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 00065074Bearing · corrodedCORROSION ON PROPELLER BLADE BEARINGS.SDR 0064492Counterweight · corrodedCORROSION ON COUNTERWEIGHT.SDR TXHA6881Blade · looseON 11/5/02, POST FLIGHT INSPECTION WAS CARRIED OUT. FOUND 2 BLADES ON RIGHT PROP SN-AP37 TO HAVE EXCESSIVE FORWARD AND ACT PLAY. PROP MFG O/H FACILITY CONSULTED AND CONFIRMED PLAY TO BE EXCESSIVE. PROP REMOVED AND REPLACED. PREVENT RECURRENCE IS NOT TO USESDR CA030103001Bearing · dented(CAN) AFTER DISASSEMBLY OF THE PROPELLER IT WAS NOTED THAT ALL THREE BLADE THRUST BEARINGS WERE BADLY DENTED, BEYOND REUSE. THE BEARINGS, LUBRICANTS, AND BALLS WERE ALL REPLACED AND THE PROPELLER WAS ASSEMBLED.SDR 2002FA0001381Blade · crackedDURING INSPECTION, MAINTENANCE WAS UNABLE TO DETERMINE COMPLIANCE WITH AD. DUE TO INADEQUATE RECORDS, PROPELLER WAS SUBMITTED FOR OVERHAUL AND ALSO TO REPLACE THE HUB IAW AD. AT DISASSEMBLY, PROP WAS FOUND TO HAVE COLD COMPRESSION ROLLED SHANKS. HOWEVER, DUSDR 2003F00158Blade · crackedFOUND CRACK ON NR 1 BLADE OF NR 2 ENGNE PROP ASSEMBLY. REMOVED NR 1 BLADE OF NR 2 ENGINE PROP ASSEMBLY IAW HAMILTON SUNDSTRAND MM 61-10-00, PATE 307-311 PARA 5A. INSTALLED NEW PROP BLADE IAW HAMILTON SUNSTRAND MM 61-10-00, PAGE 705-714 PAR, G/H. GROUND RUN-SDR KPVA200236Blade · crackedMAINTENANCE FOUND CRACK ON NR 1 BLADE OF NR 2 ENGINE PROP ASSY. REMOVED NR 1 BLADE OF NR 2 ENGINE PROP ASSY IAW HAMILTON SUNDSTRAND MM 61-10-00, PAGE 307-311 PARA 5A. INSTALLED NEW PROP BLADE IAW HAMILTON SUNSTRAND MM 61-10-00, PAGE 705-714 PAR, G/H. GROUNDSDR CA021204003Dowel Pin · broken(CAN) DURING OVERHAUL A BROKEN COUNTERWEIGHT DOWEL PIN WAS DISCOVERED. NEW INSTALLED.SDR CA021125009Propeller · misrepaired(CAN) PROPELLER WITH NO HISTORY SENT IN FOR OVERHAUL. - DURING LIQUID PENETRANT INSPECTION, FOUND SUSPICIOUS WELDING WITH EDDY CURRENT CONDUCTIVITY PROBE AS WELDED AREA MATCHED GOOD AREA. KELLERS ETCH SHOWED DISCOLOURATION AND CHROMIC ACID ANODIZING CONFIRMED SDR CA021120005Blade · cracked(CAN) ENGINEER NOTICED CRACKED TRAILING EDGE OF PROPELLER BLADE, FOUND DURING POST FLIGHT INSPECTION IN THE HANGER.SDR HNAA0200077Bearing Race · brokenNOISE COMING FROM NR 2 PROPELLER WHEN ROTATING. REPLACED NR 2 PROPELLER ASSEMBLY. DISASSEMBLY SHOWED DAMAGE TO THE NR 2 BLADE AND ITS SPLIT RING BEARING RACE. APPROXIMATELY ONE INCH OF MATERIAL HAS CRACKED/BROKEN AWAY FROM THE END OF ONE BEARING SPLIT RING SDR CA021119005Blade · improper part(CAN) PROPELLER HAD BEEN WELDED TO COVER UP DEFECTS. PROPELLER IS SCRAP. THIS IS A REOCCURRING PROBLEM.SDR L10666Clamp · crackedPROPELLER WAS RECEIVED FOR OVERHAUL AND DURING DYE PENETRANT INSPECTION TWO CRACK INDICATIONS WERE NOTED IN THE BOLT HOLE AREA. THEN AN EDDY CURRENT INSPECTION WAS PERFORMED WHICH CONFIRMED PRIOR INDICATIONS. CLAMP WAS RED TAGGED AND REMOVED FROM SERVICE. PARTSDR AUS20021098Blade · delaminated(AUS) PROPELLER LEADING EDGE DELAMINATING IN AREA OF TIP.SDR CA021007008Seal · leaking(CAN) DURING ENGINE RUN FOLLOWING MAINTENANCE THE LEFT PROP STARTED LEAKING OIL. LT PROP NR 1 BLADE SEAL WAS REPLACED AND ENGINE RE RUN WITH NO FURTHER EVIDENCE OF LEAKAGE. THE INNER SPRING OF THE FAILED BLADE SEAL HAD BROKEN AT THE WELD.SDR CA020913006Bearing · broken(CAN) AFTER TAKING THE PROPELLER APART, IT WAS NOTED THAT NR 2 BLADE THRUST BEARING WAS BROKEN INTO SEVERAL SMALL PIECES. AS A RESULT OF THIS BROKEN BEARING, THERE WAS SOME MINOR DAMAGE TO THE BLADE SHOULDERS. ONE BEARING WAS ALSO FOUND CORRODED ON THE OUTESDR VNAA0209007Blade · out of adjustDURING CLIMBOUT, THE CREW REPORTED THAT THE LEFT HAND FUEL SHUT OFF VALVE IS CLOSED AND THERE WAS A TORQUE SPLIT OF 5 PERCENT. THE CREW ELECTED TO RETURN TO YOW. THE AIRCRAFT WAS THEN FERRIED TO PIT WHERE MAINTENANCE PERFORMED OPERATIONAL CHECKS ON THE FUEL SDR 2002FA0001139Blade · crackedPROPELLER BLADE SHANK CRACKED RADIALLY AT THE JUNCTION OF THE SHANK AND THE BLADE. SLIGHT FORE AND AFT BLADE MOVEMENT DETECTABLE. ALL 3 BLADES CRACKED. INSTALLATION LOOKED PROPER WITH CORRECT TORQUE ON HUB AT BLADE ATTACH POINT.SDR AUS20020931Blade · unapproved part(AUS) PROPELLER BLADE SUSPECT UNAPPROVED PART. INVESTIGATION FOUND THAT THE BLADE HAD ORIGINALLY BEEN AN FC7666A BLADE BUT HAD BEEN ILLEGALLY MODIFIED BY UNKNOWN PARTIES TO AN F7666A BLADE. THE BLADE MANUFACTURER WAS CONTACTED AND CONFIRMED THAT THE BLADE WISDR CA020912006Clamp · cracked(CAN) PROPELLER EXPERIENCED VIBRATIONS, WENT IN FOR SCHEDULED MAINTENANCE, CRACKED CLAMP WAS FOUND. ALSO BLADES HAD SLIPPED IN CLAMPS. PROPELLER WAS SENT IN FOR OVERHAUL AND REPAIR.SDR CA020821003Clamp · cracked(CAN) DURING A SCHEDULED INSPECTION, THE NR 3 REAR BLADE CLAMP WAS FOUND TO HAVE A 2 INCH CRACK ACROSS IT. THE PROPELLER WAS REMOVED AND SENT IN FOR OVERHAUL.SDR AUS20020900Plug · cracked(AUS) LT PROPELLER NR 2 BLADE BUTT PLUG CRACKED ALLOWING OIL TO LEAK INTO THE BLADE CAVITY.SDR AUS20020897O-Ring · leaking(AUS) RT PROPELLER BLADE O-RING SEAL STICKING. OIL LEAKING PAST THE SEAL ENTERED THE ENGINE AIR INTAKE AND FLOWED THROUGH THE RT BLEED AIR SYSTEM INTO THE CABIN.SDR AUS20020808Blade · bird strike(AUS) AIRCRAFT SUFFERED A BIRDSTRIKE ON TAKEOFF. INSPECTION COULD FIND NO IMPACT DAMAGE ON AIRFRAME OR ENGINE. EVIDENCE OF SUPERFICIAL DAMAGE TO RT PROPELLER BLADES.SDR CA020729003Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. EXTRA WORK REQUIRED TO REMOVE CORROSION CARRIED OUT: AN OVERHAUL. AS PER MCCAULEY MANUAL 730720SDR AUS20020622Blade · corroded(AUS) PROPELLER BLADES CORRODED IN AREA OF BLADE SHANK RADIUS.SDR CA020724003Blade · cracked(CAN) PROP WAS SLOW TO CYCLE THROUGH HIGH PITCH. PROP INSPECTED & HUB FOUND CRACKED ABOUT 6 INCHES LONG AROUND NR 1 BLADE SHANK. PROP SENT TO HOPE AERO FOR OVERHAUL.SDR C2XA02IA102Blade · wornIAH- FLIGHT 3797, DURING TAKEOFF THE CREW NOTED THAT THE NR 1 ENGINE HAD A VIBRATION. THE AIRCRAFT DID AN AIR RETURN, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 BLADE, NR 1 PROPELLER ASSEMBLY (DUE TO A WORN PIN/ROLLER ASSESDR CA020502002Blade · cracked(CAN) DURING A DAILY INSPECTION, A CRACK ON A PROP BLADE APPROX 5 LONG, NO REPORT FROM THE PILOT AND NO SIGN OF IMPACT WAS FOUND DURING THE VISUAL INSPECTION. IT WAS REPORTED THAT A FEW DAYS BEFORE PAINT STARTED PEELING OFF FROM THAT BLADE AND KEPT PROGRESSINGSDR 2002F00439Blade · crackedLEADING EDGES CRACKED ON TWO BLADES.SDR 2002F00362Erosion Shield · crackedLEADING EDGES CRACKED ON 2 BLADES.SDR CA020307007O-Ring · failed(CAN) PROPELLER LEAKING RED DYE OIL FROM BLADE NR 2. BLADE NR 2 O-RING FOUND SHREDED WHICH WAS THE REASON FOR THE OIL LEAK. ALSO FOUND 2 CRACKED SLOT BLOCKS AND A WORN ACTUATING PIN ASSEMBLY.SDR TYW2002F00000Blade · failed11 INCHES SEPRATED FROM ONE PROPELLER BLADE DURING FLIGHT. AIRCRAFT WAS SPRAYING A CROP AND WAS IN A TURN WHEN BLADE TIP SEPARATED.SDR AUS20020102Pin · broken(AUS) PROPELLER BLADE ACTUATING PIN BROKEN.SDR AUS20020103Pin · broken(AUS) PROPELLER BLADE PITCH ACTUATING PIN BROKEN.SDR AUS20020083Blade · cracked(AUS) LT PROPELLER NR 2 BLADE CRACKED. CRACK LENGTH APPROXIMATELY 40MM (1.57IN) RUNNING CHORDWISE ACROSS THE BLADE FROM THE TRAILING EDGE. CRACK IS LOCATED APPROXIMATELY 150MM (5.9IN) FROM THE BLADE TIP.SDR CA020205004Bearing · dented(CAN) BEARING WAS BADLY DENTED ON BALL SURFACE. MUSHROOM CRACKED AROUND BASE. ALL BEARINGS REPLACED.MUSHROOM REPLACED.BEARINGS P/N A0971MUSHROOM P/N A0856SDR AUS20020087Blade · misrepaired(AUS) INSPECTION OF PROPELLER WHEN RECEIVED FOR REPAIR FOUND THAT THE BLADE THREADS HAD BEEN TRUNCATED TO COMPLY WITH AD/PMC/24/3 BUT HAD NOT BEEN SHOT PEENED. THE RETENTION NUTS DID NOT HAVE THE O-RING GROOVE WIDENED AS LISTED IN SL 1990-2. AD/PMC/41HAD NOT BSDR 2002F00036Blade · crackedTWO CRACK INDICATIONS ON THE BLADE SHANK. ONE IN THE FILLET AREA AND THE OTHER IN THE BLADE BUTT AREA. INDICATIONS WERE PARALLEL AND 2 TO 3 INCHES IN LENGTH.SDR 2002FA0000210Blade · brokenBLADE LOST APPROXIMATELY 11 INCHES INBOARD FROM TIP. HAD PREVIOUS KNOWN GROUND STRIKE ALL BLADES. REMOVED SUBJECT BLADES AND HUB FROM SERVICE. REPLACED WITH NEW. 2 OTHER BLADES SHOW SIGNS OF STRAIGHTING 02-01-2002SDR 2001FA0000648Blade · crackedPROPELLER WAS REMOVED FROM AIRCRAFT TO CORRECT GREASE LEAK. AT DISASSEMBLY, BLADE (SN 279) WAS FOUND TO BE CRACKED ON OUTER SLEEVE AT ROOT END. BLADE REJECTED FROM FURTHER SERVICE.SDR CA011218006Blade · burned(CAN) CREW REPORTED FIRE ON THE NR 1 ENGINE, NO INDICATION FROM THE FIRE WARNING SYSTEM, APPEARS TO BE COMING FROM PROP SPINNER AREA. MAINTENANCE TOLD VERBALLY THAT THIS EVENT HAPPENED 5 MINUTES AFTER TAKEOFF FROM THE AIRPORT. THE AIRCRAFT RETURNED TO BASE. THSDR 2001FA0000645Blade · crackedPROPELLER RECEIVED FOR ROUTINE OVERHAUL. AT TEARDOWN, FOUND BLADE (PN 6607132886 SN 2) CRACKED IN OUTER SLEEVE APPROXIMATELY 2.5 INCHES LONG. BLADE REJECTED FROM FURTHER SERVICE.SDR NSV2001F00000Blade · chippedMIX DISCOVERED A CHIP IN THE BLADE FACE OF THE NR 1 PROP DURING A PREFLIGHT INSPECTION. MECHANIC LOG ENTRY READS OK FOR CONTINUED SERVICE (IAW 811303 FROM HARTZELL PROPELLERS)SDR 2001FA0000492Blade · crackedCRACK FOUND IN BLADE SHANK BETWEEN TWO SHOULDERS APPROX 2 INCHES IN LENGTH. THREE HUNDRED HOURS EST SINCE LAST INSPECTION.SDR CA011001008Erosion Shield · cracked(CAN) DURING ROUTINE INSPECTION, MAINTENANCE DISCOVERED DELAMINATION AT A CRACK IN THE NR 2 BLADE EROSION SHEATH OF THE NR 1 PROPELLER. FURTHER INVESTIGATION REVEALED THAT THE CRACK HAD ORIGINATED AT THE TERMINATION POINT OF THE HEATER ELEMENT EROSION TAPE ON SDR 2001FA0000443Blade · crackedMCAULEY BLADE PART S90AT-2 WITH SERIAL NUMBER OD044YSC WAS RECEIVED FOR OVERHAUL. BLADE TIMES ARE UNKNOWN. BLADE RECEIVED AS A SINGLE BLADE WITH FERRULE INSTALLED. AFTER FERRULE REMOVAL, DURING BLADE BUTT, FLORESCENT PENETRATE INSPECTION, BLADE WAS DISCOVERSDR 2001FA0000210Blade · crackedPILOT REPORTED ON TAKE OFF THAT THE PROPELLER WOULD NOT MAKE FULL POWER. PILOT RETURNED TO THE FIELD. PRIOR TO TOUCHDOWN, PILOT EXPERIENCED A VIBRATION. IMMEDIATELY AFTER TOUCHDOWN, THE VIBRATION INCREASED SIGNIFICANTLY, AND THE ENGINE SHUT DOWN. A FIELD ISDR CA010725007Seal · broken(CAN) THE PROPELLER BLADE SEAL HAD SPRING INSIDE OF IT AND THE TWO ENDS ARE WELDED TOGETHER BY THE MANUFACTURE. THE SPRING BROKE AT THE WELDED JOINT CAUSING OIL TO LEAK OUT OF THE HUB AT THE BLADE ROOT. IT WAS NOTICED DURING A D.I AFTER THE FLIGHT. THE SEAL ANSDR B2P2001F00000Bearing · damagedPROPELLER WAS RECEIVED FOR O/H WITH EXCESSIVE GREASE LEAKAGE FROM ALL BLADES. WHEN PROP WAS DISASSEMBLED, THE HUB UNIT WAS FILLED WITH EXCESSIVE AMOUNTS OF GREASE. UPON FURTHER INSPECTION, THE GREASE WAS FOUND TO CONTAIN SEVERAL PIECES OF THE BLADE BEARING R
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