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 jasc_code = '3242' 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 jasc_code = '3242' 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 CA040603006Brake · disintegrated(CAN) NR 5 AFT BRAKE DISINTEGRATED ON T/O. NR 5 BRAKE ASSY REPLACED IAW J/C 6-232A, NR 5 WHEEL ASSY REPLACED IAW J/C 6-232B.SDR AUS20040472Seal · failed(AUS) LT MAIN LANDING GEAR NR 1 BRAKE PISTON SEAL PARTIALLY FAILED ALLOWING BRAKE FLUID TO LEAK ONTO BRAKE ROTORS.SDR AUS20040465Brake · failed(AUS) NR 3 BRAKE ASSEMBLY, BRAKE PADS SEPARATED AND JAMMED THE BRAKE ONTO THE WHEEL.SDR AUS20040417Brake · faulty(AUS) RT MAIN LANDING GEAR IB BRAKE FAULTY.SDR CA040528007O-Ring · cutUPON LANDING, THE LEFT BRAKE DID NOT WORK. TWO O-RINGS IN THE BRAKE ASSEMBLY WERE DISCOVERED TWISTED AND CUT WHICH CAUSED A LARGE BRAKE FLUID LEAK. THE O-RINGS WERE REPLACED, THE SYSTEM WAS BLED AND TESTED.SDR 2004FA0000401Pad · bindingPILOT WAS IN PROCESS OF TAKEOFF ROLL, PILOT REPORTED A/C VEERED TO LT HITTING A RUNWAY LIGHT, WENT OVER SOME TERRAIN AND ENDED PARTIALLY SUBMERGED IN A BODY OF WATER. AN EXAMINATION OF THE A/C WAS CONDUCTED. THE A/C CONFIG INCLUDES A FREE CASTORING NOSE WHEEL SDR CA040506004Rivet · broken(CAN) DURING INSPECTION IT WAS NOTICED THAT ONE OF THE RIVETS THAT RETAIN THE BRAKE PAD ON TO THE BRAKE ASSEMBLY WAS BROKEN, THE BRAKE ASSEMBLY WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THIS IS THE THIRD OCCURRENCE IN THE LAST FEW MONTHS, (SDR 2003092SDR CA040503006Pin · sheared(CAN) DURING C-CHECK NR 4 BRAKE ASSEMBLY LOCATOR PIN FOUND SHEARED. PIN REPLACED. AREA CHECKED AND NO OTHER FAULTS FOUND. TIMES 58561:01CYCLES 54866.SDR P5CA0401085Accumulator · leakingAFTER ENG START, NR 1 AND 4 LOST HYD SYSTEM QTY. REPLACED BRAKE ACCUMULATOR AS PER MM 32-41-23. OPS AND LEAK CK NORMAL. RESTARTED NR 1 AND 4, HYD SYSTEM TO PROPER LEVEL.SDR AALA20040524Module · inoperativeJFK INFLIGHT T1015/30 RIGHT SYSTEM HYDRAULIC QUANTITY EICAS STATUS PAGE INDICATED .42 QUANTITY. RETURNED TO JFK AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION WITH NO DAMAGE NOTED. SERVICED RIGHT HYDRAULIC SYSTEM TO FULL. SYSTEM GRSDR DHL2004362004Brake Assy · malfunctionedAUTO BRAKES IN "MED" BRAKES WOULD NOT RELEASE WITHIN + - 10SEC., RENGAGED TWICE AFTER THEY RELACED. PERFORMED AUTO BRAKE CONTROL UNIT FUNCTIONAL TEST IAW M/M 32-42-54. OPS CK GOOD.SDR 0027Stator · brokenAFTER LANDING THE PILOT WROTE UP, RIGHT BRAKE HAS INTERMITTENT RAPID CYCLES OF, ON AND OFF BRAKE PRESSURE. ALSO INDICATED, APPEARS TO BE LEAKING HYDRAULIC FLUID. MAINTENANCE INSPECTED THE BRAKE AND FOUND THE INNER BRAKE CARRIER LINING BROKEN. THE PIECE OF TSDR AUS20040302Pad · separated(AUS) BRAKE ASSEMBLY WEAR PAD SEPARATED FROM BRAKE DISC ROTOR AND DAMAGED FOUR MORE PADS CAUSING THE BRAKE UNIT TO LOCK UP.SDR CA040423009Quick Disconnect · leaking(CAN) AC LANDED, ON ROLL-OUT, WAS OBSERVED TO HAVE SMOKE ISSUING FROM UNDERSIDE OF AC. TOWER ADVISED CREW AND CALLED OUT AFF. RT MAIN GEAR WAS FULLY ENGULFED IN HEAVY SMOKE. SMOKE WAS BROUGHT UNDER CONTROL AND AC PASSENGERS AND CREW EVACUATED ONTO RUNWAY. MAISDR BAQA093765Caliper · weakCALIPER IS WEAK, SPONGY AND LEAKING EXCESSIVELY. REPLACED WITH SERVICEABLE UNIT FROM AEC, 04/21/2004SDR CA040427017Transducer · malfunctioned(CAN) AFTER LANDING, DURING ROLL OUT AND TAXI, THE PILOT REPORTED THAT HIS LT BRAKE PEDAL WAS GRINDING AND WOULD NOT SPRING BACK UNLESS HE TAPPED IT AND QUICKLY RELEASED THE PEDAL. ALSO, THE AIRCRAFT PULLED SLIGHTLY TO THE LT WHILE THE PEDAL WAS STUCK. THE LSDR FCPR200400013Brake Assy · crackedTORQUE PLATE BROKE WHEN APPLYING BRAKES, APPEARS THAT CRACK STARTED UNDER BUSHING THAT CARRIES THE CALIPER PINS, DOES NOT HAVE A PROCEDURE TO REMOVE BUSHINGS TO CHECK FOR CRACKS.SDR DAT2004F00002Control Valve · failedTHE BRAKES WENT OUT ON THE GROUND. THE FLIGHT CREW LOST CONTROL AND HIT ANOTHER AIRCRAFT. THE RIGHT WING TIP HIT THE RT VERTICAL STABILIZER ON OTHER AC. MECHANICS WERE DISPATCHED, THE RT WING TIP WAS REMOVED AND REPLACED. THE BRAKE CONTROL VALVE WAS ALSO RSDR AUS20040282Brake · worn(AUS) RT OB BRAKE WORN BEYOND LIMITS. BRAKE SEIZED ON WHEEL.SDR RAIA00404007Brake · inoperativeLT OB BRAKE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 BRAKE ASSEMBLY.SDR RAIA00404017Sensor · fluctuatesRT INBOARD BRAKE TEMP INDICATION FLUCTUATES. MAINTENANCE DEFERRED RT I/B BRAKE TEMP INDICATION SYSTEM PER MEL 32-40-1. SUBSEQUENTLY CLEARED DMI BY REMOVING AND REPLACING THE RT I/B BRAKE TEMP SENSOR.SDR DHL2004362002Servo Valve · malfunctionedAFTER LANDING THE TOWER REPORTED SMOKE COMING FROM RIGHT MAIN GEAR. BRAKE TEMPERATURES WERE NORMAL, TILLER OPERATED NORMAL DURING TAXI. REMOVED AND REPLACED NR 8 TIRE SERVO VALVE, BRAKE ANTI-SKID & AUTO BRAKE CONTROL UNIT IAW M/M 32-42-48; M/M 32-42-72. ALSSDR AUS20040436Torque Tube · cracked(AUS) BRAKE ASSEMBLY TORQUE TUBE CONTAINED NUMEROUS CRACKS IN TENON SLOTS. FOUND USING FLUORESCENT MAGNETIC PARTICLE INSPECTION. CRACKS WERE FOUND UP TO APPROXIMATELY 6.35MM (0.25IN) IN LENGTH. BRAKE IS FROM A REGISTERED AIRCRAFT. BRAKE HAD BEEN REMOVED DUESDR DHL2004362001Brake Assy · malfunctionedBRAKES FEEL LIKE THEY ARE GRABBING ON TAXI. AS A PRECAUTION REMOVED AND REPLACED NR 8 BRAKE ASSEMBLY DUE TO NR 8 TIRE FAILURE, DUE TO SUSPECTING BRAKE WAS DRAGGING M/M 32-42-27.SDR CA040415008Valve · slow(CAN) ON TAXI TO HANGER, BRAKES OVERHEATED CAUSING FIRE ON NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES AND NR 1 AND NR 2 BRAKE ASSEMBLIES TO GLOW RED HOT. ALL FOUR MAIN WHEEL AND BRAKE ASSEMBLIES REPLACED. RT MAIN LANDING GEAR SHOCK STRUT REPLACED. OTHER ITEMS, BRAKESDR DHL2004363003Brake Assy · draggingON TAKEOFF ROLL BRAKES HOT LIGHT ILLUMINATED ON MASTER WARNING PANEL (MWP). REJECTED TAKEOFF, COMPLETED ABNORMAL PROCEDURE. SPEED AT TIME OF RTO =<60 KIAS, A/C WEIGHT = 301,000, OAT = 23 DEGREES C, MAXIMUM BRAKE TEMPERATURE NR 6 260 DEGREES. CREW COMPLIED WSDR AALA20040396Brake · draggingMIA - T1550 NEAR THE V1 SPEED THE AIRCRAFT YAWED TO THE LEFT ABOUT 5 DEGREES. THE TAKEOFF WAS CONTINUED AND A NORMAL ROTATION WAS ACCOMPLISHED. LANDED AT MIA WITHOUT INCIDENT. ACCOMPLISHED SPIN CHECK OF LEFT HAND MAIN GEAR AND FOUND NUMBER ONE BRAKE DRAGGINSDR GTIA040241Brake · wornACY - FLT 1296 - AT SLOW SPEEDS BRAKING IS VERY ROUGH VIBRATION CHALTER. FOUND NR 1 MAIN GEAR WHEEL BRAKES WORN BEYOND LIMITS. REMOVED AND REPLACED MAIN GEAR WHEEL BRAKES NR 1. LEAK CHECKED NORMAL. (M)SDR 59816Nut · looseON TAKE OFF ROLL CREW NOTED A LACK OF PROPER ACCELERATION. ABORTED TAKE OFF RETURNED TO GATE. FOUND BRAKE ROD NUT LOOSE. IT WAS TIGHTENED.SDR CA040317002Brake Disc · cracked(CAN) DISC FAILED AROUND FLANGE. PART 6 OF SB 7071 ASK PILOTS TO LOOK AT WHEELS DISC ON PRE-FLIGHT INSPECTION, AT THE STAGE OF THE CRACK NOW IT WOULD HAVE BEEN NEXT TO IMPOSSIBLE TO SEE THE CRACK WITHOUT CLEANING THE DISC.SDR AALA20040336Brake · failedMAN - DURING ROLLOUT, NR 5 MAIN LANDING GEAR WHEEL DEFAULTED. INSPECTION REVEALED NR 5 BRAKE REACTION PLATE SHEAR PINS FAILED AND CAUSED DAMAGE TO BRAKE AND WHEEL ASSEMBLY, INCLUDING THERMAL RELIEF PLUG CAUSING DEFLATION. REPLACED NR 5 BRAKE AND NR 5 AND NR SDR RAIA00403007Valve · inoperativeEICAS MESSAGE BRAKE OTBD INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE O/B BRAKE CONTROL VALVE.SDR CA040303005Brake · contaminated(CAN) NR 5 BRAKE SMOKING ON ARRIVAL. A/C HAS JUST RETURNED FROM PAINT, IT IS SUSPECTED THAT EXCESS FLUID HAD COLLECTED ON THE SURROUNDING AREA OF NR 5 BRAKE. BRAKE AND WHEEL AREA THOROUGHLY CLEANED.SDR DHL2004364003Brake Assy · intermittentBRAKES OCCASIONALLY RELEASES DURING TAXI AND NR 8 ANTI-SKID RELEASES INTERMITTENTLY. PERFORMED ANTI-SKID ADJ./TEST IAW MM 32-42-00. ANTI-SKID SYSTEM. OK FOR SERVICE.SDR 58817Knob · unsecureRT BRAKE WILL NOT RELEASE. RESECURED BRAKE PARKING KNOB, LUBED ACT.SDR AUS20040088Rotor · broken(AUS) RT BRAKE ROTOR BROKEN INTO TWO PIECES WITH ONE PIECE LODGING BETWEEN THE BRAKE ASSEMBLY AND WHEEL. ON DISASSEMBLY IT WAS NOTED THAT THE ROTOR HAD BEEN BROKEN FOR SOME TIME.SDR AWXA200400165Brake · bindingDURING TAKEOFF, BOTH ENGINES AT 60 PERCENT, TOGA SWITCH WAS ACTIVATED & ENGS ACCELERATED NORMALLY, WITHIN SECONDS F/O STATED HE COULD NOT CONTROL A/C & NEEDED FULL RT RUDDER TO KEEP THE A/C STRAIGHT, NWS TILLER WAS CENTERED, REJECTED TAKEOFF AT 90 KTS. ON RETSDR 58580Brake · malfunctionedWHILE AIRCRAFT ARRIVED IN FARMINGTON, NEW MEXICO ON FLIGHT 715 THE PARKING BRAKE WHEN APPLIED THE PEDALS WERE MUSHY. MAINTENANCE BLED THE BRAKES. THE AIRCRAFT RETURNED TO SERVICE. NO PARTS WERE USED.SDR IJA2004F00000Plate · brokenON LANDING PILOT NOTICED LT BRAKE WAS SOFT. AFTER SHUT DOWN PILOT NOTICED THAT THE LT AFT BRAKE CALIPER WAS BROKEN IT APPEARS THAT THE LT BRAKE TORQUE PLATE LOWER AFT CALIPER ATTACH POINT BROKE WHEN THE BRAKES WERE APPLIED.SDR CA040128007Brake Disc · deformed(CAN) DURING REMOVAL OF THE BRAKE UNIT FROM THE AIRCRAFT, HALF OF THE BRAKE DISC DROPPED ONTO THE FLOOR. ONCE THE BRAKE UNIT WAS REMOVED FROM THE AIRCRAFT, THE REMAINING HALF OF THE DISC WAS RECOVERED FROM THE BRAKE UNIT. IT APPEARS TO BE SOME DEFORMITY OF THESDR DLM88040058Bowl · failedON CLIMBOUT LOST RIGHT HYD SYSTEM QTY AND PRESSURE. AIR TURNBACK TO IAH. FOUND LEFT INBOARD ANTISKID VALVE FILTER BOWL BROKEN. REPLACED LEFT INBOARD ANTISKID VALVE, NO OTHER LEAKS NOTED.SDR CA040116006Pin · worn(CAN) DURING GROUND HANDLING THE RT RUDDER PEDAL BRAKE ASSY SEEMED SLOPPY COMPARED TO THE LT UNIT. INVESTIGATION REVEALED THAT THE PIN THAT CONNECTS THE BRAKE PEDAL TO THE MASTER CYLINDER WAS ALMOST COMPLETELY WORN THROUGH, THIS IS A HOLLOW SHAFT PIN ASSY. WSDR CA040112003Brake Pads · damaged(CAN) DURING TAXI, CREW REPORTED THAT THERE WAS SOME DRAGGING FELT WHEN THE BRAKES WERE APPLIED. THE AIRCRAFT RETURNED TO THE BLOCKS. A DETAILED INSPECTION WAS CARRIED OUT AND NR 4 BRAKE WAS FOUND UNSERVICEABLE. THE BRAKE PADS WERE DAMAGED AND BROKEN. A SERVISDR UIA9301Brake Assy · jammedRT MLG BRAKE JAM DURING TAXI, CHK FOUND NR 1 AND NR 4 BRAKE STUCK. REPLACED NR 1 AND NR 4 BRAKE AND PERFORM BRAKE SYSTEM BLEED AND ANTI-SKID FUNCTIONAL TEST NML.SDR AUS20031335Brake Assy · broken(AUS) NR 1 BRAKE ASSEMBLY FAILED. INSPECTION FOUND THAT THE PISTONS HAD HOLED THE CARBON DISK PRESSURE PLATE CAUSING IT TO DELAMINATE AND THEN ALLOW THE PISTONS TO CONTACT THE FIRST ROTATING DISK R1 CAUSING SEVERE WEAR TO R1 AND THE PISTONS.SDR 57453Brake · inoperativeUPON LANDING RT BRAKES FELT SOFT. MAINTENANCE CALLED. BRAKES WERE BLEED. OPS CK NORMAL.SDR AUS20031337Piston · jammed(AUS) NR 2 FRONT MAIN BRAKE ASSEMBLY PISTON JAMMED AND ROTORS DISINTEGRATING.SDR AUS20031341Torque Tube · cracked(AUS) BRAKE ASSEMBLY TORQUE TUBE CRACKED. CRACK LENGTH 3.175MM(0.125IN). FOUND DURING MAGNETIC PARTICLE INSPECTION (MPI).SDR AUS20031336Housing · cracked(AUS) RT MAIN LANDING GEAR BRAKE HOUSING CRACKED ON MOUNT FLANGE.SDR 57206Brake · malfunctionedAFTER LANDING IN PIT. CREW REPORTED THAT THE LT BRAKE HAD VERY LITTLE PRESSURE ON TAXI. BLEED LT BRAKES SYS. IAW MM 32-40-00. OPS AND LEAK CK GOOD.
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