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 GLBA20091110FSpar · damagedDURING ROUTINE SCHEDULED MX, A STEPPED LOCK FASTENER WAS FOUND IN THE LT WING SPAR AT WS 124.588. DEPTH OF THE STEP IS APPROX .150" DEEP. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1900-57-006. MATERIALS Nov 6, 2009 · N195GL · Beech 1900D · Wing SparSDR GUUA93657110609AGas Generator · low pressureWHILE ENROUTE, THE RT ENG OIL PRESSURE DROPPED TO THE YELLOW ARC AND FLUCTUATED BETWEEN 60-70 PSI. THE RT LOW OIL PRESSURE ANNUNCIATOR STARTED FLASHING, SECURED THE RT ENGINE. PERFORMED EMERGENCY CHECKLIST, DECLARED AN EMERGENCY WITH ATC AND RETURNED TO DEPANov 6, 2009 · N81536 · Beech 1900D · Turbine SectionSDR GLBA20091104FAngle · crackedDURING ROUTINE SCHEDULED MAINTENANCE A RIGHT HAND HEAVY ANGLE WAS FOUND CRACKED IN THE RADIUS AT F.S. 303.25. CRACK LENGTH APPROXIMATELY 2" LONG EXTENDING 1" FORWARD AND OF AFT OF F.S. 303.25. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RNov 4, 2009 · N195GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20091104HSkin · crackedDURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND IN THE RIGHT HAND FUSELAGE SKIN AT F.S. 498.25 ABOVE STRINGER 10R. THE CRACK RADIATES THROUGH A RIVET HOLE. MAINTENANCE REPAIRED THE AFT FUSELAGE SKIN AT F.S. 498.25 AND COMPLIED WITH REQUIRED RII INSPECTINov 4, 2009 · N182YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20091104JFrame · bentDURING ROUTINE SCHEDULED MAINTENANCE A FRAME WAS FOUND BENT AT F.S. 451 BETWEEN STRINGER 6R & 7R. DAMAGE FOUND UNDER PREVIOUS REPAIR TO FUSELAGE SKIN. MAINTENANCE REPLACED THE DAMAGED FRAME AND PERFORMED THE REQUIRED II INSPECTIONS AT F.S. 451 BETWEEN STRINGERNov 4, 2009 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20091104GSkin · crackedDURING ROUTINE SCHEDULED MAINTENANCE THE FUSELAGE SKIN WAS FOUND CRACKED AT F.S. 447 BETWEEN STRINGERS 6R AND 7R. CRACK LOCATED AT UPPER FORWARD CORNER OF A PREVIOUS REPAIR. CRACK IS APPROXIMATELY .5" IN LENGTH. MAINTENANCE REPAIRED THE SKIN AND PERFORMED THE Nov 4, 2009 · N182YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA94757110209ASpar · corrodedREPORT: DURING SCHEDULED X-RAY INSPECTION DISCOVERED CORROSION INDICATIONS ON FORWARD LOWER SPAR ANGLE AT WS 125.5. BLENDED OUT CORROSION AND INSTALLED REINFORCEMENT STRAP.Nov 2, 2009 · N69547 · Beech 1900D · Wing SparSDR GUUA93532110209AUplock Switch · out of adjustAFTER TAKEOFF, LANDING GEAR WILL NOT RETRACT, GEAR UNSAFE LIGHT REMAINS ON WITH GEAR HANDLE IN THE UP POSITION. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. ADJUSTED LT MLG UPLOCK SWITCH AND RT MAIN GEAR DRAG BRACE. LANDING GEAR OPS, CHECK GOOD.Nov 2, 2009 · N81535 · Beech 1900D · Landing Gear Position and WarningSDR GUUA91221110109AUnknown · odorFLIGHT: 6003 DURING DESCENT A STRONG DISGUSTING ODOR COMES THROUGH EYEBALL VENTS DESCENDING THROUGH TEN TO FIVE THOUSAND FT. SMELLS LIKE MOLD AND WARM RUBBER. PERFORMED SATISFACTORY TEST FLIGHT NO DEFECTS NOTED.Nov 1, 2009 · N45AR · Beech 1900D · Air Distribution SystemSDR GUUA94157103109BSpar · corrodedDURING SCHEDULED X-RAY INSP OF LT WING COLLECTOR TANK FOUND SEVERAL SPOTS OF CORROSION ON LWR MAIN SPAR. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR STRAP.Oct 31, 2009 · N17541 · Beech 1900D · Wing SparSDR GUUA94157103109AStringer · corrodedDURING SCHEDULED X-RAY INSP DISCOVERED LT WING COLLECTOR TANK LWR SKIN AFT OF MAIN SPAR BONDED STR HAS MINOR SURFACE CORROSION. REMOVED CORROSION AND INSTALLED AN EXTERNAL REPAIR DOUBLER.Oct 31, 2009 · N17541 · Beech 1900D · Wing, Longeron/StringerSDR GLBA20091031AConnector · disconnectedPILOTS REPORTED THAT UPON APPROACH NEITHER THE LETTER "R" OR THE LETTER "H" GREEN LIGHTS ILLUMINATED ON THE RT SIDE UPON GEAR EXTENSION NOR WITH THE MANUAL EXTENSION PROCEDURE. MX FOUND THE RT MLG ACTUATOR DOWNLOCK SWITCH CONNECTOR NOT CONNECTED PROPERLY. MX Oct 30, 2009 · N202UX · Beech 1900D · Landing Gear System WiringSDR GLBA20091030AIndicator · inoperativeNEITHER R OR H GREEN LIGHTS ILLUMINATED ON THE RT SIDE ON EXTENSION OR WITH MANUAL EXTENSION PROCEDURE.Oct 30, 2009 · N202UX · Beech 1900D · Landing Gear Position and WarningSDR GLBA20091030GFrame · bentSCHEDULED MAINTENANCE A FUSELAGE FRAME WAS FOUND BENT AT FS 198.25 ON THE LEFT HAND SIDE OF THE FUSELAGE AT STRINGER 6L. MAINTENANCE REPAIRED THE FRAME AND PERFORMED THE REQUIRED RII INSPECTIONS AT FS 198.25 AT STRINGER 6L IAW EO 09-1900-53-025 REV.1. MATERIALOct 29, 2009 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20091030JFrame · bentDURING ROUTINE SCHEDULED MAINTENANCE STRINGER 6L WAS FOUND BENT JUST AFT OF FUSELAGE FRAME AT F.S. 198.25. MAINTENANCE REPAIRED STRINGER 6L AND PERFORMED THE REQUIRED RII INSPECTIONS AT F.S. 198.25 IAW EO 09-1900-53-026 R1. MATERIALS UTILIZED ARE INCLUDED IN TOct 29, 2009 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GUUA94621102809AUnknown · odorPILOT REPORTED STRONG FUEL ODOR IN COCKPIT. SEALED AUK FUEL TANK NO LEAKS NOTED.Oct 28, 2009 · N81546 · Beech 1900D · Air Distribution SystemSDR GUUA95132102809AUplock Switch · intermittentAFTER TAKEOFF LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED FOR FIVE MINUTES AFTER GEAR RETRACTED. REPLACED RT MAIN LANDING GEAR UPLOCK SWITCH. OPS CHECK NORMAL.Oct 28, 2009 · N87551 · Beech 1900D · Landing Gear Position and WarningSDR GLBA20091030FSkin · damagedWHILE TOWING THE ACFT INTO HANGAR IN "FMN" THE ELEAVATOR WAS DAMAGED. UPON INSP OF THE ACFT, DAMAGE WAS FOUND ON THE RT ELEVATOR T/E. BOTH THE TOP AND BOTTOM SKINS AND RIBS DAMAGED 11" INBD OF TAB CUTOUT BENT DOWN 3" AND SKIN BUCKLED 23.5"L. MX REPAIRED THEOct 27, 2009 · N254GL · Beech 1900D · Elevator, Plate/SkinSDR GLBA20091030LAngle · crackedDURING ROUTINE SCHEDULED MAINTENANCE A PREVIOUS REPAIR WAS FOUND CRACKED ON THE RIGHT HAND HEAVY ANGLE AT F.S. 303.25. CRACK LENGTH APPROXIMATELY 1". MAINTENANCE REPAIRED THE RIGHT HAND HEAVY ANGLE AND PERFORMED THE REQUIRED RII INSPECTIONS IAW E.O. 09-1900-53Oct 26, 2009 · N182YV · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20091030HAngle · crackedDURING ROUTINE SCHEDULED MAINTENANCE A RIGHT HAND HEAVY ANGLE WAS FOUND CRACKED IN BEND RADIUS AT F.S. 303.25 AFT OF FUSELAGE FRAME. CRACK LENGTH APPROXIMATELY 1". PREVIOUS REPAIR INSTALLED BETWEEN F.S. 288 & 303.25. MAINTENANCE REPAIRED THE HEAVY ANGLE AT F.SOct 26, 2009 · N182YV · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA93957102609ASkin · delaminatedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING SKIN DELAMINATED AROUND FUEL PANEL 532 EB. OPENOct 26, 2009 · N82539 · Beech 1900D · Wing, Plate/SkinSDR CA091104003Bracket · cracked(CAN) 6TH 200 HR DETAILED INSP - RUDDER AFT TORQUE TUBE ATTACH BRACKET, LT - CRACK 1" LONG, SLIGHT BEND AT APEX OF BRACKET. REF IPC 27-20-00 -11 ITEM 292. BRACKET REPLACED - NOTE: THIS IS A GOOD EXAMPLE OF DILIGENT VISUAL INSP AS ACCESS TO THIS AREA IS LIMITEDOct 25, 2009 · Beech 1900D · Rudder StructureSDR GUUA93957102509BSkin · delaminatedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT WING LOWER SKIN DELAMINATED AROUND FUEL PANEL 631DB. REPAIRED RIGHT WING LOWER SKIN AROUND FUEL ACCESS PANEL 631DB.Oct 25, 2009 · N82539 · Beech 1900D · Wing, Plate/SkinSDR GUUA93957102509ASkin · delaminatedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT WING LOWER SKIN DELAMINATED AROUND FUEL PANEL 531DB. REPAIRED LEFT WING LOWER SKIN AROUND FUEL ACCESS PANEL 531DB.Oct 25, 2009 · N82539 · Beech 1900D · Wing, Plate/SkinSDR GLBA200910251Bulb · inoperativeFO'S EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS INSTRUMENT LIGHT BY REMOVING THE LAMP AND THEN PRESSING INOT THE SOCKET AND TURNING UNTIL SEATED. OPERATIONAL CHECK OF THE LIGHT WAS GOOD.Oct 25, 2009 · N255GL · Beech 1900D · Emergency LightingSDR GUUA94053102309ASpar · damagedREPORT: DURING BELLY SKIN REPAIR DISCOVERED RIGHT MAIN SPAR HAS TWO ELONGATED FASTENER HOLES AT FS 288.00. COLD WORK FASTENER HOLES AND INSTALLED BLIND FASTENERSOct 23, 2009 · N16540 · Beech 1900D · Fuselage Main, FrameSDR GUUA94057102309ASpar · damagedDURING BELLY SKIN REPAIR, DISCOVERED RT MAIN SPAR LWR FLANGE HAS 2 ELONGATED FASTENER HOLES AT FS288.00. COLD WORK FASTENER HOLES AND INSTALLED BLIND FASTENERS. PREVIOUSLY SUBMITTED OPEN UNDER CONTROL NR GUUA94053102309A UPDATED TO GUUA94057102309AOct 23, 2009 · N16540 · Beech 1900D · Wing, Plate/SkinSDR GUUA94053102109ASkin · corrodedDISCOVERED CTR BELLY SKIN CORROSION AT FS 327.63 BETWEEN STR 16 TO 15R OUT OF LIMITS REQUIRES REPAIR. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.Oct 21, 2009 · N16540 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA94257102009ASpar · corrodedDURING SCHEDULED RT WING X-RAY INSP DISCOVERED INDICATION OF CORROSION ON FWD LWR SPAR ANGLE AT WS 126.5. BLENDED OUT CORROSION AND INSTALLED REINFORCEMENT STRAP.Oct 20, 2009 · N47542 · Beech 1900D · Wing SparSDR GLBA20091026GEngine · smokePILOTS REPORTED THAT AFTER ENGINE START UP A RAMP AGENT NOTICED SMOKE COMING FROM THE OIL HEATER EXIT ON THE NR 1 ENGINE AND THERE WAS A SMOKE ODOR IN THE CABIN MAINTENANCE INSPECTED THE NR 1 ENGINE FOR LEAKS . NO LEAKS WERE NOTED. CREW RAN THE ENGINES AND NO Oct 20, 2009 · N220GL · Beech 1900D · Engine (Turbine/Turboprop)SDR GLBA20091026FBulb · inoperativeEES - PILOTS REPORTED THAT THE FIRST OFFICERS EMERGENCY INSTRUMENT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS INSTRUMENT LIGHT BY REMOVING THE LAMP AND THEN PRESSING INOT THE SOCKET AND TURNING UNTIL SEATED. OPERATIONAL CHECK OFOct 20, 2009 · N255GL · Beech 1900D · Emergency LightingSDR GUUA94952102009ALatch · damagedPILOT REPORTED AIRSTAIR DOOR ONCE CLOSED, LATCH DIFFICULT TO TURN AND LOCK. RIGGED LATCH POST. OPS CHECK GOOD.Oct 20, 2009 · N69549 · Beech 1900D · Entrance StairsSDR GLBA200910211Bearing · deterioratedUPON LANDING, IT FELT LIKE THE LT BRAKE WAS SLUGGISH AND THE SWA THE LT MAIN TIRE OUTSIDE WHEEL FALL OFF OF THE HUB ASSY. MX REMOVED AND REPLACED THE LT MLG IAW MM 32-10-00, RII INSP COMPLIED IAW TASKCARD 4.3.6 AND RII OF UP/DOWN/SAFETY SWITCH INSTALLATION WAOct 20, 2009 · N237YV · Beech 1900D · Wheel/Ski/FloatSDR GUUA91221101909AHousing · contaminatedFLIGHT: 6003 ASD/PBI DESCENDING THROUGH 10 TO 5 THOUSAND FEET A STRONG DISGUSTING ODOR COMES TRHOUGH EYBALL VENTS. CLEANED AIRCRAFT BELLY FOUND FORWARD AND AFT EVAPORATOR HOUSINGS HAD MOLD AND WATER. TEST FLIGHT SATISFACTORY.Oct 19, 2009 · N45AR · Beech 1900D · Air Distribution SystemSDR GUUA94952101709AHinge · damagedPILOT REPORTED WHEN CLOSING MAIN CABIN DOOR, UPPER LT CAM LOCK SCRAPES AGAINST LOCK. REPLACED AIRSTAIR DOOR TOP AND BOTTOM HINGES.Oct 17, 2009 · N69549 · Beech 1900D · Entrance StairsSDR GUUA93332101709ASwitch · out of adjustDURING FLIGHT GEAR WARNING HORN SOUNDS ON 2300 LBS OF TORQUE. RIGGED RT LANDING GEAR WARNING HORN SWITCHES. OPS CHECK NORMAL. TEST FLIGHT SATISFACTORY.Oct 17, 2009 · N81533 · Beech 1900D · Landing Gear Position and WarningSDR GUUA94952101609ADoor · out of adjustPILOT REPORTED CABIN DOOR VERY HARD TO CLOSE. LUBRICATED CAMS AND REPOSITIONED DOOR CABLES. OPS CHECK GOOD.Oct 16, 2009 · N69549 · Beech 1900D · Passenger/Crew DoorsSDR GUUA93932101509ATube · brokenDURING APPROACH, UPON EXTENDING LANDING GEAR THERE WERE EXTREMELY LOUD GEAR GRINDING NOISES, IT TOOK APPROX 15 SECONDS FOR THE GEAR TO FULLY EXTEND. THE GEAR MOTOR SEEMED TO BE RUNNING IN INTERMITTENT SEGMENTS, THE RT MAIN EXTENDED FIRST FOLLOWED BY THE LT MAIOct 15, 2009 · N82539 · Beech 1900D · Pneumatic Distribution SystemSDR CA091016002Fitting · cracked(CAN) DEPARTED AIRPORT 10/14/09 ON FLIGHT 7435 AND BEGAN TO HAVE LT ENG OIL PRESSURE FLUXUATIONS AFTER REACHING CRUSE ALTITUDE. CAPTAIN SHUTDOWN ENG IN FLIGHT AFTER OIL PRESSURE DROPPED BELOW MINIMUMS. ACFT DIVERTED. AFTER TALKING WITH MFG, OUR PRELIMINARY REOct 14, 2009 · Beech 1900D · Turbine Engine Oil SystemSDR GUUA94053101309ASkin · corrodedDURING SCHEDULED ROUTINE INSP RT BELLY SKIN HAS SKIN DEBONDING AT FS 288.00. REMOVED SURFACE CORROSION FROM SKIN REQUIRES REPAIR. REMOVED DAMAGED SKIN AND INSTALLED SKIN FILLER AND EXTERNAL DOUBLER REPAIR.Oct 13, 2009 · N16540 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA91221101209AHose · deterioratedDURING DESCENT, A STRONG ODOR OF MILDEW COMES THROUGH THE VENT BLOWERS. REPLACED NR 2 ENGINE BLEED AIR HOSE . TEST FLIGHT SATISFACTORY.Oct 12, 2009 · N45AR · Beech 1900D · Pneumatic Distribution SystemSDR GUUA94052101109AControl Cable · frayedDURING SCHEDULED ROUTINE MX, DISCOVERED AIRSTAIR DOOR FWD UPPER CONTROL CABLE FRAYED. REPLACED AIRSTAIR DOOR FWD UPPER CONTROL CABLE. ACFT DOWN FOR STRUCTURAL INSP.Oct 11, 2009 · N16540 · Beech 1900D · Entrance StairsSDR GUUA93932101109AConnector · corrodedDURING APPROACH, LANDING GEAR DOWN, NO INDICATION OF GEAR DOWN. MANUALLY EXTENDED LANDING GEAR, GOT 3 GREEN DOWN AND LOCKED INDICATION. LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR SERVICE VALVE. OPS CHECK NORMAL. TEST FLIGHT SATISFACTORY.Oct 11, 2009 · N82539 · Beech 1900D · Landing Gear System WiringSDR GUUA93732101009ASocket · loosePILOT REPORTED UPPER LANDING GEAR WARNING LIGHT INTERMITTENT. SECURED LOOSE BULB AND SOCKET ON THE LANDING GEAR HANDLE.Oct 10, 2009 · N38537 · Beech 1900D · Landing Gear Position and WarningSDR GUUA93932101009AControl Handle · no indicationFLIGHT: 9202, DURING APPROACH WHEN SELECTED LANDING GEAR CONTROL DOWN GOT NO INDICATION OF THREE GREEN OR THE RED LIGHT LIGHT ON THE GEAR HANDLE. RECYCED GEAR HANDLE TWO TIMES WITH THE SAME RESULT ON THIRD CYCLE GOT THE THREE GREEN DOWN AND LOCKED INDICATION.Oct 10, 2009 · N82539 · Beech 1900D · Landing Gear SelectorSDR GUUA93532100909AConnector · looseFLIGHT: 9302, DURING DESCENT WITH THE POWER LEVERS AT IDLE DID NOT GET GEAR WARNING HORN AND GEAR UNSAFE LIGHTS IN THE GEAR HANDLE. LOWERED LANDING GEAR AND UNSAFE LIGHTS AND WARNING HORN PROCEEDED TO WORK. LANDED WITHOUT INCIDENT. RESEATED CONNECTOR ON PCOct 9, 2009 · N81535 · Beech 1900D · Landing Gear System WiringSDR GUUA94053100609ASkin · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT FUSELAGE HAS CORROSION BETWEEN STRINGERS 9L TO 10L AT F.S 408.25. REMOVED DAMAGED SKIN INSTALLED FILLERS AND SHIMS, FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.Oct 6, 2009 · N16540 · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20091009FDisplay · failedAIR RETURN - PILOTS REPORTED THE CAPTAINS EHSI WENT OUT FOLLOWED BY SMOKE IN THE COCKPIT. TURNING THE PILOTS SIDE SCREENS OFF STOPPED THE SMOKE. IT APPEARED TO THE PILOTS THAT THE CAPTAINS SIDE MIC (HEADSET) WAS LOSING IT'S EFFECTIVENESS AS WELL. OPENOct 6, 2009 · N231YV · Beech 1900D · Central DisplaySDR GUUA94053100509ASkin · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED SKIN BULGING AND SEVERAL RIVETS PULLED THROUGH SKIN AT LEFT EMERGENCY EXIT AFT CUT OUT FRAME. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN INTERNAL WEB REINFORCEMENT AND AN EXTERNAL DOUBLER REPAIR.Oct 5, 2009 · N16540 · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA200910051Wire · chafedAIR RETURN - PILOTS REPORTED THE LANDING GEAR RELAY POPPED AND A MANUAL GEAR EXTENSION WAS PERFORMED. MAINTENANCE REPAIRED A BROKEN WIRE AT THE THE HYDRAULIC POWER PACK SHUTTLE VALVE IAW MM 20-13-00. MAINTENANCE PERFORMED A GEAR RETRACTION AND EXTENSION TEST Oct 5, 2009 · N231YV · Beech 1900D · Landing Gear System Wiring
Back to Beech 1900D