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 95ZZZX5995Blade Pin · brokenDISASSEMBLED PROPELLER, FOUND ONE BLADE PIN BROKEN. BROKEN PIN WAS FOUND TO HAVE BEEN GROUND SHORT ON STONE AND NOT MACHINED AS SB NR 99 SECTION C STATES. REMAINING TWO BLADE PINS WERE FOUND OVERTORQUED BY AT LEAST 5 POUNDS PER MANUAL 720415.SDR 96ZZZX59Counterweight · clamp brokeAIRCRAFT WAS ON TAKEOFF ROLL, NO INDICATION OF PROBLEM DURING RUN-UP OR INITIAL POWER APPLICATION DURING TAKEOFF. ABOUT 750 FEET DOWN THE RUNWAY, THE RT ENGINE'S RPM SURGED. THE PILOT THOUGHT MAYBE A CABLE BROKE. AS ACFT SLOWED DOWN, PILOT NOTICED THE RT SPSDR SIMA952771Prop Blde Sheath · missingDURING CLIMB-OUT AT 4,000, PILOT NOTICED AND ENGINE SURGE AND ASSOCIATED PROP VIBRATION FROM NR 2 ENGINE. UPON RETURNING TO DFW, MAINTENANCE FOUND THE RIGHT PROP NR 3 BLADE MISSING APPROXIMATELY 10 INCH SECTION OF THE EDGE SHEATH AND FOUND A .25 INCH DENT ON SDR C2XA95IA270Propeller Blade · crackedIAH - DURING AN A-CHECK INSPECTION, THE NR 1 PROPELLER, NR 4 BLADE WAS REMOVED AND REPLACED TO CORRECT A PROP DE-ICE DISCREPANCY. UPON REMOVAL OF THE HEATER SHEATH, A CRACK IN THE LEADING EDGE OF THE PROPELLER BLADE WAS DISCOVERED. THE BLADE WAS THEN ROUTED SDR 95ZZZX6084Blade · below widthINSPECTION FOUND BLADE WIDTH BELOW MINIMUM SPECIFICATIONS.SDR 95ZZZX6083Blade · below widthINSPECTION FOUND BLADE WIDTH BELOW MINIMUM SPECIFICATIONS.SDR 95ZZZX6082Blade · below widthINSPECTION FOUND BLADE WIDTH BELOW MINIMUM SPECIFICATIONS.SDR 95ZZZX6081Blade · below widthINSPECTION FOUND BLADE WIDTH BELOW MINIMUM SPECIFICATIONS.SDR 95ZZZX6080Blade · below widthINSPECTION FOUND BLADE WIDTH BELOW MINIMUM SPECIFICATIONS.SDR 95ZZZX6079Blade · below widthINSPECTION FOUND BLADE WIDTH BELOW MINIMUM SPECIFICATIONS.SDR 95ZZZX6078Blade · below widthINSPECTION FOUND BLADE WIDTH BELOW MINIMUM SPECIFICATIONS.SDR 95ZZZX6077Blade · below widthINSPECTION FOUND BLADE WIDTH BELOW MINIMUM SPECIFICATIONS.SDR 95ZZZX6076Blade · below widthINSPECTION FOUND BLADE WIDTH BELOW MINIMUM SPECIFICATIONS.SDR 95ZZZX6075Blade · below widthINSPECTION FOUND BLADE WIDTH BELOW MINIMUM SPECIFICATIONS.SDR 95ZZZX6458Blade · debondedFOUND LEADING EDGE OF COMPOSITE BLADE DEBONDED UNDER DEICE BOOT.SDR 95ZZZX6810Blade · crackedDURING OVERHAUL AND C/W THE REPETATIVE INSPECTIONS REQUIRED BY AD 68-19-04, BLADE WAS FOUND CRACKED IN THE BLADE SHANK. IN THE AREA DETAILED IN THE AD, THE CRACK WAS EXTREMELY TIGHT AND ALMOST IMPOSSIBLE TO DETECT WITH LIQUID PENETRANT INSPECTION, HOWEVER, THSDR 95ZZZX5708Clamp · crackedINSPECTION FOUND BLADE CLAMP BACK HALF CRACKED. SUSPECT POSSIBLE ENGINE VIBRATION.SDR 95ZZZX5606Blade · defectiveTRIANGULAR PIECE OF WOOD/COMPOSITE MATERIAL APPROXIMATELY .2187 INCH LONG BY .1250 INCH DEEP, SEPARATED FROM LEADING EDGE OF PROPELLER BLADE AT THE BEVELED JOINT BETWEEN THE WOOD/COMPOSITE AND THE METAL LEADING EDGE. DEFECT LOCATED APPROXIMATELY 15.8750 INCHESDR 95ZZZX5531Clamp · crackedPROPELLER INSPECTION REVEALED BLADE CLAMP CRACKED.SDR 95ZZZX5257Blade Clamp · crackedBLADE CLAMP IS CRACKED WHERE THE HOLE IS DRILLED FOR COUNTERWEIGHT DOWEL PIN.SDR 95ZZZX6159Blade · failedAFTER TAKEOFF AND CLIMB TO 8,500 FEET ALTITUDE, LEVELED OFF IN NORMAL CRUISE FLIGHT. I.A.S. 220 MPH. WTH NO PRIOR WARNING, SEVERE VIBRATION OCCURRED. SHUT DOWN ENGINE AND DECLARED EMERGENCY AND MADE A SUCCESSFUL FORCED LANDING. GROUND INSPECTION DISCLOSED SDR 95ZZZX5113Blade · crackedINSPECTION FOUND CRACKED BLADE SHANK.SDR 95ZZZX5112Blade · crackedINSPECTION FOUND CRACKED BLADE SHANK.SDR 95ZZZX5109Blade · crackedINSPECTION FOUND CRACKED BLADE SHANK.SDR 95ZZZX5161Blade · crackedRIGHT PROPELLER BLADE, SN 518MA, DE-ICE BOOT PARTIALLY MISSING AND LEADING EDGE CRACKED IN AREA OF BOOT OPERATION. REMOVED AND REPLACED PROPELLER WITH ZERO TIME OVERHAULED UNIT. (CRACK NOTED WAS IN LEADING EDGE ABRASION STRIP. THIS IS SECOND FAILURE OF THISSDR 95ZZZX5758Blade · crackedUPON INSPECTION, BLADE WAS FOUND CRACKED IN THREADS. BLADE HAS BEEN SCRAPPED.SDR C2XA95IA216Blade · failedIAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE RIGHT PROPELLER NR 4 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)SDR C2XA95IA218Blade · failedIAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE LEFT PROPELLER NR 2 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)SDR C2XA95IA217Blade · failedIAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE LT PROPELLER NR 3 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (X)SDR C2XA95IA215Blade · failedIAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE RT PROPELLER NR 2 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)SDR C2XA95IA214Blade · failedIAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE RT PROPELLER NR 1 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)SDR C2XA95IA213Blade · failedIAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE LT PROPELLER NR 3 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)SDR C2XA95IA212Blade · failedIAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE RIGHT PROPELLER NR 3 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)SDR C2XA95IA211Blade · failedIAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE RIGHT PROPELLER NR 2 BLADE FAILED THE SHEAR WAVE ULTRASONIC INSPECTION. THE PROPELLER BLADE WAS REMOVED AND REPLACED, AND THE AIRCRAFT WAS APPROVED FRO RETURN TO SERVICE. (X)SDR 95ZZZX4497Blade · broke3.50 INCHES BROKE OFF NR 2 BLADE WHILE IN CRUISE FLIGHT. SUBMITTER STATED UNABLE TO DETERMINE CAUSE, NO VISIBLE NICKS. FRACTURE APPEARED TO BE INSTANTANEOUS ACROSS THE FULL CHORD. NO ACCIDENT.SDR CA970902016Blades · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. CORROSION WAS FOUND ON THE PROPELLER BLADES AND THE CYLINDER WAS FOUND TO BE OVERSIZE.SDR HEEA955430Blade · tip damageDAMAGE TO ONE BLADE TIP. TSO DUE 9-97.SDR 95ZZZX3734Blade · crackedDEFECT IS IN THE DOUBLE SHOULDER OF THE 3 BLADES WHERE IT IS RETAINED BY THE CLAMP.SDR 95ZZZX3733Blade · crackedDEFECT IS IN THE DOUBLE SHOULDER OF THE 3 BLADES WHERE IT IS RETAINED BY THE CLAMP.SDR 95ZZZX3732Blade · crackedDEFECT IS IN THE DOUBLE SHOULDER OF THE 3 BLADES WHERE IT IS RETAINED BY THE CLAMP.SDR 95ZZZX3573Snap Ring · looseA NEW PROP WAS INSTALLED 8-15-94 AFTER ENGINE OVERHAUL AND A REPAIR TO AIRFRAME. PROP REPORTED VIBRATING BY PILOTS. RPM HAD TO BE ABOVE 2500 TO LESSEN VIBRATION. ON 10-12-94, A SNAP RING AND SHIMS WERE FOUND LOOSE ON NR 2 BLADE AND BLADE WAS LOOSE IN HUB. SDR 95ZZZX3964Le Sheath · separatedJAN - FLT 4596 - RIGHT ENGINE TO FLUX 7 PERCENT DURING CLIMB FOLLOWED BY MINOR VIBS. CREW SELECTED TORQUE-MOTOR-LOCKOUT, BUT DID NOT CURE PROBLEM. CREW SHUT DOWN RIGHT ENGINE AND SAFELY RETURNED TO JACKSON. INSPECTION REVEALED THE RIGHT NR 3 PROPELLER BLADESDR 95ZZZX3638Blade · tip brokenAPPROXIMATELY 6 INCHES OF PROPELLER BLADE TIP SEPARATED FROM PROPELLER DURING FLIGHT. AIRCRAFT EXECUTED AN EMERGENCY LANDING. NO DAMAGE TO AIRCRAFT. A REVIEW OF AIRCRAFT MAINTENANCE RECORDS SHOWS HISTORY OF SUDDEN PROPELLER STOPPAGE.SDR 95ZZZM466Blade · nickedGRI - ON WALK AROUND, THE PILOT FOUND A NICK ON ONE BLADE OF RT PROP. MAINTENANCE DETERMINED THAT THE NICK WAS OUT OF LIMITS AND CHANGED THE PROPELLER.SDR RAIA950622Propeller · out of adjustSTL - FLT 7071 - RT ENGINE DID NOT MAKE TORQUE. MAINTENANCE ADJUSTED RT PROPELLER BLADE ANGLE. GROUND RUNS GOOD. (X)SDR 95ZZZX4283Blade Shank · crackedTHE SUBJECT BLADE WAS RECEIVED FOR A TORN DE-ICE BOOT. DURING DYE CHECK OF THE BLADE SHANK, TWO CRACKS WERE FOUND; ONE IN THE FILLET, AND ONE ON THE BUTT OUTSIDE DIAMETER. BOTH CRACKS WERE LOCATED ADJACENT TO THE COLLAR PARTING LINE ON THE FACE SIDE, AND WERSDR 95ZZZM108Sleeve · wornPROP ASSEMBLY REMOVED FOR A REPORTED VIBRATION. FURTHER INSPECTION REVEALED MOVEMENT WAS NOTED OUTBOARD OF THE COUNTER WEIGHT ASSEMBLY ON ALL FOUR BLADES. THIS MOVEMENT WAS DEEMED UNSERVICEABLE PER DOWTY CM 61-10-36 CHECK SECTION PG 501-506. ASSEMBLY WAS DISDR 95ZZZX3969Prop Blade · separatedMIA - FLT 5725 - CREW REPORTS LEFT ENGINE VIBRATION IN-FLIGHT, SHUT ENGINE DOWN IN-FLIGHT. FOUND BLADE SHEATH SEPARATED FROM LEFT PROPELLER BLADE. REPLACED PROPELLER BLADE.SDR 95ZZZX4295Snap Ring · corrodedUPON INSPECTION, THE STEEL SNAP RING AT THE BASE OF THE BLADES WAS FOUND SEVERELY CORRODED. THIS CONDITION INCLUDED THE BLADES NEXT TO THE SNAP RINGS AS THE PAINT ON BLADES WAS LOOSE AND WHITE POWDER WAS FOUND UNDER THE PEELED PAINT. THIS PROP WAS NEW AND HASDR 95ZZZX3035Blade · undersizeUPON FINDING BLADES, MODEL NR T10173B-8R, S/NS C84204, C84280, C84314, C21475, C34127, AND C34121, DIMENSIONALLY UNDER WIDTH WISE, CUSTOMER REPORTED PROPS HAVING APPROXIMATELY 200 HOURS SINCE OVERHAUL. PROPELLERS WERE OVERHAULED LAST IN MEXICO.
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