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 NSVA2009040Propeller · out of balanceLEFT AILERON WAS VIBRATING IN FLIGHT CAUSING A VIBRATION IN THE FLIGHT CONTROLS AND THE AIRFRAME. CHECKED AILERON CABLE TENSIONS IN BOTH WINGS IAW SAAB AMM 27-11-00. CHECKED ALL AILERON BELLCRANKS AND BOTH CENTERING MECHANISMS IAW SAAB AMM 27-11-40 AND 27-11SDR QXEA2009082400630Buss Bar · failedBZN - NR 1 PEC CAUTION MSG W/ POWERPLANT MSG ON CLIMBOUT ABOVE 10,000FT. NR 1 PROPELLER WENT TO 1050 TO 1060 NP. UNABLE TO GET PROPELLER UNDER 1020 NP. NR 1 ENGINE SHUTDOWN PER EA CHECKLIST. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. FOUND NSDR CA090730006Spring · wrong partPROP INSTALLED ON ACFT HAD PROP ZERO PITCH LATCH KIT INSTALLED IAW STC SP96-1. THE PROP HAD A HARD TIME COMING OFF LATCHES. PROP WAS DISMANTLED TO THE EXTENT NECESSARY TO DETERMINE THAT THE WRONG FLYWEIGHT SPRINGS HAD BEEN INSTALLED AT THE PREVIOUS O/H. SPRSDR 2009FA0000668Diaphragm · crackedACFT EXPERIENCED AN IN FLIGHT FAILURE OF THE PROPELLER PITCH CHANGE DIAPHRAGM. THE PILOT PERFORMED AN EMERGENCY DECENT AND A NORMAL LANDING AT THE AIRPARK. UPON SHUTDOWN A TOTAL OF 7 QUARTS OF OIL HAD BEEN LOST. THE DIAPHRAGM HAD BEEN REPLACED 2 YEARS AGO ASDR CA090619013Retainer · crackedDURING ROUTINE PHASE INSP OF THE PROP MX, FOUND THAT THE LT ENG PROP SHAFT SEAL RETAINER HAD MULTIPLE CRACKS COMING OUT FROM UNDER EACH OF THE ATTACHMENT STUDS. PART REMOVED AND REPLACED. ACFT RETURNED TO SERVICE.SDR CA090313004Blade · unserviceable(CAN) PROP BLADE CUFF DAMAGED, LARGE CHUNK FOUND MISSING (8 INCH BY 8 INCH) AND DE-ICE BOOT DE-LAMINATED. ON PREVIOUS FLIGHT PILOT REPORTED - DE-ICE SELECTED ON PROP DE-ICE AMMETER PEGGED FULL DEFLECTION WHEN SAID BLADE SEQUENCED. UPON INSPECTION OF THE AFT SISDR CA090112014Seal · leaking(CAN) SHORTLY AFTER DEPARTING YELLOWKNIFE, AT APPROXIMATELY 55 NAUTICAL NORTH THE CREW OBSERVED A NR 2 PROP LOW OIL INDICATION ILLUMINATED. THE CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE REPLSDR 2008FA0000680Screw · wornCUSTOMER COMPLAINED OF AN EXCESSIVELY LOOSE BLADE PRELOAD ON (1) BLADE 4 MONTHS AFTER OVERHAUL. INSP REVEALED EXCESSIVE WEAR ON END OF BLADE PRELOAD SCREWS CAUSING LOOSENESS OF BLADE. OPPOSITE SCREW WAS WORN ALSO BUT NOT TO EXTENT TO BE NOTICEABLE. SECOND OCCUSDR CA080930002Propeller · vibration(CAN) PROPELLER REMOVED FOR EVALUATION DUE TO SMALL VIBRATION. NOT CONSIDERED SERIOUS.SDR 2008FA0000615Ring · brokenBETA RING CRACKED, BROKEN. PROPELLER WAS INVOLVED IN PROP STRIKE AT MID STATION OF BLADE NR 2 BY A FOREIGN OBJECT. MALFUNCTION FOUND 3 HOURS FLIGHT TIME AFTER LOCAL REPAIR OF BLADE. (K)SDR 2008FA0000614Rod · brokenBETA ROD CRACKED, BROKEN. PROPELLER WAS INVOLVED IN PROP STRIKE AT MID STATION OF BLADE NR 2 BY A FOREIGN OBJECT. MALFUNCTION FOUND 3 HOURS FLIGHT TIME AFTER LOCAL REPAIR OF BLADE. (K)SDR SWIA200819961Propeller · malfunctionedPERFORMED GO-AROUND WHEN ENGINES WOULD NOT GO INTO GROUND IDLE. PERFORMED OPERATIONAL TEST OF FLIGHT IDLE STOP SYSTEM IAW AMM 76-13-00 WITH NO FAULTS. REPLACED LEFT PROP ASSEMBLY WITH SERVICEABLE UNIT IAW MM 61-10-00 DUE TO TORQUE.
SDR SWIA200819917O-Ring · damagedRT ENGINE NP SURGED AFTER TAKE-OFF. (FLIGHT NR 5702) REPLACED TRANSFER TUBE O-RINGS AND ADJUSTED PCU IAW AMM 61-10-02. OPS CHECK GOOD.
SDR CA080807003Thrust Washer · cracked(CAN) THE CRACKED BLADE RING IS PART OF THE BLADE ASSEMBLY. A CRACKED RING TYPICALLY RESTRICTS BLADE ROTATION AND CAN SET UP A VIBRATION. PROPELLER WAS REMOVED AND AFTER TEAR DOWN AND INSPECTION A CRACKED BLADE RING (THRUST WASHER) WAS DETERMINED AND OTHER DAMSDR 2008FA0000487Bulkhead · crackedPROPELLER SPINNER BULKHEAD CRACKING BETWEEN ATTACH BOLT HOLES IN (2) PLACES. CRACK COULD BE INDUCED FROM VIBRATION. INSPECT VISUALLY EVERY PRE-FLIGHT. A BETTER HEAT TREATING PROCESS MAY STRENGTHEN THE BULKHEAD AND REDUCE THE CRACKING FROM VIBRATION. (K)SDR 2008FA0000354Bolt · shearedWHILE DOING A RGB CHANGE ON THE NR 1 ENGINE OF DASH-8, N802MR, DURING REINSTALLATION OF THE PROPELLER WHILE DOING THE TORQUE SEQUENCE, WE BROKE ONE PROP MOUNTING BOLT. WE SENT THE HUB OUT FOR REPAIR AND SENT THE TORQUE WRENCH TO THE CAL PLACE TO BE VERIFIED. TSDR SIMA200815101Propeller · malfunctionedON FLIGHT 3204 ON ABORTED TAKEOFF AT 100 KTS, NR 1 ENGINE PROP RPM GAUGE WENT TO 1440 RPM, DURING ABORT POWER LEVERS TO FLIGHT IDLE NR 1 PROP RPM STAYED ABOVE 1300 RPM FOR AT LEAST 3 SECONDS.SDR SWIA200819500O-Ring · unknownFLT 5747 - THE RIGHT PROPELLER NP EXCEEDED 100 PERCENT. REPLACED RIGHT PROP TRANSFER TUBE O-RINGS. OPS CHECKS GOOD PER AMM 61-00-00.
SDR R025878Clamp · cracked838-67 CLAMP ASSY SN EF3099. CRACK FOUND INTERSECTING THE THREADED LINK SCREW HOLE.SDR HNAA0800109Propeller · out of balanceAIRCRAFT WAS EN ROUTE FROM LGA TO ORF, THE CAPTAIN NOTIFIED DISPATCH NORTH OF SBY THAT THE AIRCRAFT WAS ENCOUNTERING A MODERATE TO HEAVY PROPELLER VIBRATION AT ALL RPM SETTINGS. THE AIRCRAFT WAS DIVERTED TO SBY. IT WAS DETERMINED THAT NR 2 PROPELLER WAS CAUSSDR SJ3R025859Fork · crackedCRACK INDICATIONS FOUND DURING MAG PARTICLE INSPECTION. CRACKS ARE LOCATED ON THE THIN SIDE OF ALL (4) FORK SLOTS RADI.SDR SWIA200819206Signal Cond Unit · malfunctionedLEFT PROP AUTO FEATHERED UNCOMMANDED WHILE EXITING THE RUNWAY, FLIGHT NR 3715. REPLACED TORQUE SIGNAL CONDITIONER IAW EMB MM 77-12-00, PN 30005-0000-52, SN OFF 2229.
SDR SJ3R080124001Cam Follower · brokenREMOVED DUE TO SUSPECTED INTERNAL HUB COMPONENT FAILURE. BLADE S/N 4152 WAS FOUND TO ROTATE FREELY +/- 12.5 DEGREE POST FIRST GROUND RUN AFTER INSTALLATION. INSPECTION AFTER DISASSEMBLY REVEALED ONE BROKEN B-6545 PITCH CHANGE KNOB CAM FOLLOWER. THIS PART WASSDR CA080122007Propeller · leaking(CAN) AFTER START UP AND REPOSITION OF AC FOR FUEL, A HYD LEAK WAS NOTED FROM THE PROPELLER, RUNNING FROM THE BLADE ROOT TO THE BLADE TIP. THE PROPELLER WAS REMOVED AND ROUTED TO A OVERHAUL SHOP FOR REPAIR. (TC NR 20080122007)SDR CA071212026Flange · cracked(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION IAW AD 2003-12-05. A SMALL CRACK WAS LOCATED RADIALLY AT THE EDGE OF ONE MOUNTING BOLT HOLE. TIME SINCE LAST INSPECTED FOR AD 2003-12-05 WAS 409.2 HOURS. (TC NR 20071212026)SDR CA071126002Diaphragm · split(CAN) RUBBER ON DIAPHRAM WAS FOUND SPLIT AT INNER SECTION. UNCERTAIN AS TO WHY THE RUBBER APPEARED STIFFER THAN THE PREVIOUS DIAPHRAM. THE DIAPHRAM IS BEING RETURNED TO MFG FOR INSP. WILL UPDATE WHEN RECEIVE THE INFORMATION BACK FROM THE MFG. (TC NR 200711260SDR CA071106008Retainer · cracked(CAN) WHILE ENGINE WAS BEING REPLACED MAINTENANCE NOTICED FATIQUE CRACKS EMINATING FROM THE (PROP SHAFT) RETAINING BOLT AREA. (TC NR 20071106008)SDR CA070910001Propeller · corroded(CAN) WHILE PERFORMING A 5 YEAR CORROSION INSPECTION ON SUBJECT PROPELLER IAW CAR 625 APPENDIX C, PARA.5, CORROSION WAS NOTED IN THE MOUNTING HOLE BORE. IN CONSULTATION WITH THE PROPELLER OVERHAUL AMO, IT WAS DECIDED TO SEND IT TO THEM FOR FURTHER EVALUATION. SDR R0240301Bracket · crackedFIVE B-3493 START LOCK BRACKETS WERE FOUND DURING PENETRANT INSPECTION TO BE CRACKED AT THE SAME LOCATION. CRACKS ARE LOCATED ON THE EXTERIOR START PIN BORE NEXT TO THE SPINNER MOUNTING BOLT RELIEF CUT-OUT. THIS BRACKET IS PART OF THE 830-34L START LOCK UNIT ISDR CA070824006Seal · torn(CAN) CREW NOTICED A LARGE AMOUNT OF OIL ON THE LT NACELLE WHICH APPEARED TO ORIGINATE FROM THE PROPELLER. THE ENGINE WAS SHUTDOWN DUE TO THE EXCESSIVE LEAKAGE AND THE AIRCRAFT RETURNED TO BASE. THE PROPELLER NR 1 BLADE SEAL WAS REPLACED AND GROUND LEAK CHECKSDR CA070815002Seal · missing(CAN) PROPELLER WAS RECEIVED BY SHOP BECAUSE OF GREASE LEAKAGE AROUND BLADE CLAMPS. UPON DISASSEMBLY TO PERFORM REPAIRS IT WAS NOTICED THAT THE DUST SEAL WAS MISSING FROM THE PROPELLER PISTON ASSEMBLY. SINCE THIS ITEM CAN`T PHYSICALLY FALL OUT IT IS ASSUMED THSDR CA070816001Connector · unsecure(CAN) ENGINE NR 1 RPM UNSTABLE, REDUCED RPM TO 13,600. AIRCRAFT DIVERTED TO NEAREST AIRPORT. ENGINE WAS SHUTDOWN IN FINAL APPROACH, DUE TO RPM REDUCTION TO 13500 RPM. MAINTENANCE WAS SENT ON SITE AND FOUND THAT OIL PROPELLER FILLER PLUG WAS NOT SECURED PROPESDR EY2R0097613Bearing · corrodedPROPELLER BLADE BEARING CORRODED.SDR 0097614Bearing Race · corrodedBEARING RACE CORROSION.SDR 0097442Dome · corrodedDOME CORRODED.SDR 2007FA0000693Bolt · loosePILOT REPORTED SLIGHT VIBRATION DURING FLIGHT OF APPROX (1) HOUR. WHEN POWER WAS REDUCED FOR LANDING, VIBRATION BECAME MORE EVIDENT. INITIAL INSP FOUND (1) PROP BOLT HAD COME OUT FWD AND THROUGH SPINNER AND PROP WAS LOOSE. WITH REMOVAL OF SPINNER, FOUND (2)SDR 2007FA0000443Rod · failedRECEIVED PROPELLER FOR OVERHAUL. DURING PREFUNCTION TEST FOUND BLADE NR 1 WAS NOT LINKED TO THE PITCH CHANGE ROD. AFTER DISASSEMBLY OF PROPELLER FOUND NR 1 BLADE ACTUATING PIN PN B5072-1 DISCONNECTED FROM BLADE. ACTUATING PIN ATTACHMENT SCREWS WERE SAFETIED ANSDR 2007FA0000456Fork · unserviceableSTEEL FATIGUE CRACK NDT (MAGNETIC PARTICLE) DETECTED. PROPELLER ASSY RECEIVED FOR STANDARD OVERHAUL AND DEFECT FOUND IN PROPELLER ASSY (PN C2K00500, DESCRIPTION HC-C2YK-2CUF/FC8477A-4, SN AU9949B), UNDER WO NR 38425A.SDR DATA200700004Bolt · looseDURING INSPECTION OF AD 2006-22-12 TWO PROPELLER BOLTS WERE FOUND LOOSE. REPLACED PROPELLER BOLTS AND PROPELLER ASSEMBLY.SDR R022366Seal Ring · debondedTEFLON (BLADE SEAL) DEBONDED FROM THE SHANK OF BLADE SN A0336 CAUSING GREASE LEAK.SDR CA070322010Tape · blistered(CAN) DURING VISUAL INSP, IT WAS FOUND THAT THE TAPE USED ON THE L/E OF THIS PROP WHICH WAS INSTALLED BY THE MFG UNDER SPECIFICATION SP-127 WAS STARTING TO BLISTER AND SEPERATE FROM THE L/E, WORSE AT THE TIPS. TAPE WAS REMOVED AND LOG ENTRIES CARRIED OUT. NO WSDR QXEA200700246Unknown · unknownBOI FLIGHT NR 2202 - DURING NR 1 BETA LOCK-OUT TEST PROP GROUND RANGE LIGHT ILLUMINATES IMMEDIATELY WHEN BRINGING POWER LEVER TO DISC BEFORE PUSHING TEST BUTTON ON PROP RPM GAUGE. MAINTENANCE RESET BETA LOCK-OUT. NO PART REPLACED. OPERATIONAL CHECK GOOD. ASDR CA070209004Propeller · leaking(CAN) DURING FLIGHT OIL WAS NOTICED ON THE WINDSCREEN WHILE ON ROUTE. UPON INSPECTION AFTER LANDING, MAINTENANCE FOUND EXCESSIVE OIL ON ENGINE COWLING. PROP WAS REMOVED AND SENT FOR REPAIRS. REPAIR SHOP CHANGED ALL THE INTERNAL SEALS AND RETURNED THE PROP. REPSDR CA070118004Plate · cracked(CAN) PROPELLER RECEIVED FROM CUSTOMER FOR ROUTINE OVERHAUL. PROPELLER DISMANTLED, PARTS NDT INSPECTED AND CRACK FOUND. NO AD`S OR BULLETIN`S ON THAT PART. (TC NR 20070118004)SDR CA070111010Propeller · damaged(CAN) PROPELLER WAS RECEIVED FOR COMPLIANCE WITH AD 2006-24-07. PROPELLER PREVIOUSLY OVERHAULED ON SEPTEMBER 20, 2000. THE PROPELLER WAS DISSASSEMBLED AND THE FOLLOWING FINDINGS WERE CORRECTED. (4) LOW STOP RODS WERE CORRODED BEYOND REPAIR. (4) BLADE CLAMP ASSDR 2006FA0001228Clamp · crackedDURING A ROUTINE PRE-FLIGHT INSPECTION OF PROPELLER ASSY, A CRACK WAS IDENTIFIED ON BLADE CLAMP PN D-6831-5A, REV K, SN 3194A. PROP WAS REMOVED FROM AC FOR FURTHER INSPECTION. INSPECTION CONFIRMED OPERATOR IDENTIFIED DEFECT AND PART FORWARDED FOR FURTHER EVASDR CA070226003Propeller · corroded(CAN) PROP COME IN FOR 10 YEAR OVERHAUL. PIS, CLEAN, NDT, VISUAL INSPECTION, LUB UNSERVICEABLE DUE TO RUST. LINK ARMS P/N 861-3C WORN UNSERVICEABLE, P/N A971 BEARING CORRODED UNSERVICEABLE P/N VL9333C-5 BLADE BORES CORRODED HAD TO BE REAMED AND RE-SHOT PEENED.SDR SJ3R021444Bearing · brokenBLADE POSITION 4, S/N 1091 THRUST BEARING BROKEN. DAMAGE TO PROPELLER HUB BLADE SOCKET NR 4 IS BEYOND REPAIRABLE LIMITS. MFG SB 287 HAS NOT BEEN PERFORMED ON THIS PROPELLER.SDR CA061205006Shim · broken(CAN) AFTER LANDING, A POST-FLIGHT INSPECTION REVEALED AN OIL LEAK IN THE NR1 PROP. FURTHER INVESTIGATION SHOWED THAT THE BLADE SHIMS HAD BEEN INSTALLED ON THE WRONG SIDE OF THE BLADE RETAINING RING. THE SHIMS HAD BROKEN AND DAMAGED THE OIL SEALS. THE OTHER 3 SDR CA061219014Seal · leaking(CAN) DURING CRUISE, THE ENGINE OIL PRESSURE BEGAN TO FLUCTUATE IN THE RED BAND. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED A LEAK AT THE PROP SHAFT OIL SEAL. MFG WILL INVESTIGATE THE EVE
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