Raytheon 1900D

Service difficulty reports · 7,152

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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 AMWA9Spar Cap · chafedUPON A SERVICE INSPECTION MAINTENANCE FOUND THE LEFT AND RIGHT LOWER SPAR CAP BEHIND THE NACELLE INNER FEN WAS CHAFED. BLENDED, ALODINED AND PRIMED BOTH OF THE LOWER WING SPAR CAP IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. REFERENCE NUMBER JV/0215-03. NO TEARDFeb 12, 2003 · N231YV · Beech 1900D · Wing SparSDR AMWA8Spar Cap · chafedUPON A DETAILED INSPECTION MAINTENANCE FOUND THE ELECTRIC LINE CHAFING ON RIGHT FORWARD WING SPAR IN THE WHEEL WELL. BLENDED LOWER WING SPAR CAP IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT IS REQUIRED.Feb 12, 2003 · N182YV · Beech 1900D · Wing SparSDR S2YA03007Seal · blew outDURING FLIGHT 1403, THE AIRSTAIR DOOR SEAL BLEW OUT IN FLIGHT. THE CREW MADE AN AIR TURNBACK. MECHANIC INSPECTED THE AIRCRAFT AND REPLACED DOOR SEAL AND RETURNED THE AIRCRAFT TO SERVICE.Feb 11, 2003 · N118SK · Beech 1900D · Entrance StairsSDR AMWA10Spar Cap · chafedUPON A DETAILED INSPECTION MAINTENANCE FOUND THAT THE LEFT AND RIGHT LOWER SPAR CAP BEHIND NACELLE INNER WAS CHAFED. BLENDED BOTH OF THE LOWER SPAR CAPS IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. REFERENCE NUMBER JMP/0209-03. NO TEARDOWN REPORT WILL BE REQUIREFeb 11, 2003 · N142ZV · Beech 1900D · Nacelle/Pylon, Frame/Spar/RibSDR S2YA03006Squat Switch · dirtyAFTER TAKEOFF OF FLIGHT 1007, THE GEAR INTRANSIT LIGHT ILLUMINATED WITH THE GEAR HANDLE UP AFTER, THE GEAR SHOULD HAVE RETRACTED. THE CREW MADE AN AIR TURNBACK. MECHANIC INSPECTED THE AIRCRAFT AND REPLACED THE RIGHT UPLOCK SWITCH. MECHANIC OPS CHECK THE SYSFeb 9, 2003 · N831SK · Beech 1900D · Landing Gear Position and WarningSDR S2YA03005Garlock Seal · leakingAFTER TAKEOFF ON FLIGHT 1167, A LEFT ENGINE OIL PRESSURE FLUCTUATION BETWEEN 70 AND 90. THE CREW MADE AN AIR TURNBACK. MECHANIC INSPECTED THE AIRCRAFT, SERVICED THE LEFT ENGINE WITH 4 QUARTS OF OIL AND RETURNED THE AIRCRAFT TO SERVICE. MECHANIC INSPECTED THFeb 7, 2003 · N92SK · Beech 1900D · Turbine Engine Oil SystemSDR CA030207007Indicator · failed(CAN) AIRCRAFT TAXIED FOR TAKEOFF AND AT APPROX 45 KNOTSTHE CAPTAIN NOTICED THAT THE R/H TORQUE GAUGE WAS NOT RISING. THEY ABORTED TAKEOFF AND RETURNED TO GATE TO DEPLANE PASSENGERS. MAINTENANCE REPLACED THE R/H TORQUE GAUGE AND GROUND TESTED SYSTEM SERVICABLEFeb 6, 2003 · Beech 1900D · Engine BMEP/Torque IndicatingSDR NSVA200300005PropellerDuring climb out from LGA, @ approximately 1000 ft., crew noted that a ring of sparks were coming from the RH engine. With engine indications normal crew reduced power-sparks continued. In flight emergency was declared-air return to LGA. Aircraft landing was uFeb 6, 2003 · N191CJ · Beech 1900D · Propeller Blade SectionSDR 047632Tube · crackedUPON APPROACH FOR LANDING ON FLIGHT 5441 IN CHARLOTTE NORTH CAROLINA, THE LEFT ENGINE TORQUE FELL TO BETWEEN 0-500LBS. ALL THE OTHER ENGINE INDICATIONS WERE NORMAL. THE CREW THEN SHUT DOWN THE ENGINE. THE CREW ALSO DID THE EMERGENCY CHECKLIST AND DECLARED AN EFeb 6, 2003 · N218YV · Beech 1900D · Engine Bleed Air SystemSDR GLBA2003016Fuel CapLH FUEL CAP LEAKING FUEL, R&R FUEL CAPFeb 6, 2003 · N94GL · Beech 1900D · Aircraft Fuel SystemSDR GLBA2003015Uplock Switch · out of adjustLANDING GEAR IN-TRANSIT LIGHTS FLICKER WITH GEAR UP, ADJUSTED RT MLG UPLOCK SWITCH OPS CHECKED GOODFeb 4, 2003 · N100UX · Beech 1900D · Landing Gear Position and WarningSDR NSVA200300004CableAirstair door would not open. Maintenance found one door support cable "jamed" on the forward edge between the door and structure. Maintenance dislodged cable, performed multiple operational check of door with no defects noted.Feb 4, 2003 · N243CJ · Beech 1900D · DoorsSDR CA030207008Engine · cracked(CAN) DURING CLIMB PILOT NOTICED LARGE FLUCTUATIONS IN RT ENGINE TORQUES APPROX 300-400 LBS AT TAKEOFF CLIMB POWER. THEY ELECTED TO RETURN AND MADE UNEVENTFUL LANDING. DURING INSPECTION BY MAINTENANCE THE GAS GENERATOR SPEED WAS ALSO NOTICED TO BE UNUSUALLY HFeb 2, 2003 · Beech 1900D · Compressor Bleed ValveSDR 2003F00148Blade · brokenFLT - 9161 - DURNG TAKEOFF, LOUD BANG OCCURRED ON LEFT ENGINE. ABORTED TAKEOFF. SEPARATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT FOUR POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LEFJan 31, 2003 · N69549 · Beech 1900D · Turbine SectionSDR GLBA2003014Controller · failedA/C WOULD NOT PRESSURIZE, R&R CABIN PRESSURE CONTROLLER OPS CHK GOODJan 30, 2003 · N240GL · Beech 1900D · Cabin Pressure ControllerSDR AMWA7Truss · crackedWHILE PERFORMING AN "H" CHECK ON THE RT ENGINE TRUSS, MAINTENANCE FOUND A CRACK LOCATED ON THE TRUSS. THE CRACK IS YET TO BE DETERMINED OF THE LOCATION. MAINTENANCE REMOVED AND REPLACED IT WITH ANOTHER ENGINE TRUSS. TEARDOWN REPORT WILL BE AVAILABLE AT A LATERJan 29, 2003 · N139ZV · Beech 1900D · Engine Mount SectionSDR GLBA2003013Transducer · failedOIL PRESSURE ON NR 1 ENGINE WENT TO 140 PSI, R&R LEFT OIL PRESSURE TRANSDUCERJan 24, 2003 · N118GL · Beech 1900D · Engine Oil PressureSDR 047205Switch · dirtyAFTER DEPARTING, THE CREW HAD THE PASSENGER DOOR ANNUNCIATOR ILLUMINATE. THE CREW THEN DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THE AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED THE SWITCHES. NO PARTS WERE USED. TEARDJan 24, 2003 · N242YV · Beech 1900D · Door Warning SystemSDR S2YA03004Starter Gen · inoperativeAFTER STARTING THE NR 2 ENGINE, THE CREW HAD DIFFIUCULTY GETTING THE NR2 GENERATOR ON LINE. THEN THERE WAS A FIRE INDICATION ON THE RIGHT ENGINE, THE CREW PULLED THE FIRE HANDLE BUT DID NOT BLOW THE BOTTLE. MECHANIC INSPECTED THE SYSTEM AND FOUND THE RIGHT GJan 23, 2003 · N118SK · Beech 1900D · Starter-GeneratorSDR CA030123010Carbon Seal · cracked(CAN) DURING CRUISE, CREW NOTICED OIL PRESSURE DROPPING AND ELECTED TO SHUTDOWN THE LT ENGINE AS A PRECAUTION. THE FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. THE AGB WAS REMOVED TO INVESTIGATE OIL LOSS THRU THE OVERBOARD VENT AND THE STARTER Jan 23, 2003 · Beech 1900D · Turbine Engine Accessory DriveSDR S2YA03002Valve · inoperativeSHORTLY AFTER TAKEOFF, THE CREW SELECTED GEAR UP BUT THE GEAR DID NOT RETRACT. THE CREW DID AN AIR-TURN-BACK AND HAD AN UNEVENTFUL LANDING. MECHANIC INSPECTED THE SYSTEM AND REPLACED THE HYDRAULIC SERVICE VALVE. MECHANIC OPS CHECKED THE SYSTEM WITH NO FURTHJan 20, 2003 · N891SK · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA2003011Pump · failedRIGHT FUEL LOW PRESS LIGHT ILLUM. REMOVED AND REPLACED LP FUEL PUMP, OPS CHECK GOOD.Jan 20, 2003 · N184UX · Beech 1900D · Aircraft Fuel Distribution SystemSDR 2003F00111Warning System · activatedFLT 9198 - MIA-TPA - AFTER LANDING, RED LIGHT IN LANDING GEAR HANDLE ILLUMINATED AND LANDING GEAR WARNING HORN WOULD NOT CEASE. RESECURED LANDING GEAR HANDLE LIGHT KNOB. OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY. (M)Jan 17, 2003 · N87552 · Beech 1900D · Landing Gear Position and WarningSDR AMWA6Truss · crackedWHILE PERFORMING AN "H" CHECK ON THE RT ENGINE TRUSS, MAINTENANCE FOUND A CRACK IN THE INBOARD AND OUTBOARD COWLING SUPPORT BRACKETS. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPLACED IT WITH ANOTHER ENGINE TRUSS. TEARDOWN REPORT REVEALED THAT THJan 17, 2003 · N10675 · Beech 1900D · Engine Mount SectionSDR GLBA2003008Cap · brokenNOSE GEAR ACTUATOR CAP BROKE. REMOVED AND REPLACED NOSE GEAR.Jan 17, 2003 · N204GL · Beech 1900D · Landing Gear ActuatorSDR GLBA2003009Bearing · failedREPLACED PROP DUE OVERHAUL FOUND NR 2 BLADE BEARING HAD FAILED. REMOVED AND REPLACED PROP.Jan 17, 2003 · N201GL · Beech 1900D · Propeller Blade SectionSDR GUU2004F00010Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET.Jan 14, 2003 · N81535 · Beech 1900D · Elevator StructureSDR GUU2003F00004Actuator · bypassingDURING APPROACH WHEN LANDING GEAR IS SELECTED DOWN THE AIRCRAFT JOLTS AS THE LEFT GEAR LIGHTS ILLUMINATE. REMOVED AND REPLACED LEFT MLG ACTUATOR. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPERATIONAL CHECK NORMAL.Jan 14, 2003 · N69547 · Beech 1900D · Landing Gear ActuatorSDR GLBA2003007Indicator · stuckABORTED TAKEOFF, LT TORQUE GAUGE STUCK AT 750 LBS. REMOVED AND REPLACED TORQUE IND.Jan 14, 2003 · N96UX · Beech 1900D · Engine BMEP/Torque IndicatingSDR FFS2003F00009Bolt · undertorquedWHILE PERFORMING AN INSPECTION OF THE TAIL SECTION, THE UPPER FOUR ATTACH BOLTS FOR THE VERTICAL STABILIZER FORWARD SPAR WERE SMOKING AND THE WASHERS WERE LOOSE UNDER THE RT SIDE BOLT HEADS. ALL FOUR BOLTS WERE BELOW MINIMUM TORQUE SPECS.Jan 13, 2003 · N575D · Beech 1900D · Vertical StabilizerSDR CA030115003Squat Switch · malfunctioned(CAN) DURING APPROACH, FLT CREW SELECTED GEAR DOWN, HEARD GEAR ACTUATE BUT INDICATION DID NOT IDENTIFY THREE GREEN. CREW WAS CONFIDENT THAT GEAR WAS DOWN BUT SELECTED AND PERFORMED MANUAL GEAR EXTENSION AS PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT. LT MAIN Jan 13, 2003 · Beech 1900D · Landing Gear Position and WarningSDR GLBA2003005Shutoff Valve · failedRT ENVIRO FAIL ANNUN ILLUM, R&R PRSOV OPS CHECK GOODJan 13, 2003 · N118GL · Beech 1900D · Cabin Pressure Control SystemSDR S2YA03001Compressor · stalledDURING FLIGHT 1044 MKE-GRB THE CREW REDUCED ENGINE TORQUE TO 2200 LBS. THE FIRST OFFICER OBSERVED FLAME COMING OUT OF FROM THE RIGHT ENGINE. THERE NO INSTRUMENT INDICATION OF ANY ENGINE PROBLEMS. THE CREW SHUT DOWN THE RIGHT ENGINE AS A PRECAUTION, DECLAREDJan 12, 2003 · N891SK · Beech 1900D · Turbine Engine Compressor SectionSDR GUU2003F00002Bracket · crackedAT SCHEDULED INSPECTION, THE LT RUDDER TORQUE SHAFT SUPPORT BRACKET WAS FOUND TO BE CRACKED. REMOVED AND REPLACED LT RUDDER TORQUE SHAFT SUPPORT BRACKET.Jan 12, 2003 · N81556 · Beech 1900D · Vertical StabilizerSDR FFS2003F00007Tube · crackedWHILE INVESTIGATING A RT BLEED AIR FAIL ANNUNCIATOR. DISCOVERED THE WELD FOR THE PRESSURE SWITCH CRACKED ON THE RT WING DEICE TUBE, INBOARD OF THE RT INSTRUMENT AIR VALVE. REMOVED TUBE AND DISCOVERED THAT THE B-NUT FLARE WAS MISFORMED AND PARTIALLY RESTRAIGJan 11, 2003 · N575D · Beech 1900D · Airfoil Anti/De-ice SystemSDR GLBA2003003WindshieldFO'S WINDOW CRACKED, R&R FO'S WINDSHIELDJan 11, 2003 · N201GL · Beech 1900D · Window/Windshield SystemSDR GUU2004F00009Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET.Jan 10, 2003 · N17534 · Beech 1900D · Elevator StructureSDR GUU2003F00003Valve · lockedDURING TAXI, BRAKES STUCK. REMOVED AND REPLACED PARKING BRAKE VALVES. OPERATIONAL CHECK GOOD.Jan 10, 2003 · N81556 · Beech 1900D · Landing Gear Brake SystemSDR GLBA2003002Gyro · malfunctionedAMBER ROL INDICATOR OF EADI SEEMED TO BE F/O'S ADF. REMOVED AND REPLACED NR 2 VG, OPS CHECK GOOD.Jan 10, 2003 · N118GL · Beech 1900D · Attitude Gyro and Indicating SystemSDR 046605Switch · out of adjustUPON APPROACH ON FLIGHT 5490, THE AUTOFEATHER SWITCH ARMED ANNUNCIATOR FAILED TO ILLUMINATE. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED THE PEDESTAL SWITCHES. NO PARTS WERE USED. NO TEARDOWN REPORT WILL BE REQUIRED.Jan 9, 2003 · N10675 · Beech 1900D · Propeller Controlling SystemSDR 046592Valve · out of adjustON TAXI, THE LEFT PROPELLER FAILED TO FEATHER MANUALLY. THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED THE FEATHER VALVE. NO PARTS WERE USED. TEARDOWN REPORT WILL NOT BE REQUIRED.Jan 9, 2003 · N139ZV · Beech 1900D · Propeller Feathering/ReversingSDR GLBA2003001Computer · malfunctionedSTALL WARNING HORN WENT OFF AT 60 KTS ON T/O ROLL. CALIBRATED STALL WARNING COMPUTER, TEST FLIGHT SATISFACTORY.Jan 9, 2003 · N240GL · Beech 1900D · Stall Warning SystemSDR 57708Actuator · malfunctionedAPPROACH, L/G HANDLE MOVED TO LWR GEAR, RED INTRANSIT LAMPS FLICKERED, 5-AMP L/G IND ON RT C/B PANEL POPPED. L/G EXTENDED, 3 GEAR DOWN LIGHTS FAILED TO ILLUM, WOULD NOT RESET. TOWER VERIFIED NOSE L/G EXTENDED. MALFUNCTION NOT DUPLICATED ON GROUND. L/G IND Jan 7, 2003 · N126YV · Beech 1900D · Landing Gear ActuatorSDR 046484Annunciator · damagedUPON ARRIVAL,FLIGHT 5481, THE LANDING GEAR HANDLE WAS DOWN. THERE WAS NO GREEN INDICATION ON THE NOSE. THE CREW THEN PERFORMED A MANUAL EXTENSION. THE TOWER CONFIRMED THAT THE GEAR APPEARED DOWN. THE CREW LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPAIRJan 6, 2003 · N174YV · Beech 1900D · Landing Gear Position and WarningSDR AMWA113Rib · crackedDURING INSPECTION THE LEFT I/B WING OF ENG NACELLE RIB THAT SUPPORTS LANDING GEAR POWER PACK WAS FOUND TO BE CRACKED ON TOP SIDE IN RADIOUS OF RIB APPROX 3 INCHES LONG. REPAIRED BY REPLACING RIB ASSY.Jan 2, 2003 · N174YV · Beech 1900D · Nacelle/Pylon, Frame/Spar/RibSDR GLBA2002212InverterLH INVERTER FAILED, R&R INVERTERDec 28, 2002 · N170GL · Beech 1900D · Electrical Power SystemSDR GLBA2002211Thermocouple · faultyLT ENGINE TEMP LIMITED. REMOVED AND REPLACED THERMOCOUPLE, OPS CHECK GOOD.Dec 28, 2002 · N255GL · Beech 1900D · Engine Temperature Indicating SystemSDR GLBA2002209Oil System · lowOIL PRESSURE ON NR 2 ENGINE FLUCTUATES 65 TO 90 ASI. SERVICED RT ENG, OPS CHECK GOOD.Dec 26, 2002 · N219GL · Beech 1900D · Engine Oil Storage (Airframe Furnished)SDR GUU2003F00005Connector · dirtyON PREFLIGHT, THE FIREWALL SHUT OFF HANDLE ILLUMINATES WHEN LEFT FIRE LOOP IS TESTED. CLEANED LEFT FORWARD FIRE LOOP CONNECTOR OPERATIONAL CHECK NORMAL.Dec 24, 2002 · N87551 · Beech 1900D · Fire DetectionSDR GLBA2002208Indicator · malfunctionedABORTED T/O, NO AIRSPEED IND CAPT'S SIDE. PERFORMED OPS AND LEAK CHECK, OPS CHECK GOOD.Dec 23, 2002 · N228GL · Beech 1900D · Airspeed/Mach Indicator
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