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 99ZZZX1743Erosion Shield · debondedDE-ICE BOOT LIFTING, EROSION SHIELD DEBOND UNDER BOOT, NR 1 BLADE. REPAIRED EROSION SHIELD DEBOND AND INSTALLED DEICE BOOT ON NR 1 BLADE IAW HARTZELL CMM.Apr 8, 1999SDR 99ZZZX1741Erosion Shield · debondedNR 1 BLADE EROSION SHIELD DEBONDED UNDER BOOT BLADE. PRELOADS AND LOOSE. DISASSEMBLED AND CLEANED PROPELLER, REQUIRED DEBONDED EROSION SHIELD ON NR 1 BLADE AND INSTALLED NEW DEICE BOOT. SET PRELOADS ON ALL BLADES, RE-ASSEMBLED PROP, SET BLADE ANGLES AT 42 IApr 8, 1999SDR 99ZZZX1740Erosion Shield · debondedEROSION SHIELD DEBOND. DEBOND ON BLADE NR 2 UNDER DEICE BOOT. REPAIRED AND INSTALLED NEW DEICE BOOT IAW MFG CMM.Apr 8, 1999SDR 99ZZZX1577Blade · crackedCRACK IN ZONE 2B OUTER EDGE OF FILLET RADIUS ON PROPELLER.Apr 7, 1999 · Emb EMB120SDR 99ZZZX1576Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. 4 CRACKS.Apr 7, 1999 · Beech 1900DSDR 99ZZZX2140Erosion Shield · debondedBLADE EROSION SHIELD DEBONDED. FOUND DURING OVERHAUL. REPLACED EROSION SHIELD ON BLADE 11743.Apr 1, 1999SDR CA990330026Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. CAMBER AND LEADING EDGES OF PROPELLER BLADES REQUIRED OVERHAUL.Mar 30, 1999SDR 99ZZZX1533Bearing · crackedINNER BEARING BRACE CRACKED THREE-FOURTHS WAY AROUND ON PROPELLER BLADE.Mar 29, 1999 · Beech 1900DSDR 99ZZZX1532Bearing · crackedINNER BEARING RACE CRACKED ONE-HALF WAY AROUND ON PROPELLER BLADE.Mar 29, 1999 · Beech 1900DSDR CA990412013Blade · corroded(CAN) PAINT REMOVED FROM PROPELLER BLADES FOR INSPECTION. CORROSION WAS FOUND AND EXTRA WORK WAS REQUIRED TO REMOVE THE CORROSION PER HARTZELL MANUAL 133C.Mar 26, 1999 · Piper PA32300SDR CA990401007Blade · corroded(CAN) DURING OVERHAUL, CORROSION WAS FOUND ON THE PROPELLER BLADES SHANK AND IN THE BLADE TAPER BORES. THE BLADES WERE MACHINED TO THE OVERHAUL SPECIFICATIONS AND RETURNED TO SERVICE.Mar 18, 1999SDR CA990330016Bearing · failed(CAN) ON PROPELLER INSPECTION, ONE BLADE WAS NOTICEABLY LOOSE. THE NR 2 BLADE WAS REMOVED AND THE PROP BEARING OUTER RACE WAS FOUND BROKEN IN TWO PIECES. THE EDGE OF THE SAME RACE WAS CHIPPED AT APPROXIMATELY 180 DEGREES OPPOSITE THE BROKEN AREA. FURTHER INMar 16, 1999 · Dhav DHC8102SDR CA990318010Blade · corroded(CAN) INSPECTION FOUND CORROSION ON THE FACE SIDE OF THE PROPELLER BLADES. THE CORROSION WAS REMOVED WITH LIGHT GRINDING.Mar 11, 1999SDR CA990318046Blade · corroded(CAN) DEEP CORROSION ON PROPELLER THRUST FACE. EXTRA WORK WAS REQUIRED TO REMOVE CORROSION IAW SENSENICH MANUAL SPRM 590.Mar 8, 1999 · Piper PA20SDR 99ZZZX2074Sleeve · crackedOUTER AREA OF SLEEVE CRACKED.Mar 8, 1999SDR 99ZZZX2073Ferrel · crackedLOWER FERREL HAS CRACK.Mar 8, 1999SDR 99ZZZX1159Fork · wornPROPELLER S/N HL271 WAS RETURNED FOR VIBRATION AND COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020. INITIAL INSPECTION REVEALED BLADE S/N 984C TO BE OUT OF ANGLE TOLERANCE. AFTER DISASSEMBLY, INSPECTION REVEALED THE CAM FOLLOWER FORK SLOT OF THE D-5110-5 FORK,Mar 8, 1999 · Dorner DO328100SDR 99ZZZX1158Bracket · wornPROPELLER S/N HL271 WAS RETURNED FOR VIBRATION AND COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020. INITIAL INSPECTION REVEALED BLADE S/N 984C TO BE OUT OF ANGLE TOLERANCE. AFTER DISASSEMBLY, INSPECTION REVEALED WEAR ON THE CAM FOLLOWER SUPPORT AREA OF THE D-6Mar 8, 1999 · Dorner DO328100SDR 99ZZZX1157Fork · damagedPROPELLER S/N HL271 WAS RETURNED FOR COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020. AFTER DISASSEMBLY, INSPECTION REVEALED SCORING LINES THROUGH THE CHROME PLATING OF THE D-5630 PITCH CHANGE ROD AS INSTALLED IN THE D-5990-1 HYDRAULIC UNIT S/N S223. THE HYDRAMar 8, 1999 · Dorner DO328100SDR 99ZZZX1156Fork · wornINSPECTION REVEALED 4 PITCH CHANGE FORK SLOTS WORN BEYOND ALLOWABLE LIMITS. THE FORK WAS RETIRED FROM SERVICE.Mar 8, 1999 · Dorner DO328100SDR 99ZZZX1155Fork · wornDURING THE OVERHAUL PROCESS OF THE D-5110-5 FORK S/N S140, INSPECTION REVEALED THE CAM FOLLOWER FORK SLOTS WORN BEYOND ALLOWABLE LIMITS. THE FORK WAS RETIRED FROM SERVICE.Mar 8, 1999 · Dorner DO328100SDR 99ZZZX1154Cam Follower · wornPRPELLER S/N HL112 WAS RETURNED FOR COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020. AFTER DISASSEMBLY, INSPECTION REVEALED ONE EACH B-6077-1 CAM FOLLOWER INSIDE DIAMETER TO BE WORN BEYOND ALLOWABLE LIMITS. THE CAM FOLLOWER WAS RETURNED TO HARTZELL ENGINEERINGMar 8, 1999 · Dorner DO328100SDR 99ZZZX1153Fork · wornPROPELLER S/N HL112 WAS RETURNED FOR COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020. AFTER DISASSEMBLY, INSPECTION REVEALED PITCH CHANGE FORK S/N S9 WAS WORN, AT THE CAM FOLLOWER FORK SLOTS, BEYOND ALLOWABLE LIMITS. THE FORK WAS RETURNED TO HARTZELL ENGINEERINMar 8, 1999 · Dorner DO328100SDR 99ZZZX1152Cam Follower · wornDURING THE OVERHAUL PROCESS OF 6 EACH B-6077-2 CAM FOLLOWERS, INSPECTION REVEALED THE INSIDE DIAMETER TO BE WORN BEYOND ALLOWABLE LIMITS. THE CAM FOLLOWERS WERE RETIRED FROM SERVICE.Mar 8, 1999 · Dorner DO328100SDR 99ZZZX1151Spring · brokenAFTER DISASSEMBLY, INSPECTION REVEALED THE A-6404 SPRING BROKEN INTO 2 PIECES. THE SPRING WAS RETIRED FROM SERVICE.Mar 8, 1999 · Dorner DO328100SDR 99ZZZX1150Bracket · wornPROPELLER S/N HL112 WAS RETURNED FOR COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020. AFTER DISASSEMBLY, INSPECTION REVEALED PITCH CHANGE BRACKET S/N S164 TO BE WORN AT THE CAM FOLLOWER SUPPORT AREA BEYOND ALLOWABLE LIMITS. THE BRACKET WAS RETURNED TO HARTZELLMar 8, 1999 · Dorner DO328100SDR 99ZZZX1149Cam Follower · wornPROPELLER S/N HL271 RETURNED FOR VIBRATION AND COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020. INITIAL INSPECTION REVEALED BLADE S/N 984C TO BE OUT OF ANGLE TOLERANCE. AFTER DISASSEMBLY, INSPECTION REVEALED WEAR ON THE B-6077-2 CAM FOLLOWER INSIDE DIAMETER, AMar 8, 1999 · Dorner DO328100SDR CA990330033Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADES WERE FOUND WITH STONE DAMAGE. THE BLADES WERE TRIMMED.Mar 4, 1999 · Gulstm AA5SDR CA990318008Blade · corroded(CAN) DURING INSPECTION ,CORROSION WAS FOUND ON BOTH PROPELLER BLADES. THE CORROSION WAS REMOVED AND LPI INSPECTION FOUND NO FURTHER TRACES OF CORROSION.Mar 4, 1999 · Cessna 172NSDR 99ZZZX1179Erosion Shield · debondedEROSION SHIELD DEBONDED UNDER DE-ICE BOOT ON BLADE NR 1. REPAIRED DEBOND, .50 INCH BY 2 INCHES AND .50 INCH BY 1 INCH, AT BASE OF EROSION SHIELD. REPAIRED IAW MFG CMM.Mar 4, 1999SDR 99ZZZX1178Erosion Shield · debondedEROSION SHIELD DEBONDED UNDER DE-ICE BOOT ON BLADE NR 4. REPAIRED DEBOND AND INSTALLED NEW DE-ICE BOOT IAW MFG CMM.Mar 4, 1999SDR 99ZZZX1177Erosion Shield · debondedEROSION SHIELD ON NR 4 BLADE DEBONDED. REPAIRED EROSION SHIELD DEBOND IN BOOT AREA. REPLACED DE-ICE BOOT IAW MFG CMM.Mar 4, 1999SDR 99ZZZX1176Erosion Shield · debondedEROSION SHIELD DEBONDED ON BLADE NR 3. REPAIRED DEBOND, .50 INCH BY 3 INCHES, AT BASE OF EROSION SHIELD. REPAIRED IAW MFG CMM.Mar 4, 1999SDR 99ZZZX1175Erosion Shield · debondedEROSION SHIELD ON BLADE NR 1 DEBONDED. DISASSEMBLED AND CLEANED PROPELLER, INSTALLED NEW EROSION SHIELD, AND OVERHAULED BLADE NR 1.Mar 4, 1999SDR CA990318007Link · worn(CAN) PROPELLER WAS SENT FOR PROPELLER STRIKE INSPECTION/REPAIR. DURING INSPECTION,THE LINK ARMS AND THE BETA RING WERE FOUND WORN BEYOND LIMITS.Mar 3, 1999SDR 99ZZZX1130Bolts · failedFOUND DURING PHASE INSPECTION. COUNTERWEIGHT BOLTS FAILING DUE TO CORROSION. PROPELLER HAS 324 HOURS TSOH.Mar 3, 1999 · N24SX · Beech 200BEECHSDR 99ZZZX1097Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495 PITCH CHANGE FORK, SN 2359NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.Mar 1, 1999SDR 99ZZZX1096Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495 PITCH CHANGE FORK, SN 2198NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.Mar 1, 1999SDR 99ZZZX1095Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495 PITCH CHANGE FORK, SN 2178NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.Mar 1, 1999SDR 99ZZZX1094Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495 PITCH CHANGE FORK, SN 1104NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.Mar 1, 1999SDR 99ZZZX1093Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495 PITCH CHANGE FORK, SN 3365NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.Mar 1, 1999SDR 99ZZZX1092Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495 PITCH CHANGE FORK, SN 3399NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.Mar 1, 1999SDR 99ZZZX1091Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495 PITCH CHANGE FORK, SN 2139NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.Mar 1, 1999SDR 99ZZZX1090Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495 PITCH CHANGE FORK, SN 1657NR. THE FORK WAS SENT TO HARTZELL ENGINEERING.Mar 1, 1999SDR 99ZZZX1089Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495 PITCH CHANGE FORK, SN 2357NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.Mar 1, 1999SDR 99ZZZX1088Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495 PITCH CHANGE FORK, SN 3069NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.Mar 1, 1999SDR 99ZZZX1087Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495 PITCH CHANGE FORK, SN 3230NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.Mar 1, 1999SDR 99ZZZX1086Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495 PITCH CHANGE FORK, SN 2840NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.Mar 1, 1999SDR 99ZZZX1085Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495 PITCH CHANGE FORK, SN 3468NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.Mar 1, 1999SDR 99ZZZX1084Fork · crackedDURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH D-495 PITCH CHANGE FORK, SN 3228NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.Mar 1, 1999
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