPERLY SECURED TO CARBURETOR ARM. THE BOLT WAS TOO LONG JAMMING CARBURETOR HOUSING. SUBMITTER STATED IMPROPER NUT USED AND NO COTTER PIN. SPECIAL CLAMP FOUND INSTALLED IN RESDR 98ZZZX4321Transmitter · wornSK152-21A KIT WAS INSTALLED DUE TO ERRONEOUS FUEL QUANTITY INDICATIONS. DURING REMOVAL OF OLD TRANSMITTERS. NOTICED THE FLOATS WERE WORN FROM CONTACT WITH THE INSIDE OF THE FUEL TANK AND ALSO AROUND PIVOT HOLE WHERE THEY ATTACH TO TRANSMITTERS. SUBMITTER STASDR 99ZZZX700Set Screw · malfunctionedAIRCRAFT AT CRUISE SPEED AT APPROXIMATELY 3,000 FEET, VALVE ADJUSTING SCREW COMPLETELY BACKED OUT OF ROCKER ASSY. LOSS OF INTAKE VALVE FOR THAT CYLINDER ENSUED CAUSING LOSS OF POWER, AND EMERGENCY LANDING OF AIRCRAFT.SDR 98ZZZX4262Air Pump · failedAIR PUMP FAILED AT START UP. SEE AIRBORNE SL 48. PUMP STILL TURNS, BUT SHAFT FAILED.SDR 98ZZZX3878Pin Plug · wornFOUND EXCESSIVE ALUMINUM FLAKES IN OIL FILTER. SUCTION SCREEN OK. COMP CHECK OK. REMOVED ALL CYLINDERS. PIN PLUG WORN, NR 1 CYL ASSY. SCUFFED CYLINDER WALL.SDR CA981006005Mount · broken(CAN) LOWER OLEO COLLAR FOUND BROKEN WHERE THE MOUNT LEG IS WELDED TO THE COLLAR. SOME OTHER IRREGULARITIES WERE FOUND USING NDT.SDR CA980922003Valve · leaking(CAN) ON TAXI FROM RAMP, EXCESSIVE FUEL WAS NOTICED COMING FROM THE LEFT WING VENT. VENT VALVE FOUND LEAKING.SDR 98ZZZX3440Hub · crackedCESSNA152 PROPELLER WAS RECEIVED FOR AD 9521-01 HUB INSPECTION. AFTER STRIPPING HUB, DISCOVERED CRACK AT LEADING EDGE BOLT HOLES. NR 1 AND NR 2 BLADES RUNNI NG ABOUT 2 INCHES LONG. PROPELLER RETURNED TO CUSTOMER.SDR 98ZZZX3452Push Rod · brokenDURING 100-HOUR INSPECTION NOTED DURING COMPRESSION TEST THAT NR 1 AND NR 3 CYLINDERS WERE LEAKING BY EXHAUST VALVES. WHEN CYLINDERS WERE REMOVED FOR REPAIR, FOUND NR 3 CYLINDER INTAKE PUSH ROD WAS DAMAGED. CAP PORTION AT ROCKER ARM END PULLED OUT OF ROD AS SDR 98ZZZX3310Antenna · separatedDURING ROUTINE PRE-FLIGHT INSPECTION, ANTENNA WAS FOUND BROKEN. THE WHIP HAD COME DISCONNECTED FROM BASE DURING A PRIOR FLIGHT. THE POTTING COMPOUND SECURING THE ANTENNA PARTS WAS SOFTENED AS LIKE PUTTY. APPARENTLY, EITHER THE POTTING COMPOUND WAS IMPROPERLSDR 98ZZZX3016Valve · failedNR 2 EXHAUST VALVES SEIZED IN VALVE GUIDE AND VALVE HEAD SEPARATED AFTER CONTACT WITH PISTON. SEIZURE OF VALVE STEM IN GUIDE MOST LIKELY DUE TO CARBON ACCUMULATION. AIRCRAFT OPERATED UNDER 14CFR PART 141. SUBMITTER RECOMMENDATION: C/W SB 388B AT MORE FREQUSDR GLBR98100Magneto · failedLEFT MAGNETO QUIT IN-FLIGHT. REMOVED AND REPLACED DISTRIBUTOR BLOCK AND GEAR ASSY IAW UNISON SPECS. INSTALLED ONE ENGINE IAW TEXTRON LYC SPECS. TIMED TO ENGINE. MAGS CHECK GOOD. (X)SDR AU980778Floor Panel · cracked(AUS) FLOOR PAN LOCATED ON THE TOP OF THE RT MAIN LANDING GEAR BOX STRUCTURE AT STN 56.69 CONTAINED SEVERAL CRACKS (APPROXIMATELY SIX) UP TO 52.8 MM (2 INCHES) LONG BETWEEN THE RIVETS ON TOP OF THE BULKHEAD AT THE REAR OF THE CABIN SEATS. SUSPECT CAUSED BY HEASDR 99ZZZX632Float · stuckAIRCRAFT IS USED FOR FLIGHT TRAINING. PILOT INDUCED POWER ON STALL. AT THIS TIME, AIRCRAFT BEGAN RUNNING ROUGH DUE TO AN EXCESSIVE RICH MIXTURE. AFTER AN EMERGENCY LANDING WAS MADE, THE PILOT TAPPED ON THE CARBURETOR WITH A HAMMER HANDLE, AND RE-STARTED THSDR CA980602028Guide · worn(CAN) DURING 100 HOUR INSPECITON, THE COMPRESSION ON #3 CYLINDER WAS FOUND LOW. TROUBLESHOOTING FOUND THE EXHAUST VALVE LOOSE WITHIN THE GUIDE. A CIRCULAR PIECE OF METAL WAS FOUND IN THE OIL RETURN GALLEY. IT WAS NOT READILY EVIDENT WHERE THE METAL ORIGINATED,SDR 98ZZZX2138Piston Ring · wornTHIS ENGINE HAD 3 CYLINDERS OVERHAULED WITH RINGS IN THE FIELD. THE FOURTH WAS REPLACED WITH A COMPLETE CHROME CYLINDER ASSY. AFTER 30 HOURS OF FLIGHT, THE OIL CONSUMPTION AND BLOW-BY BECAME EXCESSIVE. A COMPRESSION TEST SHOWED 20/80 OR THE 3 OVERHAULED ANDSDR CA980521012Control Cable · failed(CAN) ON INSPECTION, THE LOWER ELEVATOR TRIM CABLE FOUND BADLY CORRODED. WHEN PULLED ON, IT BROKE. REPLACED.SDR 98ZZZX1862Cylinder · defectiveINSTALLED NEW CYLINDER ASSEMBLIES. HAD NO COMPRESSION NR 1 CYLINDER. REMOVED, FOUND METAL CHIP UNDER VALVE. SUSPECT CAUSE - IMPROPER CLEANING PROCEDURE PRIOR TO ASSEMBLY. SUBMITTER RECOMMENDATION - MORE USEFUL INSPECTION (QC).SDR 98ZZZX1711Mount · crackedINSPECTION FOUND ENGINE MOUNT CRACKED AT NLG ATTACH.SDR 98ZZZX1929Warning Horn · failedAFTER A TRAINING FLIGHT, IT WAS REPORTED THE STALL WARNING HORN SOUNDED IN LEVEL FLIGHT. ON LANDING APPROACH, TONE CHANGED TO HIGHER PITCH (NORMAL STALL WARNING HORN). WHEN MECHANIC BLEW INTO WING STALL WARNING OPENING, HORN WOULD SOUND. IT ALSO SOUNDED WHESDR 98ZZZX2160Valve Keeper · wornVALVE KEEPERS WORN, BUT STILL INSTALLED. LET VALVE ASSY MOVE DOWN IN KEEPER ASSY. VALVE WOULD NOT COMPLETELY CLOSE. NO DAMAGE TO CYLINDER OR PISTON.SDR 98ZZZX1597Cylinders · crackedWHILE INVESTIGATING AN OIL LEAK, STAINS WERE NOTED ON THE LOWER SIDE OF THE ENGINE CYLINDERS. THE 4 EACH CYLINDERS WERE REMOVED FOR FURTHER INVESTIGATION AND CRACKS WERE NOTED APPROXIMATELY 1.25 INCHES DOWN FROM THE BARREL TO END. THE CRACKS WERE ON THE UPPESDR 98ZZZX2634Carburetor · misoverhauledDURING DISASSEMBLY FOR REPAIR, NOTED THAT ALL INSTALLED COTTER PINS WERE STANDARD STEEL HARDWRE AND NOT THE STAINLESS STEEL COTTER PINS SPECIFIED IN THE ILLUSTRATED PARTS LIST OF THE APPROPRIATE COMPONENT MM.SDR 98ZZZX1285Wire · shortedPILOT REPORTED FIRE ERUPTED FROM THE FUEL VENT IN-FLIGHT. AIRCRAFT LANDED SAFELY WITH NO VISIBLE DAMAGE. TROUBLESHOT CAUSE TO SENDING UNIT POWER WIRE CHAFING AT LT WING ROOT RIB. REPLACED WIRING FROM SENDING UNIT TO GAUGE.SDR 98ZZZX1020Coil · failedMAG COIL AT 500 HOURS BURNED THROUGH ON THE OPPOSITE SIDE OF HIGH TENSION LEAD. HAVE TO PULL COIL OUT TO SEE DAMAGED SPOT. ENGINE LOST POWER, TOOK MORE MANIFOLD PRESSURE TO MAINTAIN SAME RPM.SDR 98ZZZX1629Bracket · crackedCRACK FOUND DURING ROUTINE 100 HOUR INSPECTION. CRACK FOUND IN BRACKET ASSY THAT ATTACHES TO REAR SPAR OF HORIZONTAL STABILIZER WHICH ALSO HOUSES FITTING FOR ELEVATOR. SUBMITTER RECOMMENDATIONS: CLOSE INSPECTION OF AREA TO POSSIBLY INCLUDE DYE PENETRANT AFTSDR CA980302008Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. BLADES NOT ANODIZED AT LAST OVERHAUL. CORROSION FOUND UNDER PAINT.SDR 98ZZZX1083Fuel Gauge · errorsUPON RETURNING FROM FLIGHT, PILOT COMPLAINED THE ACFT REQUIRED MORE FUEL TO FILL TANKS THAN GAUGES INDICATED. ASKED MAINT TO CHECK GAUGES FOR ACCURACY. FUEL WAS COMPLETELY DRAINED FROM A/C, AND GAUGES READ ONE-EIGHTH (LT) AND ONE-FOURTH (RT). GAUGES WERE INSDR CA980311007Throttle Cable · jammed(CAN) DURING PRACTICE STALLS AND SPIN RECOVERIES THE THROTTLE CONTROL JAMMED FULL ON. AFTER LANDING THE THROTTLE WAS DISCONNECTED AT THE CARBURETOR. CARB LINKAGE OK BUT CABLE STILL JAMMED. CABLE REPLACED.SDR 98ZZZX691Rocker Adj Nut · looseAIRCRAFT REPORTED SUDDEN LOSS OF POWER ON TAKEOFF. UPON INSPECTION, FOUND ALL EXHAUST ROCKER VALVE ADJUSTING NUTS HAD INSUFFICIENT TORQUE. NR 3 CYLINDER ADJUSTMENT HAD BACKED OFF COMPLETELY. ENGINE HAS 90.9 HOURS SINCE OVERHAUL.SDR AU971569Pushrod · loose(AUS) PILOT REPORTED REDUCTION IN RPM AND ROUGH RUNNING IN FLIGHT.INVESTIGATION FOUND THE NO2 CYLINDER EXHAUST PUSHROD END FITTINGS WERE LOOSE, WITH ONE END OF THE PUSHROD SPLAYED AND CRACKED.SDR 98ZZZX102Magneto · failedINSTALLED TWO NEW 4381 MAGNETOS ON AN ENGINE REBUILD. LEFT MAG ROTATING MAGNET APPEARS TO HAVE FAILED DUE TO FACTORS UNKNOWN. RESULT IS A BENT SHAFT AT THE IMPULSE COUPLING. NO DAMAGE TO DRIVE GEARS NOTED.SDR 98ZZZX230Oil Filter · bulgedFILTER REPLACED 11-24-97. ENGINE GROUND CHECKED. 0IL PRESSURE NORMAL. ON NEXT FLIGHT, OIL WAS LOST OVERBOARD. ON EXAMINATION, FILTER WAS FOUND ELONGATED AND BULGED. FILTER TAKEN TO HAGGLIN MOTOR FOR INVESTIGATION. CONCLUSION WAS BULGING LIFTED FILTER OFFSDR 97ZZZX5159Control Cable · failedDURING STALL RECOVERY WORK, THE FLAPS WERE BEING MOVED TO A 20 DEGREE POSITION WHEN THE LEFT FLAP RETRACTED TO FULL UP TRAIL POSITION AND RIGHT FLAP REMAINED DOWN (THIS OCCURRED AFTER A LOUD BANG). THE ACFT ROLLED LEFT. PILOT INITIATED EMERGENCY PROCEDURES ASDR CA971117010Coupling · damage(CAN) DURING CHECK, FOUND THAT ALTHOUGH FLAP MOTOR WAS TURNING NORMALLY, FLAPS DID NOT APPEAR TO BE RESPONDING QUICKLY. INVESTIGATION REVEALED DEFECTIVE SPLINE COUPLING ON FLAP MOTOR SHAFT.SDR 97ZZZX4879Piston · failedINSPECTION FOUND HALF OF PISTON SKIRT BROKEN AWAY AND MISSING FROM BOTTOM RING GROOVE TO JUST BEFORE EACH PISTON PIN BOSS. OWNER HAD REPORTED AN INCREASE IN OIL COMSUMPTION. VISUAL INSPECTION OF ENGINE WAS OK. CYLINDER COMP ALL CHECKED 70 OVER 80 OR BETTER.SDR 97ZZZX4800Rib · crackedINSPECTION FOUND FAR RIGHT RIB IN HORIZONTAL STABILIZER CRACKED. LOWER CRACK FOUND TO BE 1 INCH, WHILE TOP, .75 INCH. THESE CRACKS ARE OVER AND BELOW THE ELEVATOR HINGE ATTACH POINT. IF NOT FOUND, COULD, IN TIME, CAUSE SEPARATION OF ELEVATOR FROM STABILIZER.SDR 97ZZZX4729Bolt · wrong partPURCHASED PART FROM CESSNA. PART DID NOT MATCH OLD PART, REORDERED AND NOTIFIED CESSNA ACCORDINGLY. SECOND ORDER ALSO DID NOT MATCH. BOLTS RECEIVED WERE NAS464P3A8 BOLTS, AND WERE TOO LONG TO USE - BOLTS HOLDING VERTICAL FIN TO FUSELAGE BRACKET.SDR 97ZZZX4496Control Cable · frayedDURING 100-HOUR INSPECTION, NOTED THE UPPER ELEVATOR TRIM TAB CABLE HAD SEVERAL BROKEN STRANDS. UPON REMOVAL, FOUND THE .0937 INCH 7 BY 7 CABLE WAS BROKEN IN TWO AREAS. ONE FORWARD OF AND THE OTHER AFT OF THE PULLEYS WHICH CHANGE CABLE DIRECTION IN THE HORIZSDR 97ZZZX3916Valve · mismanufacturedFUEL DRAIN VALVE DELIVERED NEW FROM CESSNA WOULD NOT SEAT PROPERLY. PART MANUFACTURERED BY AUTO VALVE INC, DAYTON, OHIO 45427. CURE DATE 1Q96. ASSY DATE 1Q97.SDR 97ZZZX3917Coil · failedINSPECTION FOUND BAD COIL IN MAGNETO. MAGNETO IN LEFT POSITION. AIRCRAFT ENGINE WOULD DIE WHEN LEFT MAG WAS SELECTED.SDR CA970902029Tappet · broken(CAN) SEVERE ENGINE VIBRATION IN FLIGHT. AIRCRAFT MADE FORCED LANDING. POST FLIGHT INSPECTION FOUND THE NR2 CYLINDER PUSH ROD LOOSE AND INTAKE PUSH ROD BENT. IT IS SUSPECTED THE TAPPET IS BROKEN. ENGINE WAS RETURNED TO MANUFACTURER.SDR 97ZZZX4210Hub · chafedREPLACED PROPELLER DUE TO FAILED AD 97-06-16. NEW PROPELLER HAS A LARGER HUB AND THERE IS INTERFERENCE WITH PROPELLER SPINNER.SDR 97ZZZX3864Switch · failedOWNER REPORTED DEAD BATTERY. BATTERY FOUND TOO HOT TO TOUCH, AND DEVOID OF ELECTROLYTE. TROUBLESHOOTING INDICATED SYSTEM VOLTAGE TO BE 1.6 VOLTS ABOVE NORMAL VALUES. FOUND INTERMITTENT RESISTANCE IN ALTERNATOR CONTROL SWITCH. RECOMMEND REGULAR SYSTEM VOLTASDR 97ZZZX3861Seal · crackedCARBURETOR BOX SEAL CESSNA PART MADE FROM THIN PLASTIC, LESS THAN 200 HOURS, AND CRACKS OUT DUE TO VIBRATION. ALL MODEL CESSNAS WITH CARBURETOR AIR BOX SEALS VIBRATE AND CRACK APART INTO ENGINE COMPARTMENT. SUBMITTER STATED SHOULD BE CONSTRUCTED OF MORE DURASDR 97ZZZX3831Control Unit · failedLOW VOLTAGE LIGHT ILLUMINATED IN-FLIGHT. INSPECTION REVEALED NO VOLTAGE TO FIELD TERMINAL ON ALTERNATOR. VERIFIED POWER SUPPLY TO ACU. NO ACU OUTPUT. INSTALLATION OF TWO ACU'S (ZERO TIME SINCE REPAIR/OVERHAUL) DID NOT RESTORE POWER. INSTALLATION OF ZEFTRO
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