Beech 1900C

Service difficulty reports · 1,841

Newest first. General aviation reporting is voluntary.

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 95ZZZM589Truss · crackedDURING A INSPECTION OF AREA 'A' ON THE RIGHT ENGINE TRUSS A .5 INCH CRACK. REPAIRED BY WELDING CRACK. (M)Aug 19, 1995 · N137YV · Beech 1900C · Engine Mount SectionSDR 95ZZZM482Vsi · failedDUL - THE CREW ELECTED AN AIR TURNBACK AFTER THE NR 2 VSI FAILED. FOLLOWING AN UNEVENTFUL LANDING, MAINTENANCE REPLACED THE UNIT WHICH TESTED SATISFACTORILY.Aug 16, 1995 · N159GL · Beech 1900C · Rate of Climb IndicatorSDR 95ZZZM483Truss · crackedESC - DURING THE ROUTINE TRUSS INSPECTION REQUIRED BY AD95-02-18, A .75 INCH CRACK WAS FOUND NEAR THE LINSEED OIL PLUG OF THE INBOARD AREA 'A' OF THE RIGHT TRUSS. THE TRUSS WAS REPAIRED IAW BEECH KIT 129-9006, REPAIR NR 2.Aug 15, 1995 · N45GL · Beech 1900C · Engine Mount SectionSDR 95ZZZM593Rib · crackedDURING ROUTINE MAINTENANCE, A CRACK WAS FOUND FOURTH RIB INBOARD 1.5 INCHES UP FROM TRAILING EDGE. REPAIRED WITH PATCH.Aug 13, 1995 · N158YV · Beech 1900C · Trailing Edge FlapsSDR PLGA812951GDiode · failedLGA - FLT NR 4654 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO LGA LANDING WITHOUT INCIDENT. THE AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR FERRY FLIGHT TO ALB MAINTENANCE BASE FOR REPAIRS. ALB MAINTENANCE REMOVED AND REPLACED TWAug 12, 1995 · N15503 · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 95ZZZX4500Oil Press Trans · failedON CLIMB CHECK, RT OIL PRESSURE FLUCTUATING BETWEEN 30-50 PSI. SUBSEQUENTLY, WENT TO OPSI WITHOUT ILLUMINATION OF OIL PRESSURE LIGHT. GPX MAINTENANCE REPLACED TRANSDUCER, GROUND RUN CHECKED GOOD. RETURNED AIRCRAFT TO SERVICE.Aug 12, 1995 · N318BH · Beech 1900C · Engine Oil PressureSDR 95ZZZM479Flap · crackedDURING ROUTINE MAINTENANCE, A .5 INCH CRACK WAS FOUND INBOARD OF ATTACH POINT. REPAIRED WITH PATCH. (M)Aug 12, 1995 · N137YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZM477Bracket · crackedDURING AREA 'A' INSPECTION, LEFT INBOARD TOP FORWARD COWL ATTACH BRACKET WAS FOUND TO HAVE A SMALL CRACK. WELDED CRACK AND RETURNED TO SERVICE.Aug 12, 1995 · N119YV · Beech 1900C · Nacelle/Pylon StructureSDR 95ZZZM476Bracket · crackedDURING THE AND INSPECTION, FOUND CRACK IN THE TOP FORWARD TOP OUTBOARD COWLING ATTACH BRACKET. WELDED CRACK AND RETURNED TO SERVICE. (M)Aug 12, 1995 · N119YV · Beech 1900C · Nacelle/Pylon StructureSDR 95ZZZM484Wire · brokenGRI - THE CREW ELECTED AN AIR TURNBACK AFTER NOTING THAT THE LEFT OIL PRESSURE GAUGE FLUCTUATED BETWEEN 60-90 PSI IN CRUISE. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE SOLDERED BROKEN WIRES ON A CANNON PLUG AT THE PRESSURE TRANSDUCER. SYSTEM WAS OPAug 9, 1995 · N123UE · Beech 1900C · Engine Oil System WiringSDR 95ZZZM487Truss · crackedSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE OUTER LEFT ENGINE TRUSS CRACKED AT UPPER WELD ON COWL ATTACH BRACKET ON TUBE, APPROXIMATELY .5 INCH LONG ON OUTER AND .125 INCH LONG ON INNER. BOTH CRACKS WERE REPAIRED IAW BEECH KIT NR 129-9006.Aug 8, 1995 · N101UE · Beech 1900C · Engine Mount SectionSDR 95ZZZM485Engine · oil leakORD - ON FINAL APPROACH, THE CREW NOTED FAINT SMOKE WAS ENTERING THE CABIN. AFTER AN UNEVENTFUL LANDING, MAINTENANCE DETERMINED THAT THE LEFT ENGINE HAD AN INTERNAL OIL LEAK. THE ENGINE WAS REPLACED AND TESTED SATISFACTORILY.Aug 8, 1995 · N79GL · Beech 1900C · Engine (Turbine/Turboprop)SDR 95ZZZX4499Fuel Control · out of adjustGSO - FLT 2135 - APPROACH INTO COLUMBUS FROM GSO, EXPERIENCED DIRECTIONAL CONTROL PROBLEMS. GO-AROUND WAS INITIATED ON NEXT APPROACH, SAME DIFFICULTIES. GO-AROUND INITIATED, EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. RE-RIGGED LOW PITCH STOP ANDAug 6, 1995 · N317BH · Beech 1900C · Fuel Controlling SystemSDR 95ZZZM478Flap · crackedDURING ROUTINE MAINTENANCE, A CRACK WAS FOUND 10 INCH FROM O/B EDGE 3.5 INCH FROM TRAILING EDGE. REPAIRED WITH PATCH 4 INCH BY 5 INCH. (M)Aug 2, 1995 · N160AM · Beech 1900C · Trailing Edge FlapsSDR 95ZZZM486Nozzle Gasket · leakingDEN - THE CREW ELECTED AN AIR TURNBACK WHEN THE LEFT ENGINE LOST POWER IN FLIGHT AND TORQUE DROPPED TO 1000 AT FULL POWER. MAINTENANCE FOUND SEVERAL FUEL NOZZLE GASKETS (MS937116) LEAKING. ALL FUEL NOZZLES AND GASKETS WERE CHANGED AND LEAKED CHECKED GOOD. AJul 31, 1995 · N84GL · Beech 1900C · Fuel Injector NozzleSDR 95ZZZM488Uplock Switch · defectiveFOD - THE CREW ELECTED TO DIVERT TO SPW AFTER THEY COULD NOT GET A GEAR SAFE LIGHT INDICATION ON APPROACH TO FOD. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE INSTALLED A NEW UPLOCK SWITCH AND CYCLED THE GEAR. ALL INDICATIONS WERE SATISFACTORY.Jul 29, 1995 · N55594 · Beech 1900C · Landing Gear Position and WarningSDR 95ZZZM489Receiver/Trans · intermittentDVL - THE CREW ELECTED AN AIR TURNBACK AFTER THE WEATHER RADAR PICTURE SHRUNK AND THE HORIZONTAL WAS INTERMITTENT. AN UNEVENTFUL LANDING WAS ACCOMPLISHED FOLLOWED BY THE REPLACEMENT OF THE RADAR R/T.Jul 27, 1995 · N45GL · Beech 1900C · Weather Radar SystemSDR 95ZZZX4046Fire Loop · brokenFLT 5626 - ON CLIMB-OUT, THE RIGHT FIRE WARNING ILLUMINATED, PULLED FIRE T-HANDLE AND LIGHT EXTINGUISHED. RETURNED TO FIELD ON LEFT ENGINE. MAINTENANCE FOUND AFT FIRE LOOP BROKEN, REPLACED LOOP, OPS CHECKED NORMAL.Jul 25, 1995 · N163AM · Beech 1900C · Fire DetectionSDR 95ZZZM490Truss · crackedESC - DURING INSPECTION OF AREA 'A' AS REQUIRED BY AD 95-02-18, THE RIGHT TRUSS WAS FOUND CRACKED. THE .5 INCH CRACK WAS CENTERED AT THE OIL PLUG ON THE UPPER LEFT FORWARD LEG. A WELD REPAIR WAS ACCOMPLISHED IAW BEECH REPAIR KIT NR 129-9006-1 REPAIR NR 2.Jul 24, 1995 · N166GL · Beech 1900C · Engine Mount SectionSDR 95ZZZM492Motor · failedGRI - THE CREW ELECTED AN AIR TURNBACK AFTER REPEATED LANDING GEAR RELAY CIRCUIT BREAKER FAILURES. THE GEAR WAS EXTENDED MANUALLY FOLLOWED BY AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE LANDING GEAR MOTOR (P/N 571203 S/N 1060A) AND PRESSURE SWITCH (P/N 5Jul 19, 1995 · N67UE · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 95ZZZM491Wire · brokenDEN - THE CREW ELECTED AN AIR TURNBACK AFTER THE LANDING GEAR RELAY BREAKER POPPED. THE GEAR WAS EXTENDED MANUALLY FOLLOWED BY AN UNEVENTFUL LANDING. MAINTENANCE REPAIRED BROKEN WIRE AT SQUAT SWITCH. REPLACED SQUAT SWITCH P/N 44EN49-6 AND K-3 RELAY P/N MS24Jul 19, 1995 · N67UE · Beech 1900C · Landing Gear System WiringSDR 95ZZZM461Le Skin · dentedSPW - LEFT OUTBOARD WING LEADING EDGE DAMAGED BY A TRACTOR. THE DAMAGE WAS REMOVED AND A SLUSH DOUBLER INSERT WAS INSTALLED IAW BEECH SRM.Jul 17, 1995 · N55668 · Beech 1900C · Wing, Plate/SkinSDR PLGA716952Keel Web · crackedDURING A WING INSPECTION, THE LEFT ENGINE NACELLE OUTBOARD UPPER KEEL WEB (P/N 114-980022-1) WAS FOUND TO HAVE ONE CRACK ON THE FORWARD FLANGE. THE CRACK RAN VERTICALLY BETWEEN THE FORWARD ATTACHING RIVETS. THE KEEL WEB WAS REPAIRED IAW AERODESIGN ENGINEERINJul 16, 1995 · N808BE · Beech 1900C · Nacelle/Pylon StructureSDR PLGA716951Keel Web · crackedDURING RIGHT ENGINE CHANGE THE NACELLE INBOARD UPPER KEEL WEB (P/N 114-980021-2) WAS FOUND TO BE CRACKED ON THE FORWARD FLANGE. THE CRACK WAS APPROXIMATELY 4 INCHES IN LENGTH RUNNING VERTICALLY BETWEEN THE ATTACHMENT RIVETS ON THE FORWARD FLANGE. THE KEEL WAJul 16, 1995 · N3067X · Beech 1900C · Nacelle/Pylon StructureSDR HERA9514Wire · brokenANC - FLT 1421 - AIR RETURN DUE TO LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. THE AIRCRAFT LANDED ANC WITHOUT INCIDENCE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE LANDING GEAR RELAY CIRCUIT BREAKER. THREE LANDING GEAR RETRACTIONS SHOWED THE SYSTEM TO BE Jul 15, 1995 · N1553C · Beech 1900C · Landing Gear System WiringSDR 95ZZZW805Oil Syst · over servicedMIA-ELH - FLT 465 - SMOKE IN CABIN, AC RETURNED TO MIA WITHOUT FURTHER INCIDENT. DETERMINED RT ENGINE TO BE OVER SERVICED. DRAINED OIL TO PROPER LEVEL. AC WAS TEST FLOWN WITH SATISFACTORY RESULTS AND RELEASED FOR SERVICE.Jul 15, 1995 · N198GA · Beech 1900C · Turbine Engine Oil SystemSDR PLGA71495G1Gcu · malfunctionedFLT 4306 RETURNED TO BOS DUE TO A RIGHT HAND GENERATOR TIE LIGHT FOLLOWED BY ABNORMAL BUSS VOLTAGE PROBLEMS. THE AIRCRAFT RETURNED TO BOS WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE REPLACED THE RIGHT HAND DC POWER PANEL AND BOJul 14, 1995 · N823BE · Beech 1900C · DC Generating SystemSDR 96ZZZX4Nozzle · burned vaneLEFT ENGINE ITT ROSE ABOVE LIMITS MOMENTARILY. WHEN THE ENGINE WAS SEPARATED FROM THE POWER SECTION, DISCOVERED THE CT VANE RING HAD A SECTION COMPLETELY BURNED THROUGH. THE INVESTIGATION IS LOOKING AT THE FUEL NOZZLES AS A POSSIBLE CAUSE. THE FUEL NOZZLES Jul 14, 1995 · N160AM · Beech 1900C · Turbine SectionSDR 95ZZZM255Power Panel · malfunctionedFLT 4306 RETURNED TO BOS DUE TO A RIGHT HAND GENERATOR TIE LIGHT FOLLOWED BY ABNORMAL BUSS VOLTAGE PROBLEMS. THE AIRCRAFT RETURNED TO BOS WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE REPLACED THE RIGHT HAND DC POWER PANEL AND BOJul 14, 1995 · N823BE · Beech 1900C · DC Generating SystemSDR PLGA71395G1Hydraulic Hose · leakingBOS - ON APPROACH THE LANDING GEAR CIRCUIT BREAKER POPPED. THE CREW PUMPED THE GEAR DOWN, LANDING WITHOUT INCIDENT. THE AIRCRAFT WAS INSPECTED BY BOS MAINTENANCE AND FERRIED GEAR DOWN TO ALB. ALB MAINTENANCE REPLACED THE HYDRAULIC PRESSURE HOSE TO THE RIGHTJul 13, 1995 · N818BE · Beech 1900C · Hydraulic System, MainSDR PLGA71095GKeel Web · crackedDURING INSPECTION THE LEFT ENGINE NACELLE OUTBOARD UPPER KEEL WEB (P/N 114-980022-1) WAS FOUND TO HAVE TWO CRACKS ON THE FORWARD FLANGE. BOTH CRACKS RAN VERTICALLY ON THE FLANGE. ONE CRACK WAS BETWEEN THE TWO CENTER ATTACH RIVETS APPROXIMATELY 1 INCH IN LENGJul 10, 1995 · N810BE · Beech 1900C · Nacelle/Pylon StructureSDR 95ZZZX3960Engine · failedAT FL 21,000, SMOKE BEGAN TO FILL THE CABIN. SELECTED RIGHT BLEED-OFF TO CLEAR SMOKE. OBSERVED OIL PRESSURE NR 2 ENGINE DROPPING TO 85 PSI. REDUCED ENGINE POWER TO 1,000 POUNDS TORQUE. OIL PRESSURE CONTINUED TO DROP AND ENGINE WAS SHUT DOWN WHEN OIL PRESSUJul 9, 1995 · N259AF · Beech 1900C · Engine (Turbine/Turboprop)SDR 95ZZZM462Bracket · looseSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE AIRSTAIR DOOR SNUBBER ATTACH BRACKET LOOSE AND THE ATTACH BRACKET WAS REMOVED AND REPLACED WITH BEECH KIT 114-4032-1.Jul 6, 1995 · N167GL · Beech 1900C · Passenger/Crew DoorsSDR 95ZZZM242P3 Line · crackedCOMING OUT OF OMA LEFT ENGINE LOST TORQUE, CREW SHUT DOWN LEFT ENGINE AND RETURNED TO OMA. MAINTENANCE FOUND P3 LINE CRACKED. REPLACED LINE OPS CHECKED NORMAL. (M)Jul 5, 1995 · N80ZR · Beech 1900C · Fuel Controlling SystemSDR 95ZZZX4048Gas Generator · failedMCI/SLN - EN ROUTE, LEFT ENGINE FAILED AND CREW DIVERTED TO FOE. REMOVED AND REPLACED GAS GENERATOR AND POWER SECTION. GG TSO 51 HRS., 15,884 TT, PS S/N 32472, TSSV 1602, TT 8781. HSK S/N 72A912. TSN 1667, TSSV 1602. TEAR DOWN REPORT SHOWED NR 1 BEARING HJul 4, 1995 · N119YV · Beech 1900C · Turbine SectionSDR SW019515Indicator Lamp · failedDURING APPROACH INTO PITTSBURGH, PA, PILOT SELECTED GEAR DOWN AND DID NOT GET A LEFT MAIN DOWN AND LOCK INDICATION. AFTER PILOT ABORTED HIS APPROACH, FLAPS WERE SELECTED UP, BUT REMAINED IN 'LANDING' POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE Jul 2, 1995 · N155YV · Beech 1900C · Landing Gear Position and WarningSDR MASA9515Lamp · failedDURING APPROACH INTO PITTSBURGH, PA, PILOT SELECTED GEAR DOWN AND DID NOT GET A LT MAIN DOWN AND LOCK INDICATION. AFTER PILOT ABORTED APPROACH, FLAPS WERE SELECTED UP, BUT REMAINED IN 'LANDING' POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACEJul 2, 1995 · N155YV · Beech 1900C · Landing Gear Position and WarningSDR 95ZZZX4346Relay · failedDURING APPROACH INTO PITTSBURGH, PA, PILOT SELECTED GEAR DOWN AND DID NOT GET A LEFT MAIN DOWN AND LOCK INDICATION. AFTER PILOT ABORTED HIS APPROACH, FLAPS WERE SELECTED UP, BUT REMAINED IN 'LANDING' POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE Jul 2, 1995 · N155YV · Beech 1900C · Trailing Edge Flap Control SystemSDR 95ZZZX4059Relay · failedDURING APPROACH INTO PITTSBURGH, PA, PILOT SELECTED GEAR DOWN AND DID NOT GET A LT MAIN DOWN AND LOCK INDICATION. AFTER PILOT ABORTED APPROACH, FLAPS WERE SELECTED UP, BUT REMAINED IN 'LANDING' POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACEJul 2, 1995 · N155YV · Beech 1900C · Landing Gear Position and WarningSDR 95ZZZM463Skin · crackedSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND 2 SKIN CRACKS AT THE INTERSECTION OF THE DORSAL FIN AND THE REAR PRESSURE BULKHEAD. CRACKS WERE STOP DRILLED AND REINFORCED IAW BEECH 1900 SRM.Jul 2, 1995 · N734GL · Beech 1900C · Fuselage Main, Plate/SkinSDR 95ZZZM464Bracket · looseSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE AIRSTAIR DOOR SNUBBER BRACKET LOOSE. THE ATTACH BRACKET WAS REMOVED AND REPLACED WITH BEECH KIT 114-4032-1.Jul 1, 1995 · N734GL · Beech 1900C · Passenger/Crew DoorsSDR 95ZZZM465Truss · crackedSPW - DURING ROUTINE VISUAL INSPECTION OF AREA 'A' IAW AD95-02-18, THE RT ENGINE TRUSS WAS FOUND CRACKED. THE TRUSS WAS REMOVED AND REPLACED WITH A SERVICEABLE TRUSS. (M)Jun 30, 1995 · N152GL · Beech 1900C · Engine Mount SectionSDR 96ZZZX2Bearing · fracturedNEITHER THE COMPRESSOR OR THE CT DISK ROTATED FREELY AND HEAVY RUB WAS NOTED ON THE FIRST STAGE COMPRESSOR ROTOR. THE NR 1 BEARING INNER BALL CAGE WAS FRACTURED AND THE BALLS SHOWED SIGNS OF SKIDDING.Jun 24, 1995 · N119YV · Beech 1900C · Turbine Engine Compressor SectionSDR 95ZZZX4049Gas Generator · failedFLT 5630 - CREW REPORTED SMOKE IN COCKPIT FOLLOWED BY LT ENGINE OIL LIGHT. CREW SHUT DOWN LEFT ENGINE AND RETURNED TO FIELD AT FYV. REMOVED AND REPLACED ENGINE. RECORDS SHOWED ENGINE HAD 54 HOURS SINCE IT CAME OUT OF SHOP FOR REAR HUB REPLACEMENT. GAS GENEJun 23, 1995 · N119YV · Beech 1900C · Turbine SectionSDR 95ZZZM466Blade · nickedGRI - ON WALK AROUND, THE PILOT FOUND A NICK ON ONE BLADE OF RT PROP. MAINTENANCE DETERMINED THAT THE NICK WAS OUT OF LIMITS AND CHANGED THE PROPELLER.Jun 21, 1995 · N123UE · Beech 1900C · Propeller Blade SectionSDR 95ZZZM467Tire · separatedSQI - AFTER TAKEOFF, CREW REPORTED A VERY SEVERE NOSE WHEEL SHIMMY. AS A PRECAUTION, THE AIRCRAFT WAS DIVERTED TO SPI WHERE IT MADE AN UNEVENTFUL LANDING. MAINTENANCE NOTED THAT THE RECAP TREAD WAS GONE. THE NOSE WHEEL ASSY, P/N 11480013, CHANGED ALONG WITHJun 20, 1995 · N174GL · Beech 1900C · TireSDR 96ZZZX3Bearing · fracturedTHERE ARE TWO AREAS THAT ARE BEING TAKEN UNDER INVESTIGATION WITH THIS ENGINE. A MATERIAL FAILURE OF THE NR 1 BEARING AND A BAD STARTER GENERATOR.Jun 15, 1995 · N119YV · Beech 1900C · Turbine Engine Compressor SectionSDR 95ZZZM468Bracket · looseSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE AIRSTAIR DOOR SNUBBER BRACKET LOOSE. THE ATTACH BRACKET WAS REMOVED AND REPLACED WITH BEECH KIT 114-4032-1.Jun 15, 1995 · N98GL · Beech 1900C · Passenger/Crew DoorsSDR 95ZZZX4050Gas Generator · seizedFYV - FLT 5635 - ON CLIMB AFTER TAKEOFF, LEFT ENGINE SHUT DOWN MAINTENANCE, FOUND POWER SECTION AND GAS GENERATOR SEIZED. REMOVED AND REPLACED GAS GENERATOR AND POWER SECTION. POWER SECTION HAD 2533 HOURS SINCE SHOP VISIT. GAS GENERATOR HAD 75 HOURS SINCE SJun 14, 1995 · N119YV · Beech 1900C · Turbine SectionSDR 95ZZZM469Switch · out of adjustTVC - AFTER TAKEOFF, THE CREW ELECTED AN AIR TURNBACK DUE TO AN UNSAFE CABIN DOOR INDICATION. AN UNEVENTFUL LANDING WAS ACCOMPLISHED, AFTERWHICH MAINTENANCE ADJUSTED THE DOOR MICROSWITCH.Jun 14, 1995 · N60UE · Beech 1900C · Door Warning System
Back to Beech 1900C