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 CA000907005Blade · misrepaired(CAN) . BLADE SER #841280. BLADE RECD FROM OPERATOR WITH FIBREGLASS DAMAGE BEYONG MANUAL LIMITSL. BLADE RETURNED TO MFG FOR REPAIR. BLADE RETURNED FROM MFG AFTER REPAIR ANDFOUND NOT TO COMPLY WITH COMPONENT MAINT MANUAL IN 2 AREAS. CMM61-13-01.1ST: ALUMINUM POAug 26, 2000 · Dhav DHC71SDR 20000911SH017Hub · damagedRELEVANT ET INDICATION, 4TH THREAD UP. (X)Aug 23, 2000SDR EY2R57207Erosion Shield · crackedTHREE EROSION SHIELDS HAD CRACKS IN VARIOUS PLACES. REPLACED WITH NEW S/N C2082, C2071, C2075. (X)Aug 15, 2000 · Beech 1900DSDR EY2R57100AErosion Shield · crackedEROSION SHIELD HAD CRACKS IN VARIOUS AREAS ON BLADE NR 2. REPLACED WITH NEW S/N C2074. (X)Aug 3, 2000 · Beech 1900DSDR 20000907SH025Screw · failedBLADE PRELOAD ADJUSTMENT SCREW FAILED AT JAM NUT ALLOWING THE NUT TO FLOAT FREELY WITHIN THE HUB. PILOT REPORTED OCCASIONAL STICKING OF THE PROPELLER. THE CONDITION WAS CAUSED BY THE JAM NUT HANGING BETWEEN THE HUB AND THE BETA PICK-UP PLATE. THE RESULTING Aug 2, 2000 · N81WU · Beech 200BEECHSDR EY2R57093ANut · corrodedTHREADS ON BLADE RETENTION NUT CORRODED. REPLACED. (X)Aug 1, 2000 · Cessna 210SDR 20000816SH032Blade · crackedPROPELLER LEAKING RED DYE. TEAR-DOWN INSPECTION REVEALED BLADE CRACKED ALL THE WAY THROUGH INTO THE WEIGHT HOLE. DYE COMING FROM BLADE PATCH. CAUSE UNKNOWN. PROPELLER USED IN AG OPERATION. (X)Jul 31, 2000 · Cessna 188CESSNASDR 20000816SH030Blade · corrodedHUB (SN 6757N) AND BOTH BLADES (SN A2545 AND A3412) SCRAP DUE TO CORROSION. SUBMITTER STATED: CAUSE DUE TO NEGLECT OVER THE LAST 53 YEARS. (X)Jul 31, 2000SDR EY2R57007AErosion Shield · crackedEROSION SHIELD CRACKED IN VARIOUS PLACES ON THREE BLADES. REPLACED EROSION SHIELD ON THREE BLADES. REPLACEMENT S/N'S C2083, C2081, C1512Jul 27, 2000 · Beech 1900DSDR 20000731SH021Blade · scratchedTHE BLADE WAS REJECTED DUE TO SCRATCHES IN THREADS PER MCAULEY SB 150. (X)Jul 13, 2000 · N5466J · Cessna T310RSDR 20000731SH020Blade · scratchedTHE BLADE WAS REJECTED DUE TO SCRATCHES IN THREADS PER MCAULEY SB 150. (X)Jul 13, 2000 · N5466J · Cessna T310RSDR 20000731SH019Blade · scratchedTHE BLADE WAS REJECTED DUE TO SCRATCHES IN THREADS PER MCAULEY SB 150. (X)Jul 13, 2000 · N5466J · Cessna T310RSDR 20000731SH018Blade · scratchedTHE BLADE WAS REJECTED DUE TO SCRATCHES IN THREADS PER MCAULEY SB 150. (X)Jul 13, 2000 · N5466J · Cessna T310RSDR 20000731SH017Blade · scratchedTHE BLADE WAS REJECTED DUE TO SCRATCHES IN THREADS PER MCAULEY SB 150. (X)Jul 13, 2000 · N5466J · Cessna T310RSDR 20000731SH016Blade · scratchedTHE BLADE WAS REJECTED DUE TO SCRATCHES IN THREADS PER MCAULEY SB 150. (X)Jul 13, 2000 · N5466J · Cessna T310RSDR CA000808005Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.Jul 11, 2000 · Piper PA28140SDR CA000808006Propeller · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. REQUIRED OVERHAUL DUE TO CORROSION. (X)Jul 10, 2000 · Piper PA28140SDR EY2R56924AErosion Shield · crackedTHREE AREAS OF EROSION SHIELD ON THREE BLADES CRACKED ON BOTH FACE AND CAMBER SIDES. REPLACED ALL EROSION SHIELDS. S/N''S INSTALLED C1951, C1623, C1610, AND C2084.Jul 10, 2000 · Beech 1900DSDR CA000808004Propeller · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION; TRIMMED, ANODIZED, PAINTED. (X)Jul 7, 2000 · Piper PA28140SDR 20000821SH002Blade · crackedPROPELLER RECEIVED FOR REPAIR WITH CUSTOMER COMPLAINT OF EXCESSIVE BLADE TIP MOVEMENT. DISASSEMBLED PROPELLER AND FOUND THAT BLADE, S/N 1193, HAD A CRACK 360 DEGREES AROUND OUTER SLEEVE ON ROOT END. BLADE REJECTED FROM SERVICE. (X)Jun 27, 2000SDR EY2R49550CBlade · corrodedBLADES HAVE EXFOLIATION, SENT TO MANUFACTURER FOR EVALUATION. BLADE S/N''''S KF043, KF044, KF046 REMOVED FROM SERVICE.Jun 26, 2000 · Cessna 208SDR CA000714033Blade · failed(CAN) BLADES REPLACED NEW: 21 OCT 83 - PAGE 2 OF LOG. TSN: 3742.3. LAST COMPLETE OVERHAUL: 15 MAR 99 - PAGE 16 OF LOG. TSO: 6947.93. PROPELLER TIME SINCE NEW - EXCEPT FOR BLADES: 5459.4. GREASE SPLASH DETECTED ON A/C SIDE OF FUSELAGE AND ICE SHIELD. Jun 24, 2000 · Piper PA31SDR CA000712030Propeller · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. (X)Jun 22, 2000 · Cessna 172MSDR 20000714SH024Blade · crackedPROPELLER SUBMITTAL FOR AD 97-18-02 INITIAL INSPECTIONS. S/N A69152 (BLADE NR 1) FOUND CRACKED IN AREA OF A/O?????? USING EDDY CURRENT INSPECTION EQUIPMENT. NOTE: A/O??????WAS OVERDUE. SUBMITTER STATED SHOULD HAVE BEEN COMPLETED NO LONGER THAN SEPT, 1999. Jun 16, 2000 · N87K · Beech S35SDR CA000621025Blade · corroded(CAN) FOUND CORROSION ON THE BLADE THREADS DURING THE CORROSIION INSPECTION. BLADES REPLACED WITH USED SERVICEABLE. IN ACCORDANCE WITH MCCAULEY MANUAL 720415.Jun 13, 2000 · Beech 3533SDR EY2R56802Bearing · corrodedBLADE BEARING SURFACE CORRODED.Jun 13, 2000SDR CA000614047Propeller · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.Jun 8, 2000 · Piper PA38112SDR CA000606034Propeller · eroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.Jun 6, 2000 · Cessna 172MSDR EY2R56492Nut · crackedBLADE NUT CRACKED IN THREAD AREA. (X)Jun 5, 2000 · Cessna 185SDR EY2R56491BNut · crackedBLADE NUT CRACKED IN THREAD AREA. (X)Jun 5, 2000 · Cessna 185SDR EY2R56491ABlade · crackedTWO EACH BLADES CRACKED IN THREAD AREA. (X)Jun 5, 2000 · Cessna 185SDR CA000614041Blade · inaccurate(CAN) DIMENSIONAL CHECK, FOUND PROPELLER TO BE JUST UNDER MINIMUM ALLOWABLE THICKNESS AT THE 34.20 INCH STATION. PROPELLER RETIRED FROM SERVICE.Jun 2, 2000 · Beech C23SDR CA000606033Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. BLADES TRIMMED, ALODINED, PAINTED.May 31, 2000 · Cessna 182RSDR EY2R56151BPiston · corrodedPISTON CORROSION ON OUTSIDE DIAMETER BEYOND LIMITS.May 25, 2000 · Piper PA24250SDR EY2R56151Clamp · corrodedCLAMP ASSY'S CORRODED ON BOTH INNER AND OUTER SURFACE.May 25, 2000 · Piper PA24250SDR AU000405Blade · cracked(AUS) RT PROPELLER BLADE CRACKED FROM THE CENTRE LINE OF THE LEADING EDGE AND PROGRESSING ALONG THE LEADING EDGE TOWARDS THE TRAILINGEDGE.May 24, 2000 · Frchld SA227DCSDR CA000530033Propeller · corroded(CAN) CORROSION ON CAMBER AND FACE OF PROPELLER BLADE.May 17, 2000 · Cessna 172MSDR AU000383Blade · loose(AUS) PROPELLER BLADES LOOSE ON FERRULE ASSEMBLIES. LOW TORQUE.May 15, 2000 · Cessna 210LSDR EY2R56446AErosion Shield · debondedCRACKED AND DEBONDED FROM BLADE BENEATH DE-ICER BOOT. SEPARATED FROM BLADE AND REMAINED ATTACHED TO DE-ICER DURING REMOVAL OF DE-ICER.May 12, 2000 · Beech 1900DSDR EY2R56446Bearing · corrodedBLADE BEARING CORRODED.May 12, 2000 · Beech 1900DSDR EY2R56679Blade · brokenTIP OF NR 2 BLADE SNAPPED OFF 3.50 INCHES.May 10, 2000 · Cessna 172SDR CA000516032Blade · corroded(CAN) BLADES CORRODED FACE AND CAMBER.May 8, 2000SDR EY2R54036Fork · crackedFORWARD EARS OF PITCH CHANGE FOR CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. 2 EACH CRACKS.May 3, 2000 · Beech 200BEECHSDR EY2R811KBlade · crackedBLADE CRACKED IN SHANK AND THREAD AREA.Apr 28, 2000 · Beech A2324SDR CA000505016Blade Root · corroded****THIS SDR ATA NEEDS PROP MDL*****(CAN) BLADES RECEIVED FOR REWORK - SB81A. HEAVY CORROSION FOUND DURING LPI.Apr 27, 2000SDR CA000516031Propeller · corroded(CAN) NO TEXTApr 26, 2000 · Piper PA22150SDR AU000203Retainer · damaged(AUS) LEFT PROPELLER FEEDBACK RING RETAINING CIRCLIP DEFORMED. PROPELLER WENT TO UNCOMMANDED FULL REVERSE ON LANDING.Apr 20, 2000 · Reims F406SDR CA000427037Separator · mismanufactured(CAN) PROPELLER BALL SPACER REF. 61-10-00. FIG 1 ITEM 240 FOUND TO BE OF INSUFFICIENT LENGTH. RECEIVED WITH FAA 8130-3. ITEM SENT TO MAINTENANCE AND MANUFACTURING FOR UNAPPROVED PARTS FOLLOW-UP.Apr 18, 2000 · Dhav DHC8102SDR 20000515SH005Blade · crackedBLADE RECEIVED FROM CUSTOMER WITH A CRACK AROUND BLADE ROOT OUTER SLEEVE. BLADE REJECTED FROM FURTHER SERVICE. (X)Apr 17, 2000SDR MALA000257Blade · crackedAFTER REMOVAL OF PROP DUE TO GREASE LEAK WHILE INSPECTING MX FOUND 1 INCH BLADE ON LEFT PROP TO BE CRACKED .75 INCH AROUND THE BLADE ROOT OUTER SLEEVE. BLADE WILL BE SENT OUT FOR ANALYSIS AND DETERMINED CAUSE WITH ENGINEERING EVALUATION. PROP ASSY (P/N R389Apr 11, 2000 · N98XJ · Saab SF340A
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