Raytheon 1900D

Service difficulty reports · 7,152

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 = '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 017041Powerpack · failedLANDING GEAR WOULD NOT EXTEND, MANUAL EXTENSION PERFORMED. REPLACED HYD POWER PACK IAW MM, OP AND LEAK CHECKED GOOD.Jan 13, 2004 · N172MJ · Beech 1900D · Hydraulic System, MainSDR GLBA20030531Circuit Board · failedNR 1 AND NR 2 ENVIRO FAILS, REMOVED AND REPLACED A130 PCB. OPS CK GOOD.Jan 13, 2004 · N204GL · Beech 1900D · Air Conditioning System WiringSDR 57841Downlock · inoperativeAFTER NORMAL EXTENSION OF LANDING GEAR RT MAIN DID NOT SHOW DOWN AND LOCK AFTER TOWER FLY BY. A/C LANDED WITH NO FURTHER INCIDENT. REPLACED RT MAIN GEAR DOWN LOCK SWITCH AND HARNESS ASSY, RIGGED SWITCHES AND PERFORMED GEAR SWINGS AS REQUIRED. OPS CK GOOD.Jan 12, 2004 · N155ZV · Beech 1900D · Landing Gear Position and WarningSDR 57827Autofeather Sys · malfunctionedON TAXI OUT CREW BEGAN STARTING LT ENGINE, AFTER GETTING IT STARTED PROPS WOULDN'T COME OUT. ALSO THE AUTOFEATHER WOULDN'T TEST. CREW RETURNED TO THE GATE WITH NO FURTHER INCIDENT. RAN BOTH ENGINES, ALL SYS OPS CK NORMAL.Jan 11, 2004 · N244YV · Beech 1900D · Propeller Feathering/ReversingSDR CA040202011Handle · failed(CAN) DURING TAKEOFF ROLL THE AIRSTAIR DOOR EXTERIOR HANDLE SEPARATED FROM THE DOOR. FURTHER INSPECTION FOUND IMPACT DAMAGE TO LT PROPELLER AND LT IB FLAP. APPROXIMATELY ONE INCH MISSING FROM TIP OF ONE PROPELLER BLADE AND DENT IN LOWER SKIN OF IB FLAP. HANDLEJan 9, 2004 · Beech 1900D · Entrance StairsSDR CA040122004Bracket · cracked(CAN) DURING GROUND HANDLING, CREW ATTEMPTED TO OPEN DOOR FROM INSIDE AND THE MAIN HANDLE UPON APPLYING PRESSURE, RELEASED WITHOUT ACTUATING DOOR CAMS. MAINTENANCE FOUND THAT THE MAIN DOOR ACTUATION BRACKETHAD BROKEN INTO TWO PIECES. THE BRACKET WAS REPLACED AJan 8, 2004 · Beech 1900D · Passenger/Crew DoorsSDR GLBA20030528Connector · dirty104 PERCENT, N1 WITH 2000 LB TORQUE ON NR 2 ENG, CLEANED CONNECTOR ON TORQUE TRANSDUSER ON NR 2 ENGINE.Jan 8, 2004 · N255GL · Beech 1900D · Engine RPM Indicating SystemSDR GLBA2003528Connector · inoperative104 PERCENT N1 WITH 2000 LB TORQUE ON NR 2 ENG, CLEANED CONNECTOR ON TORQUE TRANSDUSER ON NR 2 ENGINE.Jan 8, 2004 · N255GL · Beech 1900D · Engine BMEP/Torque IndicatingSDR GLBA20030527Flap · stuckFLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTIONJan 7, 2004 · N154GL · Beech 1900D · Trailing Edge Flap Control SystemSDR GLBA2003527Flap · stuckFLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTIONJan 7, 2004 · N154GL · Beech 1900D · Trailing Edge Flap Control SystemSDR GLBA20030525Windshield · crackedFO'S CRACKED WINDSHIELD, REMOVED AND REPLACED FO'S WINDSHIELD.Jan 5, 2004 · N100UX · Beech 1900D · Flight Compartment WindowsSDR GLBA20030524Indicator · intermittentCAPT HAS NO AIRSPEED INDICATION, ASI STARTED WORKING ABOUT HALF WAY ON FERRY FLIGHT. DID PITOT STATIC TEST OPS CK GOOD.Jan 5, 2004 · N170GL · Beech 1900D · Airspeed/Mach IndicatorSDR GLBA2003525Windshield · crackedFO'S CRACKED WINDSHIELD, REMOVED AND REPLACED FO'S WINDSHIELD.Jan 5, 2004 · N100UX · Beech 1900D · Flight Compartment WindowsSDR GLBA2003524Indicator · intermittentCAPT HAS NO AIRSPEED IND, ASI STARTED WORKING ABOUT HALF WAY TO DEN ON FERRY FLIGHT. DID PITOT STATIC TEST, OPS CK GOODJan 5, 2004 · N170GL · Beech 1900D · Airspeed/Mach IndicatorSDR AMWA112Seal · crackedDURING INSPECTION RT ENGINE FIRE SEAL WAS FOUND TO BE CRACKED ON THE O/B CENTER WEB, IN CENTER AREA OF WEB APPROX 3.5 INCHES LONG. REPAIRED BY REPLACING WEB ASSY ACCORDANCE WITH SRM.Jan 2, 2004 · N138ZV · Beech 1900D · Engine FiresealsSDR AMWA111Firewall · crackedDURING INSPECTION RT ENGINE FIRE WALL WAS FOUND CRACKED AROUND THE O/B SECTION OF WEB APPROX AT 5 INCHES LONG IN VERT POSITION. BEHIND ATTACH ANGLE FOR COWLING. THEN CRACK TURNS HORIZONTAL GOING I/B APPROX 2.5. REPAIRED DAMAGE AREA BY STOP DRILLING CRACK ENJan 2, 2004 · N138ZV · Beech 1900D · Nacelle/Pylon, Bulkhead/FirewallSDR GLBA20030523Antenna · malfunctionedBOTH VOR DISPLAYS SHOWED FULL SCALE DEFECTION ON ALL VOR STATIONS, R&R ANTENNAJan 1, 2004 · N208GL · Beech 1900D · Visual Omnirange (VOR) SystemSDR GLBA2003523Display · defectiveBOTH VOR DISPLAYS SHOWED FULL SCALE DEFECTION ON ALL VOR STATIONS, PENDING CORRECTIVE ACTION.Jan 1, 2004 · N208GL · Beech 1900D · Visual Omnirange (VOR) SystemSDR 57548Coupling · wornUPON APPROACH TO MCI LANDING GEAR WOULD NOT EXTEND. CREW AND MX CONTROL DECIDED TO HAVE AIRCRAFT RETURN TO LIT, AS IT WAS A REPOSITION FLIGHT. UPON ARRIVAL AT LIT, THE GEAR WAS PUMPED DOWN AND HAD 3 GREENS. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. Jan 1, 2004 · N174YV · Beech 1900D · Hydraulic System, MainSDR GLBA20030522Switch · out of adjustCARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT, ADJUSTED DOOR AJAR SWITCH OPS CK GOODDec 30, 2003 · N202UX · Beech 1900D · Door Warning SystemSDR GLBA20030521Warning Light · illuminatedPULLED O2 MASKS FOR PAX WITH CAB ALT HI ANNUNCIATORS COULD NOT DESCANT DUE TO ICING, REINSTALLED MASKS CAB ALT HIGH LIGHT CAME ON DUE TO RT BLEED SYS IN OFF. OPS CK GOOD.Dec 30, 2003 · N192GL · Beech 1900D · Central WarningSDR 364032Switch · sparksWHEN THE NR 2 FLIGHT DIRECTOR PITCH SYNC BUTTON WAS PUSHED IT CAUSED ELECTRICAL SPARKS. REMOVED AND REPLACED NR 2 FLIGHT DIRECTOR PITCH SYNC BUTTON, SPARKS WHERE CAUSED BY LOOSE BUTTON WHICH SHORTED AGAINST YOKE.Dec 30, 2003 · N172MJ · Beech 1900D · Propeller Synchronizer SectionSDR 57453Brake · inoperativeUPON LANDING RT BRAKES FELT SOFT. MAINTENANCE CALLED. BRAKES WERE BLEED. OPS CK NORMAL.Dec 29, 2003 · N176YV · Beech 1900D · BrakeSDR GLBA20030520Brush Block · inoperativeRT PROP DEICE AND PILOT AND COPILOT W/S NOT HEATING, REMOVED AND REPLACED BRUSH BLOCK PN 4E3196-1GLA AND PROP AMP IND PN 114-380049-5.Dec 29, 2003 · N201GL · Beech 1900D · Propeller/Rotor Anti-Ice/De-Ice SystemSDR 2004F00360Brake · malfunctionedFLT 9227 - NAS-FLL - AFTER LANDING, BRAKES ARE SPONGY AND LOSE PRESSURE WHILE TURNING AND STOPPING. BLED BRAKES. LEAK CHECK OK. OPERATIONAL CHECK NORMAL. (M)Dec 27, 2003 · N69547 · Beech 1900D · Landing Gear Brake SystemSDR 364031Door Frame · wornWORN NOTCH IN CARGO DOOR FRAME LOWER EDGE MID SPAN, REMOVED DAMAGED AREA AND INSTALLED AN INSERTION REPAIR WITH SPLIT DOUBLER ON UNDERSIDE TO SUPPORT THE RIB IAW SRM SKIN DAMAGE ( NON PRESSURIZED AREA).Dec 26, 2003 · N136MJ · Beech 1900D · Fuselage Main, StructureSDR GLBA20030519Windshield · crackedCAPT WINDSHIELD CRACKED RETURN TO AIRPORT, REMOVED AND REPLACED WINDSHIELD PN 101-384025-17.Dec 26, 2003 · N220GL · Beech 1900D · Flight Compartment WindowsSDR AMWA110Rib · crackedDURING INSPECTION FOUR CRACKS FOUND ON THIS RIB, TWO ON THE LT SIDE AND TWO ON THE RT SIDE LOCATED ON STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-46 & 101-640000-38. LT STRINGER P/N 101-640000-39 & 101-640000-45.Dec 22, 2003 · N139ZV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA109Rib · crackedDURING INSPECTION, FIVE CRACKS FOUND IN THIS RIB, THREE ON THE RT SIDE AND TWO ON THE LT SIDE LOCATED ON THE STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-45, 101-640000-42 & 101-640000-38. LT STRINGER P/N 101-640000-43, 10Dec 22, 2003 · N139ZV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA107Rib · crackedDURING INSPECTION, ONE CRACK FOUND ON THIS RIB ON THE LT SIDE AT STRINGER TO RIB INTERSECTION STRINGER. P/N 101-640000-39.Dec 22, 2003 · N139ZV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA108Rib · crackedDURING INSPECTION, ONE CRACK FOUND ON THIS RIB ON RT SIDE ON STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-46.Dec 22, 2003 · N139ZV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA20030516Switch · dirtyCARGO DOOR ANNUNCIATOR LIGHT CAME ON IN FLIGHT, CLEANED CARGO DOOR WARNING SWITCHES & ADJUSTED CARGO DOOR AJAR SWITCH OPS CK GOODDec 21, 2003 · N96UX · Beech 1900D · Door Warning SystemSDR 57206Brake · malfunctionedAFTER LANDING IN PIT. CREW REPORTED THAT THE LT BRAKE HAD VERY LITTLE PRESSURE ON TAXI. BLEED LT BRAKES SYS. IAW MM 32-40-00. OPS AND LEAK CK GOOD.Dec 20, 2003 · N140ZV · Beech 1900D · BrakeSDR 57174Indicator · failedAFTER TAXING OUT FROM GATE. CREW NOTED LT TORQUE INDICATOR WENT TO ZERO ON INITIAL SPOOL UP FOR TAKEOFF. CREW THEN RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE INDICATOR.Dec 18, 2003 · N144ZV · Beech 1900D · Engine BMEP/Torque IndicatingSDR 57171Gyro · inoperativeSHORTLY AFTER DEPARTURE FROM PIT CREW NOTICED CAPT'S GYROSCOPIC DIRECTIONAL COMPASS SYSTEM WASN'T WORKING CORRECTLY. SO DECEIDED TO RETURN TO PIT. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. T/S REPAIRED PINS 5 AND 7 OF CONNECTOR J203 AT NR 1 FLUX DETECTODec 18, 2003 · N218YV · Beech 1900D · Directional Gyro and Indicating SystemSDR AMWA98Doubler · debondedDURING SCHEDULED ABCD STRUCTURAL INSPECTION, ONE RIGHT BONDED DOUBLER WAS FOUND TO BE DISBONDED.Dec 16, 2003 · N133YV · Beech 1900D · Fuselage Miscellaneous StructureSDR AMWA104Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, FASTENER AT LWS 124 WAS FOUND TO HAVE EVIDENCE OF CORROSION.Dec 16, 2003 · N133YV · Beech 1900D · FastenersSDR AMWA97Doubler · delaminatedDURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE LEFT DOUBLER WAS FOUND TO BE DISBONDED.Dec 16, 2003 · N133YV · Beech 1900D · Fuselage Miscellaneous StructureSDR AMWA102Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, FASTENERS AT LWS 102 WAS FOUND TO HAVE EVIDENCE OF CORROSION.Dec 16, 2003 · N133YV · Beech 1900D · FastenersSDR AMWA95Rivet · shearedDURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE RIGHT SIDE HEAVY ANGLE HAD ONE SHEARED RIVET.Dec 16, 2003 · N133YV · Beech 1900D · FastenersSDR AMWA96Seat Track · damagedDURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE LEFT AFT SEAT TRACK WAS FOUND TO BE DAMAGED.Dec 16, 2003 · N133YV · Beech 1900D · Fuselage, Seat/Cargo Attach FittingsSDR AMWA106Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, TWO FASTENERS AT RWS 105 WERE FOUND TO HAVE EVIDENCE OF CORROSION.Dec 16, 2003 · N133YV · Beech 1900D · FastenersSDR AMWA103Fastener · corrodedDURING SCHEDULED STRUCTURAL INSPECTION, TWO FASTENERS AT LWS 55 WERE FOUND TO HAVE EVIDENCE OF CORROSION.Dec 16, 2003 · N133YV · Beech 1900D · FastenersSDR AMWA94Rivet · shearedDURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE RIGHT SIDE WINDOW FINGER DOUBLER WAS FOUND TO HAVE ONE SHEARED RIVET.Dec 16, 2003 · N133YV · Beech 1900D · FastenersSDR AMWA105Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, FASTENER AT LWS 128 WAS FOUND TO HAVE EVIDENCE OF CORROSION.Dec 16, 2003 · N133YV · Beech 1900D · FastenersSDR AMWA100Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, TWO FASTENERS AT RWS 124 WERE FOUND TO HAVE EVIDENCE OF CORROSION.Dec 16, 2003 · N133YV · Beech 1900D · FastenersSDR AMWA99Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, SEVEN FASTENERS AT RWS 125-131 WERE FOUND TO HAVE EVIDENCE OF CORROSION.Dec 16, 2003 · N133YV · Beech 1900D · FastenersSDR AMWA101Fastener · corrodedDURING SCHEDULED D-STRUCTURAL INSPECTION, THREE FASTENERS AT RWS 102 WAS FOUND TO HAVE EVIDENCE OF CORROSION.Dec 16, 2003 · N133YV · Beech 1900D · FastenersSDR AMWA93Keelbeam · wornDURING A DETAIL INSPECTION, THE FORWARD LEFT INBOARD LOWER KEEL WAS WORN AT THE GRAVEL FENDER ATTACH BRACKET.Dec 12, 2003 · N26YV · Beech 1900D · Fuselage Main, KeelSDR AMWA91Angle · crackedDURING AN ABC STRUCTURAL INSPECTION, THE RIGHT HEAVY ANGLE WAS FOUND TO BE CRACKED.Dec 12, 2003 · N26YV · Beech 1900D · Fuselage Miscellaneous Structure
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