Beech 1900D

Service difficulty reports · 7,152

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 = '1900D'
  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 V0DR200500001Bearing Race · brokenDURING DISASSEMBLY FOR OVERHAUL, FOUND NR 2 AND NR 3 BLADE BEARING RACES CRACKED AND BROKEN. HUB SIDE RACES (P/N) D-7745-A (S/NS) A059 & A075. BLADE SIDE RACES (P/N) D-7745-B (S/NS) A417 & A453.Aug 4, 2005 · N94GL · Beech 1900D · Propeller Blade SectionSDR 08042005CWire · brokenNO DOWNLOCK INDICATION WHEN GEAR DOWN. REPAIRED BROKEN WIRE.Aug 4, 2005 · N124CJ · Beech 1900D · Landing Gear System WiringSDR S2YA05047Boot · shortedDURING FLIGHT, THE CREW REPORTED A GLOW COMING FROM THE RT PROPELLER. AFTER CONSULTING WITH DISPATCH AND MAINTENANCE, THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE INSPECTED THE RT PROP AND FOUND THE DEICE BOOT HAD SHORTED AND BURNED. MAINTENANCE REPLACEAug 3, 2005 · N92SK · Beech 1900D · Propeller/Rotor Anti-Ice/De-Ice SystemSDR CA050803006Drive Shaft · sheared(CAN) ON CLIMBOUT, ELEC TRIM WAS OPERATED, IT WOULD ONLY MOVE 1.5 DEG FROM FULL NOSE UP, COULD NOT BE MOVED MANUALLY. AC RETURNED TO DEPARTURE AIRPORT. ELEV TRIM WAS STILL JAMMED ON GROUND ELECTRICALLY AND MANUALLY. INSP OF ACTUATOR MOTOR, IN TAIL SECTION, Aug 2, 2005 · Beech 1900D · Elevator Tab Control SystemSDR 08022005BElevator · stuckAT ROTATION SPEED (100 KIAS) CONTROL COLUMN WAS TEMPORARILY STUCK UNTIL EXTREME BACK PRESSURE WAS APPLIED. CONTROL COLUMN THEN MOVED RAPIDLY AFT AND A/C JUMPED OFF RUNWAY. IN FLIGHT A/C ELEVATOR TRIM VERY SLOWLY MOVED TO NOSE UP, REQUIRING APPROX 1/2 UNIT CHAug 2, 2005 · N136MJ · Beech 1900D · Elevator Control SystemSDR 72066Indication Sys · malfunctionedON TAKEOFF ROLL OUT, CREW OBSERVED RIGHT ENGINE TORQUE NOT ABOVE 500LBS. RETURN TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED INDICATOR AND TRANSMITTER.Aug 1, 2005 · N155YV · Beech 1900D · Engine BMEP/Torque IndicatingSDR AMWA72057Connector · dirtyON TAKEOFF ROLL OUT, CREW OBSERVED RIGHT ENGINE UNABLE TO ACHIEVE TAKEOFF POWER. RETURNED TO GATE WITH NO FURTHER INCIDENT. THE CORRECTIVE ACTION WAS AS FOLLOWED: MAINTENANCE CLEANED AND SECURED CONNECTOR AT TORQUE INDICATOR. THEREFORE NO PARTS WERE USED.Aug 1, 2005 · N155YV · Beech 1900D · Engine BMEP/Torque IndicatingSDR CA050802002Wire · broken(CAN) AFTER TAKEOFF ,THE GEAR WAS RETRACTED AND THE RED INTRANSIT LIGHT DID NOT EXTINGUISH. THE GEAR WAS EXTENDED AND OPERATED NORMALLY. THE FLIGHT CONTINUED, THE CREW DID A FLYBY OF TOWER TO CONFIRM GEAR POSITION WHEN UP. THE TOWER THOUGHT THE NOSE WAS LOWEJul 31, 2005 · Beech 1900D · Landing Gear System WiringSDR GUU2005F00040Bracket · corrodedAT SCHEDULED INSPECTION, RT ELEVATOR CENTER HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RT ELEVATOR CENTER HINGE BRACKET. (K)Jul 30, 2005 · N81538 · Beech 1900D · Elevator Miscellaneous StructureSDR 2005FA0001140Mount · faultyTRANSISTOR MOUNT, INSTRUMENT PANEL INDIRECT LISHTS OPERATE AT FULL BRIGHT REGARDLESS OF POTENTIATOR POSITION. TROUBLESHOOTING FOUND THAT TRANSISTOR MOUNT WAS INSTALLED BEHIND LOCATION CALLED OUT AS COPILOTS FLIGHT INSTRUMENTS. IDENTIFYING FAULTY TRANSISTOR CJul 29, 2005 · N842E · Beech 1900D · Flight Compartment LightingSDR GUU2005F00039Brake · inadequateDURING TAXI, RT BRAKE INEFFICIENT. BLED RT BRAKES. (K)Jul 25, 2005 · N87557 · Beech 1900D · Landing Gear Brake SystemSDR 71931Roller · obstructedAFTER LANDING IN DUBOIS, PA ON REPOSITIONING FLIGHT 9415, THE PASSENGER DOOR FAILED TO OPEN DUE TO THE DOOR TRIM STUCK IN CAM ROLLER ON DOOR FRAME. THE CORRECTIVE ACTION WAS AS FOLLOWED: MAINTENANCE REINSTALLED THE TRIM. THEREFORE NO PARTS WERE USED.Jul 25, 2005 · N162ZV · Beech 1900D · Passenger/Crew DoorsSDR 71936Oil Filter · fouledAFTER DEPARTURE FROM PITTSBURGH, PA RIGHT ENGINE OIL PRESSURE WENT TO RED LINE, 30 MILES OUT OF DUBOIS, PA. MAINTENANCE REQUESTED THE AIRCRAFT TO LAND IN DUBOIS, PA FOR FURTHER INSPECTION. THE CORRECTIVE ACTION WAS AS FOLLOWED: MAINTENANCE INSTALLED A NEW OIL Jul 25, 2005 · N155YV · Beech 1900D · Turbine Engine Oil SystemSDR 07242005AShutoff Valve · stuckRIGHT ENGINE STANDBY BOOST PUMP INOP. FOUND FIREWALL VALVE STUCK IN CLOSED POSITIONJul 24, 2005 · N220CJ · Beech 1900D · Fuel StorageSDR S2Y2005F00000Pcb · shortedDURING APPROACH, THE CREW DID NOT RECEIVE THE DOWN AND LOCK INDICATION FOR THE NOSE LANDING GEAR. THE CREW ALSO NOTED A SMOKE ODOR IN THE COCKPIT. THE CREW MADE A SAFE LANDING. MAINTENANCE INSPECTED THE SYSTEM AND FOUND BOTH THE ANNUNCIATOR FAULT DETECT PCBJul 22, 2005 · N891SK · Beech 1900D · Landing Gear Position and WarningSDR S2YA05046Pcb · shortedDURING APPROACH OF FLIGHT, THE CREW DID NOT RECEIVE THE DOWN AND LOCK INDICATION FOR THE NOSE LANDING GEAR. THE CREW ALSO NOTED A SMOKE ODOR IN THE COCKPIT. THE CREW MADE A SAFE LANDING. MAINTENANCE INSPECTED THE SYSTEM AND FOUND BOTH THE ANNUNCIATOR FAULT Jul 22, 2005 · N891SK · Beech 1900D · Landing Gear Position and WarningSDR 07212005Steering Sys · malfunctionedDURING TAXI, AIRCRAFT MAINTAINS STRAIGHT LINE WHEN EITHER RUDDER PEDAL IS DEFLECTED FULL TRAVEL.Jul 21, 2005 · N155CJ · Beech 1900D · Landing Gear Steering SystemSDR S2YA05044Pressure System · fluctuatesSHORTLY AFTER TAKEOFF, THE CREW REPORTED THE OIL PRESSURE DROPPED TO ABOUT 40 PSI ACCOMPANIED BY A TEMPERATURE INCREASE TO 800 DEGREES AND TORQUE FLUCTUATIONS. THE CREW PERFORMED AN AIR-TURN-BACK. MAINTENANCE INSPECTED THE AC AND REPLACED THE RT ENGINE. WITHJul 20, 2005 · N891SK · Beech 1900D · Engine Oil PressureSDR CA050725020Bleed Valve · failedDURING A RAPID DESCENT, THE ENGINE SURGED ACCOMPANIED BY TORQUE FLUCTUATIONS. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT PROCEEDED TO DESTINATION. SUBSEQUENT INVESTIGATION WAS UNABLE TO REPRODUCE THE PROBLEM. THE ENGINE BLEED VALVE WAS REPLACED ANDJul 18, 2005 · Beech 1900D · Compressor Bleed ValveSDR 20030865Switch · defectiveON APPROACH RT ENGINE POWER WAS REDUCED AND FLT CREW REPORTED THE ENGINE AUTOFEATHERED. AIRCRAFT LANDED SAFELY. MAINTENANCE TROUBLESHOT TO RT LOW PRESSURE SWITCH, REPLACED OP/CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.Jul 18, 2005 · N254GL · Beech 1900D · Propeller Controlling SystemSDR 71813Brake Assy · malfunctionedUPON TAXI INTO DUJ, CREW EXPERIENCED RIGHT BRAKE SPONGY. PARKED AND CHOCKED AIRCRAFT WITH NO FURTHER INCIDENT. MAINTENANCE BLED BRAKES. THEREFORE THERE WERE NO PARTS USED.Jul 17, 2005 · N163YV · Beech 1900D · Landing Gear Brake SystemSDR 07152005AWarning Light · illuminatedCARGO DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF.Jul 15, 2005 · N221CJ · Beech 1900D · Door Warning SystemSDR S2YA05042Circuit Breaker · intermittentDURING APPROACH OF FLIGHT, THE CREW REPORTED THE GEAR WAS NOT EXTENDING NORMALLY BUT IS THEY JIGGLED THE HANDLE IT WOULD OPERATE. THE CREW PUMPED THE GEAR DOWN AND ACHIEVED THREE GREEN. MAINTENANCE FOUND INTERMITTENT HIGH OHMS READING THROUGH LANDING GEAR CIJul 14, 2005 · N881SK · Beech 1900D · Landing Gear System WiringSDR 71722Switch · out of rigAFTER TAKEOFF, CREW WAS NOT ABLE TO RETRACT FLAPS TO ZERO. RETURNED TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENT. THE CORRECTIVE ACTION WAS THE FLAP LIMIT CAM SWITCH S-4 WAS RIGGED. THEREFORE NO PARTS WERE USED.Jul 11, 2005 · N155YV · Beech 1900D · Trailing Edge Flap Control SystemSDR 71222Flap System · malfunctionedAFTER TAKEOFF, CREW NOT ABLE TO RETRACT FLAPS TO ZERO. RETURNED TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENT. STILL AWAITING MORE INFORMATION.Jul 11, 2005 · N155YV · Beech 1900D · Trailing Edge Flap Control SystemSDR CA050711001Diode · shortedAIRCRAFT STILL POWERED UP AFTER BATTERY IS SELECTED OFF. BATTERY BUSS TIE CONTROL T/S. FOUND THAT BATTERY RELAY WELDED CLOSED. REPLACED BATTERY RELAY. BATTERY BUSS TIE RELAY INSPECTED AND FOUND CONTACTS BADLY PITTED. REPLACED BATTERY BUSS TIE RELAY. OPS Jul 8, 2005 · Beech 1900D · DC Power Distribution SystemSDR CA050725010Engine · failed(CAN) ON TAKEOFF, THE ENGINE EMITTED A LOUD BANG AND LOST POWER. THE TAKEOFF WAS ABORTED. SUBSEQUENT INSPECTION REVEALED TURBINE DISTRESS. PWC WILL MONITOR INVESTIGATION OF THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED.Jul 5, 2005 · Beech 1900D · Turbine SectionSDR GUU2005F00031Engine · failedLOUD BANG FROM NR 2 ENGINE UPON INITIAL POWER ADVANCEMENT, ABORTED TAKEOFF. NR 2 ENGINE FIRE T-HANDLE, BLEW BOTTLE. EVACUATED PASSENGERS. DETERMINED RT POWER SECTION TO BE SEIZED. EVIDENCE OF DEBRIS DAMAGE TO INSIDE OF EXHAUST STACKS. INVESTIGATION IN PROJul 5, 2005 · N81556 · Beech 1900D · Engine (Turbine/Turboprop)SDR 71599Warning Light · illuminatedUPON FINAL, CREW EXTENDED MAIN LANDING GEAR AND OBSERVED RIGHT MAIN LANDING GEAR GREEN. DOWN AND LOCKED INDICATOR WILL NOT ILLUMINATE. CREW ACCOMPLISHED TOWER FLY-BY FOR DOWN AND LOCK VERIFICATION AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED ANDJul 5, 2005 · N159YV · Beech 1900D · Main Landing GearSDR 07042005Governor · malfunctionedLT ENGINE SURGING. REMOVED AND REPLACED PROPELLER GOVERNOR.Jul 4, 2005 · N243CJ · Beech 1900D · Propeller GovernorSDR 20030858Pressure Switch · malfunctionedON APPROACH, CREW REPORTED RT ENGINE AUTOFEATHERED. MAINTENANCE CHECKED AND CLEANED PRESSURE SWITCHES AND PERFORMED OPERATIONAL CHECK OF AUTOFEATHER SYSTEM WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.Jul 2, 2005 · N254GL · Beech 1900D · Propeller Controlling SystemSDR 71535Release Mech · failedAIRCRAFT PASSENGER DOOR WILL NOT RELEASE THE RELEASE LOCK. FOUND BEFORE CHECK FLIGHT. MAINTENANCE REMOVED AND REPLACED THE RELEASE MECHANISM BUTTON ASSY. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE.Jun 30, 2005 · N10675 · Beech 1900D · Passenger/Crew DoorsSDR CA050715003Actuator · malfunctionedAIRCRAFT WAS ON APPROACH ,WHEN SELECTED GEAR DOWN DID NOT GET NOSE GEAR INDICATION ALTHOUGH THE HANDLE WAS NO LONGER RED. DUE TO THE NO AVAILABILITY OF MAINTENANCE ELECTED TO RETURN TO BASE. THE LIGHT OPERATED NORMALLY BUT THEY STILL ELECTED TO HAVE EMERGENCJun 27, 2005 · Beech 1900D · Landing Gear ActuatorSDR 06272005BActuator · lack of lubeAILERON STIFF TO OPERATE. LUBED AILERON TRIM ACTUATOR.Jun 27, 2005 · N172MJ · Beech 1900D · Aileron Tab Control SystemSDR 20030856Fire Loop · defectiveDURING FLIGHT, FLIGHT CREW NOTICED RT ENGINE T-HANDLE ANNUNCIATOR AND YELLOW (LOOP) ANNUCIATOR FLICKERING ON AND OFF AND WAS DETERMINED BY CREW THAT IT WAS A FALSE INDICATION. MAINTENANCE TROUBLESHOT PROBLEM TO DEFECTIVE RT AFT FIRE LOOP IN ENGINE COMPARTMENT.Jun 25, 2005 · N211GL · Beech 1900D · Fire DetectionSDR 06272005Eadi · failedBURNING ODOR PRESENT AND NR 1 EADI FLASHING ON AND OFF.Jun 24, 2005 · N60MJ · Beech 1900D · Integrated Flight SystemSDR 71405Control System · malfunctionedAFTER TAKEOFF, CREW OBSERVED FLAPS WILL NOT RETRACT TO ZERO. AIRCRAFT RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE CHECKED RIGGING AND CLEAND FLAP SPLIT FLAP SAFETY SWITCHES. THEREFORE NO PARTS WERE USED.Jun 21, 2005 · N138YV · Beech 1900D · Trailing Edge Flap Control SystemSDR CA050621015Engine · shutdown(CAN) DURING CRUISE, ENGINE OIL PRESSURE WAS OBSERVED TO FLUCTUATE AND SUBSEQUENTLY DECREASE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED INTERNAL OIL LEAKAGE. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE, ONCE ESTABLISHEJun 19, 2005 · Beech 1900D · Engine (Turbine/Turboprop)SDR CA050621018Windshield · crackedCRACKED WINDSHIELD.Jun 18, 2005 · Beech 1900D · Flight Compartment WindowsSDR S2YA05038Pressure Switch · malfunctionedON CLIMB OUT, THE CREW REPORTED TO MAINTENANCE THE LT AUTO IGNITION REMAINS ILLUMINATED IN FLIGHT. MAINTENANCE REQUEST THE AC RETURN TO DEPARTURE. THE CREW PERFORMED AN AIR-TURN-BACK TO DEPARTURE. MAINTENANCE REPLACED THE LT HIGH PRESSURE SWITCH AND RETURNEJun 17, 2005 · N841SK · Beech 1900D · Ignition SystemSDR 06172005BTrim System · lack of lubeAILERON TRIM NOT MOVING. INSPECTED AND LUBED TRIM KNOB.Jun 17, 2005 · N172MJ · Beech 1900D · Aileron Control SystemSDR 71342Brake · malfunctionedAFTER LANDING IN DUJ AND TAXIING TO GATE WITH NO INCIDENT, CREW CALLED MAINTENANCE TO WRITE UP THE RIGHT BRAKE AS WEAK. MAINTENANCE BLED BRAKE. THEREFORE NO PARTS WERE USED.Jun 17, 2005 · N143YV · Beech 1900D · BrakeSDR 71331Warning Light · false activationTAXIED INTO GATE WHEN MASTER WARNING FLASHER ILLUMINATED INDICATING FIRE IN RT ENG. FIREWALL FUEL VALVE WAS ILLUMINATED. DECLARED AN EMERGENCY, ACCOMPLISHED APPROPRIATE CHECKLISTS & CONDUCTED AN ORDERLY DEBARKATION WHILE DIRECTING PASSENGERS AWAY FROM PLANE.Jun 16, 2005 · N167YV · Beech 1900D · Indicating/Recording SystemSDR 71323Brake Assy · malfunctionedON LANDING IN LWB LEFT BRAKE WAS WEAK. MAINTENANCE BLED THE BRAKES. THEREFORE NO PARTS WERE USED.Jun 16, 2005 · N161YV · Beech 1900D · BrakeSDR 06092005AGovernor · malfunctionedNOTICED RIGHT YAW WHEN POWER REDUCED DURING LANDING FLARE. REMOVED AND REPLACED PROP GOVERNOR.Jun 9, 2005 · N124CJ · Beech 1900D · Propeller GovernorSDR CA050823003Skin Panel · corroded(CAN) SEVER CORROSION FOUND BETWEEN BONDED MEMBERS OF THE SKIN PANEL ASSY STRETCHING THRU THE ENTIRE LENGTH OF THE PANEL.Jun 8, 2005 · Beech 1900D · Nacelle/Pylon, Plate/SkinSDR 06072005BActuator · malfunctionedLANDING GEAR EXCESSIVELY SLOW TO EXTEND. CHANGED RT MLG ACTUATOR.Jun 7, 2005 · N155CJ · Beech 1900D · Landing Gear ActuatorSDR 2005FA0000920Drive Assy · shearedRT IB FLAP ACTUATOR WOULD NOT ACTUATE. UPON TEARDOWN INSPECTION DISCOVERED THE 90 DEGREE DRIVE ASSEMBLY, FLAP CABLE CONNECTOR COUPLING HAD SHEARED THE ROLL PIN THAT CONNECTS THE COUPLING TO A DRIVE GEAR. THIS 90 DEGREE DRIVE ASSEMBLY HAS NO FIELD MAINTENANCEJun 7, 2005 · N81SK · Beech 1900D · Trailing Edge Flap ActuatorSDR GUU2005F00023Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET. (K)Jun 5, 2005 · N87550 · Beech 1900D · Horizontal Stabilizer StructureSDR GUU2005F00022Packing · leakingLT BRAKE INOPERATIVE. PEDAL GOES TO FLOOR. REPLACED LT BRAKE INTERCONNECT PACKINGS. BLED BRAKE SYS. (K)Jun 5, 2005 · N82539 · Beech 1900D · Landing Gear Brake System
Back to Beech 1900D