Beech 1900C

Service difficulty reports · 1,840

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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 = '1900C'
  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 YADA20170216001Flap System · failedFLAPS FAILED TO EXTEND.Feb 16, 2017 · N119AX · Beech 1900C · Trailing Edge Flap Control SystemSDR JIKA2017021401Unknown · smokeIN CRUISE FLIGHT FROM KSMX TO KSBA WHEN HE NOTICED A BURNING SMELL AND SAW A SMALL AMOUNT OF SMOKE COMING FROM BETWEEN THE GLARE SHIELD AND THE INSTRUMENT BEZEL OF THE PILOT’S ATTITUDE INDICATOR. THE PILOT CHECKED ALL INSTRUMENTATION AND NOTED NO DEFECTS. THFeb 14, 2017 · N347AF · Beech 1900C · Air Distribution SystemSDR JIKA2017020401Amplifier · shortedDURING ILS APPROACH THE LEFT RMI WENT INOPERATIVE FOLLOWED BY THE NUMBER TWO HSI TURNING 90 DEGREES AND PILOT SIDE ATTITUDE INDICATOR SHOWING A 15-30 DEGREE ROLL. EXECUTED A MISSED APPROACH AND INFORMED ATC OF THE ISSUE. ATC DIRECTED HIM TO HIS ALTERNATE KSJT.Feb 4, 2017 · N3071A · Beech 1900C · Integrated Flight SystemSDR TIMA20170203002Rib · crackedNUMEROUS CRACKS WERE FOUND IN THE VERTICAL STAB RIBS. THE CRACKS WERE LOCATED IN THE STRINGER TO RIB JUNCTIONS. SIX CRACKS WERE ON THE RIGHT SIDE AND SEVEN ON THE LEFT SIDE OF THE VERTICAL STAB.Feb 3, 2017 · N194GA · Beech 1900C · Vertical Stabilizer, Spar/RibSDR YADA20170202001Stringer · corrodedDURING MAINTENANCE, COLLECTOR TANK INSPECTION. CORROSION WAS FOUND ON STRINGER STATION 305.7.Feb 2, 2017 · N118AX · Beech 1900C · Wing, Longeron/StringerSDR EPUA2017012517001Connector · failedDUAL GPS FAILURE DURING FLIGHT. AIRCRAFT RETURNED TO BASE DUE TO THIS FAILURE AND LANDED WITHOUT INCIDENCE. MAINTENANCE REPLACED THE NR 2 GPS (GNC420)UNIT AS WELL AS BOTH GPS ANTENNA TNC CONNECTORS.Jan 19, 2017 · N815GV · Beech 1900C · Navigation System WiringSDR JIKA201801220001Valve · bypassingTHE PILOT REPORTED THAT ON APPROACH TO KLBB WHEN THE LANDING GEAR WAS SELECTED “GEAR DOWN” THE PILOT DID NOT SEE THREE GREEN LIGHTS ON THE GEAR INDICATOR, THEN ALSO NOTICED THE GEAR CIRCUIT BREAKER HAD POPPED OUT. THE PILOT ATTEMPTED TO RESET THE CIRCUIT BREAKJan 16, 2017 · N112YV · Beech 1900C · Landing Gear Retraction/Extension SystemSDR JIKA2017011601Circuit Breaker · faultedPILOT WAS ON APPROACH AND WHEN THE LANDING GEAR WAS SELECTED TO THE DOWN POSITION. THE LANDING GEAR DID NOT EXTEND AND HAD NO INDICATION. THE PILOT THEN EXECUTED A LOW PASS AT AIRPORT TOWER AND COULD NOT VERIFY LANDING GEAR POSITION. THE PILOT FOLLOWING PROCEDJan 16, 2017 · N575G · Beech 1900C · Landing Gear System WiringSDR YADA20160109001Gusset · crackedDURING MAINTENANCE A,B,C STRUCTURAL INSPECTION, FOUND LT INTERCOSTAL GUSSET CRACKED AT FUSELAGE STATION 107. PART HAS BEEN REMOVED AND REPLACED IAW STRUCTURAL REPAIR MANUAL.Jan 9, 2017 · N113AX · Beech 1900C · Fuselage Miscellaneous StructureSDR YADA20161231001Blower · burnedSMELL OF POSSIBLE ELECTRIC ON CLIMB.Dec 31, 2016 · N119AX · Beech 1900C · Air Distribution FanSDR TIMA20161213019Windshield · crackedTHE PILOT’S SIDE WINDSHIELD CRACKED DURING FLIGHT. THERE WAS A 3 INCH WIDE BAND OF SHATTERING OF THE OUTER LAYER THAT RAN FROM THE TOP TO THE BOTTOM OF THE WINDSHIELD ON THE INBOARD EDGE NEXT TO THE CENTER POST.Dec 13, 2016 · N153GA · Beech 1900C · Flight Compartment WindowsSDR YADA20161130001Windshield · crackedLT WINDSHIELD CRACKED INFLIGHT.Nov 29, 2016 · N113AX · Beech 1900C · Flight Compartment WindowsSDR TIMA20161125017Doubler · crackedDURING A SCHEDULED SIM CHECK, CRACKS WERE DISCOVERED IN THE DOUBLERS OF THE HORIZONTAL STABILIZER FORWARD ATTACHMENT TO THE VERTICAL STABILIZER. TWO, ONE INCH CRACKS WERE FOUND IN THE LT DOUBLER AND ONE, ONE1 INCH CRACK WAS FOUND IN THE RT DOUBLER. BOTH DOUBNov 25, 2016 · N197GA · Beech 1900C · Horizontal Stabilizer StructureSDR YADA20161101001Buss Bar · burnedRIGHT GENERATOR FAILED LIGHT, RIGHT GEN TIE OPEN LIGHT, SECONDARY PROBLEM NR 1 NAV/CO AND TRANSPONDER FAILED WITH NO TRANMITT ON NR 1 COM. FOUND BURNED INSULATION ON RT GEN BUSS BAR AND REPLACED RT STARTER GEN.Nov 1, 2016 · N117AX · Beech 1900C · AC Generator-AlternatorSDR YADA20161029001Ground Wire · disconnectedDURING DEPARTURE, RECIEVED A BATTERY CHARGE LIGHT THAT DID NOT EXTINGUISH. RETURNED TO DEPARTURE. RECONNECTED BATTERY GROUND TERMINAL AND PERFORMED OPS CHECKED OF BATTERY PASSED.Oct 29, 2016 · N113AX · Beech 1900C · Electrical Power System WiringSDR 2016F00213Window · blew outA PORTION OF THE COPILOT SIDE WINDOW DEPARTED THE AIRCRAFT DURING CLIMB AT 15,000 FT. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. UPON INSPECTION, THE AIRFRAME STRUCTURE AND WINDOW FLANGE WERE NOT DAMAGED. THE REMNANTS OF THE EXISTING WINDOW WERE REMOVED, AND AOct 28, 2016 · N124GP · Beech 1900C · Flight Compartment WindowsSDR YADA20161014001Seal · debondedPILOT REPORTED WITH ENG BLEEDS OFF AND VENT ON HIGH, THE ODOR OF BURNING OIL/FUMES FILLED THE COCKPIT. PILOT HAD PREVIOUSLY REPORTED THAT THE AIRCRAFT WOULD NOT PRESSURIZE WITH BLEEDS ON UNLESS TEMPERATURE SWITCH WAS HELD IN INCREASE & COCKPIT WAS EXTREMELY WAOct 14, 2016 · N115AX · Beech 1900C · Emergency ExitsSDR TIMA20160923015Unknown · fumesDURING CLIMB OUT, PILOT DETECTED FUMES COMING FROM THE CARGO AREA. THERE WAS NO VISIBLE SMOKE, ONLY A BURNING ODOR. THE FUMES CONTINUED UNTIL CABIN WAS DEPRESSURIZED. WHEN THE CABIN WAS RE-PRESSURIZED THE FUMES DID NOT RETURN. AIRCRAFT LANDED UNEVENTFULLY.Sep 23, 2016 · N114AX · Beech 1900C · Air Distribution SystemSDR YADA20160917001Downlock Switch · failedNOSE GEAR DOWNLOCK SWITCH FAILED FOR WATER INTRUSION.Sep 17, 2016 · N110AX · Beech 1900C · Landing Gear Position and WarningSDR YADA20160908001Circuit Board · burnedTAIL STROBE CIRCUIT BOARD BURNED.Sep 8, 2016 · N118AX · Beech 1900C · Exterior LightingSDR YADA20160901001Downlock Switch · out of rigRED HANDLE LIGHT ON, MAINS DOWN AND LOCKED NO NOSE GEAR GREEN LIGHT. GEAR WAS MANUALLY PUMPED DOWN TO GET 3 GREEN DOWN AND LOCKED LIGHTS. NOSE GEAR DOWN LOCK SWITCH RERIGGED.Sep 1, 2016 · N110AX · Beech 1900C · Landing Gear Position and WarningSDR YADA20160815001Wire · chafedSMOKE COMING FROM RIGHT WING TIP IN VICINITY OF FUEL VENT, FUEL FOUND ON UNDERSIDE OF WING NEAR HEATED FUEL VENT. MAINTENANCE REPLACED FUEL VENT ON RT WING DUE TO CHAFFING AND SHORTING WIRE ON OLD FUEL VENT.Aug 15, 2016 · N113AX · Beech 1900C · Fuel System WiringSDR TIMA20160810013Skin · corrodedCORROSION WAS FOUND ON THE RIGHT FUSELAGE SKIN ABOVE THE SEAT SIDE SUPPORT RAIL DURING MAINTENANCE.Aug 10, 2016 · N194GA · Beech 1900C · Fuselage Main, Plate/SkinSDR TIMA20160810012Skin · corrodedCORROSION WAS FOUND ON THE RIGHT FUSELAGE SKIN ABOVE THE SEAT SIDE SUPPORT RAIL DURING MAINTENANCE.Aug 10, 2016 · N194GA · Beech 1900C · Fuselage Main, Plate/SkinSDR TIMA20160810011Skin · corrodedFUSELAGE BELLY SKIN, CORROSION WAS FOUND DURING MAINTENANCE.Aug 10, 2016 · N194GA · Beech 1900C · Fuselage Main, Plate/SkinSDR TIMA20160810010Seat Track · corrodedDURING MAINTENANCE, THE RIGHT SIDE SEAT TRACK WAS FOUND TO BE CORRODED.Aug 10, 2016 · N194GA · Beech 1900C · Fuselage, Seat/Cargo Attach FittingsSDR YADA20160809001Rudder Pedal · frozenPILOT REPORT RUDDER PEDALS FROZEN AT ALTITUDE WITH YAW DAMP OFF. MAINTENANCE DISCOVERED AND REMOVED ICE AND WATER UNDER FLOOR BOARDS, CLEANED AND INSPECTED, OPS CHECKED GOOD.Aug 9, 2016 · N115AX · Beech 1900C · Rudder Control SystemSDR EPUA20160728001Stringer · corrodedDURING SCHEDULED INSPECTION OF LEFT AND RIGHT SYSTEM MAIN FUEL TANK WING STATION 124 TO 130 FOR VIA X-RAY INSPECTION, CORROSION PITS WERE NOTED AT WING STATION 126 ON BOTH THE LEFT AND RIGHT WINGS AT STRINGER K. DEFECTS WERE REPAIRED IAW HAWKER BEECHCRAFT FIEJul 28, 2016 · N1553C · Beech 1900C · Wing, Longeron/StringerSDR YADA20160713001Windshield · crackedCOPILOT WINDSHIELD CRACKED IN FLIGHT. MAINTENANCE REPLACED COPILOT WINDSHIELDJul 13, 2016 · N118AX · Beech 1900C · Flight Compartment WindowsSDR EPUA20160709001Stringer · corrodedDURING SCHEDULED INSPECTION OF LEFT AND RIGHT MAIN FUEL TANK WING STATION 124 - 130 VIA X-RAY INSPECTION, X-RAY INSPECTION REVEALED CORROSION ON RIGHT COLLECTOR TANK STRINGER 6-7 INCHES IN FRONT OF RIGHT FUEL PUMP. REPAIRED BY SPLICING STRINGER IAW SRM 57-90Jul 9, 2016 · N15503 · Beech 1900C · Wing, Longeron/StringerSDR YADA20160629001Circuit Breaker · burnedCIRCUIT BREAKER PANEL STARTED SMOKING AFTER LANDING. FLIGHT CREW SHUTDOWN ACFT AND EVACUATED SAFELY. MAINTENANCE LOCATED AND REPLACED OVERHEATED 5 AMP CIRCUIT BREAKER FOR ENGINE INSTRUMENT LIGHTING.Jun 27, 2016 · N111AX · Beech 1900C · Flight Compartment LightingSDR YADA20160611001Unknown · odorWITH LT BLEED AIR OPEN EXHAUST ODOR IN CABIN, MAINTENANCE COULD NOT DUPLICATE ON GROUND RUNS. ACFT GOING INTO CAMP INSPECTION.Jun 11, 2016 · N113AX · Beech 1900C · Air Distribution SystemSDR TIMA20160510009Powerpack · weakWHEN LANDING GEAR WAS LOWERED FOR LANDING THE TIME DELAY FEATURE OPENED THE CIRCUIT. PILOT USED MANUAL GEAR EXTENSION & LANDED UNEVENTFULLY. PROBLEM WAS FOUND TO BE A WEAK HYD POWER PACK.May 10, 2016 · N125BA · Beech 1900C · Hydraulic Pump (Electric/Engine), MainSDR TIMA20160509008Windshield · cracked3 TO 4 MINUTES AFTER LEVEL OFF AT FL230 THE RT WINDSHIELD INNER PLY DEVELOPED MULTIPLE CRACKS. PILOT LANDED AT THE NEAREST SUITABLE AIRFIELD. DESCENT & LANDING WAS UNEVENTFUL.May 9, 2016 · N218SL · Beech 1900C · Flight Compartment WindowsSDR YADA20160504001Skin Panel · debondedPOST LANDING INSPECTION REVEALED THAT THE NR 1 ENG HAD A SEPARATION OF PN 114-980077-17 SKIN FROM THE PN 114-980077-5 BOND ASSEMBLY & WAS NO LONGER ATTACHED TO THE ACFT. MX VERIFIED THAT ALL BOND ASSEMBLY FASTENERS WERE IN PLACE & THAT THE FAILURE WAS THE BONMay 4, 2016 · N115AX · Beech 1900C · Nacelle/Pylon, Plate/SkinSDR JIKA2016050301Bleed Valve · stickingTHE TRAINING CAPTAIN REPORTED WHILE PERFORMING TRAINING STALL MANEUVERS, THE FIRST OFFICER REDUCED POWER, A MOMENTARY COMPRESSOR STALL OCCURRED, BETWEEN 500 - 1000 FT & LBS TORQUE ON THE LT ENG. TRAINING CAPTAIN REDUCED POWER, THIS RESULTED IN ANOTHER STALL. May 3, 2016 · N338AF · Beech 1900C · Compressor Bleed ValveSDR YADA20160501001Motor · burned outBURNING/SMOKE ODOR COMING FROM FRESH AIR VENTS WHEN BLOWER MOTOR ON. MAINTENANCE REPLACED AFT VENT BLOWER DUE BAD MOTOR.May 1, 2016 · N117AX · Beech 1900C · Air Distribution FanSDR YADA20160428001Rib · corrodedCORROSION FOUND BY X-RAY INSPECTION ON LOWER FLANGE LT ENG RIB PN 118-110050-5, ADJACENT TO FWD SPAR LOWER CAP. BLENDED & TREATED AREA.Apr 28, 2016 · N118AX · Beech 1900C · Wing, Rib/BulkheadSDR EPUA20160428001Reinforcement · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED IN THE 101-430142-63 LOWER CLOSURE REINFORCEMENT, WHICH IS A PART OF KIT NR 114-4023-3, THAT WAS PREVIOUSLY USED TO REPAIR A CRACK IN THE AIRSTAIR DOOR BOND ASSEMBLY LOWER CLOSURE. THE DEFECTS FOUND REQUIRApr 28, 2016 · N404GV · Beech 1900C · Passenger/Crew DoorsSDR YADA20160422001Printed Ckt Board · failedIN FLIGHT, AFTER LG HAD BEEN RETRACTED & STOWED, THE LG RELAY CB POPPED. THE LG HANDLE WAS SELECTED DOWN & CB PUSHED IN, CB POPPED AGAIN. MANUAL GEAR EXTENSION WAS THEN ACHIEVED. FOUND THE LG PUMP MOTOR BURNED. THE MOTOR WAS REPLACED AS WELL AS THE SUSPECTApr 22, 2016 · N115AX · Beech 1900C · Landing Gear Retraction/Extension SystemSDR JIKA2016033001Squat Switch · shortedDURING CLIMB OUT, THE PILOT REPORTED THAT DURING THE LG RETRACTION THE RED IN TRANSIT LIGHT REMAINED ILLUMINATED & THE LG WOULD NOT FULLY RETRACT. THE PILOT ATTEMPTED TO EXTEND THE LG & THE LG WOULD NOT EXTEND NORMALLY. THE PILOT EXTENDED THE LG USING THE EMMar 29, 2016 · N346AF · Beech 1900C · Landing Gear Position and WarningSDR TIMA20160326006Bearing · failedPILOT EXPERIENCED AN UNCOMMANDED AILERON INPUT WHEN FLAPS WERE LOWERED FROM TAKEOFF TO APPROACH POSITION, DURING APPROACH. PILOT RETRACTED THE FLAPS TO TAKEOFF POSITION & THE INTERFERENCE WITH THE AILERON WAS ELIMINATED. ACFT WAS LANDED UNEVENTFULLY WITH FLAMar 26, 2016 · N127BA · Beech 1900C · Trailing Edge FlapsSDR YADA20160312001Knob · brokenPILOT ALTIMETER ALTITUDE SELECTOR KNOB BROKEN, CAN'T SELECT ALTITUDE, BARO, IN COLLSMAN WINDOW. RETURNED TO DEPARTURE AIRPORT. REPLACED ALTIMETER.Mar 12, 2016 · N117AX · Beech 1900C · Altimeter, Barometric/EncoderSDR YADA20160308001Frame · corrodedDURING STRUCTURAL INSPECTION, CORROSION WAS FOUND ON TOP FLANGE OF FUSELAGE FRAME AT FS 468.25. SUSPECT CORROSION WAS CAUSED BY CARGO SPILLAGE. FRAME WAS REPAIRED IAW SRM.Mar 8, 2016 · N113AX · Beech 1900C · Fuselage Main, FrameSDR TIMA20160305005Sensor · intermittentWHEN GEAR WERE LOWERED FOR LANDING, DID NOT HAVE 3 GREEN GEAR LIGHTS. PILOT TRIED PRESS TO TEST OF BULBS & TURNED DIMMING OFF TO NO AVAIL. PILOT TERMINATED APPROACH & GOT VISUAL CONFIRMATION FROM TOWER THAT GEAR WAS DOWN. PILOT EVENTUALLY SAW ALL 3 GEAR LIGMar 5, 2016 · N133BA · Beech 1900C · Landing Gear Position and WarningSDR CA160216023Motor · failed(CAN) FLIGHT CREW REPORTED ELECTRICAL SMOKE ODOR IN FLIGHT DECK. FLAP MOTOR FOUND U/S AND CIRCUIT BREAKER TRIPPED.Feb 11, 2016 · Beech 1900C · Trailing Edge Flap ActuatorSDR YADA2016FA0000077Flap System · failedFLAPS WOULD NOT RETRACT FROM TAKEOFF TO UP. RETURNED TO DEPARTURE AIRPORT. UNEVENTFUL LANDING MADE FLAPS WORKED ON GROUND AFTER LANDING - MAINTENANCE VERIFIED FLAPS UP AND SECURE - DEFERRED. MAINTENANCE REPLACED FLAP MOTOR RELAY AFTER THE NEXT FLIGHT AND PROBFeb 8, 2016 · N117AX · Beech 1900C · Trailing Edge Flap Control SystemSDR JIKA2016013103Fire Loop · defectiveAFTER TAKEOFF, DURING CLIMB, THE PILOT REPORTED THAT THE RT ENG FIRE WARNING LIGHT ILLUMINATED. THE PILOT SHUTDOWN THE RT ENG & EXTINGUISHED THE RT ENG FIRE BOTTLE. THE PILOT DECLARED AN EMER & LANDED WITHOUT INCIDENT. FOUND THE RT ENG FIRE DETECTION LOOP HJan 28, 2016 · N331AF · Beech 1900C · Fire DetectionSDR JIKA2016010802Check Valve · malfunctionedDURING CRUISE FLIGHT, THE PILOT NOTICED A STRONG ODOR THAT SMELLED LIKE JET FUEL, FOLLOWED BY A SMALL PUFF OF SMOKE FROM THE LT AIR VENT. THE PILOT DESCENDED BELOW 12,000 FT & PERFORMED CABIN PRESS DUMP. THE PILOT ADVISED ATC OF CONDITION, RETURNED & LANDED Jan 8, 2016 · N31702 · Beech 1900C · Heating SystemSDR TIMA20160108001Pressure Switch · faultyIMMEDIATELY AFTER ROTATION THE LT PROPELLER AUTO FEATHERED. PILOT REDUCED POWER & IMMEDIATELY LANDED, ABORTING THE TAKEOFF. THE PROBLEM WAS DISCOVERED TO BE A FAULTY AUTO FEATHER LOW PRESS SWITCH.Jan 8, 2016 · N127BA · Beech 1900C · Propeller Feathering/Reversing
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