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 AMWA78291Switch · out of rigCREW OBSERVED THE PAX DOOR ANNUNICATOR ILLUMINATE INTERMITTENTLY WITH PAX DOOR CLOSED. THE AIRCRAFT LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE WAS CALLED AND CLEANED AND RE-RIGGED THE MICRO SWITCHES ON THE DOOR. OPS CHECKED NORMAL.Jul 6, 2006 · N127ZV · Beech 1900D · Door Warning SystemSDR GUUA07060601Odor · detectedFLIGHT: 9196 GGT/FLL DURING FLT INTERMITTENT OIL ODOR VENTING THROUGH THE ENVIRONMENTAL SYSTEM WITH THE LT OR RT BLEED ON. RAN ENGINES WITH BLEEDS ON TOGETHER AND INDEPENDENTLY, NO DEFECTS NOTED. OPERATIONAL CHECK GOOD.Jul 6, 2006 · N87551 · Beech 1900D · Air Distribution SystemSDR GUUA07050601Turbine Blades · failedMCO/LEE DURING TAKEOFF ROLL RIGHT ENGINE FAILED, ABORTED TAKEOFF. REPLACED RIGHT ENGINE, OPERATIONAL CHECK NORMAL. SUSPECT 2ND STAGE PT BLADE FATIGUE CRACKING.Jul 5, 2006 · N81533 · Beech 1900D · Turbine SectionSDR NSVA200600096Fire Loop · inoperativeLT LOOP/DETECT SWITCH NOT INDICATING PROPERLY. REMOVED AND REPLACED AFT FIRE LOOP ON LT ENGINE, PERFORMED OPS CHECK SATISFACTORY MM 26-10-01.Jul 3, 2006 · N220CJ · Beech 1900D · Fire DetectionSDR GUUA07030601Brake · weakFLIGHT:9196 GGT/FLL DURING TAXI LEFT BRAKE SINKS LOW TO THE FLOOR WHEN DEPRESSED. BLED LEFT BRAKES, OPERATIONAL CHECK GOOD.Jul 3, 2006 · N53545 · Beech 1900D · Landing Gear Brake SystemSDR GLBA20060796Motor · shortedIRRITATING SMELL / SMOKE IN COCKPIT/CABIN AFTER FLAP EXTENSION. SHUT ENGINES DOWN ON TAXIWAY, INSPECTED AIRCRAFT AND FOUND FLAP MOTOR SHORTED. REPLACED FLAP MOTOR, OPS CHECK SATISFACTORY.Jul 3, 2006 · N240GL · Beech 1900D · Trailing Edge Flap Control SystemSDR BSAASDR0617Wire · chafedCREW SELECTED GEAR DOWN IN PREPARATION FOR LANDING. THE GEAR INDICATOR CB POPPED, CREW RESET THE CB, & REPLACED BURNED OUT NLG INDICATOR BULBS. THE GEAR WAS CYCLED UP AND DOWN, WITH NORMAL OPERATION. AN OPERATIONAL CHECK FLIGHT WAS PERFORMED AFTER MAINTENANJul 1, 2006 · N3199Q · Beech 1900D · Landing Gear System WiringSDR 78192Handle · detachedAFTER PAX WERE BOARDED AND STATION WENT TO CLOSE THE PAX DOOR THE HANDLE DETACHED. MAINTENANCE WAS CALLED, INSPECTED CABIN DOOR HANDLE, RESECURED DOOR HANDLE RETAINER RING. DOOR OPS CHECKED NORMAL. WORK DONE IAW BMM 52-10-00.Jun 30, 2006 · N167YV · Beech 1900D · Passenger/Crew DoorsSDR 1060530035ASeat Track · wornSEAT SUPPORT ASSY TRACK WORN. MAINTENANCE REPAIRED THE TRACK IAW RAYTHEON FR-CO-01365 REV 1.Jun 26, 2006 · N166YV · Beech 1900D · Fuselage, Seat/Cargo Attach FittingsSDR 1060530035BSeat Track · wornAFT LT SEAT TRACK WORN. MAINTENANCE REPAIRED THE SEAT TRACK IAW RAYTHEON FR-CO-01364 REV 1.Jun 26, 2006 · N166YV · Beech 1900D · Fuselage, Seat/Cargo Attach FittingsSDR 1060530036RSpar Cap · corrodedRT MAIN SPAR CAP BIO-CORROSION CLEANED AND TREATED AND REPAIRED IAW RAYTHEON FR-CO-01358 REV 1.Jun 26, 2006 · N166YV · Beech 1900D · Wing SparSDR 1060530036LSpar Cap · corrodedLT MAIN SPAR CAP BIO-CORROSION. CLEANED AND TREATED AND REPAIRED IAW WITH RAYTHEON FR-CO-01359 REV 1.Jun 26, 2006 · N166YV · Beech 1900D · Wing SparSDR GUUA06260601Strut · lowFLIGHT: 9214 MIA/TPA AFTER LANDING DISCOVERED NOSE WHEEL WELL DAMAGED DURING GEAR EXTENSION. SERVICED NOSE LANDING GEAR STRUT LANDING GEAR EXTENSION AND RETRACTION, OPERATIONAL CHECK NORMAL.Jun 26, 2006 · N81546 · Beech 1900D · Nose/Tail Landing Gear Strut/AxleSDR GUUA06250601Landing Gear · malfunctionedFLIGHT: 9166 NAS/FLL AFTER TAKEOFF UNABLE TO RETRACT MAIN LANDING GEARS. RECYCLED AND LANDING GEARS RETRACTED OK. INSPECTED LANDING GEAR, CHECKED FLUID LEVEL, COMPLIED WITH OPERATIONAL CHECK. NO DEFECTS NOTED.Jun 25, 2006 · N16540 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR BSAASDR0616Tube · blownDURING CLIMBOUT, AT 500FT AGL, LT ENVIRO FAIL LIGHT CAME ON, CREW DEACTIVATED LT BLEED SYSTEM, LIGHT STAYED ON. CREW RETURNED TO FIELD. MX FOUND & REPAIRED LEAK IN THE LT BLEED AIR EVA TUBING.Jun 24, 2006 · N171ZV · Beech 1900D · Engine Bleed Air SystemSDR NSVA200600089Latch · out of adjustCABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. ADJUSTED AIRSTAIR DOOR LATCH HANDLE SWITCH PER AMM 52-70-02. RAN AND PRESSURIZED AIRCRAFT TO MAX DIFF. CHECKED SECURITY AND CONDITION OF DOOR LATCHING MECHANISM, OPS CHECK GOOD.Jun 21, 2006 · N152MJ · Beech 1900D · Passenger/Crew DoorsSDR GLBA20060792Skin · corrodedCORROSION ON SKIN UNDER STRINGERS 14L, 15L , 15R AND 16 FS 1987.00 TO 288.00. REPAIR PENDING.Jun 21, 2006 · N245GL · Beech 1900D · Fuselage Main, Plate/SkinSDR NSVA200600083Fire Bottle · inoperativeLEFT T HANDLE ILLUMINATED WHILE TAXING TO THE GATE AFTER LANDING ACTIVATED LEFT FIRE BOTTLE BUT IT FAILED TO DISCHARGE WITH T HANDLE PULLED. REMOVED AND REPLACED LT FIRE BOTTLE IAW SAAB WORK CARD 26-20-05 P/N ON AND OFF 30100023 S/N ON 28764A1 S/N OFF 25307A1Jun 19, 2006 · Beech 1900D · Fire Bottle, FixedSDR 1060607019Web · wornHOLE WORN ON WEB OF LT FIREWALL. LOOSE FASTENER FOUND TO HAVE CAME LOOSE AND WORE OUT THE HOLE. EXTRA CARE HAS BEEN TAKEN TO ENSURE THE FASTENER TO BE CHECKED FOR PROPER TORQUE. HOLE REPAIRED IAW MFG FR-CO-01357 REV 1.Jun 13, 2006 · N176YV · Beech 1900D · Nacelle/Pylon, Bulkhead/FirewallSDR GUUA06110601Actuator · malfunctionedFLIGHT:9280 EYW/TPA AFTER TAKEOFF WHEN LANDING GEAR SELECTED UP THREE GREEN ANNUNCIATOR ILLUMINATED, MOTOR RUNS INTERMITTENT, BREAKER POPS. CONTINUED TO TPA LANDED WITHOUT INCIDENT. MAINTENANCE FERRY TO FLL. REPLACED LEFT MAIN LANDING GEAR ACTUATOR. TEST FJun 11, 2006 · N218YV · Beech 1900D · Landing Gear ActuatorSDR CA060704008Elbow · fractured(CAN) DURING CRUISE THE ENGINE LOW OIL PRESSURE WARNING ANNUNCIATED. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT DIVERTED FOR AN UNSCHEDULED LANDING. SUBSEQUENT INSPECTION REVEALED THE REDUCTION GEARBOX PRESSURE OIL ELBOW IMPROPERLY SECURED AND FRACTJun 9, 2006 · Beech 1900D · Turbine Engine Oil SystemSDR 1060606018Skin · lightning strikeLIGHTING STRIKE DAMAGE REPAIRED IAW WITH RAYTHEON FR-CO-01356 REV 1.Jun 9, 2006 · N167YV · Beech 1900D · Fuselage Main, Plate/SkinSDR CA060614005Case · leakingAPPROX 20 MIN INTO CRUISE FLIGHT, THE LT LOW OIL PRESSURE LIGHT CAME ON . THE ENGINE WAS SHUT DOWN AS IT REACHED 50 PSI. ELECTED TO RETURN TO PLACE OF DEPARTURE AND A SUCCESSFUL LANDING WAS MADE. UPON STOPPING A LARGE QUANTITY OF OIL WAS FOUND UNDERNEATH LTJun 9, 2006 · Beech 1900D · Engine (Turbine/Turboprop)SDR BSAASDR0615Connector · disconnectedTHE AIRCRAFT DID NOT PRESSURIZE & THE CABIN WARNING LIGHT CAB ALT HI DIDN'T COME ON WHEN THE CABIN ALTITUDE WENT ABOVE 10,000FT. ONE OF THE ELECTRICAL CONNECTORS ON THE CAB ALT HI PRESSURE SWITCH WAS FOUND DISCONNECTED. THE CONNECTOR WAS REINSTALLED. THE CRJun 7, 2006 · N139ZV · Beech 1900D · Cabin Pressure IndicatorSDR BSAASDR0614Skin · corrodedLEVEL 1 SURFACE CORROSION WAS FOUND IN THE LEFT AND RIGHT WINGS IN THE AREA OF THE QUICK DRAINS OUTBOARD OF THE NACELLES AND FORWARD OF THE SPAR AT WS 125 TO 128. CORROSION WAS EVALUATED, DETERMINED TO BE LEVEL 1 SURFACE CORROSION, IT WAS CLEANED OFF, AND THEJun 6, 2006 · N165YV · Beech 1900D · Wing, Plate/SkinSDR 77791Printed Ckt Board · faultyUPON APPROACH, CREW EXTENDED LANDING GEAR AND DID NOT GET 3 GREEN DOWN AND LOCK INDICATIONS. CREW THEN COMPLETED THE EMERGENCY CHECKLIST AND LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND GROUNDING CIRCUIT BAD ON PCB. RJun 4, 2006 · N127YV · Beech 1900D · Landing Gear Position and WarningSDR GUUA94957060206ASpar Cap · damagedRT WING REAR SPAR LOWER CAP AFT FLANGE DEFLECTED .046 INCHES UPWARD. LOCATED AT WS 104.50. HAND FORMED SPAR FLANGE BACK TO ORIGINAL PROFILE, PERFORMED NDT EDDY CURRENT INSP BY A QUALIFIED LEVEL III INSPECTOR NO CRACK INDICATIONS NOTED. FABRICATED AND INSTALLJun 2, 2006 · N69549 · Beech 1900D · Wing SparSDR 77773Indicator · malfunctionedUPON APPROACH CREW EXTENDED THE LANDING GEAR AND DID NOT GET A GREEN DOWN AND LOCK INDICATION ON ANY OF THE THREE LANDING GEAR DOWN AND LOCK INDICATORS, FOLLOWED REQUIRED GEAR EXTENSION EMERGENCY CHECK LIST AND LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED Jun 2, 2006 · N127ZV · Beech 1900D · Landing Gear Position and WarningSDR CA060601005Turbine Blades · fractured(CAN) DURING TAKE-OFF ROLL THE ENGINE EMITTED A LOUD NOISE AND TAKE-OFF WAS ABORTED. SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES AND RESULTS, EXHAUST STUB DAMAGE. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (May 31, 2006 · Beech 1900D · Turbine SectionSDR CA060531016Blade · failed(CAN) UPON APPLYING TAKEOFF POWER FOR DEPARTURE, THE PILOT HEARD A LOUD BANG. HE THEN INITIATED A SUCCESSFULL REJECTED TAKEOFF. UPON STOPPING, A PASSENGER CAME FORWARD AND STATED THAT HE THOUGHT SOMETHING FELL OFF THE RT WING. THE RT ENGINE WAS SECURED. THE May 30, 2006 · Beech 1900D · Turbine SectionSDR CA060606008Relay · damaged(CAN) WHEN GROUND POWER WAS APPLIED TO THE AIRCRAFT IT WAS NOTICED THAT THE LT HEATED WINDSHIELD WAS WARM AND ANTI-ICE SWITCH WAS OFF. POWER TO WINDSHIELD, LIMITER IN LT NACELLE, WAS PULLED. INSP OF THE LT WINDSHIELD ANTI-ICE HI/LO RELAYS, BEHIND INSTRUMENT PAMay 27, 2006 · Beech 1900D · Window System WiringSDR GUUA05270601Compressor · failedFLIGHT: 9192 EYW/TPA DURING FLIGHT AIRCRAFT HAS NAUSEOUS ODOR WITH BLOWERS ON. REPLACED VCM COMPRESSOR. OPERATION CHECK GOOD.May 27, 2006 · N87550 · Beech 1900D · Cabin Cooling SystemSDR CA060525004Bracket · cracked(CAN) DURING A BASE INSPECTION THE RT OB FLAP ACTUATOR BRACKET WAS FOUND CRACKED. WHEN THE BRACKET WAS REMOVED FROM THE SKIN, IT WAS DISCOVERED THAT THE SKIN WAS ALSO CRACKED. FURTHER INSPECTION REVEALED THAT THE RIB UNBER THE SKIN WAS ALSO DAMAGED. THE FLAP WMay 24, 2006 · Beech 1900D · Trailing Edge FlapsSDR 1060504022ASpar Cap · corrodedBIO-CORROSION RT MAIN SPAR CAP AT WS 124.588. REPAIRED IAW MFG FR-CO-01350 REV.1May 23, 2006 · N244YV · Beech 1900D · Wing SparSDR 1060504022Spar Cap · corrodedBIO-CORROSION LT MAIN SPAR CAP AT WS124.588. REPAIRED IAW MFG FR-CO-01350 REV.1May 23, 2006 · N244YV · Beech 1900D · Wing SparSDR CA060531015Engine · making metal(CAN) DURING DESCENT THE ENGINE WAS REPORTED TO LOSE POWER ACCOMPANIED BY A FIRE. THE CREW DEPLOYED FIRE EXTINGUISHERS AND SHUT THE ENGINE DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METAL IN THE ENGINE EXHAUST. MFG WILL INVESTIGATE THE EVENT AND ADVISE May 21, 2006 · Beech 1900D · Engine (Turbine/Turboprop)SDR 05242006ADoor Seal · blownCLIMBING THROUGH 16K TO FL 200 HAD VERY LOUD POP SOUND FOLLOWED BY CONSTANT HISSING COMING FROM FRONT OVERHEAD OF AIRCRAFT. FOUND MAIN ENTRANCE DOOR SEAL TO HAVE BEEN BLOWN. REMOVED AND REPLACED MAIN ENTRANCE DOOR SEAL.May 21, 2006 · N220CJ · Beech 1900D · Passenger/Crew DoorsSDR GUUA05210602Spar Cap · damagedFLIGHT: 9137 SAQ/FLL RT LANDING GEAR COLLAPSE BACKWARDS ON LANDING FOUND RT WING REAR SPAR LOWER CAP AFT FLANGE DEFLECTED .046 INCHES UP. HAND FORMED SPAR FLANGE BACK TO ORIGINAL PROFILE PERFORMED NDT EDDY CURRENT INSPECTION BY A QUALIFIED LEVEL III INSPECTORMay 21, 2006 · N69549 · Beech 1900D · Wing SparSDR GUUA05210601Bolt · brokenFLIGHT: 9137 SAQ/FLL DURING APPROACH RT MLG UNSAFE INDICATION. RT LANDING GEAR COLLAPSE BACKWARDS ON LANDING. FOUND RT MLG DRAG BRACE ATTACH BOLT BROKEN.May 21, 2006 · N69549 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR BSAASDR0613Combustion Case · corrodedCREW ABORTED TAKEOFF DUE TO LOW POWER INDICATION AT MAX CONTINUOUS ITT. DURING THE TROUBLESHOOTING FOR THIS PROBLEM A SMALL PINHOLE WAS FOUND CORRODED IN THE EXTERNAL COMBUSTION CASE JUST FORWARD OF THE AFT DRAIN. THE ENGINE WAS REMOVED FOR REPAIR. THE AIR May 19, 2006 · N3199Q · Beech 1900D · Turbine Engine Combustion SectionSDR GUUA05180601Valve · faultyFLIGHT: 9235 JAX/TPA DURING APPROACH LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER AND LOWERED LANDING GEAR NORMALLY. REPLACED LANDING GEAR SERVICE VALVE.May 18, 2006 · N218YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 05182006BWarning Switch · malfunctionedDURING T/O ROLL, LEFT LOW ANNUNCIATOR ILLUMINATED. COULD NOT DUPLICATE DISCREPANCY. AS A PRECAUTION, INSPECTED RELATED C/B, DISCONNECTED CLEANED VISUALLY INSPECTED AND RECONNECTED LOW LEVEL SENSOR CANNON PLUG SUMPED LT WING FUEL TANKS, SYSTEM OPS CHECK GOOD.May 15, 2006 · N243CJ · Beech 1900D · Fuel Quantity SensorSDR GLBA20060763Skin · corrodedCORROSION FOUND AT FS 214, OUTER SKIN & STRINGER 16, REPAIR PENDING, INSTALL FLUSH PATCH APPROXIMATLY 12" X 12"May 15, 2006 · N261GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20060764Doubler · crackedSTRUCTURAL INSPECTION - LEFT ( 114-430002-7180) AND RIGHT (114-430002-7179) HEAVY DOUBLERS CRACKED F.S. 288-327 & WL 100, REPAIR PENDING, REPLACED DOUBLERSMay 15, 2006 · N261GL · Beech 1900D · Fuselage Main, Plate/SkinSDR CA060531009Engine · malfunctioned(CAN) DURING TAKE-OFF ROLL THE ENGINE WAS REPORTED TO EMIT A LOUD NOISE ACCOMPANIED BY SEIZURE OF THE POWER SECTION. SUBSEQUENT INSPECTION REVEALED DAMAGED POWER TURBINE BLADES. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TCMay 8, 2006 · Beech 1900D · Engine (Turbine/Turboprop)SDR 05092006CBuss Tie · out of positionAPPROX 10 MIN AFTER T/O F/O NOTICED SMOKE COMING FROM C/B PANEL AREA ON RIGHT SIDE, BOTH PILOTS SMELLED SMOKE IN COCKPIT. INSPECTED C/B PANEL ON FO'S SIDE FOR ARCING DAMAGE. FOUND ELECTRICAL CONTACT BETWEEN C/B BUS TIE BAR AND CB TERMINAL ENDS. REPOSITIONED May 8, 2006 · N155CJ · Beech 1900D · AC Power Distribution SystemSDR 77367Wire · chafedDURING GEAR RETRACTION LT MAIN GEAR W/N RETRACT CB POPPED. FOUND HYDRALIC POWER PACK SLECTOR VALVE WIRE G9B22 CHAFFED AND CUT NEAR CONNECTOR P209.May 8, 2006 · N10675 · Beech 1900D · Landing Gear System WiringSDR GUUA05080601Connector · faultyFLIGHT: 9259 FLL/MHH AFTER TAKEOFF LANDING GEAR WILL NOT RETRACT. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. INSTALLED CONNECTOR A325P1 WITH JUMPER P1-A-P1-C IN NOSE WHEEL WELL. OPERATIONAL CHECK NORMAL.May 8, 2006 · N81556 · Beech 1900D · Landing Gear System WiringSDR CA060510007Shaft · corrodedINTERNAL CABIN PORTION OF PHASE 3 INSPECTION FOUND BOTH RT EMERG EXIT DOORS WOULD NOT OPEN FROM INSIDE. BOTH DOORS WERE REMOVED VIA EXT HANDLE AND DISASSEMBLED, UPON INSPECTION, FOUND RT COUPLING P/N 129-514065-2 WAS MATED TO SHAFT P/N 129-514033-2 AT ALL TIMMay 7, 2006 · Beech 1900D · Emergency ExitsSDR GUUA05070601Hinge Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE RT CTR ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED RT CTR ELEVATOR HINGE BRACKET.May 7, 2006 · N82539 · Beech 1900D · Elevator Structure
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