Beech 1900C

Service difficulty reports · 1,841

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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 2006FA0000837Fire Loop · brokenPILOT EXPERIENCED A FIRE WARNING ANNUNCIATION DURING TAKEOFF ROLL. PILOT ABORTED TAKEOFF. MAINTENANCE FOUND THAT ONE FIRELOOP HAD FAILED AND CAUSED THE FALSE FIRE INDICATION. (K)Jun 7, 2006 · N172GA · Beech 1900C · Fire DetectionSDR CA060526001Shroud · looseDURING TAKEOFF ROLL IT WAS NOTED, RT ENG ITT WAS AT RED LINE AND ENG TQ WAS BELOW REQUIRED T/O VALUE. T/O WAS ABORTED AND A/C RETURNED TO RAMP. DURING MX INVESTIGATION, LARGE INCREASES IN ITT READINGS COULD BE SEEN WHEN SELECTING BLEED AIR ON OR ACCELERATINGMay 25, 2006 · Beech 1900C · Turbine SectionSDR CA060511009Landing Gear · malfunctioned(CAN) GEAR WAS RETRACTED AND GEAR HORN AND GEAR HANDLE LIGHT STAYED ON. (TC NR 20060511009)May 11, 2006 · Beech 1900C · Landing Gear Retraction/Extension SystemSDR CA060518004Windscreen · failedWINDSCREEN INSIDE PANE SHATTERED IN FLIGHT.May 8, 2006 · Beech 1900C · Flight Compartment WindowsSDR ACE04302006Spar Cap · corrodedMAINTENANCE FOUND CORROSION ON FORWARD SPAR LOWER CAP FORWARD FLANGE, IN THE CENTER FUSELAGE BAY, UNDER ORIGINAL SEALANT. REPAIR REQUIRED REMOVAL OF CORROSION AND STRAP DOUBLER PER FR-CO FACTORY REPAIR DESIGN.Apr 30, 2006 · N113AX · Beech 1900C · Wing SparSDR CA060511008Doubler · cracked(CAN) DOUBLER P/N 114-120048-54 FOUND CRACKED AT FWD OB CORNER. CAN NOT SEE CRACK UNLESS COLLECTOR FUEL TANK IS REMOVED. (TC NR 20060511008)Apr 26, 2006 · Beech 1900C · Wing, Plate/SkinSDR CA060511006Skin · cracked(CAN) OB FWD CORNER OF COLLECTOR TANK OPENING. SKINS P/N 114-120048-73 AND 74 FOUND CRACKED. HEAVY SKIN .071 (TC NR 20060511006)Apr 18, 2006 · Beech 1900C · Wing, Plate/SkinSDR HSYA200600001Downlock Switch · inoperativeON APPROACH WHEN LG SELECTED DOWN CREW DID NOT GET RT MLG SAFE (GREEN) INDICATION. MLG WAS IN FACT DOWN AND LOCKED. MX DETERMINED FAULTY DOWNLOCK SWITCH INCORPORATED INTO MLG ACTUATOR. THE MLG ACTUATOR WAS R&R AND GEAR SWINGS ACCOMPLISHED WITH SATISFATORY RESUApr 18, 2006 · N319BH · Beech 1900C · Landing Gear Position and WarningSDR CA060511005Skin · corroded(CAN) HEAVY CORROSION BETWEEN SKIN AND STRINGERS (BONDED) AT STRINGER SPLICES IN BELLY AT CENTERLINE STRINGER AND 2 LT AND RT OF CENTER. (TC NR 20060511005)Apr 14, 2006 · Beech 1900C · Fuselage Main, Plate/SkinSDR ACE040606Circuit Breaker · trippedPILOT REPORTED LANDING GEAR CONTROL CIRCUIT BREAKER TRIPPED TWICE, GEAR WAS MANUALLY EXTENDED AT DESTINATION, UNEVENTFUL LANDING MADE. MAINTENANCE C/N/D ON GROUND, NO FAULTS DETECTED.Apr 6, 2006 · N112AX · Beech 1900C · Landing Gear Retraction/Extension SystemSDR CA060315006Shutoff Valve · unknownDURING PRE FLIGHT INSPECTION, FUEL PRESSURE ANNUNCIATOR EXTINGUISHED WHILE THE FIRE WALL SHUTOFF VALVE T HANDLE WAS PULLED. THIS INDICATED THAT THE VALVE WAS STILL OPEN. DURING THE MX T/S IT WAS FOUND THAT VALVE POSITION INDICATOR ARM WAS CONTACTING THE FUELMar 14, 2006 · Beech 1900C · Fuel Selector/Shut-Off ValveSDR FFS2006F00002Cable Assy · chafedFIRE WARNING FOR LT ENGINE ILLUMINATED CONTINUOUSLY IN FLIGHT. INSPECTED ENGINE AND NACELLE FOR EVIDENCE OF FIRE OR OVERHEAT. INSPECTED FORE AND AFT FIRE LOOP INSTALLATION FOR DAMAGE AND GENERAL CONDITION. NO FAULT FOUND. COULD NOT DUPLICATE WARNING ON THEMar 12, 2006 · N575P · Beech 1900C · Fire DetectionSDR ACE030906Flange · corrodedMAINTENANCE FOUND CORROSION ON FORWARD SPAR LOWER CAP FORWARD FLANGE, IN THE CENTER FUSELAGE BAY, UNDER PREVIOUSLY REPLACED SEALANT. REPAIR REQUIRED REMOVAL OF CORROSION AND STRAP DOUBLER PER FR-CO FACTORY REPAIR DESIGN.Mar 9, 2006 · N114AX · Beech 1900C · Wing SparSDR CA060125004Cam · brokenHEARD A BANG DURING APPROACH, FOUND RT UPPER FWD COWL INNER PORTION HAD LIFTED FROM NORM POSITION. FOUND CAM BOLT FAILED THAT PROVIDES TENSION TO LWR COWL ASSY. OVER CTR COWL FASTENERS ON THESE A/C (4) INSTILL CONSIDERABLE FORCE AND HAVE A HISTORY ON ALL SIMJan 24, 2006 · Beech 1900C · Aerodynamic FairingsSDR ACE012406Stringer · corrodedFOUND CORROSION ON STRINGER 15 LH AT FUSELAGE STATION 210. THE REPAIR REQUIRED DER. ENGINEERING ASSISTANCE DUE NO OEM DOCUMENT COVERING THE REQUIRED REPAIR.Jan 24, 2006 · N111AX · Beech 1900C · Fuselage Main, Longeron/StringerSDR FFS2006F00000Windshield · crackedPILOT`S WINDSHIELD SHATTERED WITH MULTIPLE VERTICAL CRACKS IN OUTER GLASS PLY. FAILURE OCCURRED WITHOUT WARNING WHILE AIRCRAFT WAS IN LEVEL CRUISE AT 14,500 FT APPROXIMATELY 20 MINUTES AFTER TAKEOFF. (K)Jan 19, 2006 · N575Z · Beech 1900C · Flight Compartment WindowsSDR TIM2006F00000Relay · failedLANDING GEAR DID NOT EXTEND WHEN SELECTED. PILOT EXTENDED GEAR MANUALLY AND LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED THAT THE HYDRAULIC POWER PACK MOTOR RELAY HAD WELDED IN THE CLOSED POSITION RESULTING IN THE MOTOR RUNNING CONTINOUSLY UNTIL IT FAILEDJan 17, 2006 · N197GA · Beech 1900C · Hydraulic Pump, AuxiliarySDR FFS2005F00007Wire Rope · stretchedLT GOVERNOR WOULD NOT GOVERN AFTER TAKE-OFF, SECURED ENGINE, DECLARED EMERGENCY. RETURNED TO DEPARTURE. LANDING UNEVENTFUL. CHANGED BETA VALVE O-RINGS AND CHANGED WIRE ROPE FOR PROPELLER REVERSING LINKAGE. RE-RIGGED BETA VALVE. (K)Dec 11, 2005 · N575X · Beech 1900C · Turbine GovernorSDR ACE120105Windshield · crackedPILOT REPORTED RT FORWARD WINDSHIELD CRACKED. REPLACED CRACKED WINDSHIELD.Dec 1, 2005 · N113AX · Beech 1900C · Flight Compartment WindowsSDR ACE112805Bearing · failedPILOT REPORTED RT GEN OFF LINE AND NO ENGINE STARTER AFTER LANDING - REPLACED STARTER/GENERATOR DUE FRONT BEARING FAILURENov 28, 2005 · N114AX · Beech 1900C · Starter-GeneratorSDR CA051206009Bearing · wrong partSTARTER-GEN SUFFERED A BEARING FAILURE THAT TOOK THE GENERATOR OFF-LINE. THE ANTI-DRIVE END (ADE) BEARING FAILED, CAUSING THE ARMATURE TO DESTROY ITSELF BY RUBBING ON THE STATOR POLES. ON DISASSEMBLY BY OVERHAUL SHOP, THE BEARING WAS FOUND TO BE P/N 03-6009-Nov 23, 2005 · Beech 1900C · Starter-GeneratorSDR TIM2005F00014Skin · damagedTHE FASTENERS WERE DISCOVERED TO BE WORKING INTO THE LOWER SKIN WHILE DOING AN INSPECTION OF THE WING. IT APPEARS THAT THIS WAS CAUSED BY NORMAL WING FLEX IN THIS AREA. (K)Nov 10, 2005 · N154GA · Beech 1900C · Wing, Plate/SkinSDR TIM2005F00012Circuit Board · shortedTHE GEAR HANDLE PLACED IN THE DOWN POSITION, GEAR FAILED TO GO DOWN AND THE CIRCUIT BREAKER POPPED. FOLLOW INSPECTION, FOUND A BROKEN WIRE. (K)Nov 4, 2005 · N195GA · Beech 1900C · Landing Gear System WiringSDR CA051104012Engine · shutdown(CAN) DURING CRUISE, THE ENGINE WAS REPORTED TO EMIT A LOUD (BANG) FOLLOWED BY SEVERE VIBRATION.THE ENGINE WAS SHUTDOWN IN FLIGHT AND A SINGLE ENGINE LANDING ACCOMPLISHED. MFG WILL INVESTIGATE THE INCIDENT AND WILL ADVISE OF ROOT CAUSE ONCE DETERMINED.Oct 25, 2005 · Beech 1900C · Engine (Turbine/Turboprop)SDR ACE102505Wire · overheatedTAIL FLOOD WHEN TURNED ON, CAN SMELL ELECTICAL SMOKE. THEN SWITCH (FLOOD LIGHTS) FLIPS OFF. INSPECTED WIRING AT FLOOD LIGHT SWITCH AND FOUND OVERHEATED WIRE AT LOOSE TERMINAL ON CIRCUIT BREAKER SWITCH.Oct 25, 2005 · N112AX · Beech 1900C · Light System WiringSDR ACE101005Pump · leakingNR 2 ENGINE LEAKING FUEL FROM NACELLE. MAINTENANCE REPLACED LOW PSI FUEL PUMP DUE EXTRUDED VALVE BODY GASKET. FUEL WAS NOT DUMPED OVERBOARD AS THE VALVE BODY WAS LEAKING EXTERNALLY.Oct 10, 2005 · N114AX · Beech 1900C · Engine Fuel PumpSDR TIM2005F00010Line · leakingNOSE GEAR WARNING LIGHT ILLUMINATED WHEN LANDING GEAR EXTENDED. GEAR DEPLOYED AFTER 15 TO 20 SECONDS. PROBLEM WAS A LEAK IN THE HYDRAULIC LINE. THE LINE DEVELOPED A PIN HOLE LEAK BECAUSE OF CORROSION FROM THE INSIDE OF THE LINE. (K)Oct 3, 2005 · N195GA · Beech 1900C · Hydraulic System, MainSDR TIM2005F00008Line · leakingNOSE GEAR WARNING LIGHT ILLUMINATED WHEN LANDING GEAR EXTENDED. GEAR DEPLOYED AFTER 15 TO 20 SECONDS. PROBLEM WAS A LEAK IN THE HYDRAULIC LINE. THE LINE DEVELOPED A PIN HOLE LEAK BECAUSE OF CORROSION FROM THE INSIDE OF THE LINE. (K)Oct 3, 2005 · N195GA · Beech 1900C · Hydraulic System, MainSDR ACE100305Relay · contaminatedPIREP - HAD TO EXTEND LANDING GEAR MANUALLY. MAINTENANCE REPLACED "WATER LOGGED" HYDRAULIC POWER PACK RELAY.Oct 3, 2005 · N112AX · Beech 1900C · Hydraulic Power System WiringSDR TIM2005F00007Gas Generator · seizedRT ENGINE GAS GENERATOR SECTION SEIZED ON TAKEOFF ROLL, CAUSE OF THE FAILURE IS UNKNOWN AT THIS TIME. (K)Sep 22, 2005 · N194GA · Beech 1900C · Turbine Engine Compressor SectionSDR CA050926003Governor · faulty(CAN) DURING CRUISE, THE RT PROPELLER RPM OCCASIONALLY FLUCTUATED 100 RPM WITH NO INPUT FROM THE CREW. THE DEFECT WAS CONFIRMED ON THE GROUND BY MAINTENANCE AND THE PROPELLER GOVERNOR WAS REPLACED.Sep 20, 2005 · Beech 1900C · Propeller GovernorSDR ACE091905Diaphragm · rupturedPIREP - FUEL OBSERVED DRIPPING FROM NR 1 ENGINE DRAIN MAST. VERIFIED LOW PSI FUEL PUMP DIAPHRAGM RUPTURE, THIS UNIT WAS IN COMPLIANCE WITH THE LATEST SB FOR DIAPHRAGM DESIGN.Sep 19, 2005 · N114AX · Beech 1900C · Fuel Boost PumpSDR ACE091305Relay · contaminatedPIREP - LANDING GEAR FAILED TO EXTEND USING NORMAL SYSTEM. MANUAL EXTENSION PERFORMED. MAINTENANCE REPLACED WATER LOGGED HYDRAULIC POWER PACK RELAY (SUSPECT THAT RELAY WAS FROZEN AFTER FLIGHT AT ALTITUDE). SEALED WING LEADING EDGE GAP TO HELP REDUCE FREE WASep 13, 2005 · N112AX · Beech 1900C · Landing Gear Retraction/Extension SystemSDR CA050922005Skin · damaged(CAN) DURING INSPECTION OF THE ELEVATOR IAW AD 2005-18-21 AND COMMUNIQUE NO. 261, SMOKING RIVETS WERE DISCOVERED IN THE LOWER SKIN OF BOTH ELEVATORS (2 IN THE LT, 4 IN THE RT). REQUIRED REPAIRS WERE CARRIED OUT.Sep 12, 2005 · Beech 1900C · Elevator, Plate/SkinSDR ACE082605Diaphragm · rupturedPILOT REPORTED LOW FUEL PRESSURE WARNING LIGHT CAME ON IN FLIGHT. MAINTENANCE REPLACED LEAKING LOW PSI BOOST PUMP. VERIFIED DIAPHRAGM HAD FAILED. FUEL WAS OBSERVED IN AGB AREA.Aug 26, 2005 · N113AX · Beech 1900C · Fuel Boost PumpSDR HSYA01081205Transmitter · failedON CLIMBOUT, NR 2 ENGINE OIL PRESSURE DROPPED TO ZERO. ENGINE WAS SECURED AND SHUT DOWN AND AIRCRAFT RETURNED TO SJU, EMERGENCY DECLARED. PROPELLER FEATHERED. APPARENT CAUSE OF PROBLEM - RT ENGINE OIL PRESSURE TRANSMITTER FAILURE. TROUBLESHOT AND FOUND OIL Aug 12, 2005 · N318BH · Beech 1900C · Engine Oil PressureSDR FFS2005F00006Splice · mismanufacturedTHE FRAME SPLICES ADJACENT TO STRINGER 4L ON FUSELAGE FRAME AT FS 523.5, HAD POOR FIT-UP BETWEEN THE LT FRAME (114-430059-5), THE TOP FRAME (114-430127-3) AND THE LT SPLICE CLIP (114-43006019). THERE WAS A 0.030 TO 0.060 INCH GAP BETWEEN THE FRAME FLANGE AND TJul 25, 2005 · N575P · Beech 1900C · Fuselage Miscellaneous StructureSDR CA050726005Bolt · loose(CAN) DURING AN INSPECTION OF THE BOLTS ACCORDING TO AD2005-14-12 ALL OF THE BOLTS FAILED THE TEST TORQUE.THE BOLTS WERE ALL OF BATCH NUMBER 56.THIS IS ONE OF THEBATCHES THAT IS REQUIRED TO BE REPLACED BY THE AD.THE BOLTS WERE REPLACED.Jul 24, 2005 · Beech 1900C · Propeller Hub SectionSDR 072405Smoke · detectedODOR OF SMOKE IN COCKPIT - SHUT OFF BLEED AIR AND EVIRONMENTAL AIR, ODOR WENT AWAY - MAINTENANCE COULD NOT LOCATE ANY SOURCE OF THE ODOR - OPS CHECK FLIGHT SCHEDULED.Jul 24, 2005 · N111AX · Beech 1900C · Air Distribution SystemSDR CA050718002Starter Gen · failedAFTER THE LEFT ENGINE START, THE GENERATOR WOULD NOT COME ON LINE. DURING THE SUBSEQUENT ENGINE START BY MAINTENANCE A LOUD GRINDING NOISE WAS HEARD FROM THE LEFT ENGINE. THE START WAS ABORTED AND THE COWLINGS REMOVED. THE STARTER GENERATOR WAS VERY HOT ANDJul 16, 2005 · Beech 1900C · Starter-GeneratorSDR CA050714004Bearing · spalledDURING NR 5 PHASE INSPECTION, NOSE WHEEL WAS ROTATED BY HAND WHICH REVEALED A DEEP RUMBLING NOISE. WHEN DISASSEMBLED BEARING WAS FOUND TO BE DRY AND BADLY WORN. BEARING CUP WAS ALSO DAMAGED DUE TO LACK OF LUBRICATION. DISOVERY FOLLOWED COMPLAINTS BY CREW OFJul 11, 2005 · Beech 1900C · Wheel/Ski/FloatSDR CA050711002Tube · failedRIGHT HAND ENGINE BLEED AIR FAILURE ANNUNCIATOR ON IN CRUISE. RIGHT HAND BLEED AIR ISOLATED AS PER SOP. BLEED AIR TUBE FOUND TO HAVE FAILED AT B NUT IN RIGHT HAND WING. EVA TUBING HAD MELTED CAUSING ANNUNCIATOR TO LIGHT. TUBE WAS REPLACED. EVA TUBING REPAJul 8, 2005 · Beech 1900C · Engine Bleed Air SystemSDR ACE070805Fuel Heater · crackedMAINTENANCE NOTICED OIL RESIDUE ON ENGINE COWLING. LOCATED ENGINE OIL LEAK AT OIL / FUEL HEATER. REPLACED CRACKED HEATER.Jul 8, 2005 · N113AX · Beech 1900C · Fuel HeaterSDR CA050718011Windscreen · crackedCAPTAIN'S WINDSCREEN CRACKED WHILE AT CRUISE AT 19,000 FT, THE AIRCRAFT CHECK LIST WAS FOLLOWED AND CABIN PRESSURIZATION WAS REDUCED. THE AIRCRAFT WAS RETURNED TO THE BASE WITHOUT FURTHER INCIDENT. THE SUSPECT WINDSCREEN WAS REPLACED AND AIRCRAFT RETURNED TO Jul 1, 2005 · Beech 1900C · Flight Compartment WindowsSDR FFS2005F00005Bearing · disintegratedLT OB WHEEL AND TIRE ASSEMBLY SEPARATED FROM AIRCRAFT ON TAKEOFF ROLL. PILOT LANDED UNEVENTFULLY AT NEXT SCHEDULED DESTINATION UNAWARE OF THE LOSS OF THE WHEEL. OUTER WHEEL BEARING FAILED ALLOWING WHEEL TO SEPARATE OVER THE AXLE NUT. WHEEL AND TIRE ASSEMBY HJun 13, 2005 · N575G · Beech 1900C · Wheel/Ski/FloatSDR ACE060305Relay · malfunctionedPIREP - LANDING GEAR HANDLE HAD TO BE CYCLED SEVERAL TIMES BEFORE GEAR WOULD EXTEND. MAINTENANCE COULD NOT DUPLICATE. REPLACED HYDRAULIC PUMP MOTOR RELAY FOR T/S (COULD NOT VERIFY RELAY FAILURE).Jun 3, 2005 · N112AX · Beech 1900C · Hydraulic Power System WiringSDR ACE052405Diaphragm · rupturedPIREP - FUEL LEAKING FROM NR 1 ENGINE GANG DRAIN. REPLACED LOW PSI DUEL PUMP DUE RUPTURED DIAPHRAGM.May 24, 2005 · N114AX · Beech 1900C · Fuel Boost PumpSDR ACE052105Windshield · crackedPILOT REPORTED LT WINDSHIELD CRACKED ON DESCENT. REPLACED FAILED WINDSHIELD (OUTER PLY FAILED).May 21, 2005 · N113AX · Beech 1900C · Flight Compartment WindowsSDR ACE051805Windshield · crackedPILOT REPORTED LT WINDSHIELD CRACKED OUTER PLY VERIFIED CRACKED - REPLACED WINDSHIELD (WITHIN MFG. WARRANTY PERIOD).May 18, 2005 · N111AX · Beech 1900C · Flight Compartment WindowsSDR ACE051405Fire Loop · shortedPIREP - RIGHT T-HANDLE LIGHT COMES ON INTERMITTENTLY. MAINTENANCE VERIFIED "OPEN" RIGHT ENGINE FORWARD FIRE LOOP.May 14, 2005 · N112AX · Beech 1900C · Fire Detection
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