Beech C90

Service difficulty reports · 278

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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 aircraft_model_key = 'C90'
  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 2015FA0000285Attach Fitting · crackedRIGHT UPPER FWD WING BOLT FITTING CRACKED.Jun 24, 2015 · N96DQ · Beech C90 · Fuselage, Wing Attach FittingsSDR 7AJA201503020001Panel · burnedPILOT SMELLED BURNING ODOR AND SAW SMOKE IN COCKPIT IN FLIGHT, 20 MINS FROM DESTINATION. PILOT OPENED ADF CB IN ASSUMING IT WAS THAT CB THAT WAS SMOKING. INSPECTION REVEALED CO-PILOT SIDE STORM WINDOW WAS NOT PROPERLY SECURED THUS LEAKING RAIN WATER ON TO CB Mar 1, 2015 · N438CA · Beech C90 · Electrical Power SystemSDR VQMA20150224001Heat Exchanger · crackedWHILE CLIMBING TO FL220, THE CABIN HEAT WAS TURNED UP. THE TEMP CONTROL KNOB WAS POSITIONED TO THE 6 O'CLOCK POSITION AS THE ACFT CLIMBED THROUGH 10,000 FT. WITHIN ONE MINUTE OR SO, THE FLIGHT CREW BEGAN TO NOTICE AN ODOR IN THE FLIGHT DECK. AFTER APPROX ONFeb 24, 2015 · N122K · Beech C90 · Heating SystemSDR 7AJA20150219011Powerpack · faultyACFT WAS ON FINAL APPROACH WHEN DURING LG EXTENSION THE SYS CB TRIPPED DURING THE FINAL PHASE OF THE EXTENSION CYCLE. THE LG EMER HAND PUMP WAS UTILIZED TO FINISH THE GEAR EXTENSION LOCK. THE GEAR DOWN WAS CONFIRMED BY THREE GREEN INDICATION LIGHTS. THE ACFFeb 17, 2015 · N588SA · Beech C90 · Hydraulic Pump (Electric/Engine), MainSDR E81R2015021640672Bolt · crackedDURING SCHEDULED INSPECTION OF THE WING STRUCTURE IAW THE SRM 57-13-01, LIQUID PENETRANT INSPECTION OF THE RT OTBD WING LOWER AFT ATTACH BOLT SHOWED A POSSIBLE CRACK INDICATION AROUND THE HEAD AREA. AVAILABLE RECORDS SHOW OTBD WING ATTACH BOLTS WERE INSTALLEDFeb 16, 2015 · N48AZ · Beech C90 · Wing Main, Frame StructureSDR CA141201007Actuator · failed(CAN) SHORTLY AFTER SCHEDULED MAIN GEAR ACTUATOR REPLACEMENT THE GEAR WAS FOUND RETRACTING SLOWLY IN FLIGHT. AT ONE POINT THE GEAR STALLED OUT AND HAD TO BE CYCLED IN ORDER TO GET IT TO FULLY RETRACT. UPON INSPECTION IT WAS FOUND THAT THE RT ACTUATOR HAD A GNov 24, 2014 · Beech C90 · Landing Gear ActuatorSDR 2014FA0000421Downlock Switch · out of rigON LOWERING THE LANDING GEAR, THE RT MLG GAVE UNSAFE INDICATION. PERFORMED EMERGENCY PROCEDURES, UNEVENTFUL LANDING. CHECKED HYD PAK, MOTOR, WIRING RELAYS NO DEFECTS FOUND. CHECKED RT MLG ACTUATOR AND MLG DOWNLOCK SWITCH AND FOUND TO BE WITHIN LIMITS BUT ALJul 10, 2014 · N13 · Beech C90 · Landing Gear Position and WarningSDR 2014FA0000390Landing Gear · inoperativeRT MLG DID NOT COME DOWN AND LOCK DURING NORMAL OPERATIONS. USED EMERGENCY EXTENTION TO LOWER GEAR DOWN AND MAKE SAFE. MADE UN-EVENTFUL LANDING.Jun 20, 2014 · N13 · Beech C90 · Landing Gear Retraction/Extension SystemSDR 2014FA0000204Wire · overheatedPILOT REPORTED, CABIN WENT TO MAXIMUM DIFERENTIAL PRESSURE DURING CLIMBOUT AND REMAINED AT MAXIMUM DIFERENTIAL THROUGHOUT THE FLIGHT. CABIN HAD TO BE MANUALLY DUMPED FOR DESCENT/LANDING. FOUND PLASTIC TUBING IN PEDESTAL, FROM CONTROLLER TO OUTFLOW VALVE, HAD Apr 1, 2014 · N48AZ · Beech C90 · Air Conditioning System WiringSDR CA140326014Fcu · malfunctioned(CAN) THE CUSTOMER CALLED AND ADVISED THAT THE PILOT WAS UNABLE TO REDUCE POWER BELOW 80 PERCENT ON 1 OF THE ENGINES, ESN TO BE CONFIRMED, THE PILOT FEATHERED THE ENGINE PRIOR TO LANDING, IFSD NOT CARRIED OUT. THE ON-GROUND TROUBLESHOOTING LEAD TO THE FUEL COMar 17, 2014 · Beech C90 · Fuel Control/Turbine EnginesSDR LJEA20140320001Fuel Control · faultyDURING DESCENT REDUCED POWER LEVERS TO IDLE, RT ENG WOULD NOT DECREASE BELOW 80 PERCENT N1, 500 PDS TORQUE, NORMAL SETTINGS 63 PERCENT & 100 PDS. INFORMED TOWER THAT WE HAD AN ENG ABNORMALITY & MAY NEED TO SHUT DOWN ON THE RUNWAY BUT DIDN'T NEED OTHER ASSISTAMar 17, 2014 · N964GB · Beech C90 · Fuel Control/Turbine EnginesSDR 2014FA0000102Warning Light · illuminatedLANDING GEAR UNSAFE LIGHT ILLUMINATED DURING LANDING.Feb 19, 2014 · N787TT · Beech C90 · Landing Gear Position and WarningSDR MFGA20140208011Engine · shutdownAIRCRAFT WAS FLYING WITHOUT PASSENGERS, ON DECENT ABOUT TEN MILES OUT FROM THE AIRPORT THE LT ENG SHUTDOWN. THE PILOTS REPORTED THAT PRIOR TO THE SHUTDOWN THERE WERE NO LIGHTS, NO ABNORMAL PARAMETERS ON ANY OF THE GAUGES, THE PROP FEATHERED & THEY LANDED UNEVEFeb 7, 2014 · N24GJ · Beech C90 · Engine (Turbine/Turboprop)SDR UA2R20131118015Channel · crackedDURING INSPECTION OF THE NR 2 ENGINE, THE FIRE SEAL ASSY OTBD CHANNEL LOWER FLANGE WAS FOUND CRACKED AND DEFORMED AT THE BOLT HOLES.Nov 12, 2013 · N12 · Beech C90 · Nacelle/Pylon Miscellaneous StructureSDR UA2R20131118014Channel · crackedDURING INSPECTION OF THE NR 2 ENGINE, THE FIRE SEAL ASSY INBD CHANNEL LOWER FLANGE WAS FOUND CRACKED AND DEFORMED AT THE BOLT HOLES.Nov 12, 2013 · N12 · Beech C90 · Nacelle/Pylon Miscellaneous StructureSDR UA2R20131118013Channel · crackedDURING INSPECTION OF THE NR 1 ENGINE, FIRE SEAL ASSY INBD CHANNEL LOWER FLANGE WAS FOUND CRACKED AND DEFORMED AT THE BOLT HOLES.Nov 12, 2013 · N12 · Beech C90 · Nacelle/Pylon Miscellaneous StructureSDR UA2R20131114012Channel · crackedDURING INSPECTION OF NR 1 ENGINE, FIRE SEAL ASSY OTBD CHANNEL LOWER FLANGE WAS FOUND CRACKED AND DEFORMED AT THE BOLT HOLES.Nov 12, 2013 · N12 · Beech C90 · Nacelle/Pylon Miscellaneous StructureSDR CA131021016Engine · unknown(CAN) ENGINE HAD AN EVENT DURING FLIGHT, CAUSING THE SHUTDOWN OF THE LT ENGINE. THE PILOT PERFORMED AN UNEVENTFUL SINGLE ENGINE LANDING.Oct 11, 2013 · Beech C90 · Engine (Turbine/Turboprop)SDR UA2R20131001011Channel · crackedDURING INSPECTION, FOUND NR 2 ENGINE OTBD FIRE SEAL CHANNEL CRACKED AT THE FOOT WHERE IT BOLTS TO THE LOWER AFT COWL.Oct 1, 2013 · N11 · Beech C90 · Nacelle/Pylon, Main FrameSDR UA2R20131001010Channel · crackedDURING INSPECTION, FOUND NR 2 ENGINE INBD FIRE SEAL CHANNEL CRACKED AT THE FOOT WHERE IT BOLTS TO THE LOWER AFT COWL.Oct 1, 2013 · N11 · Beech C90 · Nacelle/Pylon, Main FrameSDR UA2R20131001009Channel · crackedDURING INSPECTION, FOUND NR 1 ENGINE INBD FIRE SEAL CHANNEL CRACKED AT THE FOOT WHERE IT BOLTS TO THE LOWER AFT COWL.Oct 1, 2013 · N11 · Beech C90 · Nacelle/Pylon, Main FrameSDR UA2R20131001008Channel · crackedDURING INSPECTION, FOUND NR 1 ENGINE OTBD FIRE SEAL CHANNEL CRACKED AT THE FOOT WHERE IT BOLTS ATTACH TO THE LOWER AFT COWL.Oct 1, 2013 · N11 · Beech C90 · Nacelle/Pylon, Main FrameSDR UA2R20131001007Inlet · crackedDURING INSPECTION FOUND NR 1 ENGINE INLET CRACKED AT THE RIVET ATTACHING THE BRACKET FOR THE INLET HEAT DUCT. CRACKED WHERE THE INLET IS STARTING TO CURVE.Oct 1, 2013 · N11 · Beech C90 · Turbine Engine Air Inlet SectionSDR NXTA201309160001Cap · misinstalledFUEL LEAKING FROM RT NACELLE UPPER AREA BY FUEL CAP. DETERMINED UPPER NACELLE FUEL CAP WAS IMPROPERLY SEATED AFTER REFUEL.Sep 16, 2013 · N149CF · Beech C90 · Fuel StorageSDR UA2R20130912006Channel · crackedNR 1 ENGINE OTBD FIRE SEAL CHANNEL IS CRACKED AT THE FOOT WHERE IT BOLTS TO THE LOWER AFT COWL.Sep 4, 2013 · N15 · Beech C90 · Nacelle/Pylon Miscellaneous StructureSDR UA2R20130912005Channel · crackedNR 1 ENGINE INBD FIRE SEAL CHANNEL IS CRACKED AT THE FOOT WHERE IT BOLTS TO THE LOWER AFT COWL.Sep 4, 2013 · N15 · Beech C90 · Nacelle/Pylon Miscellaneous StructureSDR UA2R20130910004Duct · crackedDURING INSPECTION, FOUND NR 2 ENGINE FWD AIR INLET DUCT CRACKED AT THE OTBD RIVET THAT ATTACHES THE BRACKET FOR THE INLET HEAT DUCT. CRACKED WHERE THE INLET IS STARTING TO CURVE.Aug 29, 2013 · N15 · Beech C90 · Turbine Engine Air Inlet SectionSDR UA2R20130910003Duct · crackedDURING INSPECTION, FOUND NR 1 ENGINE FWD AIR INLET DUCT CRACKED AT THE INBD RIVET THAT ATTACHES THE BRACKET FOR THE INLET HEAT DUCT. CRACKED WHERE THE INLET IS STARTING TO CURVE.Aug 29, 2013 · N15 · Beech C90 · Turbine Engine Air Inlet SectionSDR 2013FA0000146Bolt · crackedFOUND RIGHT WING LOWER FORWARD WING BOLT CRACKED DURING DYE PENETRANT INSPECTION, CRACK WAS JUST BELOW THE BOLT HEAD RADIUS, INSTALLED NEW BOLTMar 5, 2013 · N332DE · Beech C90 · Wing StructureSDR UA2R20130207002Wheel · corrodedDISCOVERED CORROSION ON THIS MAGNESIUM WHEEL. FURTHER INVESTIGATION REVEALED CORROSION IN THE BEARING AREA (UNDER THE RACE) TO WHICH THERE ARE NO REPAIRABLE LIMITS. CONDEMNED THE WHEEL AND CONTACTED THE MANUFACTURER.Feb 6, 2013 · N15 · Beech C90 · Wheel/Ski/FloatSDR UA2R20130207001Fitting · crackedUPON INSPECTION FOUND HYDRAULIC LEAK COMING FROM MANUFACTURED FITTING GOING TO INLET SIDE OF HYDRAULIC PUMP. UPON EXAMINATION WITH AIRCRAFT HYDRAULIC PRESSURE ON PUMP, SAW FLUID COMING FROM SOLDERED JOINT IN FITTING WHERE IT IS BRAZED TOGETHER. ON DISASSEMBFeb 5, 2013 · N15 · Beech C90 · Hydraulic System, MainSDR 2012FA0000824Power Supply · burnedPASSENGER SMELLED AND SAW A SMALL AMOUNT OF SMOKE COMING FROM THE LT FORWARD FACING SEAT WINDOW FLUORESCENT LIGHT. FOUND FLUORESCENT LIGHT POWER SUPPLY ASSY MELTED AND BURNED.Dec 10, 2012 · N11SN · Beech C90 · Passenger Compartment LightingSDR CA120518003Engine · power loss(CAN) DURING DESCENT, PASSING THROUGH 1300 FT, THE ENGINE TEMPERATURE INCREASED RAPIDLY POWER WAS LOST. THE PILOT SHUT THE ENGINE DOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED AT TROUBLESHOOTING IS ONGOING.May 3, 2012 · Beech C90 · Engine (Turbine/Turboprop)SDR 5BMA20120418001Turbine Blades · failedTHE PILOT REPORTED THE FOLLOWING, DURING CLIMB AFTER TAKEOFF FROM KOMA AT APPROXIMATELY 11,000 MSL THE RIGHT ENGINE ABRUPTLY LOST POWER. TORQUE WENT TO ZERO, ITT RAPIDLY DISMINISHED. COMPLETED EMERGENCY MEMORY ITEMS PER MANUFACTURE'S CHECKLIST. SHUTDOWN ANDApr 6, 2012 · N4950 · Beech C90 · Turbine SectionSDR 3MI2012F00000Pressure Switch · failedOIL PRESSURE SWITCH QUIT WORKING.Mar 24, 2012 · N203BK · Beech C90 · Engine Oil PressureSDR 2012FA0000176Transducer · failedRT ENGINE OIL PRESSURE TRANDUCER QUIT WORKING DURING CLIMB OUT.Mar 24, 2012 · N203BK · Beech C90 · Engine Oil PressureSDR CA120127007Rod · cracked(CAN) WHILE PERFORMING PHASE 3 CHECK, VISUAL INSPECTION OF MAIN CABIN DOOR UPPER AFT LATCHING ROD REVEALED A CRACK STARTING FROM HOLE FOR APPROXIMATELY 1.25" IN LENGTH. PART REPLACED BY NEW.Jan 26, 2012 · Beech C90 · Passenger/Crew DoorsSDR 2011FA0000781Antenna · inoperativeTROUBLESHOT BOTH NR 1 & 2 GPS SYSTEMS DUE TO BEING INOPERATIVE. FOUND NR 2 ANTENNA RESISTANCE CHECKED OK, ANY TIME NR 2 GPS SYSTEM TURNED ON IT CAUSED A BLOCKAGE OF ALL GPS SIGNALS TO ACFT. WITH NR 2 GPS SYS TURNED OFF NR 1 GPS SYS OPERATED GOOD WITH NO PRONov 8, 2011 · N117MF · Beech C90 · Global Positioning SystemSDR CA110929012Actuator · unserviceable(CAN) CRACK DISCOVERED ALONG PISTON SHAFT DURING O/H FOLLOWING CUSTOMER COMPLAINT (LT OTBD FLAP MAKES A RACKET WHEN IT IS RETRACTED). CRACK EXPANSION CAUSED PISTONS CIRCUMFERENCE TO EXPAND AND BIND IN ACTUATOR, WHICH COULD HAVE LEAD TO COMPLETE SEIZURE OF THESep 28, 2011 · Beech C90 · Trailing Edge Flap ActuatorSDR 2011FA0000521Restrictor · failedACFT WAS SQUAWKED FOR INSUFFICIENT FUEL TRANSFER OPERATION ON THE LT SIDE. BECAUSE THE PUMP WAS MAKING NOISE BUT THERE WAS MINIMAL FLOW, THE PUMP WAS REPLACED WITH AN O/H UNIT. THE O/H PUMP MADE THE SAME NOISE AND BEHAVED THE SAME. FURTHER TROUBLESHOOTING (ANAug 12, 2011 · N85TB · Beech C90 · Aircraft Fuel Distribution SystemSDR FCPR20110007Downlock Switch · looseON LANDING, WHEN GEAR SELECTED DOWN, 3 GREEN DOWN AND LOCKED LIGHTS ILLUMINATED. SHORTLY AFTER, LT DOWN AND LOCKED LIGHT EXTINGUISHED. PILOT WENT AROUND AND EMERGENCY EQUIPMENT DISPATCHED TO THE RUNWAY. ACFT LANDED WITHOUT INCIDENT. UPON INSP, LT GEAR DOWNAug 2, 2011 · N904KS · Beech C90 · Landing Gear Position and WarningSDR UA2R1105Wheel · crackedWHEEL WAS REJECTED BY NDT SHOP DUE TO A CRACK IN TIE BOLT HOLE.Mar 24, 2011 · N13 · Beech C90 · Wheel/Ski/FloatSDR 2011F00044Channel · chafedELEVATOR MOVEMENT TO CERTAIN DISTANCE CAUSES POPPING SOUND IN EMPENNAGE. INVESTIGATION RESULTED IN FINDING THE ELEVATOR TRIM MOTOR TURNBUCKLE UPPER BOLT & NUT RUBBING AGAIN THE ELEVATOR RIGGING CHANNEL, CAUSING CHAFING.Feb 18, 2011 · N11 · Beech C90 · Horizontal Stabilizer StructureSDR 1HYR20110202Frame · wornDURING A PHASE INSP, IT'S BEEN NOTED THAT THE NLG HAD SIGNIFICANT "FOR AND AFT" PLAY AT THE UPPER DRAG STRUT ATTACH POINT. FURTHER INSP REVEALED THAT THE DRAG LEG BEAM FRAME ASSY PN 50-410012-249 WAS SHOWING MOVEMENT ALONG THE ROW OF FASTENERS THAT SECURE THIJan 25, 2011 · N3GC · Beech C90 · Fuselage, Landing Gear Attach FittingsSDR 2011FA0000048Brace · lack of lubeCOMING FROM THE TAXI HOLDING BAY, ACFT WENT OUT OF THE RUNWAY DUE TOO NOSE WHEEL STEERING INOP. INVESTIGATION AND INSP PERFORMED BY MX, FOUND A LACK OF GREASING ON THE STEERING BRACE PN 101-820024-15. NO OTHER FINDINGS OR PROBLEMS DETECTED ON THE STEERING. Jan 13, 2011 · Beech C90 · Landing Gear Steering SystemSDR 2011FA0000047Buss Bar · arcedPILOT COMPLAINED OF INTERMITTENT POPPING OF STALL WARNING, RT PITOT HEAT, RECOGNITION LIGHT AND STROB LIGHT CIRCUIT BREAKER SWITCHES ON REMOVAL OF LT SUBPANEL REVEALED THAT THE BUSS BAR PN 101364084-219 WAS PHYSICALLY ATTACH TO THE STALL WARNING HEAT SWITCH. Jan 11, 2011 · N232BG · Beech C90 · Electrical Power System WiringSDR FCPR20110001Line · chafedLT AND RT RUDDER CABLES CHAFING ON TOP OF FILL LINE, PN 90-580088-1,TO HYD RESERVOIR AT FUSELAGE STA 150.0 AND 15" LT OF FUSELAGE CTR LINE.Jan 3, 2011 · N790RV · Beech C90 · Hydraulic System, MainSDR FCPR2010000235Gear · cracked(FCPR) AT THE 6 YEAR LANDING GEAR INSP, FOUND INDICATION OF CRACK IN INPUT GEAR.Nov 10, 2010 · N89TM · Beech C90 · Landing Gear Retraction/Extension SystemSDR UA2R1103Flex Hose · broken(UA2R) RT ENGINE HAS BROKEN AIR DUCT INBD FLEX TUBE. R & R.Nov 5, 2010 · N13 · Beech C90 · Air Intake Anti/De-Ice SystemSDR FCPR201000236Strut · corroded(FCPR) LT LANDING GEAR CYLINDER SEVERELY CORRODED INTERNALLY AT LOWER END.Oct 28, 2010 · N89TM · Beech C90 · Main Landing Gear Strut/Axle/Truck
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