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 RAIA00408004Switch · out of adjustCONFIG WARNING ON TAKEOFF ROLL. MAINTENANCE ADJUSTED CONDITION LEVER SWITCH.SDR ASMF200407035Lever · brokenAIRCRAFT RETURNED TO PLATFORM, FUEL LEVER UNLOCKED. DURING MAINTENANCE REVISION, SPRING LOCK LEVER WAS DETECTED BROKEN. AIRCRAFT WAS SENT TO THE HANGAR AND SPRING WAS REPLACED IAW MM 76-12-00, TEST CORRECT.SDR CA040723007Switch · stuck(CAN) ON CLIMB THE PILOT REPORTED THE GEAR IN TRANSIT LIGHT WAS ON. LANDING GEAR WAS EXTENDED WITH NO DIFFICULTIES AND MAINTENNACE WAS CONTACTED. AIRCRAFT RETURNED TO BASE. AIRCRAFT WAS PUT ON JACKS AND THE RT POWER LEVER 70 PERCENT SWITCH WAS FOUND STUCK. SDR 2004FA0000888Cable · wornSWEDGED-IN PORTION OF THE CABLE GUIDE DISPLAYED .110 INCH FORE AND AFT PLAY INDICATING IMPENDING FAILURE OF THE SWIVEL JOINT. CABLE WAS REMOVED AND GIVEN FOR EVALUATION. THIS CONDITION WAS APPARENTLY CAUSED BY DIRT CONTAMINATION. (THE PROTECTIVE RUBBER BOOTSDR DXTA200400331Engine · malfunctionedWITH POWER AT TAKEOFF THRUST AIRCRAFT YAWS SHARPLY LEFT, POWER ON BOTH ENGINES MATCHED. RAN AIRCRAFT TO TAKEOFF POWER, TAXI CHECKED BRAKES, TOP CHECKED RUDDER BIAS, COULD NOT DUPLICATE. FOUND RIGHT ENG ACCELERATING FASTER AND HIGHER THRUST THAN LEFT, COULD NSDR CA040628004Control Cable · worn(CAN) THIS IS THE SECOND OCCURRENCE OF SUCH A DEFECT NOTED BY THE SAME OPERATOR WITHIN THE PAST FEW WEEKS. THE SWAGED SWIVEL JOINT ON THE THROTTLE CONTROL WAS NOTED TO BE WORN TO THE POINT WHERE THE BALL END COULD BE REMOVED FROM ITS SWAGED SOCKET WITH EASE. DSDR CA040621010Throttle Control · looseTHROTTLE CONTROL WAS REPLACED AT A SCHEDULED INSPECTION RECENTLY AND HAS ALREADY COME LOOSE AT THE CRIMPED PIVOT END AFTER ONLY APPROX 160 HOURS TIS. THIS PART WAS INSTALLED AS A NEW PART SUPPLIED FROM THE MANUFACTURER. DEFECTIVE PART REMOVED AND TO BE REPLASDR AMTA200400678Control Box · malfunctionedSEVERAL TIMES DURING DESCENT LEFT THROTTLE LEVER WOULD JAM AND WAS NOT ABLE TO BE POSITIONED TO IDLE. FORCING T-LEVER FORWARD FREED MOVEMENT. REMOVED AND REPLACED NR 1 ENGINE LOWER CONTROL BOX ASSEMBLY PER 76-11-10-4. NO BINDING NOTED AT THIS TIME AT THIS TSDR AUS20040502Washer · missing(AUS) THROTTLE QUADRANT FRICTION ADJUSTER WASHER MISSING. FOUND DURING INSPECTION IAW AD/BN2/69 AND SB 272.SDR 04FDEA01541Cable · out of rigON TAKEOFF NR 2 THROTTLE WOULD NOT GO PAST V2WAY, DUE TO BINDING. ABORTED BELOW 70 KTS. RETURNED TO GATE. THROTTLE LEVER FEEDBACK CABLE MECHANISM FOUND OUT OF RIGGING RANGE. T/L FEEDBACK MECHANISM RIGGED IAW MM 78-31-38-2.SDR CA040609013Throttle Cable · broken(CAN) AFTER A PREFLIGHT CHECK, THE PILOT COMPLAINED OF AN EXTREMELY LOOSE THROTTLE CONTROL. AFTER FURTHER INSPECTION, THE CONTROL CABLE WAS DETERMINED TO BE INTERNALLY BROKEN. THE CABLE WAS REMOVED AND THE CONTROL LEVER END OF THE CABLE PULLED OUT OF THE EXTSDR A6WA200440067Gearbox · damagedLT THRUST LEVER WHEN MOVED TO IDLE STOP SHUT OFF FUEL TO ENGINE. 2 INCH PLAY IN THRUST LEVER WITH NO ENGINE RESPONSE. REMOVED AND REPLACED THROTTLE CONTROL GEARBOX. OPS CHECK GOOD. IWA ENG SHOP MANAGER, REMOVED AND REPLACED NR 1 ENGINE THROTTLE GEARBOX IAWSDR 2004FA0000566Control Cable · chafedMIXTURE CONTROL AND ALTERNATOR BATTERY AND CABLE ARE TIED TOGETHER. CONTROL AND CABLE CHAFED INSULATION OFF CABLE AND SHORTED TO MIXTURE CABLE, CAUSING MIXTURE CABLE TO FREEZE UP AT ITS CURRENT SETTING. WHEN TYING WIRES AND CABLE AND LINES OR HOSE TOGETHER USDR CA040527005Control Module · stiffRT POWER LEVER 'PIGGYBACK' LEVER VERY STIFF, DIFFICULT TO MOVE TO STOW POSITION. THROTTLE CONTROL MODULE REPLACED.SDR CA040513008Spring · damaged(CAN) ON TAKE OFF ROLL, PWR SET TO 1290 FT LBS. AFTER ROTATION NOTICED TORQUE INCREASING ON RT ENG. FO ATTEMPTED TO REDUCE PWR BUT PWR LEVER WOULD NOT MOVE. TORQUE INCREASED TO APPROX 1500 FT LBS FOR ABOUT 90 SECONDS. AFTER REACHING SAFE ALTITUDE RT ENG SHSDR 2004FA0000563Clip · failedLT THROTTLE CONTROL LEVER FAILED TO CHANGE POWER DURING CHANGE FROM TAKE-OFF TO CRUISE POWER SETTING. IT WAS DISCOVERED THT THE CRIMPING HAS FAILED ON THE CLIP THROTTLE CONTROL PN RA1039C WHICH IS PART OF THE THROTTLE CABLE ASSY PN 50-389012-15. THIS CLIP ISSDR 2004FA0000534Nut · missingJUST TURNED FINAL AND WENT TO PULL POWER BACK AND FOUND NO THROTTLE RESPONSE. PILOT WAS ABLE TO LAND USING MAG SWITCH TO ADD AND REDUCE POWER. UPON INSPECTION FOUND LOCK NUT MISSING FROM THROTTLE CONNECTION AND BOLT LAYING HALF OUT OF THROTTLE /TURBO ACTUATOSDR JIKA200400005Throttle Cable · brokenAFTER LANDING PILOT ATTEMPTED TO ACCELERATE ENGINE TO TAXI TO THE RAMP AREA. THERE WAS NO RESPONSE FROM THE THROTTLE LEVER INPUTS, THE ENGINE WOULD NOT ACCELERATE ABOVE IDLE RPM. PILOT SHUT DOWN ENGINE AND THE AIRCRAFT WAS TOWED TO THE RAMP AREA. MAINTENANCSDR CA040423001Bolt · failedTHE PILOT WAS UNABLE TO CHANGE PWR SETTINGS IN FLT AS THE THROTTLE DID NOT RESPOND FROM MOVEMENTS IN THE PWR LVR. THE A/C IMMEDIATELY RETURNED FOR AN UNEVENTFUL LANDING WITH THE RPM SET AT 2300. INSPECTION OF A/C FOUND THAT THROTTLE CNTRL WAS DISCONNECTED FROSDR 04FDEA00970Control Cable · stuckNR 2 THROTTLES STUCK AT 91 PERCENT N1 FL310 SHUTDOWN ENGINE AT 6000 HIGH THROTTLE BROKE FREE ON TAXI IN. REMOVED AND REPLACED NR 2 ENG PUSH PULL CABLE IN REF TO DC10 MM 76-11-01-2 RIG CHECKED GOOD. INSTALLED ALL SCREWS ON NR 2 ENGINE ACCESS PANELS, CLOSED WSDR DXTA200400288Control Cable · out of rigLEFT ENGINE FLAMED OUT AFTER DOING PREFLIGHT WING SPOILER CHECK. INSPECTED LEFT ENGINE CONTROLS AT FUEL CONTROL UNIT AND ACCOMPLISHED ENGINE POWER CONTROLS CHECK. PERFORMED ADJUSTMENT AND RIGGING CHECK IAW CESSNA 560 MM CHAPTER 76-11-00 PG. 501 NO DISCREPANCISDR QXEA200400237Switch · malfunctionedSEA FLIGHT 2195 RETURN TO FIELD, NR 1 ENGINE INFLIGHT SHUTDOWN, TORQUE FLUCTUATION AT ALL POWER SETTINGS. MAINTENANCE REPLACED THE POWER LEVER SWITCH. OPERTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR CA040326003Gearbox · binding(CAN) PILOT REPORTED THROTTLE ACTION STIFF. MAINTENANCE TROUBLESHOT PROBLEM TO NR 1 ENGINE THROTTLE CONTROL GEARBOX BINDING. NR 1 THROTTLE CONTROL GEARBOX REPLACED. IT IS NOTED THAT AD CF-2004-01, HAS BEEN ISSUED AGAINST GEARBOX P/N 2100140-007, ALTHOUGH IN SDR 2004F00082Control Rod · looseAIRCRAFT RELEASED FROM MAINTENANCE. DEPARTED VPC. CLIMBING OUT FROM 9,000 FT, RIGHT THROTTLE WOULD NOT RESPOND. RETURNED TO VPC WITH UNEVENTFUL LANDING. MAINTENANCE FOUND THE THROTTLE PUSH PULL ROD CAME LOOSE AT THE FIREWALL (ROD END SEPARATED FROM THE BARSDR SWIA200413008Gearbox · malfunctionedNR 1 THRUST LEVER STUCK AT CRUISE POWER SETTINGS. PERFORMED QRH AND SHUT DOWN NR 1 ENGINE. REMOVED AND REPLACED LT POWER LEVER CONTROL GEAR BOX IAW CRJ MM 76-11-17. OPS CHECK GOOD.SDR CA040309001Control Cable · severed(CAN) AFTER LANDING AND SUBSEQUENT TAXI THE RT ENGINE SPOOLED UP AND DID NOT RESPOND TO POWER LEVER MOVEMENT. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT COMPLETED TAXI TO THE TERMINAL ON THE LT ENGINE. MAINTENANCE INVESTIGATED AND DISCOVERED THAT THE POWER LEVESDR 04FDEA00540Roller · brokenGEAR UNSAFE HORN SOUNDED WHEN LEVER WAS RAISED ON T/O. HORN WAS SILENCED NORMALLY WITH THE GEAR HORN OFF BUTTON. THREE RED LIGHTS ON BOTH PANELS STAYED ON WITH HANDLE IN UP POSITION. GEAR WAS LOWERED AND 3 GREEN ANNUNCIATED. HYD PRESSURE & QUANTITY NORMALSDR AKG2004F00004Rod End · failedWHILE REPLACING THE ENGINE POWER CONTROL CABLE. THE ROD END AT THE THROTTLE BODY WAS FOUND WITH THE BRASS INSERT AND THE STEEL PIVOT BALL FALLING OUT OF THE ROD END HOUSING. THERE IS NOT A LARGE AREA SAFETY WASHER INSTALLED. IT WAS JUST A MATER OF TIME AND SDR Q2A2004F00000Linkage · lack of lubePILOT REPORTED RT THROTTLE LOCKED IN FLIGHT. NON EVENTFUL LANDING. INSPECTION FOUND DRY FUEL CONTROL LINKAGE CAUSING BINDING. LUBRICATED IAW MM, FUNCTION CHECKS OK. NO PRESENCE OF LUBE SINCE NEW.SDR SWAA040444Cable · out of adjustABORTED TAKEOFF, NR 2 THRUST LEVER MOVEMENT RESTRICTED. ADJUSTED NR 2 ENGINE THRUST REVERSER FOLLOW-UP CABLE PER MM.SDR DL73S040143Control Cable · stiffDURING CLIMB TO 370 FROM 330 NR 1 THROTTLE POPPED BACK AND FORTH. A/T DISCONNECTED AND THROTTLE STIFF. AFTER DESCENT BELOW 330 THROTTLE WORKED NORMAL AND NOT AS STIFF. REPLACED NR 1 ENGINE THROTTLE PUSH-PULL CABLE. RAN ENGINE PER PFHB. OPS GOOD.SDR 04036629Gearbox · seizedDURING FLIGHT THE CREW REPORTED THE RIGHT HAND ENGINE THROTTLE LEVER LOCKED UP. THE FLIGHT LANDED UNEVENTFULLY. THE THROTTLE GEARBOX ASSEMBLY WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURSDR DLM88040132Throttle Cable · bindingABORTED TAKEOFF AT 65 KIAS ENGAGED AUTOTHROTTLES FOR FLEX 50 TAKEOFF AT 75 PERCENT N1 THROTTLES IMMEDIATELY CLAMPED AND DID NOT ADVANCE AT ALL TOWARDS TAKEOFF THRUST. ABORTED T/O FOR THIS REASON. FOUND THRUST CABLE AT ENGINE BINDING. REPLACED SAME.SDR 58501Solenoid · dirtyON TAKEOFF ROLL IN TAMPA FLORIDA ON FLIGHT 5536, THE LT ENGINE POWER LEVER FULL FORWARD WOULD ONLY GO TO 2000 LBS OF TORQUE AND 1500 PROP RPM. THE CREW ABORTED THE TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED THE LOW PSDR MALA040143Housing · contaminatedDURING FLIGHT 3011 INFLIGHT RT POWER LEVER STUCK. WHILE ATTEMPTING TO MOVE RT POWER LEVER HAD LOTS OF RESISTANCE AND SPRUNG BACK TO ORIGINAL STUCK POSITION. PILOT MOVED RT BACK AND FORTH AND WAS ABLE TO REDUCE ENGINE TORQUE TO 20-25 PERCENT FOR LANDING. ONCSDR XNOA1174Track · obstructedNR 1 THROTTLE WILL NOT ADVANCE PAST 35. FOUND METAL DEBRIS ON NR 1 ENGINE THROTTLE TRACK. REMOVED (FOD) & ADVANCED THROTTLE SEVERAL TIMES WITH NO FURTHER DEFECTS. AIRCRAFT OKAY FOR SERVICE IAW A-300 AMM 76-11-00.SDR 2004F00062Control Cable · seizedIN AN ATTEMPT TO REDUCE POWER FOR DESCENT, NR 1 ENGINE POWER LEVER LOCKED UP AT CRUISE POWER. DESCENDING THROUGH 8000 FEET, ENGINE WAS SECURED AND AIRCRAFT LANDED SAFELY. REPLACED POWER CONTROL CABLE ASSEMBLY. (M)SDR 0407Throttle Cable · brokenON APPROACH, RT ENGINE HAD NO RESPONSE, SHUT ENGINE DOWN LANDED NO PROBLEM. REMOVED AND REPLACED THROTTLE CABLE, OPS CHECK GOOD.SDR 2004FA0000053Throttle · stuckTHE STUDENT PILOT AND FLIGHT INSTRUCTOR WERE PRACTICING POWER-OFFS STALLS WHEN THE THROTTLE BECAME STUCK AT THE IDLE POSITION. DUE TO THE MECHANICAL PROBLEM, THE FLIGHT INSTRUCTOR LANDED THE AIRCRAFT IN A VACANT FIELD. THERE WERE NO INJURIES TO THE PILOT OR SDR MEX2003573Throttle · lack of lubeAIRCRAFT RETURNED TO PLATFORM, DUE TO SLOW ACCELERATION IN THE RIGHT ENGINE. THE WATER SUMP WAS DRAINED AND THE THROTTLE CHAMBER WAS LUBRICATED IAW MM 73-20-03. AT OVERNIGHT SERVICE IN MEX, PERFORMED A TRIM TO BOTH ENGINES AND AN ACCELERTION TEST IAW MM 71-0SDR UIEA200300072Control Cable · icedNR 3 ENGINE THROTTLE UNABLE TO SELECT IDLE DURING DESCENT. THROTTLE STUCK AT 4 DEGREE THROTTLE ANGLE AND 80 PERCENT N1. ENGINE SHUTDOWN USING ENGINE FAILURE/SHUTDOWN CHECKLIST. PERFORMED INSPECTION IAW 73-21-01 AND 76-11-03 THRUST CONTROL CABLE INSPECTED ALLSDR AUS20031244Power Lever · incorrect(AUS) LT ENGINE FUEL BYPASS LIGHT ILLUMINATED DURING TAKEOFF. EXTENSIVE INVESTIGATION COULD FIND NO CAUSE FOR THE DEFECT. ENGINE GROUND RUNS AND POWER CHECKS WERE OK. SUSPECT CAUSED BY INCORRECTLY SET SPEED LEVER. DEFECT NOT CONFIRMED.SDR 21200003Control Cable · chafedDURING TAKE OFF PREPORATION, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTION REVEALED THE POWSDR 22811290376Control Cable · chafedDURING TAKE OFF PREPARATION, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTION REVEALED THE POWSDR SDR11290376Control Cable · chafedDURING TAKE OFF PREP, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LEFT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTIN REVEALED THE POWER LEVSDR 11290376Control Cable · chafedDURINE TAKE OFF PREPORATION, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LEFT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTIN REVEALED THE POSDR 11280376Control Cable · chafedDURINE TAKE OFF PREP, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTION REVEALED THE POWER LEVESDR SDR11280376Control Cable · chafedDURINE TAKE OFF PREPORATION, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LEFT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTIN REVEALED THE POSDR 2004FA0000098Throttle Cable · inoperativeDURING LANDING PILOT REPORTED THAT HE COULD NOT RETARD THROTTLE. SUSPECT BEARINGS INSIDE CABLE ARE FREEZING UP. REMOVED AND REPLACED CABLE ASSY.SDR UIEA200300065Throttle · stuckNR 3 ENGINE THROTTLE STUCK AT POSITION IT WAS IN AT CRUISE POWER. IT FINALLY CAME LOOSE AT 10,000 FT. SHUT DOWN ENGINE AT 10,000 FT AND RESTARTED BETWEEN 10,000 FT AND 4,000 FT. OPERATED OK AFTER START. INSPECTED NR 3 ENGINE FOR WINDMILLING PER MM 72-00-00
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