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.
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
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 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.SDR CA980504019Bearing · corroded(CAN) PROPELLER RECEIVED FOR FIVE YEAR CORROSION INSPECTION. INSPECTION FOUND NR 1 BLADE BEARING RACE CORRODED. BEARING RACE REPLACED.SDR 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.SDR 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.SDR CA980504012Bearing · galled(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADE BEARINGS WERE FOUND DAMAGED WITH PITTING AND GALLING. THE BEARINGS WERE REPLACED.SDR 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.SDR 98ZZZX1907Fork · crackedPROPELLER INSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. ONE CRACK.SDR 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 CSDR 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.SDR 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.SDR CA980421026Nut · cracked(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. BLADE RETAINING NUT WAS FOUND CRACKED. THE FAILURE OF THE RETAINING NUT COULD CAUSE BLADE SEPARATION.SDR 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 SERVICSDR 98ZZZX1904Fork · crackedPROPELLER INSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. TWO CRACKS.SDR CA980421022Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADES WERE FOUND WITH EXTENSIVE STONE/ROCK DAMAGE. THE BLADES WERE NOT REPAIRED.SDR 98ZZZX1905Fork · crackedPROPELLER INSPECTION FOUND FORWARD EARS OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FOUR CRACKS.SDR 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.SDR 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.SDR 98ZZZX1537Blade · crackedPROPELLER BLADE INSPECTION FOUND CRACK IN V-GROOVE ON SHANK.SDR 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.SDR 98ZZZX1536Blade · crackedPROPELLER BLADE INSPECTION FOUND CRACK IN V-GROOVE ON SHANK.SDR 98ZZZX1906Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FOUR CRACKS.SDR 98ZZZX1901Fork · crackedPROPELLER INSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FOUR CRACKS.SDR CA980403002Threads · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER BLADE FERRULES FOUND CORRODED IN THE THREADED AREA.SDR 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.SDR 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.SDR 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.SDR CA980330010Blade · cut(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. LEADING EDGES OF PROPELLER BLADES WERE FOUND SPRAY CUT. THE BLADES WERE TRIMMED.SDR 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.SDR 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,SDR 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.SDR 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 INSPECTIOSDR 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.SDR 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.SDR 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.SDR 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 SDR 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.SDR 99ZZZX2091Blade · crackedBLADE IS CRACKED AT TRAILING EDGE CAMBER SIDE RETENTION AREA.SDR 99ZZZX2089Blade · crackedBLADE IS CRACKED AT TRAILING EDGE RETENTION AREA.SDR 98ZZZX1535Blade · crackedPROPELLER BLADE INSPECTION FOUND CRACK IN V-GROOVE ON SHANK.SDR CA980311016Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER BLADES WERE REPAIRED IN THE FIELD AND FOUND TO BE BELOW MANUFACTURERS MINIMUM WIDTHS (LIMITS).SDR 98ZZZX1100Fork · crackedPROPELLER INSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. THREE CRACKS.SDR CA980302010Blade · corroded(CAN) PROPELLER BLADES BADLY CORRODED IN THE SHANK AREA.SDR CA980302008Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. BLADES NOT ANODIZED AT LAST OVERHAUL. CORROSION FOUND UNDER PAINT.SDR 98ZZZX3323Fork · crackedFOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. TWO CRACKS.SDR 99ZZZX2094Blade · crackedBLADE IS CRACKED AT RETENTION AREA TRAILING EDGE SIDE.SDR 99ZZZX2093Blade · crackedBLADE IS CRACKED AT RETENTION AREA TRAILING EDGE OF BLADE.SDR 99ZZZX2092Blade · crackedBLADE IS CRACKED AT RETENTION AREA TRAILING EDGE SIDE OF BLADE.SDR 99ZZZX2090Blade · crackedBLADE IS CRACKED AT TRAILING EDGE SIDE IN RETENTION AREA.SDR 99ZZZX2088Blade · crackedBLADE IS CRACKED AT TRAILING EDGE RETENTION AREA.SDR 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.
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