Beech 1900C

Service difficulty reports · 1,841

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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 HSYA20080102Rib · crackedDURING SCHEDULED MX - SIM TASK 55-30-00 (1200 FLT HR/ 24 MO) REF. B1900 STRUCTURAL INSPECTION MANUAL, MX PERFORMED A VISUAL INSPECTION OF THE VERTICAL STABILIZER STRUCTURAL COMPONENTS AND FOUND RIB, AT CANTED STAB. STA. 69.184, CRACKED ON THE RT SIDE FLANGE ATJan 6, 2008 · N101UE · Beech 1900C · Vertical Stabilizer, Spar/RibSDR ACE122407Tube · failedPILOT STOPPED AIRCRAFT ON TAXIWAY DUE NOSE TIE VIBRATION. REPLACED FLAT NOSE TIRE. TEARDOWN INSPECTION OF TIRE INDICATED A BURST TUBE AT A INSTALLATION FOLD. INSPECTION OF TUBE MATERIAL AT BURST AREA APPEARED TO RESEMBLE A CRACK MORE THAN A TEAR. THIS IS TDec 24, 2007 · N111AX · Beech 1900C · Tire TubeSDR ACE120407Tube · failedPILOT STOPPED AIRCRAFT ON TAXIWAY DUE VIBRATION FROM NOSE TIRE. MAINTENANCE REPLACED FLAT TIRE. INSPECTION OF TIRE AND TUBE IDENTIFIED A NAIL IN TIRE (UNDETERMINED IF THIS WAS CAUSE OF FAILURE) ADDITIONAL INSPECTION OF TUBE INDICATED POSSIBLE PROBLEM WITH TDec 4, 2007 · N113AX · Beech 1900C · Tire TubeSDR HSYA20071201Engine · reads highDURING CRUISE, THE CREW REPORTED THAT THE LT ENGINE INDICATED ABNORMALLY HIGH ITT. THE CREW ELECTED TO RETURN DEPARTURE AND LANDED WITH OUT INCIDENT. MX PERFORMED A LT ENGINE ITT THERMOCOUPLE LOOP RESISTANCE CHECK AND ADJUSTED. MX ALSO PERFORMED AND ITT CALIDec 3, 2007 · N101UE · Beech 1900C · Engine (Turbine/Turboprop)SDR CA071130003Windshield · cracked(CAN) COPILOTS WINDSHIELD INNER PANE SHATTERED DURING NORMAL CRUISE FLIGHT. WINDSHIELD REPLACED UPON RETURN TO MAINTENANCE BASE. (TC NR 20071130003)Nov 28, 2007 · Beech 1900C · Flight Compartment WindowsSDR CA071102006Downlock Switch · inoperative(CAN) UNABLE TO GET NLG (GREEN LIGHT) ON APPROACH. RECYCLED 3 TIMES AND GREEN LIGHT OBTAINED. NLG DRAG LINK DOWN AND LOCK SWITCH REPLACED. GEAR SWINGS COMPLETED. NO FURTHER FAULTS AT THIS TIME. (TC NR 20071102006)Oct 31, 2007 · Beech 1900C · Landing Gear Position and WarningSDR GUUA09270702Hinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RT OB ELEVATOR HINGE BRACKET.Sep 27, 2007 · N87555 · Beech 1900C · Horizontal Stabilizer StructureSDR CA070926001Valve · worn(CAN) FOUND WORN TORQUE METER VALVE IN POWER SECTION OF ENGINE GIVING ERRATIC ENGINE TORQUE INDICATION AT COCKPIT INDICATOR. VALVE REPLACED. NO OTHER PROBLEMS NOTED. (TC NR 20070926001)Sep 24, 2007 · Beech 1900C · Engine BMEP/Torque IndicatingSDR CA070921002Rib · cracked(CAN) CRACK FOUND IN VERTICAL STABILIZER AT RIB CSS 11.500. CRACK REPAIRED IAW SRM 51-70-17-001. CRACKED RIB REPAIR (NON-PRESSURIZED AREA). (TC NR 20070921002)Sep 19, 2007 · Beech 1900C · Vertical Stabilizer, Spar/RibSDR CA070907004Fuel Line · chafed(CAN) FUEL LINE ASSY WAS FOUND TO HAVE BEEN CHAFED BY THE STARTER GENERATOR VENT HOSE, CAUSING A VERY SMALL PIN HOLE IN THE RIGID STAINLESS FUEL LINE, RESULTING IN A FUEL LEAK. (TC NR 20070907004)Sep 6, 2007 · Beech 1900C · Engine Fuel DistributionSDR HSYA20070702Airstair · crackedDURING PREFLIGHT INSPECTION, CREW REPORTED A CRACK ON THE AIRSTAIR DOOR NEAR THE HINGE. MX FOUND A CRACK ON THE INNER DOOR SKIN NEAR THE AFT END DOOR HINGE. UPON INITIATION OF A REPAIR TO AFFECTED AREA, MX FOUND CORROSION ON THE INNER DOOR SKIN, CLOSURE AND MEJul 1, 2007 · N122GL · Beech 1900C · Entrance StairsSDR ACE060507Diaphragm · rupturedFUEL DRIPPING FROM NR 1 ENGINE, GANG DRAIN. REPLACED NR 1 LOW PSI FUEL PUMP. DISASSEMBLY OF PUMP REVEALED A RUPTURED DIAPHRAGM, PN RA5326 WITH 1165 TSI.Jun 5, 2007 · N112AX · Beech 1900C · Engine Fuel PumpSDR CA070528009Line · chafed(CAN) FUEL FLOW TRANSMITTER LINE P/N 3032791 FOUND CHAFED. NEW PART ON ORDER. (TC NR 20070528009)May 27, 2007 · Beech 1900C · Engine Fuel DistributionSDR ACE052607Wire · shortedPILOT REPORTED (CAN NOT TURN ON BATTERY POWER), LOCATED BLOWN 60 AMP. CURRENT LIMITER CAUSED BY SHORT TO GROUND ON NR 6 GAUGE WIRE (WIRE NR P30A6) AT BLEED AIR DUCT PN. 114-550159-1. REPAIRED WIRE AND DUCT (HOLE IN DUCT), REMOVED 1 FOOT OF EXCESS LENGTH OF WMay 26, 2007 · N111AX · Beech 1900C · Electrical Power System WiringSDR CA070522005Turbine Wheel · unknown(CAN) ECTM TREND INDICATED ENGINE ITT WAS INCREASING WITH TIME. ENGINE SPLIT. CT WHEEL NOTED AS CONTACTING THE GUIDE VANE ASSY. ENGINE TO BE SENT TO MFG TO INVESTIGATE. (TC NR 20070522005)May 21, 2007 · Beech 1900C · Turbine SectionSDR CA070424010Connector · corroded(CAN) ON (GEAR DOWN) SELECTION, CIRCUIT BREAKER FOR THE GEAR CONTROL POPPED AND THE GEAR REMAINED RETRACTED. AFTER A MISSED APPROACH THE NORMAL SOP`S WERE CARRIED OUT AND THE GEAR MANUALLY EXTENDED. AN UNEVENTFUL LANDING WAS THEN CARRIED OUT. ON INVESTIGATION Apr 18, 2007 · Beech 1900C · Landing Gear System WiringSDR CA070328004Oil Cooler · leaking(CAN) EXCESSIVE OIL NOTED ON LT ENGINE NACELLE. OIL LEAK TRACED TO LT ENGINE OIL COOLER. NEW OIL COOLER INSTALLED.Mar 27, 2007 · Beech 1900C · Engine Oil CoolerSDR ACE032707Stringer · corrodedLOCATED CORRODED STRINGER NR 14LH AT FS. 250.Mar 25, 2007 · N113AX · Beech 1900C · Fuselage Main, Longeron/StringerSDR CA070705005Fcu · defective(CAN) IN FLIGHT THE ENGINE EXPERIENCED AN UNCOMMANDED ACCELERATION RESULTING IN AN OVER-TORQUE CONDITION. SUBSEQUENT INSPECTION REVEALED A FAULTY FCU. (TC NR 20070705005)Mar 3, 2007 · Beech 1900C · Fuel Control/Turbine EnginesSDR CA070228006Mount · chafed(CAN) DURING ROUTINE MAINTENANCE A BLEED AIR LINE WAS FOUND CHAFING AN ENGINE TRUSS MOUNT TUBE. BLEED AIR LINE PN: 118-910033-93 TRUSS MOUNT PN: 129-910047-17. THE DAMAGE WAS FOUND TO BE WITHIN REPAIRABLE LIMITS IAW THE AIRCRAFT SRM. THE MOUNT WAS REPAIRED BY Feb 28, 2007 · Beech 1900C · Engine Mount SectionSDR HSYA200700001Rotor Shaft · shearedUPON REACHING ALTITUDE THE RT ENGINE LOST OIL AND FUEL PRESSURE AND THE ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. THE NR 2 ENGINE WAS REMOVED AND SENT FOR TEARDOWN TO DETERMINE CAUSE OF THE FAILURE. ON TEARDOWN TFeb 27, 2007 · N101UE · Beech 1900C · Turbine Engine Accessory DriveSDR ACE021607Relay · contaminatedMANUAL GEAR EXTENSION DUE NO GREEN LIGHTS AFTER HANDLE DOWN. CONFIRMED HYDRAULIC MOTOR RELAY LOGGED WITH WATER AND DUPLICATED FAILURE BY FREEZING RELAY, REPLACED RELAY.Feb 16, 2007 · N112AX · Beech 1900C · Landing Gear Retraction/Extension SystemSDR ACE02050702Motor · failedFLAPS STOPPED AT TAKEOFF. RETRACTED TO UP ON THE GROUND. THE SMELL OF HOT ELECTRICAL WAS STRONG. REPLACED FAILED FLAP MOTOR AND GEAR BOX.Feb 5, 2007 · N113AX · Beech 1900C · Trailing Edge Flap Control SystemSDR ACE020507Pump · rupturedRT FUEL PRESSURE ILLUMINATED WHEN RT STANDBY PUMP NOT ON, REPLACED FAILED LOW PSI PUMP DUE FUEL LEAKING FROM DIAPHRAGM.Feb 5, 2007 · N112AX · Beech 1900C · Fuel Boost PumpSDR ACE011507Diaphragm · rupturedPILOT REPORTED FUEL LEAKING FROM NR 1 ENGINE DRAIN LINE. REPLACED LOW PSI PUMP DUE DIAPHRAGM RUPTURE (SUSPECTED CAUSE).Jan 15, 2007 · N112AX · Beech 1900C · Fuel Boost PumpSDR ACE011107Coupling · disconnectedPILOT REPORTED NR 2 ENGINE LOW FUEL PRESSURE WARNING CAME ON. WARNING EXTINGUISHED AFTER SELECTING ELECTRIC STANDBY PUMP ON. MAINTENANCE REPLACED LOW PSI FUEL PUMP DUE INTERNALLY DISCONNECTED DRIVE SHAFT (SECOND OCCURRENCE OF THIS TYPE FAILURE ON THIS ENGINEJan 11, 2007 · N112AX · Beech 1900C · Engine Fuel PumpSDR CA070111013Fuel Line · chafed(CAN) THE FLIGHT CREW REPORTED FUEL LEAKAGE FROM THE RT ENGINE AREA AFTER SHUTDOWN. THE ENGINE COWLING WAS REMOVED AND INVESTIGATION HAD SHOWN THAT THE ENGINE DRIVEN FUEL PUMP TO FCU LINE HAD CHAFED AN THE BACK EDGE OF THE FCU. THE LINE IS ON CONDITION AND NOJan 8, 2007 · Beech 1900C · Engine Fuel DistributionSDR ACE010507Windshield · crackedPILOT REPORTED LT WINDSHIELD CRACKED AT 400 FT ON DEPARTURE. PILOT BURNED OFF FUEL AND RETURNED TO DEPARTURE FOR WINDSHIELD REPLACEMENT.Jan 5, 2007 · N111AX · Beech 1900C · Flight Compartment WindowsSDR CA070108002Downlock Switch · malfunctioned(CAN) THE AIRCRAFT ORIGINALLY EXPERIENCED A GEAR WARNING SYSTEM FAILURE ON APPROACH. SUBSEQUENTLY, THE DOWNLOCK SWITCHES WERE CLEANED AND LUBRICATED AND THE SYSTEM TESTED SERVICEABLE. THE NEXT FLIGHT HAD A LT MAIN GEAR INDICATION FAILURE, EMERGENCY PROCEDURESJan 3, 2007 · Beech 1900C · Landing Gear Position and WarningSDR CA070108001Landing Gear · inoperative(CAN) AIRCRAFT EXPERIENCED NO NOSE GEAR. (TC NR 20070108001)Jan 3, 2007 · Beech 1900C · Nose/Tail Landing GearSDR CA061220004Engine · malfunctioned(CAN) THE ENGINE EMITTED A LOUD NOISE ON TAKE-OFF ROLL. TAKE-OFF WAS ABORTED AND THE ENGINE SHUTDOWN. MFG WILL MONITOR INVESTIGATION OF THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20061220004)Nov 28, 2006 · Beech 1900C · Engine (Turbine/Turboprop)SDR ACE111406Actuator · failedPILOT REPORTED FLAPS WOULD NOT RETRACT AFTER LANDING, VERIFIED FAILED LT IB FLAP ACTUATOR, 1116 CSOH.Nov 14, 2006 · N112AX · Beech 1900C · Trailing Edge Flap ActuatorSDR ACE110706Diaphragm · rupturedPILOT REPORTED FUEL LEAK IN RT ENGINE. MAINTENANCE REPLACED LOW PSI FUEL PUMP DUE FUEL LEAKING FROM RELIEF VALVE AREA, DIAPHRAGM FAILURE VERIFIED (3Q05 DATED DIAPHRAGM). THIS WAS A NEW (NEW STYLE) PUMP.Nov 7, 2006 · N112AX · Beech 1900C · Fuel Injector NozzleSDR CA061026003Wheel · departed(CAN) PILOTS DISCOVERED NR 4 WHEEL ASSY MISSING AFTER ARRIVING AT DESTINATION. PASSENGER SAID A BANG WAS HEARD DURING TAKE-OFF. MAINTENANCE PERSONNEL DISPATCHED TO INSPECT AIRCRAFT, AND IF INSPECTED SERVICEABLE INSTALL NEW WHEEL ASSY AND RETURN TO BASE. AIRCROct 25, 2006 · Beech 1900C · Wheel/Ski/FloatSDR CA061002011Connector · damaged(CAN) FAULT - LT SIDE AUTOFEATHER LIGHT DOES NOT ARM. NR 2 HIGH PRESS FEATHER SWITCH CONNECTOR, CONNECTOR PIN LETTER B REPLACED. SWITCH CONNECTORS CLEANED. PROBLEM SEEMED TO BE CAUSED BY CONTAMINATION. (TC NR 20061002011)Sep 29, 2006 · Beech 1900C · Propeller/Propulsor System WiringSDR ACE092706Pulley · frozenPILOT REPORTED, THOUGHT THAT THE RUDDER HAD EXPERIENCED A -FREEZING- CONDITION WHILE IN FLIGHT (PROBLEM HAD RESOLVED ITSELF PRIOR TO LANDING). MAINTENANCE INSPECTED A KNOWN PROBLEM AREA UNDER THE CARGO FLOOR INSIDE THE CARGO DOOR (FS 505 WL 88) AT THE RUDDER Sep 27, 2006 · N111AX · Beech 1900C · Rudder Control SystemSDR FFS2006F00007Rivet · broken(3) RIVETS THROUGH THE WING SKIN INTO THE LT WING, REAR SPAR LOWER CAP, AFT FLANGE, AT LBL 115.875, 116.625 AND 117.625 WERE DISCOVERED BROKEN OR SHEARED. THE SHOP HEADS (TOP) OF THE RIVETS WERE IN PLACE AND LOOKED NORMAL DURING THE INSPECTION IAW AD 2006-16-Sep 10, 2006 · N575Y · Beech 1900C · Wing Main, Frame StructureSDR CA060911001Indicator · inoperative(CAN) DURING FLIGHT TRAINING GEAR WAS EXTENDED. THERE WAS NO RT MAIN GEAR DOWN AND LOCKED LIGHT. AN EMERGENCY GEAR EXTENSION WAS CARRIED OUT. RT MAIN GEAR LIGHT STILL NOT ILLUMINATED. LAMP TEST CARRIED OUT WITH GEAR HANDLE RED INTRANSIT LIGHT ILLUMINATED. PILOSep 9, 2006 · Beech 1900C · Landing Gear Position and WarningSDR ACE0830061Windshield · crackedPIREP - ON CLIMBOUT ONE WINDSHIELD SHATTERED AND THEN, FIVE MINUTES LATER, THE OTHER WINDSHIELD SHATTERED. UNEVENTFUL LANDING MADE, CREW VERIFIED ONLY OUTER PLYS WERE CRACKED AND AIRCRAFT RETURNED TO MAINTENANCE BASE FOR WINDSHIELD REPLACEMENTS.Aug 30, 2006 · N113AX · Beech 1900C · Flight Compartment WindowsSDR ACE0830062Windshield · crackedPIREP - ON CLIMBOUT ONE WINDSHIELD SHATTERED AND THEN, FIVE MINUTES LATER, THE OTHER WINDSHIELD SHATTERED. UNEVENTFUL LANDING MADE, CREW VERIFIED ONLY OUTER PLYS WERE CRACKED AND AIRCRAFT RETURNED TO MAINTENANCE BASE FOR WINDSHIELD REPLACEMENTS.Aug 30, 2006 · N113AX · Beech 1900C · Flight Compartment WindowsSDR ACE081306Fuel Control · defectivePILOT REPORTED NR 1 ENGINE WOULD NOT ACCELERATE ABOVE 35% ON START - REPLACED DEFECTIVE FUEL CONTROL UNIT.Aug 13, 2006 · N112AX · Beech 1900C · Fuel Control/Turbine EnginesSDR FFS2006F00006Door Frame · crackedDURING THE THIRD 200-HOUR INTERVAL DETAILED INSPECTION, A CRACK WAS DISCOVERED IN THE DOOR FRAME RUNNING HORIZONTALLY BETWEEN THE RIVET HOLES OF THE UPPER LINE OF RIVETS THAT HOLD THE AIRSTAIR DOOR HINGE HALF TO THE FUSELAGE. THE DOORFRAME PN 1144200341 WAS CAug 7, 2006 · N575P · Beech 1900C · Passenger/Crew DoorsSDR HSYA200600002Switch · out of adjustWHEN PERFORMING GEAR DOWN FOR LANDING, NO NOSE GEAR INDICATION. PERFORMED MANUAL EXTENSION IAW CHECKLIST. DID 2 FLYBYS SO MAINTENANCE COULD CHECK FROM GROUND. MAINTENANCE DETERMINED NOSE GEAR DOWN AND LOCKED. FOUND NOSE GEAR POSITION SWITCH OUT OF ADJUSTMEJul 24, 2006 · N319BH · Beech 1900C · Landing Gear Position and WarningSDR CA060731022Turbine Blades · fractured(CAN) FOLLOWING TAKEOFF THE ENGINE EMITTED A NOISE ACCOMPANIED BY AN UNCOMMANDED REDUCTION IN POWER. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES. MFG WILL MJul 20, 2006 · Beech 1900C · Turbine SectionSDR CA060731013Compressor · seized(CAN) DURING FLIGHT AN OIL SMELL WAS REPORTED IN THE COCKPIT. THE ENGINE SUBSEQUENTLY SURGED ACCOMPANIED BY A LOW OIL PRESSURE WARNING AND WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED OIL LEAKAGE AND A PARTIALLY SEIZED HIGH PRESSURE COMPRESSOR. MFJul 12, 2006 · Beech 1900C · Turbine Engine Compressor SectionSDR ACE071206Gas Generator · bindingPIREP - CREW SMELLED/SAW SMOKE IN COCKPIT, NR 1 ENGINE BEGAN TO SURGE, NR 1 ENGINE OIL PRESSURE WARNING LIGHT CAME ON. CREW SHUT DOWN NR 1 ENGINE. MAINTENANCE VERIFIED NR 1 ENGINE GAS GENERATOR INTERNAL FAILURE.Jul 12, 2006 · N112AX · Beech 1900C · Turbine SectionSDR ACE062306Pump · leakingPIREP - NR 1 ENGINE LEAKING FUEL AT DRAIN LINE. REPLACED FAILED (DIAPHRAGM RUPTURED) LOW PSI BOOST PUMP. THIS IS A NEW SYTLE PUMP.Jun 23, 2006 · N112AX · Beech 1900C · Engine Fuel PumpSDR CA060623002Fastener · loose(CAN) RUDDER QUADRANT P/N 101-500057-3 FOUND LOOSE ON INSPECTION. THREE MONEL BLIND RIVETS ATTACHING QUADRANT TO SHAFT ASSY. P/N 114-524025-1 WERE FOUND LOOSE AND DETERMINED TO BE THE CAUSE OF THE QUADRANT LOOSNESS. (TC# 20060623002)Jun 19, 2006 · Beech 1900C · Rudder StructureSDR CA061006016Planetary Gear · worn(CAN) DURING CLIMB, ENGINE POWER FLUCTUATED ACCOMPANIED BY AN INCREASE IN ITT TEMPERATURE AND LOW OIL PRESSURE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INVESTIGATION REVEALED FIRST STAGE PLANETARY GEAR DISTRESS. (TC NR 20061006016)Jun 15, 2006 · Beech 1900C · Turbine Engine Reduction GearSDR CA060615003Engine · surgesON CLIMB-OUT, THE AIRCRAFT EXPERIENCED A LEFT ENGINE SURGE WITH HIGH ITT AND LOW OIL PRESSURE INDICATIONS. THE CREW SHUT DOWN THE ENGINE IN FLIGHT AND RETURNED FOR AN UNEVENTFUL LANDING. MAINTENANCE PERSONNEL REPORTED DEBRIS IN THE EXHAUST AND OIL LEAKING FROJun 15, 2006 · Beech 1900C · Engine (Turbine/Turboprop)
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