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 GLBA201300147Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS ON THE LT FORWARD SPAR CAP ANGLE AT VSS 84.10 AND 20 PERCENT CHORD FROM THE TOP OF THE ANGLE DOWN AND STARTING ABOVE THE SECOND FASTENER DOWN AND EXTENDING PAST THE FASTENER HOLE, 1.125" IN LENGTH. REPAIJan 5, 2013 · N219GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA201300145Wire · brokenPILOT REPORTED THAT WHEN THE LANDING GEAR HANDLE WAS SELECTED TO THE UP POSITION, THE RT MAIN DID NOT FULLY RETRACT, LANDING CIRCUIT BREAKER TRIPPED AND HAD TO PUMP GEAR DOWN BEFORE LANDING. MX REPAIRED WIRE G10A22, OPS CK GOOD.Jan 5, 2013 · N169GL · Beech 1900D · Landing Gear System WiringSDR ERAA20120128Actuator · defectiveLEFT MAIN GEAR LIGHT FAILED TO ILLUMINATE. REMOVED AND REPLACED LT MLG ACTUATOR AND RIGGED IAW B1900D MAINTENANCE MANUAL 32-30-10 AND 32-30-09. BLED IAW 32-30-00 GEAR SWING COMPLIED WITH SYSTEM OP CHECKS GOOD.Dec 30, 2012 · N972EA · Beech 1900D · Landing Gear ActuatorSDR 29GA94732122812Line · crackedFLIGHT: 4068 DUJ PILOT REPORTS RIGHT MAIN LANDING GEAR DOES NOT FULLY RETRACT, NO INDICATION IN THE COCKPIT. FOUND PRESSURE RELIEF LINE CRACKED. REPLACED LINE, OPERATIONAL CHECKS GOOD.Dec 28, 2012 · N69547 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 2012FA0000837Support · damagedLEFT SUPPORT, AFT FLANGE RIVETS WERE MISSING. SUPPORT IS LOCATED BELOW THE CABIN FLOOR UNDER THE CENTER PEDESTAL.Dec 28, 2012 · N842E · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA2012122600144Wire · brokenPILOT REPORTED THE THE F/O'S EMERGENCY LIGHTS ARE INOPERATIVE. MX REPLACED THE BULB AND REPAIRED A WIRE, OPS CHECKED GOOD.Dec 25, 2012 · N153GL · Beech 1900D · Light System WiringSDR GLBA2012122400141Door Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AFT SIDE OF LOWER DOOR FRAME ON RADIUS, ONE INCH IN LENGTH. REPAIRED IAW EO 12-1900-53-078.Dec 24, 2012 · Beech 1900D · Fuselage Main, StructureSDR GLBA2012122400140Eadi · odorPILOT REPORTED AN ODOR OF SMOKE AND BURNING WIRES IN COCKPIT, DECLARED AN EMERGENCY AND LANDED. REPLACED CAPTAIN`S EADI IAW BMM 34-52-00, OPS CHECKED GOOD.Dec 23, 2012 · N122UX · Beech 1900D · Navigation SystemSDR GLBA2012122400139Bulb · inoperativePILOT REPORTED THAT THE CAPT'S INSTRUMENT EMERGENCY LIGHTS WILL NOT TURN ON. MX REPLACED THE BULB, OPS CHECKED GOOD.Dec 23, 2012 · N240GL · Beech 1900D · Emergency LightingSDR GLBA2012122400143Skin · corrodedDURING A SCHEDULED ROUTINE INSP FOUND BELLY SKIN CORROSION AT FS 228.25 AND STRINGER 16. REPAIRED IAW EO 12-1900-53-076. MAJOR REPAIRDec 22, 2012 · N170GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012122400142Stringer · corrodedDURING A SCHEDULED ROUTINE INSPECTION, FOUND STRINGER 16 CORRODED BETWEEN FS 228.25 AND 213.25. REPAIRED IAW EO 12-1900-53-077. MAJOR REPAIR.Dec 22, 2012 · N170GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2012122100138Spar · chafedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CHAFED SPAR .035 ON TOP AND BOTTOM FLANGES AT HSS 98.197 AND A .5" CRACK EXTENDING FROM A RIVET HOLE ON THE BACK WALL OF THE SPAR ON THE LT ELEVATOR. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-27-005. MAJOR REDec 21, 2012 · N202UX · Beech 1900D · Elevator, Spar/RibSDR GLBA2012122000137Attach Angle · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT INBD WING, LOWER INBD ATTACH ANGLE, JUST FWD OF FWD WING SPAR AT BL 29, 1.1" IN LENGTH. REPAIRED IAW EO 12-1900-57-012. MAJOR REPAIR.Dec 20, 2012 · N170GL · Beech 1900D · Wing, Attach FittingsSDR GLBA2012122000136Web · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE AFT HORIZONTAL STAB WEB, 0.125" IN LENGTH. REPAIRED IAW EO 12-1900-558-070. MAJOR REPAIR.Dec 20, 2012 · N170GL · Beech 1900D · Horizontal Stabilizer StructureSDR GLBA2012122000135Spar Cap · crackedDURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE RT SPAR CAP ON VERTICAL STAB AT TOP HOLE, .5" IN LENGTH. REPAIRED IAW EO 12-1900-55-069. MAJOR REPAIR.Dec 20, 2012 · N170GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR CA121220006Circuit Breaker · shorted(CAN) ON APPROACH TO LAND CREW SELECTED GEAR DOWN, AFTER A FEW SECONDS THEY NOTICED NO MOVEMENT FROM THE GEAR. CREW WENT THRU THE CHECK PROCEDURES AND WHEN GEAR STILL DID NOT MOVE, GEAR WAS MANUALLY EXTENDED. ACFT LANDED WITHOUT INCIDENT. ACFT WAS PLACED ONDec 14, 2012 · Beech 1900D · AC Power Distribution SystemSDR GLBA2012121100133Stabilon · damagedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE LT STABILON AFT OTBD CORNER HAS FIBERGLASS DAMAGE MEASURING APPROX 4" X 3". REPAIRED IAW EO 13-1900-55-001. MAJOR REPAIRDec 11, 2012 · N255GL · Beech 1900D · Horizontal Stabilizer Miscellaneous StructureSDR GLBA2012121000132Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT THE EDGE OF A LIGHTNING HOLE, HORIZONTAL STABILIZER AFT SPAR WEB CENTERLINE AT HSS 0.00, .1" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-068.Dec 10, 2012 · N195GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR 29GA94632120912Printed Ckt Board · faultyFLIGHT: 4067 DUJ/DUJ AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT, AFTER SELECTED UP CIRCUIT BREAKER POPPED. REPLACED PCB A316, OPERATIONAL CHECKS GOOD.Dec 9, 2012 · N81546 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA2012121000131Bulb · inoperativePILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHT IS INOPERATIVE. MX REPLACED THE BULB, OPS CHECKED GOOD.Dec 7, 2012 · N184UX · Beech 1900D · Emergency LightingSDR GLBA2012120700130Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION FOUND CORROSION AT FS 228.25, ON SKIN, CORROSION FOUND JUST OTBD OF THIS REPAIR, STRINER 14R 4" OTBD. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-075. MAJOR REPAIRDec 7, 2012 · N195GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012120600129Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT SPAR CAP ANGLE ON VERTICAL STAB AT SECOND FASTENER FROM THE TOP, .75" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-066. MAJOR REPAIRDec 5, 2012 · N195GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012120600128Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND 2 CRACKS IN THE RT SPAR CAP ANGLE ON VERT STAB AT SECOND FASTENER FROM THE TOP, 1.25" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-067. MAJOR REPAIRDec 5, 2012 · N195GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012120600127Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION FOUND BELLY CORROSION AT FS 243.25, APPROX 1" LEFT OF STRINGER 16. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-074. MAJOR REPAIRDec 5, 2012 · N195GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012120400126Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE, RADIATES FROM THE UPPER FWD TASTENER UPWARD TO EDGE OF SPAR CAP, .375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW FR-CO-02586, STEP 1. MAJOR REPAIRDec 4, 2012 · N210GL · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012120400125Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT FWD SPAR CAP ANGLE, RADIATES FROM THE UPPER FWD FASTENER UPWARD TO THE EDGE OF THE SPAR CAP ANGLE, 0.375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW FR-CO-02586, STEP 1. MAJOR REPAIRDec 4, 2012 · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012113000124Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND T/E DAMAGE .35" -.35" ON THE OTBD END OF THE LT ELEVATOR. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-27-005. MAJOR REPAIR.Nov 30, 2012 · N202UX · Beech 1900D · Elevator, Plate/SkinSDR GLBA2012112900123Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND CRACK ON THE LT VERTICAL STAB FWD SPAR CAP ANGLE AT VSS 84.10 AND 20 PERCENT CHORD MOVING DOWNWARD, 2.5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-062. MAJOR REPAIR.Nov 29, 2012 · N253GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012112900122Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE RT VERTICAL STAB FWD SPAR CAP ANGLE AT THE 2ND RIVET FROM THE TOP AT FSS 84.10 AND 20 PERCENT CHORD, .375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-063. MAJOR REPAIR.Nov 29, 2012 · N253GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012112800121Longeron · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS COMING OUT OF A RIVET HOLE ON LONGERON UNDER FINGER DOUBLER AT FS 107, .5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-072. MAJOR REPAIR.Nov 28, 2012 · N202UX · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2012112800120Structure · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS COMING OUT OF RIVET HOLE, ONE CRACK COMING OUT OF ANOTHER RIVET HOLE ON THE LONGERON UNDER FINGER DOUBLER AT FS 107, 0.375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-073. MAJOR REPAIR.Nov 28, 2012 · N202UX · Beech 1900D · Vertical StabilizerSDR GLBA2012112800119Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS ON THE LT FWD SPAR CAP ANGLE ON VERTICAL STABILIZER, ONE CRACK GOING DOWN TO THE FIRST FASTENER HOLE AND 1 NEXT TO THE SECOND FASTENER HOLE, 0.875" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW FR-CO-02580Nov 27, 2012 · N254GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR CA121129002Attach Angle · cracked(CAN) WHILE CARRYING OUT THE BORESCOPE INSPECTION AS REQUIRED BY HBC MSB 55-4114, IT WAS OBSERVED THAT THERE WAS A CRACK VISIBLE COMING FROM UNDERNEATH THE TOP RIVET OF THE LT HORIZONTAL STABILIZER ATTACH POINT ANGLE. THIS WAS LATER CONFIRMED BY EDDY CURRENT INov 26, 2012 · Beech 1900D · Horizontal Stabilizer, Attach FittingsSDR GLBA2012112700118Switch · failedPILOT REPORTED GLARE SHIELD EMERGENCY LIGHTS FAIL TO ILLUMINATE ON CAPTAIN`S SIDE. MAINTENANCE REPLACED THE SWITCH, OPS CHECKED GOOD.Nov 26, 2012 · N178YV · Beech 1900D · Emergency LightingSDR GLBA2012112600117Current Limiter · failedPILOT REPORTED THAT 2 MINUTES INTO CRUISE, HAD SMOKE AND FUMES IN COCKPIT AND COMING FROM THE EYEBALL VENTS IN CABIN, CLOSED LT BLEED AIR AND SMOKE CLEARED, DECLARED EMERGENCY, LANDED WITH NO FURTHER INCIDENT. MX REPLACED THE CURRENT LIMITER AND AFT BLOWER, OPNov 26, 2012 · N261GL · Beech 1900D · Air Conditioning SystemSDR GLBA2012112600116Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE LT VERTICAL FWD SPAR CAP ANGLE HAS A CRACK AT TWO RIVETS AT FSS 84.10 AND 20 PERCENT CHORD, .25" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-059. MAJOR REPAIR.Nov 26, 2012 · N202UX · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012112600115Web · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND THE HORIZONTAL STABILIZER AFT SPAR WEB HAS A CRACK PROTRUDING OUT OF THE ACCESS HOLE AT HSS 00.00, .5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-058. MAJOR REPAIR.Nov 26, 2012 · N202UX · Beech 1900D · Horizontal Stabilizer StructureSDR GLBA2012112600114Angle · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND THE VERTICAL STABILIZER RT FWD SPAR CAP ANGLE CRACKED BY TOP RIVET AT FSS 84.10 AND 20 PERCENT CHORD, .25" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO12-1900-55-060. MAJOR REPAIR.Nov 26, 2012 · N202UX · Beech 1900D · Vertical StabilizerSDR GLBA2012112600113Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND FUSELAGE FRAME AT FS 107 AND STRINGER 8R CRACKED AT INBD FLANGE AT UPPER FASTENER HOLE, .5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-070. MAJOR REPAIR.Nov 26, 2012 · N202UX · Beech 1900D · Fuselage Main, FrameSDR GLBA2012112600112Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND FUSELAGE FRAME AT FS 107.00 AND STRINGER 8L CRACKED AT INBD FLANGE TO UPPER FASTENER HOLD, .5" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-071. MAJOR REPAIR.Nov 26, 2012 · N202UX · Beech 1900D · Fuselage Main, FrameSDR 29GA93532112012Amplifier · faultyFLIGHT: 4069 CLE/DUJ LANDING GEAR WARNING HORN DOES NOT SOUND WHEN POWER LEVERS ARE RETARDED. REPLACED AURAL ANNUNCIATION AMPLIFIER, OPERATIONAL CHECKS GOOD.Nov 20, 2012 · N81535 · Beech 1900D · Landing Gear Position and WarningSDR GLBA2012111400107Screw · loosePILOT REPORTED THAT ON SHORTLY AFTER LEVELING OFF FROM DECENT NR 1 ENG BEGAN TO TQ SURGE PAST AT 4500 FT LBS REDUCED PWR PROP BEGAN TO SURGE RAN MEM ITEMS BROUGHT POWER TO IDLE, RAN CKLIST, FEATHER PROP, COMPLETED ENG SHUTDOWN. RPM NEVER EXCEEDED 1700. PROP Nov 14, 2012 · N220GL · Beech 1900D · Propeller GovernorSDR GLBA2012111400109Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS ON THE VERTICAL STAB RT FWD SPAR CAP ANGLE TOP TWO RIVETS, 1.25" IN LENGTH. MAINTENANCE REPAIRED IAW EO 12-1900-55-057. MAJOR REPAIR.Nov 13, 2012 · N257GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012111400110Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS ON THE VERTICAL STAB LT FWD SPAR CAP ANGLE TOP TWO RIVETS, 2 INCHES IN LENGTH. MAINTENANCE REPAIRED IAW EO 12-1900-55-056. MAJOR REPAIR.Nov 13, 2012 · N257GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2012111400111Bulkhead · gougedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A GOUGE IN THE UPPER PRESSURE BULKHEAD AT FS 84.00 AT ANGLE ATTACH AREA ABOVE CENTER AVIONICS SHELF, TORN IN A TRIANGLE SHAPE 1.35",.8",.7". MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-069.Nov 13, 2012 · N165YV · Beech 1900D · Fuselage Main, BulkheadSDR 29GA93332111312Warning Horn · out of adjustFLIGHT: 3573 LWT/BIL GEAR WARNING HORN ACTIVATES AT HIGH POWER SETTINGS THAN NORMAL. PERFORMED LANDING GEAR WARNING HORN ADJUSTMENT, OPERATIONAL CHECK GOOD.Nov 13, 2012 · N81533 · Beech 1900D · Landing Gear Position and WarningSDR GLBA2012111200106Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND SEVEN CRACKS IN THE RT FWD PRESSURE BULKHEAD AT FASTENERS, THE OTBD ROW TO DOUBLE ROW TO FASTENERS AT THE INBD EDGE OF BULKHEAD, 2.375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-068.Nov 12, 2012 · N165YV · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2012111200105Bulb · missingPILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHT BULB IS MISSING. MX REPLACED THE BULB, OPS CK GOOD.Nov 9, 2012 · N261GL · Beech 1900D · Emergency LightingSDR GLBA2012110800104Spar · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE LT VERTICAL STAB FWD SPAR CAP ANGLE AT 84.10 AND 20 PERCENT CHORD RADIATING UPWARD FROM THE TOP FASTENER HOLE AND THE OTHER CRACK RADIATING AROUND THE SECOND FASTENER HOLE FROM THE TOP, .875" IN TNov 8, 2012 · N251GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR 29GA95555110712Angle · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED VERTICAL SPAR LEFT AND RIGHT ANGLES BELOW RUDDER ATTACH BRACKET HAS CORROSION. BLENDED CORROSION FROM LEFT AND RIGHT VERTICAL SPAR ANGLES AND PERFORMED NDT INSPECTION NO EVIDENCE OF CORROSION NOTED.Nov 7, 2012 · N87555 · Beech 1900D · Vertical Stabilizer, Spar/Rib
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