Beech 1900C

Service difficulty reports · 1,840

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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 = '1900C'
  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 TIMA2010000012Switch · burnedPILOT SMELLED BURNING ODOR. DIVERTED TO NEAREST AIRPORT. INVESTIGATION DETERMINED FUEL TRANSFER SWITCH FAILED INTERNALLY. SWITCH AND ATTACHED WIRE OVERHEATED CAUSING SMOKE AND ODOR.Apr 12, 2010 · N154GA · Beech 1900C · Aircraft Fuel Distribution SystemSDR TIMA2010000011Seat Track · corrodedLEFT SIDE SEAT RAIL CORRODED.Mar 10, 2010 · N153GA · Beech 1900C · Fuselage, Seat/Cargo Attach FittingsSDR TIMA2010000010Actuator · crackedMAIN LANDING GEAR ACTUATOR ROD END CAP FOUND CRACKED DURING NDT INSPECTION TO C/W AD 2009-23-01.Mar 4, 2010 · N172GA · Beech 1900C · Landing Gear ActuatorSDR CA100212003Skin · corroded(CAN) UPON FUSELAGE BELLY PROTECTIVE TAPE INSP, FOUND LOWER FUSELAGE SKIN CORRODED (THROUGH CABIN AFTER REMOVAL OF FLAKING MATERIAL) AT BS 290 LBL 19 TO 24. (TC 20100212003)Feb 11, 2010 · Beech 1900C · Fuselage Main, Plate/SkinSDR 2010FA0000135Line · chafedMAIN FUEL LINE WAS REMOVED TO FACILITATE REPLACEMENT OF THE LT WING INBD WHEEL WELL KEEL. THE LINE WAS CHAFED APPROX HALF WAY THRU WHERE IT PASSES THRU THE KEEL. THIS AREA IS VERY DIFFICULT TO INSPECT AS IT IS ABOVE AND BEHIND THE MLG. THE RT WING MAIN FUEL LFeb 8, 2010 · Beech 1900C · Aircraft Fuel Distribution SystemSDR CA100203010Structure · debonded(CAN) AFTER THE DAYS FLIGHT, THE PILOTS NOTICED THE MAIN CABIN PASSENGER DOOR STRUCTURE WAS SEPARATED AT THE HINGE ATTACH AREA. SEVERE CORROSION FOUND BY MX. THE HONEYCOMB INNER DOOR STRUCTURE WAS SEVERELY CORRODED. SOME RIVETS ATTACHING THE BONDED ASSY TO THFeb 2, 2010 · Beech 1900C · Passenger/Crew DoorsSDR HSYA2010012410Resistor · hotENROUTE, PILOT OF FLIGHT 145 REPORTED THAT HE OBSERVED AN ACRID/BURNING ODOR IN THE COCKPIT. ATTEMPTED TO ISOLATE THE SOURCE VIA TURNING OFF ALL NON ESSENTIAL SYS THEN REACTIVATING THEM ONE BY ONE. HE WAS UNABLE TO ISOLATE THE SOURCE. ACFT LANDED WITHOUT INCIDJan 24, 2010 · N101UE · Beech 1900C · Ice/Rain Protection System WiringSDR CA100126003Skin · cracked(CAN) THERE WAS HAIRLINE CRACK ON THE UNDERSIDE OF THE SKIN OF THE LT AILERON. THE SKIN WAS ALSO SLIGHTLY WRINKLED, SO THERE WAS AN INSPECTION DONE ON THE AILERON SPAR AND A CRACK WAS FOUND IN THE ACTUAL SPAR.Jan 23, 2010 · Beech 1900C · AileronsSDR CA100125008Line · chafed(CAN) THERE WAS A FUEL LINE ON BOTH SIDES OF THE AIRPLANE THAT WAS FOUND TO BE SEVERELY CHAFED. THIS FUEL LINE IS LOCATED AT THE BACK OF THE MLG WHEEL WELL. THE LINE ON BOTH SIDES (LT & RT) WERE REPLACED. THIS LINE WAS DISCOVERED DURING A REPLACEMENT OF THE IJan 22, 2010 · Beech 1900C · Aircraft Fuel Distribution SystemSDR CA100122009Shaft · worn(CAN) STARTER GENERATOR WAS FOUND TO HAVE FAILED. DISCOVERED DURING ENGINE START-UP, ENGINE FAILED TO ROTATE FOR START. UPON REMOVAL AND STARTER DISSASSEMBLY IT WAS DISCOVERED THAT THE ARMATURE SHAFT END, THAT RIDES IN THE BRG, WAS WORN TO THE POINT THAT IT HAJan 12, 2010 · Beech 1900C · Starter-GeneratorSDR TIMA201000008Trim Tab · corrodedFOUND INTERGRANULAR CORROSION ON ELEVATOR TRIM TAB HORN.Dec 18, 2009 · N194GA · Beech 1900C · Elevator, Tab StructureSDR TIMA201000007Hinge · corrodedFOUND INTERGRANULAR CORROSION ON HINGE.Dec 18, 2009 · N194GA · Beech 1900C · Vertical StabilizerSDR TIMA201000006Hinge · corrodedFOUND INTERGRANULAR CORROSION ON HINGE.Dec 18, 2009 · N194GA · Beech 1900C · Vertical StabilizerSDR 2010FA0000083Hinge · corrodedFOUND INTERGRANULAR CORROSION ON HINGE.Dec 18, 2009 · N194GA · Beech 1900C · Vertical StabilizerSDR 2010F00018Hinge · corrodedFOUND INTERGRANULAR CORROSION ON HINGE.Dec 18, 2009 · N194GA · Beech 1900C · Vertical StabilizerSDR TIMA201000005Hinge · corrodedFOUND INTERGRANULAR CORROSION ON INBOARD ELEVATOR HINGE ASSY.Dec 18, 2009 · N194GA · Beech 1900C · Elevator StructureSDR TIMA201000004Hinge · corrodedFOUND INTERGRANULAR CORROSION ON CENTER ELEVATOR HINGE ASSY.Dec 18, 2009 · N194GA · Beech 1900C · Elevator StructureSDR TIMA201000003Hinge · corrodedFOUND INTERGRANULAR CORROSION ON OUTBOARD ELEVATOR HINGE ASSY.Dec 18, 2009 · N194GA · Beech 1900C · Elevator StructureSDR CA091215004Drive Shaft · sheared(CAN) RT OB FLAP WOULD NOT MOVE WHEN SELECTED. MAINTENANCE DISCOVERED THE RT OB FLEXIBLE FLAP DRIVE SHAFT SEVERLY CORRODED AND SHEARED OF. THIS IS THE SECOND INSTANCE OF FLAP FLEXIBLE DRIVE SHAFTS SEVERLY CORRODED CAUSING FAILURE.Dec 10, 2009 · Beech 1900C · Trailing Edge Flap Control SystemSDR CA091217006Firewall · damaged(CAN) FIREWALL WEB P/N 114-980025-87 WORN THROUGH AT THREE LOCATIONS, PRESUMABLY FROM ENGINE HOSES WEARING ON IT. (TC NR 20091217006)Dec 8, 2009 · Beech 1900C · Nacelle/Pylon, Bulkhead/FirewallSDR FFSA200900004Terminal · meltedSHORTLY AFTER TAKEOFF, SMOKE WAS OBSERVED COMING OUT OF F/OS GLARE SHIELD. ACFT RETURNED FOR LANDING. FOUND TERMINAL BLOCK AND RING TERMINAL INSULATION FOR CO-PILOT WINDSHIELD LOW HEAT PWR LEAD MELTED AND CRACKED. THE TERMINAL APPEARED TO BE LOOSE CAUSING A HNov 19, 2009 · N575F · Beech 1900C · Ice/Rain Protection System WiringSDR CA091130003Shaft · broken(CAN) NR 3 FLAP FLEX SHAFT (RT INBD) SHEARED CAUSING SPLIT FLAP PROTECTION TO SHUTOFF FLAP SYSTEM. (TC NR 20091130003)Nov 18, 2009 · Beech 1900C · Trailing Edge Flap Control SystemSDR YADA111709Exhaust Stack · crackedPILOT REPORTED OCCASIONAL EXHAUST FUMES IN CABIN. CONFIRMED THAT THE CREW SMELLED EXHAUST ON ROLLOUT WITH PROPS IN BETA AND HAD SMELLED IT AT AN ENGINE START (AS IS COMMON WHEN STARTING WITH A TAIL WIND). MX LOCATED A CRACKED HEATED INTAKE LIP STUB PIPE ON TNov 17, 2009 · N111AX · Beech 1900C · Engine Collector/Tailpipe/NozzleSDR CA091118013Doubler · cracked(CAN) DURING A SCHEDULED 1200 HOUR INSPECTION, A CRACK WAS FOUND ON A DOUBLER WHERE THE HORIZONTAL STAB MEETS THE VERTICAL STAB ON THE TAIL. MAINTENANCE GROUNDED THE AIRPLANE IMMEDIATELY. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE BOLTS THAT HOLDS THENov 15, 2009 · Beech 1900C · Horizontal Stabilizer, Plate/SkinSDR CA091112004Lever · worn(CAN) THE ALUMINUM INPUT LEVER ARM THAT GOES ONTO THE SHAFT FOR THE ENGINE CONTROL CAMBOX, LOCATED ON THE ENGINE, SLIPPED ON THE SHAFT CAUSING A RE-INDEXING OF THE ENGINE RIGGING, PILOTS WERE UNABLE TO REDUCE THE POWER TO IDLE. THIS IS A VERY POOR DESIGN FROMNov 10, 2009 · Beech 1900C · Power LeverSDR YADA11042009Potentiometer · failedON GROUND ROLL ONTO RAMP, CREW REPORTED DETECTING AN ELECTRICAL SMOKE AND SAW SMOKE EMITTING FROM BEHIND LT SIDE OF INSTRUMENT PANEL. CREW TURNED OFF BATTERY POWER AND PARKED ON RAMP. NO FURTHER ACTIONS REQUIRED. MX FOUND OVERHEAT EVIDENCE ON THE ANNUNCIATNov 4, 2009 · N112AX · Beech 1900C · Electrical Power SystemSDR CA091103010Motor · unserviceable(CAN) ELECTRIC POWERPACK MOTOR SUFFERED AN INTERNAL SHORT CAUSING THE MOTOR TO FAIL, CAUSE SEEMED TO BE FAULTY INTERNAL GROUND CONNECTION.Nov 3, 2009 · Beech 1900C · Landing Gear Retraction/Extension SystemSDR CA091023005Tube · worn(CAN) DURING HEAVY MAINTENANCE CHECK OF A HARD TO SEE AREA OF THE WHEEL WELL, THE MAIN FUEL FEED LINE FROM THE TANKS TO THE ENGINE WAS FOUND TO BE CHAFING ON THE AIRFRAME. THE RIGID TUBE WAS NOT YET WORN THROUGH BUT WAS WORN APPROXIMATELY 50% OF THE WAY THROUGOct 23, 2009 · Beech 1900C · Aircraft Fuel Distribution SystemSDR CA091020005Spar · corroded(CAN) DURING INCORPORATION OF SB 27-3928 OF WEIGHT BALANCE CLIP INSP AND REPLACEMENT, THE TECH DISCOVERED SEVERE EXFOILATION CORROSION OF THE AILERON REAR SPAR IN A AREA OF THE AILERON TRIM TAB. REAR SPAR WAS REPLACED WITH NEW.Oct 16, 2009 · Beech 1900C · AileronsSDR CA090924009Motor · failed(CAN) ON APPROACH GEAR WAS SELECTED DOWN, HYDRAULIC POWERPACK FAILED. GEAR HAD TO BE MANUALLY EXTENDED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. UPON INSPECTION IT WAS FOUND THAT THE ELECTRIC MOTOR THAT DRIVES THE HYDRAULIC PUMP HAD FAILED DUE TO INTERNAL SHOSep 22, 2009 · Beech 1900C · Hydraulic Pump (Electric/Engine), MainSDR CA090921001Purge Can · failed(CAN) AIRCRAFT WAS SMOKING UPON SHUTDOWN. PURGE CAN END WALL WAS FOUND BLOWN OUT. (TC# 20090921001)Sep 20, 2009 · Beech 1900C · Engine (Turbine/Turboprop)SDR YADA09022009Windshield · crackedPILOT REPORTED THAT THE COPILOT WINDSHIELD CRACKED ON DEPARTURE. ACFT RETURNED AND MADE AN UNEVENTFUL LANDING AT THE AIRPORT OF DEPARTURE. MX INSPECTED CRACKED OUTER PANE OF COPILOTS WINDSHIELD AND ELECTED TO REPLACE WINDSHIELD (OPS COULD HAVE BEEN CONTINUEDSep 2, 2009 · N112AX · Beech 1900C · Window/Windshield SystemSDR HSYA2009082109Engine · malfunctionedON ROTATION RT ENG TORQUE WENT TO 4000 LBS. FOR APPROXIMATELY 2 SECONDS. ENG STARTED TO AUTOFEATHER & PILOT PULLED THROTTLE BACK & SHUTDOWN ENG. PERFORM A BORESCOPE INSPECTION OF ENGINE, NO DEFECTS NOTED. PERFORMED REMOVAL & INSPECTION OF OIL FILTER & HOUSING Aug 21, 2009 · N122GL · Beech 1900C · Engine (Turbine/Turboprop)SDR JDWA31764AOil Filter · cloggedAFTER TAKEOFF DURING CLIMB, PILOT NOTICED RT OIL PRESSURE ANNUNCIATOR LIGHT AND NOTED OIL PSI TO BE 50PSI. PILOT REDUCED PWR AND RETURNED TO BASE WITHOUT INCIDENT.Aug 7, 2009 · N719GL · Beech 1900C · Turbine Engine Oil SystemSDR YADA080509Cable · separatedPILOT REPORTED THAT PITCH TRIM SEEMED TO SLIP - RETURNED TO AIRPORT. MAINTENANCE REPLACED A BROKEN ELEVATOR TRIM CABLE.Aug 5, 2009 · N111AX · Beech 1900C · Elevator Tab Control SystemSDR CA090807006Slip Ring · damagedNR 1 PROPELLER DEICE FAULT IN FLIGHT. MX INSPECTED AND FOUND NR 1 PROPELLER SLIP RING IN POOR CONDITION. SLIP RING REPLACED.Jul 25, 2009 · Beech 1900C · Propeller/Rotor Anti-Ice/De-Ice SystemSDR CA090708002Feeder Cable · burned(CAN) BATTERY FEEDER CABLES TO LT DC PWR CONTROLLER WAS FOUND BURNED OFF AT WING DISCONNECT TERMINAL WHICH IS FOUND AT FLIGHT STA 350-380. IT LOOKS LIKE THE TERMINAL BLOCK WHICH THESE WIRES WHERE CONNECTED TO WAS DESIGNED TO ACCOMMODATE A FUSIBLE LINK, NONE WJul 3, 2009 · Beech 1900C · Electrical Power System WiringSDR HSYA2009061809Attach Fitting · crackedFOUND BOTH THE LT AND RT AILERON BALANCE WEIGHT CLIPS CRACKED IN HALF. REMOVED AND REPLACED BALANCE WEIGHT CLIPS IAW KIT NR 129-4036-001.Jul 2, 2009 · N101UE · Beech 1900C · AileronsSDR CA090625007Line · cracked(CAN) PY LINE CRACKED AT FLARE FITTING AT PROP GOVENOR ATTACH POINT, ENGINE DECREASED TO IDLE.Jun 24, 2009 · Beech 1900C · Propeller Feathering/ReversingSDR CA090619002Wire Rope · broken(CAN) WHEN THE CREW MOVED THE FLAPS THE LT OTBD FLAP DID NOT MOVE. MX INSPECTED THE FLAP SYS AND DISCOVERED THE LT OTBD FLAP SHAFT WIRE ROPE WAS BROKEN AT THE FLAP ACTUATOR END.Jun 18, 2009 · Beech 1900C · Trailing Edge Flap Control SystemSDR CA090605002Clamp · damaged(CAN) PROPELLER RECEIVED FOR OVERHAUL. UPON VISUAL INSP, DAMAGE TO ONE OF THE BLADE CLAMPS CONSISTENT WITH LIGHTENING STRIKE WAS OBSERVED. CLAMP IS UNSERVICABLE IAW MANUAL 118F AND 202A.Jun 1, 2009 · Beech 1900C · Propeller Blade SectionSDR CA090511002Tube · chafed(CAN) FUEL LINE FOUND CHAFED AND LEAKING. LINE WAS CHAFED BY STARTER GENERATOR COOLING SCAT HOSE.May 11, 2009 · Beech 1900C · Aircraft Fuel Distribution SystemSDR CA090508001Selector · unknown(CAN) GEAR DID NOT RETRACT WHEN HANDLE SELECTED UP. 3 GREEN INDICATED, NO RED LIGHT AND NO HYDR FLUID LOW ANNUNCIATOR INDICATED.May 7, 2009 · Beech 1900C · Landing Gear SelectorSDR CA090507002Actuator · intermittent(CAN) INTERMITTENT OPERATION CONCERNING ELECTRIC NOSE WHEEL STEERING ACTUATOR.May 7, 2009 · Beech 1900C · Steering UnitSDR CA090505010Bearing · failed(CAN) REAR BEARING FAILURE ON STARTER GENERATOR. COOLING FAN BLADES BROKE OFF AS WELL.May 2, 2009 · Beech 1900C · Starter-GeneratorSDR CA090505005Bolt · missing(CAN) DURING WHEEL REPLACEMENT A BOLT WAS FOUND TO BE MISSING FROM THE WHEEL. DAMAGE TO THE WHEEL AND BRAKE HAS SHOWN THE BOLT WAS FITTED AT ASSY AND BECAME DETACHED DUE TO A BOLT FAILURE. THE BOLT PARTS WERE NOT RECOVERED AND THE TIME OF FAILURE WAS NOT ESTABMay 2, 2009 · Beech 1900C · Wheel/Ski/FloatSDR CA090422003Governor · malfunctioned(CAN) DURING ENGINE START IT WAS NOTED THAT THE RT ENGINE TORQUE WAS SLOW TO INCREASE WHEN THE PROP WAS TAKEN OUT OF FEATHER. MX COFIRMED THE SNAG AND REPLACED THE RT PROPELLOR GOVERNOR. THIS FIXED THE PROBLEM.Apr 19, 2009 · Beech 1900C · Propeller GovernorSDR CA090507004Compressor · leaking(CAN) THE PULLEY SHAFT WAS NOTED AS LEAKING. AIR CONDITIONING COMPRESSOR REPLACED.Apr 10, 2009 · Beech 1900C · Cabin Cooling SystemSDR TIMA20090002Skin · corrodedWHILE CLEANING LITE CORROSION ON SURFACE OF BELLY AFT OF WINGS, NOTICED SOME APPARENT BLISTERING OF THE SKIN. INVESTIGATION REVEALED THERE WAS CORROSION BETWEEN THE SKIN AND THE FUSELAGE FRAME. AFFECTED SKIN WAS CUT OUT AND REPLACED AS A COVER PATCH IN ACCORApr 3, 2009 · N172GA · Beech 1900C · Fuselage Main, Plate/SkinSDR FFSA200900003Terminal · meltedSHORTLY AFTER TAKE OFF, SMOKE WAS OBSERVED COMING OUT OF FIRST OFFICER’S GLARE SHIELD. AIRCRAFT RETURNED FOR LANDING. FOUND TERMINAL BLOCK AND RING TERMINAL INSULATION FOR CO-PILOT WINDSHIELD LOW HEAT POWER LEAD MELTED AND CRACKED. THE TERMINAL APPEARED TO BEMar 24, 2009 · N575F · Beech 1900C · Ice/Rain Protection System Wiring
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