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 CA970918005Propeller · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. INSPECTION FOUND THE PROPELLER HAD EXTENSIVE CORROSION AND AN OVERHAUL WAS REQUIRED.SDR 97ZZZX4312Bolt · misinstalledDURING ANNUAL INSPECTION, PROPELLER COUNTERWEIGHT ATTACH BOLTS FOUND UNSAFTIED POST OVERHAUL. HARTZELL MANUAL NR 117D REQUIRES THESE BOLTS TO BE REPLACED AT OVERHAUL AND RE-DRILLED FOR ROLL-PIN SAFETY. THESE BOLTS WERE RE-USED AFTER OVERHAUL SINCE THEY WERE DSDR WTAA970168Propeller · bird strikeLAX - EVIDENCE OF BIRD STRIKE FOUND ON LEFT PROPELLER SPINNER AND BLADES. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (X)SDR 97ZZZX4734Shield · debondedLEADING EDGE EROSION SHIELD ON RT PROPELLER IS DEBONDED 10 INCHES FROM ROOT OF BLADE OUT ON ONE BLADE. REPAIRED IAW CMM 61-13-35, PAGE 505. (X)SDR REXA97222Propeller · vibrationBAD VIBRATION NOTED FROM RT SIDE OF AIRCRAFT. SLIGHT PROPELLER VIBRATION ON RT SIDE. AFTER RETURNING, VIBRATION SEEMED TO GET BETTER. INSPECTED THE RT PROPELLER AND PERFORMED GROUND RUNS, NO DEFECTS NOTED. (X)SDR 97ZZZX3937Propeller · departedTHIRTY MINUTES AFTER TAKEOFF, PILOT REPORTS VIBRATION AND THEN PROPELLER SEPARATED FROM ENGINE. PILOT SAYS NOT SURE IF BIRD STRIKE OR PART FAILURE. AIRCRAFT LANDED WITHOUT INJURY TO PILOT OR FURTHER DAMAGE TO AIRCRAFT.SDR 97ZZZX3765Propeller · seals failedOIL LEAK FROM RT PROPELLER/ENGINE. REPLACED PROPELLER.SDR 97ZZZX3477Propeller · crackedTWO CRACKS FOUND AT EDGE OF BOLT HOLES, APPROXIMATELY .50 INCH LONG. FOUND DURING INSPECTION REQUIRED BY SB 221 AND AD 97-06-16.SDR 97ZZZX3786Retain Nut · failedAIRCRAFT ACCIDENT IN WHICH PROPELLER SEPARATED FROM AIRCRAFT. SUSPECT CAUSE: RETAINING NUT FAILURE. SUBMITTER RECOMMENDATION: RETAINING NUT BE REPLACED AT SPECIFIC INTERVALS. RETAINING NUT BE INSPECTED PRIOR TO EACH PROPELLER INSTALLATION.SDR SWIA97912Propeller · over torquedLEFT ENGINE INADVERTENT AUTO FEATHER ON CLIMB OUT AND TORQUE WENT TO 133 PERCENT. REMOVED AND REPLACED LEFT PROPELLER AND LEFT TORQUE SIGNAL CONDITIONER, OPS CHECKS GOOD.SDR COMA9710319Propeller · damagedRT PROPELLER STRUCK GROUND EQUIPMENT DURING TAXI OPERATION. REPLACED THE RT PROPELLER AND ENGINE.SDR COMA9710309Bearing · wornBLADE ASSEMBLY REMOVED FROM AIRCRAFT FOR DE-ICE BOOT INSPECTION. UPON INITIAL RECEIVING INSPECTION THE BEARING INSERT WAS FOUND TO BE WORN .012 ALONG THE ENDS. INSERT WAS REMOVED FROM SERVICE AND HELD FOR FURHTER EVALUATION.SDR AU970647Slideblock · damaged(AUS) PROPELLER ADJACENT SLIDEBLOCKS (2OFF) DISLODGED AND DAMAGEDSDR VNAA9706002Prop · birdstrikeON TAKEOFF ROLL, RIGHT PROP WAS STRUCK BY A BIRD. ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND NO DAMAGE WAS FOUND. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR AU970572Propeller · fluctuates(AUS) PROPELLER CAUSING RPM FLUCTUATIONS - PROPELLER WAS STRIPPED AND INSPECTED WITH NO SATISFACTORY CAUSE OF THE PROBLEM FOUNDSDR CA970527014Propeller · mis ohauled(CAN) PROPELLER RECEIVED FOR BENCH CHECK. NUMEROUS FAILURES FOUND INCLUDING: WRONG TYPE OF DE-ICER BOOT; BULKHEAD INSTALLED ON WRONG SIDE OF SLIP RING; LOW STOP COLLAR INSTALLED IN WRONG POSITION; LOW STOP COLLAR RUNOUT WAS GREATER THAN MAX ALLOWABLE; SLIP RINSDR VTZA97286Propeller · out of adjustIAD/ROC - AT 1210 HRS ON 5-19-97, ABORTED TAKEOFF DUE TO LEFT ENGINE RED BETA WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED LEFT PROP BLADE ANGLE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APSDR VTZA97283Propeller · out of adjustPWM/BOS - FLT 6402 - DURING TAKEOFF AT 2120 HRS ON 5-16-97, ABORTED TAKEOFF DUE TO RT ENGINE RED BETA CAPTION ILLUMINATED DURING TAKEOFF ROLL. AIRCRAFT REUTRNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED BLADE ANGLES, OPS CHECK OK. SDR C2XA97CL046Prop Assembly · wornCLE - DURING A SCHEDULED INSPECTION, THE LEFT HAND PROPELLER ASSEMBLY WAS FOUND TO HAVE ONE BLADE WITH EXCESSIVE FORE/AFT AND SIDE/SIDE MOVEMENT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND PROPELLER ASSEMBLY IAW B1900 MM 61-10-00. THE OPERATIONAL LEAK CHSDR CA970422031Propeller · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER REQUIRED OVERHAUL DUE TO CORROSION.SDR CA970409007Propeller · corrosion(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.SDR AU970309Spring · faulty(AUS) PROPELLER CONTAINED THE FOLLOWING DEFECTS:- 1. LATCH PNO B318 BROKEN. 2. LATCH BOLTS PNO A1595 (2OFF) SHEARED AND ONE BOLT BENT 3. CYLINDER PNO B2423-1 DAMAGED 4. PISTON PNO B3237 WORN 5. INCORRECT PRESSURE DECAL FITTED. PERSONNEL/MAINTENANCE ERRORSDR MASA97017Prop Assy · leakingLRU/ABQ - FLT 401 - SHORTLY AFTER PASSING THROUGH 1,500 FEET AGL, THE FLIGHT CREW NOTICED OIL PRESSURE ON THE NR 2 ENGINE DROPPED BELOW 70 PSI. THE CREW REDUCED POWER ON THE RT ENGINE AND PROCEEDED TO RETURN TO THE FIELD. ON DESCENT, THE OIL PRESSURE DROPPEDSDR AU970266Propeller · faulty(AUS) LH PROPELLER SUSPECT OUT OF BALANCE - LH ENGINE FORWARD ENGINE MOUNT LOOSE - INVESTIGATION FOUND PROBLEM CAUSED BY BLADE ANGLES AND PROFILESSDR COMA9710180Bearing Insert · wornPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR SCHEDULED ENGINE CHANGE. ASSEMBLY WAS RECEIVED IN THE PROPELLER SHOP DUE TO BLADES BEING EXCESSIVELY LOOSE CAUSING AN IMBALANCE SITUATION. FOUND BEARING INSERT WORN IN AN OVAL FASHION, MEASURING FROM 0.0665 - 0.09SDR COMA9710179Bearing Insert · wornPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR SCHEDULED ENGINE CHANGE. ASSEMBLY WAS RECEIVED IN THE PROPELLER SHOP DUE TO BLADES BEING EXCESSIVELY LOOSE CAUSING AN IMBALANCE SITUATION. FOUND BEARING INSERT WORN IN AN OVAL FASHION, MEASURING FROM 0.0725 - 0.09SDR COMA9710178Bearing Insert · wornPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR SCHEDULED ENGINE CHANGE. ASSEMBLY WAS RECEIVED IN THE PROPELLER SHOP DUE TO BLADES BEING EXCESSIVELY LOOSE CAUSING AN IMBALANCE SITUATION. FOUND BEARING INSERT WORN IN AN OVAL FASHION, MEASURING FROM 0.0775 (WALL SDR 97ZZZX1922Propeller · oil leakDURING PRE-FLIGHT, DISCOVERED LT PROPELLER LEAKING OIL.SDR COMA9710177Stop Tab · bentPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB S/N 248 WAS FOUND TO BE BENT APPROXIMATELY 0.125. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND HELD FOR PROPOSED FUTURE REPAIR.SDR COMA9710176Bearing Insert · wornPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE BLADE PIN BEARING INSERT WAS FOUND TO BE WORN IN AN OVAL FASHION. FURTHER INSPECTION SHOWED THAT THE INSERT HAD WORN TO .083 AT THE THINNEST POINT AND .0SDR COMA9710175Bearing Insert · wornPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE BLADE PIN BEARING INSERT WAS FOUND TO BE IN AN OVAL FASHION. FURTHER INSPECTION SHOWED THAT THE INSERT HAD WORN TO .082 AT THE THINNEST POINT AND .099 ATSDR 97ZZZX4725Clamp Assy · failedCLAMP ASSY RAPCO P/N RA1983-2 WAS SUBSTITUTED FOR A BFG 3E1883-2 UNDER THE ASSUMPTION OF JORDAN PROPELLER SERVICE CRS NR 2273. THIS IS REPORTED AS AN FAA-PMH APPROVED PART WHICH IS IN FACT A NON FAA-PMA PART. THIS CLAMP ASSY FAILED CAUSING THE FOLLOWING REPASDR AU970189Propeller · wrong torque(AUS) PROPELLER INSTALLATION TORQUE DISCREPANCY - PROPELLER DECAL AND AIRCRAFT MANUAL INDICATE DIFFERENT TORQUE SETTINGSSDR AU970093Seal · pinched(AUS) PROPELLER BLADE NUT SEALS PINCHED GIVING INEFFECTIVE SEALING -SEALING WAS ACHIEVED BY THE USE OF SILASTIC SEALANT BETWEEN THE BLADE NUT THREADS AND HUB AND LOCK RING ASSEMBLY - INCORRECT ASSEMBLY - PERSONNEL/MAINTENANCE ERROR - PROPELLER HAD BEEN MODIFIESDR AU970071Propeller · loose(AUS) LH ENGINE PROPELLER LOOSE ON CRANKSHAFT - ALL SIX RETAINING NUTS WERE LOOSE - FOLLOWING REMOVAL OF PROPELLER ONE OF TWO DOWELS WAS FOUND TO BE BROKEN - SUSPECT BOLTS WERE NOT TORQUED WHEN PROPELLER WAS REFITTED TWENTY THREE HOURS PREVIOUSLY (DEC 1996) - SDR WTAA970017Propeller · bird strikeBFL - BIRD STRIKE REPORTED TO LEFT PROPELLER ON LANDING ROLL-OUT. MAINTENANCE C/W BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (X)SDR CA970206005Propeller · high vibration(CAN) HARTZELL PROPELLER INSTALLED AS PER STC #SA685AL. TROUBLESHOT VIBRATION SINCE INSTALLATION. INSTALLED SECOND PROP AND DID DYNAMIC BALANCE, THIS CHANGED THE POSITION OF VIBRATION. REMOVED PROP AND INSTALLED ZERO TIME MCCAULEY PROP. VIBRATION GONE.SDR UF6A970106Prop · out of balanceORD - FLT 5719 - VIBRATION DEVELOPED IN FLIGHT WORSE AT HIGHER POWER SETTINGS WITHOUT NP HIGHER. MAINTENANCE BALANCED BOTH PROP ASSEMBLIES. BALANCE CHECK GOOD. (M)SDR UF6A970105Prop · out of balanceORD - FLT 5751 - EXCESSIVE VIBRATION AT HIGH RPM. MAINTENANCE PERFORMED PROP BALANCE OF LEFT AND RIGHT PROP ASSEMBLIES. BALANCE CHECK GOOD. (M)SDR 97ZZZM301Prop · out of balanceORD - FLT 5751 - EXCESSIVE VIBRATION AT HIGH RPM. MAINTENANCE PERFORMED PROP BALANCE OF LEFT AND RIGHT PROP ASSEMBLIES. BALANCE CHECK GOOD. REFERENCE UF6A970105.SDR 97ZZZM300Prop · out of balanceORD - FLT 5719 - VIBRATION DEVELOPED IN FLIGHT WORSE AT HIGHER POWER SETTINGS WITHOUT NP HIGHER. MAINTENANCE BALANCED BOTH PROP ASSEMBLIES. BALANCE CHECK GOOD. REFERENCE UF6A970106.SDR UF6A970104Prop · out of balanceORD - FLT 5764 - AIRCRAFT HAS PRONOUNCED VIBRATION DURING CRUISE FLIGHT. MAINTENANCE BALANCED NR 1 AND NR 2 PROP ASSEMBLIES. SYSTEM OPS CHECK GOOD. (M)SDR 97ZZZM299Prop · out of balanceORD - FLT 5764 - AIRCRAFT HAS PRONOUNCED VIBRATION DURING CRUISE FLIGHT. MAINTENANCE BALANCED NR 1 AND NR 2 PROP ASSEMBLIES. SYSTEM OPS CHECK GOOD. REFERENCE UF6A970104.SDR M8XA970003Propeller · vibrationFLT 7001 - TRAINING FLIGHT. CREW REPORTED A SLIGHT PROPELLER VIBRATION WHEN PROPELLER CONTROLS WERE SET AT 80 PERCENT NP. CREW ELECTED TO RETURN TO FIELD. AIRCRAFT LANDED AT COS WITHOUT FURTHER INCIDENT. MAX - MX REPLACED LT PROPELLER ASSEMBLY IAW AMM 61-1SDR AU971370Spacer · wrong part(AUS) INCORRECT SPACER FITTED TO PROPELLER. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.SDR SRAA970108Dome Nut · looseDURING FLIGHT, NR 1 PROP LOW OIL LIGHT CAME ON WITH .5 PERCENT RPM FLUX, SHUT DOWN NR 1 ENGINE AND LANDED AT PTY WITHOUT INCIDENT. FOUND NR 1 PROPELLER DOME NUT AND CAP LOOSE. TIGHTENED SAME AND RAN ENGINE, LEAK CHECK GOOD PER MM CH 61-01.SDR COMA9610430Bearing · wornPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. INSPECTION REVEALED UNEVEN WEAR ON THE BLADE BEARING INSERT. WEAR HAD OCCURED IN AN OVAL FASHION AND INSERT WALL THICKNESS HAD DETEIORATED FROM ORIGINAL .100\ WITH THE THICKNESSES RANGSDR COMA9610429Bearing · wornPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. INSPECTION REVEALED UNEVEN WEAR ON THE BLADE BEARING INSERT. WEAR HAD OCCURED IN AN OVAL FASHIION AND INSERT WALL THICKNESS HAD DETERIORATED FROM ORIGINAL .100\ WITH THE THICKNESSES RASDR COMA9610428Bearing · wornPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. INSPECTION REVEALED UNEVEN WEAR ON THE BLADE BEARING INSERT. WEAR HAD OCCURED IN AN OVAL FASHION AND INSERT WALL THICKNESS HAD DETERIORATED FROM ORIGINAL .100\ WITH THICKNESS RANGING FSDR COMA9610410Pitchlock Screw · failedPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. ONCE REMOVED, THE ACTUATOR PITCHLOCK SCREW FEATHER STOP TAB WAS FOUND TO BE DISPLACED APPROXIMATELY .125 INCH. PITCHLOCK SCREW WAS REMOVED FROM SERVICE AND RETURNED TO MANUFACTURER.
Back to JASC 6110