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 = 'R172K' 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 = 'R172K' 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 CA970530004Blade · spray cut(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER BLADE HAD SPRAY CUT ON LEADING EDGE. THE PROPELLER HUB REAR BORE AS OVERSIZE.SDR CA970501003Blade · spray cut(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. INSPECTION FOUND SPRAY CUTS ON THE LEADING EDGE AND THE TIP ANGLES OUT. THE BLADE EDGES WERE FILED AND THE TIP ANGLES WERE REPAIRED.SDR 96ZZZX5659Adapter Assy · wornBYPASS PLUG CAME OUT OF HOUSING. FOUND WORN PLUG AND DAMAGED HOUSING. PLUG IS STAKED IN IF BYPASS VALVE IS NOT USED. FOUND METAL IN OIL FILTER AT PREVIOUS OIL CHANGE 10 HRS PRIOR AND AT THIS OIL CHANGE. SUBMITTER STATED MFG NEEDS BETTER WAY TO SECURE PLUG.SDR AU961213Spar · cracked(AUS) HORIZONTAL STABILISER FRONT SPAR AND DOUBLER CRACKED - FOUND DURING INSPECTION IAW AD/C170/59 - AIRCRAFT IS USED FOR CATTLE MUSTERINGSDR CA961002015Mount · cracked(CAN) DURING ROUTINE INSPECTION THE AME NOTICED UNUSUAL MOVEMENT IN THE ENGINE COWLING. INVESTIGATION FOUND THE STEEL END FITTING ON THE LEFT HAND UPPER ENGINE MOUNT STRINGER ON THE AFT FACE OF THE FIREWALL TO BE SEVERELY CRACKED. THE ENGINE MOUNT WAS FOUND PUSDR 96ZZZX3762Elt · malfunctionEMERGENCY LOCATER TRANSMITTER CESSNA P/N C589510-0209, WOULD NOT PASS G-SWITCH OPERATIONAL CHECK PER FAR 91.207(D). LIGHT TOO EXCESSIVE FORCE, WOULD NOT SET OFF G-SWITCH. ELT WOULD PUT OUT SIGNAL WHEN SWITCHED ON MANUALLY.SDR 96ZZZX3870Piston · ring failedUPON DISASSEMBLY AFTER LOW COMPRESSION READING, FOUND THE LOWER PORTION BY OIL SCRAPER RING MISSING FROM THE PISTON. SUSPECT DUE TO THE OIL SCRAPER RING HANGING UP, THUS, STUCTRURAL MALFUNCTION.SDR 96ZZZX3364Bulkhead · crackedCUSTOMER COMPLAINED OF ROUGH RUNNING ENGINE DURING SHORT FINAL UPON LANDING. FOUND SPINNER BULKHEAD TO BE CRACKED APPROXIMATELY 95 PERCENT AROUND ATTACHMENT TO CRANKSHAFT. FURTHER INSPECTION FOUND THE SPINNER BULKHEAD STABILIZER MISSING FROM PROELLER HUB INSDR 96ZZZX3363Stabilizer · missingCUSTOMER COMPLAINED OF ROUGH RUNNING ENGINE DURING SHORT FINAL UPON LANDING. FOUND SPINNER BULKHEAD TO BE CRACKED APPROXIMATELY 95 PERCENT AROUND ATTACHMENT TO CRANKSHAFT. FURTHER INSPECTION FOUND THE SPINNER BULKHEAD STABILIZER MISSING FROM PROELLER HUB INSDR 96ZZZX885Control Cable · seizedINSTALL NEW CONTROL CABLE ASSY AS SUPPLIED BY CESSNA AIRCRAFT. INSTALLED AND RIGGED PER CESSNA R172K SM. ALL OPS CHECK OK ON GROUND. RUN-UP OPS CHECK OK. FLOWN FOR 2.0 HOURS, NO ATTEMPT TO MOVE CONTROL WHILE IN-FLIGHT. UPON RETURN TO GROUND, GOVERNOR CONTSDR 96ZZZX1277Control Assy · seizedINSTALL NEW CONTROL CABLE ASSY AS SUPPLIED BY CESSNA AIRCRAFT. INSTALLED AND RIGGED PER CESSNA R172K SM AND UNDER THE SUPERVISION OF A CESSNA FIELD SERVICE ENGINEER. ALL OPS CHECK OK ON GROUND. RUN-UPS CHECK OK. FLOWN FOR 2.0 HRS, NO ATTEMPT MADE TO ADJUSTSDR 96ZZZX1050Control Assy · seizedTHIRD TIME TO INSTALL NEW CONTROL CABLE ASSY AS SUPPLIED BY CESSNA AIRCRAFT. INSTALLED AND RIGGED PER CESSNA R172K SERVICE MANUAL. ALL OPS CHECK OK ON GROUND. RUN-UP OPS CHECK OK. FLOWN FOR 2 HOURS, NO ATTEMPT TO MOVE CONTROL WHILE IN-FLIGHT. UPON RETURN SDR 96ZZZX1049Control Assy · frozenINSTALLED NEW CONTROL CABLE ASSY AS SUPPLIED BY CESSNA AIRCRAFT. INSTALLED AND RIGGED PER CESSNA R172K SERVICE MANUAL. ALL OPS CHECK OK ON GROUND PRIOR TO FLIGHT. RUN-UP OPS CHECK OK. FLOWN FOR 2.0 HOURS FOR ENGINE BREAK-IN. ALL OPS NORMAL. UPON RETURN TSDR 96ZZZX369Cylinder · head separatedIMMEDIATELY AFTER LIFT OFF HEARD A LOUD BANG FROM ENGINE COMPARTMENT, 3 MORE ENTERED CABIN, ABORTED TAKEOFF AND SHUT DOWN ENGINE. REMOVED COWL AND FOUND NR 1 CYLINDER HEAD SEPARATED FROM BARREL.SDR 95ZZZX5934Filter Adapter · threads strippedOIL FITLER ADAPTER SEPARATED FROM ENGINE AT CRANKCASE COVER MOUNTING BOSS ALLOWING OIL SUPPLY TO BE EXHAUSTED. INVESTIGATION REVEALED 80 PERCENT OF THE MOUNTING THREADS CONTAINED IN THIS BOSS WERE STRIPPED. HIGH TEMP RTV WAS FOUND ON THESE THREADS AS WELL ASSDR 95ZZZX4004Torque Tube · adapter looseDURING ANNUAL INSPECTION, TORQUE TUBE ADAPTER ON THE LEFT ELEVATOR DISCOVERED LOOSE AND WORKING. A BALANCE CHECK OF THE ELEVATORS REVEALED THEM TO BE CLOSE TO THEIR LIMITS, BUT STILL SERVICEABLE. LEFT ELEVATOR WAS UNDER BALANCED AT 17.5 INCHES/POUNDS. ITS LSDR 95ZZZX3622Hose · leakingFUEL HOSE RUNS ACROSS THE TOP OF THE ENGINE. WHEN PRESSURE CHECKED, IT LEAKED ALONG THE ENTIRE LENGTH. TAG ON HOSE HAS THE FOLLOWING DATA: PAW 601000-4-0544. PT10-89. A4Q89. 1000 PSI. RUBBER. 00624. TSO - 053A. SEE AEROQUIP SBAA135 - THESE HOSES ARE SDR 95ZZZX2678Screen · crackedWHILE PERFORMING AN ANNUAL INSPECTION ON AIRCRAFT MODIFIED BY BRACKETT STC SA-71GL, FILTER SUPPORT SCREEN WAS FOUND INSTALLED WITH THE MATING FLANGE MISALIGNED CAUSING 2 CRACKS ABOUT 1 CM LONG, CREATING THE POSSIBILITY OF FOD ENTERING THE INDUCTION SYSTEM. THSDR 95ZZZX2318Battery Vent · looseBATTERY ACID IN BELLY OF AIRCRAFT FROM BATTERY BOX FORWARD. CAUSED FROM BATTERY BOX OVERBOARD VENT DISCONNECTING FROM BOX WHEN BATTERY IS REMOVED. OVERBOARD VENT SHOULD BE CLAMPED TO BATTERY BOX TO PREVENT PROBLEM.SDR 96ZZZX4784Transponder · burnedPILOT LANDED AIRCRAFT AFTER DETECTING BURNING SMELL. AFTER INVESTIGATING PROBLEM, TRANSPONDER WAS REPLACED BY RADIO SHOP (POWER SUPPLY IN TRANSPONDER HAD BURNED CAUSING SMELL).SDR 95ZZZX1616Wrist Pin · failedPISTON WRIST PIN BROKE IN NR 3 CYLINDER CAUSED PISTON SKIRT TO BREAK. POLLUTED THE ENGINE WITH ALUMINUM. DAMAGED NR 3 CYLINDER, ROD, AND NR 4 PISTON WAS MARRED. THE ONLY INDICATION OF A PROBLEM WAS THE OIL PRESSURE DROPPED OFF TO HALF OF NORMAL DUE TO METAL
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