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 = '550' 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 = '550' 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 2002FA0000445Seat · crackedUPPER CHAIR BASE ASSY CRACKED AT CHAIR BACK ATTACH POINTS. (PHOTOS) STRESS ON CHAIR BACK AND METAL FATIQUE PROBABLE CAUSE. CHAIR WAS REPAIRED.SDR 2002FA0000381Motor · misoverhauledNR 1 ACM BLOWER MOTOR WAS REPLACED WITH A FRESH OVERHAULED UNIT. THE OVERHAULED BLOWER MOTOR FLEW 9.1 HOURS BEFORE FAILING. WHILE PREPARING TO REPLACE UNIT, IT WAS DISCOVERED THAT THERE HAD BEEN SEVERE ELECTRICAL ARCING TAKING PLACE, AFTER INITIAL INSTALLATIONSDR SIIA004KAccess Door · missingRIGHT ENGINE OIL ACCESS DOOR DISCOVERED MISSING ON POST-FLIGHT INSPECTION. IN-FLIGHT SEPARATION PROBABLY OCCURRED APPROXIMATELY 2.5 HOURS INTO FLIGHT WHEN CREW NOTICED SLIGHT VIBRATION. WHEN QUERIED, CESSNA REPORTS PROBLEMS WITH SEPARATIONS OF THESE ENGINE OSDR CA020313004Diode · missing(CAN) HYDRAULIC POWER STAYED ON WHEN GEAR WAS SELECTED DOWN. FOUND WHEN CESSNA HAD INSTALLED SB 550-32-40 REV.3. THEY DID NOT INSTALL DIODE CAUSING POWER FEEDBACK AND HYDRAULIC CENTRE VALVE STAYING CLOSED.SDR EWO2002F00000Sprocket · brokenDURING PHASE 1 INSPECTION, FLAP MOTOR OPERATIONAL TEST, THE LEFT MOTOR WOULD NOT DRIVE FLAPS. THE FLAP DRIVE WAS INSPECTED AND LEFT SPROCKET WAS FOUND BROKEN IN TWO. THIS CAUSED MOTOR TO BE INEFFECTIVE. NO BINDING OF FLAPS WAS FOUND. THE SPROCKET WAS REPLASDR CA020220008Motor · loose(CAN) THE SUBJECT LT MOTOR WILL MOVE TO ITS EXTREME END TRAVEL AND LOCK THE ARMATURE CAUSING THE C.B. TO POP AND THE FLAP SYSTEM TO STOP. WHEN THE CB WAS RESET THE FLAPS WOULD OPERATE NORMALLY, THIS HAPPENED TWICE DURING FLAP SELECTION AND WAS SNAGGED IN THE LSDR B3OR20020003Stator · crackedACFT WAS INDUCTED INTO A 1 & 2 AND 5 A&B INSPECTION. DURING INSPECTION DISCOVERED THE LT MLG BRAKE ASSY HAD A CRACK IN ONE OF THE STATOR DISCS. BRAKE ASSY WAS RECEIVED FROM OUR PARTS DEPT HAD ABNORMAL WEAR ON THE WEAR PLATES & LININGS. BRAKE ASSY WAS REPAIRSDR B3OR20020004Combustion Liner · failedAIRCRAFT WAS INDUCTED INTO A PHASE 1,2, 5A & B INSPECTION. DURING THE INSPECTION THE ENGINE IGNITERS WERE TO BE REMOVED. WHILE REMOVING THE IGNITERS OF THE NR 2 ENGINE, THE OUTBOARD IGNITER BECAME STUCK ON THE FLOATING WASHER IN THE COMBUSTION LINER. THE IGNITSDR B3OR20020005Duct · crackedAIRCRAFT WAS INDUCTED INTO A PHASE1,2,5A & B INSPECTION.DURING THE INSPECTION OF THE NUMBER 2 ENGINE, THE FRONT BY-PASS DUCT WAS FOUND CRACKED AND A PIECE MISSING FROM IT. THE DUCT WAS REMOVED AND REPLACED WITH A SERVICEABLE DUCT.SDR B3OR20020002Drain Valve · crackedDURING A PHASE 1 & 2 INSPECTION, THE ENGINES WERE DE-COWLED FOR THE OIL FILTER CLEANING ITEM. A MECHANIC NOTICED SOME FUEL RESIDUE AROUND THE FUEL DRAIN "EPA" CAN. UPON INSPECTION THE CAN WAS FOUND TO HAVE A MOUNTING BRACKET BROKEN OFF OF IT. THE BREAK WAS WHESDR M672002F00000Line · chafedDURING A ROUTINE INSPECTION. FOUND THAT THE LEFT SPEEDBRAKE RETRACT LINE HAD BEEN CHAFED NEARLY ALL THE WAY THRU BY THE CENTER FLAP BELLCRANK ROD ATTACH BOLT. RECOMMEND CLOSE INSPECTION OF TUBING FOR PROPER CLEARANCE.SDR GVR2003F00000Structure · crackedUPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. PREVIOUS IN APPROPRIATE REPAIR MADE. CHAIR WAS REPAIRED IAW STC ST01042WI STRUCTURAL SEAT REPAIR.SDR B3OR20020001Switch · stuckA GROUND RUN WAS PERFORMED ON THE AIRCRAFT PRIOR TO A SCHEDULED LAUNCH.UPON ENGINE SHUTDOWN THE MECHANIC NOTICED THAT THE "HYDRAULIC PRESSURE LOW" LIGHT ON THE RIGHT HAND ENGINE DID NOT ILLUMINATE.DURING TROUBLE-SHOOTING, IT WAS DICOVERED THAT THE RIGHT HAND HSDR AUS20020019Line · ruptured(AUS) ENGINE HEAT EXCHANGER FUEL TUBE LEAKING. FUEL SPRAYING INSIDE COWLS AND ENTERING ENGINE THROUGH INTAKE.SDR 2002FA0000171Line · chafedREPORTED HYDRAULIC LEAK INSPECTED AND FOUND TO BE SPEED BRAKE RETRACT LINE. LINE HAS BEEN CHAFFED THROUGH BY CENTER FLAP BELLCRANK PUSH ROD ATTACH HARDWARE. FABRICATED REPLACEMENT LINE AND MADE APPROPRIATED BENDS TO CLEAR OFFENDING AREA OF FLAP BELLCRANK.SDR 2002TU65Actuator · damagedON PREINSTALLATION INSPECTION, THE MECHANIC NOTICED DAMAGE IN THE ATTACH THREADS ON THE ACTUATOR. THE BOLT WOULD NOT THREAD IN EVEN ONE TURN WITH OUT BINDING. AFTER FURTHER INVESTIGATING IT WAS FOUND TO HAVE PART OF A BROKEN BOLT STILL INSIDE THE HOUSING.THISDR CA020102002Stator · broken(CAN) DISASSEMBLED BRAKE UNIT AND FOUND STATOR DISC P/N 133-89302 CHG "B" BROKEN. (SEE ATTACHED PHOTO'S).SDR 2001F00730Bearing · frozenAFT ELEVATOR BELLCRANK BEARING DW6 FROZE CAUSING BELLCRANK MOUNTING BOLT TO ROTATE AND ENLARGE MOUNTING HOLES IN BELLCRANK SUPPORT ASSEMBLY BRACKETS 565344-17 AND 5565344-18.SDR BLI2001F00008Pump · inoperativeABORTED START; NO OIL PRESSURE OR TURBINE SPEED INDICATION. REMOVED ACCESSORY GEARBOX AND SENT TO MFG. THE ABOVE ENGINE EXPERIENCED PROBLEMS IN THE FIELD THAT RESULTED IN THE ACCESSORY GEARBOX ASSEMBLY AND THE OIL PUMP TO BE SENT TO MFG FOR REPAIRS.SDR BLIA512C11250Gearbox · failedABORTED START; NO OIL PRESSURE OR TURBINE SPEED INDICATION. REMOVED ACCESSORY GEARBOX AND SENT TO MFG. UPON RECEIPT, IT WAS EVIDENT THE THE SHAFT HAD SHEARED. THIS WAS APPARENTLY CAUSED BY AN ELEMENT IN THE OIL PUMP ASSEMBLY, INSTALLED NEW AT OVERHAUL, BEISDR 2001FA0000512Controller · misrepairedUPON INSTALLATION OF A REPAIRED CABIN PRESSURE RATE CONTROLLER IT WAS FOUND THAT THE AC WOULD NOT TEST OR PRESSURIZE ON THE GROUND. AFTER CHECKING THE ATTACHING SYSTEMS THE CANNON PLUG ON THE CONTROLLER WAS DISCONNECTED AND INSPECTED. AT INSPECTION IT WAS FOSDR 2001FA0000532Dipstick · brokenFAILURE OF OIL DIPSTICK AT ATTACHMENT LOCK NUT CAUSING LOSS OF OIL AND LOWER THAN NORMAL OIL PRESSURE.SDR BLI2001F00005Exciter · failedLEFT ENGINE FAILED TO START. CALLED DIRECTOR OF MAINTENANCE, ARRIVED TO REPAIR AIRCRAFT. REPLACED BOTH IGNITERS BUT FAILED TO START. REPLACED IGNITER EXCITER. STARTS NORMAL. AIRCRAFT RETURNED TO NORMAL.SDR AUS20011114Pin · worn(AUS) ELEVATOR TRIM INDICATOR SKIPPED GROOVES ON TRIM WHEEL GIVINGINCORRECT TRIM POSITION INDICATION. BOTH WHEEL FUSE PLUGS BLEWDUE TO EXCESSIVE BRAKING.SDR AUS20011108Spar Cap · debonded(AUS) LT AND RT WING SPAR CAPS DEBONDED AND CORRODED. FOUND DURING ULTRASONIC INSPECTION IAW JWP/2531/01 AND JWP/2503/01.SDR 2001FA0000397Stringer · damagedDURING AN AVIONICS INSTALLATION EVENT WITH THE AIRCRAFTS' INTERIOR REMOVED IT WAS NOTED THAT THE FUSELAGES' UPPER CROWN SKIN, ABOUT THE CENTERLINE HAD BEEN PREVIOUSLY MODIFIED AT ONE TIME TO "BLANK OUT" A ANTENNA INSTALLATION NO LONGER IN USE. EXTREMELY POOR WSDR CA011018021Wire Harness · chafed(CAN) LARGE WIRE BUNDLE TOO CLOSE TO VENT BLOWER MOTOR.SDR B3OR20010009Bearing · corrodedTHE ELEVATOR WAS REMOVED TO FACILLITATE OTHER MAINTENANCE. UPON REMOVAL OF THE RIGHT HAND ELEVATOR, THE INBOARD ELEVATOR BEARING, INNER RACE CAME OFF WITH THE INBOARD MOUNT BOLT. DURING THE REMOVAL OF THE ELEVATOR, THE BALL BEARINGS FELL OUT OF THE OUTER RACE.SDR CA011018018Manifold · cracked(CAN) SEVERAL CRACKS (SEVEN) FOUND AROUND RING WHERE RADIUS MEETS TUBE.SDR CA011018020Skin · cracked(CAN) DURING SCHEDULED MAINTENANCE CESSNA 550 PHASE "5" AND PHASE "49" INSPECTIONS, OF THE R/H F.S. 287.78 SKIN SEAM, A 1.5" LONG CRACK WAS FOUND CENTERED ABOUT 115.25 (W.L.). - CESSNA INFORMATION: THIS HAVE OCCUR ON SOME AIRCRAFT, FOLLOWING REPAINTING. - OUR SDR CA011018016Rivet · loose(CAN) AIRCRAFT DOWN FOR PHASE 5 INSPECTION. L/H ENGINE - 2 RIVET IN THE 5 O'CLOCK POSITION AND 3 RIVETS AT 7 O'CLOCK POSITION HAD THE HEADS PULLED 1/3 TO 2/3 AROUND THE SHANK DIAMETER.R/H ENGINE 5 TO 6 RIVETS IN THE 3 TO 6 O'CLOCK POSITION HAD THE HEADS PULLEDSDR AUS20011045Skin · corroded(AUS) RH WING SKIN SPLICE CORRODED. SUBSEQUENT INVESTIGATION REVEALED EXTENSIVE DEBONDING. ULTRASONIC INSPECTION OF LH WING FOUND SIMILAR RESULTS.SDR AUS20010964Splice · corroded(AUS) RH WING SKIN SPLICE CORRODED. AREAS OF SPLICE ASSEMBLY DISBONDED.SDR 2001FA0000400Stator · brokenFOLLOWING A NORMAL LANDING AND ROLL OUT FOR A RIGHT TURN ON TO THE TAXI WAY THE RIGHT MAIN WHEEL LOCKED UP. AFTER JACKING THE MAIN WHEEL AND PULLING THE TIRE, A PIECE OF STATOR WAS FOUND COMPLETE BROKEN OUT OF THE STATOR CAUSING THE WHEEL TO LOCK. THIS BRAKESDR 2001F00501Engine · failedAPPARENT CATASTROPHIC FAILURE OF ENGINE WHILE ON DESCENT TO LAND RESULTING IN ENGINE SHUTDOWN. (M)SDR 0121Seal · damagedAIRCRAFT WAS FLYING AT FL39, HEARD AN AIR NOISE NEAR THE CABIN DOOR. STARTED TO LOOSE PRESSURIZATION. DECLARED AN EMERGENCY AND DESCENDED TO A SAFE ALTITUDE. DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. MX DETERMINED THE CABIN DOOR SEAL WAS BAD AND REPLACESDR AMB20011Tire · failedDURING A DAILY INSPECTION THE SIDE WALL WAS FOUND TORN OUT WHERE THE SIDE WALL AND TIRE TRED ARE BONDED TOGOTHER. THERE IS ANOTHER AREA APROX. 6 INCHES AWAY FROM THIS TEAR, WHERE YOU CAN SEE THAT THE RUBBER IS ALSO STARTING TO SEPERATE. THE INNER AREA OF THE TSDR CA010814021Squat Switch · worn(CAN) WHILE IN DESCENT FROM FL330, AND DESCENDING THROUGH 15,000 FT CABIN ALTITUDE STARTED TO INCREASE RAPIDLY. AIRCRAFT DIVERTED TO CYQM FOR MAINTENANCE. WHILE AT 10,000 FT CABIN ALTITUDE RECOVERED. WHEN THROTTLES REDUCED FROM 88 TO 70 PERCENT N1, CABIN PRESSDR 0119Squat Switch · out of adjAIRCRAFT WAS FLYING AT 37,000 FT WHEN THE PILOTS HEARD A LOUD HISS. CABIN STARTED TO CLIMB 6000 FT/MIN. THE PILOTS DECLARED AN EMERGENCY AND DESCENDED, LANDED IN WILLIAMSPORT PA WITH NO FURTHER INCIDENT. THE CAUSE OF THE PROBLEM WAS THE LT SQUAT SWITCH WAS SDR B3OR20010007Harness · deterioratedDUR HI-PWR ENG RUN, NOTICED LT ENG ITT AT 690 DEG. ITT CLIMBED, REDUCED PWR IN ORDER NOT TO EXCEED 700 DEG RED LINE OF ITT. A 5 PT PERFORMANCE RUN PERF AT P&W REQUEST. ITT AT 695 DEG. CHECKED T1 HARNESS & T6 THERMOCOUPLES. RESISTANCE OF BOTH OF THE HARNESSDR R3R220010621Seal · leakingFOUND HYDRAULIC PUMP DRIVE PAD ON ENGINE NR 2 LEAKING. NEWLY INSTALLED SEAL I.D. FOUND APPROX. .015 INCH TOO LARGE FOR SHAFT IT IS SUPPOSED TO SEAL. SHAFT DIAMETER: 0.865 INCH, SEAL ID: 0.880 INCH. THIS PROBLEM OCCURRED WITH AT LEAST SIX SEALS BEFORE ONE WASDR CA010814020Controller(CAN) PRESSURIZATION PROBLEMS OCCURRED SHORTLY AFTER TAKEOFF BACK TO OTTAWA (CONTROL). ON DESCENT THROUGH 23,000 FEET. CREW EXPERIENCED RAPID DEPRESSURIZATION. MASKS WERE DONNED AND DESCENT ACCELERATED TO BELOW 10,000 FT. MAINTENANCE DETERMINED THE CAUSE TO BESDR OIB2001F00000Battery Pack · malfunctionedAIRCRAFT WAS TAXING TO THE RUNWAY FOR TAKE OFF WHEN THE PILOTS SMELLED A BURNING ODOR, THEN SAW SMOKE COMING FROM THE COCKPIT HEADLINER. THEY NOTIFIED THE TOWER THAT THEY HAD SMOKE IN THE COCKPIT, PULLED OFF TO THE SIDE AND ASKED FOR THE FIRE TRUCKS TO STANDBSDR CA010621027Stator · cracked(CAN) UPON LANDING IN QUESNEL B.C, WHEN THE PILOT APPLIED BRAKE HE FELT THE AIRCRAFT VIBRATE AND SHUTTER WHEN LH BRAKE APPLIED. THEY TAXIED TO THE RAMP AND NOTIFIED MAINTENANCE AFTER SHUTDOWN. INVESTIGATIONBY MAINTENANCE FOUND THAT THE BRAKE WEAR PINS STILL INSDR CA010621018Stator · broken(CAN) WHEN AIRCRAFT WAS TAXING FOR TAKE-OFF PILOTS REPORTED A LOUD NOISE AND THE AIRCRAFT BECAME DIFFICULT TO TAXI. THE PILOTS MADE AN ATTEMPT TO RETURN TO THE HANGAR BUT WERE UNABLE TO DO SO. MAINTENANCE PERSONNEL WERE CALLED, ANDUPON INSPECTION OF THE R/H BRSDR 2001F00046Skin · crackedDURING A SCHEDULED PHASE INSPECTION THE LEFT AILERON WAS REMOVED. UPON REMOVAL THE LEADING EDGE SKIN AT THE WEIGHT ATTACHMENT SCREWS WAS FOUND CRACKED. THIS HAD ALLOWED THE SKIN TO CRACK ABOVE AND BELOW A SCREW APPROX. .5000. THE RIGHT AILERON WAS ALSO REMOSDR 20010511CW012Window · crackedWHILE COMPLETING S/B FOUND CO PILOTS SIDE WINDOW CRACKED AT HOLES 3 AND 5. REQUIRING WINDOW REPLACEMENT.SDR CA010504009Pin · mismanufactured(CAN) FOUND ELEVATOR TRIM TAB HING PIN SHORT IN LENGTH ON LEFT SIDE ELEVATOR.SDR 2001F00024Bulkhead · crackedDURING SCHEDULED INSP, BULKHEAD (P/N 551202731) WAS FOUND CRACKED; IT IS AT STATION 456.50 LT SIDE. IT SHOULD BE NOTED THAT THE CRACK STARTS AT A HOLE THAT WAS MISDRILLED DURING PRODUCTION THEN FILLED AT THE FACTORY BY INSTALLING A DOUBLE FLUSH RIVET. THE HSDR 20010503CW011Door · out of rigDURING CLIMB, GEAR WOULD NOT LOCK UP. PER COCKPIT GEAR LIGHT INDICATION. APPARENT CAUSE IS GEAR RIGGING. RIGGED NOSE LANDING GEAR DOORS. OPERATIONAL CHECK NORMAL.
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