Beech 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 76473Actuator · crackedUPON ARRIVAL, CREW REPORTED EVIDENCE OF HYDRAULIC FLUID COMING FROM RIGHT WHEEL WELL. CONTRACT MAINTENANCE WAS CALLED AND REPORTED HYDRAULIC FLUID LEAKING FROM THE TOP OF THE RIGHT MAIN GEAR ACTUATOR. COMPANY MAINTENANCE ARRIVED AND FOUND THE TOP CAP OF THE ACMar 20, 2006 · N127ZV · Beech 1900D · Landing Gear ActuatorSDR 76399Fire Loop · warning lightRT FIRE LOOP WARNING ILLUMINATED IN FLIGHT WITH RT FIRE HANDLE ILLUMINATION MORE INFO TO BE ADDED LATER. CONTROL NR 76398.Mar 15, 2006 · N244YV · Beech 1900D · Fire DetectionSDR 76398Fire Loop · out of positionRIGHT FIRE LOOP WARNING ILLUMED IN FLIGHT WITH RIGHT FIRE HANDLE ILLUMINATION. MAINTENANCE WAS CALLED AND REPOSITIONED FIRELOOP OPS CHECKS NORMAL. NO PARTS WERE USED.Mar 15, 2006 · N244YV · Beech 1900D · Fire DetectionSDR GUUA03150602Warning Switch · inoperativeFLIGHT 9133 VPS/TPA DURING APPROACH LANDING GEAR WARNING HORN NOT WORKING. REPLACED LANDING GEAR WARNING HORN SWITCH BUTTON.Mar 15, 2006 · N190YV · Beech 1900D · Landing Gear Position and WarningSDR GLBA20060692Control Handle · wornON CLIMBOUT GEAR INTRANSIT LIGHT REMAINED ILLUMINATED WITH GEAR WARNING HORN. CYCLED GEAR AND FLAPS, OPERATION NORMAL. FLAP HANDLE 17 PERCENT DETENT WORN MEL'D 23208.Mar 13, 2006 · N219GL · Beech 1900D · Trailing Edge Flap Control SystemSDR GUUA03110601Skin · damagedAT SCHEDULED ROUTINE MAINTENANCE LEFT FUSELAGE HAS CREASED SKIN LOCATED 3 INCHES AFT OF CARGO DOOR BETWEEN FUSELAGE STATIONS 513.00 THRU 544.250 AT STRINGER 9L AND 10L. INSTALLED REINFORCEMENT DOUBLER OF 2024-T3 .050 IN DIMENSION 19.0 IN X 7.0 IN ACCORDANCE WMar 11, 2006 · N87551 · Beech 1900D · Fuselage Main, Plate/SkinSDR AMWA76315Structure · bird strikeON APPROACH INTO MHK AIRCRAFT STRUCK MULTIPLE GEESE. AIRCRAFT DAMAGE TO RIGHT STUB WING AND RIGHT WING OUTBOARD NACELLE. MAINTENANCE REMOVED AND REPLACED THE ENTIRE RT LEADING EDGE IAW FR-CO-01332,01333,01334.Mar 10, 2006 · N166YV · Beech 1900D · Wing Main, Frame StructureSDR GUUA03090601Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, VERTICAL FIN UPPER HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED UPPER HINGE BRACKET.Mar 9, 2006 · N87551 · Beech 1900D · Vertical StabilizerSDR R019280Bearing Race · brokenCUSTOMER REMOVED PROPELLER DUE TO LOOSE BLADE IAW HARTZELL SERVICE BULLETIN HC-SB-61-283. ONE D-7745 BLADE SIDE BEARING INSTALLED ON BLADE SERIAL NUMBER 2828 WAS FOUND CRACKED CIRCUMFERENTIALLY.Mar 3, 2006 · Beech 1900D · Propeller AssemblySDR GUUA03020603Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RIGHT CENTER ELEVATOR HINGE BRACKET.Mar 2, 2006 · N87550 · Beech 1900D · Elevator Miscellaneous StructureSDR GUUA03020602Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, VERTICAL FIN UPPER RUDDER HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED UPPER RUDDER HINGE BRACKET.Mar 2, 2006 · N87550 · Beech 1900D · Vertical Stabilizer, Attach FittingsSDR GUUA03020601Spar · corrodedAT SCHEDULED ROUTINE MAINTENANCE, VERTICAL FIN AFT RIGHT SPAR ANGLE 3.0 THRU 4.5 INCHES BELOW UPPER HINGE BRACKET SHOWS SIGN OF EXFOLIATION. REMOVED CORRODED MATERIAL, BLENDED AREA AND INSTALLED REINFORCEMENT DOUBLER IN ACCORDANCE WITH FAA APPROVED DATA CONTAMar 2, 2006 · N87550 · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA20060688Smoke · detectedSMOKE IN CABIN. SMOKE APPEARED TO DISSIPATE AFTER TURNING OFF MASTER SWITCH. INSPECTED ELECTRICAL SYSTEM, COULD NOT DUPLICATE.Mar 1, 2006 · N122UX · Beech 1900D · Air Distribution SystemSDR BSAASDR0608Rib · corrodedPITTING CORROSION WAS FOUND ON THE RIGHT WING INBOARD MILLED RIB ON THE LOWER FLANGE ADJACENT, BUT NOT AFFECTING, THE RIVET HOLE INBOARD OF THE WING DRAIN LOCATED JUST OUTBOARD OF THE NACELLE IN THE WING LEADING EDGE. THE DAMAGE AREA IS APPROXIMATELY .3 INCH Feb 28, 2006 · N131YV · Beech 1900D · Wing, Rib/BulkheadSDR 76110Bolt · wornCLUNKING NOISE HEARD WHEN ELEVATOR CONTROL MOVED. FOUND AND REPLACED WORN BOLTS ATTACHING ROD END AT FORWARD ELEVATOR BELLCRANK AND CONTROL COLUMN.Feb 28, 2006 · N162ZV · Beech 1900D · Elevator Control SystemSDR 76087Trim Panel · looseAFTER ARRIVAL INTO PIT, THE CREW REPORTED THAT THE DOOR WOULD NOT OPEN FROM THE OUTSIDE. THE CREW THEN OPENED THE DOOR FROM THE INSIDE NORMALLY. MAINTENANCE RE-SECURED TRIM PIECE AND TRIM BACK.Feb 27, 2006 · N155ZV · Beech 1900D · Passenger/Crew DoorsSDR BSAASDR0607Spar Cap · damagedPITTING CORROSION WAS FOUND ON THE RIGHT WING ON THE LOWER WING SPAR CAP IN THE THIRD ELEMENT SPAR STRAP JUST AFT OF THE WING DRAIN LOCATED JUST OUTBOARD OF THE NACELLE IN THE WING LEADING EDGE. THE DAMAGE AREA IS APPROXIMATELY .5 INCH WIDE AND WENT INTO THE Feb 27, 2006 · N182YV · Beech 1900D · Wing SparSDR 03012006DFlap System · unknownFLAP WILL NOT RETRACT.Feb 26, 2006 · N191CJ · Beech 1900D · Trailing Edge Flap Control SystemSDR 02232006ALight · inoperativeLEFT FIRE PUSH TO EXTINGUISH LIGHT INOP.Feb 22, 2006 · N152MJ · Beech 1900D · Fire Protection SystemSDR BSAASDR0606Bonding Jumper · looseCREW WAS DESCENDING WHEN SMOKE WAS NOTED IN THE COCKPIT, APPROXIMATELY 15 TO 20 MNIUTES FROM DESTINATION. CREW DECLARED EMERGENCY, CONTINUED DESCENT, AND LANDED WITH NO FURTHER INCIDENTS. THE WINDSHIELD HEAT WAS TURNED ON THE TIME. A LOOSE GROUND LEAD WIRE Feb 22, 2006 · N171ZV · Beech 1900D · Windshield/Door Rain/Ice RemovalSDR BSAASDR0605Static Inverter · inoperativeDURING INITIAL CLIMB AT APPROX 200FT AGL THE LT AC BUSS FAILED, CREW TRIED RESET, AND THIS DIDN'T WORK, TRANSFER WAS SELECTED AND WORKED, CREW RETURNED TO STATION. FOUND STATIC INVERTER FAILED, REPLACED UNIT AND DURING SUBSEQUENT RUNS, FOUND INVERTER COOLING Feb 20, 2006 · N3199Q · Beech 1900D · AC InverterSDR GLBA20060690Fuel Tank · leakingRIGHT AUX TANK FUEL LEAK FROM WEEP HOLE. VISUALLY INSPECTED AFFECTED SYSTEM AND FOUND SAFE FOR INTENDED FERRY FLIGHT GRI TO CYS.Feb 17, 2006 · N210GL · Beech 1900D · Fuel StorageSDR GUUA02170601Warning Light · false activationDURING FLIGHT RIGHT FIRE DISCHARGE ANNUNCIATOR ILLUMINATED INTERMITTENTLY. INSPECTED THE RIGHT FIRE PROTECTION SYSTEM, NO DEFECTS NOTED.Feb 17, 2006 · N49543 · Beech 1900D · Smoke DetectionSDR GLBA20060679Smoke · detectedREPORT OF SMOKE (ELECTRICAL) SMELL IN COCKPIT, FLIGHT DIRECTOR C/B POPPED, RESET CIRCUIT BREAKER, OPS CHECKED SYSTEM GOOD.Feb 17, 2006 · N122UX · Beech 1900D · Air Distribution SystemSDR GLBA200606680Smoke · detectedSMOKE REPORTED IN COCKPIT, PERFORMED HIGH POWER ENGINE RUN UP WITH ELECTRICAL SYSTEMS ENERGIZED, NO FAULTS FOUND.Feb 17, 2006 · N195GL · Beech 1900D · Air Distribution SystemSDR GUUA02160601Skin · crackedAT SCHEDULED INSPECTION DISCOVERED A 2.0 INCH CRACK ON THE RT WING BELLY SKIN RUNNING LATERALLY AT FS 303.25 X BL 30.62. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURAL MM 53-90-18Feb 16, 2006 · N87555 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA02160602Warning Light · false activationDURING FLIGHT RIGHT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATES INTERMITTENTLY. CLEANED CONTACTS AT THE RIGHT FIRE EXTINGUISHER.Feb 16, 2006 · N49543 · Beech 1900D · Detection SystemSDR BSAASDR0603Wire · out of positionNR 1 ENGINE FIRE WARNING LIGHT CAME ON BRIEFLY 3-5 SECONDS, WHILE IN CRUISE, AND WENT OUT AS CAPTAIN BEGAN TO REACH FOR THE EMERGENCY CHECKLIST. SYSTEM WAS CHECKED AFTER ARRIVAL, VISUAL AND OPERATIONAL INSPECTION REVEALED NO DEFECTS, WITH THE FIRE DETECTER WIFeb 16, 2006 · N139ZV · Beech 1900D · Fire Protection System WiringSDR BSAASDR0604Fire Detector · shortedDURING CRUISE, LEFT FIRE DETECTOR LOOP LIGHT CAME ON AND STAYED ILLUMINATED, CREW LANDED WITH NO FURTHER INCIDENT. REPLACED FORWARD FIRE DETECTOR LOOP DUE TO FINDING CENTER WIRE SHORTED TO SHIELD. SYSTEM OPS CK GOOD.Feb 16, 2006 · N139ZV · Beech 1900D · Fire DetectionSDR 75883Safety Switch · failedAFTER TAKEOFF, CREW COULD NOT RETRACT THE FLAPS. RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE THEN REMOVED AND REPLACED RIGHT FLAP SAFETY SWITCH. THE FLIGHT WAS A REPOSTION FROM ICT TO MCI, NO PAX ON BOARD.Feb 16, 2006 · N138YV · Beech 1900D · Trailing Edge FlapsSDR 1051229025Spar Cap · corrodedCORROSION ON LT WING MAIN SPAR FWD SPAR CAP FLANGE. FOUND DURING INSPECTIONFeb 15, 2006 · N155ZV · Beech 1900D · Wing SparSDR 1051229028ASpar Cap · corrodedBIO CORROSION ON RIGHT WING MAIN SPAR CAP FLANGE NEAR WS 124588. MAINTENANCE FOUND DURING INSPECTION.Feb 15, 2006 · N155ZV · Beech 1900D · Wing SparSDR 1051229028Spar Cap · corrodedBIO CORROSION ON LEFT WING MAIN SPAR FWD SPAR CAP FLANGE. FOUND DURING INSPECTION.Feb 15, 2006 · N155ZV · Beech 1900D · Wing SparSDR CA060218001Motor · burnedAFTER TAKEOFF, AIRCRAFTS LANDING GEAR WOULD NOT RETRACT. CREW CONTACTED MX AND CREW AND MX DECIDED TO LEAVE THE LANDING GEAR DOWN AND CONTINUE THE 30 MINUTE FLIGHT TO THE MAIN BASE. ALL INDICATIONS SHOWED THAT THE LANDING GEAR WAS DOWN AND LOCKED. THE AIRCRFeb 14, 2006 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR AMWA76372Motor · odorDURING TAXI OUT, FLAPS STUCK BETWEEN ZERO AND 17 DEGREES. THE CREW NOTICED AN ELECTRICAL SMELL IN THE CABIN AREA AND RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE FLAP MOTOR/GEARBOX.Feb 14, 2006 · N138YV · Beech 1900D · Trailing Edge Flap Control SystemSDR AMWA76380Connector · looseRIGHT FIRE LOOP CAUSES MASTER WARNING TO ILLUMINATE IN FLIGHT. MAINTENANCE CAME AND RESECURED A LOOSE CONNECTION AT THE FORWARD CONNECTOR. OPS CHECK NORMAL.Feb 14, 2006 · N244YV · Beech 1900D · Fire Protection System WiringSDR 1060106041ASpar Cap · corrodedCORROSION RIGHT SPAR CAP NEAR WS 124.588. FOUND DURING INSPECTION.Feb 14, 2006 · N138YV · Beech 1900D · Wing SparSDR GLBA20060669Actuator · intermittentLEFT MAIN LANDING GEAR GREEN INDICATOR ILLUMINATED ON EXTENSION BUT FLICKERED, WHEN RETRACTED WENT BACK ABOUT HALFWAY. MANUALLY EXTENDED GEAR, INSPECTED AND REPLACED LEFT MAIN LANDING GEAR ACTUATOR.Feb 11, 2006 · N122UX · Beech 1900D · Landing Gear ActuatorSDR BSAASDR0602Windscreen · crackedTHE LEFT COCKPIT WINDSHIELD INNER PANE CRACKED DURING CRUISE AS FL230, OAT WAS -40, WINDSHIELD HEAT WAS ON AT THE TIME, AIRCRAFT WAS NOT IN ICING CONDITIONS AT THE TIME, FLIGHT CONDITIONS WERE VFR. CREW LANDED WITH NO FURTHER INCIDENT. THE WINDSHIELD WAS CHAFeb 10, 2006 · N173YV · Beech 1900D · Flight Compartment WindowsSDR 1060106041Spar Cap · corrodedCORROSION LEFT MAIN SPAR CAP FWD FLANGE NEAR WS 124.588. FOUND DURING INSPECTION.Feb 10, 2006 · N138YV · Beech 1900D · Wing SparSDR GUUA95453020906ASkin · crackedDURING SCHEDULED ROUTINE MX DISCOVERED 2.0 INCH CRACK IN FUSELAGE BELLY SKIN IN SPAR AREA AT BL 30.62. STOP DRILLED CRACK AND INSTALLED REINFORCEMENT DOUBLER REPAIR.Feb 9, 2006 · N87554 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA02090603Unknown · crackedAT SCHEDULED INSPECTION DISCOVERED A 2.0 INCH CRACK RUNNING LATERALLY AT FS 303.25 X BL 30.62. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 53-90-18.Feb 9, 2006 · N8755 · Beech 1900D · Fuselage Main, StructureSDR GUUA02090602Unknown · crackedAT SCHEDULED INSPECTION DISCOVERED A 2.0 INCH CRACK RUNNING LATERALLY AT FS 303.25 X BL 30.62. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 53-90-18.Feb 9, 2006 · N8755 · Beech 1900D · Fuselage Main, StructureSDR GUUA02090601AUnknown · crackedAT SCHEDULED INSPECTION DISCOVERED A 2.0 INCH CRACK RUNNING LATERALLY AT FS 303.25 X BL 30.62. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 53-90-18.Feb 9, 2006 · N8755 · Beech 1900D · Fuselage Main, StructureSDR GUUA020906Unknown · crackedAT SCHEDULED INSPECTION DISCOVERED A 2.0 INCH CRACK RUNNING LATERALLY AT FS 303.25 X BL 30.62. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 53-90-18.Feb 9, 2006 · N8755 · Beech 1900D · Fuselage Main, StructureSDR GUUA02080601Tube · crackedMIA/MCO DURING FLIGHT LEFT ENGINE FUEL FLOW AND TORQUE WENT TO ZERO. ENGINE SHUT ITSELF DOWN, SECURED ENGINE. DIVERTED TO PBI. REPLACED P3 AIR TUBE ASSEMBLY BETWEEN FUEL CONTROL AND P3 AIR FILTER.Feb 8, 2006 · N87555 · Beech 1900D · Engine (Turbine/Turboprop)SDR GLBA20060667Motor · shortedELECTRICAL SMELL IN CABIN - INSPECTED FOUND FLAP MOTOR SHORTED, PLACED ON MEL.Feb 8, 2006 · N100UX · Beech 1900D · Trailing Edge Flap ActuatorSDR GUUA02060603Wire · out of positionDURING FLIGHT RIGHT ENGINE FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY. REPOSITION WIRES AT THE RIGHT FIRE EXTINGUISHER ANNUNCIATOR.Feb 6, 2006 · N49543 · Beech 1900D · Fire Protection System WiringSDR GUUA02060602Wire Harness · looseDURING FLIGHT RIGHT ENGINE DISCHARGE LIGHT ILLUMINATED ON AND OFF. SECURED WIRE BUNDLE AT THE RIGHT WHEEL WELL FIRE EXTINGUISHER BOTTLE.Feb 6, 2006 · N49543 · Beech 1900D · Fire Protection System WiringSDR GUUA02060601Odor · detectedTPA/TLH DURING FLIGHT AT CRUISE CREW NOTICED BURNING SMELL. REMOVED STANDING WATER ALONG CENTER AISLE UNDER FLOORBOARDS AND INSPECTED ELECTRICAL SYSTEMS, NO DEFECTS NOTED COULD NOT DUPLICATE.Feb 6, 2006 · N69547 · Beech 1900D · Air Distribution System
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