JASC 6111

Service difficulty reports · 1,725

Reports filed under 6111 · Propeller Blade 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 = '6111'
  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.

SDR 98ZZZX897Blade · crackedPROPELLER WAS SHOWING SIGNS OF ERRATIC PITCH CHANGE AND STICKING. BLADE SHOWS EVIDENCE OF PREVIOUS IMPACT STRIKE. THIS AIRCRAFT HAD PREVIOUSLY HAD A STUCK PRESSURE RELIEF VALVE IN THE GOVERNOR WHICH, AFTER DISCUSSION WITH THE PILOT, MAY HAVE CAUSED AN OVERSPFeb 10, 1998 · N979ND · Cessna 182JSDR 98ZZZX3324Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. THREE CRACKS.Feb 9, 1998 · Beech 1900DSDR 98ZZZX1040Fork · crackedINSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS.Feb 3, 1998 · Beech 1900DSDR 98ZZZX622Counterweight · failedPROPELLER ASSY COUNTERWEIGHT FAILURE. COUNTERWEIGHT WAS FLUNG FROM BLADE NR 1 AND HIT BLADE NR 2 DESTROYING BLADE.Jan 26, 1998SDR 98ZZZX855Blade Pin · looseREFERENCE: FR34201. REASON FOR REMOVAL: LOOSE BLADE PIN. RECOMMENDATIONS: BLADE HISTORY TO BE REVIEWED FOR PIN INSTALLATION ISSUES. CUSTOMER: ALM ANTILLEAN AIRLINES.Jan 24, 1998 · Dhav DHC8*SDR CA000801019Propeller · loose(CAN) LOOSE PROPELLER BLADES.Jan 22, 1998 · Rhnflu EA300LSDR 98ZZZX1041Fork · crackedINSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FOUR CRACKS.Jan 21, 1998 · Beech 1900DSDR 98ZZZX694Blade · crackedDURING INSPECTION FOR AD 97-18-02, BOTH PROPELLER BLADES WERE FOUND CRACKED USING PHASE ANALYSIS EDDY CURRENT INSPECTION TECHNIQUE. BOTH BLADES CONTAIN SEVERAL SMALL CRACKS NOT DETECTABLE USING AN ED520 OR SIMILAR METER BASED INSTRUMENTS. SUBMITTER RECOMMENDJan 20, 1998 · N6937T · Cessna 310DSDR 98ZZZX693Blade · crackedDURING INSPECTION FOR AD 97-18-02, BOTH PROPELLER BLADES WERE FOUND CRACKED USING PHASE ANALYSIS EDDY CURRENT INSPECTION TECHNIQUE. BOTH BLADES CONTAIN SEVERAL SMALL CRACKS NOT DETECTABLE USING AN ED520 OR SIMILAR METER BASED INSTRUMENTS. SUBMITTER RECOMMENDJan 20, 1998 · N6937T · Cessna 310DSDR 98ZZZX518Blade · corrodedCORROSION FOUND BELOW THE PTICH LINE IN THE THREADS CAUSING THE BLADE TO BE UNAIRWORTHY PER MCAULEY SM NR 720415. SUBMITTER STATED ADHERING TO PROPER COMPLIANCE TIMES OF AD 91-15-04 MAY HAVE PREVENTED THIS.Jan 20, 1998 · N8015R · Beech A24RSDR 98ZZZX517Blade · corrodedCORROSION WAS FOUND BELOW TTE PITCH LINES OF THE BLADE THREADS CAUSING THE BLADE TO BE UNAIRWORTHY PER MCCAULEY SM NR 720415. SUBMITTER STATED ADHERING TO COMPLIANCE TIMES OF AD 91-15-04 MAY HAVE PREVENTED THIS CONDITION.Jan 20, 1998 · N8015R · Beech A24RSDR COMA9810023Bearing · wornDURING PROPELLER DYNAMIC BALANCING PROCEDURES, IT WAS DETERMINED THAT THE PROPELLER COULD NOT BE BALANCED. FURTHER INSPECTION OF PROPELLER FOUND NR 2 BLADE TO BE EXCESSIVELY LOOSE. FURTHER INSPECTION FOUND BLADE PIN BEARING TO BE WORN TO 0.080 WALL THICKNESSJan 13, 1998 · N263CA · Emb EMB120RTSDR 98ZZZX3322Fork · crackedFOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. TWO CRACKS.Jan 12, 1998 · Beech 1900DSDR CA971231019Locking Pins · missing(CAN) DURING INSPECTION PRIOR TO DECONTAMINATION, FOUND THE COUNTERWEIGHT LOCKING ROLL PINS WERE MISSING ON ALL THREE BLADES (6 BOLTS). ALSO, THE COUNTERWEIGHT BOLTS WERE NOT DRILLED FOR THE 57A0285 ROLL PINS.Dec 20, 1997 · Piper PA31SDR 98ZZZX560Bearing · crackedBLADE INNER BEARING HALF CRACKED. CRACK IS APPROXIMATELY 2.750 INCHES LONG IN ONE-HALF ONLY.Dec 16, 1997 · Beech 1900DSDR CA971231017Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. CORROSION FOUND ON ALL SURFACES ACCOMPANIED BY STONE DAMAGE.Dec 12, 1997SDR 98ZZZX57Bearing · crackedINNER AND OUTER RACE OF NR 1 BLADE SHANK BEARING FOUND BROKEN AND SEPARATED INTO NUMEROUS PIECES. HUB RENDERED SCRAP AS A RESULT OF BEARING FAILURE. SUBMITTER SUGGESTED ENGINEERING REVIEW OF LOADS IMPOSED AT BLADE/HUB INTERFACE. UNDER LOW C.F. LOADING, IF TDec 3, 1997 · Beech 1900DSDR 98ZZZX56Fork · crackedINSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. ONE CRACK.Dec 3, 1997 · Beech 1900DSDR 98ZZZX55Bearing · crackedINNER AND OUTER RACE OF NR 4 BLADE SHANK BEARING FOUND BROKEN AND SEPARATED INTO NUMEROUS PIECES. HUB RENDERED SCRAP AS A RESULT OF BEARING FAILURE. SUBMITTER SUGGESTS ENGINEERING REVIEW OF LOADS IMPOSED AT BLADE/HUB INTERFACE. UNDER LOW C.F. LOADING, IF THDec 3, 1997 · Beech 1900DSDR CA971118007Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE WAS FOUND ON THE LEADING EDGE AND FACE OF THE BLADE.Nov 13, 1997SDR CA971118006Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE WAS FOUND ON THE LEADING EDGE AND FACE OF THE PROPELLER BLADE.Nov 12, 1997 · Cessna 150MSDR 97ZZZM1209Blade · crackedDURING A SERV CHECK INSPECTION, A MECH DISCOVERED A CRACKED BLADE ON THE LT PROPELLER. THE HAIRLINE CRACK IS ABOUT ONE AND ONE HALF INCHES LONG AND IS LOCATED ABOUT 6 INCHES INBOARD FROM THE END OF THE PROPELLER BLADE ON THE TRAILING EDGE. MAINTENANCE REMOVENov 7, 1997 · N163MA · Swrngn SA226TCSDR 98ZZZX871Blade · crackedWHILE C/W AD 97-18-02, A LARGE CRACK WAS DISCOVERED IN THE 'V' OF THE DOUBLE SHOULDER BLADE SHANK AREA.Nov 5, 1997SDR 98ZZZX870Blade · crackedWHILE C/W AD 97-18-02, A LARGE CRACK WAS DISCOVERED IN THE 'V' OF THE DOUBLE SHOULDER BLADE SHANK AREA.Nov 5, 1997SDR CA971112002Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. CORROSION FOUND UNDER DEICER BOOT.Nov 3, 1997SDR 98ZZZX35Blade · brokeAPPROXIMATELY 4 INCHES OF PROPELLER TIP BROKE OFF IN-FLIGHT. AIRCRAFT MADE EMERGENCY LANDING.Nov 1, 1997 · N6278R · Cessna 172RGSDR CA971112003Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE FOUND ON THE LEADING EDGES AND THE FACE OF THE BLADES. THE BLADES WERE REPAIRED AND ANODIZED.Oct 30, 1997 · Mooney M20JSDR CA971112001Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE FOUND ON THE PROPELLER BLADE LEADING EDGE AND FACE.Oct 30, 1997SDR 97ZZZX4894Clamp · crackedINSPECTION REPORT CONDUCTED BY HARTZELL PROPELLER INC., REVEALED CRACK IN PROPELLER BLADE CLAMP. SUSPECT CAUSE OF CRACK DUE TO FATIGUE.Oct 29, 1997 · N21CJ · Mtsbsi MU2B60SDR 97ZZZX4893Clamp · crackedINSPECTION REPORT CONDUCTED BY HARTZELL PROPELLER INC., REVEALED CRACK IN PROPELLER BLADE CLAMP. SUSPECT CAUSE OF CRACK DUE TO FATIGUE.Oct 29, 1997 · N21CJ · Mtsbsi MU2B60SDR AU971340Clamp · failed(AUS) PROPELLER BLADE CLAMP FAILED AT THE LAST SPOT WELD POSITION OFTHE REINFORCING STRAP.Oct 27, 1997SDR 97ZZZX4805Blade · crackedINSPECTION FOUND ALL 3 BLADES HAVE CHORDWISE CRACKS BEYOND THE 3.5 INCH LIMIT. ALL CRACKS LEAD UP TO AND POSSIBLY UNDER THE EROSION SHIELD. THE CRACKS WERE FOUND DURING INSPECTION PER HARTZELL JB 169A. PROPELLER REMOVED FROM SERVICE AT THIS TIME.Oct 22, 1997 · N931FE · Cessna 208BSDR 97ZZZX4804Blade · crackedINSPECTION FOUND ALL 3 BLADES HAVE CHORDWISE CRACKS BEYOND THE 3.5 INCH LIMIT. ALL CRACKS LEAD UP TO AND POSSIBLY UNDER THE EROSION SHIELD. THE CRACKS WERE FOUND DURING INSPECTION PER HARTZELL JB 169A. PROPELLER REMOVED FROM SERVICE AT THIS TIME.Oct 22, 1997 · N931FE · Cessna 208BSDR 97ZZZX4803Blade · crackedINSPECTION FOUND ALL 3 BLADES HAVE CHORDWISE CRACKS BEYOND THE 3.5 INCH LIMIT. ALL CRACKS LEAD UP TO AND POSSIBLY UNDER THE EROSION SHIELD. THE CRACKS WERE FOUND DURING INSPECTION PER HARTZELL JB 169A. PROPELLER REMOVED FROM SERVICE AT THIS TIME.Oct 22, 1997 · N931FE · Cessna 208BSDR AU971439Blade · fod(AUS) LH PROPELLER BLADE TIP BENT. BLOOD ON THE BLADE LEADS TO THE ASSUMPTION OF AND ANIMAL STRIKE.Oct 21, 1997 · Beech B200CSDR LR7A9724Blade Seal · leakingNR 3 PROP LOW OIL LIGHT FOLLOWED BY OUT OF LIMITS FLUX. ENGINE SHUTDOWN IAW AFM. REMOVED AND REPLACED NR 3 PROPELLER ASSY PER JC6101. OPS OK PER JC7101.Oct 17, 1997 · N401LC · Lkheed 382GSDR CA971021005Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE WAS FOUND TO THE PROPELLER BLADE ON THE LEADING EDGE AND THE FACE.Oct 15, 1997SDR 97ZZZX4675Fork · crackedINSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. TWO CRACKS.Oct 13, 1997 · Beech 1900DSDR CA971020010Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE WAS FOUND ON THE LEADING EDGESOct 10, 1997SDR 97ZZZX4733Blade · crackedDURING ROUTINE ANNUAL INSPECTION, THE PROPELLER WAS STRIPPED OF PAINT. AFTER VISUAL INSPECTION, A CRACK MEASURING .5625 INCH IN LENGTH WAS FOUND APPROXIMATELY 14.50 INCHES IN FROM THE TIP OF THE 'FACE' (BACK) OF THE PROPELLER BLADE. THIS CRACK WAS ONLY VISIBOct 10, 1997 · N8474G · Cessna 150SDR AU971386Blade · cracked(AUS) PROPELLER BLADE CRACKED. CRACK ORIGINATED FROM A NICK IN THE BLADE LOCATED APPROXIMATELY 76.2MM (3IN) FROM THE BLADE TIP.CRACK LENGTH 12.7MM (0.5IN). SUSPECT THE CRACK WAS INITIATED BY A PIECE OF METAL WIRE WHICH WAS FOUND IN THE BLADE DURING DRESSING OUOct 7, 1997 · Gulstm 680FLPSDR 97ZZZX4446Blade · crackedPILOT REPORTED SLIGHT ENGINE VIBRATION AND PROPELLER SLOW TO RESPOND IN RETURN TO LOW PITCH. DISASSEMBLY REVEALED ONE BLADE WAS CRACKED 180 DEGREES NEAR BEARING SURFACE AT ROOT END. CAUSE UNKNOWN. CATASTROPHIC FAILURE IMMINENT. BLADE UNDER ANALYSIS AT MCCAOct 7, 1997 · N75870 · Cessna T207ASDR CA971003006Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. INSPECTION FOUND CORROSION ON THE PROPELLER BLADE FACEOct 3, 1997SDR 97ZZZX4441Blade · crackedPROPELLER RECEIVED FOR AD NOTE INSPECTION (97-18-02). AFTER DISASSEMBLY, NR 2 BLADE FOUND CRACKED IN 'V' OF BLADE BUTT.Oct 3, 1997SDR 97ZZZX4676Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. THREE CRACKS.Oct 1, 1997 · Beech 1900DSDR 97ZZZX4881Blade · crackedCRACK FOUND DURING PROPELLER DYE PENETRANT INSPECTION. CRACK PRESENT IN RETENTION THREAD.Sep 30, 1997 · N3674Y · Cessna 210CSDR CA970930013Blade · damage(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE WAS FOUND ON THE LEADING EDGE OF THE PROPELLER BLADES, BLADES WERE TRIMMED. MOUNTING BOLTS (P/N B4622-12) WERE FOUND BENT AND WERE REPLACED.Sep 24, 1997 · Cessna A150MSDR CA970930014Blade · damage(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE WAS FOUND ON THE LEADING EDGE AND FACE OF THE BLADESep 23, 1997SDR COMA9710409Bearing · wornPILOT REPORTED EXCESSIVE VIBRATION OF PROPELLER WHILE AIRCRAFT WAS TAXIING. INSPECTION OF PROPELLER FOUND NR 1 BLADE TO BE EXCESSIVELY LOOSE. FURTHER INSPECTION FOUND BLADE PIN BEARING TO BE WORN TO 0.053 WALL THICKNESS ON ONE SIDE AND WEARING IN AN OVAL FASSep 22, 1997 · N1150 · Emb EMB120RTSDR CA970930012Blade · damage(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER BLADE FOUND WITH STONE DAMAGE. PROPELLER BLADE WAS TRIMMED.Sep 19, 1997 · Cessna R172K
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