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 CA040720001Skin · lightning strikeIN CRUISE OUT OF JFK NOTICED LIGHTNING STRIKE ON LEFT PROP/SITUATION WAS EVALUATED AND ALL PARAMETERS WERE NORMAL. FLIGHT WAS CONTINUED AND UPON LANDING ON YOW BASE NOTICED UPON CLOSE INSPECTION: LEFT PROP BLADE DAMAGED, PROP REPLACED. LEFT OUTBOARD AILERON SDR 160041Connector · damagedNR 2 LEFT PROP OIL TEMP GAUGE INDICATES EXCESSIVE TEMP IN FLT, AIRCRAFT DIVERTED FROM DCA TO HEF. FOUND BROKEN WIRE ON TEMP SENSOR CONNECTOR. REPLACED PIN IN CONNECTOR IAW SAAB WM 20-30-25, OP CHECKED GOOD.SDR CA040610012Seal · torn(CAN) DURING POST FLIGHT WALK AROUND OF AC FOLLOWING ARRIVAL , CREW IDENTIFIED THAT CONSIDERABLE QTY OF LUBRICATING OIL HAD BEEN LIBERATED FROM THE LT PROPELLER. CREW TERMINATED FLIGHT AND CALLED FOR ENGINEERING ASSISTANCE. ENGINEERING INVESTIGATION REVEALED FSDR CA040610011Seal · inadequate(CAN) DURING POST FLIGHT WALK AROUND OF AC FOLLOWING ARRIVAL, CREW IDENTIFIED CONSIDERABLE QTY OF LUBRICATING OIL HAD BEEN LIBERATED FROM LT PROPELLER. CREW TERMINATED FLIGHT AND CALLED FOR ENGINEERING ASSISTANCE. ENGINEERING INVESTIGATION REVEALED FAILURE OFSDR CA040429006Propeller · corroded(CAN) PROPELLER WAS RECIEVED FOR 5 YR. CORROSION IAW CAR 625, APPENDIX C, PARAGRAPH 5. PROPELLER SPACER WAS VERY DIFFICULT TO REMOVE. UPON VISUAL INSPECTION OF SPACER DOWEL HOLES IT WAS FOUND THAT THEY WERE CORRODED BEYOND REPAIR RENDERING THE PROPELLER UNSERVSDR MALA040344Propeller · faultyLEFT PROP DEICE ANNUNCIATION ILLUMINATES IN NORM AND MAX INFLIGHT. AIR RETURN TO MEM. MAINTENANCE REMOVED & REPLACED LEFT PROP IAW JC 6110-303. P\N OFF R390/4-123/F27. P\N ON R389/4-123/F26. S/N ON DAP0199, S/N OFF DAP/0003/92. ALL CHECKS GOOD.SDR O05R200400109Propeller · corroded1 PROPELLER ASSEMBLY REJECTED FOR CORROSION.SDR O05R200400108Propeller · damaged1 PROPELLER ASSEMBLY REJECTED FOR IMPACT DAMAGE.SDR AUS20040197Blade · lightning strike(AUS) LT PROPELLER BLADE EXHIBITED LIGHTNING EXIT MARKS. FURTHER INVESTIGATION FOUND BOTH LT AND RT PROPELLERS MAGNETISED BEYOND LIMITS. LT ENGINE POWER SECTION MAGNETISM BEYOND LIMITS. LIGHTNING EXIT MARKS FOUND ON LT ELEVATOR OB TRAILING EDGE.SDR 2004FA0000512Cylinder · damagedCYLINDER (PN B2452-1) SEPARATED FROM PROPELLER ON GROUND RUN. INSPECTION SHOWED THREAD DAMAGE OF CYLINDER. AFTER DISCUSSION WITH MANUFACTURER THE LIKELY CAUSE IS DUE TO HIGH PRESSURE FROM GOVERNOR, USUALLY CAUSED BY STICKING PRESSURE RELIEF VALVE.SDR GLBA20030571Bearing Race · crackedALL 4 MAIN BEARING (PROP) AND RACES WERE CRACKED AND DISINTEGRATED, REPLACED WITH IMPROVED BEARINGS IAW SERVICE BULLETINSDR 690A0220004MTPropeller · incorrectTHE NR 1 PROPELLER WAS REMOVED TO FACILITATE ENGINE MAINTENANCE. WHILE THE PROP WAS OFF IT WAS SENT TO A REPAIR STATION TO HAVE THE BLADES RETURNED TO FEATHER. THE PROP WAS THEN INSPECTED AND TESTED. PROPELLER INSPECTION FOUND THAT THE BLADE ANGEL SETTING FROMSDR CA040202001Seal · blown(CAN) PILOT NOTICED ENGINE SEEPING FROM LT ENGINE COWL, THEY WERE NEAR THE AIRPORT AND DECIDED TO SHUTDOWN LT ENGINE TO PREVENT ENGINE DAMAGE. IT WAS DETERMINED ON THE GROUND BY MAINTENANCE THAT THE LT PROP SEAL HAD BLOWN DUE TO A FROZEN BREATHER. IT WAS DETERSDR AUS20040089Propeller · faulty(AUS) LT AND RT PROPELLERS FAULTY. BOTH ENGINES OVERTEMPED.SDR W1J2004F00000Retaining Ring · out of positionON 2/6/04 A NORMAL ENGINE RUN AND TAXI WAS BEING PERFORMED. AS WE ATTEMPTED TO TAXI OUT THE LT SIDE SEEMED TO HAVE NO THRUST OR MOVEMENT. WE HEARD A LOUD THUMP OR POP ON THE LT SIDE OF THE AIRCRAFT. AT THAT TIME WE ABORTED THE TAXI AND SHUT DOWN BOTH ENGINESDR 2004FA0000234Plate · crackedDURING AN INSPECTION, THE BULKHEAD MOUNTING PLATES WERE FOUND CRACKED AND BROKEN AROUND THE HOLES THROUGH WHICH THE PROPELLER MOUNTING STUDS PASS. THIS CONDITION IS FOUND VERY OFTEN AND THE PLATES REALLY NEED TO BE REDESIGNED TO NOT CRACK AS EASILY AS THEY DOSDR RAIA00402004Propeller · faultyJLN - LEFT PROP HEAT INOP. MAINTENANCE DEFERRED PROP HEAT PER MEL. SUBSEQUENTLY CLEARING DMI BY REMOVING AND REPLACING NR 1 PROP.SDR 2004FA0000218Piston · seizedPISTON SEIZED IN HIGH PITCH POSITION TO PISTON ROD TUBE (HAD TO BE REMOVED AND PRESSED OUT OF PISTON PROP) WOULD NOT CYCLE ON AIRCRAFT. PISTON TUBE AND PISTON SENT TO MFG TECH REP. SUSPECT THAT PROP GOV WORN PARTS ALLOWED METAL INTO PROP AND SEIZED PISTON TUSDR W592004F00000Spacer · crackedPROPELLER SPACER WAS FOUND CRACKED FROM DOWEL PIN HOLES. ONE CRACK PROGRESSED COMPLETELY THROUGH SPACEER, THE SECOND WAS 90 PERCENT THROUGH SPACER. PROPELLER DOWEL PIN HOLES ARE ELONGATED AND OVERSIZE, PROPELLER WAS BENT SEVERELY AT ONE TIME AND IMPROPERY RESDR 2004FA0000149Counterweight · crackedPART HAD APPROX 700.00 HOURS SINCE OVERHAUL, FATIGUE CRACK APPEARS TO HAVE ORIGINATED AT FORWARD BOLT HOLE. PROPELLER/ENGINE BEGAN VIBRATING IN FLIGHT DUE TO COUNTER WEIGHT SHIFTING ON FERRULE. AIRCRAFT REDUCED POWER, LANDED AND WAS REPAIRED BEFORE FURTHER SDR QXEA200400017Propeller · out of balanceSEA FLIGHT 2026 RETURNED TO FIELD. PROP VIBRATION AT 1050 NP. BALANCED PROP. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR AUS20040003Propeller · lightning strike(AUS) LIGHTNING STRIKE ON RT PROPELLER AND RT FUSELAGE ADJACENT TO SAS VANE. SAS CIRCUIT BREAKER POPPED. DAMAGE TO RT PROPELLER AND RT FUSELAGE CONSISTENT WITH LIGHTNING STRIKE.SDR HNAA0300090Blade · burnedWITH PROP HEAT ON NR 2 PROP STARTED GLOWING ORANGE CEASED WITH PROP HEAT OFF REMOVED AND REPLACED NR 2 BLADE AND BLADE RETAINING RING OPS AND LEAK CK GOOD IAW W/C 61-10-07R.SDR AUS20031188Propeller · damaged(AUS) LT PROPELLER FAULTY. LIMITED INFORMATION PROVIDED.SDR PCAA0310129Control Unit · out of rigFLIGHT 3961 INTO DCA, NR 1 PROPELLER WAS UNABLE TO BE REDUCED BELOW 930 RPM IN CRUISE FLIGHT. MAINTENANCE RE-RIGGED NR 1 ENGINE PROPELLER CONTROL UNIT AND GROUND RAN AIRCRAFT, OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE.SDR 2004FA0000151Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000158Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000157Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TOT HE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000156Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000155Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000154Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000153Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000152Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR 2004FA0000150Gasket · leakingRED DYE OIL LEAKAGE AT THE CYLINDER TO HUB ATTACH POINT. OIL IS LEAKING PAST THE CYLINDER GASKET TO THE ATTACHING SCREWS AND FOLLOWING THE THREADS OUT. ADDITIONAL SEALANT NEEDS TO BE ADDED TO THE SCREWS DURING INSTALLATION AND PARTICULAR ATTENTION SHOULD BE SDR GLBA2003140Ring · mismanufacturedTORQUE WAS HIGH, REMOVED PROPELLER, INSPECTION FOUND INTERNAL SPACER RING NOT DRILLED AND RESULTED IN A PIN NOT BEING INSTALLED AND SPACER RING BACKED-OFF CAUSING TORQUE ISSUE. LAST OVERHAUL WAS AT HARTZELL TSO 438.0.SDR CA031015007O-Ring · worn(CAN) CUSTOMER COMPLAINED OF RED OIL IN HIS ENGINE OIL. THE PROPELLER WAS SENT IN OFR REPAIR, AND IT WAS DETERMINED THAT THE CYLINDER WAS BADLY WORN INTERNALLY AND THAT THE SEAL WAS ALSO BADLY WORN. THIS ALLOWED RED OIL FROM INSIDE THE HUB TO ENTER THE OIL SYSDR 00067538Latch · crackedCRACK ON PROPELLER LATCH PAWL.SDR 0067538Latch · crackedCRACK ON LATCH PAWL.SDR CA030818004Pitch Stop · stripped(CAN) DURING INSPECTION OF THE PROP, MAINTENANCE ATTEMPTED TO REMOVE THE SPINNER BUT COULDN'T BECAUSE THE LOW PITCH STOP THREADS WERE STRIPPED, WHERE THE SPINNER ATTACHES TO THE LOW PITCH STOP. THE LOW PITCH STOP HAD TO BE REMOVED FROM THE P ROPELLER SO THE SPSDR 0075982Bearing Race · corrodedPROPELLER HAS CORROSION ON BEARING RACE.SDR CA030729001Clamp · corroded(CAN) PROP WAS SENT IN TO US FOR AD 2003-13-17. PROP INSPECTION WAS NOT REQUIRED BY S/N, BUT IN THE AD THEY RECOMMENDED THAT ANY PROP THAT HAD BEEN OVERHAULED BY T&W BE INSPECTED IAW PARAGRAPH H. UPON DISASSEMBLY & VISUAL INSPECTION OF PARTS, FOUND TWO OF C838SDR 2003FA0000754Propeller · inoperativePROPELLER ASSY, AIRCRAFT CREW REPORTED RT PROPELLER GOES TO FEATHER ON TAXI WITH HOT OIL. ENGINE AND PROP GOVERNOR CHANGED. PROPELLER SWAPPED. PROBLEM FOUND TO BE PROPELLER AIR CHARGE PROCEDURE WAS CHANGED IAW MFG LS. C/W THIS SL FIXED PROBLEM .SDR 2003FA0000756Bearing · failedPROPELLER LOCKED INTO LOW PITCH TWICE. REMOVED NR 2 BLADE TO INSPECT NR 1 BLADE BUTT. FOUND SEVERAL BALL BEARINGS PRESSED INTO SIDE OF INNER HUB WALL AND FERRULE. BEARING RACE BROKEN, WITH SEVERAL SMALL PIECES IN BOTTOM OF HUB. PROPELLER, HUB HAD BEEN SERSDR AUS20030749Dowel Pin · misinstalled(AUS) CRANKSHAFT PROPELLER MOUNTING FLANGE PROPELLER LOCATING DOWELS INCORRECTLY FITTED. DOWELS HAVE A SLIGHT TAPER WHICH ALLOWS FOR A SLIP FIT INTO THE CRANKSHAFT AND AN INTERFERENCE FIT ONTO THE PROPELLER. THE DOWELS WERE INCORRECTLY FITTED WITH THE INTERFERSDR AUS20030656Propeller · faulty(AUS) PROPELLER REMOVED DUE TO OIL LEAK. DISASSEMBLY AND INVESTIGATION FOUND THE FOLLOWING DEFECTS; INCORRECT LOCKING OF BALANCE WEIGHT SCREWS. SCREWS WERE LOCKWIRED IN A MANNER THAT THE SCREWS WERE UNDOING EACH OTHER. PN A2433 LONG BOLTS WERE USED INSTEAD OSDR AUS20030623Bolt · sheared(AUS) PROPELLER COUNTERWEIGHT BOLT HEAD SHEARED. THE OTHER BOLT HEAD ALSO SHEARED WHEN THE LOCKWIRE WAS REMOVED. PROPELLER CAME FROM A NEW ZEALAND REGISTERED AIRCRAFT.SDR CA030605016Nut · cracked(CAN) PROP WAS REMOVED DURING ENGINE REPAIRS, NUT HOLDING PROP TO CRANKSHAFT WAS FOUND CRACKED. NUT WAS CRACKED FROM NOTCH FOR INSTALL/REMOVAL TOOL TO HOLE FOR LOCKING CLIP. NUT WAS REPLACED WITH OVERHAULED UNIT AND PROP WAS REINSTALED & AIRCRAFT RETURNED TO SDR 0074567Clamp · corrodedCORRISION ON CLAMP ASSEMBLYSDR CA030324002Bearing Race · cracked(CAN) PROP REMOVED DUE TO EXCESSIVE BLADE RADIAL PLUS END PLAY. UPON DISASSEMBLY 2 OPPOSING BLADE BEARING WERE FOUND TO BE CRACKED. HUB FORWARDED TO HARTZELL FOR EVALUATION OF DAMAGE.SDR 74451Bearing Race · crackedCRACK IN RACE
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