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 GLBA20090403FKeelbeam · crackedLT INBD KEEL REPAIR REQUIRES ACCOMPLISHMENT IAW EO 09-251-03 REV.0. MX REPAIRED THE LT INBD KEEL IAW EO 09-251-03. FABRICATED POCKET DOUBLER USING INSTRUCTIONS DIMENSIONS AND MATERIALS ON DRAWING DRW-HBGA-001 AND FIGURE 1. HYSOL EA 9394 USED TO BOND POCKET DOApr 2, 2009 · N251GL · Beech 1900D · Fuselage Main, KeelSDR 19MA20091128Wheel · wornPILOT REPORTED VIOLENT SHIMMY ON TAKEOFF AND LANDING. REMOVED NOSE WHEEL AND INSTALLED SERVICEABLE NOSE WHEEL AND TIRE ASSY. INSPECTED NLG AND FOUND NO DISCREPANCIES. CHECKED SHIMMY DAMPENER AND FOUND TO BE SERVICEABLE. OK.Mar 31, 2009 · N567MA · Beech 1900D · Wheel/Ski/FloatSDR GLBA20090331ACircuit Board · wornAIR RETURN- A/C N192GL - FLIGHT 5028 PILOTS REPORT THAT LANDING GEAR UNSAFE LIGHT WILL NOT GO OUT ON GEAR RETRACTION ON TAKEOFF AND HORN CAME ON. MAINTENANCE REMOVED AND REPLACED THE A119 PRINTED CIRCUIT BOARD PER MM 32-60-00. OPERATIONAL CHECK FLIGHT WAS PEMar 31, 2009 · N192GL · Beech 1900D · Landing Gear System WiringSDR GUUA93832032909ASwitch · out of adjustLANDING GEAR WARNING HORN IS ACTIVATED AT 79.5 TO 80 PERCENT, N1 WITH LT POWER LEVER AND 75 PERCENT, N1 WITH RT PWR LEVER. ADJUSTED LANDING GEAR POWER LEVER SWITCHES. TEST FLIGHT SATISFACTORY.Mar 29, 2009 · N81538 · Beech 1900D · Power LeverSDR GUUA94132032909APcb · failedPILOT REPORTED NO 3 GREEN GEAR INDICATION LIGHTS. REPLACED PCB A319. LANDING GEAR OPERATIONAL CHECK NORMAL.Mar 29, 2009 · N17541 · Beech 1900D · Landing Gear Position and WarningSDR GUUA94132032908APcb · damagedPILOT REPORTED NO 3 GREEN GEAR INDICATION LIGHTS. REPLACED PCB A319. LANDING GEAR OPS CHECK, NORMAL.Mar 29, 2009 · N17541 · Beech 1900D · Landing Gear Position and WarningSDR GLBA20090329AWindshield · crackedPILOTS REPORTED THAT THE CAPTAINS WINDSHIELD CRACKED ON/IN CRUISE FLIGHT. AIRCRAFT RETURNED TO "DEN". MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDOW IAW SRM 56-10-00.Mar 29, 2009 · N237YV · Beech 1900D · Flight Compartment WindowsSDR GLBA20090329BSwitch · dirtyPILOTS REPORTED THAT UPON GEAR RETRACTION THE HORN WAS ON WITH GEAR UNSAFE LIGHTS. MAINTENANCE INSPECTED & CLEANED LANDING GEAR UPLOCK SWITCHES & INSPECTED PRINTED CIRCUIT BOARD CONNECTOR. NO DEFECTS WERE NOTED. REFEREMCE BMM 32-60-00. OPS CHECK FLIGHT WAS PMar 29, 2009 · N192GL · Beech 1900D · Landing Gear Position and WarningSDR GUUA94132032809ACircuit Breaker · trippedDURING APPROACH LANDING GEAR INDICATION CIRCUIT BREAKER POPPED AFTER SELECTING GEAR DOWN. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. OPS CHECK FOUND TO BE WORKING OK. INSPECTED LANDING GEAR SYSTEMS UNABLE TO FIND ANY PROBLEM OPERATIONAL CHECK OK.Mar 28, 2009 · N17541 · Beech 1900D · Landing Gear System WiringSDR GUUA95652032709ADoor · out of rigDURING SCHEDULED ROUTINE INSP, DISCOVERED EMERGENCY EXIT DOOR AT SEAT 4F OUT OF RIG. RIGGED AND LUBED SEAT 4F EMERGENCY EXIT DOOR. OPS CHECK GOOD.Mar 27, 2009 · N81556 · Beech 1900D · Emergency ExitsSDR GUUA93357032709ASkin · corrodedDURING FURTHER INSP OF RT WING UPPER SKIN SURFACE CORROSION DISCOVERED DEBOND BETWEEN WS 146.00 THROUGH 171.00. REMOVED DAMAGED OF RIGHT WING UPPER SKIN FROM WS 126.50 TO 196.06 AND INSTALLED EXTERNAL DOUBLER REPAIR.Mar 27, 2009 · N81533 · Beech 1900D · Wing, Plate/SkinSDR GUUA93355032709AHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED LT ELEVATOR CENTER HINGE BRACKET CORRODED. REPLACED LT ELEVATOR CTR HINGE BRACKET.Mar 27, 2009 · N81533 · Beech 1900D · Elevator StructureSDR GLBA200903261Landing Gear · malfunctionedPILOTS REPORTED THAT THE LANDING GEAR WOULD NOT COME UP. MAINTENANCE INSPECTED ALL UP AND DOWNLOCK SWITCHES AS WELL AS THE SQUAT SWITCHES. PERFORMED LANDING GEAR SWINGS AND ALL OPERATIONALLY CHECKED GOOD. COULD NOT DUPLICATE DISCREPANCY. REFERENCE B1900D MM 3Mar 26, 2009 · N192GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20090326ACircuit Board · malfunctionedPILOTS REPORTED A LEFT HAND FIRE LOOP ANNUNCIATOR REPEATEDLY TRIPPED IN FLIGHT. ALSO STARTED TRIPPING LEFT HAND T-HANDLE AND MASTER WARNING ANNUNCIATOR (FLASHES). MAINTENANCE RE-RACKED THE FIRE EXTINGUISHING MONITOR PRINTED CIRCUIT BOARD P173. OPERATIONAL CHEMar 26, 2009 · N220GL · Beech 1900D · Detection SystemSDR GUUA93355032609AHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT ELEVATOR OTBD HINGE BRACKET CORRODED. REPLACED RT ELEVATOR OTBD HINGE BRACKET.Mar 26, 2009 · N81533 · Beech 1900D · Horizontal Stabilizer StructureSDR 2009FA0000250Doubler · corrodedDURING SCHEDULED INSP, NOTED CORRODED STEEL DOUBLER INSTALLED UNDER 13R STRINGER AFT OF FS 557.5 AFT PRESSURE BULKHEAD FRAME. STEEL DOUBLERS OR SHIMS NOT TYPICALLY INSTALLED, THIS LOCATION, NOT NOTED IN IPC OR SRM. INSTALLATION INFORMATION NOT AVAILABLE FROM OMar 24, 2009 · N152MJ · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA91227032309ATrim Tab · corrodedDURING SCHEDULED MX, DISCOVERED RUDDER TRIM ATTACH HORN HAS CORROSION. REPLACED RUDDER TRIM TAB.Mar 23, 2009 · N45AR · Beech 1900D · Rudder, Tab StructureSDR GLBA20090326FSkin · dentedMAJOR REPAIR - LT OUTBOARD WING LEADING EDGE BIRDSTRIKE REPAIR AT APPROXIMATELY WS 281 TO 301. DENT APPROXIMATELY 5/8TH INCH DEEP. MAINTENANCE REPAIRED THE LT OUTBAORD LEADING EDGE AT WS 281 TO 301 IAW EO 09-UE257-01. SKIN REPAIRED OUT OF PN 118-110047-81. Mar 23, 2009 · N257GL · Beech 1900D · Wing, Plate/SkinSDR GLBA200903212Actuator · wornPILOTS REPORTED THAT DURING GEAR EXTENSION THE LEFT MAIN GEAR WAS FLICKERING ON AND OFF AND REC IN TRANSIT LIGHTS WERE ILLUMINATED. THEY RECYCYLED THE LANDING GEAR AND STILL HAD NO GREEN LIGHTS ON THE LEFT MAIN GEAR. THEY PERFORMED A MANUAL GEAR EXTENSION AND Mar 21, 2009 · N182YV · Beech 1900D · Landing Gear ActuatorSDR GLBA200903211Cable · loosePILOTS REPORTED THAT TAKEOFF ABORTED DUE TO 2 PROP RPM AT 1500. MAINTENANCE FOUND THE GOVERNOR CONTROL CABLE LOOSE FROM FORWARD MOUNT. RE-ATTACHED & SAFETIED. OPERATIONAL CHECKS GOOD I.A..W 61-20-00.Mar 21, 2009 · N218YV · Beech 1900D · Propeller Controlling SystemSDR GLBA20090320ASolenoid · out of rigPILOTS REPORTED THAT THE AIRCRAFT YAWED TO THE LEFT JUST PRIOR TO TOUCHDOWN. MAINTENANCE RIGGED THE RIGHT HAND LOW PITCH SOLENOID. OPERATIONAL CHECKS WERE GOOD.Mar 20, 2009 · N154GK · Beech 1900D · Propeller Controlling SystemSDR GLBA20090320BSolenoid · out of rigPILOTS REPORTED THAT WHILE ADDING TAKEOFF POWER THE RIGHT ENGINE WENT INTO FEATHER THROUGH APPROXIMATELY 1500 LB OF. TORQUE. MAINTENANCE RIGGED THE RIGHT HAND PROP BETA VALVE AND RIGHT HAND LOW PITCH SOLENOID. REFERENCE MM 76-10-00. OPERATIONAL CHECK WAS GOOD.Mar 20, 2009 · N153GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20090319GSkin · crackedDURING ROUTINE MX A SKIN CRACK WAS FOUND AROUND (3) RIVETS AT FS 150.6 AND STRINGER 1. CRACK LENGTH VARIED FROM .450 INCH TO .100 INCH. MX REPAIRED SKIN CRACKS AT FS 150.6 AND STRINGER 1 IAW. EO-09-UE251-02. REPAIR AREA 4 INCH BY 7 INCH OUT OF 2024-T3, .040Mar 18, 2009 · N251GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA200903181Skin · crackedSKIN FUSELAGE CRACK ON TOP AT FS 150.6 AT AROUND STRINGER NR 1.Mar 18, 2009 · N251GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090319HAngle · crackedDURING ROUTINE SM A 1.625 INCH CRACK WAS FOUND ON THE LT HEAVY ANGLE AT F.S.288.0. MX REPAIRED THE LT HEAVY ANGLE DOUBLER IAW EO-UE245-01. REPAIR APPROX 13.6 INCH OUT OF PN 114-430002-7179, PLT210-8-10, HLT 428-6, CR3553P6 MS20470AD5, MS20470AD6 RIVETS.Mar 14, 2009 · N245GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20090319FSkin · dentedON THE POST FLIGHT CHECK THE PILOT FOUND A DENT AND 10 INCH SCRATCH WERE FOUND AT FRAME STA470- 480 . SCRATCH/DENT WAS APPROX 10 INCH IN LENGTH. MX CUT OUT DAMAGED AREA AND PATCHED. PATCH MADE OUT OF .050 INCH 2024 T-3 ALCLAD AND INSTALLED USING MS20470AD RIVEMar 14, 2009 · N251GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090313BSkin · scratched10 INCH SCRATCH AND ASSOCIATED DENT BELOW THE CARGO DOOR ON THE FUSELAGE.Mar 13, 2009 · N251GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2009031309ACircuit Board · malfunctionedON EXENED BASE POWER AT 1200 FT. LBS. ENGINES WERE GOING IN AND OUT OF FEATHER. MAINTENANCE RE-RACKED THE AUTOFEATHER PRINTED CIRCUIT BOARD AND THEY SYSTEM OPERATIONALLY CHECKED GOOD PER BMM 61-21-00-0001. OPERATION CHECK OF AUTOFEATHER SYSTEM GOOD PER 61-21-0Mar 13, 2009 · N202UX · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20090312ARelay · deterioratedPILOTS REPORTED THAT THE FLAPS STUCK INTERMITTENTLY AT 17 DEGREES AND EVENTUALLY CAME UP UPON LANDING. MAINTENANCE REMOVED AND REPLACED FLAP RELAY I.A.W. BMM 27-50-05 OPERATIONAL CHECKS WERE GOOD PART NUMBER ON/OFF. SM50B7 CLEARED MEL AND PLACARDS WERE REMOVEMar 12, 2009 · N154GL · Beech 1900D · Trailing Edge Flap Control SystemSDR CA090310013Hub · cracked(CAN) DURING LPI, A CRACK WAS FOUND IN ONE OF THE MOUNTING FLANGE DOWEL HOLES. HUB IS U/S IAW MANUAL NR 202ARV3R31.Mar 10, 2009 · Beech 1900D · Propeller Hub SectionSDR GUUA92753030809ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED CORROSION ON THE FUSELAGE BELLY UNDER BEACON LIGHT MOUNTING PLATE AT FS 370.750. REMOVED CORROSION AT BEACON LIGHT CUTOUT AND INSTALLED EXTERNAL DOUBLER REPAIR.Mar 8, 2009 · N46AR · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA94252030709AHandle · lack of lubeDURING SCHEDULED ROUTINE INSP DISCOVERED EMERGENCY EXIT DOOR AT SEAT 6F EXTERNAL HANDLE IS TIGHT AND DOES NOT SPRING OUT. LUBRICATED HANDLE, OPS CHECK GOOD.Mar 7, 2009 · N47542 · Beech 1900D · Emergency ExitsSDR GUUA94057030709ASkin · corrodedDURING FUTHER INSPECTION OF SURFACE CORROSION DISCOVERED SEVERE CORROSION EXTENDS FROM WS 140.00 TO 190.00 APROXIMATELY. CUT OUT DAMAGED AREA AND INSTALLED AN EXTERNAL DOUBLER REPAIR.Mar 7, 2009 · N16540 · Beech 1900D · Wing StructureSDR GUUA94055030609AHinge Bracket · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT ELEVATOR OTBD HINGE BRACKET HAS SURFACE CORROSION. REPLACED LT ELEVATOR OUTBOARD HINGE BRACKET.Mar 6, 2009 · N16540 · Beech 1900D · Elevator Miscellaneous StructureSDR GLBA20090305ALanding Gear · malfunctionedFLIGHT 5158 UPON APPROACH THE PILOTS REPORTED THAT THE RIGHT MAIN LANDING GEAR WOULD NOT EXTEND. PILOTS PERFORMED A MANUAL EXTENSION. MAINTENANCE CLEANED THE RIGHT HAND DOWNLOCK SWITCH AND PERFORMED SIX LANDING GEAR EXTESNIONS AND RETRACTIONS IAW MM 32-30-00. Mar 5, 2009 · N253GL · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA94952030509ACable Assy · frayedDURING SCHEDULED ROUTINE INSP, DISCOVERED AIRSTAIR DOOR COUNTER BALANCE CABLE ASSEMBLY FRAYED. REPLACED AIRSTAIR DOOR COUNTER BALANCE CABLE ASSY.Mar 5, 2009 · N69549 · Beech 1900D · Entrance StairsSDR GLBA200903041Pedestal · out of adjustUPON SHORT FINAL THE PILOTS REPORTED THAT THE RIGHT HAND PROPELLER BEGAN TO CYCLING IN AND OUT OF AUTOFEATHER. THE PILOT INCREASED POWER HOWEVER IT DID NOT FIX THE PROBLEM. PILOTS TURNED OF THE AFX AND IT STOPPED FEATHERING. MAINTENANCE INSPECTED THE AUTOFEATHMar 4, 2009 · N211GL · Beech 1900D · Propeller Feathering/ReversingSDR GUUA95052030409BDoor · out of adjustDURING SCHEDULED ROUTINE INSP, DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. ADJUSTED RT AFT EMERGENCY EXIT DOOR. OPS CHECK GOOD.Mar 4, 2009 · N87550 · Beech 1900D · Emergency ExitsSDR GUUA95052030409ADoor · out of adjustDURING SCHEDULED ROUTINE INSP, DISCOVERED RT FWD EMERGENCY EXIT STUCK ON FUSELAGE CUT OUT. ADJUSTED RT FWD EMERGENCY EXIT DOOR. OPS CHECK GOOD.Mar 4, 2009 · N87550 · Beech 1900D · Emergency ExitsSDR GLBA20090305FAngle · misrepairedMAJOR REPAIR - DURING ROUTINE SHEDULED MAINTENANCE, DURING CONFORMITY CHECKS, A PREVIOUS REPAIR ON THE RIGHT HAND SIDE OF FUSELAGE TO VERTICAL DORSAL FIN ANGLE DOES NOT CONFORM. FS 557.5 11.4" LONG. MAINTENANCE REPAIRED THE RT SIDE OF THE FUSELAGE TO VERTICALMar 4, 2009 · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA92753030109ASkin · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED AIRCRAFT FUSELAGE BELLY EXFOLIATION AT F.S 227.630 BETWEEN STRINGERS 2R AND 3R. DURING FUTHER INSPECTION EXFOLIATION LOCATED FS 327.630 AIRCRAFT BELLY BETWEEN STRINGER 14R AND 15R NOT STRINGERS 2R AND 3R REMOVED Mar 4, 2009 · N46AR · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090315AGovernor · low torqueABORTED TAKEOFF BECAUSE THE RT PROPELLER RPM ONLY CAME UP TO 1600 AND THEY THEN ABORTED THE TAKEOFF. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE RIGHT PROPELLER GOVERNOR OUT RIG. MAINTENANCE RIGGED THE ENGINEBY TURNING THE PROP RPM SCREW OUT AND TESTED THMar 3, 2009 · N218YV · Beech 1900D · Propeller GovernorSDR GLBA20090304ISkin · dentedDURING ROUTINE SHEDULED MAINTENANCE THE LT WING, OUTBOARD LEADING EDGE WAS FOUND DENTED AND REQUIRES REPLACEMENT. REPAIRED LT LEADING EDGE SECTION FROM WS 223-271. WORK PERFORMED PER FR-CO-01895 REV.2. STEPS 1 -15, 16 LEAK CHECK OF AFFECTED AREAS PERFORMEMar 3, 2009 · N165YV · Beech 1900D · Wing, Plate/SkinSDR GLBA20090304HSwitch · out of adjustFLT 5106 - ON APPROACH THE PILOTS REPORTED THAT THE NR 2 ENGINE CYCLES IN AND OUT OF FEATHER AT APPROXIAMTELY 1000 LBS. OF TORQUE AS THEY INCREASED POWER ON FINAL. THEY WERE NOT SURE OF THE N1 AT THE TIME. MAINTENANCE REMOVED AND REPLACED THE PROP OVERSPEED GMar 3, 2009 · N255GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20090302FSkin · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE LEFT FUSELAGE SKIN AT FS 273.25 AT STRINGER 10L. CRACK APPROXIMATELY 3.6 INCH IN LENGTH RUNNING PARALLEL TO STRINGER 10L. ABOVE CRACK AT STRINGER 10L AT NEXT RIVET LOCATION. MAINTEMar 1, 2009 · N153GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090301BIndicator · wornFLIGHT 5014- NO AIRSPEED INDICATION ON CA AIRSPEED ON T/O ROLL. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIRSPEED INDICATOR IAW TASKCARD 1900.3411.00-1. OPERATIONAL CHECK WAS GOOD.Mar 1, 2009 · N154GL · Beech 1900D · Airspeed/Mach IndicatorSDR GLBA20090301ASquat Switch · dirtyFLIGHT 5062- GEAR WOULD NOT RETRACT ON DEPARTURE. CLEANED RT SQUAT SWITCH PERFORMED GROUND RETRACTS OPS CK NORMAL IAW BMM 32-60-00. OPERATIONAL CHECKS WERE NORMAL.Mar 1, 2009 · N245GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA20090228AEngine · out of rigPOWER LEVERS SEEM OUT OF ADJUSTMENT. THERE IS A LARGE SPLIT BETWEEN LEVERS IN FLIGHT, THE LANDING GEAR WARNING HORN GOES ON AT ABOUT 2100 LBS OF TORQUE, AND THE ENGINES IDLE AT ABOUT 74% N1 WITH THE POWER LEVERS AT IDLE. MAINTENENANCE RIGGED THE NR 1 & 2 ENGFeb 28, 2009 · N255GL · Beech 1900D · Power LeverSDR GLBA20090227CSquat Switch · dirtyFLIGHT 5189 - PILOTS REPORTED THAT AFTER TAKEOFF THE STALL HEAT ANNUNCIATOR ILLUMINATED AND THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT. MAINTENANCE INSPECTED AND CLEANED THE LEFT HAND SQUAT SWITCH IAW MM 32-60-05. NO DEFECTS WERE NOTED AND THE OPERATIONAL CHFeb 27, 2009 · N257GL · Beech 1900D · Landing Gear Position and WarningSDR GLBA20090227AAltimeter · inoperativeFLIGHT 5096 - PILOTS REPORTED THAT THE FIRST OFFICERS ALTIMETER WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS ALTIMETER IAW MM 31-10-00. PERFORMED ENCODER CHECK WHICH OPERATIONALLY CHECKED GOOD IAW FAR 43 APPENDIX (E) (A) & (C) (A). MAIFeb 27, 2009 · N231YV · Beech 1900D · Altimeter, Barometric/Encoder
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