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 95ZZZX3325Screw · brokenDURING DISASEMBLY, INNER CLAMP SCREW FOUND BROKEN OFF ON THE SHANK AT TOP THREAD, ENTERING CLAMP. SURFACE OF BREAK APPEARED CLEAN WITH A SMALL PIT ORIGINATING IN THE MIDDLE OF THE THREAD AREA. SUSPECT PIT WAS CAUSED BY MOISTURE CREEPING AROUND SOCKET HEAD OFJun 1, 1995 · Beech 95SDR 97ZZZX889Blade · delaminatedINSPECTION FOUND DELAMINATION AT BASE OF BLADE. SUBMITTER STATED CAUSE UNKNOWN. AWAITING INFORMATION FROM MANUFACTURER.May 26, 1995 · N30367 · Slnsby T67M260SDR COM1083Prop Blade · damagedRT PROPELLER, BLADE LEADING EDGE ERROSION GUARD IS LOOSE. REPLACED PROPELLER ASSY.May 19, 1995 · N341CA · Saab SF340ASDR PLGA412951Blade · looseDURING A ROUTINE INSPEC, THE NR 3 BLADE HAD EXCESSIVE MOVEMENT O/B OF THE OUTER SLEEVE. ONE OF THE SLIDER BLOCKS HAD DETACHED FROM THE CROSSHEAD AND WAS MOVING AROUND THE HUB ASSY. ALSO, SEVEN SMALL PINS WERE FOUND INSIDE THE HUB ASSY. ALL PINS WERE MISSINGApr 12, 1995 · N366BE · Saab 340BSDR 95ZZZX1738Blade · corrodedANNUAL INSPECTION REVEALED DEEP PITS ON CAMBERED SURFACE OF PROPELLER. FACE OF PROP PROTECTED BY FLAT BLACK PAINT, CAMBER UNPROTECTED, UNPAINTED EXCEPT FOR WHITE TIPS. DEEP LINES OF CORROSION AT INTERSECTION OF PAINTED TIPS AND UNPAINTED CAMBER. ONE PROPELLMar 22, 1995 · N8792N · Piper PA28140SDR 95ZZZX1698Blade · crackedPROPELLER WAS REMOVED FROM AIRCRAFT FOR VIBRATION. AFTER DISASSEMBLY, NR 1 BLADE WAS CRACKED IN HALF IN FILLET AREA, ONLY BLADE BUSHING PREVENTED SEPARATION FROM THE HUB.Mar 1, 1995 · N984UA · Ayres S2RNORMALSDR 95ZZZZ129Prop Blade · leakingPILOT REPORTED OIL LEAKING FROM RIGHT PROPELLER. MAINTENANCE INSPECTED AND DETERMINED THE NR 4 BLADE WAS LEAKING AT THE BLADE ROOT. THE PROPELLER WAS REPLACED AND A FUNCTIONAL CHECK PERFORMED WITH ALL INDICATIONS NORMAL AND NO LEAKS NOTED.Feb 20, 1995 · N359AE · Swrngn SA227ACSDR 95ZZZX1259Blade · defectiveTHE PROPELLER WAS RECENTLY OVERHAULED BY AN APPROVED O/H FACILITY. AFTER INSTALLATION ON THE AIRCRAFT, THE PROPELLER WOULD EMIT A LOUD NOISE AND VIBRATION AT/OR NEAR 100 PERCENT POWER. THIS VIBRATION AND NOISE IS BELIEVED TO BE FROM BLADE FLEX ON THE PROPELLFeb 16, 1995 · N7069A · Beech C12ASDR 95ZZZX989Rod End Bearing · nut loosePROPELLER PITCH CHANGE THROUGH-LINKS AND ROD-END BEARINGS. INSPECTION FOUND NUT LOOSE ON STUD HOLDING ROD-END BEARING. NUT HAD DEFECTIVE SELF-LOCKING FEATURE. A FIX WAS DONE BY USING STEEL LOCK NUTS WITH LOCK-TITE. ALSO, NO SAFETY WASHERS WERE USED ON THOSFeb 14, 1995 · N9737Y · Beech 35B33SDR 95ZZZX1169Blade · corrodedINSPECTION OF PROP FOUND HEAVY CORROSION IN BLADE BORE OF BLADE NR 3.Feb 13, 1995 · Beech C90SDR 95ZZZX1168Blade · corrodedINSPECTION OF PROP FOUND HEAVY CORROSION IN BLADE BORE OF BLADE NR 2.Feb 13, 1995 · Beech C90SDR 95ZZZX1167Blade · corrodedINSPECTION OF PROP FOUND HEAVY CORROSION IN BLADE BORE OF BLADE NR 1.Feb 13, 1995 · Beech C90SDR 95ZZZX4195Blade · tip departedNINE INCHES OF TIP OF BLADE CAME OFF IN-FLIGHT. BLADE HAD BEEN SENT TO HARTZELL PROPELLER, INC., FOR EVALUATION.Feb 10, 1995SDR C2XA95IA022Blade · crackedIAH - DURING C-CHECK INSPECTION, THE NR 1 PROPELLER, NR 1 BLADE WAS FOUND TO HAVE A LIFTING AND TORN EROSION SHEATH. UPON REMOVAL OF THE SHEATH. THE BLADE LEADING EDGE BELOW THE SHEATH, WAS FOUND CRACKED THROUGH THE RESIN INTO THE HEATING ELEMENT IN SEVERAL PFeb 7, 1995 · N57734 · Emb EMB120RTSDR 95ZZZX926Blade · crackedINSPECTION FOUND BLADE CRACKED. SUBMITTER STATED AD 68-19-04 SHOULD APPLY TO THESE BLADES ALSO.Feb 6, 1995 · N6106X · Gulstm 500BSDR 95ZZZX748Blade · damagedBLADE WAS RECEIVED WITH SCORING DAMAGE AROUND THE O.D. OF THE BUTT AREA. DAMAGE EXISTS 360 DEGREES AROUND BUTT AND IS APPROXIMATELY .020 INCH DEEP BY .025 INCH HIGH. DAMAGE APPEARS TO HAVE BEEN CAUSED BY RESIDUAL SHOT PEEN BALLS WHICH WERE TRAPPED INSIDE BLAJan 30, 1995SDR 95ZZZX747Blade · damagedSUBJECT BLADE RECEIVED WITH SCORING DAMAGE AROUND THE O.D. OF THE BUTT AREA. DAMAGE EXITS 360 DEGREES AROUND THE BUTT AND IS APPROXIMATELY .010 INCH DEEP BY .025 INCH HIGH. DAMAGE APPEARS TO HAVE BEEN CAUSED BY RESIDUAL SHOT PEEN BALLS WHICH WERE TRAPPED INSJan 30, 1995SDR 95ZZZX4479Blade · damagedSUBJECT BLADE WAS RECEIVED WITH SCORING DAMAGE AROUND THE OUTSIDE DIAMETER OF THE BUTT AREA. DAMAGE EXISTS 360 DEGREES AROUND THE BUTT AND IS APPROXIMATELY .015 INCH DEEP BY .015 INCH HIGH. DAMAGE APPEARS TO HAVE BEEN CAUSED BY RESIDUAL SHOT PEEN BALLS WHICHJan 30, 1995SDR 95ZZZX4478Blade · damagedSUBJECT BLADE RECEIVED WITH SCORING DAMAGE AROUND THE OUTSIDE DIAMETER OF THE BUTT AREA. DAMAGE EXISTS 360 DEGREES AROUND THE BUTT AND IS APPROXIMATELY .015 INCH DEEP BY .020 INCH HIGH. DAMAGE APPEARS TO HAVE BEEN CAUSED BY RESIDUAL SHOT PEEN BALLS WHICH WERJan 30, 1995SDR 95ZZZX3317Fork · crackedDURING TIME OVERHAUL OF THESE PROPS, THE PITCH CHANGE FORK WAS FOUND CRACKED. FAILURE OF THIS PART WOULD CAUSE ONE BLADE NOT TO BE CONTROLLED DURING PITCH CHANGE OF THE PROP AND COULD CAUSE SEVERE VIBRATION BECAUSE BLADE ANGLES WOULD NO LONGER MATCH BETWEEN BJan 27, 1995 · Beech 200BEECHSDR 95ZZZX1611Blade · failedPROPELLER HAD BLADE FAILURE AT THE 30 INCH STATION. DURING DISASSEMBLY, ALSO NOTICED THAT AT LAST ASSY, THE A4140 LOCKING PLUGS FOR THE BLADE RETENTION NUTS HAD NOT BEEN INSTALLED. AFTER FURTHER DISASSEMBLY, THE BLADE THAT HAD FAILED ALSO HAD A CRACKED BLADEJan 27, 1995 · Cessna 188CESSNASDR PLGA51951Prop Blades · looseON JANUARY 22, 1995, PROPELLER ASSY WAS REMOVED FOR PROP DE-ICE FAILURE ON THE NR 1 BLADE. AFTER REMOVAL OF THE BAD DE-ICE BOOT, MOVEMENT WAS NOTED BETWEEN THE OUTER SLEEVE AND THE COMPOSITE MATERIAL. ALL BLADES WERE THEN INSPECTED AND 2 MORE BLADES WERE FOUJan 22, 1995 · N342BE · Saab SF340ASDR 95ZZZX580Pitch Rod · failedTHE ROD FAILED AT THE SPLIT RETAINER INDICATING THE TUBE IS NOT STRONG ENOUGH TO WITHSTAND SPRING PRESSURE. SUBMITTER RECOMMENDS ALL HARTZELL PROPS WITH THE OLD STYLE ROD BE CHANGED WITH THE NEW STRONGER ROD, PN C-1948, IAW HARTZELL SB 177.Jan 17, 1995 · N3330K · Mtsbsi MU2B35SDR 95ZZZX629Blade · scoredSUB JECT BLADE WAS RECEIVED WITH SCORING DAMAGE AROUND THE OUTSIDE DIAMETER OF THE BLADE BUTT AREA. DAMAGE IS INTERSPERSED 360 DEGREES AROUND THE BUTT, AND IS APPROXIMATELY .010 INCH DEEP BY .200 INCH HIGH. THE DAMAGE APPEARS TO POSSIBLY HAVE BEEN CAUSED BY Jan 10, 1995SDR 95ZZZX628Blade · scoredSUBJECT BLADE WAS RECEIVED WITH SCORING DAMAGE AROUND THE OUTSIDE DIAMETER OF THE BLADE BUTT AREA. DAMAGE IS LOCATED 360 DEGREES AROUND THE BUTT, AND IS APPROXIMATELY .020 INCH DEEP BY .300 INCH HIGH. THE DAMAGE APPEARS TO POSSIBLY HAVE BEEN CAUSED BY RESIDUJan 10, 1995
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