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 = 'E90' 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 = 'E90' 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 99ZZZX932Control Cable · brokenDURING CRUISE, A LOUD POP WAS HEARD, THE CONTROL COLUMN FELL AGAINST THE FWD STOP AND ACFT PITCHED UP. PILOT FOUND HE HAD UP ELEV CONTROL ONLY. EMERG DECLARED AND ACFT SAFELY LANDED USING ENG POWER AND TRIM. INVEST FOUND THE DOWN ELEVATOR CABLE HAD CHAFED TSDR 98ZZZX3462Wire · burnedDURING COMPLETE PHASE INSPECTION, FOUND BATTERY WIRES FROM BATTERY BUS TO RT AND LT MAIN BUS (P83A0, P83B0) CURRENT LIMITERS (325 AMPS) TO BE SEVERELY BURNT FROM THE CURRENT LIMITER CONNECTIONS APPROXIMATELY 6 INCHES ALONG THE WIRE. SUBMITTER STATES IT APPEARSDR 98ZZZX834Line · corrodedFOUND BOTH PNEUMATIC LINES AFT OF FIREWALL SEVERELY CORRODED WHERE AN ADELL CLAMP WENT. INSTALLED NEW LEFT AND RIGHT PNEUMATIC LINES. SUBMITTER SUGGESTED CLOSE INSPECTION OF THESE LINES ON THESE OLDER AIRCRAFT.SDR 98ZZZX833Line · corrodedFOUND BOTH PNEUMATIC LINES AFT OF FIREWALL SEVERELY CORRODED WHERE AN ADELL CLAMP WENT. INSTALLED NEW LEFT AND RIGHT PNEUMATIC LINES. SUBMITTER SUGGESTED CLOSE INSPECTION OF THESE LINES ON THESE OLDER AIRCRAFT.SDR 98ZZZX696Exhaust Stack · crackedNORMAL PHASE CHECK. 200 HR LT ENGINE, LT EXHAUST DUCT FOR LIP DEICE SYSTEM. BROKEN OFF OF TAIL PIPE. NO DAMAGE TO ENGINE OR COWLING. DETERMINED TO BE MATERIAL FAILURE. SUGGEST MORE FREQUENT INSPECTION OF EXHAUST SYSTEM. THIS COULD BE VERY DANGEROUS.SDR 98ZZZX342Tire · imbalanceTIRE SUDDENLY BECAME UNBALANCED DUE TO THE RUBBER BALANCE PATCH ON THE INTERIOR BECOMING DETACHED UNDER NORMAL CONDITIONS, 281 LANDINGS, 185 HOURS, 3.7 MONTHS IN SERVICE. SUBMITTER STATED MANUFACTURER'S DEFECT.SDR 98ZZZX338Tire · imbalanceTIRE SUDDENLY BECAME UNBALANCED DUE TO THE RUBBER BALANCE PATCH ON THE INTERIOR BECOMING DETACHED. SUBMITTER STATED MANUFACTURER'S DEFECT. 92 LANDINGS, 1.8 MONTHS IN SERVICE. NORMAL OPERATING CONDITIONS.SDR 97ZZZX5115Skin · crackedAFTER REMOVAL OF THE SURFACE DE-ICE BOOT, A SMALL CRACK APPROXIMATELY .6250 INCH LONG WAS FOUND RADIATING FROM A RIVET HOLE ON THE LEFT HORIZONTAL STABILIZER AT STA 63.0. THE CRACK WAS RADIATING OUTBOARD AND AFT. CRACKED AREA WAS REMOVED AND A FLUSH DOUBLER SDR 97ZZZX4479Aileron · crackedWHEN REBONDING STATIC WICKS TO AILERON, MECHANIC NOTICED CRACKS BENEATH BOTH INBOARD AND OUTBOARD STATIC WICK BASES.SDR 97ZZZX4478Cell · seam leakINSTALLED NEW PMA FUEL TANK IN AIRCRAFT. TANK STARTED LEAKING FROM A SEAM IN THE TANK. SUBMITTER STATED THIS IS THE SECOND OCCURRENCE. REPLACED CELL WITH ANOTHER CELL.SDR 97ZZZX4298Control Cable · brokenFOLLOWING TAKEOFF, AIRCRAFT RETURNED DUE TO ELEVATOR MALFUNCTION. INSPECTION FOUND ELEVATOR CABLE BROKEN DUE TO CHAFE ON A CLAMP ON THE BLEED AIR LINE. EMERGENCY GEAR HANDLE FORCES BLEED LINE DOWNWARD ON TO ELEVATOR CABLE. SUGGEST RE-ROUTE BLEED LINE.SDR 98ZZZX792Skin · crackedIT APPEARS THAT VIBRATION AND LEFT HAND PROPELLER HARMONICS CAUSED OIL CANNING BETWEEN TWO STRINGERS THAT INDUCED THE ORIGINAL SKIN CRACK WHICH ENLARGED ITSSELF. FOUND DURING THE BEECH COMPLETE INSPECTION. SUBMITTER STATED IF GONE UNDETECTED COULD CAUSE HORISDR 97ZZZX4301Fuel Cell · leakingUPON RETURN FROM A CHECK FLIGHT, THE LEFT NACELLE FUEL CELL STARTED LEAKING (MASSIVELY) JUST PRIOR TO ENGINE SHUT DOWN. WHEN THE FUEL SHUT OFF VALVES WERE SET TO THE OFF POSITION, FUEL CONTINUED TO LEAK. AN INVESTIGATION DISCLOSED THE LEFT NACELLE MAIN FUEL LSDR 97ZZZX1157Shim · corrodedENGINE MOUNT PLATE AND SHIM WERE FOUND CORRODED UNDER THE AREA OF THE LEFT AND RIGHT ENGINE MOUNT TO FIREWALL ATTACHMENT. THE SHIMS WERE FLAKING AWAY SEVERELY AND IF LEFT UNREPAIRED, WOULD CAUSE THE MOUNT TO FIREWALL BOLT TORQUE TO DROP. THESE PARTS SHOULD BESDR 97ZZZX1156Plate · corrodedENGINE MOUNT PLATE AND SHIM WERE FOUND CORRODED UNDER THE AREA OF THE LEFT AND RIGHT ENGINE MOUNT TO FIREWALL ATTACHMENT. THE SHIMS WERE FLAKING AWAY SEVERELY AND IF LEFT UNREPAIRED, WOULD CAUSE THE MOUNT TO FIREWALL BOLT TORQUE TO DROP. THESE PARTS SHOULD BESDR CA961218004Generator · failed(CAN) #2 ENGINE STARTER GENERATOR FAILED IN FLIGHT. THERE WAS A SLIGHT SMELL OF SMOKE IN THE COCKPIT PRIOR TO FAILURE. AFTER THE FAILURE THERE WAS A BRIEF FLICKER OF #2 ENGINE FIRE DETECTION LIGHT. THE RIGHT HAND GENERATOR LIGHT ALSO ILLUMINATED. DUE TO THE INSDR 96ZZZX5816Torque Knee · crackedAFTER AN INCIDENT CAUSED BY AN UPPER TORQUE KNEE FAILURE, OTHER AIRCRAFT IN THE FLEET ARE BEING INSPECTED. DURING THIS INSPECTION THE UPPER TORQUE KNEE ON THE RIGHT GEAR WAS VISUALLY FOUND TO BE CRACKED. A NEW UNIT WAS INSTALLED. BOTH THE NEW UNIT AND THE OSDR 96ZZZX5329Torque Knee · brokeRT UPPER TORQUE KNEE BROKE AT PIVOT POINT WHERE THE LOWER TORQUE KNEE ATTACHES TO IT. THE PILOT WAS ON TAKEOFF ROLL WHEN HE THOUGHT HE HAD A RT MAIN TIRE BLOW. HE THEN BROUGHT THE ACFT TO A STOP. WHEN THE TORQUE KNEE BROKE, THE TIRE SPUN AROUND AND RIPPED HSDR 96ZZZX2076Skin · crackedDURING ROUTINE INSPECTION AFTER AIRCRAFT WAS PAINTED, FOUND CRACK IN HINGE. FOUND UPPER RIVETS WORKING ON OUTBOARD RIB FLANGE. REMOVED ELEVATOR TIP CAP AND FOUND OUTBOARD RIB ATTACHMENT HOLES MISSING REAR PART OF RIB. REPLACED RIB AND RIB FLANGE. STOP DRILSDR 96ZZZX2075Rib · misinstalledDURING ROUTINE INSPECTION AFTER AIRCRAFT WAS PAINTED, FOUND CRACK IN HINGE. FOUND UPPER RIVETS WORKING ON OUTBOARD RIB FLANGE. REMOVED ELEVATOR TIP CAP AND FOUND OUTBOARD RIB ATTACHMENT HOLES MISSING REAR PART OF RIB. REPLACED RIB AND RIB FLANGE. STOP DRILSDR 96ZZZX973Torque Plate · crackedOUTER PORTION OF UPPER FORWARD BUSHING BOSS OF BRAKE IS CRACKED CLEAN THROUGH. SUSPECT EXCESSIVELY HARD BRAKING WHILE BRAKE IS HOT. INFORMATION RETRIEVED FROM CLEVELAND INSTALLATION MANUAL FOR CONVERSION KIT NR 199-90/199-90A.SDR 96ZZZX357Intercostal · crackedINTERCOSTAL FOUND CRACKED. THIS PART SUPPORTS CABIN DOOR HAND RAIL AND IF FAILED, WILL CAUSE DOOR TO STRIKE THE GROUND. SUBMITTER STATED DOOR NEEDS DUAL SUPPORT CABLES TO ELIMINATE THIS PROBLEM.SDR 95ZZZX5544Line · splitLEFT ENGINE OIL COOLER LINE SPLIT CAUSING LOSS OF OIL. LEFT ENGINE SHUT DOWN. OIL LINE WAS REPLACED, APRIL, 1995, AT 5-YEAR INSPECTION.SDR 95ZZZX5255Wheel · crackedCRACKS WERE FOUND IN THE BOLT HOLES OF THE WHEEL HALF CAUSING THE TIRE TO DEFLATE MORE THAN THE ALOTTED AMOUNT.SDR 95ZZZX4611Inverter Harness · miswiredDURING AN INSPECTION, A DUAL FEEDER BUS CONFORMITY TEST WAS PERFORMED. THE INVERTER POWER HARNESS WAS FOUND WIRED TO THE WRONG BUSS (LT WIRED TO RT, AND VICE VERSA). SHOULD THE 325-AMP ISOLATION LIMITER BECOME OPEN, BOTH INVERTERS WOULD FAIL. THIS IS SECONDSDR 95ZZZX6191Control Cable · severedPILOT REPORTED PARTIAL LOSS OF ELEVATOR CONTROL. UPON TROUBLESHOOTING THE SYSTEM, FOUND THE DOWN CONTROL CABLE SEVERED BELOW PILOT'S FLOORBOARDS AT A POINT WHERE A WIRING BUNDLE CROSSES THIS CABLE. IN THIS WIRE BUNDLE, WIRE NR H16A10 WHICH IS FOR THE COPILOTSDR 95ZZZX5248Wheel · bearing failedLEFT MAIN WHEEL CAME OFF ON TAKEOFF. INSPECTION REVEALED OUTSIDE BEARING FAILURE. DISINTEGRATION OF BEARING, RACE, CUP AND HOUSING ALLOWED WHEEL TO EXIT OVER AXLE NUT. SUBMITTER STATED POSSIBLE DEFECT DURING MANUFACTURE. CLOSE INSPECTION OF BEARINGS AT EACSDR 95ZZZX4532Line · leakPILOT NOTICED FUEL LEAKING FROM COWLING AT MID-NACELLE AREA. ALSO, A HIGHER FUEL FLOW INDICATION WAS NOTED. UPON INVESTIGATION AFTER PRECAUTIONARY LANDING, IT WAS NOTED THE FUEL BYPASS LINE WAS LEAKING AT ONE END. A CRACK WAS DISCOVERED JUST AFT OF THE FERRSDR 95ZZZX3597Wheel · splitDURING TAKEOFF ROLL, PILOT HEARD A LOUD BANG. WHEN AIRCRAFT CAME TO A STOP, THE OUTBOARD WHEEL HALF HAD SPLIT IN HALF STARTING AT INBOARD WHEEL HALF MATING FLANGE AND CRACK WORKING ITS WAY TOWARD WHEEL BEAD AREA.SDR 95ZZZX3035Blade · undersizeUPON FINDING BLADES, MODEL NR T10173B-8R, S/NS C84204, C84280, C84314, C21475, C34127, AND C34121, DIMENSIONALLY UNDER WIDTH WISE, CUSTOMER REPORTED PROPS HAVING APPROXIMATELY 200 HOURS SINCE OVERHAUL. PROPELLERS WERE OVERHAULED LAST IN MEXICO.SDR 95ZZZX3199Harness · terminal brokenDURING FLIGHT, PILOT NOTICED I.T.T. HAD DROPPED TO ZERO. MAINTENANCE WAS NOTIFIED AND A RESISTANCE CHECK WAS DONE. MAINTENANCE FOUND A TERMINAL ON THE T-5 HARNESS HAD BROKEN LOOSE IN THE CERAMIC HOUSING CAUSING T-5 TO DROP OFF. ENGINE C-FLANGE WAS SPLIT ANDSDR 95ZZZX3220Lever Assy · bentFOUND LEVER ASSY WORN THIN TO POINT OF BENDING. WORN THIN BY RUBBING ON PEDESTAL AND BENDING.SDR 95ZZZX2123Rib · crackedINSPECTION ON LEFT ELEVATOR INBOARD WHERE TORQUE TUBE ATTACHES TO END RIB, FOUND RIB AND BRACKET CRACKED. REPLACED PARTS WITH NEW.SDR 95ZZZX2122Bracket · crackedINSPECTION ON LEFT ELEVATOR INBOARD WHERE TORQUE TUBE ATTACHES TO END RIB, FOUND RIB AND BRACKET CRACKED. REPLACED PARTS WITH NEW.SDR 95ZZZX2121Rib · crackedFOUND RIB AND BRACKET CRACKED ON LEFT ELEVATOR INBOARD WHERE TORQUE TUBE ATTACHED TO END RIB. CAUSE UNKNOWN. REPLACED PARTS WITH NEW. SPAR END ALSO CRACKED FROM WORKING OF TORQUE TUBE. REPAIRED BY DOUBLER IAW AC 43.13.SDR 95ZZZX2120Bracket · crackedFOUND RIB AND BRACKET CRACKED ON LEFT ELEVATOR INBOARD WHERE TORQUE TUBE ATTACHED TO END RIB. CAUSE UNKNOWN. REPLACED PARTS WITH NEW. SPAR END ALSO CRACKED FROM WORKING OF TORQUE TUBE. REPAIRED BY DOUBLER IAW AC 43.13.SDR 95ZZZX3304Skin · crackedRIGHT AILERON FOUND CRACKED ON TOP AFT OUTBOARD SKIN FORWARD SIDE. DURING ROUTINE, 4 INCH CRACK FOUND AT FORWARD SECTION OF AFT SKIN WHERE IT MEETS FORWARD SKIN AT AILERON CENTER SPAR.SDR 95ZZZX681Antenna · defectiveBOTH COMMS AND NAVS WOULD HAVE EXCESSIVE STATIC IN LIGHT PRECIPITATION. THE COMMS WOULD BECOME UNREADABLE AND BOTH NAVS WOULD FLAG WITH LOSS OF L/R DEVIATION VOR OR LOC. TEST AIRCRAFT WITH DAYTON GRANGIER HIGH VOLTAGE STATIC TESTER AND FOUND LORAN ANTENNA SOSDR 95ZZZX515Boot · shortedON DEPARTURE FROM AIRPORT, LEFT INLET BOOT (ELECTRIC) SHORTED AND BURNED, CIRCUIT BREAKER DID NOT TRIP. BOOT WAS TURNED OFF, LEFT ENGINE SHUT DOWN AND RETURNED TO AIRPORT.
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