Beech 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 GUUA94752022609ADoor · stuckDURING SCHEDULED ROUTINE INSP, DISCOVERED EMERGENCY EXIT AT SEAT 6F WILL NOT PULL FREE FROM FRAME. ADJUSTED SIDE WALL TRIM AND RESET EMERGENCY DOOR.Feb 26, 2009 · N69547 · Beech 1900D · Emergency ExitsSDR GLBA20090227FFuel Tank · damagedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE DAMAGE ON THE LEFT AFT AUXILIARY FUEL TANK WALL WAS DISCOVERED. MAINTENANCE REMOVED AFT WALL OF THE LEFT HAND AUX FUEL TANK. FABRICATED NEW, ALODINED AND PRIMED. REINSTALLED AFT WALL PER EO 09-UE165-02.Feb 26, 2009 · N165YV · Beech 1900D · Fuel StorageSDR GUUA95732022409AUplock Switch · shortedAFTER TAKEOFF, LANDING GEAR UNSAFE RED LIGHT IN HANDLE REMAINS ON AFTER GEAR UP IS SELECTED. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED LT MAIN UPLOCK SWITCH. OPS CHECK NORMAL.Feb 24, 2009 · N87557 · Beech 1900D · Landing Gear Position and WarningSDR GLBA2009022809GKeel · crackedMAJOR REPAIR - DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE LEFT INBOARD KEEL. MAINTENANCE REPAIRED THE LEFT HAND INBOARD KEEL AT FS 321 IAW ENGINEERING ORDER 09-195-01.Feb 23, 2009 · N195GL · Beech 1900D · Fuselage Main, KeelSDR GLBA20090224FSkin · chafedDURING ROUTINE SCHEDULED MX A CHAFE WAS FOUND ON THE BELLYSKIN AT APPROX FS 224.0 BETWEEN STRINGER 15L & 16L. ONE OF THEM WAS 2.9 INCHES IN LENGTH AND THE OTHER WAS 2.4 INCHES IN LENGTH RUNNING PARALLEL TO EACH OTHER. MAINTENANCE REPAIRED THE BELLY SKIN AT FSFeb 23, 2009 · N201GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090224MInsulation · out of positionSMOKE SMELL - ENROUTE FROM "DEN" TO "CYS" THE PILOTS REPORTED A BURNING SMELL AFTER OPENING THE BLEEDS AFTER TAKEOFF. MX FOUND A PIECE OF SIDEWALL INSULATION AGAINST THE RECIRCULATION EJECTOR. MX RE-POSITIONED AND SECURED THE INSULATION. MX RAN THE ACFT WITH FFeb 23, 2009 · N208GL · Beech 1900D · Passenger Compartment EquipmentSDR GLBA200902231Connector · dirtyON TAKEOFF LT ENGINE ITT AT 850 DEG C WITH A TORQUE OF 3200 FT LBS. ABORTED T/O. MAINTENANCE CLEANED THE LEFT ITT CONNECTOR AND PERFORMED GROUND RUNS I.A.W. BEECH 1900D MM 77-20. ALL OPERATIONAL CHECKS WERE GOOD.Feb 23, 2009 · N192GL · Beech 1900D · Fire Protection System WiringSDR GUUA94132022109BCircuit Breaker · unknownFLIGHT: 9233 DURING FLIGHT LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED UNABLE TO RESET. RETURNED TO FLL. REPLACED LANDING GEAR INDICATOR CIRCUIT BREAKER. LANDING GEAR OPERATIONAL CHECK NORMAL.TEST FLIGHT SATISFACTORY.Feb 21, 2009 · N17541 · Beech 1900D · Landing Gear Position and WarningSDR GUUA94132022109AWire · brokenFLIGHT: 9270 DURING APPROACH LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED AFTER GEAR EXTENSION. FOUND BROKEN BROKEN WIRE ON LEFT LANDING GEAR DOWN LOCK CONNECTOR. SPLICED BROKEN WIRE.LANDING GEAR OPERATIONAL CHECK NORMAL.Feb 21, 2009 · N17541 · Beech 1900D · Landing Gear System WiringSDR GLBA20090223PSkin · damagedDURING ROUTINE SCHEDULED MAINTENANCE A HOLE IN THE FUSELAGE WAS FOUND AT F.S. 405.5 LEFT OF STRINGER 14L APPROXIMATELY 1.5 INCHES. HOLE SIZE APPROXIMATELY .375 X .125. MAINTENANCE REMOVED DAMAGE, HOLE .875” CIRCLE, INSTALLED COVER PATCH. COVER PATCH ALODINEDFeb 20, 2009 · N201GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090223NFrame · crackedDURING ROUTINE SCHEDULED MAINTENANCE FOUND A FRAME CRACKED ON THE FORWARD SIDE OF THE AIRSTAIR DOOR ENTRANCE FRAME AT THE LOWER SNUBBER MOUNT BRACKET UPPER NUTPLATE. MAINTENANCE REPAIRED THE AIRSTAIR DOOR ENTRANCE FRAME IAW EO 09-UE201-05.Feb 20, 2009 · N201GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20090220JFrame · crackedDURING ROUTINE SCHEDULED MX A CRACK WAS FOUND ON FRAME AT FS 177.35 STRINGER 9R RELIEF CUTOUT. MAJOR REPAIR, MAINTENANCE DETERMINED THIS DID NOT MEET THE CRITERIA OF A MAJOR REPAIR, HOWEVER, MAINTENANCE REPAIRED THE AFFECTED AREA PER BEECH 1900 SRM 51-70-21.Feb 20, 2009 · N211GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20090220IFrame · crackedDURING ROUTINE SCHEDULED MX CRACK WAS FOUND ON FRAME AT STRINGER 9R FS 163.975 STRINGER RELIEF CUTOUT. MAINTENANCE DETERMINED THIS DID NOT MEET THE CRITERIA OF A MAJOR REPAIR, HOWEVER, MAINTENANCE REPAIRED THE AFFECTED AREA PER BEECH 1900 SRM 51-70-21.Feb 20, 2009 · N201GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20090223HStringer · crackedDURING ROUTINE SCHEDULED MX A CRACK WAS FOUND ON FRAME AT FSS 150.60 STRINGER 9R RELIEF CUTOUT. MAINTENANCE DETERMINED THIS DID NOT MEET THE CRITERIA OF A MAJOR REPAIR, HOWEVER, MAINTENANCE REPAIRED THE AFFECTED AREA PER BEECH 1900 SRM 51-70-21.Feb 20, 2009 · N201GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20090220KAngle · crackedDURING ROUTINE SCHEDULED MX THE LT HEAVY ANGLE WAS FOUND CRACKED AT FS 288.0. MAJOR REPAIR - MAINTENANCE REPAIRED THE RIGHT HAND HEAVY DOUBLER IAW EO 09-201-2. REPAIR APPROXIMATELY 13.5". RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.Feb 20, 2009 · N201GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20090220LAngle · crackedDURING ROUTINE SCHEDULED MX, THE RT HEAVY ANGLE WAS FOUND CRACKED AT FS 288.0. MAINTENANCE REPAIRED THE RIGHT HAND HEAVY DOUBLER I.A.W. .EO. 09-201-2. REPAIR APPROXIMATELY 13.5". PART NUMBER 114-430002-7180. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.Feb 20, 2009 · N201GL · Beech 1900D · Fuselage Main, StructureSDR GUUA95157022009FStringer · corrodedDURING SCHEDULED INSP DISCOVERED RT WING CORROSION INSIDE COLLECTOR TANK ON J STRINGER AFT FLANGE BETWEEN WS 114.25 TO 124.25. CLEANED CORROSION AND INSTALLED EXTERNAL STRAP ON RIGHT WING J STRINGER.Feb 20, 2009 · N87551 · Beech 1900D · Wing, Longeron/StringerSDR GUUA95157022009ESpar · corrodedDURING SCHEDULED INSP, DISCOVERED CORROSION ON RT WING J STRINGER FWD FLANGE AND RT FWD SPAR, FD FLANGE BETWEEN WS 124.58 TO 135.86. CLEANED CORROSION SPOT ALLOWABLE DAMAGE WITHIN LIMITS ALSO CLEANED AND TREATED AND PRIMED SURFACE AREA AT RIGHT WING J STRINGEFeb 20, 2009 · N87551 · Beech 1900D · Wing SparSDR GUUA95157022009DSpar · corrodedDURING SCHEDULED INSP DISCOVERED CORROSION ON RT WING INSIDE COLLECTOR TANK FWD SPAR AFT FLANGE AND K STRINGER FWD FLANGE BETWEEN WS 114.25 TO 124.25. CLEANED CORROSION AT RIGHT FORWARD AFT FLANGE MATERIAL LOSS IS STILL ABOVE DESIGN MINIMUM STRENGTH.CLEANED CFeb 20, 2009 · N87551 · Beech 1900D · Wing SparSDR GUUA95157022009CSpar · corrodedDURING SCHEDULED INSP DISCOVERED CORROSION ON LT WING FWD SPAR FWD FLANGE AND J STRINGER FWD FLANGE BETWEEN WS 124.58 TO 135.86. REMOVED CORROSION AND INSTALLED FILLER AND REPAIR DOUBLER ON LEFT FORWARD SPAR FORWARD FLANGE AND INSTALLED EXTERNAL STRAP ON J STFeb 20, 2009 · N87551 · Beech 1900D · Wing SparSDR GUUA95157022009BStringer · corrodedDURING SCHEDULED INSP DISCOVERED CORROSION ON LT WING INSIDE COLLECTOR TANK ON K STRINGER FWD FLANGE BETWEEN WS 114.25 TO 124.25. INSTALLED EXTERNAL STRAP ON K STRINGER ON LT WING.Feb 20, 2009 · N87551 · Beech 1900D · Wing, Longeron/StringerSDR GUUA95157022009ASpar · corrodedDURING SCHEDULED INSP DISCOVERED CORROSION ON LT WING INSIDE COLLECTOR TANK FWD SPAR AFT FLANGE AND J STRINGER AFT FLANGE BETWEEN WS 114.25 TO 124.25. REMOVED CORROSION INSTALLED INTERNAL STRAP ON LEFT FORWARD SPAR FLANGE AND EXTERNAL STRAP ON J STRINGER.Feb 20, 2009 · N87551 · Beech 1900D · Wing SparSDR GLBA20090223FSkin · crackedDURING ROUTINE SCHEDULED MX THE SKIN OF FUSELAGE WAS FOUND CRACKED AROUND TWO RIVETS ONE ON EACH SIDE OF STRINGER ONE AT F.S. 150.60. MAINTENANCE REMOVED CRACKS BY .750” DIAMETER CUT OUTS. FABRICATED FILLERS FOR LT AND RT SIDE. FABRICATED EXTERNAL PATCH.Feb 20, 2009 · N201GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA94132022009ACircuit Breaker · trippedAFTER TAKEOFF, LANDING GEAR CIRCUIT BREAKER POPPED AFTER GEAR RETRACTED, RESET CIRCUIT BREAKER, STAYED IN THE REST OF THE FLIGHT. PERFORMED OPS CHECK OF LANDING GEAR. OPS CHECK GOOD. COULD NOT DUPLICATE.Feb 20, 2009 · N17541 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20090220BPressure Switch · inoperativeON SHORT FINAL, RT ENGINE HAD ABOUT 5 TO 6 POWER SURGES. DURING THE SURGES, RT TORQUE FLUCTUATED BETWEEN APPROX 500LB-1200LB. FIRST POWER SURGES OCCURED AT APPROX 500LB OF TORQUE AS THE F/O ADVANCED POWER ON BOTH POWER LEVERS FROM 500LB TO 700LB OF TORQUE. Feb 20, 2009 · N255GL · Beech 1900D · Engine (Turbine/Turboprop)SDR GLBA20090223GSkin · corrodedDURING ROUTINE SCHEDULED MX THE SKIN OF THE FUSELAGE IS CORRODED UNDERNEATH FRAME AT FS 203.25 AT STRINGER 15R TOWARDS 16R. LENGTH IS APPROIMATELY 3.5" AND RUNS UNDER FRAME. MX REMOVED DAMAGED SKIN AND INSTALLED INSERTION PATCH AND DOUBLERS. SKIN PATHC 11 X 5.Feb 19, 2009 · N201GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA95255021609CMount · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT ELEVATOR TORQUE TUBE MOUNT BASE EXFOLIATED. REPLACED RIGHT ELEVATOR TORQUE TUBE MOUNT BASE.Feb 16, 2009 · N87552 · Beech 1900D · Elevator StructureSDR GUUA95255021609BHinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED UPPER RUDDER HINGE BRACKET SHOW SIGNS OF EXFOLIATION. REPLACED UPPER RUDDER HINGE BRACKET.Feb 16, 2009 · N87552 · Beech 1900D · Rudder Miscellaneous StructureSDR GUUA95255021609AHinge Bracket · corrodedDURING SCHEDULED ROUTINE MX, DISCOVERED LOWER RUDDER HINGE BRACKET SHOW SIGNS OF EXFOLIATION. REPLACED LOWER RUDDER HINGE BRACKET.Feb 16, 2009 · N87552 · Beech 1900D · Rudder Miscellaneous StructureSDR GLBA20090214BFrame · crackedDURING SCHEDULED STRUCTURAL INSP, A FRAME WAS FOUND CRACKED AROUND 2 RIVETS AT APPROX FS 544.75 AT STRINGERS 1R AND 13R. TWO CRACKS TOTALING .625". MX MANUFACTURED DOUBLER AND REPAIRED AFFECTED AREA IAW EO 09-UE202-05. OUT OF .040 INCH, 2024 T3 AL ALCLAD. MS2Feb 14, 2009 · N202UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20090214DFrame · buckledDURING SCHEDULED STRUCTURAL INSP A FRAME ANGLE WAS FOUND BUCKLED AT THE INTERSECTION OF FS 544.75 AND STRINGER 12R. MX INSTALLED DOUBLER APPROXIMATELY 6" X 4" MADE FROM .040" 2024 T3 AL ALCLAD AND INSTALLED USING MS20470AD RIVETS ANS SEALED WITH AC240 B 1/2. RFeb 13, 2009 · N202UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20090214CFrame · crackedDURING SCHEDULED STRUCTURAL INSP A FRAME CRACK WAS FOUND AROUND ONE RIVET AT FS 544.75 BETWEEN STRINGER 12L AND 13L. ONE CRACK .500" LONG. MX REPAIRED FRAME AT F.S. 544.75 INBD OF STRINGER 12L IAW EO-09-UE202-04. REPAIR ANGLE 4.125" X 2.750", 2024 T3, .040", Feb 13, 2009 · N202UX · Beech 1900D · Fuselage Main, FrameSDR GUUA93657021309BSpar · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED POSSIBLE AREAS OF CORROSION IN LT WING FUEL COLLECTOR TANK ON MAIN SPAR. REMOVED CORROSION ON LEFT MAIN SPAR LOWER CAP AND INSTALLED INTERNAL AND EXTERNAL DOUBLERS.Feb 13, 2009 · N81536 · Beech 1900D · Wing SparSDR GUUA93657021309AStringer · corrodedDURING SCHEDULED INSP DISCOVERED POSSIBLE AREAS OF CORROSION IN LT WING FUEL COLLECTOR TANK FWD BONDED STRINGER. FABRICATED AND INSTALLED REPAIR STRINGER AND FORWARD AND AFT REPAIR DOUBLERS.Feb 13, 2009 · N81536 · Beech 1900D · Wing, Longeron/StringerSDR GLBA20090213CFrame · crackedDURING SCHEDULED STRUCTURAL INSPECTION A FRAME WAS FOUND CRACKED ON THE LEFT SIDE OF STRINGER 1 AT FS 150.60. MAINTENANCE REPAIRED FRAME IAW EO 09-UE202-03.Feb 13, 2009 · N202UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20090220ASkin · distortedMAJOR REPAIR - LEFT HAND INBOARD WING UPPER AFT WING SKIN OUT OF CONTOUR AT STATIONS F.S. 301 W.S. 70 .022" F.S. 311 W.S. 70 .032", F.S. 319 W.S. 70 .035" F.S. 329 W.S. 70 .035". MAINTENANCE REPLACED LT UPPER INBOARD SKIN IAW E.O.-09-165-01.Feb 12, 2009 · N165YV · Beech 1900D · Wing, Plate/SkinSDR GLBA20090213BSkin · crackedMAJOR REPAIR - DURING SCHEDULED STRUCTURAL INSPECTION A SKIN CRACK AT INSERTION OF STRINGER 1 AND FS 150.60 WAS DISCOVERED. MAINTENANCE REPAIRED SKIN CRACK IAW EO 09-UE202-01.Feb 12, 2009 · N202UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090213AFrame · crackedMAJOR REPAIR - DURING SCHEDULED STRUCTURAL INSPECTION A FRAME WAS FOUND CRACKED AT STRINGER 9R AT RELIEF CUTOUT AT FS 163.975. MAINTENANCE REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW EO 09-UE202-02 AT FS 163.975 AND STRINGER 9R, REPAIR APPROXIMATELY 5" Feb 12, 2009 · N202UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20090212ATurnbuckle · obstructedIN FLIGHT AILERON WOULD STICK AND POP LOOSE WHEN TURNING FLIGHT CONTROLS BOTH DIRECTIONS. MAINTENANCE INSPECTED AILERON SYSTEM IAW MM 27-10-02 . FOUND TURNBUCKLE RUBBING ON LIGHTNING HOLE ANTI-CHAFE PROTECTION. REPAIRED PROTECTION AS REQUIRED. MAINTENANCE CFeb 12, 2009 · N122UX · Beech 1900D · Aileron Control SystemSDR GLBA20090212AARib · wornMAJOR REPAIR - DURING SCHEDULED INSPECTION MAINTENANCE THE LEFT FORWARD INBOARD NACELLE KEEL RIB FLANGE WORN AT THE UPPER CORNER AREA AT APPROXIMATELY BL 91.75. MAINTENANCE REPAIRED THE LT FORWARD INBOARD KEEL RIB FLANGE AT THE UPPER CORNER AREA AT APPROXIMATFeb 12, 2009 · N253GL · Beech 1900D · Nacelle/Pylon, Frame/Spar/RibSDR GUUA94355021009CHinge Bracket · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED RT ELEVATOR OTBD HINGE BRACKET HAS EXFOLIATION. REPLACED RT ELEVATOR OTBD HINGE BRACKET.Feb 10, 2009 · N49543 · Beech 1900D · Wing, Control Surface Attach FittingsSDR GUUA94355021009BHinge Bracket · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED RUDDER UPPER HINGE BRACKET HAS EXFOLIATION. REPLACED RUDDER UPPER HINGE BRACKETFeb 10, 2009 · N49543 · Beech 1900D · Rudder/Tab, Attach FittingsSDR GUUA94355021009AHinge Bracket · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED LOWER RUDDER HINGE BRACKET HAS EXFOLIATION. REPLACED LOWER RUDDER HINGE BRACKET.Feb 10, 2009 · N49543 · Beech 1900D · Rudder/Tab, Attach FittingsSDR GUUA95453020909ASkin · damagedDURING SCHEDULED ROUTINE MX DISCOVERED UPPER FORWARD SKYTRACK ANTENNA CONNECTOR HOLE ELONGATED SKIN DAMAGE BETWEEN FS 280.75 AND 303.25. REPAIRED SKIN DAMAGE BY INSTALLING AN EXTERNAL DOUBLER REPAIR.Feb 9, 2009 · N87554 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA95052020709ADoor · stiffDURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT INNER AND OUTER HANDLES. OPS CHECK NORMAL.Feb 7, 2009 · N87550 · Beech 1900D · Emergency ExitsSDR GLBA2009020503Cowling · looseAT 1000FT WITH TORQUE AT 1000'S PROP AT 1550 THE LT ENGINE JUMPED SEVERAL TIMES FROM 50 TO 2000 POUNDS OF TORQUE. MAINTENANCE PERFORMED ENGINE RUNS AND FOUND NO TORQUE SURGE PER BEECH MM 76-10-00. UPON FURTHER INVESTIGATION MAINTENANCE DISCOVERED THE COWLINGFeb 5, 2009 · N184UX · Beech 1900D · Nacelle/Pylon, Main FrameSDR GLBA20090205ACircuit Board · shortedSUSPECTED AUTO FEATHER - PILOTS REPORTED THAT ON SHORT FINAL THE RT ENGINE CYCLED IN AND OUT OF FEATHER. MX R&R THE A123 PRINTED CIRCUIT BOARD AND OPS CHECKED THE SYSTEM IAW MM 61-21-00.Feb 5, 2009 · N210GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20090205DGovernor · malfunctionedSUSPECTED AUTO FEATHER - PILOTS REPORTED THAT THE RT PROPELLER AUTO FEATHERED IN FLIGHT WITH CORRESPONDING ENGINE ISSUE. AUTOFEATHER INOPERATIVE. MX R&R THE RT OVERSPEED GOVERNOR IAW MM 61-20. RIGGED BOTH LOW IDLES AND CORRECTED POWER SPLIT. OPS CHECKS WERFeb 5, 2009 · N153GL · Beech 1900D · Propeller Feathering/ReversingSDR GUUA94952020509ADoor · stiffDURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT DOOR DIFFICULT TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT DOOR INTERIOR LOCKING MECHANISM.Feb 5, 2009 · N69549 · Beech 1900D · Emergency ExitsSDR GLBA20090204AOil System · underservicedOIL PRESSURE GAUGE FLUCTUATES BETWEEN 45-55 PSI IN FLIGHT ON THE NR 1 ENGINE. MX SERVICED ENGINE WITH 2 QUARTS OF OIL IAW EMB-120 12-12.Feb 4, 2009 · N71GL · Beech 1900D · Turbine Engine Oil System
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