Beech 1900D

Service difficulty reports · 7,152

Newest first. General aviation reporting is voluntary.

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 GUUA94153050410BShim · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED CORROSION FS 363 FWD AND AFT OF ANGLE BETWEEN STRINGERS 15L AND STRINGER 16. REMOVED AREA OF CORROSION AND REPLACED SECTION OF DAMAGED SHIM.May 4, 2010 · N17541 · Beech 1900D · Fuselage Main, StructureSDR GUUA94153050410AStringer · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED INTERIOR CORROSION APPROX FS 258, STRINGER 14L, FWD OF ANGLE AT SPLICE AREA OF STR 14L. REMOVED DAMAGED SECTION OF STRINGER AND SPLICED IN NEW STRINGER AND INSTALLED EXTERNAL DOUBLER REPAIRS.May 4, 2010 · N17541 · Beech 1900D · Fuselage Main, StructureSDR GUUA94152050410AHandle · bindingDURING SCHEDULED ROUTINE INSP DISCOVERED SEAT 6A EMERGENCY EXIT INTERIOR HANDLE IS HARD TO OPERATE. LUBRICATED SEAT 6A EMERGENCY EXIT INTERIOR AND EXTERIOR DOOR HANDLES. OPS CHECKS GOOD.May 4, 2010 · N17541 · Beech 1900D · Emergency ExitsSDR GUUA94153043010Angle · crackedDURING SCHEDULED ROUTINE INSP, DISCOVERED INTERIOR FUSELAGE ANGLE CRACKED AT FS 150 STR, 9AL AT AIRSTAIR DOOR TOP AFT ATTACH POINT OF LOWER BRACKET. REMOVED 2.25 INCHES OF DAMAGED ANGLE AND INSTALLED REPAIR ANGLE.Apr 30, 2010 · N17541 · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA94032043010ABrake Assy · weakPILOT REPORTED BRAKES ON LT SIDE OF ACFT SPONGY AND WEAK. REPLACED NR (1) BRAKE ASSY.Apr 30, 2010 · N16540 · Beech 1900D · Landing Gear Brake SystemSDR GUUA94153043010AAngle · crackedDURING SCHEDULED ROUTINE INSP DISCOVERED INTERIOR FUSELAGE ANGLE CRACKED AT FS 150 STRINGER 9AL AT AIRSTAIR DOOR TOP AFT ATTACH POINT OF LOWER BRACKET. (OPEN)Apr 30, 2010 · N17541 · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA94032042910ABrake · weakPILOT REPORTED BRAKES FEEL WEAK. INSPECTED BRAKE SYS FOUND NO LEAKS. BLED BRAKE SYS TAXIED ACFT AND FOUND BRAKE SYS OPS CHECK GOOD NO DEFECTS NOTED.Apr 29, 2010 · N16540 · Beech 1900D · Landing Gear Brake SystemSDR GUUA93757042810APanel · debondedDURING SCHEDULED ROUTINE INSP DISCOVERED LT AND RT INTERNAL DOUBLERS FOR FUEL PANEL 532DB, 532FB, 631DB AND 642FB DEBONDED. REBONDED RING DOUBLERS AT FUEL PANELS 532DB, 532FB, 631DB AND 642FB.Apr 28, 2010 · N38537 · Beech 1900D · Wing, Plate/SkinSDR GUUA94032042610ABrake Sys · contaminatedFLIGHT: 9168 MIA/TPA PILOT REPORTED BRAKES FEEL WEAK. BLED ALL FOUR BRAKES, OPERATIONAL CHECK NORMAL.Apr 26, 2010 · N16540 · Beech 1900D · Landing Gear Brake SystemSDR GLBA20100422GFloor Support · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT FS 482 APPROX 24" INBD OF DOOR THRESHOLD. CRACK APPROX 1". CRACK IS AFT OF NUTPLATE IN RADIUS OF UPPER ANGLE FOR FLOOR SUPPORT WEB. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RIIApr 21, 2010 · N201GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20100422FAngle · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND AT FS 456 JUST LT OF STRINGER NR 1 FWD OF THE REINFORCING ANGLE ATTACHED TO THE FUSELAGE SECTION CRACK EXTENDS FROM EDGE OF ANGLE THROUGH FASTENER HOLE APPROX .375". TOTAL LENGTH OF CRACK APPROX 1".Apr 20, 2010 · N201GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA95652041810AHandle · brokenPILOT REPORTED CABIN DOOR HANDLE BROKEN. REPLACED CABIN DOOR HANDLE OPS CHECK GOOD.Apr 18, 2010 · N81556 · Beech 1900D · Passenger/Crew DoorsSDR GUUA93732041810ASwitch · intermittentPILOT REPORTED GEAR WARNING SILENCE BUTTON DOES NOT SILENCE THE GEAR WARNING HORN. REPLACED GEAR WARNING SILENCE SWITCH, OPS CHECK GOOD.Apr 18, 2010 · N38537 · Beech 1900D · Landing Gear Position and WarningSDR GUUA93552041610ACable · brokenPILOT REPORTED AFT CAM LOCKS ON AIRSTAIR DOOR WILL NOT ROTATE. REPLACED TOP AFT AIRSTAIR DOOR MECHANISM CABLE AND RIGGED, OPS CHECK GOOD.Apr 16, 2010 · N81535 · Beech 1900D · Entrance StairsSDR GUUA93672041610ATurbine Blades · damagedDURING CLIMBOUT LT PROPELLER KEPT ON INCREASING TO 1700 RPM EVEN AFTER CLIMB POWER SET. ALL ENGINE PARAMETERS WERE NORMAL. DURING POST FLIGHT OBSERVED HOLES IN BOTH EXHAUST STACKS AND LT PROPELLER FAILED TO ROTATE. REPLACED LT ENGINE POWER SECTION, OPS CHEApr 16, 2010 · N81536 · Beech 1900D · Turbine SectionSDR GUUA94327041610ATrimmer · bindingDURING FLIGHT ELEVATOR TRIM WHEEL BINDS UP UNABLE TO SEE TRIM TABS ON WHEEL FOR ALL STAGES OF FLIGHT. REPLACED ELEVATOR TRIM TAB INDICATOR OPS CHECK OK. TEST FLIGHT SATISFACTORY.Apr 16, 2010 · N49543 · Beech 1900D · Elevator Tab Control SystemSDR GUUA94627041610ATrimmer · bindingDURING FLIGHT, ELEVATOR TRIM WHEEL BINDS UP UNABLE TO SEE TRIM TABS ON WHEEL FOR ALL STAGES OF FLIGHT. REPLACED ELEVATOR TRIM TAB INDICATOR OPS CHECK OK. TEST FLIGHT SATISFACTORY.Apr 16, 2010 · N49543 · Beech 1900D · Elevator Tab Control SystemSDR GLBA20090416AControl Handle · deterioratedPILOTS REPORTED THAT THE LANDING GEAR CIRCUIT BREAKER TRIPPED, THEY OBSERVED 3 GREEN DOWN LIGHTS. PILOTS THEN RETARDED THE LOWER LEVERS BACK WITH GEAR DOWN AND GOT A GEAR HORN, THE C/B THEN POPPED AGAIN. A MANUAL EXTENSION WAS THEN PERFORMED. MX R & R THE LApr 16, 2010 · N211GL · Beech 1900D · Landing Gear SelectorSDR GLBA20100416JDoor Frame · crackedMAJOR REPAIR - THE AIRSTAIR DOOR FRAME AT FUSELAGE FRAME AT FS 150 BETWEEN STRINGERS 10L & 11L WAS FOUND CRACKED. CRACK APPROX .15" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-015 STEPS 5-8. MATERIALSApr 15, 2010 · N122UX · Beech 1900D · Fuselage Main, StructureSDR GLBA20100416HDoor Frame · crackedMAJOR REPAIR - THE FUSELAGE FRAME AT F.S. 177 AT STRINGER 11L WAS FOUND CRACKED IN THE BEND RADIUS. CRACK LENGTH APPROX .2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-015 STEPS 1-4. MATERIALS UTILIZEDApr 15, 2010 · N122UX · Beech 1900D · Fuselage Main, StructureSDR GLBA20100416GSkin · crackedMAJOR REPAIR - NEAR THE FWD AIRSTAIR DOOR CUTOUT AT THE LOWER FWD CORNER, FUSELAGE EXTERIOR SKIN AT FS 150 AND STRINGER 11L WAS FOUND CRACKED AT A RIVET HOLE. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 10-1900-53-015, STEPS 9-14.Apr 15, 2010 · N122UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100416FDoor Frame · bentMAJOR REPAIR - THE FUSELAGE FRAME AT F.S. 177 BETWEEN STRINGERS 10L & 11L WERE FOUND BENT AND DENTED ON THE SURFACE INSIDE THE AIRSTAIR DOOR CUTOUT AT THE LOWER AFT CORNER AREA. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 10-1900-Apr 15, 2010 · N122UX · Beech 1900D · Fuselage Main, StructureSDR GLBA20100415FDoor Frame · crackedMAJOR REPAIR - UPON A POST FLIGHT CHECK IT WAS DISCOVERED THAT A SMALL DENT AND A CRACK WAS PRESENT AT THE LOWER AFT CORNER OF THE FUSELAGE AIRSTAIR DOOR FRAME. DENT APPROX .125" DEEP AND THE CRACK IS APPROX 1" IN LENGTH WITHIN THE DENT. MX REPAIRED THE AFFECApr 14, 2010 · N122UX · Beech 1900D · Fuselage Main, StructureSDR GUUA93657041310ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED INBD RT WING UPPER T/E HAS SURFACE CORROSION BETWEEN WS 140.36 TO WS 196.06. REMOVED DAMAGE AND INSTALLED AND EXTERNAL REPAIR DOUBLER.Apr 13, 2010 · N81536 · Beech 1900D · Wing, Plate/SkinSDR GUUA93653041310ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED FUSELAGE SKIN EXFOLIATED AT FS 393.25 AND FS 408.25. REMOVED CORRODED SECTION OF SKIN AND INSTALLED AN EXTERNAL DOUBLER REPAIR.Apr 13, 2010 · N81536 · Beech 1900D · Fuselage Main, Plate/SkinSDR 19MA201004141471Condition Lever · crackedON SHUT DOWN PILOT NOTICED CONDITION LEVER WAS LOOSE. UPON INSPECTION FOUND CONDITION LEVER WORN AND CRACKED MOST OF THE WAY THROUGH. INSPECTION REVEALED POSSIBLE CONSTANT RUBBING CAUSED WORN SPOT LEADING TO THINNING OF THE METAL AND FATIGUE FROM BENDING TO Apr 12, 2010 · N567MA · Beech 1900D · Power LeverSDR GUUA94957041210ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED LT WING T/E BY THE NR 1 FLAP, 2 SPOTS OF SURFACE CORROSION. DURING CLEANING OF SURFACE CORROSION DISCOVERED UPPER WING SKIN CORROSION BETWEEN LWS 136 THROUGH 196. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR Apr 12, 2010 · N69549 · Beech 1900D · Wing, Plate/SkinSDR GUUA93732041110AWarning Horn · malfunctionedPILOT REPORTED GEAR WARNING HORN STILL SOUNDS OCCASIONALLY WITH SILENCE BUTTON DEPRESSED. CLEANED AND RERACKED PCB CONNECTOR P273 OPS CHECK NORMAL.Apr 11, 2010 · N38537 · Beech 1900D · Landing Gear Position and WarningSDR 19MA201004136468Relay · stuckON DESCENT TO LAND, PILOT PUT LANDING GEAR HANDLE IN DOWN POSITION AND GEAR FAILED TO GO INTO DOWN AND LOCK POSITION. CONTROL CIRCUIT BREAKER POPPED. PILOT ELECTED TO RESET BREAKER AND GEAR WENT TO DOWN AND LOCK POSITION AND ALL TREE GEAR LIGHTS CAME ON. BRApr 11, 2010 · N886MA · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA94332041110AUplock Switch · out of adjustDURING FLIGHT LANDING GEAR CONTROL HANDLE RED LIGHTS FLICKER ON AND OFF WHEN IN TURBULENT FLIGHT CONDITIONS. C/A: ADJUSTED RT MLG UP POSITION INDICATOR SWITCH. LANDING GEAR OPS CHECK GOOD.Apr 11, 2010 · N49543 · Beech 1900D · Landing Gear Position and WarningSDR GLBA20100409FSkin · puncturedCOMPONENT MAJOR REPAIR - UPON RECEIVING A SERVICEABLE AIRSTAIR DOOR THAT WAS PURCHASED, IT WAS DETERMINED THAT IT REQUIRED A MAJOR REPAIR ON THE EXTERIOR DOOR SKIN DUE TO 3 SCRATCHES AND 1 PUNCTURE THROUGH THE SKIN. MX REPAIRED THE AFFECTED AREA AND PERFORMED Apr 9, 2010 · N210GL · Beech 1900D · Passenger/Crew DoorsSDR GUUA93853040710APaint · peelingDURING POST FLIGHT, FOUND PAINT PEELING OFF ON TOP OF ACFT. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED FILLER 4X5 INCHES AND AN EXTERNAL DOUBLER REPAIR.Apr 7, 2010 · N81538 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA93557033110ASpar · crackedRT WING LOWER AFT SPAR FLANGE 2 FASTNER LOCATIONS AT WING STA 115.0 AND 115.5 SHOW NDI INDICATIONS. DRILLED AND REAMED FASTENER HOLES AND INSTALLED SPAR ANGLE REPAIR.Mar 31, 2010 · N81535 · Beech 1900D · Wing SparSDR GLBA20100330FSkin · buckledMAJOR REPAIR - DURING ROUTINE SCHEDULED MX, THE BELLY SKIN WAS FOUND BUCKLED IN NUMEROUS SPOTS BETWEEN THE FWD AND AFT SPAR FROM APPROX FS 288 TO 335, 32" FROM CENTERLINE. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900Mar 30, 2010 · N254GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100329GCircuit Board · deterioratedSUSPECTED AUTOFEATHER - PILOTS REPORTED THAT THE NR 2 ENGINE AUTOFEATHER WAS CYCLING DURING FINAL APPROACH. MX R & R THE HIGH AND LOW PRESSURE SWITCHES IAW BMM 61-21-01. MX ADDITIONALLY R & R THE AUTOFEATHER PRINTED CIRCUIT BOARD IAW BMM 20-03-00. OPS CHECK Mar 28, 2010 · N184UX · Beech 1900D · Propeller Feathering/ReversingSDR GUUA95752032710ACable · out of toleranceDURING SCHEDULED ROUTINE INSP DISCOVERED AIRSTAIR DOOR CABLE TENSIONS AT 20 LBS. READJUSTED FWD AND AFT AIRSTAIR DOOR CABLE TENSIONS. OPS CHECK GOOD.Mar 27, 2010 · N87557 · Beech 1900D · Passenger/Crew DoorsSDR GUUA95652032610AHandle · bindingPILOT REPORTED CABIN DOOR HANDLE HARD TO ROTATE AND LOCK. ADJUSTED AFT UPPER CAMS ON AIRSTAIR DOOR FRAME. OPS CHECK GOOD.Mar 26, 2010 · N81556 · Beech 1900D · Passenger/Crew DoorsSDR GUUA93952032510ADoor · bindingDURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT DOOR HARD TO OPEN. LUBED RT AFT EMERGENCY EXIT.Mar 25, 2010 · N82539 · Beech 1900D · Emergency ExitsSDR GUUA93957032510ASkin · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT WING T/E TOP SURFACE HAS CORROSION AT WS 223.48. CUT OUT CORRODED SECTION OF RT WING T/E AT WS 223.48 AND INSTALLED EXTERNAL DOUBLER REPAIR.Mar 25, 2010 · N82539 · Beech 1900D · Wing, Plate/SkinSDR GLBA20100324FSkin · dentedMAJOR REPAIR - PILOTS REPORTED THAT A BIRD STRIKE OCCURRED ON SHORT FINAL ON THE LT WING, LT OTBD SECTION OF THE WING. BETWEEN WING SIDE 249.5 & WING SIDE 261.5. DENT IS APPROX 12" IN LENGTH AND APPROX .5" IN DEPTH.Mar 23, 2010 · N182YV · Beech 1900D · Wing, Plate/SkinSDR GLBA201003231Bulb · burned outTHE PILOTS DISCOVERED THAT THE CAPTAINS SIDE INTRUMENT EMERGENCY LIGHT WAS BURN OUT. MAINTENANCE REMOVED AND REPLACED THE BULB AND THE LIGHT OPERATIONALLY CHECKED GOOD I.A.W. 1900D MM 33-10-00.Mar 23, 2010 · N201GL · Beech 1900D · Emergency LightingSDR GUUA93552032210AControl Cable · out of toleranceDURING SCHEDULED ROUTINE INSP DISCOVERED AIRSTAIR/MAIN PAX DOOR CONTROL CABLES TENSIONS LOW. ADJUSTED AIRSTAIR DOOR CONTROL CABLES. OPS CHECK GOOD.Mar 22, 2010 · N81535 · Beech 1900D · Passenger/Crew DoorsSDR GUUA93553032210ASkin · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED CORROSION ON BELLY FUSELAGE AT STA 250 S15L. REMOVED DAMAGED SKIN AND INSTALLED INSERTION PATCH AND EXTERNAL DOUBLER REPAIR.Mar 22, 2010 · N81535 · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20100323FCable · out of rigSUSPECTED AUTOFEATHER - PILOTS REPORTED THAT UPON SHORT FINAL WITH TORQUE BETWEEN 800-1000, PROPELLER WENT IN AND OUT OF FEATHER. TORQUE SEARCHED TO BETWEEN 1600-1800 LBS. THE RT SIDE WAS THE ONE THAT SURGED. MX ADJUSTED POWER LEVER CABLES AT THE GREEN ARM ANDMar 21, 2010 · N153GL · Beech 1900D · Propeller Feathering/ReversingSDR GUUA95457032010ASpar · damagedCOMPLIED WITH COLD EXPANSION OF FASTENER HOLES IN THE WING REAR SPAR LOWER CAP IAW FAA APPROVED DATA CONTAINED IN THE ACFT COMPANY KIT 118-4014-0003. NOTE: ACFT DOWN FOR KIT WING REAR SPAR INSTALLATION.Mar 20, 2010 · N87554 · Beech 1900D · Wing SparSDR GUUA93327031710AHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR OTBD SUPPORT HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR OTBD HINGE BRACKET.Mar 17, 2010 · N81533 · Beech 1900D · Elevator StructureSDR GLBA20100315FFrame · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND IN THE BEND RADIUS OF A FRAME AT FS 451 JUST ABOVE STRINGER 10R. CRACK IS APPROX .9" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-012. MATERMar 15, 2010 · N170GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20100315GFrame · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX, A CRACK WAS FOUND IN A FRAME AT FS 456 AND STR 10R. CRACK IS APPROX .3" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-011. MATERIALS UTILIZED ARE INCLUDED IN Mar 15, 2010 · N170GL · Beech 1900D · Fuselage Main, FrameSDR GUUA95727031510ATorque Tube · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT ELEVATOR TORQUE TUBE, SHOWS SIGNS OF EXFOLIATION. REPLACED LT ELEVATOR TORQUE TUBE ASSY.Mar 15, 2010 · N87557 · Beech 1900D · Elevator Control SystemSDR GUUA94027031410ATorque Tube · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT ELEVATOR TORQUE TUBE EXFOLIATED. REPLACED LEFT ELEVATOR TORQUE TUBE.Mar 14, 2010 · N16540 · Beech 1900D · Elevator Structure
Back to Beech 1900D