JASC 6113
Service difficulty reports · 364
Reports filed under 6113 · Propeller Spinner 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 = '6113' 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 = '6113' 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 SROM20260402002Spinner · wornUPON APPROACH INTO PAKU IT WAS IDENTIFIED BY THE FLIGHT MECHANIC ONBOARD THAT THE NR 2 SPINNER SEEMED OFF OF CENTER AND HAD MORE MOVEMENT DURING ROTATION THAN TYPICAL. AFTER LANDING THE MECH INVESTIGATED FURTHER & FOUND WHAT APPEARED TO BE LOOSE SLEEVE NUT FASDR 2024FA0000522Bulkhead · crackedFORWARD SPINNER BULKHEAD CRACKED IN MULTIPLE LOCATIONS.SDR 2024FA0000521Bulkhead · crackedFORWARD SPINNER BULKHEAD CRACKED IN MULTIPLE LOCATIONS. DISCOVERED DURING ANNUAL INSPECTION.SDR 2022FA0000003Spinner · fracturedON RUNUP AFTER AN OIL CHANGE, DETECTED A NOTICEABLE WOBBLE ON THE PROPELLER SPINNER. AFTER ENGINE SHUTDOWN FOUND THAT THE SPINNER WAS EASILY DEFLECTED AN INCH OR SO. REMOVED SPINNER,AND FOUND THAT THE INNER FLANGE ON THE SPINNER FORWARD BULKHEAD WAS FRACTURED SDR 8HBR20211116037None · crackedDURING PRE-FLIGHT, PILOT FOUND THE SURROUNDING AREA OF ONE OF THE AFT SPINNER BULKHEAD NUTPLATES CRACKED AND SEPARATED FROM BULKHEAD.SDR IKBR2020072200005Bulkhead · crackedWHILE PERFORMING A PREFLIGHT INSPECTION THE PILOT FOUND THE AFT SPINNER BULKHEAD CRACKED AT THE EDGE WHERE THE PROP EXITS THE SPINNER. REMOVED PROP AND INSTALLED NEW SPINNER BULKHEAD P/N 0550321-12.SDR 2020FA0000286Spinner · separatedIN VFR CRUSE FLIGHT WITH ATC, THE PILOT REPORTED HEARING A LOUD BANG AND A SLIGHT ENGINE VIBRATION. A PRECAUTIONARY LANDING WAS MADE, INSPECTION OF THE AIRCRAFT REVEALED THE PROPELLER SPINNER HAD FAILED AND HAD DEPARTED THE AIRCRAFT, AND PORTIONS OF THE FIBESDR CA190625009Plate · cracked(CAN) DURING GROUND RUN MAINTENANCE OBSERVED SPINNER NOT RUNNING TRUE. SPINNER REMOVED AND FOUND BACK PLATE CRACKED. BACK PLATE REPLACED. (TC# 20190625009)SDR CA190415002Spinner · separated(CAN) PILOT REPORTED WHAT SEEMED TO BE EXHAUST SMELL IN THE CABIN AND LOAD ENGINE NOISE AFTER TAKEOFF. FOUND THAT THE DYNAMIC BALANCE WEIGHT FROM THE BACK OF THE SPINNER BULKHEAD HAD SEPARATED FROM THE BACK PLATE AND ENDED UP SCRAPING AGAINST THE NOSE OF THE CSDR COEA2017022245913Spinner · crackedLEFT PROPELLER SPINNER IS CRACKED AT SCREW MOUNT. REPAIRED IAW CMM 61-13-02, REPAIR 6-5.SDR 2016FA0000670Bulkhead · crackedSPINNER BULKHEAD FOUND CRACKED AFTER 2 MONTHS OF OPERATION, WITH NEW ONE PREVIOUSLY INSTALLED. HAVE TO REPLACE THESE AT ABOUT EVERY 200 HRS DO TO CRACKS.SDR 7C7A2016090900254Actuator · damagedNR 1 ENGINE OIL PRESSURE DROPPED BELOW 40 PSI AND THE NR 1 ENGINE WAS SHUTDOWN. R & R THE NR 1 PROPELLER ACTUATOR DUE TO DOME PISTON SEALING SURFACE DAMAGED IAW CMM 61-13-02.SDR 5SWS2016FA0000367Bulkhead · crackedPART WAS INSTALLED. DURING ANNUAL INSPECTION, TACH 1238.6 SPINNER BULKHEAD FOUND TO BE CRACKED.SDR CA150930012Bulkhead · cracked(CAN) DURING MFG PROGRESSIVE CARE INSPECTION THE SPINNER DOME WAS FOUND TO BE LOOSE. UPON FURTHER INSPECTION THE SPINNER BULKHEAD WAS FOUND TO BE CRACKED ALL THE WAY AROUND CRANKSHAFT FLANGE. SPINNER AND PROPELLER RE & RE AND NEW BULKHEAD INSTALLED, PN D-752SDR 2015FA0000451Spinner · missingDURING CRUISE FLIGHT THE COMPOSITE PROPELLER SPINNER, PN 1054-1 SEPARATED OR BROKE APART AND IMPACTED 1 BLADE OF THE WOODEN PROPELLER, MODEL 6272. THE PROPELLER SUSTAINED DAMAGE AND PARTIAL SEPARATION OF THE OUTER .3333 OF THE BLADE. AN UNEVENTFUL EMERGENCY SDR FJTA201502275641Spinner · contaminatedON THE FLIGHT, DURING CLIMB OUT EXPERIENCED MODERATE VIBRATIONS IN THE ACFT THAT BEGAN TO INTENSIFY. ALL ENG PARAMETERS & INDICATIONS WERE NORMAL. THE CAPTAIN DISCONNECTED THE AUTOPILOT FOR THE REMAINDER OF THE FLIGHT & NOTICED NO ABNORMAL VIBRATIONS IN THE SDR 7IL2015F00008Bulkhead · crackedWHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND SPINNER REAR BULKHEAD CRACKED. BULKHEAD SN DY-1863.SDR CA141023004Bulkhead · cracked(CAN) PROPELLER FORWARD BULKHEAD FOUND CRACKED UPON INSPECTION OF THE PROPELLER. THE CRACKS ARE LOCATED AT 5 OF THE 6 BOLT HOLES, IN A SEMI-CIRCLE PATTERN WHERE THE PROPELLER BOLTS WASHERS SITS. CRACKS ARE CAUSED BY WASHERS EDGE & THE PRESENCES OF THE INHERISDR NYGS2014082600505Bulkhead · crackedCRACKS IN FRONT SPINNER BULKHEAD .SDR CA140422003Bulkhead · cracked(CAN) FORWARD SPINNER BULKHEAD WAS FOUND CRACKED NEAR THE OUTSIDE OF AT LEAST 4 OF THE 6 PROPELLER BOLT HOLES. NO DAMAGE OR OTHER TRAUMA WAS NOTED ON THE SPINNER, PROPELLER OR AFT SPINNER BULKHEAD AND THE BULKHEAD WAS NOT FOUND TO HAVE BEEN STRESSED WHILE INSSDR HNAA2014022400053Spinner · crackedIN CRUISE FLIGHT, ACFT EXPERIENCED MODERATE TURBULENCE WITH A 45 DEGREE LT BANK AND A 20 DEGREE PITCH UP ACCOMPANIED BY NUMEROUS ITEMS BEING DISLODGED FROM POSITION. YD AND AP BOTH DISENGAGED AND ACFT EXPERIENCED A 300 TO 400 FOOT LOSS IN ALTITUDE. COMPLIED SDR PNSA2013122107Spinner · vibrationAIRCRAFT VIBRATION, REMOVED SPINNER ON L/T SIDE AND FOUND SEAL PEELING OFF. REPLACED SPINNER.SDR CA131219014Plate · cracked(CAN) DURING HANGAR MOVEMENT THE SPINNER WAS NOTICED TO BE LOOSE. WHEN THE SPINNER WAS REMOVED, THE INSIDE OF SPINNER WAS ALL BLACK FROM CHAFING AND THE BULKHEAD WAS CRACKED. THE SPINNER BACKPLATE WAS SEVERELY CRACK FROM ALL 4 MOUNTING HOLES. WHEN THE BACKPLSDR CA131018010Bulkhead · cracked(CAN) UPON ACFT INSPECTION THE SPINNER WAS REMOVED TO DO A VISUAL INSPECTION OF THE PROPELLER MOUNTING BOLTS AND SPINNER BULKHEADS, FORWARD AND AFT. THE FORWARD SPINNER BULKHEAD PN 0550321-4 WAS OBSERVED TO HAVE 2 CRACKS PRESENT AROUND THE HOLES FOR THE MOUNTSDR CA130819019Bulkhead · gouged(CAN) RIGHT PROPELLER HAS LIGHT GOUGE MARKS ON THE PROPELLER SIDE OF THE PROPELLER SPINNER MOUNTING PLATE. ACFT MFG IS IN CONTACT WITH THE PROPELLER MANUFACTURE.SDR CA131018007Bulkhead · cracked(CAN) UPON ACFT INSPECTION THE SPINNER WAS REMOVED TO DO A VISUAL INSPECTION OF THE PROPELLER MOUNTING BOLTS AND SPINNER BULKHEADS, FORWARD AND AFT. THE FORWARD SPINNER BULKHEAD PN 0552231-2 WAS OBSERVED TO HAVE 3 CRACKS PRESENT AROUND THE HOLES FOR THE MOUNTSDR CA130625004Bulkhead · cracked(CAN) WHILE REMOVING SPINNER FOR INSPECTION, CRACK FOUND ON OUTER FLANGE OF SPINNER BULKHEAD.SDR CA131018006Bulkhead · cracked(CAN) UPON ACFT INSPECTION THE SPINNER WAS REMOVED TO DO VISUAL INSPECTION OF THE PROPELLER MOUNTING BOLTS AND SPINNER BULKHEADS, FORWARD AND AFT. THE FORWARD SPINNER BULKHEAD, PN 0550321-4, WAS OBSERVED TO HAVE 5 CRACKS PRESENT AROUND THE HOLES FOR THE MOUNTSDR 2013FA0000245Plate · damagedPROPELLER SPINNER BACKING PLATE DISCOVERED WITH SEVERAL SHEARED RIVETS DURING 100HR INSPECTION. THIS IS THE THIRD UNIT FOUND IN THIS CONDITION DURING ROUTINE INSPECTIONS.SDR 2013FA0000244Plate · damagedPROPELLER SPINNER BACKING PLATE DISCOVERED WITH SEVERAL SHEARED RIVETS DURING 100HR INSPECTION. THIS IS THE THIRD UNIT FOUND IN THIS CONDITION DURING ROUTINE INSPECTIONS.SDR 2013FA0000230Spinner · crackedINTERNAL MOUNTING AND ALIGNMENT COMPONENTS OF THE PROPELLER SPINNER CRACKED DURING NORMAL OPERATIONS.SDR LC1R20130206001Bulkhead · crackedDURING ANNUAL INSPECTION SOME CRACKS WERE DISCOVERED IN THE SPINNER BACK BULKHEAD NECESITATING A REPLACEMENT OF THE BULKHEAD. WHEN THE PROP WAS REMOVED AND THE BOLTS HOLDING THE BULKHEAD TO THE PROP WERE LOOSENED, IT WAS DISCOVERED THAT ALL 16 RIVETS WERE SHESDR CA121203014Mount · worn(CAN) THE SPINNER MOUNTING PLATE BOLTS WERE ALL LOOSE, FINGER TIGHT AND SHOULD HAVE BEEN TORQUED. THIS CAUSED MOVEMENT IN THE BULKHEAD WHICH ELONGATED THE HOLES IN THE SPINNER MOUNTING PLATES. THERE IS A SB CONCERNING THE DRILLING OF CLAMP COUNTERWEIGHT DOWESDR CA130108001Spinner · cracked(CAN) PROP WAS IMPROPERLY INSTALLED DURING NEW PROP INSTALLATION. DURING WALK ROUND INSPECTION OWNER FOUND CRACK IN THE SPINNER. UPON SPINNER REMOVAL PROPELLER WAS FOUND LOOSE. THE BLADES COULD BE WIGGLED FORWARD AND BACK APPROXIMATLY 5". SIGNIFICANT DAMAGSDR CA120910002Spinner · cracked(CAN) SPINNER DOME CRACKED. THIRD CRACKED DOME IN 2 YEARS. MFG WELL AWARE OF PROBLEM.SDR CA120706002Bulkhead · cracked(CAN) DURING 100 HRS INSPECTION LT SPINNER BACK PLATE FOUND CRACKED.SDR 2012FA0000141Support · crackedDURING A ROUTINE TAKEOFF, NOTICED THAT THE LT PROPELLER SPINNER WAS OSCILLATING UP AND DOWN APPROX 4.0" AT THE SPINNER TIP. AN IMMEDIATE RETURN FOR LANDING AND THE REMOVAL OF THE AFFECTED PROPELLER SPINNER FOUND THE PROBLEM TO BE A SHATTERED SPINNER SUPPORT.SDR HALA2012011800042Spinner · leakingETOPS SIGNIFICANT SYS - ON OVERNIGHT CHECK FOUND OIL LEAK FROM NOSE SPINNER AREA ON NR 2 ENGINE. INLET CONE LEAKAGE WITHIN LIMITS IAW FIM 71-08-00-1, FIG 113.SDR CA120103022Spinner · cracked(CAN) PROPELLER SPINNER CRACKED FROM A ATTACHEMENT SCREW TO THE BLADE CUTOUT AND A 3 INCH PIECE SEPERATED IN FLIGHT. AIRCRAFT WAS GROUNDED AND A NEW SPINNER INSTALLED PER HARTZELL ALERT SERVICE BULLETIN HC-ASB-61-332.SDR 2012FA0000004Adapter · crackedINSTALLED A NEW STC PROPELLER WITH A NEW SPINNER AND ADAPTER PLATE SUPPLIED IAW STC SA02414CH-D. AFTER 30 HOURS OF OPERATION, WHILE DOING A WALK AROUND INSP, NOTICED THE SPINNER WAS CRACKED AT A SCREW HOLE. REMOVED SPINNER AND FOUND ADAPTER PLATE CRACKED. TSDR 2012FA0000003Spinner · crackedINSTALLED A NEW STC PROPELLER WITH A NEW SPINNER AND ADAPTER PLATE SUPPLIED IAW STC SA02414CH-D. AFTER 30 HOURS OF OPERATION, WHILE DOING A WALK AROUND INSPECTION, NOTICED THE SPINNER WAS CRACKED AT A SCREW HOLE. REMOVED SPINNER AND FOUND ADAPTER PLATE CRACKSDR FK8R2011120100001Support · crackedCENTER SPINNER SUPPORT CRACKED.SDR CA111121001Spinner · iced(CAN) VIBRATION ON RT ENGINE, ACFT RETURNED TO BASE. TROUBLESHOT AND FOUND THE SPINNER TO HAVE ICE ACCUMULATED ON THE INTERIOR. ICE WAS REMOVED, SPINNER WAS CLEANED AND ENGINE/PROPELLER OPERATIONAL. GROUND CHECKS WERE CARRIED OUT WITH NO FURTHER VIBRATIONS NSDR CA111117005Bulkhead · cracked(CAN) CRACKS FOUND AT PROPELLER BOLT HOLES.SDR FK8R201110240001Bulkhead · crackedAFT SPINNER BULKHEAD CRACKED.SDR 2011FA0000678Bulkhead · crackedTHE BULKHEAD WAS INSTALLED ON 5/5/2007, 1476.4 TT. ON LATEST INSPECTION, A CRACK WAS DISCOVERED AT THE BASE OF THE PROPELLER HUB. ON REMOVAL OF PROPELLER, IT WAS DISCOVERED THAT SEVERE CRACK WENT 85 PERCENT THE WAY AROUND THE CENTER OF THE BULKHEAD. SPINNERSDR CA130116010Spinner · cracked(CAN) UPON INSPECTION OF AIRCRAFT IT WAS NOTICED THAT LEFT HAND ENGINE FORWARD SPINNER CAP WAS CRACKED. CRACK FOUND RADIATING FROM ONE OF ITS SCREW MOUNTING HOLES, TOTAL CRACK LENGTH WAS 1 3/4 INCH LONG. FORWARD SPINNER CAP REMOVED AND REPLACED NEW (P#C-4563-PSDR CA110613010Bulkhead · crackedPROPELLER SPINNER BULKHEAD HAS SEVERAL CRACKS AROUND BOLT HOLES.SDR CA110526011Bulkhead · crackedTHIS FORWARD SPINNER BULKHEAD WAS INSTALLED NEW 1 APRIL 2010 AND THE PROP WAS DYNAMICALLY BALANCED. MULTIPLE CRACKS AROUND SEVERAL BOLT HOLES WERE FOUND VISUALLY DURING ROUTINE SCHEDULED INSP. THIS PART CRACKS VERY OFTEN NOT JUST ON THIS ACFT. IT SEEMS THE SDR CA130116003Bulkhead · cracked(CAN) UPON ROUTINE INSPECTION OF THE PROPELLER AND SPINNER. IT WAS NOTICED UPON REMOVAL OF THE SPINNER THAT THE FORWARD SPINNER BULKHEAD HAD 2 CRACKS IN THE AREA AROUND THE CIRCUMFERENCE OF 2 SEPARATE PROPELLER MOUNTING BOLT HOLES. FORWARD SPINNER BULKHEAD R
Back to JASC 6113