Beech B200

Service difficulty reports · 830

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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 = 'B200'
  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 QFY2002F00002Transorb · failedTRANSORB FAILED TO SHORTED CONDITION. RESULTED IN LANDING GEAR CIRCUIT BREAKER TO POP CAUSING NEED FOR MANUAL EXTENSION OF LANDING GEAR.Nov 1, 2002 · N875DM · Beech B200 · Landing Gear Retraction/Extension SystemSDR 2003FA0000357Windshield · crackedLEFT WINDSHIELD INNER PLY FAILED INFLIGHT, SPIDER WEB, CRACKED OVER ENTIRE INNER PLY. FLIGHT CONDITIONS AT TIME, NOT REPORTED. NO OBVIOUS EXTERIOR DEFECTS OR FOD OBSERVED.Oct 31, 2002 · N363CA · Beech B200 · Flight Compartment WindowsSDR PF212LWWindshield · failedINNER PANE OF PILOTS WINDSHIELD SHATTERED WHILE CLIMBING THROUGH 28000 FEET.Oct 29, 2002 · N212LW · Beech B200 · Flight Compartment WindowsSDR 2002FA0001259Fork · crackedFOUND HOLE FORK CRACKED, INSTALLED KIT.Oct 21, 2002 · N4PT · Beech B200 · Nose/Tail Landing Gear Strut/AxleSDR CA021104010Hinge · cracked(CAN) UPON INSPECTION IT WAS NOTED THAT THE DOOR ASSY BYPASS ICE VANE WAS RUBBING AGAINST THE COWLING. AFTER CLOSE INSPECTION IT WAS NOTED THAT THE HINGE HAD CRACKED FROM THE INBOARD END OUTBOARD ABOUT 3 INCH ALONG THE HINGE PIN. THE HINGE ASSEMBLY WAS REPLACOct 16, 2002 · Beech B200 · Air Intake Anti/De-Ice SystemSDR CA021001006Windshield · overheated(CAN) SHORTED AND OVERHEAT CONDITION ON LT WINDSHIELD GROUND TERMINAL CAUSING A HEAVY SMELL OF BURNED PLEXIGLASS TYPE OF ODOUR. PILOTS SWITCHED OFF LT WINDSHIELD ANTI-ICE AND SMOLDERING SUBSIDED.Sep 25, 2002 · Beech B200 · Windshield/Door Rain/Ice RemovalSDR 2002FA0001136Skin · crackedFOUND A 3.5 INCH CRACK APPROXIMATELY 6 INCHES DOWN AND .0200 INCH ON THE RIGHT SIDE TRAILING EDGE OF THE RUDDER.Aug 15, 2002 · N942CE · Beech B200 · Rudder, Plate/SkinSDR DYM2002F00000Compressor · damagedON TRAINING FLIGHT COPILOT NOTICED HOLE IN RIGHT INBOARD COWLING. UPON INSPECTION THE (FREON COMPRESSOR) HAD A SILVER DOLLAR SIZED HOLE IN THE SIDE. IT HAD A FLASH FIRE AND TORCHED A HOLE IN THE SIDE OF THE COWLING. SEVERAL COMPONENTS WERE ALSO DAMAGED.Jul 18, 2002 · N457TC · Beech B200 · Cabin Cooling SystemSDR 2002FA0000901Windshield · failedIN CRUISE AT WINDSHIELD SHATTERED, WINDSHIELD REMOVED AND SUBMITTED FOR EXAMINATION ( PEEL CHIP OR SPALLING FAILURES OF THE INNER LAMINATION OF BOTH WINDSHIELDS WAS AN INTERNAL STRESS BUILT INTO THE WINDSHIELDS AT MANUFACTURE.Jul 8, 2002 · N525SK · Beech B200 · Flight Compartment WindowsSDR 2002FA0000900Windshield · failedIN CRUISE RIGHT WINDSHIELD SHATTERED FOLLOWED BY EMERGENCY DESCENT. UPON AFTER LANDING INSPECTION LEFT W/S OBSERVED TO HAVE A 2 X 4.7500 INCH PEEL CHIP FAILURE, UPPER LEFT CORNER. CAUSE OF PEEL CHIP FAILURE OF INNER GLASS LAMINATION WAS AN INTERNAL STRESS BUJul 8, 2002 · N525SK · Beech B200 · Flight Compartment WindowsSDR 2002FA0000925Brush Block · inoperativeAFTER PROPELLER OVERHAUL AND PROPELLER DE-ICE BRUSH REPLACEMENT, PILOT REPORTED DEICE SYSTEM CIRCUIT/BREAKER SWITCH TRIPPED IN FLIGHT. COULD NOT DUPLICATE PROBLEM ON GROUND WITH ENGINES RUNNING. INSPECTED SYSTEM AND FOUND IF SIDE PRESSURE WS APPLIED TO RIGHJul 3, 2002 · N87SA · Beech B200 · Propeller/Rotor Anti-Ice/De-Ice SystemSDR GW12002F00000Line · fracturedPILOT EXPERIENCED LEFT ENGINE ROLL BACK TO IDLE, ENROUTE. INVESTIGATION REVEALED FRACTURED P3 AIR DELIVERY TUBE (PN 3027791) AT THE TUBE/FERRULE JOINT (B) NUT ON THE FUEL CONTROL UNIT. THE P3 TUBE WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERIVCE.Jun 5, 2002 · N992TJ · Beech B200 · Engine Fuel and ControlSDR JEM2002F00001Line · chafedTHIS LINE ASSEMBLY WAS CHAFING AGAINST AN ENGINE POWER CONTROL CABLE LOCATED BEHIND THE REMOVEABLE LEFT HAND INBOARD LEADING EDGE PANEL. VIBRATION CAUSED THE OUTER SHEATH OF THE CONTROL CABLE TO CHAFE DEEP SERRATIONS INTO THIS LANDING GEAR HYDRAULIC LINE. ITMay 24, 2002 · N362EA · Beech B200 · Hydraulic System, MainSDR T4O2002F00000Bulkhead · scratchedDURING THE 10,000 CYC AFT PRESSURE BULKHEAD INSPECTION IT WAS FOUND. AFT PRESSURE BULKHEAD SCRATCHED IN TWO HORIZONTAL LINES, 1.5 INCHES APART TO .006 INCH DEEP, FORWARD SIDE OF BULKHEAD. CAUSED BY CUTTING TOO DEEP (CARPET OR INSULATION) ALONG EDGES OF CENTEApr 22, 2002 · N200QS · Beech B200 · Fuselage Main, BulkheadSDR YE92002F00001Switch · defectiveLANDING GEAR WAS RETRACTED AFTER TAKEOFF AND LANDING GEAR SEEMED SLUGGISH. LOCAL MAINTENANCE DETERMINED DEFECTIVE GEAR SWITCH. NEW GEAR SWITCH WAS INSTALLED AND TESTED. LANDING GEAR IS OPERATIONAL AT THIS TIME.Apr 11, 2002 · N87SA · Beech B200 · Landing Gear Retraction/Extension SystemSDR CGO2002F00000Tab · mismanufacturedTAB, LEFT ELEVATOR. RECEIVED TAB ASSEMBLY, LEFT ELEVATOR NEW FROM MANUFACTURER MISSING THE REQUIRED RIVETS. ASSEMBLY WAS BONDED AND PRIMERED BUT HAD NOT BEEN RIVETED.Apr 10, 2002 · N728AM · Beech B200 · Elevator StructureSDR 2002FA0000534A/C Pack · malfunctionedFLOW PACK HAS LOW FLOW TO CABIN.Apr 2, 2002 · N87SA · Beech B200 · Cabin Cooling SystemSDR YE92002F00000A/C Pack · malfunctionedPILOT NOTICED CABIN CLIMBING AT A HIGHER THAN NORMAL RATE. AIRCRAFT RETURNED TO AIRPORT AND LOCAL MAINTENANCE DETERMINED. FLOW PACK NEEDED TO BE CHANGED. BOTH FLOW PACKS WERE CHANGED. ALL OPERATIONAL TEST ARE GOOD AT THIS TIME, PRESSURIZATION, NORMAL.Mar 26, 2002 · N87SA · Beech B200 · Air Distribution SystemSDR 2002FA0000533Bushing · looseDURING A SCHEDULED CORROSION INSPECTION THE RIGHT ELEVATOR WAS REMOVED. UPON REMOVAL THE BUSHING IN THE END OF THE ACTUATOR WAS FOUND TO BE LOOSE ON THE SHAFT. WITH THIS BUSHING NOT INSTALLED THE POSSIBILITY OF TAB FLUTTER OR NOT ALLOWING THE TAB ITS FULL MOMar 25, 2002 · N311MP · Beech B200 · Stabilizer ActuatorSDR 2002FA0000395Windshield · brokenINNER PANE OF PILOT WINDSHIELD SHATTERED IN CRUISE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENCE. WINDSHIELD HEAT CONTROLLER CHANGED IN CONJUNCTION WITH WINDSHIELD. NO PROBABLE CAUSE FOR BREAKAGE.Mar 19, 2002 · N969WB · Beech B200 · Flight Compartment WindowsSDR 2002FA0000387Windshield · brokenINNER PANE OF PILOT WINDSHIELD SHATTERED IN CRUISE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. WINDSHIELD HEAT CONTROLLER CHANGED IN CONJUNCTION WITH WINDSHIELD.Mar 19, 2002 · N969WB · Beech B200 · Flight Compartment WindowsSDR EPD2002F00000Windshield · crackedCOCKPIT WINDSHIELD INNER PANEL CRACKED AT ALTITUDE. OUTER PANEL REMAINED INTACT. WINDSHIELD HEAT WAS ON. NO STRIKES NOTED.Mar 18, 2002 · N149SR · Beech B200 · Flight Compartment WindowsSDR CTU2002F00004Windshield · crackedCOPILOT WINDSCREEN INNER PANE FAILED AT 27,000 FEET IN LEVEL FLIGHT OUTSIDE AIR TEMPERATURE AT 32 DEGREES. WINDSHIELD (PN 10138402522) (SN 97112H4959) WINDSHIELD INSTALL KIT (PN 101-50413) (SN 21851).Mar 15, 2002 · N74RF · Beech B200 · Flight Compartment WindowsSDR CA020226005Pump · leaking(CAN) DURING SCHEDULED MAINTENANCE, NOTICED A DRIP OF FUEL COMING OFF OF THE ENGINE DRIVEN FUEL PUMP TO ENGINE FLANGE. WITH A CLOSER LOOK FOUND A BROWN STAIN AS WELL. REMOVED ENGINE DRIVEN FUEL PUMP ASSEMBLY AND INSPECTED. FOUND SPLINE DRIVE COUPLING WHICH ENTFeb 7, 2002 · Beech B200 · Engine Fuel PumpSDR 2002FA0000257Windshield · crackedWINDOW SHATTERED DURING FLIGHT AT ALTITUDE. REPLACED WITH NEW UNIT USING MFG SUPPLIED INSTALLATION KIT.Feb 5, 2002 · N63791 · Beech B200 · Flight Compartment WindowsSDR CA020207002Blade · cracked(CAN) TWO (2) CT BLADES CRACKED.Feb 3, 2002 · Beech B200 · Turbine SectionSDR 2002FA0000173Intercostal · crackedUPON PHASE INSPECTION OF CABIN DOOR, FOUND EXCESSIVE MOVEMENT FROM HAND RAIL ASSEMBLIES AT HINGE AREAS ON BOTH FORWARD AND AFT HANDRAILS. UPON FURTHER INSPECTION, FOUND BOTH INTERCOSTAL STRUCTURES CRACKED AROUND RIVETS.Jan 31, 2002 · N417MC · Beech B200 · Passenger/Crew DoorsSDR 2002FA0000444Flow Divider · leakingRECEIVED NEW FLOW DIVIDER TO REPLACE FLOW DIVIDER WITH SUSPECTED LEAKING DUMP VALVE. AT MFG REQUEST, A LEAK CHECK WAS PERFORMED ON THE NEW FLOW DIVIDER. IT WAS FOUND THAT THE NEW FLOW DIVIDER LEAKED AT THE DUMP VALVE AND IS NOT SERVICEABLE. THIS IS SECOND FJan 4, 2002 · N520DG · Beech B200 · Engine Fuel DistributionSDR 2001FA0000535Window · crackedLEFT HAND BAGGAGE COMPARTMENT WINDOW OUTER PANE CRACKED WHILE IN CRUISE FLIGHT. INNER PLY REMAINED INTACT AND FLIGHT CONTINUED UNPRESSURIZED TO HOME BASE WITHOUT FURTHER INCIDENT.Oct 16, 2001 · N185XP · Beech B200 · Passenger Compartment WindowsSDR U9R2001F00000Cell · defectiveDURING FIRST FEW WEEKS OF FLYING, BEGAN TO BLOW ONE MAIN 325 AMP CURRENT LIMITS. BATTERY WAS NOT DUE ANY MAINTENANCE, BUT REMOVED AND BENCH CHECKED IT BECAUSE OF POSSIBLE HIGH CURRENT DRAW. FOUND CELL NR 9 TO NOT MEET SPECS. IN RELATION TO MM CAP CHECK. THISep 19, 2001 · N67SD · Beech B200 · Battery/Charger SystemSDR 2001FA0000340Actuator · crackedNORMAL FLIGHT OPERATION THE CENTER SHAFT OF THE ACTUATOR CRACKED THE ENTIRE LENGTH CAUSING FLAP BOUNCING SIMILAR TO BAD ROLLERS. RECOMMEND INSPECTING TOP AND BOTTOM OF ACTUATOR CENTER SHAFT DURING REGULAR PHASE INSPECTIONS.Aug 1, 2001 · N711HA · Beech B200 · Trailing Edge Flap ActuatorSDR 2001FA0000329Bolt · backed outAN5-4A BOLT IN BOTTOM PIVOT POINT ROD ATTACHMENT BACKED OUT CAUSING LOSS OF ENGINE CONTROL. AN936B516 LOCK WASHER WAS PRESENT.Aug 1, 2001 · N424RA · Beech B200 · Power LeverSDR Z4MR601462Relief Valve · leakingA RANDOM INSPECTION OF THE FUEL PUMP REVEALED FUEL LEAKING FROM THE ENGINE DRIVEN LOW PRESSURE FUEL PUMP RELIEF VALVE GASKET.Jul 14, 2001 · N726CB · Beech B200 · Engine Fuel PumpSDR CA010627055Switch · intermittent(CAN) WHEN LANDING GEAR SELECTED UP AFTER TAKE OFF, GEAR DID NOT RETRACT. GEAR SELECTED BACK DOWN WITH NORMAL DOWN AND LOCKED INDICATION ON ALL GEAR. NORMAL LANDING CARRIED OUT WITHOUT INCIDENT. TROUBLESHOOTING FOUND INTERMITTENT MIRCOSWITCH CONTACTS IN LANDINJun 15, 2001 · Beech B200 · Landing Gear SelectorSDR 20010613CW007Window · brokenTHE AIRCRAFT WAS CLIMBING TO ALTITUDE PRESSURIZED WHEN PILOT HEARD BANG IN BACK OF CABIN. THE SMALL WINDOW AFT OF CABIN DOOR HAD CATASTROPHIC FAILURE AND AIRCRAFT DEPRESSURIZED. LOG BOOKS WERE NOT AVAILABLE FOR REVIEW. PILOT STATED HE BELIEVED THE WINDOW HAMay 7, 2001 · N132N · Beech B200 · Passenger Compartment WindowsSDR 20010410AP024Float Valve · bentTHE FUEL VENT FLOAT VALVE IN THE TOP OF THE RT NACELLE TANK WAS IMPROPERLY INSTALLED. THE FLOAT PIVOT BRACKET WAS BENT. THIS WOULD PREVENT THE VALVE FROM SEATING PROPERLY. THIS WAS ALLOWING FUEL TO TRANSFER INTO THE AUX TANK WHEN EVER THE MAIN TANK WAS FULLApr 5, 2001 · N773TP · Beech B200 · Fuel StorageSDR CA010322004Tire · imbalanced(CAN) SEVERE VIBRATION WAS FELT ON TAKEOFF. AIRCRAFT RETURNED TO BASE. NOSE WHEEL REMOVED AND UNABLE TO BALANCE. UPON TIRE REMOVAL AN INTERNAL BALANCE PATCH WAS FOUND UNATTACHED. THIS TIRE WAS PURCHASED NEW IS A GOODYEAR P/N 301-392-641, S/N 91851436 WAS INSTAMar 11, 2001 · Beech B200 · TireSDR 20010322CW005Bracket · crackedTHE LT ATTACH BRACKET THAT SECURES THE HORIZONTAL STABILIZER TO THE VERTICAL FIN HAD A CRACK AT THE LOWER HUCKBOLT HOLE ATTACHING IT TO THE VERTICAL FIN. REPLACEMENT OF THE BRACKET WAS REQUIRED DUE TO THIS CRACK. AREA IS HARD TO SEE, LOCATED ON THE FORWARD LFeb 15, 2001 · N333RD · Beech B200 · Horizontal Stabilizer StructureSDR 20010416CW009Fuel Control · inoperativeDURING TRAINING FLIGHT IN AN EMERGENCY DECENT SIMILATION, THE LEFT ENGINE FLAMED OUT AND COULD NOT BE RESTARTED. REPLACED THE FUEL CONTROL AND OPERATION IS NORMAL.Jan 10, 2001 · N63791 · Beech B200 · Fuel Control/Turbine EnginesSDR 20010228CW007Windshield · crackedCOPILOT SIDE WINDSHIELD WAS INSTALLED AT MAINT FACILITY. AC COMPLETED 1 FLIGHT WHEN OUTER PLY OF WINDSHIELD CRACKED. AC LANDED AT MAIN FACILITY FOR REPLACEMENT OF WINDSHIELD.INSTALLATION IS ACCOMPLISHED USING STRESS FREE KITS AND PROCEDURES. QUESTIONS CONCEDec 27, 2000 · N713TA · Beech B200 · Flight Compartment WindowsSDR 20001214SH001Harness · burnedWIRE BUNDLE SPIRAL WRAP MELTED AND CHAFING AGAINST THE BRAKE DE-ICE HEAT LINE WHERE IT MAKES THE TURN TO COME INTO THE FORWARD INBOARD PART OF WHEELWELL AT WS 85, ACCESS PANEL NR 13 AS SEEN ON CHAP 12-20-00 PAGE 249, FIG. 205 OF MM. (X)Dec 12, 2000 · N773TP · Beech B200 · Electrical Power SystemSDR T58A20001127Fire Detector · malfunctionedRIGHT ENGINE FIRE LIGHT ILLUMINATED DURING INITIAL CLIMB-OUT. RIGHT ENGINE WAS SECURED, AND THE FIRE LIGHT REMAINED ILLUMINATED. RIGHT ENGINE FIRE EXTINGUISHER WAS THEN DISCHARGED AND ABOUT 2 MINUTES LATER THE FIRE LIGHT EXTINGUISHED. UPON LANDING, ENGINE WNov 28, 2000 · N1PD · Beech B200 · Fire DetectionSDR CA001205023Skin · cracked(CAN) CRACKED SPAR PART NR 35-165050-229. (X)Nov 20, 2000 · Beech B200 · Trailing Edge FlapsSDR 20001108SH036Actuator · failedAFTT 6,692.3 HOURS. TC 6,876. THE PILOT RETRACTED THE LANDING GEAR AFTER TAKEOFF. SEVERAL MINUTES LATER, A LOUD BANG OCCURRED AND THE PILOT NOTED THE GREEN LEFT MAIN GEAR DOWNLOCK AND THE RED INTRANSIT LIGHT HAD ILLUMINATED. THE PILOT CYCLED THE LANDING Oct 24, 2000 · N75ZT · Beech B200 · Landing Gear ActuatorSDR CA001212019Harness · broken(CAN) WHEN GEAR SELECTED DOWN - R/H GEAR DID NOT INDICATE DOWN AND LOCKED.MAINTENANCE FOUND BROKEN WIRE IN HARNESS OF DOWN LOCK SWITCH.Oct 4, 2000 · Beech B200 · Landing Gear Position and WarningSDR 20001011SH004Actuator · shearedUNSAFE GEAR INDICATION. INSPECTION REVEALED LT MAIN GEAR ACTUATOR JACKSCREW FAILURE INVOLVING SEPARATION OF SPLINES INTERNALLY. FAILURE REPORTED TO FSDO-13 OF COLUMBIA, SC. FAA INSPECTOR PRESENT DURING ARRIVAL AND LANDING. AIRCRAFT LANDED WITHOUT INCIDENTOct 4, 2000 · N27LJ · Beech B200 · Landing Gear ActuatorSDR 20001024SH006Gasket · splitGASKET SPLITTING AND FUEL LEAKING FROM NACELLE AND AUXILIARY TANKS INTO ENGINE EXHAUST PATH. AIRCRAFT N NR YV-988CP. (X)Sep 20, 2000 · Beech B200 · Fuel StorageSDR 20001024SH005Gasket · splitGASKET SPLITTING AND FUEL LEAKING FROM NACELLE AND AUXILIARY TANKS INTO ENGINE EXHAUST PATH. AIRCRAFT N NR YV0988CP. (X)Sep 20, 2000 · Beech B200 · Fuel StorageSDR CA001030002Compressor · failed(CAN) SHORTLY AFTER TAKEOFF, THE CABIN FILLED WITH FUMES AND LIGHT SMOKE. THE AIRCRAFT RETURNED TO THE POINT OF DEPARTURE. ENGINE WAS SPLIT AT THE C-FLANGE. NO OBVIOUS DAMAGE OR ABNORMALITIES WERE FOUND. A NEW NR 2 BEARING COVER AND GASKET WERE INSTALLED.Sep 19, 2000 · Beech B200 · Turbine Engine Compressor SectionSDR 20001025SH019Gasket · splitGASKET SPLITTING AND FUEL LEAKING FROM NACELLE AND AUXILIARY TANKS INTO ENGINE EXHAUST PATH. (X)Sep 9, 2000 · N523GM · Beech B200 · Fuel Storage
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