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"

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 GLBA20060665Downlock Switch · out of adjustLEFT MAIN LANDING GEAR HAD NO INDICATION OF GEAR DOWN AND LOCKED, INDICATOR INOPERATIVE-WILL NOT TEST. OVERFLEW LAR TO DEN LANDED WITHOUT INCIDENT. INSPECTED AND RIGGED LEFT MAIN LANDING GEAR DOWNLOCK SWITCH.Feb 6, 2006 · N122UX · Beech 1900D · Landing Gear Position and WarningSDR CA060205001Wire · burnedON START, THE CREW ATTEMPTED TO START THE RIGHT ENGINE. BUT NO LUCK STARTING THE ENGINE. AIRCRAFT BROUGHT TO HANGAR AND MAINTENANCE DISPATCHED. UPON ARRIVAL, MAINTENANCE ATTEMPTED TO START THIS ENGINE. NO JOY. THE STARTING ONLY HAD APPROX 300 HOURS REMAINFeb 2, 2006 · Beech 1900D · Electrical Power System WiringSDR 02072006AUnknown · unknownWHEN LANDING GEAR IS EXTENDED AIRCRAFT YAWS TO THE RIGHT. PERFORMED OPERATIONAL TEST OF AILERON AND RUDDER INTERCONNECT IAW 27-10-08 AND LANDING GEAR TEST IAW 32-30-00. NO DEFECTS NOTED DURING BOTH TEST.Feb 2, 2006 · N152MJ · Beech 1900D · Flight Control SystemSDR AMWA75602Wire · disconnectedAC INBOUND, COULD NOT GET NOSE DOWN AND LOCK LIGHT ILLUMINATED. CREW THEN DECLARED EMERGENCY. FLEW OVER THE GROUND, GROUND VERIFIED GEAR DOWN. CREW LANDED THE AIRCRAFT WITH NO FURTHER INCIDENT. MAINTENANCE REPAIRED WIRE AND GEAR DOWNLOCK SWITCH. NO PARTS WERE Feb 2, 2006 · N174YV · Beech 1900D · Landing Gear System WiringSDR GLBA20060658Bearing Race · brokenPROPELLER REMOVED FROM SERVICE DUE TO EXCESSIVE BLADE END PLAY. TEARDOWN FOUND NR 3 BLADE BEARING RACE BROKEN AND INTERNAL HUB DAMAGE.Feb 2, 2006 · N254GL · Beech 1900D · Propeller Hub SectionSDR GUUA94753020106ASkin · dentedDURING INSP DISCOVERED LT FUSELAGE HAD (3) FLAT DENTS 8 INCHES BELOW CARGO DOOR BETWEEN FS 468.250 THROUGH 482.250. FILLED DENTS WITH AERODYNAMIC FILLER , FABRICATED AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER REPAIR OVER ALL (3) DENTS.Feb 1, 2006 · N69547 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA02010601Annunciator · looseEYW/FLL DURING APPROACH LANDING GEAR WARNING SOUNDED. TIGHTENED LANDING GEAR ANNUNCIATOR HOUSING.Feb 1, 2006 · N218YV · Beech 1900D · Landing Gear Position and WarningSDR GUUA02010602Skin · dentedEYW/FLL DENT FOUND EIGHT INCHES BELOW CARGO DOOR. FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR IN ACCORDANCE WITH 1900 STRUCTURAL REPAIR MANUAL.Feb 1, 2006 · N69547 · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20060660Anti-Ice System · smokeCAPTAINS WINDSHIELD HEAT CYCLED ON AND OFF WITH SWITCH OFF, DESCENDING INTO DENVER HAD ELECTRICAL ODOR AND SMOKE STARTED COMING OUT FROM CAPTAINS CONTROL COLUMN, TURNED OFF ALL ICE PROTECTION SMOKE DISSAPATED, LANDED WITHOUT INCIDENT, PENDING REPAIRSFeb 1, 2006 · N202UX · Beech 1900D · Ice/Rain Protection SystemSDR CA060202001Wire · chafedA/C BROUGHT INTO HANGAR AFTER THE DAY OF FLYING. WHILE IN THE HANGAR THE CARGO DOOR WARNING CAME ON. INSPECTED THE DOOR WARNING AND FOUND THE DOOR AJAR SWITCH STICKY AND THE LATCH HANDLE SWITCH CRACKED. SWITCHES REPLACED ALL CHECKED OK. THE REASON FOR THISJan 31, 2006 · Beech 1900D · Door System WiringSDR GUUA01300601Skin · dentedDURING ROUTINE SCHEDULED MAINTENANCE FOUND LEFT FUSELAGE FORWARD OF CARGO DOOR HAS DENTED AREAS. REPAIRED DENTED AREAS BY INSTALLING INSERTION PATCH AND INTERIOR REINFORCEMENT DOUBLER IN ACCORDANCE WITH 1900 STRUCTURAL REPAIR MANUAL.Jan 30, 2006 · N81546 · Beech 1900D · Fuselage Main, Plate/SkinSDR BSAASDR0601Switch · malfunctionedDURING CLIMB-OUT, CARGO DOOR OPEN ANNUNCIATOR WARNING LIGHT CAME ON AS CREW ASCENDED THROUGH 12,000 FT. CREW RETURNED TO STATION. THE CARGO DOOR OPEN LIGHT WAS INITIALLY DEFERRED IAW THE MEL, AND ACFT WAS RETURNED TO SERVICE. DEFERRAL WAS CLEARED BY ADJUSTIJan 28, 2006 · N173YV · Beech 1900D · Door Warning SystemSDR GLBA20060655Downlock Switch · dirtyLEFT MAIN GEAR ANNUNCIATOR DID NOT ILLUMINATE WITH GEAR SELECTED DOWN, PERFORMED MANUAL GEAR EXTENSION. INSPECTED AND CLEANED ALL THREE DOWNLOCK SWITCHES, OPS CHECKED SATISFACTORY.Jan 26, 2006 · N208GL · Beech 1900D · Landing Gear Position and WarningSDR 01302006AGauge · sticksRT TORQUE GAUGE STICKS ON GROUND AND INFLIGHT. RT TORQUE GAUGE PN ON/OFF 129-380004-3, SN ON 304, SN OFF 368. OPS CHECK GOOD IAW 31-10-00.Jan 25, 2006 · N124CJ · Beech 1900D · Engine BMEP/Torque IndicatingSDR CA060126008Bearing · worn(CAN) DURING A GENERAL WALKAROUND THE RUDDER WAS MOVED BY HAND. NOTICING THAT THE RUDDER SEEMED TO MOVE UP AND DOWN AND APPEARED TO RUB AGAINST THE TAIL CONE. RUDDER ATTATCHMENT INSPECTED. INVESTIGATION REVEALED THAT ALL THREE BEARINGS HAVING SOME PLAY. THE LOJan 24, 2006 · Beech 1900D · Rudder StructureSDR GUU2006F00010Master Cylinder · inoperativeDURING TAXI, LT PEDAL WENT FLAT. RETURNED TO GATE. REPLACED FO LT MASTER CYLINDER. (K)Jan 23, 2006 · N82539 · Beech 1900D · Master Cylinder/Brake ValveSDR 75431Unknown · unknownON TAXI OUT THE GEAR TRANSIT INDICATION ILLUMINATED AND GEAR WARNING HORN SOUNDED. CREW STOPPED, SHUT DOWN ENGINES AND DEPLANED PAX ON TAXI WAY. NO FURTHER INCIDENTS.Jan 23, 2006 · N174YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUU2006F00009Pitot Tube · overheatedDURING APPROACH, FO ALTIMETER, FLT DIRECTOR AND YAW DAMP BECAME INOPERATIVE FOLLOWED BY SMOKE IN THE COCKPIT THROUGH THE FO INSTRUMENT PANEL. DETERMINED THAT THE RT PITOT TUBE OVERHEATED CAUSINGTHE RT PITOT HOSES TO BURN FROM THE INSIDE OUT PRODUCING SMOKE, AJan 20, 2006 · N87551 · Beech 1900D · Pitot/Static SystemSDR 01252006ASwitch · failedNOSE GEAR INDICATOR LIGHT FAILED TO ILLUMINATE WHEN GEAR SELECTED DOWN, RED HANDLE LIGHT STAYED ON (UPON LANDING GREEN LIGHT CAME ON, RED LIGHT WENT OUT.) REMOVED AND REPLACED NOSE GEAR DOWN LOCK SWITCH PN 100-381006-1, RIGGING AND OPS CHECK GOOD IAW 32-60-01Jan 19, 2006 · N243CJ · Beech 1900D · Landing Gear Position and WarningSDR GLBA20060648Bearing Race · brokenEXCESSIVE PROPELLER BLADE END PLAY REMOVED FROM SERVICE, TEARDOWN OF THE ASSEMBLY FOUND A BROKEN BEARING RACE WITH ADDTIONAL DAMAGE TO THE HUB AND A PROPELLER BLADE. HUB, BLADE BEARINGS, PRELOAD PLATES, BLADE SEAL AND CLAMPS WERE REPLACED AT PREVIOUS OVERHAUL.Jan 14, 2006 · N220GL · Beech 1900D · Propeller Hub SectionSDR CA070123011Engine · oil consumption(CAN) CREW NOTED THEIR NR 1 OIL PRESSURE, FLUCTUATING AROUND 75 PSI. THEY RETURNED TO THE GATE AND REPORTED TO MAINTENANCE. INSPECTION OF THE CHIP DETECTOR AND OIL FILTER REVEALED NO FAULTS. THE ENGINE WAS FILLED WITH OIL AND GROUND RUN WITH NO CONSUMPTION OF Jan 12, 2006 · Beech 1900D · Turbine Engine Oil SystemSDR R018723Bearing · brokenPROPELLER WAS RETURNED DUE TO FOREIGN OBJECT STRIKE. DISASSEMBLY REVEALED ONE BROKEN D-7745 BLADE THRUST BEARING ON BLADE POSITION ONE, SERIAL NUMBER 994.Jan 9, 2006 · Beech 1900D · Propeller AssemblySDR 1051213026AAngle · crackedDURING ABC STRUCTURAL INSPECTION ANGLE WAS FOUND CRACKED.Jan 6, 2006 · N126YV · Beech 1900D · Fuselage Miscellaneous StructureSDR 1051213026Angle · crackedDURING ABC STRUCTURAL INSPECTION ANGLE WAS FOUND CRACKED.Jan 6, 2006 · N126YV · Beech 1900D · Fuselage Miscellaneous StructureSDR CA060106004Windshield · crackedDEPARTING AIRPORT THE LT HEATED WINDSHIELD CRACKED. TURNED AROUND AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS SENT TO MAINTENANCE WHO REPLACED THE WINDSHIELD.Jan 5, 2006 · Beech 1900D · Flight Compartment WindowsSDR CA060106003Wire · damagedUPON ARRIVAL, THE GEAR WAS SELECTED DOWN BUT NO DOWN AND LOCKED ANNUNCIATORS ILLUMINATED. THE IN TRANSIT LIGHT WAS ALSO NOT ILLUMINATED SO THE PILOT DID A FLY BY OF TOWER TO CONFIRM GEAR POSITION, THEY ALSO HAD EMERGENCY SERVICES ON STANDBY. AN UNEVENTFUL LAJan 5, 2006 · Beech 1900D · Landing Gear System WiringSDR 01092006Motor · burned outEVACUATED A/C DUE TO SMOKE WHICH FILLED CABIN ON TAXI FOR DEPARTURE. FOUND FLAP MOTOR UNDER FLOORBOARD WAS BURNED, ALSO FLAP C/B WAS POPPED UNDER THE FLOORBOARD. TRIED TO TO RESET BREAKER AND OPERATE FLAPS BUT BREAKER POPPED AGAIN. REMOVED AND REPLACED FLAP MJan 3, 2006 · N220CJ · Beech 1900D · Trailing Edge Flap Control SystemSDR CA060129012Engine · low pressure(CAN) DURING TAKE-OFF ROLL, THE ENGINE LOW PRESSURE WARNING ANNUNCIATED AND THE TAKE-OFF WAS ABORTED. MFG WILL MONITOR INVESTIGATION OF THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20060129012)Jan 2, 2006 · Beech 1900D · Engine Oil PressureSDR 75068Warning Light · illuminatedDURING CRUISE, GEAR UNSAFE LIGHT AND HORN ILLUMINATED CONTINUOUSLY AND WOULD NOT SILENCE. MADE NO CONFIGURATION CHANGES TO CAUSE EVENT. DESCEND TO LOWER ALTITUDE, LIGHT WENT OUT 14000FT. CYCLED GEAR PRIOR TO TRAFFIC PATTERN, INDICATION NORMAL. PROCEED FOR NJan 2, 2006 · N174YV · Beech 1900D · Main Landing GearSDR 75059Brake Pads · malfunctionedUPON ARRIVING INTO DUJ, THE CREW CALLED IN AND WROTE UP THE BRAKES AS BEING SPONGY. MAINTENANCE THEN CHANGED LEFT I/B BRAKE ASSY, AND BLED ALL BRAKES.Jan 2, 2006 · N242YV · Beech 1900D · Landing Gear Brake SystemSDR 01092006DIndicator · inoperativeABORTED TO DUE TO COPILOT'S AIRSPEED AT 0 KNOTS INITIATED DECELERATION AT 80 KNOTS WHILE DECELERATING COPILOT'S AIRSPEED NEEDLE POPPED UP, MATCHING PILOT'S SIDE AT ABOUT 60 KNOTS AND DECELERATING. PERFORMED PITOT STATIC TEST, SYSTEM OPERATING NORMAL. TESTED Jan 1, 2006 · N172MJ · Beech 1900D · Airspeed/Mach IndicatorSDR GUU2006F00008Pressure Panel · crackedSEVERAL SMALL CRACKS IN NOSE WHEEL WELL CEILING FROM NOSE WHEEL TIRE IMPACT DUE TO NOSE UP LANDING. DAMAGE LOCATION AT FUSELAGE STA 81, WATER LINE 100.00 AT CENTER BUTT LINE. REMOVED DAMAGE AREA AND INSTALLED EXTERNAL DOUBLER IAW MM. (K)Jan 1, 2006 · N53545 · Beech 1900D · Fuselage Main, BulkheadSDR GUU2006F00007Connector · looseDURING FLIGHT, RT FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR ILLUMINATED INTERMITTENTLY. RESECURED WIRE CONNECTORS AT RT FIRE EXTINGUISHER ANNUNCIATOR SWITCH. (K)Dec 28, 2005 · N49543 · Beech 1900D · Fire Protection System WiringSDR GUU2006F00006Hinge · corrodedAT SCHEDULED INSPECTION, DETERMINED VERTICAL FIN UPPER RUDDER HINGE BRACKET TO BE EXFOLIATED. REPLACED VERTICAL FIN UPPER RUDDER HINGE BRACKET. (K)Dec 28, 2005 · N69547 · Beech 1900D · Rudder StructureSDR GUU2006F00005Hinge · corrodedAT SCHEDULED INSPECTION, DETERMINED VERTICAL FIN CENTER RUDDER HINGE BRACKET TO BE EXFOLIATED. REPLACED VERTICAL FIN CENTER RUDDER HINGE BRACKET. (K)Dec 28, 2005 · N69547 · Beech 1900D · Rudder StructureSDR S2YA05083Line · looseDURING FLIGHT, THE CREW REPORTED RT ENVIRO FAIL AND CABIN ALT HIGH. SINCE THE FLIGHT LEVEL WAS RESTRICTED TO 9500 FT THE CREW PERFORMED AN AIR-TURN-BACK. MX REPLACED THE LT PRSOV BUT THAT DID NOT FIX THE PROBLEM. MX INSPECTED THE SYSTEM AND FOUND A LOOSE TEDec 23, 2005 · N87SK · Beech 1900D · Air Conditioning SystemSDR 74809Fire Loop · failedWHILE IN ROUTE, THE LT T-HANDLE ILLUMINATED. CREW COMPLIED WITH EMERGENCY CHECKLIST AND DIVERTED DECLARED EMERGENCY AND LANDED SAFELY WITH NO FURTHER INCIDENT. IT WAS THEN FERRIED, MAINTENACE REMOVED AND REPLACED LT FWD FIRE LOOP ASSY.Dec 19, 2005 · N176YV · Beech 1900D · Fire DetectionSDR 74806Display · failedCAPT EHSI WENT BLANK AND CREW SMELLED AN ODOR THEY DETERMINED IT TO BE ELECTRICAL RELATED. AIRCRAFT LANDED WITH NO FUTHER INCIDENT. MAINTENANCE REPAIRED WIRES. NO PARTS WERE USED.Dec 19, 2005 · N142ZV · Beech 1900D · Instrument PanelSDR 74784Brake · weakWHILE TAXING IN, THE CREW NOTICED THE BRAKES WERE SPONGEY. THE AIRCRAFT WAS THEN FERRIED AND MAINTENANCE BLED THE BRAKES. NO PARTS USED.Dec 18, 2005 · N176YV · Beech 1900D · Landing Gear Brake SystemSDR 74798Master Cylinder · failedDURING TAXI IN, THE CREW REPORTED THE BRAKES FEELING SPONGY. THEN FERRIED TO ICT WHERE MAINTENANCE REMOVED AND REPLACED THE MASTER CYLINDER.Dec 18, 2005 · N176YV · Beech 1900D · Master Cylinder/Brake ValveSDR GUU2006F00003Hinge · corrodedAT SCHEDULED INSPECTION, DETERMINED RT ELEVATOR CENTER HINGE BRACKET TO BE EXFOLIATED. REPLACED RT ELEVATOR CENTER HINGE BRACKET. (K)Dec 16, 2005 · N87557 · Beech 1900D · Horizontal Stabilizer StructureSDR GUU2006F00002Hinge · corrodedAT SCHEDULED INSPECTION, DETERMINED LT ELEVATOR CENTER HINGE BRACKET TO BE EXFOLIATED. REPLACED LT ELEVATOR CENTER HINGE BRACKET. (K)Dec 16, 2005 · N87557 · Beech 1900D · Horizontal Stabilizer StructureSDR AU510001632Cable · failedCABIN DOOR TOP FORWARD LATCHING CABLE SNAPPED ALLOWING TOP FORWARD LOCK TO UNLATCH.Dec 12, 2005 · Beech 1900D · Passenger/Crew DoorsSDR AU510001493Engine · low pressureRT ENGINE LOST OIL PRESSURE. ENGINE SHUT DOWN WHEN OIL PRESSURE DROPPED TO 60 PSI.Dec 12, 2005 · Beech 1900D · Turbine Engine Oil SystemSDR S2YA05082Windshield · crackedDURING FLIGHT, THE LT WINDSHIELD CRACKED. THE CREW PERFORMED AN AIR-TURN-BACK. MX REPLACED THE LT WINDSHIELD AND RETURNED THE AC TO SERVICE. (K)Dec 11, 2005 · N79SK · Beech 1900D · Flight Compartment WindowsSDR CA051213009Uplock Switch · malfunctionedA/C SCHEDULED DEPARTURE AND DESTINATION. AFTER T/O CREW SELECTED GEAR UP AND THEY HAD THE INTRANSIT LIGHT STAY ON (GEAR HANDLE LIGHT). CREW CALLED MX FROM THE AIR AND CYCLED GEAR. CYCLING OF GEAR DID NOT MATTER. MX AND CREW DECIDED IT WOULD BE BEST TO RETUDec 9, 2005 · Beech 1900D · Landing Gear Position and WarningSDR CA051207005Uplock Switch · intermittentON CLIMB WHEN GEAR WAS SELECTED UP, THE INTRANSIT LIGHT IN GEAR HANDLE STAYED ILLUMINATED. PILOT CYCLED GEAR AND DOWNLOCK GREEN LIGHTS GOOD BUT HANDLE ALWAYS RED IN GEAR UP POSITION. ELECTED TO RETURN TO MAINTENANCE BASE. THE GEAR WAS GOOD IN THE DOWN AND LDec 6, 2005 · Beech 1900D · Landing Gear Position and WarningSDR GUU2006F00004Hinge Bracket · corrodedAT SCHEDULED MAINTENANCE, DETERMINED VERTICAL STABILIZER LOWER HINGE BRACKET TO BE EXFOLIATED. REPLACED VERTICAL STABILIZER LOWER HINGE BRACKET. (K)Dec 5, 2005 · N69549 · Beech 1900D · Horizontal Stabilizer StructureSDR 12062005ACowling · looseLT TOP FWD ENGINE COWL CAME LOOSE IN FLIGHT. REMOVED AND INSPECTED LT TOP FWD ENGINE COWL, NO DEFECTS NOTED. REINSTALLED COWL AND SECURED LATCHES, NO DEFECTS NOTED.Dec 4, 2005 · N60MJ · Beech 1900D · Engine Cowling SystemSDR 74424Shutoff Valve · failedON CLIMB OUT, CREW WENT TO PRESSURIZE AIRCRAFT AND THE CABIN DOOR ANNUNCIATOR ILLUMINATED. CREW RETURNED TO FIELD WITH NO FURTHER INCIDENT. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REPLACED THE RIGHT INSTRUMENT AIR SHUT OFF VALVE. MORE INFORMATION WILL BE AVDec 2, 2005 · N10675 · Beech 1900D · Passenger/Crew Doors
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