Raytheon 1900D

Service difficulty reports · 7,152

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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 MASA99029Pin · damagedFLT 5299 - IAD-SYR - PRIOR TO DEPARTURE, CREW REPORTED THAT THE EXTERIOR DOOR HANDLE SPINS FREELY. MAINTENANCE INSPECTED THE DOOR HANDLE AND COULD NOT DUPLICATE THE DISCREPANCY, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. THAT EVENING DURING ROUTINEFeb 18, 1999 · N133YV · Beech 1900D · Passenger/Crew DoorsSDR CA990303018Motor · seized(CAN) ON FINAL, FLAPS 17 DEGREES SELECTED, THEY TRAVELLED TO 17 DEGREES. ON SELECTION TO FULL, THEY DID NOT MOVE. ON GROUND,THEY STILL DID NOT MOVE. FLAP MOTOR REPLACED. THIS IS FOURTH MOTOR REPLACEMENT. SUBMITTER SUGGESTS THAT THIS IS AN UNACCEPTABLE FAIFeb 18, 1999 · Beech 1900D · Trailing Edge Flap ActuatorSDR 99ZZZM216Gearbox · strippedFLAPS FAILED TO RETRACT, FLAP MOTOR GEAR BOX FAILURE. REPLACED FLAP MOTOR/GEAR BOX ASSEMBLY IAW RAYTHEON MM CHAPTER 27. (M)Feb 18, 1999 · N842CA · Beech 1900D · Trailing Edge Flap Control SystemSDR C2XA99CL017Switch · out of adjustCLE - FLT 4399 - CREW REPORTED THAT THE AUTO-FEATHER DISABLED AT 700 FEET WITH ENGINES AT FULL POWER AND IT FAILED TO RE-ARM. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE AUTOFEATHER POWER SWITCHES IAW B1900 MM 61-21-02, Feb 14, 1999 · N38537 · Beech 1900D · Propeller Feathering/ReversingSDR MASA99022Dpu · malfunctionedFLT 5347 - BOS-HYA - AFTER DEPARTURE FROM BOS, THE CREW REPORTED THE MASTER WARNING FLASHED ON THE CONSOLE. THNE THE F/O'S EFIS SCREENS STARTED TO BLANK OUT INTERMITTENTLY. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO BOS WITHOUT FURTHER INCIDFeb 10, 1999 · N4ZV · Beech 1900D · Integrated Flight SystemSDR AU990140Line · loose(AUS) HIGH PRESSURE FUEL PUMP TO FUEL TANK UNLOADING LINE LOCATED IN THE LT ENGINE NACELLE LOOSE AND LEAKING FUEL.Feb 9, 1999 · Beech 1900D · Engine Fuel DistributionSDR CA990311056Indicator · failed(CAN) CREW REPORTED FLICKERING ON DIGITAL DISPLAY. UNIT THEN FLAGGED FAILED. REMOVED AND REPLACED WITH YET ANOTHER REPLACEMENT. MANUFACTURER OF ALTIMETER, MEGGITT AVIONICS.Feb 8, 1999 · Beech 1900D · Altimeter, Barometric/EncoderSDR CA990311044Indicator · failed(CAN) FLIGHT CREW REPORTED THE DIGITAL DISPLAY OF RIGHT ALTIMETER WENT BLANK DISPLAYING THE FAILED FLAG. MAINTENANCE REPLACED THE UNIT WITH ANOTHER UNIT. THIS IS THE ELEVENTH UNIT REPLACED IN LESS THAN 6 MONTHS. MANUFACTURED BY MEGGITT ELECTRONICS.Feb 8, 1999 · Beech 1900D · Altimeter, Barometric/EncoderSDR CA990223021Check Valve · missing(CAN) BLEED AIR LINE REMOVED TO ALLOW REPLACEMENT OF AIR FILTER. IT WAS THEN NOTED THAT THE CHECK VALVE WAS NOT INTACT. THE EXHAUST COOLING DUCT WAS REMOVED TO FIND THE REMAINING PARTS OF VALVE.Feb 8, 1999 · Beech 1900D · Pneumatic Distribution SystemSDR CA990210015Window · damaged(CAN) 7 OF 14 CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED AS LONG AS WINDOWS ARE REVERSED 180 DEGREES AND UNTIL REPLACEMENT AND ARE OK FOR OUT OF CONTOUR TEST.Feb 3, 1999 · Beech 1900D · Passenger Compartment WindowsSDR CA990210014Window · damaged(CAN) BOTH FRONT CABIN WINDOWS REPLACED AS THEY WERE FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. PRESSUIRZED FLIGHT ALLOWED IF WINDOWS ARE REVERSED 180 DEGREES AND UNTIL REPLACEMENT AND THEY ARE PASSED FOR OUT OF CONTOUR TEST.Feb 3, 1999 · Beech 1900D · Passenger Compartment WindowsSDR CA990210013Window · damaged(CAN) 10 OF 14 CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED AS LONG AS WINDOWS ARE REVERSED 180 DEGREES AND PASS TEST. THIS ALLOWED UNTIL REPLACEMENT AVAILABLE.Feb 3, 1999 · Beech 1900D · Passenger Compartment WindowsSDR CA990210012Window · damaged(CAN) BOTH FRONT CABIN WINDOWS WERE FOUND OUT OF LIMITS FOR THE 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED IF WINDOWS ARE REVERSED 180 DEGREES, UNTIL THEY ARE REPLACED AND PASS OUT OF CONTOUR TEST.Feb 3, 1999 · Beech 1900D · Passenger Compartment WindowsSDR CA990210011Window · damaged(CAN) 11 OF 14 CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED IF WINDOWS ARE REVERSED 180 DEGREES, UNTIL THEY ARE REPLACED AND PASS OUT OF CONTOUR TEST.Feb 3, 1999 · Beech 1900D · Passenger Compartment WindowsSDR CA990210010Window · damaged(CAN) BOTH FRONT CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED IF WINDOWS ARE REVERSED 180 DEGREES, UNTIL THEY ARE REPLACED AND PASS OUT OF CONTOUR TEST.Feb 3, 1999 · Beech 1900D · Passenger Compartment WindowsSDR CA990210009Window · damaged(CAN) 11 OF 14 CABIN WINDOWS FOUND OUT OF LIMITS FOR THE 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED AS LONG AS WINDOWS ARE REVERSED, UNTIL THEY ARE REPLACED AND PASS OUT OF CONTOUR TEST.Feb 3, 1999 · Beech 1900D · Passenger Compartment WindowsSDR CA990210008Window · damaged(CAN) BOTH FRONT CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. OPERATION APPROVED PRESSURIZED FLIGHT AS LONG AS THE WINDOWS WERE REVERSED. THIS ALLOWED UNTIL WINDOWS ARE REPLACED AND AS LONG AS THEY PASS OUT OF CONTOUR TEST.Feb 3, 1999 · Beech 1900D · Passenger Compartment WindowsSDR CA990210007Window · damaged(CAN) ALL CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. PRESSURIZED FLIGHT ALLOWED BY RAYTHEON IF WINDOWS WERE REVERSED 180 DEGREES AND UNTIL REPLACEMENT AND THEY PASS OUT OF CONTOUR TEST.Feb 3, 1999 · Beech 1900D · Passenger Compartment WindowsSDR CA990210006Window · damaged(CAN) BOTH FRONT CABIN WINDOWS FOUND OUT OF LIMITS FOR 'OUT OF CONTOUR' TEST. FLIGHT INITIALLY RESTRICTED TO UNPRESSURIZED UNTIL WINDOW REPLACEMENT AND LATER ALLOWED PRESSURIZED FLIGHT IF WINDOWS WERE REVERSED 180 DEGREES AND PASSED 'OUT OF CONTOUR' TEST.Feb 3, 1999 · Beech 1900D · Passenger Compartment WindowsSDR CA990209023Arm Rest · shorted(CAN) WHEN COPILOT SEAT IN FULL FORWARD POSITION, THE RIGHT HAND ARM REST BLOCKS THE CIRCUIT BREAKERS FROM TRIPPING. ARM RESTS REMOVED AS A TEMPORARY MEASURE. PROBLEM COMMON TO ALL OF SUBMITTER'S FLEET.Feb 3, 1999 · Beech 1900D · Flight Compartment EquipmentSDR C2XA99IA126Switch · inoperativeIAH - FLT 3462 - THE CREW REPORTED THAT AFTER THE GEAR WAS RETRACTED THE RED INTRANSIT LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK SWITCH IAW B1900Feb 3, 1999 · N81536 · Beech 1900D · Landing Gear Position and WarningSDR 99ZZZM170Actuator · defectiveRIGHT MAIN LANDING GEAR ACTUATOR INDICATOR SLOW TO ILLUMINATE DOWN AND LOCKED. TROUBLESHOOTING FOUND DEFECTIVE DOWN AND LOCKED SWITCH INSIDE ACTUATOR. REPLACED RIGHT MAIN LANDING GEAR ACTUATOR. (M)Feb 3, 1999 · N857CA · Beech 1900D · Landing Gear ActuatorSDR MASA99018Relay · failedFLT 5999 - MBS-PIT - ON APPROACH TO PIT, THE GEAR WOULD NOT EXTEND. THE LANDING GEAR CIRCUIT BREAKER POPPED AND THE CREW RESET THE GEAR AND THE CIRCUIT BREAKER POPPED AGAIN. CREW MANUALLY EXTENDED THE GEAR AND RECEIVED A NORMAL INDICATION. EMERGENCY EQUIPMEFeb 2, 1999 · N65YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR CA990209022Windshield · delaminated(CAN) WINDSHIELD FOUND DELAMINATED. CAUSED BY WATER INFILTRATION. ALSO, SOME CORROSION.Feb 1, 1999 · Beech 1900D · Flight Compartment WindowsSDR 99ZZZX743Altimeter · stuckCAPTAIN'S ALTIMETER STUCK AT 16,000 FEET. UNIT STARTED OPERATING SHORTLY AFTERWARD. REPLACED ALTIMETER.Jan 31, 1999 · N846CA · Beech 1900D · Altimeter, Barometric/EncoderSDR CA990303004Case · corroded(CAN) ON INSPECTION, SEVERE CORROSION WAS FOUND AT THE 6 O'CLOCK POSITION ON THE GAS GENERATOR CASE. THE CORROSION WAS SO SEVERE THAT IT RESULTED IN PIN HOLES IN THE GAS GENERATOR CASE.Jan 29, 1999 · Beech 1900D · Turbine Engine Combustion SectionSDR CA990209021Switch · shorted(CAN) DURING INSPECTION, AURAL LANDING GEAR WARNING COULD NOT BE CANCELLED. BAD INSULATION BETWEEN PIN NR 8 AND GROUND (SWITCH CASE).Jan 29, 1999 · Beech 1900D · Landing Gear Position and WarningSDR 99ZZZX921Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FOUR EACH CRACKS.Jan 29, 1999 · Beech 1900D · Propeller Blade SectionSDR CA990311042Light · failed(CAN) CREW REPORTED DURING LANDING PHASE, THE GEAR HANDLE LIGHTS WOULD NOT EXTINGUISH. NO ACTION WOULD CLEAR THESE LIGHTS. MAINTENANCE FOUND A FLAP SENSE WIRE AT W.S. 45.00, RT WING, HAD CHAFED THROUGH, SHORTING OUT WIRE NR W50A22. WIRE WAS REPAIRED. SUBMJan 21, 1999 · Beech 1900D · Landing Gear SelectorSDR C2XA99CL009Valve · failedCLE - FLT 3161 - CREW REPORTED THAT THE RIGHT HAND BLEED AIR FAIL LIGHT ILLUMINATED IN-FLIGHT. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND BLEED AIR SHUT OFF VALVE IAW B1900 MM 36-00-02, OPERATIONAL ANJan 21, 1999 · N81546 · Beech 1900D · Pneumatic Distribution SystemSDR MASA99012Tube · crackedFLT 5409 - BOS-BGR - AFTER TAKEOFF, CAPTAIN NOTED THE NR 1 ENGINE OIL PSI WAS DECREASING. THE CAPTAIN SHUT DOWN THE NR 1 ENGINE AS A PRECAUTIONARY MEASURE. CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANJan 20, 1999 · N127ZV · Beech 1900D · Turbine Engine Oil SystemSDR 99ZZZX874Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. TWO CRACKS.Jan 20, 1999 · Beech 1900D · Propeller Blade SectionSDR 99ZZZM188Washer · failedUNABLE TO STEER AIRCRAFT FROM RUNWAY AFTER LANDING. INSPECTION OF AIRCRAFT FOUND RIGHT MAIN LANDING GEAR TORQUE KNEE SEPARATED DUE TO WASHER FAILURE, CAUSING CENTER TORQUE KNEE BOLT TO PULL THROUGH TORQUE KNEE. RIGHT MAIN LANDING GEAR, WHEEL ASSEMBLIES, AND Jan 19, 1999 · N852CA · Beech 1900D · Steering UnitSDR AMWA002467Switch · malfunctionedON APPROACH TO DSM FROM MCI, THE RT PROP WAS CYCLING IN/OUT OF FEATHER. DSM MAINTENANCE REPLACED THE RT LOW PRESSUER SWITCH. OPS CHECK NORMAL. THE FOLLOWING DAY, THE PROBLEM REOCCURED IN MCI WHERE THE PEDESTAL SWITCHES WERE ADJUSTED. OPS CHECK NORMAL. NO Jan 18, 1999 · N64YV · Beech 1900D · Propeller Controlling SystemSDR CA990311036Circuit Breaker · failed(CAN) CIRCUIT BREAKER FOR ANTI-ICE ACTUATOR WOULD OPEN DURING FLIGHT. CIRCUIT BREAKER WAS REPLACED WITH NEW.Jan 13, 1999 · Beech 1900D · Air Intake Anti/De-Ice SystemSDR MASA99009Engine · fodFLT 5872 - PIT-PKB - DURING TAKEOFF ROLL, ATC NOTIFIED THE CREW THAT THEY OBSERVED SPARKS FROM THE NR 2 ENGINE EXHAUST. ATC CALLED FOR EMERGENCY VEHICLES TO STANDBY. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. CREW REPORTED NO GAUGE FLUCTUATIONJan 12, 1999 · N190YV · Beech 1900D · Engine (Turbine/Turboprop)SDR MASA99075Spar · crackedDURING NIGHT MAINTENANCE, FOUND THE HORIZONTAL STABILIZER MAIN SPAR CENTER WEB CRACKED. MAINTENANCE REPAIRED THE CRACKED WEBBING IAW RO NR B1900D-55-0001. (M)Jan 10, 1999 · N6YV · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR C2XA99CL003Harness · failedCLE - FLT 3069 - CREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR SWITCH HARNESS ASSEMBLE IAW B1900D MM 32-60-02, ADJUSTJan 9, 1999 · N81538 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR C2XA99CL002Actuator · inoperativeCLE - FLT 3099 - CREW REPORTED THAT AFTER LANDING, WHILE TAXIING TO THE GATE THE NOSE WHEEL STEERING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NOSE WHEEL STEERING DISCONNECT ACTUATOR IAW B1900 MM 32-50-01, OPERATIONAL CHECKS WERE SATISFACTORY. AIJan 8, 1999 · N81546 · Beech 1900D · Landing Gear Steering SystemSDR CA990125002Retainer · cracked(CAN) SPRING RETAINER FOUND CRACKED DURING ROUTINE OVERHAUL.Jan 6, 1999 · Beech 1900D · Propeller Hub SectionSDR CA990125003Set Screw · worn(CAN) PROPELLER BLADE (S/N 2879J) HAD END PLAY OF 1. SET SCREW FOUND TO BE WORN 0.030 INCH BELOW MINIMUM LENGTH.Jan 5, 1999 · Beech 1900D · Propeller Blade SectionSDR MASA99003Air Dist · smokeFLT 5328 - BOS-MVY - DURING CRUISE AT 5000 FT, THE CREW VISUALLY DETECTED SMOKE IN THE COCKPIT ACCOMPANIED BY A BURNED SMELL. THE SMOKE LASTED APPROXIMATELY 30 SECONDS TO 1 MINUTE BEFORE IT DISSIPATED. THE CREW CONTINUED DESCENT INTO MVY, WHERE THE AIRCRAFT Jan 4, 1999 · N125YV · Beech 1900D · Air Distribution SystemSDR CA990311041Switch · failed(CAN) CREW REPORTED DURING FLARE, AIRCRAFT PROPS WOULD GO TO IDLE POSITION BEFORE TOUCHDOWN. FOUND RIGHT SQUAT SWITCH WAS SHORTED BETWEEN PINS A AND B CAUSING INTERMITTENT SELECT SIGNALS. SWITCH REPLACED.Jan 4, 1999 · Beech 1900D · Landing Gear Position and WarningSDR 99ZZZX564Link · brokenNOSE LANDING GEAR FAILED TO EXTEND. UPON INSPECTION OF AIRCRAFT, NOSE GEAR CENTERING LINK ASSEMBLY FOUND BROKEN. REPLACED NOSE GEAR CENTERING LINK ASSEMBLY WITH NEW ASSEMBLY. PERFORMED INSPECTION OF NOSE GEAR CENTERING LINK ASSEMBLY ON ALL AIRCRAFT IN FLEETJan 4, 1999 · N830CA · Beech 1900D · Landing Gear Retraction/Extension SystemSDR CA990203025Pin · loose(CAN) INERTIAL VANE CONTROL (IVC) LINKAGE DOWEL PIN WORKED ITSELF LOOSE, LINKAGE CAME APART. SPRING FOUND LYING ON TOP OF THE AIR INLET SCREEN, REST OF LINKAGE FOUND IN BOTTOM OF THE ENGINE COWLING. DOWEL PIN WAS NOT FOUND. FOD DAMAGE ON 1ST STAGE COMPRESSOJan 3, 1999 · Beech 1900D · Turbine Engine Compressor SectionSDR MASA99001Windshield · crackedFLT 6459 - FMN-PHX - IN FLIGHT, THE RIGHT PILOT WINDSHIELD CRACKED TOP TO BOTTOM WITH CRACKS RADIATING FROM BOTH SIDES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS DIVERTED TO INW. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS SUBSEQUENTLY FERRIED TO FMJan 2, 1999 · N93ZV · Beech 1900D · Flight Compartment WindowsSDR CA990111003Motor · failed(CAN) CREW DETECTED AN ODOR FOLLOWED BY SMOKE. DEPLOYED OXYGEN. LANDING MADE OK. THE FLAP MOTOR WAS FOUND BLACKENED AND EMITTING ODOR. MOTOR WAS SEIZED. THE 20-AMP CIRCUIT BREAKER HAD TRIPPED.Dec 30, 1998 · Beech 1900D · Trailing Edge Flap ActuatorSDR C2XA98IA549Lamp · failedIAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT BULB IN THE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE BULB AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Dec 29, 1998 · N87550 · Beech 1900D · Emergency LightingSDR C2XA98CL089Pc Board · failedCLT - FLT 3268 - CREW REPORTED THAT AFTER DEPARTURE, THE LANDING GEAR WOULD NOT RETRACT, AIRCRAFT CONTINUED ON TO CLE FROM CVG. AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED PC BOARD A316 IAW B1900 MM 32-30-00. THE RIGHT Dec 27, 1998 · N81538 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 99ZZZM38Seal · leakingOIL LEAK FROM RIGHT ENGINE ACCESSORY SECTION. INVESTIGATION AND INSPECTION FOUND FUEL CONTROL UNIT GARLOCK SEAL LEAKING. REPLACED WITH NEW GARLOCK SEAL. (M)Dec 26, 1998 · N860CA · Beech 1900D · Turbine Engine Accessory Drive
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