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.

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 COLJun 11, 2001SDR 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) DAMAJun 11, 2001SDR 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.Jun 8, 2001 · N327EN · Dhav DHC8311SDR 20010604CW017Clamp · crackedCRACK DISCOVERED DURING ROUTINE 100 HOUR INSPECTION. DETECTED VISUALLY. REASON FOR CRACK NOT KNOWN. CLAMP ASSEMBLY REPLACED WITH FACTORY NEW UNIT.Jun 4, 2001 · N117BH · Casa C212200SDR 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.May 30, 2001 · N915AE · Bag JETSTM3201SDR 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.May 30, 2001 · N915AE · Bag JETSTM3201SDR 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.May 24, 2001SDR 20010612CW012Blade · crackedBLADE FOUND CRACKED IN THE SECOND RETENTION THREAD DURING PENETRANT INSPECTION PERFORMED AT OVERHAUL. NO RED DYE LEAKAGE REPORTED. NO ABNORMAL VIBRATION REPORTED.May 18, 2001 · N7735R · Beech E33CSDR 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 DISApr 18, 2001 · N1140P · Piper PA23150SDR 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 REPLAApr 17, 2001 · N231LN · Saab 340BSDR AU010265Erosion Shield · separated(AUS) PROPELLER BLADE EROSION SHIELD SEPARATED.Mar 25, 2001 · Fokker F27MK50SDR AU010299Ferrule · cracked(AUS) PROPELLER BLADE FERRULE CRACKED AROUND BEARING SHELF ORIGINATINGFROM A PREVIOUSLY DRILLED ACTUATING PIN HOLE. CRACK LENGTH 50.8MM (2IN).Mar 20, 2001 · Beech 95B55SDR AU010219Block · cracked(AUS) PROPELLER PITCH CHANGE BLOCKS CRACKED. PITCH CONTROL FORK WORNEXCESSIVELY. HUB PRELOAD PLATE DAMAGED DUE TO PREVIOUS FOREIGN OBJECT STRIKE.Mar 6, 2001 · Beech C24RSDR 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.Mar 5, 2001 · Emb EMB120SDR NWOR140K5Blade · crackedFOUND 3.5 INCH CRACK ALONG TRAILING EDGE SIDE OF RETENTION AREA OF BLADE.Mar 1, 2001SDR NWOR140K4Blade · crackedON INSPECTION 4.5 INCH CRACK WAS FOUND ON TRAILING EDGE SIDE OF BLADE RETENTION AREA.Mar 1, 2001SDR NWOR140K3Blade · crackedDURING INSPECTION CRACK WAS FOUND ALONG TRAILING EDGE OF RETENTION AREA.Mar 1, 2001SDR NWOR140K2Blade · crackedDURING INSPECTION, CRACK FOUND ALONG TRAILING EDGE OF RETENTION AREA OF BLADE.Mar 1, 2001SDR NWOR140K1Blade · crackedINSPECTION FOUND CRACK ALONG LEADING EDGE SIDE OF RETENTION AREA.Mar 1, 2001SDR NWOR140KBlade · crackedINSPECTION FOUND CRACKS AT TRAILING EDGE SIDE OF RETENTION AREA.Mar 1, 2001SDR 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.Feb 27, 2001 · Emb EMB120SDR 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 RFeb 19, 2001 · N269CA · Emb EMB120RTSDR 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 REFeb 19, 2001 · N269CA · Emb EMB120RTSDR 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 Feb 12, 2001 · Piper PA23250SDR 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)Feb 8, 2001 · N304AE · Saab 340BSDR 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.Jan 29, 2001 · Emb EMB120SDR AU010038Tape · loose(AUS) LT PROPELLER BLADE LEADING EDGE TAPE LOOSE ON ONE BLADE.Jan 11, 2001 · Dhav DHC8102SDR 20010302AP002Blade · failedPROPELLER BLADE FAILED 14 INCHES FROM CENTER OF HUB.PROPELLER WAS FORWARDED TO NTSB LAB FOR FURTHER ANALYSIS.Dec 12, 2000 · N582SP · Cessna 172SSDR 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 TADec 5, 2000 · N68XJ · Saab SF340ASDR 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 SEPARDec 1, 2000 · N708T · Multec D16ASDR 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 TDec 1, 2000 · N708T · Multec D16ASDR 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 HARTZENov 21, 2000 · Beech 1900CSDR 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)Oct 22, 2000 · Beech D95ASDR AU001328Blade · damaged(AUS) LT PROPELLER BLADE HOLED.Oct 20, 2000 · Dhav DHC8*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 ASOct 16, 2000 · N938AE · Bag JETSTM3201SDR 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)Oct 16, 2000SDR 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)Oct 16, 2000SDR CA001102006Blade · cracked(CAN) CRACK FOUND ON LEADING EDGE IN SHOT PEENED AREA, LOCATED IN A OLD LOCAL REPAIR AT STATION 46 INCH.Oct 12, 2000 · Cndair CL2151A10SDR 20001101SH029Blade · crackedDURING EDDY CURRENT INSPECTION, FOUND EVIDENCE OF A POSSIBLE CRACK IN THE BLADE BETWEEN THE 39 AND 42 INCH STATIONS. (X)Oct 11, 2000 · N936AE · Bag JETSTM3201SDR 20001026SH014Blade · crackedDURING EDDY CURRENT INSPECTION, FOUND EVIDENCE OF A POSSIBLE CRACK IN THE BLADE BETWEEN THE 39 AND 42 INCH STATIONS. (X)Oct 11, 2000 · N936AE · Bag JETSTM3201SDR 20001018SH028Counterweight · crackedRELEVANT MAGNETIC PARTICLE INDICATION. (X)Sep 25, 2000 · N401PC · Cessna 401ASDR 20001018SH027Blade · corrodedPROPELLER BLADE CORRODED. (X)Sep 21, 2000 · N401PC · Cessna 401ASDR 20001018SH026Blade · corrodedPROPELLER BLADE CORRODED. (X)Sep 21, 2000 · N401PC · Cessna 401ASDR AU000918Blade · split(AUS) RT PROPELLER NR 1 BLADE TRAILING EDGE SPLIT FROM THE BLADE TIP. LENGTH OF SPLIT 355.6MM (14IN).Sep 12, 2000 · Saab SF340ASDR 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 ESPECIALLSep 12, 2000 · N4120D · Helio H391BSDR 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 ESPECIALLSep 12, 2000 · N4120D · Helio H391BSDR 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 Sep 11, 2000 · Dhav DHC8311SDR 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. CREWSep 6, 2000 · N770MA · Mtsbsi MU2B35SDR AU000783Blade · corroded(AUS) PROPELLER BLADES CORRODED CAUSING PAINT TO LIFT. (X)Sep 4, 2000 · Cessna 150FSDR 20000914SH018Seal · leakingPROPELLER OIL LEAKING FROM SERVICE PLUG, AND BLADE SEALS. NO INSTRUCTIONS PROVIDED FOR APPROVAL FOR RETURN TO SERVICE. (X)Sep 3, 2000 · N913CT · Cessna 182S
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