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 02210176Screw · loosePILOT REPORTED THAT LT ENGINE RPM CONTINUED TO DECREASE IN FLIGHT. ON APPROACH, ELECTED TO SHUT THE LT ENGINE DOWN. UPON INSPECTION, IT WAS DETERMINED THAT THE LT ENGINE RPM ADJUSTING SCREW SELF LOCKING INSERT WAS LOOSE, ALLOWING SCREW TO BACK OFF DUE TO SDR MWEA010163Throttle Cable · stuckSTARTED DESCENT FROM FLIGHT LEVEL 350 AND LEFT THROTTLE STUCK AT 80 PERCENT N2. THROTTLE FREED UP PRIOR TO LANDING. MAINTENANCE DISASSEMBLED LEFT THROTTLE CABLE, CLEANED AND LUBRICATED INNER ELEMENT. ALSO FOUND CABLE CLAMPED IN A WAY CAUSING MISALIGNMENT. SDR ERYA682D3Throttle Cable · frozenDURING FLIGHT FROM KLGA TO CYYZ AT FLIGHT LEVEL 310, THE RIGHT ENGINE THROTTLE FROZE IN POSITION. THE AIRCRAFT DECENDED TO 14000 FT. DURING THE APPROACH, THE THROTTLE WAS STILL FROZEN SO THE RIGHT ENGINE WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED. THE AIRCSDR AU010127Cable · damaged(AUS) ENGINE THRUST CONTROL SYSTEM CABLES, PULLEYS AND FITTINGS DAMAGED. FOUND DURING INSPECTION IAW AD/B747/229 AND FAAAD/2000-05-30 AMDT39-11640.SDR MALA010153Power Lever · undertorquedLT AND RT ENGINE WILL ONLY MAKE 72 PERCENT TORQUE WITH POWER LEVERS FIREWALLED. AT FL210 WHILE SETTING POWER FOR TREND TRIED TO SET TORQUE TO 74 PERCENT, PL''S MAXED OUT AT 73 - 74 PERCENT AFTER RAM RISE. MAINTENANCE COMPLETED GPA RUNS WITH BOTH ENGINES, FOUSDR CA010301007Cable · damaged(CAN) DURING SCHEDULED INSPECTION OF THE NR 2 ENGINE, THE LOWER POWER CONTROL CABLE WAS FOUND TO BE BLENDED TO MAX ALLOWABLE LIMITS IN THE AREA OF CONTACT WITH THE STEEL PULLEY JUST FORWARD OF THE FIREWALL. THE CABLE WAS REPLACED AND THE AIRCRAFT WAS RETURNED SDR MEX2002021Spring · failedFLT 587 - MEX-CUN - RETURN TO PLATFORM DUE TO THAT THE FUEL CONTROL LEVER DOES NOT LOCK AND AUTOBRAKE SYSTEM O/S. SPRING OF THE FUEL LEVER WAS CHANGED IAW MM 76-10-01 AND AIRCRAFT DISPATCH IAW MEL 32-9. AT RON IN MEX 26/27 THE SOLENOID PRESSURE SWITCH NR 1 ASDR USAASB1017Throttle Cable · failedEWR - FLT 1024 - EN ROUTE FROM DCA TO ALB, THE NR 2 THRUST LEVER STUCK AT CLIMB POWER. CREW DISENGAGED AUTO THROTTLES BUT WAS STILL UNABLE TO RETARD THRUST LEVER. CREW DECLARED AN EMERGENCY, ACCOMPLISHED ENGINE SHUTDOWN CHECKLIST AND SHUTDOWN THE NR 2 ENGINESDR MALA010299Clip · misinstalledFOUND DURING C-CHECK, BY AIR ALTANTIC, IN ST JOHNS, NF. NR 1, 2, AND 4 THROTTLE CABLE TURNBUCKLES FOUND NOT SAFETIED PROPERLY IN FUSELAGE. SAFETY CLIPS TO BE INSTALLED. MAINTENANCE SAFETIED RN 1, 2, AND 4 TURNBUCKLES PN MS21256-1 IAW STANDARD PRCTICES.SDR MALA010298Turnbuckle · out of adjFOUND DURING C-CHECK, IN ST. JOHNS, NF. NR 3 THROTTLE CABLE TURNBUCKLE FOUND BACKED OFF BEYOND LIMITS (6 THREADS EXPOSED) REQUIRES ADJUSTMENT AND RETENSIONING. REF: MM 76-11-00 BLOCK 501(FUSELAGE TURNBUCKLES). MAINTENANCE ADJUSTED NR 3 THRUST CONTROL CABLE TUSDR AU010042Cable · loose(AUS) ENGINE THROTTLE CABLE OUTER CONDUIT DISCONNECTED AT FIREWALL. THE NUT SECURING THE CONDUIT HAD NO LOCKWIRE.SDR CA010125008Cable · worn(CAN) DURING SCHEDULED ENGINE INSPECTION, THE NR 1 ENGINE LOWER CONDITION LEVER CABLE WAS FOUND TO BE WORN TO LIMITS IN THE USUAL PLACE, FORWARD OF THE FIREWALL. THE CABLE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR AU001252Control Box · damaged(AUS) NR 1 ENGINE FFR THROTTLE CONTROL BOX RACK DAMAGED.SDR AU001259Cable · contaminated(AUS) NR 4 ENGINE THROTTLE CABLE CONTAMINATED WITH DIRT AND STIFF IN OPERATION.SDR C1HA200093007Throttle · binding#1 eng throttle binding.Do not have full motion.ACTION TAKEN:checked rig and lubed throttle quadrant. OPs checked goodSDR CA010112004Cable · seized(CAN) R/H POWER LEVER CABLE GOING FROM PEDESTAL TO FIRST JOINT FOUND TO BE SEIZED. POWER LEVER REQUIRED GREAT FORCE TO OPERATE. CABLE REPLACED REPLACED. OLD CABLE FOUND TO BE KINKED INTERNALLY.SDR 00FDEA00884Throttle · stuck00-363 PRIOR TO TOP OF DESCENT NR 1 THROTTLE BECAME STUCK AT 95 PERCENT NL. ** S/D ** R&R NR 1 ENGINE THROTTLE DRUM AND FUEL SHUTOFF SECTOR RAN ENGINE CK GOOD PER JRH.SDR CA010108002Cable · frayed(CAN) DURING SCHEDULED ENGINE INSPECTION. THE NR 2 ENGINE LOWER CONDITION LEVER CABLE WAS FOUND WITH TWO BROKEN STRANDS AT THE POINT WHERE THE CABLE RIDES ON THE ENGINE COMPARTMENT PULLEY WITH THE CONTROL SELECTED TO THE MIN GOVERNING POSITION. THE CABLE WAS RSDR CA001218021Throttle Cable · failed(CAN) A/C WAS BEING PREPARED FOR THE DAYS FLYING WHEN THE PILOT NOTICED THE THROTTLE WAS STIFF. HEAT WAS APPLIED TO THE CABIN AS IT WAS -22 DEGREES OAT. THE CABLE GOT STIFFER AND FAILED. THE INTERNAL CABLE FAILED AT SWAGGED END BY THE THROTTLE HAND KNOB. THE SDR 20010117AP002Control Cable · seizedLEFT THROTTLE CABLE FROZEN IN FLIGHT-INSPECTION REVEALED THAT CHAFFED ELECTRICAL WIRE CONTACTED THROTTLE, THROTTLE SIEZED IN PLACE.SDR CA001218014Lever · worn(CAN) LEVER THAT ATTACHES POWER LEVER CONTROL ROD TO FCU ON ENGINE SLIPPPED WHEN L/H POWER LEVER WAS BROUGHT FROM REVERSE INTO IDLE, CAUSING N1 TO READ 3% HIGHER THAN NORMAL.INSPECTION OF LEVER SHOWED NO ABNORMALITIES, ONLY THING NOTED IS INSIDE BORE OF LEVER SDR CA001207017Control Arm · broken(CAN) THE LEVER BROKE AT THE DETENT PLATE IN THE COCKPIT PEDESTAL AREA WHEN THE CONDITION LEVER WAS OPERATED AT START-UP OF THE ENGINE. (X)SDR MALA000678Lever · stuckRIGHT POWER LEVER STUCK AT 55 PERCENT POWER. SHUT DOWN RIGHT ENGINE. ON DESCENT RIGHT POWER LEVER STUCK WITH TORQUE AT 60 PERCENT. SHUT DOWN RIGHT ENGINE, COMPLETED ORH. REPLACED QUADRANT WITH SERVICEABLE UNIT. P/N OFF 53710-6, ON 53082-14, S/N OFF 0-179SDR COMA0060961Amplifier · malfunctionedPOWER LEVER SPLIT IN FLIGHT. REPLACED THE N1 CONTROL AMPLIFIER.SDR AU001097Pin · sheared(AUS) THROTTLE FRICTION ADJUSTMENT SHAFT SPLIT PIN SHEARED DURING FRICTION ADJUSTMENT. FOUND DURING INVESTIGATION OF EXCESSIVETHROTTLE FRICTION AND AD/BN-2/69. (X)SDR 20010112SG065Connecting Rod · out of adjFLT 9137 - FLL - DURING FLIGHT, LEFT ENGINE SURGES THREE TIMES AT DIFFERENT POWER SETTINGS. ENGINE SHUTDOWN AND SECURED. ADJUSTED GOVERNOR INTERCONNECT ROD. OPERATIONAL CHECK NORMAL. (M)SDR CA001129036Pin · failed(CAN) DURING DISASSEMBLY OF THROTTLE QUADRANT TO COMPLY WITH BOMBARDIER SB 604-76-001/RATHER FIGEAL SB FE210-76-01 IT WAS FOUND THAT PIN 160 HAD MIGRATED OUT OF LATCH ASSEMBLY. THIS PIN IS A PRESS FIT AND WE FOUND IT COULD BE REMOVED BY HAND. IF THIS PIN IS RESDR 20001207SH009Throttle Arm · failedRIGHT THROTTLE ARM, PN 632555-35, FAILED PER DRAWING. THIS IS AT LEAST 10 TIMES ON 10 DIFFERENT AIRPLANES IN PAST 8 YEARS THIS PART OR SAME P/N MIXTURE ARM HAD FAILED. NEEDS SB OR AD. (X)SDR CA001123006Throttle Cable · failed(CAN) THROTTLE CABLE SHEATH DETACHED FROM END FITTING. THROTTLE STUCK IN THE OPEN POSITION 00-10-09.CABLE REPLACED.SDR CA011120006Throttle Cable · chafed(CAN) CABLE CHAFED THROUGH AT ENGINE DECK, OPENING IN ENGINE DECK PRESSURE SEAL INCREASED TO PREVENT RE-OCCURRENCE.SDR 20001030SH008Throttle Cable · brokenSDF - RIGHT ENGINE THROTTLE CABLE BROKEN ON APPROACH INTO SDF. REMOVED AND REPLACED CABLE ASSY. OK FOR SERVICE. (X)SDR CA000925022Control Cable · worn(CAN) DURING ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE #1 ENGINE LOWER CONDITION CONTROL CABLE WAS WORN BEYOND LIMITS AT THE STEEL PULLEY IN THE ENGINE COMPARTMENT. THE CABLE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR COMA0010365Switch · brokenAUTOFEATHER WARNING DURING TAKEOFF ROLL, AIRCRAFT RETURNED TO THE GATE. REPLACED BROKEN MICRO-SWITCH ON THE LEFT POWER LEVER.SDR VNAA0009008Power Lever · stuckTHE CREW ADVANCED POWER FOR TAKEOFF, THE LEFT HAND LEVER WAS STICKING. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECT AND LUBRICATED THE LEVER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED SDR AU000820Pin · damaged(AUS) THROTTLE FRICTION ADJUSTER SHAFT SPLIT PIN DEFORMED AND PARTIALLY SHEARED. (X)SDR CA000925015Actuator · failed(CAN) THE FLIGHT CREW REPORTED THAT NR 3 ENGINE LOW OIL PRESS LIGHT CAME ON AFTER LANDING. THE ENGINE HAD SHUT ITSELF DOWN DURING THE LANDING. INVESTIGATION REVEALED THAT THE NR 3 ENGINE TMS ACTUATOR HAD FAILED OUT OF THE CENTRED POSITION, CAUSING THE ENGINE TSDR 20000908SH002Throttle Cable · separatedAFTER TAKEOFF DURING POWER REDUCTION, RIGHT THROTTLE WOULD NOT DECREASE BELOW 20 INCHES MANIFOLD PRESSURE. AIRCRAFT RETURNED TO BASE UNEVENTFULLY. INSPECTION REVEALED THROTTLE CABLE SEIZED AT ENGINE SIDE WHERE CABLE EMERGES FROM OUTER SHEATH. THE OUTER SHEATHSDR CA000927011Rod End · worn(CAN) DURING TAKEOFF OUT OF SANDY LAKE, THE PILOT NOTICED NR 1 THROTTLE SETTING LOOSE. HE ABORTED THE TAKEOFF AND SHUT DOWN THE ENGINE. UPON INSPECTION, IT WAS FOUND THAT THE JAM NUT CAME LOOSE, AND WORE THE THREADS OUT OF THE ROD END. (X)SDR AU000731Power Lever · stuck(AUS) NR 3 ENGINE THRUST LEVER STUCK AT CRUISE POWER. INVESTIGATIONCOULD FIND NO CAUSE OF DEFECT.SDR AU000694Control Cable · worn(AUS) ENGINE THRUST CONTROL CABLES TLA-2 AND TRA-2 LOCATED IN THE RHFORWARD CARGO HOLD WERE WORN BEYOND LIMITS. FOUND DURING INSPECTION IAW AD/B767/118.SDR AU000643Control Cable · worn(AUS) ENGINE THRUST CONTROL CABLES PN TLA2 AND PN TRA2 WORN BEYOND LIMITS. FOUND DURING INSPECTION IAW AD/B767/118.SDR AU000623Power Lever · damaged(AUS) AFTER TAKEOFF ERRATIC ENGINE INDICATIONS WERE OBSERVED ON THE RT ENGINE INSTRUMENTS. ENGINE WAS SHUT DOWN. SUBSEQUENT INVESTIGATION INCLUDED RIGGING CHECK, SPEED LEVER FRICTION CHECK AND ENGINE GROUND RUNS. FAULT COULD NOT BE DUPLICATED. SUSPECT THE SPEESDR CA000919003Gearbox · failed(CAN) FLIGHT NR 5743 FROM CVG TO CLT, THE FLIGHT CREW REPORTED: IN FLIGHT (DESCENT), NR 2 ENGINE, THE N2 SET AT 82%, DID NOT RESPOND THE THRUST LEVER MOVEMENT. SHUT ENGINE DOWN IN FLIGHT, ECLRED EMERGENCY LANDING WITH NR 1 ENGINE ONLY, LANDING WAS UNEVENTFUL. SDR DL72S001659Rod · brokenA/C WAS IN CRUISE AT FL 280 WHEN A LOSS OF THRUST CONTROL OCCURRED ON NR 3 ENGINE. ENG DID NOT RESPOND TO ANY THROTTLE INPUTS. IN-FLT SHUTDOWN WITH ENGINE AT 2.65 EPR N1 101 N2 100 EGT 630. FOUND BROKEN CONTROL ROD= PYLON QUADRANT TO CROSS OVERSHAFT. REPLASDR CA001005013Cable · missing(CAN) NR 1 ENGINE THROTTLE LEVER BINDING WILL NOT GO INTO IDLE POSITION & REVERSE ISNOT SELECTABLE. NR 1 ENGINE THROTTLE CABLE REPLACED DUE TO HEAT DAMAGE. CHANGED AS PER I.A.W. & M.M. 76-11-41. 3. HALF CLAMP & BUSHING FOUND MISSING ANTI-ICING VALVE REPLACESDR 20000912SH022Roller · detachedTHE PIN THAT HOLDS THE ROLLER FOR POSITIVE THROTTLE DETENTS FAILED COMPLETELY AND THE ROLLER AND PIN ASSEMBLY FELL INTO THE THROTTLE QUADRENT. SINCE THE QUADRENT IS IN AN OVERHEAD POSITION, THERE WAS NO THROTTLE RESTRICTION WITH THIS FAILURE. (X)SDR 20000829SH012Throttle · brokenPILOT STARTED TO REDUCE POWER IN ORDER TO LOSE ALTITUDE. AT THIS TIME, THE THROTTLE CABLE BROKE CAUSING A LOSS IN ENGINE POWER. PILOT MADE SAFE LANDING IN A REMOTE FIELD. UPON INSPECTION, MAINTENANCE PERSONNEL FOUND THROTTLE CABLE BROKEN JUST ABOVE THE CABLSDR QXEA00002048Switch · dirtySEA- AUTOFEATHER ARM LIGHT CAME ON IN CRUISE FLIGHT WHILE NOT SELECTED. APPEARED TO BE ASSOICATED WITH THE SWITCH IN THE POWER LEVER QUADRANT. MAINTENANCE RESEATED THE ADVISORY CONTROL BOX AND CLEANED THE POWER LEVER SWITCHES IN THE QUADRANT. OPERATIONAL CHSDR 20000811SH003Nut · failedINSTALLED LYCOMING FACTORY REBUILT ENGINE IAW PIPER PA-46-310/350 MM 71-00-00, PG 19-22(A) (8). SECURED ENGINE CONTROL WITH SELF-LOCKING NUTS PER PIPER PRACTICES. AFTER LANDING, ON FIRST FLIGHT, THROTTLE CONTROL WAS LOST DUE TO LOSS OF HARDWARE AT THROTTLE TSDR CA000719019Cable · separated(CAN) DURING CRUISE FLIGHT, THE RIGHT THROTTLE CABLE FAILED RESULTING IN A FULL THROTTLE CONDITION. THE ENGINE WAS SHUT DOWN AND SECURED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. THE THROTTLE CABLE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.
Back to JASC 7603