Beech B200

Service difficulty reports · 830

Newest first. General aviation reporting is voluntary.

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 GNL2007F00000Connector · corrodedAC WAS FLYING THROUGH IMC WEATHER, WITH A LARGE ACCUMULATION OF MOISTURE, WHEN THE PILOT NOTICED A LT ENGINE FIRE LIGHT. ALL THE OTHER SYSTEMS WERE MONITORED AND THE ENGINE FIRE LIGHT WAS DETERMINED TO BE FALSE. THE AC WAS LANDED WITHOUT EVENT. UPON INSPECTApr 1, 2007 · N200VU · Beech B200 · Fire Protection System WiringSDR CA070329008Torque Knee · worn(CAN) WHILE TAXING BACK TO THE RAMP, THE PILOT NOTICED THAT THE STEERING WAS MORE DIFFICULT AND INEFFECTIVE. HE SHUTDOWN BOTH ENGINES AND ON INVESTIGATION FOUND THE LT LANDING GEAR TORQUE KNEE BOLT DISCONNECTED. THE CAUSE OF THE DISCONNECTION WAS A WORN OUT REMar 27, 2007 · Beech B200 · Landing Gear Steering SystemSDR CA070514030Line · fractured(CAN) A FUEL LEAK WAS NOTED DURING GROUND OPERATIONS. SUBSEQUENT INSPECTION REVEALED A FRACTURE FUEL LINE AT THE FUEL CONTROL. (TC NR 20070514030)Mar 22, 2007 · Beech B200 · Engine Fuel DistributionSDR 2007F00025Engine · making metalSHORTLY AFTER TAKEOFF CLIMBING THROUH 6,000 FEET, THE LT CHIP DETECTOR LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DEPARTURE WITHOUT INCIDENT. NO OTHER ABNORMAL ENGINE PARAMETERS WERE NOTED. INVESTIGATION FOUND FERROUS METAL ON THE CHIP DETECTOR AND METAL PMar 22, 2007 · N209CM · Beech B200 · Turbine Engine Oil SystemSDR CA070316003Tach Generator · failed(CAN) N1 TACH GENERATOR FAILED IN FLIGHT. (TC NR 20070316003)Mar 13, 2007 · Beech B200 · Engine RPM Indicating SystemSDR CA070802003Hinge · cracked(CAN) ON INSPECTION THE LT DOOR WAS FOUND CRACKED ALONG THE FRONT HINGE. (TC NR 20070802003)Mar 12, 2007 · Beech B200 · Fuselage, Door HingeSDR 2007FA0000470Evaporator · unserviceableAFT CABIN AIR CONDITIONER EVAPORATOR RECEIVED FROM VENDER IN OVERHAULED CONDITION. INITIAL INSPECTION REVEALED HARD LINE. WHICH SHOULD RUN PARALLEL TO HEAT EXCHANGER, WAS INSTALLED APPROXIMATELY 25 DEGREES TO HEAT EXCHANGER. THE EVAPORATOR COULD NOT HAVE BEFeb 26, 2007 · Beech B200 · Humidity Control SystemSDR CA070226010Connector · loose(CAN) CREW REPORTED THAT THE GEAR INDICATION WOULD NOT INDICATE DOWN AND LOCKED ON APPROACH. MAINTENANCE PERSONNEL LATER CARRIED OUT AIRCRAFT LANDING GEAR SWINGS AND FOUND RT SQUAT SWITCH CONNECTOR PLUG LOOSE ON BULKHEAD. CLEANED, SECURED AND GEAR SWINGS FUNFeb 25, 2007 · Beech B200 · Landing Gear System WiringSDR CA070326003Frame · cracked(CAN) FRAME SEGMENT P/N 115-43008-35 CRACKED AT OB ENDS. AIRCRAFT IS AN EMS MACHINE. DEFECT APPEARS TO BE RELATED TO HIGH FLOOR LOADING. (TC NR 20070326003)Feb 14, 2007 · Beech B200 · Fuselage Main, FrameSDR CA070207007Light · inoperative(CAN) WHILE ON FINAL APPROACH, SMOKE WAS OBSERVED IN COCKPIT COMING FROM THE LOWER LT C/B PANEL. SIDE LIGHT C/B POPPED AND SMOKE STOPPED. LANDING COMPLETED WITHOUT FURTHER INCIDENT. MAINTENANCE WAS CONTACTED AND IN CONVERSATION WITH FLIGHT CREW SMOKE PROBLEM Feb 6, 2007 · Beech B200 · Flight Compartment LightingSDR 2007FA0000086Downlock Switch · failedNOSE LANDING GEAR DID NOT HAVE A DOWN AND LOCKED INDICATION GEAR WARNING SYSTEMS ACTIVATED (LIGHT IN SELECTOR HANDLE AND GEAR HORN). AN UNEVENTFUL LANDING HAS MADE VISUAL CHECK OF NOSE GEAR SHOWED TO BE IN THE DOWN AND LOCKED POSITION. SWITCH REMOVED AND REPLAJan 26, 2007 · N200EW · Beech B200 · Landing Gear Position and WarningSDR CA070201007Tire · scored(CAN) DURING MAINT WALK AROUND INSP, IT WAS NOTED THAT ALL (4) MLG LOCATIONS RECEIVED SIDE WALL DAMAGE ON FIRST 20 HRS OF FLIGHT ON A FACTORY NEW AC DUE TO INTERFERENCE FIT. AC HAS (2) STC’S INCLUDED IN THE MLG. THEY ARE AS FOLLOWS: AC EQUIPPED WITH (P/N:02Jan 23, 2007 · Beech B200 · TireSDR CA070209011Line · fractured(CAN) ON INSPECTION FOLLOWING A REPORT OF FUEL ODOR IN THE CABIN, THE ENGINE HIGH PRESSURE FUEL DELIVERY TUBE WAS FOUND CRACKED. (TC NR 20070209011)Jan 18, 2007 · Beech B200 · Engine Fuel DistributionSDR CA070122010Control Panel · shorted(CAN) CREW REPORTED COCKPIT OVERHEAD PANEL LIGHTS CIRCUIT BREAKER POPPED AND ABOUT THE SAME TIME REPORTED SMELLING SMOKE. PCB PANEL REMOVED AND FOUND TO OF SHORTED OUT CAUSING SMALL BURN HOLE THROUGH PANEL SCORCHING METAL BEHIND PANEL. CAUSE OF SHORT BELIVED TJan 6, 2007 · Beech B200 · Electrical Power System WiringSDR CA070114003Indicator · malfunctioned(CAN) CREW REPORTS THAT IN CRUISE NOTED THE WEATHER RADAR FAILED AND IMMEDIATELY BOTH MAIN GENERATOR BUSES FAILED. CREWS RESET GENERATORS AND MONITORED BUS VOLTAGES AND LOADS, NORMAL. CREW THEN NOTED THE 28VDC CIRCUIT BREAKER POPPED ON THE AVIONICS BUS FOR THEJan 4, 2007 · Beech B200 · Weather Radar SystemSDR 2007FA0000001Line · chafedDURING A SCHEDULED PHASE INSPECTION P/N 100-920041-15 ALUMINUM MAIN FUEL LINE WAS FOUND CHAFED IN THE LT MAIN LANDING GEAR WHEEL WELL WHERE IT ENTERS INTO THE BACK OF THE WING. THE EDGES OF THE HOLE THAT THE LINE PASSES THROUGH WAS PROTECTED WITH PLASTIC ANTI Jan 2, 2007 · N155AV · Beech B200 · Fuel StorageSDR CA061222007Seal · leaking(CAN) PILOT NOTICED OIL PRESSURE FLUCTUATIONS IN CRUISE FLIGHT. ENGINE LIMITS NOT EXCEEDED AND THE AIRCRAFT LANDED AT DESTINATION. ENGINE OIL WAS LOST THROUGH A LEAKING STARTER GENERATOR DRIVE GARLOC SEAL. SEAL REPLACED WITH NEW PN 3059046-01 IAW MFG CATEGORY Dec 20, 2006 · Beech B200 · Starter-GeneratorSDR BIOR061211001Fairing · corrodedDURING A PHASE 4 INSPECTION PAINT BLISTERS WERE NOTED ON THE LT AND RT WING ROOT FAIRING LOWER AFT PANELS P/N 101-420024-43 AND 101-420024-8. UPON FURTHER INSPECTION BOTH PANELS WERE FOUND TO BE CORRODED THRU IN SEVERAL PLACES FROM THE INSIDE OUT. AFTER REMOVDec 11, 2006 · N200MJ · Beech B200 · Aerodynamic FairingsSDR CA061128008Battery · thermal runaway(CAN) WHILE CONNECTED TO A GPU, DURING ROUTINE MAINTENANCE, THE TECHNICIANS NOTED SMOKE IN THE AREA OF THE BATTERY BOX COMPARTMENT. THE GPU WAS IMMEDIATELY DISCONNECTED, BATTERY POWER TURNED OFF AND THE BATTERY DISCONNECTED FROM THE AIRCRAFT BY REMOVAL OF THE Nov 20, 2006 · Beech B200 · Battery/Charger SystemSDR DHL2006363550Support Fitting · wornLT WING ALL SPEED AILERON SUPPORT FITTINGS FOR ACTUATORS THE 3RD FROM INBD HAS THE SLIDING PLATE AND FITTING WITH A WORN OUT GROOVE AT OUTBD SIDE MADE BY ACTUATOR GUIDE PLATE. PERFORMED MAJOR REPAIR OF L/W ALLSPEED AILERON B3/327 AS PER SKETCH NR 14001-003 RENov 14, 2006 · N363D · Beech B200 · AileronsSDR 2006FA0001071Web · crackedDURING PHASE 1 THROUGH 4 INSPECTION, AFTER REMOVING MOVING ALL WING INSPECTION PANELS. 4 (EA) CRACKS NOTICED IN WEB FLANGE COMMON TO AND EMITTING FROM RIVETS ON LT IB WING BOX AREA, BL-65.50, (2EA) CRACKS AT WS 65, (1EA) CRACK AT WS 56. (K)Oct 28, 2006 · N828FM · Beech B200 · Wing Miscellaneous StructureSDR 2006F00051Windscreen · failedON A LEG, AT CRUISE ALTITUDE OF FL250, THE INNER PANE OF THE RT WINDSCREEN SHATTERED, THE CREW THEN LANDED AT THE NEAREST SUITABLE AIRPORT (ERI), WITHOUT FURTHER INCEDENT. THE AIRCRAFT WAS FERRIED BACK TO DEPARTURE WERE THE WINDSCREEN WAS REPLACED WITH P/N 101Oct 21, 2006 · N942CE · Beech B200 · Flight Compartment WindowsSDR 2006F00050Windscreen · failedON A LEG, ENROUTE, AT CRUISE ALTITUDE OF FL250, THE INNER PANE OF THE RT WINDSCREEN SHATTERED, THE CREW THEN LANDED AT THE NEAREST SUITABLE AIRPORT (ERI), WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRIED BACK, WHERE THE WINDSCREEN WAS REPLACED WITH P/N 101-3Oct 21, 2006 · N942CE · Beech B200 · Flight Compartment WindowsSDR 2006F00040Engine · fireENGINE SURGE WITH FLAMES OUT OF THE EXHAUST DURING FINAL APPROACH TO LAND.Sep 18, 2006 · N200EW · Beech B200 · Engine (Turbine/Turboprop)SDR 2007FA0000993Relay · intermittentDURING FLIGHT WHEN THE FLAPS SELECTED DOWN & DID NOT RESPOND. AIRCRAFT LANDED IN A FLAPS UP CONDITION & DELIVERED TO MAINTENANCE. INVESTIGATION REVEALED THE FLAP MOTOR POWER RELAY WAS OPERATING INTERMITTENTLY. A NEW FLAP MOTOR RELAY, PROCURED FROM RAPID (RAYAug 28, 2006 · N185XP · Beech B200 · Trailing Edge Flap Control SystemSDR CA060906017Engine · malfunctioned(CAN) ENGINE TORQUE WAS SEEN TO FLUCTUATE ON APPROACH AND THE ENGINE WOULD NOT RESPOND TO THROTTLE INPUT. THE ENGINE WAS SHUTDOWN IN FLIGHT. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20060906017)Aug 18, 2006 · Beech B200 · Engine BMEP/Torque IndicatingSDR 080106Tube · damagedDURING ROUTINE INSPECTION IT WAS DISCOVERED THAT THE PILOT SIDE RUDDER CABLE HAD BEEN RUBBING ON THE PILOTS SIDE RT BRAKE TUBE ASSY P/N 101-580218-1 NEAR THE FORWARD END OF THE TUBE ASSY CAUSING IT TO BECOME NOTCHED. THE DAMAGE IS TO THE EXTENT THAT REPLACEMEAug 1, 2006 · N6300F · Beech B200 · Hydraulic System, MainSDR CA060531013Engine · surges(CAN) DURING CRUISE THE ENGINE WAS REPORTED TO SURGE AND SUBSEQUENTLY FLAME OUT. MFG WILL INVESTIGATE THE EVENT AND WILL ADVISEOF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20060531013)Apr 27, 2006 · Beech B200 · Engine (Turbine/Turboprop)SDR XOR2006F00000Bracket · crackedCRACK AT AIR COMPRESSOR BRACKET DURING ROUTINE POSTFLIGHT INSPECTION. BELT TENSION AND ALIGNMENT WAS INSPECTED AT THE LAST PHASE INSPECTION PERFORMED AT 299.7 HRS. AIRCRAFT TT 3064.5, LANDINGS 3146. UNIT LOCATION IS OB OF RT POWERPLANT NACELLE. SUGGEST ADDApr 25, 2006 · N200EG · Beech B200 · Cabin Cooling SystemSDR CA060422009Lock Nut · missingDURING L/G EXT IN FLT, LT MAIN AND NOSE GEAR DOWN AND LOCKED IND PRESENT, WITH NO RT IND AND LOUD BANGING SOUND FROM RT SIDE OF A/C. C/O FLY-BY TO VISUALLY VERIFY ALL THREE LANDING GEARS WERE DOWN. A/C LANDED SAFELY, VERIFIED ALL 3 L/G WERE DOWN AND LOCKED BApr 21, 2006 · Beech B200 · Landing Gear ActuatorSDR CA060419007Bolt · failedWHILE CLIMBING THROUGH 10000 FT, A LOUD BANG WAS HEARD FOLLOWED BY A CONSTANT HISSING SOUND. THE FLIGHT RETURNED UNEVENTFULLY AND MAINT FOUND THE UPPER FWD DRAW BOLT ROLLER HAD FAILED CAUSING THAT PORTION OF THE DOOR TO SHIFT SLIGHTLY. BOTH UPPER DRAW BOLT RApr 12, 2006 · Beech B200 · Passenger/Crew DoorsSDR CA060410004Pump · unserviceableON TAKEOFF, THE CREWS ROTATED AND HAD RT ENGINE POWER ROLL BACK. CREWS FEATHERED AND SHUT DOWN THE ENGINE AND TURNED AROUND AND LANDED. MAINTENANCE FOUND FUEL LEAKING FROM RT ENGINE DRIVEN HIGH PRESSURE FUEL PUMP P/N 025323-300-03. PUMP ASSY REPLACED AND GRApr 9, 2006 · Beech B200 · Engine Fuel PumpSDR XRR2006F00000Windshield · crackedINSIDE LAYER OF PILOTS WINDSHIELD CRACKED WHILE IN CRUISE AT 28,000 FT. AC LANDED AT CDU UNEVENTFULLY. FERRIED AC BACK TO DVN IAW AIRWORTHINESS MANUAL. TALKED TO TECH REP AT MFG TOLD ME THAT PPG HAD PROBLEMS WITH THIS SERIES OF WINDSHIELD MFG AROUND 1999-20Mar 29, 2006 · N764CA · Beech B200 · Flight Compartment WindowsSDR CA060329001Motor · failedAFTER TAKEOFF, EN ROUTE TO DESTINATION, GEAR WARNING LIGHT CAME ON. PILOT TRIED EXTENDING THE GEAR AND NO EXTENSION WAS NOTED. AIRCRAFT RETURNED TO BASE AND GEAR WAS EXTENDED USING MANUAL EXTENSION. AIRCRAFT PUT ON LOCKS. GEAR MOTOR CIRCUIT BREAKER WAS FOUMar 21, 2006 · Beech B200 · Landing Gear Retraction/Extension SystemSDR CA060403015Fuel Sys · fluctuatesDURING INITIAL DESCENT, ENGINE FUEL FLOW WAS OBSERVED TO FLUCTUATE. THROTTLE INPUT RESULTED IN EXCESSIVE INTERTURBINE TEMPERATURE INCREASE AND THE ENGINE WAS SHUT DOWN IN FLIGHT. P&WC WILL MONITOR INVESTIGATION OF THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCEMar 16, 2006 · Beech B200 · Fuel Controlling SystemSDR 2006FA0000356Duct · crackedLT ENGINE LOWER AFT COWLING, LWR DUCT FOUND CRACKED ABOUT 80 PERCENT ITS ENTIRE WIDTH ALONG FIRST RIVET ROW. REMOVED CRACKED DUCT AND FOUND NOT TO BE ROLLED ENOUGH. THIS PUT STRESS ON RIVET ROW. NEW SPARE PART ORDER FROM MFG WAS ROLLED CORRECTLY AND FIT WITMar 13, 2006 · N326PG · Beech B200 · Powerplant SystemSDR CA060317010Actuator · seizedNOSE LANDING GEAR ACTUATOR SEIZED AND OVER-LOADED MLG MOTOR BREAKER.Mar 11, 2006 · Beech B200 · Landing Gear ActuatorSDR BB461001Windshield · crackedCOPILOT WINDSHIELD BROKEN IN FLIGHT, INNER PANE SHATTERED, NO LOOSE PIECES. REASON FOR BREAK UNKNOWN. CRUISE FLIGHT AT FL 230, NO ICE OR CLOUDS. DEFROSTER HEAT ON, NO ELECTRIC HEAT.EMERGENCY DECLARED, LANDED AT DESTINATION.Feb 26, 2006 · N227RS · Beech B200 · Flight Compartment WindowsSDR 4381002Gcu · malfunctionedAIRCRAFT CAME IN FOR GENERATOR PARALLELING. LEFT GENERATOR CONTROL UNIT NEEDED REPLACEMENT. INSTALLED OVERHAULED GCU S/N 10853A; GCU FAILED ON INITIAL RESET. INSTALLED SECOND GCU S/N 9183; GCU FAILED ON INITIAL RESET. BOTH ABOVE GCU'S HAD JUST BEEN OVERHAUFeb 7, 2006 · N1509G · Beech B200 · AC Generation SystemSDR CA060130005Hinge · failedCABIN DOOR SIDE OF HINGE WAS REPLACED ON MARCH 15 2005 AT 5248.4 TTAF AND 4829 CYCLES. DOOR SIDE OF HINGE FAILED JAN 23 2006 AT 5846.8 TTAF AND 5480 CYCLES DOOR AND HINGE AREA WAS INSPECTED AND NO ADDITIONAL DAMAGE WAS NOTED CHERRYMAX RIVETS WHICH WERE INSTALJan 24, 2006 · Beech B200 · Fuselage, Door HingeSDR CA060405008Seal · failedAIRCRAFT DEPARTED AND ON CLIMB THE PILOT REPORTED A LOW OIL PRESSURE INDICATION ON THE LEFT HAND ENGINE. THE AIRCRAFT RETURNED TO BASE. A TECHNICIAN WAS CALLED IN, AND FOUND THAT THE FCU/FUEL PUMP DRIVE SEAL HAD MIGRATED, AND WAS LEAKING. A NEW SEAL P/N:302Jan 19, 2006 · Beech B200 · Engine Fuel PumpSDR 2005FA0001644Support · misinstalledOPERATOR NOTED (2) NON-STANDARD RIVETS INSTALLED ATTACHING THE PN 101-524017-4 RT RUDDER MECHANISM SUPPORT BRACKET ANGLE TO THE FS 437.234 CANTED BULKHEAD. DURING RIVET REPLACEMENT FOUND THAT IB RIVET HAD FORMED A SHOP HEAD BETWEEN THE BULKHEAD AND SUPPORT ANDec 7, 2005 · N912JS · Beech B200 · Rudder Control SystemSDR DJFA2005171Windshield · crackedTRIP ID NR 934736 WINDSHIELD HEAT WAS TURNED ON AT 10,000 FT WITH AN OUTSIDE AIR TEMPERATURE OF + 2 DEGREES CELSIUS. AFTER REACHING CRUISE ALTITUDE OF FL 250 THE PILOTS SIDE WINDSHIELD SHATTERED. THE CREW DONNED THEIR OXYGEN MASKS AND DECLARED AN EMERGENCY.Dec 7, 2005 · N616TA · Beech B200 · Flight Compartment WindowsSDR CA051206010Downlock Switch · failedON APPROACH, CREW DID NOT GET A NOSE GEAR DOWN INDICATION ON SELECTION. EMERG PROCEDURES COMPLETED WITH NO INDICATION. FLY BY VISUAL SHOWED NOSE GEAR DOWN, INDICATION ILLUMINATED ON TOUCH DOWN. MAINTENANCE FOUND NOSE GEAR ACTUATOR INTERNAL DOWN LOCK SWITCH Dec 1, 2005 · Beech B200 · Landing Gear Position and WarningSDR 2005FA0001621Control Cable · out of rigDURING INSPECTION OF FLIGHT CONTROL SYSTEM, DURING INITIAL 200 HOUR PHASE 1 INSPECTION, IAW SAFETY COMMUNIQUE NR 265, FOUND RUDDER CABLE TENSIONS, RUDDER TAB CABLE TENSIONS, AND ELEVATOR TAB CABLE TENSIONS BELOW APPLICABLE MM SERVICE LIMITS. NO OTHER FAULTS NDec 1, 2005 · N351CB · Beech B200 · Flight Control SystemSDR 2005FA0001590Windshield · crackedAT 27,000 FT THE PILOT SIDE WINDSHIELD SHATTERED. THE PILOTS VIEW WAS TOTALLY OBSTRUCTED. THE COPILOT WAS ABLE TO LAND THE AIRCRAFT SAFELY. AFTER REMOVAL, THE OUTSIDE PANEL WAS NOT DAMAGED. THE INSIDE PANEL WAS STILL IN TACT BUT COMPLETELY SHATTERED. THE Nov 22, 2005 · N946CE · Beech B200 · Flight Compartment WindowsSDR CA051116003Boot · tornIN CRUISE FLIGHT, A THUMPING NOISE WAS DETECTED ON THE RIGHT SIDE OF AIRCRAFT. AFTER LANDING IT WAS FOUND THAT A NEWLY INSTALLED RIGHT INBOARD WING BOOT LOWER HALF HAD TORE LOOSE FROM THE GLUE, AND WAS TRAILING BEHIND THE AIRCRAFT ABOUT 8 FEET HITTING THE LOWNov 13, 2005 · Beech B200 · Airfoil Anti/De-ice SystemSDR 2006RC02001Bulkhead · cracked(CAN) PRESSURIZATION ERRATIC IN THE AIR. THE AIRCRAFT WAS TESTED ON THE GROUND AND LEAK WAS DETECTED WITH A 6 INCH CRACK LT OF THE OUTFLOW VALVE. A REPAIR DESIGN WAS CARRIED OUT.Oct 12, 2005 · Beech B200 · Fuselage Main, BulkheadSDR 2005FA0001426Hinge · corrodedDURING SCHEDULED PHASE 2 INSPECTION OF AIRCRAFT, FOUND THE CENTER RUDDER HINGE ASSY HAVING INTERGRANULAR CORROSION AROUND THE HARDWARE ATTACHING TEE TO THE HINGE ASSY. THIS TYPE OF CORROSION IS PROBABLY DUE TO THE LOCATION OF THE PART AND THE AGE OF THE AIRCROct 12, 2005 · N585CE · Beech B200 · Rudder Miscellaneous StructureSDR CA051103004Web · cracked(CAN) WEB CRACKED HORIZONTALLY APPROX. 10 INCHES. CRACK COINCIDES WITH FLANGE OF UNDERLYING Z CHANNEL. PROBLEM APPEARS TO BE RELATED TO POOR MANUFACTURING PRACTICES. PRC SEALANT BEAD APPLIED TO Z CHANNEL FLANGE CURED BEFORE RIVETING. THE RESULT WAS THAT THE SOct 11, 2005 · Beech B200 · Fuselage Miscellaneous Structure
Back to Beech B200