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 NSVA200600192Propeller · fireBRIGHT FLAME FROM RT PROP THEN MASTER CAUTION AND RT PROP LIGHT. REMOVED AND REPLACED RT PROP PN R390/4-123-F/27, SN OFF DRG/1528/91, SN ON DRG/10175/89 IAW AMM 61-00-00 OPS CK GOOD.SDR CA061025004Stud · unserviceable(CAN) WHILE INSTALLING THE MCCAULEY MODEL D3A34C403-B PROPELLER ONTO A CESSNA 185, THE ENGINEER WAS TIGHTENING THE FIBER LOCK NUTS ONTO THE PROPELLER MOUNTING STUDS, WHEN ONE OF THE NUTS KEPT ON TURNING AND DID NOT SEEM TO BE GETTING ANY TIGHTER. HE TRIED ANOTSDR CA061011011Fitting · open(CAN) PILOT EXPERIENCED EXCESSIVE GREASE LEAKAGE ON WINDSCREEN DURING TAKEOFF AND CLIMB, RETURNED TO MAINTENANCE BASE IMMEDIATELY. ON INSPECTION ONE GREASE FITTING WAS FOUND DEFECTIVE. GREASE FITTING WAS REPLACED. PROP RE-GREASED IAW PROP OWNERS MANUAL, PN115NSDR NSVA200600157Propeller · vibrationDURING CRUISE, CREW EXPERIENCED ENGINE VIBRATION ON RT SIDE. MOVING THE CL FROM LOW TO HIGH THE VIBRATION WOULD GET WORSE. AT FLIGHT IDLE THE VIBRATION WAS LESS. CREW PERFORMED EMERGENCY CHECK LIST, SHUT DOWN THE ENGINE AND RETURNED TO IAH. PERFORMED BOROSSDR I5HA0358007Pump · failedON APPROACH, CREW REPORTED THE NR 1 PROP RPM INCREASE TO MAX RPM AND WOULD NOT CONTROL ENGINE SPEED. THE ENGINE WAS SHUT DOWN PRECAUTIONARY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. ON LANDING INSPECTION OF THE PROPELLER INDICATEDSDR R020646Plate · mismarkedPRELOAD PLATES ARE MARKED WITH PN 100641 BUT CONFIGURED AS PN 100641-1. LOGBOOK INDICATES PROP WAS REMOVED ON 5/17/05 FROM AIRCRAFT D2-EVN, S/N UE-370 RT POSITION DUE TO DEEP GOUGE OVER ACCEPTABLE LIMITS. PROP WAS OVERHAULED ON 7/14/05 WITH 824.0 TSN. PRELOASDR CA060814003Brush Block · damaged(CAN) AFTER TAKEOFF CREW NOTICED NR 2 BETA LIGHT ILLUMINATED AND PROP RPM ERRATIC THE CREW ELECTED TO SHUT-DOWN NR 2 ENG. AND RETURN TO BASE FOR MAINTENANCE. BRUSH BLOCK WAS CHANGED ENG. WAS GROUND RUN AND FOUND SERVICABLE. (TC NR 20060814003)SDR 25869Structure · crackedPROPELLER PILOT BORE FOUND CRACKED BY PENETRANT INSPECTION BEING PERFORMED DURING OVERHAULSDR DAT2006F00005Bolt · damagedDURING THE COMPLIANCE OF AD (SB A203A) ON LT PROPELLER, THE MECHANIC FOUND (1) LOOSE BOLT. AS REQUIRED BY AD, THIS PROPELLER WAS REMOVED IAW THE SD3-30 MM. AFTER REMOVAL OF THE PROPELLER THE PROPELLER AND ENGINE FLANGES WERE INSPECTED AND NO DAMAGE OF FRETTISDR CA060718002Thrust Plate · damaged(CAN) UPON DISASSEMBLY OF THE PROPELLER, IT WAS FOUND TO HAVE A BROKEN THRUST PLATE SCREW (PN A3204). THE THRUST PLATE SCREW WAS FOUND JAMMED BETWEEN THE THRUST PLATE AND THE BLADE BUTT. AS A RESULT OF THIS BROKEN SCREW IT ALSO DAMAGED THE BETA PICKUP PLATE (PSDR 2006FA0000732Nut · failedWHEN TORQUING OUTER CLAMP NUT PN ACA1373, NEW OUTER CLAMP NUT THREADS FAILED BEFORE REACHING SPECIFIED TORQUE. PROPELLER WAS BEING REASSEMBLED DURING OVERHAUL. ASSEMBLED USING CALIBRATED TOOLS AND NEW HARDWARE. (K)SDR 2006FA0000686Nut · failedWHEN TORQUING OUTER CLAMP NUT P/N ACA1373, 1 EACH NEW OUTER CLAMP NUT THREADS FAILED BEFORE REACHING SPECIFIED TORQUE. PROPELLER WAS BEING REASSEMBLED DURING OVERHAUL. ASSEMBLED USING CALIBRATED TOOLS AND NEW HARDWARE.SDR CA060711007Bulkhead · cracked(CAN) THIS FORWARD SPINNER BULKHEAD HAS BEEN IN SERVICE WITH THE ORIGINAL (THIN MATERIAL) SPINNER. THE BULKHEAD HAS CRACKS TO 1.25 INCHES ACROSS EACH/ALL 6 PROP BOLK HOLES. (TC NR 20060711007)SDR PNSA060403Propeller · damagedON TAKEOFF THE NR 1 PROPELLER WAS DAMAGED BY ROCKS DUE TO SOFT SPOT IN GRAVEL RUNWAY. MX REPLACED PROPELLER, AND ENGINE WAS TO BE INSPECTED PER LYCOMING SB 475C AND AD 2004-10-14 BEFORE BEING RETURNED TO SERVICE.SDR CA060320001Seal · damagedIN CRUISE 16,000 FT, NOTICED OIL LEAK ON TOP RT FWD ENG COWL. LEAK PROGRESSIVELY GOT WORSE, PILOTS ELECTED TO RETURN TO BASE. EVEN THOUGH ENG OIL TEMP AND PRESS NORM, PILOTS SHUTDOWN RT ENG. CREW DECLARED EMERG. BECAUSE QTY OF OIL LOST, PROP SHAFT SEAL SHOULSDR CA060403014Seal · leakingDURING FLIGHT, AN ENGINE OIL LEAK WAS OBSERVED AND THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A LEAKING PROPELLER SHAFT SEAL AND A LOOSE BETA VALVE RETAINING NUT.SDR R019184Bushing · looseCUSTOMER REMOVED PROP DUE TO OIL LEAKING FROM BLADE. DISASSEMBLY OF THE PROPELLER REVEALED A LOOSE PITCH CHANGE ROD BORE BUSHING CAUSING THE OIL LEAK. THE PC ROD BUSHING WAS FOUND WEDGED BETWEEN THE FORK AND HUB. CENTRAL WEB AREA OF HUB WAS FULL OF OIL. THSDR R019280Bearing Race · brokenCUSTOMER REMOVED PROPELLER DUE TO LOOSE BLADE IAW HARTZELL SERVICE BULLETIN HC-SB-61-283. ONE D-7745 BLADE SIDE BEARING INSTALLED ON BLADE SERIAL NUMBER 2828 WAS FOUND CRACKED CIRCUMFERENTIALLY.SDR R019142Hub · crackedCUSTOMER WAS INVESTIGATING AN ABNORMAL GREASE LEAK ON THE RIGHT HAND PROPELLER. REMOVED THE SPINNER, DISCOVERED THAT THE ENGINE-SIDE HUB HALF WAS VISIBLY CRACKED. CRACKS ARE LOCATED ON THE PROPELLER MOUNTING FLANGE HUB HALF, LEAD EDGE SIDE OF BLADE SOCKETS NSDR 77670Clamp · corrodedCORRODED CLAMP ASSEMBLY PN 838-17, SN U5211, U5188, U5109.SDR R018909O-Ring · wrong partPROP LEAKING GREASE FROM BLADES. INSPECTION REVEALED INCORRECT BLADE SEALS INSTALLED. SRM 113B REQUIRES ITEM 540, B-3883-4339 QUAD RING WITH NO ALTERNATE. SEALS REMOVED FROM PROPELLER ARE O-RINGS.SDR QXEA200600084Propeller · vibratesSUN FLIGHT NR 2358, VIBRATION IN AIRFRAME WHEN PROPS BROUGHT OUT OF FEATHER ON STARTUP. MORE PRONOUNCED AS POWER LEVERS ARE ADVANCED TOWARDS FLIGHT IDLE. SEEMS TO ORIGINATE FROM NR 2 ENGINE. MAINTENANCE FOUND NR 1 PROP CAUSE OF VIBRATION. AIRCRAFT FERRIED SDR R018723Bearing · brokenPROPELLER WAS RETURNED DUE TO FOREIGN OBJECT STRIKE. DISASSEMBLY REVEALED ONE BROKEN D-7745 BLADE THRUST BEARING ON BLADE POSITION ONE, SERIAL NUMBER 994.SDR AU510001976Cylinder · unserviceableDURING STRIP IT WAS FOUND THAT THE PROPELLER CYLINDER HAD BEEN OVERTORQUED WHEN LAST FITTED. FURTHER INVESTIGATION FOUND THAT THE NUT HOLDING THE PISTON UNIT TO THE CONTROL ROD WAS LOOSE AND THE SPLIT PIN WAS SHEARED. THE REMAINS OF THE SPLIT PIN WERE FOUND SDR QXEA200501565Propeller · out of balancePDX FLT 9851 ON CLIMBOUT WITH PROPS AT 1050 RPM'S HAD A GREAT DEAL OF VIBRATIONS FROM THE PROPS. MAINTENANCE BALANCED BOTH PROPS IAW MTC'S 9610003. OPS CHECK GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR 2005FA0001592Snap Ring · missingTHIS PROPELLER CAME INTO OUR SHOP FOR STC BLADE ANGLE CHANGE ON A NEW PROPELLER. ON OUR FIRST CHECK OF THE BLADE ANGLE WE GOT 4 DEGREES AND KENW SOMETHING WAS WRONG. SO WE PULLED TH DOEM AND THE PISTON SNAP RING HAD NOT BEEN INSTALLED FROM THE FACTORY. (K)SDR R017794Bearing · brokenPROP WAS REMOVED FOR LOOSE BLADE. PROP WAS OVERHAULED BY MFG SERVICE CENTER ON 10/7/03 AND INSTALLED NEW D-7745 BEARINGS AT THAT TIME. HUB SIDE BEARINGS ON BLADES 2 AND 3 ARE CRACKED CIRCUMFERENTIALLY. HUB SIDE BEARING ON BLADE 4 IS BROKEN.SDR DAT2005F00011Flange · failedDURING THE COMPLIANCE OF AD, SB, FRO THE RT SIDE PROPELLER, THE (8) PROP ATTACH BOLTS, FAILED THE DESCRIBED TORQUE CHECK AS DESCRIBED IN AD (SB). THE PROPELLER WAS REMOVED IAW MM. AFTER THE PROP WAS REMOVED, THE INSPECTION FOUND FRETTING ON THE PROP FLANGE, SDR 2005FA0001211O-Ring · cutAT THE OUTER MARKER ON APPROACH, THE PILOT NOTICED AN OIL ODOR IN THE ENVIRONMENTAL SYSTEM. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT WALK AROUND REVEALED OIL LEAK AT THE RT PROPELLER. MAINTENANCE WAS DISPATCHED AND INVESTIGATION REVEALED THE RT PROSDR 20050615Lock Plate · separatedINSP MX RUN-UP, VIBRATION NR 2 PROP ASSY, VIBRATED A FEW SEC THEN DIMINISHED. DISCOVERED 2 SAFETY WIRED BOLTS HEADS ON GROUND THAT SNAPPED OFF PROP ASSY. SPINNER HAD PUNCTURE DAMAGE, MINOR DAMAGE TO 2 PROP BLADES. SPINNER REMOVED, 2 LOCK WIRED BOLTS HAD SHESDR LU4R12482Spring · stretchedSPRING ASSY STRETCHED TOO LARGE. (K)SDR CA050421005Nut · failed(CAN) PROPELLOR DEPARTED FROM ENGINE. BOTH MECHANICS THAT INSTALLED PROPELLOR AND TORQUED NUT, CLAIMED 720 FT LBS CALCULATED WITH THEIR BODY WEIGHTS ON A LEVER ARM TO THE SPLINED WRENCH AND WITNESSED THE LOCK IN PLACE. MORE TO FOLLOW WHEN NUT HAS BEEN INDEPESDR RAI00504010Propeller · malfunctionedRIC - PROP HEAT FAULTED. MAINTENANCE REMOVED AND REPLACED NR 1 PROP, LEAK CHECKS GOOD.SDR RAI00504007Propeller · defectiveSTL - LEFT PROP HEAT FAULTS IN LONG AND SHORT CYCLES. MAINTENANCE REMOVED AND REPLACED LEFT PROP.SDR CA050404002Bolt · cracked(CAN) AD 2003-12-05 (MFG SB 221C) REQUIRES MAGNETIC PARTICLE INSP. OF PROP MOUNTING BOLTS. DURING INSP 1 OF THE 6 PROP MOUNTING BOLTS WAS NOTED AS CRACKED IN THE GRIP APPROX .25 BELOW THE BOLT HEAD.SDR CA050330001Bearing · worn(CAN) ENG WAS REMOVED FROM AC DUE TO EXCESS RADIAL PLAY FOUND AT PROP SHAFT. OIL LEAK WAS EVIDENT FROM PROP SHAFT SEAL AREA. MOUNTED DIAL IND ON ENG, MEASURED APPROX, 0.010 TO 0.018 INCH PROP SHAFT RADIAL PLAY. THIS WAS SECOND SEAL INSTALLED, ENG STILL LEASDR 2005FA0000433Tube · misrepairedPISTON PILOT TUBE, PAPER TOWEL INSTALLED INSIDE OF TUBE, BLOCKED OIL. PROP HAD / HOUR TIME ON IT.SDR 2005FA0000431Sleeve · incorrectPROPELLER WAS REPAIRED AND O/H IN MY SHOP. PROP HAD A2499-10 HIGH PITCH STOP SLEEVE INSTALLED BUT APPARENTLY ASSEMBLER DID NOT KNOW IT TAKES A 2499-9. WHEN ASSEMBLED TO GET BLADE ANGLES CORRECT, ALTERED -10 TO A -9 IAW PRINT A2499. TT ON PROP 120 HRS SINCESDR CA050323008Propeller · misinstalled(CAN) PROPELLER INCORRECTLY INSTALLED IAW AD2003-12-05 / SB 221C. BOLTS INCORRECT AND SPACER MISSING.SDR CA050316002Cylinder · leaking(CAN) PROP WAS IN FOR BETA LIGHT FLICKERING, TORQUE FLUC, OIL PRESS FLUC. PROP HAD A SLOW PITCH CHANGE, OIL LEAK BETWEEN BASE OF CYL & HUB, GREASE LEAKAGE FROM ALL FOUR BLADE CLAMPS. FOUND NR 4 BLADE OUT 0.6 DEG IN ANGLE. LATCH ANGLES OUT ABOUT 0.7 DEGREES. SDR 2005FA0000498Fork · crackedNDT SHOWS CRACKED IN (2) PLACES ON FORK. (K) (12235)SDR 2005FA0000346Seal · leakingPROPELLER SHAFT SEAL WAS LEAKING, CAUSING HIGH OIL CONSUMPTION. (K)SDR 2005FA0000305Ferrule · crackedDURING DISASSEMBLY FOR OVERHAUL, BLADE RETENTION FERRULE C4451 FOUND CRACKED IN BEARING FLANGE ON NR 2 BLADE. THE CRACK APPEARS TO HAVE STARTED AT AN OLD ACTUATING PIN HOLE AND IS OVER THREE INCHES LONG. S/B 196B HAD NOT BEEN ACCOMPLISHED ON THIS PROPELLER.SDR 20030779Propeller · defectiveWHILE MAINTENANCE WAS PERFORMING A PRE-RELEASE AUTOFEATHER TEST, UNUSUAL VIBRATION WAS NOTED COMING FROM LT ENGINE AND PROP. ENGINE WAS SHUTDOWN WITHOUT INCIDENT AND UPON INVESTIGATION INTERNAL FAILURE WAS OBVIOUS DUE TO BLADE MOVEMENT. PROPELLER REMOVED FROSDR MALA040816Blade · debondedDURING 4K INSPECTION IN LAN, MAINTENANCE NOTED 1,2,3 BLADES HAVE DISBONDS IN NICKEL LEADING EDGE. MAINTENANCE REPLACED RT PROPELLER, IAW MESABA JOB CARD 6110-303. REFER TO NRC NR 196549 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/24/04.SDR MALA040815Blade · damagedDURING 4K INSPECTION IN LAN, MAINTENANCE NOTED ALL BLADES HAVE DISBANDS IN NICKEL LEADING EDGE LT PROPELLER. MAINTENANCE REPLACED PROPELLER IAW MESABA JOB CARD 6110-B03. REFER TO NRC NR 196539 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 10/24/0SDR CA040928011Shaft · cracked(CAN) THE PROP SHAFT FOUND TO HAVE CRACKED ADJACENT TO A PREVIOUSLY REPAIRED DIAMETER (OVERHAUL, NOV 2001). PWC WILL INVESTIGATE TO ESTABLISH ROOT CAUSE.SDR CA041018007Housing · damaged(CAN) INBOUND, NR 4 PROP RPM DROPPED BELOW LIMIT ACOMPANIED BY RPM FLUCTUATION AND TORQUE ROLL.THE ENGINE WAS SHUTDOWN AS A PRECAUTION. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 4 VALVE HOUSING AND AIRCRAFT WAS RETURNED TO SERVICE.SDR HNAA0400120Mount · brokenFLIGHT 4079 REPORTED A PROP VIBRATION DURING CLIMB, CRUISE, DESCENT WITH PROPS AT 900 RPM. MAINTENANCE FOUND THE RIGHT HAND INBOARD REAR MOUNT STRUT TO BE AT FAULT. UNIT WAS REMOVED AND REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR KRCX0101AACounterweight · displacedON ANNUAL INSPECTION SAW FINE ALUMINUM POWDER ON ONE BLADE SHANK ON REAR PROP. FOUND SPINNER HAD A LARGE BLISTER CAUSED BY PRESSURE FROM WITHIN. WHEN WE REMOVED THE SPINNER WE SAW THE COUNTERWEIGHT FOR THAT BLADE WAS ADVANCED ABOUT 30 DEGREES IN THE CRUISE DIR
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