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 DAT2005F00008Blade · crackedDURING THE SCHEDULED COMPLIANCE OF AD ON THE LT PROPELLER IT WAS FOUND 1 OF 6 PROPELLER BLADES WERE CRACKED. MECHANIC REMOVED AND REPLACED THE PROPELLER IAW MM. OPS CHECK GOOD. AC WAS RETURNED TO SERVICE. (K)Jun 30, 2005 · N263GA · Stbros SD360SDR CA050630005Blade · broken(CAN) AC WAS IN CRUISE AT 3500 FEET. PILOT HEARD A LOUD BANG, AC STARTED TO SHAKE VIOLENTLY. PILOT WAS ABLE TO MAINTAIN ALTITUDE AND TURNBACK. EMERGENCY CALL WAS MADE. ENGINE STARTED TO SURGE ON SHORT FINAL, OIL LIGHT CAME ON, ENGINE QUIT. MADE A SAFE LANDJun 9, 2005 · Gippld GA8SDR CA050602004Blade · unserviceable(CAN) PILOT REPORTED THAT THEY HAD NO INDICATION OR LOAD ON B-PHASE OF NR 2 PROPELLER DEICE SYSTEM. INSPECTION OF NR 2 PROPELLER FOUND THAT NR 4 BLADE HAD AN OPEN CIRCUIT IN HEATER MAT. BLADE REPLACED WITH SERVICEABLE GROUND RUNS CARRIED OUT AND FOUND SERVICEAMay 31, 2005 · Dhav DHC8102SDR CA050518016Blade · crackedDURING FLUORESCENT PENETRANT INSPECTION, FOUND THE FILLET RADIUS WITH CRACK INDICATIONS RADIALLY IN THREE PLACES ABOUT 1/8 INCH FROM THE OUTSIDE DIAMETER. THE LONGEST IS ABOUT 1/2 INCH LONG. THERE IS ALSO A CRACK INDICATION ON THE OUTSIDE DIAMETER ABOUT 1/8 May 18, 2005SDR 1050326Blade · crackedBLADE 1, S/NR H20755R WAS FOUND WITH A 1 INCH CRACK, STARTING FROM LEADING EDGE, ABOUT 4 INCHES FROM BLADE TIP. THE BLADE WAS ALREADY REWORKED AT THIS AREA BECAUSE OF A EARLIER STONE NICK. PROPELLER WAS OVERHAULED IN MARCH 2003 AND HAS 387 TSO UNTIL CRACK WAS Mar 30, 2005 · Socata TB20TRINIDADSDR CA050331002Blade · failed(CAN) EXCESSIVE LT/RT MOVEMENT ON ONE PROP BLADE DUE TO WORN BUSHINGS ON LINK BETWEEN BLADE AND PITCH CONTROL. LINK WAS REPLACED.Mar 28, 2005 · Cessna 425SDR CA050316004Blade · cracked(CAN) PROPELLER, W/O T 64571, RECEIVED FOR 10 YEAR OVERHAUL. LAST OVERHAUL MAY 1996. NOW 667.9 HOUR SINCE OVERHAUL. FOUND BLADE S-90AT-2, SN B34101YS, CRACKED IN BLADE THREADS, FOUND WITH EDDY CURRENT.Mar 14, 2005 · Cessna 180HSDR 2005FA0000501Blade · crackedPROPELLER RECEIVED FOR REPAIR OF BURNED OUT DE-ICER. PROP REQUIRED COMPLIANCE OF AD. PROP FAILED AD. PROP WAS DISASSEMBLED AND A CRACK WAS FOUND IN ROOT END OUTER SLEEVE OF NR 4 BLADE, SN 258. BLADE IS REJECTED FROM FURTHER SERVICE. (K)Jan 27, 2005SDR CA050113006Blade · broken(CAN) DURING TAKE OFF ROLL OUT, THE LT PROP STRUCK DEBRIS ON RUNWAY AND A 3 INCH PORTION OF THE TIP OF THE PROP BROKE OFF AND WENT THROUGH THE FUSELAGE JUST BEHIND AND BELOW THE AIRSTAIR DOOR. A 2 -3 INCH HOLE IN RT PROP SPINNER WAS ALSO DISCOVERED AT THE SAMJan 11, 2005 · Swrngn SA227ACSDR CA041222010Nut · cracked(CAN) RETENTION NUT THREAD CRACKED, 3 INCHES IN LENGTH, . DISCOVERED DURING OVERHAUL L.P.I. INSPECTION.Dec 17, 2004 · Cessna A185FSDR 2005FA0000036Pitch Rod · crackedMULTIPLE CRACKS WERE FOUND DURING MAGNAFLUX INSPECTION. BOTTOM AND TOP OF PITCH CHANGE YOKE. EXCESSIVE STRESS MIGHT HAVE BEEN THE CAUSE OF FAILURE.Dec 16, 2004SDR CA041115002Blade · brokenDETAILS EXTRACTED FROM MAJOR DEFECT REPORT: DAMAGE IN THE FORM OF SLASH TYPE CUTS TO THE DE-ICE BOOT WAS FOUND ON THE RIGHT PROPELLER, NR 3 BLADE, WHICH AS A RESULT REQUIRED THE PROPELLER BLADE TO BE REPLACED. DURING REPLACEMENT OF THE NR 3 BLADE SERIAL NUMBENov 12, 2004 · Dhav DHC8*SDR CA041110018Clamp · crackedPROPELLER RECEIVED FOR INSPECTION UNDER AD 88-24-15. DURING ROUTINE VISUAL INSPECTION OF THE BLADE CLAMP ASSEMBLES, A CRACKED WAS DETECTED IN ONE OF THE OUTBOARD CLAMP BOLT HOLES ON S/N EE1910. CLAMP HAS BEEN REMOVED FROM SERVICE AND REPLACED WITH AN OVERHAUNov 10, 2004 · Swrngn SA226TCSDR CA041019009Shaft Seal · seized(CAN) PROP SHAFT SEAL WAS FOUND LEAKING.DURING DISASSEMBLY THE SHAFT SEAL WAS FOUND WITH ABNORMAL WEAR AND DETERIATION IN THE SLOTS OF THE CARBON PORTION OF THE SEAL.THE SLOTS WERE WORN HEAVILY AND THE METAL TABS APPEARED TO BE JAMBED INTO THE SIDES OF THE SLOOct 4, 2004 · Swrngn SA227ACSDR CA040930006Pad · missing(CAN) AFTER FLIGHT, PILOT SAW ON RT PROPELLER, ONE PROP DE-ICE PAD MISSING ON ONE BLADE. AFTER INSPECTION OF THE DEFECT, WE SAW THE GLUE WAS NOT HARD. THE DE-ICE PAD WAS INSTALLED AT O/H SHOP WITH NEW KIND OF GLUE. WE REMOVED THE OLD GLUE AND REINSTALLED A NSep 24, 2004 · Cessna 402BSDR 2005FA0000081Blade · crackedPROPELLER BLADE CRACKED .33 OF DIAMETER AT RETENTION GROVE. (K)Sep 1, 2004SDR CA040901006Blade · corroded(CAN) BLADE RECEIVED FOR REPAIR OF FIBERGLASS DAMAGE ON THE OUTER SURFACE. DURING INITIAL INSPECTION, THE PLUG FOR THE BLADE TAPER BORE WAS REMOVED, FOUND THAT THE TAPER BORE WAS PRESSURIZED AS THE PLUG POPPED OUT WHEN RETAINING RING WAS REMOVED. FOUND CORRAug 31, 2004 · Dhav DHC8*SDR 2004FA0000726Blade · crackedBLADE CRACKED .7500 AROUND RETENTION AREA. PROP IS BEING USED ON S OR V MODEL.Aug 26, 2004SDR CA040624007Strip · separated(CAN) DEPARTING, AN UNUSUAL NOISE WAS DETECTED FROM THE NR 2 ENGINE. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. THE LEADING EDGE PROTECTION STRIP ON ONE BLADE WAS SEPARATED 6 INCHES AT THE OB END. MAINTENANCE REMOVED THE STRIPS FROM ALL 4 BLADES AND THE AIRJun 21, 2004 · Braero HS7482ASDR O05R200400122Blade · scratchedSCRATCH IN SHOT PEEN ON SHANK.Jun 17, 2004 · Cessna 425SDR O05R200400121Blade · scratchedSCRATCH IN SHOT PEEN ON SHANK.Jun 17, 2004 · Cessna 425SDR O05R200400120Blade · scratchedSCRATCH IN SHOT PEEN ON SHANK.Jun 17, 2004 · Cessna 425SDR O05R200400119Blade · scratchedSCRATCH IN SHOT PEEN ON SHANK.Jun 17, 2004 · Cessna 425SDR O05R2004117Blade · scratchedSCRATCH IN SHOTPEEN ON SHANK. AMMENDED SERIAL NO IN BOX 5 (D) BF024Jun 17, 2004 · Cessna 425SDR O05R200400118Blade · scratchedSCRATCH IN SHOTPEEN ON SHANK.Jun 17, 2004 · Cessna 425SDR O05R200400117Blade · scratchedPROPELLER BLADE HAS A SCRATCH IN SHOTPEEN ON SHANK.Jun 17, 2004 · Cessna 425SDR AUS20040408Seal · incorrect(AUS) LT PROPELLER NR 4 BLADE SEAL FAILED. INSPECTION OF THE REMOVED SEAL REVEALED THE SEAL TO BE A SEAL FOR A 14SF TYPE PROPELLER WITH A 14RF TYPE PROPELLER GLAND SPRING SUPPLIED. THE 14RF GLANDSPRING IS OF A SMALLER DIAMETER WHEN COMPARED TO THE 14SF GLAND May 16, 2004 · Dhav DHC8315SDR AUS20040407Seal · incorrect(AUS) LT PROPELLER NR 4 BLADE SEAL FAILED. INSPECTION OF THE REMOVED SEAL REVEALED THE SEAL TO BE A SEAL FOR A 14SF TYPE PROPELLER WITH A 14RF TYPE PROPELLER GLAND SPRING SUPPLIED. THE 14RF GLAND SPRING IS OF A SMALLER DIAMETER WHEN COMPARED TO THE 14SF GLANMay 12, 2004 · Dhav DHC8315SDR O05R200400114Blade · out of tolerance1 BLADE REJECTED FOR DIMENSIONS.Apr 5, 2004 · Beech 200BEECHSDR O05R200400113Blade · out of tolerance1 BLADE REJECTED FOR DIMENSIONS.Apr 5, 2004 · Beech 200BEECHSDR O05R200400112Blade · out of tolerance1 BLADE REJECTED FOR DIMENSIONS.Apr 5, 2004 · Beech 200BEECHSDR O05R200400110Blade · damaged1 BLADE REJECTED FOR DAMAGE IN SHOT PEEN AREA.Apr 5, 2004 · Beech 58SDR O05R200400107Blade · out of tolerance1 BLADE REJECTED FOR DIMENSIONS.Apr 5, 2004 · Swrngn SA226TSDR O05R200400106Blade · out of tolerance1 BLADE REJECTED FOR DIMENSIONS.Apr 5, 2004 · Swrngn SA226TSDR O05R200400105Blade · out of tolerance1 BLADE REJECTED FOR DIMENSIONS.Apr 5, 2004 · Swrngn SA226TSDR O05R200400104Blade · scratched1 BLADE REJECTED FOR SCRATCH IN SHOT PEEN.Apr 5, 2004 · Piper PA28R200SDR O05R200400101Blade · out of tolerance2 BLADES REJECTED FOR DIMENSIONS.Apr 5, 2004 · Piper PA34200SDR O05R200400100Blade · out of tolerance2 BLADES REJECTED FOR DIMENSIONS.Apr 5, 2004 · Piper PA34200SDR CA040407014Thrust Bearing · cracked(CAN) PROPELLER WAS REMOVED FROM AIRCRAFT DUE TO EXCESSIVE GREASE LEAKAGE AND BLADE END PLAY. UPON SPLITTING THE HUB IT WAS FOUND THAT 2 BLADE THRUST BEARINGS HAD CRACKED.Apr 1, 2004 · Beech 1900DSDR AUS20040221Latch · failed(AUS) PROPELLER EXPERIENCED UNCOMMANDED FEATHER FOLLOWING GROUND RUN. SUSPECT CAUSED BY FAILURE OF THE LOW PITCH STOP LATCH PINS.Mar 24, 2004 · Cessna 404CESSNASDR MALA040283Blade · damagedNR 4 LEFT PROP BLADE DAMAGED. MAINTENANCE INSPECTED AND STATED IT APPEARED THE BLADE STRUCK SOMETHING DURING THE TAXI IN FROM NR 3321. MX REPLACED LEFT PROP, LEFT PROP ASSY IAW MAL TC NR 6110-303, P/N OFF&ON R390/4-123-F/27, S/N OFF DAP1403, S/N ON DAP0099, Mar 21, 2004 · N452XJ · Saab 340BSDR AUS20040223Blade · corroded(AUS) PROPELLER BLADES CONTAINED SEVERE INTERGRANNULAR CORROSION.Mar 19, 2004 · Piper PA38112SDR AUS20040190Blade · corroded(AUS) PROPELLER BLADES CONTAINED SEVERE INTERGRANNULAR CORROSION.Mar 15, 2004 · Piper PA38112SDR AUS20040189Blade · corroded(AUS) PROPELLER BLADES CONTAINED SEVERE INTERGRANNULAR CORROSION.Mar 12, 2004 · Piper PA38112SDR AUS20040139Seal · unserviceable(AUS) RT PROPELLER NR 3 BLADE SEAL BADLY SPLIT AND SPRING DISTORTED. NR 1 AND NR 4 BLADE SEALS BROKEN WITH SIGNS OF DISTORTION. SEALS WERE FOUND TO HAVE INCORRECT SPRINGS FITTED. LT PROPELLER NR 2 AND NR 3 BLADE SEALS ALSO DAMAGED DUE TO FIT OF INCORRECT SPRIFeb 23, 2004 · Dhav DHC8315SDR CA040407013Bearing · cracked(CAN) PROPELLER WAS REMOVED FROM THE AIRCRAFT TO REPAIR DAMAGE TO THE ERROSION SHIELD INSTALLED ON NR 1 BLADE. UPON SPLITTING THE HUB 2 OB BLADE BEARINGS WERE FOUND TO BE CRACKED. ALL 4 BLADE BEARINGS HAVE BEEN REPLACED BY NEW D7745 BEARINGS IAW MM NR 143A ANFeb 21, 2004 · Beech 1900DSDR O05R200400010Blade · out of toleranceBLADES WERE FOUND TO BE UNDER MINIMUM DIAMETER AND MINIMUM THICKNESS AT STATION 34. BLADE SERIAL NUMBERS E19818R AND E19873R.Feb 13, 2004 · Piper PA34200SDR O05R200466978Blade · damagedBLADE REJECTED IAW MFG CONCESSION 102556/C/P.Jan 27, 2004 · N698FA · Frchld 22C7ASDR O05R200423591Blade · unserviceableBLADE REJECTED IAW MFG CONCESSION 102566/C/P.Jan 27, 2004 · N698FA · Frchld 22C7ASDR O05R200416973Blade · damagedBLADE REJECTED IAW MFG CONCESSION 102566/C/P.Jan 27, 2004 · N698FA · Frchld SA227CC
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