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 96ZZZX1796Bulkhead · 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), BELOWSDR 96ZZZX1795Bulkhead · 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 EY2R9600461Hub · corrodedCORROSION FOUND ON HUB.SDR 96ZZZX1097Control Unit · failedPILOT REPORTED LOSS OF ELECTRICAL POWER. AFTER LANDING, UNCOWLED ENGINE AND FOUND THE ACU WAS SMOKED. TROUBLESHOT AND FOUND THE ALTERNATOR WINDINGS OPEN. INSTALLED A NEW ACU AND INSTALLED A SERVICEABLE ALTERNATOR, PN C611503-0102. PERFORMED GROUND RUN, OPESDR 96ZZZX475Roller Assy · frozenDURING 100-HOUR INSPECTION, NOTICED THE RT FLAP VIBRATING AS IT WAS LOWERED. INSPECTION FOUND THE AFT INBOARD ROLLER WAS FROZEN. UPON REMOVAL OF THE ROLLER, FOUND THE OUTER BRASS (?) RING HAD PARTIALLY SLID OFF OF THE INNER BEARING ASSY CAUSING THE ROLLER TOSDR AU960022Structure · corroded(AUS) AFT FUSELAGE TAILCONE TUNNEL CONTAINED SEVERE CORROSION AT THE AFT ENDSDR CA951211011Torque Tube · broken(CAN)SHORTLY AFTER TAKEOFF THE PILOT HEARD A LOUD BANG, AFTER WHICH RUDDER AUTHORITY WAS LOST. AIRCRAFT LANDED SAFELY AND INVESTIGATION FOUND THE FORWARD RUDDER PEDAL TORQUE TUBE HAD CRACKED APPROXIMATELY 3/4 OF THE WAY AROUND. THIS ALLOWED THE TORQUE TUBE TSDR 95ZZZX7020Motor · defectiveDURING A ROUTINE ANNUAL INSPECTION, THE MLG HYD POWER PACK MOTOR WOULD NOT SHUT OFF AT THE END OF THE RETRACT OR EXTEND CYCLE WHILE ON JACKS USING ONLY SHIPS ELECTRICAL POWER (24V). THE MLG CYCLED PROPERLY DURING FLIGHT AND PILOT NOTICED NO DISCREPANCIES BEFOSDR 95ZZZX6817Downlock Sys · malfunctionAFTER A GEAR INSPECTION (ROUTINE), THE AIRCRAFT WAS PLACED ON THE GROUND. THE GEAR HANDLE WAS 'DOWN', THE LIGHT 'GREEN', AND THE BREAKER 'IN'. THE STRUT WAS AT MAX EXTENSION. ROUTINE MAINTENANCE PERFORMED ON ACFT FOR THE 100-HOUR INSPECTION. APPROXIMATELY SDR 95ZZZX6405Pivot · crackedEXPERIENCED LOSS OF BRAKING ON RT SIDE. FOUND CRACK IN PIVOT ASSEMBLY WHERE SHAFT RADIUS JOINS SPLINE. NO RECORD OF PREVIOUS COMPLANCE WITH SEB 90-1 R2.SDR 95ZZZX6404Pivot · crackedEXPERIENCED LOSS OF BRAKING. INSPECTION FOUND CRACK IN MAIN GEAR PIVOT ASSEMBLY AT RADIUS WHERE SHAFT JOINS SPLINE. NO RECORD OF PREVIOUS COMPLIANCE WITH SEB 90-1 R2.SDR 95ZZZX6400Pivot · failedUNABLE TO FULLY EXTEND OR RETRACT RIGHT LANDING GEAR. GEAR UP LANDING WITH NOMINAL DAMAGE. INSPECTION FOUND SPLINE BROKEN OFF OF PIVOT ASSEMBLY. SUBMITTER STATED IT APPEARS TO BE A FATIGUE FAILURE.SDR 95ZZZX6912Bulkhead · crackedDURING ANNUAL INSPECTION, IT WAS DETERMINED THAT BOTH UPPER AND LOWER BULKHEADS WERE CRACKED NEAR RUDDER BAR ATTACH POINTS. P/N 241001-3, 241001-4, 241001-5, AND 241001-6. BULKHEADS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. SUBMITTER SUGGESTS SDR 95ZZZX6168Bulkhead · crackedDURING ANNUAL INSPECTION, DETERMINED THAT UPPER AND LOWER BULKHEADS NEAR RUDDER BAR ATTACH POINTS WERE CRACKED. ALL BULKHEADS WERE REPLACED. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA DURING INSPECTION, WITH POSSIBLE REINFORCEMENT ADDED.SDR 95ZZZX6167Bulkhead · crackedDURING ANNUAL INSPECTION, DETERMINED THAT UPPER AND LOWER BULKHEADS NEAR RUDDER BAR ATTACH POINTS WERE CRACKED. ALL BULKHEADS WERE REPLACED. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA DURING INSPECTION, WITH POSSIBLE REINFORCEMENT ADDED.SDR 95ZZZX6166Bulkhead · crackedDURING ANNUAL INSPECTION, DETERMINED THAT UPPER AND LOWER BULKHEADS NEAR RUDDER BAR ATTACH POINTS WERE CRACKED. ALL BULKHEADS WERE REPLACED. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA DURING INSPECTION, WITH POSSIBLE REINFORCEMENT ADDED.SDR 95ZZZX6165Bulkhead · crackedDURING ANNUAL INSPECTION, DETERMINED THAT UPPER AND LOWER BULKHEADS NEAR RUDDER BAR ATTACH POINTS WERE CRACKED. ALL BULKHEADS WERE REPLACED. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA DURING INSPECTION, WITH POSSIBLE REINFORCEMENT ADDED.SDR 95ZZZX6163Cylinder · crackedENGINE BECAME ROUGH DURING FLIGHT. UPON LANDING AND INSPECTION, IT WAS DETERMINED THAT CYLINDER NR 4 WOULD NOT PASS CYLINDER LEAKAGE TEST. AFTER FURTHER INSPECTION, CYLINDER WAS FOUND TO BE CRACKED ONE-HALF WAY AROUND CIRCUMFERENCE BETWEEN FINS AT JUNCTION OSDR 95ZZZX5643Actuator · crackedGEAR WAS REPORTED TO HAVE NOT RETRACTED ALL THE WAY. UPON INSPECTION, THE LEFT GEAR WOULD NOT FULLY RETRACT INTO THE WELL. INSPECTING THE GEAR ACTUATOR, A CRACK WAS DISCOVERED IN THE HOUSING. AFTER REMOVAL OF THE ACTUATOR, DISCOVERED THE SECTOR GEAR, PN 488SDR 95ZZZX5987Wire · failedLANDING GEAR FAILED TO COMPLETELY RETRACT WHEN SELECTED. CAUSE WAS DETERMINED TO BE BROKEN WIRE FOR SQUAT SWITCH WHICH WAS SHIELDED INSIDE VINYL TUBING WHICH HAD BECOME BRITTLE AND HARD CAUSING WIRE TO FLEX REPEATEDLY IN ONE SPOT.SDR 95ZZZX6437Housing · crackedDURING FLIGHT AND GEAR-UP, ONE GEAR WOULD NOT FULLY RETRACT. INSPECTION REVEALED MAIN LANDING GEAR ASSY HOUSING CRACKED FORWARD OF PISTON ROLLER BOSS. SUBMITTER STATED THIS CONDITION WAS NOTED ON TWO OTHER AIRCRAFT IN THIS FLEET, ALL CESSNA 172RG.SDR 96ZZZX2017Actuator · crackedTHE RADIUS OF THE ACTUATOR APPEARED TO BE CRACKED, THE PART WAS REMOVED AND DYE PENETRANT INSPECTION PERFORMED. FOUND NUMEROUS CRACKS AROUND THE RADIUS WHERE THE MAIN GEAR ACTUATING GEAR IS BOLTED TO THE ACTUATOR. THE BOSS FOR THE SHAFT AND BEARING WHICH ALISDR 95ZZZX6145Actuator · crackedTHE RADIUS OF THE ACTUATOR APPEARED TO BE CRACKED, THE PART WAS REMOVED AND DYE PENETRANT INSPECTION PERFORMED. FOUND NUMEROUS CRACKS AROUND THE RADIUS WHERE THE MAIN GEAR ACTUATING GEAR IS BOLTED TO THE ACTUATOR. THE BOSS FOR THE SHAFT AND BEARING WHICH ALISDR 95ZZZX4592Shroud Assy · chafe mufflerSCREWS ATTACHING THE SHROUD TO THE MUFFLER CAME OUT CAUSING SHROUD TO SIT ON THE COILS OF THE MUFFLER. IT THEN RUBBED THROUGH COILS. THIS AIRCRAFT IS ON A 50-HOUR INSPECTION PROGRAM, SO IT HAPPENED WITH 50 HOURS.SDR 95ZZZX4299Fitting · bolts looseDURING 100-HOUR INSPECTION OF NOSE GEAR ACTUATOR, FOUND BOLTS LOOSE IN NOSE GEAR ACTUATOR FITTING. NON-COMPLIANCE OF SB SEB93-8 LED TO DEFECT. SUBMITTER RECOMMENDS A RECURRING AD BE ATTACHED TO SB UNTIL SERVICE KIT SK A2-142 INSTALLED.SDR 95ZZZX4493Bulkhead · corrodedFOUND BULKHEAD WITH SEVERE CORROSION IN RT GEAR WELL WHERE LANDING GEAR PIVOT ATTACHES. RIVETS IN THIS LOCATION CORRODED AND SHEARED. EVIDENCE OF PLAY IN RT GEAR. COMPLETE BULKHEAD NEEDED REPLACEMENT. AIRCRAFT SPENT MOST OF ITS TIME IN SALT WATER ENVIRONMESDR 95ZZZX3654Carburetor Valve · seizedPILOT REPORTED THROTTLE WOULD NOT MOVE FROM IDLE AFTER START. REMOVED CARBURETOR, FOUND CONTROL ARM SEIZED. REPLACED CARBURETOR UNDER WARRANTY. SENT CARBURETOR TO PRECISION AIRMOTIVE FOR WARRANTY/PROBLEM INSPECTION.SDR 95ZZZX4330Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX4329Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX3808Muffler · crackedEND FLANGE CRACKED TWO-THIRDS OF THE WAY AROUND, 45 HOURS TOTAL TIME. AD 83-14-04 HAD BEEN DONE REGULARLY EACH 50 HOURS. MUFFLER WHICH THIS REPLACED 45 HOURS AGO HAD THE FLANGE OBLITERATED. TOTAL TIME ON THAT MUFFLER COULD NOT BE DETERMINED, BUT IT WAS NOT SDR 95ZZZX3482Air Box · crackedDISCOVERED CRACK AROUND OUTER EDGE OF WELD OF CARBURETOR AIR INTAKE ELBOW TUBE TO CARBURETOR HEAT VALVE BODY, THROUGH 240 DEGREES ARC, DURING ANNUAL/100-HOUR VISUAL INSPECTION OF ENGINE. SUSPECT CAUSE IS POOR MANUFACTURING/WELDING TECHNIQUES. SUBMITTER RECOMSDR 95ZZZX2735Wire · brokenUPON SELECTING GEAR DOWN, DOWN AND LOCKED LIGHT WOULD NOT ILLUMINATE WITH GEAR DOWN. PILOT DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. UPON INSPECTION, A WIRE AT NOSE GEAR UP INDICATION SWITCH WAS FOUND BROKEN. REPAIRED WIRE. PERFORMED RETRACTION TEST. SDR 95ZZZX2686Stiffener · crackedFOUND UPON PRE-PURCHASE INSPECTION, THE FLOORBOARD AND STIFFENER CRACKED BELOW BOTH INNER RUDDER TORQUE TUBE BEARINGS. THIS WILL, IF NOT CORRECTED, CAUSE THE RUDDER TUBE ASSEMBLY TO ROTATE FORWARD. NO REPAIRS WERE MADE AT THIS TIME. SUBMITTER STATED THIS IS SDR 95ZZZX1124Casting · creepWHEN THIS INSTRUMENT WAS TESTED, NOTICED IT OPERATED WITH HESITATIONS OF 100 FEET TO 150 FEET WHEN TESTED FROM MINUS 1,000 FEET TO 20,000 FEET. ONE HESITATION WHICH OCCURRED AT APPROX 250 FEET HAD A HESITATION OF APPROX 220 FEET DURING WHICH IT SLOWLY CAME TOSDR 95ZZZX1094Bulkhead · crackedFOUND UPPER BULKHEADS CRACKED AT TOP OF RUDDER PEDAL TORQUE TUBE OPENING JUST AFT OF MOUNTING BOLT FOR PN 2460004-1 BELLCRANK ASSY. LT SIDE CRACKED COMPLETELY THROUGH. RT SIDE ALSO DAMAGED DUE TO BOLT HEAD ON THE BELLCRANK HITTING IT. FOUND UPPER BULKHEADS,SDR 95ZZZX1093Bulkhead · crackedFOUND UPPER BULKHEADS CRACKED AT TOP OF RUDDER PEDAL TORQUE TUBE OPENING JUST AFT OF MOUNTING BOLT FOR PN 2460004-1 BELLCRANK ASSY. LT SIDE CRACKED COMPLETELY THROUGH. RT SIDE ALSO DAMAGED DUE TO BOLT HEAD ON THE BELLCRANK HITTING IT. FOUND UPPER BULKHEADS,SDR 95ZZZX1092Bulkhead · crackedFOUND UPPER BULKHEADS CRACKED AT TOP OF RUDDER PEDAL TORQUE TUBE OPENING JUST AFT OF MOUNTING BOLT FOR PN 2460004-1 BELLCRANK ASSY. LT SIDE CRACKED COMPLETELY THROUGH. RT SIDE ALSO DAMAGED DUE TO BOLT HEAD ON THE BELLCRANK HITTING IT. FOUND UPPER BULKHEADS,SDR 95ZZZX1091Bulkhead · crackedFOUND UPPER BULKHEADS CRACKED AT TOP OF RUDDER PEDAL TORQUE TUBE OPENING JUST AFT OF MOUNTING BOLT FOR PN 2460004-1 BELLCRANK ASSY. LT SIDE CRACKED COMPLETELY THROUGH. RT SIDE ALSO DAMAGED DUE TO BOLT HEAD ON THE BELLCRANK HITTING IT. FOUND UPPER BULKHEADS,SDR 95ZZZX1083Actuator · crackedTHE FEBRUARY ISSUE STATED THE BOLTS USED TO SECURE MLG ACTUATOR WERE NOT DRILLED AND WERE LOOSE. SUBMITTER SUGGESTS THESE BOLTS SHOULD HAVE DRILLED HEADS AND SHOULD BE SAFETY WIRED. SUBMITTER HAS FOUND NUMEROUS CRACKED ACTUATORS, ALL WITH PROPERLY TORQUED BOSDR 95ZZZX933Rudder Bar · brokenRUDDER BAR BROKEN IN HALF ADJACENT TO WELD THAT HOLDS STEERING BUNGEE BRACKET. THIS BAR HAS THE TWO RIGHT RUDDER PEDALS CONNECTED TO IT AND IS LOCATED IN THE REAR OF THE TWO RUDDER BARS. STRESS OF FACTORY WELD CAUSED CRACKING TO OCCUR WITH ULTIMATE FAILURE OSDR 95ZZZX380Door · hung upNOSE LANDING GEAR FAILED TO EXTEND RESULTING IN DAMAGE TO NOSE L/G DOORS, LOWER ENGINE COWL ASSY, AND PROPELLER. AFTER REPAIR, L/G OPERATES NORMALLY. BELIEVED THAT DOORS 'HUNG' ON LOWER COWL SKIN OR BUMPERS, PN 2452006-15, AND PN 2452006-16. RECOMMEND INDUCSDR 95ZZZX379Door · hung upNOSE LANDING GEAR FAILED TO EXTEND RESULTING IN DAMAGE TO NOSE L/G DOORS, LOWER ENGINE COWL ASSY, AND PROPELLER. AFTER REPAIR, L/G OPERATES NORMALLY. BELIEVED THAT DOORS 'HUNG' ON LOWER COWL SKIN OR BUMPERS, PN 2452006-15, AND PN 2452006-16. RECOMMEND INDUC
Back to Cessna 172RG