Beech 1900C

Service difficulty reports · 1,841

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 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 AUS20040474Circuit Board · faulty(AUS) AIRFRAME DE-ICE SYSTEM PRINTED CIRCUIT BOARD (PCB) TIMER INOPERATIVE.May 25, 2004 · Beech 1900C · Airfoil Anti/De-ice SystemSDR CA040518007Hose · cracked(CAN) AFTER TAKE OFF CREW OBSERVED SPARKS AND GLOW FROM RT ENGINE COWL. CREW SHUTDOWN RT ENGINE AND RETURNED TO AIRPORT. MAINTENANCE FOUND THE FLEXIBLE HOSE FROM THE EXHAUST STACK TO THE LIP HEATER HAD CRACKED AND SEPERATED FROM THE COWLING. THIS ALLOWED THEMay 17, 2004 · Beech 1900C · Air Intake Anti/De-Ice SystemSDR CA040518003Hose · kinked(CAN) AFTER TAKE OFF, CABIN BEGAN TO FILL WITH FUMES AND OIL VAPOR. CREW TURNED OFF ENGINE BLEED AIR AND RETURNED TO AIRPORT. MAINTENANCE FOUND NR 1 ENGINE BREATHER HOSE HAD BEEN KINKED AND PINCHED CAUSING THE ACCESSORY CASE TO PRESSURIZE AND FORCE OIL TO PASSMay 15, 2004 · Beech 1900C · Turbine Engine Air Inlet SectionSDR CA040518008Selector Valve · intermittent(CAN) DURING APPROACH THE CREW NOTICED THAT THE LANDING GEAR WAS LOUDER THAN USUAL ANDSLOWER TO EXTEND. MAINTENANCE FOUND THE POWER PACK SELECTOR VALVE TO BE INTERMI TTENT AND THE POWER PACK TO BE NOISY. WITH THE AIRCRAFT ON JACKS THERE WERE TIMES WHEN THE GEAMay 8, 2004 · Beech 1900C · Hydraulic System, MainSDR ACE050504Pump · leakingPILOT REPORTED FUEL LEAKING FROM ENGINE DRAIN. MAINTENANCE REPLACED LOW PSI FUEL PUMP.May 5, 2004 · N112AX · Beech 1900C · Fuel Boost PumpSDR GLBA20030617Circuit Breaker · trippedGEAR WILL NOT TRANSIT UP OR DOWN, RESET 60 AMP C/B OPS CK GOODApr 26, 2004 · N122GL · Beech 1900C · Landing Gear SystemSDR 106041Display · inoperativeCAPTAINS VSI DISPLAY UN-USEABLE AND DISCHARGING BURNED ODORS IN CABIN REMOVED AND REPLACED CAPTAINS VSI PERFORMED SATISFACTORY STATIC CHECK IAW AMM 34-10-06.Apr 13, 2004 · N119CJ · Beech 1900C · Flight Environment DataSDR ACE032304Diaphragm · rupturedFOUND DIAPHRAGM LEAKING (RUPTURED) - THIS PUMP WAS BEING INSPECTED DUE TO AN ABORTED TAKEOFF AFTER ENGINE FLAME OUT. 1384 HOUR & 6 MONTHS AFTER INSTALL.Mar 22, 2004 · N114AX · Beech 1900C · Fuel Boost PumpSDR ACE032204Engine · flamed outNR 2 ENGINE FLAMED OUT ON TAKEOFF. ABORTED TAKEOFF. MAINTENANCE COULD NOT DUPLICATE.Mar 22, 2004 · N114AX · Beech 1900C · Engine (Turbine/Turboprop)SDR 072041Screw · looseDURING FLIGHT CONTROL CHECK, CONTROL COLUMN WOULD NOT RETURN TO FULL FORWARD POSITION. INSPECTED AND FOUND ONE SCREW MIGRATED FROM LEFT ELEVATOR, RESET SCREW AND SECURED WITH SPEED TAPE, FERRIED AIRCRAFT TO HEF, FOUND BALANCE WEIGHT ASSY AT O/B ELEVATOR L/E WMar 9, 2004 · N119CJ · Beech 1900C · FastenersSDR AUS20040165Transducer · unserviceable(AUS) RT ENGINE OIL PRESSURE TRANSDUCER FAULTY.Mar 6, 2004 · Beech 1900C · Engine Oil PressureSDR CA040309001Control Cable · severed(CAN) AFTER LANDING AND SUBSEQUENT TAXI THE RT ENGINE SPOOLED UP AND DID NOT RESPOND TO POWER LEVER MOVEMENT. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT COMPLETED TAXI TO THE TERMINAL ON THE LT ENGINE. MAINTENANCE INVESTIGATED AND DISCOVERED THAT THE POWER LEVEMar 3, 2004 · Beech 1900C · Power LeverSDR AUS20040058Hinge · corroded(AUS) RUDDER CENTER HINGE CONTAINED EXFOLIATION CORROSION IN THE HINGE BRACKET WEB.Feb 2, 2004 · Beech 1900C · Rudder/Tab, Attach FittingsSDR ACE013104Indicator · failedPILOT REPORTED CAPTAIN'S ALTIMETER FAILED (FLAGGED) AT 600 FT AFTER TAKEOFF. RETURNED TO AIRPORT. MAINTENANCE REPLACED THE FAILED ALTIMETER.Jan 31, 2004 · N114AX · Beech 1900C · Altimeter, Barometric/EncoderSDR CA040203004Relay · failed(CAN) LANDING GEAR FAILED TO EXTEND ON APPROACH. EMERGENCY EXTENSION WAS CARRIED OUT AND AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THAT THE LANDING GEAR MOTOR WAS NO LONGER RUNNING. THE LANDING GEAR RELAY WAS FOUND INTERNALLY DAMAGED WITH THE CONTACTS STUCK INJan 30, 2004 · Beech 1900C · Landing Gear Retraction/Extension SystemSDR ACE012504Diaphragm · rupturedMAINTENANCE NOTICED FUEL DRAINING FROM ENGINE GANG DRAIN - REPLACED LOW PSI FUEL PUMP DUE RUPTURED DIAPHRAGMJan 25, 2004 · N114AX · Beech 1900C · Fuel Boost PumpSDR FFS2004F00000Wire · shortedWHEN PERFORMING BUSS SENSE TEST, LOW VOLTAGE (11V-18V) WAS STILL PRESENT ON CENTER BUSS WITH BUSS TIE RELAYS OPEN. IT WAS DETERMINED SOURCE OF VOLTAGE WAS RT GENERATOR BUSS. WHILE SYSTEMATICALLY OPENING CB POWERED OFF RT GENERATOR BUS, VOLTAGE ON CENTER BUSSJan 16, 2004 · N575Z · Beech 1900C · Light System WiringSDR 2004F00226Skin · crackedDURING A SCHEDULED INSPECTION, A CRAC WAS DISCOVERD IN THE RUDDER SKIN. THE CRACK LOCATION WAS ABOUT 4 INCHES DOWN FROM THE TOP OF THE RUDDER. THE CRACK SPLIT THE TRAILING EDGE FOR ABOUT 1.5 INCHES THEN CRACKED TO OPPOSITE SIDES OF THE RUDDER FROM EITHER ENDJan 15, 2004 · N575X · Beech 1900C · Rudder, Plate/SkinSDR 015042Computer · odorR ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION, ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF ODOR YAW DAMP COMPUTER, YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C.Jan 14, 2004 · N210CJ · Beech 1900C · Autopilot SystemSDR 018041Actuator · maladjustmentNOSE GEAR UNSAFE, NOSE GEAR WOULD NOT EXTEND AND LOCK, NO GREEN LIGHT, AND RED LIGHT IN THE HANDLE REMAINED ILLUMINATED. RESET CIRCUIT BREAKER, NOSE GEAR CAME DOWN. REPLACED ALL THREE RETRACT ACTUATORS, HYD SERVICE VALVE, AND FLUSHED SYSTEM.Jan 14, 2004 · N32017 · Beech 1900C · Landing Gear ActuatorSDR 016041Computer · malfunctionedRT ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF ODOR YAW DAMP COMPUTER. YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C.Jan 14, 2004 · N210CJ · Beech 1900C · Autopilot SystemSDR 015043Computer · malfunctionedRIGHT ENVIR OFF LIGHT FAILS TO ILLUMINATE WITH BLEED AIR VALVE IN OFF POSITION, ELECTRICAL ODOR IN MAIN CABIN. SOURSE OF ODOR YAW DAMP COMPUTER. YAW DAMP COMPUTER DEFERRED PER MEL 22-1 CAT C.Jan 14, 2004 · N210CJ · Beech 1900C · Autopilot SystemSDR 013041Handle · lack of lubePAX DOOR HANDLE HARD TO TURN. LUBED DOOR HANDLE, OPS CHECKED GOOD.Jan 12, 2004 · N210CJ · Beech 1900C · Passenger/Crew DoorsSDR CA040121004Windshield · broken(CAN) WINDOW SHATTERED IN CRUISE, INSIDE AND OUT SIDE PANE.Jan 4, 2004 · Beech 1900C · Flight Compartment WindowsSDR ACE122403Exhaust Duct · disconnectedPILOT REPORTED EXHAUST SMELL IN CABIN ON TAKEOFF AND CLIMB. MAINTENANCE LOCATED A DISCONNECTED NR 1 ENGINE INTAKE HEATED LIP (EXHAUST DUCT) TUBE. EXHAUST COULD HAVE BEEN INGESTED BY THE ENGINE AND THEN MIXED WITH THE BLEED AIR. NO PART FAILURE WAS OBSERVED.Dec 24, 2003 · N111AX · Beech 1900C · Engine Collector/Tailpipe/NozzleSDR AUS20031295Seal · split(AUS) CABIN DOOR SEAL SPLIT ALONG TOP SECTION. LENGTH OF SPLIT APPROXIMATELY 50MM (1.96IN).Dec 23, 2003 · Beech 1900C · Passenger/Crew DoorsSDR CA040107005Heater · cracked(CAN) OIL PRESSURE ANNUNCIATOR ILLUMINATED FOLLOWED BY OIL PRESSURE FLUCTUATIONS. CREW THEN SHUT ENGINE DOWN AND LANDED WITH NO FURTHER PROBLEMS. UPON INSPECTION BY MAINTENANCE IT WAS CLEAR THAT THERE WAS AN EXCESSIVE OIL LEAK AND LOW OIL LEVEL. THIS WAS THE CDec 19, 2003 · Beech 1900C · Fuel HeaterSDR CA031218003Latch · failed(CAN) AFTER COMPLETING FLIGHT AND TAXIING THE PILOT WAS UNABLE TO OPEN THE AIRSTAIR DOOR TO DISEMBARK PASSENGERS. THEY WERE REQUIRED TO EXIT THE AIRPLANE USING THE OVER WING EMERGENCY EXIT. BEFORE MAINTENANCE PERSONNEL WERE ABLE TO ARRIVE ON THE SCENE THE PILNov 29, 2003 · Beech 1900C · Passenger/Crew DoorsSDR AUS20031218Cap · cracked(AUS) NOSE LANDING GEAR ACTUATOR END CAP CRACKED.Nov 25, 2003 · Beech 1900C · Landing Gear ActuatorSDR ACE112503Warning System · malfunctionedNOSE GEAR FAILED TO SHOW DOWN AND LOCKED UNTIL GEAR WAS CYCLED TWICE. MAINTENANCE COULD NOT DUPLICATE FAULT.Nov 25, 2003 · N113AX · Beech 1900C · Landing Gear Position and WarningSDR JIKA200300002Line · chafedAFTER SHUT DOWN OF LT ENGINE GROUND CREW OBSERVED FUEL LEAKING FROM LT ENGINE COWLING. UPON INVESTIGATION MAINTENANCE FOUND THE FUEL FLOW TRANSDUCER INLET LINE CHAFED AND LEAKING FROM THE CHAFED AREA. THE STARTER GENERATOR COOLING DUCT SCAT TUBING WAS THE CANov 16, 2003 · N31701 · Beech 1900C · Engine Fuel DistributionSDR TIM2003F00001Bulkhead · crackedBULKHEAD FOUND TO BE CRACKED AT INSPECTION. (CNTRL NR 81)Nov 5, 2003 · N195GA · Beech 1900C · Fuselage Main, BulkheadSDR 297031Circuit Card · malfunctionedDURING TAKEOFF ROLL MASTER CAUTION ILLUMINATED TO INDICATE THAT BOTH THE LEFT AND RIGHT GEN TIES WERE OPEN ONE ATTEMPT WAS MADE TO RESET. DID NOT RESET, THE TAKEOFF WAS ABORTED.Oct 22, 2003 · N207CJ · Beech 1900C · Central WarningSDR CA031027008Shaft · sheared(CAN) ELECTRIC TRIM (ELEVATOR) DRIVE SHAFT SHEARED. THIS CAUSED ONE CAPSTAND TO OPERATE AND THE OTHER TO MOVE FREELY ON ITS OWN. THIS MOVEMENT CAUSED THE BRIDAL CABLES TO UNWIND AND CREATE RESTRICTION. THE TRIM WAS RESTRICTED FROM GOING NOSE DOWN. MANUAL MOVEMOct 11, 2003 · Beech 1900C · Elevator Tab Control SystemSDR 2004F00207Windshield · crackedCO-PILOT OUTER WINDSHIELD PANE CRACKED. CRACKS OCCURRED DURING THE APPROACH PHASE OF THE FLIGHT AT ABOUT 3,000 FEET MSL WITH MINIMAL CAIBN DIFFERENTIAL PRESSURE. WINDSHIELD HEAT WAS ON AND WORKING AT THE TIME. OUTSIDE AIR TEMPERATURE WAS WITHIN A COUPLE OF Oct 6, 2003 · N575A · Beech 1900C · Flight Compartment WindowsSDR CA031016003Line · cracked(CAN) ON APPROACH INTO SEATTLE THE RT ENGINE POWER DECREASED SLOWLY ON ITS OWN. THE CREW SHUTDOWN AND SECURED THE ENGINE. THE AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED FROM THE RAMP. DURING INVESTIGATION BY MAINTENANCE IT WAS FOUND THAT THE ENGINE WOULD ACTUOct 5, 2003 · Beech 1900C · Propeller GovernorSDR AUS20031030Engine · fluctuates(AUS) LT ENGINE TORQUE FLUCTUATIONS. FUEL FLOW, N1 AND ITT STABLE. GROUND RUN CARRIED OUT. UNABLE TO FAULT. DEFECT NOT CONFIRMED.Oct 2, 2003 · Beech 1900C · Engine (Turbine/Turboprop)SDR ACE093003Csd · failedPILOT REPORTED NR 2 ENGINE TORQUE STARTED TO SURGE (1500 LBLS) AND WAS SHUT DOWN PER THE QRH. MAINTENANCE REPLACED THE NR 2 ENGINE CONSTANT SPEED GOVERNOR AND OVERSPEED GOVERNOR FOR TROUBLESHOOTING (THE REPORTED PROBLEM COULD NOT BE DUPLICATED ON THE GROUND).Sep 30, 2003 · N112AX · Beech 1900C · AC Generation SystemSDR CA030924001Seal · detached(CAN) SEAL BECAME DETACHED FROM RETAINER AT UPPER AFT CORNER OF AIRSTAIR DOOR CAUSING RAPID DEPRESSURIZATION OF AIRCRAFT IN FLIGHT.Sep 22, 2003 · Beech 1900C · Passenger/Crew DoorsSDR ACE0918021Diaphragm · perforatedON PREFLIGHT INSPECTION, PILOT NOTICED FUEL LEAKING FROM THE ENGINE GANG DRAIN. MAINTENANCE REPLACED THE LOW PSI FUEL PUMP DUE TO FUEL DRAINING FROM THE DRY SIDE OF THE PRESSURE RELIEF VALVE ASSEMBLY. DISASSEMBLY OF THE PUMP REVEALED MULTIPLE HOLES IN THE DISep 18, 2003 · N1563C · Beech 1900C · Aircraft Fuel Distribution SystemSDR JIKASkin · corrodedDURING MAINTENANCE FOR A PRESSURIZATION SQUAWK FOUND THE LOWER BELLY SKIN AT FUSELAGE STATION 258.25 HAD A CRACK EMINATING FROM A RIVET HEAD AND THE SKIN AROUND THE RIVET WAS BULGED OUT. UPON FURTHER INSPECTION UNDER THE FLOOR BOARDS FOUND HEAVY CORROSION ON Sep 18, 2003 · N31701 · Beech 1900C · Fuselage Main, Plate/SkinSDR ACE091103Pump · leakingPILOT NOTICED FUEL LEAKING FROM ENGINE DRAIN ON PRE-FLIGHT. MAINTENANCE REPLACED THE DEFECTIVE PUMP.Sep 11, 2003 · N114AX · Beech 1900C · Fuel Boost PumpSDR AUS20030924Bearing · collapsed(AUS) LT ENGINE STARTER-GENERATOR DRIVE END BEARING COLLAPSED.Sep 8, 2003 · Beech 1900C · Starter-GeneratorSDR AUS20030887Indicator · inoperative(AUS) LT ENGINE PERCENT RPM INDICATOR FAULTY.Sep 1, 2003 · Beech 1900C · Engine RPM Indicating SystemSDR ACE082503Fuel Control · faultyNR 2 ENGINE STARTED TO SURGE AND THEN LOST POWER - PILOTS SECURED THE ENGINE AND MADE AN UNEVENTFUL LANDING AT THE AIRPORT OF ORIGIN. REPLACED FCU.Aug 25, 2003 · N112AX · Beech 1900C · Fuel Controlling SystemSDR ACE081603Relay · contaminatedPILOT REPORTED THAT IT TOOK MULTIPLE ATTEMPTS TO EXTEND THE GEAR WITH THE ELECTRO/HYDRAULIC SYSTEM. GEAR DID EXTEND AND UNEVENTFUL LANDING ACCOMPLISHED IN ANC. MAINTENANCE REPLACED THE HYD. POWER PACK RELAY (HEAVY CONDENSATION).Aug 16, 2003 · N112AX · Beech 1900C · Landing Gear Retraction/Extension SystemSDR AUS20030731Uplock Switch · unserviceable(AUS) RT MAIN LANDING GEAR UPLOCK SWITCH UNSERVICEABLE.Jul 23, 2003 · Beech 1900C · Landing Gear Position and WarningSDR ACE071903Fire Loop · defectiveRIGHT ENGINE FIRE LIGHT CAME ON IN FLIGHT REQUIRING ENGINE SHUTDOWN. PILOT REPORTED THAT WARNING DISCONTINUED 15 MINUETS AFTER ENGINE SHUTDOWN. SYSTEM OPS CHECKED GOOD ON GROUND AFTER LANDING. MAINTENANCE INSPECTED WARNING SYSTEM AND REPLACED FORWARD LOOP DJul 19, 2003 · N112AX · Beech 1900C · Fire DetectionSDR 1850301Handle · out of adjustEMERGENCY EXIT LOOSE IN LOCKED POSITION. ADJUSTED EXIT DOOR HANDLE TENSION.Jul 2, 2003 · N207CJ · Beech 1900C · Emergency ExitsSDR 113AX62603Intercostal · crackedWHILE C/W STRUCTURAL INSPECTION 53-10-02, FOUND .5 INCH CRACK IN OUTER FLANGE RADIUS OF INTERCOSTAL PN 114-430116-7 AT STATION NR 498.25 AND ADJACENT TO THE CARGO DOOR AFT UPPER GAS STRUT ATTACH BRACKET MOUNTED TO THE DOOR FRAME.Jun 26, 2003 · N113AX · Beech 1900C · Fuselage Miscellaneous Structure
Back to Beech 1900C