Beech 1900C

Service difficulty reports · 1,840

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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 = '1900C'
  ORDER BY difficulty_date DESC"

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SDR CA141204013Line · chafed(CAN) A FUEL LEAK WAS SNAGGED BY THE RIGHT WHEEL WELL ON C-GSKW. THE AME INVESTIGATED AND FOUND THE RIGID FUEL LINE WHICH RUNS THROUGH THE LANDING GEAR WHEEL WELL TO BE CHAFFED THROUGH. CHAFFING WAS CAUSED BY THE BULKHEAD THAT IT RUNS THROUGH.Dec 4, 2014 · Beech 1900C · Aircraft Fuel Distribution SystemSDR YADA20141129001Light · intermittentNOSE GEAR GREEN LIGHTS INTERMITTENT ON LANDING, NO OTHER WARNING INDICATION. DECLARED AN EMER FOR PRECAUTION. ACFT LANDED WITHOUT INCIDENT. CAUSE OF INTERMITTENT GREEN LIGHT NOT YET DETERMINED.Nov 29, 2014 · N111AX · Beech 1900C · Landing Gear Position and WarningSDR CA141127002Bearing · mismanufactured(CAN) QTY 2 3D CAM FOLLOWER BEARINGS FOUND IN FCU DO NOT CONFORM TO MANUFACTURERS DRAWING FOR P/N 8061-328B. BEARING P/N 1412-642 SHOULD BE UNSHIELDED PER OEM AND THE TWO BEARINGS REMOVED WERE FOUND TO BE SHIELDED BEARINGS.Nov 26, 2014 · Beech 1900C · Fuel Control/Turbine EnginesSDR CA141215005Wire · chafed(CAN) PROP DE-ICE LEADS ON THE RIGHT HAND AND LEFT HAND PROPS WERE FOUND STICKING OUT OF THE SPINNER WHERE THE PROP BLADE IS LOCATED. ONE OF THE LEADS ON THE LEFT HAND PROP HAD CHAFFED THROUGH TO THE BARE WIRE AND WAS SHORTING OUT ON THE SPINNER.Oct 30, 2014 · Beech 1900C · Ice/Rain Protection System WiringSDR ERAA201410240065Bushing · crackedRIGHT ENGINE TRUSS TO NACELLE STRUCTURE MOUNT BUSHINGS CRACKED. REPAIRED IAW RDO-CO102750-1.Oct 24, 2014 · N575A · Beech 1900C · Engine Mount SectionSDR CA141021014Sealant · failed(CAN) SHORTLY AFTER TAKE OFF WHEN FLIGHT CREW TURNED ON BOTH BLEED AIR SYSTEMS THROUGH 400 FT, SMOKE & ENVIRO ODOR WAS NOTICED IN THE CABIN. FLIGHT CREW TURNED OFF BLEEDS AT 1000 FT AND RETURNED TO AIRPORT. MAINTENANCE WAS ABLE TO DETERMINE SMELL CAUSED BY RH Oct 17, 2014 · Beech 1900C · Air Distribution SystemSDR CA141009008Uplock Switch · broken(CAN) THE RT GEAR WOULD NOT RETRACT. WHEN INSPECTED, THE R/G GEAR UPLOCK SWITCH WAS FOUND BROKEN AND PREVENTING FULL RETRACTION OF THE RT MLG.Oct 9, 2014 · Beech 1900C · Landing Gear Position and WarningSDR JIKA2014100401Skin · damagedTHE PILOT REPORTED THAT ON DESCENT APPROX 35 MILES SOUTH OF THE AIRPORT AT 6000 FT & 179 KTS, A QUICK FLASH OF BIRDS APPEARED IN FRONT OF THE ACFT FOLLOWED BY A BUMP HEARD ON THE RT SIDE OF THE ACFT. THERE WAS NO VISIBLE DAMAGE WHILE IN FLIGHT. UPON LANDING Oct 4, 2014 · N1568G · Beech 1900C · Wing, Plate/SkinSDR JIKA2014092101Circuit Breaker · poppedDURING APPROACH TO PILOT SELECTED LG TO THE EXTEND POSITION. LANDING POSITION INDICATORS DID NOT ILLUMINATE. PILOT PERFORMED TEST OF LG WARNING HORN SYS, HORN PERFORMED NORMAL. PILOT RECEIVED VERIFICATION FROM TOWER THAT THE LG APPEARED DOWN. AN EMER WAS DSep 21, 2014 · N575G · Beech 1900C · Landing Gear Position and WarningSDR JIKA2014091801Skin · damagedDURING CRUISE FLIGHT PILOT ENCOUNTERED HEAVY RAIN & HAIL. PILOT DIVERTED AROUND WEATHER & WITHOUT FURTHER INCIDENT. GND INSPECTION REVEALED SEVERE HAIL DAMAGE ON LT & RT HORIZONTAL, VERTICAL & LT & RT WING LE. MX IS IN THE PROCESS OF CONTACTING A STRUCTURE Sep 21, 2014 · N718AF · Beech 1900C · Horizontal Stabilizer, Plate/SkinSDR CA140920002Indicator · inaccurate(CAN) LEFT FUEL QTY INDICATOR WOULD NOT INDICATE CONSISTANT FUEL LEVEL AT MID RANGE OF INDICATOR GAUGE WOULD DROP OFF TO ZERO.Sep 19, 2014 · Beech 1900C · Fuel Quantity IndicatorSDR JIKA2014090901Windshield · crackedDURING CRUISE FLIGHT AT 20,000 FEET PILOT & FIRST OFFICER HEARD A LOUD BANG. FIRST OFFICER NOTICED THE RT WINDSHIELD HAD SHATTERED. PILOT DECLARED AN EMER & RECEIVED VECTORS TO DIVERT, PILOT LANDED WITHOUT FURTHER INCIDENT. R & R RT WINDSHIELD IAW MM. TIMESep 9, 2014 · N346AF · Beech 1900C · Flight Compartment WindowsSDR YADA20140819001Vsi · failedWHILE TAXIING TO REPOSITION ACFT, FLIGHT CREW REPORTED SMELLING & SEEING SMOKE FROM THE INSTRUMENT PANEL. THE ACFT RETURNED TO THE RAMP WITHOUT INCIDENT. PERFORMED A GND RUN ON THE ACFT & OBSERVED THE COPILOTS ELECTRONIC VSI INDICATOR SCREEN FLICKER & THEN WAug 19, 2014 · N115AX · Beech 1900C · Rate of Climb IndicatorSDR TIMA20140811022Support · corrodedDURING MX INSPECTION THE RT SIDE SEAT SUPPORT RAIL WAS FOUND TO BE CORRODED.Aug 11, 2014 · N197GA · Beech 1900C · Fuselage, Seat/Cargo Attach FittingsSDR TIMA20140811021Support · corrodedDURING MX INSPECTION THE LT SIDE SEAT SUPPORT RAIL WAS FOUND TO BE CORRODED.Aug 11, 2014 · N197GA · Beech 1900C · Fuselage, Seat/Cargo Attach FittingsSDR JIKA2014073101Line · leakingON LANDING THE PILOT REPORTED THERE WAS NO PRESS ON THE RT BRAKE. TAXIED TO PARKING WITHOUT INCIDENT. INSPECTED THE RT BRAKE SYS & FOUND THE FLEXIBLE BRAKE LINE PN MS28741-4-0226 LEAKING AT THE FITTING. REPLACED BRAKE LINE, BLEED BRAKE SYS. RT BRAKE OPERATJul 31, 2014 · N31704 · Beech 1900C · Landing Gear Brake SystemSDR YADA20140721001Handle · missingPILOT REPORTED CARGO DOOR EXTERIOR HANDLE MISSING AFTER LANDING.Jul 21, 2014 · N111AX · Beech 1900C · Cargo/Baggage DoorsSDR TIMA20140715013Bellows · failedPILOT REDUCED POWER FROM CRUISE TO PERFORM A MANEUVER. WHEN POWER WAS RE-APPLIED THERE WAS NO RESPONSE FROM THE RT ENG. POWER LEVER WAS CYCLED BACK & FORTH SEVERAL TIMES WITH NO EFFECT. PILOT ELECTED TO SHUT DOWN THE ENG & RETURNED TO LAND WITHOUT FURTHER IJul 15, 2014 · N133BA · Beech 1900C · Fuel Control/Turbine EnginesSDR ERAA201406180042Downlock Switch · defectiveRIGHT MAIN GEAR FAILED TO INDICATE DOWN & LOCK. R & R LG ACTUATOR DUE TO DEFECTIVE DOWN LOCK SWITCH NOT ACTUATING.Jun 13, 2014 · N575A · Beech 1900C · Landing Gear Position and WarningSDR JIKA2014061301Unknown · smokeDURING DESCENT THROUGH 5000’ AGL PILOT NOTICED SMOKE COMING FROM UNDERNEATH THE RT SUB PANEL & COULD SMELL BURNING ODOR. TURNED OFF ALL NON-ESSENTIAL ELEC EQUIP & LANDED WITHOUT FURTHER INCIDENT. NO LONGER NOTICED THE ODOR ONCE THROTTLES WERE REDUCED TO IDLE.Jun 13, 2014 · N49UC · Beech 1900C · Air Distribution SystemSDR YADA20140611001Bearing · failedAFTER TAKEOFF PILOT REPORTED THAT HE SAW SMOKE & COULD SMELL FUMES IN COCKPIT. PILOT DECLARED EMERGENCY & RETURNED TO DEPARTURE AIRPORT ANC WITHOUT INCIDENT. MX IDENTIFIED THE SOURCE OF THE SMELL AS FAILED BEARINGS LOCATED THE FWD VENTILATION BLOWER, NO DAMAJun 11, 2014 · N119AX · Beech 1900C · Air Distribution FanSDR CA140603006Bearing · misinstalled(CAN) ACFT RETURNED TO BASE AFTER A LT DC GENERATOR FAILURE IN FLIGHT. THE STARTER GENERATOR WAS REPLACED AND THE ACFT CONTINUED ON ITS INTENDED ROUTE. ON RECEIPT OF THE TEAR-DOWN REPORT, IT WAS FOUND THAT THE LAST O/H COMPLETED HAD THE BEARINGS INSTALLED INJun 3, 2014 · Beech 1900C · Starter-GeneratorSDR YADA20140516002Angle · crackedCRACK IN VERTICAL STABILIZER FWD SPAR LT ANGLE AT ATTACH BRACKET FASTENER. SEE SB 55-4114 & AD 2013-24-03.May 16, 2014 · N113AX · Beech 1900C · Vertical Stabilizer Miscellaneous StructureSDR YADA20140516001Angle · crackedCRACKS IN VERTICAL STABILIZER FWD SPAR RT ANGLE AT BRACKET ATTACH FASTENERS.May 16, 2014 · N113AX · Beech 1900C · Vertical Stabilizer Miscellaneous StructureSDR YADA20140514001Spar · crackedFOUND CRACKS IN HORIZONTAL STABILIZER AFT CENTER SPAR WEB.May 14, 2014 · N113AX · Beech 1900C · Horizontal Stabilizer, Spar/RibSDR YADA2014051700327Spar · crackedFOUND CRACKS IN VERTICAL STAB AFT CENTER SPAR WEB.May 14, 2014 · N113AX · Beech 1900C · Horizontal Stabilizer, Spar/RibSDR EPUA20140508001Structure · crackedDURING A SCHEDULED INSPECTION TO COMPLY WITH AD 2013-24-03, A CRACK WAS IDENTIFIED ON PN 101-6400 11-4. THIS PART IS LOCATED ON THE HORIZONTAL ATTACH POINT OF THE VERTICAL STABILIZER. A REPAIR WAS DEVELOPED BY THE MANUFACTURER TO CORRECT THIS IAW DWG FR-CO-1May 8, 2014 · N1553C · Beech 1900C · Vertical Stabilizer Miscellaneous StructureSDR JIKA2014042801Connector · brokenON APPROACH TO BQN PILOT SELECTED LG DOWN, RECEIVED THE RED IN TRANSIT WARNING LIGHT FOR 10 SECONDS THEN THE LIGHT WENT OUT BUT LG DID NOT EXTEND & THREE GREEN DOWN & LOCK INDICATOR LIGHTS DID NOT ILLUMINATE. TRIED TO CYCLE THE LG, THE LG WOULD NOT EXTEND. PApr 28, 2014 · N31704 · Beech 1900C · Landing Gear System WiringSDR JIKA2014042501Cable · looseDURING APPROACH INTO BGI LG FAILED TO EXTEND WITH NO INDICATION, IN TRANSIT LIGHT, PILOT ATTEMPTED TO CYCLE LG WITH SAME RESULTS. THE PILOT MANUALLY EXTENDED LG, GEAR WAS EXTENDED WITH THREE GREEN DOWN & LOCK INDICATION LIGHTS ILLUMINATED. LANDED AT BGI WITHApr 25, 2014 · N31704 · Beech 1900C · Landing Gear System WiringSDR TIMA20140422019Skin · debondedLEFT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.Apr 22, 2014 · N198GA · Beech 1900C · Wing, Plate/SkinSDR JIKA2014041401Wire · damagedON APPROACH AT TLPC PILOT SELECTED LG DOWN, LG FAILED TO DEPLOY & THREE GREEN LIGHT LG POSITION INDICATORS FAIL TO ILLUMINATE. PILOT TRIED SEVERAL TIMES TO CYCLE GEAR WITH SAME RESULTS, AT THAT TIME PILOT DECIDED TO MANUALLY EXTEND THE LG. AFTER SUCCESSFULLYApr 14, 2014 · N31704 · Beech 1900C · Landing Gear System WiringSDR YADA2014041461319Fitting · crackedCRACK FOUND IN RT AILERON BALANCE WEIGHT CLIP WHILE PERFORMING BORESCOPE INSPECTION OF CLIP.Apr 11, 2014 · N119AX · Beech 1900C · AileronsSDR JIKA2014040701Unknown · odorPILOT REPORTED THAT THE SMELL OF SMOKE WAS PRESENT IN THE COCKPIT DURING FINAL APPROACH TO DFW. PILOT DID NOT DECLARE, OR TAKE ANY EMERGENCY ACTION. INSPECTED WIRING CONDUITS BEHIND INSTRUMENT PANEL, LT & RT CB PANELS & RT LOWER LATERAL PANEL INSIDE COCKPIT.Apr 3, 2014 · N49UC · Beech 1900C · Air Distribution SystemSDR TIMA20140402018Spar Cap · corrodedINSPECTION REVEALED CORROSION DEVELOPING ON THE LT UPPER MAIN SPAR CAP UNDER THE VORTEX GENERATORS.Apr 2, 2014 · N172GA · Beech 1900C · Wing SparSDR EPUA20140325001Adapter · looseRIGHT POWER LEVER HIT STOP WITHOUT DEVELOPING FULL POWER. RT STARTER GEN COOLING DUCT ADAPTER PN 101-910062-7, LOOSE FROM THE STARTER GEN & INTERFERING WITH THE FUEL CONTROL INPUT LINKAGE TRAVEL. RE SECURED THE COOLING ADAPTER CAP PROPERLY TO REMEDY THIS CONMar 24, 2014 · N575Z · Beech 1900C · Engine Cooling SystemSDR YADA20140319001Control Cable · brokenPILOT REPORTED FLAPS STUCK AT TAKEOFF POSITION. REPLACED FAILED FLAP DRIVE CABLE.Mar 15, 2014 · N117AX · Beech 1900C · Trailing Edge Flap Control SystemSDR TIMA20140312017Skin · crackedSEVERAL CRACKS DEVELOPED IN THE SKIN OTBD OF THE LT NACELLE & AFT OF THE MAIN SPAR ORIGINATING FROM VARIOUS RIVETS.Mar 12, 2014 · N172GA · Beech 1900C · Wing, Plate/SkinSDR TIMA20140312016Skin · debondedLEFT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.Mar 12, 2014 · N172GA · Beech 1900C · Wing, Plate/SkinSDR TIMA20140312015Skin · debondedRIGHT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.Mar 12, 2014 · N172GA · Beech 1900C · Wing, Plate/SkinSDR CA140326015Tube · unsecure(CAN) ON THE CLIMB, DURING THE WING INSPECTION CHECK, SMOKE WAS OBSERVED COMING OUT OF THE RT COWLING FROM AROUND THE EXHAUST STACKS AND PROPELLER RING. ENGINE INDICATIONS WERE NORMAL EXCEPT FOR HIGH FUEL FLOW. THE CREW PERFORMED THE CHECKLIST ITEMS FOR A PREMar 10, 2014 · Beech 1900C · Engine Fuel DistributionSDR YADA20140312001Downlock Switch · inoperativePIREP, RED GEAR HANDLE LIGHT ILLUMINATES WITH GEAR DOWN & HANDLE DOWN. REPLACED NOSE GEAR DOWN LOCK SWITCH AFTER UNEVENTFUL LANDING AT ORIGINATING AIRPORT.Mar 10, 2014 · N115AX · Beech 1900C · Landing Gear Position and WarningSDR ERAA20140005Light · inoperativeRIGHT MLG DOWN ANNUNCIATOR NOT ILLUMINATING. REPLACED GEAR LIGHT ASSEMBLY PN 351-33790-007 IAW DIAGRAM 32-61-01. OPERATIONS CHECKED GEAR SWING SAT IAW BE19000C MM 32-30-00.Mar 10, 2014 · N575Q · Beech 1900C · Landing Gear Position and WarningSDR CA140226007Compressor · seized(CAN) ENGINE WAS SENT FOR INVESTIGATION AFTER THE CUSTOMER REPORTED THAT DURING FLIGHT, THE OIL PRESSURE LIGHT TURNED ON AND THE ENGINE WAS IMMEDIATELY SHUTDOWN. POST CHECK OF THE ENGINE REVEALED THE COMPRESSOR WAS SEIZED, METAL IN THE OIL FILTER AND METAL ON Feb 26, 2014 · Beech 1900C · Turbine Engine Compressor SectionSDR JIKA2014021101Connector · dirtyON VISUAL APPROACH, PILOT SELECTED LG HANDLE DOWN, THERE WAS NO AUDIBLE REACTION TO MOVING THE HANDLE & THE GEAR HANDLE REMAINED RED WITH NO GREEN INDICATOR LIGHTS, VISUALLY VERIFIED GEAR WAS NOT EXTENDED, TRIED CYCLING GEAR SEVERAL TIMES WITH SAME RESULTS, DEFeb 11, 2014 · N31704 · Beech 1900C · Landing Gear System WiringSDR JIKA2014010401Door Seal · out of positionDURING CLIMB OUT FROM KTYS, THE FWD CABIN DOOR ANNUNCIATOR CAME ON PASSING 14,000 FT. SHORTLY AFTER AIRCRAFT BEGIN TO DE-PRESSURIZE WITHOUT PILOT INPUT. PILOT RAN THE ASSOCIATED EMERGENCY CHECKLIST & DECLARED AN EMERGENCY WITH ATC. PILOT DIVERTED BACK TO KTYJan 4, 2014 · N575G · Beech 1900C · Passenger/Crew DoorsSDR CA140106001Oil System · low pressure(CAN) THE PILOTS NOTICED DURING CLIMBOUT AT AROUND 14,000 FT THAT THE FLASHING LIGHT FOR THE OIL PRESSURE ON THE LT ENGINE WAS FLASHING. OIL PRESSURE WAS ZERO, THE PILOTS SHUTDOWN THE LT ENGINE AND RETURNED. THE LT ENGINE WAS SEIZED WHEN CHECKED BY CREWS ON TJan 3, 2014 · Beech 1900C · Engine Oil PressureSDR CA140109002Brushes · burned(CAN) SHORTLY AFTER DEPARTURE, THE CREW ADVISED THEY WERE RETURNING TO THE AIRPORT DUE TO AN ODOR INSIDE THE ACFT. LANDED SAFELY. NO OPS IMPACT. MAINTENANCE REPORTED THAT THE FWD CABIN AIR BLOWER MOTOR WAS THE SOURCE OF THE ODOR. THE BLOWER MOTOR WAS REPLACDec 30, 2013 · Beech 1900C · Air Distribution FanSDR CA131218004Engine · fluctuates(CAN) SHORTLY AFTER TAKEOFF THE PILOT OBSERVED TORQUE FLUCTUATIONS BEFORE THE ENGINE DROPPED TO IDLE AND THE PROPELLER FEATHERED. THE ACFT RETURNED TO THE POINT OF DEPARTURE WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. POST FLIGHT INSPECTION WAS ABLE TO REPDec 17, 2013 · Beech 1900C · Engine (Turbine/Turboprop)SDR JIKA2013121601Fuel Divider · defectiveDURING CLIMB OUT FROM SFO, RT ENG LOST POWER AT APPROXIMATELY 100 FT AGL. BOTH RT SIDE ANNUNCIATOR’S ENG OIL PRESS & LOW FUEL PRESS WERE ILLUMINATED. ENG TORQUE WAS FLUCTUATING BETWEEN 0 & 500 FT LB. PILOT PULLED THE RT ENG CONDITION LEVER TO CUTOUT & DECLADec 16, 2013 · N347AF · Beech 1900C · Fuel DividerSDR JIKA2013120302Connector · corrodedDURING APPROACH INTO EKO PILOT SELECTED LG HANDLE DOWN, LG POSITION INDICATOR GREEN LIGHT NR 3 DID NOT ILLUMINATE. AFTER PILOT BRIEFLY TRIED TO TROUBLESHOOT PROBLEM DECIDED TO MANUALLY EXTEND LG, ONCE GEAR WAS EXTENDED PILOT VERIFIED ALL 3 GREEN LIGHTS WERE IDec 3, 2013 · N31702 · Beech 1900C · Landing Gear System Wiring
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