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 = '7603' 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 = '7603' 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 SWIA200311733Rivet · chafedA RIVET ON THE NR 2 ENGINE PUSH-PULL ROD FROM THE THROTTLE GEARBOX TO THE MFC WAS FOUND TO BE RUBBING ON A SCREW ON THE FACE OF THE GEARBOX WHEN THROTTLE MOVED INTO OR OUT OF FUEL SHUTOFF POSITION. RIVET BUCKED TO PROPER DIMENSIONS AND SCREW TIGHTENED. GAP FSDR VNAA0301013Switch · malfunctionedDURING TAKEOFF, THE CREW RECEIVED A TAKEOFF CONFIGURATION HORN AND RED WARNING PANEL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE POWER LEVER MICRO SWITCH RACK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECSDR HEEA083233Power Lever · wornPOWER LEVER WORN. SCRAPPED.SDR HEEA083232Power Lever · wornPOWER LEVER WORN. SCRAPPED.SDR HEEA083231Power Lever · wornPOWER LEVER WORN. SCRAPPED.SDR BSY2003F00002Throttle Cable · brokenLT ENGINE, NO THROTTLE CONTROL, SHUT ENGINE DOWN, LANDED NO PROBLEM. FOUND THROTTLE CABLE BROKEN, REMOVED AND REPLACED THROTTLE CABLE, OPS CHECKED GOOD.SDR SWAA030046Control Quadrant · obstructedIN-FLT SHUTDOWN, PRIOR TO DESCENT, NR 1 ENGINE THRUST LEVER WOULD NOT RETARD. FOUND DEBRIS INSIDE THROTTLE QUADRANT, REMOVED DEBRIS AND OPS CK GOOD PER MM.SDR PCAA0301012Strut · brokenLGA-IAD FLIGHT 3802 CREW REPORTED, UNABLE TO REDUCE NR 1 PROP RPM ON CLIMBOUT, AND UNABLE TO SHUT DOWN NR 1 ENGINE WITH CONDITION LEVER AT FUEL OFF. ENGINE SHUT DOWN ACCOMPLISHED WITH FUEL OFF HANDLE. MAINTENANCE REPLACED SPRING STRUT IN ACCORDANCE WITH ENGISDR QXEA0202265Power Lever · out of trimSEA ON FLIGHT 2374- RETURNED TO FIELD DUE TO: WHEN POWER LEVERS ADVANCED INTO TAKEOFF DETENT, TORQUE INDICATOR NEEDLES POINTED ONE NEEDLE WIDTH ABOVE TARGET TORQUE BUG. HAD NOT EXCEEDED DETENT AND NO RED NEEDLES. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED SDR AUS20021450Cable · failed(AUS) ENGINE THROTTLE CABLE FAILED.SDR ABXA020355Control Cable · contaminatedTHROTTLES EXTREMELY DIFFICULT TO MOVE DURING FLIGHT. EXPECTED ICE CONTAMINATION. CLEANED AND LUBRICATED CABLES AND FAIRLEADS ABOVE FORWARD BAG BIN. ICE REMNENTS NOTED ON GILL LINER ABOVE BAG BIN. THROTTLE MOVEMENT NORMAL. REMOVED ICE. MOPPED CARGO COMPARTMESDR SWAA022839Cable · wornDURING SCHEDULED RON, FOUND NR 1 ENGINE THRUST CONTROL TELEFLEX CABLE WORN. REMOVED AND REPLACED NR 1 ENGINE THRUST CONTROL TELEFLEX CABLE PER MM.SDR NSVA200200004Control Cable · brokenIAD-ON TAKEOFF ROLL RIGHT ENGINE DROPPED OFF LINE TO GROUND IDLE, ABORTED TAKEOFF. POWER LEVER DID NOT RESPOND TO ANY INPUTS. MAINTENANCE FOUND RT POWER LEVER CABLE HAD SEPARATED/BROKEN INTERNALLY (ON CONDITION). REMOVED AND REPLACED BROKEN CABLE IAW SAAB 3SDR 2004F00026O-Ring · displacedRIGHT THROTTLE FROZE AT ALTITUDE. MAINTENANCE FOUND THE NR 2 AIR SEAL, AT CENTER CONSOLE DISPLACED. REPLACED CONTROL ASSEMBLY. (M)SDR 2002FA0001354Throttle Cable · brokenUPON INVESTIGATION FOUND THROTTLE CABLE BROKEN JUST AFT OF FULL CONTROL.SDR AUS20021338Cable · chafed(AUS) NR 4 THROTTLE LEVER CABLE FOULING ON CENTER ROOF PANEL. PREVIOUS MAINTENANCE HAD BEEN CARRIED OUT FOR BATTERY PACK REPLACEMENT. PERSONNEL/MAINTENANCE ERROR.SDR 2002FA0001321Switch · inoperativeHIGH RESISTANCE (8 OHMS) IN RIGHT LOW NR THROTTLE LEVER SWITCH. 6 OHMS MAX PER SPEC SHEET. SPOILER CONTROL UNIT RECEIVES ELECTRICAL SIGNAL FROM LOW N1 THROTTLE SWITCH AS A SUBSYSTEM TO SATISFY LIFT DUMP EXTEND AND RETRACT LOGIC. SCU WILL NOT EXTEND OR RETRASDR 2002FA0001397Control Cable · brokenDURING 100 HOUR INSPECTION, FOUND THAT THE FOLLOWING CONTROL CABLE WHERE BROKEN ON THE ENGINE SIDE WHERE TWO PIECES OF SHROUD OF SWAGED TOGETHER.SDR CA021024004Throttle Cable · broken(CAN) AFTER SEVERAL UNSUCCESSFUL ATTEMPTS BY THE PILOT TO START NR 1 ENGINE, MAINTENANCE PERSONNEL DISCOVERED THAT THE THROTTLE CABLE WAS BROKEN APPROX. 12 INCHES FROM THE FUEL CONTROL UNIT ATTACHMENT. CABLE HAS BEEN REPLACED AND A/C RETURNED TO SERVICE. A/SDR A6WA200230037Connector · contaminatedUPON ARRIVAL, WHEN CONDITION LEVERS ADVANCE TO MAXIMINUM, LT PROP SPEED WAS APPROXIMATELY 68 PERCENT, LT TORQUE WOULD NOT DECREASE BELOW 60 PERCENT. MAINTENANCE RAN ENGINE TO FULL POWER TO ENSURE PROPER OPERATION. OPS CHECK GOOD. INSPECTED CONTROL CABLES FOSDR 2002FA0001180Clamp · wornOWNER COMPLAINED THAT HE WAS UNABLE TO CLOSE THROTTLE TO LAND. THE MIXTURE HAD TO BE MOVED TO CUT-OFF TO LAND. INVESTIGATION REVEALED THAT THE THROTTLE CABLE HOUSING WAS MOVING IN THE CLAMP LOCATED AT THE THROTTLE BODY PREVENTING THE THROTTLE FROM CLOSING ALSDR AUS20021121Sensor · faulty(AUS) ENGINE AUTOTHROTTLE SENSOR SUSPECT FAULTY. LIMITED INFORMATIONPROVIDED.SDR SWAA022257Cable · stiffNR 1 ENGINE THRUST LEVER DIFFICULT TO MOVE. REMOVED AND REPLACED NR 1 ENG THROTTLE TELEFLEX CABLE PER MM.SDR C8GA20020012Throttle Arm · out of adjustFLT 712 FROM TOL TO BNA. ON CLIMBOUT, NR 3 ENGINE WENT TO AN OVERSPEED CONDITION WITH NO THROTTLE RESPONSE. THE NR 3 ENGINE WAS SHUTDOWN AN APPROPRIATE CHECKLIST ACCOMPLISHED. DECLARED AN EMERGENCY AND NOTIFIED ATC, AIR TURNBACK TO TOL AND AIRCRAFT LANDED WISDR CA021031014Bearing · worn(CAN) BEARING ON CARBURETOR LOOSE IN THROTTLE. REPLACED BEARING.SDR CA020918007Clutch · malfunctioned(CAN) BOTH THRUST LEVERS APPEARED TO STICK (AS IF THEY WERE IN A DETENT) AT FLIGHT IDLE AT TOP OF DECENT. THEY WERE VERY STIFF TO MOVE FORWARD FROM THAT POSITION. STICKING WAS ACCOMPANIED BY AN AUTO THROTTLE DISCONNECT. THROTTLE CLUTCH ASSY REPLACED AND OPERASDR AUS20021114Servo · sticking(AUS) LH AUTO THROTTLE SERVO BINDING.SDR DP02002F00000Control Unit · failedNEW ENGINE INSTALLED FROM FACTORY. ENGINE DRIVER PUMP PRESSURES ADJUSTED IAW MFG MM. ENGINE FUEL FLOWS WOULD NOT REACH SPECIFIED VALUE OF 32.4 TO 34.1 GPH. IAW SD. ENGINE CHT AND TLT HOT. MFG RECOMMEDED INCREASING UNMETERED PRESSURE 5 PSI BEYOND THEIR PUBLSDR 2002FA0001078Throttle Control · bindingPILOT REPORTED BINDING OF LEFT ENGINE THROTTLE. INVESTIGATION REVEALED GALLING OF MIXTURE ADJUSTMENT ROD WHERE IT ATTACHES TO THE THROTTLE LEVER, WITH A SIGNIFICANT AMOUNT OF TRANSFER OF METAL FROM THE LEVER TO THE ROD, PREVENTING FULL THROTTLE MOVEMENT. THISDR AUS20020915Cable · worn(AUS) THROTTLE CONTROL INNER CABLE WORN BY MORE THAN 60% OF THE DIAMETER. WIRE DIAMETER WAS 0.5MM (0.019IN) INSTEAD OF THE NORMAL 1.5MM (0.059IN).SDR PCAA0207075Spring · weakPHL-FLIGHT 3810. CREW REPORTED POWER LEVERS CAN BE SELECTED TO BETA WITHOUT LIFTING TRIGGERS. MAINTENANCE CLEANED AND LUBED POWER LEVER MECHANISM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. AS A FOLLOW UP, MAINTENANCE INSPECTED POWER LEVER REVESDR AUS20020790Cable · worn(AUS) ENGINE THROTTLE CABLE WORN. CABLE WAS STIFF TO OPERATE AND JAMMED ON SEVERAL OCCASIONS.SDR AUS20020757Cable · failed(AUS) ENGINE CONTROL CABLE INNER CABLE FAILED AT SWAGED ATTACHMENT TO THE COCKPIT END FITTING.SDR HEEA080442Bearing · wornWORN BEARING P/N MS027647-4. REPLACED BEARING AND RETURNED TO SERVICE.SDR CA020726009Control Cable · broken(CAN) PILOT MAKES NORMAL LDG AT FIRE BASE CAMP IN PELICAN NARROWS, SASK. PILOT PULLS / RETARDS THROTTLE LEVER & HEARS CLUNK. THROTTLE LEVER IS VERY LOOSE & ENGINE DOES NOT SHUTDOWN, IDLES AT 55 PERCENT NG. THROTTLE LEVER IS UNRESPONSIVE TO ANY POSITIIONS . PILSDR C2XA02IA133Control Cable · lack of lubeIAH- FLIGHT 3581, THE CREW NOTED THAT THE NUMBER TWO (2) POWER LEVER WAS BINDING ON TAKEOFF ROLL. THE CREW ABORTED TAKEOFF. MAINTENANCE INSPECTED THE POWER LEVER QUADRANT AND FOUND NO OBSTRUCTION AT THE CONSOLE. INSPECTED THE ENGINE POWER LEVER QUADRANT ANSDR MALA020371Lock · malfunctionedCONFIG LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF, NOT HIGH ENERGY ABORT. CLEANED FRICTION LOCKS, ALL CHECKS GOOD.SDR HEEA080285Power Lever · wornPOWER LEVER BOLT HOLE WORN. REPLACED WITH SERVICEABLE PART.SDR CA030726003Throttle · malfunctioned(CAN) NEW THROTTLE INSTALLED DUE TO MALFUNCTION.SDR CA020726008Throttle Cable · broken(CAN) APPROXIMATELY 6 INCHES FROM ENGINE END THROTTLE CABLE BROKE. REPLACED THROTTLE CABLE.SDR CA020612008Lever · broken(CAN) PILOT RETURNED AIRCRAFT TO AIRPORT UNEVENTFULLY AFTER THROTTLE CONTROL GRIP BROKE OFF THROTTLE LEVER. PILOT WAS ABLE TO RETAIN CONTROL USING THE STUB OF LEVER REMAINING, HOWEVER SITUATION COULD HAVE BEEN VERY SERIOUS HAD THE LEVER BROKEN IN A DIFFERENT SDR HMN2002F00003Control Cable · frayedFRAYED LT ENGINE POWER LEVER CABLE FOUND DURING ROUTINE 100 HOUR INSPECTION. FRAYED PORTION UNDER CENTER PEDESTAL IN COCKPIT. (SW15200210206)SDR AWXA200200509Throttle · malfunctionedTUS - ABORTED TAKEOFF - FLT 0673 - WHILE PREPARING FOR TAKEOFF AT TUS EN ROUTE FOR PHX WHEN THRUST WAS APPLIED A LAG WAS EXPERIENCED IN THE NR 2 ENGINE. TAXIED OFF RUNWAY AND PERFORMED TWO MORE THROTTLE ADVANCES TO POWER WITH NO LAG EXPERIENCED. CONTACTED MOSDR HEEA079764Control Cable · bentCABLE IMPOSSIBLE TO MOVE. FOUND THREADED PORTION OF CABLE TO BE BENT. REPLACED WITH SERVICEABLE CABLE.SDR HMN2002F00002Control Cable · frayedFRAYED THROTTLE CABLE FOUND DURING ROUTINE 100 HOUR INSPECTION. FRAYED PORTION IN AFT FUSELAGE ON A 90 DEGREE TURN PULLEY. FOUND AND REPLACED.SDR HMN2002F00001Control Cable · frayedFRAYED CABLE FOUND DURING ROUTINE 100 HOUR INSPECTION. FRAYED PORTION IN AFT FUSELAGE ON A 90 DEGREE TURN PULLEY. FOUND AND REPLACED. (SW15200209702)SDR HMN2002F00000Control Cable · brokenON ENGINE SHUTDOWN, PILOT COULD NOT BRING LEFT PROP BACK ON LOCKS. INSPECTION FOUND LEFT ENGINE POWER LEVER CONTROL CABLE BROKEN BELOW CENTER PEDISTAL IN COCKPIT AT LOWER PULLEY. (SW15200209701)SDR P2EA2002M037Throttle Cable · bindingRIGHT THROTTLE (NR 2 ENGINE) MECHANICAL BINDING. ONLY APPROX 1/2 THROTTLE MOVEMENT. REMOVED AND REPLACED THE RIGHT ENGINE THROTTLE CABLE PER MM 76-11-01, OPS CHECK GOOD.SDR BTV2002F00001Throttle Cable · wornTHREE EACH THROTTLE CABLES FRAYING WHERE THEY PASS OVER PULLEYS AT FS512. INSPECTED, FOUND NO EVIDENCE OF CHAFING ON STRUCTURE AND CABLE TENSIONS WERE ADJUSTED PROPERLY.SDR 2002FA0000750Control Cable · frayedDURING INSPECTION IN THE AFT FUSELAGE FOUND ONE OF THE ENGINE CONTROL CABLES FRAYED WHERE THE CABLE GOES OVER A PULLEY AND TURNS 90 DEGREES. THIS IS THE 2ND OF THREE REPORTED BY THE SAME OPERATOR IN 90 DAYS. ALL HAVE BEEN THE LEFT ENGINE CONTROL
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