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 98ZZZX1119Control Cable · failedTHROTTLE CABLE BROKE APPROXIMATELY 1.5 INCHES FROM THROTTLE LEVER. OLDER AIRCRAFT USED QQ-2-470 MUSIC WIRE .090 INCH DIAMETER. INNERGRANULAR CORROSION WAS NOTED IN THE BROKEN AREA. SUBMITTER RECOMMENDED CABLE BE REPLACED WITH 20253-P2 PIN MATERIAL OR UPGRADSDR DHL98726115Crank · crackedAT D CHECK, 33 ENGINE PYLON THROTTLE CRANK CRACKED. REMOVED AND REPLACED CRANK PER MM 76-12-41. N/R 6342.SDR PNSA980201Clevis Pin · looseLT POWER LEVER BECAME DISCONNECTED DURING START. RESECURED CLEVIS PIN, OPS CHECK OK.SDR 9802736642Coupling Screw · brokenAT START OF TAKEOFF ROLL, THE NR 4 ENGINE DID NOT ACCELERATE OR RESPOND TO POWER LEVER INPUTS. THE TAKEOFF WAS ABORTED AND RETURNED TO THE GATE. MAINTENANCE FOUND A BROKEN COUPLING SCREW IN THE STRUT AREA. REPLACED THE SCREW AND A FUNCTIONAL TEST OF THE THRSDR MALA975981Solenoid · lack of lubeAFTER TAKEOFF, FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE COMPLETED OPS CHECK OF FLIGHT IDLE STOP SOLENOID, LUBRICATED SOLENOID. OPS CHECK GOOD.SDR CA980311007Throttle Cable · jammed(CAN) DURING PRACTICE STALLS AND SPIN RECOVERIES THE THROTTLE CONTROL JAMMED FULL ON. AFTER LANDING THE THROTTLE WAS DISCONNECTED AT THE CARBURETOR. CARB LINKAGE OK BUT CABLE STILL JAMMED. CABLE REPLACED.SDR 9802586642Control Cable · disconnectedON TAKEOFF ROLL (PEK), THE NR 4 ENGINE DID NOT RESPOND TO POWER LEVER MOVEMENT AND THE TAKEOFF WAS ABORTED. MAINTENANCE FOUND THE POWER LEVER PUSH/PULL CABLE DISCONNECTED AT THE CABLE DRUM IN THE STRUT AREA. REPLACED THE CABLE DRUM. OPERATIONAL CHECK NORMALSDR REXA98045Condition Lever · out of adjustLEFT PROP RPM BELOW 1000, AND TORQUE VERY SLOW TO RISE ON TAKEOFF ROLL. RERIGGED LEFT CONDITION LEVER AT SECTOR PULLEY. GROUND RUN AND CTOT CHECKS GOOD. (M)SDR CA980210013Shaft · broken(CAN) DURING A POWER RUN UP WITH CONDITION LEVERS AT MAXIMUM AND POWER LEVERS ADVANCED TO APPROXIMATELY 80 PERCENT TORQUE, THE NR 2 CONDITION LEVER SUDDENLY MOVED BY ITSELF TO MINIMUM SETTING. ATTEMPT TO FEATHER PROP USING CONDITION LEVER WAS UNSATISFACTORY. SDR CA980303003Throttle Cable · stiff(CAN) LEFT ENGINE POWER LEVER WAS DIFFICULT TO MOVE WHILE IN CRUISE.SDR 98ZZZX514Control Cable · failedTHROTTLE CABLE PLASTIC OUTER COVER MADE OF PLASTIC BECAME BRITTLE FROM AGE AND HEAT AND FAILED. THE WHOLE ASSEMBLY WAS MOVING WITH POWER CHANGES. SUBMITTER STATED THESE ORIGINAL CESSNA SUPPLIED CABLES ARE ALL REACHING THEIR SERVICE LIFE ON PLASTIC DETERIORATISDR 98ZZZX856Control Cable · failedPILOT ATTEMPTED TO ADVANCE LT THROTTLE FROM FLIGHT IDLE. ENGINE DID NOT RESPOND. FOUND THE CABLE ELEMENT BROKEN 6 INCHES AFT OF FUEL CONTROL POWER CONTROL ASSEMBLY.SDR 98ZZZX975Throttle Control · failedPILOT REPORTED A SNAP OR SOMETHING GAVE AS HE ADVANCED THROTTLE ON GROUND. ENGINE RPM STAYED AT 1,100 RPM. INVESTIGATION REVEALED THAT CABLE OUTER HOUSING SLIPPED OUT OF METAL RETAINER AT CLAMP NEAR CARBURETOR. OUTER HOUSING APPARENTLY SHRUNK FROM HEAT. RESDR REXA98013Condition Lever · out of adjustBOTTOMING GOVERNOR IS ENGAGED BELOW MINIMUM GATE ON RIGHT HAND ENGINE. RIGGED RIGHT HAND CONDITION LEVER IAW AMM 76-10-00. GROUND RUNS CHECKED GOOD. (X)SDR 98ZZZX527Spring · brokenFUEL CONTROL/THROTTLE LINKAGE SPRING BROKEN. LOW HOURS SINCE NEW.SDR MALA975882Flight Idle Stop · trippedAFTER TAKEOFF, THE FLIGHT STOP OPEN LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE RESET FLIGHT IDLE STOP OVERRIDE THAT WAS TRIPPED IN OVERRIDE POSITION, ALL CHECKS GOOD.SDR EIAA98001Throttle · froze upGEG - UNABLE TO RETARD LEFT THROTTLE AT TOP OF DESCENT. COULD NOT MOVE THROTTLE UNTIL DESCENT TO LOWER ALTITUDE AND RAT READS, 15 DEGREE CELSIUS. (M)SDR REXA97281Friction Lock · looseGOT CONFIG WARNING DURING TAKEOFF ROLL. ABORTED TAKEOFF AT 100 KTS. TIGHTENED CONDITION LEVER FRICTION LOCK. (M)SDR CALA9701797Control Cable · wornWHEN REDUCING FROM CLIMB TO CRUISE THRUST, THE LEFT THROTTLE STUCK AT 85 PERCENT N1. A RETURN TO CLE WAS INITIATED AND THE NR 1 ENGINE WAS SHUTDOWN AT 6000 FEET. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE THROTTLE PUSH-PULL CABLSDR 98ZZZX678Control Cable · frozenDFW/ASE - FLT 429 - WHILE IN CRUISE AT FL 310 WITH OAT - -46 C, NOTED NO RESPONSE FROM LT PWR LEVER. WHEN ACFT REACHED FL 280 (OAT - -35 C). AFTER NUMEROUS ATTEMPTS TO FREE LEVER, LEVER BECAME UNSTUCK. ACFT CONTINUED TO ASE. MX GROUNDED ACFT AND INITIATEDSDR 98ZZZX133Control Cable · frozenASE - FLT 429 - WHILE IN CRUISE WITH OAT = -46 DEG C, LOST RESPONSE FROM LT POWER LEVER. MAINT ADVISED TO DESCEND WHEN ACFT REACHED FL 280 (OAT= -35 DEG C). POWER LEVER WOULD MOVE 1 INCH WITH NO CHANGE IN ITT OR TORQ INDICATION. POWER LEVER WOULD THEN SPRINSDR REXA97279Switch · failedAFTER TAKEOFF WHEN GEAR WAS RETRACTED THE GEAR HORN WENT OFF. REMOVED AND REPLACED BOTH POWER LEVER MICROSWITCHES. (M)SDR K3HA9700135Throttle Lever · looseON DESCENT, NR 3 ENGINE FAILED TO RESPOND TO THROTTLE. ENGINE SHUTDOWN BY KIWI PROCEDURES AND A/C LANDED IN NEWARK WITHOUT FURTHER INCIDENT. SHUTDOWN WAS 14 MINUTES WITH POSITIVE OIL PRESSURE. FOUND CROSSOVER SHAFT THROTTLE LEVER NUT BACKED OFF AND LEVER LSDR ASE97005Control Cable · frozenDFW-SAF - WHILE IN CRUISE AT FL 310 WITH OAT EQUALS MINUS CELCIUS EXPERIENCED LACK OF RESPONSE FROM LEFT POWER LEVER WHLE ATTEMPTING TO MAKE MINOR TRIM ADJUSTMENT. MX CONTROL WAS CONTRACTED AND CREW ADVISED THAT THEY WERE GOING TO ATTEMPT TO FREE POWER LEVERSSDR 99ZZZX685Control Cable · malfunctionedON LANDING, NR 1 ENGINE WOULD NOT GO FROM IDLE OFF. SHUT DOWN WAS DONE BY USING FUEL LEVER AND ROTOR BRAKE. WHEN BRAKE WAS APPLIED, RPM WAS TOO HIGH AND R/B CAUGHT FIRE. FIRE WAS PUT OUT AND ENGINE SHUT DOWN. FOUND THROTTLE CABLE BROKEN INTERNALLY. REMOVESDR CA971219005Controls · frozen(CAN) DURING CLIMB ABOVE 12,000 FEET, PROP CONDITION AND POWER LEVERS BECAME DIFFICULT TO OPERATE. SUSPECTED MOISTURE IN TELEFLEX CABLES. UPON DESCENT, BOTH SETS OF CONTROLS BECAME FREE.SDR WRLA97145Control Cable · frozenDURING INITIAL DESCENT, FLIGHT CREW FOUND NR 2 THROTTLE WOULD NOT MOVE, FLIGHT CREW ELECTED TO SHUT DOWN ENGINE IN FLIGHT. ENGINE SHUTDOWN ACCOMPLISHED PER ABNORMAL PROCEDURES. AIRCRAFT CONTINUED TO DESTINATION. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MASDR TWAA9714002Control Cable · wornSTL - FLT 218 - DURING DESCENT, THE LEFT THROTTLE STUCK GOING THROUGH 33,000, IT BROKE FREE DESCENDING THROUGH 28,000 AND OPERATED NORMALLY THE REMAINDER OF THE FLIGHT. REPLACED THE THROTTLE PUSH PULL CABLE. (M)SDR 98ZZZX36Control · failedLOSS OF ENGINE THROTTLE CONTROL CONTRIBUTED TO A FORCED LANDING AND SUBSEQUENT LOSS OF DIRECTIONAL CONTROL. INVESTIGATION DISCLOSED A CRACK IN THE RIGID THROTTLE CONTROL CONDUIT ALLOWING THE FLEXIBLE CONDUIT TO SEPARATE FROM THE FIXED CONDUIT HOUSING. RECOMMSDR CA971219032Cable · contaminated(CAN) LEFT HAND THROTTLE VERY STIFF, ALMOST FROZEN WHEN CLIMBING THROUGH 20,000 FEET. THIS IS A REPEAT SNAG. LEFT HAND THROTTLE CABLE AFT OF THROTTLE CONTROL BOX CHANGED. MOISTURE INGRESS RECTIFICTION SB A601R-76-013B COMPLETED.SDR TWAA9713801Clutch Assy · froze upSTL - FLT 8603 - AFTER LANDING NR 1 ENGINE SHUTDOWN DUE TO THROTTLE LINKAGE FROZEN. REPLACED AUTO THROTTLE CLUTCH ASSY TWA P/N 37221. CHECK C 4-29-97. (M)SDR CA971208007Cable · stiff(CAN) UNABLE TO MOVE LEFT HAND THROTTLE IN-FLIGHT. IT WAS VERY STIFF. THROTTLE CABLE, AFT OF THE THROTTLE CONTROL BOX, RE-ROUTED AND RIGGING CHECKED. PART TC: 3,734.SDR 98ZZZX1546Control Cable · brokenRIGHT THROTTLE CABLE BROKE DURING ENGINE POWER UP. PART TOTAL TIME: 7,358.0 HOURS.SDR GLBA97172Power Levers · out of adjustOHS - ENGINE GOES TO GROUND LOW PITCH IN AIR WHEN POWER LEVERS ARE PULLED BACK. RE-RIGGED ENGINE CONTROLS. (M)SDR VNAA9711006Power Lever · lack of lubeAT FLIGHT LEVEL 220, THE RIGHT POWER LEVER FROZE IN POSITION AT 84 PERCENT TORQUE. THE CREW DECENDED TO FLIGHT LEVEL 110. CONTROL WAS REGAINED AND THE AIRCRAFT WAS LANDED IN LAN WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, CLEANED AND LUBED THE ENGINE CSDR 97UAL900808Bearing · failedRIGHT ENGINE FUEL CUTOFF VALVE SHUT DOWN INDICATION WITH RIGHT ENGINE SHUTDOWN EICAS AND SPEEDS DISPLAYED. ENGINE CONTINUED TO RUN. SUPPLEMENTAL DATA UPDATE FAILED BEARING INSIDE CONDITION MOTOR ACTUATOR .SDR CA971110007Cable · broken(CAN) RT ENGINE CONTROL FAILED ON APPROACH. INVESTIGATION REVEALED BREAK OCCURRED AT COCKPIT END OF THROTTLE CONTROL APPROXIMATELY .25 INCH FROM SWAGED FITTING. BOTH CONTROL CABLES RT AND LT REPLACED.SDR VTZA97608Friction Levers · not setMHT/IAD - FLT 6574 - DURING TAKEOFF ON 10-27-97 AT 0640 HOURS, THE CREW EXPERIENCED A DISCREPANCY WITH THE TOCWS SYSTEM ACTIVATING. THE CREW ABORTED THE TAKEOFF AND TAXIED CLEAR OF THE ACTIVE. CREW THEN NOTICED THE CONDITION LEVERS HAD CREPT BACKWARDS DUE TOSDR PLGA971023BCircuit Breaker · trippedBOS - FLT 4319 - AFTER TAKEOFF THE FLIGHT IDLE OPEN LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET SYSTEM CIRCUIT BREAKER AND SYSTEM CHECKED GOOD. (M)SDR UPS97225068Bracket · crackedINSPECTION TYPE-D, SUSPECT CRACK ON CONTROL QUADRANT SUPPORT BRACKET IN L/E OF NR 1 PYLON BRACKET. REPLACED IAW MM 76-12-41.SDR REXA97257Control Cable · failedUPON REMOVING THE CONTROL QUADRANT FOR A MAINTENANCE ACTION IT WAS DISCOVERED THAT THE OPERATING CABLE FOR THE FI STOP OVERRIDE HAD SEPARATED FROM THE OVERRIDE CONTROL ACTUATOR SWITCH. RETURNED TO VENDOR. (M)SDR 97FDEA00722Throttle Rod · failed97-0200 - NR 1 ENGINE ROLLED BACK. NR 1 ENGINE WAS SHUTDOWN IN ACCORDANCE WITH RED TABS. ALT FL310. N1 50.0 PERCENT EGT 380 N2 75 PERCENT FF 2160. NOTE: WENT TO IDLE NO THROTTLE RESPONSE.OPEN FAN COWL ON NR 1 ENG AND FOUND THE THROTTLE ROD DISCONNECTED FRSDR SCNA97340Bolt · missingDURING CLIMBOUT, COULD NOT ADVANCE NUMBER 2 ENGINE THROTTLE PAST 85 PERCENT N1. AT TOP OF CLIMB, N1 WAS AT 99 PERCENT AND COULD NOT PULL BACK POWER. SHUT DOWN ENGINE FOR PRECAUTIONARY REASONS. FOUND FUEL CONTROL ROD FOR THROTTLE, FORWARD END, MISSING BOLT. SDR 9718839301Control Cable · damagedDURING DESCENT AS THROTTLES WERE ADVANCED, THE LEFT ENGINE WAS UNRESPONSIVE TO THROTTLE MOVEMENT AND REMAINED AT IDLE POWER LEVEL. AIRCRAFT LANDED AT IND WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE THROTTLE CABLE, OPERATIONAL CHECK OK.SDR 97ZZZM1080Eiu · inoperativeDURING CLIMB-OUT OF PVR TO ORD, AIRCRAFT EXPERIENCED A NR 1 EIU FAULT FOLLOWED BY A AUTO THRUST AND NR 1 AND NR 2 PACK FAULTS. AIRCRAFT DIVERTED TO DGO. DURING DESCENT OXYGEN MASKS DROPPED. REMAINDER DESCENT LANDING WAS WITHOUT INCIDENT. (M)SDR MALA975673Idle Stop Light · illuminatesFLT 3410 - AFTER GEAR RETRACTION AFTER TAKEOFF, THE FLIGHT IDLE STOP LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW. CURRENTLY, A DEFERRED ITEM. (X)SDR 97ZZZX5112Cable Assy · partedDURING PRE-FLIGHT OPERATIONAL CHECKS, THE LEFT ENGINE THROTTLE CABLE STAINLESS STEEL RIBBON CORE PARTED WHERE THE CABLE PASSES THROUGH A CUT-OUT IN THE AILERON BELLCRANK RT MOUNTING BRACKET. ENGINE CONTROL WAS LOST AND THE MISSION ABORTED. INVESTIGATION REVESDR MALA975621Switch · out of adjustFLT 3294 - FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO MSP. MAINTENANCE RESET FLIGHT IDLE STOP OVERRIDE SWITCH. RAN AIRCRAFT FLIGHT IDLE STOP, OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. (X)SDR TC8A97045Power Lever · lack of lubeUPON START OF TAXI OUT, UNABLE TO MOVE NR 1 THROTTLE FOWARD OF IDLE. SHUT DOWN ENGINE, POWER LEVER BINDING. LUBRICATED POWER CONTROL DRUM IN NR 1 PYLON. CHECKED PYLON CABLES AND COCKPIT MECHANISM AND CABLES FOR DEBRIS, NO DISCREPANCIES NOTED. AFTER LUBE, NSDR GAIA9742Comp Rod Mount · looseMMMY/IAH - FLT 727 - ON APPROACH TO IAH, THE FLIGHT CREW DISCOVERED THE NR 3 ENGINE THRUST LEVER WAS STUCK IN THE MID-POSITION. AN EMERGENCY WAS DECLARED AND THE ENGINE WAS SHUT DOWN. AN UNEVENTFUL LANDING WAS MADE AT IAH. INVESTIGATION REVEALED THE COMPENS
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