JASC 6197
Service difficulty reports · 99
Reports filed under 6197 · Propeller/Propulsor System Wiring, 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 = '6197' 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 = '6197' 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 QXEA2010051400301Connector · contaminatedABORTED TAKEOFF BELOW 60 KTS FOR "POWERPLANT" MESSAGE. NOTICED THE MESSAGE AS WE TOOK CTRLINE AND POWER LEVERS ADVANCED JUST ABOVE FLIGHT IDLE. RETURNED TO THE GATE. INTEROGATED CDS FOUND FAULT CODES ON P-PLANT 1 CH A 14,28,30,456. CH B 794. POWERPLANT 2 CH SDR MASA2010032000225Connector · dirtyRTG FOR AUTO FEATHER AND POWER UP TRIM WOULD NOT TEST DURING TAXI. CLEANED PCU CONNECTOR, RESET AND OPS NORM.SDR GLBA20090926APcb · looseON FINAL APPROACH INTO ALS WITH GEAR DOWN AND FLAPS 35 DEG RT PROPELLER TRIED TO AUTOFEATHER RT OIL PSI WAS AROUND 95-100. MAINTENANCE REMOVED AND RE-INSTALLED THE A123 PRINTED CIRCUIT BOARD AND PERFORMED AN OPERATIONAL CHECK WICH WAS GOOD IAW MM 61-21-00-001SDR QXEA2009092800718Buss Bar · failedON DESCENT INTO BIL NR 1 PEC CAUTION ILLUMINATED AND POWERPLANT MESSAGE APPEARED ON ED. NP WAS 1060. PERFORMED PRECAUTIONARY SHUTDOWN. F/O HAD 18% TORQUE ON BOTH ENGINES AND HAD JUST REDUCED POWER TO FLIGHT IDLE WHEN CAUTION LIGHT ILLUMINATED. ALL INDICATIONS SDR COEA2009081201965Connector · contaminatedTAXI BACK - GEG FLT 8777. DURING TAXI THE PILOT DISCOVERED THE NP INOP, READS ZERO AT ALL PROP SPEEDS. REMOVED NP CONNECTOR, CLEANED, DRIED AND REINSTALLED. AIRCRAFT RETURNED TO SERVICE.SDR S9BA20090012Wire · chafedACFT GROUNDED, LT PROP FEATHERED FOR 5 SECONDS AND RETURNED TO NORMAL OPERATION. DURING TAKEOFF. REPAIRED CHAFED WIRE ON LT PROP BETA SOLENOID. CHECKED LT ENG CHIP DETECTOR AS PRECAUTIONARY MEASURE. CHECK WAS NEGATIVE. REQUESTED POERATIONAL CHECK FLIGHT. SDR CA090622002Connector · failed(CAN) IN FLIGHT SHUTDOWN OF THE NR 1 ENGINE DUE TO AN OVERSPEED, PAN-PAN DECLARED. THE CREW REPORTED THEY WERE APPROX FL140 WHEN THEY RECEIVED THE NR 1 PEC CAUTION LIGHT WITH NR 1 PROPELLER SPEED INCREASED ABOVE 1020 RPM (RECORDED EXCEEDENCE WAS 1081 RPM OR 10SDR GLBA20090531FCircuit Board · inoperativeTHE PILOTS REPORTED THAT THE AFX SYS FEATHERED THE NR 1 PROPELLER WHILE ON FINAL WITH PROPS FULL FWD AND TORQUE AT 1000 LBS. MX REMOVED AND REPLACED THE A123 PRINTED CIRCUIT BOARD IAW MM 20-00-01. OPS CHECKS WERE NORMAL.SDR GLBA20090414AConnector · looseLT PROP GAUGE READ 2000 RPM AFTER SETTING T/O POWER. MAINTENANCE CLEAND AND RE-SECURED CONNECTOR ON THE INDICATOR. ENGINE RUNS WERE PERFORMED WITH THE PILOTS AND THE OPERATIONAL CHECKS WERE GOOD PER MM 77-10-00.SDR GLBA20090405BConnector · loosePILOTS REPORTED THAT EXPERIENCED A DROP IN THE RIGHT HAND PROPELLER RPM AND THAT IT HAD DROOPED TO 1620 RPM ON TAKEOFF. MAINTENANCE CLEANED THE CONNECTOR ON THE RIGHT HAND PROPELLER TACH GENERATOR AND RE-INSTALLED. REFERENCE BEECH 1900 MM 77-10-00.SDR HNA2008F00038Wire · brokenABORTED TAKEOFF DUE TO AUTOFEATHER ARM LIGHT DID NOT ILLUMINATE. FERRIED TO SBY. MAINTENANCE REPAIRED WIRE AT POWER LEVER MICROSWITCH 6121S13. OPS CHECK GOOD. (S)SDR 2008FA0000505Connector · damagedON JUNE 28TH, 2008, DURING CLIMB OUT, PASSING THROUGH 4000 FEET THE ENGINE SUDDENLY WENT INTO AN OVER SPEED CONDITION OF OVER 3100 RPM. THE AIRCRAFT REMAINED UNDER CONTROL AND WAS LANDED SAFELY AT AIRPORT AFTER AN EMERGENCY WAS DECLARED. UPON DISASSEMBLY OF TSDR SWIA200819582Switch · damagedFLT 5538 - LEFT AUTO-FEATHER SYSTEM FAILED. REPLACED PIN 1 ON AUTO-FEATHER TEST SWITCH. OPS CHECKS GOOD.SDR MASA200800230Connector · looseASH FLT 7177 RAP-DEN, NR 2 ENGINE UNSCHEDULED AUTO FEATHER CONDITION IN FLIGHT AT AROUND 1000 FT. CREW DECLARED AN EMERGENCY AND RTF. RE-SECURED CONNECTOR ON TORQUE SENSOR, OPS CHECK GOOD.SDR HNAA0800040Connector · contaminatedWHEN PILOT ADVANCED POWER FOR TAKEOFF, THE NR 2 PROPELLER WENT INTO FEATHER UNCOMMANDED. THE PROP SPEED WAS APPROXIMATELY 1200 RPM AND REACHED A TORQUE OF 100-105% FOR ABOUT 3 SECONDS. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT WAS RETURNED TO THE MAINTENANCE SDR NSVA20070231Connector · dirtyLT PROP OIL TEMP GAUGE EXCEEDED IT'S LIMITS, SUDDEN FULL SCALE DEFLECTION. CLEANED CONNECTION ON LT PROP OIL/TEMP GAUGE. OP CHECK GOOD 79-30-15.SDR CA071003025Wire Harness · unknown(CAN) IN CRUISE, THE PROPELLER ELECTRONIC CONTROL (PEC) AND POWER PLANT WARNINGS ACTIVATED. THE ENGINE WAS SHUTDOWN IN FLIGHT. THE PEC, SENSOR AND RELATED HARNESS WERE SUBSEQUENTLY REPLACED. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISDR CA070802008Connector · unserviceable(CAN) ON CLIMB OUT SHORTLY AFTER TAKEOFF, THE BETA WARNING LIGHTS (BOTH) CAME ON AND THE NR 2 PROPELLER STARTED TO FEATHER. THE PILOT PULLED THE BETA SYSTEM CIRCUIT BREAKER BUT THE LIGHTS DID NOT GO OFF, BUT THE PROPELLER STOPPED GOING TO FEATHER. THE PILOT SDR QXEA200701146Connector · misalignedSEA FLIGHT NR 2104 - DURING TAKEOFF ROLL AUTO FEATHER FAILED TO ARM THROUGH 80 PERCENT. TORQUE ON BOTH NR 1 AND NR 2. FOUND CONNECTOR 6121-P9 TO BE ASKEW. RESEATED CONNECTOR 6121-P9. FUNCTIONAL CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR NSVA20070132Wire · damagedP3 TEST FAILED ON BOTH ENGINES. REPAIRED WIRING AT PROPELLER CONTROL UNIT.SDR QXEA200700599Connector · dirtySEA FLIGHT NR 2418: POWER PLANT MESSAGE AFTER ENGINES STARTED. AIRCRAFT RETURNED TO GATE. MAINTENANCE INTERROGATED CDS. FOUND FAULT CODES 130B ON 32 PROP AND 274 ON NR 1 PROP. CLEARED FAULTS PER Q400 AMM TASK 61-20-36-070-801. CLEANED ALL ELECTRICAL CONNESDR HNAA0700047Connector · disconnectedNR 2 PROP FLUXES PLUS OR MINUS 10 RPM DURING CLIMB WITH TORQUE FOLLOWING. FOUND CONNECTOR NOT CONNECTED TO TORQUE MOTOR ON NR 1 ENGINE.SDR CA070321009Buss Bar · shorted(CAN) NR 2 ENGINE SHUTDOWN MANUALLY IN FLT DUE PEC FAIL CAUTION AND PROP SPEED AT 1060 RPM. FAULT CODES RT CH A/B 160 AND 162. MAINT DISPATCHED TO T/S. FOUND BUSBAR FOR PROPELLER DEICE CHAFFING ON MPU BRACKET, CAUSING MPU TO PICKUP SENS FROM BUSBAR. MPU ADJUSTSDR MAC010701Wire · out of positionDURING DESCENT INTO DHN THE NR 2 ENGINE BEGAN SURGEING (PROP CHANGEING PITCH). WIRE NR 101 WAS FOUND NEARLY SEPARATED FROM IT'S PIN IN THE CONNECTOR TO THE RIGHT FEATHER SOLENOID.SDR NSVA200600219Wire · burnedLT ENG AUTOFEATHER DID NOT ARM ON DEPARTURE. PERFORMED AUTOFEATHER OPS CHECKS IAW BEECH 340 1900 AMM 61-21-00. OPS CHECKS NO GOOD. RT AFX REPEATER LIGHT NOT ILLUMINATING AND RT CWP RT AUTOFEATHER LIGHT NOT ILLUMINATING. DURING TROUBLESHOOTING FOUND PCB A14SDR CA061124002Buss Bar · shorted(CAN) NO.1 ENGINE SHUTDOWN DURING FLIGHT DUE PEC FAIL CAUTION LIGHT AND PROP SPEED AT 1060 RPM. FAULT CODES LH CH A/B 160 AND 162. MAYDAY CALLED AND A NORMAL LANDING PERFORMED. PAX DEBRIEFED DURING TAXING AND AFTER PARKING. MAINTENANCE DISPATCHED TO TROUBLE SHSDR LX5R200600003Wire Harness · shortedUPON TAKEOFF ROLL, THE CREW GOT THE AUTO FEATHER OFF LIGHT AND THE MASTER CAUTION LIGHT. THE CREW THEN OPTED TO ABORT TAKEOFF ROLL AND RETURN TO RAMP WITHOUT INCIDENT. UPON RETURNING TO RAMP, THE CREW NOTICED THAT THE AUTO FEATHER CRICUIT BREAKER HAD POPPED,SDR LX5R200600002Wire Harness · shortedUPON TAKEOFF ROLL THE CREW GOT THE AUTOFEATHER OFF LIGHT AND THE MASTER CAUTION LIGHT. THE CREW THEN OPTED TO ABORT TAKEOFF ROLL AND RETURN TO RAMP WITHOUT INCIDENT. UPON RETURNING TO RAMP THE CREW NOTICED THAT THE AUTOFEATHER CIRCUIT BREAKER HAD POPPED, IT WASDR CA061114001Buss Bar · chafed(CAN) NO.1 ENGINE SHUTDOWN MANUALLY IN FLT DUE PEC FAIL CAUTION AND PROP SPEED AT 1060 RPM. FAULT CODES LH CH A/B 160 AND 162. MAINT DISPATCHED TO T/S. FOUND BUSBAR FOR PROPELLER DEICE CHAFING ON MPU BRACKET, CAUSING MPU TO PICKUP SENS FROM BUSBAR. MPU ADJUSTESDR QXEA200602703Connector · dirtyFLIGHT NR 2403: DURING TAXI OUT, POWER PLANT MESSAGE ON ED. MAINTENANCE INTERROGATED EMU AND CDS. FOUND FAULT CODE 131B ON NR 1 ENGINE. PERFORMED FAULT ISOLATION IAW FIM 61-21-03-810-815. FOUND DIRTY PIN A PCU TRANSDUCER CONNECTOR P28. CLEANED CONNECTOR. FAULTSDR CA061002011Connector · damaged(CAN) FAULT - LT SIDE AUTOFEATHER LIGHT DOES NOT ARM. NR 2 HIGH PRESS FEATHER SWITCH CONNECTOR, CONNECTOR PIN LETTER B REPLACED. SWITCH CONNECTORS CLEANED. PROBLEM SEEMED TO BE CAUSED BY CONTAMINATION. (TC NR 20061002011)SDR QXEA200600381Connector · looseSEA FLIGHT NR 2400: POWERPLANT MESSAGE OCCURRED AFTER PUSHBACK AND AFTER CONDITION LEVERS PUSHED FORWARD. MAINTENANCE FOUND FAULT CODE 130 ON NR 2 ENGINE CHAN B. CLEARED FAULT CODE. CLEANED ALL PEC AND PCU CONNECTOR PLUGS ON NR 2 ENGINE. GROUND RAN NR 2 ENSDR QXEA200600198Wire Harness · inoperativeLAX - ON FLIGHT 2448, RETURNED TO GATE, AFTER ENGINE START AND PUSHBACK AND CONDITION LEVERS BROUGHT TO MAX. NR 1 ENGINE/PROPELLER WOULD NOT COME OUT OF FEATHER, NP AT 200. CONCURRENT NR 1 PEC CAUTION LIGHT AND POWERPLANT MESSAGE ON ED. NO ENGINE EXCEEDANCESDR QXEA200600181Connector · dirtyPOWER PLANT MESSAGE ON ED. MAINTENANCE INTERROGATED CDS AND FOUND FAULT CODE 130B NR 2 ENGINE. CLEAN AND RESEATED CONNECTORS ON PCU-PEC AND C/W Q400 FIM TASK 61-20-03-810-815, STEPS 1-4. NO FURTHER FAULTS NOTED. SECURED OB NR 2 ENGINE COWL. C/W GROUND RUN IAWSDR CA050901005Wire Harness · shortedA/C DEPARTED YYC, DURING CLIMB-OUT LIGHTS FLICKERED LT GEN KICKED OFFLINE AND CREW LOST FMS SCREEN AND PROP SYNC CB POPPED. AS DEPARTING MX BASES, ELECTED TO RETURN TO YYC. PAX`S WHERE DISEMBARKED AND A/C RETURNED TO HANGAR. GENERATOR CAME ON LINE DURING STSDR PCAA0406227Wire Harness · groundedFLIGHT NR 3765 HAD TO RETURN TO GATE DUE TO HAVING THE NR 1 PROP FEATHER WHEN THE AUTOFEATHER SELECT SWITCH WAS SELECTED TO TEST. MAINTENANCE FOUND THE NR 2 ENGINE INTERFACE HARNESS SHOWING A STRAY GROUND TO THE TORQUE SIGNAL CONDITIONING UNIT. HARNESS WAS RESDR GLBA20030635Wire · chafedRIGHT PROP AUTOFEATHERED WHEN CONTROL LEVERS MOVED TO MAX DURING APPROACH AROUND 40 PERCENT TQ. REPAIRED CHAFED WIRING ON TSU, RIGGED RIGHT AIR FROM RIGGING ON POWER LEVER AND TRIMMED RT ENGINE.SDR GLBA20030632Propeller · malfunctionedRT PROP FEATHERED WHEN CONDITION LEVERS PUSHED FWD ON 5 MILE FINAL. RAN A/C, INSPECTED SYSTEMS, COULD NOT DUPLICATE. NTSB REPORT: MX REPAIRED CHAFED WIRE ON RT ENGINE TORQUE SIGNAL CONDITIONER.SDR CA040330001Wire · chafed(CAN) AN OPERATOR CARRIED OUT AN UNSCHEDULED LANDING DUE TO UNCOMMANDED NR 2 PROPELLER FEATHER DURING CLIMB, AND SUBSEQUENT OVERTORQUE OF THE NR 2 ENGINE. THEY FOUND THE CAUSE OF THIS PROBLEM WAS: CHAFING OF SEVERAL WIRES (HYDRAULIC SYSTEM, PROPELLER AUTOFEATHSDR CA030925006Switch · shorted(CAN) WHILE TAXIING FROM DOCK, NR 1 ENGINE DID NOT RESPOND TO (REVERSE) COMMAND BUT POWERED UP TO FORWARD MODE. FOUND WIRING WRAP INTERFERED WITH PROP RESET SWITCH IN OVERHEAD POWER LEVER QUADRANT. MODIFICATION WAS COMPLETED IAW DHC-6-100, MOD6/1912 (INSTALLATSDR CA030514009Wire Harness · shorted(CAN) WHILE IN FLIGHT, THE (DE-ICE CAUTION) AMBER CAUTION LIGHT ILLUMINATED AND THE GREEN (PROP DE-ICE) WAS FLASHING. AFTER INVESTIGATING THE PROBLEM. THE WIRE THAT WAS PROVIDING HEAT TO THE DE-ICE WAS ALREADY REPLACED. 2 BARE HEATING WIRES ON INTERIOR OF DESDR D5H2002F00000Pin · loosePILOT REPORTED SMOKE IN COCKPIT 30 MINUTES INTO FLIGHT. CONNECTOR FROM PROPELLER HEAT CIRCUIT BREAKER (P-186/J-186). CONNECTOR, 12 GAUGE WIRE(HA-36). MAINTENANCE CREW FOUND CONNECTOR FULLY ENGAGED AND STILL ATTACHED TO WIRE BUNDLE. MAINTENANCE FOUND TERMINSDR BSY2002F00020Wire · looseON TAKE OFF OUT OF BOSTON, SPARKS WERE FLYING OUT FROM UNDERNEATH PILOTS PANEL, RETURNED TO BASE. FOUND EXPOSED WIRE OUT OF CONNECTOR P160 ON WIRE NR HA20 ON PROPELLER DEICE CIRCUIT, SHORTED ON SIDE PANEL REPAIRED CONNECTOR, OPS GOOD.SDR AUS20020791Wire · failed(AUS) LT PROPELLER GROUND IDLE STOP SOLENOID FAILED. BROKEN CONDUCTOR AT WIRING ENTRY INTO SOLENOID BODY.SDR CA020411009Wire · chafed(CAN) AFTER DEPARTURE, CREW NOTICED FAINT ODOUR AND SAW AUTOFEATHER CB WAS POPPED. ELECTED TO RETURN AND DURING DECENT ODOUR INCREASED ACCOMPANIED BY SMOKE. DEPLOYED AND DONNED O2 MASKS. WENT THRU EMERGENCY PROC: SMOKE DISSIPATED, UNEVENTFULL LANDING. DURINGSDR CA020227007Wire · shorted(CAN) DURING CRUISE FLT, CREW NOTICED FAINT SMOKE SMELL, & NOTICED THAT PROP AUTOFEATHER CIRCUIT BREAKER HAD POPPED. THEY DECIDED TO RETURN TO YYC. DURING APPROACH / LDG PHASE OF FLT, SMELL OF SMOKE BECAME MORE NOTICEABLE. THE LDG & TAXIING TO GATE WENT UNEVESDR AU000526Wire · broken(AUS) LT PROPELLER INDICATION SYSTEM WIRE BROKEN.SDR EY2R9601562Wire · damagedPROP ASSY I.D. WIRE DAMAGESDR VTZA95248Harness · failedFLT NR 6506 - LYH-CHO - DURING CLIMB-OUT, RETURNED TO LYH DUE TO THE LEFT PROP HEAT FAILING. AIRCRAFT LANDED AT LYH WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 21935 IAW MEL 61-1. MAINTENANCE LATER CLEARED DMI NR 21935 BY REPLACING THE PROP HEATER
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