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 AMWA72Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED ONCE ON THE RIGHT SIDE. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03.Nov 5, 2003 · N165YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA71Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGES AT CANTED STAB STA 69.184 WAS FOUND CRACKED, ONCE ON THE LEFT AND ONCE ON THE RIGHT SIDE. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE TO BMM P/N 114-590021-9, 51-70-03.Nov 5, 2003 · N165YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA70Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 69.184 WAS FOUND CRACKED AT FWD CENTER STRINGER INTERSECTION. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE BMM P/N 114-590021-9, 51-70-03.Nov 5, 2003 · N23YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA69Rib · crackedWHILE PERFORMING AND INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 54.026 WAS FOUND CRACKED IN TWO PLACES ON THE RIGHT SIDE NEAR THE FWD, CENTER STRINGERS AND TWO PLACES ON THE LEFT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BMM P/Nov 5, 2003 · N23YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA81Riser · crackedWHILE PERFORMING AN A-CHECK STRUCTURAL INSPECTION, THE AIRSTAIR DOOR FOWARD STEP RISER WAS FOUND TO BE CRACKED.Nov 4, 2003 · N127YV · Beech 1900D · Entrance StairsSDR AMWA80Pressure Panel · chafedWHILE PERFORMING AN A-CHECK STRUCTURAL INSPECTION, RIVET HEAD CHAFED WAS FOUND TO THE RIGHT PRESSURE PLATE, RBL 30.28.Nov 4, 2003 · N127YV · Beech 1900D · Fuselage Main, Plate/SkinSDR AMWA79Rivet · chafedWHILE PERFORMING AN A-CHECK STRUCTURAL INSPECTION, RIVET HEAD CHAFED WAS FOUND TO THE LEFT PRESSURE PLATE, LBL 30.28.Nov 4, 2003 · N127YV · Beech 1900D · FastenersSDR AMWA78Bracket · wornWHILE PERFORMING AN A-CHECK STRUCTURAL INSPECTION, THE CARGO DOOR UPPER FORWARD GAS SPRING ASSEMBLY BRACKET HAD WORKING RIVETS.Nov 4, 2003 · N127YV · Beech 1900D · Fuselage Main, StructureSDR AMWA77Riser · crackedWHILE PERFORMING AN A-CHECK STRUCTURAL INSPECTION, THE CARGO DOOR UPPER AFT GAS SPRING ASSEMBLY BRACKET WORKING RIVETS.Nov 4, 2003 · N127YV · Beech 1900D · Cargo/Baggage DoorsSDR AMWA76Riser · crackedWHILE PERFORMING AN A-CHECK STRUCTURAL INSPECTION, THE AIRSTAIR DOOR AFT STEP RISER WAS FOUND TO BE CRACKED.Nov 4, 2003 · N127YV · Beech 1900D · Entrance StairsSDR AMWA75Actuator · stiffDURING FLIGHT, CREW DISCOVERED THE ELEVATOR TRIM WAS STIFF AND HAD DIFFICULTY MOVING THE ELEVATOR TRIM WHEEL. THE LT ELEVATOR CLEVES WAS ADJUSTED AND THE ACFT WAS RETURNED TO SERVICE.Nov 3, 2003 · N3199Q · Beech 1900D · Elevator Tab Control SystemSDR AMWA74Bolt · looseDURING A NR 6 DETAIL, IT WAS FOUND THAT THE FOUR BOLTS SECURING THE RUDDER TORQUE TUBE TO THE RUDDER AT THE LOWER ATTACH POINT FLANGE WERE LOOSE. CAUSING PLAY IN THE RUDDER CONTROL SYS AFTER REPLACING THE 4 BOLTS AND PERFORMING RUNNING TORQUE TESTS ON THE FASNov 2, 2003 · N3199Q · Beech 1900D · FastenersSDR GLBA2003144Bearing · failedNR 4 MLG WHEEL ASSEMBLY BEARING SPUN, REMOVED AND REPLACED WHEELS AND MLG STRUT ASSY.Nov 1, 2003 · N220GL · Beech 1900D · TireSDR GLBA2003143Circuit Board · failedNR 2 PROP FEATHERED ON LANDING APPROACH, REMOVED AND REPLACED PCB. OPS CK GOOD.Nov 1, 2003 · N255GL · Beech 1900D · Propeller Controlling SystemSDR GLBA2003142Wire · looseSTALL HEAT ANN ILLUM, RESECURED WIRE H91B16 ON TRANSDUCER.Nov 1, 2003 · N97UX · Beech 1900D · Ice/Rain Protection System WiringSDR 55727Squat Switch · malfunctionedAFTER TAKE OFF GEAR UP. SELECTED GEAR WOULD NOT RETRACT. C/B RESEATED AND ANOTHER ATTEMP WAS MADE WITH THE SAME RESULT. ACFT RETURNED TO FIELD WITH 3 GREENS LANDED WITH NO FURTHER INCIDENTS.(REMOVED AND REPLACED RIGHT SQUAT SWITCH)Oct 31, 2003 · N167YV · Beech 1900D · Landing Gear Position and WarningSDR AMWA117Stringer Clip · crackedWHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, STRINGER 13R WAS FOUND TO HAVE A CRACKED CLIP.Oct 30, 2003 · N23YV · Beech 1900D · Fuselage Main, Longeron/StringerSDR AMWA116Rivet · chafedWHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, THE LEFT WING ROOT PRESSURE PLATE WAS FOUND TO HAVE A RIVET HEAD CHAFED.Oct 30, 2003 · N23YV · Beech 1900D · FastenersSDR AMWA115Plate · chafedWHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, THE RIGHT WING ROOT PRESSURE PLATE WAS FOUND TO HAVE A RIVET HEAD CHAFE.Oct 30, 2003 · N23YV · Beech 1900D · Wing, Plate/SkinSDR AMWA114Stringer · crackedWHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, SKIN UNDER STRINGER 10R WAS FOUND CRACKED.Oct 30, 2003 · N23YV · Beech 1900D · Fuselage Main, Longeron/StringerSDR CA031029008Gcu · failed(CAN) A/C DEPARTED AND SHORTLY AFTER TAKEOFF THE LT GENERATOR FELL OFFLINE. IT COULD NOT BE RESET SO THE CREW ELECTED TO RETURN TO THE AIRPORT. THRU TROUBLESHOOTING BY MAINTENANCE THE LT GENERATOR CONTROL UNIT WAS FOUND AT FAULT. IT WAS REPLACED AND TESTED SEROct 29, 2003 · Beech 1900D · DC Generating SystemSDR 55657Brake · weakCREW REPORTED BRAKES ON RT SIDE FELT SPONGY. MAINT. BLEED BRAKES AND FOUND NO LEAKS. OPS CK NORMALOct 29, 2003 · N133YV · Beech 1900D · Landing Gear Brake SystemSDR GLBA2003139Controller · failedBOTH ENG TEMP LIMITED, CALIBRATED LT TRIM STICK AND REMOVED AND REPLACED RT TRIM STICK.Oct 29, 2003 · N96UX · Beech 1900D · Engine Temperature Indicating SystemSDR 55631Brake · weakAFTER LANDING CAPT REPORTED BRAKES WEAK. MAINTENANCE BLED BRAKES. OPS CK NORMAL. (BLED BRAKES CAPT SIDE AND SERVICED RESERVOIR).Oct 28, 2003 · N133YV · Beech 1900D · Landing Gear Brake SystemSDR AMWA68Rib · cracked6 CRACKS ON THIS RIB. 3 ON LT AND 3 ON RT SIDES AT STRINGER TO RIB INTERSECTION. CRACKS LOCATED AT FIRST RIVET HOLE. LT STRINGER P/N 101-640000-37, 101-640000-39, 101-640000-45. RT STRINGER P/N 101-640000-38,101-640000-46, 101-640000-42Oct 24, 2003 · N174YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA67Rib · cracked3 CRACKS FOUND ON THIS RIB AT STRINGER TO RIB INTERSECTION. 1 AT STRINGER P/N 101-640000-37 FIRST RIVET HOLE ON RIB RT SIDE. 1 LOCATED LT STRINGER 101-640000-39 AND 1 RT STRINGER 101-640000-42. BOTH AT FIRST RIVET HOLE OF RIB.Oct 24, 2003 · N174YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA66Rib · cracked5 CRACKS LOCATED ON THIS RIB. 2LT AND 3 RT LOCATED AT STRINGER TO RIB INTERSECTIONS ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-38, 101-640000-42, 101-640000-46. LT STRINGER P/N 101-640000-39, 101-640000-37Oct 24, 2003 · N174YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR 55495Landing Gear · malfunctionedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. ACFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. GEAR DOWN AND LOCKED. PERFORMED OPERATIONAL CHECK OF LANDING GEAR, OP CHECKED GOOD.Oct 23, 2003 · N3YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 55504Fire Warning · activatedDURING TAXI TO RUNWAY FOR TAKEOFF CREW OBSERVED THE ILLUMINATION OF THE RT ENG FIRE HANDLE. CREW ACCOMPLISHED THE EMERGENCY PROCEDURES FOR ENG FIRE. SECURED THE ENG AND RETURNED TO GATE. REMOVED AND REPLACED NR 2 ENG FIRE BOTTLE/SQUIB P/N 30100023, S/N 2939Oct 23, 2003 · N133YV · Beech 1900D · Fire DetectionSDR CA031020006Pump · leaking(CAN) CREW ARRIVED AT TERMINAL AND UPON SHUTDOWN WERE ALERTED TO FUEL COMING FROM RIGHT COWL. MAINTENANCE FOUND LOW PRESSURE FUEL PUMP HAD BLOWN OUT GASKET BETWEEN MAIN BODY AND THE REGULATOR ASSEMBLY. PUMP WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Oct 20, 2003 · Beech 1900D · Engine Fuel PumpSDR AMWA82Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED ON THE LEFT SIDE NEAR THE FWD STRINGER INTERSECTION. REPAIRED CRACK TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03.Oct 15, 2003 · N23YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR 55265Landing Gear · failedUPON DECENT FOR LANDING IN MCO. GEAR WOULD NOT EXTEND. IT HAD TO BE EMERGENCY EXTENDED (PUMPED DOWN) CREW GOT THREE DOWN AND LOCKED IND AHD SAFETY WITH NO FURTHER INCIDENTS.Oct 15, 2003 · N173YV · Beech 1900D · Main Landing GearSDR AMWA62Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGES AT CANTED STAB 24.973 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE TO BMM P/N 114-590021-9, 51-70-03.Oct 15, 2003 · N26YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA61Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED IN TWO PLACES ON THE RIGHT SIDE BY THE FOWARD AND AFT STRINGER INTERSECTION. REPAIRED CRACKS TO RIB FLANGE ACCORDANCE WITH BMM P/N 114-590021-9, 51Oct 15, 2003 · N23YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA60Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 69.184 WAS FOUND CRACKED IN ONE PLACE ON THE RIGHT SIDE NEAR THE AFT STRINGER INTERSECTION AND TWO CRACKS ON THE LEFT SIDE AT THE FORWARD AND CENTER STRINGS INTERSECTIONS. Oct 15, 2003 · N26YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA59Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE CANTED STAB STA 54.026 WAS FOUND CRACKED IN THREE PLACES ON THE RIGHT SIDE NEAR THE FORWARD, CENTER AND AFT STRINGERS AND TWO PLACES ON THE LEFT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE TOct 15, 2003 · N26YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR 55265AMWALanding Gear · malfunctionedUPON DECENT FOR LANDING IN MCO. GEAR WOULD NOT EXTEND IT HAD TO BE EMERGENCY EXTENDED (PUMPED DOWN). CREW GOT THREE DOWN AND LOCKED INDICATIONS AND LANDING SAFETY WITH NO FURTHER INCIDENTS. P/N 1143640681 S/N506D95 PCB TIME DELAY RELAY.Oct 15, 2003 · N173YV · Beech 1900D · Main Landing GearSDR GLBA2003140Ring · mismanufacturedTORQUE WAS HIGH, REMOVED PROPELLER, INSPECTION FOUND INTERNAL SPACER RING NOT DRILLED AND RESULTED IN A PIN NOT BEING INSTALLED AND SPACER RING BACKED-OFF CAUSING TORQUE ISSUE. LAST OVERHAUL WAS AT HARTZELL TSO 438.0.Oct 14, 2003 · N251GL · Beech 1900D · Propeller AssemblySDR 55177AMWAControl Unit · failedAFTER TAKE OFF CREW TRIED TO RETRACT THE FLAPS. THE FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENTS.Oct 13, 2003 · N133YV · Beech 1900D · Trailing Edge Flap Control SystemSDR AMWA65Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED IN ONE PLACE ON THE RIGHT AND ONE PLACE ON THE LEFT SIDE NEAR THE CENTER STRINGER INTERSECTION. REPAIRED CRACK TO RIB FLANGE IN ACCORDANCE TO BMM POct 10, 2003 · N218YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA64Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 69.184 WAS FOUND CRACKED IN ONE PLACE ON THE RIGHT SIDE NEAR AFT STRINGERS INTERSECTION REPAIRED CRACK TO RIB FLANGE IN ACCORDANCE TO BMM P/N 114-590021-9, 51-70-03.Oct 10, 2003 · N218YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA63Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 54.026 WAS FOUND CRACKED IN THREE PLACES ON THE RIGHT SIDE NEAR THE FORWARD, CENTER AND AFT STRINGERS AND TWO PLACES ON THE LEFT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCOct 10, 2003 · N218YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR 55100AMWABrake · malfunctionedDURING TAXING IN FROM FLT 701 ABQ TO FMN. THE RT BRAKE PEDAL WAS SOFT AND MUSHY DURING THE TAXI. RT BRAKE PEDAL FEELS MUSHY/RT BRAKE IS GRABBING P/N1143880251, APR89-594 WHEEL ASSY MAIN(ABS P/N 5006028).Oct 10, 2003 · N142YV · Beech 1900D · Landing Gear Brake SystemSDR 55097AMWAAltimeter · malfunctionedAFTER TAKE OFF FROM FMN TO ABQ CAPT'S ALTIMETER FLAGGED. AIRCRAFT RETURNED TO FMN WITH NO FURTHER INCIDENTS.Oct 10, 2003 · N131ZV · Beech 1900D · Altimeter, Barometric/EncoderSDR GLBA2003138Governor · out of rigRT ENGINE FUEL FLOW AND PROP TORQUE FLUX, RIGGED RT GOV INTERCONNECT.Oct 10, 2003 · N170GL · Beech 1900D · Turbine GovernorSDR 55039Pitot Tube · defectiveDURING TAKE OFF ROLL FO AIRSPEED INDICATOR FAILED TO RESPOND. TAKE OFF WAS ABORTED AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. REMOVED AND REPLACED FO'S PITOT TUBE AIRSPEED IND P/N1293640797 S/N593D95Oct 8, 2003 · N161YV · Beech 1900D · Pitot/Static SystemSDR 55032Line · looseODOR OF FUMES FROM COCKPIT. TIGHTENED RT ENG P3 SUPPLY LINE B NUT. OPS CK NORMAL. NO FUMES NOTEDOct 7, 2003 · N190YV · Beech 1900D · Aircraft Fuel Distribution SystemSDR 54992Indicator · failedRIGHT TORQUE GAUGE FAILED ON TAKE OFF DURING INITIAL POWER UP. RETURNED TO GATE AND CALLED MX. REPLACED GAUGE OPS CK GOOD P/N 114-3800-653 SN 390MU.Oct 6, 2003 · N126YV · Beech 1900D · Engine BMEP/Torque IndicatingSDR 54987Indicator · fluctuatesON TAKE OFF CREW NOTICED A 4O TO 50 KNT SPLIT BETWEEN THE CPT AND FO AIRSPEED IND. FO READING LOW DREW ABORTED TAKEOFF AND RETURNED TO GATE.Oct 6, 2003 · N242YV · Beech 1900D · Airspeed/Mach IndicatorSDR CA031010001Spar Cap · cracked(CAN) A CRACK WAS FOUND IN THE RT LOWER SPAR CAP HORIZONTAL FLANGE AT STATION 117.0 BL.THE CRACK EXTENDED FROM THE RIVET HOLE AFT TO THE EDGE OF THE FLANGE, AND FORWARD JUST SHY OF THE FLANGE RADIUS (OF THE VERTICAL LEG).THE CRACK WAS NOTICED ON A PREFLIGHT INOct 2, 2003 · Beech 1900D · Wing Spar
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