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 GLBA20120214FSkin · corrodedDURING A SCHEDULED ROUTINE INSP FOUND BELLY CORROSION AT FS 198.25 BETWEEN STRINGER 15 AND 16L, AREA BETWEEN A DOUBLE ROW OF FASTENERS, AREA .75" BY .5". REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-011. MATERIALS UFeb 14, 2012 · N261GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20120214GDoor Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE A/S DOOR ENTRANCE LOWER FRAME CRACKED IN THE AFT CORNER AT FS 176 AND STRINGER 11L, .1250" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 12-1900-53-010. MATERIALS UTFeb 14, 2012 · N261GL · Beech 1900D · Fuselage Main, StructureSDR 29GA93871021012AAttach Bracket · crackedDURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS COWLING ATTACH BRACKET WELD AREA CRACKS AND ENGINE MOUNT ATTACH POINTS WELD AREA CRACKS AND TRUSS TUBE CHAFE. PERFORMED WELD REPAIRS TO ENGINE TRUSS IN ACCORDANCE WITH FAA APPROVED DATA.Feb 10, 2012 · N81538 · Beech 1900D · Engine Cowling SystemSDR GLBA20120210GFrame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE STRINGER CUTOUT OF FRAME AT STRINGER 9AR AND FS 150.6, .2" IN LENGTH. REPAIRED IAW EO 12-1900-53-009. MAJOR REPAIR.Feb 9, 2012 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20120210FAngle · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS, EACH .4 INCHES IN LENGTH IN THE VERTICAL ANGLE FS 107 JUST BELOW AND FWD OF THE RT OPENABLE WINDOW. REPAIRED IAW EO 12-1900-53-008. MAJOR REPAIR.Feb 9, 2012 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20120209FCircuit Board · damagedPILOT REPORTED THAT THE LANDING GEAR DID NOT EXTEND WHEN SELECTED AND RELAY CIRCUIT BREAKER TRIPPED, MANUALLY EXTENDED GEAR, NO IN-TRANSIT LIGHTS, LANDED SAFELY. MX REPLACED THE PCB A116 AND THE LANDING GEAR RELAY, OPS CK GOOD.Feb 8, 2012 · N210GL · Beech 1900D · Landing Gear System WiringSDR 29GA94555020812AHinge · corrodedDURING SCHEDULED ROUTINE C-6 INSPECTION DISCOVERED RIGHT ELEVATOR OUTBOARD HINGE HAS CORROSION. REPLACED RIGHT ELEVATOR OUTBOARD HINGE.Feb 8, 2012 · N53545 · Beech 1900D · Elevator StructureSDR GLBA20120207FFrame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE FUSELAGE FRAME AT FS 509.5 BETWEEN STRINGER 4L AND 5L AT THE AFT LONG SNUBBER MOUNT.1.5" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-006. MATERIAFeb 7, 2012 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20120207GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND A CRACK ON THE FUSELAGE FRAME AT FS 456 BETWEEN STRINGER 4L AND STRINGER 5L AT THE FORWARD LONG SNUBBER MOUNT, .75" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12Feb 7, 2012 · N251GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20120206GKeelbeam · damagedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT OTBD KEEL UPPER FENDER MOUNT FLANGE HAS OVERSIZED HOLES. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-54-001. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Feb 6, 2012 · N251GL · Beech 1900D · Fuselage Main, KeelSDR GLBA20120206FFrame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON FRAME AT FS 163 AND STRINGER 9AR, .9 INCHES IN LENGTH. REPAIRED IAW EO 12-1900-53-005. MAJOR REPAIR.Feb 6, 2012 · N251GL · Beech 1900D · Fuselage Main, FrameSDR 29GA95757020512ASkin · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT WING TRAILING EDGE TOP HAS HOLE AT WING STATION 153.50. REMOVED DAMAGE AND INSTALLED AN EXTERNAL REPAIR DOUBLER.Feb 5, 2012 · N87557 · Beech 1900D · Wing, Plate/SkinSDR GLBA20120203GDoor Frame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, FOUND THE AIR STAIR DOOR FRAME AFT CORNER AT FS 177.35 CRACKED, 2" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-003. MATERIALS UTILIZED ARE INCLUDED IN THE Feb 3, 2012 · N251GL · Beech 1900D · Fuselage Main, StructureSDR GLBA20120203FAngle · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, FOUND THE RT HEAVY CLOSING ANGLE CRACKED AT FS 288, 1.5" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-004. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Feb 3, 2012 · N251GL · Beech 1900D · Fuselage Miscellaneous StructureSDR 29GA93871020312ATruss · crackedDURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS COWLING ATTACH BRACKET WELD AREA CRACKS AND ENGINE MOUNT ATTACH POINTS WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE TRUSS ATTACH BRACKETS WELD AREAS AND ENGINE MOUNT ATTACH POINTS WELD AREAS IN Feb 3, 2012 · N81538 · Beech 1900D · Engine Mount SectionSDR CA120206001Bracket · bent(CAN) THE ACFT HAD A DOOR UNSAFE LIGHT COME ON IN FLIGHT THAT RESULTED IN THE ACFT DIVERTING TO ANOTHER AIRPORT. THE DOOR WARNING LIGHT SYS WAS INSPECTED WITH NO FAULTS FOUND AND RETURNED TO SERVICE. THE ACFT COMPLETED THE FLIGHT WITH NO PROBLEMS. THE NEXT Jan 31, 2012 · Beech 1900D · Passenger/Crew DoorsSDR 29GA95721012712AEngine · malfunctionedFLIGHT: 4005 TPA/TPA DURING CLIMBOUT LOUD POP CAME FROM LEFT ENGINE FOLLOWED BY SMOKE COMING FROM PILOT AIR VENTS. SECURED AND SHUT DOWN LEFT ENGINE. NO PRIMARY OR SECONDARY INDICATION OF A FIRE. RETURNED TO TPA LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINJan 27, 2012 · N87557 · Beech 1900D · Air Distribution SystemSDR GLBA20120127FB-Nut · leakingPILOT REPORTED AT 22,000 MASTER WARNING WITH A RT LOW OIL PRESSURE ANNUNCIATOR, GOT THE LIGHT AND HAD 2300 LBS OF TORQUE DROPPED TO BELOW 2000 LBS, OIL WAS 45 TO 50, PRECAUTIONARY-SHUTDOWN THE RT ENG & DELCARED AN EMERGENCY. MX FOUND A LOOSE B-NUT ON THE RT EJan 27, 2012 · N192GL · Beech 1900D · Turbine Engine Oil SystemSDR CA120127009Flap System · malfunctioned(CAN) ON FINAL APPROACH, WITH FLAPS SET TO 17 DEG, THE CREW NOTICED THAT THEY WERE HAVING TO APPLY A SUBSTANTIAL AILERON CORRECTION. WHEN THE FLAPS WERE SELECTED FULL DOWN FOR LANDING, NO MOVEMENT WAS NOTED. THE CREW SUSPECTED A SPLIT FLAP CONDITION AND LANDJan 26, 2012 · Beech 1900D · Trailing Edge Flap Control SystemSDR 29GA94052012612BHandle · lack of lubeDURING SCHEDULED ROUTINE C-2 INSPECTION DISCOVERED RIGHT FORWARD EMERGENCY EXIT OUTER HANDLE DOES NOT SPRING OPEN. LUBRICATED RIGHT FORWARD EMERGENCY EXIT OUTER HANDLE OPERATIONAL CHECK NORMAL.Jan 26, 2012 · N16540 · Beech 1900D · Emergency ExitsSDR 29GA94052012612AHandle · lack of lubeREPORT: DURING SCHEDULED ROUTINE C-2 INSPECTION DISCOVERED RIGHT AFT EMERGENCY EXIT INNER AND OUTER HANDLE STIFF TO OPERATE. LUBRICATED RIGHT AFT EMERGENCY EXIT INNER AND OUTER HANDLE OPERATIONAL CHECK NORMAL.Jan 26, 2012 · N16540 · Beech 1900D · Emergency ExitsSDR 29GA93352012612ACable · out of adjustFLIGHT:3570 OLF/BIL PILOT REPORTED LEFT CABIN DOOR CABLE WRAPS AROUND POST MAKING OPENING AND CLOSING THE DOOR DIFFICULT. RE-ADJUSTED DOOR CABLE.Jan 26, 2012 · N81533 · Beech 1900D · Passenger/Crew DoorsSDR 29GA94352012412BHandle · lack of lubeDURING SCHEDULED ROUTINE C-3 INSPECTION DISCOVERED RIGHT FORWARD EMERGENCY EXIT OUTER HANDLE WILL NOT SPRING OPEN. LUBRICATED RIGHT FORWARD EMERGENCY EXIT DOOR OUTER HANDLE.Jan 24, 2012 · N49543 · Beech 1900D · Emergency ExitsSDR 29GA94352012412AHandle · lack of lubeDURING SCHEDULED ROUTINE C-3 INSPECTION DISCOVERED RIGHT AFT EMERGENCY EXIT INNER HANDLE STIFF. LUBRICATED RIGHT AFT EMERGENCY EXIT HANDLE.Jan 24, 2012 · N49543 · Beech 1900D · Emergency ExitsSDR 29GA94132012112APowerpack · lowFLIGHT: 4068 FKL/DUJ AFTER LANDING GEAR HANDLE IS MOVED UP GEAR IN TRANSIT LIGHT AND MOTOR DO NOT ACTUATE FOR 2.4 SECONDS AFTER THIS TIME GEAR RETRACTS AND EXTENDS AS NORMAL. COMPLIED WITH VISUAL INSPECTION OF LANDING GEAR, SERVICED LEVEL OF POWER PACK CYCLEDJan 21, 2012 · N17541 · Beech 1900D · Hydraulic Pump (Electric/Engine), MainSDR 2012F00046Warning Light · illuminatedDURING FLIGHT AT FL235, 'LT BLEED AIR FAIL' ANNUNCIATOR ILLUMINATED. LT BLEED AIR WAS TURNED OFF, WHICH INDUCED A CABIN CLIMB. ACFT FT DESCENDED TO FL 175 BUT CABIN WOULD NOT DESCEND TO BELOW 14,000 ELEVATION. DONNED OXYGEN MASKS AND TURNED ON CABIN OXYGEN.Jan 20, 2012 · N172MJ · Beech 1900D · Central WarningSDR 29GA94132011912AUnknown · lowFLIGHT: 4070 CLE/CLE AFTER DEPARTING AND PUTTING THE GEAR HANDLE UP NOTHING HAPPENED AFTER 1500 FEET LOOKED AT GEAR AND SAW GEAR RELAY CIRCUIT BREAKER WAS POPPED. COMPLIED WITH LANDING GEAR FILLING AND BLEEDING PROCEDURES OPERATIONAL CHECKS GOOD.Jan 19, 2012 · N17541 · Beech 1900D · Landing Gear SystemSDR GLBA20120116FPlacard · missingPILOT REPORTED THAT THE EMERGENCY EVACUATION PLACARD AT 7A IS MISSING. MX REPLACED PLACARD AT SEAT 7A IAW AIM 5.2.2.Jan 13, 2012 · N220GL · Beech 1900D · Placards and MarkingsSDR 29GA93532011012AMotor · defectiveFLIGHT: 4070 FKL/DUJ PILOT REPORTED WHEN LANDING GEAR IS RETRACTED GEAR MOTOR DOES NOT START AND GEAR INTRANSIT LIGHT DOES NOT ILLUMINATE FOR 2 TO 3 SECONDS, GEAR RETRACTS NORMALLY AFTER THAT TIME. TROUBLESHOT EXTENSION AND RETRACTION HYDRAULIC SYSTEM LOCATEJan 10, 2012 · N81535 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 29GA94521010812AUnknown · odorFLIGHT: 4040 FLL/FLL PILOT REPORTED ON TAKEOFF BURNING PLASTIC SMELL IN COCKPIT WHEN BLEEDS WERE OPENED. VISUALLY INSPECTED BLEED LINES IN WINGS FUSELAGE AND CABIN NO DEFECTS NOTED PERFORMED ENGINE RUNS AT DIFFERENT POWER SETTINGS WITH BLEEDS ON AND OFF, NO SJan 8, 2012 · N53545 · Beech 1900D · Air Distribution SystemSDR GLBA20120109FFrame · corrodedDURING A SCHEDULED ROUTINE INSP, FOUND CORROSION ON THE FRAME AT FS 228.25 APPROX 2" INBD OF STRINGER 14R NEXT TO AN EXISTING REPAIR. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-002. MATERIALS UTILIZED ARE INCLUDEDJan 7, 2012 · N257GL · Beech 1900D · Fuselage Main, FrameSDR 29GA94553010612ASkin · crackedDURING SCHEDULED C-5 INSPECTION DISCOVERED LEFT FUSELAGE SKIN CRACK BETWEEN FS 378.25 TO 393.25. REMOVED SKIN CRACK AND INSTALLED FILLER AND DOUBLER REPAIR.Jan 6, 2012 · N53545 · Beech 1900D · Fuselage Main, Plate/SkinSDR 29GA2012010494153Skin · corrodedDURING SCHEDULED STRUCTURAL INSPECTION DISCOVERED AREA OF CORROSION THROUGH OUTER SKIN AT APPROXIMATELY FS 327.630 STRINGER 16-15R APPROXIMATELY. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED INSERTION PATCH AND AN EXTERNAL DOUBLER REPAIR.Jan 4, 2012 · N17541 · Beech 1900D · Fuselage Main, Plate/SkinSDR 29GA94153010412ASkin · corrodedDURING SCHEDULED STRUCTURAL INSPECTION DISCOVERED AREA OF CORROSION THROUGH OUTER SKIN AT APPROXIMATELY FS 327.630 STRINGER 12L APPROXIMATELY. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED INSERTION PATCH AND AN EXTERNAL DOUBLER REPAIR.Jan 4, 2012 · N17541 · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA201201031Altimeter · failedIN FLIGHT, F/O ALTIMETER BEGAN SMOKING, SAW FLAME AND SMOKE INSIDE OF ALTIMETER, WENT OUT ON ITS OWN AFTER 5-10 SECONDS. MX REPLACED THE ALTIMETER IAW TC 1900-3412.04 AND C/W FAR 43 E(A)(C). OPS CHECKED GOOD.Jan 3, 2012 · N192GL · Beech 1900D · Altimeter, Barometric/EncoderSDR 29GA93952010112AHandle · lack of lubeDURING SCHEDULED C-4 INSPECTION DISCOVERED LEFT EMERGECNY EXIT OUTER HANDLE STIF TO SPRING OPEN. GREASED AND LUBED LEFT EMERGENCY EXIT OUTER HANDLE.Jan 2, 2012 · N82539 · Beech 1900D · Emergency ExitsSDR GLBA20120103FSeat Track · wornMAJOR REPAIR - SEAT TRACK AT FS 423 AND WL 95, CORNER WORN .05", .12" ON LT SIDEWALL. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-001. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Jan 2, 2012 · N178YV · Beech 1900D · Fuselage, Seat/Cargo Attach FittingsSDR 29GA2011123195255Stringer · crackedDURING SCHEDULED C-6 INSPECTION DISCOVERED VERTICAL STABILIZER BAY 331 DL RIGHT OF CANTED RIB 54.026 ONE CRACK AT 39.5% CHORD STRINGER AND ONE CRACK AT VERTICAL STABILIZER BAY 331 CL RIGHT OF CANTED RIB 69.184 AT 49.25% CHORD STRINGER. INSTALLED REPAIRS AT RDec 31, 2011 · N47542 · Beech 1900D · Vertical Stabilizer, Spar/RibSDR 29GA201112394255Stringer · crackedDURING SCHEDULED C-6 INSPECTION DISCOVERED VERTICAL STABILIZER BAY 331 DL RIGHT OF CANTED RIB 54.026 ONE CRACK AT 29.75 STRINGER AND ONE CRACK AT 49.25 PERCENT CHORD STRINGER. REPAIRED.Dec 31, 2011 · N47542 · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA20111229ABulb · inoperativeONE INSTRUMENT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD.Dec 29, 2011 · N245GL · Beech 1900D · Emergency LightingSDR 29GA94152122811AHandle · lack of lubeREPORT: DURING SCHEDULED ROUTINE C-2 INSPECTION DISCOVERED RIGHT FORWARD EMERGENCY EXIT DOOR OUTSIDE HANDLE STIFF (HARD TO OPEN. LUBRICATED RIGHT FORWARD EMERGENCY EXIT DOOR OUTSIDE HANDLE.Dec 28, 2011 · N17541 · Beech 1900D · Emergency ExitsSDR GLBA20111227FSwitch · dirtyCABIN DOOR ANNUNCIATOR ILLUMINATED ON DESCENT THEN EXTINGUISHED SHORTLY AFTER. MX CLEANED THE SWITCH, OPS CHECKED GOOD.Dec 24, 2011 · N154GL · Beech 1900D · Door Warning SystemSDR 29GA94652122211BLinkage · defectiveFLIGHT: 3982 PNS/TPA PILOT REPORTED LOUD RATTLING NOISE COMING FROM WHEEL WELL WITH WITH GEAR EXTENDED. REPLACED NOSE GEAR DOOR RIGHT UPPER BRACKET BUSHING AND RIGHT DOOR LINKAGE AND ROD ENDS.Dec 22, 2011 · N81546 · Beech 1900D · Landing Gear DoorsSDR 29GA94652122211ACam · obstructedFLIGHT: 3982 PNS/TPA PILOT REPORTED CABIN DOOR DIFFICULT TO OPEN FROM INSIDE AIRCRAFT WHEN HANDLE IS LIFTED LOUD CLICKING NOISE IS HEARD. CLEANED EXCESSIVE GREASE FROM TWO UPPER DOOR CAMS OPERATIONAL CHECK NORMAL.Dec 22, 2011 · N81546 · Beech 1900D · Passenger/Crew DoorsSDR GLBA20111222GDoor Frame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND THE AS DOOR FRAME LWR CRACKED AT FS 172, LWR AFT CORNER AREA OF FRAME, .75" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-069. MATERIALS UTILIZED ARE INCDec 22, 2011 · N219GL · Beech 1900D · Fuselage Main, StructureSDR GLBA20111222FCable · tornSIG EVENT - PILOT REPORTED THAT THE AIR STAIR DOOR ROPE HAS TORN RUBBER SHEATHING. MX REPLACED THE UPPER AFT CABLE IAW BMM 52-10-02, PN: 1440-40GLA.Dec 21, 2011 · N257GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20111221FSkin · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE BELLY SKIN CRACKED AT FS 303, 2.3" INBD FROM WING SKIN, .2500" IN LENGTH, SECOND CRACK .1" IN LENGTH, SEPARATED BY .4" THIRD CRACK 1.8" INBD FROM WING SKIN AND IS .6" IN LENGTH. REPAIRED THE AFFECTED AREA AND PDec 21, 2011 · N219GL · Beech 1900D · Fuselage Main, Plate/SkinSDR 29GA95553121811AStringer · debondedDURING SCHEDULED ROUTINE C-3 INSPECTION DISCOVERED SKIN DEBONDED FROM STRINGER AT AFT EVAPORATOR BLOWER APPROXIATELY AT FS 363.25-393.25. REBONDED AND INSTALLED DOUBLER AND FILLER REPAIR TO 10.0 INCH SECTION OF STRINGER TO SKIN.Dec 18, 2011 · N87555 · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20111219GPcb · inoperativePILOT REPORTED THAT THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF, LANDING GEAR RELAY CB TRIPPED. MX REPLACED THE PCB A316, IAW MI 24-01, OPS CHECKED GOOD IAW MI 32-01.Dec 18, 2011 · N220GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20111219FSwitch · dirtyPILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. MX CLEANED THE SWITCH, OPS CHECKED GOOD.Dec 17, 2011 · N211GL · Beech 1900D · Door Warning System
Back to Beech 1900D