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 GLBA2012091700061Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT VSS 84.10, 20 PERCENT CHORD AT 2ND RIVET FROM TOP, 1" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-035. MAJOR REPAIR.Sep 17, 2012 · N192GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012091700060Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE VERT STAB RT FWD SPAR CAP ANGLE AT VSS 84.10, 20 PERCENT CHORD BY 2ND RIVET FROM THE TOP, .5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-036. MAJOR REPAIR.Sep 17, 2012 · N192GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012091700059Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 6 CRACKS IN THE RT LWR FWD BULKHEAD AROUND FASTENERS AT THE EDGE OF THE BULKHEAD, THAT RADIATE FROM FASTENER HOLES AT FS 84.0, 3.6" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-049. MAJOR REPAIR.Sep 17, 2012 · N192GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012091700058Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS IN THE RT LOWER PRESSURE BULKHEAD FWD, AROUND FASTENERS AT THE INBD EDGE OF BULKHEAD, THAT RADIATES FROM FASTENER HOLES AT FS 84.0, 2" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-049. MSep 17, 2012 · N192GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012091700057Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE VERTICAL STAB RT SIDE AFT LWR SPAR SKIN 8.5" UP FROM BOTTOM, 3" IN LENGTH. REPAIRED IAW EO 12-1900-55-038. MAJOR REPAIR.Sep 17, 2012 · N261GL · Beech 1900D · Vertical Stabilizer, Plate/SkinSDR GLBA2012091700056Attach Fitting · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT SPAR CAP ON VERTICAL STAB AT HORIZONTAL STAB ATTACHMENT FITTING AT 2ND FASTENER FROM TOP, VSS 84.10 AT 20 PERCENT CHORD, .875" IN LENGTH. REPAIRED IAW FR-CO-02526, REV 1, STEP 1. MAJOR REPAIR.Sep 17, 2012 · N261GL · Beech 1900D · Elevator Tab, Attach FittingsSDR ERAA20120066Uplock Switch · defectiveON TAKEOFF GEAR INTRANSIT LIGHT FAILED TO EXTINGUISH, RECYCLED GEAR 1 TIME STILL DID NOT EXTIGUISH. OPTED TO CONTINUE TO ANCHORAGE GEAR DOWN, GEAR DOWN INDICATION NORMAL. REMOVED AND REPLACED NLG UPLOCK SWITCH IAW B1900D MAINT MANUAL 32-60-00. COMPLIED WITHSep 15, 2012 · Beech 1900D · Landing Gear Position and WarningSDR CA120918027Actuator · malfunctioned(CAN) THE ACFT HAD RETURNED WITH A LT MAIN GEAR FAILING TO SHOW GREEN ANNUCIATOR FOR DOWN AND LOCKED. THE LANDING GEAR MOTOR RELAY CIRCUIT BREAKER ALSO POPPED AT THIS TIME. THE REASON FOR THIS IS THAT THE INTERNAL SWITCH OF THE GEAR ACTUATOR APPEARED TO HAVSep 14, 2012 · Beech 1900D · Landing Gear ActuatorSDR CA120914004Tube · leaking(CAN) CREW REPORTED FUMES COMING OUT FROM THE VENTILATION SYS. MAINTENANCE FOUND THE LT ENGINE HAD A FUEL PRESSURE DELIVERY TUBE TO THE FUEL FLOW DIVIDER WAS LEAKING NEAR THE COMPRESSOR INTAKE. FUEL MIST WAS BEING DRAWN INTO THE BLEED AIR SYS CAUSING THE FSep 11, 2012 · Beech 1900D · Engine Fuel DistributionSDR GLBA2012091200054Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE VERTICAL STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD TOP FASTENER AT VSS 84.18, .125" IN LENGTH. REPAIRED IAW FR-CO-02520R1 STEP 1. MAJOR REPAIRSep 11, 2012 · N122UX · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012091200053Angle · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND THREE CRACKS ON THE VERTICAL STAB RT SPAR CAP ANGLE AT THE 20 PERCENT CHORD TOP FASTENER AT VSS 84.10, .5" IN LENGTH. REPAIRED IAW FR-CO-02520R1, STEP 1. MAJOR REPAIRSep 11, 2012 · N122UX · Beech 1900D · Vertical Stabilizer Miscellaneous StructureSDR GLBA2012091000051Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB RT SPAR CAP ANGLE AT 20 PERCENT AT VSS 84.10, 1.25" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-55-031. MAJOR REPAIRSep 10, 2012 · N208GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012091000050Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT SPAR CAP ANGLE AT 20 PERCENT AT VXX 84.10, 1.25" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-55-030. MAJOR REPAIR.Sep 10, 2012 · N208GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012091000052Spar · crackedDURING A SCHEDULED ROUTINE INSP FOUND A CRACK IN THE HORIZONTAL STAB AFT SPAR WEB AT HSS 00.00 AT THE LIGHTENING HOLE, .125" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-55-032. MAJOR REPAIR.Sep 10, 2012 · N208GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012090700048Web · crackedDURING A SCHEDULED ROUTINE INSP FOUND 2 CRACKS IN THE HORIZONTAL STAB FWD WEB AT HSS 00.0 AND FS 630 AT THE DEICE TUBE HOLE, 1" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-028. MAJOR REPAIRSep 7, 2012 · N211GL · Beech 1900D · Horizontal Stabilizer StructureSDR GLBA2012091000049Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT SPAR CAP ANGLE AT 20 PERCENT CHORD AT VSS 84.10, .75" IN LENGTH. REPAIRED IAW FR-CO002516R1, STEP 1. MAJOR REPAIR.Sep 7, 2012 · N153GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012090600047Rib · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT WING INBD RIB AT BL 29.06 AND WING SPAR JUNCTION, RIBS DOUBLER, 1" IN LENGTH. REPAIRED AFFECTED AREA IAW EO 12-1900-57-010. MAJOR REPAIRSep 6, 2012 · N211GL · Beech 1900D · Wing, Rib/BulkheadSDR GLBA201209071Landing Gear · malfunctionedLANDING GEAR FAILED TO EXTEND NORMALY. LANDING GEAR LIGHTS DID NOT ILLUMINATE. MX INSPECTED ALL SYS WIRING AND REPLACED THE LANDING CONTROL HANDLE, PERFORMED SEVERAL GEAR SWINGS, OPS CHECKED GOOD.Sep 6, 2012 · N169GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA2012090500046Web · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS IN THE HORIZONTAL STAB FWD WEB AT HSS 00.00 PROTRUDING FROM GROMMET HOLE, ONE INCH IN LENGTH. REPAIRED IAW EO 12-1900-55-027. MAJOR REPAIR.Sep 5, 2012 · N220GL · Beech 1900D · Horizontal Stabilizer Miscellaneous StructureSDR GLBA201209031Bulb · inoperativeEMERGENCY INSTRUMENT LIGHT ON F/O'S SIDE INOPERATIVE. MX REPLACED THE BULB, OPS CK GOOD.Sep 3, 2012 · N169GL · Beech 1900D · Emergency LightingSDR GLBA2012090400044Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB RT FWD SPAR CAP ANGLE AT 20 PERCENT CHORD AND APPROX VSS 84.10 PROTRUDING FROM THE 2ND FROM TOP FASTNER APPROX .125" TO EITHER SIDE, 2 CRACKS, .25" IN LENGTH. REPAIRED IAW EO 12-1900-5Sep 2, 2012 · N220GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA201209032Terminal · dirtyEMERGENCY LIGHTS WILL NOT COME ON DURING TEST. MX CLEANED CORROSION AND SECURED THE CONNECTION ON THE HOT BUSS BAR.Sep 2, 2012 · N254GL · Beech 1900D · Light System WiringSDR 29GA95732090112AAnnunciator · inoperativeFLIGHT: 4017 TPA/FLL NOSE GEAR POSITION INDICATOR NOT LIGHTING. REMOVED AND REPLACED ANNUNCIATOR ASSEMBLY, OPERATIONAL CHECK NORMAL.Sep 1, 2012 · N87557 · Beech 1900D · Landing Gear Position and WarningSDR GLBA2012090400045Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK IN THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT 20 PERCENT CHORD AND APPROX VSS 84.10, EXTENDING FROM TOP OF ANGLE TO JUST PAST 2ND FROM TOP FASTENER, 1.5" IN LENGTH. REPAIRED IAW EO 12-1900-55-025.Aug 31, 2012 · N220GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012083100043Skin · burned.5 X .5 INCH BURN HOLE IN TOP AND BOTTOM SKIN, 3.8750" CENTER FROM OTBD TIP OF LT ELEVATOR T/E. REPAIRED THE AFFECTED AREA IAW EO 12-1900-27-002.Aug 31, 2012 · N210GL · Beech 1900D · Elevator, Plate/SkinSDR GLBA2012083100042Attach Fitting · crackedVERTICAL STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD IS CRACKED AT THE UPPER END AT VSS 84.10. CRACK IS .7500 INCH IN LENGTH, BEGINNING AT THE SECOND FASTENER HOLE ON LT FORWARD HORIZ STABILIZER ATTACH FITTING. REPAIRED IAW FR-00-02506, REV 1, STEP 1.Aug 30, 2012 · N245GL · Beech 1900D · Vertical Stabilizer, Attach FittingsSDR 29GA94032083012Uplock Switch · out of adjustFLIGHT:4001 TLH/TPA GEAR UNSAFE LIGHT INTERMITTENTLY ILLUMINATES LIGHT AND HORN ACTIVATED IN CLIMBOUT WITH GEAR UP. ADJUSTED LEFT MAIN LANDING GEAR UPLOCK SWITCH, OPERATIONAL CHECK OK.Aug 30, 2012 · N16540 · Beech 1900D · Landing Gear Position and WarningSDR 29GA95553082912Skin · corrodedDURING SCHEDULE ROUTINE MAINTENANCE DISCOVERED EXFOLIATION ON OUTER BELLY SKIN BETWEEN STRINGER 14L AND 15L AT FS 318.25. REMOVED DAMAGED AREA AND INSTALLED EXTERNAL REPAIR DOUBLER.Aug 29, 2012 · N87555 · Beech 1900D · Fuselage Main, Plate/SkinSDR 29GA93732082912Downlock Switch · looseFLIGHT 3563 SDY/BIL RED LIGHT IN GEAR HANDLE COMES ON AND GEAR WARNING HORN ACTIVATES ON TOUCHDOWN WITH POWER LEVERS AT IDLE. TIGHTENED RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH, OPERATIONAL CHECKS GOOD.Aug 29, 2012 · N38537 · Beech 1900D · Landing Gear Position and WarningSDR 29GA95771082812Attach Bracket · crackedDURING MAGNETIC PATRICLE INSPECTION DISCOVERED ENGINE TRUSS ENGINE MOUNT ATTACH BRACKET WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE MOUNT ATTACH BRACKET WELD AREAS.Aug 28, 2012 · N87557 · Beech 1900D · Engine Mount SectionSDR GLBA2012082800040Bulb · inoperativePILOT REPORTED THAT THEY HAD A GEAR INDICATION PROBLEM, SWAPPED ANNC'S AND IT WORKED, ATC DECLARED EMERGENCY, MX REPLACED THE BULB, OPS CK GOOD.Aug 26, 2012 · N240GL · Beech 1900D · Landing Gear Position and WarningSDR CA120917027Tube · melted(CAN) RT HORIZONTAL STABILIZER DEICE LINE FOUND MELTED ON LOGO LIGHT ASSY DURING ROUTINE INSPECTION CHECK.Aug 24, 2012 · Beech 1900D · Ice DetectionSDR GLBA2012082300037Attach Angle · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS AT THE RT ANGLE AT FS 107.00 AS IT ATTACHES TO THE LONGERON, RT ANGLE AT THE UPPER END OF THE BEND RADIUS, .5" IN LENGTH, AND AT THE UPPER FASTENER AREA, .375" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EAug 23, 2012 · N154GL · Beech 1900D · Fuselage Main, Attach FittingsSDR GLBA2012082300038Attach Angle · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK ON THE LT SIDEWALL AT FS 107.00, LT ANGLE UPPER INBD FLANGE PORTION IN THE BEND RADIUS AS IT ATTACHED TO THE LONGERON, .75" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-047.Aug 23, 2012 · N154GL · Beech 1900D · Fuselage Main, Attach FittingsSDR GLBA2012082300036Longeron · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT LONGERON AT JUNCTION WITH RT ANGLE AT FS 107.00 CRACKED FROM THE INBD FLANGE AT THE LONGERON TO THE BEND RADIUS, .75" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-048. MAJOR REPAIRE.Aug 23, 2012 · N154GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2012082400039Bulb · inoperativePILOT REPORTED THAT THE F/O EMERGENCY LIGHT BULB IS INOPERATIVE. MX REPLACED BULB, OPS CHECKED GOOD.Aug 23, 2012 · N184UX · Beech 1900D · Emergency LightingSDR 2012FA0000624Resistor · malfunctionedACFT AFT VENT BLOWER ASSY REMOVED BEFORE SCHEDULED MAINTENANCE PERIOND. FOUND THAT RESISTORS HAD GONE BAD DURING THE OPS CHECK. REMOVED AND REPLACED RESISTORS.Aug 22, 2012 · N535M · Beech 1900D · Air Conditioning System WiringSDR 2012FA0000619Resistor · malfunctionedACFT FWD VENT BLOWER ASSY REMOVED BEFORE SCHEDULED MAINTENANCE PERIOD. FUNT THAT RESISTOR(S) HAD GONE BAD DURING THE OPS CHECKS OF SAID ASSY. THE REMOVAL AND REPLACEMENT OF ASSY WAS THE END RESULT OF C/A. BLOWER ASSY RESISTOR(S) NEED TO BE UPGRADED OR MODIFAug 22, 2012 · N535M · Beech 1900D · Air Distribution SystemSDR GLBA2012082100035Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND VERT STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD IS CRACKED AT THE UPPER END AT VSS 84.10, BEGINNING AT THE TOP EDGE AND RADIATES DOWNWARD, THE CRACK IS ON THE FWD FAIRING PORTION OF THE ANGLE, 4.25" IN LENGTH. Aug 20, 2012 · N154GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012082100034Pressure Blkhd · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND RT LWR FWD PRESSURE BULKHEAD CRACKED AROUND FASTENERS ALONG THE BULKHEADS INBD EDGE, FOUND 2 CRACKS APPROX .1 INCH IN LENGTH THAT RADIATES FROM FASTENER HOLES AT FS 84.0. REPAIRED IAW EO 12-1900-53-045.Aug 20, 2012 · N154GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012082100033Pressure Blkhd · crackedDURING A SCHEDULED INSPECTION, FOUND LT LWR FWD PRESSURE BULKHEAD IS CRACKED ALONG THE INBD EDGE DOUBLE ROW OF FASTENER, 3 CRACKS .2 INCHES IN LENGTH RADIUS FROM FASTENER HOLES AT FS 84. REPAIRED IAW EO 12-1900-53-045.Aug 20, 2012 · N154GL · Beech 1900D · Fuselage Main, BulkheadSDR 29GA2012082293753Skin · gougedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED AIRSTAIR DOOR FRAME INNER SKIN 2.0 INCH GOUGE DAMAGE AT FS 150 STRINGER 8. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED COVER PATCH REPAIR.Aug 19, 2012 · N38537 · Beech 1900D · Fuselage Main, Plate/SkinSDR 29GA93753082012Angle · crackedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT AIRSTAIR DOOR FORWARD ANGLE CRACKED APPROXIMATELY AT FS 150. REMOVED 2.0 INCH SECTION OF DAMAGED ANGLE AND INSTALLED REPAIR ANGLE.Aug 19, 2012 · N38537 · Beech 1900D · Passenger/Crew DoorsSDR 29GA93753081912Angle · crackedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT HEAVY ANGLE CRACKED LESS THAN 2.25 INCHES AT FS 288. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE.Aug 19, 2012 · N38537 · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA2012081400032Bulkhead · debondedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND THE FWD UPPER PRESSURE BULKHEAD AT FS 34.0 THE 2ND & 3RD BONDED STRAP FROM THE RT OTBD EDGE OF BULKHEAD HAS DEBONDED AREAS AT THE BOTTOM AREA OF STRAPS, THE 2ND STRAP DEBONDED AREA 2.3" X 1.3", 3RD STRAug 14, 2012 · N100UX · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012081400031Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND LT UPPER FWD PRESSURE BULKHEAD AT FS 84.0 CRACKED AT FASTENER HOLE ALONG BOTTOM EDGE OF PRESSURE BULKHEAD, 5.75" FROM THE LT OTBD PRESS BULKHEAD EDGE, CRACK RADIATES UPWARD FROM FASTENER HOLE, .1875" IN LENGTH. REPAug 13, 2012 · N100UX · Beech 1900D · Fuselage Main, BulkheadSDR GLBA201208151Flow Divider · inoperativeAC PRODUCES STRANGE ODOR AFTER TAKEOFF AFTER BLEEDS ARE OPENED. MX REPLACED THE RT ENGINE FLOW DIVIDER, OPS CHECKED GOOD.Aug 13, 2012 · N122UX · Beech 1900D · Cabin Cooling SystemSDR GLBA201208131Bulb · burned outCAPTAIN'S SIDE INSTRUMENT EMERGENCY LIGHTS BURNED OUT AND 1 INST INDIRECT LIGHT BULB. MX REPLACED THE BULB, OPS CHECKED GOOD.Aug 13, 2012 · N170GL · Beech 1900D · Instrument PanelSDR 2012FA0000623Resistor · malfunctionedACFT VENT BLOWER WAS REMOVED BEFORE SCHEDULED MAINTENANCE PERIOD. FOUND THAT THE RESISTORS HAD GONE BAD UPON FURTHER INSPECTION OF VENT BLOWER ASSY. RESISTORS REMOVED AND REPLACED.Aug 11, 2012 · N535M · Beech 1900D · Air Conditioning System WiringSDR GLBA2012081300030Skin · dentedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND A DENT AT WS 290.06 ON RT WING, 9" BY 4" AREA. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-57-009. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Aug 11, 2012 · N202UX · Beech 1900D · Wing, Plate/Skin
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