Rolls-Royce 250-C28
Service difficulty reports · 70
Newest first. General aviation reporting is voluntary.
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.
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
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 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 FUSDR C9PA201711030001Packing · leakingPILOT DETECTED FUEL ODOR IN CABIN. FOUND THE FUEL SWITCH PACKING LEAKING.SDR YTRA2016060715801Fuel Control · failedIN THE COURSE OF A PRACTICE AUTOROTATION, THE ENGINE FLAMED OUT WHEN THE THROTTLE WAS ROLLED TO THE IDLE DETENT POSITION.SDR 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.SDR EVCA201304220040Bulkhead · crackedRT BULKHEAD ASSY AT FS 146 CRACKED AT INBD SECTION NEAR THE BOX BEAM ASSY.SDR EVCA201304230041Channel · crackedAT FS 155 CHANNEL CRACKED AT BOTH ENGINE MOUNT ATTACHMENT FITTINGS.SDR CA121106008Magnetic Seal · leaking(CAN) MAIN ROTOR TRANSMISSION INPUT MAG SEAL LEAKING. SEAL REPLACED.SDR 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.SDR 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 CALLSDR 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.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 NOTSDR 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.SDR EVCA00003Support · crackedDURING A ROUTINE INSP, MECHANIC FOUND RT (PILOT) SUPPORT ASSY CRACKED. SUPPORT ASSY R & R.SDR EVCA731DAttach Fitting · crackedDURING A ROUTINE INSP, MX FOUND UPPER LT ATTACHMENT FITTING ON FUSELAGE AFT BULKHEAD CRACKED. ATTACHMENT FITTING R & R.SDR 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)SDR CA070706004Fuel Control · unserviceable(CAN) FUEL CONTROL WAS INTERMITTENT ON ENGINE LIGHT-OFF DURING A START. FUEL CONTROL CHANGED OUT. (TC NR 20070706004)SDR CA070601003Fuel Cell · leaking(CAN) FUEL SMELL NOTED. INSPECTION FOUND SMALL FUEL LEAK. FUEL CELL REMOVED SENT OUT FOR REPAIR, REINSTALLED. (TC NR 20070601003)SDR 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)SDR 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)SDR 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 FLANGSDR 2005FA0001637Oil Tank · leaking206-061-505-109 ENGINE OIL RESERVOIR BEGAN TO LEAK ENGINE OIL.SDR 2005FA0001638Oil Tank · leaking206-061-505-109 ENGINE OIL RESERVOIR BEGAN TO LEAK ENGINE OILSDR B65A106298Shield · brokenSHIELD, BROKEN AND REPLACED.SDR B65A106299Shield · brokenSHIELD, BROKEN AND REPLACED.SDR B65A106300Shield · brokenSHIELD, BROKEN AND REPLACED.SDR CA051018006Restraint · delaminatedDELAMINATION FOUND ON AFT TRANSMISSIN MOUNT ELASTOMERIC. MOUNT CHANGED.SDR B65A106278Hydraulic System · leakingLEAKING HYDRAULIC UNIT.SDR B65A106130Meter · unserviceableTORQUE KEEPS FLUCTUATING.SDR B65A106213Control Unit · unserviceableCONTROL UNIT IS CAUSING AN UNCONTROLLABLE LATERAL INPUT.SDR 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 DSDR YTRR104956Fuel Filter · crackedFILTER HEAD WEBBING INSIDE WAS CRACKED. REPLACED FILTER HEAD ASSY.SDR CA050706009Cartridge · noisy(CAN) FUEL BOOST PUMP MAKING NOISES. PUMP CHANGED.SDR 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 RESETSDR HE66100341Firewall · crackedFIREWALL IS CRACKED BY FASTNERS AND HAS BEEN REPAIRED SEVERAL TIMES BEFORE. INTEGRITY IS COMPROMISED AND DO NOT WANT ENGINE TO INGEST FOD.SDR HE66100337Skid · unserviceableRIVETS PULLED AND GOUGES IN BOTTOM OF TUBE.SDR HE66099998Starter Gen · unserviceableNR 2 ENG FAILED TO START. STARTER GENERATOR UNSERVICEABLE.SDR PG9R97953Fuel Nozzle · crackedFUEL NOZZLE SPRAY SHROUD CRACKED. A NEW MATERIAL SHOULD BE USED FOR THE SPRAY SHROUD. (K)SDR HE66097817Torquemeter · unserviceableFLUCTUATING OVER 40 PERCENT WITH NO CHANGE IN N1 OR TOT.SDR HE66097244Bearing · wornBEARINGS ARE WORN CAUSING EXCESSIVE PLAY.SDR HE66096553Seat · tornSEAT TORN, CUSHION HAS NO SUPPORT.SDR HE66096552Seat · crushedCRUSHABLE SEATS WERE CRUSHED.SDR HE66096545Pressure Switch · unserviceablePRESSURE SWITCH FAILED AND REPLACED.SDR ALGA093984Blade · corrodedFOUND MAIN ROTOR TRAILING EDGE EXTRUSION EXFOLIATED APPROXIMATELY 2.5.SDR 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 GROUSDR 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 GREASSDR 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. MAINTENANCSDR 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.SDR HE66084852Igniter Box · defectiveNR 1 ENGINE WOULD NOT START, EXCITER BOX WAS NOT PUTTING OUT REPLACEDSDR 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.SDR HEEA083304Bleed Valve · failedLOUD BANG FROM COMPRESSOR ON TAKEOFF FOLLOWED BY 4 MORE BANGS. REPLACED WITH SERVICEABLE BLEED VALVE.
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