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 95ZZZX1386Pulley · jammedCEN/TUS - EN ROUTE - PILOT EXPERIENCED LEFT FLUTTER AND BUFFETING DURING PITCH OR ACFT ATTITUDE CHANGES. SUSPECTED CONTROL SURFACE PROBLEM ON THE GROUND, DURING AILERON MOVEMENT WITH THE YOKE AND HAND MOVEMENT ON THE CONTROL SURFACE, FELT SLIGHT BINDING. INSFeb 9, 1995 · N11ZR · Beech 1900C · Aileron Control SystemSDR 95ZZZW331Flap · crackedDURING SCHEDULED MAINTENANCE AN INSPECTION OF THE RIGHT INBOARD FLAP REVEALED A 1 INCH CRACK IN THE LOWER SKIN ALONG THE TRAILING EDGE LOCATED BETWEEN THE THIRD AND FOURTH RIB OUTBOARD FROM THE INBOARD END. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLIFeb 9, 1995 · N119YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZW330Flap · crackedDURING SCHEDULED MAINTENANCE AN INSPECTION OF THE LEFT OUTBOARD FLAP REVEALED A 1.5 INCH CRACK IN THE UPPER SKIN ALONG THE TRAILING EDGE LOCATED BETWEEN THE FIRST AND SECOND RIB OUTBOARD FROM THE INBOARD END. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALFeb 9, 1995 · N119YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZX1953Frame · crackedSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE FUSELAGE FRAME CRACKED AT THE POINT WHERE THE FIRST AIR DOOR SNUBBER BRACKET IS ATTACHED. REPAIRED FRAME IAW BEECH SRM 51-70-00, PAGE 52.Feb 8, 1995 · N130UE · Beech 1900C · Fuselage Main, FrameSDR 95ZZZX1387Close Out Panels · missingHMO/TUS - EN ROUTE, CARGO DOOR, PN 1144301093, (AFT CABIN DOOR), OPENED IN-FLIGHT. PERFORMED FULL FUNCTIONAL, OPS CHECK AND RIG CHECK OF CARGO DOOR SYSTEM AND WARNING SYSTEM. ALL FUNCTIONS CHECK NORMAL. NO DEFECTS FOUND. INSPECTED AIRFRAME AND CARGO DOOR FFeb 7, 1995 · N11ZR · Beech 1900C · Cargo/Baggage DoorsSDR 95ZZZZ138Truss · crackedWHILE COMPLIED WITH AD 92-06-09 A CRACK WAS FOUND IN AREA A OF THE LT TRUSS (RT SIDE). TRUSS WAS REPLACED WITH A NEW 'D' STYLE TRUSS, PN 129-910032-79. AIRCRAFT WAS RETURNED TO SERVICE. (Z)Feb 5, 1995 · N38015 · Beech 1900C · Engine Mount SectionSDR 95ZZZX1533Truss Kit · crackedDURING C/W AD 92-06-09 AMENDMENT 39-8189, LT ENGINE TRUSS WAS FOUND WITH A .1250 INCH CRACK IN AREA 'A' AT THE UPPER FORWARD GUSSET ON THE RIGHT INBOARD SIDE OF THE CLUSTER. REPAIRED THE TRUSS IAW BEECH SB 2255, REV 6, AND RETURNED THE AIRCRAFT TO SERVICE.Feb 5, 1995 · N807BE · Beech 1900C · Engine Mount SectionSDR 95ZZZZ99Split Flap Cam · failedCIU - AFTER TAKEOFF THE CREW ELECTED AN AIR TURN BACK BECAUSE THE FLAPS WERE STUCK IN THE TAKEOFF POSITION. AFTER AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE RT SPLIT FLAP CAM AND RE-RIGGED THE SWITCH.Feb 4, 1995 · N86UE · Beech 1900C · Trailing Edge Flap Control SystemSDR 95ZZZZ100Elevator · damageRHI - DURING DE-ICING OPERATIONS, THE DE-ICE TOWER CONTACTED THE LEFT ELEVATOR RESULTING IN DAMAGE BEYOND LIMITS. MAINTENANCE REMOVED THE DAMAGE ELEVATOR, INSPECTED THE AREA FOR DAMAGE, AND INSTALLED A SERVICEABLE ELEVATOR.Feb 4, 1995 · N104GL · Beech 1900C · Elevator StructureSDR 95ZZZW465Window · brokenFLT NR 2375 - DEPARTING DEN WAS UNABLE TO PRESSURIZE. AIRCRAFT RETURNED TO DEN WHERE GP EXPRESS MAINTENANCE DEFERRED THE PRESSURIZATION SYSTEM. LATER THAT DAY GP EXPRESS MAINTENANCE FOUND THE INSPECTION WINDOW FOR THE AFT CARGO DOOR LOCK MECHANISM BROKEN. WFeb 4, 1995 · N124GP · Beech 1900C · Inspection WindowsSDR 95ZZZZ102Frame · crackedSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE ENTRANCE DOORWAY FUSELAGE BULKHEAD CRACKED AT THE POINT WHERE THE AIRSTAIR DOOR DAMPNER BRACKET ATTACHES. REPAIRED BY INSTALLING AN ANGLE REINFORCEMENT INSIDE THE BULKHEAD IAW BEECH SRM 53-90-00 PGS 24 ANFeb 3, 1995 · N174GL · Beech 1900C · Fuselage Miscellaneous StructureSDR 95ZZZX875Wire · failedMHT - AFTER THE LANDING GEAR WAS CYCLED DOWN, THE NOSE GEAR GREEN DID NOT INDICATE DOWN AND LOCKED. FLIGHT CREW PERFORMED ABNORMAL CHECK. LIST VERIFIED GEAR DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. ACFT WAS INSPECTED AND FOUND SAFE FOR FERRY TO PFeb 2, 1995 · N815BE · Beech 1900C · Landing Gear System WiringSDR HERA9505Switch · dirtyANC - FLT 1481 - AIR RETURN DUE WING FLAPS WOULD NOT RETRACT PAST THE TAKEOFF POSITION AFTER TAKEOFF. A LANDING WAS MADE AT ANC WITHOUT INCIDENCE. MAINTENANCE CLEANED AND LUBED THE LEFT AND RIGHT FLAP SAFETY SWITCHES. AFTER OPERATIONAL CHECKS CONFIRMED THE Jan 31, 1995 · N80346 · Beech 1900C · Trailing Edge Flap Control SystemSDR 95ZZZZ101Seals · leakingOTW - UPON ARRIVAL OTW, THE CREW REPORTED LEFT ENGINE LOW OIL PRESSURE. INSPECTION REVEALED INTERNAL SEEPAGE ALLOWING OIL LEAKS AT THE COMPRESSOR. MAINTENANCE REMOVED THE ACCESSORY GEARBOX AND REPLACED PERFORMED PACKINGS, SEALS, AND GASKETS. THE NR 2 BEARINJan 31, 1995 · N98GL · Beech 1900C · Turbine Engine Oil SystemSDR 95ZZZX923Switch · dirtyANC - FLT 1481 - AIR RETURN DUE WING FLAPS WOULD NOT RETRACT PAST THE TAKEOFF POSITION AFTER TAKEOFF. A LANDING WAS MADE AT ANC WITHOUT INCIDENCE. MAINTENANCE CLEANED AND LUBED THE LEFT AND RIGHT FLAP SAFETY SWITCHES. AFTER OPERATIONAL CHECKS CONFIRMED THE Jan 31, 1995 · N80346 · Beech 1900C · Trailing Edge Flap Control SystemSDR 95ZZZZ103Rivets · looseSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE RIGHT WING SEEPING FUEL OUTBOARD OF THE NACELLE ALONG THE SPAR. SEVERAL RIVETS WERE REPLACED AND THE AREA WAS SEALED WITH MIL-S-8802F SEALANT.Jan 30, 1995 · N45GL · Beech 1900C · Wing, Plate/SkinSDR HERA9504Control Cable · bindingKSM - FLT 5691 - ON DESCENT, THE WING FLAPS BECAME STUCK IN THE APPROACH POSITION. A LANDING WAS MADE WITHOUT INCIDENCE. THE AIRCRAFT WAS THEN REPOSITIONED TO ANC ON A SPECIAL FLIGHT PERMIT. AFTER TROUBLESHOOTING THE WING FLAP SYSTEM, MAINTENANCE REMOVED ANJan 26, 1995 · N5632C · Beech 1900C · Trailing Edge Flap Control SystemSDR 95ZZZZ59Shroud Segment · brokenGJT TRAINING FLIGHT, WHILE ADVANCING THE POWER LEVERS DURING STALL RECOVERY NOTICED FLAMES EMITTING FROM THE RT ENGINE EXHAUST STACKS. ENGINE WAS SHUTDOWN, PROP WAS FEATHERED ANDFIRE BOTTLE WAS DISCHARGED. AIRCRAFT LANDED SAFELY IN GJT. INITIAL INSPECTION BYJan 26, 1995 · N17012 · Beech 1900C · Engine (Turbine/Turboprop)SDR 95ZZZX922Control Cable · bindingKSM - FLT 5691 - ON DESCENT, THE WING FLAPS BECAME STUCK IN THE APPROACH POSITION. A LANDING WAS MADE WITHOUT INCIDENCE. THE AIRCRAFT WAS THEN REPOSITIONED TO ANC ON A SPECIAL FLIGHT PERMIT. AFTER TROUBLESHOOTING THE WING FLAP SYSTEM, MAINTENANCE REMOVED ANJan 26, 1995 · N5632C · Beech 1900C · Trailing Edge Flap Control SystemSDR 95ZZZX1918Engine · failedDURING FLIGHT, CREW REPORTS A FLASH FROM RT ENGINE FOLLOWED BY FLAMES COMING OUT OF EXHAUST STACKS. RT ENGINE WAS THEN SHUT DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. AFTER FURTHER INVESTIGATION BY MAINTENANCE, RT ENGINE OIL FILTER WAS FOUND TO HAVE LARGE AMJan 25, 1995 · N158YV · Beech 1900C · Turbine Engine Compressor SectionSDR 95ZZZX1818Bearing · fracturedTHERE ARE 4 AREAS THAT SUBMITTER IS INVESTIGATING. A. A MATERIAL FAILURE OF THE NR 1 BEARING. B. ELECTRICAL DISCHARGE DUE TO THE MAGNETISM ON THE STARTER DRIVE GEAR. C. PLASTIC BEAD MATERIAL. D. THE FIT OF THE NR 1 BEARING ONTO THE REAR STUB SHAFT. FOUJan 25, 1995 · N158YV · Beech 1900C · Turbine Engine Compressor SectionSDR 95ZZZX705Rotary Switch · dirtyCDR - FLT 2092 - DEPARTING, HAD THE RT FIRE T-HANDLE ILLUMINATE. FLIGHT CREW SHUT DOWN AND FEATHERED THE ENGINE AND DISCHARGED THE FIRE BOTTLE. AIRCRAFT RETURNED SAFELY TO CDR. MAINTENANCE INSPECTED ENGINE AND NO SIGN OF FIRE WAS NOTED. ENGINE WAS CLEARED Jan 22, 1995 · N125GP · Beech 1900C · Detection SystemSDR 95ZZZZ45Squat Switch · inopGRI - AFTER TAKEOFF, THE CREW ELECTED AN AIR TURN BACK. PILOT REPORTED THAT WITH GEAR RETRACTED, THE GEAR HANDLE LIGHT STAYED ON AND THE WARNING HORN WILL NOT SILENCE. MAINTENANCE REPLACED THE RT MLG SQUAT SWITCH. THE GEAR WARNING SYSTEMS WORKED SATISFACTORJan 21, 1995 · N87GL · Beech 1900C · Landing Gear Position and WarningSDR 95ZZZZ49Engine Truss · chafedESC - DURING SCHEDULED TRUSS INSPECTION, THE RT TRUSS WAS FOUND CHAFED BEYOND LIMITS IN THE AREA OF THE FREON COMPRESSOR. THE TRUSS WAS REPLACED WITH SERVICEABLE TRUSS. (Z)Jan 20, 1995 · N67UE · Beech 1900C · Engine Mount SectionSDR 95ZZZZ48Engine Truss · chafedESC - DURING SCHEDULED TRUSS INSPECTION, THE RT TRUSS WAS FOUND CHAFED BEYOND LIMITS IN THE AREA OF THE FREON COMPRESSOR. THE TRUSS WAS REPLACED WITH SERVICEABLE TRUSS. (Z)Jan 20, 1995 · N67UE · Beech 1900C · Engine Mount SectionSDR 95ZZZZ36Py Line · looseFLT NR 2090 DEPARTED CDR, THE RIGHT ENGINE DECELERATED AND WENT INTO FEATHER (AUTO FEATHER ENGAGED) AFTER TAKEOFF. FLIGHT CREW SHUT DOWN ENGINE AND LANDED SAFELY BACK IN CDR. MAINTENANCE FOUND THE PY LINE LOOSE AT THE FIRESHIELD. 'B' NUT WAS TIGHTENED AND SJan 20, 1995 · N17012 · Beech 1900C · Fuel Controlling SystemSDR HERA9503Bleed Air · failedSDP/ANC - FLT 1476 - AIRCRAFT EXPERIENCED A DUAL BLEED AIR FAILURE. TOTAL TIME OF FAILURE WAS APPROXIMATELY 10 SECONDS. THE FAILURES OCCURRED WHILE DESCENDING THROUGH 15,000 FEET IN CLEAR WEATHER AND MINUS 20 DEGREES CELSIUS OAT. CONDITIONS PRIOR TO THE FAIJan 19, 1995 · N55456 · Beech 1900C · Pneumatic Distribution SystemSDR 95ZZZZ46Gear Control · inopMSP - PILOT REPORTED THAT THE LANDING GEAR UNSAFE LIGHTS DO NOT LIGHT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL. A GEAR SWING WAS SUCCESSFUL. (Z)Jan 18, 1995 · N98GL · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 95ZZZX1845Sun Gear · failedINDICATIONS ARE THAT THE FAILURE OCCURRED IN THE 1ST STAGE GEAR REDUCTION AREA. THE INVESTIGATION CENTERS AROUND THE 1ST STAGE GEAR AND THE 1ST STAGE SUN GEAR AREA.Jan 18, 1995 · N156YV · Beech 1900C · Turbine Engine Reduction GearSDR HERA9502Windshield · crackedBET - FLT 1495 - EN ROUTE AT FL220, THE OUTSIDE LAYER OF THE RT FORWARD WINDSHIELD CRACKED. THE OUTSIDE AIR TEMPERATURE WAS MINUS 34 DEGREES CELSIUS AND THE WINDSHIELD HEAT WAS ON AT THE TIME. THE AIRCRAFT CONTINUED ON TO BET AND A LANDING WAS MADE WITHOUT IJan 17, 1995 · N55456 · Beech 1900C · Flight Compartment WindowsSDR HERA9501Switch · dirtyANC - FLT 1495 - AIR RETURN DUE WING FLAPS STUCK IN THE TAKEOFF POSITION AFTER DEPARTURE. A LANDING WAS MADE AT ANC WITHOUT INCIDENCE. MAINTENANCE CLEANED THE LEFT AND RIGHT FLAP SAFETY SWITCHES AND CHECKED THE RIGGING OF THE SWITCHES. AFTER OPERATIONAL CHEJan 17, 1995 · N55456 · Beech 1900C · Trailing Edge Flap Control SystemSDR 95ZZZX924Switch · dirtyANC - FLT 1495 - AIR RETURN DUE WING FLAPS STUCK IN THE TAKEOFF POSITION AFTER DEPARTURE. A LANDING WAS MADE AT ANC WITHOUT INCIDENCE. MAINTENANCE CLEANED THE LEFT AND RIGHT FLAP SAFETY SWITCHES AND CHECKED THE RIGGING OF THE SWITCHES. AFTER OPERATIONAL CHEJan 17, 1995 · N55456 · Beech 1900C · Trailing Edge Flap Control SystemSDR 95ZZZW524Switch · dirtyCREW SELECTED LANDING GEAR UP AND OBSERVED A GEAR HANDLE 'INTRANSIT LIGHT'. MAINTENANCE INSPECTED GEAR SWITCHES, CLEANED AND LUBED AS NEEDED, FUNCTION CHECKED GEAR. RETURNED TO SERVICE.Jan 17, 1995 · N91YV · Beech 1900C · Landing Gear Position and WarningSDR 95ZZZW467Switch · out of adjustWHEN LANDING GEAR WAS SELECTED DOWN, THERE WAS NO DOWNLOCK NOSE INDICATION. MAINTENANCE ADJUSTED DOWNLOCK SWITCH. FUNCTION CHECKED LANDING GEAR AND RETURNED TO SERVICE.Jan 16, 1995 · N77YV · Beech 1900C · Landing Gear Position and WarningSDR PLGA418951Retract Mech · malfunctionedBOS - AFTER TAKEOFF, FLAPS WOULD NOT RETRACT. ACFT RETURNED TO LAND WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. FLAPS WERE SECURED IN THE 'FULL-UP' POSITION AND DEFERRED IAW WITH THE MEL. ACFT WAS RELEASED TO SERVICE.MAINTENANCE REPLACED Jan 15, 1995 · N809BE · Beech 1900C · Trailing Edge Flap Control SystemSDR 95ZZZX1815Bearing · fracturedTHE PRELIMINARY INVESTIGATION IS INDICATING THE NR 1 BEARING FAILED.Jan 12, 1995 · N118YV · Beech 1900C · Turbine Engine Compressor SectionSDR 95ZZZW466Switch · dirtyCREW REPORTED WHEN GEAR WAS SELECTED DOWN, THERE WAS NO NOSE GEAR DOWN AND LOCK INDICATION. MAINTENANCE INSPECTED NOSE DOWN AND LOCKED SWITCHES AND WIRING, CLEANED AND LUBED SWITCHES. FUNCTION CHECKED LANDING GEAR. RETURNED AIRCRFT TO SERVICE.Jan 12, 1995 · N77YV · Beech 1900C · Landing Gear Position and WarningSDR 95ZZZW41Skin · crackedDURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE LT O/B FLAP (P/N 35165050258), REVEALED A 1.5 INCH CRACK IN THE UPPER SKIN, AND A 1 INCH CRACK IN THE LOWER SKIN ALONG THE TE BETWEEN THE FIRST AND SECOND RIB O/B FROM THE I/B END. THE CRACKS WERE REPAIRED BYJan 4, 1995 · N143AM · Beech 1900C · Trailing Edge FlapsSDR 95ZZZX538Latch · looseCLE - FLT 3223 - DEPARTING, HAD THE LT COWL OUTBOARD SIDE COME UNLATCHED. AIRCRAFT RETURNED TO CLE WHERE GPX MAINTENANCE INSPECTED THE COWL AND LATCH MECHANISM WITH NO DISCREPANCIES NOTED. COWL WAS SECURED AND AIRCRAFT WAS RETURNED TO SERVICE.Jan 3, 1995 · N120GP · Beech 1900C · Engine Cowling SystemSDR 95ZZZX539Actuator · malfunctionedDEN - FLT 2072 - FLIGHT INBOUND, WAS UNABLE TO OBTAIN A NLG DOWN AND LOCK LIGHT. GP EXPRESS MAINTENANCE CLEANED AND ADJUSTED THE DOWNLOCK SWITCH AND CYCLED THE GEAR SEVERAL TIMES WITH NO DISCREPANCIES NOTED. AIRCRAFT WAS RETURNED TO SERVICE. LATER THAT DAY,Jan 2, 1995 · N38011 · Beech 1900C · Landing Gear Door ActuatorSDR 95ZZZX1814Valve Assy · frettedSUSPECT CAUSE OF FAILURE IS A FAULTY BLEED VALVE. THE DEFINITE CAUSE IS STILL UNDER INVESTIGATION.Jan 2, 1995 · N76YV · Beech 1900C · Compressor Bleed Valve
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