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 CA990119015Bearing · corroded(CAN) PROPELLER RECEIVED FOR TBO OVERHAUL. UPON DISMANTLE INSPECTION, THE BLADE THRUST BEARINGS WERE FOUND CORRODED. THE BEARINGS WERE REPLACED WITH NEW BEARINGS.SDR CA990119014Link Pins · worn(CAN) PROPELLER RECEIVED FOR TBO OVERHAUL. UPON DISMANTLE TOLERANCE INSPECTION, THE LINK PINS WERE FOUND WORN BELOW THE MANUFACTURER'S MINIMUM TOLERANCES. THE LINK PINS WERE REPLACED.SDR 99ZZZX650Fitting · crackedNOSE GEAR ACTUATOR ASSY ATTACHING BOLT TO FITTINGS/CASTING FROZEN CAUSING CASTING TO CRACK. INSPECT ACTUATOR FOR FREE MOVEMENT, REMOVE BOLTS, CLEAN AND GREASE BOTH ENDS OF ACTUATOR.SDR CA981214014Torque Tube · broken(CAN) WHILE TAXIING, THE PILOTS RIGHT RUDDER PEDAL TORQUE TUBE FAILED. WELD HAD BROKEN.SDR 99ZZZX72Bumper · wornNOSE GEAR WOULD NOT EXTEND CAUSING A LANDING WITHOUT THE NOSE GEAR DEPLOYED, CAUSING DAMAGE TO THE PROPELLER AND NOSE SECTION. THE NOSE GEAR BUMPER AT THE TOP OF THE WHEELWELL WHICH DETERMINES THE NOSE GEAR RETRACTION HEIGHT WAS WORN OUT. THIS ALLOWS THE NOSSDR 98ZZZX4230Wing · crackedLEFT WING RIB WAS FOUND CRACKED AT STA 190.0. THIS LOCATION IS AT THE OUTBOARD HINGE LOCATION OF THE AILERON. THIS IS WHERE ALL THE BALANCE LEAD IS LOCATED. SUBMITTER SUGGESTED CAUSE AS FATIGUE DUE TO RIB FLEXING DURING TURBULENCE. AIRCRAFT IS USED FOR TRASDR CA981109020Bungee · broken(CAN) PILOT UNABLE TO STEER AIRCRAFT STRAIGHT AFTER A TIGHT TURN INTO WIND. INSPECTION FOUND THE STEERING BUNGEE LOCATED ABOVE THE RUDDER TORQUE TUBES BETWEEN THE PILOT'S AND CO-PILOT'S PEDALS TO BE BROKEN AND JAMMED. THIS IS SECOND INCIDENT ONE OF SUBMITTERSDR AU981360Electrical · fire(AUS) ELECTRICAL FIRE IN REAR RADIO AND BATTERY COMPARTMENT.SDR CA981022007Pin · broken(CAN) FUEL SELECTOR GEAR ASSY AND U-JOINT SHAFT WAS REMOVED TO REPAIR EXCESS PLAY. ONE GEAR WAS LOOSE ON ITS SHAFT. WHEN ROLL PIN WAS REMOVED IT WAS FOUND TO BE BROKEN IN 3 PIECES. ROLL PIN HOLDS GEAR ON SHAFT.SDR 98ZZZX3611Actuator · crackedLEFT GEAR WOULD NOT EXTEND FOR LANDING. PILOT TRIED TO BRING GEAR UP, LEFT GEAR JUST HUNG HALF WAY. AIRCRAFT LANDED WITH GEAR UP. INVESTIGATION REVEALED LEFT GEAR ACTUATOR WAS CRACKED AND SECTOR GEAR COULD NOT ENGAGE.SDR 98ZZZX3436Actuator · crackedDURING A ROUTINE INSPECTION, BOTH MLG ACTUATORS WERE FOUND CRACKED JUST BELOW THE BEARING CUPS. THIS IS AN ONGOING PROBLEM WITH THE DESIGN OF THE ACTUATOR. MECHANICS MUST INSPECT THESE ACTUATORS CAREFULLY EACH INSPECTION FOR CRACKS.SDR 98ZZZX3416Pivot · crackedWHILE REMOVING A CRACKED ACTUATOR, THE LT MAIN GEAR PIVOT WAS ALSO FOUND CRACKED. THIS PIVOT IS OF THE NEW STYLE AND PART NUMBER. THIS IS AN ONGOING PROBLEM WITH THIS DESIGN. SUBMITTER STATED MECHANIC SHOULD COMPLY WITH SB 90-1 AT LEAST EVERY 500 HOURS AND SDR 98ZZZX3273Structure · corrodedDURING ANNUAL INSPECTION, CORROSION WAS FOUND IN BELLY OF AIRCRAFT IN MAIN GEAR WHEEL AREA BETWEEN FS 72.0 AND FS 133.0. GEAR WELL CENTER SUPPORT TUNNEL WAS ALSO CORRODED SEVERELY. REPAIR ACCOMPLISHED BY REPLACING SKINS, DOUBLERS, BULKHEADS, AND REAR DOOR POSDR CA980814004Bungee · failed(CAN) AFTER TAKEOFF, THE RUDDER PEDALS JAMMED IN THE FULL LEFT POSITION. CONTINUED CLIMB TO ALTITUDE AND WAS ABLE TO UNJAM THE PEDALS. CARRIED OUT NORMAL LANDING. ON GROUND AND STOPPED PEDALS JAMMED IN FULL LEFT POSITION. THE STEERING BUNGEE SHAFT BROKEN ASDR 98ZZZX3047Fitting · crackedINSPECTION FOUND NLG ACTUATOR FITTING CRACKED. THE FITTING IS A MACHINED PIECE OF ALUMINUM THAT THE NOSE GEAR ACTUATOR ATTACHES TO THE AIRFRAME. IT IS POSSIBLE THE CENTER PART OF THE CASTING CRACKED ON BOTH SIDES DUE TO HARD LANDING OR IMPROPER ACTUATOR RIGGISDR CA980623004Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION REPAIR. INSPECTION FOUND STONE DAMAGE TO THE BLADES. THE DAMAGE WAS REPAIRED.SDR 98ZZZX2056Snap Ring · brokenPILOT NOTICED SCRATCHES ON PROPELLER DURING POST-FLIGHT INSPECTION FOLLOWING COMPLETION OF A BREAK-IN FLIGHT FOR NEWLY OVERHAULED ENGINE AND PROPELLER. INSPECTION FOUND SPINNER AND SPINNER BULKHEAD DAMAGED AND REQUIRED REPLACEMENT. PROP TT: 1,887.8 HOURS. SDR 98ZZZX1999Dampener · crackedSHIMMY DAMPENER WELDED AFTER DAMAGE. AFTER 6 MONTHS USE, CRACK DEVELOPED WHILE IN SERVICE. RESULTING LEAK OF FLUID CAUSED SEVERE SHIMMY ON ATTEMPTED TAKEOFFS. UNIT REPLACED WITH NEW ITEM FROM CESSNA.SDR 98ZZZX2055Pivot Assy · crackedA FLIGHT SCHOOL AIRCRAFT WAS PRACTICING GEAR EXTENSIONS. ON FINAL EXTENSION, THE LT MAIN GEAR WOULD NOT EXTEND. THE GEAR WAS CYCLED SEVERAL TIMES WITH NO SUCCESS. A DEEP STALL FOLLOWED BY A QUICK PUSH-OVER LOCKED THE LT MAIN GEAR DOWN. A DOWN AND LOCKED INDSDR 98ZZZX2054Pivot Assy · crackedA FLIGHT SCHOOL AIRCRAFT WAS PRACTICING GEAR EXTENSIONS. ON FINAL EXTENSION, THE LT MAIN GEAR WOULD NOT EXTEND. THE GEAR WAS CYCLED SEVERAL TIMES WITH NO SUCCESS. A DEEP STALL FOLLOWED BY A QUICK PUSH-OVER LOCKED THE LT MAIN GEAR DOWN. A DOWN AND LOCKED INDSDR 98ZZZX2140Bolt · failedFOUR EACH OF THESE BOLTS HOLD THE OIL COOLER TO RT BAFFLE. TWO OF THESE BOLTS FAILED LEAVING ONLY THE TWO INBD BOLTS SECURING THE OIL COOLER. FAILURE WAS DISCOVERED AT OIL CHANGE. THIS IS THE P/N CESSNA CALLS FOR IN THE IPM (ILLUSTATED PARTS MANUAL). BOTH SDR AU980240Housing · cracked(AUS) MAIN LANDING GEAR ACTUATOR HOUSING CRACKED.SDR AU980239Pivot · cracked(AUS) RT MAIN LANDING GEAR PIVOT CRACKED.SDR 98ZZZX1054Actuator · crackedDURING A 100-HOUR INSPECTION, BOTH MAIN LANDING GEAR ACTUATOR HOUSINGS PN 1281001-3 WERE INSPECTED AS PART OF A FLEET INSPECTION AND BOTH HOUSINGS WERE FOUND CRACKED IN THE SAME AREA JUST BELOW THE BEARING PN S1997C7-8. BOTH ACTUATORS WERE REPLACED.SDR 98ZZZX1053Actuator · crackedDURING A 100-HOUR INSPECTION, BOTH MAIN LANDING GEAR ACTUATOR HOUSINGS PN 1281001-3 WERE INSPECTED AS PART OF A FLEET INSPECTION AND BOTH HOUSINGS WERE FOUND CRACKED IN THE SAME AREA JUST BELOW THE BEARING PN S1997C7-8. BOTH ACTUATORS WERE REPLACED.SDR 98ZZZX1049Actuator · crackedDURING A 100-HOUR INSPECTION, BOTH MAIN LANDING GEAR ACTUATOR HOUSINGS PN 1281001-3 WERE INSPECTED AS PART OF A FLEET INSPECTION RESULTING WITH ONE HOUSING FOUND CRACKED IN THE AREA JUST BELOW THE BEARING PN S1997C7-8. THE ACTUATOR WAS REPLACED.SDR 98ZZZX1073Actuator · crackedDURING A 100-HOUR INSPECTION, BOTH MAIN LANDING GEAR ACTUATOR HOUSINGS PN 1281001-3 WERE INSPECTED AS PART OF A FLEET INSPECTION AND ONE HOUSING WAS FOUND CRACKED IN THE AREA JUST BELOW THE BEARING PN S1997C7-8. THE ACTUATOR WAS REPLACED.SDR 98ZZZX1059Actuator · crackedDURING A 100-HOUR INSPECTION, BOTH MAIN LANDING GEAR ACTUATOR HOUSINGS PN 1281001-3 WERE INSPECTED AS PART OF A FLEET INSPECTION AND BOTH HOUSINGS WERE FOUND CRACKED IN THE SAME AREA JUST BELOW THE BEARING PN S1997C7-8. BOTH ACTUATORS WERE REPLACED.SDR 98ZZZX1058Actuator · crackedDURING A 100-HOUR INSPECTION, BOTH MAIN LANDING GEAR ACTUATOR HOUSINGS PN 1281001-3 WERE INSPECTED AS PART OF A FLEET INSPECTION AND BOTH HOUSINGS WERE FOUND CRACKED IN THE SAME AREA JUST BELOW THE BEARING PN S1997C7-8. BOTH ACTUATORS WERE REPLACED.SDR 98ZZZX515Fitting · crackedMLG LEG FITTING FOUND CRACKED. SUBMITTER STATES POSSIBLE CAUSE AS HARD LANDINGS.SDR 98ZZZX1064Actuator · crackedDURING A 100-HOUR INSPECTION, BOTH MAIN LANDING GEAR ACTUATOR HOUSINGS PN 1281001-3 WERE INSPECTED AS PART OF A FLEET INSPECTION AND BOTH HOUSINGS WERE FOUND CRACKED IN THE SAME AREA JUST BELOW THE BEARING PN S1997C7-8. BOTH ACTUATORS WERE REPLACED.SDR 98ZZZX1063Actuator · crackedDURING A 100-HOUR INSPECTION, BOTH MAIN LANDING GEAR ACTUATOR HOUSINGS PN 1281001-3 WERE INSPECTED AS PART OF A FLEET INSPECTION AND BOTH HOUSINGS WERE FOUND CRACKED IN THE SAME AREA JUST BELOW THE BEARING PN S1997C7-8. BOTH ACTUATORS WERE REPLACED.SDR 98ZZZX1062Actuator · crackedDURING A 100-HOUR INSPECTION, BOTH MAIN LANDING GEAR ACTUATOR HOUSINGS PN 1281001-3 WERE INSPECTED AS PART OF A FLEET INSPECTION AND BOTH HOUSINGS WERE FOUND CRACKED IN THE SAME AREA JUST BELOW THE BEARING PN S1997C7-8. BOTH ACTUATORS WERE REPLACED.SDR 98ZZZX1061Actuator · crackedDURING A 100-HOUR INSPECTION, BOTH MAIN LANDING GEAR ACTUATOR HOUSINGS PN 1281001-3 WERE INSPECTED AS PART OF A FLEET INSPECTION AND BOTH HOUSINGS WERE FOUND CRACKED IN THE SAME AREA JUST BELOW THE BEARING PN S1997C7-8. BOTH ACTUATORS WERE REPLACED.SDR 98ZZZX1056Actuator · crackedDURING A 100-HOUR INSPECTION, THE RIGHT MAIN LANDING GEAR ACTUATOR ASSEMBLY PN 9882015-2 ATTACH BOLT WAS FOUND LOOSE WHICH ALLOWED THE ACTUATOR TO HAVE MOVEMENT DURING RETRACTION AND EXTENSION. UPON FURTHER INSPECTION OF THE ACTUATOR HOUSING PN 1281001-3, A CSDR 98ZZZX1055Actuator · crackedDURING A 100-HOUR INSPECTION, THE RIGHT MAIN LANDING GEAR ACTUATOR ASSEMBLY PN 9882015-2 ATTACH BOLT WAS FOUND LOOSE WHICH ALLOWED THE ACTUATOR TO HAVE MOVEMENT DURING RETRACTION AND EXTENSION. UPON FURTHER INSPECTION OF THE ACTUATOR HOUSING PN 1281001-3, A CSDR 99ZZZX375Shaft · wrong partFOUND ENGINE OVERHAULED WITH INCORRECT ROCKER SHAFTS INSTALLED ON ALL CYLINDERS. NOTICED SHAFTS WERE DAMAGING ROCKER COVERS. UPON FURTHER INSPECTION, DETERMINED THE ROCKER SHAFTS WERE NOT THE CORRECT PART NUMBER, WERE TOO LONG, AND DID NOT CONTAIN THE PLASTISDR 98ZZZX192Switch · corrodedUPON APPROACH TO LNG, GEAR LOWERED, GREEN DOWN AND LOCKED LIGHT DID NOT COME ON. CYCLED GEAR, STILL NO GREEN LIGHT. GEAR VISUALLY APPEARED DOWN AND LOCKED (IN POSITION). LANDED WITH NO PROBLEMS. FOUND RT MLG DOWN AND LOCKED SWITCH CORRODED AND INTERMITTENTSDR 98ZZZX445Fuel Pump · wrong partA FACTORY OVERHAULED ENGINE WAS BEING INSTALLED WHEN MECH REPORTED UNABLE TO CONNECT THE FUEL LINES TO THE NEW FUEL PUMP (ENG DRIVEN). THE 'IN' AND 'OUT' PORTS WERE REVERSED. MFG WAS CONTACTED, AND A SECOND PUMP SENT, BUT IT WAS THE SAME P/N AS THE ORIG, BUTSDR 97ZZZX4964Piston Ring · failedEXCESSIVE OIL OUT OF ENGINE BREATHER PROMPTED ENGINE COMPRESSION CHECK WHICH REVEALED LOW COMPRESSION ON NR 1 CYLINDER. REMOVAL OF CYLINDER REVEALED TOP COMPRESSION RING SHATTERED INTO APPROX .25 INCH SEGMENTS AND SECOND COMPRESSION RING BROKEN IN SEVERAL PLASDR 98ZZZX35Blade · brokeAPPROXIMATELY 4 INCHES OF PROPELLER TIP BROKE OFF IN-FLIGHT. AIRCRAFT MADE EMERGENCY LANDING.SDR 97ZZZX5129Barrel · failedAIRCRAFT WAS BROUGHT TO MAINTENANCE AFTER A TRAINING FLIGHT WITH REPORT OF A SEVERE NOSE WHEEL VIBRATION. AN INSPECTION REVEALED THAT THE END OF THE SHIMMY DAMPENER BARREL CLOSEST TO THE SERVICE HOLE WAS BROKEN OFF. THE OUTER RETAINING LINE AND BEARING HEAD SDR 97ZZZX4801Torque Tube · brokenPILOT REPORTED LOSS OF RUDDER CONTROL IN-FLIGHT ALTHOUGH HE WAS ABLE TO MAINTAIN CONTROL OF THE AIRCRAFT AND MADE AN UNEVENTFUL LANDING. FOUND THE AFT (RIGHT HAND) RUDDER PEDAL TORQUE TUBE WAS BROKEN APPROXIMATELY 7/8 OF THE WAY AROUND THE TUBE JUST TO THE LESDR 97ZZZX4469Pivot Splines · shearedRIGHT MAIN LANDING GEAR PIVOT SPLINE SHEARED OFF DURING GEAR RETRACTION. AIRCRAFT LANDED WITH GEAR-UP CONFIGURATION. MINOR DAMAGE TO FUSELAGE UNDERCARRIAGE AND PROPELLER. SUSPECT CAUSE - EXCEEDED LIFE CYCLES. SUBMITTER RECOMMENDATION: AN AD ISSUED MAKING CSDR 97ZZZX4262Carburetor · stop wornFULL THROTTLE STOP WORN CAUSING A LEAN MIXTURE. WHEN THE PART IS FULL RICH WITH THE SCREW TYPE MIX CONTROL, PRESSURE IS PUT ON THE FULL RICH STOP. STOP IS BEHIND A COVER PLATE WHICH HAMPERS VISABILITY. WEAR CAUSES THE METER HOLE ON MIXTURE TO OVER-CENTER CASDR 97ZZZX4190Axle Fitting · crackedCASTING CRACKED IN TWO LOCATIONS. CRACKS WERE LOCATED AT 90 DEGREES TO THE BOLT HOLES, AND PARALLEL TO THE BORE DIAMETER. ONE CRACK APPROXIMATELY 2.500 INCHES LONG WAS LOCATED IN THE WEB SECTION ABOVE THE BOLT HOLES. SECOND CRACK LOCATED IN THE LOWER WEB SESDR 97ZZZX4055Hose · leakDEFECTIVE HOSE FOUND DURING ROUTINE INSPECTION. CLAMPS FOR HEAT SLEEVE WERE TIGHTENED EXCESSIVELY, LEAKING AT THAT AREA.SDR 97ZZZX4043Stabilizer · rivets looseDURING INSPECTION, FOUND WORKING RIVETS ON TOP OF STABILIZER SKIN JUST UNDERNEATH FAIRING FOR HORIZONTAL STABILIZER TO FUSELAGE.SDR 97ZZZX3920Float · failedPILOT REPORTED ENGINE QUIT ON FINAL APPROACH OVER RUNWAY. DELIVERED TO MAINTEANCE, UNABLE TO GET GOOD RUN-UP. DISCOVERED CARBURETOR FLOAT FULL OF FUEL. REPLACED WITH SERVICEABLE FLOAT. ENGINE OPS CHECK GOOD.SDR 97ZZZX3938Diode · failedALTERNATOR IN-FLIGHT FAILURE TOGETHER WITH FAILURE OF NAV 1 AND GPS. ALTERNATOR FIELD BREAKER OPEN. REPLACED TWO SHORTED DIODES WITH CESSNA P/N 1N6391. AIRCRAFT WITH ONE HOUR TEST FLIGHT WAS UNEVENTFUL AND AIRWORTHY WITH ALL ELECTRICAL DEVICES WORKING.
Back to Cessna 172RG