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 CA150108010Blade · cracked(CAN) DURING PRE-FLIGHT INSPECTION THE NR 1 PROPELLOR BLADE ON THE NR 2 PROPELLOR ASSY WAS FOUND TO HAVE A LARGE CRACK ON THE LEADING EDGE, AT APPROXIMATELY THE CENTER OF THE PROPELLOR BLADE.SDR CA150106008Blade · cracked(CAN) PROPELLER BLADE TRAILING EDGE FOUND WITH A 2.5 INCH LONG CRACK RUNNING CORD-WISE, LOCATED APPROMAXIMATELY 50 INCH FROM THE BLADE TIP.CRACK IS OPEN, AT THE END OF TRAILING EDGE OF ABOUT 0.020 INCH WIDTH. BLADE WAS OVERHAUL AND REPAIRED 3000 HRS AGO. MANYSDR SWIA2015F00020Blade · crackedDURING MAJOR INSPECTION, FOUND FPI CRACK INDICATION IN FILLET RADIUS OF BLADE SHANK.SDR CA141217005Blade · cracked(CAN) OWNER REPORTED TO DIAMOND CANADA THAT HE FOUND ONE OF THE THREE PROPELLER BLADES SPLIT OPEN AT ROOT SECTION. SPLIT APPROX. FOUR INCHES IN LENGTH. BLADES HAD BEEN OVERHAULED AT 216.5 HOURS TOTAL TIME, CRACKED DISCOVERED AT 360 HOURS. TIME SINCE OVERHAUL 1SDR FAA2015120900010Blade · crackedCRACK INDICATION OF FILLET RADIUS OF BLADE SHANK, FOUND DURING MAJOR INSPECTION.SDR CA141210008Blade · cracked(CAN) FLIGHT CREW FELT PROPELLER VIBRATION ON GROUND WHEN OUT OF FEATHER. A CRACK WAS FOUND COMING OUT FROM UNDERNEATH THE EROSION SHEATH AT APPROX. MID-WAY OF BLADE. THE CRACK WAS ON BOTH SIDES OF PROPELLER BLADE. BLADE CHANGED AND AIRCRAFT RETURNED TO SERVISDR CA141114004Blade · cracked(CAN) UPON INSPECTION, A CRACK WAS FOUND IN THE TRAILING EDGE OF THE NR 6 BLADE OF THE NR 2 PROPELLER. THE PROPELLER BLADE WAS REPLACED AND THE AIRCRAFT SUBSEQUENTLY RETURNED TO SERVICE. THE VISIBLE CRACK IS APPROX. 1/2 INCH IN LENGTH AND IS LOCATED APPROX. 17SDR CA140929007Bearing · damaged(CAN) WHILE INVESTIGATING AN OIL LEAK ON THE RT PROP AT THE NR 1 BLADE, MAINTENANCE FOUND THE BLADE BEARING RACE DAMAGED. ADDITIONAL DAMAGE WAS FOUND IN THE BLADE BORE OF THE HUB. THE RT PROP ASSEMBLY WAS REPLACED.SDR CA140818015Blade · deformed(CAN) THE PROPELLER BLADE WAS REMOVED AND DISASSEMBLED FOR INSPECTION. THE INSPECTION REVEALED THAT THE BLADE TIP DEFORMITY WAS CAUSED BY THE FAILURE OF THE BLADE INTERNAL RUBBER CENTRE SECTION RIB. PORTIONS OF THE RIGHT SIDE TRAILING EDGE CENTRE SECTION RIB HSDR CA140721022Blade · damaged(CAN) DUE TO REPORTS OF A MINOR VIBRATION SUSPECTED TO BE COMING FROM NR 2 PROP, THE PROPELLER WAS INSPECTED. THE CABLE ASSY ON PROP NR 2 BLADE NR 6 HAD UNUSUALLY DARK GREASE RELATIVE TO THE OTHER BLADES, SO BLADE NR 6 WAS REMOVED FOR FURTHER INVESTIGATION. SDR CA140828008Snap Ring · stretched(CAN) BLADE NR 1 SNAP RING FAILED AND RELEASED FROM THE SNAP RING GROOVE.SDR 2014FA0000396Snap Ring · corrodedPROPELLER WAS OVERHAULED 5 MONTHS, 96 HOURS AGO, AND IS IN FOR INSPECTION. SNAP RING AROUND BASE OF A BLADE AND THE GROOVE IN THE BLADE HAS CORROSION. PROPELLER WAS REMOVED AND BEING SENT BACK FOR REPAIR. NO CORROSION PREVENTATIVE WAS OBSERVED ON THE SNAP SDR CA140701017Blade · fractured(CAN) LEFT ENGINE PROPELLER, A PORTION OF THE BLADE TIP SEPARATED DURING LIFT OFF FROM WATER. THE SEPARATED SEGMENT PENETRATED THE LT SIDE FUSELAGE AND EXITED ON THE RT SIDE. ACFT RETURNED TO BASE WITH NO FURTHER INDIDENT.SDR QXEA2014061200504Blade · out of balanceABNORMAL VIBRATION DURING CLIMBOUT WITH CONDITION LEVERS AT 850 RPM. VIBRATION LESSONED AT 900 & 1020 RPM BUT RETURNED AT 850 RPM AGAIN. RETURNED TO FIELD. LANDING UNEVENTFUL. PERFORMED BALANCE ON NR 1 & NR 2 PROPELLERS, PERFORMED 6 BLADE RETORQUE ON NR 1 PSDR 39LA2014060900005Propeller · splitIN CRUISE FLIGHT HEARD A LOUD BANG. SCANNED THE ENG INSTRUMENTS, THE LT TORQUE GAUGE WAS AT 120%, THE LT EGT HAD DROPPED BY APPROXIMATELY 100 DEGREES & THE LT FUEL FLOW HAD DROPPED TO 215 PPH FROM 300PPH. THERE WAS NO OTHER INDICATIONS OF A PROBLEM. PULLEDSDR CA140526009Blade · unsecure(CAN) ACFT EXPERIENCED HEAVY VIBRATION, AND MANAGED TO LAND SAFELY AT DEPARTURE AIRPORT. ON THE GROUND, MAINTENANCE FOUND THAT LT PROPELLER BLADE WAS IN A ZERO PITCH ANGLE WHEN ALL THE OTHER WERE IN FEATHER. AFTER DISSASSEMBLY, THE PROPELLER BLADE PIN WAS FOSDR CA140918015Blade · cracked(CAN) DURING A SCHEDULED INSPECTION CRACKS WERE VISIBLE ON THE PROPELLER BLADE TIPS. PROPELLER WAS REMOVED AND FORWARDED FOR FURTHER INSPECTION. AFTER REMOVAL OF THE PAINT IT WAS FOUND THAT THE CRACKS WERE THROUGH THE FIBRE GLASS LAYER AND INTO THE UNDER LYINGSDR CA140510001Blade · contaminated(CAN) DURING DEFECT MAINTENANCE AND GROUND RUN, AN UNUSUAL VIBRATION WAS FELT WHICH SEEMED TO BE PROP RELATED, FURTHER INSPECTION REVEALED WHAT LOOKED LIKE WATER SWELLING OF THE PROPELLER BLADES. PROP REMOVED AND SENT FOR REPAIR.SDR CA140501006Plug · cracked(CAN) PRIOR TO RETURN THE AIRCRAFT TO SERVICE, AFTER COMPLETION OF PROPELLER ASSEMBLY INSTALLATION, AN ENGINE RUN UP HAS BEEN CARRIED OUT TO CONFIRM PROPER PERFORMANCE. SHORTLY AFTER L/H ENGINE START, THE MAINTENANCE CREW FELT A STRONG VIBRATION COMING FROM THSDR CA140319007Bearing · split(CAN) NR 1 PROPELLER ASSY REMOVED FOR UNSCHEDULED MAINTENANCE. IT WAS DISCOVERED THAT ONE BALL BEARING WAS SPLIT IN HALF IN THE BALL RETAINER ASSY. DAMAGED BALL WAS LOCATED IN THE MIDDLE OF THE RETAINER. THE SPLIT BALL BEARING DAMAGED ADJACENT BEARING RACE, SDR CA140224025Blade · misrepaired(CAN) PROPELLER BLADES DEEM UNSERVICEABLE BY FACTORY DUE TO IMPROPER/UNAPPROVED SHOTPEENING BY LAST REPAIR SHOP.SDR CA140129004Boot · cracked(CAN) ON WALK AROUND OF THE ACFT AND PROPELLERS A CHORDWISE CRACK WITHIN 6" OF THE BOOT WAS FOUND ON THE EROSION SHIELD. THE PROP SHOWED NO SIGN OF IMPACT DAMAGE THAT MAY HAVE CONTRIBUTED TO THIS CRACKING. PROP WAS REPLACE. THIS IS THE THIRD INCIDENT WE HAVSDR CA140213006Blade · cracked(CAN) CREW FOUND DURING WALK AROUND INSPECTION, THE NR 2 PROPELLER, NR 6 BLADE HAD A CRACK ABOUT 2.5" X 2" DOWN THE BOTTOM OF THE T/E OF THE BLADE. SERVICEABLE BLADE ASSY INSTALLED IAW AMM 61-10-01-400-801, NR 2 PROP, NR 6 BLADE.SDR HNAA2013110600566Blade · vibrationNR 2 PROPELLER HAS EXCESSIVE VIBRATION IN FLIGHT. SHIMMED NR 3 AND NR 4 BLADES IAW MM 61-10-00. OPS CHECKED GOOD.SDR S3LY013FA0000583Blade · damagedREPORTED PROPELLER VIBRATION AND DOME NOT RUNNING CONCENTRICALLY (WOBBLING) IN OPERATION. DISCOVERED THAT THE BEVELLED THRUST BEARING OF BLADE NR 3 WAS CRACKED. CHAFING RING FOR THIS BLADE WAS DISINTEGRATING. ON BARREL SPLIT IT WAS OBSERVED THAT THE CHAFISDR CA130904012Blade · damaged(CAN) DURING THE 50 HOUR INSPECTION ON ACFT, A "BUBBLE" WAS NOTICED ON ONE OF THE LT PROP BLADES. FURTHER INVESTIGATION SHOWED DELAMINATION ON THE PROP BLADE THAT WAS 23" FROM THE BLADE TIP, AND ABOUT 1.320" X 0.745" IN SIZE. THE LT PROP SN IS FWA2835.SDR 2013FA0000476Retaining Ring · detachedRETAINING RINGDEPARTED PROPELLER BLADE, NR 1 IN FLIGHT. LANDED, REMOVED PROPELLER AND SENT FOR REPAIR AFTER 4.4 HRS SINCE O/H. BLADE NR 1 REMOVE SCRATCH MARKS SANDED AND REPAIR IAW BOM100, ALL DIMENSION CHECK FOR COMPLIANCE. PAINTED BLADE AND INSTALLED FACTSDR CA130802003Collar · cracked(CAN) OPERATOR REPORTED DISCOVERY OF DAMAGED BLADE COLLAR DURING ROUTINE AFTER FLIGHT INSPECTION. SOME MATERIAL OF THE COLLAR WAS NOTED AS MISSING. NO OTHER INFORMATION TO REPORT. BLADE HAS BEEN SENT FOR INSPECTION AND REPAIR. PHOTO IN ATTACHMENTS. HS BULLETSDR CA130712006Blade · eroded(CAN) DURING A ROUTINE 100 HR/ANNUAL INSPECTION IT WAS DISCOVERED THAT THE WOOD PROPELLER WAS QUITE ERODED ESPECIALLY ALONG THE BLADE LEADING EDGES. CLOSER INSPECTION OF 1 BLADE IN PARTICULAR NOTED THAT THE FIBERGLASS L/E WAS ERODED AND STARTING TO SEPARATE FSDR CA130522006Blade · damaged(CAN) LEFT PROPELLER PROP BLADE NR 3 FOUND WITH PLAY AND LEAKING, BLADE NR 3 WAS REMOVED AND BALL BEARINGS, PN 69992A16 WERE FOUND DAMAGED, MELTED AND BLADE BUTT WAS ALSO FOUND WITH DAMAGE, GROOVED. PROPELLER STILL UNDER INVESTIGATION AND BLADE NR 1, 2 & 4 WISDR CA130308001Bearing Race · corroded(CAN) BLADE WAS REMOVED SERVICEABLE FROM A HUB THAT WAS DUE FOR O/H. DURING INSTALLATION ONTO A SERVICEABLE HUB, TSO 0, THE LOCKING CABLE ASSY COULD NOT BE INSERTED DUE TO HIGH RESISTANCE. BLADE WAS DISSASSEMBLED TO INSPECTE THE SLEEVE INTERNAL AREA FOR POSSSDR CA130308002Blade · cracked(CAN) PROPELLER BLADE FOUND CRACKED ON L/E APPROXIMATELY 1.25" FROM THE BLADE TIP. THE CRACK IS APPROX .1875" LONG. THIS CRACK WAS NOTED IN A SMALL SMOOTH ROCK CHIP. PROPELLER WAS REMOVED FROM SERVICE. THIS DEFECT WAS FOUND DURING A ROUTINE 100HR TYPE INSPECTSDR 2013FA0000139Blade · failedPROPELLER BLADE FAILURE. SUSPECTED DUE TO PRE-DELAMINATION DAMAGE.SDR CA130128019Blade · cracked(CAN) BLADE SHANK WAS REWORKED FOR CORROSION TO MAXIMUM LIMITS IN ZONE 1, QUADRANT 2. LPI INSPECTION SUBSEQUENTLY REVEALED WHAT LOOKS TO BE A CRACK.SDR HNAA2012123101136Blade · sparksSPARKS OBSERVED COMING FROM NR 2 PROPELLER AFT OF THE SPINNER. NO VIBRATION AND PROP HEAT INDICATED NORMAL. FOUND RT PROPELLER NR 4 BLADE HEATER MAT BURNED. R & R NR 4 BLADE IAW 61-10-07.SDR SWIA201232244Blade · crackedLEFT PROP NR 2 BLADE LEADING EDGE IS CRACKED. (SERVICE) REPLACED LEFT PROP NR 2 BLADE IN REFERENCE TO CMM.SDR CA121217002Blade · distorted(CAN) DURING PREFLIGHT INSPECTION, ENGINEERS NOTICED THAT THE LT ENGINE, NR 4 PROPELLER BLADE WAS DEFORMED. THE BLADE WAS IMMEDIATELY REMOVED FROM THE ACFT AND SENT FOR ANALYSIS.SDR CA121114011Blade · cracked(CAN) REF: DEFECT-1085552, THE RT PROPELLER, NR 4 BLADE HAS AN APPROXIMATELY 3" CRACK EMANATING FROM UNDER THE EROSION STRIP AT APPROXIMATELY BS 46 ON THE CAMBER SIDE. RESOLVED ON WO: 360653, TASKCARD: NR-00008, RT 4 PROPELLER BLADE REPLACED IAW MM. PN- SFA13SDR CA121030006Bearing Race · failed(CAN) PROPELLER SCHEDULED REMOVAL. DURING THE DISASSEMBLY, THEY FOUND THE INNER RACE ON RT-3 BLADE HAD FAILED AND THE BEARING SURFACE WAS BROKEN AND SPLIT RADIALLY ALONG THE BALL BEARING PATH. A 6" PIECE HAD SPLIT AND BROKEN AWAY. REF: IPC-61-13-06, PG 1037SDR CA120824001Collar · debonded(CAN) FLIGHT CREW REPORTED A BIRD STRIKE DURING THE APPROACH. DURING THE BIRD STRIKE INSPECTION, MAINTENANCE FOUND THE RT PROPELLER NR 1 BLADE REAR COLLAR HALF DISBONDED, CMM 61-10-00, IPL FIG 1, ITEM 720. THE BLADE ASSY WAS REPLACED AND THE ACFT RELEASED FORSDR 2012FA0000539Blade · damagedPROPELLER LOST APPROXIMATELY 5.5 INCHES FROM TIP IN FLIGHT.SDR SWIA201231227Blade · crackedLEFT PROPELLER ASSEMBLY NR 2 BLADE IS CRACKED AT THE SHANK AREA. (SERVICE) REPLACED LEFT NR 2 PROPELLER BLADE IN REFERENCE TO AMM.SDR 2012FA0000445Blade · brokenPROPELLER SEPARATION IN FLIGHT, AFTER TAKEOFF THE PROPELLER LOST APROX 66 PERCENT OF NR 1 BLADE, FORCING THE PILOT TO DO AN EMERGENCY LANDING.SDR 2012FA0000481Blade · looseDURING SECOND ENGINE START OF THE DAY, THE RT PROP STARTED VIBRATING. START WAS ABORTED AT APPROX 40 PERCENT N1. ON INSPECTION OF PROPELLER, FOUND 3 BLADES FEATHERED AND IN LOW PITCH. NR 1 BLADE COULD BE REPOSITIONED BY HAND. REMOVED PROPELLER AND SENT FORSDR CA120604009Blade · cracked(CAN) WHILE CARRYING OUT AN OIL CHECK, MAINTENANCE NOTICED BLADE TAPE COMING OFF NR 2 PROP, NR 1 BLADE. DURING BLADE TAPE REPLACEMENT A 3 CRACK WAS FOUND IN THE COMPOSITE PORTION OF THE BLADE EXTENDING AFT FROM THE L/E TOWARD THE T/E. THE BLADE WAS REPLACED SDR 2012FA0000363Blade · gougedNOTICED OIL ON NOSE COWL. PROP REMOVED TO REPLACE CRANKSHAFT O-RING. BUT DURING REMOVAL, IT WAS DISCOVERED THAT THE SEEPAGE WAS ACTUALLY COMING FROM A BLADE. SEEPAGE WAS CONSIDERED MINOR AND PROPELLER OPERATION APPEARED NORMAL. REPAIR SHOP DISCOVERED DURINSDR CA120522008Blade · damaged(CAN) DURING APPROACH AT APPROXIMATELY 1500 FT A LOUD TAP NOISE WAS HEARD. THIS NOISE SOUNDED UNLIKE THE TYPICAL THUD THAT A BIRD MAY MAKE UPON IMPACT. CREW FOUND DURING WALK AROUND TO CHECK THE ACFT FOR DAMAGE AND SUBSEQUENTLY DISCOVERED A LARGE IMPACT MARKSDR CA120425002Blade · damaged(CAN) DURING A RAMP SERVICE CHECK, THE ENGINEER NOTICED THAT A BLADE ON THE NR 1 PROP ASSY HAD THE HEATER ELEMENT BURNED AND A HOLE WAS BURNING INTO THE PROP BLADE ASSY. LINE MAINTENANCE REPLACED THE AFFECTED BLADE IAW THE AMM. ACFT RETURNED TO SERVICE.SDR CA120321008Blade · cracked(CAN) AME DISCOVERED IMPACT DAMAGED ON PROPELLER BLADE DURING AN INSPECTION. SENT FOR EVALUATION. REPAIR STATIONS VISUALLY INSPECTED IMPACT DAMAGE. ROCK IMPACT HIT FACE SIDE OF BLADE. IMPACT WAS DEEP AND SEVERE ENOUGH TO CAUSE FURTHER DAMAGE THROUGH TO CAMSDR CA120302003Bearing Race · deteriorated(CAN) DURING SCHEDULED MAINTENANCE ON THE LT PROPELLER ASSY, DAMAGE WAS FOUND ON THE NR 3 BLADE. UPON REMOVAL OF THE BLADE METAL FLAKES WERE FOUND IN THE OIL. FURTHER TROUBLESHOOTING REVEALED THAT THE HUB ASSY NR 4 BLADE OUTER RACE, PN 782301-1 WAS DETERIORAT
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