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 GLBA20100716ADownlock Switch · failedPILOT REPORTED THAT NOSE GEAR ANNUNCIATOR FAILED TO ILLUMINATE ON GEAR EXTENSION, PILOTS CONFIRMED THERE WAS A POSITIVE PRESSURE USING THE MANUAL EXTENSION PUMP IN CASE IT WOULD BE REQUIRED, GEAR WAS DOWN AND LOCKED, MANUAL EXTENSION WAS NOT PERFORMED. MAINTENJul 16, 2010 · N240GL · Beech 1900D · Landing Gear Position and WarningSDR GUUA94753071210ANut Plate · missingDURING SCHEDULED ROUTINE INSP, DISCOVERED AFT LOWER COUNTER BALANCE UPPER ATTACH POINT HAS A MISSING NUT PLATE. GAINED ACCESS THROUGH DOOR FRAME SKIN REPLACED BROKEN NUT PLATE AND INSTALLED DOUBLER REPAIR.Jul 12, 2010 · N69547 · Beech 1900D · Fuselage Main, Attach FittingsSDR GLBA201007121Spline · strippedPILOT REPORTED THAT DURING TAKEOFF (CLIMB OUT) ENROUTE, NR 1 ENGINE FAILED & AUTOFEATHERED, ENGINE SHUTDOWN BY ITSELF, THE AIRCRAFT LANDED BACK AT FIELD WITHOUT INCIDENT. MX INSPECTED NR 1 ENGINE GAS GENERATOR FOR ROTATION, NO OBSTRUCTIONS IN THE INTAKE, CHECKJul 12, 2010 · N182YV · Beech 1900D · Engine Fuel PumpSDR GLBA20100712FFrame · crackedDURING A SCHEDULED ROUNTINE INSP A CRACK WAS FOUND IN THE FRAME AT FS 288 STRINGER CUTOUT 4R, .25" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-043. MATERIALS UTILIZED ARE INCLUDED IN THE ENGJul 11, 2010 · N219GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100712GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT THE AIRSTAIR DOOR FRAME ANGLE FS 150.60, AT THE NUTPLATE AREA OF THE DOOR LOWER STRUT MOUNT, AFT UPPER MOUNT HOLES BETWEEN STRINGER 8L & 9L. MAINTENANCE REPAIRED THE AFFECTJul 11, 2010 · N219GL · Beech 1900D · Fuselage Main, FrameSDR GUUA93957071110ASkin · debondedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED FUEL PANELS 542DB, 542CB AND 532FB HAD SEVERE DEBONDING OF DOUBLER RING ACCESS HOLES AT WING SKIN. FABRICATED AND INSTALLED REPAIR DOUBLERS FOR FUEL PANEL ACCESS HOLES.Jul 11, 2010 · N82539 · Beech 1900D · Wing, Plate/SkinSDR GUUA93532071010AHandle · stiffFLIGHT 9295 FKL/DUJ PILOT REPORTED LANDING GEAR HANDLE VERY STIFF TO COME DOWN HAD TO JOGGLE THE HANDLE. COMPLIED WITH LANDING GEAR OPERATIONAL CHECK NO DEFECTS NOTED.Jul 10, 2010 · N81535 · Beech 1900D · Landing Gear SelectorSDR GUUA93532070810APrinted Ckt Board · faultyFLIGHT 9294 FKL/DUJ PILOT REPORTED LANDING GEAR WARNING HORN INTERMITTENT. REPLACED PCB A119, OPERATIONAL CHECK GOOD.Jul 8, 2010 · N81535 · Beech 1900D · Landing Gear Position and WarningSDR GUUA93357070510ASkin · dentedDURING INSPECTION FOUND SKIN DENTS ON SEVERAL AREAS OF RIGHT WING UPPER SKIN BETWEEN WS 236.62 AND WS 249.75. CUT OUT DAMAGED AREAS AND INSTALLED AN INSERTION PATCH AND REPAIR DOUBLERS.Jul 5, 2010 · N81533 · Beech 1900D · Wing, Plate/SkinSDR GUUA93532070510AControl Handle · intermittentFLIGHT 9292 CLE/DUJ DURING DESCENT LANDING GEAR HANDLE ILLUMINATES INTERMITTENTLY WITH POWER AT IDLE WARNING HORN AND NO GEAR UNSAFE LIGHT. REPLACED LANDING GEAR CONTROL HANDLE OPERATIONAL CHECK GOOD.Jul 5, 2010 · N81535 · Beech 1900D · Landing Gear SelectorSDR GUUA95532070310ARelay · failedFLIGHT 9242 MHH/FLL PILOT REPORTED LANDING GEAR DID NOT RETRACT. REPLACED LANDING GEAR MOTOR RELAY, OPERATIONAL CHECK OK.Jul 3, 2010 · N87555 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA94753070110AAngle · crackedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED CRACK APPROXIMATELY 1.75 INCHES AT RADIUS IN HEAVY ANGLE AT LEFT FS 288.0. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE, CLIP AND FASTNERS .Jul 1, 2010 · N69547 · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA94753070110BAngle · crackedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED CRACK APPROXIMATELY 1.75 INCHES AT RADIUS IN HEAVY ANGLE AT FS 288 AND CRACK APPROXIMATELY 1.5 INCHES AT RADIUS IN HEAVY ANGLE AT RIGHT FS 303.Jul 1, 2010 · N69547 · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20100630KSkin · corrodedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP FOUND CORROSION ON BELLY SKIN AT FS 213.25 BETWEEN STRINGER 16L AND 15L, WITH AN AREA OF 1" BY .75". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-042. MATERJun 30, 2010 · N245GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100630JFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT FS 288.00 AT STRINGER 4R CUTOUT, .35" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-041. MATERIALS UTILIZEDJun 30, 2010 · N245GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100630FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT FS 177.35 AT STRINGER 6R CUTOUT, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-038. MATERIALS UTILIZED Jun 30, 2010 · N245GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100630HStringer · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND AT FS 451 ON THE STRINGER 10R ON THE HORIZONTAL PORTION OF THAT STRINGER, .45" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-5Jun 30, 2010 · N245GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20100630GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT F.S. 456 AT STRINGER 10R CUTOUT, .4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-039. MATERIALS UTILIZED Jun 30, 2010 · N245GL · Beech 1900D · Fuselage Main, FrameSDR GUUA93332063010AControl Handle · intermittentFLIGHT 9200, DURING APPROACH WHEN LANDING GEAR IS EXTENDED THE IN TRANSIT LIGHTS IN THE GEAR HANDLE DO NOT ILLUMINATE. REPLACED LANDING GEAR SWITCH CONTROL HANDLE, OPERATIONAL CHECK GOOD.Jun 30, 2010 · N81533 · Beech 1900D · Landing Gear SelectorSDR GUUA94952062910AHand Rail · out of positionFLIGHT 9174 PILOT REPORTED DURING PREFLIGHT FOUND CABIN DOOR HARD TO OPEN. REPOSITIONED CABIN DOOR TOP HANDRAIL CABLE OPERATIONAL CHECKED GOOD.Jun 29, 2010 · N69549 · Beech 1900D · Passenger/Crew DoorsSDR ERAAA201000002Handle · separatedCARGO DOOR HANDLE FELL OFF. REMOVED DOOR HANDLE, REPLACED SNAP RING AND REINSTALLED DOOR HANDLE IAW HB1900D MM 52-30-00.Jun 27, 2010 · N972EA · Beech 1900D · Cargo/Baggage DoorsSDR GLBA20100628GCircuit Board · dirtySUSPECTED AUTOFEATHER - PILOTS REPORTED THAT THE LT AUTO FEATHER SYS DISENGAGED REPEATEDLY IN ALL POWER SETTINGS. MX REMOVED THE A123 PRINTED CIRCUIT BOARD, CLEANED CONTACTS, RE-INSTALLED THE A123 PRINTED CIRCUIT BOARD IAW MX INSTRUCTION 24-01. MX RAN THE ENGIJun 27, 2010 · N255GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20100628FSwitch · dirtySMOKE/SMELL - PILOTS REPORTED THAT WITH THE BATTERY ON, ALL OF THE ANNUNCIATORS REMAINED ILLUMINATED WITH A SLIGHT BURNING SMELL BEING NOTICED. MX REMOVED AND CLEANED THE MICRO SWITCHES ON THE PUSH TO TEST SWITCH. THE OPS CHECK WAS GOOD. REF MM 33-10-00.Jun 27, 2010 · N182YV · Beech 1900D · Indicating/Recording SystemSDR GUUA95221062610AUnknown · odorDURING FLIGHT NOTICED PLASTIC TYPE ODOR COMING FROM FLIGHT DECK. INVESTIGATED FLIGHT DECK FOR ODOR. NO ODOR NOTICED, RAN ENGINES FOR 45 MINUTES WITH ALL ELECTRICAL EQUIPMENT ON AND BLEEDS OPEN NO PLASTIC OR UNUSUAL ODOR NOTED.Jun 26, 2010 · N87552 · Beech 1900D · Air Distribution SystemSDR GUUA93332062510AWire Harness · inoperativePILOT REPORTED UPON DEPARTURE, LANDING GEAR J HOOK WOULD NOT MOVE TO THE LT TO PRESS DOWN LOCK RELEASE TO RETRACT GEAR. REPLACED LT SQUAT SWITCH AND HARNESS, OPS CK NORMAL.Jun 25, 2010 · N81533 · Beech 1900D · Landing Gear System WiringSDR GUUA93734062410AAltimeter · reads lowFLIGHT: 9174 AFTER TAKEOFF CAPTAINS ALTIMETER HAD A 300 FT SPLIT AT 11,000 FT AND 240 FT SPLIT ON LANDING. DECLARED AN EMERGENCY RETURNED TO TPA LANDED WITHOUT INCIDENT. REPLACED CAPTAINS ALTIMETER.Jun 24, 2010 · N38537 · Beech 1900D · Altimeter, Barometric/EncoderSDR GUUA94032062410ABrake · faultedPILOT REPORTED AT TIMES WHEN APPLYING RT BRAKES PEDAL GOES ALL THE WAY TO THE FLOOR WITH NO BRAKE PRESSURE HAVE TO PUMP THE BRAKE TO GET PRESSURE. BLED BRAKES AND REMOVED TRAPPED AIR IN RT BRAKE SYS.Jun 24, 2010 · N16540 · Beech 1900D · Landing Gear Brake SystemSDR CA100625002Engine · damagedRT ENGINE REPORTED RUNNING HOT. ENGINE TROUBLESHOOTING PERFORMED, HSI INSP REQUIRED. UPON INSP OF ENGINE FOUND EXTREME BUCKLES AND SHROUD SEGMENTS DISHED/WARPED. VERY LARGE .030 GAPS BETWEEN CT DISK AND SEGMENTS. CT DISK HAD ALSO RUBBED ON THE GUIDE VANE. Jun 22, 2010 · Beech 1900D · Turbine SectionSDR GUUA95721062210AO-Ring · leakingDURING TEST FLIGHT WITH BLOWERS AND ENVIRONMENTAL ON AN EXTREME ODOR OF JET FUEL COMES THROUGH ACFT. FOUND FUEL LEAK AT RT FUEL FILTER BOWL REPLACED O-RING. PERFORMED ENGINE RUNS, NO EVIDENCE OF FUEL SMELL.Jun 22, 2010 · N87557 · Beech 1900D · Engine Fuel DistributionSDR GLBA20100622FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A CRACK WAS FOUND IN THE FRAME ANGLE AT FS 150 AT THE ATTACH POINT FOR THE LOWER PAX DOOR STRUT MOUNTS UPPER AFT NUTPLATE AREA. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS Jun 21, 2010 · N240GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100622HSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION CRACKS WERE FOUND IN THE UPPER SKIN AT FS 273.25 BETWEEN STRINGER 1 AND STRINGER 3R, CRACKS RANGE FROM .5" TO .7", APPROXIMATELY 7" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRJun 21, 2010 · N240GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100622GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT F.S. 456 AT STRINGER 10R CUTOUT, .35" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-035. MATERIALS UTILIJun 21, 2010 · N240GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100622JFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A .75" CRACK WAS FOUND ON THE FRAME FLANGE AT F.S. 273.25 AND STRINGER 2R CUTOUT OUTBOARD OF STRINGER 2R, AND CRACKED .7" ON THE FRAME FLANGE INBOARD OF STRINGER 2R, AND A CRACK .7" I/B OF STRINGER 10R. MAIJun 21, 2010 · N240GL · Beech 1900D · Fuselage Main, FrameSDR GUUA94952061910ADoor · bindingPILOT REPORTED CABIN DOOR DIFFICULT TO OPEN. CLEANED EXCESS GREASE FROM LOCKING MECHANISM, OPS CK GOOD.Jun 19, 2010 · N69549 · Beech 1900D · Passenger/Crew DoorsSDR GUUA93932061810BIndication Sys · malfunctionedDURING APPROACH, UPON LANDING, GEAR SELECTED. GEAR DOWN RT GEAR ANNUNCIATOR DID NOT ILLUMINATE, AFTER CYCLING GEAR THE A SECOND TIME THE RT GEAR ANNUNCIATOR ILLUMINATED. PERFORMED RT LANDING GEAR DOWNLOCK. OPS CHECK AND PERFORMED LANDING GEAR OPS CHECK COULJun 18, 2010 · N82539 · Beech 1900D · Landing Gear Position and WarningSDR GUUA93932061810ALanding Gear · malfunctionedAFTER TAKEOFF HAD TO USE DOWNLOCK TO RAISE LANDING GEAR. CHECKED RT SAFETY SWITCH AND LANDING GEAR CONNECTOR FOR SECURITY NO DEFECTS NOTED OPS CK NORMAL.Jun 18, 2010 · N82539 · Beech 1900D · Main Landing GearSDR GUUA94952061710ACable Assy · frayedDURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR LWR FWD CABLE FRAYED. REPLACED AIRSTAIR DOOR LOWER FWD CABLE.Jun 17, 2010 · N69549 · Beech 1900D · Entrance StairsSDR GUUA94353061610ASkin · corrodedDURING SCHEDULED ROUTINE MX, DISCOVERED FUSEALGE BELLY SKIN EXFOLIATION AT FS 423.25 STRINGER 16. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL DOUBLER REPAIR.Jun 16, 2010 · N49543 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA95757061510AStructure · damagedPILOT REPORTED CHECK FOR BIRD STRIKE ON RT OTBD WING. FOUND BIRD STRIKE ON RT OTBD WING L/E REPAIRED DAMAGED SECTION OF WING.Jun 15, 2010 · N87557 · Beech 1900D · Wing Main, Frame StructureSDR GLBA20100617FConnector · not seatedSIG EVENT - PILOT REPORTED THAT WHEN ATTEMPTING TO EXTEND THE LANDING GEAR, GEAR DID NOT EXTEND, IN TRANSIT GEAR HANDLE LIGHT CAME ON INTERMITTANTLY, THEN EXTINGUISHED, WITH HANDLE DOWN, DID NOT RECEIVE 3 GREENS, UPON PERFORMING MANUAL EXTENDED AND RECEIVED 3 Jun 15, 2010 · N173YV · Beech 1900D · Landing Gear System WiringSDR GLBA201006151Unknown · odorSIG EVENT - CREW AND PASSENGERS SMELT SMOKE FOR APPROX. 15 SECONDS DURING DESCENT INTO OLF, SMELL CLEARED AND NO FURTHER EVIDENCE OF FIRE, SWEPT CABIN, CARGO, AND COCKPIT WITH NO EVIDENCE OF FIRE. MAINTENANCE INSPECTED ENVIRONMENTAL SYSTEM, FOUND NO EVIDENCE OJun 15, 2010 · N165YV · Beech 1900D · Air Distribution SystemSDR GUUA93926061310AFire Loop · chafedDURING CLIMB, RT FIRE HANDLE ILLUMINATED. SECURED THE ENG RETURNED TO AIRPORT, LANDED WITHOUT INCIDENT. REPLACED RT ENG FWD FIRE LOOP CABLE. OPS CHECK GOOD.Jun 13, 2010 · N82539 · Beech 1900D · Fire DetectionSDR GLBA20100618GSpar · damagedMAJOR REPAIR UPON SUBSEQUENT INSPECTION MAINTENANCE FOUND LEFT FORWARD SPAR AFT LOWER FLANGE FOUND TO HAVE BEEN DAMAGED BY LEFT DRAG BRACE NEXT TO UPLOCK BRACKET IN LEFT WHEEL WELL. DAMAGE AT BL 107.0 TO 99.0 AND 104.5 TO 101.5 DELAMINATION IS APPROX 8 " LONGJun 12, 2010 · N195GL · Beech 1900D · Wing SparSDR GLBA20100615FArm · failedSIG EVENT - UPON LANDING IN "DEN" THE LEFT HAND MAIN LANDING GEAR COLLAPSED CAUSING SIGNIFICANT DAMAGE TO THE LEFT MAIN LANDING GEAR AND ASSOCIATED SPAR AREA. IT HAS BEEN ISOLATED AT THIS TIME TO A FAILURE OF THE UPPER DRAG BRACE "A" ARM ASSEMBLY LUGS WHICH BJun 12, 2010 · N195GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA94352061210ACable · frayedDURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR LOWER AFT CABLE FRAYED AND LOWER BELLCRANK LOOSE. REPLACED AIRSTAIR DOOR LOWER AFT CABLE AND ADJUSTED LOWER BELLCRANK SCREWS.Jun 12, 2010 · N49543 · Beech 1900D · Entrance StairsSDR GLBA20100611LFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND IN THE FRAME ANGLE AT FS 150 AT THE ATTACH POINT FOR THE LOWER PAX DOOR STRUT MOUNTS UPPER AFT NUTPLATE AREA. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIJun 11, 2010 · N220GL · Beech 1900D · Fuselage Main, FrameSDR GUUA93757061110AAccess Panel · delaminatedDURING SCHEDULED ROUTINE INSP DISCOVERED LT WING FUEL ACCESS PANEL 542CB LEAKS. REPAIRED DELAMINATED SKIN AT WING ACCESS PANEL 542CB.Jun 11, 2010 · N38537 · Beech 1900D · Wing, Plate/SkinSDR GLBA20100611KFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT FS 164 AT CUTOUT FOR STRINGER 9AR, .15" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-033. MATERIALS UTILIJun 11, 2010 · N220GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100611HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT FS 456 AT STRINGER 10R CUTOUT, .4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-030. MATERIALS UTILIZED ARJun 11, 2010 · N220GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100611JStringer · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND IN STRINGER 10R AT RIVET 1.2" FORWARD OF FRAME AT FS 451, CRACK PASS THROUGH RIVET HOLE .1" ON EACH SIDE. STRINGER CRACKED AT FS 451, LENGTH .5", CRACKS ARE 1.2" APART. MAINTENANCE REPAIREJun 11, 2010 · N220GL · Beech 1900D · Fuselage Main, Longeron/Stringer
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