Raytheon 1900D

Service difficulty reports · 7,152

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Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 98ZZZM934Temp Controller · failedFUMES REPORTED IN CABIN EN ROUTE FROM ELM TO BOS. AIRCRAFT DIVERTED TO ALB. UPON INSPECTION OF AIRCRAFT, THE PCB IN THE CABIN TEMPERATURE CONTROLLER HAD BURNED. ADDITIONAL INSPECTION, FOUND WIRES NR H177A22 AND NR H178A22, TO DUCT TEMP SENSOR SHORTED IN CABNov 6, 1998 · N852CA · Beech 1900D · Cabin Temperature ControllerSDR C2XA98CL071Brush Block · wornCLE - FLT 3291 - CREW REPORTED THAT AFTER TAKEOFF THE RIGHT PROPELLER ANTI-ICE SYSTEM WAS INDICATING 24 AMPS. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE RIGHT PROPELLER ANTI-ICE SYSTEM THEN REMOVED AND REPLACED THE DE-Nov 5, 1998 · N48544 · Beech 1900D · Propeller/Rotor Anti-Ice/De-Ice SystemSDR MASA98196Unknown · smokeFLT 700 - FMN-ABQ - AFTER TAKEOFF, CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. AIRCRAFT RETURNED TO THE FIELD. NO EMERGENCY WAS DECLARED, THE MASKS WERE NOT DEPLOYED. MAINTENANCE T/S THE SYSTEM BUT WERE UNABLE TO DUPLICATE THE DISCREPANCY. NO DISCREPANCINov 3, 1998 · N104YV · Beech 1900D · Air Distribution SystemSDR CA981109039Drain · clogged(CAN) ON REMOVAL OF THE HORIZONTAL STABILIZER UPPER INSPECTION PANEL, FOUND THERE WAS WATER ACCUMULATION NEXT TO THE BULKHEAD PN 101-600015-9. THIS CONDITION WAS CAUSED BY THE INCORRECT LOCATION OF A WATER DRAIN HOLE. SUBMITER STATED IF THE WATER IS ALLOWED Nov 3, 1998 · Beech 1900D · Horizontal Stabilizer StructureSDR CA981109038Drain · sealed(CAN) DURING INSPECTION, WATER WAS FOUND TRAPPED IN THE RUDDER 4 INCHES ABOVE THE TRIM TAB. DRAIN HOLES WERE FOUND TO BE SEALED. DRAINS OPENED AND WATER RELEASED. SUBMITTER STATED APPARENTLY HOLES WERE SEALED AT THE FACTORY, BEECH NOTIFIED OF THE PROBLEM. Nov 3, 1998 · Beech 1900D · Rudder StructureSDR MASA98193Retaining Ring · shearedFLT 5342 - GON-PHL - UPON CLOSING, THE AIRSTAIR DOOR, THE OUTER DOOR HANDLE FELL OFF. MAINTENANCE REPLACED THE RETAINING RING AND REINSTALLED THE DOOR HANDLE, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)Oct 30, 1998 · N70ZV · Beech 1900D · Entrance StairsSDR 98ZZZM887Temp Controller · failedDURING DESCENT AT APPROXIMATELY 14,000 FT, A SUDDEN AND STRONG BURNING SMELL WITH A HAZE OF SMOKE FILLED COCKPIT. INSPECTION OF AIRCRAFT FOUND CIRCUIT CARD FAILURE IN CABIN TEMPERATURE CONTROLLER IN CABIN CEILING. UNIT WAS REPLACED AND SYSTEM CHECKED SATISFAOct 24, 1998 · N852CA · Beech 1900D · Cabin Temperature ControllerSDR 98ZZZM886Actuator · failedFLAPS STUCK AT 17 DEGREES. SECURED FLAPS TO UP POSITION. INSPECTION OF COMPONENTS FOUND LT INBD ACTUATOR FAILURE. REMOVED AND REPLACED LT INBD FLAP ACTUATOR IAW RAYTHEON MAINTENANCE MANUAL CHAPTER 27. (M)Oct 24, 1998 · N858CA · Beech 1900D · Trailing Edge Flap Control SystemSDR 98ZZZM825Pump · leakingFUEL LEAK RIGHT ENGINE NACELLE. INSPECTION OF AIRCRAFT FOUND RIGHT ENGINE LOW PRESSURE FUEL BOOST PUMP LEAKING. REPLACED PUMP IAW MM CHAPTER 73-10-00. (M)Oct 23, 1998 · N838CA · Beech 1900D · Fuel Boost PumpSDR AU981591Blade · bird strike(AUS) LEFT ENGINE SUFFERED A BIRD STRIKE (BROLGA) DURING TAXIING RESULTING IN A PROPELLER BLADE SEPARATING APPROXIMATELY 25.4 MM TO 50.8 MM (1 INCH TO 2 INCHES) FROM THE BLADE ROOT. THE RESULTING OUT OF BALANCE CAUSED ADDITIONAL DAMAGE TO THE FIREWALL AND THEOct 20, 1998 · Beech 1900D · Propeller Blade SectionSDR 98ZZZX4209Fork · crackedFORWARD EAR OF PICH CHANGE FOR CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. THREE CRACKS.Oct 20, 1998 · Beech 1900D · Propeller Blade SectionSDR CA981027017Display · failed(CAN) SHORTLY AFTER TAKEOFF, CREW LOST RIGHT EFDU SCREEN FOLLOWED BY A BURNING SMELL. THE SYSTEM WAS ISOLATED AND BOTH AC BUSES WERE SHUT DOWN. AIRCRAFT LANDED SAFELY. UPON FURTHER INVESTIGATION BY MAINTENANCE IT WAS DETERMINED THE RIGHT ELECTRONIC FLIGHT DOct 16, 1998 · Beech 1900D · Integrated Flight SystemSDR 98ZZZX4134Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. TWO CRACKS.Oct 14, 1998 · Beech 1900D · Propeller Blade SectionSDR 98ZZZX4133Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. THREE CRACKS.Oct 14, 1998 · Beech 1900D · Propeller Blade SectionSDR 98ZZZM891Switch · malfunctionedFLT 5633 - RETURNED TO THE FIELD IN MCI WHEN THE LEFT FIRE LOOP LIGHT CAME ON IN FLIGHT. MCI MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY, BUT DID CHANGE THE T-HANDLE AND RETURNED THE AIRCRAFT TO SERVICE AFTER A TEST FLIGHT THAT PRODUCED NO DISCREPANCY. (Oct 10, 1998 · N176YV · Beech 1900D · Detection SystemSDR 98ZZZM885Switch · malfunctionedFLT 5665 - ICT-MCI - EN ROUTE, T-HANDLE AND FIRE LOOP ILLUMINATE INTERMITTENTLY. ICT MAINTENANCE FOUND AND REPAIRED CHAFFED WIRES UNDER THE LEFT FORWARD FLOORBOARD AND REPLACED THE LEFT FIRE LOOP TEST SWITCH. THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTOct 10, 1998 · N176YV · Beech 1900D · Detection SystemSDR 98ZZZM883Harness · looseFLT 5600 - RTF WHEN THE LT ENGINE FIRE WARNING ILLUMINATED IN FLIGHT. THE LEFT ENGINEWAS SHUT DOWN. EMERGENCY EQUIPMENT WAS CALLED. AIRCRAFT LANDED WITHOUT INCIDENT. ICT MAINTENANCE THEN RETURNED THE AIRCRAFT TO SERVICE. (M)Oct 9, 1998 · N176YV · Beech 1900D · Detection SystemSDR 98ZZZM903Fire Loop · malfunctionedFLT 5601 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED INTERMITTENTLY IN FLIGHT. MAINTENANCE REPLACED FORWARD AND AFT FIRE LOOP DETECTORS, PERFORMED GROUND RUN OPS CHECK NORMAL. (M)Oct 8, 1998 · N176YV · Beech 1900D · Detection SystemSDR 98ZZZM902Fire Loop · malfunctionedFLT 5601 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED INTERMITTENTLY IN FLIGHT. MAINTENANCE REPLACED FORWARD AND AFT FIRE LOOP DETECTORS, PERFORMED GROUND RUN OPS CHECK NORMAL. (M)Oct 8, 1998 · N176YV · Beech 1900D · Detection SystemSDR 98ZZZM884Ehsi · failedFLT 5633 - SGF-MCI - EN ROUTE, THE CREW REPORTED SMOKE IN THE COCKPIT AFTER THE CAPTAINS EHSI FAILED. EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED IN MCI WITHOUT INCIDENT. MCI MAINTENANCE REPLACED THE EHSI AND INSPECTED AIRCRAFT FOR DAMAGE. THE AIRCRAFT WASOct 8, 1998 · N140ZV · Beech 1900D · Integrated Flight SystemSDR 98ZZZM901Fire Loop · looseFLIGHT 5609 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED. INTERMITTENTLY IN FLIGHT. MAINTENANCE FOUND LOOSE WIRE AT LOOP CONNECTOR. WIRE WAS RESOLDERED, PERFORMED GROUND RUN OPS CHECK NORMAL. (M)Oct 7, 1998 · N176YV · Beech 1900D · Detection SystemSDR CA981028010Support · misinstalled(CAN) THE TWO CENTER HOLE BOSSES OF THE PRESSURE MANIFOLD SUPPORT PLATE ARE CHAFING AGAINST THE INNER SIDE OF THE PROPELLER PRESSURE MANIFOLD DUE TO THE CLOSE TOLERANCE BETWEEN THE TWO PARTS. SUBMITTER STATED RAYTHEON HAS BEEN ADVISED OF THIS CONDITION AND AROct 5, 1998 · Beech 1900D · Propeller Controlling SystemSDR MASA98183Switch · malfunctionedFLT 5435 - GNV-MIA - ON APPROACH INTO MIA WITH GEAR SELECTED DOWN, THE LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. A MANUAL GEAR EXTENSION WAS PERFORMED BUT A SAFE CONDITION COULD NOT BE VERIFIED. THE CREW DECLARED AN EMERGENCY. THE GEAR WAS VISUALLY VOct 2, 1998 · N46YV · Beech 1900D · Landing Gear Position and WarningSDR CA981013002Structure · damaged(CAN) ON LANDING ROLL OUT, AIRCRAFT STRUCK A DEER AND DAMAGED THE INBOARD LEADING EDGE AND LEFT INBOARD FLAP. THE FLAP WAS REMOVED AND INSPECTED FOR INTERNAL DAMAGE ALONG WITH THE LEADING EDGE. THE FLAP WAS INSTALLED AND SECURED IN THE RAISED POSITION. A LISep 30, 1998 · Beech 1900D · Wing Main, Frame StructureSDR 98ZZZX4011Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INOBARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FIVE CRACKS.Sep 24, 1998 · Beech 1900D · Propeller Blade SectionSDR CA980928035Tube · chafed(CAN) DURING MAINTENANCE INSPECTION, THE TUBE (P/N 114-820030-3) WAS FOUND CHAFED BY THE BOOT (P/N 50-820125) THAT IS HELD TIGHT ON THE TUBE BY A TIE WRAP. PART TC: 6,383.Sep 22, 1998 · Beech 1900D · Landing Gear Steering SystemSDR CA980928034Screw · loose(CAN) THE PILOT NOTICED SOME LOOSENESS IN THE RIGHT CONDITION LEVER DURING PRE-START CHECK LIST. MAINTENANCE DETERMINED THE LOOSENESS WAS DUE TO A LOOSE SCREW SECURING THE LEVER TO THE SHAFT. SCREW TIGHTENED. PART TC: 6,347.Sep 22, 1998 · Beech 1900D · Power LeverSDR 98ZZZM788Switch · failedAUTOFEATHER OFF ANNUNCIATOR STAYS ON INFLIGHT. LEFT MAIN LANDING GEAR UPLOCK SWITCH FAILED. REPLACED LEFT MAIN LANDING GEAR UPLOCK SWITCH, RETRACTION CHECK SAT IAW CHAPTER 32. (M)Sep 22, 1998 · N858CA · Beech 1900D · Landing Gear Position and WarningSDR CA981125079Actuator · malfunctioned(CAN) DURING APPROACH, THE GEAR WAS SELECTED DOWN BUT THE RIGHT MAIN WAS VERY SLOW TO GREEN UP. MAINTENANCE HAD PREVIOUSLY REPLACED LEFT ACTUATOR FOR THE SAME PROBLEM. HOWEVER, THE PROBLEM TRANSFERRED TO THE RIGHT SIDE. RIGHT ACTUATOR TO BE REPLACED AS A PRSep 18, 1998 · Beech 1900D · Landing Gear ActuatorSDR MASA98180Seal · looseFLT 5329 - FLL-TPA - DURING CLIMB-OUT, THE CREW HEARD A LOUD NOISE COMING FROM THE CABIN. THEY DETERMINED THAT THE AIRSTAIR DOOR SEAL HAD POPPED OUT OF ITS SEAT. THE AIRCRAFT EXPERIENCED A SLIGHT DEPRESSURIZATION, BUT THE OXYGEN MASKS WERE NOT DEPLOYED. AIRSep 17, 1998 · N68ZV · Beech 1900D · Entrance StairsSDR CA980930024Elt · cracked(CAN) DURING AIRCRAFT TOW OUT, IT WAS NOTICED THE ELT TRANSMIT LIGHT WAS ON. RESETTING THE REMOTE SWITCH HAD NO EFFECT AND RESETTING THE ELT ON/OFF SWITCH HAD NO EFFECT. THE ELT BATTERY HAD TO BE DISCONNECTED FOR THE ELT TO STOP TRANSMITTING. THE CASE OF THSep 17, 1998 · Beech 1900D · Emergency Locator BeaconSDR 98ZZZM776Acm · failedAIRCRAFT WILL NOT COOL. REPLACED AIR CYCLE MACHINE AND HEAT EXCHANGER. (M)Sep 15, 1998 · N842CA · Beech 1900D · Cabin Cooling SystemSDR CA980916047Switch · intermittent(CAN) ON GEAR DOWN SELECTION, THE LEFT HAND MAIN INDICATOR WOULD OCCASIONALLY DELAY SLIGHTLY BEFORE ILLUMINATING. MAINTENANCE FOUND THE INTERNAL DOWN POSTION MICROSWITCH IS SOMEWHAT INTERMITTENT. ACTUATOR REPLACED. PART TC: 774.Sep 14, 1998 · Beech 1900D · Landing Gear Position and WarningSDR MASA98175Switch · out of adjustFLT 5331 - RDG-PHL - THE LEFT AUTOFEATHER WOULD NOT ARM ON TAKEOFF, AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE ADJUSTED THE PEDESTAL SWITCHES, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 12, 1998 · N126YV · Beech 1900D · Propeller Feathering/ReversingSDR 98ZZZM777Servicing Valve · failedLANDING GEAR FAILED TO RETRACT ON TAKEOFF. CIRCUIT BREAKER OPENED. SERVICING VALVE FOUND TO BE DEFECTIVE. REPLACED DEFECTIVE SERVICING VALVE IAW CHAP 32 RAYTHEON MM. OPS CHECK SATISFACTORY. (M)Sep 10, 1998 · N860CA · Beech 1900D · Landing Gear Retraction/Extension SystemSDR S2YA98029Connector · contaminatedFLT 1837 - MKE-MSN - DURING APPROACH, THE CREW SELECTED THE LANDING GEAR DOWN. WITH THE GEAR EXTENDED THE LEFT MAIN GEAR DOWN ANNUNCIATOR FAILED TO ILLUMINATE UNTIL 60 SECONDS HAD PASSED. THE CREW DISCONTINUED APPROACH, CYCLED GEAR SEVERAL TIMES, THE ANNUNCISep 8, 1998 · N87SK · Beech 1900D · Landing Gear Position and WarningSDR S2YA98028Fire Loop · damagedFLT 1254 - MKE-GRR - ABORTED TAKEOFF DUE TO LT FIRE LOOP ANNUNCIATOR ILLUMINATING DURING TAKEOFF ROLL. MAINTENANCE INSPECTED A/C FOUND FWD AND AFT FIRE LOOPS BAD. MAINTENANCE REPLACED FWD AND AFT FIRE LOOPS, OPS CHECK GOOD. RETURNED A/C TO SERVICE. (M)Sep 8, 1998 · N901SK · Beech 1900D · Fire DetectionSDR CA980915021Inverter · faulty(CAN) AFTER TAKEOFF, BOTH AC BUSSES WENT OFF THE LINE. COULD NOT BE RESET. BOTH ATTITUDE AND HEADING REFERENCE WERE LOST. AS THEY WERE IN VMC CONDITIONS, RETURNED TO THE AIRPORT. INVESTIGATION REVEALED THE RIGHT HAND INVERTER WAS AT FAULT. BUT A SINGLE LOSSep 8, 1998 · Beech 1900D · AC InverterSDR CA981030006Power Pack · failed(CAN) LANDING GEAR DID NOT RETRACT ON UP SELECTION. GEAR SELECTED DOWN AND GEAR INDICATION STILL SHOWED DOWN AND LOCKED. MAINTENANCE PERSONNEL INSPECTED LANDING GEAR INTEGRITY IN THE DOWN AND LOCKED POSITION AND DISABLED THE GEAR DOWN AND LOCKED. FURTHER TSep 6, 1998 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR S2YA98027Tach Gen · malfunctionedFLT 1020 - GRB-MKE - ABORTED TAKEOFF DUE TO DECREASE IN PROPELLER RPM FROM 1700 RPM TO 1400 RPM IN FIVE SECONDS. THE A/C WAS FERRIED BACK TO MKE. MAINTENANCE INSPECTED A/C FOUND RT N2 TACH GENERATOR BAD. REPLACED RT N2 TACH GENERATOR OPS CHECK GOOD. RETURNSep 5, 1998 · N841SK · Beech 1900D · Engine RPM Indicating SystemSDR CA980916046Line · leaking(CAN) DURING ROUTINE MAINTENANCE, THE RIGHT HAND ENGINE MAIN FUEL PUMP HOSE ASSY WAS FOUND TO BE LEAKING. HOSE ASSY REPLACED. LEAKING OF HOSE WAS DUE TO INTERNAL FAILURE OF HOSE LINING. PART TC: 293.Sep 2, 1998 · Beech 1900D · Aircraft Fuel Distribution SystemSDR 98ZZZX3438Flyweight · crackedCUP STYLE FLYWEIGHT HAS INDICATION ON OUTSIDE OF CUP APPROXIMATELY6 .75 INCHES LONG. CORRESPONDING INDICATION ON INSIDE OF CUP. THIS WAS A STOCK GOVERNOR FOR INVENTORY.Sep 1, 1998 · Beech 1900D · Propeller Hub SectionSDR MASA98167Latch · dirtyHII/IFP - FLT 5021 - CAPTAIN CLOSED MAIN PASSENGER DOOR AND NOTED THE CABIN DOOR ANNUNCIATOR STAYED ILLUMINATED. FURTHER INVESTIGATION SHOWED THE PASSENGER DOOR WAS NOT LOCKING PROPERLY. AIRCRAFT FERRIED TO PHX WHERE THE DOOR LATCH MECHANISM WAS CLEANED AND Aug 30, 1998 · N93ZV · Beech 1900D · Entrance StairsSDR MASA98164Cam Locks · out of adjustDUJ/PIT - FLT 5954 - CREW REPORTED THE PASSENGER DOOR CAMLOCKS WOULD NOT LATCH COMPLETELY. MAINTENANCE RIGGED THE DOOR CAMLOCKS, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X)Aug 27, 1998 · N173YV · Beech 1900D · Passenger/Crew DoorsSDR MASA98162Actuator · failedPIT/DBE - FLT 5918 - ON APPROACH TO CBE, THE LT GEAR WOULD NOT INDICATE DOWN AND LOCKED. CREW DECLARED AN EMERGENCY, AND RETURNED TO PIT. AIRCRAFT LANDED WITHOUT INCIDENT AND WAS SUBSEQUENTLY FERRIED TO DUJ WHERE MAINTENANCE REMOVED AND REPLACED THE MAIN LANAug 26, 1998 · N17YV · Beech 1900D · Landing Gear ActuatorSDR MASA98161Air Dist System · condensationFLT 401 - ROW-ABQ - CREW REPORTED SMOKE IN CABIN IN FLIGHT, AIRCRAFT RETURNED TO ROW. UPON INSPECTION, THE SMOKE PROVED TO BE MOIST AIR FROM THE AIR VENTS, A NORMAL OCCURANCE. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 26, 1998 · N35YV · Beech 1900D · Air Distribution SystemSDR C2XA98IA319Block Unit · failedIAH - DURING FLIGHT 3992, THE PILOT REPORTED THE NR 2 PROP FEATHERED, UNCOMMANDED, IN FLIGHT. THE AIRCRAFT RETURNED AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BETA BLOCK ASSEMBLY. SUBSEQUENTLY, THE PROPELLER ASSY, AND GOVERNOR Aug 25, 1998 · N17534 · Beech 1900D · Propeller Controlling SystemSDR MASA98159Tcas · malfunctionedFLT 5998 - MBS-PIT - APPROXIMATELY 15 MILES FROM PIT, THE TCAS DISPLAY SCREEN BLANKED OUT, THEN RESET. THE CREW SMELLED A FAINT ELECTRICAL ODOR. CREW DONNED OXYGEN MASKS AND GOGGLES AS A PRECAUTION AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT Aug 23, 1998 · N161YV · Beech 1900D · Air Collision Avoidance SystemSDR MASA98157Emergency Door · mis-alignedFLT 5320 - FLL-TPA - DURIG PRE-FLIGHT WALK AROUND, CREW NOTICED THAT THE RIGHT REAR EMERGENCY EXIT EXTERIOR HANDLE WAS NOT FLUSH WITH THE DOOR. MAINTENANCE REMOVED AND REINSTALLED THE DOOR. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 21, 1998 · N23YV · Beech 1900D · Emergency ExitsSDR 98ZZZX3402Line · crackedRT PROPELLER WENT INTO FEATHER ON APPROACH. CRACKED P3 DELIVERY LINE. REPLACED RT P3 DELIVERY LINE.Aug 21, 1998 · N854CA · Beech 1900D · Propeller Feathering/Reversing
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