Beech 1900C

Service difficulty reports · 1,841

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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 GUU2001F00019Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE BRACKET. NOTE: TIME SINCE LAST INSPECTION: 180.1Jul 6, 2001 · N150GA · Beech 1900C · Elevator StructureSDR GUU2001F00022Fire Loop · shortedDURING TAXI, LEFT T-HANDLE ILLUMINATED THEN EXTINGUISHED TWICE. CORRECTIVE ACTION: REMOVED AND REPLACED FORWARD FIRE LOOP. OPERATIONAL CHECK NORMAL.Jun 30, 2001 · N143GA · Beech 1900C · Fire DetectionSDR GUU2001F00021Fire Loop · looseDURING TAXI, LEFT FIRE LIGHT HANDLE ILLUMINATED. ENGINE WAS SHUT DOWN AND EMERGENCY CHECKLIST ACCOMPLISHED. CORRECTIVE ACTION: INSPECTED FORWARD AND AFT FIRE LOOPS. SECURED FORWARD FIRE LOOP. PERFORMED ENGINE RUNS. NO DEFECTS NOTED. OPERATIONAL CHECK NOJun 29, 2001 · N143GA · Beech 1900C · Fire DetectionSDR GUU2001F00020Actuator · failedAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. TROUBLESHOT SYSTEM, FOUND RIGHT MAIN LANDING GEAR ACTUATOR BYPASSING INTERNALLY. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPERATIONAL CHECK NORMALJun 28, 2001 · N151GA · Beech 1900C · Landing Gear ActuatorSDR NSVA0104Cable · brokenBOSTON, CREW WAS UNABLE TO OPEN THE FORWARD CABIN DOOR. AIRCRAFT WAS RELEASED UNDER SPECIAL FLIGHT PERMIT TO HYA FOR REPAIRS. MAINTENANCE REPLACED AIRSTAIR DOOR CABLE, OPERATIONAL CHECK WAS SATISFACTORY.Jun 23, 2001 · N119CJ · Beech 1900C · Passenger/Crew DoorsSDR YAD2001F00007Diaphragm · leakingPILOT FOUND FUEL LEAKING OUT OF NR 1 ENGINE DRAIN MANIFOLD. THIS AC IS IN COMPLIANCE WITH SB 71-3307 THAT INCORPORATED A DRAIN LINE FROM THE LOW PRESS FUEL PUMP TO THE DRAIN MANIFOLD. DETERMINED THAT DIAPHRAGM IN THE PUMP HAD FAILED AND ALLOWED FUEL TO DRAINJun 18, 2001 · N1566C · Beech 1900C · Fuel Boost PumpSDR YAD2001F00006Diaphragm · damagedPILOT FOUND FUEL LEAKING OUT OF NR 1 ENGINE DRAIN MANIFOLD. DETERMINED THAT THE DIAPHRAGM IN THE PUMP HAD FAILED AND ALLOWED FUEL TO DRAIN OUT OF THE DRAIN MANIFOLD. DUE TO THE COMMON FAILURE OF THE FUEL PUMP DIAPHRAGM (AND ASSOCIATED FUEL VENTING-SB71-3307)Jun 18, 2001 · N1566C · Beech 1900C · Fuel Boost PumpSDR 2001F00243Diaphragm · rupturedPOST RAYTHEON AIRCRAFT SERVICE BULLETIN 71-3307, ENGINE DRIVEN LOW PRESSURE FUEL PUMP DRAIN MOD. EXPERIENCED A FAILURE OF THE LOW PSI ENGINE DRIVEN FUEL PUMP ON THE NR 1 ENGINE. THE RESULT OF THE DIAPHRAGM RUPTURE WAS TO HAVE FUEL VENTED OUT OF THE NACELLE TJun 14, 2001 · N1566C · Beech 1900C · Engine Fuel PumpSDR AUS20010613Spring · broken(AUS) LH PROPELLER PITCH CONTROL LEVER FEATHER DETENT FEEL SPRING BROKEN.Jun 12, 2001 · Beech 1900C · Propeller Controlling SystemSDR CA010622004Garlock Seal · failed(CAN) LT ENGINE LOST OIL PRESSURE DURING CLIMB OUT OF AFTER APPROX. 20 MINUTES. PILOT SECURED ENGINE WHEN OIL PRESSURE WAS IN YELLOW ARC OF OIL GAUGE. AIRCRAFT LANDED UNEVENTUALLY ATER RETURNING TO YUR. MAINTENANCE FOUND THAT MOST OF THE OIL HAD BEEN EJECTED OMay 31, 2001 · Beech 1900C · Turbine Engine Oil SystemSDR 2001F00090Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET. (M)May 25, 2001 · N1568W · Beech 1900C · Horizontal Stabilizer StructureSDR 2001F00010Switch · shortedFLT 9396 - MIA/EYW - AFTER DEPARTURE FROM MIAMI, STRONG ELECTRICAL SMELL OBSERVED. FOUND LEFT LANDING LIGHT SWITCH SHORTED. REMOVED AND REPLACED SWITCH AND SECURED WIRE AT LEFT LANDING LIGHT. OPS CHECK NORMAL. (M)May 22, 2001 · N130GA · Beech 1900C · Exterior LightingSDR 20010613CW015B-Nut · looseOIL LINE TO THE TORQUE MANIFOLD B-NUT CAME LOOSE. OIL PRESSURE FLUCTUATED AND ENGINE SHUT DOWN. AIRCRAFT LANDED. ENGINE WAS INSPECTED AS PER PWA MM. LOW OIL PRESSURE PROCEDURE, NO DAMAGE FOUND. OIL SERVICED AND ENGINE TEST RUN, PER PWA CHECK.May 22, 2001 · N172GA · Beech 1900C · Engine Oil Distribution (Airframe Furnished)SDR GUU2001F00015Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M)May 9, 2001 · N143GA · Beech 1900C · Elevator StructureSDR GUU2001F00017Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE BRACKET. (M)May 2, 2001 · N147GA · Beech 1900C · Elevator StructureSDR GUU2001F00016Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET. (M)May 2, 2001 · N147GA · Beech 1900C · Elevator StructureSDR GUU2001F00014Link · out of rigFLT 9122 - NAS/FLL - DURING FLIGHT AT 2000 FEET WITH LEFT ENGINE TORQUE SET TO 2000 FT/LBS AND PROPELLER SET TO 1500 RPM, PROPELLER SURGED TO 1750 RPM AND TOQUE FELL TO 1500 FT/LBS. RIGGED LOST MOTION LINK ON LEFT ENGINE. OPERATIONAL CHECK NORMAL. (M)Apr 28, 2001 · N139GA · Beech 1900C · Engine ControlsSDR CA010503011Fuel Cell · leaking(CAN) A/C DEPARTED SMITHERS, BC ENROUTE TO VANCOUVER. AT APPROX 15 MIN. OUT A PASSENGER NOTED TO CREW THAT RT WING HAD A SMALL LEAK OF FUEL COMING FROM A RIVET HEAD JUST O/B OF ENGINE NACELLE. THE CREW HAD NO IND.S OUT OF ORDINARY BUT AFTER CONFERRING WITH MAApr 27, 2001 · Beech 1900C · Fuel StorageSDR GUU2001F00010Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M)Apr 24, 2001 · N199GA · Beech 1900C · Elevator StructureSDR GUU2001F00009Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, LEFT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR CENTER HINGE BRACKET. (M)Apr 24, 2001 · N199GA · Beech 1900C · Elevator StructureSDR GUU2001F00011Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE BRACKET. (M)Apr 23, 2001 · N38011 · Beech 1900C · Elevator StructureSDR GUU2001F00004Valve · out of adjFLT 2050 - FLL - DURING FLIGHT, LEFT PROPELLER GOES TO GROUND FINE WITH POWER AT FLIGHT IDLE. ADJUSTED LEFT PROPELLER BETA VALVE. (M)Apr 23, 2001 · N138GA · Beech 1900C · Propeller Controlling SystemSDR GUU2001F00003Squat Switch · out of adjFLT 9230 - NAS/FLL - DURING FLIGHT, LEFT PROPELLER GOES INTO GROUND FINE PRIOR TO LANDING WITH POWER STILL ON LEFT ENGINE. RIGGED AND ADJUSTED RIGHT SQUAT SWITCH. (M)Apr 22, 2001 · N147GA · Beech 1900C · Landing Gear Position and WarningSDR 20010524SG009Linkage · looseFLT 9437 - MCO - AFTER TAKEOFF, RIGHT PROPELLER RPM FLUCTUATED BETWEEN 200 AND 1200 AND TORQUE WENT TO 5000 LBS. DETERMINED RIGHT PROPELLER LOW PITCH CONTROL LINKAGE TO BE SAFETIED BUT LOOSE. RIGGED PROPELLER LOW PITCH CONTROL LINKAGE TO BE SAFETIED BUT LOOSApr 22, 2001 · N1568W · Beech 1900C · Propeller Controlling SystemSDR 20010524SG002Warning System · malfunctionedFLT 9401 - JAX-TPA - DURING FLIGHT, FIRE DISCHARGE LIGHT ILLUMINATED. SECURED CANNON PLUG AT LEFT DISCHARGE LIGHT ASSEMBLY. (M)Apr 20, 2001 · N151GA · Beech 1900C · Central WarningSDR 20010524SG010Linkage · out of rigFLT 9411 - MCO/MIA - ON TAKEOFF AT V1 SPEED ROTATION, NR 2 ENGINE LOST POWER. RERIGGED RIGHT ENGINE LOW PITCH CONTROL SYSTEM. (M)Apr 19, 2001 · N1568W · Beech 1900C · Propeller Controlling SystemSDR 20010524SG007Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE BRACKET. (M)Apr 16, 2001 · N1568W · Beech 1900C · Elevator StructureSDR 20010524SG006Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M)Apr 16, 2001 · N1568W · Beech 1900C · Elevator StructureSDR CA010522022Valve · leaking(CAN) P3 AIR LEAKING THROUGH PRE COOLER VALVE (BYPASS) CAUSED INABILITY TO PRESSURE CABIN ON LT SIDE.Apr 12, 2001 · Beech 1900C · Cabin Temperature Control SystemSDR GUU2001F00006Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M)Apr 10, 2001 · N141UE · Beech 1900C · Elevator StructureSDR GUU2001F00005Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR OUTBOARD HINGE BRACKET. (M)Apr 10, 2001 · N141UE · Beech 1900C · Elevator StructureSDR 20010524SG005Spar Cap · corrodedAT SCHEDULED EMPENNAGE INSPECTION, DISCOVERED SOME EXFOLIATION CORROSION .5 INCH BY .125 INCH BY .020 INCH, ON LEFT HORIZONTAL STABILIZER LOWER SPAR CAP ANGLE SIXTEEN INCHES FROM AIRCRAFT CENTERLINE. REMOVED CORRODED MATERIAL AND RE-PROTECTED EXPOSED MATERIALApr 10, 2001 · N187GA · Beech 1900C · Horizontal Stabilizer, Spar/RibSDR 20010524SG004Bracket · corrodedDURING ROUTINE MAINTENANCE, FOUND RIGHT CENTER ELEVATOR HINGE ATTACH BRACKET CORRODED. REMOVED AND REPLACED CENTER ELEVATOR HINGE ATTACH BRACKET. (M)Apr 10, 2001 · N187GA · Beech 1900C · Elevator StructureSDR 20010524SG003Hinge Bracket · corrodedDURING SCHEDULED MAINTENANCE, LEFT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED LEFT OUTBOARD ELEVATOR HINGE BRACKET. (M)Apr 9, 2001 · N187GA · Beech 1900C · Elevator StructureSDR CA010515014Engine · failed(CAN) ENGINE SPOOL DOWN NOTED TO BE VERY SHORT HIGH RESISTANCE TO TURNING REDUCTION GEAR BOX THROUGH PROP BLADES AND INTERNAL RUBBING DETECTED INDICATING INTERNAL PROBLEMS. - CAUSE TO BE DETERMINED UPON ENGINE TEAR DOWN. - ENGINE WAS INVOLVED IN A PROP STRIKE Apr 4, 2001 · Beech 1900C · Engine/Transmission CouplingSDR 20010507CW017Trim Tab · corrodedRUDDER TAB HORN, CORRODEDApr 4, 2001 · N195GA · Beech 1900C · Rudder Tab Control SystemSDR 20010507CW013Cap · corrodedLOWER CAP LEFT STABILIZER OUTER 6 IS CORRODED.Apr 4, 2001 · N172GA · Beech 1900C · Horizontal Stabilizer StructureSDR 20010507CW012Trim Tab · corrodedELEVATOR TRIM TAB HORN CORRODEDApr 4, 2001 · N195GA · Beech 1900C · Elevator Tab Control SystemSDR 20010507CW011Trim Tab · corrodedLEFT AILERON TRIM TAB HORN CORRODED.Apr 4, 2001 · N172GA · Beech 1900C · Aileron Tab Control SystemSDR 20010509CW006Spar Cap · corrodedFOUND THE OUTBOARD 6 INCHES LOWER RIGHT REAR SPAR CAP EXTRUSION CORRODED. CORROSION WAS FOUND WHILE REPLACING A CORRODED OUTBOARD ELEVATOR HINGE BRACKET.Apr 2, 2001 · N172GA · Beech 1900C · Horizontal Stabilizer, Spar/RibSDR 20010509CW005Intercostal · crackedP43 INSPECTION FOUND A .8 INCH CRACK IN THE OUTDBOARD FLANGE RADIUS OF THE INTERCOSTAL AT THE UPPER CARGO DOOR FRAME AT FS 494.Apr 2, 2001 · N172GA · Beech 1900C · Fuselage Miscellaneous StructureSDR 20010509CW004Hinge Bracket · corrodedDURING INSPECTION, THE RIGHT OUTBOARD AND THE RIGHT MIDDLE ELEVATOR HINGE BRACKET WERE FOUND TO BE CORRODED.Apr 2, 2001 · N172GA · Beech 1900C · Elevator StructureSDR 20010425CW005Spring · crackedDURING DISASSEMBLY AND VISUAL INSPECTION, SPRING WAS FOUND CRACKED IN HALF, IAW AIRCREW, NO DISCREPANCY WAS NOTED DURING INCOMING FLIGHT. PROPELLER HUB REPLACED, SPRING REPLACED, PROPELLER REASSEMBLED AND INSTALLED ON THE AIRCRAFT WITH NO DISCREPANCIES NOTED.Mar 27, 2001 · N125BA · Beech 1900C · Propeller AssemblySDR GUU2001F00001Wire · looseFLT 9432 - NAS/MIA - DURING APPROACH, LANDING GEAR CIRCUIT BREAKER POPPED. UNABLE TO POWER LANDING GEAR. AFTER RESETTING CIRCUIT BREAKER LANDING GEAR CAME DOWN, BUT NO GREEN INDICATOR UNTIL AFTER GEAR RECYCLED. SECURED LINE GOING TO BLEED VALVE. ALSO SECURMar 26, 2001 · N150GA · Beech 1900C · Landing Gear System WiringSDR GUU2001F00002Static Wick · defectiveFLT 9253 - FLL/FPO - PASSENGER REPORTED SPARKS COMING FROM TOP OF RIGHT WING OUTBOARD OF ENGINE NEXT TO INSPECTION PLATE. REMOVED AND REPLACED BAD STATIC WICKS. ALSO, REMOVED AND REPLACED NR 2 INVERTER. (M)Mar 24, 2001 · N139GA · Beech 1900C · Static Discharge SystemSDR NSVA01034Hinge · crackedCREW REPORTED AIRSTAIR DOOR WAS DIFFICULT TO OPEN FROM THE INSIDE. MAINTENANCE ADJUSTED MAIN CABIN DOOR LATCH AND LUBRICATED CAMS AS REQUIRED. UPON FURTHER INVESTIGATION MAINTENANCE DISCOVERED THE AIRSTAIR DOOR SEAL RETAINER TRACK RIVETS WERE SHEARED AND CRAMar 23, 2001 · N550CJ · Beech 1900C · Entrance StairsSDR 20010601CW003Stop Pin · loosePIN TO ARM WELD JOINT FAILED AND ALLOWED PIN TO MOVE/FALL OUT OF ARM (STOP PIN REPLACED BY FLEET SUPPORT SERVICES AT PREVIOUS REPAIR). WITH PIN OUT OF LOCATION, POWER LEVER REVERSE WHILE IN FLIGHT. THIS HAS BEEN A CONTINUING PROBLEM WITH FLEET REPAIRED UNITSMar 20, 2001 · N41UE · Beech 1900C · Power LeverSDR AU010253Altimeter · failed(AUS) ALTIMETER INTERNAL FAILURE.Mar 19, 2001 · Beech 1900C · Altimeter, Barometric/EncoderSDR 20010426AP003Bleed Valve · failedFLT 9363 - FLL/EYW - EN ROUTE TO EYW, SHUTDOWN RIGHT ENGINE DUE TO BAD SURGING OF ENGINE, PLUS/MINUS 700 LBS OF TORQUE. TROUBLESHOT RIGHT ENGINE AND FOUND BLEED VALVE CLOSING EARLY. RECLASSED BLEED VALVE. PERFORMED ENGINE RUNS. OPS CHECK NORMAL. NO EVIDENMar 18, 2001 · N152GA · Beech 1900C · Compressor Bleed ValveSDR CA010322007Compressor · failed(CAN) DURING ROUTINE 5TH DETAILED CHECK THE FOLLOWING ITEMS WERE FOUND DEFECTIVE ON THE VAPOR CYCLE COMPRESSOR. QUILL SHAFT, TEETH STRIPPED P/N 115-555025-9PULLEY DRIVE, TEETH STRIPPEDP/N 114-555065-1OUTER PULLEY DRIVE BEARING P/N 206SZZC STIFF & ROUGH TO TURMar 14, 2001 · Beech 1900C · Cabin Compressor System
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