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 2010FA0000185Tab · mismanufacturedRECEIVED NEW AILERON TRIM TAB FROM VENDOR. TAB WAS A NEW PART FROM MFG. INCOMING INSP NOTED THE RIVETS THAT SHOULD HAVE BEEN INSTALLED TO SECURE THE ACTUATOR HORN TO THE TAB WERE MISSING. THERE IS ALSO A ROW OF RIVETS, ALONG THE HINGE LINE, THAT WERE MISSINFeb 2, 2010 · N221CJ · Beech 1900D · Aileron TabsSDR 2010F00024Tab · mismanufacturedRECEIVED NEW AILERON TRIM TAB FROM VENDOR. TAB WAS A NEW PART FROM THE MFG. INCOMING INSP NOTED THE RIVETS THAT SHOULD HAVE BEEN INSTALLED TO SECURE THE ACTUATOR HORN TO THE TAB WERE MISSING. THERE IS ALSO A ROW OF RIVETS, ALONG THE HINGE LINE, THAT WERE MISSFeb 2, 2010 · N221CJ · Beech 1900D · Aileron Tab Control SystemSDR GUUA93332012910AValve · stickingAFTER TAKEOFF, WHEN SELECTING GEARS UP NOTHING HAPPENED BECAUSE OF TRIPPED CIRCUIT BREAKER. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR SERVICE VALVE. TEST FLIGHT SATISFACTORY.Jan 29, 2010 · N81533 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA93553012810ADoor Frame · crackedDURING SCHEDULED ROUTINE INSP DISCOVERED FWD AIRSTAIR DOOR FRAME IS CRACKED AT ATTACH POINT AT AIRSTAIR DOOR SNUBBER UPPER ATTACH BRACKET AND LINE SUPPORT BRACKET AT FS 150.00. REMOVED DAMAGED SECTION OF ANGLE AND INSTALLED FRAME ANGLE REPAIR.Jan 28, 2010 · N81535 · Beech 1900D · Fuselage Main, StructureSDR GUUA93932012810ASocket · looseDURING FINAL APPROACH, RT MLG "R" INDICATION INOPERATIVE. RESECURED RT GEAR INDICATION SOCKET. OPS CHECK GOOD.Jan 28, 2010 · N82539 · Beech 1900D · Landing Gear Position and WarningSDR GUUA93332012810ASwitch · brokenAFTER TAKEOFF, TRIED TO PUT THE LANDING GEAR UP HAD TO USE THE DOWN LOCK RELEASE BUTTON TO GET HANDLE UP, GEAR CIRCUIT BREAKER POPPED. RAN QRH RETURNED GEAR HANDLE TO THE DOWN POSITION. RETURNED TO DEPARTURE LANDED WITHOUT INCIDENT. TROUBLESHOT LANDING GEAR Jan 28, 2010 · N81533 · Beech 1900D · Landing Gear SelectorSDR GLBA20100129FSkin · damagedCOMPONENT REPAIR - DURING A LIGHTINING STRIKE INSP OF THE ACFT AN EXIT HOLE WAS FOUND ON THE LT ELEVATOR. THE ELEVATOR WAS REMOVED AND REPLACED. IAW MM 27-30-00. EXIT HOLE IS ON OTBD. T/E HOLE .75" WIDE X .5" DEEP. DETERMINATION THAT THE ELEVATOR REQUIRED AJan 25, 2010 · N182YV · Beech 1900D · Elevator, Plate/SkinSDR GUUA95432012510AUplock Switch · out of adjustDURING CLIMB OUT UP TO 3000 FT LANDING GEAR INTRANSIENT LIGHT , GEAR WARNING HORN ILLUMINATED AND SOUNDED INTERMITTENTLY. REPLACED RT MAIN LANDING GEAR UP LOCK SWITCH LANDING GEAR OPS CHECK NORMAL.Jan 25, 2010 · N87554 · Beech 1900D · Landing Gear Position and WarningSDR GUUA94129012410ALine · leakingDURING FLIGHT HYD LOW LIGHT ILLUMINATED UPON LANDING GEAR EXTENSION, FOUND LARGE HYD FLUID PUDDLE UNDER WING. REPLACED HAND PUMP HYD RETURN LINE. LANDING GEAR OPS CHECK GOOD.Jan 24, 2010 · N17541 · Beech 1900D · Hydraulic System, MainSDR GUUA95432012410AWarning Horn · malfunctionedAFTER TAKEOFF LANDING GEAR HORN GOES OFF AFTER GEAR IS UP. LANDING GEAR OPS CHECK GOOD COULD NOT DUPLICATE.Jan 24, 2010 · N87554 · Beech 1900D · Landing Gear Position and WarningSDR GUUA94653012310ADoor Frame · crackedDURING SCHEDULED ROUTINE INSP DISCOVERED AIRSTAIR DOOR FUSELAGE FRAME CRACKS AT FS 150.60 WL 103.50 AND WL 106.00. REMOVED DAMAGED SECTION OF DOOR FRAME AND INSTALLED FRAME INSERT ANGLE REPAIR.Jan 23, 2010 · N81546 · Beech 1900D · Fuselage Main, StructureSDR GUUA93532012210AControl Handle · intermittentPILOT REPORTED LANDING GEAR CONTROL HANDLE LIGHT ILLUMINATES INTERMITTENTLY WITH POWER AT IDLE. CLEANED GEAR HANDLE PERFORMED LANDING GEAR OPS CHECK COULD NOT DUPLICATE.Jan 22, 2010 · N81535 · Beech 1900D · Landing Gear SelectorSDR GUUA94721012110ABlower · smokeDURING FLIGHT BURNING ODOR IN COCKPIT WITH WHITE SMOKE. ODOR AND SMOKE STOPPED WHEN BLOWERS AND LT BLEED BROUGHT OFF LINE. REPLACED FWD VENT BLOWER OPS CHECK GOOD.Jan 21, 2010 · N69547 · Beech 1900D · Air Distribution FanSDR GUUA94652012010ACable Assy · frayedDURING SCHEDULED ROUTINE INSP DISCOVERED AIRSTAIR DOOR UPPER AFT AND LOWER FWD DOOR CABLES NEED REPLACED. REPLACED UPPER AFT AND LOWER FWD DOOR CABLES. ACFT DOWN FOR STRUCTURAL INSP.Jan 20, 2010 · N81546 · Beech 1900D · Entrance StairsSDR GUUA94532012010ALight · inoperativeDURING APPROACH LANDING GEAR HANDLE BOTTOM HANDLE LIGHT INOPERATIVE. SECURED LANDING GEAR HANDLE BOTTOM LIGHT OPS CHECK GOOD.Jan 20, 2010 · N53545 · Beech 1900D · Landing Gear SelectorSDR GUUA94652011910AHandle · bindingDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT AFT EMERGENCY EXIT INSIDE HANDLE BINDS AND HARD TO REACH FULL TRAVEL TO OPEN. LUBRICATED EMERGENCY EXIT INNER HANDLE, CORE OPS CHECK NORMAL. ACFT DOWN FOR STRUCTURAL INSP.Jan 19, 2010 · N81546 · Beech 1900D · Emergency ExitsSDR GUUA94952011910ADoor · bindingDURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT INSIDE HANDLE BINDS AND HARD TO REACH FULL TRAVEL TO OPEN. LUBRICATED EMERGENCY EXIT INNER HANDLE CORE OPS CHECK NORMAL. ACFT DOWN FOR STRUCTURAL INSP.Jan 19, 2010 · N81546 · Beech 1900D · Emergency ExitsSDR GUUA95052011910AHandle · loosePILOT REPORTED DURING PREFLIGHT, FOUND 6A EMERGENCY EXIT WINDOW HANDLE APPEARS NOT TO BE SECURED. LUBRICATED 6A EMERGENCY EXIT HANDLE OPS CHECKS OK.Jan 19, 2010 · N87550 · Beech 1900D · Emergency ExitsSDR GUUA94353011910AFrame · crackedDURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR FUSELAGE FRAME ANGLE CRACKED AT FS 150.60 AT GAS STRUT LOWER ATTACH POINT. REMOVED DAMAGED SECTION OF ANGLE AND INSTALLED FRAME ANGLE REPAIR.Jan 19, 2010 · N49543 · Beech 1900D · Fuselage Main, FrameSDR GLBA20100118ABoot · sparksSPARKS WERE COMING FROM NR 1 PROP WHEN DE-ICE WAS ENGAGED HAD LARGE BURN MARK ON BOOT. MX R & R THE LT PROPELLER IAW TASKCARD 1900-6110.00. THE OPS CHECK AND LEAK CHECK WERE GOOD PN HC-E4A-3J SN ON HJ2050, SN OFF HJ1695. RII INSPECTIONS WAS SATISFACTORY IAW Jan 18, 2010 · N237YV · Beech 1900D · Propeller/Rotor Anti-Ice/De-Ice SystemSDR GUUA94132011710AActuator · bypassingDURING FLIGHT LANDING GEAR MOTOR RECYCLING IN AIR ABOUT EVERY THREE TO FOUR MINUTES. REPLACED LT MLG ACTUATOR, OPS CHECK GOOD.Jan 17, 2010 · N17541 · Beech 1900D · Landing Gear ActuatorSDR GUUA93352011710ADoor · obstructedPILOT REPORTED PLASTIC INTERIOR OF CABIN DOOR GETS STUCK ON DOOR JAMB WHEN OPENING. REPLACED WELL NUTS AND RESECURED AIRSTAIR DOOR FWD COVER, OPS CHECK GOOD.Jan 17, 2010 · N81533 · Beech 1900D · Passenger/Crew DoorsSDR GUUA93921011710AUnknown · smokeAFTER TAKEOFF BLACK SMOKE CAME FROM UNDER FLOORBOARDS OF ROWS 2 AND 3, ACRID AS IF ELECTRICAL. TURNED THE BLEEDS OFF AND THE SMOKE STOPPED. THE ELECTRICAL ODOR STILL VERY STRONG DECLARED EMERGENCY. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. PERFORMED Jan 17, 2010 · N82539 · Beech 1900D · Air Distribution SystemSDR GUUA93652011510ACable · brokenDURING SCHEDULED ROUTINE INSP DISCOVERED PAX DOOR TOP FWD CABLE BROKEN NEEDS TO BE REPLACED. REPLACED PAX DOOR TOP FWD CABLE.Jan 15, 2010 · N81536 · Beech 1900D · Passenger/Crew DoorsSDR GUUA94532011510AActuator · stuckDURING EXTENDED DOWNWIND LANDING GEAR WARNING HORN SILENCE BUTTON DOES NOT SILENCE GEAR WARNING HORN WHEN POWER LEVERS REDUCED BELOW 87 PERCENT N1 AND LOWER. TROUBLESHOT SYS FOUND STEERING DISCONNECT ACTUATOR STUCK. REPLACED STEERING DISCONNECT ACTUATOR.Jan 15, 2010 · N53545 · Beech 1900D · Landing Gear ActuatorSDR GLBA20100113GSkin · crackedMAJOR REPAIR - DURING A ROUTINE DE-ICE REPLACEMENT, A CRACK WAS FOUND ON THE RT WING AT WS 190.74 AT THE WING BOOT TUBE CONNECTION HOLE, PROTRUDING INBD. CRACK LENGTH APPROX 1.250" IN LENGTH. MX REPAIRED THE CRACK IAW EO 10-1900-87-001. RII INSPECTIONS COMPLJan 13, 2010 · N245GL · Beech 1900D · Leading Edge DevicesSDR GLBA20100112FSkin · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND BETWEEN 2 RIVETS AT FS 290 AND BL 30L ON THE BOTTOM OF THE LT LOWER FUSELAGE AFT OF THE FWD WING SPAR, CRACK APPROX .4" IN LENGTH. MAINT REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSJan 12, 2010 · N231YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA201001111Fcu · out of adjustRT ENGINE AUTOFEATHERED ON APPROACH. MX ADJUSTED THE RT FCU ROD TO SPEED UP THE RT ENGINE TO MATCH THE LT ENG IAW MM 76-10-01. OPS CHECK ON GROUND GOOD. RII INSP FOR FCU RIG COMPLIED WITH IAW TASKCARD 4.3.13. IT WAS SATISFACTORY.Jan 11, 2010 · N253GL · Beech 1900D · Fuel Control/Turbine EnginesSDR GUUA93652011010ADoor · corrodedDURING SCHEDULED ROUTINE MX, DISCOVERED AIRSTAIR DOOR LOWER FWD SKIN EXFOLIATED AND CRACKED AND LOWER AFT AREA DEBONDED. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED INNER SKIN FILLER AND EXTERNAL DOUBLER REPAIR. OPENJan 10, 2010 · N81536 · Beech 1900D · Passenger/Crew DoorsSDR GUUA93352011010ASkin · corrodedDURING SCHEDULED ROUTINE MX, DISCOVERED AIRSTAIR DOOR LOWER FWD SKIN EXFOLIATED AND CRACKED AND LOWER AFT AREA DEBONDED. OPENJan 10, 2010 · N81533 · Beech 1900D · Entrance StairsSDR GLBA20100113FSkin · damagedMAJOR REPAIR - DURING ROUTINE TOWING OF ACFT ON 01/10/2010 THE RT WING CAME INTO CONTACT WITH ANOTHER ACFT RESULTING IN DAMAGE TO THE RT WING BETWEEN WS 183 & WS 236. UPON EVALUATION OF THE DAMAGE, THE AREA WAS DETERMINED TO REQUIRE A MAJOR REPAIR. MX REPAIREJan 10, 2010 · N254GL · Beech 1900D · Wing, Plate/SkinSDR GLBA20100107FSkin · crackedDURING ROUTINE SCHEDULED MX, A SMALL CRACK IN THE SKIN WAS FOUND AT FS 265 2.5" OTBD OF STR 13R. CRACK APPROX .250" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS IAW EO 09-120-53-004. MATERIALS UTLIZED ARE LISTED IN THE Jan 7, 2010 · N231YV · Beech 1900D · Fuselage Main, Plate/SkinSDR CA100108002Relay · failed(CAN) ON APPROACH WHEN CREW SELECTED DOWN GEAR THE CONTROL CB POPPED AND CREW HAD TO MANUALLY EXTEND THE GEAR. UPON ARRIVAL WHEN OUTSIDE THE AIRCRAFT WITH POWER ON THE CREW HEARD THE HYDRAULIC PUMP RUNNING SO THEY TURNED OFF POWER, CONTACTED MAINTENANCE AND WJan 4, 2010 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20100104JFrame · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX 2 CRACKS WERE FOUND AT THE AIRSTAIR DOOR FUSELAGE FRAME AT FS 150 AT THE LWR STRUT MOUNT AREA. CRACKS MEASURE 1" AND 1.25" RESPECTIVELY. MX REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS IAW Jan 4, 2010 · N231YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20100104HStringer · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND AT STRINGER 4R CUTOUT AT FS 288. IT EXTENDS OUTWARD AND DOWNWARD AT A 45 DEG ANGLE. CRACK IS APPROX .4" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED REQUIRED RII INSPECTIONS IAW EO 09-120Jan 4, 2010 · N231YV · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20100104GFrame · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX CRACK WAS FOUND IN THE RT SIDEWALL FRAME AT TS 164 AND STRINGER 9AR CUTOUT. CRACK IS APPROX 1.75" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS IAW EO 09-120-53-001. MATERIALS Jan 4, 2010 · N231YV · Beech 1900D · Fuselage Main, FrameSDR GUUA93652010310AAngle · crackedDURING SCHEDULED ROUTINE INSP DISCOVERED CRACKS ON AIRSTAIR DOOR FRAME INTERIOR ANGLE AT FS 150.50 BETWEEN STINGERS 9L TO 10L. REPAIRED AIRSTAIR DOOR FRAME ANGLE. INSTALLED FRAME ANGLE AND JOINT ANGLES.Jan 3, 2010 · N81536 · Beech 1900D · Passenger/Crew DoorsSDR GLBA20100104FSkin · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND IN THE UPPER FUSELAGE DOME SKIN AT FAS 150. CRACK IS APPROX.3" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS IAW EO 09-120-53-040. MATERIALS UTLIZED ARE LISTEDDec 31, 2009 · N231YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA94652122609ADoor · inoperativePILOT REPORTED AIRSTAIR DOOR WILL NOT OPEN FROM INSIDE. PERFORMED OPS CHECK ON AIRSTAIR DOOR NO DEFECTS NOTED.Dec 26, 2009 · N81546 · Beech 1900D · Entrance StairsSDR GLBA20091223AHandle · deterioratedLANDING GEAR WOULD NOT COME DOWN PERFORMED CHECKLIST AND HAND PUMPED THE GEAR ALL 3 GREEN ANNUNCIATORS ILLUMINATED. MX REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW MM 31-10-00-201, SECTION 5 AND THE OPERATIONAL CHECK WAS GOOD IAW MM 32-30-00.Dec 23, 2009 · N169GL · Beech 1900D · Landing Gear SelectorSDR GLBA200912211ASwitch · deterioratedUPON APPROACH THE PILOTS REPORTED THAT THE LANDING GEAR WOULD NOT COME DOWN. THEY PERFORMED CHECKLISTS AND HAND PUMPED THE GEAR DOWN. ALL 3 GREEN ANNUNCIATORS ILLUMINATED. MX REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW MM 31-10-00-201 SECTION 5Dec 21, 2009 · N231YV · Beech 1900D · Landing Gear Position and WarningSDR GLBA200912211Autofeather Sys · malfunctionedAUTOFEATHER SYS WOULD NOT ARM ON LT ENGINE DURING T/O WITH T/O POWER SET.Dec 21, 2009 · N231Y · Beech 1900D · Propeller Feathering/ReversingSDR GUUA94658121909AWire · chafedAFTER EXECUTING BEFORE LANDING CHECKLIST, LANDING GEAR FAILED TO EXTEND. MANUALLY EXTENDED LANDING GEAR AND LANDED WITHOUT FURTHER INCIDENT. REPAIRED CHAFED WIRE G16C22 AT RT TOP NACELLE.Dec 19, 2009 · N81546 · Beech 1900D · Landing Gear System WiringSDR GUUA94155121409BHinge · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RUDDER CTR HINGE HAS CORROSION. REPLACED RUDDER CTR HINGE.Dec 14, 2009 · N17541 · Beech 1900D · Rudder StructureSDR GUUA94155121409AHinge · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED VERTICAL STABILIZER UPPER RUDDER HINGE HAS CORROSION. REPLACED VERTICAL STABILIZER UPPER RUDDER HINGE.Dec 14, 2009 · N17541 · Beech 1900D · Rudder StructureSDR GUUA95157121409ASkin · delaminatedDURING SCHEDULED ROUTINE MX DISCOVERED WING SKIN DELAMINATED AROUND FUEL ACCESS PANEL 632 AT. REMOVED INTERNAL RING CLEAN AREA AND INSTALLED EXTERNAL REPAIR DOUBLER AROUND FUEL ACCESS PANEL.Dec 14, 2009 · N87551 · Beech 1900D · Wing, Plate/SkinSDR CA091216005Fire Loop · cracked(CAN) PIREP- "IN CRUISE AT 10,000 FEET WE HAD A FIRE WARNING ON THE RT T-HANDLE + MASTER WARNING FLAG. (NO OTHER PARAMETERS OBSERVED OUT OF NORM) EXECUTED ENGINE SHUT DOWN WITH DISCHARGE OF THE FIRE BOTTLE." SUBSEQUENT EMERGENCY CALLED AND LANDED IN YVR. NODec 13, 2009 · Beech 1900D · Fire DetectionSDR GLBA200912111Landing Gear · inoperativeLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MX JACKED THE ACFT AND PERFORMED A GEAR RETRACTION AND EXTENSION TEST IAW MM 32-30-00. THE OPS CHECK WAS GOOD ON THE GROUND. SUBSEQUENT OPS CHECK FLIGHT WAS UNSATISFACTORY. MX REMOVED AND REPLACED THE MLG SQUAT SWDec 11, 2009 · N169GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA94957121009AStringer · corrodedDURING REMOVAL OF MINOR CORROSION FROM LT WING COLLECTOR TANK J STRINGER, DISCOVERED CORROSION OUT OF LIMITS BETWEEN WS 114.25 TO WS 124.25. REMOVED CORROSION AND INSTALLED EXTERNAL REPAIR STRAP.Dec 10, 2009 · N69549 · Beech 1900D · Wing, Longeron/StringerSDR GUUA94652120909ADoor · stiffDURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. INSPECTED CLEANED AND LUBED RT AFT EMERGENCY EXIT. OPS CHECK GOOD.Dec 9, 2009 · N81546 · Beech 1900D · Emergency Exits
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