Beech 1900D

Service difficulty reports · 7,152

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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 GLBA2016120800622Unknown · malfunctionedSIG EVENT, PILOT REPORTED THAT THEY HAD A BLEED AIR FAIL AND DESCENDED TO FL110 AND DROPPED THE MASKS, NO EMER DECLARED. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK. **Dec 8, 2016 · N251GL · Beech 1900D · Passenger Oxygen SystemSDR GLBA2016110700621Warning System · malfunctionedSIG EVENT, PILOT REPORTED THAT WHEN EXTENDING THE LANDING GEAR, LT MAIN GEAR ANNC FAILED TO ILLUMINATE WITH GEAR DOWN, LANDING GEAR INTRANSIT LIGHT DID NOT ILLUMINATE, ANNC ILLUMINATES WITH PUSH TO TEST. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLDec 7, 2016 · N245GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA2016112900619Duct · damagedPILOT REPORTED THAT THE CAPTAIN`S YOKE HAS ADNORMALY HIGHT AMOUNT OF RESISTANCE WHEN PRESSING FORWARD IN LEVEL FLIGHT, NO RESISTANCE WHEN MOVING YOKE AFT. MAINTENANCE FOUND DUCTING IN THE PATHWAY OF THE YOKE SPROKET ASSY AND CHAIN, SECURED DUCTING OUT OF THE WNov 28, 2016 · N100US · Beech 1900D · Elevator Control SystemSDR GLBA2016112900618Rudder Pedal · stiffPILOT REPORTED THAT DURING TAXI THE RUDDER PEDELS ARE EXTREMELY STIFF MAKING IT HARD TO TAXI. MANTENANCE RERACKED THE YAW DAMP COMPUTER, TAXI CHECKS NORMAL.Nov 26, 2016 · N208GL · Beech 1900D · Landing Gear Steering SystemSDR GLBA2016111800617Frame · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE FOUND FUSELAGE FRAME AT BS 183.25 BETWEEN STRINGERS 2R AND 3R CRACKED AT THE INBOARD LOWER CORNER AREA OF DUCT CUTOUT, FRAME COMPLETELY CRACKED, 2" IN LENGTH. MAJOR REPAIR.Nov 18, 2016 · N261GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2016111700616Cable · brokenSIG EVENT, PILOT REPORTED THAT THE LOWER FORWARD CABIN DOOR CABLE BROKEN (HANDRAIL CABLE). MAINTENANCE REMOVED AND REPLACED THE LOWER FORWARD MAIN CABIN DOOR CABLE REF 52-10-02, P/N 1440-43GLA.Nov 16, 2016 · N202UX · Beech 1900D · Passenger/Crew DoorsSDR GLBA2016111400615Cable · brokenPILOT REPORTED THAT THE CABLE BROKE BETWEEN THE CABIN DOOR AND THE SNUBBER. MAINTENANCE REPLACED THE AIRSTAIR DOOR CABLE FROM THE SNUBBER TO THE DOOR.Nov 12, 2016 · N255GL · Beech 1900D · Passenger/Crew DoorsSDR 8EKA20161104019Fuel Line · chafedRETURNED TO BASE AFTER LOW OIL PRESSURE ANNUNCIATOR CAME ON DURING TAXI. FOUND ENGINE IDLING AT 54-59% N1. UPON OPENING ENGINE COWLS FOUND ENGINE BAY WET WITH FUEL. FOUND FUEL LINE BETWEEN FCU AND FUEL PRESSURE TRANSDUCER, P/N 3040637, CHAFFED THROUGH TO WHNov 3, 2016 · N105EV · Beech 1900D · Engine Fuel DistributionSDR 8EKA201609Skin · bulgedCORROSION CRACKING FOUND ON BELLY SKIN BETWEEN BS 273.25 AND 288, BL 0 AND 12 INCHES LEFT AND RIGHT OF SAID BUTT LINE. NO VISUAL CORROSION IS DETECTABLE FROM EITHER INSIDE OR OUTSIDE THE AIRCRAFT. ONLY THE BULGING IN THE SKIN STRUCTURE IS VISIBLE.Sep 15, 2016 · N171CJ · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2016090100609Printed Ckt Board · defectivePILOT REPORTED THAT DURING APPROACH, AUTOFEATHER DISARM ANNUNCIATOR ILLIMINATED WITH BOTH AFX LIGHTS ILLUMINATED. SYSTEM WOULD RESEST IF POWER WAS REDUCED THEN REAPPLIED. THEN AFX DISARM ANNUNCIATOR WOULD ILLUMINATE AGAIN. MAINTENANCE RR PCB A123 PN:129-36Aug 31, 2016 · N192GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA2016082500607Bracket · wornPILOT REPORTED THAT THE LEFT PROPELLER SEEMS LIKE IT TRIES TO AUTOFEATHER FURING FINAL. MAINTENANCE R & R THE BETA ARM LEVER IAW BMM 61-20-00 STEP 2 PN:3054890-01, RR BETA ARM BRACKET BY REMOVING THE 2 NUTS & INSTALLED THE NEW ONE IN REVERSE ORDER PN:3111379-Aug 23, 2016 · N184UX · Beech 1900D · Propeller SystemSDR GLBA2016082400606Trim Panel · unsecurePILOT REPORTED THAT THE AIRSTAIR DOOR AFT TRIM IS LOOSE AND BINGING THE DOOR, PREVENTING THE DOOR FROM OPENING. MAINTENANCE REPLACED THE NUTS AND SECURED THE TRIM PIECE, DOOR OPERATES NORMALLY.Aug 23, 2016 · N165YV · Beech 1900D · Passenger/Crew DoorsSDR GLBA2016082300605Stringer · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE FOUND STRINGER 4R IS CRACKED IN THE RADIUS ON THE FORWARD END. MAJOR REPAIRAug 23, 2016 · N201GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2016081000603Tire · flatPILOT REPORTED THAT DURNG LANDING ROLL OUT, IT BECAME HARD TO KEEP THE ACFT ON THE CENTERLINE. AFTER EXITING THE RUNWAY, CAPTAIN SAW THAT BOTH LT MAIN TIRES WERE FLAT. OPEN.Aug 9, 2016 · N257GL · Beech 1900D · TireSDR GLBA2016080300602Stringer · corrodedDURING A SCHEDULED INSPECTION, MAINTENANCE FOUND STRINGER 16 DEEPLY PITTED WITH CORROSION AT BS 198.25. MAJOR REPAIR.Aug 3, 2016 · N254GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2016080200601Motor · failedPILOT REPORTED THAT THEY HAD A GEAR ISSUE, LOW HYD LIGHT ILLUMINATED, MANUALLY EXTENDED THE GEAR, DECLARED AN EMERGENCY, HAD 3 GREENS ILLUMINATED, LANDED SAFELY. CIRCUIT BREAKER POPPED, RESET, POPPED WITHIN 4 SEC. HYD FLOW LOW ANNUNCIATOR ILLUM IN FLT. HYD Aug 1, 2016 · N251GL · Beech 1900D · Hydraulic Pump (Electric/Engine), MainSDR GLBA2016072600600Bolt · dislodgedMAINTENANCE PERSONNEL NOTED THAT THE AIRSTAIR DOOR ACCUMULATOR TOP ATTACH BOLT FELL OUT OF THE HOUSING. MAINTENANCE ATTACHED THE AIRSTAIR DOOR SNUBBER TOP BOLT IAW TC 1900-5210.01.Jul 23, 2016 · N202UX · Beech 1900D · Passenger/Crew DoorsSDR GLBA2016072600001Bolt · unsecureSIGNIFICANT EVENT, PILOT NOTED THAT THE CABIN DOOR SNUBBER TOP ATTACH BOLT FELL OUT. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK.Jul 23, 2016 · N202UX · Beech 1900D · Passenger/Crew DoorsSDR GLBA2016071500599Bulkhead · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACKED BULKHEAD AT BS 588.1 AND STRINGER 8L ON THE BULKHEAD FLANGE, .5" IN LENGTH. MAJOR REPAIR.Jul 15, 2016 · N254GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2016071500598Bulkhead · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACKED BULKHEAD AT BS 588.1 AND STRINGER 8R ON THE BULKHEAD FLANGE, .4" IN LENGTH. MAJOR REPAIR.Jul 15, 2016 · N254GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2016071400597Frame · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACK AT THE FUSELAGE FRAME AT BS 456, STRINGER 10R. MAJOR REPAIRJul 14, 2016 · N254GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2016071300596Snubber · disconnectedPILOT REPORTED THAT THE AIRSTAIR DOOR SNUBBER ARM CENTER PIVOT BOLT WAS DISCONNECTED. OPENJul 12, 2016 · N195GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA2016071100594Skin · corrodedDURING A SCHEDULED INSPECTION, MAINTENANCE FOUND EVIDENCE OF BELLY CORROSION BETWEEN STRINGERS 15 - 16L ALONG FRAME AT BS 198.25. MAJOR REPAIR.Jul 11, 2016 · N254GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2016070800593Bolt · brokenPILOT REPORTED THAT THE ATTACHING BULT ON THE CABIN DOOR BROKE. MAINTENANCE REPLACED THE BOLT ON THE LOWER END OF THE CABIN DOOR STRUT IAW MM 52-10-01(1)(B) STEPS 9-10, OPS CHECKED GOOD.Jul 5, 2016 · N202UX · Beech 1900D · Passenger/Crew DoorsSDR GLBA2016060600591Master Cylinder · wornPILOT REPORTED THAT THE CAPTAINS SIDE LT BRAKE PEDAL IS NOT HOLDING & WENT TO THE FLOOR. REPLACED THE CAPTAINS LT BRAKE CYLINDER IAW 32-40-06, PN 90-380001-33 & SN 2912 OFF, SN 3549 ON, BRAKE BLEED & OPERATIONS CHECKED GOOD.Jun 3, 2016 · N231YV · Beech 1900D · Master Cylinder/Brake ValveSDR GLBA2016060100590Downlock Switch · inoperativePILOT REPORTED THAT THEY HAD NO NLG INDICATIONS ON GEAR EXTENSION, RAN ABNORMAL CHECKLIST, DECLARED AN EMER & LANDED WITHOUT INCIDENT. R & R THE NOSE GEAR DRAG BRACE DOWN LOCK SWITCH IAW TC 1900-3220.0 REV 1 STEPS 3,4, & 21. PERFORMED GEAR SWING, OPERATIONS May 31, 2016 · N153GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA2016052700589Warning System · false activationTHE CABIN DOOR ANNC ILLUMINATED IN FLIGHT, CREW DECLARED AN EMER, INDICATION SYS WAS MEL'D. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.May 23, 2016 · N245GL · Beech 1900D · Door Warning SystemSDR GLBA2016051900588Stringer · corrodedMAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND CORROSION ON STRINGER 14 AT FS 213.25, APPROX 1.5" BY 2" AREA. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.May 19, 2016 · N251GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2016051700587Angle · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND THE LT HEAVY ANGLE CRACKED ON THE FWD SIDE, .5" IN LENGTH. FOUND TO NOT BE A MAJOR REPAIR, THE PART WILL BE REPLACED VERSES REPAIRED.May 16, 2016 · N251GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA2016051200586Skin · corrodedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND BELLY CORROSION AT FS 213.35 & STRINGER 14L, JUST AFT OF ADF ANTENNA. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.May 11, 2016 · N251GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2016050200585Stringer · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND STRINGER 9F CRACKED, AT JUNCTION WITH CANT BULKHEAD AT FS 588.10, .7" IN LENGTH. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.May 2, 2016 · N251GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2016050200584Stringer · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND STRINGER 9L CRACKED AT JUNCTION WITH CANT BULKHEAD AT FS 588.10, .2" IN LENGTH. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.May 2, 2016 · N251GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2016042500583Pcb · faultyPILOT REPORTED THAT THE AUTOFEATHER ARMED WITH N1 ABOUT 95%, AFX DISABLE ILLUMINATED & RT AUTOFEATHER FAILED TO ARM. REPLACED PCB A123, PN ON & OFF 129-364091-9, SN OFF 446C95, SN ON 925I94, IAW AIM 10-24-01. VERIFIED RIGGING OF ARMING SWITCHES IAW MM 61-21-Apr 24, 2016 · N231YV · Beech 1900D · Propeller Feathering/ReversingSDR GLBA2016042500582Unknown · malfunctionedPILOT REPORTED THAT AFTER TAKEOFF, POWER WAS APPLIED, AFX DISABLE ANNUNCIATOR ILLUMINATED & RT AUTOFEATHER DISARMED, THEN REARMED. THEN AFTER ROTATION, RT AUTOFEATHER DISARMED. ON CLIMB OUT SYS REARMED FOR THE REMAINDER OF THE FLIGHT. SUPPLEMENTAL INFORMATIApr 23, 2016 · N231YV · Beech 1900D · Propeller Feathering/ReversingSDR GLBA2016041400580Unknown · malfunctionedPILOT REPORTED THAT THEY HAD UNSCHEDULED AUTOFEATHER CYCLING ON FINAL. PERFORMED AUTOFEATHER OPERATIONAL CHECKS & COULD NOT DUPLICATE DISCREPANCY SIGNED OFF USING REF 1900DMM 61-21-00. OPERATIONS CHECKED GOOD.Apr 14, 2016 · N153GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA2016040700578Skin · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND THE FUSELAGE BELLY SKIN CORRODED & CRACKED AT FS 213.25 & STRINGER 14R, .2" IN LENGTH. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.Apr 6, 2016 · N202UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2016040800579Autofeather Sys · unknownPILOT REPORTED THAT THE LT ENG AUTO FEATHER CYCLED SEVERAL TIMES ON APPROACH. COMPLIED WITH FCD 1900-08-61-01, NO DEFECTS NOTED.Apr 5, 2016 · N254GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA2016040500577Brace · damagedMAJOR REPAIR. DURING A SCHEDULED INSPECTION, FOUND THE NLG BRACE, RT UPPER ATTACH LUG DAMAGED. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.Apr 1, 2016 · Beech 1900D · Nose/Tail Landing Gear Strut/AxleSDR GLBA2016031800575Support · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE LT SIDEWALL SEAT TRACK SUPPORT, STRINGER 10L, CRACKED IN THE FLANGE BEND RADIUS, AT FS 327.63, 1" IN LENGTH. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPMar 18, 2016 · N184UX · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA2016030200574Panel · crackedMAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE NUTPLATE PANEL FOR THE ACCESS DOOR 632IB, WS 148.2, RT WING LOWER SIDE, 1.4" IN LENGTH. WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.Mar 2, 2016 · N184UX · Beech 1900D · Wing Miscellaneous StructureSDR CA160229004Hose · leaking(CAN) ON APPROACH WITH GEAR SELECTED TO THE DOWN POSITION THE CREW NOTICED THERE WERE NO THREE GREEN OR RED GEAR HANDLE LIGHTS ILLUMINATED. THE GEAR WAS CYCLED A SECOND TIME WITH THE SAME RESULT. THE GEAR RELAY POPPED. THE CREW USED THE MANUAL GEAR EXTENSION PFeb 26, 2016 · Beech 1900D · Hydraulic System, MainSDR GLBA2016021700571Bracket · wornMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE INBD ATTACH BOLT WORN INTO BRACKET ON THE RT INBD FLAP ACTUATOR. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.Feb 15, 2016 · N184UX · Beech 1900D · Trailing Edge FlapsSDR GLBA2016021500570Frame · crackedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND FUSELAGE FRAME FLANGE CRACKED, FROM THE BEND RADIUS TO THE EDGE OF THE FLANGE, FS 150.60 BETWEEN STRINGER 2R & 3R, .75" IN LENGTH. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & REFeb 12, 2016 · N184UX · Beech 1900D · Fuselage Main, FrameSDR GLBA2016021500569Skin · dentedDURING A SCHEDULED INSPECTION, FOUND A DENT IN THE FUSELAGE SKIN, BETWEEN FS 378.25 & 381.25, BELOW STRINGER 12L. DENT APPROX SIZE 2.7 X 2. MAJOR REPAIR.Feb 12, 2016 · N184UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2016021500568Skin · crackedDURING A SCHEDULED INSPECTION, FOUND THE BELLY SKIN AT FS 225.25, BETWEEN STRINGER 16 & 15R, CRACKED APPROX .2" IN LENGTH, EVIDENCE OF CORROSION FROM STRINGER 15R GOING INBD 4 FASTENERS. MAJOR REPAIR.Feb 12, 2016 · N184UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2016021500567Bracket · wornMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE OTBD ATTACH BOLT WORN INTO THE BRACKET OF THE RT INBD FLAP ACTUATOR. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.Feb 12, 2016 · N184UX · Beech 1900D · Trailing Edge FlapsSDR GLBA2016020900566Skin · damagedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND AT FS 281.00, BETWEEN STRINGERS 14L & 13L, A 3" LONG, .5" WIDE WARE IMPRESSION FROM THE HYD LINE & A SMALL PIN HOLE IN THE CTR. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENFeb 8, 2016 · N184UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2016020900565Control Handle · brokenPILOT REPORTED THAT THE LG FAILED TO EXTEND NORMALLY, FOLLOWED CHECKLIST. PERFORMED MANUAL EXTENSION, DOWN WITH 3 GREENS. JACKED ACFT RETRACTED GEAR 10 TIMES, NO DEFECTS NOTED. CHECKED CONTINUITY OF WIRES IAW WDM 32-31-01-01 & 32-31-0202, FROM A316 TO P532,Feb 8, 2016 · N231YV · Beech 1900D · Landing Gear SelectorSDR CA160209004Angle · cracked(CAN) DURING A STRUCTURAL INSPECTION MAINTENANCE FOUND THE RH CLOSING ANGLE CRACKED 1.5 INCHES RFS 303. CLOSING ANGLE CRACK WAS REPAIRED IAW CAS ENGINEERING EA B1900-53-011, RDA-A-RA16-009/D. ORIGINAL SRM CLOSING ANGLE REPAIR REMOVED AND AN EXTENDED REPAIR AFeb 4, 2016 · Beech 1900D · Fuselage Miscellaneous StructureSDR CA160202006Line · melted(CAN) DURING INSPECTION FOUND RT TAILET DE-ICE BOOT NOT INFLATING. HAD POSITIVE INDICATION, DE-ICE BOOT SHOULD BE INFLATED. FOUND DE-ICE LINE TO TAILET MELTED BY TAIL LOG LIGHT. WHEN DE-ICE LINE MELTED IT SEALED LINE COMPLETELY NOT ALLOWING PRESSURE SENSOR Feb 2, 2016 · Beech 1900D · Ice Detection
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