Beech 400A

Service difficulty reports · 1,397

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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 = '400A'
  ORDER BY difficulty_date DESC"

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SDR E81RJW303462Transducer · out of limitsDURING DESCENT, "RUDDER BOOST FAIL" ANNUNCIATOR ILLUMINATED AT 8000 FT AND 250 KTS. FLIGHT CREW ACCOMPLISHED ABNORMAL PROCEDURES IAW AFM, LIGHT DID NOT EXTINGUISH. TROUBLESHOT RUDDER BOOST SYS IAW MM 27-21-00. FOUND THE LT ENGINE LOWER PRESSURE TRANSDUCER TO Oct 9, 2010 · N161QS · Beech 400A · Rudder Control SystemSDR DXTA2010100104255Servo · failedFLASH OF RUDDER BOOST FAIL ANNUNCIATOR AND YAW DAMP KICKED OFF SHORTLY AFTER TAKEOFF. 600-800 FT. TWICE DURING DESCENT, AUTOPILOT AND YAW DAMP KICKED OFF WITH GA INDICATIONS ON PFD. 12,000-11,000FT AND 9,000-8,000FT. TWICE RUDDER BOOST FAIL AND YAW DAMP KICSep 30, 2010 · N149QS · Beech 400A · Autopilot SystemSDR DJFA2010027Rib · crackedDURING A SCHEDULED MX INSP, WHILE PERFORMING A BOROSCOPE INSP OF THE HORIZ STABILIZER RIBS, SEVERAL CRACKS WERE FOUND ON RIBS IN THE LT AND RT SIDES OF THE HORIZ STABILIZER. THE CRACKS WERE FOUND ON THE ATTACHMENT FLANGES FROM THE RIBS WHERE THEY ARE RIVETED TSep 27, 2010 · N473FL · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA2010092004243Sensor · faultedTHE "H STAB FAIL" LIGHT CAME ON WHEN THE HORIZONTAL STAB ANTI ICE WAS TURNED ON. DID THE APPROPRIATE CHECKLIST WHICH INCLUDED PULLING THE HORIZONTAL STAB PROTECT CIRCUIT BREAKER. ISOLATED FAULT AT SENSOR NR 1 AND THERMALLY MATCHED MATE AND SPLICED IV SPARE TSep 19, 2010 · N151QS · Beech 400A · Airfoil Anti/De-ice SystemSDR DJFA2010025Fuel · odorDURING FLIGHT, PASSENGERS NOTED A STRONG FUEL ODOR IN THE CABIN. ACFT DIVERTED AND LANDED SAFELY. MX TECHS FOUND RESIDUAL FUEL IN THE ACFT BELLY AND CONFIRMED THE ODOR. FURTHER INVESTIGATION WAS UNABLE TO DETECT ANY FUEL LEAKS FROM THE FUEL TANKS. RESIDUASep 10, 2010 · N476LX · Beech 400A · Air Distribution SystemSDR DXTA2010090704220Brake · weakON LANDING AND TAXI IN, BRAKES ON LT AND RT SIDES APPLY WHAT FEELS LIKE MINIMAL BRAKING ON INITIAL APPLICATION. UPON INCREASE IN TOE PEDAL PRESSURE, BRAKES WILL THEN GRAB CAUSING A NOTICEABLE JERKING OF THE ACFT WHEN THEY GRAB. BLED SYS POWER BRAKE BLEED. FOSep 5, 2010 · N114QS · Beech 400A · Landing Gear Brake SystemSDR E81R_JW30312_2Limit Switch · failedFLIGHT CREW REPORTED SPEED BRAKES WOULD NOT DEPLOY ON DESCENT GOING THROUGH 9000 FT AT 250 KIAS. SPEED BRAKES EVENTUALLY DEPLOYED AFTER CYCLING SPEED BRAKE CONTROL SWITCH SEVERAL TIMES. TROUBLESHOT SYS, FOUND HIGH INTERNAL RESISTANCE IN THE S156 SPEED BRAKE Aug 27, 2010 · N153QS · Beech 400A · Drag Control SystemSDR DXTA2010083004215Brake Sys · malfunctionedAFTER GEAR RETRACTION THE RED GEAR UNSAFE LIGHT REMAINED ON AS WELL AS THE HYD PRESS CAUTION LIGHT. AFTER LOWERING THE GEAR ALL THREE GREEN LIGHTS ILLUMINATED AND THE GEAR UNSAFE LIGHT WENT OUT. LANDING WAS NORMAL. REPLACED LEFT AND RIGHT MAIN GEAR ACTUATOR RAug 26, 2010 · N114QS · Beech 400A · Landing Gear Brake SystemSDR DJFA2010024Bolt · brokenDURING A SCHEDULED MX EVENT, THE RT MLG UPLOCK ACTUATOR MOUNTING BOLT WAS FOUND BROKEN. SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.Aug 18, 2010 · N415LX · Beech 400A · Main Landing GearSDR DJFA2010023Rib · crackedDURING A SCHEDULED MX EVENT, WHILE PERFORMING A BOROSCOPE INSP OF THE HORIZ STABILIZER RIBS, SEVERAL CRACKS WERE FOUND ON SEVERAL RIBS IN THE LT AND RT SIDES OF THE HORIZ STABILIZER. THE CRACKS WERE FOUND ON THE ATTACHMENT FLANGES FROM THE RIBS WHERE THEY ARE Aug 17, 2010 · N415LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2010022Rib · crackedDURING A SCHEDULED MX EVENT, WHILE PERFORMING A BOROSCOPE INSP OF THE HORIZ STABILIZER RIBS, SEVERAL CRACKS WERE FOUND ON SEVERAL RIBS IN THE LT AND RT SIDES OF THE HORIZ STABILIZER. THE CRACKS WERE FOUND ON THE ATTACHMENT FLANGES FROM THE RIBS WHERE THEY ARE Aug 16, 2010 · N493LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2010019Drain · cloggedCREW REPORTED SEVERE MOLD SMELL IN THE CABIN DURING FLIGHT WITH THE AIR CONDITIONING ON. MAINTENANCE DISCOVERED THE AFT EVAPORATOR DRAIN PLUGGED, RESULTING IN WATER SPILLAGE ONTO THE CARPET. THE CARPET WAS FOUND SATURATED WITH MOISTURE AND MOLDY. THE DRAIN WJul 19, 2010 · N203FL · Beech 400A · Fuselage Miscellaneous StructureSDR DJFA2010018Carpet · moldedCREW REPORTED AN EXTREMELY STRONG MOLD SMELL IN THE CABIN DURING FLIGHT. MAINTENANCE FOUND THE CARPET DIRTY AND MOLDING. THE CARPET WAS REPLACED.Jul 18, 2010 · N471LX · Beech 400A · Passenger Compartment EquipmentSDR DXTA2010071904158Unknown · odorON APPROACH AT APPROX 1500 FT, A STRONG ODOR IN COCKPIT. SIMILAR TO CANDLE WAX BURNING. ODOR DID NOT OCCUR DURING TAXI OR ANY OTHER PHASE OF FLT. ONLY DURING APPROACH & DID NOT APPEAR TO BE ELECTRICAL IN NATURE. AFTER OPENING FWD ENTRY DOOR, ODOR REMAINED IN CJul 18, 2010 · N125QS · Beech 400A · Air Distribution SystemSDR DJFA2010015Switch · inoperativeDURING CLIMB T THROTTLE MOVED BACK TO 86 PERCENT N1 UNCOMMANDED. RUDDER BOOST WAS INITIATED AND THE THROTTLE WOULD NOT ADVANCE FURTHER. ACFT RETURNED TO THE DEPARTURE AIRPORT SAFELY. A SIMILAR PROBLEM HAD BEEN REPORTED ON THE PREVIOUS FLIGHT WHICH RESULTED Jul 4, 2010 · N448LX · Beech 400A · Engine Thrust ReverserSDR DJFA2010013Cable · brokenDURING A SCHEDULED INSPECTION, MX FOUND THE LT FWD FLAP FOLLOW-UP CABLE SEVERELY CORRODED AND SEVERED AT THE MID BELL CRANK FERRULE. THE CABLE WAS REPLACED.May 26, 2010 · N203FL · Beech 400A · Trailing Edge Flap Control SystemSDR 2010F00112Valve · looseFUSELAGE FUEL WOULD NOT GRAVITY FEED DURING REFUELING FROM THE FUSELAGE FILL TANK TO FORWARD MAIN FUSELAGE FUEL TANKS. THE FUEL DID FINALLY FEED TO THE MAIN FUSELAGE TANKS OVER A 3 DAY PERIOD. THE AFT TANK WAS INTERNALLY ACCESSED AND THE AFT FUSELAGE TANK SURGMay 24, 2010 · N625W · Beech 400A · Fuel Transfer ValveSDR T17A420CT5/21Entertain Sys · odorDURING CLIMB OUT, CREW DETECTED ELECTRICAL SMOKE ODER AT SAME TIME PASSENGER REPORTED SMOKE COMING FROM LT PASSENGER ENTERTAINMENT DISPLAY UNIT. THE CAPTAIN IMMEDIATLY TURNED OFF GALLEY POWER. F/O WENT INTO CABIN AND PASSENGER HAD DISCONNECTED THE POWER CORD May 21, 2010 · N420CT · Beech 400A · Entertainment SystemSDR DJFA2010010Fitting · wornDURING CLIMB, CREW REPORTED AN UNUSUAL AIRFRAME VIBRATION. AFTER LEVELING OFF, CREW REPORTED THE VIBRATION CEASED AND A LOUD BANG; DECISION TO DIVERT WAS MADE. DURING DESCENT, VIBRATION RETURNED & SECOND BANG HEARD, IMMEDIATELY FOLLOWED BY A SUDDEN YAW MOVEMMay 9, 2010 · N440LX · Beech 400A · Fuselage, Landing Gear Attach FittingsSDR DJFA2010009Bracket · crackedDURING A SCHEDULED MX VISIT WHILE PERFORMING A HORIZ STABILIZER ROLLER INSP OF THE HORIZ STABILIZER INBD RIB AND BRACKET ASSEMBLIES, THE RT RIB BRACKET WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE NR 70. THE LT AND RTApr 27, 2010 · N447LX · Beech 400A · Horizontal Stabilizer StructureSDR E81RJT227916BTire · wrong part(E81R) DURING REPLACEMENT OF WORN NOSE WHEEL TIRE, NOTED PN OF INSTALLED NOSEWHEEL TIRE INCORRECT IAW THE ACFT MFG IPC (32-40-05-01). IAW MFG TIRE APPLICATION DATA, THE REMOVED PN TIRE WOULD BE INSTALLED ON ANOTHER ACFT. HAVE NOTED THIS INCORRECT TIRE PN INSTAApr 8, 2010 · N445CT · Beech 400A · TireSDR E81RJT227916AWheel Half · corroded(E81R) DURING DISASSEMBLY OF NOSEWHEEL FOR TIRE REPLACEMENT NOTED CORROSION PITTING IN BOLT HOLES. PITTING WAS DEEPER THAN FIELD REPAIRABLE SERVICE LIMITS. THIS IS THE SECOND NOSEWHEEL ASSY FROM A RELATIVELY NEW ACFT REJECTED IN LAST 30 DAYS DUE TO EXCESSIVApr 8, 2010 · N445CT · Beech 400A · Wheel/Ski/FloatSDR DXTA2010032304050Brake · weakBRAKES ARE DIFFICULT TO MODULATE & PERFORMANCE IS LESS THAN NORMAL. BRAKE PEDAL DEFLECTION ON BOTH SIDES IS MUCH MORE THAN NORMAL OPS. APPLIED & HELD STEADY BRAKES APPEARED TO LET GO & ADDITIONAL BRAKING DEFLECTION REQUIRED. LONGER THAN ANTICIPATED RUNWAY RMar 19, 2010 · N114QS · Beech 400A · Landing Gear Brake SystemSDR T17A462TM3/10Diode · burnedDURING TRAINING FLT, DURING 1 MANEUVER, NOTICED VARIOUS ANNUNCIATORS FLICKER ON & OFF. NOTICED SMOKE COMING OUT OF GLARE SHIELD. FOLLOWED CHECKLIST & IMMEDIATELY TURNED BATTERY & MASTER GENS TO EMER, SMOKE STOPPED. OPENED MANUAL PRESSURE KNOB & SMOKE EXITED COMar 10, 2010 · N492TM · Beech 400A · Electrical Power System WiringSDR DJFA2010007Rib · crackedDURING A SCHEDULED MX VISIT WHILE PERFORMING A HORIZ STABILIZER ROLLER INSP OF THE HORIZ STABILIZER INBD RIB AND BRACKET ASSEMBLIES, THE LT INBD RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. THE LT AND RT RIMar 7, 2010 · N471LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA2010030804019Fuel Control · malfunctionedRT ENG EFC FAIL LIGHT ILLUMINATED SEVERAL TIMES IN FLIGHT WITH RPM ROLLBACK ON THE RT ENGINE. EFC RESET SUCCESSFULLY TWICE, THEN WOULD NOT RESET THEREAFTER. TROUBLESHOT IAW MM 76-10 & 73-20, ASSISTED BY MFG TECH SUPPORT. REMOVED THE LT & RT EEC & T/O PROBES Mar 7, 2010 · N132QS · Beech 400A · Fuel Control/Turbine EnginesSDR DJFA2010005Rib · crackedDURING A MX VISIT WHILE PERFORMING A HORIZ STABILIZER ROLLER INSP OF THE HORIZ STABILIZER INBD RIB AND BRACKET ASSEMBLIES, THE RT INBD RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. THE LT AND RT RIB ASSEMBLIFeb 28, 2010 · N470LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA2010012903959Master Cylinder · weakLT BRAKE PEDAL ON CO-PILOTS SIDE NEARLY GOES TO THE FLOOR DURING BRAKE APPLICATION. OPERATION ON PILOTS SIDE APPEARS NORMAL. R & R LT BRAKE PEDAL MASTER CYLINDER ON COPILOTS SIDE WITH AN OVERHAULED UNIT. BLED BRAKES SYS; OPS CHECK SATISFACTORY IAW MM CHAPTEJan 28, 2010 · N138QS · Beech 400A · Master Cylinder/Brake ValveSDR DJFA201002Duct · failedDURING FLIGHT, CREW NOTED BLEED AIR DUCT FAILURE WARNING. ACFT PERFORMED AN UNSCHEDULED LANDING. DETERMINED A BLEED AIR DUCT FAILED. ACFT SCHEDULED TO FERRY TO A MX STATION. AFTER TAKE-OFF FOR FERRY FLT, CREW DETECTED AN OIL ODOR WHEN THROTTLES ADVANCED & Jan 3, 2010 · N438LX · Beech 400A · Engine Bleed Air SystemSDR DJFA2009048Rib · crackedDURING A SCHEDULED MX VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER INBD RIB AND BRACKET ASSEMBLIES, BOTH INBD RIBS WERE FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. THE LDec 27, 2009 · N451LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DBCA2009121095GKO-Ring · failedON CLIMBOUT FROM MKE CREW NOTICED RUMBLE FROM NOSE AREA FOLLOWED BY A NOSE GEAR UNSAFE INDICATION. CREW DETERMINED NOSE GEAR HAD RELEASED FROM UPLOCK AND EXTENDED. CREW EXTENDED LANDING GEAR AND RETURNED TO MKE. LANDING WAS UNEVENTFUL. STERLING MAINTENANCEDec 10, 2009 · N95GK · Beech 400A · Nose/Tail Landing Gear Strut/AxleSDR DJFA2009046Coalescer Bag · frozenON CLIMB OUT, AFTER TAKEOFF, CREW REPORTED VIBRATION FELT THROUGHOUT THE ACFT. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. MX PERFORMED ENG RUNS AND ENG OPS CHECKS, CHECKED ALL FLIGHT CONTROL RIGGING, AND PERFORMED LANDING GEAR OPS AND VISUAL CHECKS BUT WADec 7, 2009 · N422FL · Beech 400A · Humidity Control SystemSDR DXTA2009120703882Master Cylinder · defectiveDURING TAXI OUT, CAPTAIN'S LT BRAKE PEDAL WENT ALL THE WAY TO STOP WHILE ATTEMPTING BRAKE APPLICATION, WITHOUT BRAKE EFFECTIVENESS. MADE 2 ATTEMPTS W/O SUCCESS. CO-PILOT BRAKES WORKED AND STOPPED ACFT. CAPT SIDE BRAKES REGAINED EFFECTIVENESS SHORTLY THEREAFTDec 6, 2009 · N179QS · Beech 400A · Master Cylinder/Brake ValveSDR DJFA2009045Rib · crackedDURING A SCHEDULED MX VISIT WHILE PERFORMING A HORIZ STABILIZER ROLLER INSP OF THE HORIZ STABILIZER INBD RIB AND BRACKET ASSEMBLIES, BOTH INBD RIBS WERE FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. THE LT AND RT RIDec 2, 2009 · N477FL · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2009043Rib · crackedDURING A SCHEDULED MX VISIT WHILE PERFORMING A HORIZ STABILIZER ROLLER INSP OF THE HORIZ STABILIZER INBD RIB AND BRACKET ASSEMBLIES, BOTH INBD RIBS WERE FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. THE LT AND RT RNov 12, 2009 · N463LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2009042Rib · crackedDURING A SCHEDULED MX VISIT WHILE PERFORMING A HORIZ STABILIZER ROLLER INSP OF THE HORIZ STABILIZER INBD RIB AND BRACKET ASSEMBLIES, THE RT INBD RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. THE LT AND RT Nov 10, 2009 · N480LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2009040Power Supply · failedON 11/3/09 CREW REPORTED SMOKE IN THE COCKPIT EMINATING FROM THE ALTITUDE SELECT PANEL DURING PREFLIGHT. MX CHANGED THE ALTITUDE SELECT PANEL AND OPS CHECKS WERE SATISFACTORY. ON 11/5/09, THE EVENT REPEATED, ONCE AGAIN OCCURING DURING THE PREFLIGHT CHECKS, MNov 5, 2009 · N447LX · Beech 400A · Flight Compartment LightingSDR 2010FA0000017Rotor · brokenENGINE GEAR DRIVEN ALTERNATOR FAILED AFTER 14 HOURS TIME-IN SERVICE. ROTOR SHAFT BROKE AT STOP COLLAR GROVE. NO PHYSICAL DAMAGE FOUND INSIDE ALTERNATOR AND BEARINGS TURN FREELY. SUSPECT MATERIAL FLAW OR IMPROPPER MATERIAL IN ROTOR SHAFT, COMBINED WITH SHARP EDOct 27, 2009 · Beech 400A · AC Generator-AlternatorSDR DJFA2009039Circuit Breaker · shortedWHILE RUNNING ENGINES ON THE GROUND, PRIOR TO DEPARTURE, CREW REPORTED A POPPING SOUND COMING FROM THE LT SIDE OF THE COCKPIT, FOLLOWED BY SMOKE EMINATING FROM THE LT WINDSCREEN AREA. MX DISCOVERED THE RT ANTI-ICE AND WING AINTI-ICE CIRCUIT BREAKERS CONTACTINOct 11, 2009 · N474LX · Beech 400A · Ice/Rain Protection System WiringSDR DJFA2009038Warning Light · false activationDURING FLIGHT, CREW REPORTED HYD OVERPRESSURE CONDITION WITH AN INDICATION OF OVER 1850 PSI. EMERGENCY PROCEDURES WERE FOLLOWED AND THE ACFT LANDED SAFELY. MX RESET THE PRESSURE RELIEF VALVE AND CHECKED THE SYS WITH DIRECT READING GAUGES BUT COULD NOT DUPLICOct 7, 2009 · N463LX · Beech 400A · Central WarningSDR E81R_JW30187Downlock Switch · openFOLLOWING LANDING GEAR EXTENSION ON APPROACH, FLIGHT CREW NOTED NO RT MLG DOWN AND LOCKED INDICATION. FERRIED ACFT FOR REPAIRS. FOUND RT MLG DOWNLOCK SWITCH S018 TO HAVE HIGH INTERNAL RESISTANCE ON INDICATION SIDE OF SWITCH CONTACTS. REPLACED SWITCH AND ADJOct 7, 2009 · N435CT · Beech 400A · Landing Gear Position and WarningSDR VIBR RK125 LEFTTube · blew outDURING SCHEDULED AIRFRAME MX, A AND B CHECKS AND INSP OF ACFT BLEED AIR TUBES IN REFERENCE TO AD2001-03-06 FOUND LEFT BLEED AIR TUBE BELLOWS RUPTURED.Oct 1, 2009 · N939G · Beech 400A · Pneumatic Distribution SystemSDR E81R_JT22650Diode · openFLIGHT CREW REPORTED NORMAL HORIZ STAB NOSE DOWN PITCH TRIM WOULD NOT OPERATE AT AIRSPEEDS ABOVE 250 KIAS. REQUIRED EXTENSIVE TROUBLESHOOTING AND FLIGHT CHECKS WITH MFG TECH SUPPORT TO CORRECT. REPLACED AND SWAPPED NUMEROUS ELECTRICAL COMPONENTS, PITCH TRIM ASep 21, 2009 · N493TM · Beech 400A · Flight Control System WiringSDR E81RJT22642Transducer · malfunctionedFLIGHT CREW NOTED "RUDDER BOOST FAILURE" INDICATION SHORTLY AFTER DEPARTURE FROM KRFD, RETURNED TO KRFD. TROUBLESHOOTING INDICATED FAILED R/H ENGINE #1 RUDDER BOOST PRESSURE TRANSDUCER MT106. REPLACED PRESSURE TRANSDUCER WITH NEW PRESSURE TRANSDUCER, RUDDER BOSep 16, 2009 · N495CT · Beech 400A · Rudder Control SystemSDR E81RJT22643Landing Gear · false indicationON APPROACH, FLT CREW NOTED RT MLG WOULD NOT INDICATE DOWN AND LOCKED CONDITION FOLLOWING MLG EXTENSION. FLT CREW PERFORMED MLG EMERGENCY EXTENSION PROCEDURES AND ABLE TO OBTAIN RT MLG FULL EXTENSION AND LOCKING INDICATION. RESTORED SYSTEM TO NORMAL PER MM 32Sep 16, 2009 · N419TM · Beech 400A · Landing Gear Position and WarningSDR E81R_JT22631Switch · faultyFLIGHT CREW OBSERVED LT WING FUEL TANK OVERPRESSURE ANNUNCIATOR INDICATION IN CRUISE FLIGHT. CREW FOLLOWED PROCEDURES IAW CHECKLIST AND INDICATION RETURNED. TROUBLESHOT SYS AND FOUND LT WING FUEL TANK OVERPRESSURE SWITCH OPERATION FAULTY. REPLACED SWITCH ASSYSep 8, 2009 · N470CT · Beech 400A · Fuel StorageSDR 2009F00062Spacer · misinstalledINVESTIGATED FLIGHT CREW REPORT OF HUMMING/WHISTLING NOISES COMING FROM AFT CABIN CEILING AREA. FOUND SIGNIFICANT LEAKAGE FROM BETWEEN ADF ANTENNA ASSY AND FUSELAGE SKIN. UPON ADF ANTENNA REMOVAL NOTED AFT SPACER INSTALLED INCORRECTLY AND GASKET CUT TO FIT INAug 24, 2009 · N491TM · Beech 400A · Fuselage Main, StructureSDR 2009FA0000722Bracket · crackedDURING SCHEDULED A, B, AND C INSP FOUND ROLLER BRACKETS CRACKED ON LT AND RT INBD FWD HORIZ STAB RIBS. REPLACED INBD RIB COMPONENTS WITH IMPROVED PN COMPONENTS IAW MFG COMMUNIQUE 83. RECOMMEND MFG ISSUE A RECOMMENDED SB OR KIT TO REPLACE THE ORIGINAL PN COMPAug 17, 2009 · N68JV · Beech 400A · Horizontal Stabilizer Miscellaneous StructureSDR 2009F00063Bracket · crackedDURING SCHEDULED A, B, AND C INSP FOUND ROLLER BRACKETS CRACKED ON LT AND RT INBD FWD HORIZ STAB RIBS. NEW RT INBD RIB ASSY HAD BEEN INSTALLED 1190.3 HRS PREVIOUSLY FOR REPLACEMENT OF CRACKED ROLLER BRACKETS. INSTALLED NEW IMPROVED PN RIBS AND BRACKET ASSY. Aug 17, 2009 · N68JV · Beech 400A · Horizontal Stabilizer Miscellaneous StructureSDR DJFA2009033Rib · crackedDURING A SCHEDULED MX VISIT WHILE PERFORMING A HORIZ STAB ROLLER INSP OF THE HORIZ STAB INBD RIB AND BRACKET ASSEMBLIES, BOTH INBD RIBS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. THE LT AND RT RIB Aug 11, 2009 · N745TA · Beech 400A · Horizontal Stabilizer, Spar/Rib
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