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 CA130313006Cooling Fan · broken(CAN) ACFT WAS ON THE GROUND, PILOTS WERE UNABLE TO START THE ENGINE, HUNG START. SO THEY SHUTDOWN, AND OBSERVED SMOKE FROM THE BACK OF THE ENGINE. THEY EXITED THE ACFT, NO PASSENGERS ON BOARD, REPOSITIONING FLIGHT, WITH FIRE EXTINGUISHERS IN HAND, BUT THE SMMar 6, 2013 · Beech 1900D · Starter-GeneratorSDR GLBA2013030700199B-Nut · loosePILOT REPORTED THAT WHILE EXTENDING THE GEAR, MAINS SHOWED DOWN AND LOCKED, NOSE DID NOT SHOW GREEN INDICATION, GEAR HANDLE IN TRANSIT, REMAINED ILLUMINATED, RAN CHECKLIST, MANUALLY PUMPED GEAR DOWN, HAD 3 GREEN INTRANSIT LIGHT EXT, LANDED WITH NO FURTHER INCIMar 6, 2013 · N255GL · Beech 1900D · Hydraulic System, MainSDR GLBA2013030600198Diode · failedPILOT REPORTED THAT THERE WAS ELECTRICAL SMOKE COMING FROM THE FUEL GAUGE PANEL, RT FIRE WALL CIRCUIT BREAKER TRIPPED. MX REPLACED THE CR3 DIODE ON THE FUEL PANEL.Mar 5, 2013 · N100UX · Beech 1900D · DC Power Distribution SystemSDR GLBA2013030500197Spar Web · damagedDURING A SCHEDULED ROUTINE INSPECTION, CHANGED AFT SPAR WEB. REPAIRED IAW EO 13-1900-55-006.Mar 4, 2013 · N122UX · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2013030500196Stringer · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN A STRINGER AT FS 588.1 AND STRINGER 9R, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-022. MAJOR REPAIR.Mar 4, 2013 · N257GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2013030500195Bulkhead · damagedDURING A SCHEDULED ROUTINE INSPECTION, FOUND BULKHEAD AT FS 588.1 DAMAGED JUST UNDER STRINGER 8R, PROTRUDING OUT OF A RIVET APPROX .25". REPAIRED IAW EO 13-1900-53-021. MAJOR REPAIR.Mar 4, 2013 · N257GL · Beech 1900D · Fuselage Main, BulkheadSDR GLBA2013030500194Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS AT FS 588.1 STRINGER 9L, 1.25 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-019. MAJOR REPAIR.Mar 4, 2013 · N257GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013030500193Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT FS 588.1 STRINGER 8L, PROTRUDING UPWARD, 1 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-020. MAJOR REPAIR.Mar 4, 2013 · N257GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2013030400192Bulb · burned outPILOT REPORTED THAT THE EMERGENCY LIGHT ON F/O'S SIDE IS INOPERATIVE, EMERGENCY AND INDIRECT MODE. MX REPLACED THE BULB, OPS CHECKED GOOD.Mar 1, 2013 · N254GL · Beech 1900D · Emergency LightingSDR GLBA2013030100191Skin · damagedRT ELEVATOR OTBD EDGE & OTBD T/E DAMAGE APPROX 13" X 15.5". T/E ALSO BUCKLED JUST INBD OF OTBD HINGE ATTACH POINT APPROX 4" X 7". REPAIRED IAW TC 1900-2730.00. MAJOR REPAIR.Mar 1, 2013 · N257GL · Beech 1900D · Horizontal Stabilizer, Plate/SkinSDR 29GA2013022794627Chain · out of adjustFLIGHT: 4069 CLE/DUJ ELEVATOR TRIM WILL NOT TRIM NOSE DOWN INFLIGHT. ELECTRIC ELEVATOR TRIM MOTOR UNABLE TO OVERCOME TENSION IN THE TRIM WHEEL, WHEN MANUALLY TRIMMED THE WHEEL ROLLED ONE UNIT DOWN AND SPRINGS HALF A UNIT BACK UP. INSPECTED ELEVATOR TRIM SYSTFeb 27, 2013 · N81546 · Beech 1900D · Elevator Control SystemSDR 29GA94627022713Trim System · stuckFLIGHT: 4061 CLE/PKB ELEVATOR TRIM STUCK IN FLIGHT, ELEVATOR TRIM BECAME UNSTUCK DURING APPROACH. INSPECTED AND FUNCTIONAL CHECK ELEVATOR TRIM SYSTEM NO DEFECTS NOTED.Feb 27, 2013 · N81546 · Beech 1900D · Elevator Tab Control SystemSDR GLBA2013022700187Skin · crackedEMERGENCY EXIT 6A SKIN PANEL LOWER FWD CORNER CRACKED IN 2 LOCATIONS. 1 CRACK IS 1.4" IN LENGTH, THE OTHER CRACK IS 1.8" IN LENGTH. REPAIRED IAW EO 13-1900-52-001. MAJOR REPAIR.Feb 26, 2013 · N208GL · Beech 1900D · Emergency ExitsSDR GLBA2013002600186Skin · crackedFUSELAGE SKIN CRACKED AT FS 150.60 & STRINGER 1. CRACK ON LT SIDE OF STRINGER 1 IS .25" IN LENGTH, CRACK ON RT SIDE OF STRINGER 1 IS .65" IN LENGTH. REPAIRED IAW EO 13-1900-53-016. MAJOR REPAIR.Feb 26, 2013 · N208GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2013022600185Skin · corrodedBELLY SKIN CORROSION AT FS 228.25 BETWEEN STRINGERS 16 & 15R. CORROSION INDICATIONS RUN ON FRAME AREA BETWEEN STRINGERS 16 & 15R. REPAIRED IAW EO 13-1900-53-015. MAJOR REPAIR.Feb 26, 2013 · N208GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2013022800189Frame · crackedFUSELAGE FRAME DOUBLER AT FS 177.25 & STRINGER 13L CRACKED 1.2" IN LENGTH IN FLANGE BEND RADIUS TO SECOND FASTENER FROM THE OTBD EDGE OF DOUBLER. REPAIRED IAW EO 13-1900-53-018. MAJOR REPAIR.Feb 25, 2013 · N208GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013022600184Frame · crackedRIGHT SIDEWALL AT FS 107, FRAME CRACKED AT UPPER FASTENER AREA. LONGERON AT FS 107 CRACKED. REPAIRED IAW EO 13-1900-53-014. MAJOR REPAIR.Feb 25, 2013 · N208GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013022600183Rib · crackedLEFT WING INBD RIB AT 288 & BL 29.0 CRACKED. CRACK 1" IN LENGTH FROM OTBD EDGE INWARD TO BEND RADIUS AREA. REPAIRED IAW EO 13-1900-57-006. MAJOR REPAIR.Feb 25, 2013 · N208GL · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2013022600182Rib · crackedRT INBD WING RIB AND DOUBLER AT AT 288 & BL 29.0 CRACKED & WORN. CRACK IS 1.0" IN LENGTH. REPAIRED IAW EO 13-1900-57-005. MAJOR REPAIR.Feb 25, 2013 · N208GL · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2013022500179Motor · inoperativeSIG EVENT - PILOT REPORTED SMOKE AND FUMES IN THE CABIN. MX VISUALLY INSPECTED ACFT, FOUND TO BE FLAP MOTOR. R & R THE FLAP MOTOR IAW BMM 27-50-03. OPS CHECKED GOOD.Feb 23, 2013 · N219GL · Beech 1900D · Trailing Edge Flap Control SystemSDR CA130222003Handle · twisted(CAN) DURING TURN AROUND GROUND CREWS TRIED TO OPEN CARGO DOOR THEY THOUGHT THE HANDLE WAS STIFF BUT DOOR OPENED. ACFT WAS LOADED, WHEN THE CREW TRIED TO CLOSE DOOR THE HANDLE WAS JAMMED. CREW CALLED MAINTENANCE AND ADVISED THEM OF THE SITUATION. AN AME WASFeb 19, 2013 · Beech 1900D · Cargo/Baggage DoorsSDR GLBA2013022800188Plenum · debondedLT OTBD PLENUM PANEL DEBONDED APPROX 5" FROM THE TOP OF PANEL TO APPROX 15" DOWN, THE FULL WIDTH OF THE HONEYCOMB. REPAIRED IAW WITH A FIELD REPAIR.Feb 19, 2013 · N220GL · Beech 1900D · Nacelle/Pylon, Main FrameSDR GLBA2013021400176Unknown · odorPILOT REPORTED THAT THERE WAS A STRONG ELECTRICAL ODOR IN THE COCKPIT. MX INSPECTED ACFT DUCT SYS, RAN ACFT AND OPS CHECKED SYS WITH FLIGHT CREW, NO DEFECTS NOTED.Feb 13, 2013 · N178YV · Beech 1900D · Air Distribution SystemSDR 29GA94752021213Cable · brokenFLIGHT: 4061 PKB/CLE FORWARD DOOR CAM LOCKS WILL NOT MOVE. REPLACED BROKEN DOOR CABLE, OPERATIONAL CHECK GOOD.Feb 12, 2013 · N69547 · Beech 1900D · Passenger/Crew DoorsSDR GLBA2013021300175Bulb · inoperativePILOT REPORTED THAT THE INSTRUMENTS EMERGENCY LIGHTS ON CAPS SIDE WILL NOT ILLUMINATE. MX REPLACED THE BULB, OPS CHECKED GOOD.Feb 12, 2013 · N100UX · Beech 1900D · Emergency LightingSDR GLBA2013021300173Skin · damagedFUSELAGE SKIN DAMAGE BETWEEN FS 456 & 490.50, AND BETWEEN STRINGER 15L & STRINGER 12L, INTERCOSTAL AT FS 468, FS 468 & 14L & 13L DAMAGE, FS 475.00 AND FS 462. REPAIRED IAW EO 13-1900-53-012. MAJOR REPAIR.Feb 11, 2013 · N192GL · Beech 1900D · Fuselage Main, Plate/SkinSDR 29GA94732020413Uplock Switch · out of adjustFLIGHT: 4062 PKB/CLE LANDING GEAR UNSAFE LIGHT INTERMITTENT IN FLIGHT. INSPECTED AND ADJUSTED LEFT MAIN LANDING GEAR UPLOCK SWITCH, OPERATIONAL CHECK GOOD.Feb 4, 2013 · N69547 · Beech 1900D · Landing Gear Position and WarningSDR GLBA2013010400170Spar Cap · crackedDURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN RT FORWARD SPAR CAP ANGLE AT CSS 69.184 AND 20 PERCENT CHORD, 2.5" IN LENGTH. REPAIRED IAW EO 13-1900-55-005. MAJOR REPAIR.Feb 2, 2013 · N240GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2013010400169Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE AT CSS 69.184 AND 20 PERCENT CHORD, 1.75" IN LENGTH. REPAIRED IAW EO 13-1900-55-004. MAJOR REPAIR.Feb 2, 2013 · N240GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2013010400168Skin · damagedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE RT ELEVATOR ON THE T/E RIGHT ABOVE THE OTBD STATIC WICK, APPROX 0.3125 INCHES DEEP BY .25 INCHES WIDE. REPAIRED IAW EO 13-1900-27-002. MAJOR REPAIR.Feb 2, 2013 · N240GL · Beech 1900D · Elevator, Plate/SkinSDR GLBA2013010400167Uplock Switch · inoperativePILOT REPORTED THAT ON LANDING, LOWERED THE GEAR, INTRANSIT LIGHT CAME ON AND WENT OUT, GOT GREEN ON MAINS, NOT ON NOSE, MANUALLY EXTENDED GEAR AND STILL NO GREEN ON NOSE. MX REPLACED THE NOSE UPLOCK SWITCH, OPS CK GOOD.Feb 2, 2013 · N247GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA2013013000166Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 107 AND STRINGER 8R, FRAME CRACK PROTRUDING OUT OF RIVET, .5 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-007.Jan 30, 2013 · N231YV · Beech 1900D · Fuselage Main, FrameSDR GLBA2013013000165Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS AT FS 107 AND STRINGER 8L IN THE BEND RADIUS, CRACK PROTRUDING OUT OF RIVET, 1.25 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-008.Jan 30, 2013 · N231YV · Beech 1900D · Fuselage Main, FrameSDR GLBA2013013000164Frame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 456 AT THE GAS STRUT UPPER INBD NUTPLATE BETWEEN STRINGERS 3L AND 4L, .75" IN LENGTH. REPAIRED IAW EO 13-1900-53-002.Jan 30, 2013 · N231YV · Beech 1900D · Fuselage Main, FrameSDR 29GA2013022795453Door Frame · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED CRACK AT LOWER CORNER FOR AIRSTAIR DOOR FUSELAGE SIDE. REMOVED DAMAGED AREA AND INSTALLED A DOUBLER AND SPLICE REPAIR.Jan 28, 2013 · N87554 · Beech 1900D · Fuselage Main, StructureSDR GLBA2013012800163Downlock Switch · dirtyPILOT REPORTED THAT WHILE EXTENDING THE GEAR, THE LT GEAR INDICATOR DID NOT ILLUMINATE, IN TRANSIT LIGHT WAS NOT ILLUMINATED, RAN QRH CK LIST AND MANUALLY PUMPED THE GEAR DOWN, STILL DID NOT RECEIVE 3 GREENS, PERFORMED GPWS TEST HAD NO WARNING HORN, LANDED WITJan 27, 2013 · N254GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA2013012200160Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS ON A LT ELEVATOR ASSY IN THE T/E, APPROX 23.1875" OTBD OF TRIM TAB OTBD CUTOUT, ON BOTH SIDES OF THE ELEVATOR SKIN, (TOP AND BOTTOM SIDES), 1" IN LENGTH. REPAIRED IAW EO 13-1900-27-001. MAJOR REPAIR.Jan 22, 2013 · N247GL · Beech 1900D · Elevator, Plate/SkinSDR GLBA2013012100159Bulb · inoperativePILOT REPORTED THAT THE CAPT'S SIDE EMERGENCY LIGHT IS INOPERATIVE. MX REPLACED LIGHT BULBS, OPS CHECKED GOOD.Jan 18, 2013 · N184UX · Beech 1900D · Emergency LightingSDR GLBA2013011500158Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND FRAME CRACKED AT THE AFT LOWER CARGO DOOR FRAME AT FS 509.5, 2 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-002.Jan 15, 2013 · N245GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013011500157Frame · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND FRAME CRACKED AT FS 107, LT SIDE FRAME BEHIND FINGER DOUBLER IN THE BEND RADIUS, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-004.Jan 15, 2013 · N245GL · Beech 1900D · Fuselage Main, FrameSDR GLBA2013011500156Skin · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND SKIN CRACKED AT FS 438 AND JUST ABOVE STRINGER 8L PROTRUDING OUT OF RIVET, .25" IN LENGTH. REPAIRED IAW EO 13-1900-53-003.Jan 15, 2013 · N245GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2013011400155Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE RT VERTICAL STAB FWD SPAR CAP ANGLE BY THE TOP RIVET GOING TOWARDS THE BEND RADIUS, 1" IN LENGTH. REPAIRED IAW EO 13-1900-55-003.Jan 14, 2013 · N245GL · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2013011400154Structure · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT INBD WING, INBD LOWER AFT CORNER BY SPAR RIB FLANGE , 1" IN LENGTH. REPAIRED IAW EO 13-1900-57-003.Jan 14, 2013 · N245GL · Beech 1900D · Wing Main, Frame StructureSDR GLBA2013011400153Skin · corrodedDURING A SCHEDULED ROUTINE INSPECTION, FOUND BELLY SKIN CORRODED BETWEEN STRINGERS 14R AND 15R AT FRAME LOCATION AT FS 243.25. REPAIRED IAW EO 13-1900-53-001.Jan 14, 2013 · N245GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2013011400150Diode · failedPILOT REPORTED THAT THE INST EMERGENCY LIGHTS FAILED TO ILLUMINATE WITH THE INSTRUMENT EMERGENCY LIGHT SWITCH. MX REPLACED DIODES, OPS CHECKED GOOD.Jan 12, 2013 · N261GL · Beech 1900D · Emergency LightingSDR GLBA2013011400151Bulb · burned outPILOT REPORTED THAT THE CAPTAIN'S SIDE EMERGENCY LIGHT WILL NOT ILLUMINATE. MX REPLACED THE BULB, OPS CHECKED GOOD.Jan 11, 2013 · N100UX · Beech 1900D · Emergency LightingSDR GLBA2013011000149Pcb · failedPILOT REPORTED THAT ON FINAL, EXTENDED GEAR, INTRANSIT LIGHT ILLUMINATED AND NOTHING ELSE HAPPENED, MANUALLY EXTENDED GEAR, LANDED SAFELY, ATC DECLARED EMERGENCY. MX REPLACED PCB AND LG RELAY, OPS CHECKED GOOD.Jan 10, 2013 · N122UX · Beech 1900D · Landing Gear System WiringSDR GLBA2013010800148Fuse · inoperativePILOT REPORTED THAT THE EMERGENCY INSTRUMENT LIGHTS ARE INOPERATIVE. MX REPLACED THE HOT BATTERY FUSE, OPS CHECKED GOOD.Jan 7, 2013 · N261GL · Beech 1900D · Indicating/Recording SystemSDR GLBA201300146Line · inoperativePILOT REPORTED THAT AFTER TAKEOFF, BROUGHT THE GEAR TO THE UP POSITION AND RETRACED NORMALLY, GEAR IN TRANSIT LIGHT ILLUMINATED SHORTLY AFTER, LANDING GEAR FAILS TO REMAIN RETRACTED, LANDING GEAR FAILS TO EXTEND NORMALLY, LANDING GEAR MANUAL EXT, ABNORMAL CHECJan 6, 2013 · N122UX · Beech 1900D · Hydraulic System, MainSDR GLBA2013011400152Spar 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/Rib
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