Beech 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 2005F00065Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RIGHT CENTER ELEVATOR HINGE BRACKET. (M)Mar 28, 2005 · N87554 · Beech 1900D · Elevator StructureSDR CA050401013Safety Switch · failed(CAN) AFTER TAKEOFF, LANDING GEAR WAS SELECTED UP BUT THE GEAR DID NOT RETRACT. AIRCRAFT RETURNED TO AIRPORT SAFELY. DURING TROUBLESHOOTING MAINTENANCE FOUND THAT THE RT GEAR SAFETY SWITCH WAS FAULTY. SAFETY SWITCH WAS REPLACED WITH NO FURTHER PROBLEMS.Mar 27, 2005 · Beech 1900D · Landing Gear Position and WarningSDR 20030808Spar · crackedHORIZONTAL STAB MAIN SPAR CENTER WEB SKIN CRACKED AT DEICE HOLE IN FOUR PLACES APPROX 1 INCH LONG. REPAIRED PER EO. AIRCRAFT RETURNED TO SERVICE.Mar 26, 2005 · N251GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR 20030809Skin · corrodedDURING ROUTINE INSPECTION, UNDER FUSELAGE SKIN CORROSION WAS FOUND WHERE SKIN BONDS TO AIRCRAFT STRUCTURE FS 243-249 AT STRINGER 16, WL75. ALL AFFECTED SKIN AND CORROSION WAS REMOVED AND REPAIRED PER EO. AIRCRAFT RETURNED TO SERVICE.Mar 25, 2005 · N153GL · Beech 1900D · Fuselage Main, Plate/SkinSDR 69959Wire · damagedCREW REPORTED STRONG ELECTRICAL SMELL IN COCKPIT. FIRST OFFICER OBSERVED SMOKE FROM AVIONICS BAY AREA. ALL AIRCRAFT SYSTEMS WERE OPERATING NORMALLY. REMOVED AND REPLACED INVERTER. NR 1 INVERTER WIRING AT A226 PANEL BROKEN AND LOOSE CAUSING ARCING. REPAIREDMar 25, 2005 · N165YV · Beech 1900D · Electrical Power System WiringSDR 69932Handle · unsecureUPON PREFLIGHT WALK AROUND INSPECTION, CREW NOTICED 6F EMERGENCY DOOR EXTERIOR HANDLE POPPED OUT. MAINTENANCE RESECURED DOOR WITH NO FURTHER INCIDENT. THEREFORE NO PARTS WERE USED.Mar 23, 2005 · N127ZV · Beech 1900D · Emergency ExitsSDR CA050322005Switch · false activation(CAN) DURING TAXI TO DEPART, THE MAIN CABIN DOOR WARNING LIGHT ILLUMINATED. THE DOOR WAS CHECKED VISUALLY AND CONFIRMED CLOSED BUT THE DOOR ANNUNCIATOR WOULD NOT EXTINGUISH. DUE UN-MEL-ABLE, THE AIRCRAFT WAS FERRIED TO MAINTENANCE FACILITY AND THE SWITCH WAS Mar 21, 2005 · Beech 1900D · Door Warning SystemSDR 69805Line · brokenON CLIMBOUT NR 1 PROP RPM DECREASED WITH NO PROP LEVER INPUT. PLACED PROP TO FULL RPM POSITION & RPM DECREASE. TRIED TO MATCH RPM ON BOTH ENG, STOPPED WHEN NR 2 GOOD ENG WAS 1300 RPM. ENG HAD OUT OF SYNC PROP BEAT, ACFT YAWING. TORQUE ON NR 1 ENG ROSE, RPMMar 16, 2005 · N242YV · Beech 1900D · Fuel Controlling SystemSDR 69761Annunciator · illuminatedTHE PILOTS TOOK OFF FROM DUJ ABOUT 60NM FROM PKB. ON LAST FLIGHT OF THE DAY CHECKS, NOTICED THAT WHEN THE SURFACE DEICE WAS CYCLED THAT THE TAIL DEICE AND INBOARD WING DEICE ANNUNCIATORS REMAINED ILLUMINATED, ALONG WITH ABNORMAL INDICATIONS ON THE VACUUM AND Mar 15, 2005 · N143YV · Beech 1900D · Airfoil Anti/De-ice SystemSDR S2YA05024Relay · malfunctionedAFTER TAKEOFF, THE CREW WAS UNABLE TO RETRACT THE GEAR. THE CREW PERFORMED AN AIR TURNBACK. MECHANIC INSPECTED THE AC AND REPLACED THE LANDING GEAR RELAY AND THE POWER PACK MOTOR. (K)Mar 14, 2005 · N91SK · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUU2005F00010Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RT CENTER ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT CENTER ELEVATOR HINGE BRACKET. (K)Mar 13, 2005 · N81533 · Beech 1900D · Elevator StructureSDR 2005F00082Screen · contaminatedFLT - 9141 - FLL/FPO - DURING FLIGHT, DETECTED SMOKE AND FUMES IN THE CABIN. RETURNED TO FLL. LANDED WITHOUT INCIDENT. CLEANED CARBON FROM RIGHT ENGINE INTERNAL SCAVENGE PUMP INLET SCREEN. RAN ENGINE. NO SMOKE OR FUMES DETECTED. (M)Mar 11, 2005 · N81556 · Beech 1900D · Turbine Engine Oil SystemSDR 20030825Window · crackedDURING ROUTINE INSPECTION, EMERGENCY EXIT 4C WINDOW PAN FOUND CRACKED AT RADIUS. REPLACED WINDOW PAN IAW EO. AIRCRAFT RETURNED TO SERVICE.Mar 11, 2005 · N184UX · Beech 1900D · Door WindowsSDR 69686Bulb · burned outUPON GEAR EXTENSION FOR LANDING IN PIT, CREW NOTED NOSE GEAR ANNUNCIATOR DID NOT SHOW GEAR DOWN AND LOCKED. CREW C/W EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE FOUND BULBS BAD. MAINTENANCE RELAMPED ANMar 11, 2005 · N167YV · Beech 1900D · Landing Gear Position and WarningSDR S2YA05023Valve · inoperativeDURING APPROACH, THE CREW REPORT THEY WHERE UNABLE TO EXTEND THE GEAR. THE CREW EXECUTED A MISSED APPROACH AND MANUALLY EXTENDED THE GEAR ACHIEVED 3 GREEN AND PROCEEDED TO LAND WITHOUT INCIDENT. THE AC WAS INSPECTED AND MECHANIC WAS UNABLE TO DUPLICATE THE PMar 10, 2005 · N91SK · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 20030824Bulkhead · crackedDURING ROUTINE INSPECTION, BULKHEAD AT FRAME STATION 492.75 FOUND TO BE CRACKED WHERE IT ATTACHES TO TOP OF CARGO DOOR FRAME. REPAIRED IAW EO. AIRCRAFT RETURNED TO SERVICE.Mar 10, 2005 · N184UX · Beech 1900D · Fuselage Main, BulkheadSDR 20030823Structure · corrodedDURING ROUTINE INSPECTION, CORROSION DISCOVERED AROUND AIRSTAIR DOOR HANDLE APPROX 2 INCH IN DIA AREA REPAIRED IAW EO. AIRCRAFT RETURNED TO SERVICE.Mar 10, 2005 · N184UX · Beech 1900D · Entrance StairsSDR 20030822Frame · crackedDURING ROUTINE INSPECTION, FOUND WEB CRACK ON FRAME FS 466.0 STRINGER 10R. REPAIRED CRACK IAW WITH EO. AIRCRAFT RETURNED TO SERVICE.Mar 10, 2005 · N184UX · Beech 1900D · Fuselage Main, FrameSDR GUU2005F00007Gasket · leakingDURING FLIGHT, RT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. SECURED THE RT ENGINE. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT ENGINE OVERSPEED GOVERNOR GASKET. OPS LEAK CHECK NORMAL. (K)Mar 9, 2005 · N178YV · Beech 1900D · Turbine Engine Oil SystemSDR GUU2005F00012Odor · detectedFLT 9191 - EYW/MCO - DURING FLIGHT, SMELLED SMOKE IN THE COCKPIT. DIVERTED TO RSW. LANDED WITHOUT INCIDENT. CLEANED CARBON FROM INTERNAL SCAVENGE PUMP SCREEN. OPERATIONAL CHECK OF OIL PRESSURE AND OIL TEMPERATURE SYSTEMS NORMAL. NO SMOKE NOTICED IN THE COMar 8, 2005 · N87557 · Beech 1900D · Air Distribution SystemSDR GUU2005F00008Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET. (K)Mar 5, 2005 · N87552 · Beech 1900D · Horizontal Stabilizer StructureSDR CA050307012Relay · intermittent(CAN) CREW REPORTED FLAP MOVEMENT AS INTERMITTENT. MAINTENANCE REPLACED THE FLAP CONTROL RELAY AND THE AIRCRAFT WAS RELEASED. FURTHER INVESTIGATION INTO THE RELAYS IDENTIFIED A KNOWN MANUFACTURER PROBLEM WITH RELAYS PRIOR TO DATE CODE 0444. THE CODE IDENTIFMar 3, 2005 · Beech 1900D · Trailing Edge Flap Control SystemSDR 20030803Autofeather Sys · malfunctionedTHE LT AUTO FEATHER AFX ANNUNCIATOR STARTED FLICKERING THEN EXTINGUISHED COMPLETELY AND THEN EVEN PRESS TO TEST WOULD NOT FUNCTION. PERFORMED AIR RETURN WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE AND SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFMar 2, 2005 · N245GL · Beech 1900D · Propeller Feathering/ReversingSDR 69476Brake · malfunctionedAFTER TAXI OUT LEFT BRAKE WILL NOT RELEASE. PASSENGERS DEPLANED ON TAXIWAY. MTC DETERMINED PARKING BRAKE WAS NOT RELEASING COMPLETELY. A/C RETURNED TO GATE AND PARKING BRAKE DEFERRED PER MEL 32-7. A/C RETURNED TO SERVICE. INSTALLED PARKING BRAKE KNOB.Mar 2, 2005 · N163YV · Beech 1900D · Landing Gear Brake SystemSDR R9E2005F00000Spar · corrodedDURING AN (I) CHECK INSPECTION THE UPPER AND LOWER HORIZONTAL SPAR CAPS WERE FOUND WITH CORROSION IN THE AREA OF THE ELEVATOR HINGES. THIS AREA WAS NOT TREATED OR PRIMED BY THE FACTORY DURING AC MANUFACTURE AND THUS WAS CONDUCIVE TO CORROSION. THIS IS CONSIDMar 1, 2005 · N46AR · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR CA050228007Relay · burned(CAN) DURING APPROACH, CREW ATTEMPTED TO EXTEND THE GEAR BUT REQUIRED MANUAL EXTENSION. MAINTENANCE FOUND THE LANDING GEAR MOTOR RELAY TO BE BURNED IN THE CONTACT AREA. THE RELAY WAS REPLACED AND THE AIRCRAFT RELEASED. THIS OPERATOR HAS HARD TIMED THE RELAYFeb 27, 2005 · Beech 1900D · Landing Gear System WiringSDR 20030802Structure · damagedON ROUTINE INSPECTION, A SMALL LIGHTNING HOLE FOUND ON BOTTOM SIDE OF FUSELAGE DIRECTLY IN FRONT OF AFT PRESS BULKHEAD AT FS 545.50. REPAIRED, AIRCRAFT RETURNED TO SERVICE.Feb 26, 2005 · N150GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GUU2005F00011Valve · failedFLT 9132 - EYW/TPA - DURING TAXI, RIGHT BRAKE LOCKED UP. REMOVED AND REPLACED RIGHT PARKING BRAKE VALVE. (M)Feb 25, 2005 · N81538 · Beech 1900D · Landing Gear Brake SystemSDR S2YA05019Switch · malfunctionedFLT 1071 - SDF-MKE - AFTER TAKEOFF, THE CREW WAS UNABLE TO RAISE THE FLAPS, PERFORMED AIR TURN BACK TO SDF. THE FLAPS WHERE RETRACTED USING THE BYPASS SWITCH AND THE SYSTEM WAS MEL'D. THE MEL WAS CLEAR BY ADJUSTING THE RT FLAP SAFETY SWITCH AND REPLACING THEFeb 25, 2005 · N85SK · Beech 1900D · Trailing Edge Flap Control SystemSDR CA050228006Motor · shorted(CAN) DURING LANDING THE CREW ATTEMPTED TO EXTEND THE GEAR BUT THE GEAR WOULD NOT RESPOND. MANUAL EXTENSION OF THE GEAR WAS COMPLETED. MAINTENANCE FOUND THE HYD PACK MOTOR SHORTED AND INOPERATIVE. THE MOTOR WAS REPLACED AND THE AIRCRAFT RELEASED.Feb 24, 2005 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 2005FA0000498Fork · crackedNDT SHOWS CRACKED IN (2) PLACES ON FORK. (K) (12235)Feb 23, 2005 · Beech 1900D · Propeller AssemblySDR 2005FA0000190Fork · crackedNDT SHOWS CRACKED IN 2 PLACES ON FORK. (K) (REF: 12235)Feb 23, 2005 · Beech 1900D · Propeller SystemSDR 20030801Door · corrodedON ROUTINE STRUCTURAL INSPECTION, THE AIRSTAIR DOOR HAS CORROSION ON INNER SKIN NEAR HANDLE. AFFECTED AREA IS APPROX 5.75" TO 7.5" IN DIA. DOOR REPAIRED, AIRCRAFT RETURNED TO SERVICE.Feb 22, 2005 · N153GL · Beech 1900D · Entrance StairsSDR 69268Handle · unsecureUPON OST FERRY FLIGHT WALK AROUND INSPECTION, CREW NOTICED EMERGENCY EXIT DOOR 6A EXIT HANDLE PARTIALLY OUT. ADVISED MX CONTROL AND EXPERIENCED NO FURTHER INCIDENT. THE DOOR WAS RESECURED, THEREFORE NO PARTS WERE USED.Feb 21, 2005 · N143YV · Beech 1900D · Emergency ExitsSDR CA050222002Relay · burned(CAN) LANDING GEAR WAS SELECTED DOWN BUT THERE WAS NO LANDING GEAR EXTENSION. CREW NOTICED THAT THE TWO AMP LANDING GEAR RELAY CIRCUIT BREAKER, ADJACENT TO THE LANDING GEAR SELECTOR, WAS TRIPPED. LANDING GEAR WAS SELECTED DOWN AND THE MANUAL HANDPUMP USED TO Feb 18, 2005 · Beech 1900D · Landing Gear System WiringSDR GUU2005F00014Blade · failedDURING TAKEOFF ROLL, WITH LT ENGINE AT APPROXIMATELY 1,000 LBS OF TORQUE, UNUSUAL NOISE HEARD. LT ENGINE CEASED. ABORTED TAKEOFF. DETERMINED LT POWER SECTION SEIZED. REMOVED AND REPLACED LT ENGINE ASSEMBLY AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REFeb 16, 2005 · N81538 · Beech 1900D · Turbine SectionSDR 2005F00054Engine · stoppedFLT 9133 - JAX - DURING TAKEOFF ROLL, WITH LEFT ENGINE AT APPROXIMATELY 1,000 LBS OF TORQUE, UNUSUAL NOISE HEARD. LEFT ENGINE CEASED. ABORTED TAKEOFF. DETERMINED LEFT POWER SECTION SEIZED. REMOVED AND REPLACED LEFT ENGINE ASSEMBLY AND ROUTED FAILED UNIT FOFeb 16, 2005 · N81538 · Beech 1900D · Engine (Turbine/Turboprop)SDR 2003795Hinge · shearedDURING ROUTINE STRUCTURAL INSPECTION, CARGO DOOR HINGE HAD SHEARED RIVIT AND BROKEN LUG. CARGO DOOR HINGE WAS REPLACED, AIRCRAFT RETURNED TO SERVICE.Feb 14, 2005 · N179GL · Beech 1900D · Fuselage, Door HingeSDR 2003794Frame · crackedDURING ROUTINE STRUCTURAL INSPECTION, A 1.3 INCH FRAME CRACK WAS DISCOVERED AT FS 450 STRINGER 10R. REPAIRED CRACKED FRAME AREA, AIRCRAFT RETURNED TO SERVICE.Feb 14, 2005 · N179GL · Beech 1900D · Fuselage Main, FrameSDR 2003793Skin · corrodedDURING ROUTINE STRUCTURAL INSPECTION, CORROSION WAS FOUND ON INSIDE SKIN NEAR MAIN PAX DOOR HANDLE DOUBLER APPROX 2" BY 2" AREA. AREA REPAIRED, AIRCRAFT RETURNED TO SERVICE.Feb 14, 2005 · N179GL · Beech 1900D · Fuselage Main, Plate/SkinSDR 2003792Window Frame · crackedON ROUTINE STRUCTURAL INSPECTION, ALL THREE EMERGENCY EXIT WINDOW PANS HAVE CRACKS. WINDOW PANS REPLACED, AIRCRAFT RETURNED TO SERVICE.Feb 14, 2005 · N179GL · Beech 1900D · Fuselage Main, StructureSDR GUU2005F00013Blade · failedDURING FLIGHT, DETECTED SMOKE IN THE COCKPIT AND CABIN. RT ENGINE LOW PRESSURE ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED RT ENGINE. OPERATIONAL CHECK NORMAL. NOTE: VERIFIED TO BE 2ND STAGE PT BLADE FAILURE. (K)Feb 11, 2005 · N87550 · Beech 1900D · Engine (Turbine/Turboprop)SDR S2YA05015Wire · corrodedFLT 1851 - GRR-MKE - AFTER TAKEOFF, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AND THE INSTRANSIT LIGHTS REMAINED ILLUMINATED. THE CREW CONTINUED TO MKE WITH THE GEAR DOWN. MAINTENANCE INSPECTED THE SYSTEM AND FOUND A CORRODED JUMPER WIRE AT A325P1Feb 11, 2005 · N92SK · Beech 1900D · Landing Gear System WiringSDR 2005F00045Engine · malfunctionedFLT - FLL/EYW - DURING FLIGHT, DETECTED SMOKE IN THE COCKPIT AND CABIN. RIGHT ENGINE LOW PRESSURE ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED RIGHT ENGINE. OPERATIONAL CHECK NORMAL. (M)Feb 11, 2005 · N87550 · Beech 1900D · Engine (Turbine/Turboprop)SDR GUUA94053021005ASeat Track · brokenDURING SCHEDULED ROUTINE INSP DISCOVERED RT SEAT TRACK FLOORBOARD ATTACH TAB BROKEN AT FS 380. REPAIRED BROKEN RT SEAT TRACK FLOOR SUPPORT TAB AT FS380.Feb 10, 2005 · N16540 · Beech 1900D · Fuselage, Seat/Cargo Attach FittingsSDR CA050217005Selector Valve · intermittent(CAN) YAW DAMPER KICKED OFF UNCOMMANDED, GEAR SELECTED DOWN WITH NO FUNCTION, IT WAS NOTICED THAT L/G CNTRL C/B WAS TRIPPED, RESET, LANDING WAS UNEVENTFUL. PILOTS CONTINUED, C/B WAS TRIPPED WITH YAW DAMP ON. YAW DAMPER WAS DISENGAGED, C/B RESET, GEAR SELECTFeb 10, 2005 · Beech 1900D · Hydraulic System, MainSDR 2006FA0000149Structure · corrodedAIR STAIR DOOR LOWER CLOSURE, MFG FROM 4130 STEEL, WAS CORRODED THRU UNDER FOLDING STEP. THIS CLOSURE HAD BEEN PREVIOUSLY REPAIRED BY REMOVING CORROSION, TREATING AND A DOUBLER INSTALLED. REMOVED CLOSURE DUE TO CORROSION AND DISBOND FROM DOOR CORE MATERIAL.Feb 7, 2005 · N891SK · Beech 1900D · Fuselage Main, StructureSDR 2003788Spar · crackedDURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1 INCH LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE.Feb 7, 2005 · N100UX · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR S2YA05012Gyro · inoperativeFLT 6116 - IMT-MKE - BEFORE TAKEOFF, THE CREW REPORTED THE FO DISPLAY UNIT WENT BLANK, WHEN THEY TRIED TO RESET IT THE CA DISPLAY WENT BLANK ALSO. THE CREW RETURNED TO THE GATE AND REPORT THE RED ATT AND FD FLAP ON THE FO ADI. THE AIRCRAFT WAS FERRIED BACK TFeb 5, 2005 · N801SK · Beech 1900D · Attitude and Direction Data SystemSDR 20030789Spar · crackedDURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1" LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE.Feb 5, 2005 · N253GL · Beech 1900D · Horizontal Stabilizer, Spar/Rib
Back to Beech 1900D