JASC 6110
Service difficulty reports · 1,590
Reports filed under 6110 · Propeller Assembly, 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 = '6110' 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 = '6110' 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 2003FA0000302Case · crackedAT 689 HOUR TSO OF ENGINE AND 689 HOURS SINCE REMOVAL OF 2 BLADE PROPELLER AND INSTALLATION OF 3 BLADE PROPELLER IAW STC. CASE CRACKED CAUSING AN OIL LEAK. THE CASE WAS NOT REPAIRABLE.SDR 0074382Clamp · corrodedCORROSION ON CLAMP ASSEMBLY.SDR AUS20030274Propeller · damaged(AUS) PROPELLER FAULTY. FOLLOWING FEATHERING CHECK IAW AD/PROP/2 AMDT2IT WAS FOUND THAT TWO BLADES COULD BE ROTATED BACK TO FULL FINE POSITION BY HAND.SDR 0065074Clamp · corrodedCORROSION ON PROPELLER HUB CLAMPSDR 2003FA0000052Nut · crackedDURING ROUTINE OVERHAUL OF THIS PROPELLER FOUND NR 2 THREAD IN THE NR 2 HUB SOCKET CRACKED. VISUAL/MAGNAFYING GLASS AND CONFIRMED WITH EDDIE CURRENT AND DYE-CHECK NDT. FOUND THE ASSOCIATED BLADE RETENTION NUT CRACKED ON THE NR 2 THREAD AS WELL VIA THE SAME MESDR PIY2003F00000Screw · misinstalledRIGHT PROPELLER DEICE BRUSH MOUNTING SCREWS WERE PAN HEAD SCREWS WITH NO LOCKING DEVICE. THE PARTS BOOK CALLS FOR PN MS35275243 SCREW. THIS IS FILLISTER HEAD SCREW WITH THE HEAD DRILLED FOR SAFETY WIRE. THE PROPER SCREWS WERE OBTAINED, INSTALLED, AND SAFETISDR CA021211003Beta Ring · misinstalled(CAN) THE BETA RING WAS RUBBING ON THE ENGINE NOSE CASE STUDS. PROPELLER WAS REMOVED AND THE BETA RING WAS ADJUSTED AND REINSTALLED ONTO THE ENGINESDR QXEA0202034Propeller · vibrationPDX- NR 2 PROP VIBRATION IN FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. BALANCED NR 2 PROP. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR CA021204002Bolt · failed(CAN) DURING PROPELLER OVERHAUL, BOLT PN A2431 WAS MAGNAFLUXED AND FOUND A CRACK INDICATION RUNNING LENGTH WISE ON THE BOLT THREADS. NEW BOLT INSTALLED.SDR MALA020651Propeller · malfunctionedDURING CLIMBOUT OF FLIGHT 2907, RT ENGINE SURGED DURING CLIMB. TORQUE WENT TO 120 PERCENT FOR 10 SECONDS, TEMP WENT TO 968 DEGREES FOR 10 SECONDS. PROP RPM REMAINED STABLE. CTOT WAS OFF, AUTO COARSEN OFF, AUTO PILOT ON. PILOT WENT TO TORQUE MOTOR LOCK OUT PESDR CA021119007Counterweight · cracked(CAN) PROPELLER RECEIVED FOR AD 97-18-02 REPETITIVE INSPECTION. CRACK DISCOVERED DURING M.P.I. INSPECTION OF THE CLAMPS. AT ONE TIME DURING THE HISTORY OF THE PROP THE COUNTERWEIGHT SHOWS DAMAGE FROM CONTACT AGAINST THE PROP PISTON. PUSHING OUT THE THIN WALL ASDR CA021108012Hub · damaged(CAN) UPON DISASSEMBLY, C792 BEARING WAS FOUND TO BE BROKEN CAUSING DAMAGE TO HUB RENDERING IT UNSERVICEABLE. UPON REMOVING PAINT FROM 3 BLADES, CRACKS WERE DISCOVERED IN THE SHANK AREA IN THE COMPOSITE MATERIAL. AS THIS DAMAGE IS NOT ADDRESSED IN THE O/H MANUSDR 2002FA0001118Blade · crackedRECEIVED PROPELLER FOR ROUTINE OVERHAUL. NO OVERHAUL OR INSPECTION SINCE 1982 (START OF LOG BOOK). PENETRANT INSPECTION OF PARTS REVEALED CRACK IN 1ST THREAD OF NR 1 BLADE. CONFIRMED WITH EDDY CURRENT. PROP WAS OIL FILLED IN 1982. NO INSPECTIONS PERFORMED ON BSDR 2002FA0001113Blade · damagedPROP WAS REMOVED WITH 135.0 HOURS SINCE OVERHAUL. REASON FOR REMOVAL WAS TO EVALUATE PROP FOR POSSIBLE TRADE IN. DURING PRELIMINARY INSPECTION OF BLADE WIDTH AND THICKNESS FOR VALUE ASSESSMENT, BOTH BLADES WERE FOUND TO BE BELOW MFG MINIMUM SPECS AT 34 INCH SDR V5S2002F00000Sleeve · looseDURING NORMAL CRUISE FLT, PILOT NOTICED AN UNUSUAL VIBRATION COMING FROM THE RT ENGINE. SHUT DOWN ENGINE AS A PRECAUTION AND MADE A SINGLE ENGINE LANDING. MAINTENANCE REMOVED SPINNER FROM THE RT PROPELLER AND FOUND THAT THE REVERSE CONTACT SLEEVE HAD BACKESDR 2002FA0001135Bracket · crackedTHE BRACKETS (PN E6977-11D) THAT SUPPORT THE QUICK DISCONNECT PLUG ASSEMBLY FOR THE PROP DEICE BOOT DUG INTO THE PROPELLER BACKPLATE. THIS WAS DONE TO VARYING DEGREES AT EACH BLADE POSITION ON THE BACKPLATE. THIS OCCURRED ON BOTH PROPS ALTHOUGH IT WAS WORSE SDR SQM212002Propeller · leakingAPPROXIATELY 3.5 HRS INTO THE FLIGHT AT 0515 Z (ENROUTE TO OKO), PILOT ENCOUNTERED PROPELLER LOW OIL LIGHT. VISUAL INSPECTION CONFIRMED FLUID LEAKED AT NR 4 PROPELLER HOUSING. THE NR 4 ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO PLA. DURING THE DEFECT SIMUSDR S2YA02031Propeller · leakingSHORTLY AFTER TAKEOFF OF FLIGHT, THE CREW NOTICED OIL ON THE RIGHT NACELLE. THE MADE AND AIR TURN BACK. MECHANIC INSPECTED THE ENGINE AND REPLACED THE PROP FOR LEAKING.SDR CA020722005Pin · broken(CAN) CUSTOMER COMPLAINED THAT PROPELLER DURING FLT WOULD NOT GO ALL THE WAY OUT OF FEATHER, INTO LOW PITCH. WHILE ON GROUND TRIED TO MOVE PROP TO LATCH WITH PADDLE, BUT ONLY ABLE TO MOVE IT PART WAY. UPON OUR REMOVAL OF LOW PITCH STOP IT NOTED THAT A3205 L.P.SDR CA020719004Bearing Race · cracked(CAN) PROPELLER WAS REPORTED TO BE STICKING, AND UPON TEARDOWN OF THE PROPELLER IT WAS NOTED THAT THE CAP RACE WAS CRACKED. AS A RESULT THE CWT SHAFT WAS WORN BEYOND USE. OTHER FINDINGS WERE TWO BROKEN CWT. PINS IN THE CWT BRACKET, ONE WORN CHAFING RING, AND WSDR MALA020412Propeller · malfunctionedDURING FLIGHT 3237, DURING INITIAL CLIMBOUT OF ATY, AFTER REDUCING CTST AND SELECTING CTOT SW OFF LT ENGINE TORQUE INCREASED RAPIDLY TO APPROXIMATELY 120 PERCENT TORQUE AND ITT INCREASED TO 903 C. AFTER REDUCING POWER LEVER POSITION BELOW 64 DEGREES SWITCH ENSDR CA020626003Snap Ring · missing(CAN) PROPELLER RECEIVED FROM CUSTOMER AFTER LOSS OF SNAP RING. PROPELLER WAS DISMANTLED, BLADES DRESSED, PAINTED AND ASSEMBLED.SDR GLBA2002073Propeller · malfunctionedRIGHT PROP WOULD NOT ADJUST OR FEATHER ON GROUND. REPLACED PROPELLER ASSEMBLY.SDR CA020510022Thrust Link · corroded(CAN) THE PROPELLER WAS OVERHAULED ON JULY 18, 1996, WAS REMOVED FOR AD 97-18-02 WITH 42.4 HRS. TSO. ON JUNE 29, 1999 THE AD WAS COMPLETED AND THE PROPELLER INSTALLED ON JULY 2, 1999. ON APRIL 19, 2000 THE PROPELLER WAS REMOVED FROM THE AIRCRAFT WITH 88.3 HRS.SDR RAIA00204131Propeller · vibrates5645-STL - CREW REPORTED RIGHT ENGINE VIBRATION. MAINTENANCE REMOVED AND REPLACED RIGHT PROPELLER ASSEMBLY.SDR CA020510020Clamp · cracked(CAN) COUNTERWEIGHT CLAMP FOUND TO BE CRACKED IN THE MIDDLE MID-WAY BETWEEN THE CLAMP RETAINING BOLTS.SDR 2002F00361Latch · crackedLATCH PAWL CRACKED ON TOP EDGE.SDR CHQ000132Propeller · vibrationVIBRATION OF RT SIDE PROP MOST NOTICEABLE WHEN BRINGING PROP INTO AND OUT OF FEATHER IN FLIGHT, SEEMS WORSE AT HIGHER AIRSPEEDS RAN A/C.SDR 2002FA0000325Propeller · separatedWHILE CRUISING AT 5000 FEET THE PILOT REPORTED SEVERE VIBRATION. AFTER PERFORMING AN UNEVENTFUL LANDING AND ENGINE SHUT DOWN, THE PILOT OBSERVED THAT APPROXIMATELY 4 INCH INCHES OF ONE BLADE TIP WAS MISSING. FURTHER INVESTIGATION REVEALED THAT A SMALL STONE HSDR CA020131005Thrust Plate · cracked(CAN) CRACK FOUND AROUND THIN LIP OF THRUST PLATE.SDR AUS20020017Propeller · faulty(AUS) PROPELLER BLADE CLAMP BOLTS NOT IN SAFETY. NO SPACERS BETWEEN SPINNER BACKPLATE AND PROPELLER HUB. PROPELLER BLADES CONTACTINGBACKPLATE WHEN BLADE IS IN THE FEATHER POSITION.PERSONNEL/MAINTENANCE ERROR.SDR SWIA200110509Propeller · faultyON ROLLING TAKEOFF, TORQUE ON LEFT ENGINE SHOT UP TO 134 PERCENT TQ. TAKEOFF AURAL WARNING AUTO FEATHER SOUNDED WITH SWITCH ON. ABORTED TAKEOFF. WHEN POWER LEVERS PULLED BACK TO GROUND IDLE, RT ENGINE READ 75 PERCENT TQ AND 53 PERCENT NH. WHEN AUTO FEATHERSDR AUS20011460Propeller · faulty(AUS) THE FOLLOWING DEFECTS WERE FOUND ON THE PROPELLER WHEN RECEIVED FOR OVERHAUL:-1. ZERO BEARING TENSION ON BOTH BLADES2. REAR BARREL HALF HAS BEEN DRILLED, TAPPED AND GREASE NIPPLES FITTED. NO CERTIFICATION COULD BE FOUND TO SUBSTANTIATE THIS MODIFICATIONSDR 2001FA0000491Fork · crackedRELEVANT INDICATION (CRACK) FOUND BY NON DESTRUCTIVE TEST INSPECTION.SDR 2001FA0000490Fork · crackedRELEVANT INDICATION(CRACK) FOUND BY NON DESTRUCTIVE TEST INSPECTION.SDR LU42001F00002Bearing · failedRELEVANT INDICATION.SDR SWIA200110244Propeller · out of balanceBAD VIBRATION INFLIGHT, POSSIBLY DUE TO PROP ICING. RETURNED TO SLC. FOUND PROPS OUT OF BALANCE. PERFORMED PROP BALANCE ON BOTH. OPS CHECK GOOD.SDR LU42001F00001Bearing · crackedRELEVANT INDICATION.SDR RRI2001F00000Propeller · separatedPROP HUB SEPARATED AT BOLTS, LEAVING JUST THE AREA OF THE HUB THAT THE BOLTS ATTACH TO. THE HUB WAS NEW AT THE OVERHAUL. THERE WAS NO VIBRATION AT ALL DURING THE FLIGHTS AND STARTS THAT LOOK PLACE EARLY THAT DAY OR THE DAY BEFORE. THERE WAS NO EVIDENCE OF OSDR 2001FA0000453Tube · crackedPROPELLER WAS FOR RECEIVED FOR STANDARD 60 MONTH OVERHAUL. CURRENT PROPELLER TIMES ARE TTSN 445.0 AND TSO N/A. THIS IS THE PROPELLER`S FIRST OVERHAUL. DURING THE INSPECTION OF THE PROPELLER COMPONENTS, HUB PART NUMBER 840-118, SERIAL NUMBER EVA2042 WITH PILSDR 2001FA0000434Fork · crackedPROPELLER WAS RECEIVED FOR STANDARD 60 MONTH OVERHAUL IAW MFG SL. CURRENT PROPELLER TIMES ARE: TTSN1113.80 TSO N/A. THIS IS THE PROPELLERS FIRST OVERHAUL. DURING THE INSPECTION OF THE PROPELLER COMPONENTS, FOR PART NUMBER C-4503, SERIAL NUMBER N0901 WAS FOSDR 2001FA0000431Bearing · crackedRELEVANT INDICATION.SDR CA010823015Spacer · corroded(CAN) PART CORRODED AND INSTALLED UPSIDE DOWN.SDR 2001FA0000317Pin · crackedPROPELLER SHOWS RELEVENT INDICATION.SDR 2001FA0000314Propeller · damagedAIRCRAFT LANDED RENO, PILOTS NOTICED DIFFICULTY GETTING PROP INTO BETA AND SLIGHT VIBRATION DURING ROLLOUT. AT HANGER, PILOTS NOTICED LOWER NG ON NR 1 ENGINE ADN ON SHUTDOWN. NR 1 PROP STAYED IN A FLIGHT PITCH ANGLE WHILE NR 2 PROP WENT TO FEATHER PER NORMALSDR 2001FA0000222Fork · crackedRELEVANT INDICATIONSDR 2001FA0000221Bearing · crackedRELEVANT INDICATIONSDR BB1Blade · separatedEXPERIMENTAL AMATEUR BUILT AIRCRAFT, INITIAL FLIGHT WITH NEW NON-CERTIFICATED VARIABLE PITCH PROPELLER MANUFACTURED BY AEROTEK AUCKLAND, NEW ZEALAND. BOTH COMPOSITE BLADES SEPARATED SIMULTANEOUSLY ON TAKE OFF AT 500 FT. AGL. INSPECTION REVEALED THAT THE BLADSDR RAIA00107016Propeller · damaged7272-STL-LEFT PROPELLER TIPS DAMAGED DUE TO GROUND EQUIPMENT STRIKE. MAINTENANCE INSPECTED AND REPLACED LEFT PROPELLER, MAINTENANCE REPLACED LEFT ENGINE DUE TO PROPELLER STRIKE.SDR 2001FA0000072Shaft · shearedAIRCRAFT PROPELLOR WENT INTO FEATHER ON APPROACH. AFTER LANDING, RESTARTED ENGINE AND PROPELLOR FELL OFF. PROP SHAFT SHEARED IN HALF. ENGINE HAD A PROP STRIKE 400 HOURS PREVIOUS.
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