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 = '402B' 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 = '402B' 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 99ZZZX4215Rib · crackedDURING THE COURSE OF COMPLETING A 100-HOUR INSPECTION, A CRACK WAS DISCOVERED IN THE FORWARD PORTION OF RIB, CESSNA P/N 0822175-79. THE RIB HAD BEEN MODIFIED IAW CESSNA SK 414-8E APPROXIMATELY 4,303 HOURS AGO, WHICH, BY LOCATION, IS NOT ASSOCIATED WITH THE CRSDR 99ZZZX3845Filter · blockedIF CENTRAL INSTRUMENT AIR FILTER GETS WET, THE FILTER FIBERS EXPAND AND BLOCKS THE FLOW OF AIR TO VACUUM INSTRUMENT SYSTEM. THIS BLOCKAGE OF AIR FLOW RESULTED IN THE PILOT MAKING AN EMERGENCY LANDING IN LOW CEILINGS/IFR CONDITIONS DUE TO THE VACUUM INSTRUMENTSDR CA990907083Wire · broken(CAN) LEFT MAIN LANDING GEAR GREEN (DOWN AND LOCKED LIGHT AFTER LANDING GEAR SELECTED DOWN. EMERGENCY GEAR EXTENSION SYSTEM ACTIVATED WITH NO RESULTS. AFTER UNEVENTFUL LANDING, FAULT WAS TRACED TO A BROKEN WIRE AT THE LEFT GEAR DOWN AND LOCKED MICROSWITCH.SDR 99ZZZX2752Data Tag · loosePILOT REPORTED RIGHT ENGINE WOULD NOT PRIME. TROUBLESHOT AND FOUND RIGHT BOOST PUMP NOT PRODUCING ENOUGH PRESSURE. UPON OPENING THE FUEL TANK TO REPLACE PUMP, FOUND THE PUMP'S DATA TAG HAD COME UNGLUED AND WAS DIRECTLY UNDER THE PICK-UP TUBE. WHEN PUMP WAS SDR 99ZZZX2759Hub · crackedHUB CRACKED IN THREAD AREA ON PROPELLERSDR AU990509Crankshaft · cracked(AUS) RT ENGINE CRANKSHAFT CRACKED IN THE AREA OF THE COUNTERWEIGHT BUSHING. FOUND DURING ULTRASONIC INSPECTION IAW TCM CSB99-3A AND AD/CON/79.SDR AU990317Bearing · failed(AUS) ALTERNATOR BEARING FAILURE. ALTERNATOR DAMAGED BEYOND REPAIR.SDR CA990308022Spacer · missing(CAN) PILOT APPARENTLY HAVING A BRAKE PROBLEM AFTER LANDING. IT TURNED OUT THAT THE LEFT HAND GEAR LINKS OR SCISSORS HAD SEPARATED AS IF DISCONNECTED. THE OVERSIZE RETAINING WASHER WAS MISSING.SDR CA990310065Bellcrank · cracked(CAN) THE NOSE STEERING BELLCRANK WAS FOUND CRACKED/BROKEN BETWEEN ATTACH FLANGES. NO OTHER FAULTS FOUND DURING FLEET CHECK.SDR AU981671Actuator · seized(AUS) RIGHT ELEVATOR TRIM ACTUATOR SEIZED.SDR AU981676Switch · malfucnitioned(AUS) LANDING GEAR WOULD NOT RETRACT DUE TO A FAULTY 'SQUAT' MICROSWITCH.SDR 98ZZZX4487Circuit Breaker · failedAFTER TAKEOFF, THE LANDING GEAR WOULD NOT COME UP. REPLACED LANDING GEARA BREAKER, P/N S1235-515. OPS CHECK GOOD.SDR 98ZZZX4218Bellcrank · failedDURING A PHASE INSPECTION, DISCOVERED THE NOSE WHEEL STEERING BELLCRANK (P/N 5042010-1) HAD FAILED WITH THE LEFT HALF PULLED AFT BY THE STEERING CABLE. THE PILOT STATED THE RUDDER PEDALS WERE OFFSET DURING TAXI, BUT INLINE DURING FLIGHT. A FURTHER INSPECTION SDR AU981184Switch · failed(AUS) RIGHT MAIN LANDING GEAR DOWNLOCK MICROSWITCH FAULTY.SDR CA980928008Cylinder · failed(CAN) DURING CRUISE, THE NR 1 ENGINE BEGAN RUNNING ROUGH, AIRCRAFT RETURNED TO DEPARTURE POINT. POST-FLIGHT INSPECTION FOUND NO COMPRESSION ON NR 6 CYLINDER AND METAL WAS FOUND IN THE OIL FILTER. THE ENGINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICSDR 98ZZZX3806Pivot Pin · looseTHE PILOT STATED HE HEARD A FUNNY NOISE WHEN LANDING GEAR WAS RETRACTED. WHEN LANDING GEAR WAS EXTENDED TO LAND, DID NOT GET A SAFE INDICATION ON LT MAIN GEAR. UPON LANDING, ACFT SETTLED ON ITS GEAR, ROLLED SEVERAL FEET AND THE LT GEAR CAME OFF OF THE ACFT. SDR AU981000Harness · damaged(AUS) RT MAIN LANDING GEAR DOWNLOCK SWITCH WIRING LOOM FOULED IN GEAR LINKAGE DURING LANDING GEAR DOWN SELECTION CAUSING THE WIRING LOOM TO BE TORN OUT OF THE DOWNLOCK SWITCH.SDR AU980928Engine Cylinder · cracked(AUS) NR 2, NR 3, AND NR 5 CYLINDERS CRACKED BETWEEN TOP SPARK PLUG HOLE AND INJECTOR NOZZLE HOLE.SDR AU980927Crankcase · cracked(AUS) RIGHT ENGINE CRANKCASE CRACKED IN AREA OF NR 1 CYLINDER MOUNT PAD. CRACK LENGTH 50.8MM (2 INCHES).SDR 98ZZZX3037Stud · failedDURING 100-HOUR INSPECTION, MECHANIC NOTICED RIGHT ENGINE, NR 6 CYLINDER, PER MOST AFT AND THE LOWER TWO MOST AFT STUDS HAD BROKEN OFF FLUSH WITH THE CYLINDER BASE/SKIRT. THE CASE WAS INSPECTED FOR CRACKS, AND A CRACK APPROXIMATELY A .50 INCH LONG WAS OBSERVSDR 98ZZZX2982Line · chafedWHILE READING THE ACFT HOUR METER, A STRONG FUEL SMELL WAS NOTICED. A FUEL STAIN WAS NOTICED UNDER THE LEFT WING STARTING AT THE INBD ENGINE NACELLE AND SEEPING DOWN THE MAIN WING SPAR TO THE INBD MAIN GEAR DOOR. CROSS-FEED FUEL LINE HAD BEEN CHAFED AFT OF TSDR CA980811013Bearing · seized(CAN) WHILE TAXIING, THE PILOT FELT THAT THE A/C WANTED TO TURN RIGHT, HE STOPPED AND FOUND THE NOSE WHEEL FORK BROKEN DUE TO OVERHEAT AND WEAR CAUSED BY THE AXLE SPINNING INSTEAD OF THE BEARING TURNING. REPLACED.SDR 99ZZZX99Emergency Exit · separatedEMERGENCY EXIT WINDOW DEPARTED THE AIRCRAFT IN-FLIGHT FROM HOPE, ARK TO LITTLE ROCK, ARK. THIS WAS A CHARTER FLIGHT WITH ONE PILOT AND THREE PASSENGERS ON BOARD. THE AIRCRAFT LANDED AT LITTLE ROCK AIRPORT UNEVENTFULLY. THIS STYLE EMERGENCY EXIT WINDOW HAS SDR 99ZZZX680Hinge · crackedHINGE ATTACHMENT DOUBLER CRACKED FOR UPPER RADIUS CORNER FORWARD AND DOWN. CRACK LENGTH, APPROXIMATELY 1.25 INCHES.SDR AU980482Fuel Tank · leaking(AUS) LT WING FUEL TANK LEAKING. INVESTIGATION REVEALED A MOULDED-IN SPIGOT HAD TORN LOOSE FROM UNDER THE OUTER TANK OF THE RT AUXILIARY TANK SYSTEM. THE INNER TANK WAS INSPECTED AND WAS FOUND TO BE CLOSE TO A SIMILAR FAILURE - BOTH TANKS WERE MANUFACTURED ISDR 98ZZZX1994Crankcase Stud · brokenDURING THE COURSE OF A 100-HOUR INSPECTION, THE MECHANIC NOTICED THE LEFT ENGINE, NR 1 CYLINDER, MOST FORWARD UPPER STUD HAD BROKEN OFF FLUSH WITH THE CYLINDER BASE/SKIRT. THE CYLINDER WAS REMOVED AND THE CASE WAS INSPECTED FOR CRACKS AND ANY SIGNS OF CHAFINGSDR CA980430030Torque Tube · cracked(CAN) AFTER TAKEOFF, THE CONTROL TOWER INFORMED THE PILOT THAT THE LEFT MLG WAS DOWN. AIRCRAFT RETURNED TO BLOCKS. INVESTIGATION REVEALED THAT THE CROSS SHAFT WAS CRACKED AND DISTORTED. REPLACED.SDR 98ZZZX1996Crankcase Bolt · crackedDURING THE COURSE OF A 100-HOUR INSPECTION, THE MECHANIC NOTICED A SIZEABLE AMOUNT OF OIL ON THE TOP LEFT PORTION OF THE ENGINE CASE. A CLOSER INSPECTION REVEALED A CRACK APPROXIMATELY 1.6250 INCH LONG EMITTING FROM THE 9TH BACKBONE BOLT (COUNTING FROM FRONT SDR 98ZZZX1547Hub · crackedBLADE SOCKET NR 1 HAS AN EDDY CURRENT INDICATION IN EXCESS OF MANUFACTURER'S SPECS.SDR 98ZZZX1310Torque Tube · failedPILOT REPORTED RT MAIN GEAR WOULD NOT RETRACT. MECHANICS FOUND TORQUE TUBE 504501032 PEELED LIKE A PILLSBURY CAN OF BISCUITS.SDR 98ZZZX1334Actuator · looseDURING PRE-FLIGHT, PILOT FOUND THAT RUDDER TRIM WAS ABNORMAL. AFTER INVESTIGATION, THE (ACTUATOR SCREW HAD BEEN BENT AND CRACKED ON THE LAST TREAD) THE ACTUATOR SCREW BROKE DURING REMOVAL AND WAS SHIPPED AS A CORE. SUBMITTER STATED CAUSE OF FAILURE UNKNOWN, SDR 98ZZZX1174Bracket · failedPILOT SEAT BACK RECLINED IN-FLIGHT. BRACKET ON RIGHT SIDE OF SEAT BROKEN. CASTING APPEARS TO HAVE BEEN CRACKED PRIOR TO FAILURE.SDR 98ZZZX1012Rod Bearing · failedLEFT ENGINE SPUN NR 6 CYLINDER ROD BEARING ON TRIP BACK FROM NASSAU. ENGINE WAS OVERHAULED BY T.W. SMITH ENGINE. THE ENGINE HAD 1,313.9 HOURS SINCE OVERHAUL.SDR AU980056Fuel Cell · wrong size(AUS) NEW FUEL CELL IS INCORRECT SIZE. WHEN FITTED THE FUEL CELL HAS LARGE CREASES IN UPPER OUTBOARD FORWARD CORNER. FUEL CELL PNO 4142-3 REPLACES CELL PNO 4026102-3. CELL MANUFACTURED BY FFC MANUFACTURING MEMPHIS TENNESSEE USA. SERIAL NUMBER CR 1135. DATE OF SDR 98ZZZX1005Trunnion · crackedRETRACT ATTACH EAR CASTING BROKEN. SPACER P/N S133-4P32 AND BOLT P/N 464 P4-26 REPLACED WITH 1 'AN' 5 BOLT AND OVERTORQUED CAUSING UNDO STRESS TO CASTING.SDR 99ZZZX957Crankcase · crackedWHILE REPAIRING AN UNRELATED ITEM, THE MECHANIC NOTICED A CRACK APPROXIMATELY ONE INCH LONG (RUNNING TOP TO BOTTOM) ASSOCIATED WITH THE MOST FORWARD UPPER THROUGH-STUD ON THE NR 4 CYLINDER. THE CASE WAS INSPECTED IAW TCM SB M90-17 AND DETERMINED TO BE UNAIRWOSDR 98ZZZX556Skin · crackedCRACK IN UPPER WING SKIN ABOVE GEAR SUPPORT FOUND DURING 100-HOUR INSPECTION. SUBMITTER STATED POSSIBLY CAUSED BY A HARD LANDING.SDR AU971636Exhaust Pipe · cracked(AUS) RH ENGINE INBOARD EXHAUST HEADER PIPE CRACKED UNDER CLAMP ATFLANGE JOINT.SDR 98ZZZX2616Crankshaft · failedENGINE SHUT DOWN DURING FLIGHT FROM HOUSTON TO DALLAS. UPON TEAR DOWN, DISCOVERED THAT THE CRANKSHAFT HAD BROKEN. SUBMITTER STATED CAUSE IS UNKNOWN PENDING FURTHER INVESTIGATION.SDR 98ZZZX188Harness · shortedDURING THE COURSE OF NORMAL OPERATION, PILOT NOTICED LEFT ENGINE RUNNING ROUGH. AFTER LANDING, MAINTENANCE DETERMINED THE LEFT MAGNETO HARNESS, NR 5 CYLINDER, BOTTOM LEAD, HAD SHORTED INTERNALLY CAUSING THE SPARK PLUG TO NOT FUNCTION PROPERLY.SDR 98ZZZX351Bracket · brokenDURING A 100-HOUR INSPECTION, MECHANIC FOUND THE RIGHT TURBO MOUNTING BRACKET BROKEN. CESSNA BRACKET 0851139-3 HAD ITS OUTBOARD LOWER ATTACH LEG BROKEN OFF. UNABLE TO DETERMINE THE CAUSE OF THIS PROBLEM.SDR 98ZZZX347Doubler · crackedDURING A 100-HOUR INSPECTION, THE MECHANIC NOTICED A TEAR IN THE RIGHT SIDE OF THE NOSE GEAR WHEELWELL SKIN UNDER THE DOWNLOCK HINGE BRACKET (CESSNA BRACKET PART 0842105-2). THE DOUBLER THAT ATTACHES TO THE SKIN/BRACKET ASSEMBLY (DOUBLER CESSNA PART 5213045-2SDR 98ZZZX637Terminal Board · shortedDURING ROUTINE MAINTENANCE, CHANGING RIGHT COWL FLAP CABLE, THE HEATER'S FUEL LINE CONTACTED THE NON-INSULATED TERMINAL BOARD'S STUD AT RIGHT WING STA 27.125. PLACING MASTER SWITCH IN ON POSITION PROVIDED A SHORT CIRCUIT AND FIRE. THE TERMINAL BOARD'S STUDS SDR AU971457Fork · failed(AUS) NOSE LANDING GEAR FORK END FITTINGS CRACKED. NLG FAILED TO LOCK DOWN.SDR 97ZZZX4636Cylinder · crackedDURING FLIGHT FROM EWR TO PWM, THE PILOT EXPERIENCED THE LEFT ENGINE FAILURE. ENGINE WAS SHUT DOWN. FOUND NR 6 CYLINDER CRACKED AT CYLINDER BASE CAUSING COMPLETE FAILURE. ENGINE COMPLETELY DISASSEMBLED AND INSPECTED.SDR 97ZZZX4579Cylinder · separationDURING NORMAL FLIGHT, PILOT NOTICED LEFT ENGINE RUNNING ROUGH AND RETURNED TO POINT OF DEPARTURE. DETERMINED THE NR 1 CYLINDER ON THE LEFT ENGINE HAD SEPARATED THE HEAD FROM THE BARREL. SUBMITTER SUGGESTED FROM PAST EXPERIENCE, THIS IS TYPICAL OF A TCM TSIO5SDR 97ZZZX4447Skin · crackedMID-WAY BETWEEN FORWARD AND AFT SPAR UNDER NACELLE SKIN INBOARD OF NACELLE AUXILIARY FUEL TANK FOUND CRACKS IN WING SKIN. WOULD NOT HAVE BEEN FOUND UNLESS SKIN OVER WING LOCKER AND AUXILIARY FUEL TANK WAS REMOVED FOR REPAIR. NO ACCESS.SDR 97ZZZX4264Bulkhead · crackedFOUND BULKHEAD CRACKED. SUBMITTER STATED MOST LIKELY FROM FATIGUE. CRACK STARTED IN COMPOUND BEND AND HAD NOT YET MADE IT TO THE EDGE. SUBMITTER STATED THE BULKHEAD IS MADE OF TOO LIGHT OF MATERIAL AND SUGGESTS CESSNA MAKE A REPLACEMENT BULKHEAD OUT OF HEAVSDR AU971387Bellcrank · cracked(AUS) RH MAIN LANDING GEAR DOOR IDLER BELLCRANK BROKEN. FURTHER INVESTIGATION FOUND THE LH IDLER BELLCRANK CRACKED IN THE SAMEAREA.SDR 97ZZZX4211Bellcrank · failedRIGHT MAIN GEAR DOOR DID NOT CLOSE WHEN GEAR SELECTED UP. FOUND BELLCRANK P/N 0841106-6 CRACKED INTO TWO PIECES. SUSPECT FATIGUE CAUSED THE FAILURE.
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