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 GLBA20110304GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME CRACKED AT STRINGER CUTOUT F.S. 183 STRINGER 9AR, .4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-0Mar 4, 2011 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20110308FMount · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR GAS STRUT FWD MOUNT HAS 2 CRACKS APPROX 1.3" IN LENGTH, THE AFT GAS STRUT MOUNT HAS 1 CRACK APPROX .6" IN LENGTH.Mar 4, 2011 · N100UX · Beech 1900D · Cargo/Baggage DoorsSDR GUUA91232030411ARelay · shortedDURING LANDING GEAR EXTENSION CIRCUIT BREAKER POPPED, RESET ONCE CONFIRMED 3 GREEN LIGHTS, AND CIRCUIT BREAKER POPPED AGAIN DURING TOUCHDOWN LT CIRCUIT BREAKER POPPED BUT MOTOR WOULD NOT SHUTOFF. REPLACED LANDING GEAR HYD MOTOR RELAY. LANDING GEAR OPS CHECK Mar 4, 2011 · N45AR · Beech 1900D · Landing Gear Position and WarningSDR GLBA20110303HFrame · crackedDURING A SCHEDULED ROUNTINE INSP MX FOUND THE RT SIDE WALL HEAVY ANGLE AT FS 303, CRACKED IN THE BEND RADIUS, APPROX 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-010. MATERIALS UTILIZED ARE INCLUDED IN Mar 3, 2011 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20110303GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND THE LT HEAVY ANGLE CRACKED AT FS 303 APPROX 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-009. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEEMar 3, 2011 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20110303FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND THE FUSELAGE FRAME CRACKED AT FS 273.25 & STR 2R, CRACKS ON INBD & OTBD SIDE OF STRINGER CUTOUT, .7", .8" & .6" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. Mar 3, 2011 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GLBA20110303JFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND THE FUSELAGE FRAME AT FS 456 CRACKED .3" IN LENGTH AT STRINGER 9AR CUTOUT. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-015. MATERIALS UTILIZED ARE INCLUDMar 3, 2011 · N100UX · Beech 1900D · Fuselage Main, FrameSDR GUUA95252030211ASkin · crackedDURING SCHEDULED ROUTINE MX DISCOVERED SMALL CRACK ON AIRSTAIR DOOR OUTER SKIN AROUND DOOR HANDLE. DURING FURTHER INSPECTION DISCOVERED CORROSION ON OUTER AIRSTAIR DOOR SKIN REMOVED CORRODED OUTER SKIN AND CRACK AND INSTALLED FILLER AND DOUBLER REPAIR.Mar 2, 2011 · N87552 · Beech 1900D · Passenger/Crew DoorsSDR GUUA95732030111ALine · loosePILOT REPORTED LT BRAKE LINE LOOSE, LT PEDAL WENT TO THE FLOOR. SECURED BRAKE LINE BLED BRAKE AND SERVICED RESERVOIR LEAK CHECK OK.Mar 1, 2011 · N87557 · Beech 1900D · Landing Gear Brake SystemSDR GLBA20110228FAKeel · damagedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND LT WHEEL WELL KEEL ATTACH HOLES ARE OVERSIZED, WHERE IB FENDER BRAKET ATTACHES.Feb 28, 2011 · N100UX · Beech 1900D · Nacelle/Pylon, Frame/Spar/RibSDR GUUA93761022811APropeller · malfunctionedDURING APPROACH RT ENG CYCLED BETWEEN 700 AND 1200 POUNDS OF TORQUE WITH ASSOCIATED RT AUTO FEATHER LIGHT. CHECKED AUTO FEATHER SWITCH SETTINGS AND PERFORMED MULTIPLE AUTOFEATHER TEST OPS CHECK NORMAL.Feb 28, 2011 · N38537 · Beech 1900D · Propeller Controlling SystemSDR GUUA93353022711ALongeron · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED RIGHT LONGERON CRACKED APPROXIMATELY 2.0 INCHES AND FORMER DAMAGE AT APPROXIMATELY FS 107 DIRECTLY BELOW FIRST OFFICERS STORM WINDOW. REMOVED DAMAGED SECTION OF LONGERON AND INSTALLED REPAIR REINFORCEMFeb 27, 2011 · N81533 · Beech 1900D · Fuselage Main, Longeron/StringerSDR CA110303003Hose · leaking(CAN) ENGINE FUEL PUMP TO FIREWALL HOSE ASSY ON LT ENGINE FOUND TO BE LEAKING AND IT`S FIRE SLEEVE SATURATED IN FUEL. HOSE WAS REMOVED FROM ACFT. THE FIRE SLEEVE WAS REMOVED REVEALING A HOLE IN THE HOSE.Feb 26, 2011 · Beech 1900D · Aircraft Fuel Distribution SystemSDR GLBA20110228FKeel · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND LH WHEEL WELL GRAVEL FENDER HAS LOOSE RIVETS AND IS CRACKED AROUND THE LOOSE RIVETS. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-54-Feb 26, 2011 · N100UX · Beech 1900D · Nacelle/Pylon, Frame/Spar/RibSDR GUUA94161022511AAnnunciator · no indicationPILOT REPORTED WITH N1 AT 95 PERCENT "AFX DISABLE" ANNUNCIATOR WAS ILLUMINATED AND LT AFX WAS NOT ILLUMINATED. RERACKED ANNUNCIATOR FAULT DETECTION PCB AUTOFEATHER TEST OPS CHECK GOOD.Feb 25, 2011 · N17541 · Beech 1900D · Propeller SystemSDR GLBA201102261Oxygen Mask · unwanted deployPILOT REPORTED THAT ON DECENT PASSENGER OXYGEN MASKS DEPLAYED INADVERTENTLY. MAINTENANCE REPACKED ALL PAX O2 MASKS IN CONTAINERS IAW BMM 35-20-01.Feb 25, 2011 · N247GL · Beech 1900D · Passenger Oxygen SystemSDR GUUA94132022411AIndication Sys · inoperativeFLIGHT: 9131 TPA/TLH PILOT REPORTED DURING APPROACH NO GEAR SAFE INDICATION AND LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED. RETURNED TO TPA LANDED WITHOUT INCIDENT. INSPECTED PC BOARD AND CONNECTORS PERFORMED LANDING GEAR SWING FIVE TIMES. VISUALLY INSPECFeb 24, 2011 · N17541 · Beech 1900D · Landing Gear Position and WarningSDR GUUA93353022311BFrame · crackedREPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED 2.5 INCH CRACK IN THE CARGO FRAME INNER SKIN FROM THE LIGHTNING HOLE TO EDGE AT FS 509.5 STRINGER 11L. REMOVED DAMAGED SECTION OF CRACKED FRAME AND INSTALLED INSERTION PATCH AND COVER PATCH.Feb 23, 2011 · N81533 · Beech 1900D · Fuselage Main, FrameSDR GUUA93353022311ADoor Frame · crackedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED 7.0 INCH CRACK ALLTHE WAY THROUGH THE CARGO FRAME FROM ONE END TO THE OTHER AT FS 509.5 STRINGER 15L. REMOVED DAMAGED SECTION OF CRACKED FRAME AND INSTALLED ANGLE REINFORCEMENT STRAIGHT "L" ANGLE REPAIR.Feb 23, 2011 · N81533 · Beech 1900D · Fuselage Main, StructureSDR GLBA20110223AIndicator · reads lowRIGHT ENGINE TORQUE GAUGE WENT DOWN ON CLIMB OUT. ALL OTHER ENGINE INDICATIONS WERE NORMAL,NOTICED ON TAXI IN TORQUE GAUGE WAS BELOW ZERO. MAINTENANCE PERFORMED PARAMETER RUNUP OF LT & RT ENGINES. ALL CHECKS GOOD COULD NOT DUPLICATE DISCREPANCY.Feb 23, 2011 · N169GL · Beech 1900D · Engine BMEP/Torque IndicatingSDR GUUA93932022311AWarning Horn · out of adjustFLIGHT: 9191, PILOT REPORTED INSPECT LANDING GEAR HORN AS IT COMES ON 82.9% N1 ON NUMBER ONE ENGINE AND 84.0% N1 ON NUMBER TWO ENGINE. ADJUSTED LEFT AND RIGHT LANDING GEAR WARNING HORN PEDESTAL SWITCHES. TEST FLIGHT SATISFACTORY.Feb 23, 2011 · N82539 · Beech 1900D · Landing Gear Position and WarningSDR GLBA201102231Cap · leakingPILOT REPORTED THAT FUEL WAS LEAKING OUT OF LT MAIN FUEL CAP DURING FLIGHT. MAINTENANCE REPLACED THE LT FUEL CAP IAW BMM 28-20-00.Feb 23, 2011 · N100UX · Beech 1900D · Fuel StorageSDR GUUA93353022211BAngle · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING FUSELAGE CLOSING ANGLE CRACKED 1.0 INCH AT FS 288.0. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE.Feb 22, 2011 · N81533 · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA93353022211AAngle · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED CRACK FWD ANGLE AT FS 150 TOP STRUT ASSY SUPPORT BRACKET NUTPLATE. REMOVED DAMAGED ANGLE AND INSTALLED FILLER ANGLE AND REPAIR SPLICES.Feb 22, 2011 · N81533 · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA93653022211ABulkhead · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED FWD RT PRESSURE BULKHEAD BEHIND STIFFENER CRACKED. STOP DRILLED CRACKS AND INSTALLED DOUBLER REPAIR.Feb 22, 2011 · N81536 · Beech 1900D · Fuselage Main, BulkheadSDR GUUA95652021911ADoor · out of adjustDURING SCHEDULED ROUTINE INSP, DISCOVERED RT FWD EMERGENCY EXIT, DIFFICULT TO OPEN. ADJUSTED RIGHT FORWARD EMERGENCY EXIT OPERATIONAL CHECK GOOD.Feb 19, 2011 · N81556 · Beech 1900D · Emergency ExitsSDR GUUA95652021911CDoor · out of adjustDURING SCHEDULED ROUTINE INSP, DISCOVERED LT EMERGENCY EXIT DIFFICULT TO OPEN. ADJUSTED LT EMERGENCY EXIT, OPS CK GOOD.Feb 19, 2011 · N81556 · Beech 1900D · Emergency ExitsSDR GUUA95652021911BDoor · obstructedDURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT DIFFICULT TO OPEN. ADJUSTED UPHOLSTERY ON RT AFT EMERGENCY EXIT OPS, CHECK GOOD.Feb 19, 2011 · N81556 · Beech 1900D · Emergency ExitsSDR GLBA20110218FSkin · debondedDURING A SCHEDULED ROUNTINE INSP MX FOUND THE AIRSTAIR DOOR LOWER INNER SKIN DEBONDED IN AN AREA OF 18" X 6". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-52-003. MATERIALS UTILIZED ARE INCLUDED IN THE EFeb 18, 2011 · N122UX · Beech 1900D · Passenger/Crew DoorsSDR GUUA94557021811ASkin · damagedDURING SCHEDULED ROUTINE INSP DISCOVERED FUSELAGE BELLY SKIN DAMAGE AT FS 408.25 NEAR NR 2 COMM ANTENNA. REMOVED DAMAGED AREA AND INSTALLED EXTERNAL DOUBLER REPAIR.Feb 18, 2011 · N53545 · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20110218GBulb · burned outPILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHTS ON LT SIDE WOULD NOT ILLUMINATE. MX REPLACED THE EMERGENCY LIGHT BULB PN: 1864 IAW BMM 33-10-04, OPS CK GOOD.Feb 18, 2011 · N173YV · Beech 1900D · Emergency LightingSDR GLBA20110215FStructure · crackedDURING A SCHEDULED ROUNTINE INSP MX, FOUND THE RT STABILON HAS A .5" HOLE 9" FROM T/E CORNER, CRACK RADIATED FROM INBD EDGE OF HOLE 1" IN LENGTH. MAINTENANCE COULD NOT REPAIR RT STABILON, REPLACED RT STABILON IAW BMM 55-10-01-201, NO RII REQUIRED FOR INSTALLAFeb 15, 2011 · N178YV · Beech 1900D · Vertical Stabilizer Miscellaneous StructureSDR GLBA20110214FBlower · wornPILOT REPORTED THAT WHEN BLOWER IS PLACED TO AUTO, IT GAVE OFF AN ELECTRICAL ODOR, WHEN TURNED OFF, ODOR WENT AWAY. MAINTENANCE REPLACED THE FORWARD BLOWER ASSY IAW AIM 21-02 AND CW CORROSION INSPECTION.Feb 13, 2011 · N261GL · Beech 1900D · Air Distribution FanSDR GLBA20110214GStructure · damagedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX THE RT STABILON WAS DAMAGED. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 11-1900-55-003. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Feb 12, 2011 · N218YV · Beech 1900D · Vertical Stabilizer Miscellaneous StructureSDR GUUA93971020811AVane · crackedDURING MAGNETIC PARTICLE INSP DISCOVERED RT FWD ICE VANE ATTACH POINT WELD AREA CRACK. PERFORMED WELD REPAIR TO ENGINE TRUSS ICE VANE ATTACH POINT WELD AREA.Feb 8, 2011 · N82539 · Beech 1900D · Air Intake Anti/De-Ice SystemSDR GUUA93953020811BStringer · corrodedDURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED CORROSION ON STRINGER 15L AT FS 288. REMOVED CORRODED AREA OF STRINGER AND INSTALLED STRINGER REPAIR.Feb 8, 2011 · N82539 · Beech 1900D · Fuselage Main, Longeron/StringerSDR GUUA93953020811AStringer · corrodedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION, DISCOVERED CORROSION ON STRINGER 16 AFT OF FS 288. REMOVED CORRODED AREA OF STRINGER AND INSTALLED STRINGER REPAIR AND AN EXTERNAL DOUBLER REPAIR.Feb 8, 2011 · N82539 · Beech 1900D · Fuselage Main, Longeron/StringerSDR GUUA9395302082011Stringer · corrodedDURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED CORROSION ON STRINGER 16 AFT OF FS 288. (OPEN)Feb 8, 2011 · N82539 · Beech 1900D · Fuselage Main, Longeron/StringerSDR GUUA93953020411CDoor Frame · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED ASD FRAME ANGLE CRACKED AT FS 150. FUTHER INSP FOUND ASD FRAME ANGLE REPAIR INSTALLED.Feb 4, 2011 · N82539 · Beech 1900D · Fuselage Main, StructureSDR GUUA93953020411BStringer · debondedDURING SCHEDULED ROUTINE INSP, DISCOVERED STRINGER 15R DEBONDED AT FS 385-406 21 INCHES. REPAIRED STRINGER 15R INSTALLED 1.0 X 26 INCH EXTERNAL DOUBLER REPAIR.Feb 4, 2011 · N82539 · Beech 1900D · Fuselage Main, Longeron/StringerSDR GUUA93953020411AStringer · debondedDURING SCHEDULED ROUTINE INSP, DISCOVERED STRINGER 15L DEBONDED AT FS 400-405 5 INCHES AND FS 396-285 11 INCHES. REPAIRED STRINGER 15L INSTALLED 1.0 X 26 INCH EXTERNAL DOUBLER REPAIR.Feb 4, 2011 · N82539 · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20110203FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE FRAME AT FS 280.73 AT STRINGER 5R CUTOUT, .2" IN LENGTH. MAINTENANC PERFORMED ANOTHER INSPECTION ON THE AREA AND FOUND THE THE CRACK WAS A PEN MARK FROM ORIGINAL MANUFACTURE.Feb 3, 2011 · N169GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20110204HSkin · debondedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND THE AIRSTAIR DOOR LOWER INNER SKIN DEBONDED, AREA 16" X 6" FROM LOWER EDGE INWARD TO STOP HINGE. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-52-0Feb 3, 2011 · N169GL · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110204FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND 2 CRACKS AT THE FRAME FS 456.0 RADIATING FROM STRINGER 9AR CUTOUT, UPPER CRACK .6" IN LENGTH, LOWER CRACK .35" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIOFeb 3, 2011 · N169GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20110204GStringer · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE STRINGER 9AR AT FS 451.0, .4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-007. MATERIALS UTILIZED ARE INCLUDED IN THFeb 3, 2011 · N169GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20110202FStructure · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND 4 CRACKS AROUND THE VENT HOLE IN THE VERT STAB BEHIND THE BULLET CTR WEB, ALL 4 CRACKS ARE .5" IN LENGTH. SUPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPFeb 2, 2011 · N218YV · Beech 1900D · Horizontal Stabilizer StructureSDR GUUA95157020111ASkin · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WING STATIONS 127.00 THROUGH 174.00 JUST FWD OF NR4 FLAP. REMOVED DAMAGE AND INSTALLED AN EXTERNAL DOUBLER REPAIR.Feb 1, 2011 · N87551 · Beech 1900D · Wing, Plate/SkinSDR GUUA92757013111APanel · debondedDURING SCHEDULED ROUTINE INSP DISCOVERED LT WING INBD EDGE PANEL CORROSION AND DEBOND. REMOVED DAMAGE AND INSTALLED A FILLER AND AN EXTERNAL DOUBLER REPAIR.Jan 31, 2011 · N46AR · Beech 1900D · Wing, Plate/SkinSDR GLBA20110131FSkin · crackedDURING A SCHEDULED ROUTINE INSP, MX FOUND A RIVET SHEARED AT APPROX AT FS 163.9 & WL 98, AND A CRACK ON THE RT SIDE .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-004. MATERIALS UTILIZED AJan 30, 2011 · N251GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20110131GSkin · damagedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A GAUGE & SMALL HOLE IN SKIN AT FS 508 & W.L. 90. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-005. MATERIALS UTILIZED ARE INCLUDED IJan 30, 2011 · N251GL · Beech 1900D · Fuselage Main, Plate/Skin
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