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 8383606Bolt · looseDURING DETAIL NR 6 INSPECTION, FOUND RUDDER TORQUE TUBE TO CONTROL HORN MOUNT BOLTS LOOSE. REPLACED HORN AND HARDWARE.Nov 7, 2002 · N838CA · Beech 1900D · Rudder Control SystemSDR 044910Truss · crackedWHILE PERFORMING AN "H" CHECK ON LT ENGINE TRUSS, MAINT FOUND A CRACK AT THE OUTBOARD COWLING ATTACH BRACKET. MAINT R & R WITH ANOTHER TRUSS. UPON RECEIPT OF OLD TRUSS, VENDOR DID A REPORT. REPORT REVEALED THAT A CRACK AT BOTH UPPER COWLING BRACKETS AND CHANov 7, 2002 · N171ZV · Beech 1900D · Engine Mount SectionSDR AMWA044723Fuel Control · malfunctionedAFTER LANDING IN NEW ORLEANS, LOUISIANA ON FLIGHT 5518, THE LEFT ENGINE WENT INTO REVERSE. THEN N-1 INDICATOR REACHED 104 PERCENT THE ITT INDICATOR WENT TO 830 DEGREES AND THE TORQUE WENT TO 3800 LBS FOR 5 SECONDS THE LEFT ENGINE WAS THEN SHUTDOWN AND THE AIRNov 3, 2002 · N15YV · Beech 1900D · Fuel Control/Turbine EnginesSDR GLBA2002174Switch · dirtyCARGO DOOR ANNUNCIATOR ILLUMINATED AT 250FL STAYED ILLUMINATED UNTIL SHORT FINAL, CLEANED AND ADJUSTED CARGO DOOR SWITCH OPS CHECK GOODNov 2, 2002 · N96UX · Beech 1900D · Door Warning SystemSDR 044697Squat Switch · malfunctionedAFTER TAKEOFF, FLIGHT 5431, THE LANDING GEAR HANDLE WAS PLACED IN THE UP POSITION. THE LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT AND WAS RETURNED TO THE GATE. THE ENTIRE TIME THE CREW HAD THE GEAR DOWN AND LOCKED INDICATIONov 2, 2002 · N140ZV · Beech 1900D · Landing Gear Position and WarningSDR AMWA044664Engine · failedTHE CREW OF FLIGHT 2500, ABORTED A TAKEOFF AT THE BEGINNING OF THE ROLL WHEN A LOUD BANG WAS HEARD. THE NOISE HAD CAME FROM THE LEFT ENGINE. THE CREW NEVER REACHED TAKEOFF POWER. THE LEFT ENGINE KEPT RUNNING FOR APPROXIMATELY 2-3 MINUTES AFTER THE OCCURRENCNov 1, 2002 · N143YV · Beech 1900D · Engine (Turbine/Turboprop)SDR GLBA2002175Switch · dirtyCABIN DOOR UNSAFE ANNUNCICATOR ILLUMINATED, CLEANED UPPER SWITCH OPS CHECK GOODNov 1, 2002 · N251GL · Beech 1900D · Door Warning SystemSDR GLBA2002176Beta Switch · malfunctionedLEFT TORQUE, PROP, AND FUEL FLOW IND. FLUCTUATE IN FLT. R&R ENGINE BETA LEVER AND LOW PITCH SOLENOID BEARINGSNov 1, 2002 · N94GL · Beech 1900D · Propeller Controlling SystemSDR CA021105006Hub · failed(CAN) UPON DISASSEMBLY OF PROPELLER A C792 BEARING WAS FOUND TO BE CRACKED AND BROKEN. ON FURTHER INVESTIGATION IT WAS FOUND THAT THE BEARING HAD CAUSED DAMAGE TO THE HUB RENDERING IT UNSERVICEABLE.Oct 31, 2002 · Beech 1900D · Propeller Hub SectionSDR 044606Wheel · failedUPON LANDING FLIGHT 2624, THE CREW REPORTED A BAD BRAKE ACTION FROM THE RIGHT BRAKE. THE RIGHT BRAKE PEDAL FELT MUSHY. AFTER THE AIRCRAFT WAS TAXIED, THE CREW INSPECTED THE AIRCRAFT'S RIGHT WHEEL AND FOUND METAL SHAVINGS IN THE WHEEL ASSEMBLY. CHANGED THE LAOct 30, 2002 · N140ZV · Beech 1900D · Wheel/Ski/FloatSDR CA021108012Hub · damaged(CAN) UPON DISASSEMBLY, C792 BEARING WAS FOUND TO BE BROKEN CAUSING DAMAGE TO HUB RENDERING IT UNSERVICEABLE. UPON REMOVING PAINT FROM 3 BLADES, CRACKS WERE DISCOVERED IN THE SHANK AREA IN THE COMPOSITE MATERIAL. AS THIS DAMAGE IS NOT ADDRESSED IN THE O/H MANUOct 30, 2002 · Beech 1900D · Propeller AssemblySDR 044616Wire · failedUPON LANDING IN PITTSBURGH, THE CREW REPORTED THAT THE NOSE GEAR ANNUNCIATOR DID NOT ILLUMINATE IN GEAR DOWN POSITION. THE BULB WAS THEN CHECKED WHICH WAS FOUND TO BE OKAY. THE CREW MANUALLY LOWERED THE GEAR PER THE CHECKLIST. THEN THEY DECLARED AN EMERGENCY LOct 30, 2002 · N231YV · Beech 1900D · Landing Gear System WiringSDR AMWA044606Wheel · failedUPON LANDING, FLIGHT 2624, THE CREW REPORTED A BAD BRAKE ACTION FROM THE RIGHT BRAKE. THE RIGHT BRAKE PEDAL FELT MUSHY. AFTER THE AIRCRAFT WAS TAXIED, THE CREW INSPECTED THE AIRCRAFT'S RIGHT WHEEL AND FOUND METAL SHAVINGS IN THE WHEEL ASSEMBLY . CHANGED THE Oct 30, 2002 · N140ZV · Beech 1900D · Wheel/Ski/FloatSDR AMWA044616Actuator · failedUPON LANDING, FLIGHT 5533, THE CREW REPORTED THAT THE NOSE GEAR ANNUNCIATOR DID NOT ILLUMINATE IN GEAR DOWN POSITION. THE BULB WAS THEN CHECKED WHICH WAS FOUND TO BE OKAY. THE CREW MANUALLY LOWERED THE GEAR PER THE CHECKLIST. THEN DECLARED AN EMERGENCY LANDOct 30, 2002 · N231YV · Beech 1900D · Landing Gear ActuatorSDR L10666Clamp · crackedPROPELLER WAS RECEIVED FOR OVERHAUL AND DURING DYE PENETRANT INSPECTION TWO CRACK INDICATIONS WERE NOTED IN THE BOLT HOLE AREA. THEN AN EDDY CURRENT INSPECTION WAS PERFORMED WHICH CONFIRMED PRIOR INDICATIONS. CLAMP WAS RED TAGGED AND REMOVED FROM SERVICE. PARTOct 30, 2002 · N855CA · Beech 1900D · Propeller Blade SectionSDR NSVA200200003StringerDiscovered during "A", "B" check. Stringer R 10 is cracked at FS 451Oct 30, 2002 · Beech 1900D · Standard Practices/StructuresSDR NSVA200200002Stringer · crackedNom-routine work card inspection- frame at FS 456 has a crack that runs through a rivit hole to the "cutout" where stringer #10 intersects.Oct 30, 2002 · Beech 1900D · Standard Practices/StructuresSDR AMWA044554O-Ring · failedON TAXI OUT, FLIGHT 6841, THE RIGHT BRAKE BECAME MUSHY. THE AIRCRAFT THEN RETURNED TO THE GATE WITH NO FURTHER INCIDENT. THE REASON FOR THE PROBLEM WAS THAT THERE WAS LOW FLUID IN THE RESERVOIR. REMOVED AND REPLACED AN O-RING, SECURED THE FITTING, AND SERVIOct 29, 2002 · N3YV · Beech 1900D · Hydraulic System, MainSDR CA021101004Hub · corroded(CAN) UPON NDT INSPECTION BEARING RETENTION AREAS UNSERVICEABLE DUE TO CORROSION.Oct 25, 2002 · Beech 1900D · Propeller Hub SectionSDR GLBA2002170Anti-Ice System · malfunctionedRT. ENGINE ICE-VANE WOULD NOT EXTEND IN FLIGHT, RIG DOOR OPS CHECK GOODOct 24, 2002 · N153UE · Beech 1900D · Air Intake Anti/De-Ice SystemSDR GLBA2002169Connector · looseLT PROP DE-ICE FLUCUATED 0-3 AMPS IN OFF MODE UP TO 35 AMPS. SECURED LOOSE CONNECTION ON DE-ICE AMMETER IAW M.M AIRCRAFT RELEASED FOR SERVICE.Oct 23, 2002 · N255GL · Beech 1900D · Propeller/Rotor Anti-Ice/De-Ice SystemSDR GLBA2002168Brush Block · damagedRIGHT PROP HEAT SLOWLY DROPS TO ZERO AMPS, DIVERTED AC TO CYS. R&R RIGHT PROP HEAT BRUSH BLOCK.Oct 23, 2002 · N228GL · Beech 1900D · Propeller/Rotor Anti-Ice/De-Ice SystemSDR 044288Handle · failedAFTER THE DEPARTURE FROM ROSWELL, NEW MEXICO TO ALBUQUERQUE NEW MEXICO ON FLIGHT 415, THE LANDING GEAR FAILED TO RETRACT. THERE WAS NO ABNORMAL INDICATIONS IN THE COCKPIT.THE AIRCRAFT CONTINUED ON ITS FLIGHT TO ALBUQUERQUE AND LANDED WITH NO FURTHER INCIDENT. Oct 22, 2002 · N142ZV · Beech 1900D · Landing Gear SelectorSDR 044284Uplock Switch · failedAFTER TAKE OFF FROM ENID OKLAHOMA TO DENVER COLORADO ON FLIGHT 2501, THE CREW RETRACTED THE LANDING GEAR AFTER A POSITIVE RATE OF CLIMB WAS ESTABLISHED. WHEN THE GEAR WAS SELECTED UP, THE GEAR TRANSIT INTRANSIT LIGHT WOULD NOT EXTINGUISH. THEREFORE THE AIRCRAFOct 22, 2002 · N131YV · Beech 1900D · Main Landing GearSDR GLBA2002166Engine · failedNR 2 ENGINE PRODUCED A SEVERE VIBRATION AND EXPELLED SPARKS ON TAKE OFF POWER UP, REMOVED & REPLACED RT ENGINE. OPS CHECK GOOD.Oct 21, 2002 · N249GL · Beech 1900D · Engine (Turbine/Turboprop)SDR S2YA02041Switch · out of adjustFLT 1371 - MKE-LSE - SHORTLY AFTER TAKEOFF, THE CARGO DOOR ANNUNCIATOR ILLUMINATED. THE CREW MADE AN AIR TURN BACK TO MKE. MAINTENANCE INSPECTED THE DOOR, CLEANED AND ADJUST THE MICRO-SWITCHES. THE A/C WAS RETURN TO SERVICE WITH NO FURTHER DEFECTS. (M)Oct 20, 2002 · N145SK · Beech 1900D · Door Warning SystemSDR GLBA2002165Indicator · failedDISC TORQUE INDIATOR FAILED ON TAKE OFF. REMOVED AND REPLACED INDICATOR.Oct 18, 2002 · N251GL · Beech 1900D · Engine BMEP/Torque IndicatingSDR GLBA2002164Controller · out of adjustLEFT PROPELLER 1650 MAX RPM AT TAKE OFF/ADJUSTED LEFT PROP. MAX RPMOct 18, 2002 · N179GL · Beech 1900D · Propeller Controlling SystemSDR 2002F00989Truss · crackedAIRCRAFT 166 WAS IN FOR A STRUCTURAL INSPECTION. WHILE IN MAINTENANCE, THE RT TRUSS WAS DISCOVERED TO HAVE A CRACK AT THE INBOARD AND OUTBOARD UPPER COWLING SUPPORT BRACKETS. REMOVED AND REPLACED THE RT TRUSS. REPORT STATES THAT VENDOR FOUND THE TRUSS CRACKED Oct 16, 2002 · N166YV · Beech 1900D · Engine Mount SectionSDR 044109Switch · dirtyAFTER TAKE OFF FROM ITHACA, NEW YORK TO PHILADELPHIA, PENNSYLVANIA ON FLIGHT 5460, THE CABIN DOOR ANNUNCIATOR ILLUMINATED. THE AIRCRAFT WAS THEN RETURNED TO FIELD WITH NO FURTHER INCIDENT. THE CABIN DOOR ANNUNCIATOR WAS DEFERRED ON THE FOLLOWING MEL 52-1-C. THOct 16, 2002 · N26YV · Beech 1900D · Door Warning SystemSDR GLBA2002163Bulb · burned outLANDING GEAR LIGHT RIGHT SIDE WILL NOT ILLUMINATE, REPLACED BULBOct 14, 2002 · N184UX · Beech 1900D · Landing Gear Position and WarningSDR GLBA2002162Tube · failedAFTER TAKE OFF LT & RT ENVIRONMENTAL FAIL ANNUNCIATORS ILLUMINATED WITH LT BLEED ON AND RT BLEED OFF, REPAIRED RIGHT INSTRUMENT AIR TUBE OPS CHECKED SATISFACTORY.Oct 11, 2002 · N204GL · Beech 1900D · Instrument PanelSDR GLBA2002161Tube · damagedRT BLEED FAIL ANNUNCIATOR ILLUMINATED AFTER TAKE OFF, THEN RT & LT ENVIRONMENTAL FAIL ANNUNCIATOR ILLUMINATED, REPAIRED RT INSTRUMENT AIR TUBEOct 11, 2002 · N204GL · Beech 1900D · Instrument PanelSDR 2002F00990Truss · crackedAIRCRAFT 123 WAS IN FARMINGTON NEW MEXICO FOR A STRUCTURAL INSPECTION. WHILE IN MAINTENANCE, THE RIGHT TRUSS WAS FOUND TO BE CRACKED ON THE INBOARD AND OUTBOARD COWLING SUPPORT BRACKETS. THE CORRECTIVE ACTION WAS THAT THEY REMOVED AND REPLACED THE RIGHT TRUSS.Oct 10, 2002 · N123YV · Beech 1900D · Engine Mount SectionSDR GLBA2002159Generator · failedAIR RETURN, LT GENERATOR TIE OPEN ANNUNCIATOR ILLUMINATED IN FLIGHT, REMOVED AND REPLACED P172 & A257 OPS CHECK GOOD.Oct 8, 2002 · Beech 1900D · DC Generator-AlternatorSDR 043874Control Head · failedWHILE THE AIRCRAFT WAS IN CRUISE FROM RALEIGH-DURHAM, NORTH CAROLINA TO NORFOLK, VIRGINIA THE DISPLAY ON THE NAV CONTROL HEAD 1 BECAME INOPERABLE. THE CREW SMELLED AN ELECTRICAL FUME. THEY TURNED NAV CONTROL HEAD 1 OFF AND THE ELECTRICAL SMELL WENT AWAY. THE COct 8, 2002 · N166YV · Beech 1900D · Navigation System WiringSDR 8303762Bolt · looseDURING DETAIL NR 6 INSPECTION, FOUND RUDDER TORQUE TUBE TO CONTROL HORN MOUNT BOLTS LOOSE. REPLACED HORN AND HARDWARE.Oct 2, 2002 · N830CA · Beech 1900D · Rudder Control SystemSDR GLBA2002156Torque Knee · brokenLEFT MAIN GEAR TORQUE KNEE BROKE ON ROLL-OUT, REPLACED MAIN GEAROct 2, 2002 · N228GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA2002155Control Panel · failedLEFT DC GENERATOR FAILED ON TAKE OFF, REPLACED DC POWER PANEL.Oct 2, 2002 · N257GL · Beech 1900D · DC Generating SystemSDR 043682Motor · failedON AN ATTEMPT TO LAND, THE CREW TRIED TO EXTEND LANDING GEAR, BUT THE CIRCUIT BREAKER POPPED. THEY RESET CIRCUIT BEAKER ND LANDING GEAR STILL WOULD NOT EXTEND. THE CREW PERFORMED AN EMERGENCY EXTENSION. RECEIVED 3 GREEN GEAR DOWN INDICATORS. THE CREW DECLARED Sep 30, 2002 · N13ZV · Beech 1900D · Hydraulic System, MainSDR 043636Switch · looseAFTER DEPARTURE ON FLIGHT 5637, THE CABIN DOOR ANNUNCIATOR ILLUMINATED. THE AIRCRAFT WAS THEN DIVERTED TO PANAMA CITY, FLORIDA WHERE MAINTENANCE INSPECTED THE DOOR AND DEFERRED THE ANNUNCIATOR SYSTEM. THE CORRECTIVE ACTION WAS THAT AFTER THE INSPECTION OF THE Sep 29, 2002 · N3199Q · Beech 1900D · Door Warning SystemSDR GLBA2002153Actuator · failedGEAR WARNING RT SIDE AFTER LANDING, R&R MLG ACTUATOR.Sep 24, 2002 · N261GL · Beech 1900D · Landing Gear ActuatorSDR AMWA5Truss · crackedWHILE PERFORMING AND "H" CHECK ON THE RT TRUSS IN, MECHANICS DISCOVERED A CRACK LOCATED ON THE UPPER RT COWLING BRACKET. THE CRACK WAS ON THE OUTBOARD SIDE OF THE TRUSS. THE CORRECTIVE ACTION WAS THAT THEY REMOVED AND REPLACED THE TRUSS. UPON RECEIPT OF THE TRSep 21, 2002 · N166YV · Beech 1900D · Engine Mount SectionSDR GLBA2002152Gyro · failedBOTH PILOT & CO-PILOT EHSI SCREENS FROZE WHILE TURNING, REMOVED AND REPLACED FIRST OFFICER'S DIRECTIONAL GYRO.Sep 21, 2002 · N251GL · Beech 1900D · Directional Gyro and Indicating SystemSDR JJB2002F00002Bolt · bentDURING INSPECTION OF RUDDER CONTROL SYSTEM, FOUND TORQUE TUBE MOUNT BOLTS LOOSE AND CONTROL HORN MOUNT BOLT BENT. PARTS RETURNED TO MFG FOR ANALYSIS.Sep 20, 2002 · N855CA · Beech 1900D · Rudder StructureSDR AMW2002F00006Switch · stuckWHILE ENROUTE, THE CARGO DOOR ILLUMINATED 60 MILES OUTSIDE OF DESTINATION. THE AIRCRAFT CONTINUED, WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THAT THE SWITCH WAS STUCK. C/A: LUBRICATED THE SWITCH.Sep 20, 2002 · N233YV · Beech 1900D · Door Warning SystemSDR CA020925004Relay · intermittent(CAN) AIRCRAFT DEPARTED AND FLAPS WOULD NOT RETRACT FROM TAKE OFF POSITION. CREW ELECTED TO RETURN AND AN UNEVENTFULL LANDING WAS COMPLETED. DURING TAXI FLAPS RETRACTED. FLAPS WHERE DEEMED TO BE INTERMITTENT AND WHERE DEFERRED AND CB PULLED. AT ARRIVAL TO MAISep 20, 2002 · Beech 1900D · Trailing Edge Flap Control SystemSDR GLBA2002150Gas Generator · seizedLEFT ENGINE FAILED ON TAKE OFF, R&R GAS GENERATOR AND POWER SECTION.Sep 20, 2002 · N195GL · Beech 1900D · Turbine Engine Compressor SectionSDR 043349Pcu · failedUPON ARRIVAL INTO PANAMA CITY, FLORIDA ON FLIGHT 5466, THE LT AND RT AUTO FEATHER SYSTEM FAILED CAUSING THE CONDENSER BLOWER TO POP. THE SYSTEM WAS LOOKED AT BY THE PANAMA CITY MAINTENANCE. THE PROBLEM WAS THAT THE PRINTED CIRCUIT BOARD WAS BAD. THE CORRECTIVESep 19, 2002 · N15YV · Beech 1900D · Propeller Controlling SystemSDR GLBA2002149Gyro · failedNR 1 EHSI HDG RED FLAG, R&R NR 1 DIRECTIONAL GYRO.Sep 18, 2002 · N253GL · Beech 1900D · Directional Gyro and Indicating System
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