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 CA980507009Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE FOUND ON LEADING EDGES OF THE PROPELLER BLADES. DAMAGE WAS NOT REPAIRED PER HARTZELL SERVICE INSTRUCTIONS.Apr 30, 1998 · Piper PA44180SDR CA980504019Bearing · corroded(CAN) PROPELLER RECEIVED FOR FIVE YEAR CORROSION INSPECTION. INSPECTION FOUND NR 1 BLADE BEARING RACE CORRODED. BEARING RACE REPLACED.Apr 29, 1998 · Cessna 337GSDR CA980504011Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. BOTH PROPELLER BLADES WERE FOUND BADLY NICKED FROM FOD. FIELD REPAIRS WERE NOT MADE IN ACCORDANCE WITH THE HARTZELL MANUAL.Apr 27, 1998 · Conaer LA4200SDR AU980470Blade · cracked(AUS) PROPELLER HAD SPLITS DEVELOPING AFT OF THE METAL LEADING EDGE AND BETWEEN LAMINATION MIDWAY ALONG THE CENTER OF BLADE. FINE CRACKS WERE ALSO FOUND IN THE LEADING METAL SHEATH AT RADIUS OF STRESS RELIEVING POINTS.Apr 25, 1998 · Waco YMFSDR CA980504012Bearing · galled(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADE BEARINGS WERE FOUND DAMAGED WITH PITTING AND GALLING. THE BEARINGS WERE REPLACED.Apr 24, 1998SDR CA980504013Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADES AND FERRULES (P/N 3054) WERE FOUND CORRODED. THE PROPELLER BLADES WERE TRIMMED AND THE FERRULES WERE REPLACED.Apr 23, 1998 · Cessna 180HSDR 98ZZZX1907Fork · crackedPROPELLER INSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. ONE CRACK.Apr 22, 1998 · Beech 1900DSDR CA980504010Bearing · pitted(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADE BEARING RACE WAS FOUND PITTED IN THE RETENTION AREA. SMALL SURFACE CRACKS FROM THE PITTED AREA REQUIRED GRINDING OF BOTH RINGS TO MINIMUM, IF THE CRACKS WERE LEFT THEY WOULD PROGRESS TO CApr 21, 1998 · Cndair CL2151A10SDR CA980430025Blade · corroded(CAN) DURING OVERHAUL, THE PROPELLER CAMBER FACE IS RESURFACED BY GRINDING. DURING THE GRINDING PROCESS CORROSION WAS FOUND.. THERE WAS EXTRA GRINDING REQUIRED TO REMOVE THE CORROSION. THE PROPELLER CONTINUED IN SERVICE.Apr 21, 1998 · Cessna 172NSDR 98ZZZX1903Fork · crackedPROPELLER INSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. THREE CRACKS. TOTAL TIME ON PROPELLER ASSEMBLY IS 9,249.9 HOURS.Apr 21, 1998 · Beech 1900DSDR CA980421026Nut · cracked(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. BLADE RETAINING NUT WAS FOUND CRACKED. THE FAILURE OF THE RETAINING NUT COULD CAUSE BLADE SEPARATION.Apr 16, 1998 · Cessna 180BSDR CA980421025Blade · corroded(CAN) PROPELLER RECEIVED FOR FIVE YEAR CORROSION INSPECTION. PAINT REMOVED FROM THE PROPELLER AND A LARGE AMOUNT OF CORROSION WAS FOUND ON THE THRUST FACE OF THE PROPELLER. EXTRA WORK WAS REQUIRED TO REMOVETHE CORROSION. THE PROPELLER WAS RETURNED TO SERVICApr 15, 1998 · Beech C23SDR 98ZZZX1904Fork · crackedPROPELLER INSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. TWO CRACKS.Apr 15, 1998 · Beech 1900DSDR CA980421022Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADES WERE FOUND WITH EXTENSIVE STONE/ROCK DAMAGE. THE BLADES WERE NOT REPAIRED.Apr 14, 1998 · Mooney M20JSDR 98ZZZX1905Fork · crackedPROPELLER INSPECTION FOUND FORWARD EARS OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FOUR CRACKS.Apr 14, 1998 · Beech 1900DSDR CA980421021Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE AND CORROSION WAS FOUND ON THE LEADING EDGE AND THE FACE OF THE PROPELLER BLADES.Apr 13, 1998 · Cessna 172MSDR CA980421017Blade · debonded(CAN) ON INSPECTION, NR 3 AND NR 4 (P/N SFA13G1OA) PROPELLER BLADES WERE FOUND DEBONDED AT THE TIP AREA OF THE FACE OF THE BLADES. THE DEBONDING WAS APPROXIMATELY 2 INCHES IN LENGTH, RUNNING TO TIP CENTER OF BLADE FACE.Apr 9, 1998 · Dhav DHC8102SDR 98ZZZX1537Blade · crackedPROPELLER BLADE INSPECTION FOUND CRACK IN V-GROOVE ON SHANK.Apr 9, 1998 · Gulstm 500BSDR CA980421014Blade · cracked(CAN) DURING WALK-AROUND, THE NR 3 BLADE OF THE LEFT HAND PROPELLER WAS FOUND CRACKED ON THE FACE OF THE NICKEL SHEATH. THE CRACK WAS LOCATED 4.8750 INCHES FROM THE EDGE OF THE DE-ICER BOOT. THE BLADE WAS REPLACED.Apr 8, 1998 · Dhav DHC8102SDR 98ZZZX1536Blade · crackedPROPELLER BLADE INSPECTION FOUND CRACK IN V-GROOVE ON SHANK.Apr 8, 1998 · Gulstm 500BSDR 98ZZZX1906Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FOUR CRACKS.Mar 31, 1998 · Beech 1900DSDR 98ZZZX1901Fork · crackedPROPELLER INSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FOUR CRACKS.Mar 31, 1998 · Beech 1900DSDR CA980403002Threads · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER BLADE FERRULES FOUND CORRODED IN THE THREADED AREA.Mar 27, 1998 · Cessna 185ASDR CA980331007Ferrule · misdrilled(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. INSPECTION FOUND THE PROPELLER BLADE FERRULE HAD FIVE LINK PIN HOLES DRILLED. THE MAXIMUM PERMITTED IS FOUR.Mar 27, 1998 · Cessna 180SDR CA980331008Retaining Nut · cracked(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. TWO PROPELLER BLADES RETAINING NUTS WERE FOUND CRACKED. THIS COULD HAVE CAUSED A LOSS OF TWO PROPELLER BLADES IN THE EVENT OF TOTAL NUT FAILURES.Mar 25, 1998 · Cessna 180SDR 98ZZZX1487Blade · separatedAPPROXIMATELY 40 INCHES OF PROPELLER SEPARATED. DEFINITE 'SHADOW' OF DIFFERENT COLOR IN METAL IN CROSS-SECTION OF CHORD. 'SHADOW' OCCUPIED ONE-THIRD OF CROSS-SECTION. NO APPARENT CAUSE FOR FACTURE.Mar 23, 1998 · N9244B · Amtr WAGAROSDR CA980330010Blade · cut(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. LEADING EDGES OF PROPELLER BLADES WERE FOUND SPRAY CUT. THE BLADES WERE TRIMMED.Mar 18, 1998 · Dhav DHC2MK1SDR 98ZZZX1308Blade · crackedPROPELLER DISASSEMLBED, CLEANED, AND INSPECTED FOR AD COMPLIANCE. AD 97-18-02. BLADE SN E43779 CRACKED IN RETENTION AREA. FOUND WITH EDDY CURRENT. PERIODIC INSPECTION SHOULD ALWAYS BE DONE. EDDY CURRENT INSPECTION SHOULD BE DONE AT 1,000 HOUR INTERVALS.Mar 13, 1998SDR 98ZZZX1307Blade · crackedPROPELLER DISASSEMBLED, CLEANED, AND INSPECTED FOR AD COMPLIANCE AD 97-18-02. BLADE SN A21004 CRACKED IN RETENTION AREA. FOUND WITH EDDY CURRENT. CORROSION ALSO FOUND. PERIODIC INSPECTION SHOULD ALWAYS BE DONE. EDDY CURRENT INSPECTION SHOULD BE DONE AT 1,Mar 13, 1998SDR 98ZZZX1306Blade · crackedPROPELLER DISASSEMBLED, CLEANED, AND INSPECTED FOR AD COMPLIANCE AD 97-18-02. BLADE SN E43821 CRACKED IN RETENTION AREA. FOUND WITH EDDY CURRENT. PERIODIC INSPECTION SHOULD ALWAYS BE DONE. EDDY CURRENT INSPECTION SHOULD BE DONE AT 1,000 HOURS.Mar 13, 1998SDR 98ZZZX1305Blade · crackedPROPELLER DISASSEMBLED, CLEANED, AND INSPECTED FOR AD COMPLIANCE. AD 97-18-02, BLADE SN E43786 CRACKED IN RETENTION AREA. FOUND WITH EDDY CURRENT. CORROSION ALSO FOUND IN SHOT-PEENED AREA. PERIODIC INSPECTIONS SHOULD ALWAYS BE DONE. EDDY CURRENT INSPECTIOMar 13, 1998SDR 98ZZZX1304Blade · crackedPROPELLER DISASSEMBLED, CLEANED, AND INSPECTED FOR AD COMPLIANCE, AD 97-18-02. BLADE SN E43823 CRACKED IN RETENTION AREA. FOUND WITH EDDY CURRENT. PERIODIC INSPECTIONS SHOULD ALWAYS BE DONE. EDDY CURRENT INSPECTION SHOULD BE DONE AT 1,000-HOUR INTERVALS.Mar 13, 1998SDR 98ZZZX1303Blade · crackedPROPELLER DISASSEMBLED, CLEANED, INSPECTED FOR AD COMPLIANCE. AD 97-18-02. BLADE SN E43841, CRACKED IN RETENTION AREA. FOUND WITH EDDY CURRENT, PERIODIC INSPECTION SHOULD ALWAYS BE DONE. EDDY CURRENT INSPECTION SHOULD BE DONE AT 1,000 HOUR INTERVALS.Mar 13, 1998SDR CA980318044Roller · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE BARREL WAS FOUND CORRODED. THE BRACKET BENT AND THE ROLLER BEARINGS WERE FOUND PITTED. THE BARREL AND ROLLERS WERE REPLACED AND THE BRACKET WAS STRAIGHTENED.Mar 11, 1998SDR SABA980017Prop Blade · looseCLT - FLT 5172 - ON FLIGHT FROM CLT TO NTS, AIRCREW REPORTED A SEVERE VIBRATION AFTER TAKEOFF. AIRCRAFT RETURNED TO CLT. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. MAINTENANCE FOUND ONE OF THE BLADES, IN THE RIGHT PROP, HAD SLIPPED Mar 11, 1998 · N928AE · Bag JETSTM3201SDR LR7A9805Blade · leakingNR 2 PROP LOW OIL LIGHT FOLLOWED BY FLUX. SHUTDOWN IAW AFM. INSPECTED AND FOUND NR 2 BLADE LEAKING. PROP REMOVED FOR DETAILED INSPECTION BY VENDOR.Mar 10, 1998 · N403LC · Lkheed 382GSDR 99ZZZX2091Blade · crackedBLADE IS CRACKED AT TRAILING EDGE CAMBER SIDE RETENTION AREA.Mar 10, 1998SDR 99ZZZX2089Blade · crackedBLADE IS CRACKED AT TRAILING EDGE RETENTION AREA.Mar 10, 1998SDR 98ZZZX1535Blade · crackedPROPELLER BLADE INSPECTION FOUND CRACK IN V-GROOVE ON SHANK.Mar 5, 1998 · Gulstm 500BSDR CA980311016Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER BLADES WERE REPAIRED IN THE FIELD AND FOUND TO BE BELOW MANUFACTURERS MINIMUM WIDTHS (LIMITS).Mar 3, 1998 · Cessna 337GSDR 98ZZZX1100Fork · crackedPROPELLER INSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. THREE CRACKS.Feb 27, 1998 · Beech 1900DSDR CA980302010Blade · corroded(CAN) PROPELLER BLADES BADLY CORRODED IN THE SHANK AREA.Feb 20, 1998 · Piper PA31SDR CA980302008Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. BLADES NOT ANODIZED AT LAST OVERHAUL. CORROSION FOUND UNDER PAINT.Feb 20, 1998 · Cessna 152SDR 98ZZZX3323Fork · crackedFOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. TWO CRACKS.Feb 17, 1998 · Beech 1900DSDR 99ZZZX2094Blade · crackedBLADE IS CRACKED AT RETENTION AREA TRAILING EDGE SIDE.Feb 12, 1998SDR 99ZZZX2093Blade · crackedBLADE IS CRACKED AT RETENTION AREA TRAILING EDGE OF BLADE.Feb 12, 1998SDR 99ZZZX2092Blade · crackedBLADE IS CRACKED AT RETENTION AREA TRAILING EDGE SIDE OF BLADE.Feb 12, 1998SDR 99ZZZX2090Blade · crackedBLADE IS CRACKED AT TRAILING EDGE SIDE IN RETENTION AREA.Feb 12, 1998SDR 99ZZZX2088Blade · crackedBLADE IS CRACKED AT TRAILING EDGE RETENTION AREA.Feb 12, 1998SDR CA980309002Blade · delaminated(CAN) DURING 100 HOUR INSPECTION AND IN COMPLIANCE WITH MT PROPELLER AD 94-098, ONE BLADE SHEATH WAS FOUND DELAMINATED APPROXIMATELY 2 AT THE TIP OF THE BLADE FACE SIDE AND APPROXIMATELY 1 ON RHE BACKSIDE. THE PROPELLER WAS REMOVED FROM SERVICE AS PER THE AD.Feb 10, 1998 · Moravn Z242L
Back to JASC 6111