JASC 6100

Service difficulty reports · 193

Reports filed under 6100 · Propeller System, newest first.

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.

SDR QXEA2016051100316Propeller · malfunctionedON PREFLIGHT INSPECTION FOUND THE NR 1 PROPELLER NOT FULLY FEATHERED. C/W PROPELLER FEATHER CHECK IAW AMM TASK 71-00-00-868-819. NR 1 PROPELLER CHECKS GOOD. NO DEFECTS FOUND. RETURNED TO SERVICE.May 11, 2016 · N417QX · Bombdr DHC8402SDR ME4R2016050300205Arm · crackedLINK ARM CRACKED. FOUND DURING ROUTINE O/H USING MAG PARTICLE INSPECTION.Apr 21, 2016SDR ME4R2016FA0000204Block · crackedCRACK WAS FOUNDON THE PITCH CHANGE BLOCK, FOUND DURING ROUTINE O/H USING MAG PARTICLE INSPECTION.Apr 21, 2016SDR ME4R2016FA0000203Collar · crackedGUIDE COLLAR HAS A CRACK ON THE TOPSIDE OF THE NR 1 BUSHING HOLE. THE CRACK WAS FOUND DURING A ROUTINE O/H USING THE FLUORESCENT PENETRANT INSPECTION. NO RECOMMENDATIONS ON HOW TO PREVENT.Apr 21, 2016SDR CA160126010Propeller · malfunctioned(CAN) ON TAXI OUT TO RUNWAY IN PREPARATION FOR TAKEOFF, CREW NOTED NR 1 ENGINE PROPELLER ENCOUNTERED AN OVERSPEED CONDITION. THE CREW CONFIRMED THE OVERSPEED WAS UN-COMMANDED IN NATURE AND SUBSEQUENTLY PERFORMED AN ENGINE SHUTDOWN. THE ACFT RETURNED TO GATE Jan 24, 2016 · Aerosp ATR42300SDR QXEA2016011100019Unknown · unknownNR 2 ENGINE DID NOT COME OUT OF FEATHER AFTER ENGINE START. INTEROGATED CDS, NO FAULTS FOUND, AS PERCAUTIONARY R & R NR 2 ENGINE OVERSPEED GOVERNOR IAW AMM 61-20-26-000-801, 61-20-26-400-801, KR 44607 1-10-2016. PERFORMED OPS TEST OF THE PROPELLER OVERSPEED Jan 11, 2016 · N436QX · Bombdr DHC8402SDR HNAA2015111900341Propeller · vibrationSHORTLY AFTER ROTATION, EXPERIENCED STRONG VIBRATION, NR 2 PROP ASSY. RETURNED IMMEDIATELY TO THE FIELD. ON ROLLOUT, GOT NR 2 DC GEN CAUTION LIGHT. ON TAXI WAY SHUTDOWN NR 2 ENGINE. ALL ENGINE AND PROP PARAMETERS GOOD. Nov 18, 2015 · N329EN · Dhav DHC8311SDR QXEA2015111700614Propeller · vibrationENROUTE, ONCE CLEAR OF ICING CONDITIONS WE PICKED UP CONSTANT STRONG VIBRATION FROM BOTH ENGINES. AIRFRAME MODE SELECT SWITCH WAS SET TO FAST WITH ENGINE INTAKE BYPASS DOORS OPEN. ALL INDICATIONS ON ED WERE NORMAL. DIVERTED AND ACCOMPLISHED UNEVENTFUL LANDINov 17, 2015 · N439QX · Bombdr DHC8402SDR QXEA2015092300507Propeller · unknownDURING TAKEOFF, NR 2 PROPELLER DID NOT REACH 1020 TILL 100 KTS. NR 2 PROP INDICATED 1010 TILL 100 KTS. NR 2 PROP WAS A LITTLE SLOW TO COME OUT OF FEATHER AT START. PERFORMED ENGINE TREND DOWNLOAD FROM EMU MTC 6773101, PERFORMED OPS TEST OF THE PROPELLER OVESep 23, 2015 · N433QX · Bombdr DHC8402SDR CA150818001Brake · burned(CAN) DURING FLIGHT, THE ALARM, PROPELLER BRAKE UNLOCK, FLASHED ONE TIME, AFTER LANDING DURING TAXIING A THICK WHITE SMOKE FROM THE FRONT OF RT ENGINE WAS OBSERVED, PROPELLER BREAKS WERE NOT ENGAGED. AFTER ENGINE SHUTDOWN CUSTOMER WITNESSED A LOT OF HYD FLUIDAug 7, 2015 · Aerosp ATR42500SDR QXEA2015072300394Propeller · unknownNR 1 PROP SLOW TO COME OUT OF FEATHER WHEN CONDITION LEVER SET TO MAX. C/W FIM TASK 61-20-00-810-801, STEPS 1-5A, 10 AND, 6. NO FAULTS NOTED IN CDS FOR EMU. NO EXTERNAL PROPELLER LEAKS NOTED. PROP UNFEATHER NORMALLY WITH FEATHER PUMP. R & R NR 1 OVERSPEED GJul 23, 2015 · N421QX · Bombdr DHC8402SDR QXEA2015071300388Electronic Unit · malfunctionedNR 1 PEC CAUTION WITH POWERPLANT MESSAGE, PROP RPM 1060. SHUTDOWN ENGINE IAW EMERGENCY CHECKLIST 7.14 EMEGRENCY CHECKLIST. LANDED UNEVENTFUL. EMU INTEROGATED FOR FAULT CODES. FIM TASK ACCOMPLISHED FOR DISCOVERED FAULTS. PEC GROUND RUNS COMPLIED WITH IAW MJul 13, 2015 · N448QX · Bombdr DHC8402SDR CA150429008Controller · malfunctioned(CAN) DURING CRUISE POWERPLANT MESSAGE CAME ON. CREW ELECTED TO DIVERT. NR 1 PEC REPLACED. OK ON GROUND RUN.Apr 29, 2015 · Bombdr DHC8400SDR QXEA2014121601100Propeller · malfunctionedTAKEOFF ABORTED DUE TO NR 2 PROPELLER ONLY REACHING 1010 RPM. ALL OTHER ENGINE INDICATIONS NORMAL. SPEED 97 KNOTS. CHECKED CDS FOR FAULT CODES, NOT FOUND. C/W POWER ASSURANCE ENGINE RUN FOR NR 2 ENGINE AND APPLICABLE ENGINE RUNS. COULD NOT DUPLICATE DIDec 16, 2014 · N433QX · Bombdr DHC8402SDR SWIA2014120140227Control Unit · malfunctionedRETURNED TO DEPARTURE AFTER A RIGHT PROP OVERSPEED. PERFORMED FIM PROCEDURE HIGH NP IAW AMM. CND FAULT. FOUND NP OVERSPEED TO BE WITHIN LIMITS IAW AMM. CHANGED RT PCU.Nov 29, 2014 · N578SW · Emb EMB120ERSDR 2014FA0000626Bearing · failed10-1-14, 15:43 LOCAL TIME, ACFT WAS ON A PRACTICE ILS APPROACH, RECEIVING VECTORS FROM SOCAL ON 125.5 HEADING OF 030 AT APPROX 3500`, WHEN PILOT ENCOUTERED UNCOMMANDED HIGH RPM. PILOT IMMEDIATELY REDUCED THROTTLE, RPMS SETTLED AT APPROX 1500 RPMS. PILOT FOUNOct 1, 2014 · N2041D · Beech C35BEECHSDR CA141006014Propeller · overspeed(CAN) DURING CLIMB, THE PROPELLER HAD AN OVERSPEED AND THE PILOT SHUTDOWN THE ENGINE. ELECTED TO RETURN TO ORIGIN WHERE AN UNEVENTFULLY LANDING WAS PERFORMED. ALSO DURING CLIMB, THE PILOT SHUTDOWN THE ENGINE AFTER TORQUE FLUCTUATION OCCURRED. AT THIS TIME TSep 15, 2014 · Dhav DHC8201SDR QXEA2014090400741Propeller · malfunctionedNR 2 PROPELLER FAILS TO UNFEATHER WHILE IN MAINTENANCE MODE. REPLACED FEATHERING PUMP, STILL FAILS CHECKS. PLACED ON MEL 61-20-1. RETURNED TO SERVICE.Sep 4, 2014 · N401QX · Bombdr DHC8402SDR QXEA2014072100605Unknown · unknownDURING DAILY SYS CHECK, AUTOFEATHER CHECK IS ABORTING TEST ON LT SIDE, SEVERAL ATTEMPTS. NO FAULTS IN CDS. OP'S CHECK OF THE PROPELLER AUTOFEATHER SYS IAW AMM TASK 61-20-00-710-801. OP'S CHECKED GOOD. COULD NOT DUPLICATE. RETURNED TO SERVICE.Jul 21, 2014 · N437QX · Bombdr DHC8402SDR CA140721010Propeller · malfunctioned(CAN) IT WAS REPORTED THAT THE ACFT EXPERIENCED AN UNCOMMANDED AUTOFEATHER DURING CLIMB. MORE DETAILS WERE REQUESTED TO THE CUSTOMER.Jul 9, 2014 · Dhav DHC8314SDR HNAA2013123000643Relay · failedON TAKE OFF ROLL, AUTO FX DID NOT ARM. RTO SYS TESTS OK AFTERWARDS. R & R RELAY 6121-K5. GROUND-RAN AIRCRAFT IAW -8 RUNUP MANUAL. OK FOR SERVICE.Dec 28, 2013 · N938HA · Dhav DHC8102SDR PNSA2013121904Unknown · vibrationUNIDENTIFIED VIBRATION VISUALLY INSPECTED EXTERIOR, INSPECT MOTOR MOUNTS AND BALANCED RT PROP. FLIGHT CHECK OK.Dec 19, 2013 · N410XJ · Saab 340BSDR CA131215002Propeller · failed(CAN) DURING CLIMBOUT, THE PROPELLER FEATHERED WITHOUT THE PILOT INPUT. THE PILOT THEN NOTICED THAT OIL PRESSURE HAD REDUCED INTO THE RED AND THE LOP WARNING ILLUMINATED. THE ON GROUND INSPECTION REVEALED THAT THE PROP WAS STIFF TO TURN.Dec 2, 2013SDR CA131202010Signal Cond Unit · malfunctioned(CAN) SHORTLY AFTER TAKEOFF, NR 2 ENGINE FEATHERED. FLIGHT CREW SHUTDOWN THE ENGINE AND DECLARED AN EMERGENCY. THE ACFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. FLIGHT CREW REPORTED 155 PERCENT TORQUE ON THE NR 2 ENGINE. FLIGHT DATA RECORDER WAS DOWNLONov 27, 2013 · Dhav DHC8102SDR CA131111016Propeller · malfunctioned(CAN) DURING TAKEOFF ROTATION, THE NR 1 PROPELLER FEATHERED. THE TORQUE RAPIDLY INCREASED ABOVE NORMAL OPERATING LIMIT AND FLIGHT CREW SHUTDOWN THE ENGINE. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED, LANDED WITHOUT FURTHER INCIDENT. SOLID STATE FLIGHT DANov 7, 2013 · Dhav DHC8311SDR CA130921008Propeller · out of rig(CAN) THE ACFT EXPERIENCED ENGINE NR 2 VIBRATION DURING THE DESCENT, THAT EVENTUALLY BECAME HEAVY WITH OIL ODOR AND SOME SMOKE IN THE CABIN. SEVERAL ALARMS THEN WENT OFF AND ACFT ENTERED A DIVE REACHING OVERSPEED. THE PILOT TOOK MANUAL CONTROL, IN VFR, DECLASep 18, 2013 · Aerosp ATR72212ASDR HNAA2013073000435Propeller · vibrationAFTER TAKEOFF, ENGINE VIBRATION FELT AND CONTINUED TO WORSEN UNTIL RUNUP, NR 1 ENGINE VIBRATION INCREASES WHEN OUT OF FEATHER. COMPLIED WITH INSPECTION IAW AMM 05-50-65 AND REPLACED NR 1 PROP ASSY IAW CARDS 61-10-06 AND 61-10-07 FOR BLADE R & R. RUN AND LEAKJul 30, 2013 · N343EN · Dhav DHC8311SDR HNAA2013070500390Propeller · malfunctionedUNABLE TO GET NR 1 PROP RPM BELOW 927. ADJUSTED NR 1 PCU SPEED TRIM SCREW IAW MM 61-22-00. PROP SPEED AT 911 RPM. OK FOR SERVICE.Jul 5, 2013 · N335EN · Dhav DHC8311SDR CA130704002Propeller · slow(CAN) ERI REPORT PT6A 2013-048 R1, POWER SECTION MODULE WAS SENT FOR INVESTIGATION AFTER THE CUSTOMER REPORTED THAT THE PROPELLER SPEED WOULD NOT HOLD AT THE MAXIMUM SPEED. PROPELLER SPEED WOULD SLOWLY RECEDE FROM THE MAXIMUM.Jul 2, 2013SDR CA130530002Control Lever · malfunctioned(CAN) DURING T/O AND INITIAL CLIMB, THE PROPELLER WAS NOT MAINTAINING STEADY RPM. THE PROP. LEVER WAS SET TO FEATHER BUT THE PROPELLER DID NOT FEATHER UNTIL LATER ON FINAL APPROACH, DURING THE RETURN TO THE AIRPORT. AN UNEVENTFUL LANDING FOLLOWED. TROUBLESHOOTMay 20, 2013 · Beech B200SDR CA130603001Bearing · damaged(CAN) PILOT REPORTED VIBRATIONS ON DESCENT AND REDUCED POWER TO COMPLETE LANDING. ON INSPECTION MAINTENANCE CREW FOUND PROPELLER BLADE RETAINING BEARINGS AND RACE TO BE DAMAGED.May 19, 2013SDR VGCA20130401001Propeller · malfunctionedNR 2 PROPELLER AUTOFEATHER AFTER TAKEOFF.Apr 1, 2013 · N371FL · Cvac STC3405800SDR HNAA2012082900934Warning Horn · activatedBETA WARNING HORN SOUNDED INTERMITTENTLY AFTER LANDING, DURING TAXI. BETA WARNING HORN SYS WITH MOD VERIFIED OPS CHECK OF BETA LOCKOUT SYS IAW CREW ORIGINATING CHECKLIST. PULLED AND COLLARED CIRCUIT BREAKER C8.Aug 29, 2012 · N838EX · Dhav DHC8102SDR 2014FA0000522Filler · crackedREPLACED SPINNER AND ADAPTER PLATE WITH PN 103585F2 WHEN PROPELLER HAD 29.96 TSMOH AND SINCE NEW THAT WAS INSTALLED IAW THE MM. DURING A RECENT ANNUAL INSPECTION, REMOVED THE SPINNER FOR INSPECTION AND LUBRICATION OF THE PROPELLER. FOUND CRACK EMANATING FROMAug 19, 2012 · N6437Q · Mooney M20FSDR CA130115008Bearing · spalled(CAN) DURING APPROACH THE PROPELLER SPEED DROPPED BELOW LIMITS. ENGINE WAS SHUTDOWN AND ACFT LANDED SAFELY. MAINTENANCE REPLACED THE PROPELLER VALVE HOUSING AND THE ACFT WAS RETURNED TO SERVICE. THE O/H FACILITY REPORTED SUBSTANDARD BEARINGS SUSPECTED.Apr 26, 2012 · Lkheed 382GSDR CA120307003Plate · damaged(CAN) THE STEEL PROP SECURING PLATE IS BENDING, THE BOLT HOLES ARE BEING DAMAGED BY THE BOLT. EVERY 100 HR INSP THE PROP BOLTS NEED TO BE TORQUED BECAUSE THEY ARE LOOSE. THIS PART HAS BEEN SENT FOR SUPPORT FOR ANALYSIS. THE OWNERS HAVE BEEN RE-TORQUEING THE Mar 7, 2012SDR CA111123014Control Cable · damaged(CAN) UPON RIGGING PROP CONTROLS AFTER CABLE REPLACEMENT ON RT ENGINE, FOUND SUSPICIOUS LT PROP CONTROL ATTACHMENT. JOINT ASSEMBLY PN 469-153 WAS RUSTED, BUT MOST UNUSUAL WAS THAT A FIBRE LOCK NUT WAS USED AS SECURING DEVICE AND THAT THREADS WERE WELL BELOW FNov 23, 2011 · Piper PA31SDR CA110916002Gear · damaged(CAN) LEFT ENGINE SPOOLED DOWN AT TAKEOFF POWER.Sep 5, 2011 · Cvac 340CVACSDR CA110414001Shaft · cracked(CAN) OPERATOR DISCOVERED THAT THE PROPSHAFT WAS CRACKED. THE OPERATOR WAS INVESTIGATING REPEATED OIL LEAKAGE AROUND THE PROP AREA WHEN THE CRACK WAS DISCOVERED. THE CRACKING OF THE PROPSHAFT WAS A RESULT OF HYDROGEN EMBRITTLEMENT.Apr 11, 2011SDR GUUA94276040411APropeller · malfunctionedPILOT REPORTED WHEN PULLING PROPS BACK FROM 1550 RPM ON THE DESCENT TO 1400 RT PROP LAGGED ABOUT A KNOB AND HALF FROM LT SIDE PROPS WERE OUT OF SYNC AND COULD NOT GET INTO SYNC. WHEN PROPS PUSHED FULL FWD LT PROP REACHED ABOUT 1700 RPM WHILE RT PROP INCREASEDApr 4, 2011 · N47542 · Beech 1900DSDR GUUA94161022511AAnnunciator · no indicationPILOT REPORTED WITH N1 AT 95 PERCENT "AFX DISABLE" ANNUNCIATOR WAS ILLUMINATED AND LT AFX WAS NOT ILLUMINATED. RERACKED ANNUNCIATOR FAULT DETECTION PCB AUTOFEATHER TEST OPS CHECK GOOD.Feb 25, 2011 · N17541 · Beech 1900DSDR 2011FA0000002Unknown · unknownUNCOMMANDED AUTOFEATHER ON APPROACH.Jan 1, 2011 · N161SL · Piagio P180SDR QXEA2010122000923Unknown · unknownON PREFLIGHT NR 2 AND NR 1 PROP NOT FEATHERED. GROUND RAN ACFT, CYCLED PROPS SEVERAL TIMES, NO DEFECTS NOTED, ACFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED.Dec 15, 2010 · N422QX · Bombdr DHC8402SDR 2010F00212Unknown · unknownUNCOMANDED AUTOFEATHER ON APPROACH.Sep 27, 2010 · N164SL · Piagio P180SDR V0DR967YBJam-Nut · defective(V0DR) DURING ASSY OF A PROPELLER ASSY, THE JAM-NUTS (PN B-3368) WERE INSTALLED AND THE BETA RING RUN-OUT TOLERANCE COULD NOT BE MAINTAINED. FURTHER TROUBLESHOOTING IDENTIFIED THE JAM-NUTS (PN B-3368) WERE MFG WITH THE THREADS NOT TRUE. CAUSING THE RUN-OUT TAug 11, 2010 · Beech 1900DSDR V0DR967Y001Jam-Nut · defectiveDURING ASSY OF A PROPELLER, THE JAM-NUTS, PN B-3368 WERE INSTALLED AND THE BETA RING RUN-OUT TOLERANCE COULD NOT BE MAINTAINED. FURTHER TROUBLESHOOTING IDENTIFIED THAT THE NUT PN B-3368 WAS MFG WITH THE THREADS NOT TRUE. CAUSING THE RUN-OUT TO BECOME EXCESSIAug 11, 2010 · Beech 1900DSDR HNAA201004200079Unknown · malfunctionedNR 1 PROP WILL NOT GO ABOVE 1188 ON TAKEOFF ROLL AT 90 PERCENT TORQUE. ABORTED TAKEOFF. DURING TAXI WHEN MOVING POWER LEVERS FROM DISC TO FLIGHT IDLE, PROP INCREASED FROM 785 TO 802. INSPECTED ECP, NO EEC FLAGS NOTED. CYCLED NR 1 ENGINE ECU CIRCUIT BREAKERMar 26, 2010 · N814EX · Dhav DHC8102SDR HNAA2010012200009Beta Switch · failedNR 2 ENG TORQUE SURGED APPROX 30 PERCENT RANGE JUST AFTER TAKEOFF. AFTER TAKEOFF NR 2 ENGINE TORQUE SURGED TO APPROX 119 PERCENT AND PROP SURGED TO APPROX 1000 RPM. ACFT AT 100 AGL AND CLEARED UP AFTER LANDING. REACTIVATED BETA LOCKOUT SYS. R & R NR 2 ENG Jan 3, 2010 · N333EN · Dhav DHC8314SDR LR7A2009101900143Housing · unknownDURING DECENT CREW REPORTED NR 4 ENG RPM OUT OF LIMITS. PERFORMED ENG SHUTDOWN IAW QRH. NR 4 VALVE HSG REPLACED IAW JOB CARD HN61135, OPS CHECK GOOD. LOG PAGE 34387 ITEM M1.Nov 23, 2009 · N402LC · Lkheed 382GSDR 2009FA0000873Nut · crackedWHEN REMOVING PROPELLER FOR RESEAL, FOUND 2 MOUNTING NUTS CRACKED. THE PROP HAS 93.5 HRS SINCE INSTALLATION. THE PROPELLER PREVIOUSLY HAD THE BLADES REPLACED DUE TO PROP STRIKE.Oct 22, 2009 · N722PA · Diamon DA40
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