JASC 6111
Service difficulty reports · 1,725
Reports filed under 6111 · Propeller Blade Section, 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 = '6111' 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 = '6111' 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 2001FA0000592Clamp · crackedPROPELLER RECEIVED FOR STANDARD OVERHAUL, DUE TO TIME. (TSO) 1982.9. AFTER PROPELLER DISASSEMBLY, THE FOLLOWING COMPONENTS ARE CONDEMNED: BLADE (PN MV8433-4, SN 36637R) DAMAGED IN COLD ROLLED AREA DUE TO CLAMPS. BLADE (PN MV8433-4, SN C85096R) DAMAGED IN COLSDR 2001FA0000591Clamp · crackedPROPELLER RECEIVED FOR STANDARD OVERHAUL, DUE TO TIME IAW MFG SL. (TSO)1982.9. AFTER PROPELLER DISASSEMBLY, THE FOLLOWING COMPONENTS ARE CONDEMNED: BLADE (PN MV8433-4, SN 36637R) DAMAGED IN COLD ROLLED AREA DUE TO CLAMPS. BLADE (PN MV8433-4, SN C85096R) DAMASDR HNAA0100035Skin · departedON APPROACH AT 200 FEET, CREW AND FLIGHT ATTENDANT HEARD A LOUD BANG FOLLOWED BY AIRFRAME VIBRATION FELT THROUGHOUT THE CABIN AND FLIGHT DECK. FOUND NUMBER TWO PROP, NUMBER ONE BLADE MISSING THE NICKLE SHEATH. REMOVED AND REPLACED PROP BLADE.SDR 20010604CW017Clamp · crackedCRACK DISCOVERED DURING ROUTINE 100 HOUR INSPECTION. DETECTED VISUALLY. REASON FOR CRACK NOT KNOWN. CLAMP ASSEMBLY REPLACED WITH FACTORY NEW UNIT.SDR PAI2001F00000Blade · crackedDURING EDDY CURRENT INSPECTION, FOUND EVIDENCE OF A POSSIBLE CRACK IN THE BLADE AT THE 43.500 IN STATION. WILL SEND BLADE TO MCCAULEY FOR EVALUATION AND FINAL INSPECTION.SDR MAC15501Blade · crackedDURING EDDY CURRENT INSPECTION FOUND EVIDENCE OF A POSSIBLE CRACK IN THE BLADE AT THE 43.500 IN. STATION. WILL SEND BLADE TO MCCAULEY FOR EVALUATION AND FINAL INSPECTION.SDR 2001FA0000097Blade · crackedPROPELLER RECEIVED FOR OVERHAUL. BLADE SN 616 WAS FOUND TO HAVE A CRACKED OUTER SLEEVE AT ROOT END OF BLADE. BLADE REJECTED FROM FURTHER SERVICE.SDR 20010612CW012Blade · crackedBLADE FOUND CRACKED IN THE SECOND RETENTION THREAD DURING PENETRANT INSPECTION PERFORMED AT OVERHAUL. NO RED DYE LEAKAGE REPORTED. NO ABNORMAL VIBRATION REPORTED.SDR 20010508CW018Counterweight · brokenDURING TRAINING FLIGHT, LEFT PROPELLER WOULD NOT COME COMPLETELY OUT OF FEATHER. THE ENGINE COULD ONLY DEVELOP 1500 RPM. WHEN THE ENGINE WAS SHUTDOWN ON THE GROUND, THE PROPELLER WENT BACK INTO FEATHER REGARDLESS OF THE PROP CONTROL POSITION. UPON PROP DISSDR SIMA20011072Bearing · wornDFW - CREW REPORTED A SEVERE VIBRATION FROM THE LEFT PROPELLER AT ALL POWER SETTINGS AND PROPELLER SPEEDS. MAINTENANCE FOUND THE NR 4 BLADE IN THE LEFT PROPELLER WITH AN EXTREMELY WORN BLADE PITCH CHANGE BEARING AND PIN. PROPELLER BLADE WAS REMOVED AND REPLASDR AU010265Erosion Shield · separated(AUS) PROPELLER BLADE EROSION SHIELD SEPARATED.SDR AU010299Ferrule · cracked(AUS) PROPELLER BLADE FERRULE CRACKED AROUND BEARING SHELF ORIGINATINGFROM A PREVIOUSLY DRILLED ACTUATING PIN HOLE. CRACK LENGTH 50.8MM (2IN).SDR AU010219Block · cracked(AUS) PROPELLER PITCH CHANGE BLOCKS CRACKED. PITCH CONTROL FORK WORNEXCESSIVELY. HUB PRELOAD PLATE DAMAGED DUE TO PREVIOUS FOREIGN OBJECT STRIKE.SDR AU010186Blade · cracked(AUS) PROPELLER BLADE NICKEL SHEATH CRACKED. CRACK LENGTH APPROXIMATELY 50.8MM (2IN) LOCATED ON THE FACE APPROXIMATELY 50.8MM (2IN) FROMTHE BLADE HEATER.SDR NWOR140K5Blade · crackedFOUND 3.5 INCH CRACK ALONG TRAILING EDGE SIDE OF RETENTION AREA OF BLADE.SDR NWOR140K4Blade · crackedON INSPECTION 4.5 INCH CRACK WAS FOUND ON TRAILING EDGE SIDE OF BLADE RETENTION AREA.SDR NWOR140K3Blade · crackedDURING INSPECTION CRACK WAS FOUND ALONG TRAILING EDGE OF RETENTION AREA.SDR NWOR140K2Blade · crackedDURING INSPECTION, CRACK FOUND ALONG TRAILING EDGE OF RETENTION AREA OF BLADE.SDR NWOR140K1Blade · crackedINSPECTION FOUND CRACK ALONG LEADING EDGE SIDE OF RETENTION AREA.SDR NWOR140KBlade · crackedINSPECTION FOUND CRACKS AT TRAILING EDGE SIDE OF RETENTION AREA.SDR AU010181Blade · damaged(AUS) LT PROPELLER NR 1 BLADE DAMAGED BY FOD. LEADING EDGE SHEATH HAD APIECE MISSING APPROXIMATELY 10MM (0.393IN) IN DIAMETER. THE LEFT FRONT PASSENGER WINDOW BEHIND THE GALLEY HAD A LARGE IMPACT MARK APPROXIMATELY 12MM (0.472IN) IN DIAMETER.SDR COMA0110035Spring · brokenON POST-FLIGHT INSPECTION, CREW NOTICED OIL LEAKING FROM LEFT PROPELLER. MAINTENANCE DETERMINED SOURCE TO BE THE NR 1 PROP BLADE. THE BLADE WAS REMOVED, AND THE BLADE SEAL COIL SPRING WAS FOUND TO BE BROKEN. THE BLADE SEAL ASSEMBLY WAS REPLACED, THE BLADE RSDR COMA0110034Spring · brokenON POST-FLIGHT INSPECTION CREW NOTICED OIL LEAKING FROM LEFT PROPELLER. MAINTENANCE DETERMINED SOURCE TO BE THE NR 1 PROP BLADE. THE BLADE WAS REMOVED, AND THE BLADE SEAL COIL SPRING WAS FOUND TO BE BROKEN. THE BLADE SEAL ASSEMBLY WAS REPLACED, THE BLADE RESDR 20010321CW006Retainer · crackedMT INSPECTION REVIELD A CRACK APPROX .1250 INCH LONG ON BOTH SIDES OF RACE MATERIAL. PROPELLER WAS PURCHASED AS A OVERHAULED PROPELLER WITHOUT RECORDS. REPORTED LOST. PURCHASER SUBMITTED PROPELLER FOR OVERHAUL. IN ADDITION TO THIS CRACKED PART, THE BLADES SDR SIMA0392Seal · failedBOS - FLT 4579 - RIGHT ENGINE INTAKE SATURATED WITH OIL. CABIN AIR HAS CONTINUOUS FAINT OIL SMELL INFLIGHT. REMOVED AND REPLACED NR 1 PROP BLADE SEAL. (M)SDR AU010074Blade · damaged(AUS) LT PROPELLER BLADE DAMAGED BY MISSING SPINNER ATTACHMENT SCREW. THREE SCREWS MISSING FROM SPINNER. ONE SCREW WAS FOUND EMBEDDED IN THE PROPELLER BLADE. MAINTENANCE HAD BEEN CARRIED OUT ON THE PROPELLER PRIOR TO THE FLIGHT.SDR AU010038Tape · loose(AUS) LT PROPELLER BLADE LEADING EDGE TAPE LOOSE ON ONE BLADE.SDR 20010302AP002Blade · failedPROPELLER BLADE FAILED 14 INCHES FROM CENTER OF HUB.PROPELLER WAS FORWARDED TO NTSB LAB FOR FURTHER ANALYSIS.SDR MALA000740Tape · departedDELTA, DELTA T SHIFT OF 49 DEGREES ON LT ENGINE. CREW PERFORMED SEVERAL TRENDS WITH SAME RESULTS PULLED POWER BACK TO 40 PERCENT BEFORE STARTING SECOND TREND PER ORH. MAINTENANCE FOUND PROP TAPE FROM 1 BLADE LODGED IN INLET, LEFT ENGINE, REMOVED TAPE, ALL TASDR 20001229SH004Blade · crackedPROPELLERS REMOVED FOR OVERHAUL AND AD COMPLIANCE. BLADE SN 93464 IS SCRAP BECAUSE IT IS CRACKED IN THE SHANK. ONE OF THE BLADE THRUST BEARINGS PN A14B INSTALLED FOR THE BLADES HAD WRONG RETAINERS PN A159. S/B REPLACED WITH PN A969. COULD CAUSE BLADE SEPARSDR 20001229SH003Blade · crackedDISASSEMBLY OF PROPELLER FOR O/H AND AD COMPLIANCE REVEALED BLADE, SN 106993, IS SCRAP BECAUSE BALANCE HOLE TOO DEEP. MAX DEPTH IS 6.5 INCHES. BLADE, SN A27681, IS SCRAP BECAUSE IT IS CRACKED IN THE SHANK. BREAKAWAY TEST PERFORMED TO PUSH THE TUBE BACK IN TSDR SJ3RR003569Blade · misoverhauledTHE OVERHAUL PERFORMED ON THIS BLADE WAS NOT TO HARTZEL SPECIFICATION, AND AS A RESULT, THE BLADE HAD SOME SIGNIFICANT PROBLEMS THAT COULD HAVE RESULTED IN SAFETY OF FLIGHT ISSUES. UNABLE TO DETERMINE WHERE THE OVERHAUL WAS PERFORMED. PLEASE REFERENCE HARTZESDR AU001032Blade · separated(AUS) LEFT PROPELLER BLADE SECTION SEPARATED APPROXIMATELY 200 MM (7.87 INCHES) FROM THE BLADE TIP. FAILURE ORIGINATED FROM A PREVIOUS STONE STRIKE THAT HAD NOT BEEN ADEQUATELY BLENDED OUT. (X)SDR AU001328Blade · damaged(AUS) LT PROPELLER BLADE HOLED.SDR FJT00109382Propeller · crackedMQY - DURING NDT INSPECTION OF RIGHT PROPELLER IAW AD 2000-15-10 AND MCCAULEY 88234, THE NR 4 PROPELLER BLADE FAILED THE EDDY CURRENT INSPECTION. THIS INDICATES THAT THE BLADE WAS CRACKED. THE PROPELLER ASSEMBLY WAS REMOVED AND REPLACED WITH A SERVICEABLE ASSDR 20001120SH008Blade · crackedPROPELLER RECEIVED FOR ROUTINE OVERHAUL. AT DISASSEMBLY FOR OVERHAUL, NOTED BLADE, SN SC340-132/2239 WAS CRACKED IN OUTER SLEEVE AT ROOT END. BLADE REJECTED FROM FURTHER SERVICE. (X)SDR 20001120SH007Blade · crackedPROPELLER RECEIVED FOR REPAIR OF SLINGING GREASE AND LIGHT BLADE DAMAGE. BLADE, SN 784, WAS FOUND TO HAVE A CRACK RUNNING FROM PTFE FACE TO BLADE BEARING FACE ON OUTER SLEEVE AT ROOT END. BLADE REJECTED FROM SERVICE. (X)SDR CA001102006Blade · cracked(CAN) CRACK FOUND ON LEADING EDGE IN SHOT PEENED AREA, LOCATED IN A OLD LOCAL REPAIR AT STATION 46 INCH.SDR 20001101SH029Blade · crackedDURING EDDY CURRENT INSPECTION, FOUND EVIDENCE OF A POSSIBLE CRACK IN THE BLADE BETWEEN THE 39 AND 42 INCH STATIONS. (X)SDR 20001026SH014Blade · crackedDURING EDDY CURRENT INSPECTION, FOUND EVIDENCE OF A POSSIBLE CRACK IN THE BLADE BETWEEN THE 39 AND 42 INCH STATIONS. (X)SDR 20001018SH028Counterweight · crackedRELEVANT MAGNETIC PARTICLE INDICATION. (X)SDR 20001018SH027Blade · corrodedPROPELLER BLADE CORRODED. (X)SDR 20001018SH026Blade · corrodedPROPELLER BLADE CORRODED. (X)SDR AU000918Blade · split(AUS) RT PROPELLER NR 1 BLADE TRAILING EDGE SPLIT FROM THE BLADE TIP. LENGTH OF SPLIT 355.6MM (14IN).SDR 20001016SH027Blade · damagedPROPELLER WAS BEING SERVICED DURING AN ANNUAL 100-HOUR INSPECTION. WHILE ATTEMPTING TO GREASE THE PROPELLER, WATER WAS FOUND STREAMING FROM THE BLADE CLAMPS. PROPELLER WAS DISASSEMBLED AND LIGHT RUST AND CORROSION WAS FOUND THROUGHOUT THE PROPELLER ESPECIALLSDR 20001016SH026Blade · damagedPROPELLER WAS BEING SERVICED DURING AN ANNUAL 100-HOUR INSPECTION. WHILE ATTEMPTING TO GREASE THE PROPELLER, WATER WAS FOUND STREAMING FROM THE BLADE CLAMPS. PROPELLER WAS DISASSEMBLED AND LIGHT RUST AND CORROSION WAS FOUND THROUGHOUT THE PROPELLER ESPECIALLSDR CA001026003Blade · cracked(CAN) DURING DAILY INSPECTION, MAINTENANCE DISCOVERED A CRACK APPROXIMATELY 6 INCH LONG ALONG THE TRAILING EDGE OF NR 1 BLADE OF NR 1 PROPELLER, MIDWAY BETWEEN THE ROOT AND THE TIP. THE AFFECTED BLADE AND THE OPPOSING BLADE WERE REPLACED AS A BALANCED SET AND SDR 20001101SH003Blade · brokenAIRCRAFT AT CRUISE, ALT 11,000 FEET, NR 1 PROPELLER BLADE BROKE APPROXIMATELY 10 INCHES FROM HUB ON NR 2 ENGINE. BLADE DID NOT CONTACT AIRCRAFT. DAMAGE TO COWLING, NACELLE, REAR ENGINE MOUNT, OUTBOARD FLAP, WING TRAILING EDGE. ENGINE REMAINED ON WING. CREWSDR AU000783Blade · corroded(AUS) PROPELLER BLADES CORRODED CAUSING PAINT TO LIFT. (X)SDR 20000914SH018Seal · leakingPROPELLER OIL LEAKING FROM SERVICE PLUG, AND BLADE SEALS. NO INSTRUCTIONS PROVIDED FOR APPROVAL FOR RETURN TO SERVICE. (X)
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