Rolls-Royce 250-C28

Service difficulty reports · 70

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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 engine_model_key = '250C28'
  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 EVCA201811271Engine · flamed outENGINE FAILED WHEN THROTTLE ROLLED TO IDLE DURING AUTOROTATION SPEED CHECK. PERFORMED AUTOROTATION LANDING. AIRCRAFT WAS INSPECTED WITH NO FUEL LEAKS. PERFORMED FUEL FLOW CHECKS WITH NO DEFECTS NOTED. REPLACED ENGINE AND FUEL MANIFOLD. INSPECTED AND CLEANED FUNov 24, 2018 · N96AE · Bell 206L1 · Engine (Turbine/Turboprop)SDR C9PA201711030001Packing · leakingPILOT DETECTED FUEL ODOR IN CABIN. FOUND THE FUEL SWITCH PACKING LEAKING.Nov 3, 2017 · N305CH · Bell 206L1 · Fuel Selector/Shut-Off ValveSDR YTRA2016060715801Fuel Control · failedIN THE COURSE OF A PRACTICE AUTOROTATION, THE ENGINE FLAMED OUT WHEN THE THROTTLE WAS ROLLED TO THE IDLE DETENT POSITION.Jun 6, 2016 · N2611 · Bell 206L1 · Fuel Control/Reciprocating EnginesSDR CA150327010Skid · cracked(CAN) DURING REMOVAL OF GROUND HANDLING WHEELS THE RT SKID TUBE WAS FOUND TO BE CRACKED AROUND THE COMPLETE CIRCUMFERENCE OF THE SKID TUBE AT THE FORWARD GROUND HANDLING WHEEL ATTACHMENT.Mar 26, 2015 · Bell 206B · Wheel/Ski/FloatSDR EVCA201304220040Bulkhead · crackedRT BULKHEAD ASSY AT FS 146 CRACKED AT INBD SECTION NEAR THE BOX BEAM ASSY.Apr 22, 2013 · N176AE · Bell 206L1 · Fuselage Main, BulkheadSDR EVCA201304230041Channel · crackedAT FS 155 CHANNEL CRACKED AT BOTH ENGINE MOUNT ATTACHMENT FITTINGS.Apr 22, 2013 · N176AE · Bell 206L1 · Fuselage Miscellaneous StructureSDR CA121106008Magnetic Seal · leaking(CAN) MAIN ROTOR TRANSMISSION INPUT MAG SEAL LEAKING. SEAL REPLACED.Nov 4, 2012 · Bell 206B · Main Rotor GearboxSDR 3HCR03222012Bushing · misinstalledGOVERNOR ALLOWS ENGINE TO OVERSPEED. FAILED SHOP TEST. DIASSEMBLED AND FOUND UNIT IMPROPERLY ASSEMBLED. SPOOL BUSHING ANTI-ROTATION TANG WAS ENGAGED IN LEVER SLOT.Mar 22, 2012 · N2611 · Bell 206L1 · Turbine GovernorSDR 2011FA0000574Stud · wornACFT WAS IN CRUISE FLT, PILOT NOTICED OIL PRESSURE DEMINISHING, PILOT INITIATED LANDING. ONCE ACFT WAS ON THE GROUND PILOT NOTICED OIL PRESSURE AT FLUCTUATING FROM ZERO TO 30 PSI, AND ALSO NOTICED SMOKE COMING FROM ENGINE. ENGINE WAS SHUTDOWN AND MX WAS CALLSep 3, 2011 · N3895D · Bell 206L1 · Turbine Engine Oil SystemSDR YTRA1105401Engine · malfunctionedIN CRUISE FLIGHT THE PILOT REPORTED HIGH FREQUENCY VIBRATION AND WHINING NOISE FROM THE ENGINE COMPARTMENT. THIS WAS FOLLOWED BY AN ENGINE CHIP LIGHT INDICATION AND NOISE AT WHICH POINT THE ENGINE LOST POWER AND PROCEDED TO SHUT DOWN.Feb 22, 2011 · N2611 · Bell 206L1 · Engine (Turbine/Turboprop)SDR EVCA00007Chin Bubble · detachedAPPROX 3 NM NW OF AIRPORT HEARD A NOISE. A FEW MOMENTS PASSED AND THEN THERE WAS A "POP", A QUICK PRESSURE CHANGE AND AIRFLOW INTO THE COCKPIT. DISCOVERED THE GAPING HOLE WHERE THE CHIN BUBBLE SHOULD BE INSTALLED. IMMEDIATELY TURNED TOWARD THE AIRPORT AND NOTSep 21, 2010 · N138AE · Bell 206L1 · Flight Compartment WindowsSDR EVCA00006Bulkhead · crackedDURING A ROUTINE INSP, MECHANIC FOUND CRACK ON BULKHEAD STA NR 142, WL 61, ON THE RT SIDE GENERATING FROM A NUTPLATE SCREW LOCATION.Jun 2, 2010 · N138AE · Bell 206L1 · Fuselage Main, BulkheadSDR EVCA00003Support · crackedDURING A ROUTINE INSP, MECHANIC FOUND RT (PILOT) SUPPORT ASSY CRACKED. SUPPORT ASSY R & R.Apr 24, 2010 · N176AE · Bell 206L1 · Fuselage Main, StructureSDR EVCA731DAttach Fitting · crackedDURING A ROUTINE INSP, MX FOUND UPPER LT ATTACHMENT FITTING ON FUSELAGE AFT BULKHEAD CRACKED. ATTACHMENT FITTING R & R.Mar 9, 2010 · N176AE · Bell 206L1 · Fuselage Main, Attach FittingsSDR CA070706002Scroll · warped(CAN) DURING A GROUND RUN AN AIR LEAK WAS FOUND AT THE SCROLL DIFFUSER SPLIT LINE. COMPRESSOR ASSY WAS CHANGED OUT. (TC NR 20070706002)Jul 5, 2007 · Bell 206L1 · Turbine Engine Compressor SectionSDR CA070706004Fuel Control · unserviceable(CAN) FUEL CONTROL WAS INTERMITTENT ON ENGINE LIGHT-OFF DURING A START. FUEL CONTROL CHANGED OUT. (TC NR 20070706004)Jul 5, 2007 · Bell 206L1 · Fuel Controlling SystemSDR CA070601003Fuel Cell · leaking(CAN) FUEL SMELL NOTED. INSPECTION FOUND SMALL FUEL LEAK. FUEL CELL REMOVED SENT OUT FOR REPAIR, REINSTALLED. (TC NR 20070601003)May 28, 2007 · Bell 206L1 · Fuel StorageSDR CA070404007Fuel Cell · leaking(CAN) RETURNING FROM A FLIGHT IT WAS NOTED THERE WAS A FUEL ODOR IN THE REAR CABIN. INVESTIGATING DETERMED THE LT FWD FUEL CELL HAD A SMALL LEAK. FUEL CELL WAS CHANGED OUT. (TC NR 20070404007)Apr 4, 2007 · Bell 206L1 · Fuel StorageSDR CA060808005Scroll · cracked(CAN) HIGH TOT WAS NOTICED IN CRUISE. ON RETURNING A POWER CHECK WAS CARRIED OUT AND LOW POWER WAS DETECTED. A HAIT LINE CRACK WAS IDENTIFIED BY VISUAL INSPECTION IN THE ELBOW AREA OF SCROLL. COMPRESSOR CHANGED. (TC NR 20060808005)Jul 19, 2006 · Bell 206L1 · Turbine Engine Compressor SectionSDR B652006F00000Bolt · shearedDURING COURSE OF AN ACCIDENT INVESTIGATION, IT WAS NOTED THAT BOLTS THAT CONNECT TAIL ROTOR DRIVE SHAFT TO INPUT THOMAS COUPLING OF INTERMEDIATE GEARBOX WERE SHEARED. SHEARING TOOK PLACE JUST BELOW GRIP LENGTH AREA OF BOLT . SHEARED BOLTS WERE STILL IN FLANGApr 13, 2006 · N202LF · Bolkms BO105LSA3 · Tail Rotor GearboxSDR 2005FA0001637Oil Tank · leaking206-061-505-109 ENGINE OIL RESERVOIR BEGAN TO LEAK ENGINE OIL.Nov 16, 2005 · N2009C · Bell 206L1 · Turbine Engine Oil SystemSDR 2005FA0001638Oil Tank · leaking206-061-505-109 ENGINE OIL RESERVOIR BEGAN TO LEAK ENGINE OILNov 16, 2005 · N2009C · Bell 206L1 · Turbine Engine Oil SystemSDR B65A106298Shield · brokenSHIELD, BROKEN AND REPLACED.Oct 12, 2005 · N202LF · Bolkms BO105LSA1 · Main Rotor SystemSDR B65A106299Shield · brokenSHIELD, BROKEN AND REPLACED.Oct 12, 2005 · N202LF · Bolkms BO105LSA1 · Main Rotor SystemSDR B65A106300Shield · brokenSHIELD, BROKEN AND REPLACED.Oct 12, 2005 · N202LF · Bolkms BO105LSA1 · Main Rotor SystemSDR CA051018006Restraint · delaminatedDELAMINATION FOUND ON AFT TRANSMISSIN MOUNT ELASTOMERIC. MOUNT CHANGED.Oct 12, 2005 · Bell 206L1 · Main Rotor Transmission MountSDR B65A106278Hydraulic System · leakingLEAKING HYDRAULIC UNIT.Sep 29, 2005 · N202LF · Bolkms BO105LSA1 · Hydraulic System, MainSDR B65A106130Meter · unserviceableTORQUE KEEPS FLUCTUATING.Sep 21, 2005 · N202LF · Bolkms BO105LSA1 · Engine BMEP/Torque IndicatingSDR B65A106213Control Unit · unserviceableCONTROL UNIT IS CAUSING AN UNCONTROLLABLE LATERAL INPUT.Sep 21, 2005 · N202LF · Bolkms BO105LSA1 · Rotorcraft Flight ControlSDR CA051004004Contactor · burned(CAN) DURING CRUISE PORTION OF A SHORT (15 MIN) CREW TRANSFER FLIGHT, THE PILOT AND 2 PASSENGERS ABOARD SMELLED/SAW FUMES/SMOKE IN COCKPIT. ELECTRICAL SYSTEMS WERE SHUTDOWN AND AN UNEVENTFUL LANDING WAS CARRIED OUT NEAR CAMP SITE. UPON INVESTIGATI ON, IT WAS DSep 6, 2005 · Bell 206L1 · Battery/Charger SystemSDR YTRR104956Fuel Filter · crackedFILTER HEAD WEBBING INSIDE WAS CRACKED. REPLACED FILTER HEAD ASSY.Jul 25, 2005 · N397RL · Bell 206L1 · Aircraft Fuel Filter/StrainerSDR CA050706009Cartridge · noisy(CAN) FUEL BOOST PUMP MAKING NOISES. PUMP CHANGED.Jun 27, 2005 · Bell 206L1 · Fuel Boost PumpSDR B652005F00000Switch · stuckWHEN PERFORMING THE FUNCTIONAL TEST OF THE HYDRAULIC SYSTEM, CHAPTER 43-14, PG 24 OF THE MM. UNABLE TO GET THE HYDRAULIC UNIT TO SWITCH OVER TO THE NR 2 POSITION. DURING THE INVESTIGATION, IT WAS OBSERVED THAT THE HYDRAULIC TEST SWITCH WAS STUCK IN THE RESETMay 20, 2005 · N202LF · Bolkms BO105LSA3 · Hydraulic System, MainSDR HE66100341Firewall · crackedFIREWALL IS CRACKED BY FASTNERS AND HAS BEEN REPAIRED SEVERAL TIMES BEFORE. INTEGRITY IS COMPROMISED AND DO NOT WANT ENGINE TO INGEST FOD.Apr 17, 2005 · N202LF · Bolkms BO105LSA1 · Nacelle/Pylon, Bulkhead/FirewallSDR HE66100337Skid · unserviceableRIVETS PULLED AND GOUGES IN BOTTOM OF TUBE.Apr 16, 2005 · N202LF · Bolkms BO105LSA1 · Wheel/Ski/FloatSDR HE66099998Starter Gen · unserviceableNR 2 ENG FAILED TO START. STARTER GENERATOR UNSERVICEABLE.Mar 24, 2005 · N202LF · Bolkms BO105LSA1 · Starter-GeneratorSDR PG9R97953Fuel Nozzle · crackedFUEL NOZZLE SPRAY SHROUD CRACKED. A NEW MATERIAL SHOULD BE USED FOR THE SPRAY SHROUD. (K)Nov 5, 2004 · N3895D · Bell 206L1 · Fuel Injector NozzleSDR HE66097817Torquemeter · unserviceableFLUCTUATING OVER 40 PERCENT WITH NO CHANGE IN N1 OR TOT.Oct 21, 2004 · N202LF · Bolkms BO105LSA1 · Engine BMEP/Torque IndicatingSDR HE66097244Bearing · wornBEARINGS ARE WORN CAUSING EXCESSIVE PLAY.Sep 10, 2004 · N202LF · Bolkms BO105LSA1 · Tail Rotor Control SystemSDR HE66096553Seat · tornSEAT TORN, CUSHION HAS NO SUPPORT.Jul 29, 2004 · N202LF · Bolkms BO105LSA1 · Flight Compartment EquipmentSDR HE66096552Seat · crushedCRUSHABLE SEATS WERE CRUSHED.Jul 21, 2004 · N202LF · Bolkms BO105LSA1 · Flight Compartment EquipmentSDR HE66096545Pressure Switch · unserviceablePRESSURE SWITCH FAILED AND REPLACED.Jul 16, 2004 · N202LF · Bolkms BO105LSA1 · Engine Oil PressureSDR ALGA093984Blade · corrodedFOUND MAIN ROTOR TRAILING EDGE EXTRUSION EXFOLIATED APPROXIMATELY 2.5.Mar 21, 2004 · N2611 · Bell 206L1 · Main Rotor BladesSDR ALG2004F00001B-Nut · looseIN FLIGHT SMELLED SLIGHT ODOR OF FUEL. ON POST FLIGHT SAW DRIPS OF FUEL ON LINES AROUND FUEL CONTROL. MAINTENANCE FOUND B-NUT ON FUEL CONTROL INLET FROM PUMP SEEPING. LOOSENED NUT, CLEANED FITTING AND RETORQUED NUT. LEAKED CHECKED WITH BOOST PUMPS AND GROUNov 11, 2003 · N211EL · Cessna STC206C · Engine Fuel DistributionSDR 2003FA0001118Bearing · failedDURING ROUTINE DAILY INSPECTION OF HELICOPTER USED IN EMS, MECHANIC NOTICED NR 5 TAIL ROTOR BEARING GREASE SEAL HAD SEPARATED FROM BEARING. FRAGMENTS OF THE PHENOLIC BEARING CAGE WERE MISSING FROM BEARING ASSY. MECHANIC REPORTED NO EVIDENCE OF RESIDUAL GREASOct 17, 2003 · N25RX · Agusta A109 · Tail Rotor Drive SystemSDR ALG2003F00081Engine · failedDURING TAKE OFF, THE PILOT CALLED ON THE PHONE AND REPORTED THAT DURING TAKE OFF AND CLIMB AFTER FUELING, THE AIRCRAFT EXPERIENCED FOUR LOUD BANGS AND ENGINE CHIP LIGHT. PILOT MADE A 360 DEGREE TURN AND LANDED AT SMI-128A AND SHUT THE ENGINE DOWN. MAINTENANCAug 27, 2003 · N1067D · Cessna STC206C · Engine (Turbine/Turboprop)SDR CA030528005Frame · cracked(CAN) CRACK FOUND IN AFT FUSELAGE FRAME. CRACK APPROXIMATELY .3750 INCH IN LENGTH LOCATED ABOVE UPPER RT TAILBOOM ATTACH BOLT MOUNTING BOLT HOLE. FOUND DURING 1200 HR TAILBOOM INSPECTION AND ONLY VISIBLE WITH 10X POWER GLASS. FRAME REPLACED WITH NEW.May 12, 2003 · Bell 206L1 · Rotorcraft Tail BoomSDR HE66084852Igniter Box · defectiveNR 1 ENGINE WOULD NOT START, EXCITER BOX WAS NOT PUTTING OUT REPLACEDFeb 28, 2003 · N202LF · Bolkms BO105LSA1 · Induction VibratorSDR CA030204014Lever · failed(CAN) REQUIRED BOLT PN NAS6604D8 (AS PER 206L IPC) WOULD NOT FIT IN EXISTING HOLE OF FUEL CONTROL LEVER PN 206064713101 WITHOUT ENLARGING HOLE.Jan 20, 2003 · Bell 206L · Fuel Controlling SystemSDR HEEA083304Bleed Valve · failedLOUD BANG FROM COMPRESSOR ON TAKEOFF FOLLOWED BY 4 MORE BANGS. REPLACED WITH SERVICEABLE BLEED VALVE.Jan 9, 2003 · N2759U · Bell 206L1 · Compressor Bleed Valve
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