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 TRBA2012059001Retainer · crackedDURING MX INSPECTION RT PROPELLER BLADE NR 4 RETAINER RING CRACK AT ONE OF THE ATACHING POINT. THE ACFT WAS REMOVED FROM SERVICE. REPLACED RT PROP NR 4 BLADE RETAINER IAW 61-10-00. THE ACFT RETURNED TO SERVICE.SDR CA120223002Blade · fractured(CAN) DURING A SCHEDULED BLADE REPLACEMENT FOR RESTORATION, 10500 FLIGHT HR TASK, DAMAGES WERE FOUND ON THE BLADE RACE AND THE ASSOCIATED HUB OUTER RACE, PN 782301-1. THE BLADE RACE IS SEVERELY DAMAGED, FRACTURED, BROKEN PIECES, METAL DISPLACEMENT, PLATING MISSDR CA120215010Blade · eroded(CAN) THREE OUT OF THE FIVE BLADES HAD EROSION DAMAGE INTO THE WOOD APR .1250" TO .1875" DEEP INTO THE WOOD CORE. OVERALL DIMENSIONS OF THE DAMAGE WAS BEYOND .5 X .5 OF AN INCH. REPAIR CARRIED OUT IAW MFG. PROP WAS REMOVED IN ORDER TO FACILITATE THE REPAIR SDR CA111207008Blade · cracked(CAN) UPON VISUAL INSPECTION LT NR 1 PROPELLER BLADE FOUND A CRACK RUNNING PERPENDICULAR ALONG THE NICKEL SHEATH THAT HAS STARTED TO RUN VERITCAL AND INTO THE COMPOSITE OF THE BLADE ITSELF. PROPELLER BLADE WAS COMING DUE FOR O/H AND REMOVED EARLY DUE TO CRACKSDR CA111020003Collar · missing(CAN) THE PROP WAS INSTALLED ON THE RT SIDE OF ACFT. WE RECEIVED NOTICE FROM MFG TECH SUPPORT THAT THIS PROP MAY HAVE A BLADE COLLAR INSTALLATION ISSUE. UPON CLOSER INSPECTION, THE NR 1 BLADE COLLAR WAS MISSING. WE SUSPECT IT FELL OFF DURING ENGINE OPERATIOSDR CA111012001Blade · damaged(CAN) ON THE RT PROPELLER ASSY, COLLARS PN 802253-1 (REAR HALF) AND 802253-2 (FORWARD HALF) ON 3 BLADES (NR1,2,4) WENT AWAY DURING ENGINES OPERATIONS, IT WAS NOT NOTICED AT THE TIME IT HAPPENED SO ITS HARD TO DETERMINE IF IT HAPPENED IN FLIGHT OR DURING GROUNDSDR CA110915007Blade · debonded(CAN) PROPELLER BLADE HEATER ELEMENT BECOMING DISBONDED FROM BLADE AND BUBBLING.SDR 2011FA0000501Blade · loosePROPELLER BLADE ON PROPELLER ASSY PN HC-C2YR-2CUF/FC7666A-4 WAS DISCOVERED LOOSE ON PRE-FLIGHT INSPECTION. THIS PROPELLER HAD 240.2 HRS TSO, IT WAS OVERHAULED ON 28 MARCH 2011. THIS IS 2ND OF 2 PROPELLERS THAT HAVE DEVELOPED LOOSE PROPELLER BLADES AFTER BEINSDR CA110630004Blade · stickingTHE NR 1 PROPELLER WOULD ONLY REACH 2600 RPM AT TAKEOFF. IT APPEARED THAT AT LEAST 1 OF THE PROP BLADES WAS STICKING AS IT TRIED TO TURN IN THE HUB. PROP WAS CHANGED AND GROUND RUN PERFORMED. ONCE DEEMED SERVICEABLE, A TEST FLIGHT WAS COMPLETED AND IT WORKESDR 2011FA0000502Blade · loosePROPELLER BLADE ON PROPELLER ASSY WAS DISCOVERED LOOSE ON PREFLIGHT INSPECTION. THIS PROPELLER HAD 47.6 HRS TSO, IT WAS OVERHAULED ON 12 MAY 2011. 1ST OF 2 PROPELLERS THAT HAVE DEVELOPED LOOSE PROPELLER BLADES AFTER BEING OVERHAULED.SDR CA110620005Cuff · damagedBLADE CUFF MISSING FROM BLADE ON NR 1 PROP. ACFT PARTS WERE FOUND ON RUNWAY. IT WAS DETERMINED THE PART SEPARATED DURING THE TAKEOFF ON FLT-8562. THE ACFT WAS TAKEN OUT OF SERVICE FOR REPAIR. INVESTIGATION REVEALED THE PART MAY HAVE BEEN DAMAGED FROM TOOSDR 2011FA0000252Blade · crackedPROPELLER WAS REMOVED FROM ACFT TO INVESTIGATE VIBRATION THAT HAD STARTED IN THE LAST 10 HOURS OF FLIGHT. BLADE, SN CK010, HAS SEVERE CRACK IN BLADE SHANK THAT GOES THROUGH TO INSIDE BORE.SDR 2011FA0000220Bearing · leakingTHE BUTT BEARING IS OVER THE MAX ALLOWED DIAMETER ALLOWING THE BEARINGS TO FLOAT FREE IN THE BLADE BORE. THE PROP WAS DISASSEMBLED FOR RESEAL DUE TO GREASE LEAKAGE. DURING INSP, THE BLADE WAS FOUND TO BE LEAKING OIL BETWEEN THE BLADE AND BUTT BEARING. THE BSDR CA110216001Guard · damagedDURING DESCENT AT APPROX 6000 FT, SLIGHT VIBRATION FELT, ACFT WAS IN ICING CONDITIONS, WHICH WE THOUGHT WAS DUE TO ICE ON PROPS. POST FLIGHT WALK AROUND SHOWED THAT LT PROP BLADE WAS MINUS L/E METAL STRIP. NO VISIBLE DAMAGE TO FUSELAGE. NOTE THAT ACFT WAS OSDR CA110126004Clamp · misrepaired(CAN) DURING PREVIOUS SERVICE WHEN THE A304 LINK PINS WERE INSTALLED AND LOCKED THE LOCK PIN HOLES WERE DRILLED TO 0.720",MAXIMUM DEPTH IS 0.045". DRILL BIT WENT COMPLETELY THROUGH THE LINK HOLE AND PENETRATED THE OPPSITE SIDE WALL OF THE BLADE CLAMP. UNDER THSDR CA110112006Bearing · wrong partBLADE RETENTION BEARINGS ARE MANUFACTURED AS MATCHED SETS WITH CORRESPONDING SERIAL NUMBERS. UPON INSPECTION, IT WAS FOUND THAT 2 OF THE BEARING HALVES SERIAL NUMBERS DID NOT MATCH REQUIRING REPLACEMENT YAW MANUAL #MPC200.SDR 2010FA0001185Blade · delaminatedAPPROX 8 INCHES OUT FROM BLADE CUFF IN CTR OF THE BACK OF THE PROP FOUND TO BE AN AREA OF DELAMINATION 1 INCH DIAMETER.SDR CA100917002Blades · wrong partUPON DISASSEMBLY OF THE PROPELLER AND REMOVAL OF BLADES, THE BLADES REMOVED WERE FOUND TO BE NON APPROVED BLADES FOR THIS ACFT INSTALLATION. THESE BLADES WERE ORIGIONALY T10173A-6Q. ALSO, ACCORDING TO MFG THERE IS NO APPROVED TIP DWG IN MANUAL 133C FOR A T10SDR CA100819005Blade · damaged(CAN) ON LANDING IN YSB, THERE WERE MULTIPLE BIRD STRIKES TO THE LT PROPELLER AND WING AREA. THE A/C WAS INSPECTED PER THE AMM 05-50-26. THERE WAS DAMAGE TO 3 OF THE 4 BLADES ON THE LH PROPELLER. THE LT PROPELLER WAS REPLACED BEFORE FURTHER FLIGHT. A/C TSN 500SDR CA100730007Blade · separatedPROPELLER RECEIVED FROM CUSTOMER WITH APPROX 5" OF BLADE MISSING FROM NR2 BLADE TIP (S/N H89522). PROPELLER DISMANTLED, CLEANED, CLAMPS AND HUB SPIDER MPI INSPECTED, BLADES LPI INSPECTED (IAW MFG), ALL BEARINGS REPLACED DUE TO CORROSION AND DENTING, BLADE REPSDR QXEA2010080200457Blade · crackedNR 2 PROPELLER BLADES HAVE CUFF CRACKS, ALL BLADES. REPAIRED CUFF CRACKS ON ALL 6 BLADES OF THE 2 PROPS IAW MFG PUB 1105 BLADE REPAIR MANUAL MINOR BLADE REPAIR NR 3 (F10). PLACED ON DMI. RETURNED TO SERVICE.SDR AJAA072910Blade · damagedAIRCRAFT WAS IN FLIGHT AND STRUCK BY LIGHTNING, HITTING PROP BLADE. ALL SYSTEMS REMAINED WORKING BUT CHARGE DEPARTED OUT RT WING TIP, LEAVING HOLE IN TIP AND BURN MARKS.
SDR 2010FA0000522Blade · looseON CLIMB OUT, ACFT BEGAN TO SHAKE, IT BEGAN TO SHAKE WORSE AS THE FLIGHT PROGRESSED. FLIGHT LANDED SAFELY AT THE INTENDED AIRPORT. AFTER INSPECTION IT WAS REVEALED ONE OF THE PROPELLER BLADES WAS LOOSE. REMOVED PROPELLER AND SENT TO PROP SHOP FOR OVERHAUL.SDR 2010FA0000583Blade · failed((ZY2R)) LOSS OF BLADE TIP IN-FLIGHT. IN FLIGHT, PILOT EXPERIENCED SUDDEN VIBRATION. AS HE WAS OVER AN AIRPORT, IMMEDATELY POWERED BACK AND LANDED THE ACFT APPROX 9 MINUTES LATER. AFTER GO AROUND ACFT INSP PILOT DISCOVERED 1 TIP MISSING FROM THE 3-BLADED PSDR 2010F00105Bushing · unserviceableAS INSPECTED, THE BLADE BUSHING CLEARANCE WAS OVER THE MAX ALLOWED (0.003) AND MEASURED LOCALLY AT 0.020. CLOSER INSPECTION REVEALED THE BLADE BUSHING WAS LOOSE AND HAD BACKED OUT OF THE TAPPER BORE AND THAT THE CURRENT PUSH-FIT OF THE BLADE BUSHING IN THE TAPSDR 2010FA0000237Paint · crackedPAINT IS CRACKING PERPENDICULAR TO BLADE. LARGE CRACKS IN PAINT HAVE EXPOSED COMPOSITE LAYER.SDR 2010FA0000236Blade · crackedPAINT IS CRACKING PERPENDICULAR TO BLADE. LARGE CRACKS IN PAINT HAVE EXPOSED COMPOSITE LAYER.SDR 2010FA0000235Blade · crackedPAINT IS CRACKING PERPENDICULAR TO BLADE. LARGE CRACKS IN PAINT HAVE EXPOSED COMPOSITE LAYER.SDR 2010FA0000217Blade · cracked2 CRACKS FOUND ALONG GRAIN OF WOOD. 1 CRACK WAS .5 INCH LONG. THE OTHER CRACK WAS .25 INCH LONG. PROPELLER TIS 360.0 HOURS.SDR 2010FA0000240Blade · peelingPAINT IS PEELING AND CRACKING PERPENDICULAR TO BLADE, EXPOSING COMPOSITE LAYER. THIS PROP WAS RECENTLY REPAIRED WITH THE NEWEST METHOD OF BLADE PAINTING APPROVED BY MFG.SDR CA100129007Blades · damaged(CAN) 2 PROPELLER BLADES, SN E33784 & E33694 CONTAINED TOOL MARKS/GOUGES IN THE BOTTOM OF THE BALANCE HOLES, WHICH WERE FOUND THROUGH VISUAL INSPECTION. THE BLADES HAVE BEEN SENT OUT FOR REAMING OF THE BORES AND RESHOT PEENING IAW MM 202A VOLUMES 2 REV. 28, VOSDR 2010FA0000061Blade · corrodedPROPELLER RECENTLY OVERHAULED 10/29/2009 PROPELLER CAME IN FOR REPITCH WITH NO TIME ON SINCE OVERHAULED. 1 BLADE PAINT WAS REMOVED AND LOTS OF CORROSSION LEFT UNDER PAINT NOT REMOVED AS SHOULD BE WITH OVERHAUL. PROPELLER WILL HAVE TO BE REOVERHAULED TO DETERMISDR FCPR200900221Blade · damagedBLADE SN K51401 COUNTERWEIGHT MOUNTING HOLE HAS BEEN MODIFIED WITH A THREADED INSERT. INSERT IS NOT A HELI-COIL PN 1191-7CN0438 WHICH IS CALLED OUT IN THE SRM. BLADES SN K49771 SOCKET NR1 HAD GLUE UNDERBEARING RACE. BLADE SN K49771, SN K51401, SN K51447 HAVSDR T9ZR725Y4370/41Blade · damagedPROP WAS OBSERVED TO BE LEAKING GREASE FROM 2 BLADE SHANK AREAS. SPINNER WAS REMOVED FOR INSP AND ALL 3 BLADES APPEAR TO BE LEAKING GREASE. 1 BLADE WAS OBSERVED TO HAVE EXCESSIVE BLADE SHANK MOVEMENT BEYOND ALLOWABLE LIMITS. WHEN BLADES WERE CHECK FOR BLADE TWSDR T9ZR725Y4370/40Blade · leakingPROP WAS OBSERVED TO BE LEAKING GREASE FROM TWO BLADE SHANK AREAS. SPINNER WAS REMOVED FOR INSP AND ALL 3 BLADES APPEAR TO BE LEAKING GREASE. ONE BLADE WAS OBSERVED TO HAVE EXCESSIVE BLADE SHANK MOVEMENT BEYOND ALLOWABLE LIMITS. WHEN BLADES WERE CHECK FOR BLADSDR CA091217007Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION, PAINT REMOVED FROM PROP, FOUND CORROSION ON BLADE THRUST FACE OF PROP BLADES. EXTRA WORK REQUIRED TO REMOVE CORROSION WITHIN SPEC`S. PROPELLER RETURNED IN SERVICE (TC NR 20091217007)SDR CA091214004Blade · corroded(CAN) PROPELLER SENT IN FOR VISABLE BLADE CORROSION REMOVAL. CORROSION REMOVED AND PROP RETURNED TO SERVICE. WO 91-0294.SDR CA091201006Blade · damaged(CAN) FLIGHT 7723 ON NOV 27/09 ENCOUNTERED MULTIPLE BIRDSTRIKE ON APPROACH INTO LONDON (CYXU) AIRPORT. PILOT REPORTED STRIKE TO THE RIGHT WINDSHIELD, RT WING ROOT AND RT NACELLE. MAINTENANCE INSPECTED THE AIRCRAFT IN ACCORDANCE WITH MM 05-50-26, ENGINE MM 05SDR CA091127005Screw · broken(CAN) DURING DISASSEMBLY OF PROPELLER FOR OVERHAUL THE SAFETY LOCK WIRE ON ONE CLAMP BOLT WAS BEING CUT. AS THE WIRE WAS CUT THE BOLT FELL FROM ITS LOCATION IN THE BLADE CLAMP. IT IS BELIEVED THAT THE BOLT IS NOT A HARTZELL MANUFACTURED PART AS THE PART NUMBERSDR 2009FA0000988Retainer · failedDURING ANNUAL INSP FOUND COULD ROTATE ONE BLADE AN EXCESSIVE DISTANCE, SENT OUT FOR REPAIR AND IT WAS FOUND THAT THE INSIDE STAINLESS STEEL RETAINER HAD FAILED AND ALLOWED THE BALL BEARINGS TO FALL OUT OF THEIR SEAT, HUB WAS DAMAGED BEYOND REPAIR AND IT WAS CLSDR CA091110003Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSP, FOUND SURFACE CORROSION ON BLADE CAMBER FACE, AND THRUST FACE OF BOTH BLADES. EXTRA WORK TO GRIND OUT CORROSION. PROPELLER CONTINUE IN SERVICE.SDR CA090909001Bearing · damagedFLT CREW REPORTED ABNORMAL VIBRATION THROUGHOUT ACFT IN ALL PHASES OF FLIGHT. VIBRATION BECAME WORSE WITH PROPS AT MAX AND HIGHER TORQUE SETTINGS. ACFT LANDED WITHOUT FURTHER INCIDENT. AFTER LANDING, RT ENG NACELLE WAS FOUND TO BE COATED WITH FLUID. ALL ENGSDR KPVA200909Bearing Race · destroyedABNORMAL VIBRATION FELT THROUGHOUT THE AIRCRAFT DURING ALL PHASES OF FLIGHT. VIBRATION WAS WORSE WITH PROPS AT MAX & HIGHER TORQUE SETTINGS. UPON LANDING, NR 2 ENGINE NACELLE & PROP COATED IN FLUID. ALL ENGINE INSTRUMENT INDICATING GREEN, NO ASSOCIATED CAUTSDR CA090826010Blade · damaged(CAN) PROPELLER RECEIVED FOR O/H AND REPAIR OF BLADE DAMAGE. BLADES WERE REPAIRABLE IAW MM 100D, 133C, 202A, 159.SDR CA090817004Blade · wrong partPROPELLER WAS RECIEVED FOR O/H AFER FOREIGN OBJECT STRIKE. UPON INSP IT WAS FOUND THAT PREVIOUSLY FJC7666A BLADES WERE INSTALLED. THE TC A19SO FOR THIS ACFT APPROVES FJC7666A-2R BLADES FOR THIS APPLICATION. THIS HAS ALSO BEEN CONFIRMED WITH SRM 159N. THE MASDR 2009FA0000652Blade · crackedDURING ROUTINE INSPECTION A NICK (SUSPECT ROCK OR RUNWAY DEBRIS)WAS FOUND IN THE FACE OF ONE BLADE ON THE LEFT PROP, 3.25" IN FROM THE TIP. AFTER MINOR DRESSING IT WAS DISCOVERED TO HAVE THREE PITS IN THE BOTTOM OF THE NICK. THE THIRD PIT BACK FROM THE LEADISDR W59R6816Blade · crackedPROPELLER SUBMITTED FOR INSPECTION IAW AD 97-18-02R1. BLADE SN A70190 FOUND CRACKED APPROX 3 INCH LONG IN V GROOVE OF BLADE SHANK. BLADE SN A70477 FOUND CRACKED USING EDDY CURRENT APPROX .5 INCH LONG IN V GROOVE. BOTH CRACKS ARE IN SUBJECT AREA OF AD. TIME SDR CA090604005Thrust Bearing · cracked(CAN) UPON MPI OF THE THRUST BEARING, FOUND A CRACK RUNNING ALONG THE CENTER OF THE BEARING FROM ONE END ABOUT A .2500 INCH LONG.SDR CA090605006Clamp · unserviceable(CAN) DURING VISUAL INSP, IT WAS NOTED THAT THE LOCK HOLES FOR THE A304 LINK PINS WERE DRILLED THROUGH THE PIN AND INTO THE OPPOSITE WALL. IT APPEARS THAT THIS OCCURED DURING A PREVIOUS OVERHAUL.SDR CA090605002Clamp · damaged(CAN) PROPELLER RECEIVED FOR OVERHAUL. UPON VISUAL INSP, DAMAGE TO ONE OF THE BLADE CLAMPS CONSISTENT WITH LIGHTENING STRIKE WAS OBSERVED. CLAMP IS UNSERVICABLE IAW MANUAL 118F AND 202A.
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