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 = '6100' 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 = '6100' 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 JJBA200961510Signal Cond Unit · false indicationAFTER TAKEOFF NR2 PROP BEGAN SURGING BETWEEN 1200 AND 1600 RPM. SHUTDOWN NR2 ENGINE, AND RETURNED TO FIELD. ENGINE PARAMETERS WERE NORMAL BEFORE SHUTDOWN. WE ARE WORKING WITH MFG ON THIS PROBLEM (BETA LOCK-OUT). WE HAVE ALREADY CHANGED PCU AND OVER SPEED GOSDR CA090320001Drain · clogged(CAN) WHILE TROUBLESHOOTING A RT PROPELLER SHAFT LEAK MX FOUND 2 DRAIN HOSE LINES CLOGGED WITH OLD COKED OIL (LINES ARE LOCATED ADJACENT TO THE HOT SECTION OF THE ENGINE). ONE HOSE WAS ABLE TO BE CLEARED. HOSE P/N AE7013107G0180 (IPC REF CH 71-70-00 FIG 20 ISDR QXEA2008120401217Unknown · unknownPDX- NR 1 PROP APPEARS SLOW TO COME OUT OF FEATHER. C/W AMM TASK 61-20-00-720-801 "FUNC TEST OF PROP TIME TO UNFEATHER" TWICE. NR 1 PROP UNFEATHERED AT AROUND 17 SECONDS BOTH TIMES (WITHIN 30 SECOND LIMIT). ALSO C/W OSG TEST IAW TASK 61-20-00-710-804. OPS SDR CA081125011Sleeve · damaged(CAN) WHILE IN THE VFR PATTERN THE ACFT EXPERIENCED A LOSS OF POWER ACCOMPANIED BY A CHIP LIGHT. THE ENG STABILIZED AT A REDUCED POWER SETTING AND 85 PERCENT NP AND THE CREW MADE AN EMERGENCY LANDING. AN INSP OF THE PROPELLER TRANSFER SLEEVE REVEALED BLUING. TSDR CA081014001Shaft · cracked(CAN) EIR PW100-0477 CRACKED PROPELLER SHAFT.SDR 2008F00020Rod · misinstalledON INSTALLATION OF PROP TO ENG MOUNTING FLANGE IAW MM 61-00-45, THE PLASTIC PROTECTIVE CAP FITTED TO THE END OF THE PITCH CHANGE ROD WAS NOT REMOVED. ON FLIGHT TEST OF THE AC, ENGINE OVERSPEED WAS NOTED AT TAKEOFF TO 2850 RPM, NO SIGNIFICANT LOSS OF OIL PRESSSDR SIMA200814904Unknown · malfunctionedON FLIGHT 3229 ON TAKEOFF CREW REPORTED LEFT ENGINE PROP OIL TEMP AT 100FT AT BEGINNING OF TAKEOFF ROLL. LEFT PROP RPM WOULD NOT GO BELOW 1200 RPM AFTER ABORT TAKEOFF WHEN CONDITION LEVER AT "MIN". ALL OTHER INDICATIONS NORMAL. AIRCRAFT REMOVED FROM SERVICESDR 2008FA0000467Snap Ring · missingPROPELLER WAS INSTALLED IMPROPERLY. SNAP RING THAT HOLDS ON PROP NUT AND CRANKSHAFT EXTENSION WAS NOT INSTALLED. THIS ALLOWED CRANKSHAFT EXT TO UNSCREW AND LET PROP GOVERNOR PRESSURE OF 180 LBS TO BE PUT ON ENGINE AND PROPELLER. THIS CAUSED PROPELLER AND ENSDR 2008FA0000177Relay · burnedUPON LANDING A POWER/ TORQUE SURGE OF THE LT ENGINE WAS ENCOUNTERED. THE INCREASED THRUST FROM THE LT SIDE AND ICE COVERED RUNWAY CONDITIONS CAUSED AN OFF RUNWAY INCURSION. INVESTIGATION OF THE GROUND FINE SOLENOID SYSTEM RESULTED IN A BURNED K4 RELAY ON THESDR 2007FA0000867Screw · unsafetiedHAVE SEEN THIS ATTACHMENT ARRANGEMENT ON MANY AC. FOUND NON SAFETIED SCREWS ATTACHING PROPELLER DEICE BRUSH ASSY TO MOUNTING. REMOVED NON SAFETIED SCREWS WITHOUT LOCKING DEVICES WITH MS35265-44 SCREW THAT CAN BE LOCKED WITH SAFETY WIRE. (K)SDR SIMA200722503None · noneRIGHT PROPELLER VIBRATION, RETURNED TO DFW. PERFORMED DYNAMIC BALANCING OF THE RIGHT PROPELLER ASSEMBLY IAW SAAB AMM 61-10-00. BALANCE LEVEL ACCEPTABLE AT 0.127 IPS. AIRCRAFT RETURNED TO SERVICE.SDR QXEA200701124Unknown · unknownPDX FLIGHT NR 2466: DURING CLIMB, NR 2 PROP DROPPED TO 890 WHILE NR 1 REMAINED AT 900. PILOT TAPPED NR 2 CONDITION LEVER IN DETENT AND RPM RETURNED TO 900. ONE MINUTE LATER, NR 2 RPM JUMPED TO 910 RPM AND POWER PLANT MESSAGE APPEARED ON ED. MESSAGE REMAINEDSDR 2007FA0000567Line · leakingBAD OIL LEAK: DETERMINED METAL ID PLATE ON MP HOSE WORE HOLE INTO PROP UNFEATHERING ACCUMULATOR TUDE. NOTE: THIS IS THE SUBJECT OF AD 2007-06-07 AND MANDATORY SB 61-3806 BUT DOES NOT COVER THIS AC SN. (K)SDR CA070608004Unknown · cracked(CAN) PROPELLER RECEIVED FOR INSPECTION IAW AD 2003-12-05. INSPECTION FOUND CRACK INDICATIONS IN PREVIOUSLY REPAIRED AREAS. PROPELLER HAS BEEN REMOVED FROM SERVICE IAW THIS AD AND ASB 221C. (TC NR 20070608004)SDR QXEA200700822Unknown · unknownSEA FLIGHT NR 2053, DURING NORMAL SINGLE ENGINE TAXI WITH NR 1 PROP FEATHERED POWER LEVERS SET BETWEEN DISC AND FLIGHT IDLE. UPON MOVING NR 1 CONDITION LEVER FROM START/FEATHER TO MAX, NR 1 TORQUE INCREASED RAPIDLY TO 30 PERCENT TORQUE. ENGINE STABILIZED AFTSDR 2007FA0000464Bolt · shortINSPECTING PROPELLER DURING ANNUAL, FOUND PROPELLER BOLTS 0.25 IN SHORT OF BACK SIDE OF FLANGE INSERTS. ALL BOLT THREAD ENGAGEMENT WAS FORWARD OF INSERT BOSS. AFT .2500 INC OF INSERT, MATERIAL BEHIND CRANK FLANGE, HAD NO THREAD ENGAGEMENT. WRONG BOLTS INSTASDR 2007FA0000269None · unknownAIRCRAFT HAS RAISEBECK STC SA3593NM INSTALLED WHICH STATES THE PROPS ARE NOT TO BE OPERATED BELOW THE SET MINIMUM RPM. PRE PHASE INSPECTION RUNS REVEALED THIS CONDITION. IAW MFG SERVICE LETTER 61-254 THIS CAN CAUSE NO REACTION MODE VIBRATORY RESONANCE AND MASDR CA061212002Propeller · damaged(CAN) IN CRUISE AT FL240 AFTER DEPARTURE THE CREW OBSERVED LOW OIL QTY ON NR 2 ENGINE. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT CONTINUED TO DESTINATION. SHORTLY AFTER RE-ESTABLISHING CRUISE AT FL220 THE CREW OBSERVED LOW OIL QTY ON NR 4 PROPELLER. THE PROP SDR 2007FA0000099Propeller · crackedCRACK DETECTED LENGTHWISE AT 9 INCH STATION. LATEST LOGBOOK ENTRY FOR TSOH, DATED 7-28-2005. (SW15200706340) (K)SDR DAT2006F00009Attach Bolt · brokenDURING THE SCHEDULED MAINTENANCE, THE PROP TORQUE WAS COMPLIED WITH ON THE RT SIDE, AT 30311.5 TAT AND 37942 TAC. THE INSPECTION FOUND (1) BROKEN PROP ATTACHMENT BOLT. THE PROPELLER WAS REMOVED IAW MM. THE PROPELLER WAS INSPECTED AND FOUND TO BE WITHIN THE SDR 2006FA0001028Bearing · brokenUPON DISASSEMBLY OF THIS PROPELLER IAW WITH MFG TECH REPORT NR940. IT WAS DISCOVERED THAT THE PITCH CHANGE LINK BUSHINGS, P/N A4564, ON BLADES NR 2 AND NR 3 WERE BROKEN AND PARTIALLY MISSING. AT LEAST 50 PERCENT OF THE BUSHINGS WERE NOT IN THE LINK. THE THICKNSDR 2006FA0000707Line · chafedLT PROPELLER ACCUMULATOR OIL LINE WAS CHAFED THROUGH BY THE SHROUD FOR THE FUEL PUMP HOSE. OIL LEAK WAS OBSERVED. THE CAUSE WAS DETERMINED AND REMEDIED BEFORE LOSS OF SIGNIFICANT AMOUNT OIL.SDR 2006FA0000706Line · chafedLT PROPELLER ACCUMULATOR OIL LINE WAS CHAFED BY THE SHROUD FOR THE FUEL PUMP HOSE.SDR 2006FA0000705Line · chafedLT PROPELLER ACCUMULATOR OIL LINE WAS CHAFED BY THE SHROUD FOR THE FUEL PUMP HOSE.SDR WVB2006F00001Propeller · unserviceableWHILE PERFORMING A DETAILED INSPECTION OF THE RT PROPELLER ON 4/7/06. THE MECHANIC LUBING THE PROPELLER FOUND LIQUID BEING FORCED OUT OF THE ZERK HOLE BY THE GREASE BEING PUMPED INTO THE HUB. THE APPROXIMATE AMOUNT OF LIQUID WAS 2 TO 3 TABLESPOONS OF WHAT APSDR QXEA200600907Brush Block · malfunctionedGEG FLIGHT NR 400, RIGHT AC BUS, RTRU, RIGHT STALL WARNING, NR 2 SPU AUXILLARY POWER, RIGHT ELEVATOR HORN HEAT CAUTION LIGHTS ILLUMINATED IN CRUISE. COMPLETED ASSOCIATED CHECKLIST, NO CHANGE, MAINTENANCE ADVISED TURN PROP HEAT OFF AND RESET NR 2 AC GENERATOR.SDR MALA060156Propeller · ground damagePROP BLADE SUSTAINED DAMAGE BY CONTACT WITH PASSENGER'S STROLLER. THE AIRCRAFT IS CURRENTLY BEING EVALUATED FOR DAMAGE ASSESSMENT. RAMP AGENT LOST CONTROL OF BABY STROLLER IN HIGH WIND CONDITIONS AND IT HIT THE RT PROP WHILE ENGINE WAS RUNNING. REPLACED PROSDR 77669Hub · corrodedCORRODED CLAMP ASSEMBLY, PN 838-17, SN J4324, U4701, U4646. CORRODED BLADES MODEL NR 9349, SN A41967, A41996, A41251.SDR AU510002187Retaining Ring · missingENGINE PROPELLER SHAFT ADAPTER PLUG RETAINING RING MISSING. ADAPTER PLUG P/N 3013146 DISLODGED AND LOOSE IN THE PROPELLER SHAFT INTERNAL BORE. RETAINING RING COULD NOT BE FOUND. SUSPECT RETAINING RING HAD NOT BEEN INSTALLED. PERSONNEL/MAINTENANCE ERROR. ASDR 2005FA0001569Propeller · out of limitsPROPELLER SUBMITTED FOR INSPECTION IAW AD 03-12-05. DURING SB RESEARCH IT WAS DISCOVERED THAT AD WAS DUE AS SN IS LISTED IN AD. DURING INSPECTION FOR AD, THE PROPELLER WAS FOUND UNDER MINIMUM WIDTH. PROPELLER IS SCRAP. (K)SDR CA051007002Manual · inaccurateAFTER REVIEWING PRODUCTION FLT TEST PROCEDURE, IT WAS FOUND THAT NO MENTION OF PROP BOLTS TQ CHECK AFTER FIRST FLT AS RECOMMENDED BY MT PROPELLER DOCUMENT. AFTER REVIEWING MM , IT WAS FOUND THAT PROP BOLTS TQ CHECK AFTER FIRST 25HRS OF OP AS RECOMMENDED BY MTSDR 2005FA0001362Spring · failedPROPELLER WAS INSTALLED ON RT SIDE OF AC, THE PROP WENT FEATHER, UNCOMMANDED ON ENGINE SHUTDOWN. PROPELLER WAS REMOVED FROM AC FOR INSPECTION AND WAS RECEIVED WITH THE BLADES IN FEATHER, LOGBOOK WAS NOT SUPPLIED. ALL INFO VIA PHONE. PROP CYLINDER WAS REMOVEDSDR CA060119001Gear · failed(CAN) ON SHUTDOWN, PILOT HEARD A REPETITIVE SOUND, FROM THE LT ENGINE. INVESTIGATION SHOWED THE PROP GEAR HAD TEETH MISSING. EVIDENCE, METAL TEETH PIECES IN OIL SCREEN. NO RESISTANCE IN PROP ROTATION FOR ABOUT 10 DEGREES. ENGINE REPLACED, AIRCRAFT RETURNEDSDR TRBA2005057Switch · defectiveAUTOMATIC TAKE-OFF POWER CONTROL SYSTEM (ATPCS) DID NOT ARM DURING TAKE-OFF POWER. REPLACED DEFECTIVE SWITCH. (K)SDR 2005FA0000933Washer · improper partWHILE PERFORMING SB WHICH INCLUDES PROPELLER, REMOVING THE MOUNTING PLATE FROM THE SLIP RING, FOUND THAT THE WASHERS USED TO HOLD THESE ITEMS TOGETHER ARE TOO WIDE AND SCORED, THE PROP HUB. WERE ABLE TO POLISH OUT THE SCOPE MARKS ON THE HUB AND MODIFY THE WASSDR 2005FA0000638Spring · stretchedSPRING ASSY STRETCHED TOO LARGE. (K)SDR 2005FA0000190Fork · crackedNDT SHOWS CRACKED IN 2 PLACES ON FORK. (K) (REF: 12235)SDR DAT2004F00003Bolt · crackedDURING SCHEDULED AINT AD86-06-02 (PROP TORQUE) WAS COMPLIED WITH ON THE LT SIDE. ONE PROP ATTACHMENT BOLT, PN B3339 WAS FOUND LOOSE AND ONE BROKEN. ALL EIGHT (8) PROP ATTACHMENT BOLTS (PN B3339) AND WASHERS (PNA20482) WERE REMOVED AND REPLACED WITH NEW ONES SDR FYO2004F00000Propeller · malfunctionedPILOT STATED THAT DURING CRUISE FLIGHT, PROPELLER WENT TO FINE PITCH, AND OPERATION OF GOVERNOR CONTROLS HAD NO EFFECT. UPON GROUND RUN UP IT WAS FOUND THAT PROP WOULD NOT CYCLE. REMOVED FROM SERVICE. UNKNOWN CAUSE FOR FAILURE AT THIS TIME. (AL05200401344)SDR HNAA0400080Engine · out of rigAFTER TAKEOFF NR 2 ENGINE SURGED, POSSIBLE BETA LOCKOUT FAILURE. OPERATED PROP AT 900 RPM AND SURGE DISSIPATED. DEACTIVATED BETA LOCKOUT SYSTEM. RIGGED NR 2 ENGINE PER W/C 76-00-02Q REACTIVATED BETA LOCK OUT C/W W/C 61-20-10Q BETA LOGIC OPS CHECK BETA LOCKOSDR CA040820003Shaft · seized(CAN) RETURNING FROM A FIRE ACTION, IN CRUISE AT 9500 FEET ASL, THERE WAS A LOSS OF POWER FROM THE RT ENGINE ACOMPANIED BY VIBRATION AND NOISE. THE RT ENGINE SHUT DOWN, THE PILOT COMPLETED THE EMERGENCY CHECK LIST AND ACCOMPLISHED AN UNEVENTFUL LANDING. MAINSDR 2005FA0000426Pin · brokenON MAY 17, 2004, AUTHORIZED BY NTSB TO DO A TEARDOWN ONLY ON PROPELLER. UPON WHICH (PN 134460) ACTUATING PIN, WAS FOUND BROKEN IN HALF; START OF THREADS. PARTS INVOLVED WERE TAKEN BY FSDO. FSDO FORWARDED THEM TO NTSB FOR INVESTIGATION. CANNOT COMMENT ON PRSDR TRBA2004022Switch · faultyON TAKEOFF ROLL, THE AUTOMATIC TAKEOFF POWER CONTROL SYSTEM DID NOT ARM. TAKEOFF ABORTED. REMOVED AND REPLACED MICROSWITCH. (M)SDR GLBA2003146Control Unit · damagedRT PROP OVERSPEED, REMOVED AND REPLACED RT PROP TRANSFER TUBE, OVERSPEED GOV PN 8210-160 SN 2252121B HR 9002 10529, PCU OVERSPEED GOV PUMP PN 8210-286 SN 13326287 HR 1493 1567SDR 050516Solenoid · stuckON FLIGHT 5534 UPON THE TAKEOFF ROLL THE RIGHT ENGINE WOULD ONLY GO TO 1550 RPM. THE CREW ABORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE LOW PITCH SOLENOID TO BE STUCK. MAINTENANCE CLEANED AND LUBED THE SOLENOID.SDR HNAA0300001PropellerNUMBER 1 PROPELLER DUE TO POSSIBLE OVR TORQUE CONDITION. REMOVED AND INSPECTED PROP AND REINSTALLED.SDR VNAA0209024Propeller · failedDURING CLIMB, THE CREW NOTICED A VIBRATION SUSPECTED FROM THE LEFT HAND PROPELLER AND RETURNED TO PIT. MAINTENANCE INSPECTED AND THEN BALANCED THE LEFT HAND PROPELLER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-00-00. OPERATIONAL CHECKS WERE PERFORMED ASDR VNAA0206016PropellerAT APPROXIMATELY 1000 FEET AGL, THE CREW EXPERIENCED A STRONG VIBRATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND FOUND A FLAT SPOT ON THE NOSE WHEEL TIRE. MAINTENANCE REPLACED THE NOSE WHEEL TIRES IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-0SDR VNAA0205020Propeller · failedAPPROXIMATELY SIX MILES FROM THE BAL VOR, THE CREW EXPERIENCED A FLASH AND LOUD BOOM. THE CREW ASSUMED THAT THE AIRCRAFT HAD BEEN STRUCK BY LIGHTNING. THE CREW DECLARED AN EMERGENCY AND LANDED WITH NO FURTHER INCIDENTS. THE AIRCRAFT WAS FERRIED TO DAY WHERESDR CA011004010Bolt · broken(CAN) ONE OF THE 6 BOLTS ATTACHING THE PROPELLER TO THE ENGINE CRANK SHAFT FLANGE BROKE AT THE TOP OF THE THREADED AERA ON INITIAL TORQUE.THE PROPELLER HAD A PLACARD INDICATING TORQUE SPED FOR 1/2" BOLTS. PROLLER IS ATTACHED WITH 7/16" BOLTS. IT IS SUSPECTED T
Back to JASC 6100