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 99ZZZX1597Screw · looseBOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1596Screw · looseBOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1594Screw · looseBOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1593Screw · looseBREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1071Wire · separatedLOW VOLTAGE LIGHT CAME ON SEVERAL TIMES DURING FLIGHT. PERFORMED ENGINE RUN-UP FOR OPERATIONAL CHECK OF ALTERNATOR. ALTERNATOR CHECKS OUT GOOD. UPON FURTHER INSPECTION, THE 'GROUND' ALTERNATOR TERMINALS WERE FOUND BROKEN. THESE WIRE TERMINALS APPEAR TO BE SDR 99ZZZX1631Screw · looseBOTH DISTRIBUTOR BLOCK SCREWS, BREAKER POINT PIVOT SCREW, AND COIL GROUND SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1629Screw · looseBOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1628Screw · looseBOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1626Screw · looseMAGNETO HOUSING SCREWS, BREAKER POINT CONTACT SCREW, AND BOTH DISTRIBUTOR BLOCK SCREWS FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1625Screw · looseBOTH DISTRIBUTOR BLOCK SCREWS FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1622Screw · looseBREAKER POINT PIVOT SCREW AND BOTH DISTRIBUTOR BLOCK SCREWS FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1621Screw · looseBREAKER POINT PIVOT SCREW AND BOTH DISTRIBUTOR BLOCK SCREWS FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1620Screw · looseBOTH DISTIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1617Screw · looseDISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1616Screw · looseBREAKER POINT CONTACT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.SDR 99ZZZX1075Retainer · missingRETAINER MISSING ON OUTBOARD SIDE OF BUSHING PN 0541202-4 ON LEFT MAIN LANDING GEAR.SDR AU990127Fuse · failed(AUS) FUSE DAMAGED. FUSE SEVERED THROUGH LEG NOT THROUGH THE FUSEABLE LINK. PART TC: 978.SDR 99ZZZX1036Bushing · damagedDURING A ROUTINE INSPECTION OF THE AIRFRAME, THE RT MAIN LANDING GEAR BUSHING WAS FOUND DEFORMED. THE INSIDE BUSHING MATERIAL WAS PROTRUDING FROM THE EDGE OF THE BUSHING. THE BUSHING WAS FURTHER INSPECTED AFTER REMOVAL FOR THE AIRCRAFT AND CONTAINED STRESS CSDR 99ZZZX968Nut · misinstalledPERFORMED STATIC LEAK CHECK PER SB 97-32-02R1, ALT STATIC VALVE REPLACEMENT. STATIC CHECK FAILED DUE TO CROSS-THREADED CONNECTOR INTO PITOT TUBE ITEM 41 AND CROSS-THREADED B-NUT ITEM 42 OF IPC (34-11-00-01). REPLACED BOTH CONNECTORS. OPS CHECKS NORMAL. SUBSDR 99ZZZX966Connector · misinstalledPERFORMED STATIC LEAK CHECK PER SB 97-32-02R1, ALT STATIC VALVE REPLACEMENT. STATIC CHECK FAILED DUE TO CROSS-THREADED CONNECTOR INTO PITOT TUBE ITEM 41 AND CROSS-THREADED B-NUT ITEM 42 OF IPC (34-11-00-01). REPLACED BOTH CONNECTORS. OPS CHECKS NORMAL. SUBSDR 99ZZZX812Support · bindingCONTROL YOKE STICKING ON FLAREOUT AT LANDING. FOUND LEFT GUIDE SUPPORT WAS PUSHED UP TO GIVE CLEARANCE FOR ROLLER ON CONTROL YOKE ASSY THAT WAS BINDING WHEN IT CAME OUT OF GUIDE ASSY. ALSO, FOUND RIGHT GUIDE ASSY HAS BEEN SPREAD APART TO GIVE CLEARANCE FOR FSDR 99ZZZX1393Guide · malfunctionedDURING INSPECTION FOUND LEFT UPPER YOKE ROLLER DISENGAGING FROM SUPPORT GUIDE. REPLACED YOKE ASSY AND LEFT GUIDE SUPPORT. OPS CHECKS NORMAL.SDR 99ZZZX1392Yoke Assy · malfunctionedDURING INSPECTION FOUND LEFT UPPER YOKE ROLLER DISENGAGING FROM SUPPORT GUIDE. REPLACED YOKE ASSY AND LEFT GUIDE SUPPORT. OPS CHECKS NORMAL.SDR 99ZZZX1391Guide Assy · malfunctionedLEFT UPPER SIDE OF CONTROL YOKE ROLLER IS DISENGAGING FROM SUPPORT GUIDE WHEN SIDE PRESSURE IS APPLIED TO YOKE. CESSNA HAS FOUND THAT THE CONTROL YOKES IN ARE NOT WELDED CORRECTLY. REPLACED YOKE AND LEFT GUIDE SUPPORT, OPS CHECKS NORMAL.SDR 99ZZZX1390Yoke Assy · malfunctionedLEFT UPPER SIDE OF CONTROL YOKE ROLLER IS DISENGAGING FROM SUPPORT GUIDE WHEN SIDE PRESSURE IS APPLIED TO YOKE. CESSNA HAS FOUND THAT THE CONTROL YOKES IN ARE NOT WELDED CORRECTLY. REPLACED YOKE AND LEFT GUIDE SUPPORT, OPS CHECKS NORMAL.SDR 99ZZZX1219Connector · looseWHILE REPLACING SUPPORT GUIDE FOR CONTROL YOKE ON LEFT SIDE, REMOVED INSTRUMENT PANEL, FOUND FITTING FINGER TIGHT ITEM 29 AND ITEM 22 ON AIRSPEED INDICATOR (IPC 34-11-00-01) TIGHTENED CONNECTORS. LEAK CHECKED NORMAL. RECOMMENDATION: TIGHTEN CONNECTORS AT ASSDR 99ZZZX1199Connector · looseWHILE REPLACING SUPPORT GUIDE FOR CONTROL YOKE ON LEFT SIDE, REMOVED INSTRUMENT PANEL, FOUND FITTING FINGER TIGHT ITEM 29 AND ITEM 22 ON AIRSPEED INDICATOR (IPC 34-11-00-01) TIGHTENED CONNECTORS. LEAK CHECKED NORMAL. RECOMMENDATION: TIGHTEN CONNECTORS AT ASSDR 99ZZZX980Fuel Sender · failedDURING A POST-INSPECTION ENGINE RUN-UP, THE LEFT FUEL GAUGE NEEDLE WAS READING ERRATIC (FULL TO ZERO). INSPECTION OF THE FUEL INDICATION SYSTEM FOUND THE LEFT FUEL TANK SENDER BAD.SDR CA990308007Wire · chafed(CAN) AUTOPILOT WOULD NOT ENGAGE. FOUND THE A/P DISCONNECT WIRING OPEN FROM THE DISCONNECT SWITCH TO THE A/P COMPUTER. BROKEN WIRE BEHIND INSTRUMENT PANEL. WIRING BUNDLE CHAFING BEHIND PILOT'S PANEL.SDR 99ZZZX498Transmitter · malfunctionedRIGHT FUEL GAUGE NEEDLE READS ERRATICALLY. SHOWS ZERO TO FULL INDICATION. INSPECTED THE FUEL SYSTEM AND FOUND THE RIGHT FUEL SENDER, P/N S-3331-1, BAD. DE-FUELED THE RIGHT FUEL TANK AND REPLACED THE FUEL SENDER.SDR 99ZZZX497Transmitter · malfunctionedDURING AN INSPECTION OF THE ALTERNATOR SYSTEM, FOUND THE LEFT AND RIGHT FUEL GAUGE NEEDLES WERE FLUCTUATING FROM FULL TO ZERO. INSPECTED THE FUEL INDICATING SYSTEM AND FOUND THE LEFT SENDER, P/N S-3331-2, BAD. DE-FUELED THE LEFT FUEL TANK AND REPLACED THE FUSDR 99ZZZX493Transmitter · malfunctionedRIGHT FUEL GAUGE NEEDLE READS ERRATICALLY. SHOWS A ZERO TO FULL INDICATION. INSPECTED THE FUEL SYSTEM AND FOUND THE RIGHT FUEL SENDER, P/N S-3331-1, BAD. DE-FUELED THE RIGHT FUEL TANK AND REPLACED THE FUEL SENDER.SDR 99ZZZX492Transmitter · malfunctionedRIGHT FUEL GAUGE NEEDLE READS ERRATICALLY. SHOWS A ZERO TO FULL INDICATION. INSPECTED THE FUEL SYSTEM AND FOUND THE RIGHT FUEL SENDER, P/N S-3331-1, BAD. DE-FUELED THE RIGHT FUEL TANK AND REPLACED THE FUEL SENDER.SDR 20000714SH001Sensor · malfunctionedDURING A POST INSPECTION RUN-UP, THE RIGHT FUEL GAUGE NEEDLE WAS READING ERRATIC (FULL TO ZERO). INSPECTION OF THE FUEL INDICATION SYSTEM FOUND THE RT FUEL TANK SENDER BAD. REPLACEMENT OF THE SENDER UNIT HAS CORRECTED THIS PROBLEM FOR A SHORT TIME. THERE HASDR AU990004Control Cable · worn(AUS) AILERON CABLES SHOWED EXCESSIVE WEAR OVER PHENOLIC BLOCK FORWARD OF FLAP BAY - ESPECIALLY THE LEFT SIDE.SDR AU990003Control Cable · worn(AUS) AILERON CABLES SHOWED EXCESSIVE WEAR OVER PHENOLIC BLOCK FORWARD OF FLAP BAY - ESPECIALLY THE LEFT SIDE.SDR 99ZZZX378Elt · malfunctionedREMOTE ELT SWITCH DID NOT ACTIVATE ELT. SUBMITTER TALKED WITH FACTORY. FOUND CESSNA USED CIRCUIT TESTER AND BLEW INTERNAL FUSES IN ELT. TESTED ELT AND SWITCH WIRING PER FACTORY. SENT IN ELT'S TO FACTORY TO HAVE HIGHER AMP FUSES INSTALLED.SDR 99ZZZX496Transmitter · malfunctionedDURING INSPECTION OF THE ALTERNATOR SYSTEM, FOUND LEFT AND RIGHT FUEL GAUGE NEEDLES WERE FLUCTUATING FROM FULL TO ZERO. INSPECTED THE FUEL INDICATING SYSTEM AND FOUND THE RIGHT FUEL SENDER, P/N S-3331-1, BAD. DE-FUELED THE RIGHT FUEL TANK AND REPLACED THE FUSDR 99ZZZX648Firewall · wrinkledFOUND FIREWALL SEVERELY WRINKLED, NOSE ATTACH STRUCTURE RIVETS SHEARED. TWO INCH CRACK IN FIREWALL BELOW BATTERY BOX AT COWL MOUNT. SUBMITTER STATED A POSSIBLE CAUSE AS HARD LANDING. THICKER FIREWALL COULD PREVENT RECURRENCE.SDR 99ZZZX502Oil · mismanufacturedDID ROUTINE OIL CHANGE AT 100-HOUR/ANNUAL INSPECTION. ALL NORMAL UNTIL RUN-UP AT COMPLIANCE OF INSPECTION. LOW OIL PRESSURE AT ALL POWER SETTINGS. SPSI AT IDLE. TROUBLESHOT SITUATION AND FOUND BAD OIL FROM 2 EACH 1-GALLON JUGS (WERE SEALED) FROM OIL INVENTSDR 99ZZZX398Plug · wornDURING A NIGHT TRAINING FLIGHT, THE CREW NOTICED AN ENGINE VIBRATION THAT BECAME VIOLENT OVER A SHORT PERIOD OF TIME. DURING LANDING, THE OIL PRESSURE WENT TO ZERO PSI. THE NR 4 PISTON WAS FOUND DESTROYED. THE PISTON PIN PLUGS (LYC P/N LW-11775) WERE WORN SSDR 99ZZZX396Wire · brokenLOW VOLTAGE LIGHT CAME ON SEVERAL TIMES DURING FLIGHT. PERFORMED ENGINE RUN-UP FOR OPERATIONAL CHECK OF ALTERNATOR. ALTERNATOR CHECKS GOOD. BATTERY AND GROUND ALTERNATOR TERMINALS WERE FOUND BROKEN. THESE WIRE TERMINALS APPEAR TO BE THIN AND ARE BREAKING SDR 99ZZZX1Fuel Cell · leakingLEFT WING FUEL BAY AREA, OUTBOARD CORNER AREA WHERE BOXED CORNER MEETS THE SKIN CORNER RELIEF FOR FUEL BAY. AREA HAS B-2 FUEL BAY SEALERS OFF, AND WAS LEAKING FUEL. ON THE BACKSIDE OF THIS AREA IS WING COURTESY LIGHT. ALSO, CORNER RELIEF FOR BOX IS .25 INCHSDR 99ZZZX298Cover · looseTHE LT PROTECTIVE COVER CAME LOOSE AND PIVOTED FORWARD, TOWARD THE FIREWALL. THIS PROTECTIVE COVER IS LOCATED ON THE BOTTOM OF THE INSTRUMENT PANEL. THE PILOT PULLED THE PANEL (COVER) BACK TO THE POSITION IT WAS SUPPOSED TO BE IN AND SHORTED OUT THE SWITCHESSDR AU981573Fuse · failed(AUS) ELECTRICAL SYSTEM FUSE F2 SEPARATED AT THE BASE OF THE ASSEMBLY. FUSE HAD ARCED AND DISCONNECTED THE NR 2 BUS.SDR 98ZZZX4781Bulkhead · crackedDURING ROUTINE INSPECTION, THE FIREWALL WAS FOUND CRACKED AT THE UPPER PART OF THE LOWER FIREWALL JUST BEHIND THE COWL MOUNT AND AT THE COWL MOUNT JUST BELOW THE BATTERY BOX. THIS DEPARTMENT HAS NOTICED THE FIREWALL IS .016 INCH THICK WHICH IS THINNER THAN FISDR 98ZZZX4780Bulkhead · crackedDURING A ROUTINE INSPECTION, THE FIREWALL WAS FOUND CRACKED IN 3 PLACES. THE FIREWALL THICKNESS - .016 INCH WHICH IS THINNER THAN OLDER MODELS WHICH ARE BETWEEN .020 INCH AND .024 INCH. (IT IS DIFFICULT FOR AN ACCURATE MEASUREMENT TO BE TAKEN WITHOUT DISASSESDR 98ZZZX4777Skin · crackedDURING A ROUTINE INSPECTION, THE TRAILING EDGE WING SKIN ON THE RIGHT WING WAS FOUND CRACKED IN SEVERAL PLACES. CRACKS WERE AT THE RIVET HOLES ALONG THE REAR MOST OF THE SKIN. SUBMITTER STATED THAT IMPROPER DEBURRING OF THE HOLES AND IMPROPER RIVET SPACING FSDR AU981528Alternator · failed(AUS) ALTERNATOR INTERNAL FAILURE. CIRCUIT BREAKER TRIPPED. BATTERY DRAINED.SDR 98ZZZX4594Nutplate · separatedA PRE-FLIGHT REVEALED ELEVATOR WAS NOT HITTING DOWN STOP. FURTHER INSPECTION REVEALED DOWN STOP BOLT WAS PUSHED IN. DISASSEMBLY REVEALED MS21078-3 NUTPLATE IS A TWO-PIECE PRESSED NUTPLATE THAT CAN BE DISLODGED WITH REPEATED HITTING. OTHER AIRCRAFT OF 172R T
Back to Cessna 172R