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 AMWA82340BCBattery · dischargedBATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR DISCREPANCY. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS.Jan 30, 2007 · N166YV · Beech 1900D · Battery/Charger SystemSDR AMWA82342BCBattery · dischargedBATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR DISCREPANCY. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS.Jan 30, 2007 · N159YV · Beech 1900D · Battery/Charger SystemSDR NSVA20070021Shuttle Valve · faultedFOUND LANDING GEAR WOULD NOT COME UP DURING TAKEOFF. TROUBLESHOT GEAR IAW BE AMM 32-30-00-101 CHART 101, FOUND HYDRAULIC FLUID LOW AND RISUAL VERY CLOUDY DRAINED HYDRAULIC FLUID AND INSPECTED FILTER FOUND NO DEFECTS WITH FILTER. RESERVICED POWER PACK IAW BE Jan 29, 2007 · N155CJ · Beech 1900D · Hydraulic System, MainSDR AMW1070126025Bolt · bentWHILE PERFORMING THE INSPECTION REQUIREMENTS OF THE RUDDER SYSTEM FOR THE NR 6 DETAIL INSPECTION, IT WAS DISCOVERED THAT THE RUDDER HAD EXCESSIVE UP AND DOWN MOVEMENT. THE FIRST ACTION IS TO CHECK THE TORQUE OF THE RUDDER CONTROL HORN PIVOT BOLT (ITEM NR 312, Jan 29, 2007 · N135YV · Beech 1900D · Rudder Control SystemSDR BSAASDR0702Windshield · crackedNR 1 WINDSHIELD CRACKED AT FL 170, JUST PRIOR TO THE START OF DESCENT. CREW DECLARED INFLIGHT EMERGENCY, REVIEWED AND FOLLOWED ABNORMAL CHECKLIST PROCEDURES, AND LANDED WITHOUT FURTHER INCIDENT. WINDSHIELD WAS REPLACED. CAPTAIN STATED WINDSHIELD HEAT WAS TUJan 27, 2007 · N132YV · Beech 1900D · Flight Compartment WindowsSDR GUUA01250701Connector · loose(9262) FPO/PBI DURING FLIGHT RT FIRE DISCHARGE ANNUNCIATOR ILLUMINATED. SECURED RT FIRE BOTTLE WIRE CONNECTION OPERATIONAL CHECK NORMAL.Jan 25, 2007 · N46AR · Beech 1900D · Fire Protection System WiringSDR CA070123010Seal · leaking(CAN) CREW LANDED AND REPORTED ENGINE NR 2 LEAKING OIL. MAINTENANCE INSPECTED AND FOUND THE OIL LEVEL DOWN CONSIDERABLY, THEY INSPECTED THE FWD CHIP DETECTOR, OIL FILTER, FUEL OIL HEATER AND FOUND NO DEFECTS. THE ENGINE WAS GROUND RUN WITH A LITTLE OIL LEAKAGEJan 23, 2007 · Beech 1900D · Turbine Engine Oil SystemSDR AMWA82203BCBattery · dischargedBATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE CHARGED THE BATTERY AS NEEDED TO CLEAR DISCREPANCY. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS.Jan 23, 2007 · N162ZV · Beech 1900D · Battery/Charger SystemSDR NSVA20070016Line · leakingFOUND SMOKE IN CABIN DURING FLIGHT. SMOKE DISSIPATED BEFORE LANDING. MAINTENANCE FOUND LEAKING OIL COOLER HOSE ON THE LT ENGINE, A SMALL AMOUNT OF OIL MIGRATED INTO THE ENVIRONMENTAL SYSTEM THAT CAUSED THE CABIN SMOKE. THE OIL LINES WERE REPLACED AND IT TOOJan 22, 2007 · N171CJ · Beech 1900D · Engine Oil Distribution (Airframe Furnished)SDR AMWA82619BCBattery · dischargedBATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR DISCREPANCY. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS.Jan 22, 2007 · N176YV · Beech 1900D · Battery/Charger SystemSDR CA070314002Engine · making metal(CAN) ON CLIMB FOLLOWING TAKE-OFF, FLAMES WERE SEEN EXITING THE ENGINE EXHAUST ACCOMPANIED BY A LOUD NOISE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE ENGINE OIL AND ROTOR SEIZURE. MFG WILL INVESTIGATE THE EVENT ANJan 17, 2007 · Beech 1900D · Engine (Turbine/Turboprop)SDR AMWA82088Engine · draggingFLIGHT 450, AFTER TAKEOFF, CAPTAIN NOTICED LOUD (BANG) AND FLAMES COMING FROM LT ENGINE. PRIOR TO NOISE, ALL INDICATIONS REPORTED AS NORMAL. NO T-HANDLE (FIRE PULL) LIGHTS ILLUMINATED. CREW SHUT DOWN LT ENGINE, DISCHARGED LT FIRE BOTTLE, FIRE EXTINGUISHED AND Jan 17, 2007 · N142YV · Beech 1900D · Engine (Turbine/Turboprop)SDR R021692Bearing · brokenON 12/14/06 REPORTED AIRCRAFT VIBRATIONS FROM STBD ENGINE. INSPECTION OF PROPELLER ON GROUND REVEALED EXCESSIVE RADIAL PLAY OUT OF LIMIT OF NR 3 BLADE. PROPELLER REMOVED FROM AIRCRAFT FOR FURTHER INVESTIGATION. SERVICE CENTER NOTES: BLADE NR 3 CAM FOLLOWER BRJan 17, 2007 · Beech 1900D · Propeller Blade SectionSDR GUUA01160702Skin · crackedAT SCHEDULED INSPECTION DISCOVERED 2 CRACKS AT NR 2 COMM ANTENNA (FS400) 1 CRACK 5.5 INCHES RUNNING LONGITUDINALLY FORWARD FROM FS 403 THE OTHER CRACK 1.5 INCHES LONG RUNNING LONGITUDINALLY FORWARD FROM FS 397. STOP DRILLED CRACKS AND INSTALLED EXTERNAL REINFJan 16, 2007 · N17541 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA01160701Wire · looseFLIGHT: 9176, DURING FLIGHT RT ENGINE FIRE DISCHARGE LIGHT ILLUMINATED. CONTINUED, LANDED WITHOUT INCIDENT. SECURED LOOSE WIRE CONNECTION AT THE RT FIRE BOTTLE.Jan 16, 2007 · N69547 · Beech 1900D · Fire Protection System WiringSDR GUUA01150701Wire · looseFLIGHT: 9175, DURING FLIGHT RT ENGINE FIRE DISCHARGE LIGHT ILLUMINATED. CONTINUED, LANDED WITHOUT INCIDENT. SECURED LOOSE WIRE AT RT ENGINE FIRE BOTTLE.Jan 15, 2007 · N69547 · Beech 1900D · Fire Protection System WiringSDR NSVA20070009Transducer · malfunctionedRT OIL PRESS FLUCTUATION INFLIGHT 115-160 PSI>1800 LBS TQ. REMOVED AND REPLACED RT OIL PRESS TRANSDUCER IAW BMM 79-30-00 P/N 101-389023-5 S/N ON 5405-A-37, S/N OFF 40910. OPS CK GOOD.Jan 14, 2007 · N243CJ · Beech 1900D · Engine Oil PressureSDR GUUA01140703Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED LT OB ELEVATOR HINGE BRACKET.Jan 14, 2007 · N17541 · Beech 1900D · Horizontal Stabilizer StructureSDR GUUA01140702Wire · looseFLIGHT: 9147, DURING FLIGHT RT ENGINE FIRE DISCHARGE LIGHT ILLUMINATED. CONTINUED, LANDED WITHOUT INCIDENT. RESECURED LOOSE WIRE AT RT FIRE BOTTLE.Jan 14, 2007 · N69547 · Beech 1900D · Fire Protection System WiringSDR NSVA20070008Indicator · malfunctionedCOMPARATOR FLAG ILLUMINATED ON TAKEOFF, HEADING FLAG ON CAPTAIN EHSI. PERFORMED OPS CK OF SYSTEM DID NOT FIND ANY FAULTS, OPS CK GOOD REF 34-20-00.Jan 13, 2007 · N243CJ · Beech 1900D · Attitude and Direction Data SystemSDR GLBA20060884Skin · crackedLT FUSELAGE LOWER SKIN, FORWARD SPAR FLANGE HAS (2) PULLED RIVETS WITH 1.2500 INCH CRACK AT F.S. 289.0 AND W.S. 29.06. REPAIRED CRACK AND RIVETS IAW SRM 53-90-18.Jan 12, 2007 · N122UX · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20060885Skin · crackedRT FUSELAGE LOWER SKIN, FORWARD SPAR FLANGE HAS (2) PULLED RIVETS WITH 1.2500 INCH CRACK AT F.S. 289.0 AND W.S. 29.06. REPAIRED CRACK AND RIVETS IAW SRM 53-90-18.Jan 12, 2007 · N122UX · Beech 1900D · Fuselage Main, Plate/SkinSDR AMW107001001Skin Panel · crackedDURING THE INSPECTION PHASE OF A NR 4 DETAILED INSPECTION, A 2.5 INCH SPANWISE CRACK WAS FOUND ON THE UNDERSIDE OF THE RT WING AT WING STATION B.L. 29.06. NO SB OR AD'S APPLY TO THIS AREA OF THE AIRCRAFT. UPON FURTHER INSPECTION OF THIS AIRCRAFT, A REPAIR WASJan 11, 2007 · N127ZV · Beech 1900D · Wing, Plate/SkinSDR AMW1061010024Spar Cap · corrodedDURING STRUCTURAL INSPECTION, MAINTENANCE FOUND SOME BIO-CORROSION ON LT WING MAIN SPAR LOWER CAP BETWEEN WS 114 AND WS 124. REPAIRED IAW MFG FR-CO-01443 REV. 4 SPAR CAP PLUG INSTALLATION ACCOMPLISHED IAW MFG FR-CO-01444 REV 2 IN CONJUNCTION WITH MFG FR-CO-0Jan 10, 2007 · N127ZV · Beech 1900D · Wing SparSDR AMWA81913Actuator · failedON APPROACH, THE CREW PLACED THE GEAR HANDLE DOWN. THE LT MAIN LANDING GEAR INDICATOR FAILED TO ILLUMINATE. THE CREW PERFORMED THE INDICATOR LIGHT TEST AND FOUND THE ANNUNCIATOR TO BE OPERATIVE. THE CREW THEN DECLARED AN EMERGENCY AND CONFIRMED THE GEAR DOWN Jan 8, 2007 · N174YV · Beech 1900D · Landing Gear ActuatorSDR AMW1070010901Skin Panel · crackedDISCOVERED DURING MAINTENANCE INSPECTION FOR PRESSURIZATION PROBLEM. MAINTENANCE FOUND THE FUSELAGE SKIN TO BE CRACKED ALONG THE RT SIDE OF THE NR 1 COMM ANTENNA. THE CRACK WAS 7 IN LONG, EXTENDING FROM APPROX FS 213.00 TO FS 220.750 RUNNING PARALLEL TO THE AJan 8, 2007 · N163YV · Beech 1900D · Fuselage Main, Plate/SkinSDR AMWA81896Bulb · inoperativeWHEN GEAR WS EXTENDED FOR LANDING, THERE WAS NO DOWN AND LOCKED INDICATION ON ANNUNCIATOR. CREW DECLAIRED EMERGENCY, AND FOLLOWED PROCEDURES. A/C LANDED WITH NO FURTHER INCIDENT. REPLACED ANNUNCIATOR BULBS. PENDING ADL RETURN.Jan 7, 2007 · N126YV · Beech 1900D · Landing Gear Position and WarningSDR AM1070103027Support Beam · damagedPROBLEM DISCOVERED DURING MAINTENANCE INSPECTION. RUDDER BELLCRANK SUPPORT BEAM REPAIRED IAW AERODESIGN AIRCRAFT ENGINEERING, INC REPORT NR 6496-1 REV. 1 SHEET 1 THROUGH 33. DATED 01/04/2007.Jan 6, 2007 · N146ZV · Beech 1900D · Rudder StructureSDR AMWA81813Landing Gear · malfunctionedWHEN GEAR WAS EXTENDED FOR LANDING, THE RT MAIN GEAR DID NOT SHOW DOWN AND LOCKED. THE CREW DECLAIRED AN EMERGENCY AND FOLLOWED EMERGENCY PROCEDURES, BY PUMPING THE GEAR DOWN. THE AIRCRAFT THEN LANDED SAFELY WITH NO FURTHER INCIDENT.Jan 3, 2007 · N155ZV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR BSAASDR0701Downlock Switch · failedWHEN CREW EXTENDED GEAR FOR LANDING THE RIGHT GEAR INDICATOR DIDN'T COME ON. THE BULBS WERE CHECKED WITH THE PRESS TO TEST AND FOUND TO BE GOOD. CREW REQUESTED A MISSED APPROACH TO RUN GEAR LIGHT CHECKLIST PROCEDURES. BOTH MAIN GEAR WERE VISUALLY VERIFIED TJan 3, 2007 · N140ZV · Beech 1900D · Landing Gear Position and WarningSDR NSVA20070002Indicator · unknownFO'S AIR SPEED READS 0 DURING TAKEOFF ROLL. REPLACED FO'S AIRSPEED INDICATOR REF MM 31-10-00 PERFORMED PITOT/STATIC TEST REF W/C 34-11-01. OPS CHECK GOOD, PN: 130-380005-7, SN ON: W21642 (CANNED FROM N220 NR 2) SN OFF: W21861.Dec 30, 2006 · N171CJ · Beech 1900D · Airspeed/Mach IndicatorSDR GUUA12290601Circuit Breaker · failedFLIGHT: 9167, AFTER TAKEOFF LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED. CONTINUED, LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR INDICATION CIRCUIT BREAKER,OPERATIONAL CHECK NORMAL.Dec 29, 2006 · N69547 · Beech 1900D · Landing Gear Position and WarningSDR NSVA200600241Link · looseL AND R FLAP SAFETY (SWITCH LINKS LOOSE) MOTOR INOP. REMOVED AND REPLACED L AND R SAFETY LINKS IAW BMM 27-50-00 RAN FLAPS, OPS CK GOOD P/N 101-521030-5. REMOVED AND REPLACED FLAP MOTOR IAW B1900 MM CH 27-5003-211, OPS CHECK IAW B 1900, PN ON/OFF 100-524073-1Dec 28, 2006 · N136MJ · Beech 1900D · Trailing Edge FlapsSDR NSVA200600240Handle · looseGEAR TRANSIT LIGHTS ILLUMINATE DURING GEAR TRANSITION. DURING T/S, FOUND SCREW SECURING GEAR HANDLE LIGHT TO HANDLE LOOSE CAUSING INTERMITTENT FAILURE OF LIGHT. TIGHTENED SCREWS, OPS CHECK NORMAL NOW IAW BMM 32-30-00.Dec 28, 2006 · N152MJ · Beech 1900D · Landing Gear SelectorSDR BSAASDR0627Switch Actuator · out of adjustDURING CLIMBOUT APPROXIMATELY 30 MINUTES INTO THE FLIGHT, THE CABIN DOOR WARNING LIGHT CAME ON. CREW FOLLOWED CHECKLIST PROCEDURES & RETURNED TO STATION. DISCREPANCY WAS INITIALLY DEFERRED IAW MEL 52-1 AFTER IT WAS DETERMINED THAT THE INDICATION SYSTEM WAS IDec 28, 2006 · N131YV · Beech 1900D · Door Warning SystemSDR CA061227002Transmitter · malfunctioned(CAN) ENROUTE FROM RT OIL PRESSURE INDICATED 50 PSI. THERE WAS NO CORRESPONDING R LOW ANNUNCIATOR, DECLARED AN EMERGENCY AND PERFORMED A PRECAUTIONARY SHUTDOWN OF THE RT ENGINE. RETURNED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT INDICATION TO A FAULTY OIL PREDec 26, 2006 · Beech 1900D · Engine Oil PressureSDR AMWA81587Latch · malfunctionedON PREFLIGHT, CREW COULD NOT GET CABIN DOOR TO LATCH. MECHANIC SECURED THE DOOR AND THE AIRCRAFT WAS FERRIED. MORE TO BE ADDED WHEN ADL IS RECEIVED.Dec 24, 2006 · N146ZV · Beech 1900D · Passenger/Crew DoorsSDR NSVA200600237Switch · out of adjustFOUND CABIN DOOR ANNUNCIATOR CAME ON IN FLIGHT. PERFORMED ADJUSTMENT OF AS DOOR TOP DOOR SILL SWITCH IAW MM 57-70-00. PRESSURIZED AIRCRAFT IAW MM 21-30-00, AS DOOR ANNUNCIATOR SYSTEM. OPS CHECK GOOD AT THIS TIME.Dec 22, 2006 · N60MJ · Beech 1900D · Door Warning SystemSDR AM1061111008BSeat Track · damagedSEAT TRACK REPAIR AT STATION LOCATION 190, 257, 369, 220, 264. REPAIRED IAW EA REPAIR 1900D 133-1 REV 1.Dec 19, 2006 · N133YV · Beech 1900D · Fuselage, Seat/Cargo Attach FittingsSDR AM1061111008ASpar · corrodedREPAIRED CORRSION ON LT WING MAIN SPAR FWD FLANGE AT WS. 126 AND AFT FLANGE AT WS. 117 IAW FR-CO-01467 REV.1Dec 19, 2006 · N133YV · Beech 1900D · Wing, Rib/BulkheadSDR GUUA12170601Warning System · malfunctionedFLIGHT: 9232, DURING FLIGHT, F/O FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED AND FLICKERED. CLEANED AND INSPECTED THE F/O FIRE EXTINGUISHER ANNUNCIATOR , COULD NOT DUPLICATE.Dec 17, 2006 · N69547 · Beech 1900D · Central WarningSDR GUUA12150601Unknown · smokeFLIGHT:9279 PBI/NAS AFTER TAKEOFF ODOR OF SMOKE IN THE COCKPIT AND CABIN. RETURNED TO PBI LANDED WITHOUT INCIDENT. RAN AIRCRAFT WITH ALL EQUIPMENT ON NO SIGN OF SMOKE ODOR NOTED. TEST FLIGHT SATISFACTORY.Dec 15, 2006 · N178YV · Beech 1900D · Air Distribution SystemSDR GUUA12150603Skin · ground damageFLIGHT: 9214, DURING GROUND HANDLING BAGGAGE CART DAMAGE BELOW CARGO DOOR LOCATED AT F.S 482.75 TO F.S 500. CUT OUT DAMAGE SECTION OF SKIN 17.0 IN X 7.0 IN FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER 20.0 IN X 10.0 IN IAW STRUCTURAL REPAIR MANUAL 51-70-Dec 15, 2006 · N49543 · Beech 1900D · Fuselage Main, StructureSDR BSAASDR0626Switch · out of adjustDURING CLIMBOUT THROUGH 10,000 FT THE CABIN DOOR WARNING LIGHT CAME ON. CREW FOLLOWED EMERGENCY CHECKLIST PROCEDURES & RETURNED TO THE STATION. THE MICROSWITCH ON LATCH CAM INSIDE THE DOOR WAS FOUND SLIGHTLY OUT OF ADJUSTMENT DUE TO WEAR & WAS ADJUSTED. THEDec 15, 2006 · N3199Q · Beech 1900D · Door Warning SystemSDR GUUA12150602Connector · contaminatedFLIGHT: 9171, DURING FLIGHT FIRST OFFICERS FIRE DISCHARGE LIGHT ILLUMINATED. CONTINUED TO MIA LANDED WITHOUT INCIDENT. FOUND WET CONNECTOR AT RT ENGINE FIRE BOTTLE, DRIED AREA OPERATIONAL CHECK GOOD.Dec 15, 2006 · N69547 · Beech 1900D · Fire Protection System WiringSDR AMW1061218001Sensor · failedDURING A LANDING GEAR RETRACT CHECK, IT WAS NOTICED THAT SPARKS AND SMOKE WAS EMITTING FROM THE LIQUID LOW LEVEL SENSOR INSTALLED ON THE LANDING GEAR POWER PACK. THE SENSOR WAS REPLACED AND NO FURTHER PROBLEMS WERE NOTICED.Dec 12, 2006 · N176YV · Beech 1900D · Landing Gear Position and WarningSDR NSVA200600230Switch · lack of lubeFOUND FLAPS FAILED TO RETURN TO UP POSITION. CLEANED AND LUBED FLAP ASYMMETRIC SWITCHES (LEFT AND RIGHT SIDE) FLAP SYSTEM. OPS CHECKED GOOD IAW AFA 27-50-05.Dec 11, 2006 · N243CJ · Beech 1900D · Trailing Edge Flap Control SystemSDR GUUA12110601Wire · unsecureFLIGHT:9193 NAS/FLL - DURING LANDING, THE NR 1 FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED THREE TIMES. SECURED WIRE ON THE NR 1 FIRE EXTINGUISHER BOTTLE.Dec 11, 2006 · N53545 · Beech 1900D · Fire Protection System WiringSDR BSAASDR0625Switch · out of adjustDURING CRUISE AT FL180 THE CARGO DOOR WARNING LIGHT CAME ON. CREW FOLLOWED CHECKLIST PROCEDURES, DETERMINED IT WAS AN INDICATION PROBLEM AS THE AIRCRAFT WAS STILL PRESSURIZED WITH NO LOSS, THEN DECLARED AN EMERGENCY AND REQUESTED LOWER ALTITUDE, BUT DID NOT PDec 11, 2006 · N132YV · Beech 1900D · Door Warning SystemSDR GUUA12100601Switch · out of adjustFLIGHT:9227 DURING FLIGHT LANDING GEAR WARNING HORN SOUNDS BETWEEN 90-91 PERCENT, N1 WITH 2300-2500 POUNDS OF TORQUE. ADJUSTED LANDING GEAR WARNING HORN PEDESTAL SWITCHES. TEST FLIGHT SATISFACTORY.Dec 10, 2006 · N81533 · Beech 1900D · Landing Gear Position and Warning
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