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 YAD2002F00000Wire · damagedAFTER TAKEOFF FROM BARROW, LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT CONTINUED TO ANCHORAGE AND MADE AN UNEVENTFUL LANDING. MAINTENANCE LOCATED AND REPLACED WIRE G7C22, DUE TO HIGH RESISTANCE, BETWEEN LEFT FUSELAGE AND CONNECTOR J107.Dec 6, 2001 · N1553C · Beech 1900C · Landing Gear System WiringSDR ACE1205011Wire · shortedAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT CONTINUED AND MADE AN UNEVENTFUL LANDING. MAINTENANCE LOCATED AND REPLACED WIRE C7C22, DUE TO HIGH RESISTANCE, BETWEEN LEFT FUSELAGE AND CONNECTOR J107.Dec 2, 2001 · N1553C · Beech 1900C · Landing Gear System WiringSDR ACE1121011Blade · failedJUST AFTER TAKEOFF, THE LT ENGINE MADE A LOUD NOISE AND TORQUE DROPPED OFF. THE ENGINE WAS SECURED AND THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED A FAILURE OF THE CT DISK BLADES, CAUSE UNKNOWN. THE ENGINE WAS REMOVED FOR REPAINov 23, 2001 · N1566C · Beech 1900C · Turbine Engine Compressor SectionSDR 2001F00724Engine · malfunctionedAUG - DURING TAKEOFF ROLL, RIGHT OIL PRESS LIGHT CAME ON. ABORTED TAKEOFF. TAXI BACK TO GATE, OIL PRESS GAUGE READ BETWEEN 30-50 PSI. REMOVED AND REPLACED RIGHT ENGINE LEAK AND OPS CHECK GOOD. (M)Nov 20, 2001 · N119CJ · Beech 1900C · Engine (Turbine/Turboprop)SDR ACE1116011Control Cable · frozenPILOT REPORTED RUDDER FROZEN IN FLIGHT, UNEVENTFUL LANDING MADE. PILOT REPORTED THE RUDDER BROKE FREE WHILE TAXING REMOVED CARGO COMPARTMENT FLOOR AT CARGO DOOR AND OBSERVED WATER FROZEN AROUND RUDDER CABLE PULLEYS AT FUSELAGE STATION 495. REMOVED WATER AFTENov 16, 2001 · N111AX · Beech 1900C · Rudder Control SystemSDR ACE1105011R1Switch · failedON APPROACH TO LANDING, NOSE GEAR GREEN LIGHT DIDN`T COME ON WITH GEAR HANDLE SELECTED DOWN. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY ON THE GROUND. THE NOSE GEAR UP AND DOWNLOCK SWITCH AND CONNECTOR WERE REPLACED AND AN OPERATIONAL CHECK FLIGHT WAS PNov 8, 2001 · N41UE · Beech 1900C · Landing Gear ActuatorSDR ACE110820011Engine · failedON DESCENT, NR 2 ENGINE TORQUE BEGAN TO FALL AND THE NR 2 ENGINE OIL PRESSURE WARNING LIGHT CAME ON. THE ENGINE WAS SECURED. THE ODOR OF OIL SMOKE WAS IN THE CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED A LACK OF ENGINE OIL ON THE DIP Nov 8, 2001 · N1563C · Beech 1900C · Engine (Turbine/Turboprop)SDR ACE1105011Pin · corrodedON APPROACH TO LANDING, NOSE GEAR GREEN LIGHT DID NOT COME ON UNTIL GEAR WAS CYCLED. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY ON THE GROUND AND TROUBLE SHOT TO A CORRODED CONNECTOR PIN IN THE UP/DOWN LOCK SWITCH CIRCUIT.Nov 6, 2001 · N41UE · Beech 1900C · Landing Gear Position and WarningSDR ACE1104011Indicator · erraticON TAKE OFF RUN, PILOT OBSERVED HIGH (920 DEG). ITT INDICATION ON NR1 ENGINE AND ABORTED THE TAKE OFF. MAINTENANCE REPLACE THE NR1 ITT INDICATOR DUE ERRONEOUS INDICATION AT THE HIGH END OF THE SCALE.Nov 5, 2001 · N41UE · Beech 1900C · Engine EGT/TIT Indicating SystemSDR NSV2001F00001Governor · failedRKD-RH PROP RPM DROPPED TO 1400 DURING TAKE OFF ROLL. OFF WAS ABORTED AIRCRAFT RETURNED TO GATE. MECHANIC REMOVED AND REPLACED PROP GOVERNOR, RIGGED AS REQUIRED. OPS CHECKED GOOD.Nov 2, 2001 · N550CJ · Beech 1900C · Propeller GovernorSDR ACE1031011Pump · leakingA FAILED NR 2 ENGINE LOW PRESSURE FUEL BOOST PUMP WAS IDENTIFIED WHILE THE AIRCRAFT WAS IN THE HANGAR FOR OTHER MAINTENANCE. THE FAILURE WAS IDENTIFIED BY FUEL DRIPPING OUT OF THE NR 2 ENGINE GANG DRAIN DUE TO PREVIOUS COMPLIANCE WITH MFG MANDATORY SB 71-3307Nov 1, 2001 · N1563C · Beech 1900C · Fuel Boost PumpSDR NSV2001F00000Blade · chippedMIX DISCOVERED A CHIP IN THE BLADE FACE OF THE NR 1 PROP DURING A PREFLIGHT INSPECTION. MECHANIC LOG ENTRY READS OK FOR CONTINUED SERVICE (IAW 811303 FROM HARTZELL PROPELLERS)Nov 1, 2001 · N32017 · Beech 1900C · Propeller Blade SectionSDR ACE1029011Fitting · leakingON DEPARTURE, THE GEAR WARNING LIGHTS (HANDLE) CAME ON. THE GEAR WOULD NOT CYCLE WITH THE ELECTRIC PUMP. THE GEAR WAS EXTENDED WITH THE HAND PUMP. THE CREW CONTINUED THE FLIGHT AS REQUIRED TO BURN FUEL DOWN TO LANDING WEIGHT AND THE AIRCRAFT MADE AN UNEVENTOct 29, 2001 · N1566C · Beech 1900C · Hydraulic System, MainSDR TIM2001F00012Control Cable · defectiveINSPECTION OF FLAP CABLES AS OUTLINED IN MFG SB AS REQUIRED BY AD REVEALED THE LEFT OUTBOARD FLAP CABLE DEFECTIVE. THE CABLE HAD STARTED TO UNWIND.Oct 29, 2001 · N195GA · Beech 1900C · Trailing Edge Flap Control SystemSDR ACE1025011R1Actuator · failedON APPROACH, NOSE GEAR GREEN DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE AFTER TWO NORMAL CYCLES AND ONE MANUAL EXTENSION. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE COULD NOT CONFIRM FAILURE DUE ILLUMINATION OF THE NOSE GEAR GREEN LIGHT AFTER THE Oct 26, 2001 · N1566C · Beech 1900C · Landing Gear ActuatorSDR ACE1025011Downlock Switch · brokenON APPROACH, NOSE GEAR GREEN DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE INITIALLY, IT CAME ON A FEW MINUTES AFTER THE GEAR WAS DOWN. THE AIRCRAFT WAS FERRIED WITH THE GEAR DOWN. MAINTENANCE FOUND ONE WIRE IN THE DOWN AND LOCK SWITCH HARNESS CORRODED AND BROKOct 25, 2001 · N1566C · Beech 1900C · Landing Gear Position and WarningSDR ACE1024011Relay · burnedON ARRIVAL, THE LANDING GEAR MOTOR CIRCUIT BREAKER POPPED, THE LOW HYDRAULIC LEVEL ENUNCIATOR CAME ON AND THE GEAR HAD TO BE MANUALLY EXTENDED. AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND THE HYDRAULIC PUMP MOTOR VERY HOT AND THE CONTACTS IN THE MOTOR Oct 24, 2001 · N45GL · Beech 1900C · Hydraulic Pump (Electric/Engine), MainSDR FFSA90153Windshield · crackedON CLIMBOUT AT ABOUT 15,000 FEET ALTITUDE THE PILOTS HEATED WINDSHIELD SUDDENLY DEVELOPED CRACKS RUNNING THROUGHOUT THE WINDOW. THE AIRCRAFT DESCENDED AND RETURNED TO AIRPORT.Oct 24, 2001 · N575Z · Beech 1900C · Flight Compartment WindowsSDR 2001F00473Trim Motor · failedON APPROACH TO LANDING PILOT ATTEMPTED TO TRIM NOSE UP WITH NO RESPONSE USING ELECTRIC TRIM. PILOT ATTEMPTED TO USE MANUAL TRIM AND THE TRIM WHEEL WOULD NOT TURN. PILOT LANDED AIRCRAFT WITHOUT INCIDENT. UPON INSPECTION OF ELEVATOR TRIM SYSTEM FOUND ELECTRICOct 23, 2001 · N31701 · Beech 1900C · Elevator Tab Control SystemSDR ACE1018011Landing Gear · icedON ARRIVAL, THE LANDING GEAR SELECTOR HAD TO BE CYCLED MULTIPLE TIMES TO ACHIEVE GEAR DOWN AND SAFE INDICATION. MAINTENANCE COULD NOT DUPLICATE THE FAULT AND INSPECTED THE SYSTEM, INCLUDING MULTIPLE SATISFACTORY CYCLES. THE POSSIBILITY THAT THE FAULT WAS ICIOct 18, 2001 · N45GL · Beech 1900C · Landing Gear SystemSDR TIM2001F00010Bulkhead · crackedTHE RIGHT ENGINE COWLING BULKHEAD AT STATION 238.18 THAT THE LOWER FRONT ENGINE COWLING ATTACHES TO WAS CRACKED ON THE RIGHT LOWER SIDE. THIS LOCATION IS WERE ONE OF THE FOUR BOLTS SECURE THE LOWER COWL TO THE BULKHEAD. (PICTURES INCLUDED)Oct 15, 2001 · N153GA · Beech 1900C · Engine Cowling SystemSDR NSVA0118Fire · detectedIAD - DURING ENGINE START OF NR 2 ENGINE THE GROUND CREW NOTICED A SIX FOOT FLAME FROM THE TAIL PIPE. PILOT SHUT FUEL OFF AND FLAMES EXTINGUISHED. MX MOTORED ENGINE AND FOUND NO DAMAGE OR EVIDENCE OF RESIDUAL FUEL IN TAIL PIPE. PILOT RESTARTED ENGINE WITH NOct 10, 2001 · N32017 · Beech 1900C · Engine (Turbine/Turboprop)SDR YAD2003F00003Fire Loop · false indicationFLIGHT CREW RETURNED TO RAMP AFTER INDICATION OF FIRE IN THE NR 1 ENGINE. MAINTENANCE VERIFIED THAT THE WARNING WAS FALSE AND WAS CAUSED BY CONTACT BETWEEN THE FORWARD FIRE DETECT LOOP AND A DISCONNECTED O/B HEATED INTAKE LIP FLEX TUBE. MAINTENANCE REPLACED Oct 5, 2001 · N1563C · Beech 1900C · Fire DetectionSDR ME42001F00002Bushing · swollenPROP WAS REPAIRED FOR FAILURE TO GO INTO FEATHER. REALIGNED TWISTED BETA COLLAR AND REPAIR SPRING KIT. PROP WAS JERKING AS IT WENT INTO FEATHER, BETA RING DID NOT COME BACK TO FULLY EXTENDING POSITION. 2 OF 4 BETA SUPPORT GUIDE LUG BUSHINGS WERE FOUND SWOLLEOct 5, 2001 · N38SU · Beech 1900C · Propeller GovernorSDR 2001F00624Shaft · damagedINSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION.Oct 4, 2001 · N153GA · Beech 1900C · Trailing Edge Flap Control SystemSDR 2001F00622Shaft · damagedINSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION.Oct 4, 2001 · N153GA · Beech 1900C · Trailing Edge Flap Control SystemSDR 2001F00621Shaft · damagedINSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION.Oct 4, 2001 · N153GA · Beech 1900C · Trailing Edge Flap Control SystemSDR NSVA0115Control Panel · faultyDURING TAKEOFF ROLL FROM ACK, PILOTS NOTED AUTO FEATHER LIGHT DID NOT COME ON, ALSO LEFT AND RIGHT ANTI-ICE C/B POPPED. CAPTAIN ELECTED TO ABORT TAKEOFF AND RETURN TO GATE. MAINTENANCE TROUBLESHOT PROBLEM DOWN TO BAD LEFT BUS TIE RELAY. REMOVED AND REPLACEDOct 1, 2001 · N129CJ · Beech 1900C · DC Power Distribution SystemSDR CA011018010Wire · chafed(CAN) ON LANDING, CREW SELECTED GEAR DOWN, LANDING GEAR CIRCUIT BREAKER "POPPED", TRANSIT HANDLE LIGHT ILLUMINATED "RED", MANUAL GEAR EXTENSION PERFORMED, 3 GREEN LIGHTS INDICATED. AIRCRAFT LANDED WITHOUT INCIDENT.MAINTENANCE INVESTIGATION FOUND A CHAFED WIRSep 25, 2001 · Beech 1900C · Landing Gear Retraction/Extension SystemSDR NSVA0112Inverter · failedNR 1 INVERTER FAILED ON TAKEOFF ROLL, ABORTED TAKEOFF RETURNED. MAINTENANCE REMOVED AND REPLACED THE NR 1 INVERTER TEST RUN. OPS CHECK GOOD. AIRCRAFT RELEASE FROM MAINTENANCE. (M)Sep 25, 2001 · N129CJ · Beech 1900C · AC InverterSDR YAD2003F00005Gas Generator · seizedAC DEPARTED AND GOING THROUGH 5,000 FT THE COPILOT REPORTED SEEING AN ORANGE FLASH FROM THE RT ENGINE, THEN LOUD NOISE AND FLASH OF FIRE FROM THE NR 2 ENG EXHAUST, PILOT REPORTED THAT ENGINE SEIZED AND WAS SECURED. NO FIRE WARNING WAS RECEIVED AND THE FIRE EXSep 24, 2001 · N5632C · Beech 1900C · Turbine Engine Compressor SectionSDR NSVA0114Skin · dentedDURING ROUTINE MAINTENANCE/INSPECTION, SOME DAMAGE WAS DISCOVERED ON THE LEFT WING LEADING EDGE AREA. AIRCRAFT WAS REPAIRED IAW DER REPORT 01-249, WO 20354. (M)Sep 13, 2001 · N550CJ · Beech 1900C · Wing, Plate/SkinSDR TIM2001F00008Motor · shortedAIRCRAFT FILLED WITH SMOKE, CREW MADE AN EMERGENCY LANDING. CHECK OF AIRCRAFT SYSTEMS FOUND THE FORWARD EVAPORATOR MOTOR SHORTED. AIRCRAFT WAS FURTHER INSPECTED FOR DAMAGE, NONE FOUND.Sep 6, 2001 · N153GA · Beech 1900C · Air Distribution FanSDR CA011012004Gcu · failed(CAN) AIRCRAFT DEPARTED SMITHERS, THE LT GENERATOR KICKED OFF LINE FOLLOWED BY A FAINT ELECTRICAL ODOR. THEY RETURNED TO THE SMITHERS AIRPORT AND DEPLANED PASSENGERS. MAINTENANCE FOUND LT GENERATOR CONTROL UNIT TO BE EMITTING ODOR. IT WAS REPLACED ALONG WITH TAug 31, 2001 · Beech 1900C · Starter-GeneratorSDR CA010905005Starter Gen · overheated(CAN) A/C DEPARTED AIRPORT, 5 MINUTES AFTER TAKEOFF THE LT GENERATOR ANNUNCIATOR ILLUMINATED & CREW REPORTED SMELLING A STRANGE BURNING ODOUR. THEY TURNED A ROUND RETURNED TO AIRPORT. AN UNEVENTFUL LANDING WAS MADE & A/C SENT TO HANGAR. THE FLOOR BOARDS WERE LAug 31, 2001 · Beech 1900C · Starter-GeneratorSDR TIM2001F00007Panel · debondedLEFT INBOARD UPPER WING PANEL AFT OF WING SPAR DE-BONDING BETWEEN UPPER WING SKIN AND HONEYCOMB INSIDE FUEL BAY AREA.Aug 23, 2001 · N195GA · Beech 1900C · Wing, Plate/SkinSDR 2001F00291Fcu · failedFLT 9139 - RSW/TPA - EN ROUTE FROM RSW TO TPA, THE RIGHT ENGINE LOST POWER. ADVANCED POWER LEVER AND THE RIGHT ENGINE CONTINUED TO LOSE POWER. FLIGHT CREW SECURED THE ENGINE. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED RIGHT FUEL CONTROAug 21, 2001 · N130GA · Beech 1900C · Fuel Control/Turbine EnginesSDR NSVA0109Fcu · malfunctionedEN ROUTE FROM BOS-BHB, CREW NOTED THE FOLLOWING DISCREPANCY IN FIGHT LOG; LEFT ENGINE PARAMETERS DID NOT CHANGE WITH POWER LEVER CHANGES. AT THAT TIME THE CREW DECLARED AN IN FLIGHT EMERGENCY AND PRECEDED TO BHB. UPON LANDING ROLL OUT AT BHB, THE CREW NOTICEAug 20, 2001 · N207CJ · Beech 1900C · Fuel Control/Turbine EnginesSDR NSVA0107Fire Loop · damagedLEFT ENGINE FIRE LIGHT CAME ON DURING TAXI. PRELIMINARY INSPECTION LOCATED FAULT, AIRCRAFT RELEASED UNDER SFP TO HYA. MAINTENANCE REMOVED AND REPAIRED FORWARD SECTION OF FIRE LOOP, OPS CHECK GOOD.Aug 18, 2001 · N15031 · Beech 1900C · Fire DetectionSDR 2001F00290Wire · chafedFLT - 9262 - FPO-PBI - ON LANDING, LEFT FUEL VENT CIRCUIT BREAKER BEGAN TO EMIT SMOKE. MANUALLY PULLED CIRCUIT BREAKER. SMOKE STOPPED. CONTINUED TO LAND WITHOUT INCIDENT. DETERMINED WIRING ON LEFT FUEL VENT ASSEMBLY TO BE CHAFED. REPLACED LEFT FUEL VENT AAug 9, 2001 · N151GA · Beech 1900C · Fuel System WiringSDR 2001F00289Switch · dirtyFLT 9437 - TLH-TPA - DURING LANDING, RIGHT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED. CLEANED RIGHT FIRE EXTINGUISHER TEST SWITCH. OPERATIONAL TEST NORMAL ON THE GROUND. (M)Aug 8, 2001 · N137GA · Beech 1900C · Extinguishing SystemSDR 2001F00285Engine · lack of lubeFLT 5202 - TNT-MIA - DURING FLIGHT, LEFT ENGINE OIL PRESSURE ANNUNCIATOR ILLUMINATED AND OIL PRESSURE DROPPED TO 40 PSI. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. INSPECTED LEFT ENGINE. NO LEAKS NOTED. NO SIGNS OF CONSUMPTION NOTED. CHECKED ENGINE HISTORY Aug 8, 2001 · N120GP · Beech 1900C · Turbine Engine Oil SystemSDR NSVA0105Compressor · stalledPILOT WAS IN FLIGHT AND FOUND THE TRIM WHEEL DIFFICULT TO MOVE AFTER ADVANCING POWER LEVERS. WHILE TRYING TO DUPLICATE PROBLEM IN FLIGHT BY ADVANCING AND RETARDING THROTTLES, THE PILOT REPORTED AN INSTANTANEOUS AND MOMENTARY SHUTDOWN OF THE RIGHT ENGINE. MAIAug 4, 2001 · N210CJ · Beech 1900C · Turbine Engine Compressor SectionSDR 2001F00236Hydraulic Line · leakingFLT 9495 - MIA/FPO - DURING POST FLIGHT WALK AROUND, NOTICED RIGHT MLG HYDRAULIC LINE RUPTURED. REMOVED AND REPLACED RIGHT MLG HYDRAULIC LINE. OPS CHECK NORMAL. (M)Jul 26, 2001 · N139GA · Beech 1900C · Hydraulic System, MainSDR YAD2001F00008Switch · failedCABIN ALTITUDE WAS NOTED AT 16,000 FT (DUE IMPACT - DAMAGE TO FUSELAGE) IN FLIGHT - CREW STATED USING SUPPLEMENTAL OXYGEN AT THIS POINT. CABIN ALTITUDE WARNING DID NOT FUNCTION, WARNING LIGHT SHOULD COME ON AT 12,250 FT. REPLACED DEFECTIVE SWITCH. WARNING Jul 25, 2001 · N45GL · Beech 1900C · Ground Proximity SystemSDR CA010809003Shaft · sheared(CAN) QUILL SHAFT IN AIR CONDITIONING COMPRESSOR DRIVE SHEARED AT SHEAR POINT BEHIND SPLINE. SHAFT REPLACED & AIRCRAFT RETURNED TO SERVICE.Jul 25, 2001 · Beech 1900C · Cabin Cooling SystemSDR YAD2001F00009Gauge · shortedSMELL OF SMOKE, PULLED RIGHT FUEL GAUGE CIRCUIT BREAKER, SMELL WENT AWAY. VERIFIED SMOKE WAS FROM RIGHT FUEL GAUGE, PULLED AND BANDED RIGHT FUEL GAUGE CIRCUIT BREAKER. RIGHT FUEL QUANTITY GAUGE PREVIOUSLY DEFERRED.Jul 24, 2001 · N41UE · Beech 1900C · Fuel Quantity IndicatorSDR 2001F00212Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M)Jul 22, 2001 · N139GA · Beech 1900C · Elevator StructureSDR 2001F00217Engine · failedFLT 9307 - PBI/NAS - DURING FLIGHT FROM PBI TO NAS AT 11,000 FEET, THE RIGHT ENGINE SURGED AND INDICATIONS FELL TO ZERO. CONTINUED TO SECURE THE RIGHT ENGINE. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. DETERMINED THAT THE RIGHT GAS GENERATOR DRIVE HJul 19, 2001 · N137GA · Beech 1900C · Engine (Turbine/Turboprop)SDR GLBA2001149Cam · wornFLAPS WOULD NOT RETRACT ON T/O. REPLACED SAFETY SWITCH CAM.Jul 7, 2001 · N122GL · Beech 1900C · Trailing Edge Flap Control System
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