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 = '172P' 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 = '172P' 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 CA020411005Bulkhead · cracked(CAN) SECOND PART FAILURE IN THE SAME AREA HEARD REPORTS OF THIS PART FAILING FROM OTHER OPERATORS. SPINNER AND AFT BULKHEAD HAVE A VERY POOR FIT.SDR CA020422003Bolt · sheared(CAN) WHILE ATTEMPTING TO REMOVE THE LT MLG LEG TO FACILITATE A REPAIR TO AN ADJACENT AREA, IT WAS DETERMINED THAT THE MAIN ATTACH BOLT WAS SOMEHOW SEPARATED AS INSTALLED THROUGH THE INBOARD SUPPORT AND THE GEAR LEG. EVENTUAL REMOVAL OF THE BOLT REVEALED THAT SDR 2002FA0000324Transmitter · deterioratedFUEL QUANTITY TRANSMITTER REMOVED TO REPLACE LEAKING BASE GASKET. FOUND COMPOSITE FLOAT ON TRANSMITTER ARM WAS DETERIORATED DUE TO CONTACT WITH THE TOP OF FUEL TANK WHEN FULL. APPROXIMATELY 1/4 INCH OF FLOAT DETERIORATED ON ONE CORNER. SUBSEQUENTLY FOUND FISDR CA020116004Spar · cracked(CAN) CRACK WAS FOUND DURING A SCHEDULED INSPECTION OF THE AIRCRAFT, IN THE AREA OF THE FRONT SPAR OF THE STABILIZER. AT THE LIGHTENING HOLE BETWEEN THE TWO NOSE RIBS.SDR CA011212002Cylinder · cracked(CAN) DURING A REGULAR MAINTENANCE INSPECTION THE CYLINDERS WERE VISUALLY CHECKED USING A BORESCOPE, CRACKS WERE NOTED AT THE SPARK PLUGS PORTS OF NR 1 & 2 CYLINDERS. ALL CYLINDERS WERE REMOVED AND REPLACED.SDR CA020108002Cylinder · cracked(CAN) DURING CLIMB THE PILOT NOTICE A LOSS OF POWER AND ENGINE VIBRATION. RETURNED TO BASE. MAINTENANCE FOUND NR 3 CYLINDER CRACKED AT THE EXHAUST VALVE. THIS IS THE 3RD CYLINDER ON 2 DIFFERENT ENGINES TO CRACK IN THIS PLACE. ALL CYLINDERS REMOVED AND RETURSDR CA011127002Magneto · failed(CAN) ON LANDING ROLL PILOTS REPORTED A GRINDING NOISE FROM THE ENGINE. - THEY TAXIED OFF THE RUNWAY AND SHUT DOWN. AIRCRAFT PUSHED TO HANGAR.- INITIAL INVESTIGATION SHOWED DEAD LT MAGNETO (TIMING INDICATOR). - MAGNETO REMOVED, SHAFT BENT AND GEAR GROUND BY ENSDR 2001FA0000373Rod · failedACTUATION ROD TO RUDDER PEDAL BROKE AT BASE OF THREADS AT FORK. THERE WAS NO DAMAGE TO RUDDER PEDAL OR BRAKE MOUNT FOUND.SDR CA020411006Bulkhead · cracked(CAN) AFT SPINNER BULKHEAD CRACKED AT RADIUS OF PROP CUT OUT.SDR JGV2001F00000Line · chafedAIRCRAFT ARRIVED FOR INSPECTION WITH STRONG FUEL ODOR IN CABIN AND FUEL LEAKING FROM BELLY SKIN SEAM. FOUND AFT CABIN CARPET SOAKED WITH FUEL. REMOVED TRIM FROM RIGHT AFT DOOR PEST AREA, FOUND THAT AILERON CABLE HAD BEEN CHAFING ON THE FUEL LINE IN THIS AREASDR 20010606CW001Yoke · corrodedWHILE PERFORMING ANNUAL INSPECTION AND SB, FOUND ELEVATOR CONTROL YOKE CONTAINED RUSTY WATER, CAUSING EXCESSIVE CORROSION. IF THIS PART FAILS COMPLETE LOSS OF ELEVATOR CONTROL RESULTS. SB PERMITS DRILLING HOLE FOR RECURRING INSPECTION. SUGGEST SB SEB-01-3 BSDR CA010508010Bracket · loose(CAN) MOUNTING BRACKET FOR PORTABLE ELT ANTENNA HAS LOOSE FIT AND ALLOWS ANTENNA TO FALL OUT. MS 28775-009 O-RING USED TO RETAIN ANTENNA.SDR 20010419CW001Yoke · corrodedMAINTENANCE TECH FOUND AREA BELOW PIVET BOLT EXCESSIVELY COVERED TO THE POINT OF EXFOLIATION. WHEN DRILLING THE INSPECTION HOLE CALLED FOR, THE DRILL BIT ACTUALLY FELL THROUGH AFTER APPROXIMATELY 2 TURNS OF THE BIT. CENTRAL YOKE WAS REPLACED AT THIS TIME. TSDR CA010223014Bulkhead · cracked(CAN) DURING CESSNA PHASED INSP, BULKHEAD, STATION 108, FOUND CRACKED IN 3 PLACES AT RADIUS OF EACH CORNER EXCEPT FOR TOP LEFT. BULKHEAD FORMS BACK OF BAGAGE COMPT AREA. CRACKS RADIATE FROMTHE FLANGE OF BULKHEAD & EXTEND INTO WEB OF BULKHEAD. CHECK OF REST OFSDR CA010212006Bulkhead · cracked(CAN) DURING ROUTINE CESSNA PROGRESSIVE CARE INSPECTION, THE BULKHEAD AT THE BACK END OF THE BAGGAGE COMPARTMENT STATION 108 WAS FOUND TO BE CRACKED AT BOTH LOWER CORNERS, AND THE UPPER RIGHT CORNER. THE CRACKS ARE APPROXIMATELY 2 INCHES LONG. THIS AIRCRAFT ISSDR 20001208SH011Bracket · chafedDURING INSPECTION, FOUND THE LEFT FLAP, INBOARD HINGE FLAP SUPPORT ARMS WERE GROOVED DUE TO CHAFING BY THE AFT BEARING. THIS CONDITION IS USUALLY RELATED TO THE FORWARD BEARING CHAFING. BOTH INBOARD HINGE FLAP SUPPORT ARMS WERE CHANGED WITH NEW. SEB 95-3 ADSDR 20001207SH007Carburetor · crackedFOUND CRACKS IN FLOAT BOWL ON LOWER THROUGH-BOLT BOSS. APPEARED TO BE A FORGING PROBLEM. (X)SDR CA001201017Handle · separated(CAN) FUEL SELECTOR WAS BEING TESTED DURING TAXI WHEN FUEL SELECTOR HANDLE BECAME DISENGAGED FROM FUEL SELECTOR WHEN HANDLE WAS BETWEEN TANK POSITIONS. INVESTIGATION FOUND THE COTTER PIN THAT HOLDS THE SHAFT ASSEMBLY IN THE FUEL SELECTOR BROKEN ALLOWING THE SHSDR 20001207SH005Regulator · failedALTERNATOR CONTROL UNIT FAILED INTERNALLY EMITTING SMOKE ODOR. REPLACED ACU AND INSPECTED CHARGING SYSTEM FOR OPERATION IAW CESSNA MM. (NO DEFECTS NOTED). (X)SDR 20001012SH029Firewall · crackedFIREWALL CRACKS WHERE ENGINE COWLING SHOCK MOUNTS ARE ATTACHED TO THE LOWER FIREWALL AND FIREWALL REINFORCEMENTS. CRACKS APPEAR TO BE DUE TO THE AGE OF THE AIRCRAFT. AIRCRAFT TT, 12,705 HOURS. REPAIRS WERE MADE IAW CESSNA STRUCTURAL REPAIR MANUAL. THIS IS SDR AU000700Rotor · broken(AUS) RIGHT MAGNETO ROTOR SHAFT SHEARED. (X)SDR 20000802SH030Throttle Cable · inaccurateOWNER REQUESTED THROTTLE CABLE BE CHANGED DUE TO CABLE CREEPING. WHEN CABLE WAS COMPARED TO ORIGINAL CABLE, NEW CABLE WAS FOUND TO HAVE MANY DIFFERENCES: LENGTH WAS LONGER; FIREWALL SLEEVE IN DIFFERENT LOCATION; LARGER DIAMETER; ENGINE MOUNT ATTACHMENT COMPLSDR CA000828009Shaft · loose(CAN) IDLER GEAR SHAFT FOUND LOOSE IN ENGINE CASE ALLOWING IDLER GEAR TO CONTACT CASE CAUSING METAL CONTAMINATION.SDR CA000427005Plug · backed out(CAN) EXPANSION PLUG AT FRONT OF CRANKSHAFT HAD COME LOOSE ALLOWING OIL TO LEAK OUT.SDR CA000404021Switch · loose(CAN) DURING THE RUN-UP, THE PILOT NOTICED SMOKE COMING FROM BEHIND THE INSTRUMENT PANEL. THE AIRCRAFT WAS TAXIED BACK TO THE RAMP AND SHUT DOWN. MAINTENANCE FOUND A LOOSE/OVERHEATED CONNECTOR ON THE BACK OF THE LANDING LIGHT SWITCH.SDR CA000606014Cylinder · failed(CAN) AIRCRAFT IN-FLIGHT, OVER LETHBRIDGE CLIMB-OUT. BIG BANG, NR 2 CYLINDER EXITED LEFT COWL, OIL ALL OVER. PILOT LANDED AIRCRAFT AT LETHBRIDGE. ENGINE MADE ENOUGH POWER TO GET AIRCRAFT TO AIRPORT. CYLINDER NOT FOUND. SMALL PART OF PISTON, RINGS, HYDRAULSDR AU000093Cylinder · cracked(AUS) NR 4 CYLINDER CRACKED FROM LOWER SPARK PLUG HOLE TO EXHAUST PORT.SDR AU000037Skin · corroded(AUS) FUSELAGE SKIN CORRODED ON RIGHT SIDE WALL BENEATH SOUND DEADENING PATCH.SDR CA991112014Rivets · sheared(CAN) AFTER REMOVAL OF FUEL TANK, TWO RIVETS WERE FOUND SHEARED ON THE FRONT SPAR. THE RIVETS WERE LOCATED AT THE SPAR ANGLE (PN 0523017-14) AND THE INBOARD RIB (PN 0523010-14).SDR 99ZZZX3650Hose · crackingAIRCRAFT BEGAN TO LOSE VACUUM ON THE INSTRUMENT AIR SYS. FOUND A POSSIBLE LINE CRACKED ON THE OUTSIDE FROM AGE. AFTER REMOVING THAT LINE AND OTHER LINES ALSO CONNECTED TO THE INSTRUMENTS, DISCOVERED NOT ONLY THE OUTSIDE OF THE LINE WAS CRACKED, BUT THE INSIDSDR 99ZZZX3625Follower · brokeSTUDENT PILOT FLYING, HAD ENGINE QUIT WHILE DOING TOUCH AND GOES. A TEST RUN OF THE ENGINE AFTER RECOVERY REVEALED THE ENG WOULD MAKE 1,850 RPM'S WHEN LEANED OUT. INVESTIGATIVE DISASSEMBLY REVEALED THE NR 1 INTAKE VALVE STUCK OPEN APPROX .3750 INCH. THE VALSDR 99ZZZX4040Hose · crackedCOMPLETE VACUUM SYSTEM FAILURE, BOTH NORMAL SYSTEM AND STANDBY SYSTEM. THE FAILURE WAS CAUSED BY DETERIORATION OF VACUUM HOSES. HOSES TO THE ATTITUDE INDICATOR AND DIRECTIONAL GYRO WERE SO BRITTLE THAT BENDING THE NOSE WOULD RESULT IN COMPLETE BREAK-UP, AND SDR 99ZZZX3411Frame · crackedDURING ANNUAL INSPECTION, FOUND BOTH REAR DOOR FRAME STRUCTURES CRACKED.SDR 99ZZZX3164Oil Drain · failedDURING 11-HOUR INSPECTION, OIL DRAIN VALVE CAME APART WHILE CLOSING IT AFTER OIL DRAINING.SDR 99ZZZX2649Line · failedOIL PRESSURE LINE FROM ENGINE TO THE FITTING ON THE AFT BAFFLE BROKE OFF AT THE FLARE. CONSEQUENTLY, LOST OIL PRESSURE AND ALL BUT ONE-HALF QUART OF ENGINE OIL. AFTER SAFE LANDING, OIL FILTER WAS CUT OPEN BY MECHANIC AND FOUND METAL CONTAMINATION. ENGINE DESDR 99ZZZX2428Fuel Tank · contaminatedACFT MADE 4 FORCED LANDINGS INCLUDING 1 OFF-AIRPORT, NO DAMAGE. LANDINGS DUE TO ENG STOPPAGE. CARB ICE SUSPECTED AS ENG WOULD FIRE UP ON THE GROUND. AFTER OFF-AIRPORT LANDING, ACFT TAXIED FOR TAKEOFF WHEN ENG QUIT. WINGS WERE SUMPED AND APPROX 20 OUNCES OSDR 99ZZZX2389Carburetor · malfunctionedENGINE WOULD NOT SHUT OFF WITH MIXTURE CONTROL. FOUND CARBURETOR BOWL LOOSE, BUT MOUNTING BOLTS STILL HAD LOCK TABS IN PLACE. BOLTS APPEARED TO BE LOOSE IN THREADS IN BOWL. NEED TO HAVE A LOOK AT PAM MANUFACTURING PROCEDURES.SDR AU990498Bulkhead · cracked(AUS) AFT LOWER DOORPOST BULKHEAD CRACKED ON BOTH SIDES. CRACK LENGTH 19.05 MM (0.75 INCH).SDR 99ZZZX2123Camshaft · wornCAM LOBE WORN OUT CAUSING INTAKE VALVES ON NR 1 AND NR 2 CYLINDERS TO NOT FULLY OPEN. SYMPTOMS WERE LOW TAKEOFF POWER (2,000 RPM) AND WOULD NOT IDLE.SDR AU990418Wire · broken(AUS) ENGINE OIL TEMPERATURE PROBE RESISTOR WIRE BROKEN.SDR AU990359Vacuum Pump · removed(AUS) ENGINE RAN OUT OF OIL. VACUUM PUMP HAD BEEN REMOVED FOR REPLACEMENT AND PILOT TOOK THE AIRCRAFT WITHOUT EITHER THE NEW VACUUM PUMP OR A COVER PLATE FITTED. THE ENGINE CONSEQUENTLY RAN OUT OF OIL.SDR 99ZZZX1946Line · misinstalledTHE MAIN FUEL SUPPLY LINE WAS IMPROPERLY INSTALLED. THE RUDDER CONTROL CABLE WAS ROUTED BENEATH THE FUEL LINE IN SUCH A WAY TO BE RUBBING DIRECTLY ON THE LINE. WHEN DISCOVERED, THE LINE WAS CUT MORE THAN HALFWAY THROUGH, BUT ONLY SLIGHTLY LEAKING.SDR 99ZZZX1395Propeller · crackedPROPELLER REMOVED FOR OVERHAUL. FOUND TO BE CRACKED.SDR 99ZZZX1022Bracket · elongatedCONTROL YOKE PIVOT BOLT HAS ELONGATED BOLT HOLES IN RT BRACKET ASSY CAUSING EXCESSIVE FORE AND AFT PLAY IN CONTROL YOKE 1 INCH OF TRAVEL. PROBLEM FOUND DURING ANNUAL INSPECTION. TACHOMETER TIME: 4,326.0 HOURS. HOBBS: 6,193.0. 1982 CESSNA 172-P.SDR 99ZZZX1015Bulkhead · crackedDURING ROUTINE 100-HOUR INSPECTION, LEFT HAND FORWARD DOOR POST BULKHEAD WAS FOUND CRACKED. CRACK IS APPROXIMATELY .50 INCH IN LENGTH AROUND AFT ATTACH BOLT FOR LOWER DOOR HINGE. SUBMITTER STATED 5 FOUND IN LAST 3 MONTHS. ALL AIRCRAFT ARE USED IN TRAINING/RSDR 99ZZZX74Hub · crackedPROPELLER WAS REMOVED FROM AIRCRAFT AND INSTALLED ON ANOTHER AIRCRAFT FOR FERRY FLIGHT. WHEN PROPELLER WAS REMOVED FROM AIRCRAFT AFTER FERRY FLIGHT, CRACK WAS FOUND IN HUB.SDR CA990111001Stud · broken(CAN) DURING TAXI, A VIBRATION WAS FELT FROM THE ENGINE. INSPECTION AFTER RETURN TO RAMP FOUND ONE .50 INCH STUD AND THREE .3750 STUDS AT NR 1 CYLINDER BROKEN. ALL CYLINDERS WERE REMOVED AND INSPECTED FOR CRACKS AND CONFORMITY. ALL CYLINDERS WERE SERVICEABLSDR AU981633Nut · loose(AUS) ENGINE THERMOSTATIC VALVE (VERNATHERM) WAS REMOVED TO DETERMINE PART NUMBER WAS COMPLIANT WITH AD/LYC/78A5. IT WAS FOUND THAT THE VALVE'S P/N 53E22144 WAS NOT APPLICABLE, BUT THE VALVE STILL FAILED THE INSPECTION CRITERIA - LOOSE RETAINING NUT. NOTE: SDR CA981125053Cover · missing(CAN) AIRCRAFT HAS AN RFI 70 FIRE WALL MOUNTED RADIO NOISE FILTER. THE COVER OVER THE TERMINALS WAS MISSING. CAR WARMER MOUNTED ON AFT LEFT SIDE OF ENGINE MOUNT, THE CORD WAS ROUTED UP TO OIL FILLER DOOR ON TOP OF RIGHT SIDE. THE TYE WRAP BROKE ON THE PLUG SDR CA981202017Woodruff Key · worn(CAN) THE WOODRUFF KEY FOUND WORN CAUSING A TIMING PROBLEM WITH THE LEFT MAGNETO.
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