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 DJFA2006214Wire · frayedCREW REPORTED THAT WHILE CLIMBING THROUGH FL 240 WITH ALL OF THE ANTI-ICE SYSTEMS ON, A 150 AMP SPLIT BETWEEN THE GENERATORS WAS NOTICED AND A BURNING ODOR WAS OBSERVED IN THE CABIN. ALSO, LITE HAZY SMOKE WAS OBSERVED IN THE LAVATORY AREA OF THE CABIN. THE CMar 8, 2006 · N482LX · Beech 400A · Electrical Power System WiringSDR DJFA2006213Unknown · unknownNORMAL YOKE BACK PRESSURE WAS BEING APPLIED AT ROTATION, DID NOT SEEM TO RESPOND. FURTHER FORCE WAS APPLIED, STILL DID NOT RESPOND. PAST V1 SPEED, FELT CERTAIN AIRCRAFT WAS NOT GOING TO LIFT OFF. TAKEOFF ABORTED. HEAVY BRAKING APPLIED, THRUST REVERSERS DIDMar 7, 2006 · N898TA · Beech 400A · Flight Control SystemSDR DXTA200601276Pcb · malfunctionedNORMAL BRAKES FAILED TO ENGAGE TO STOP AIRCRAFT ON TAXI-IN,AIRCRAFT SKIDDED ABRUPTLY WHILE APPLYING NORMAL BRAKE BRESSURE,THEN CONTINUED TO ROLL FOR APPROX 3 TO 4 FT UNTILL EMERGENCY BRAKE APPLIED. - TROUBLESHOT BRAKES AND ANTI-SKID SYSTEM, BLED BRAKES AND REPMar 2, 2006 · N140QS · Beech 400A · Landing Gear Brake SystemSDR LJCR2453796Duct · out of limitsDURING SCHEDULED MAINTENANCE, FOUND BRAIDING AROUND FLEXIBLE BELLOWS DISBONDED FROM ENTIRE CIRCUMFERENCE. NEW REPLACEMENT DUCT ASSEMBLIES NOT AVAILABLE FROM MANUFACTURER. REPLACED WITH SERVICEABLE UNIT. INSPECTED REPLACEMENT UNIT PER AD 2001-03-06 EFF. 3-21Mar 1, 2006 · N999JF · Beech 400A · Air Intake Anti/De-Ice SystemSDR DJFA2006210Skin · corrodedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING AVIONICS INSPECTION TASKS, THE GLOBAL POSITIONING SYSTEM ANTENNA WAS REMOVED TO RESEAL THE BASE OF THE ANTENNA. BOTH THE ANTENNA, AND THE AIRCRAFT SKIN WHERE THE ANTENNA IS MOUNTED WERE FOUND TO BE CORRODEFeb 28, 2006 · N718TA · Beech 400A · Fuselage Main, Plate/SkinSDR DJFA2006206Door · malfunctionedDURING APPROACH INTO CYPQ AFTER THE LANDING GEAR WAS SELECTED DOWN THREE GREEN LIGHTS WERE RECEIVED BUT THE GEAR HANDLE LIGHT REMAINED ILLUMINATED. CONFIRMATION WAS MADE BY A FIXED BASE OPERATOR THAT THE LANDING GEAR DOORS WERE OPEN WHEN A LOW PASS WAS PERFORFeb 26, 2006 · N745TA · Beech 400A · Landing Gear Door Retract SectionSDR DXTA200601256Landing Gear · malfunctionedLOWERED LANDING GEAR AND GOT THREE GREEN LIGHTS AND 2 RED LIGHTS. RETRACTED LANDING GEAR AND GOT NO GREEN LIGHTS AND 2 RED LIGHTS CYCLED GEAR SEVERAL TIMES AND GOT SOME INDICATIONS, DID EMERGENCY GEAR EXTENSION GOT NORMAL GEAR INDICATION 3 GREEN. VERIFIED ADFeb 22, 2006 · N132QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR 2006FA0000234Servo · intermittentINVESTIGATED PILOT REPORT OF INTERMITTENT RUDDER BOOST FAILURE ALONG WITH SIMULATANEOUS AUTOPILOT AND YAW DAMPER DISEGAGEMENT. FOUND RUDDER SERVO INTERMITTENTLY FAILING. REPLACED RUDDER SERVO WITH OVERHAULED UNIT, RUDDER BOOST AND AUTOPILOT FUNCTIONAL TESTS Feb 20, 2006 · N467LX · Beech 400A · Autopilot Main ServoSDR DJFA2006204Trim Tab · lockedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING TASK 05B006.16 TO CHECK THE DEFLECTION ANGLE OF THE ROLL TRIM SYSTEM DURING A D-LEVEL INSPECTION, THE RIGHT ROLL TRIM TAB BECAME LOCKED IN THE UP POSITION.Feb 20, 2006 · N795TA · Beech 400A · Aileron Tab Control SystemSDR DJFA2006205Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION AS PART OF THE -B- LEVEL INSPECTION A RIGHT INBOARD HORIZONTAL STABILIZER RIB WAS FOUND CRACKED NEXT TO THE SIDE ROLLER BRACKET. THE RIB WAS REPLACED WITH A NEW ASFeb 19, 2006 · N740TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006203Bolt · misinstalledTHE CREW REPORTED THAT THE CONTROL YOKE WAS BINDING WHEN THE AIRCRAFT WAS ROLLED TO THE LEFT. MAINTENANCE DISCOVERED AN INBOARD SPOILER CONNECTING ROD ATTACHED BOLT WAS INCORRECTLY INSTALLED. THE LEFT BOLT WAS RE-INSTALLED IN THE CORRECT POSITION. NO BINDINFeb 18, 2006 · N457CW · Beech 400A · Drag Control SystemSDR DJFA2006197Door Seal · detachedTHE CREW REPORTED THAT WHILE THEY WERE IN CRUISE FLIGHT AT FL 340 HEARD A LOUD NOISE COMING FROM THE CABIN DOOR AREA THAT SOUNDED LIKE A DOOR SEAL LEAK. THE AIRCRAFT WAS DIVERTED TO KCRW AND FIRE RESCUE RESPONSE WAS GIVEN FOLLOWING AN UNEVENTFUL LANDING. THEFeb 16, 2006 · N449LX · Beech 400A · Passenger/Crew DoorsSDR DXTA200601242Flt Controls · out of positionON TAKEOFF WARNING HORN CAME ON ABORTED TAKEOFF AT 50 KNOTS FLIGHT CONTROLS APPEARED TO BE IN CORRECT POSITION. COMPLIED WITH TAKEOFF WARNING HORN CHECK IAW RAYTHEON 400/400A M/M 27-40-00 OPS CHECKS SATISFACTORY NO DEFECTS NOTED AT THIS TIME.Feb 15, 2006 · N120QS · Beech 400A · Flight Control SystemSDR DJFA2006195Bolt · shearedDURING A SCHEDULED MAINTENANCE VISIT WHILE REMOVING THE FLAP ASSEMBLIES TO CONDUCT AN -A- LEVEL INSPECTION, IT WAS DISCOVERED THAT THE LEFT FLAP ACTUATOR MOUNTING BRACKET HAD A BOLT THAT WAS SHEARED OFF. THE BOLT WAS REPLACED, AND THE AIRCRAFT WAS RETURNED TOFeb 11, 2006 · N457CW · Beech 400A · Trailing Edge FlapsSDR DJFA2006194Coupling · leakingCREW REPORTED THAT ON CLIMBOUT AT APPROX 23,500 FT THE BLEED AIR DUCT FAIL ANNUNCIATOR ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO KPBI AFTER THE CREW TRIED UNSUCCESSFULLY TO GET THE LIGHT TO EXTINGUISH. AN UNEVENTFUL LANDING WAS COMPLETED IN KPBI. MAINTENANCFeb 10, 2006 · N743TA · Beech 400A · Pneumatic Distribution SystemSDR DXTA200601236Landing Gear · unknownAFTER TAKEOFF ATTEMPTED TO BRING GEAR UP BUT THE RED GEAR HANDLE LIGHT REMAINED ILLUMINATED. CYCLED GEAR SEVERAL TIMES. THE RED GEAR HANDLE LIGHT WOULD TURN OFF W/GEAR DOWN AND THE 3 GREEN GEAR DOWN LIGHT ILLUMINATED BUT WHEN BROUGHT UP RED LIGHT STAYED ON. Feb 9, 2006 · N119QS · Beech 400A · Main Landing GearSDR 2006FA0000145Switch · overtempCREW SMELLED SMOKE/ODOR IN THE CABIN DURING FLIGHT. FOUND SLIGHT DISCOLORATION OF DUCT DUE TO AN OVERTEMP. NO DELAMINATION NOTED AND NO OTHER SIGN OF WIRING OR COMPONENT DAMAGE. WHILE TROUBLESHOOTING FOUND RELAY INSIDE OF VIP CABIN TEMP SWITCH PANEL THAT WAFeb 2, 2006 · N119QS · Beech 400A · Equipment/Furnishings WiringSDR DXTA200601220Smoke · detectedCREW SAW AND SMELLED LITE SMOKE IN THE PASSENGER CABIN. A CREW MEMBER WENT BACK AND NOTICED THAT THE RIGHT SIDEWALL PANEL FELT VERY HOT TO THE TOUCH. ITEM IS UNDER INVESTIGATION.Jan 29, 2006 · N119QS · Beech 400A · Air Distribution SystemSDR DJFA2006191Wire · burnedTHE CREW REPORTED THAT UPON LANDING, SPARKS AND A SMOKE SMELL WERE NOTED BETWEEN THE CONTROL YOKE AND THE PILOTS PRIMARY FLIGHT DISPLAY. UPON INSPECTION, BURNS WERE DISCOVERED ON BOTH PRIMARY FLIGHT DISPLAYS AND ON THE WIRES BEHIND THE YOKE.Jan 25, 2006 · N768TA · Beech 400A · Navigation System WiringSDR 2006FA0000088Window · crackedDURING INSPECTION, THE PILOTS SIDE WINDOW WAS FOUND TO BE CRACKED THROUGH THE OUTER PANE CONNECTING 5 BOLT HOLES ALONG THE TOP OF WINDOW.Jan 24, 2006 · N674SF · Beech 400A · Flight Compartment WindowsSDR 2006F00005Rib · crackedHORIZONTAL STABILIZER INBOARD RIB P/N 45A21104-012 FOUND WITH 3 INCH CRACK ALONG LOWER EDGE OF STAB CENTERING ROLLER BRACKET. BEEF UP ANGLES P/N 45A21085-004, AND 45A21086-004 ALSO FOUND WITH MULTIPLE STRESS CRACKS. EXCESSIVE LOADS ON ROLLER APPEAR TO HAVE CJan 19, 2006 · N432CW · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA200601204Indication Sys · malfunctionedAT FL320 GOT A LEFT GEAR DOWN AND LOCK LIGHT WITHOUT MOVING HANDLE. SPEED 250KIAS GEAR SPEED LIMIT IS 200 KIAS. AIRCRAFT YAWED AND ROLLED TO THE LEFT EXTENDED GEAR AND LANDED NORMALLY. PERFORMED LANDING GEAR ADJUSTMENT TEST AND CHECKED MAIN GEAR UPLOCK CLEAJan 18, 2006 · N151QS · Beech 400A · Landing Gear Position and WarningSDR 8862Wheel · misoverhauledLT MAIN TIRE DISINTEGRATED ON T/O ROLL. AFTER REMOVING WHEEL ASSY, DISCOVERED WHEEL HALVES O-RING EXPOSED BY VALUE STEM. UPON INVESTIGATION DISCOVERED WHEEL WAS NOT OVERHAULED IAW A/C BRAKING SYSTEMS COMPONENT MM. INBOARD WHEEL HALF WAS NOT REMARKED IAW TEMPOJan 15, 2006 · N234DK · Beech 400A · Wheel/Ski/FloatSDR DJFA2006188Engine · leakingTHE CREW REPORTED THAT WHILE PERFORMING A MAINTENANCE TEST FLIGHT TO CHECK FLAP ROLL RATE, A HOT OILY SMELL WAS NOTED IN THE COCKPIT AS COMING FROM A WEMAC AIR VENT. THE SMELL WAS STRONGEST ON TAKEOFF, BUT EVIDENT IN ALL FLIGHT PHASES. ALL OTHER INDICATIONS,Jan 7, 2006 · N755TA · Beech 400A · Turbine Engine Oil SystemSDR 2006FA0000039Uplock · out of rigAFTER TAKEOFF LANDING GEAR WAS SELECTED UP AND GEAR CAME UP TO BUT RED WARNING LIGHT IN GEAR HANDLE STAYED ON AND YOU COULD HEAR THE DOORS WERE STILL OPEN. SELECTED GEAR DOWN AND RETURNED TO BASE. FOUND NOSE GEAR UPLOCK WAS INTERMITTENT. RIGGED UP LOCK AND Jan 5, 2006 · N674SF · Beech 400A · Landing Gear Retraction/Extension SystemSDR 2006FA0000038Uplock · intermittentAFTER TAKEOFF LANDING GEAR WAS SELECTED UP AND GEAR CAME UP TOO BUT RED WARNING LIGHT IN GEAR HANDLE STAYED ON AND YOU COULD HEAR THE DOORS WERE STILL OPEN. SELECTED GEAR DOWN AND RETURNED TO BASE. FOUND NOSE GEAR UPLOCK WAS INTERMITTENT. RIGGED UPLOCK AND Jan 5, 2006 · N674SF · Beech 400A · Landing Gear Retraction/Extension SystemSDR DXTA200601183Position Switch · malfunctionedON TAKEOFF KTEB GEAR WOULD NOT RETRACT, USED OVER RIDE. GEAR RETRACTED NORMAL. JACKED A/C, RETRACTED GEAR SEVERAL TIMES, NO DEFECTS NOTED. CHECKED LT LANDING GEAR SAFETY SWITCH. SWITCH AT LIMIT. ADJUSTED SWITCH, OPS CHECK GOOD IAW HAWKER 400XP MM.Jan 5, 2006 · N120QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200501172A/C Pack · odorSMELL OF BURNING RUBBER SMELLED IN THE CABIN WHEN ACFT IS SET TO TAKEOFF POWER. MOST NOTABILY DURING THE FIRST TAKEOFF OF THE DAY. RAN AIRCRAFT WHEN IT FIRST CAME IN (12/30/05) NO SMELL NOTICED. RAN AGAIN FIRST THING THE NEXT DAY (12/31/05) NO SMELL NOTICED Dec 30, 2005 · N117QS · Beech 400A · Cabin Cooling SystemSDR DJFA2005183Switch · false indicationAFTER MLG RETRACTION, RED UNLOCK LIGHT REMAINED ILLUMINATED. PERFORMED A FLY-BY OF TOWER & ADVISED RT MLG DOOR DOWN. A/C LANDED W/O INCIDENT. RT MLG DOOR REMAINED DOWN. MX REPLACED RT MLG DOOR. DOOR & UPLOCK MECHANISM ADJUSTED. MLG EXTENSION & RETRACTIODec 28, 2005 · N408CW · Beech 400A · Landing Gear Door Retract SectionSDR DJFA2005181Odor · detectedDURING T/O A HEAVY ODOR SIMILAR TO MELTING PLASTIC COMING FROM PAX COMPT AT TIME OF DISCOVERY, TEMP CONTROL WAS SET ON AUTO, TEMP KNOB IN HOT POSITION. CREW DONNED THEIR OXYGEN MASKS & TURNED OFF ALL CABIN HEAT. APPROX 10 MINS ODOR DISSIPATED. A NORMAL LANDDec 26, 2005 · N709TA · Beech 400A · Air Distribution SystemSDR DJFA2005182Bulb · burned outCREW REPORTED, LT GREEN GEAR LIGHT DID NOT ILLUMINATE WHEN THE GEAR WAS EXTENDED FOR LANDING INTO KASE. GEAR LEVER WAS RECYCLED ONCE AND LEFT GEAR INDICATION STILL DID NOT ILLUMINATE. THE APPROACH TO KASE WAS ABORTED, A/C WAS DIVERTING TO KEGE. CREW EXCHANGDec 26, 2005 · N442CW · Beech 400A · Landing Gear Position and WarningSDR DJFA2006190Switch · wornON DESCENT, NR 1 THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THRUST REVERSER EMERGENCY STOW BUTTON WAS PUSHED, DIVERTED. ACFT WANTED TO ROLL LEFT. UNSURE IF ROLL WAS RELATED TO THRUST REVERSER ISSUE, DECLARED AN EMERGENCY. YAW DAMPER WAS THEN DISENGAGED. DUDec 21, 2005 · N445CW · Beech 400A · Engine Thrust ReverserSDR 2006FA0000000Tire · leakingREPLACED THE FRONT TIRE, WITH THIS NEW TIRE AND HAVE HAD A SLOW LEAK EVER SINCE. TOOK THE TIRE BACK OFF AND SUBMERGED THE TIRE AND WHEEL UNDER WATER, FOUND 10 VERY SMALL PINHOLES IN THE TIRE SIDEWALL CLOSE TO THE RIM EQUALLY SPACED AROUND THE SIDEWALL, THE PIDec 21, 2005 · N94LH · Beech 400A · TireSDR DJFA2005176Switch · faultyTHE CREW REPORTED THAT SHORTLY AFTER LIFT OFF, THE RT THRUST REVERSER ARM LIGHT BEGAN TO FLICKER, AND THEN REMAINED ILLUMINATED. AFTER THE LANDING GEAR AND FLAPS WERE RETRACTED, THE EMERGENCY STOW SWITCH WAS DEPRESSED. THE AIRCRAFT WAS DIVERTED WHERE IT LANDDec 15, 2005 · N783TA · Beech 400A · Engine Thrust ReverserSDR DJFA2005174Pitot Tube · faultyCREW REPORTED, WHEN THEY BEGAN DESCENT, NOTICED A LOSS OF AIRSPEED. AIRSPEED CONTINUOUSLY DECREASED ON BOTH PRIMARY FLT DISPLAYS, STANDBY INSTRUMENTS. SPEED DECREASED TO ZERO, WENT BLANK ALONG WITH ALTITUDE ON BOTH PRIMARY FLT DISPLAYS. PFD ARTIFICIAL HORIZDec 14, 2005 · N689TA · Beech 400A · Pitot/Static SystemSDR AU510001928Arm · brokenLT ENGINE THRUST REVERSER INBOARD LOWER IDLER ARM BROKEN AT BEARING END BATWING ATTACHMENT POINT. DURING INVESTIGATION CRACKS WERE ALSO FOUND IN THE UPPER THRUST REVERSER SKIN THROUGH A ROW OF NINE RIVETS.Dec 12, 2005 · Beech 400A · Engine Thrust ReverserSDR DJFA2005170Switch · intermittentAFTER LANDING GEAR WAS SELECTED DOWN DURING APPROACH THEY ONLY RECEIVED A GREEN NOSE AND LT GEAR INDICATION. NO RT GEAR INDICATION WAS RECEIVED, RED IN-TRANSIT LIGHT DID NOT ILLUMINATE AND GEAR HORN DID NOT SOUND. RT GEAR INDICATION WAS NOT RECEIVED AFTER ANDec 4, 2005 · N478LX · Beech 400A · Landing Gear Retraction/Extension SystemSDR DXTA200501124Hmu · out of adjustA RIGHT ENGINE WOULD NOT REACH SCHEDULED TAKEOFF POWER OF 98.2 PERCENT. FULL THROTTLE REACHED 96 PERCENT ONLY (N1). ADJUSTED HMU PRESSURE REGULATING VALVE. OPS CHECKED GOOD. PERFORMED EEC AUTHORITY CHECK.Dec 1, 2005 · N106QS · Beech 400A · Fuel Controlling SystemSDR CA051223001Engine · flamed outDURING CRUISE AT 38K FEET, BOTH ENGINES FLAMED-OUT. IN-FLIGHT RELIGHT ATTEMPTS WERE UNSUCCESSFUL AND THE AIRCRAFT DIVERTED FOR A DEAD-STICK LANDING. P&WC WILL PARTICIPATE IN THE INVESTIGATION OF THIS INCIDENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED.Nov 28, 2005 · Beech 400A · Engine (Turbine/Turboprop)SDR DJFA2005168Engine · power lossEN ROUTE, SHORTLY AFTER POWER WAS REDUCED TO BEGIN DESCENT FROM CRUISE ALTITUDE, BOTH ENGINES EXPERIENCED A SUSTAINED POWER LOSS. UNABLE TO RESTART EITHER ENGINE IN FLT. EMERGENCY DECLARED & ACFT DIVERTED. UNDER NTSB INVESTIGATION. MX REPLACED AIRFRAME & ENov 28, 2005 · N691TA · Beech 400A · Engine (Turbine/Turboprop)SDR 2005FA0001626Brushes · worn1000 HOUR OVERHAUL OF BOTH STARTER-GENERATORS, REINSTALLED AFTER OVERHAUL. (K)Nov 23, 2005 · N53MS · Beech 400A · Starter-GeneratorSDR 2005FA0001625Brushes · worn1,000 HOUR OVERHAUL OF BOTH STARTER-GENERATORS BRUSHES WORN. REINSTALLED AFTER OVERHAUL. (K)Nov 23, 2005 · N53MS · Beech 400A · Starter-GeneratorSDR DJFA2005167Generator · malfunctionedKPGD - KSGR TRIP ID NR 935498, APPROXIMATELY 125 NM FROM KSGR BOTH LEFT AND RIGHT GENERATORS WERE CYCLING ON AND OFF ONE AT A TIME. AN EMERGENCY WAS DECLARED AND THE CREW BEGAN A DESCENT TO DIVERT INTO KBPT. RADIOS AND OTHER ELECTRICAL EQUIPMENT WERE TURNINNov 23, 2005 · N744TA · Beech 400A · DC Generating SystemSDR DJFA2005166Unknown · fumesKAPA - TRIP ID NR 935454, THE CREW REPORTED SMELLING VERY STRONG FUMES IN THE COCKPIT AFTER TAKEOFF. THE FUMES COMING FROM THE "EYEBALL" VENTS WERE REPORTED TO HAVE BURNED THE EYES AND THROATS OF THE CREW. OXYGEN MASKS WERE DONNED, AND A/C WAS RETURNED TO KNov 23, 2005 · N718TA · Beech 400A · Cabin Temperature Control SystemSDR DJFA2005165Door · looseWITH LANDING GEAR IN UP POSITION GEAR DOOR LIGHT WOULD REMAIN ILLUMINATED. WHILE AC WAS BEING RETURNED. A LOW-PASS WAS FLOWN PAST TOWER AND CONFIRMED SOMETHING WAS HANGING DOWN FROM AC. TOWER DECLARED AN EMERGENCY, CREW PERFORMED A MANUAL LANDING GEAR EXTENNov 22, 2005 · N442CW · Beech 400A · Landing Gear DoorsSDR DXTA200501098Odor · detectedDURING CLIMBOUT THROUGH 15,000 FT AND UP, A PUTRID ODOR WAS COMING FROM AFT CABIN. CABIN HEAT WAS ON ALONG WITH WING HEAT AND ALL ANTI-ICE WAS ON. ODOR DISSIPATED DURING DESCENT. ITEM IS UNDER INVESTIGATION.Nov 21, 2005 · N142QS · Beech 400A · Air Distribution SystemSDR DJFA2005161Warning Light · illuminatedKRFD - KSDF DURING CRUISE FLIGHT, WHILE ENRANGE TO KLEX, THE CREW NOTED THAT THE HYDRAULIC FLUID PRESSURE WAS INDICATING 2,000 PSI. DUE TO A LONGER RUNWAY LENGTH THE AIRCRAFT WAS DIVERTED TO KSDF AND AN EMERGENCY WAS DECLARED. A MANUAL GEAR EXTENSION WAS PERNov 16, 2005 · N709TA · Beech 400A · Hydraulic System, MainSDR DJFA2005160Trim System · malfunctionedA/C TRIMMED FOR CLIMB AND AUTO PILOT WAS ENGAGED AT 5,000 FT, APPROX 8,000 FT YELLOW BOXED "E" WAS DISPLAYED ON PRIMARY FLT DISPLAY, AND SOON AFTER AUTOPILOT PITCH TRIM FAIL ANNUNCIATOR ILLUMINATED. PITCH TRIM IND POSITION WAS SLIGHTLY NOSE DOWN. WHEN CREW DNov 12, 2005 · N478LX · Beech 400A · Autopilot SystemSDR DXTA200501069Smoke · detectedSMOKE IN THE CABIN DETECTED DURING DESCENT FROM FL320 - FL240, PERSISTED AFTER ISOLATING BLEED AIR AND TURNING ANTI-ICE OFF. NON-ELECTRICAL SMOKE ODOR, BUT UNABLE TO ISOLATE SOURCE. ITEM IS UNDER INVESTIGATION.Nov 8, 2005 · N142QS · Beech 400A · Air Distribution SystemSDR 2005FA0001536Tire · debondedOPERATOR STATED, RT FROM INSTALL AT ANOTHER FACILITY, THE AIRCRAFT EXPERIENCED NOSE VIBRATION ON TAKE OFF. DISASSEMBLED WHEEL ASSY AND FOUND INNER CASING OF TIRE DEBONDING. (K)Nov 3, 2005 · N400MV · Beech 400A · Tire
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