Beech A200

Service difficulty reports · 52

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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 = 'A200'
  ORDER BY difficulty_date DESC"

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SDR 2025FA0000454Arm · brokenAIRCRAFT BEING OPERATED BY TWO PILOT CREW. SIC WAS BACK TAXIING ON RUNWAY IN PREP FOR TAKEOFF. SIC MANEUVERED FOR A RIGHT 180 ON THE RUNWAY AND MADE THE RIGHT TURN. ABOUT HALF WAY THROUGH THE 180, CREW HEARD AND FELT A LOUD THUMP COMING FROM THE FLOOR. AFTER TJun 20, 2025 · N42J · Beech A200 · Landing Gear Steering SystemSDR 2018FA0000003Bracket · crackedON 26 JAN 2017 BRACKET P/N 100-820018-7 WERE FOUND CRACKED ON THE NOSE LANDING GEAR DRAG BRACE P/N 50-820205-25.Jan 26, 2017 · Beech A200 · Nose/Tail Landing Gear Strut/AxleSDR K5L2014F00001Indicator · failedDURING CLIMB THROUGH 4000 FT, THE CAPTAIN SIDE ATTITUDE INDICATOR FLAGGED "GYRO", THEN STARTED INDICATING A BANK TO THE LEFT. CAPTAIN CALLED THE FAILURE AND POSITIVE EXCHANGE OF CONTROLS OCCURRED BETWEEN PILOT AND CO PILOT. CO PILOTFLEW THE RETURN , INTERCEPOct 1, 2014 · N636B · Beech A200 · Altimeter, Barometric/EncoderSDR K5L20140110000001Flap Track · tornAIRCRAFT WAS CLEARED TO LAND AND ON A CLOSE LT DOWNWIND, CIRCLING AT 140 KNOTS FROM A GPS13 APPROACH, CONFIGURED WITH FLAPS SET AT APPROACH AND GEAR SELECTED DOWN. CAPTAIN`S COMMANDED FULL FLAPS. WHEN THEY WERE SELECTED THE FLAPS EXTENDED ONLY TO APPROXIMATEDec 12, 2013 · N636B · Beech A200 · Trailing Edge FlapsSDR 4DSR20130425001Starter Gen · inoperativeDURING A POST-MX CHECK FLIGHT FOR REMOVAL AND REINSTALLATION OF THE FUEL CONTROL AND STARTER/GENERATOR THE GOVERNMENT FLIGHT CREW PERFORMED AN INFLIGHT SHUTDOWN OF THE NR2 ENGINE. DURING THE ATTEMPTED ENGINE RESTART THE STARTER/GENERATOR WOULD NOT CRANK TO ASApr 3, 2013 · N1559 · Beech A200 · Starter-GeneratorSDR K5L2012F00002Fire Detector · failedON SHORT FINAL APPROACH THE LEFT ENGINE FIRE DETECTOR T-HANDLE LIGHT ILLUMINATED. PILOT MADE A NORMAL LANDING AND NO SMOKE WAS NOTICED. PULLED AND RESET CIRCUIT BREAKER AND LIGHT EXTINGUISHED. MADE NORMAL SHUTDOWN. MX OPENED COWLS AND NO SIGN OF ANY FIRE Jul 13, 2012 · N636B · Beech A200 · Fire DetectionSDR K5L2012F00001Fire Detector · failedON SHORT FINAL APPROACH, THE LT ENGINE FIRE DETECTOR T HANDLE LIGHT ILLUMINATED. PILOT MADE NORMAL LANDING AND NO SMOKE WAS NOTICED, PULLED AND RESET CIRCUIT BREAKER AND LIGHT EXTINGUISHED. MADE NORMAL SHUTDOWN. MX OPENED COWLS AND NO SIGN OF ANY FIRE WAS NJul 13, 2012 · N636B · Beech A200 · Fire DetectionSDR 2011FA0000787Pitot Tube · mismarkedDURING ALTIMETER AND PITOT STATIC SYSTEM RE-CERTIFICATION, THE TECH OBSERVED THAT THE LT PITOT TUBE WAS INCORRECT AND WAS ACTUALLY A RT PITOT TUBE. UPON FURTHER INVESTIGATION, THE PN WAS MIS-IDENTIFIED AS A LT PITOT TUBE PN PH502-3 WHEN ACTUALLY THE DRAIN HOLDec 9, 2011 · N72472 · Beech A200 · Pitot/Static SystemSDR 2011FA0000723Spar · crackedINSPECTION OF FLEET ACFT SN IN THE BC AND BD RANGE HAVE REVEALED CRACKING OF THE MAIN WING SPAR WEB IN CARRY THROUGH OPENINGS AND END CAP SUPPORTS. IN THE WHEEL WELL AREA, THERE ARE 2 OPENINGS IN THE WING SPAR WEB FOR FUEL AND HYD LINE PASSAGE. ONE OPENING IS Nov 2, 2011 · Beech A200 · Wing SparSDR 2009FA0000755Relief Valve · looseDURING SCHEDULED PHASE INSP, FOUND RELIEF VALVE BACKED OUT OF FUEL FILTER PN 50-389110. THIS FIREWALL-MOUNTED FILTER HAS A BALL-AND-SPRING TYPE RELIEF VALVE THREADED INTO THE FILTER HSG (PN 02W760-140). THE MECHANIC FOUND THE VALVE SEAT AND BALL COMPLETELY BAug 31, 2009 · N49R · Beech A200 · Aircraft Fuel Distribution SystemSDR 2009FA0000292Flow Valve · failedDURING CLIMB TO ALTITUDE CABIN FAILED TO MAKE MAXIMUM DIFFERENTIAL PRESSURE AND HAD A HIGHER THAN NORMAL CABIN. FOUND A P3 AIR TUBE DISSCONNECTED AT RT HEAT EXCHANGER IN RT WING. ON MX FLIGHT FOUND LT FLOW CONTROL VALVE WEAK. REPLACED DUCT AND FLOW CONTROL VALApr 3, 2009 · N636B · Beech A200 · Cabin Pressure Control SystemSDR 2009FA0000269Bolt · failedWHILE REPLACING THE RT WING FWD WING BOLT AND BARREL NUT, HEARD A POP WHILE TIGHTENING THE NEW BOLT BEFORE REACHING FINAL TORQUE. REMOVED NEW BOLT/BARREL NUT AND FOUND THE THREADS DAMAGED AND PULLED-OUT OF BARREL NUT. THE BOLT WAS ALSO DAMAGED BUT APPEARED TO Apr 1, 2009 · N7074G · Beech A200 · Wing, Attach FittingsSDR K5LA050908001Bellcrank · twistedDRUING A ROUTINE PHASE 3 INSPECTION, IT WAS FOUND THAT THE MAIN CABIN DOOR AFT UPLOCK BELLCRANK WAS TWISTED ABOUT 10 DEGREES FROM WHAT A NEW ONE IS.. ALSO THE BOLT PN NAS110321D THAT THE UPLOCK BRACKET PIVOTS ON WAS DEFORMED SLIGHTLY. THIS WAS PROBABLY CAUSED May 5, 2008 · N636B · Beech A200 · Passenger/Crew DoorsSDR K5L2007F00002Power Supply · failedAWAITING TAKEOFF, PILOT TURNED ON CABIN LIGHTS AND NOTICED SMOKE FUMES IN COCKPIT AND CABIN. TURNED OFF VENT BLOWED AND CABIN LIGHTS AND RETURNED TO RAMP. IT WAS DETERMINED THAT THE POWER SUPPLY (BALLAST) HAD FAILED AND CAUSED THE SMOKE. POWER SUPPLY WAS RENov 25, 2007 · N636B · Beech A200 · Passenger Compartment LightingSDR K5L2007F00001Actuator · inoperativeDESCENDING, PILOT SELECTED ICE VANES EXTENDED AND ONLY THE LT ONE EXTENDED. PULLED CIRCUIT BREAKER AND SLOWED AIRCRAFT AND EXTENDED RT ICE VANE WITH THE MANUAL EXTENSION HANDLE. REPLACED RT ICE VANE ACTUATOR MOTOR. (K)Nov 25, 2007 · N636B · Beech A200 · Airfoil Anti/De-ice SystemSDR 2007FA0000995Relay · meltedRT STARTER GENERATOR RELAY P/N: 6041H190 MELTED AT BUSS BAR CONNECTION.Nov 7, 2007 · Beech A200 · AC Generation SystemSDR 2007FA0000785Sensor · faultyAT APPROXIMATELY 1635 LOCAL, IN CLOUDY CONDITIONS, ON A MAINTENANCE TEST FLIGHT, THE NR 1 ENGINE FIRE LIGHT BRIEFLY ILLUMINATED, THEN EXTINGUISHED. ALL ENGINE GAUGES INDICATED NORMALLY. ALREADY IN DESCENT, THROUGH 4,500 FT, AND CONTINUED TO A SAFE LANDING. Aug 7, 2007 · N636B · Beech A200 · Fire DetectionSDR K5L2007F00000Windshield · failedWHEN IN CRUISE FLIGHT AT FL210 AND -42 DEGREES C, THE INNER PANE ON THE CO-PILOTS WINDSHIELD SHATTERED. NO PIECES BROKE LOOSE AND NORMAL DESCENT AND SAFE LANDING WERE MADE AT KLEB. THERE WAS NO LOSS OF CABIN PRESSURE. LAST INSPECTION WAS 3 MONTH AND 100 HOUMar 6, 2007 · N636B · Beech A200 · Flight Compartment WindowsSDR 15462006H1Relay · burnedNR 2 START RELAY SHORTED TO GROUND DURING ENGINE START, APPARENTLY DUE TO WATER INCURSION OR CONTACT CORROSION. RELAY BURNED BUT START WAS SECURED BEFORE ADJACENT WIRE BUNDLE WAS DAMAGED. RELAY REPLACED. NEW RELAYS APPEAR TO HAVE ADDITIONAL SEALANT TO PREVENT Jul 10, 2006 · N1546 · Beech A200 · Engine CrankingSDR K5L2005F00002Shutoff Valve · failedAFTER NORMAL ENGINE START, DURING RUN UP NOTICED THAT THE LEFT INSTRUMENT SHUTOFF VALVE PN 101381000-9 WOULD NOT CLOSE WHEN SELECTED OFF. FOUND VALVE SOLENOID TO BE AT FAULT AND INSTALLED OVERHAULED VALVE. RUN UP AND OPS CHECKED NORMAL. (K)Nov 11, 2005 · N636B · Beech A200 · Vacuum Distribution SystemSDR K5L2005F00001Fuse · failedSELECTED APPROACH FLAPS DESCENDING, FLAPS FAILED TO EXTEND. RESET CIRCUIT BREAKER AND CYCLED FLAP SELECTOR BUT STILL NO FLAP MOVEMENT. MADE UNEVENTFUL NO FLAP LANDING. AFTER LANDING, FLAPS WORKED FINE A COUPLE OF TIMES, UP AND DOWN. TROUBLESHOT AND FOUND LJan 3, 2005 · N636B · Beech A200 · Trailing Edge Flap Control SystemSDR K5L2005F00000Uplock Switch · failedON TAKEOFF, RETRACTED GEAR AND IN TURBULENCE, GEAR HANDLE LIGHTS FLICKERED ON AND OFF. PULLED BACK ON YOKE AND LIGHTS STAY ON, PUSH FWD AND LIGHTS GO OFF. REMOVED GEAR UP LIMIT SWITCH AND FOUND IT WAS GOING OFF BEHIND AUDIAL CLICK OFF SWITCH. REPLACED SWITCDec 27, 2004 · N636B · Beech A200 · Landing Gear Position and WarningSDR B3OR20041029Attach Fitting · damagedON 22 SEPTEMBER 2004 A 5 YEAR WING BOLT INSPECTION WAS COMPLIED WITH ON A BEECHCRAFT A200 AIRCRAFT. THREE OF THE WING ATTACH FITTINGS WERE FOUND TO HAVE DAMAGE TO THE FLAT FACE PORTION OF THE FITTINGS, THE AREA WHERE THE WASHER RESTS ON THE FITTING. THE DAMAGESep 22, 2004 · N7247Y · Beech A200 · Wing, Attach FittingsSDR WK1Motor · failedSHORTLY AFTER TAKEOFF SMOKE WAS OBSERVED IN THE COCKPIT WITH ELECTRICAL ODOR. FORWARD CABIN VENT BLOWER WAS DISABLED AND THE SMOKE CLEARED. VENT BLOWER HAD FAILED INTERNALLY.May 13, 2004 · N639B · Beech A200 · Air Distribution FanSDR 2004FA0000402Actuator · separatedCREW RETRACTED FLAPS, FLAPS STOPPED .5000 WAY UP. SPLIT FLAP SAFETY CIRCUIT STOPPED FLAP RETRACTION. REVEALED THAT LT IB FLAP ACTUATOR HAD FAILED. 90 DEGREE DRIVE (P/N 50-380153-3) HAD COMPLETELY SEPARATED FROM MAIN BODY (SCREW DRIVE) OF ACTUATOR. FAILURE Mar 10, 2004 · N200ET · Beech A200 · Trailing Edge Flap ActuatorSDR K5LA620JSWindshield · crackedCLIMBING THROUGH 14000 FT IN THE CLOUDS WITH W/S HEAT ON, OAT-5C PILOTS WINDSHIELD OUTER PLY CRACKED ACROSS ENTIRE WINDSHIELD. RETURNED TO AIRPORT AND LANDED. REPLACED WINDSHIELD, NO OTHER DAMAGE NOTED.Jan 2, 2004 · N636B · Beech A200 · Flight Compartment WindowsSDR K5LA620JSafety Switch · brokenAFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT. GEAR REMAINED DOWN AND LOCKED. AFTER LANDING IT WAS DETERMINED A WIRE ON THE LANDING GEAR EMERGENCY SAFETY SWITCH HAD BEEN BROKEN OFF DURING INSPECTION AND LUBE OF NOSE GEAR CHAIN. JACKING THE AIRCRAFT AND DOINAug 5, 2003 · N636B · Beech A200 · Landing Gear Retraction/Extension SystemSDR B3OR20033014Flap Track · corrodedDURING A 14 DAY CORROSION INSPECTION THE LEFT OUTBOARD FLAP TACK WAS FOUND TO HAVE EXIFOLIATION FLAKING CORROSION ON THE FLAP TRACK. THE FLAKING WAS SEVERE ENOUGH TO CAUSE SEVERAL LAYERS OF FLAKING METAL TO BE PRESENT. THE PART WAS REMOVED AND A NEW FLAP TRACKAug 4, 2003 · N7247Y · Beech A200 · Trailing Edge FlapsSDR B3OR20033013Flap Track · corrodedDURING A 14 DAY CORROSION INSPECTION THE RIGHT HAND OUTBOARD FLAP TRACK WAS FOUND TO HAVE EXIFOLIATION FLAKING CORROSION ON THE FLAP TRACK. THE FLAKING WAS SEVERE ENOUGH TO CAUSE BUBBLING PAINT AND FLAKING METAL TO BE PRESENT. THE PART WAS REMOVED AND A NEW FLAug 4, 2003 · N7247Y · Beech A200 · Trailing Edge FlapsSDR B3OR20033012Flap Track · corrodedDURING A 14 DAY CORROSION INSPECTION THE RIGHT HAND INBORAD FLAP TRACK WAS FOUND TO HAVE DEEP EXIFOLLIATION FLAKING CORROSION ON THE INBOARD SIDE OF THE TRACK.THE FLAKING WAS SEVERE ENOUGH TO CAUSE SEVERAL LAYERS OF FLAKES TO BE PRESENT. THE PART WAS REMOVED AAug 4, 2003 · N7247Y · Beech A200 · Trailing Edge FlapsSDR B3OR2003009Hinge Bracket · corrodedMECH NOTICED (PAINT BUBBLING) ON, UPPER RUDDER HINGE BRACKET. ON INVESTIGATION, CORROSION WAS FOUND. FLAKING, CORROSION WAS TOO DEEP INTO METAL OF HINGE BRACKET. NEW HINGE BRACKET WAS ORDERED AND AFFECTED PART WAS REPLACED. WE HAVE FOUND IT DIFFICULT TO SPJun 5, 2003 · N7247Y · Beech A200 · Rudder StructureSDR B3OR2003008Hinge · corrodedDURING A 15 DAY CORROSION INSP, MECH NOTICED "PAINT BUBBLEING" ON MIDDLE RUDDER HINGE BRACKET. UPON INVESTIGATION, CORROSION FOUND. ATTEMPT WAS MADE TO CLEAN & TREAT AREA, BUT FOUND THAT MORE METAL WAS BEING REMOVED IN THE PROCESS. FLAKING, CORROSION WAS TOO DJun 5, 2003 · N7247Y · Beech A200 · Rudder StructureSDR B3OR2003007Hinge Bracket · corrodedDURING CORR INSP, MECH NOTICED "PAINT BUBBLING" ON LT, IB ELEV HINGE BRACKET. FURTHER INVESTIGATION BY SCRAPING-OFF PAINT BUBBLE, CORR WAS FOUND. ATTEMPT WAS MADE TO CLEAN AND TREAT AREA, BUT FOUND THAT MORE YOU CLEANED CORROSION, MORE METAL WAS BEING REMOVED Jun 5, 2003 · N72476 · Beech A200 · Elevator StructureSDR B3OR2003006Hinge Bracket · corrodedMECH NOTICED (PAINT BUBBLING) ON LT AND RT, MIDDLE ELEVATOR HINGE. FURTHER INVESTIGATION BY SCRAPEING-OFF PAINT BUBBLE, CORROSION WAS FOUND. ATTEMPT WAS MADE TO CLEAN AND TREAT AREA, FOUND THAT MORE YOU TRIED TO CLEAN CORROSION, MORE METAL WAS BEING REMOVED Jun 5, 2003 · N7247Y · Beech A200 · Elevator StructureSDR B3OR2003005Hinge Bracket · corrodedMECHANIC NOTICED (PAINT BUBBLING) ON LT OB ELEVATOR HINGE .UPON FURTHER INVESTIGATION BY SCRAPING-OFF THE PAINT BUBBLE, CORROSION WAS FOUND. AN ATTEMPT WAS MADE TO CLEAN AND TREAT AREA, BUT IT WAS FOUND THAT MORE YOU TRIED TO CLEAN CORROSION, MORE METAL WAS BEJun 5, 2003 · N72476 · Beech A200 · Elevator StructureSDR B30R20033011Hinge Bracket · damagedDURING A 14 DAY CORROSION INSPECTION, MECHANIC NOTED PAINT BLISTERING ON THE RIGHT INBOARD ELEVATOR HINGE BRACKET. REMOVAL OF THE PAINT BLISTERS FROM HINGE BRACKET REVEALED INTERGRANULAR CORROSION. THE HINGE BRACKET WAS REMOVED AND CORRODED AREA WAS CLEANED. AJun 4, 2003 · N7074G · Beech A200 · Elevator StructureSDR B30R20033010Hinge Fitting · corrodedDURING A 14 DAY CORROSION INSP, MECH NOTED PAINT BLISTERING AROUND RIGHT ELEVATOR HINGE FITTING MOUNTING HARDWARE. REMOVAL OF PAINT BLISTERS FROM HINGE FITTING REVEALED INTERGRANULAR CORROSION. HINGE FITTING WAS REMOVED AND CORRODED AREA WAS CLEANED. AT THIS TJun 4, 2003 · N7074G · Beech A200 · Elevator StructureSDR 2002FA0001175Rivet · missingELEVATOR TRIM TABS ON AIRCRAFT WERE INSPECTED FOR RIVETS. FOUND LT ELEVATOR TRIM TAB THAT WAS INSTALLED 10 HOURS PRIOR, TO BE MISSING ALL RIVETS. THE SKINS WERE BONDED BUT RIVETS WERE NEVER INSTALLED. THE TRIM TAB HAD BEEN SITTING ON OUR SHELF FOR 2 YEARS BAug 20, 2002 · N1554 · Beech A200 · FastenersSDR B3OR20020018Rivet · missingTRIM TAB WAS REPLACED DUE TO CORROSION, WHEN PART WAS INSTALLED IT WAS NOT NOTICED THAT THE RIVETS ALONG THE LEADING EDGE AND AROUND THE PITCH HORN WERE NOT INSTALLED.Aug 7, 2002 · N7074G · Beech A200 · Elevator Tab Control SystemSDR 2002FA0000450Hinge · corrodedTHE CENTER RUDDER HINGE ASSEMBLY WAS REMOVED FROM THE AIRCRAFT FOR REPLACEMENT DUE TO VISIBLE CORROSION NEAR THE EDGE OF THE LOWER RIGHT HAND BOLT HOLE ON THE TEE. WHEN THE TEE WAS DERIVETED FROM THE HINGE SUBSTANTIAL EXFOLIATION WAS FOUND ON THE TEE SURFACE WApr 5, 2002 · N1547 · Beech A200 · Rudder StructureSDR 2002FA0000166Drag Brace · crackedDURING SCHEDULED LANDING GEAR TIME CHANGE, THE DRAG BRACE SUPPORTS WERE CLEANED AND INSPECTED. THE RIGHT DRAG BRACE SUPPORT APPEARED TO BE CRACKED. A DYE-PENETRANT INSPECTION WAS CONDUCTED AND THE CRACKED CONFIRMED. AT THAT TIME AN ALERT WAS ISSUED TO TEST Jan 9, 2002 · N783MC · Beech A200 · Landing Gear Retraction/Extension SystemSDR 040521239ASupport · crackedLEFT HAND MAIN LANDING GEAR DRAG LEG SUPPORT FOUND TO BE CRACKED DURING FLUORESCENT PENETRANT INSPECTION. INSPECTION ORDERED BY U.S. CUSTOMS SERVICE BASED ON REPORTS BY U.S. ARMY OPERATORS.Dec 4, 2001 · N72470 · Beech A200 · Main Landing Gear Attach SectionSDR 040521239Support · crackedLEFT HAND AND RIGHT HAND MAIN LANDING GEAR DRAG LEG SUPPORTS FOUND TO BE CRACKED DURING FLUORESCENT PENETRANT INSPECTION. INSPECTION ORDERED BY U.S. CUSTOMS SERVICE BASED ON REPORTS FROM U.S. ARMY OPERATORS.Dec 4, 2001 · N1546 · Beech A200 · Main Landing Gear Attach SectionSDR WD42001F00000Valve · mismanufacturedNEW REPLACEMENT PARTS FOR THE ANTI-SIPHON VALVE ASSEMBLY ARE BEING MFG INCORRECTLY. PROBLEM IS THE FLAPPER ASSEMBLY GASKET AND BACKUP PLATE WERE TRIMMED INCORRECTLY AND HINGE IS EXPOSED LEAVING A GAP WHERE FUEL CAN BE SIPHONED OUT DURING FLIGHT IF THE FUEL CANov 1, 2001 · N638B · Beech A200 · Fuel StorageSDR B3OR200000005Tube · crackedPILOTS COMPLETED PRE-TAKEOFF ENGINE RUNS AND RETURNED ENGINES TO IDLE. WHEN POWER LEVERS WERE ADVANCED FOR TAXI TO ACTIVE, NR 1 ENGINE DID NOT RESPOND TO INPUT. AIRCRAFT WAS RETURNED TO RAMP WHERE IT WAS DISCOVERED THAT P3 SENSE LINE TO FCU WAS CRACKED NEAR Nov 2, 2000 · N7074G · Beech A200 · Engine Fuel and ControlSDR 20001120SH023Drag Brace · misoverhauledMAIN GEAR ASSEMBLY RECEIVED IN OVERHAULED CONDITION. DURING INSTALLATION PROCESS, NOTED AND VERIFIED THE DRAG LINK ATTACHMENT LUG SLEEVE WAS APPROXIMATELY .010 INCH OVERSIZE FROM SPECS CALLED OUT IN THE RAYTHEON BEECHCRAFT COMPONENT MM. REF: FAA FORM 8130-3Jun 7, 2000 · N1547 · Beech A200 · Landing Gear Retraction/Extension SystemSDR 99ZZZX2657Tube Assy · crackedPRE-TAKEOFF ENGINE RUNS COMPLETED, PILOTS TAXIED OUT ONTO ACTIVE, APPLIED TAKEOFF POWER, NR 1 ENGINE NO RESPONSE. RETURNED TO LINE, AND SHUT DOWN. MAINTENANCE INSPECTED AND FOUND TUBE ASSY CRACKED AT B-NUT FITTING AT REAR OF ENGINE. THIS TUBE IS STAINLESS SJul 1, 1999 · N1549 · Beech A200 · Propeller GovernorSDR 98ZZZX530Bolt Kit · wrong partsTHE BOLT KIT LISTED IS FOR THE UPPER AND LOWER AFT WING ATTACH FITTINGS FOR A BEECH SERIES 200, UPON RECEIVING 4 OF THESE KITS, NOTICED THE WASHERS INCLUDED IN THE KIT DID NOT HAVE A SMOOTH CONTINUOUS OUTER RADIUS WHICH IS NOTED IN BEECH 200 SRM CH 57-17-01 PJan 20, 1998 · N2MIL · Beech A200 · Wing, Fuselage Attach FittingsSDR 98ZZZX531Bolt Kit · wrong partsTHE BOLT KIT LISTED IS FOR THE UPPER FORWARD WING BOLTS FOR A BEECH 200. UPON RECEIVING 2 EACH KITS, NOTED THE WASHERS INCLUDED WERE NOT PROPERLY RADIUSED ON THE OUTER EDGE. THE BEECH 200 SRM CH 57-17-01 P 212 SPECIFICALLY INSTRUCTS TO INSTALL SMOOTH CONTINUJan 19, 1998 · N2MIL · Beech A200 · Wing, Fuselage Attach FittingsSDR 98ZZZX538Barrel Nut · wrong partKIT 101-4024-1S CONTAINS THE FORWARD LOWER WING BOLT, PL WASHER AND BARREL NUT FOR INSTALLATION ON BEECH 200 SERIES ARICRAFT. THE BARREL NUT ASSY PN 80691CF-1612 WAS OF IMPROPER TOLERANCES AND WOULD NOT FIT IN WING 'BATHTUB' FITTING. FURTHER INVESTIGATION REJan 18, 1998 · N2MIL · Beech A200 · Wing, Fuselage Attach Fittings
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