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 O05R200411256Blade · damagedBLADE REJECTED IAW MFG CONCESSION 102566/C/P.SDR AUS20040002Clip · separated(AUS) PROPELLER BLADE ROOT CIRCLIP AND ASSOCIATED SHIMS SEPARATED.SDR CA031211003Collar · cracked(CAN) DURING A FLEET INSPECTION OF PROPELLER BLADES TO CHECK INTEGRITY AND CONDITION OF THE BLADE CUFFS. AS A RESULT OF THE INSPECTIONS, ONE COLLAR ASSY WAS FOUND TO BE CRACKED, HOWEVER, STILL SECURELY ATTACHED. THE BLADE ASSY WAS REMOVED FROM SERVICE AND HAS SDR AUS20031234Collar · cracked(AUS) PROPELLER BLADE COLLAR ASSEMBLY CRACKED. FOUND DURING FLEET-WIDE INSPECTION FOLLOWING SEPARATION OF BLADE COLLAR ON ANOTHER AIRCRAFT. SEE MDR 03/1228.SDR CA031202002Collar · separated(CAN) DURING TAKEOFF ROLL NR1 PROP, NR 4 BLADE COLLAR P/N 802253-1, -2 SEPARATED FROM PROP BLADE AND STRUCK NR2 BLADE CAUSING IMPACT DAMAGE TO ITS LE NICKEL SHEATH. DEBRIS IMPACTED ONTO LT ROW 5 CABIN WINDOW CAUSING A HOLE IN OUTER PANE AND DAMAGE TO WINDOW FSDR AUS20031228Collar · separated(AUS) NR 1 PROPELLER NR 1 BLADE COLLAR SEPARATED FROM BLADE AND STRUCK THE NO3 BLADE CAUSING IMPACT DAMAGE TO THE LEADING EDGE. DEBRIS THEN STRUCK THE NR 5 LT CABIN WINDOW SURROUND STRUCTURE. INNER PANE OF THE WINDOW REMAINED INTACT.SDR GLBA2003152Bearing Race · brokenLOOSE BLADES FOUND DURING SCHEDULED INSPECTION, REPLACED PROPELLER ASSEMBLY, TEARDOWN RESULTS FOUND BROKEN LOWER BEARING RACE PN C-792-1B REV (H) SN H123.SDR AUS20031186Blade · unserviceable(AUS) LT ENGINE PROPELLER BLADE FAULTY. LIMITED INFORMATION PROVIDED.SDR AUS20031312Seal · damaged(AUS) RT PROPELLER BLADE SEAL TORN ALONG OUTER SIDE. LENGTH OF TEAR APPROXIMATELY 38.1MM (1.5IN). PROPELLER HUB LEAKING OIL.SDR 006876Blade · crackedCRACK IN BLADE POSITION NR 2 ENGINE SIDE.SDR 2003FA0001181Blade · crackedPROPELLER RECIEVED FOR OVERHAUL. AT DISASSEMBLY AND CLEANING FOUND BLADE S/N 1139 HAD A CRACKED OUTER SLEEVE AT ROOT END OF BLADE. BLADE REJECTED FROM FURTHER SERVICE.SDR 0068494Blade · crackedCRACK AT BLADE SHANK FILLET RADIOUS.SDR 00068494Blade · crackedCRACK AT BLADE SHANK FILLET RADIUS. PROPSDR 0068494ABlade · crackedCRACK AT PROPELLER BLADE SHANK FILLET RADIUS.SDR CA031008002Retainer · failed(CAN) THE PROPELLER WAS REMOVED AND DISASSEMBLED FROM THE RT SIDE OF A CL 215 FOR SHIPMENT TO AN OVERHAUL FACILITY WHEN IT WAS DISCOVERED THAT NR 1 BLADE RETAINER ASSY WAS CRACKED AND SEVERAL ROLLERS WERE DESTROYED. UPON A CLOSER INSPECTION THE OTHER TWO BLADESDR CA030923004Blade · damaged(CAN) BLADES MEASURED WHEN RECEIVED IN SHOP, FOUND BLADE WIDTH TO BE BELOW MIN. ALLOWABLE. BLADES REPLACED.SDR CA030923003Blade · damaged(CAN) PROPELLER BLADES MEASURED WHEN RECEIVED IN SHOP. BLADES FOUND TO BE BELOW MIN. WIDTH AND THICKNESS. BLADES REPLACED.SDR CA030826009Blade · corroded(CAN) EXTRA WORK TO REMOVE CORROSION FROM PROPELLER CAMBER FACE.SDR FCPR200300011Separator · leakingFOUND 1 BALL BEARING MISSING FROM BLADE NR 3, PN A1634-9, SEPARATOR PN B5223.SDR AUS20031012Blade · cracked(AUS) PROPELLER BLADE BUTT CRACKED IN OUTER BLADE SLEEVE.SDR 2003F00571Blade · crackedPROPELLER WAS REMOVED AND SENT TO PIEDMONT AVIATION COMPONENT SERVICES (REPAIR STATION QWPR503X) FOR MCCAULEY ALERT SERVICES BULLETIN 246B/REV 2 INSPECTION. DURING FLUORESENT PENETRANT INSPECTION FOUND NR 1 BLADE P/N 114HCA-0, S/N PE006 (TSN 13,090.01; TSO 1,SDR CA030806009Blade · loose(CAN) PROP (OVERHAULED IN NOV/2000) WAS PURCHASED AND INSTALLED ON PA31 AIRCRAFT. AT 51.6 HOURS SINCE OVERHAUL, 2 OF 3 PROP BLADES WERE NOTICED TO BE VERY LOOSE WHEN MANIPULATED FORE AND AFT AT THE PROP TIP.ONE BLADE IN PARTICULAR MOVED SIGNIFICANTLY. DISCUSSISDR AUS20030801Blade · animal strike(AUS) RT PROPELLER BLADE SEVERELY DAMAGED FOLLOWING WALLABY STRIKE. BLADE TIP BENT BACKWARDS ABOUT 50.8MM (2IN) FROM BLADE TIP.SDR 0067341Blade · crackedCRACK ON PROPELLER BLADESDR 67341Blade · crackedCRACK ON BLADE.SDR 2003F00428Blade · crackedPROPELLER WAS REMOVED AND SENT TO PIEDMONT AVIATION COMPONENT SEVICES (REPAIR STATION QWPR503X)FOR VIBRATION /MCCAULEY ALERT SERVICE BULLETIN 246. DURING DISASSEMBLY FOUND OIL IN NR 4 BLADE BORE DUE TO NICK IN PLUG SEAL, LEADING TO BELIEVE THE CAUSE OF VIBRATISDR SWIA200312176Blade · crackedRT ENGINE NR 3 PROP BLADE HAS APPROX .375 INCH CRACK ON TRAILING EDGE. DISCOVERED DURING LINE INSPECTION. REMOVED AND REPLACED R-3 PROP BLADE IAW MM 61-13-04.SDR 2003FA0000693Blade · brokenDURING NORMAL OPERATION, A PORTION OF BLADE TIP (P-TIP) BROKE OFF.SDR 2003FA0000684Strip · separatedAT CRUISE, PORTION OF PROP LEADING EDGE STRIP SEPARATED FROM PROP. EMERGENCY LANDING ON LAKE ERIE SHORE. PROP OVERHAULED IN 1974. APPROX 40 HOURS SINCE LAST ANNUAL INSPECTION.SDR CA030604006Blade · corroded(CAN) PROPELLER RECEIVED ON 22 MAY 2003, MODEL HC-E2YK-2B/FC847504 REMOVED FOR INSPECTION DUE TO EXCESSIVE ROTATIONAL BLADE MOVEMENT. A DECISION WAS MADE TO OVERHAUL THE PROPELLER. VISUAL INSPECTION ON ONE BLADE REVEALED EXCESSIVE CORROSION AT THE BLADE BEARINSDR 0075156Bearing · corrodedCORROSION ON BEARING BLADE PIN.SDR 0175156Bearing · corrodedCORROSION ON BEARING BLADE PIN.SDR AUS20030425Bearing · fractured(AUS) PROPELLER BLADE BEARING FRACTURED.SDR AUS20030504Blade · damaged(AUS) PROPELLER BLADES (2OFF) CONTAINED DEEP SCORING ON THE CAMBER SIDE LOCATED APPROXIMATELY 76.2MM TO 127MM (3IN TO 5IN) FROM THE TIP.SDR 0065686Blade · corrodedPROPELLER HAS CORROSION ON BLADE.SDR 00656686Blade · corrodedPROPELLER BLADE HAS CORROSION ON BLADESDR 65686Blade · corrodedCORROSION ON BLADE.SDR 0074451Bearing Race · crackedCRACK IN RACE.SDR CA040210007Blade · scored(CAN) AFTER SHUT-DOWN, PILOT NOTICED ONE PROPELLER BLADE ROOT SNAP RING HAD POPPED OUT OF ITS LOCATION DURING PREVIOUS FLIGHT. IN DOING SO, IT DAMAGED THE BLADE ROOT BY SCORING SURFACE. PROPELLER REMOVED AND SENT FOR REPAIR AT PROPELLER SHOP.SDR 2003FA0000808Blade · crackedUPON REMOVING FAIRINGS ON BLADE, CORROSION WAS UNDERFAIRING. PROPELLER CAME FOR AD. LONGITUDINAL CRACKS FOUND ON CAMBER AND FACE SIDE BLADE FAIRING. FAIRING WAS ORIGINALLY INSTALLED IN 1940'S. NEED TO REPLACE THEM.SDR 2003FA0000802Blade · crackedUPON REMVING FAIRINGS ON BLADE, CORROSION WAS UNDER FAIRING. PROPELLER CAME FOR A.D. LONGITUDINAL CRACKS FOUND ON CAMBER AND FACE SIDE BLADE FAIRING. FAIRING WAS ORIGINALLY INSTALLED IN 1940'S, NEED TO REPLACE THEM.SDR 2003FA0000800Blade · crackedUPON REMOVING FAIRINGS ON BLADE, CORROSION WAS UNDER FAIRING. PROPELLER CAME FOR AD LONGITUDINAL CRACKS FOUND ON CAMBER AND FACE SIDE BLADE FAIRING. FAIRING WAS ORIGINALLY INSTALLED IN 1940'S. NEED TO REPLACE THEM.SDR CA030305008Propeller · failed(CAN) FACTORY NEW PROPELLER STC SA00920CH. ONLY OBTAIN 2300 RPM STATIC, SHOULD BE 2600 RPM. FOUND BLADE LOW END STOPS INCORRECTLY SET.- PROP RETURNED TO OBTAIN NEEDED 2600 RPM. ERROR IN ENGINEERING APPROVAL AT MCCAULEY INCORRECT BLADE ANGLES.SDR NSVA200300005PropellerDuring climb out from LGA, @ approximately 1000 ft., crew noted that a ring of sparks were coming from the RH engine. With engine indications normal crew reduced power-sparks continued. In flight emergency was declared-air return to LGA. Aircraft landing was uSDR 2003FA0000181Blade · crackedPROPELLER RECEIVED FOR OVERHAUL AT TEARDOWN FOUND OUTER SLEEVE WAS CRACKED ON BLADE S/N 1140. CRACK APPROXIMATELY 4 INCHES LONG. BALDE WAS REJECTED FROM FURTHER SERVICE.SDR 0065187Blade · crackedPROPELLER BLADE CRACKED IN LEADING EDGE SHIELD.SDR AUS20030502Blade · damaged(AUS) PROPELLER NR 3 BLADE CONTAINED STONE DAMAGE AT THE 50 INCH STATION. BLADE LEADING EDGE CONTAINED A 6.350MM TO 12.7MM (0.25IN TO 0.5IN) TEAR. DAMAGE EXCEEDED REPAIRABLE LIMITS.SDR GLBA2003009Bearing · failedREPLACED PROP DUE OVERHAUL FOUND NR 2 BLADE BEARING HAD FAILED. REMOVED AND REPLACED PROP.SDR 2003F00099Pin · misinstalledAFTER REMOVING THE BLADE PIN SETSCREW THE BLADE PIN WAS SO LOOSE THAT IT COULD BE REMOVED BY HAND. THE ID OF THE SLEEVE BUSHING IS OVAL AND MATERIAL IS PUSHED TO BOTTOM OF BORE. THIS IS THE FIRST TIME WE HAVE SEEN THIS SINCE THE REQUIREMENT FOR THE BLADE PINSDR W592003F00000Cylinder · loosePROPELLER WAS SUBMITTED FOR REPAIR DUE TO A SEIZED SPINNER ATTACH PN A24053 WHILE ATTEMPTING TO REMOVE THE NUT. IT WAS NOTED THAT THE ENTIRE CYLINDER ASSEMBLY WAS LOOSE AND UNSCREWING FROM THE HUB. THIS PART SHOULD HAVE BEEN TORQUED TO 180 FT LBS. THIS IS A
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