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 = '172R' 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 = '172R' 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 2003FA0000911Spar · crackedDURING MAINTENANCE OF THE AIRCRAFT IN WHICH THE RIGHT FUEL TANK WAS OPENED UP, A CRACK WAS FOUND IN THE AFT SPAR. THE CRACK EXTENDS FROM WS 33.0 TO 34.375 AND IS APPROX 1.375 INCHES LONG. THE CRACK IS LOCATED IN THE UPPER BEND RADIUS OF THE AFT SPAR.SDR AUS20030918Fcu · faulty(AUS) FUEL CONTROL UNIT AIR CHAMBER CONTAMINATED WITH FUEL.SDR AUS20030863Rivet · sheared(AUS) RT FLAP INBOARD TRACK LOWER ATTACHMENT RIVETS SHEARED. OTHER RIVETS WORKING.SDR AUS20030862Rivet · loose(AUS) RT FLAP INBOARD TRACK LOWER ATTACHMENT RIVETS WORKING.SDR 2003FA0000855Inertia Reel · failedIT HAS BEEN FOUND THAT THE REAR SEAT BELT LOWER IN REELS WILL NOT PROPERLY RETRACT UNLESS THE BELTS ARE MANUALLLY INSERTED/FED INTO THE REEL ASSY. ADDITIONALLY UNLESS THE BELTS ARE FULLY RETRACTED FIRST, THEY WILL NOT EXTEND. 50 PERCENT OF THE TIME, FACTORY SDR 2003FA0000819Line · chafedNR 2 CYLINDER FUEL INJECTOR LINE RUBBING ON CYLINDER COOLING FIN, CAUSING A DEEP CUT IN OUTER WALL OF FUEL INJECTOR LINE, LEADING TO POSSIBLE ENGINE FIRE.SDR AUS20030750Wheel · corroded(AUS) NOSE WHEEL CORRODED.SDR AUS20030716Cable · misinstalled(AUS) AILERON CROSSOVER CABLE LOCATED IN RT WING WORN FLAT IN AREA WHERE CABLE RUNS ON FAIR LEAD. CABLE WAS INCORRECTLY ROUTED. PERSONNEL/MAINTENANCE ERROR.SDR 2003FA0000658Cable · brokenPILOT SEAT WOULD NOT MOVE FORWARD OR AFT WHEN MOVING SEAT LOCK CONTROL. INSPECTION FOUND OUTBOARD PIN NOT DISENGANGING FROM SEAT RAIL. FURTHER DISASSEMBLY FOUND THE CABLE BROKEN INTERNALLY JUST ABOVE PIN RETURN SPRING. (PREVIOUS MDR DATED 6/25/03 SHOWED INCORRSDR CA030704003Motor · burned(CAN) ENGINE STARTER MOTOR WAS BURNED,SDR CA030528007Starter · failed(CAN) STARTER FAILED AFTER MINIMAL USE.SDR 2003FA0000647Fuel Control · erraticDURING THE PRE TAKEOFF IDLE CHECK, THE IDLE RPM WAS FOUND VERY LOW. IT WAS ADJUSTED. THE IDLE MIXTURE/SPEED, ON THIS SERVO, IS VERY ERRATIC AND UNSTABLE WITHIN A VERY FEW NUMBER OF HOURS/DAYS.SDR 2003FA0000477Control Cable · chafedDURING A ROUTINE INSPECTION, THE RIGHT AILERON BALANCE CABLE (P/N 0510105-362) WAS FOUND CHAFING ON A FAIRLEAD LOCATED MIDWAY THROUGH THE FLAP WELL AREA. THE CABLE IS EXTREMELY DIFFICULT TO EXAMINE THOROUGHLY WHILE INSTALLED. A BORESCOPE CAN AID IN VIEWING THESDR 2003FA0000471Control Cable · chafedDURING A ROUTINE INSPECTION, THE LEFT AILERON BALANCE CABLE (P/N 0510105-364) WAS FOUND CHAFING ON A FAIRLEAD LOCATED MIDWAY THROUGH THE FLAP WELL AREA. THE CABLE IS EXTREMELY DIFFICULT TO EXAMINE THOROUGHLY WHILE INSTALLED. A BORESCOPE CAN AID IN VIEWING THE SDR 2003FA0000472Control Cable · chafedDURING A ROUTINE INSPECTION, THE RIGHT AILERON BALANCE CABLE (P/N 0510105-365) WAS FOUND CHAFING ON A FAIRLEAD LOCATED MIDWAY THROUGH THE FLAP WELL AREA. THE CABLE IS EXTREMELY DIFFICULT TO EXAMINE THOROUGHLY WHILE INSTALLED. A BORESCOPE CAN AID IN VIEWING THESDR 2003FA0000474Control Cable · chafedDURING A ROUTINE INSPECTION, THE RIGHT AILERON BALANCE CABLE WAS FOUND CHAFING ON A FAIRLEAD LOCATED MIDWAY THROUGH THE FLAP WELL AREA. THE CABLE IS EXTREMELY DIFFICULT TO EXAMINE THOROUGHLY WHILE INSTALLED. A BORESCOPE CAN AID IN VIEWING THE AREA MORE ACCURATSDR 2003FA0000473Control Cable · chafedDURING A ROUTINE INSPECTION, THE LEFT AILERON BALANCE CABLE WAS FOUND CHAFING ON A FAIRLEAD LOCATED MIDWAY THROUGH THE FLAP WELL AREA. THE CABLE IS EXTREMELY DIFFICULT TO EXAMINE THOROUGHLY WHILE INSTALLED. A BORESCOPE CAN AID IN VIEWING THE AREA MORE ACCURATESDR 2003FA0000438Fuel Control · inaccurateDURING PRE TAKE OFF GROUND CHECK, THE CREW REOPORTED THE IDLE TO BE LOW. IT WAS SUBSEQUENTLY ADJUSTED. THIS ENGINE/FUEL CONTROL COMBINATION REQUIRES SUBSTANTIAL ADJUSTMENT TO MAINTAIN PROPER OPERATION..SDR 2003FA0000442Spark Plug · fouledTHE CREW REPORTED THE ENGINE (COUGHED) ON TAKE OFF. COMPLETED AN INSPECTION ON SUSPECT ITEMS. CLEANED, TESTED AND FLOW TESTED ALL NOZZLES, CLEANED AND TESTED SPARK PLUGS. SEVERAL WERE FOUND MARGINALLY FOULED. THIS ENGINE/FUEL CONTROL COMBINATION DOES REQUIRE SSDR 2003FA0000421Servo · inaccurateDURING FLIGHT THE CREW REPORTED A ROUGH ENGINE. SUBSEQUENTLY THE FUEL SERVO AND FLOW DEVIDER WERE CHANGED.SDR 2003FA0000417Fuel Control · out of adjustDURING GROUND OPERATION, THE CREW NOTICED THE IDLE WAS TOO LOW TO CONTINUE THE FLIGHT. THIS ENGINE/FUEL CONTROL COMBINATION REQUIRES A SIGNIFICANT AMOUNT OF ADJUSTMENT TO MAINTAIN THE CORRECT IDLE MIXTURE AND SPEED.SDR CA030423007Lanyard · chafed(CAN) DURING A ROUTINE INSPECTION IT WAS NOTICED THAT THE LANYARD CABLE WHICH LINKS THE ELT SUPPORT BRACKET TO THE ELT ANTENNA SUPPORT BRACKET HAS ENOUGH SLACK IN ITS LENGTH THAT IT RUBS AGAINST THE FUSELAGE (EMPENNAGE) SKIN. THE LANYARD APPEARS TO BE STEEL, SDR 2003FA0000391Lock · misinstalledFRONT BOLT HOLE ON THE PILOT LOCK-CYLINDER WAS INSTALLED 90 DEGREES THE WRONG DIRECTION.SDR AUS20030513Fuel Control · contaminated(AUS) FUEL CONTROL UNIT AIR CHAMBER CONTAMINATED WITH FUEL. CAUSED BY OVERPRIMING.SDR 2003FA0000336Spinner · crackedDURING AN INSPECTION, THE SPINNER WAS FOUND CRACKED.SDR 2003FA0000333Carburetor · inoperativeDURING PRE-TAKEOFF CHECK, THE CREW REDUCED THE THROTTLE TO CHECK THE IDLE SPEED. THE ENGINE WOULD ALMOST QUIT EACH TIME IT WAS ATTEMPTED. THIS ENGINE/FUEL CONTROL COMBINATION REQUIRES SUBSTANTIAL ADJUST FOR A VERY FEW HOURS FLOWN.SDR 2003FA0000320Carburetor · inaccurateDURING PRE TAKEOFF GROUND OPERATIONAL CHECK, THE IDLE SPEED WAS ONLY ABOUT 400 RPM. IT WAS ADJUSTED ALONG WITH THE MIXTURE. THIS ENGINE FUEL CONTROL COMBINATION WAS THE SUBJECT OF AN AIRWORTHINESS DIRECTIVE FOR THIS PROBLEM. THE VARIOUS OTHER COMPONENTS OF THSDR 2003FA0000337Carburetor · inaccurateDURING NORMAL OPERATIONS, THE ENGINE WOULD SPUTTER AND RUN VERY IRREGULARLY AT IDLE. AFTER ROUTINE IDLE SPEED/MIXTURE ADJUSTMENT THE ENGINE RAN PROPERLY. THIS ENGINE/FUEL CONTROL COMBINATION REQUIRES ADJUSTMENT OF THE IDLE SPEED/MIXTURE MORE OFTEN THAN TYPICALSDR 2003FA0000311Carburetor · inaccurateTHE CREW REPORTED A ROUGH IDLE DURING GROUND OPERATION. THIS ENGINE/AIRCRAFT COMBINATION HAS BEEN THE SUBJECT OF AN AIRWORTHINESS DIRECTIVE REGARDING UNSTABLE IDLE/MIXTURE ISSUES. IT IS NOT UNCOMMON FOR THIS SITUATION TO OCCUR NOT ONLY DURING INSPECTION GROUNDSDR 2003FA0000310Carburetor · inaccurateTHE CREW REPORTED A ROUGH IDLE DURING GROUND OPERATION. THIS ENGINE/AIRCRAFT COMBINATION HAS BEEN THE SUBJECT OF AN AIRWORTHINESS DIRECTIVE REGARDING UNSTABLE IDLE/MIXTURE ISSUES. IT IS NOT UNCOMMON FOR THIS SITUATION TO OCCUR NOT ONLY DURING INSPECTION GROUNDSDR 2003FA0000309Carburetor · inaccurateTHE CREW REPORTED A ROUGH IDLE DURING GROUND OPERATION. THIS ENGINE/AIRCRAFT COMBINATION HAS BEEN THE SUBJECT OF AN AD REGARDING UNSTABLE IDLE/MIXTURE ISSUES. IT IS NOT UNCOMMON FOR THIS SITUATION TO OCCUR NOT ONLY DURING INSPECTION GROUND RUNS, BUT ALSO DURINSDR 2003FA0000281Fuel Control · erraticDURING A PRE TAKEOFF IDLE CHECK, THE ENGINE RAN EXTREMELY SLOW. IT WAS ADJUSTED. THIS ENGINE/FUEL CONTROL SYSTEM HAS BEEN THE SUBJECT OF AN AIRWORTHINESS DIRECTIVE CONCERNING IDLE ANOMALIES.SDR 2003FA0000244Engine · fluctuatesDURING AN INSPECTION THE IDLE WAS FOUND TO BE ABOUT 900 RPM. TYPICALLY THIS IS NOT CONSIDERED TO BE A REPORTABLE EVENT, HOWEVER THIS ENGINE/AIRCRAFT COMBINATION HAS BEEN THE SUBJECT OF AN AIRWORTHINESS DIRECTIVE REGARDING UNSTABLE IDLE/MIXTURE ISSUES. IT IS NOSDR 2003FA0000243Spinner · crackedTHE PROP SPINNER ON THE 172 RS SERIES CRACKS VERY FREQUENTLY. THE CRACKS RADIATE FROM THE CUT OUT FOR THE PROP BLADES.SDR 2003FA0000263Fuel Control · failedDURING A PRE TAKE OFF IDLE CHECK, THE ENGINE QUIT. THIS ENGINE/FUEL CONTROL SYSTEM IS THE SUBJECT OF AN AIRWORTHINESS DIRECTIVE CONCERNING UNSTABLE IDLE TENDENCIES.SDR 2003FA0000262Fuel Nozzle · obstructedON TAKE OFF THE ENGINE RAN ROUGH. INVESTIGATION SHOWED THAT ONE FUEL INJECTOR NOZZLE WAS FOUND WITH AN IRREGULAR FLOW. IT WAS REPLACED.SDR 2003FA0000359Firewall · crackedDURING A PHASE 1 INSPECTION FOUND A CRACK IN THE FIREWALL AT THE LOWER ROW OF RIVETS ATTACHING THE BATTERY BOX TO THE FIREWALL. UPON REMOVAL OF BOX FOR REPAIR FOUND 2ND CRACK UNDER THE OUTBOARD VERTICAL ROW OF RANGE IN MFG SB FIREWALL INSPECTION.SDR 2003FA0000276Bulkhead · crackedTHE SPINNER AFT BULKHEAD WAS FOUND CRACKED. IT WAS REPLACED WITH A NEW UNIT...SDR 2003FA0000271Flow Divider · stickingDURING GROUND OPERATIONS, THE CREW FELT A ROUGH AND UNSTABLE IDLE. AN INSPECTION WAS MADE OFTHE ENGINE AND SYSTEMS. 2 NOZZLES WERE DETERMINED TO HAVE AN IRREGULAR SPRAY PATTERN. AFTER CLEANING, 1 WAS REPLACED. ALSO, THE FUEL FLOW DIVIDER WAS FOUND TO BE STICKISDR 2003FA0000259Fuel Control · out of adjustTHE CREW REPORTED A PARTIAL POWER LOSS DURING STALL RECOVERY. THIS ENGINE/AIRCRAFT COMBINATION HAS BEEN THE SUBJECT OF AN AIRWORTHINESS DIRECTIVE REGARDING UNSTABLE IDLE/MIXTURE ISSUES. IT IS NOT UNCOMMON FOR THIS SITUATION TO OCCUR NOT ONLY DURING INSPECTION SDR 2003FA0000482J-Box · looseFOUND THE ELECTRICAL JUNCTION BOX (J-BOX) BRACKETS LOOSE. FURTHER INVESTIGATION REVEALED THAT THE 12 RIVETS THAT HOLD THE BRACKETS TO THE BOX WHERE LOOSE AND 6 OF THE 12 RIVETS THE RIVET HEADS WERE POPPING OFF, CRACKED AND FRACTURED (PHOTOS). IF LEFT UNATTENSDR 2003FA0000172Tire · splitFOUND SPLIT IN LT MAIN TIRE ON SIDEWALL. RECAP TIRE 6.00 X 6. SPLIT IS APPROX 50 PERCENT RADIUS OF THE SPLIT IS TO CORD.SDR CA030131007Wire · chafed(CAN) CREW REPORTED INSTRUMENT PANEL LIGHTS WOULD OPERATE INTERMITTANTLY IN FLIGHT. CONDITION ONLY SEEMED TO OCCUR WHEN PILOT OPERATED THROTTLE CONTROL. MAINTENANCE INVESTIGATING DEFECT DETERMINED THE AIRCRAFT WIRING BUNDLE BEHIND THE PANEL WAS POSITIONED IN SSDR 2003FA0000213Connector · improper partCONNECTOR FROM AIRCRAFT HARNESS TO TURN COORDINATOR HAS IMPROPERLY CRIMPED PINS AND LOOSE BACKSHELL, CAUSING AUTO-PILOT FAILURES AND INCORRECTLY DIAGNOSED FAILURES OF TURN-COORDINATORS.SDR CA030117002Check Valve · unserviceable(CAN) THE VACUUM SYSTEM CHECK VALVE MANIFOLD WAS DETERMINED TO BE UNSERVICEABLE DUE TO LEAKS PAST THE CHECK VALVE DISC. THIS FINDING WAS DETERMINED BY FOLLOWING THE INSPECTION CRITERIA CONTAINED IN CESSNA SB 02-37-04. THE PART WAS REMOVED FROM SERVICE AND A RESDR CA030117001Check Valve · unserviceable(CAN) THE VACUUM SYSTEM CHECK VALVE MANIFOLD WAS DETERMINED TO BE UNSERVICEABLE DUE TO LEAKS PAST THE CHECK VALVE DISC. THIS FINDING WAS DETERMINED BY FOLLOWING THE INSPECTION CRITERIA CONTAINED IN CESSNA SB02-37-04. THE PART WAS REMOVED FROM SERVICE AND A RESDR CA021118007Tank · cracked(CAN) HEADER TANK FOUND LEAKING. UPON REMOVAL, TANK HAS A 1 INCH CRACK ON TOP OF WELD AROUND BOTTOM AFT SIDE OF TANK.SDR 2002FA0001267P-Lead · failedREPORTS OF INTERMITTENT LT MAG FAILURE. TROUBLESHOT AND REMOVED ENTIRE P-LEAD ASSEMBLY. FOUND SHIELDING SOLDER / CRIMP AT SWITCH END CUT INTO CENTER CORE VERY SLIGHTLY. REPLACED P-LEAD ASSEMBLY. NO ADDITIONAL REPORTS OF MAG FAILURE.SDR 2002FA0001173Engine · malfunctionedENGINE SHUT DOWN IN FLIGHT. ABLE TO RESTART ON GROUND RUNUP INDICATES NO PROBLEMS. REMOVED FUEL SERVO FOR BACK/FLOW CHECK FOUND OIL IN SERVO NOT DETERMINED IF CAUSE OF SHUTDOWN. FLOW DIVIDER OVERHAULED. IGNITION SWITCH DISASSEMBLED/REPAIRED. FUEL VENT SYSSDR DF22002F00002Nut Plate · brokenDURING 100 HOUR INSPECTION, TECHNICIAN FOUND LOWER ELEVATOR STOP NUTPLATE BROKEN AND FIBER LOCK PORTION OF PART SEPARATED FROM THE REST OF NUTPLATE. STOP BOLT COULD MOVE FREELY.
Back to Cessna 172R