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"

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SDR ERAA200900009Turbine Blades · damagedLOUD NOISE FROM RIGHT ENGINE DURING TAKEOFF. ABORTED TAKEOFF. REMOVED NR 2 POWER SECTION AND FOUND DAMAGE ON 2ND STAGE POWER TURBINE BLADES. REMOVED AND REPLACED ENGINE.Oct 5, 2009 · N971EA · Beech 1900D · Turbine SectionSDR CA091008006Relay · malfunctioned(CAN) LT ENG PROP DE-ICE CAUGHT FIRE BEFORE THE START SEQUENCE TOOK PLACE. WITH PROP DE-ICE SWITCH IN THE OFF POSITION. BEFORE START UP GROUND INFORMED THE CREW OF A FIRE ON THE LT PROP. CREW NOTICED IT WAS THE DE-ICE SYS AND IMMEDIATELY CHECKED TO SEE IF THEOct 4, 2009 · Beech 1900D · Propeller/Rotor Anti-Ice/De-Ice SystemSDR GUUA95752100409ASnubber · stiffFLIGHT: 9130, PILOT REPORTED CABIN DOOR SNUBBER NEEDS TO BE SERVICED DIFFICULT TO CLOSE. SERVICED CABIN DOOR SNUBBER.Oct 4, 2009 · N87557 · Beech 1900D · Passenger/Crew DoorsSDR GUUA93632100409ASwitch · out of adjustFLIGHT: 9166, AFTER TAKEOFF THE LANDING GEAR UNSAFE HANDLE LIGHT REMAINED ON AFTER GEAR RETRACTION. CONTINUED TO DESTINATION. LANDED WITHOUT INCIDENT. ADJUSTED NOSE LANDING GEAR UP POSITION INDICATOR SWITCH. LANDING GEAR OPERATIONAL CHECK OK.Oct 4, 2009 · N81536 · Beech 1900D · Landing Gear Position and WarningSDR GUUA95252100309BDoor · stiffFLIGHT: 9204, PILOT REPORTED AIRSTAIR DOOR DIFFICULT TO OPEN. PERFORMED OPERATIONAL FUNTIONAL CHECK NO DEFECTS NOTED.Oct 3, 2009 · N87552 · Beech 1900D · Entrance StairsSDR GUUA95252100309ADoor · stiffFLIGHT: 9160, PILOT REPORTED AIRSTAIR DOOR DIFFICULT TO OPEN. ADJUSTED AIRSTAIR DOOR FORWARD LOWER LATCH CAM OPERATIONAL CHECK GOOD.Oct 3, 2009 · N87552 · Beech 1900D · Entrance StairsSDR GUUA94657100309ASkin · damagedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED FASTENERS PULLING THROUGH THE RIGHT UPPER WING SKIN BETWEEN W.S 124.25 AND 143.00. REMOVED LEAKING RIVETS, FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.Oct 3, 2009 · N81546 · Beech 1900D · Wing, Plate/SkinSDR GLBA2009100101Line · leakingPILOTS REPORTED THE GEAR INSTRANSIT LIGHT DID NOT EXTINGUISH, LANDING GEAR RELAY CIRCUIT BREAKER POPPED AND GEAR HAD TO BE MANUALLY EXTENDED. UPON FURTHER INSPECTION AFTER LANDING THE PILOTS NOTED HYDRAULIC FLUID IN THE LEFT HAND WHEELWELL. MAINTENANCE REMOVEOct 1, 2009 · N173YV · Beech 1900D · Landing Gear ActuatorSDR GUUA93632100109ADownlock Switch · out of adjustFLIGHT: 9236, AFTER TAKEOFF WHEN LANDING GEAR RETRACTED THE GEAR HANDLE LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. ADJUSTED RT DOWNLOCK SWITCH. LANDING GEAR OPERATIONAL CHECK OK.Oct 1, 2009 · N81536 · Beech 1900D · Landing Gear Position and WarningSDR GUUA94057093009DStructure · corrodedDURING SCHEDULED LEFT WING X-RAY INSPECTION DISCOVERED SMALL AREA OF CORROSION AREA 1 FWD BONDED STRINGER. CLEANED SURFACE CORROSION AT AREA 1 FOUND TO BE WITHIN ALLOWABLE LIMITS.Sep 30, 2009 · N16540 · Beech 1900D · Wing Main, Frame StructureSDR GUUA94057093009CSpar · corrodedDURING SCHEDULED LEFT WING X-RAY INSPECTION DISCOVERED SMALL CORROSION SPOTS AREA 1 WING SPAR. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP.Sep 30, 2009 · N16540 · Beech 1900D · Wing SparSDR GUUA94057093009BStringer · corrodedDURING SCHEDULED RIGHT WING X-RAY INSPECTION DISCOVERED SMALL AREA OF CORROSION AREA 1 FWD BONDED STRINGER. REMOVED CORROSION FROM RIGHT WING AREA 1 FORWARD BONDED STRINGER FOUND TO BE WITHIN ALLOWABLE LIMITS.Sep 30, 2009 · N16540 · Beech 1900D · Wing, Longeron/StringerSDR GUUA94057093009ASpar · corrodedDURING SCHEDULED RIGHT WING X-RAY INSPECTION DISCOVERED SMALL CORROSION SPOTS AREA 1 WING SPAR. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP.Sep 30, 2009 · N16540 · Beech 1900D · Wing SparSDR GLBA20091002FUplock Switch · out of adjustAIR RETURN - PILOTS REPORTED THAT A GEAR UNSAFE LIGHT WAS ILLUMINATED AFTER GEAR RETRACTION AND THEY MANUALLY EXTENDED THE GEAR. MAINTENANCE ADJUSTED THE RIGHT HAND MAIN LANDING GEAR UPLOCK SWITCH FOR MORE COMPRESSION. AN OPERATIONAL CHECK WAS JPERFORMED AND WSep 29, 2009 · N208GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA200909292Switch · faultedAIR TURNBACK - PILOTS REPORTED THAT UPON TAKEOFF AND CLIMBING THAT THE GEAR HANDLE IN TRANSIT LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. MAINTENANCE REMOVED AND REPLACED THE NOSE AND RIGHT HAND MAIN UPLOCK SWITCHES. MAINTENANCE RIGGED THE SWITCHES AND TSep 29, 2009 · N170GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA200909291Bulb · inoperativePILOTS REPORTED THAT ONE EMERGENCY INSTRUMENT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED BULB 1864 BY PUSHING IN AND TURNING THE A QUARTER UNTIL IT WAS FREE, REMOVED AND REPLACED THE BLUE SLEEVE TO THE NEW BULB AND INSTALLED BY PUSHING IN AND PERFOSep 29, 2009 · N201GL · Beech 1900D · Emergency LightingSDR GUUA93932092909ALanding Gear · unknownFLIGHT: 9192, DURING DESCENT UNABLE TO LOWER LANDING GEAR PERFORMED MANUAL LANDING GEAR EXTENSION, OBTAINED THREE GREEN GEAR DOWN AND LOCKED INDICATION. LANDED WITHOUT INCIDENT. INSPECTED LANDING GEAR SYSTEM COMPONENTS NO DEFECTS FOUND. CYCLED LANDING GEARSep 29, 2009 · N82539 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA95271092809ATruss · crackedDURING MAGNETIC PARTICLE INSP, DISCOVERED 2 ENGINE TRUSS TUBES HAVE WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENG TRUSS TUBES WELD AREAS.Sep 28, 2009 · N87552 · Beech 1900D · Engine Mount SectionSDR GLBA20090929GUplock Switch · intermittentAIR RETURN - PILOTS REPORTED THE THE LANDING GEAR WOULD NOT RAISE AFTER TAKE OFF. RED UNSAFE LIGHTS WERE ON. PILOTS RECYCLED THE GEAR THEN IT WOULD NOT LWR. GEAR WAS MANUALLY PUMPED DOWN AND GOT 3 GREEN LIGHTS AND RED HANDLE LIGHTS WERE OUT. MX REMOVED AN Sep 28, 2009 · N208GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA20090926APcb · looseON FINAL APPROACH INTO ALS WITH GEAR DOWN AND FLAPS 35 DEG RT PROPELLER TRIED TO AUTOFEATHER RT OIL PSI WAS AROUND 95-100. MAINTENANCE REMOVED AND RE-INSTALLED THE A123 PRINTED CIRCUIT BOARD AND PERFORMED AN OPERATIONAL CHECK WICH WAS GOOD IAW MM 61-21-00-001Sep 26, 2009 · N254GL · Beech 1900D · Propeller/Propulsor System WiringSDR GUUA95452092509ADoor · stiffDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT AFT EMERGENCY EXIT DOOR HARD TO OPEN. CLEANED AND LUBRICATED RIGHT AFT EMERGENCY DOOR. OPERATIONAL CHECK OK FOR SERVICE.Sep 25, 2009 · N87554 · Beech 1900D · Emergency ExitsSDR GLBA20090928GSkin · damagedUPON INSPECTION OF THE ACFT A LIGHTNING STRIKE WAS FOUND ON THE RT ELEVATOR TOP SKIN. MAINTENANCE REMOVED AND REPLACED THE ELEVATOR I.A.W. 27-30-00. MX REMOVED AND REPLACED THE ELEVATOR HOWEVER THE ELEVATOR WAS REPAIRED AND THE RII INSPECTIONS COMPLIED WITH IASep 25, 2009 · N182YV · Beech 1900D · Elevator, Plate/SkinSDR GUUA93332092509ABracket · failedFLT: 9274. PILOT REPORTED LANDING GEAR HORN COMES ON AROUND 8O PERCENT N1. REPLACED RIGHT LANDING GEAR SWITCH BRACKET ASSEMBLY AND RIGGED LANDING GEAR SWITCHES AND AUTOFEATHER SWITCHES.OPERATIONAL CHECK NORMAL ON THE GROUND.TEST FLIGHT SATISFACTORY.Sep 25, 2009 · N81533 · Beech 1900D · Main Landing GearSDR GUUA94057092409ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WING STATIONS 123.988 THROUGH 196.06. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR DOUBLER.Sep 24, 2009 · N16540 · Beech 1900D · Wing, Plate/SkinSDR GUUA95752092409AControl Cable · brokenDURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR FWD LWR CONTROL CABLE BROKEN. REPLACED AIRSTAIR DOOR FWD LWR CONTROL CABLE.Sep 24, 2009 · N87557 · Beech 1900D · Entrance StairsSDR GLBA20090925FStructure · damagedLIGHTNING STRIKE ON THE LT ELEVATOR. DISCHARGE ON TRAILING EDGE APPROXIMATELY 9" TO 10.250" FROM TAB CUTOUT ON THE TOP AND BOTTOM SIDES. TRAILING EDGE DAMAGE APPROXIMATELY 1.5" BY .750" EIGHT INCHES OUT FROM TRIM TAB. MAINTENANCE REMOVED AND REPLACED THE ELEVSep 23, 2009 · N211GL · Beech 1900D · Elevator StructureSDR GUUA95032091909AWarning Horn · false activationFLIGHT 9130 DURING DESCENT LANDING GEAR WARNING HORN COULD NOT BE SILENCED USING BUTTON. INSPECTED LANDING GEAR SYSTEM NO DEFECTS NOTED. LANDING GEAR OPERATIONAL CHECKS NORMAL.Sep 19, 2009 · N87550 · Beech 1900D · Landing Gear Position and WarningSDR GUUA91221091809AUnknown · odorFLT 6001, DESCENDING THROUGH FOUR THOUSAND FT ODOR OBSERVED. PERFORMED TEST FLIGHT NO DEFECTS NOTED.Sep 18, 2009 · N45AR · Beech 1900D · Air Distribution SystemSDR GLBA20090921GDoor Latch · lack of lubeDURING ROUTINE SCHEDULED MAINTENANCE THE EMERGENCY EXT DOOR 6C DID NOT OPEN PROPERLY. MAINTENANCE LUBED THE LATCH MECHANICAL SHAFT, RE-INSTALLED THE DOOR I.A.W. BMM 52-20-00 STEPS A-C FOR REMOVAL AND INSTALLATION AND I.A.W. 52-20-01 STEP D FOR LUBING. NO RIGGSep 18, 2009 · N261GL · Beech 1900D · Emergency ExitsSDR GLBA20090921FDoor · stiffDURING ROUTINE SCHEDULED MAINTENANCE THE EMERGENCY EXT DOOR 4C DID NOT OPEN PROPERLY. MAINTENANCE LUBED THE LATCH MECHANICAL SHAFT, RE-INSTALLED THE DOOR IAW MM 52-20-00 STEPS A-C FOR REMOVAL AND INSTALLATION AND IAW 52-20-01 STEP D FOR LUBING. NO RIGGING WASSep 18, 2009 · N261GL · Beech 1900D · Emergency ExitsSDR GUUA91221091709AUnknown · odorFLIGHT 6005, DURING CRUISE AFTER ADDING HEAT A STRONG NASTY, MILDEW BURN ODOR COMES THROUGH CABIN. INSPECTED UNDER CABIN FLOOR BOARD BLOWERS AND TEST RAN ENGINES BLEED SYSTEM OPERATIONAL CHECKED GOOD NO ODOR DETECTED.Sep 17, 2009 · N45AR · Beech 1900D · Air Distribution SystemSDR GLBA20090918FFrame · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK IN THE AIRSTAIR DOOR LOWER FUSELAGE FRAME AT F.S. 173.41 AND STRINGER 11L. CRACK LENGTH APPROXIMATELY .750" IN LENGTH. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR LOWER FUSELAGE FRAME IAW E.OSep 16, 2009 · N255GL · Beech 1900D · Fuselage Main, FrameSDR GUUA91221091609ATube · damagedFLT 6001, DURING CRUISE FLIGHT WHEN ADDING HEAT CREW NOTICED STRONG EXHAUST TYPE ODOR. FOUND HOLE IN NR 2 BLAST TUBE, REPLACED NR 2 ENGINE OUTBOARD EXHAUST BLAST TUBE.Sep 16, 2009 · N45AR · Beech 1900D · Engine (Turbine/Turboprop)SDR GUUA95553091509AStructure · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED CORROSION ON FUSELAGE APPROXIMATELY AT FS 243 TO 258 AT STRINGER 15L. REMOVED DAMAGED SKIN AND INSTALLED INSERTION REPAIR PATCH AND EXTERNAL DOUBLER REPAIR AND REPAIRED DAMAGED STR.Sep 15, 2009 · N87555 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA94732091509AConnector · looseFLT 9291, DURING TAKEOFF LANDING GEAR UNSAFE LIGHTS FLICKERED. SECURED LOOSE CONNECTOR ON PCB E193. LANDING GEAR OPERATIONAL CHECK GOOD. SECURED LOOSE CONNECTOR ON PCB E173. LANDING GEAR OPERATIONAL CHECK GOOD.Sep 15, 2009 · N69547 · Beech 1900D · Landing Gear System WiringSDR GUUA91221091409AUnknown · odorPILOT REPORTED WHEN ADDING HEAT, STRONG ODOR OF BLEED AIR THROUGHOUT THE COCKPIT. TEST RAN BOTH ENGINES AND OPERATED ENVIRONMENTAL SYS. NO ODOR NOTICED, OPS CHECK GOOD.Sep 14, 2009 · N45AR · Beech 1900D · Air Distribution SystemSDR GUUA94957091409AAccess Panel · leakingDURING SCHEDULED ROUTINE INSP DISCOVERED RT WING COLLECTOR TANK FUEL ACCESS PANEL 632 AT, FUEL LEAK. FABRICATED AND INSTALLED EXTERNAL DOUBLER RING FOR RT UPPER WING FUEL ACCESS PANEL 632 AT.Sep 14, 2009 · N69549 · Beech 1900D · Wing, Plate/SkinSDR GLBA200909141Tube · deterioratedABORTED TAKEOFF- AIRCRAFT 247GL DID AN ABORTED TAKEOFF IN HVR FLT 5186 FOR RT BLEED AIR FAIL ANNUNCIATOR ILLUMINATING. CREW RETURNED TO GATE AND CALLED MX. THE CREW AND MX AGREED THAT IT COULD BE MEL'D UNDER 21-3-2 CAT B. THE CREW BEFORE DOING THE MEL RAN TSep 14, 2009 · N247GL · Beech 1900D · Engine Bleed Air SystemSDR GUUA93357091209AAccess Panel · leakingDURING SCHEDULED ROUTINE MX DISCOVERED FUEL LEAK AT RT WING LWR PANELS FOUND FUEL PANEL 631DB DELAMINATED AND WING SKIN DELAMINATED. FABRICATED AND INSTALLED INNER DOUBLER RING REPAIR AND OUTER DOUBLER REPAIR AT RT WING LWR SKIN FUEL PANEL 631DB.Sep 12, 2009 · N81533 · Beech 1900D · Wing, Plate/SkinSDR GLBA2009091409GSkin · crackedMAJOR REPAIR - PILOTS REPORTED THAT THE FUSELAGE WAS PUNCTURED IN THE LT FUSELAGE JUST FWD OF FS 273.25 ON THE UPPER SKIN. DAMAGED AREA APPROX 2.1 INCH BY 3.5 INCH. (2) CRACKS PRESENT. (1) CRACK APPROX 2.3 INCHES AND THE OTHER 1.1 INCH IN LENGTH. MX REPASep 12, 2009 · N218YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090914FSkin · gougedMAJOR REPAIR - PILOTS REPORTED A SMALL DENT IN THE LT FUSELAGE JUST FWD OF FS 258.25 ON THE UPPER SKIN. DAMAGED AREA APPROX .250 INCH BY .750 INCH. MX REPAIRED THE AFFECTED AREA IAW EO 09-1900-53-019. RII INSP C/W IAW GLA EO 09-1900-53-019.Sep 12, 2009 · N218YV · Beech 1900D · Fuselage Main, Plate/SkinSDR CA090911006Shaft · sheared(CAN) UPON APPROACH FLAPS FAILED TO EXTEND PAST INITIAL APPROACH SETTING. VISUAL INSPECTION ON THE GROUND BY FLIGHT CREW NOTED THAT R/H OUTBOARD FLAP HAD NOT EXTENDED. FLAPS AUTOMATICALLY STOPPED DUE SPLIT FLAP. FLAPS RETRACTED AND MEL`D. UPON INSPECTION R/H OSep 10, 2009 · Beech 1900D · Trailing Edge Flap Control SystemSDR GLBA20090910ATurbine Wheel · damagedPILOTS REPORTED THAT UPON TAKEOFF WITH TORQUE ONLY AT 3200 FOOT LBS. RT ITT EXCEEDED 800 C. AND THE TAKEOFF WAS THEN ABORTED. MX PERFORMED MANY CHECKS INCLUDING AN INSP OF THE BLEED AIR VALVE IAW 75-30-00. MX PERFORMED A HOT SECTION BORESCOPE AND FOUND SOME RSep 10, 2009 · N208GL · Beech 1900D · Turbine SectionSDR GLBA2009Skin · crackedMAJOR REPAIR - WHILE PERFORMING OTHER MAINTENANCE RELATED TO AN ANTENNA REPLACEDMENT A RIVET HEAD WAS FOUND MISSING AND TWO SMALL CRACKS WERE FOUND THAT WERE APPROXIMATELY .2" IN LENGTH EMMANATING FROM RIVET HOLE ON THE TOP AT F.S. 150.6 TO RIGHT OF THE CENTERSep 9, 2009 · N182YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090909HSkin · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE BELLY SKIN AT B.L. 29.0 AND F.S. 303.25. CRACK IS APPROXIMATELY 2.250" IN LENGTH. MAINTENANCE REPAIRED THE BELLY SKIN AT F.S. 303.25 AND B.L 29.0 IAW EO 09-1900-53-016. RII INSPECTIOSep 8, 2009 · N154GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA95052090709BDoor · lack of lubeDURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT DOOR HARD TO OPEN. LUBED RT AFT EMERGENCY EXIT DOOR. OPS CHECK NORMAL.Sep 7, 2009 · N87550 · Beech 1900D · Emergency ExitsSDR GUUA95052090709ADoor · lack of lubeDURING SCHEDULED ROUTINE INSP, DISCOVERED RT FWD EMERGENCY EXIT DOOR HARD TO OPEN. LUBED RT FWD EMERGENCY EXIT DOOR. OPS CHECK NORMAL.Sep 7, 2009 · N87550 · Beech 1900D · Emergency ExitsSDR ERAA200900008Transducer · shortedFAI - UPON CLIMBOUT FROM FAI FOUND OIL PRESSURE WENT TO "0" ON RIGHT ENGINE. SHUT DOWN RIGHT ENGINE AND RETURNED TO FAI. REPLACED ENGINE OIL PRESSURE XDCR S/N 4518-1-247 WITH S/N 7651-6-137. RAN ENGINE, OPERATED NORMALLY.Sep 5, 2009 · N972EA · Beech 1900D · Engine Oil PressureSDR GUUA91252090209ADoor · lack of lubeDURING SCHEDULED ROUTINE MX, DISCOVERED LT EMERGENCY EXIT HARD TO OPEN. LUBED LT EMERGENCY EXIT, OPS CHECK SATISFACTORY.Sep 2, 2009 · N45AR · Beech 1900D · Emergency ExitsSDR GLBA20090902AOutflow Valve · malfunctionedACFT WOULD NOT PRESSURIZE DURING CLIMB OUT. MX SECURED THE RT OUTFLOW VALVE THAT WAS FOUND LOOSE IAW MM 21-30-01-201. AN OPS TEST FLIGHT WAS CONDUCTED AND FOUND TO BE SATISFACTORY.Sep 2, 2009 · N247GL · Beech 1900D · Pressure Regulator/Outflow Valve
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