JASC 6110
Service difficulty reports · 1,590
Reports filed under 6110 · Propeller Assembly, 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 = '6110' 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 = '6110' 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 2001F00118Hub · scoredPROPELLER WAS RECEIVED FOR O/H WITH EXCESSIVE GREASE LEAKAGE FROM ALL BLADES. PROP WAS DISASSEMBLED TO START O/H PROCESS. WHEN HUB UNIT WAS SPLIT, THERE WAS EXCESSIVE AMOUNTS OF GREASE INSIDE. UPON FURTHER INSPECTION, THE BEARING RACE HAD SHATTERED INTO SEVESDR ASOA01084SPropeller · overspeedFLT 4291 - DURING FINAL APPROACH INTO AVL, AIRCRAFT EXPERIENCED A PROPELLER OVERSPEED. CREW DECLARED AN EMERGENCY AND PERFORMED THE IMMEDIATE ACTION ITEMS FOR A PROPELLER OVERSPEED. AIRCRAFT LANDED SAFELY IN AVL. MAINTENANCE REMOVED AND REPLACED LEFT ENGINESDR GLBA2001130Propeller · noisyPROPELLERS NOISY. INSPECTED AND CLEANED LOW PITCH SOLENOIDS, OPS CHECK SYSTEM SATISFACTORY.SDR SABA010018Propeller · defectiveAIRCRAFT 963 ON FLIGHT 5123 FROM RDU TO ORF. AFTER ENTERING CRUISE FLIGHT THE RIGHT ENGINE PROPELLER FLUCTUATED UP TO TWO PERCENT. ALSO THE BETA CAP LIGHT ILLUMINATED. AIRCRAFT RETURNED TO RDU AND LANDED WITH NO OTHER PROBLEMS. NO INFLIGHT EMERGENCY WAS DESDR 2001FA0000085Plate · crackedTHIS PROPELLER INSTALLATION UTILIZES 2 SPINNER AFT BULKHEAD ATTACH PLATES, PN A1639-9. BOTH PLATES WERE FOUND TO BE CRACKED WITHIN 50 HR OF INSTALLATION OF PROP AFTER OVERHAUL. BECAUSE BULKHEAD ATTACHMENT PLATES ARE INSTALLED UNDER ATTACHMENT NUTS, PN A1639-SDR SW15200112284Bulkhead · crackedFORWARD PROPELLER BULKHEAD HAS BEEN CRACKING WITH MINIMAL HOURS. BOLTS HAVE BEEN PROPERLY TORQUED AND SAFETY WIND.SDR 2001FA0000157Snap Ring · damagedTHE AFOREMENTIONED AIRCRAFT ARRIVED FOR ENGINE OIL & FILTER CHANGE. UPON COMPLETION OF SERVICE, A PRE-ENGINE RUN / WALK AROUND INSPECTION WAS PERFORMED. DURING THIS WALK AROUND INSPECTION THERE WAS A CONSIDERABLE AMOUNT OF EXCESSIVE PLAY NOTED IN ONE OF THE RTSDR CA010629006Blade · burned(CAN) BOMBARDIER AEROSPACE REGIONAL AIRCRAFT HAS JUST RECEIVED A REPORTABLE SDR WEVENT WHICH WE ARE REQUIRED TO REPORT ON MAY 5/01. DURING APPROACH, THE PILOT REPORTED THAT THE R/H PROPELLER SUSTAINED A LIGHTENING STRIKE. INSPECTION OF THE PROPELLER UPON LANDISDR PNSA010501O-Ring · cutON CLIMBOUT A SLIGHT ODOR OF SMOKE WAS NOTICED IN THE CABIN. STARTED TO RETURN TO BASE WHEN RT OIL PRESSURE LOW LIGHT ILLUMINATED. THIS WAS CONFIRMED BY THE OIL PRESSURE INDICATOR. RT ENGINE WAS SECURED, AN UNEVENTFUL LANDING. FOUND PROPELLER PISTON SEAL OSDR AUS20010409Propeller · out of balance(AUS) RT PROPELLER OUT OF BALANCE. PROPELLER HAD BEEN RECENTLY REPLACED BUT HAD NOT BEEN BALANCE CHECKED FOLLOWING FITMENT.SDR CA010504002Propeller · corroded(CAN) HEAVY CORROSION THRU-OUT INTER PROPELLER, .040TH OFF MATERIAL. REMOVED TO REMOVE CORROSION.SDR BG72001F00000Seal · leakingTHE LEFT ENGINE PROPELLER SHAFT SEAL WAS REPLACED DUE TO A SUSPECTED OIL LEAK. THE WRONG PART NUMBER SEAL WITH A SMALLER OUTSIDE DIAMETER WAS INSTALLED. DURING THE MAINTENANCE GROUND RUN ON LEAKS WERE DETECTED. ONE HOUR INTO THE FLIGHT BACK TO THE AIRCRAFTSSDR 20010425CW005Spring · crackedDURING DISASSEMBLY AND VISUAL INSPECTION, SPRING WAS FOUND CRACKED IN HALF, IAW AIRCREW, NO DISCREPANCY WAS NOTED DURING INCOMING FLIGHT. PROPELLER HUB REPLACED, SPRING REPLACED, PROPELLER REASSEMBLED AND INSTALLED ON THE AIRCRAFT WITH NO DISCREPANCIES NOTED.SDR ME42001F00000Spring · brokenHARTZELL PROPELLER MODEL NUMBER HC-B4MP-3A/M10877K WITH SERIAL NUMBER FW778 WAS RECEIVED FOR HUB REPLACEMENT IAW AD NOTE 96-18-14. DURING THE DISASSEMBLY, THE SPRING, PN A3496, IN THE SPRING KIT ASSEMBLY WAS NOTED BROKEN. TALKING WITH THE FLIGHT CREW, THEY SSDR 20010411CW004Counterweight · damagedAIRCRAFT ENCOUNTERED SEVERE VIBRATION ON CLIMB OUT. REQUESTED TO RETURN TO AIRPORT AND LANDED WITHOUT COMPLICATIONS. INSPECTION OF VIBRATION FOUND THAT THE COUNTERWEIGHT FROM NR 2 PROP BLADE HAD COME LOOSE. INSPECTION SHOWED BOLT THAT HOLDS COUNTERWEIGHT HASDR 2001FA0000103Snap Ring · failedEXTERNAL SNAP RING ON PROPELLER BLADE CAME OFF AFTER PREFLIGHT ENGINE HAD STOPPED ON INITIAL START, THEN WAS RESTARTED. SNAP RING CAME OFF BLADE SHANK BUT WAS RETAINED BY SPINNER. THEN AIRPLANE WAS FLOWN FOR 2 HOURS WITH FIVE TOUCH AND GO LANDINGS, WITHOUT FSDR AU010277Spacer · misinstalled(AUS) RT PROPELLER SPACER INCORRECTLY FITTED.SDR 20010604CW015Clamp · corrodedCORROSION IN CLAMPS AND BEARING RACES, REJECTED ALL 3 CLAMPS AND 1 RACE.SDR 20010411CW007Counterweight · separatedCOUNTERWEIGHT DEPARTED LEFT PROP ON TAKEOFF ROLL. SPINNER AND BACKING PLATE WERE DESTROYED. PROP HUB WAS CRACKED IN TWO PLACES. NO OTHER DAMAGE TO AIRCRAFT OR ENGINE. ROTOR COUNTERWEIGHT WAS NOT FOUND.SDR 2001FA0000087Counterweight · crackedDURING MAGNETIC PARTICLE INSPECTION, AN INDICATION WAS FOUND IN THE TRANSITION BETWEEN THE COUNTERWEIGHT ARM AND THE ATTACHMENT AREA, WHERE IT JOINS THE BLADE ROOT. THE CRACK APPEARS LIKE A HAIR LINE BUT STRONG INDICATION, ONCE IT WAS GROUND TO MAXIMUM DEPTH SDR 20010320CW002Bolt · mismanufacturedTHE SIX A2513-92 PROPELLER MOUNTING BOLTS ARE APPROX .250 INCHES TOO SHORT. THEY ARE THREE THREADS TOO SHORT FROM BEING FLUSH WITH THE BACK SIDE OF THE PRESSED IN NUT ON CRANKSHAFT FLANGE. A LONGER BOLT (APPROX .250 IN) WOULD CORRECT THIS PROBLEM. THIS AIRSDR 20010412CW003Counterweight · crackedCOUNTERWEIGHT SLUG CRACKED. LOW TIME, HAVE SLUG.SDR LR7A00221Propeller · overspeedNR. 1 PROPELLER RPM OUT OF LIMITS - 103% DURING CRUISE IN MECHANICAL GOV MODE. SHUT DOWN NR. 1 ENGINE IAW SHUTDOWN PROCEDURES AND RETURNED TO LICZ. AIRCRAFT FERRIED TO RMS FOR REPAIR.REPLACED NR. 1 PROPELLER ASSY IAW LAC HN6101. GROUND RUN OPS CK NORMAL PERSDR 20010412CW004Counterweight · crackedCOUNTERWEIGHT SLUG CRACKED IN SLOTS. LOW TIME, HAVE SLUG.SDR 20001207SH015Lock · brokenSTART-LOCK BROKE AND PIN FELL OUT BECAUSE RETAINING COTTER PIN WAS TOO WEAK. (X)SDR AU001133Blade · mismanufactured(AUS) PROPELLER TIP EXFOLIATING. SUSPECT MANUFACTURING DEFECT/FLAW.SDR FJT00109374Propeller · misrepairedDURING DESCENT TO ROU RT PROPELLOR RPM BECAME UNCONTROLLABLE. PROPELLOR RPM WENT TO 104 PERCENT. CREW WAS UNABLE TO LOWER THE RPM TO 100 PERCENT WITH THE SPEED LEVER. A PRECAUTIONARY RT ENGINE SHUT OFF WAS PERFORMED. A/C LANDED AND TAXIED TO GATE WITHOUT FURTHSDR 20001108SH029Propeller · vibrationNEW MCAULY STC PROPELLER KIT INSTALLED, ACFT FLOWN FOR BRIEF FLIGHT. AIRCRAFT HAD SUCH VIOLENT VIBRATION, PILOT NO LONGER WILLING TO FLY IT. INSPECTION OF BLADE ANGLES WITH PROP ON ACFT, SHOWED ANGLES WERE NOT IN COMPLIANCE WITH MFG SPECS BETWEEN BLADES AND SDR 20001108SH028Propeller · vibrationNEW MCAULEY STC PROPELLER KIT INSTALLED, ACFT FLOWN FOR BRIEF FLIGHT. AIRCRAFT HAD SUCH VIOLENT VIBRATION, PILOT NO LONGER WILLING TO FLY IT. INSPECTION OF BLADE ANGLES WITH PROP ON ACFT, SHOWED ANGLES WERE NOT IN COMPLIANCE WITH MFG SPECS BETWEEN BLADES ANDSDR AU000967Propeller · leaking(AUS) PROPELLER SLOW TO FEATHER. BLADE SEALS LEAKING GREASE. (X)SDR SJ3RR003186Blade · misoverhauledCUSTOMER WORK ORDER WAS OPENED TO DYNAMIC BALANCE PROPELLERS. UPON INSPECTION OF THE AIRCRAFT, THE BLADES WERE FOUND NOT TO BE SHOT PEENED IN ACCORDANCE WITH AD 95-01-02. THE PROPELLERS HAD BEEN PREVIOUSLY OVERHAULED BY YINGLING AIRCRAFT, INC., ON 7-31-2000.SDR 20001019SH012Propeller · crackedPROPELLER SUBMITTED FOR SB 233A COMPLIANCE. PROPELLER FOUND CRACKED AS INDICATED IN THE SERVICE BULLETIN, IN THE PILOT BORE, FACE SIDE OF THE PROPELLER. PROPELLER IS TO BE RETURNED TO MANUFACTURER FOR DISPOSITION. (X)SDR 20001023SH004Link · damagedDURING PREFLIGHT INSPECTION, OPERATOR FOUND BLADE TO BE LOOSE. THE PROPELLER WAS REMOVED FROM AIRCRAFT AND SENT FOR REPAIR. DURING DISASSEMBLY, THE BLADE LINK SNAP RING WAS NOT INTACTED. THE PROPELLER RECEIVED A COMPLETE OVERHAUL WITH REPLACEMENT OF ALL UNASDR SIMA2642Actuator · damagedALB - DURING SCHEDULED PROPELLER HUB CHANGE, MAINTENANCE FOUND THE PROP ACTUATOR TO HAVE BOTH ANTI-ROTATION INSERTS (PN 78278-1) MISSING FROM ONE OF THE BLADE YOKES. THE ANTI-TORQUE ARM AND YOKE WERE DAMAGED ALSO. ONLY ONE WAS FOUND IN THE HUB AFTER ACTUATORSDR 20001109SH010Ferrule · crackedPROPELLER SENT FOR REPAIR OF OIL LEAK. AFTER INVESTIGATION OF THE PROPELLER AND DISASSEMBLY, FOUND THE OIL LEAK OCCURRED BECAUSE ONE BLADE FERRULE HAD BEEN CRACKED IN THE BEARING AREA. (X)SDR 20000914SH012Mount · crackedDURING OVERHAUL INSPECTION, VISUAL CRACK IN BOTTOM OF MOUNTING HOLE DETECTED. CONFIRMED WITH ZYGLO INSPECTION, EDDY CURRENT DEFLECTION DETECTED. (X)SDR 20000907SH016Flange · damagedPROPELLER SUBMITTER FOR REPAIR. DURING INSPECTION, DISCOVERED THE PROPELLER MOUNTING SURFACE WAS NOT FLAT AND APPEARED TO HAVE BEEN NOT SEATING PROPERLY ON THE ENGINE CRANKSHAFT. SUBMITTER STATED IT APPEARED THE PROPELLER FLANGE HAD BEEN HEAVILY GROUND OR SASDR PNSA0803Propeller · bindingPROPELLER RPM WAS LOW ON TAKEOFF. FOUND PROP WAS BINDING INTERNALLY. REPLACED PROPELLER. OPS CHECK OK. (X)SDR EY2R57102Bearing · corrodedTHREE SPLIT BEARING HAD CORROSION ON SURFACE. REPLACED. (X)SDR EY2R57100Bracket · crackedDEICE BRACKET CRACKED IN RADIUS. REPLACED. (X)SDR AU001137Propeller · unapproved part(AUS) INCORRECT PROPELLER FITTED TO AIRCRAFT. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.SDR 20000817SH013Nut · crackedPROPELLER IN FOR OVERHAUL. DISASSEMBLED, FOUND BOTH RETENTION NUTS CRACKED. (X)SDR CA000808008Propeller · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. CWT BRACKET WEB WORN BEYOND REPAIR. BLADE MERROR FINISHED WITH DEEP CORROSION. NOTE: MERROR FINISH IS NOT A GOOD THING FOR PROPELLER BLADES, IT DOES NOT OFFER ANY CORROSION PROTECTION. BLADE BEARINGS DRY.SDR AU000584Fork · out of rig(AUS) RT PROPELLER REVERSE STOP INCORRECTLY SET. PITCH CHANGE FORK CRACKED.SDR EY2R56936Lock · crackedSTART LOCK LATCH CRACKED AT THE BASE OF CUT OUT UNDER LATCH PIN.SDR 20000831SH024Bolt · failedOWNER REPORTED 5 OF 6 AN 6-60 PROPELLER BOLTS FAILED IN-FLIGHT. BOLTS SENT TO MFG, FOUND IN SPEC REASON FOR FAILURE DUE TO BOLTS BEING TOO LONG PREVENTING PROPER CLAMP-UP OF CRUSHPLATE AND SPINNER BULKHEAD TO CAMSHAFT FLANGE EXTENSION. FAILED BOLTS SHOWED 4 SDR 20000803SH007Brush Block · crackedCRACK IN METAL, PN 6506709, IN BRUSH BLOCK LEAF ASSEMBLY. (X)SDR WBVA00600Propeller · failedPILOT REPORTED PROPELLER RPM VARIES DURING CLIMB-OUT. CONTROL CABLE, PROPELLER GOVERNOR AS WELL AS HUB AIR PRESSURE AND BLADE ANGLE WERE DETERMINED TO BE SERVICEABLE. SERVICEABLE PROPELLER WAS INSTALLED AND CHECK FLIGHT WAS OK. AWAITING OVERHAUL REPORT. (X)SDR EY2R56606Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. 1 CRACK.SDR NACA200000004Washer · brokenWHILE FEATHERING NR 1 ENGINE PROP, 2 BLADES WENT TO FEATHER AND 1 BLADE DID NOT. TEAR DOWN OF PROP BEFORE SHIPPING TO REPAIR FACILITY SHOWED A BROKEN THRUST WASHER. REPLACED NR 1 PROP ASSEMBLY.
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