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 2007FA0000235Blade · misrepaired(REF NR 38430A) 2 OF 3 PROPELLER BLADES WERE PREVIOUSLY REPAIRED USING AN UNAPPROVED WELD METHOD IN SEVERAL LOCATIONS ON THE BLADE AIRFOIL. THE BLADES HAVE BEEN SCRAPED PENDING DISPOSITION INSTRUCTIONS FROM MFG. THE CUSTOMER HAS BEEN CONTACTED FOR HISTORICAMar 17, 2007SDR 2007FA0000234Blade · misrepaired(REF NR: 38430A) 2 OF 3 PROPELLER BLADES WERE PREVIOUSLY REPAIRED USING AN UNAPPROVED WELD METHOD IN SEVERAL LOCATIONS ON THE BLADE AIRFOIL. THE BLADES HAVE BEEN SCRAPED PENDING DISPOSITION INSTRUCTIONS FROM MFG. THE CUSTOMER HAS BEEN CONTACTED FOR HISTORICAMar 17, 2007SDR CA070322009Tape · damaged(CAN) DURING VISUAL INSPECTION, IT WAS FOUND THAT THE TAPE USED ON THE LEADING EDGE OF THIS PROP WHICH WAS INSTALLED BY THE MFG, UNDER SPEC SP-127, WAS STARTING TO BLISTER AND SEPARATE FROM THE LEADING EDGE, WORSE AT THE TIPS. TAPE WAS REMOVED AND LOG ENTRIES Mar 14, 2007SDR CA070528006Blade · cracked(CAN) PROPELLER RECEIVED FOR OVERHAUL AT 10 YEARS CALENDAR TIME, AT THAT TIME THE PROPELLER HAD BEEN INSPECTED PER AIRWORTHINESS MANUAL PART VI APPENDIX C (4). THE LAST OVERHAUL COMPLETED WAS OCTOBER 1991. FOUND BOTH BLADE THREADS CRACKED. FAA AD 91-15-04 APMar 1, 2007 · Cessna A185ESDR CA070227008Blade · leaking(CAN) EXCESSIVE GREASE WAS NOTED LEAKING FROM PROPELLER BLADE ROOT ON ALL (4) BLADES. PROPELLER REMOVED AND SENT FOR REPAIR. (TC NR 20070227008)Feb 23, 2007 · Pilats PC1245SDR 2007FA0000260Propeller · brokenOWNER REPORTED 5 MINUTES AFTER TAKEOFF AT 2500 ASL, ALL 3 PROPELLER BLADES DEPARTED. THERE WAS ONE VIOLENT SHAKE AND THEN SMOOTH GLIDING TO SAFE LANDING OFF AIRPORT. PRELIMINARY EXAM INDICATES ENGINE MOVED ENOUGH TO CAUSE CARBURETOR TO SEPARATE PREVENTING OVFeb 19, 2007 · N880BW · Amtr KITFOX41200SDR R021692Bearing · brokenON 12/14/06 REPORTED AIRCRAFT VIBRATIONS FROM STBD ENGINE. INSPECTION OF PROPELLER ON GROUND REVEALED EXCESSIVE RADIAL PLAY OUT OF LIMIT OF NR 3 BLADE. PROPELLER REMOVED FROM AIRCRAFT FOR FURTHER INVESTIGATION. SERVICE CENTER NOTES: BLADE NR 3 CAM FOLLOWER BRJan 17, 2007 · Beech 1900DSDR 2007F00006Clamp · crackedCRACK WAS FOUNDING STARTING AT THE DOWL PIN HOLE OF THE BLADE CUFF.Dec 26, 2006 · N21JA · Mtsbsi MU2B35SDR CA061218014Seal · leaking(CAN) BLADE GREASE SEAL FAILED. GREASE LEAVING HUB. PROP REMOVED AND SENT TO REPAIR FACILITY WHERE NEW SEALS WERE INSTALLED. PROP REINSTALLED AND A/C SERVICEABLE (TC NR 20061218014).Dec 18, 2006 · Cessna TU206GSDR CA061211005Bearing Race · fractured(CAN) LIGHT TO MODERATE PROP VIBRATION IN CRUISE, AS POWER WAS REDUCED FOR DESCENT VIBRATION BECAME EXCESSIVE. AS A RESULT THE NR 1 PROP (CONDITION LEVER) WAS SELECTED TO START FEATHER (VIBRATION STOP) AND THEN NR 1 ENGINE WAS SHUTDOWN. ALL ENGINE PARAMETERSDec 7, 2006 · Dhav DHC8301SDR CA061120008Spacer · torn(CAN) PROPELLER BLADE INSPECTED AND FOUND TIGHT IN HUB. INVESTIGATION REVEALED PROP BLADE SPACER HAD FAILED. PROP BLADE REMOVED AND NEW SPACER INSTALLED. PROP BLADE REINSTALLED AND GROUND RUN CHECKED SERVICEABLE.Nov 17, 2006 · Aerosp ATR42300SDR CA061106012Seal · incorrect(CAN) PROPELLER WAS FACTORY ASSEMBLE WITH INCORRECT BLADE SEALS ON ALL 3 BLADES. P/N 1633-56 SHOULD HAVE BEEN INSTALL BUT SEALS FOR A NON-OIL FILLED HUB WERE FOUND INSTALLED INSTEAD. THIS WAS A WARRANTY REPAIR.Oct 13, 2006SDR CA071207001Blade · unserviceable(CAN) DURING INSPECTION IAW AD 81-13-06R2 AND S/B 664, A CRACK WAS FOUND EMINATING FROM THE BLADE BUSHING SCREW HOLE. CRACK WAS FOUND TO BE TOO LARGE TO BE REMOVED. BLADE WAS RENDERED UNSERVICEABLE. BLADE S/N 852006. (TC NR 20071207001)Oct 5, 2006 · Cndair CL2151A10SDR CA060928005Blade · damaged(CAN) PROPELLER RECEIVED FOR O/H. UPON DISMANTLING DISCOLORATION ON THE BLADE SHANKS WAS NOTED. SHANKS WERE LIGHTLY MEDIA BLASTED AND THE DAMAGE IS MORE SEVERE THAN AT FIRST INSPECTION. BLADE SHANK RADIUS IS AT 4.194 INCHES MINIMUM FOR REPAIR IS 4.187 INCHES. Sep 25, 2006 · Dhav DHC2MKISDR CA060926005Blade · corroded(CAN) UPON VISUAL INSPECTION , CORROSION WAS FOUND ON THE BLADE SHANK. AFTER REWORK TO MINIMUM DIMENSION DAMAGE STILL REMAINS. BLADE WIDTH AND THICKNESS IS WELL ABOVE MINIMUM DIMENSION. ALL 5 BLADES ARE U/S. (TC NR 20060926005)Sep 13, 2006 · Stbros SD360SDR NSVA200600128Erosion Shield · failedAT 700 FT LOUD BANG ON RT SIDE OF AIRCRAFT. DECLARED EMERGENCY AND RETURNED TO FIELD. RT PROP BLADE MISSING 3/4 OF EROSION GUARD AND ENTIRE PROP MAT. REMOVED RT PROPELLER IAW BMM 61-20-00. REMOVED PANELS AND HARDWARE ARE IN THE A/C CARGO COMPARTMENT. CONTAug 23, 2006 · N243CJ · Beech 1900DSDR 2006FA0000760Snap Ring · failed2 SNAP RINGS FAILED ON PROPELLAR BLADES. (K)Aug 2, 2006 · N965B · Cessna 210MSDR 608063Clamp · crackedBLADE CLAMP CRACKED.Jun 8, 2006 · Gulstm 500SDR 608062Clamp · crackedBLADE CLAMPS CRACKED.Jun 8, 2006 · Gulstm 500SDR 60806Blade · crackedCRACKED BLADE SHANK.Jun 8, 2006SDR 0091298Bearing Race · corrodedBEARING RACE CORRODED BEYOND SPEC.May 11, 2006 · Emb EMB120SDR R019617Bearing · corrodedINSTALLED NEW BEARINGS AND FORK AND COMPLIED WITH ALL APPLICABLE SERVICE BULLETINS. PROP WAS DISASSEMBLED FOR SHIPMENT. TSN 14711:35, TSO 2101:09. 1/26/03 - PROP WAS ASSEMBLED AND INSTALLED ON AC302. 4/11/06 - PROP HAS ACCUMULATED 546 HOURS. ALL SIX C-743Apr 15, 2006 · Dorner DO328100SDR CA060414002Blade · cracked4 INCHES CRACK FROM TIP TO HUB ON NR 2 BLADE, SIMILAR TO THAT REPORTED WITH SDR #20060221008. PROPELLER REMOVED FROM SERVICE.Apr 14, 2006 · Diamon DA20C1SDR CA060804005Seal · leaking(CAN) DURING FLIGHT, NR 1 PROP LOST APPROXIMATELY 7 QUARTS OF OIL FROM THE HUB. UPON ARRIVAL AIRCRAFT WAS COVERED IN OIL (LT). THERE WAS NOT AN INFLIGHT SHUTDOWN AND NO EMERGENCY MEASURES WERE REQUIRED OR TAKEN. THE AIRCRAFT RESPONDED NORMALLY. THE PROP SEALMar 29, 2006 · Dhav DHC8301SDR CA060316008Blade · crackedCRACK FOUND ON TRAILING EDGE OF PROPELLER TIP.Mar 15, 2006 · Diamon DA20C1SDR 0089999Actuator · corrodedACTUATOR DOME CORRODED BEYOND SPEC.Feb 21, 2006 · Aerosp ATR72SDR CA060619001Blade · crackedPROPELLER D2A34C58, SERIAL NR 705814, WORK ORDER NR T68807, C-FYJJ. PROPELLER RECEIVED FOR 10 YEAR OVERHAUL. LAST OVERHAUL MARCH 1996, NOW 800.5 HOURS SINCE OVERHAUL. FOUND BLADE S-90AT-4, SERIAL NR C75151YS, CRACKED IN BLADE THREADS, FOUND WITH EDDY CURRENFeb 17, 2006 · Cessna A185ESDR CA060221008Blade · crackedDURING PRE-FLIGHT INSPECTION, THE PILOT INSTRUCTOR DISCOVERED A POSSIBLE CRACK ON THE PROPELLER. CLOSER INSPECTION REVEALED AN APPROXIMATELY 4" CRACK ON NR 2 BLADE OF PROPELLER. THE CRACK IS DEVELOPED LONGITUDINAL ON BLADE FROM TIP TO HUB. NO IMPACT MARK ORFeb 9, 2006 · Diamon DA20C1SDR 0089756Blade · corrodedCORROSION IN BLADE SHANK, NOT REPAIRABLE.Feb 3, 2006 · Cessna 425SDR CA060201003Clamp · corrodedUPON MPI INSPECTION IT WAS NOTED THAT 2 A14B BEARINGS, 3 C838-6 CLAMPS, 1 C1404 HUB, AND 2 A1496-0 ARMS WERE ALL CORRODED BEYOND LIMITS. THROUGH DIMENSIONAL INSPECTIONS THE FOLLOWING PARTS WERE FOUND TO BE WORN BEYOND SERVICEABLE LIMITS,1 B806 CYLINDER AND 1 Feb 1, 2006 · Grumav STCSCANTY30SDR CA060201002Bearing · corrodedUPON MPI INSPECTIONS, IT WAS NOTED THAT 2 A14B BEARINGS, 2 C838-6 CLAMPS, 1 C1404 HUB, AND 1 A1496-0 ARM WERE ALL CORRODED BEYOND LIMITS. THROUGH DIMENSIONAL INSPECTIONS THE FOLLOWING PARTS WERE FOUND TO BE WORN BEYOND SERVICEABLE LIMITS, 1 B806 CYLINDER AND Feb 1, 2006 · Grumav STCSCANTY30SDR 0089579Bearing Race · crackedBEARING RACE CRACKED.Jan 23, 2006 · Emb EMB120SDR CA060126007Blade · damaged(CAN) DISCOVERED WARPED TRAILING EDGE OF PROPELLER BY MAINTENANCE. UNIT HAD BEEN OVERHAULED FEB 2003 THEN RETURNED FOR THIN TRAILING EDGE APRIL 2003. REPAIRED BY SAME FACILITY. TRAILING EDGE WAS SIGNIFICANTLY THINNER THAN SIMILAR IN FLEET. REMOVED PROPELLEJan 20, 2006 · Swrngn SA226TCSDR 01182006APropeller · crackedABORTED TAKE-OFF DUE TO LT PROPELLER VIBRATION. A SIGNIFICANT CRACK WAS OBSERVED ON NR 1 ENGINE'S PROPELLER TIP. INSPECTED AND FOUND BLADE TIP DAMAGE (CRACK AND DELAMINATION) ON NR 1 PROPELLER. DAMAGE LOCATION MEASURED FROM TIP TO DAMAGE AREA .5 AND DAMAGE LOJan 13, 2006 · N237MJ · Saab 340BSDR 0089205Blade · crackedNICKEL SHEATH CRACKDec 29, 2005 · Emb EMB120SDR AU510002117Clamp · failedNR 2 PROPELLER BLADE COUNTERWEIGHT CLAMP FAILED.Dec 12, 2005 · Cessna 310KSDR AU510002072Spring · wornPROPELLER COARSE PITCH STOP P/N A2420-30 AND SPRING P/N A2213-1 WORN. SPRING WAS PREVENTED FROM RETURNING THE BLADES TO THE FINE PITCH POSITION AFTER SHUTDOWN.Dec 12, 2005 · Grob G115CSDR AU510001936Blade · crackedPROPELLER BLADE CRACKED AT 40` STATION. FURTHER INVESTIGATION OPENED UP THE CRACK AND FOUND A LARGE AREA OF CORROSION.Dec 12, 2005 · Cessna 208SDR AU510001814Spring · broken(AUS) PROPELLER FEATHERING AND UNREVERSING SPRING FAILED. (CASA# 510001814)Dec 12, 2005 · Cessna 441SDR 0088867Blade · crackedPROPELLER BLADE NICKEL SHEATH CRACKED.Dec 8, 2005 · Emb EMB120SDR GLBA20050604Blade · damagedRIGHT PROPELLER STRUCK TAXIWAY LIGHT, REPLACED RIGHT PROPELLER BLADE IN NR 4 POSITION AND PLACED ENGINE ON SPECIAL CHIP DETECTION INSPECTION FOR 50 HOURSNov 28, 2005 · N299UX · Emb EMB120ERSDR 2006FA0000052Blade · fracturedPILOT TOOKOFF, DURING CRUISE FLIGHT, SEVERE VIBRATION OCCURRED FROM ENGINE. ENGINE PULLS BACK TO IDLE AND EMERGENCY LANDING MADE ON ROAD . UPON INSPECTION IT WAS DISCOVERED THERE WAS 7.5 INCHES OF BLADE TIP MISSING. SERIAL NR OF BLADE IS NOT ACCESSIBLE AT TNov 23, 2005 · N2653X · Cessna P206SDR 0088585Unknown · corrodedCORROSION, BEYOND SPEC.Nov 18, 2005 · Emb EMB120SDR DIX2005F00001Propeller · damagedREPORTING AN ON-GROUND PROPELLER STRIKE INCIDENT THAT OCCURRED ON AIRCRAFT. THE AIRCRAFT WAS ON THE GROUND PERFORMEING PREFLIGHT CHECKS WHEN THE AIRCRAFT ROLLED OFF THE PAVED RUNUP AREA AND THE LT PROP STRUCK AN OBJECT. UPON PRELLIMINARY INSPECTION OF THE PROct 31, 2005 · N925MM · Beech C90SDR AU510002084Blade · lightning strikeLIGHTNING STRIKE ON AIRCRAFT EXITED THROUGH LT PROPELLER BLADE. UNKNOWN POINT OF ENTRY. ENGINE AND PROPELLER REMOVED FOR LIGHTNING STRIKE INSPECTION.Oct 11, 2005 · Swrngn SA227*SDR HNAA0500090Tape · peelingRETURN TO FIELD DUE TO NOISE FROM LEFT PROP. FOUND EROSION TAPE PEELING OFF BLADE.Oct 8, 2005 · N975HA · Dhav DHC8102SDR AU510001487Blade · corroded(AUS) PROPELLER BLADE CRACKED SPANWISE ON THE LEADING EDGE APPROXIMATELY 140MM (5.5IN) FROM BLADE TIP. FURTHER INVESTIGATION FOUND SEVERE INTERNAL EXFOLITAION CORROSION. THE SAME PROPELLER HAD A SIMILAR DEFECT APPROXIMATELY 50 HOURS PREVIOUS. (CASA# 510001487Oct 6, 2005 · Cessna 208SDR AU510001483Blade · failed(AUS) PROPELLER BLADE TIP SEPARATED IN FLIGHT. APPROXIMATELY 228.6 (9IN) OF BLADE SEPARATED. SEVERE VIBRATION CAUSED ENGINE TO SEIZE DURING EMERGENCY LANDING. AIRCRAFT IS REGISTERED AND OPERATING IN CANADA. (CASA# 510001483)Sep 6, 2005 · Gippld GA8SDR CA050822005Blade · corroded(CAN) AIRCRAFT, BLADE RECEIVED FOR MAJOR INSP. DURING INSP OF THE BLADE SHANK IAW CMM, WAS FOUND WITH CORROSION PITTING AND ETCHING OF THE ALUMINIUM SURFACE. DURING INSP OF THE TAPERBORE IAW CMM, CORROSION PITTING WAS FOUND. ZONE 5 IS NOT ALLOWED ANY CORROSIAug 22, 2005 · Dhav DHC8*SDR V0DR200500001Bearing Race · brokenDURING DISASSEMBLY FOR OVERHAUL, FOUND NR 2 AND NR 3 BLADE BEARING RACES CRACKED AND BROKEN. HUB SIDE RACES (P/N) D-7745-A (S/NS) A059 & A075. BLADE SIDE RACES (P/N) D-7745-B (S/NS) A417 & A453.Aug 4, 2005 · N94GL · Beech 1900D
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