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 99ZZZX4220Bracket · crackedPERFORMED A DETAILED INSPECTION OF BRACKET, PN 0432004-9, CRACKS WERE FOUND ALONG TOP PART OF BRACKET ON THE WELD AREA, ONE CRACK 2 INCHES LONG,THE OTHER CRACK, 1.25 INCHES LONG. ALSO, CRACKS WERE FOUND ALONG RIVNUT HOLES AND BOLT HOLE ON THE MAJORITY OF THE SDR 99ZZZX4250Bolt · wrong partCESSNA 152 TEXAS TAIL DRAGGER CONVERSION. TAILWHEEL HALVE SEPARATED AFTER LANDING DUE TO IMPROPER LENGTH BOLTS (TOO SHORT). INSTALLED CORRECT LENGTH BOLTS AFTER INSPECTING WHEEL HALVES.SDR CA991028053Rib · cracked(CAN) HORIZONTAL STABILIZER LEFT RIB CRACKED.SDR CA991028052Rib · cracked(CAN) HORIZONTAL STABILIZER RIGHT RIB CRACKED.SDR CA991004053Switch · burnt(CAN) WHILE IN THE CIRCUIT WITH THE LANDING LIGHT SELECTED ON, THE PILOT NOTICED SMOKE AND FUMES IN THE COCKPIT, DECLARED AN EMERGENCY AND LANDED THE AIRCRAFT. MAINTENANCE TRACED THE PROBLEM TO AN OVERHEATED LANDING LIGHT SWITCH AND REPLACED THE SWITCH.SDR 2000ZZZX20Cylinder · crackedMASSIVE OIL LEAK REVEALED CRACKED CYLINDER BARREL ON LYCOMING P/N LW16703, 506.2 TTSN. DISCOVERED 9-9-99.SDR 20000622SH001Spar · crackedDURING SCHEDULED INSPECTION, FOUND RUDDER SPAR CRACKED AT UPPER LIGHTENING HOLE NEAR THE UPPER HINGE BRACKET. AFTER EXAMINATION OF 6 OTHER 152''S IN THE FLEET, FOUND 2 OTHERS WITH SIMILAR CRACKS, CESSNA SEB 94-3 PERTAINS TO THIS SUBJECT. REPLACED SPAR WITH SSDR 99ZZZX3744Rocker Boss · failedCRUISE, LEVEL FLIGHT, ENGINE STARTED RUNNING VERY ROUGH; INSTRUCTOR LANDED SAFE IN GRASS FIELD. INSPECTION REVEALED NR 3 CYLINDER ROCKER SHAFT BOSS BROKEN OFF. ENGINE HAD 100 HRS TIS FROM MAJOR OVERHAUL.SDR 99ZZZX3576Fitting · crackedUPON INSPECTION OF AIRFRAME, DISCOVERED THAT LOWER RIGHT AFT VERTICAL STABILIZER ATTACH FITTING WAS CRACKED, AND LEFT HAND SIDE CORRODED. SUBMITTER STATED CAUSE APPEARS TO BE AGE RELATED.SDR AU990851Engine · noisy(AUS) ENGINE EXPERIENCED UNUSUAL NOISES. INSPECTION AND GROUND RUN COULD FIND NO EVIDENCE OF DEFECT. DEFECT NOT CONFIRMED.SDR 99ZZZX2794Spar Assy · mismanufacturedRECEIVED ONE NEW SPAR ASSY ON OR ABOUT 7-15-99. WHEN PART WAS INSPECTED PRIOR TO USE, IT WAS OBVIOUS THE HINGE BRACKET WAS CROOKED AS INSTALLED. THIS PART IS RIVETED TO THE SPAR BY CESSNA. THE PART WAS RETURNED TO KANSAS CITY AVIATION CENTER AND A NEW ONE WSDR AU990770Skin · corroded(AUS) AIRCRAFT CONTAINED MAJOR CORROSION. AIRCRAFT HAD BEEN STRIPPED AND REPAINTED APPROXIMATELY FOUR MONTHS PREVIOUSLY AND IT IS SUSPECTED THAT THE AIRCRAFT WAS INCORRECTLY STRIPPED AND TREATED BEFORE PAINTING.SDR CA990707053Fuel · contaminated(CAN) FUEL CONTAMINATION, WATER.SDR CA990728087Cylinder · damaged(CAN) LOSS OF ENGINE POWER. VALVE PISTON AND CYLINDER DAMAGE FOUND AT INITIAL INSPECTION, SENT FOR TEARDOWN.SDR 99ZZZX2400Dist Block · wornDURING ROUTINE 500-HOUR INSPECTION OF BOTH MAGNETOS, OILITE BUSHING IN BOTH LT AND RT DISTRIBUTOR BLOCKS WERE FOUND WORN EXCESSIVELY. REPLACED WITH NEW K3822 DISTRIBUTOR BLOCK AND GEAR ASSEMBLIES. DUE TO LOW TIME ON MAGNETOS, SUBMITTER SUGGESTED POSSIBLE CAUSDR 99ZZZX2399Dist Block · wornDURING ROUTINE 500-HOUR INSPECTION OF BOTH MAGNETOS, OILITE BUSHING IN BOTH LT AND RT DISTRIBUTOR BLOCKS WERE FOUND WORN EXCESSIVELY. REPLACED WITH NEW K3822 DISTRIBUTOR BLOCK AND GEAR ASSEMBLIES. DUE TO LOW TIME ON MAGNETOS, SUBMITTER SUGGESTED POSSIBLE CAUSDR 99ZZZX2717Hub · crackedPROPELLER CRACKED BEYOND LIMITS OF AD 97-06-16 SECTION III. PROPELLER REMOVED FROM SERVICE. TTP UNKNOWN. TTA: 5,147.8.SDR 99ZZZX2290Plug · wornFOUND METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMITS CONTAINED IN LYC SI 1492B. FOUND FORWARD PISTON PIN PLUG IN NR 1 CYINDER EXCESSIVELY WORN DUE TO PISTON RING WEAR STEP SHAVING THE PLUG ON EACH STROKE. FOUND GALLING ON UPWARD FACING PISTON SKIRT. SDR 99ZZZX2289;Plug · wornFOUND METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMITS CONTAINED IN LYC SI 1492B. FOUND FORWARD PISTON PIN PLUG IN NR 1 CYLINDER EXCESSIVELY WORN DUE TO PISTON RING WEAR STEP SHAVING THE PLUG ON EACH STROKE. FOUND GALLING ON UPWARD FACING PISTON SKIRTS.SDR 99ZZZX2288Plug · wornFOUND METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMITS CONTAINED IN LYC SI 1492B. FOUND FORWARD PISTON PIN PLUG IN NR 2 CYLINDER EXCESSIVELY WORN DUE TO PISTON RING WEAR STEP SHAVING THE PLUG ON EACH STROKE. FOUND GALLING OF UPWARD FACING PISTON SHIRT. SDR 99ZZZX2287Pug · wornFOUND METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMITS CONTAINED IN LYC ST 1492B. FOUND FORWARD PISTON PIN PLUG IN NR 1 CYLINDER EXCESSIVELY WORN DUE TO PISTON RING WEAR STEP SHAVING THE PLUG ON EACH STROKE. FOUND GALLING ON UPWARD FACING PISTON SKIRT. SDR 99ZZZX2204Spar · crackedRIGHT ELEVATOR OUTBOARD HINGE ATTACH POINT CRACKED AROUND RIVETS ON SPAR. POSSIBLE CAUSE IS OIL CANNING OF ATTACH POINT ON SPAR.SDR 99ZZZX2199Plug · wornWHILE C/W LYC SI 1492B (PISTON PIN PLUG WEAR INSPECTION) AND FINDING METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMITS CONTAINED IN SI 1492B, FOUND THE FORWARD PISTON PIN PLUG EXCESSIVELY WORN DUE TO A PISTON RING WEAR STEP IN THE NR 1 CYLINDER ON THE FORWSDR 99ZZZX2193Plug · wornWHILE C/W LYC SI 1492B (PISTON PIN PLUG WEAR INSPECTION) AND FINDING METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMITS CONTAINED IN SI 1492B, FOUND THE FORWARD PISTON PIN PLUG EXCESSIVELY WORN DUE TO A PISTON RING WEAR STEP IN THE NR 1 CYLINDER ON THE FORWSDR 99ZZZX2192Plug · wornWHILE C/W LYC SI 1492B (PISTON PIN PLUG WEAR INSPECTION) AND FINDING METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMITS CONTAINED IN SI 1492B, FOUND THE FORWARD PISTON PIN PLUG EXCESSIVELY WORN DUE TO A PISTON RING WEAR STEP IN THE NR 1 CYINDER ON THE FORWASDR 99ZZZX2182Spar · misdrilledSTABILIZER APPEARS TO HAVE BEEN REPAIRED USING NEW SKINS AND USED P/N 0432001-56 SPARS AND USED P/N 0432001-15 REINFORCEMENT. THE RIVETS SECURING THE SKINS TO THE SPARS DO NOT ALIGN WITH THE EXISTING HOLES IN THE SPARS OR REINFORCEMENT. THIS LEAVES UNFILLED SDR 99ZZZX2201Plug · wornWHILE C/W LYC SI 1492B (PISTON PIN PLUG WEAR INSPECTION) AND FINDING METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMITS CONTAINED IN SI 1492B, FOUND THE FORWARD PISTON PIN PLUG EXCESSIVELY WORN DUE TO A PISTON RING WEAR STEP IN THE NR 1 CYLINDER ON THE FORWSDR 99ZZZX2191Plug · wornWHILE C/W LYC SI 1492B (PISTON PIN PLUG WEAR INSPECTION) AND FINDING METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMITS CONTAINED IN SI 1492B, FOUND THE FORWARD PISTON PIN PLUG EXCESSIVELY WORN DUE TO A PISTON RING WEAR STEP IN THE NR 1 CYLINDER ON THE FORWSDR 99ZZZX2152Fitting · crackedTHERE ARE 2 OF THESE FITTINGS USED TO SECURE VERTICAL FIN TO FUSELAGE. THE RIGHT FITTING WAS CRACKED AT THE BASE IN THE RADIUS. THIS CRACK WAS FOUND DURING A 100-HOUR INSPECTION. BOTH FITINGS WERE CHANGED AS PRECAUTION. CAUSE UNKNOWN.SDR AU990341Shaft · misinstalled(AUS) CARBURETOR HEAT SHAFT INCORRECTLY SECURED. SPLIT PIN USED INSTEAD OF THE CORRECT ROLL PIN.SDR AU990339Hose · mismanufactured(AUS) OIL COOLER HOSE TOO LONG.SDR AU990338Bolt · loose(AUS) MIXTURE CONTROL SYSTEM BOLT LOOSE.SDR AU990337Filter · misinstalled(AUS) OIL FILTER NOT LOCKWIRED.SDR AU990336Heater · misrigged(AUS) CARBURETOR HEATING SYSTEM INCORRECTLY RIGGED. HEAT `ON' CONTINUOUSLY.SDR AU990335Lead · misrouted(AUS) ENGINE HIGH TENSION LEADS LYING AGAINST EXHAUST PIPE.SDR AU990334Throttle · misrigged(AUS) THROTTLE CONTROL LEVER INCORRECTLY RIGGED AND NOT SPLIT PINNED.SDR AU990333Clamp · loose(AUS) ROTATING BEACON CLAMP LOOSE. GLASS LOST AND BULB BROKEN.SDR CA991209093Clevis Bolt · failed(CAN) BOLTS FOUND CRACKED AFTER AIRCRAFT DESTROYED IN ACCIDENT.SDR 20000712SH028Encoder · failedREPORTING INVALID ALTITUDE SEVERAL DIFERENT DATES. REPLACED WITH NEW ENCODER OF DIFFERENT MFG. (X)SDR 99ZZZX1412Throttle Control · separatedWHILE LANDING AT INDEPENDENCE, MO, PULLED BACK ON THE THROTTLE AND THE THROTTLE KNOBS AND SHAFT DISCONNECTED AT THE CABLE AND CAME OUT OF THE INSTRUMENT PANEL. ENGINE RPM WAS LOCKED AT 1,000 RPM. NOTIFIED THE TOWER OF THE PROBLEM AND LANDED WITHOUT INCIDENT.SDR 99ZZZX1456Pushrod · crackedUPON 100-HOUR INSPECTION TO DETERMINE APPLICABILITY TO AD 80-25-02 R2, NOTED THAT NR 4 CYLINDER INTAKE PUSH ROD P/N 73806T-T WHICH DOES NOT APPLY TO AD, WAS FOUND CRACKED AT END OF ALUMINUM TUBE THAT SWAGES ONTO BALL END OF PUSH ROD, TWO CRACKS WERE OBVIOUS VISDR 99ZZZX1191Control Cable · frayedREMOVED RUDDER CABLES FOR LENGTH VARIFICATION. FOUND BROKEN STRANDS AT AFT PULLEY POSITION.SDR AU990115Blade · corroded(AUS) PROPELLER BLADE FACE CONTAINED EXFOLIATION CORROSION LOCATED APPROXIMATELY 50 MM (1.96 INCHES) FROM THE LEADING EDGE. PART TC: 198.SDR AU990314Clock · failed(AUS) CLOCK FAULTY. SMOKE IN CABIN.SDR 99ZZZX1197Spar · crackedDURING ANNUAL INSPECTION, FOUND RT ELEVATOR OUTBOARD HINGE P/N 043200171 BOLT HOLE ELONGATED. AFTER REMOVING THREE FOR REPLACEMENT, FOUND ELEVATOR SPAR, PN 0432001-21 CRACKED AT HOME ATTACHMENT RIVET HOLES. THERE IS NO WAY TO INSPECT THE SPAR WITHOUT DE-RIVESDR AU990030Angle · corroded(AUS) LEFT WING ROOT LEADING ATTACHMENT ANGLE CORRODED. FOUND DURING INVESTIGATION OF A FUEL TANK PROBLEM. PART TC: 8,168.SDR 99ZZZX582Floorboard · crackedDURING ANNUAL INSPECTION, FOUND THE FLOOR PAN CRACKED AT THE END OF THE COPILOT'S INBOARD SEAT TRACK. THIS IS THE FORTH PLANE OUT OF SIX 152'S THAT HAVE HAD TO BE REPAIRED. THE SEAT TRACK IS WEARING INTO THE RADIUS OF THE BEND OF THE FLOOR PAN. THERE IS NO SDR 99ZZZX1115Motor · failedWHILE A STUDENT PILOT WAS PRACTICING TOUCH AND GOES, THE FLAPS FAILED TO GO BEYOND 20 DEGREES. THE STUDENT CYCLED THE FLAP LEVER SEVERAL TIMES AND THE FLAPS STAYED AT 20 DEGREES. THE STUDENT HIT THE RUNWAY NOSE FIRST AFTER FAILING TO FLARE THE AIRCRAFT OVER SDR 99ZZZX2032Breather · frozeBREATHER PIPE FROZEN. DID NOT HAVE SECONDARY HOLE, HIGH ENOUGH IN TUBE CAUSED SEAL TO BLOW OUT.SDR 99ZZZX2031Breather · frozeBREATHER PIPE FROZEN. DID NOT HAVE SECONDARY HOLE, HIGH ENOUGH IN TUBE CAUSED SEAL TO BLOW OUT.
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