Beech 1900D

Service difficulty reports · 7,152

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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 = '1900D'
  ORDER BY difficulty_date DESC"

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SDR CA051130008Starter Gen · failedATTEMPTED TO START THE LEFT ENGINE BUT NO SUCCESS. MAINTENANCE WAS NOTIFIED AND AIRCRAFT BROUGHT BACK INTO HANGAR. SYSTEM INSPECTED AND FOUND THAT STARTER GENERATOR AT FAULT. REPLACED STARTER GENERATOR AND ENGINE RUN PERFORMED. SYSTEM CHECKED SATISFACTORY Nov 30, 2005 · Beech 1900D · Starter-GeneratorSDR S2YA05078Windshield · crackedDURING FLIGHT, THE RT WINDSHIELD DEVELOPED A CRACK FROM TOP TO BOTTOM. THE CREW LANDED SAFELY AND THE AC WAS FERRIED BACK. MX REPLACED TH RT WINDSHIELD AND RETURNED TO AC TO SERVICE. (K)Nov 25, 2005 · N841SK · Beech 1900D · Flight Compartment WindowsSDR CA051129002Spring · fracturedDURING TAXI, THE FLIGHT CREW NOTICED A FULL LEFT BIAS DEFLECTION IN THE AILERON SYSTEM. MAINTENANCE FOUND ONE OF THE AILERON INTERCONNECT SPRINGS HAD FRACTURED AT THE END RING THAT PROVIDES CONNECTION TO THE BRIDLE. IT IS FELT THAT THE ISSUE MAY HAVE BEEN INNov 14, 2005 · Beech 1900D · Aileron Control SystemSDR S2YA05075Altimeter · malfunctionedON CLIMB OUT OF FLIGHT, THE CREW REPORTED THE CAPTAIN`S ALTIMETER FLAGGED SHORTLY AFTER ROTATION AND STAYED FLAGGED. THE CREW PERFORMED AND AIR-TURN-BACK. UPON ARRIVAL BACK, THE ALTIMETER BEGAN TO WORK AGAIN. MX REPLACED THE AITIMETER AND RETURNED THE AC TONov 8, 2005 · N87SK · Beech 1900D · Altimeter, Barometric/EncoderSDR 11042005ACircuit Breaker · trippedGEAR WOULD NOT COME UP AFTER TAKEOFF. RESET LANDING GEAR CONTROL CIRCUIT BREAKER. CYCLED LANDING GEAR FOUR TIMES, OPS CHECK GOOD.Nov 4, 2005 · N60MJ · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 73843Brake · weakUPON LANDING, CAPT'S NOTED BOTH BRAKES WEAK WHEN APPLIED. CREW TAXIED TO THE GATE WITH NO FURTHER INCIDENT. PHONED MAINTENANCE CONTROL, OUTSIDE MAINTENANCE WAS CALLED AND BRAKES WERE BLED. OPS CHECK NORMAL. THEREFORE NO PARTS WERE USED.Nov 1, 2005 · N143YV · Beech 1900D · Landing Gear Brake SystemSDR S2YA05071Uplock Switch · inoperativeON CLIMB OUT OF FLIGHT, THE CREW REPORTED THE RED IN TRANSIT LIGHT STAYED ILLUMINATED AFTER THE GEAR WAS SELECTED UP AND APPARENTLY DID FULLY RETRACT. THE RELEASE WAS AMENDED AND THE AC CONTINUED WITHOUT STOPPING. MX REPLACED THE NOSE GEAR UPLOCK SWITCH AND Oct 31, 2005 · N85SK · Beech 1900D · Landing Gear Position and WarningSDR S2YA05072Pressure Switch · inoperativeON TAKEOFF OF FLIGHT, THE CREW REPORTED THE RT ENVIRONMENTAL BLEED AIR SYSTEM FAILED AND ABORTED THE TAKEOFF. THE SYSTEM WAS PUT ON MEL AND THE AC WAS RETURNED TO SERVICE. REPLACED A BAD PRESSURE SWITCH AND WITH NO FURTHER DISCREPANCIES RETURNED THE AC TO SEOct 31, 2005 · N87SK · Beech 1900D · Pneumatic Distribution SystemSDR 11022005ARelay · failedFLAPS STUCK AT 17 DEGREES. REMOVED AND REPLACED FLAP CONTROL RELAY OPS CHECK NORMAL, P/N SM50D7.Oct 28, 2005 · N152MJ · Beech 1900D · Trailing Edge Flap Control SystemSDR 11012005AAutofeather Sys · malfunctionedIN FLIGHT, LEFT ENGINE AUTOFEATHER LIGHTS LIGHTS EXTINGUISHED WITH POWER AT 3750 TORQUE. REMOVED AND REPLACED LT ENGINE AUTOFEATHER PRESSURE SWITCH PN 50-389121-21, SN ON 10015, SN OFF UNKNOWN.Oct 28, 2005 · N243CJ · Beech 1900D · Propeller Feathering/ReversingSDR S2YA05070Altimeter · stickingON CLIMB OUT OF FLIGHT, THE CREW REPORTED THE CAPTAIN`S ALTIMETER FROZE UP (STOPPED CLIMBING) WERE PERFORMEING AN AIR-TURN-BACK. UPON ARRIVAL BACK, THE ALTIMETER BEGAN TO WORK AGAIN. MX REPLACED THE ALTIMETER AND RETURNED THE AC TO SERVICE. (K)Oct 23, 2005 · N81SK · Beech 1900D · Altimeter, Barometric/EncoderSDR S2YA05069Bracket · inoperativeDURING FLIGHT, THE CREW REPORTED THE CARGO DOOR ANNUCIATOR ILLUMINATED AND WERE PERFORMING AN AIR-TURN-BACK. THE ANNUCIATOR WAS MEL`D AND THE AC WAS RETURNED TO SERVICE. MX REPLACED THE ACTUATOR BRACKET AND CLEARED THE MEL. (K)Oct 21, 2005 · N79SK · Beech 1900D · Door Warning SystemSDR 105092102690Stringer · crackedFOUND STRINGER 3R AT FS 163.9. CRACKED. MAINTENANCE REMOVED CORROSION AND TREATED FASTENERS WITH ALODINE. THEREFORE NO PARTS WERE USED.Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, Longeron/StringerSDR 105092102666Frame · crackedFOUND CRACKED INNERSKIN AND FRAME (ASD) STA 150.6. MAINTENANCE REPAIRED THE PROBLEM.Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, FrameSDR 1050921026131Splice Plate · crackedFOUND FS 434 CRACKED SPLICE PLATE SIDEWALL. MAINTENANCE REPAIRED THE SPLICE PLATE SIDEWALL.Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Miscellaneous StructureSDR 1050921026160Stringer · crackedFOUND STRINGER 3R AT FS 163.9 CRACKED. MAINTENANCE FABRICATED AND INSTALLED DOUBLER.Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, Longeron/StringerSDR 1050921026090Stringer · corrodedCORRSION FOUND ON FASTENERS FS 150-183 AND STRINGER 1-3R. MAINTENANCE REMOVED CORROSION AND TREATED FASTENERS WITH ALODINE.Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, Longeron/StringerSDR 1050921026120Angle · crackedFOUND LEFT FS 400 1 FT ABOVE FLOOR CRACKED. MAINTENANCE FABRICATED REPAIR ANGLE AND INSTALLED.Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Miscellaneous StructureSDR 1050921026072Frame · crackedFOUND FRAME ANGLE AT FS 456 CRACKED. MAINTENANCE INSPECTED AND NO CRACKS WERE NOTED. THEREFORE NO PARTS WERE USED.Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, FrameSDR 1050921026071Stringer · crackedSTRINGER 12 AT FS 456 RT CRACKED. MAINTENANCE REPAIRED STRINGER WHILE AIRCRAFT WAS IN STRUCTURAL REPAIR.Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, Longeron/StringerSDR 1050921026Frame · crackedCRACKED INNER SKIN AND FRAME. MAINTENANCE REPAIRED IAW SRM 51-70-00 AND 51-70-15. MORE INFORMATION WILL BE AVAILABLE AT A LATER TIME.Oct 20, 2005 · N146ZV · Beech 1900D · Fuselage Main, FrameSDR S2YA05067Pressure Switch · inoperativeDURING FLIGHT, THE CREW REPORTED THE RT AUX PUMP AUTO FUNCTION DID NOT STOP THE PUMP, RT NO AUX TRANSFER ILLUMINATED WHEN PUMP WAS IN AUTO FUNCTION. BETWEEN MX AND OPS, IT WAS DECIDED AN AIR-TURN-BACK WAS THE BEST OPTION. MX INSPECTED THE SYSTEM BUT COULD NOOct 19, 2005 · N881SK · Beech 1900D · Fuel Indicating SystemSDR 73619Bolt · unknownAFTER TAKEOFF, CREW UNABLE TO RETRACT LANDING GEAR. RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED BOLT IN RIGHT SQUAT SWITCH.Oct 19, 2005 · N127ZV · Beech 1900D · Main Landing GearSDR AMWA73619Landing Gear · malfunctionedAFTER TAKEOFF, CREW UNABLE TO RETRACT LANDING GEAR. RETURNED TO FIELD WITH NO FURTHER INCIDENT. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE.Oct 19, 2005 · N127ZV · Beech 1900D · Main Landing GearSDR 10212005AFire Detector · malfunctionedRT FIRE LOOP ANNUNCIATOR ILLUMINATED DURING RUNUP AND REMAINS ON. INSPECTED FIRE LOOPS, CANNON PLUGS AND A319 NO DEFECTS NOTED. REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT. OPS CHECK GOOD, PN 477-90005, SN 9036-005.Oct 17, 2005 · N124CJ · Beech 1900D · Fire DetectionSDR 10172005AFire Detector · malfunctionedRT FIRE LOOP STUCK IN TEST MODE. INSPECTED FIRE LOOP NO DEFECTS FOUND, INSPECTED CONTROLLER AND C/B, NO DEFECTS NOTED, DISCONNECTED LOOP AT FIREWALL, FIRE LOOP LIGHT REMAINED ON, RECONNECTED LOOP AT FIREWALL LIGHT REMAINED ON. FOUND FIRE DETECTION CONTROL BOOct 14, 2005 · N124CJ · Beech 1900D · Fire DetectionSDR S2YA05066CFlex Drive · damagedSHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WERE RAISED USING THE OVER RIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. DISCOVERED THE FLAP MOTOR/GEAR BOX STRUGGLING Oct 13, 2005 · N901SK · Beech 1900D · Trailing Edge Flap Control SystemSDR S2YA05066BFlex Drive · damagedSHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WHERE RAISED USING THE OVER RIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. DISCOVERED THE FLAP MOTOR/GEARBOX STRUGGLING Oct 13, 2005 · N901SK · Beech 1900D · Trailing Edge Flap Control SystemSDR S2YA05066AGearbox · damagedSHORTLY AFTER TAKEOFF THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WHERE RAISED USING THE OVER RIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. MX DISCOVERED THE FLAP MOTOR/GEAR BOX STRUGGLIOct 13, 2005 · N901SK · Beech 1900D · Trailing Edge Flap Control SystemSDR S2YA05066Motor · damagedSHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WERE RAISED USING THE OVERRIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. DISCOVERED THE FLAP MOTOR/GEAR BOX STRUGGLING TOct 13, 2005 · N901SK · Beech 1900D · Trailing Edge Flap Control SystemSDR GUU2005F00058O-Ring · wornNO BRAKES AFTER PRESSING THE RT BRAKE PEDAL. REPLACED NR 3 AND 4 BRAKE ASSEMBLIES. UPON BRAKE REMOVAL, DETERMINED NR 3 BRAKE SWIVEL FITTING O-RING TO BE LEAKING. (K)Oct 11, 2005 · N49543 · Beech 1900D · Landing Gear Brake SystemSDR S2YA05065BRelay · failedFLAPS FAILED TO EXTEND, SYS WAS MEL`D. MEL WAS CLEARED WHEN MX INS SYS, OPS CHECKED, COULD NOT DUPLICATE DISCREPANCY. TROUBLESHOOTING REPLACED FLAP MOTOR AND FLAP POSITION RELAY (K105). SHORTLY AFTER TAKEOFF CREW REPORTED FLAPS WERE AT 17 DEGREES AND WILL NOct 7, 2005 · N81SK · Beech 1900D · Trailing Edge Flap Control SystemSDR S2YA05065AGearbox · failedFLAPS FIALED TO EXTEND, SYS WAS MEL`D. MEL WAS CLEARED WHEN MX INSP SYS, OPS CHECKED, COULD NOT DUPLICATE DISCREPANCY. TROUBLESHOOTING REPLACED FLAP MOTOR, FLAP POSITION RELAY (K105). SHORTLY AFTER TAKEOFF CRWE REPORTED FLAPS WERE A T 17 DEGREES AND WOULD NOct 7, 2005 · N81SK · Beech 1900D · Trailing Edge Flap Control SystemSDR S2YA05065Motor · malfunctionedFLAPS FAILED TO EXTEND, SYS WAS MEL`D. MEL WAS CLEARED WHEN MX INSP SYS, OPS CHECKED IT, COULD NOT DUPLICATE DISCREPANCY. TROUBLESHOOTING REPLACED FLAP MOTOR AND FLAP POSITION RELAY (K105). SHORTLY AFTER TAKEOFF CREW REPORTED FLAPS WERE A 17 DEGREES AND WILOct 7, 2005 · N81SK · Beech 1900D · Trailing Edge Flap Control SystemSDR 1051101026Spring · brokenFLIGHT CREW REPORTED THAT WHILE ON THE GROUND WHEN THE CONTROL YOKE WAS LET LOOSE IT WOULD FLOP OVER TO THE RIGHT. MAINTENANCE PERSONNEL FOUND THE AFT AILERON/RUDDER INTERCONNECT SPRING HAD BROKEN NEAR THE HOOK END. MAINTENANCE INSTALLED NEW SPRING. INSPECTOct 1, 2005 · N127ZV · Beech 1900D · Rudder Control SystemSDR GUU2005F00050Wire · chafedRT ENGINE FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. REPAIRED CHAFED WIRE BENEATH FORWARD FLOORBOARD 131AT. (K)Sep 29, 2005 · N87555 · Beech 1900D · Fire Protection System WiringSDR S2YA05061Wire · damagedDURING APPROACH, THE CREW REPORTED THEY WERE UNABLE TO EXTEND THE GEAR AND FOUND THE CIRCUIT BREAKER (CB) POPPED. THE CREW RESET THE CB ONLY TO HAVE IT POP WHEN SELECTING GEAR DOWN. THE CREW MANUALLY EXTENDED THE GEAR, ACHIEVED 3 GREEN AND PROCEEDED TO LAND Sep 25, 2005 · N91SK · Beech 1900D · Landing Gear System WiringSDR 73127Terminal · crackedDURING A ROUTINE INSPECTION, INSPECTION PERSONNEL FOUND THE RT ENGINE BETA CABLE FRONT PUSH PULL TERMINAL CRACKED AROUND THE ENTIRE CIRCUMFERENCE. IT IS UNKNOWN HOW THIS CONDITION OCCURRED. PARTS HISTORY RESEARCH SHOWED NO RECENT USAGE. MORE INFORMATION WILL BSep 23, 2005 · N127ZV · Beech 1900D · Ice/Rain Protection System WiringSDR GUU2005F00051Bracket · corrodedAT SCHEDULED MAINTENANCE, RT ELEVATOR, CENTER HINGE BRACKET SHOWS SIGN OF EXFOLIATION. REPLACED RT ELEVATOR CENTER HINGE BRACKET. (K)Sep 23, 2005 · N16540 · Beech 1900D · Elevator Miscellaneous StructureSDR 09212005DFuel Control · failedON LEFT ENGINE START AT 44 PERCENT, ITT ROSE RAPIDLY AND ABORTED START AT 980 DEGREES CELSIUS (ENG AT 980 DEGREES FOR LESS THAN 5 SECS BEFORE SHUTDOWN). REMOVED AND REPLACED LEFT FUEL CONTROL. OPS CHECK GOOD.Sep 20, 2005 · N136MJ · Beech 1900D · Fuel Control/Turbine EnginesSDR R017794Bearing · brokenPROP WAS REMOVED FOR LOOSE BLADE. PROP WAS OVERHAULED BY MFG SERVICE CENTER ON 10/7/03 AND INSTALLED NEW D-7745 BEARINGS AT THAT TIME. HUB SIDE BEARINGS ON BLADES 2 AND 3 ARE CRACKED CIRCUMFERENTIALLY. HUB SIDE BEARING ON BLADE 4 IS BROKEN.Sep 20, 2005 · Beech 1900D · Propeller AssemblySDR 09212005CSwitch · failedDUAL ENVIROMENTAL FAIL. T/O ABORTED AT 50 KNOTS. PERFORMED OPS CHECK OF RIGHT TEST VALVE OPS CHECKED GOOD. CLEANED LEFT PNEUMATIC BLEED TEST SWITCH E305WDM, OPS CHECK GOOD.Sep 19, 2005 · N60MJ · Beech 1900D · Engine Bleed Air SystemSDR 09212005BHandle · out of rigLEFT EMERGENCY EXIT EXTERIOR HANDLE NOT FLUSHED. RIGGED DOOR HANDLE.Sep 19, 2005 · N221CJ · Beech 1900D · Emergency ExitsSDR 1050902038Intercostal · crackedINTERCOSTAL ABOVE CARGO DOOR CRACKED AT FS 468, 482 AND 495. MAINTENANCE WAS DOING A STRUCTURAL REPAIR.Sep 19, 2005 · N135YV · Beech 1900D · Fuselage Miscellaneous StructureSDR S2YA05058Gyro · inoperativeDURING FLIGHT, THE CREW REPORTED THE (D) DISCHARGE LIGHT ON THE RT PUSH TO DISCHARGE FIRE EXTINGUISHER BUTTON WAS INTERMITTENTLY ILLUMINATING. ALSO THE CREW REPORTED CAPTAIN`S DIRECTIONAL GYRO (DG) WAS INOP IN ALL MODES. THE CREW PERFORMED AN AIR-TURN-BACK. Sep 16, 2005 · N81SK · Beech 1900D · Directional Gyro and Indicating SystemSDR 09152005BSwitch · failedLT ENGINE FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY THEREAFTER. BOTTLE PRESSURE READS NORMAL. REMOVED AND REPLACED UPPER LT FIRE TEST SWITCH IAW 31-10-00, OPS CHECK GOOD.Sep 14, 2005 · N60MJ · Beech 1900D · Fire Bottle, FixedSDR GUU2005F00048Bracket · corrodedAT SCHEDULED MAINTENANCE, THE LEFT ELEVATOR, OUTBOARD HINGE BRACKET WAS DETERMINED TO HAVE EXFOLIATION CORROSION. REPLACED THE LEFT ELEVATOR OUTBOARD HINGE BRACKET. (M)Sep 12, 2005 · N81556 · Beech 1900D · Elevator, Tab StructureSDR 09132005AGround Wire · looseFLAP WILL NOT GO DOWN WHEN SELECTED 17 DEGREES. MEL'ED FLAP SYSTEM. C/W MEL ON 9/15/2005 FOUND LOOSE GROUND, RESECURED, OPS CHECK GOOD.Sep 12, 2005 · N60MJ · Beech 1900D · Flight Control System WiringSDR 09122005FCircuit Breaker · inoperativePROP OVERSPEED TEST INOP. LOW PITCH TEST INOP. AUTOFEATHER INOP. RESET CB9, OPS CHECK GOOD FOR PROP OVERSPEED, LOW PITCH, AND AUTOFEATHER TEST.Sep 11, 2005 · N171CJ · Beech 1900D · Propeller Feathering/ReversingSDR 09122005ESkin · bird strikeBIRD STRIKE ON LEFT INBOARD LEADING EDGE. REMOVED AND REPLACED LEADING EDGE, ONLY WAITING ON A BOOT.Sep 10, 2005 · N243CJ · Beech 1900D · Wing, Plate/Skin
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