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 = '172RG' 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 = '172RG' 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 97ZZZX3714Actuator · gear pin failedDURING FLIGHT, PILOT NOTICED TRIM NOT RESPONSIVE (ELEVATOR). INSPECTION OF SYSTEM FOUND PINS FELL OUT OF ACTUATOR WHICH ATTACH GEAR TO SHAFT. THE TRIM WHEEL MOVED NORMALLY, BUT TAB STAYED IN ONE POSITION.SDR 97ZZZX3877Window · plug missingPLUG ABOUT 8 INCHES IN DIAMETER MISSING IN REAR WINDOW. REPLACED WINDOW ABOUT 2 YEARS AGO FOR SAME REASON.SDR 97ZZZX4252J Box · failedIN-FLIGHT ELECTRIAL FAILURE OF ALL ELECTRICAL EQUIPMENT BEING SERVICED BY BUS NR 1. PILOT COMMENTED SPARKS COMING FROM UNDERNEATH INSTRUMENT PANEL. NO BREAKERS TRIPPED. FOUND WIRE BUNDLE RESTING ON CIRCUIT BREAKER. WIRE BURNED OUT LAYING ACROSS WARNING BRESDR 97ZZZX3756Bolt · brokenDURING INSTRUCTIONAL FLIGHT INVOLVING TAKEOFF AND LANDINGS, THE PILOT WAS INFORMED VIA RADIO FROM ANOTHER AIRCRAFT THAT THE ACFT NOSE WHEEL HAD FALLEN OFF. HE PROCEEDED TO SEE WHERE HE MADE A SUCCESSFUL EMERGENCY LANDING. INSPECTION OF THE ACFT NLG ASSY INDISDR 97ZZZX3022Float · defectivePILOTS REPORT EXCESS MAGNETO DROPS OF GREATER THAN 300 RPM'S AND SEVERE ENGINE ROUGHNESS. THE FLOAT IN THE CARBURETOR WAS REMOVED AND FOUND THAT THE REAR-MOST CHAMBER WAS FILLED WITH FUEL. FLOAT IS A PLASTIC DESIGN WITH 3 VISABLE CHAMBERS. THE CHAMBER THAT SDR 97ZZZX3390Pivot · shearedPILOT NOTICED GEAR ON RIGHT SIDE HANGING DOWN DURING APPROACH TO LAND AIRCRAFT. AFTER SEVERAL TRIES, PLOT DECIDED TO LAND GEAR UP. THERE WERE NO INJURIES, AND MINOR DAMAGE TO THE PROP AND BELLY OF AIRCRAFT. INSPECTION OF THE MAIN GEAR REVEALED THE GEAR INSISDR 97ZZZX2067Pivot Assy · crackedPIVOT ASSY CRACKED BETWEEN THE SPLINED END AND THE INTERNAL PASSAGE WAY THAT SUPPLIES THE BRAKE WITH FLUID. PART WOULD ONLY LEAK DURING GEAR EXTENSION AND WHEN APPLYING BRAKES ON ROLL-OUT.SDR AU971378Spar · cracked(AUS) RUDDER SPAR CRACKED ADJACENT TO TOP HINGE POINT.SDR 97ZZZX3971Pivot · crackedDURING A MAINTENANCE RUN, DISCOVERED THE RIGHT BRAKES HAD FAILED. INVESTIGATION REVEALED THE BELLY WAS COVERED IN HYDRAULIC FLUID. INSPECTION OF RT MAIN GEAR PIVOT DISCLOSED HYDRAULIC FLUID LEAKING FROM THE SPLINES OF PIVOT. PREVIOUS EXPERIENCE WITH CRACKS SDR AU970188Pivot · cracked(AUS) MAIN LANDING GEAR PIVOT ASSEMBLY CRACKED AS INDICATED IN SEB 90-1 REV 2.SDR 96ZZZX6163Actuator · crackedRIGHT MAIN GEAR ACTUATOR HOUSING CRACK AT SMALL END WHERE GEAR ATTACHES TO ACTUATOR. ACTUATOR CRACKED IN THREE DIRECTIONS ALLOWING PINION TO DISENGAGE FROM ACUTATOR. GEAR FAILED TO EXTEND FOR LANDING.SDR 96ZZZX6164Pad · wornGEAR WAS RETRACTED AND EXTENDED SEVERAL TIMES DURING FLIGHT. AFTER RETRACTION, GEAR WOULD NOT INDICATE GREEN LIGHT ON DOWN AND LOCKED POSITION. FOUND THE UPSTOP PAD WORN TO APPROX .25 INCH THICK, ALLOWED GEAR TO GO BEYOND NORMAL UP POSITION. NOSE WHEEL FORKSDR 96ZZZX6096Fitting · crackedDURING 100 HR INSPECTION, MECHANIC NOTICED PAINT MISSING FROM AROUND AREA THAT ALUMINUM CASTING (FITTING, AXLE) ATTACHES TO MAIN GEAR LEG - CLOSER INSPECTION OF THIS AREA REVEALED CRACK RUNNING FROM TOP OF CASTING DOWN TO ATTACH BOLT HOLE. ZYGLO FOUND DEFINITSDR 97ZZZX193Pivot · shearedSPLINE PORTION OF PIVOT ASSY SHEARED DURING NORMAL OPERATIONAL USE. RIGHT MAIN GEAR LEG WOULD NOT LOCK DOWN. PILOT DID A GREAT JOB OF MINIMIZING DAMAGE TO A/C. RECOMMEND FLUORESCENT PENETRANT INSPECT DURING ANNUAL INSPECTION OF SPLINE SHAFT WHERE IT MEETS TSDR 96ZZZX6156Valve Tang · wornTANG OF FUEL CUT OFF VALVE ASSY WORE DEEPLY INTO FULL RICH STOP AREA ALLOWING APPROX ONE-QUARTER TURN MORE THAN NORMAL. ENGINE WENT EXTREMELY LEAN. TAKEOFF ABORTED.SDR 96ZZZX5607Valve · stretchedPILOT REPORTED THAT THE ENGINE RAN ROUGH AT FULL POWER. REMOVED VALVE COVERS AND FOUND NR 4 CYLINDER EXHAUST VALVE HAD NO CLEARANCE BETWEEN THE VALVE AND ROCKER ARM. THE VALVE HEAD WAS STRETCHED.SDR 96ZZZX5638Dimming Assy · overheatedSMOKE IN COCKPIT DURING FLIGHT. OVERHEATED TRANSISTORIZED DIMMING ASSY LIKELY CAUSED BY ADDED ELECTRICAL LOAD DUE TO RECENTLY ADDED RADIO EQUIPMENT. SUBMITTER STATED AN EVALUATION NEEDED OF CURRENT DRAW ON SUBJECT SYSTEM. THAT DETERMINATION HAS NOT YET BEENSDR 96ZZZX5489Pivot Assy · brokenLT GEAR WOULD NOT RETRACT OR EXTEND. AIRCRAFT LANDED GEAR UP. SOME DAMAGE TO PROP AND BELLY. AFTER RECOVERY, REMOVED LEFT MAIN GEAR. THE GEAR PIVOT ASSY WAS SHEARED AT THE SPLINES TO THE MAIN BODY. BEFORE THE FLIGHT, THE BRAKES WERE NOT SPONGY. AFTER FAISDR 96ZZZX5408Pivot Assy · shaft shearedLEFT MAIN GEAR WOULD NOT INDICATE DOWN AND LOCK WHEN THE GEAR WAS SELECTED DOWN. THE PILOT LANDED WITH GEAR UP. THE LT MAIN GEAR ASSY WAS REMOVED FROM THE AIRCRAFT AND IT WAS DISCOVERED THE PIVOT SHAFT OF THE PIVOT ASSY HAD SHEARED FROM THE MAIN BODY OF THE SDR EY2R9601126Hub · corrodedHUB FOUND CORRODED.SDR 96ZZZX6013Pivot · crackedRIGHT LANDING GEAR FAILED TO EXTEND TO THE DOWN AND LOCKED POSITION. AFTER ATTEMPTS TO SECURE/ACTUATE TO SAFE DOWNLOCK POSITION FAILED, A SUCCESSFUL GEAR UP BELLY LANDING WAS MADE. PROPELLER AND BELLY SKIN DAMAGE RESULTED, NO INJURY TO FLIGHT CREW. INSPECTISDR AU961203Support · damaged(AUS) MAGNETO DISTRIBUTOR GEAR BEARING SUPPORT DAMAGED - FOUND DURING INSPECTION IAW AD/ELEC/46 - INTERNAL DAMAGE TO MAGNETOSDR AU961148Doubler · cracked(AUS) EMPENAGE TO FUSELAGE ATTACHMENT BULKHEAD CRACKED - SEE ALSO MDR 95/0816 AND MDR 96/1142 FOR SIMILAR DEFECTSSDR AU961142Bulkhead · cracked(AUS) FUSELAGE BULKHEADS CRACKED IN THE FOLLOWING LOCATIONS: 1. PNO 2412001-3 BULKHEAD LOWER LH STN 108.0 - CRACK LENGTH 27MM (1.06IN) 2. PNO 2412001-4 BULKHEAD LOWER RH STN 108.0 - CRACK LENGTH 30MM (1.18IN) 3. PNO 2412004-4 BULKHEAD LOWER RH STN 124.0 - SDR 97ZZZX211Pivot · shearedA SUCCESSFUL CRASH LANDING WAS ACCOMPLISHED WITH THE LANDING GEAR SELECTED UP FOLLOWING A FAILURE OF THE LT MLG LEG TO COMPLETELY LOCK DOWN. THIS EVENT HAPPENED FOLLOWING MULTIPLE TAKEOFF AND LANDINGS DURING A TRAINING FLIGHT. UPON THE LAST LANDING PRIOR TOSDR CA960927001Carburetor · abnormal wear(CAN) PILOT EXPERIENCED STARTING PROBLEMS. INVESTIGATION OF SNAG WAS INCONCLUSIVE. INSPECTION OF CARBURETOR INDICATED WEAR ON THE FLOAT ASSEMBLY, WHICH IS UNCOMMON WITH THE AMOUNT OF TIME AND USAGE OF THIS UNIT. FURTHER INVESTIGATION IS UNDERWAY.SDR EY2R9601595Hub · galledHUB ASSY GALLED BADSDR EY2R9601594Blade · galledBLADE SN IB008, GALLED BADSDR EY2R9601593Blade · galledBLADE SN IB026, GALLED BADSDR AU961038Static System · mis installed(AUS) UNAPPROVED INSTALLATION OF INSTRUMENT STATIC LINE SYSTEM - PERSONNEL/MAINTENANCE ERROR - UNAPPROVED PARTSDR EY2R9601579Ball Bearing · defectivePROP ASSY BEARINGS FLATSDR 96ZZZX3698Pivot · shearedLEFT MLG COULD NOT BE FULLY EXTENDED. EVERY POSSIBLE ATTEMPT FAILED. DURING LAST ATTEMPT BEFORE GEAR-UP LANDING, PILOT PHYSICALLY REACHED OUT AND LOCKED GEAR. (FLIGHT INSPECTER WAS ALSO ON BOARD.) SAFE LANDING WAS MADE. UPON INSPECTION, PN 24411001 WAS FOSDR AU960824Bungee · broken(AUS) AIRCRAFT STEERING SYSTEM BUNGEE JACK SCREW BROKEN DUE TO A WORN HOUSING - SYSTEM HAD BEEN MODIFIED IAW AD/CESSNA170/45SDR 96ZZZX3424Bearing · brokenPROPELLER WAS NOT CYCLING PROPERLY. REMOVED TO BENCH TEST. BLADES WERE BINDING WHEN TESTED. DISASSEMBLED AND FOUND BLADE BEARINGS DRY AND BROKEN, BALL BEARINGS PITTED, AND PITCH CHANGE LINKS AND ACTUATING PINS WORN BADLY. SUBMITTER STATED PROP MAY NOT HAVESDR 96ZZZX3080Fitting · looseWHEN ON JACKS, FORE AND AFT FORCE ON THE NOSE GEAR REVEALED A ROCKING MOTION OF THE NOSE GEAR ACTUATOR REAR FITTING TO FUSELAGE ON ITS 20 ATTACHMENT BOLTS. WITH NUTS TORQUED, COULD EASILY TURN BOLTS AS THEY HAD RUN OUT OF THREADS AND NUT WAS JAMMED AGAINST SHSDR 96ZZZX2757Pivot · crackedPIVOT CRACKED NEARLY THE ENTIRE CIRCUMFERENCE IN THE RADIUS UNDER PN 2241111-2 INNER RACE. IT IS NOT KNOWN IF A HARD LANDING OCCURRED. PART HAD SOME AREAS OF INTERGRANULAR CORROSION AND IS IN THE EXHAUST STREAM. NO EVIDENCE OF CORROSION IN AREA OF CRACK. CSDR 96ZZZX2561Fitting · crackedFOUND 2 CRACKS IN FITTING THAT HOLDS AXLE STUB TO LANDING GEAR DURING A 100-HOUR INSPECTION.SDR EY2R9600626Base Assy Pin · corrodedBASE ASSY PIN.SDR EY2R9600625Retain Bearing · corrodedRETAIN BEARING FOUND WITH CORROSION.SDR 96ZZZX2760Casting · crackedDURING A 100-HOUR INSPECTION WHILE CHECKING THE BELLY SKIN AFT OF THE NOSE GEAR, NOTICED BLACK STAINING FROM THE 6 SCREWS THAT ARE ON THE LOWER EDGE OF CASTING. REMOVED SCREWS AND FOUND ALL MOUNTING HOLES OF SKIN NR 2413000-5 ELONGATED. INSPECTED CASTING WITSDR EY2R9600525Retain Bearing · corrodedRETAIN BEARING FOUND WITH CORROSION.SDR 96ZZZX2577Sector Gear · misinstalledDURING C/W SEB 90-1 AND SUBSEQUENT REASSEMBLY OF MAIN LANDING GEAR ACTUATOR AND PIVOT ASSY, NOTICED THE SECTOR GEARS AND THE PIVOT ASSY SHAFT WERE NOT MARKED FOR PROPER ALIGNMENT PER CESSNA SERVICE MANUAL SECTION 5, PARAGRAPH 75, AND FIGURE 5-12. THE RT GEAR SDR 96ZZZX2037Starter · bolts missingDURING A 100-HOUR INSPECTION, THE STARTER REAR CASE WAS FOUND LOOSE. THREE OF THE FOUR SCREWS THAT SECURE FRONT BENDIX HOUSING TO REAR CASE FOUND MISSING. SUBMITTER STATED CAUSED BY VIBRATION OR POOR ASSEMBLY TORQUES OR LOCK WASHERS WHEN STARTER WAS BUILT. SDR AU960855Pivot · cracked(AUS) RH MAIN LANDING GEAR PIVOT CRACKED AT THE OUTBOARD END OF THE SPLINED AREA - FURTHER INVESTIGATION FOUND LH MLG PIVOT ALSO CRACKEDSDR AU960298Retainer · cracked(AUS) ENGINE PUSH ROD TUBE RETAINERS (4OFF) CRACKED - RETAINERS WERE SHIPPED WITH GASKET SET PNO SL 75439-1SDR 96ZZZX3764Shell Assy · deterioratedDURING INSPECTION AND GEAR RETRACTION TEST, FOUND MLG TO HAVE EXCESSIVE FREE PLAY WHEN DOWN AND LOCKED. UPON INVESTIGATION, FOUND MLG DOWNLOCK LATCHES WOULD NOT HOLD LANDING GEAR LEGS LATCHED DUE TO EXCESSIVE CLEARANCE BETWEEN LATCH AND PIN. THE SHELL ASSYSSDR 96ZZZX1800Bulkhead · crackedDURING 100-HOUR INSPECTION, FOUND RUDDER PEDAL TUBE MOUNTING BLOCKS FLEXING UP AND DOWN WHEN PRESSURE WAS APPLIED TO PEDALS. FURTHER INSPECTION OF THE PROBLEM REVEALED CRACKS IN THE LOWER BULKHEADS (172RG PART CATALOG, FIGURE 19, INDEX 16 AND INDEX 20) BELOW SDR 96ZZZX1799Bulkhead · crackedDURING 100-HOUR INSPECTION, FOUND RUDDER PEDAL TUBE MOUNTING BLOCKS FLEXING UP AND DOWN WHEN PRESSURE WAS APPLIED TO PEDALS. FURTHER INSPECTION OF THE PROBLEM REVEALED CRACKS IN THE LOWER BULKHEADS (172RG PART CATALOG, FIGURE 19, INDEX 16 AND INDEX 20) BELOW SDR 96ZZZX1798Bulkhead · crackedDURING 100-HOUR INSPECTION, FOUND RUDDER PEDAL TUBE MOUNTING BLOCKS FLEXING UP AND DOWN WHEN PRESSURE WAS APPLIED TO PEDALS. FURTHER INSPECTION OF THE PROBLEM REVEALED CRACKS IN THE LOWER BULKHEADS (172RG PART CATALOG, FIGURE 19, INDEX 16 AND INDEX 20) BELOW SDR 96ZZZX1797Bulkhead · crackedDURING 100-HOUR INSPECTION, FOUND RUDDER PEDAL TUBE MOUNTING BLOCKS FLEXING UP AND DOWN WHEN PRESSURE WAS APPLIED TO PEDALS. FURTHER INSPECTION OF THE PROBLEM REVEALED CRACKS IN THE LOWER BULKHEADS (172RG PART CATALOG, FIGURE 19, INDEX 16 AND INDEX 20) BELOW
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