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 GLBA20090424BGenerator · failedPILOTS REPORTED THE THE LEFT DC GENERATOR FELL OFFLINE ON TAKEOFF ROLL. MAINTENANCE PERFORMED AN OPERATIONAL CHECK PER MM 24-00-00-001. NO FAULTS WERE FOUND AND THE AIRCRAFT WAS RETURNED TO SERVICE.Apr 24, 2009 · N154GL · Beech 1900D · DC Generating SystemSDR GUUA93957042209ASpar · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED CORROSION AT RT FWD SPAR FLANGE JUST BEHIND DRAIN PLUG WS 126.5. BLENDED OUT CORROSION AT RT FWD MAIN SPAR FLANGE JUST BEHIND DRAIN PLUG.Apr 22, 2009 · N82539 · Beech 1900D · Wing SparSDR GLBA200904225Pressure Switch · wornON APPROACH AT 500 LBS TORQUE, WHILE LEVELING ALTITUDE AND ADVANCING POWER THE R/H ENGINE ATTEMPTED FEATHER CAUSING CYCLES SIMILAR TO AUTOFEATHER TEST. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND AUTOFEATHER LOW PRESSURE SWITCH AND COMPLIED WITH FCD 1900-0Apr 22, 2009 · N210GL · Beech 1900D · Propeller Feathering/ReversingSDR GUUA95032042209ASafety Switch · out of adjustFLIGHT: 9142, AFTER TAKEFOFF, LANDING GEAR WOULD NOT RETRACT. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. ADJUSTED RT MAIN GEAR SAFETY SWITCH. OPS CHECK NORMAL.Apr 22, 2009 · N87550 · Beech 1900D · Landing Gear Position and WarningSDR GUUA93957042109CStringer · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED SMALL AREA OF CORROSION AT LT COLLECTOR TANK STRINGER J WS 118.50. REMOVED CORROSION AT LEFT COLLECTOR TANK STRINGER J WS 118.50 AND INSTALLED REPAIR DOUBLER STRAP.Apr 21, 2009 · N82539 · Beech 1900D · Wing, Longeron/StringerSDR GUUA93957042109BStringer · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED SMALL AREA OF CORROSION AT LT WING COLLECTOR TANK STRINGER J WS 119.00. REMOVED CORROSION AT LEFT WING COLLECTOR TANK STRINGER J AND INSTALLED EXTERNAL DOUBLER REPAIR.Apr 21, 2009 · N82539 · Beech 1900D · Wing, Longeron/StringerSDR GUUA93957042109ASpar · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED SMALL AREA OF CORROSION AT LT WING FWD SPAR FLANGE WS 125.25. REMOVED SURFACE CORROSION AT LEFT WING FORWARD SPAR WS 125.25 AND INSTALLED REPAIR DOUBLER STRAP.Apr 21, 2009 · N82539 · Beech 1900D · Wing SparSDR GLBA20090424FSkin · leakingDURING SCHEDULED MX A FUEL LEAK WAS FOUND ON THE LT WING LE ON A PREVIOUS REPAIR FROM APPROX WS 239 TO WS 249.75. MX REPAIRED THE LT WING LE PREVIOUS REPAIR IAW EO-09-1900-57-004. ALL RII INSP REQUIREMENTS COMPLIED WITH IAW EO-09-1900-57-004.Apr 21, 2009 · N182YV · Beech 1900D · Wing, Plate/SkinSDR GLBA200904215Fcu · out of adjustON SHORT FINAL WITH PROPELLERS AT 1700 , THE NR 2 PROPELLER SEEMED LIKE IT TRIED TO FEATHER MOMENTARILY TWO OR THREE TIMES. THE RPM DROPPED TO APPROXIMATELY 1400 TO 1500 RPM EACH TIME. MAINTENANCE ADJUSTED THE RT FCU PICKUP ROD, INPUT ARM AND LOW IDLE ADJUSTApr 21, 2009 · N153GL · Beech 1900D · Fuel Control/Turbine EnginesSDR GUUA93953042009DSkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED .5 INCH CRACK ON RT FUSELAGE BELLY AT FS 213.250. CLEANED AREA OF SUSPECT CRACK DYE PENETRANT INSPECTION PERFORMED NO CRACKS FOUND.Apr 20, 2009 · N82539 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA93953042009CSkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT FUSEALGE BELLY EXFOLIATED AT FS 423.250. REMOVED CORRODED SECTION OF SKIN AND SECTION OF STRINGER 16 AT FS 423.250 BETWEEN FS 415.250 AND 430.250 REPAIRED STRINGER AND INSTALLED EXTERNAL REPAIR PATCH AND DOUBLER.Apr 20, 2009 · N82539 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA93953042009BSkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT FUSEALGE BELLY EXFOLIATED AT FS 327.630. REMOVED CORRODED SECTION OF FUSELAGE SKIN CUT STRINGER 15R AND STRINGER 16 INSTALLED REINFORCEMENT STRAP,STRINGER AND REPAIR PATCH.Apr 20, 2009 · N82539 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA93953042009ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT FUSELAGE BELLY EXFOLIATED AT FS 243.250. REMOVED CORRODED SECTION OF SKIN AT FS 243.250 AND DAMAGED SECTION OF STRINGER 15R REPAIRED STRINGER 15R,FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR FROM FS 228.250 TO 2Apr 20, 2009 · N82539 · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090423FSkin · crackedDURING A SCHEDULED STRUCTURAL INSP, A CRACK WAS FOUND IN THE BELLY SKIN AT FS 303 AND BL29 APPROX 5.6 INCH IN LENGTH. MX REPAIRED THE BELLY SKIN AT FS 303 AND BL29 IAW EO 09-1900-53-005. MATERIALS UTILIZED INCLUDE .050 INCH 2024-T3 AL ALCLAD, .040 INCH 2024-TApr 20, 2009 · N254GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2009042009AController · malfunctionedFLT.5187 WHILE AT FLIGHT LEVEL 25000, LOST CABIN PRESSURE, DEPLOYED O2 MASKS AND RETURNED TO FMN. INFLIGHT EMERGENCY DECLARED. AIR TURNBACK PILOTS REPORTED THAT DURING CRUISE THEY EXPERIENCED A LOSS OF CABIN PRESSURIZATION AT 25000 FT. CABIN WENT TO ZERO Apr 20, 2009 · N100UX · Beech 1900D · Cabin Pressure ControllerSDR GUUA93721041909AUnknown · odorFLIGHT: 9180, DURING FLIGHT, STRONG BURNING RUBBER ODOR WITH RT BLEED AIR VALVE OPEN, GOES AWAY WHEN VALVE IS CLOSED, HAPPENS ONLY IN FLIGHT. INSPECTED FUEL LINES ,OIL LINES BYPASS AND THRU VALVE PERFORMED RUN UPS AT 90 PERCENT WITH BLEEDS ON NO DISCREPANCY FOApr 19, 2009 · N38537 · Beech 1900D · Air Distribution SystemSDR GUUA91232041909ASwitch · out of adjustPILOT REPORTED LANDING GEAR WARNING HORN GOES OFF AT 79 PERCENT N1. ADJUSTED LT POWER LEVER GEAR WARNING HORN SWITCH.Apr 19, 2009 · N45AR · Beech 1900D · Landing Gear Position and WarningSDR GLBA200904191Gasket · damagedAFTER TAKEOFF, PROP GAUGE FOR NR 1 ENGINE DROPPED TO 0 RPM AND REMAINED THERE FOR THE REMAINDER OF THE FLIGHT AND TAXI. MAINTENANCE R & R NR 1 ENGINE TACH GENERATOR. MAINTENANCE THEN INSTALLED A GASKET, TACH GEN, AND GROUND RAN NR 1 ENGINE WHICH OPERATIONALLApr 19, 2009 · N153GL · Beech 1900D · Propeller Indication SystemSDR GUUA94527041809BTorque Tube · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT ELEVATOR TORQUE TUBE BASE SHOWS SIGNS OF EXFOLIATION. REPLACED RT ELEVATOR TORQUE TUBE.Apr 18, 2009 · N53545 · Beech 1900D · Elevator StructureSDR GUUA94527041809AHinge · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT ELEVATOR OTBD HINGE BLOCK SHOWING SIGNS OF EXFOLIATION. REPLACED LT ELEVATOR.Apr 18, 2009 · N53545 · Beech 1900D · Elevator StructureSDR GUUA93734041809ADisplay · intermittentDURING FLIGHT, CAPTAIN`S EADI FLICKERED A FEW TIMES, DISPLAY THEN SHRUNK FOLLOWED BY STRONG BURNING ODOR. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE AT EFIS SCREEN COOLING FAN. OPS CHECK NORMAL.Apr 18, 2009 · N38537 · Beech 1900D · Attitude and Direction Data SystemSDR GLBA20090418ACircuit Board · malfunctionedHAD MASTER WARNING AND MASTER CAUTION ANNC FLASHERS ON TAKEOFF, ABORTED. MASTER WARNING FLASHERS SEEMS TO COME ON ANYTIME MASTER CAUTION FLASHERS COMES ON. MAINTENANCE R & R PRINTED CIRCUIT BOARD. OPERATIONAL CHECKS WERE GOOD IAW MM 31-61-10.Apr 18, 2009 · N240GL · Beech 1900D · Central WarningSDR GUUA94652041609ACable · brokenPILOT REPORTED CABIN DOOR WILL NOT OPEN. REPLACED FWD LOWER DOOR CABLE, OPS CHECK OK.Apr 16, 2009 · N81546 · Beech 1900D · Passenger/Crew DoorsSDR GLBA20090420GFrame · crackedDURING A SCHEDULED STRUCTURAL CHECK, MX DISCOVERED A CRACK ON THE RT HEAVY ANGLE AT FA 288.0. LENGTH OF CRACK APPROX 1.5 INCH LONG. MX REPAIRED THE RT HEAVY ANGLE AT FA 288.0. IAW. EO-09-1900-53-003. REPAIR AREA APPROXIMATELY 13.5 INCH LONG OUT OF PN 114-430Apr 16, 2009 · N261GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20090420FSkin · crackedDURING A SCHEDULED STRUCTURAL CHECK MX DISCOVERED A CRACK ON THE LT FUSELAGE SKIN JUST INBD OF THE LT WING BOTTOM WING PANEL AT F.S. 303.25. CRACK APPROXIMATELY 2.250 INCHES IN LENGTH. MX REPAIRED THE CRACK ON THE LT FUSELAGE SKIN JUST INBD OF THE LT WING BOTApr 16, 2009 · N261GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA94132041609ASquat Switch · failedDURING TEST FLIGHT LT MAIN LANDING GEAR DID NOT EXTEND. MANUALLY EXTENDED LANDING GEAR. LT MAIN GEAR ILLUMINATED DOWN AND LOCKED. OBTAINED 3 GREEN DOWN AND LOCKED INDICATION. REPLACED LT MLG SQUAT SWITCH ASSY. TEST FLIGHT SATISFACTORY.Apr 16, 2009 · N17541 · Beech 1900D · Landing Gear Position and WarningSDR GLBA20090414AConnector · looseLT PROP GAUGE READ 2000 RPM AFTER SETTING T/O POWER. MAINTENANCE CLEAND AND RE-SECURED CONNECTOR ON THE INDICATOR. ENGINE RUNS WERE PERFORMED WITH THE PILOTS AND THE OPERATIONAL CHECKS WERE GOOD PER MM 77-10-00.Apr 14, 2009 · N253GL · Beech 1900D · Propeller/Propulsor System WiringSDR GUUA93854041209AKeel · damagedLT NACELLE KEEL DAMAGED PREVIOUS REPAIR. AMENDED REPAIR BY BONDING REPAIR DOUBLERS IAW FAA APPROVED DATA.Apr 12, 2009 · N81538 · Beech 1900D · Nacelle/Pylon, Main FrameSDR CA090504007Bearing · contaminated(CAN) BEARINGS AND RACES OF MAIN WHEEL ASSY FOUND TO BE GOLD/BROWN IN COLOR. ADEQUATE GREASE WAS PRESENT. EXTREMELY ODD COLOR FOR A BEARING. 2-3 MONTHS PRIOR CMA SWITCHED FROM 28 GREASE TO SHC 100 AVIATION GREASE. SHC 100 IS LISTED IN THE MM FOR APPROVED GREASApr 10, 2009 · Beech 1900D · Wheel/Ski/FloatSDR GLBA20090410BIndicator · fluctuatesDURING FLIGHT NOTICED 2 PERCENT FLUCTUATION ON NR 1 N 1 GAUGE AND FLUCTUATIONS ON NR 1 TORQUE GAUGE CONTINUED UNTIL SHUTDOWN. MAINTENANCE R & R LT BETA BLOCK AND RIGGED BETA VALVE LOW PITCH STOP PER MM 76-10-00. MAINTENANCE ADDITIONALLY R & R TACH GENERATOR IApr 10, 2009 · N165YV · Beech 1900D · Engine BMEP/Torque IndicatingSDR CA090423009Wire · burned(CAN) TAIL NAVIGATION LIGHT WIRES CHAFED TOGETHER CAUSING BURN HOLE IN EMPENNAGE AFT FARING ASSY. FAIRING ND NAV WIRES REPAIRED IAW WIRING DIAGRAM MANUAL ATA 51-30-06 AND SRM ATA 51-30-06. REFEREANCE T/C T 1673 NP. WIRING SECURED WITH SPIRAL WRAP. SUSPECT CHAFApr 9, 2009 · Beech 1900D · Light System WiringSDR GLBA20090409ATransducer · malfunctionedAIR RETURN - PILOTS REPORTED A LIGHTNING STIKE ON THE NOSE WHICH RESULTED IN A RUNWAWAY RUDDER BOOST SITUATION IF THE RUDDER BOOST SWITCH WAS "ON". RUDDER BOOST ACTIVATES AND STAYED ACTIVATED. MAINTENANCE PLACED THE ISSUE ON MEL 22-2 CAT.C C/N 34624 AT THE TIMApr 9, 2009 · N245GL · Beech 1900D · Autopilot SystemSDR CA090504008Spar · corroded(CAN) CORROSION FOUND, CENTER WING, MAIN SPAR, FWD FLANGE APRROX LBL 16 TO RBL 16. DURING SCHEDULED STRUCTURAL INSP, FOUND CORROSION BUBBLING UP FROM UNDER PRC COATING THAT COVERS THE SPAR CAP CORNER RADIUS. REMOVAL OF THE PRC FOUND PITTED CORROSION ON THE SPApr 8, 2009 · Beech 1900D · Wing SparSDR GUUA95727040809AHorn · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR INBD TRIM TAB HORN EXFOLIATED. REPLACED RT ELEVATOR ASSY.Apr 8, 2009 · N87557 · Beech 1900D · Elevator StructureSDR GLBA20090409GSwitch · dirtyPILOTS REPORTED THAT THE RT ENGINE NR 2 PROPELLER VIOLENTLY CYCLES IN AND OUT OF FEATHER. PROPS WERE FULL FWD, IDLE SLOWLY INCREASING, CAUSED YAWING AT 1500 FT ON APPROACH. MX CLEANED POWER LEVER AUTOFEATHER MICROSWITCHES AND PERFORMED OPSL CHECK OF AUTOFEATHEApr 8, 2009 · N170GL · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20090408BVor System · inoperativePILOTS REPORTED THAT THE NR 2 NAV RADIO WAS INOPERATIVE AND RETURNED TO DEN. MAINTENANCE REMOVED AND REPLACED THE VOR-ILS RECEIVER IAW MM 34-20-00. OPERATIONAL CHECK WAS GOOD.Apr 8, 2009 · N218YV · Beech 1900D · Visual Omnirange (VOR) SystemSDR GLBA20090408FSwitch · out of adjustSIGNIFICANT EVENT-SUSPECTED AUTOFEATHER -PILOTS REPORTED THAT THE NR 2 ENGINE PROPELLER FEATHERED VIOLENTLY IN AIR WITH PROPELLERS FULL FWD AND REDUCING POWER. AUTO FEATHER SWITCH WAS IN THE ARMED POSITION 500 FT ABOVE THE GROUND. MX GROUND RUNS SHOWED THE LT Apr 7, 2009 · N245GL · Beech 1900D · Propeller Feathering/ReversingSDR GUUA94232040309AMaster Cylinder · malfunctionedPILOT REPORTS RT BRAKE PEDAL STILL GOES TO THE GROUND. HAVE TO CONSTANTLY PUMP TO BRAKE. REPLACED NR 4 BRAKE MASTER CYL, BLED BRAKE LINES. OPS CHECK NORMAL.Apr 7, 2009 · N47542 · Beech 1900D · Master Cylinder/Brake ValveSDR GUUA91255040609BSpar · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED VERTICAL STABILIZER RT SPAR HAS CORROSION BETWEEN CSS 11.500 TO 24.973, CSS 39.289 TO CSS 69.184 AND APPROX 3.5 INCHES ABOVE CSS 69.184. CLEANED CORROSION AND INSTALLED REPAIRS STRAPS IN CORRODED AREAS BETWEEN CSS 11.50 TApr 6, 2009 · N45AR · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GUUA91255040609ASpar · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED VERTICAL STABILIZER LT SPAR HAS CORROSION BETWEEN CSS 11.50 TO CSS 24.973,CSS 24.973 TO CSS 39.289 AND CSS 39.289 TO CSS 69.184. CLEANED CORROSION AND INSTALLED REPAIR STRAPS IN CORRODED AREAS BETWEEN CSS 11.50 TO CSS 69Apr 6, 2009 · N45AR · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA20090410FDoor Frame · crackedDURING SCHEDULED STRUCTURAL INSP MX DISCOVERED CRACKS AROUND THE CARGO DOOR UPPER FRAME AT FWD CORNER AREA AT FS 456 AND UPPER FRAME AFT CORNER AT FS 509. APPROXIMATE CRACK LENGTHS 5 INCHES AND 2.75 INCHES RESPECTIVELY. MX REPAIRED THE AFFECTED AREAS IAW EO-0Apr 6, 2009 · N247GL · Beech 1900D · Fuselage Main, StructureSDR GLBA20090409FCam · wornPILOTS REPORTED THAT THE ACFT YAWS VIOLENTLY TO THE LT ON FLAIR (LANDING). MX REMOVED AND REPLACED THE RT ENGINE PROPELLER CAM/LEVER IAW MM 76-10-00. GROUND RUNS WERE PERFORMED AND WERE WITHIN GIVEN PARAMETERS.Apr 6, 2009 · N208GL · Beech 1900D · Propeller Feathering/ReversingSDR GUUA94132040609AWire · chafedDURING FLIGHT, DISCOVERED LANDING GEAR CIRCUIT BREAKER POPPED. REPAIRED CHAFED WIRE D6D22 ON TOP LT NACELLE.Apr 6, 2009 · N17541 · Beech 1900D · Nacelle/Pylon System WiringSDR GLBA20090406FConnector · looseAIR RETURN - FLIGHT NR 5 - PILOTS REPORTED THAT THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. MX TROUBLESHOT THE ISSUE AND FOUND A LOOSE CONNECTOR PLUG AT THE GEAR HANDLE. MX RESECURED THE CONNECTOR PLUG AT THE GEAR HANDLE AND PERFORMED FIVE RETRACTION ANApr 5, 2009 · N251GL · Beech 1900D · Landing Gear System WiringSDR GLBA20090405BConnector · loosePILOTS REPORTED THAT EXPERIENCED A DROP IN THE RIGHT HAND PROPELLER RPM AND THAT IT HAD DROOPED TO 1620 RPM ON TAKEOFF. MAINTENANCE CLEANED THE CONNECTOR ON THE RIGHT HAND PROPELLER TACH GENERATOR AND RE-INSTALLED. REFERENCE BEECH 1900 MM 77-10-00.Apr 5, 2009 · N255GL · Beech 1900D · Propeller/Propulsor System WiringSDR GLBA20090405AWarning Horn · false activationPILOTS REPORTED THAT THE STALL WARNING CAME ON AT WEIGHT OFF WHEELS AND STAYED ON. RETURNED TO DEN. MAINTENANCE TESTED THE STALL WARNING SYSTEM ON GROUND. JACKED AIRCRAFT AND OPERATED STALL WARNING STALL LIFT TRANSDUCER MANUALLY AND FOUND THAT STALL HORN SILApr 5, 2009 · N170GL · Beech 1900D · Stall Warning SystemSDR GLBA20090406GSkin · crackedMAJOR REPAIR - SKIN CRACKS ON TOP OF FUSELAGE AT F.S. 150.6 AT STRINGER 1 WERE FOUND DURING SCHEDULED STRUCTURAL CHECK. RIVET HEAD WAS SHEARED WITH CRACKS STARTING AT SAID RIVET AND ANOTHER CRACK AT A RIVET SAME LOCATION OTHER SIDE OF STRINGER 1. MAINTENANCE RApr 4, 2009 · N247GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA94052040409ADoor · stiffDURING SCHEDULED ROUTINE MX, DISCOVERED RT AFT EMERGENCY EXIT DIFFICULT TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT INTERIOR AND EXTERIOR HANDLE.Apr 4, 2009 · N16540 · Beech 1900D · Emergency ExitsSDR GLBA20090403ASwitch · dirtyTHE PILOTS REPORTED TAHT AFTER T.O. DURING GEAR RETRACTION, THE GEAR WARNING HORN SOUNDED AND THE GEAR UNSAFE LIGHT DID NOT EXTINGUISH. MAINTENANCE INSPECTED & CLEANED STUCK GEAR WARNING HORN SWITCHES AT POWER LEVERS AND PERFORMED A MAIN LANDING GEAR EXTENSIONApr 3, 2009 · N192GL · Beech 1900D · Landing Gear Position and WarningSDR GUUA94232040209ABrake · malfunctionedPILOT REPORTS RT BRAKE GOES TO THE GROUND. BLED BRAKES. LEAK CHECK AND OPS CHECK NORMAL.Apr 2, 2009 · N47542 · Beech 1900D · Landing Gear Brake System
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