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 DXTA200501055Filter · bypassingABORTED TAKEOFF AT 50 KTS DUE TO RIGHT FUEL BYPASS LIGHT ILLUMINATED AND STAYED ON UNTIL THROTTLES WERE BACK AT IDLE. REMOVED AND REPLACED BOTH FUSELAGE FUEL BOWL FILTERS, LEAK CHECK GOOD REF 400XP MM 28-20-00.Nov 3, 2005 · N106QS · Beech 400A · Aircraft Fuel Filter/StrainerSDR DJFA2005156Brake · malfunctionedKSJC - THE CREW REPORTED THAT WHILE THEY WERE TAXIING THE AIRCRAFT IN KSJC, THE LEFT BRAKE DEGRADED FROM POOR TO NIL. BRAKING ON THE RIGHT SIDE WAS NORMAL. MAINTENANCE BLED AIR FROM BOTH BRAKING SYSTEMS, AND PERFORMED AN OPERATIONAL CHECK. NO DEFECTS WERE NOct 30, 2005 · N744TA · Beech 400A · Landing Gear Brake SystemSDR DJFA2005153Door · malfunctionedKTUL - KSBN WHILE MAKING A VISUAL APPROACH TO LANDING IN KSBN, THE GEAR WAS SELECTED DOWN AND THE CREW RECEIVED 3 GREEN INDICATIONS, HOWEVER, THE MAIN GEAR DOORS WOULD NOT RETRACT. A MISSED APPROACH WAS EXECUTED. THE SAME INDICATION WAS RECEIVED WHEN THE LAOct 22, 2005 · N792TA · Beech 400A · Landing Gear Door Retract SectionSDR DJFA2005152Bulb · burned outUPON LANDING AT KHEZ, THE CREW DID NOT RECEIVE A DOWN AND LOCKED INDICATION FOR THE LEFT MAIN GEAR. THE GEAR INDICATION BULB WOULD NOT ILLUMINATE WHEN TESTED. THE AIRCRAFT WAS DIVERTED TO KHOU FOR MAINTENANCE. FIRE/RESCUE RESPONSE WAS GIVEN AND THE AIRCRAFTOct 19, 2005 · N480LX · Beech 400A · Landing Gear Position and WarningSDR DXTA200501030Position Switch · malfunctionedON APPROACH RT MAIN GEAR LIGHT WOULD NOT ILLUMINATE WHEN GEAR SELECTED DOWN. GEAR CYCLED TWICE AND LIGHT CAME ON, 3 GREEN. REPLACED FAULTY RT GEAR DOWNLOCK SWITCH WITH NEW. OPS CHECK GOOD IAW 400XP MM 32-31-02.Oct 18, 2005 · N108QS · Beech 400A · Landing Gear Position and WarningSDR 2005FA0001457Transmitter · out of adjustFLAP ASYMMETRY ANNUNCIATOR ILLUMINATED DURING APPROACH. FOUND MIDBOARD ASYMMETRY DETECTOR READING 5.7 VOLTS. FOUND IB ASYMMETRY DETECTOR READING 7.8 VOLTS. ADJUSTED LT AND RT FLAP POSITION TRANSMITTERS AS REQUIRED IAW MM TO BRING VOLTAGES TO 5.8 VOLTS +/- 0Oct 10, 2005 · N419CW · Beech 400A · Trailing Edge Flap Control SystemSDR DXTA200501014Indicator · inoperativeLEFT GREEN LANDING GEAR DOWN INDICATOR LIGHT WOULD NOT ILLUMINATE WITH GEAR SELECTED . CYCLED GEAR 2 TIMES NO CHANGE, DID EMERGENCY GEAR RETRACTION (PNEUMATIC) AND LEFT LIGHT STILL DIDN'T ILLUMINATE . TURNED ON ALL INDICATOR LIGHTS AND LEFT GEAR WOULD NOT ILLUOct 10, 2005 · N102QS · Beech 400A · Landing Gear Position and WarningSDR DJFA2005147Shimmy Dampener · wornUPON ARRIVAL AFTER APPROACH AND NORMAL LANDING WITH NORMAL DECELERATION USING THRUST REVERSERS, AND AFTER ACHIEVING TAXI SPEED OF A FAST PACED WALK, THE AIRCRAFT EXPERIENCED A SEVERE NOSEWHEEL VIBRATION. NORMAL BRAKING APPEARED TO BE LOST, AND EMERGENCY BRAKIOct 6, 2005 · N783TA · Beech 400A · Shimmy DamperSDR DXTA200501002Uplock Switch · out of adjustAFTER GEAR RETRACTION, RED GEAR UNSAFE LIGHT HANDLE STAYS ILLUMINATED, CYCLED GEAR THREE TIMES, SAME RESULT. ADJUSTED LEFT AND RIGHT MAIN LANDING GEAR DOOR UPLOCK SWITCHES IAW BEECHJET 400XP M/M CHAP 32-60-00, PERFORMED LANDING GEAR RETRACTIONS, OPERATIONAL COct 5, 2005 · N108QS · Beech 400A · Landing Gear Position and WarningSDR 2005FA0001463Servo · intermittentINVESTIGATED PILOT REPORT OF INTERMITTENT (RUDDER BOOST FAIL) ANNUNCIATOR LIGHT DURING TAKEOFF, CRUISE, AND CLIMB SEGMENTS. FOUND RUDDER SERVO WOULD SPIKE HIGH VOLTAGE BUT YAW DAMPER WOULD STAY ENGAGED. REPLACED RUDDER BOOST SERVO W/OVERHAULED REPLACEMENT UNOct 4, 2005 · N480LX · Beech 400A · Rudder Tab Control SystemSDR DJFA2005146Smoke · detectedDURING CRUISE FLIGHT, LT GENERATOR FAIL ANNUNCIATOR ILLUMINATED. AFTER APPROX 1-2 MIN, LIGHT SMOKE WAS VISIBLE IN THE LT SIDE OF COCKPIT. AN IMMEDIATE DESCENT WAS INITIATED, ANTI-ICING SYS FOR WINGS, HORIZ STAB, ENGINES WERE TURNED ON. AFTER ANTI-ICE WAS TUOct 4, 2005 · N457CW · Beech 400A · Air Distribution SystemSDR DJFA2005145Control Cable · brokenDURING A ROUTINE MAINTENANCE VISIT WHILE PERFORMING "A" LEVEL INSPECTION, CORROSION WAS FOUND ON THE RT WING MAIN INBOARD FLAP FOLLOW UP CABLE AT THE END SWEDGE FITTING. WHILE CHECKING THE INTEGRITY IF THE CABLE IN THE FITTING, THE CABLE COMPLETELY SEPERATED Sep 30, 2005 · N746TA · Beech 400A · Trailing Edge Flap Control SystemSDR DXTA200500991Bulb · burnedWITH GEAR DOWN, R MAIN GREEN LIGHT DID NOT ILLUMINATE. BULB TEST CHECKED GOOD. PERFORMED ALTERNATE GEAR EXTENSION. NO RED LIGHT TO INDICATE UNSAFE GEAR ONCE ALTERNATE GEAR EXTENSION CHECKLIST COMPLETED. RESET GEAR EMERGENCY EXTENSION SYSTEM PER HAWKER 400 Sep 29, 2005 · N108QS · Beech 400A · Landing Gear Position and WarningSDR DJFA2005142Terminal · looseKBNA - THE CREW REPORTED THAT SMOKE WAS COMING FROM THE WINDSHIELD HEATER SWITCHES DURING CLIMB-OUT. THE SWITCHES WERE TURNED OFF. AN EMERGENCY WAS DECLARED AND THE CREW DONNED OXYGEN MASKS. THE AIRCRAFT WAS RETURNED TO KBNA AND AN UNEVENTFUL LANDING WAS MASep 24, 2005 · N799TA · Beech 400A · Light System WiringSDR DJFA2005141Connector · defectiveCREW REPORTED DURING CRUISE FLT, HYDRAULIC PRESSURE INDICATED 2,000 PSI AND ON RED LINE. WHEN PRESSURE RELIEF SWITCH MOVED, HYDRAULIC PRESSURE INDICATED 100 PSI. DUE TO A LONGER RUNWAY LENGTH AIRCRAFT DIVERTED TO KLGB AND AN EMERGENCY DECLARED. A MANUAL GEASep 22, 2005 · N709TA · Beech 400A · Hydraulic Power System WiringSDR DXTA200500977Odor · detectedWHEN ENGINE, WING, AND TAIL ANTI ICE ON STRONG ODOR WAS PRESENT IN CABIN. ITEM IS UNDER INVESTIGATION.Sep 20, 2005 · N140QS · Beech 400A · Air Distribution SystemSDR 2005FA0001321Line · damagedDURING COMPLIANCE WITH INSPECTION PORTION OF SB NOTED CHAFE DAMAGE TO PN 128580101-1 NOTED CHAFE DAMAGE TO PN 128-580101-1 HYDRAULIC BRAKE LINE FROM ADJACENT FLOORBOARD ATTACH SCREW. DAMAGE FOUND LESS THAN 10 PERCENT OF TUBING WALL THICKNESS. RECOMMEND THATSep 12, 2005 · N907JE · Beech 400A · Landing Gear Brake SystemSDR DJFA2005138Cooling Turbine · dragging10 MINS AFTER T/O, SMOKY ELECTRICAL ODOR NOTICED. ODOR COMING FROM RT COCKPIT. NO SMOKE OR FIRE SEEN. DONNED O2 MASKS. RETURNED W/O INCIDENT. AFTER LANDING ODOR DISSIPATED. MX INSP CONNECTOR & WIRING. NO SIGNS OF HEAT OR ARCING. A/C POWERED FOR 5 HRS, Sep 11, 2005 · N740TA · Beech 400A · Cabin Cooling SystemSDR DXTA200500952Position Switch · inoperativeDURING CRUISE FLIGHT AT FL,360/.78 MACH THE LT DEPLOY LIGHT ILLUMINATED (THE DEPLOY ONLY-NO ARM OR UNLOCK.) DESCENDED AND PUSHED EMERGENCY STOW. THE BOTTOM PORTION OF THE EMERGENCY STOW THRUST REVERSER. ARM AND DEPLOY WERE NOW ILLUMINATED. THE DEPLOY LIGHT Sep 5, 2005 · N120QS · Beech 400A · Engine Thrust ReverserSDR DJFA2005137Flap System · out of adjustKPVD - KCLT TRIP ID 893929 DURING CLIMBOUT WHILE PASSING FL 260 AT A SPEED OF 250 KTS THE FLAP ASYMMETRY LIGHT ILLUMINATED WHILE THE FLAPS WERE SET AT ZERO DEGREES, AND INDICATING ZERO DEGREES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS DIVERTED TO KBDL.Sep 5, 2005 · N402CW · Beech 400A · Trailing Edge Flap Control SystemSDR 2005FA0001308Fastener · looseDURING SCHEDULED 1ST (D) INSPECTION FOUND HI-LOK PIN COLLAR LOOSE (UPPER HEX SECTION STILL INTACT) FOR (1) FASTENER (OF 3) ATTACHING PN 454A23202-3 LT VERTICAL STABILIZER PIVOT PLATE TO VERTICAL STABILIZER AFT SPAR, UPPER LT SIDE. AREA IS JUST BELOW WHERE PN Sep 2, 2005 · N907JE · Beech 400A · Horizontal Stabilizer StructureSDR DJFA2005136Controller · intermittentKMEM - KRUS TRIP ID 888513 THE CREW REPORTED THAT THE PITCH TRIM FAILED ON CLIMBOUT AT 10,500 FT 255 KTS. THE PITCH TRIM BEGAN OPERATING AT 30,000 FT, AND THEN FAILED AGAIN AT 12,500 FT DURING DESCENT. WHEN THE EMERGENCY PITCH TRIM WAS USED IT WAS OPERATING Aug 31, 2005 · N455CW · Beech 400A · Elevator Tab Control SystemSDR 2005FA0001305Wire · damagedINVESTIGATED REPORT OF HORIZONTAL STABILIZER TRIM INOPERATIVE AND SYSTEM CIRCUIT BREAKER TRIPPING WHEN TRIM ACTUATED ON LANDING. CREW REPORTED NORMAL TRIM OPERATIONS SLOW JUST PRIOR TO FAILURE. FOUND BARE WIRING IN COPILOTS CONTROL WHEEL AT PITCH TRIM SWITCHAug 30, 2005 · N494CW · Beech 400A · Flight Control System WiringSDR DJFA2005134Warning Light · illuminatedTHE CREW REPORTED THAT DURING TAKEOFF THE LEFT THRUST REVERSER UNLOCK AND LEFT THRUST REVERSER ARM LIGHTS ILLUMINATED. THIS WAS FOLLOWED BY THE ASSOCIATED MASTER WARNING AND EMERGENCY STOW LIGHTS ILLUMINATING. THE THRUST REVERSER WAS STOWED MANUALLY BY USE OAug 28, 2005 · N698TA · Beech 400A · Engine Thrust ReverserSDR AJC2005F00012Squat Switch · defectiveDEPARTED, ENROUTE, AFTER TAKEOFF THE CREW REPORTED THAT THE LANDING GEAR HANDLE WAS LOCKED IN THE DOWN POSITION AND THEY COULD NOT RETRACT THE GEAR. THE LANDING GEAR DOWN LOCK OVER RIDE WAS ENGAGED AND THE GEAR RETRACTED NORMALLY. ON DESCENT, THE CREW REPORTAug 26, 2005 · N400HS · Beech 400A · Landing Gear Position and WarningSDR DJFA2005135Pump · wornTHE CREW REPORTED THAT THE HYDRAULIC PRESSURE WAS READING HIGH IN FLIGHT. WHEN THE HYDRAULIC PRESSURE DROPPED TO ZERO THE CREW CLOSED THE EMERGENCY DUMP VALVE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS DIVERTED TO KSAN DUE TO THE HIGHER RUNWAY LENGTH INAug 24, 2005 · N709TA · Beech 400A · Hydraulic Pump (Electric/Engine), MainSDR DXTA200500911Warning Light · illuminatedAFTER TAKEOFF RED AP PITCH TRIM FAIL LIGHT CAME ON AND AP KICKED OFF. AIRCRAFT CHECKLIST COMPLETED AND LANDED AS SOON AS PRACTICAL. ITEM IS UNDER INVESTIGATION.Aug 21, 2005 · N140QS · Beech 400A · Autopilot SystemSDR DXTA200500907Circuit Card · malfunctionedDURING T/O ROLL AT 70-80 KIAS OVERSPEED TONE ACTIVATED MOMENTARILY. REMOVED AND REPLACED NR 2 FCC CARD IAW HAWKER 400XP MM CH 22-13-00.Aug 19, 2005 · N108QS · Beech 400A · Autopilot SystemSDR DXTA200500908Pcb · defectiveAFTER T/O RED LIGHT IN HANDLE ILLUMINATED. CYCLED GEAR, GOT 3 GR AND 1 RD. RAN ALT GEAR EXT PROCEDURE. JACKED THE AIRCRAFT, SWUNG THE GEAR FOUND THAT THE MAIN GEAR DOORS WILL OPEN BUT WILL NOT CLOSE. TROUBLESHOT SYSTEM AND FOUND RELAY KIT IN PCB 162 BAD. RAug 19, 2005 · N116QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR 2005FA0001282Switch · failedLANDING GEAR SYS RED (GEAR UNSAFE) WARNING LIGHT REMAINED ILLUMINATED FOLLOWING GEAR EXTENSION WHILE LANDING. ALL (3) GREEN LANDING GEAR DOWN AND LOCKED POSITION INDICATING LIGHTS ILLUMINATED. AC FERRIED FOR REPAIRS. FOUND LT MLG DOOR POSITION SWITCH S097 FAug 17, 2005 · N430CW · Beech 400A · Landing Gear Position and WarningSDR DJFA2005131Control Valve · inoperativeTHE CREW REPORTED THAT WHILE IN CRUISE FLIGHT AT FL 250 THERE WAS EXTREMELY HOT AIR BLOWING FROM THE REAR VENT IN THE LAVATORY. THE AFT CABIN WALL WAS FOUND TO BE EXTREMELY HOT AND WAS SMELLING LIKE BURNING RUBBER. A REQUEST WAS MADE TO DIVERT THE AIRCRAFT, Aug 17, 2005 · N731TA · Beech 400A · Cabin Pressure Control SystemSDR DJFA2005130Engine · odorDURING CRUISE FLIGHT WHILE AT 28,000 FT BOTH PILOTS NOTICED A STRONG ENVIRONMENTAL ODOR IN THE COCKPIT. THE CREW DONNED OXYGEN MASKS AND REVIEWED THEIR CHECKLIST. WHEN THE LEFT CABIN PRESSURE SOURCE WAS SELECTED THE ODOR HAD IMMEDIATELY DISSIPATED. THE FLT WAug 16, 2005 · N696TA · Beech 400A · Engine (Turbine/Turboprop)SDR 2005FA0001246Connector · looseINVESTIGATED IN-FLIGHT (GPWS), (TERR), AND (WINDSHEAR) FAILE INDICATIONS. SYSTEM FAILURES CONFIRMED ON GROUND. FOUND AIRFRAME WIRING CONNECTOR (3446J1B UNSEATED FROM EGPWS UNIT CONNECTOR DUE TO TENSION ON WIRING BUNDLE. RESEATED CONNECTOR PINS AND RESECUREDAug 15, 2005 · N36997 · Beech 400A · Navigation System WiringSDR DJFA2005129Wire Harness · brokenON DESCENT, CREW NOTICED HYDRAULIC SYSTEM PRESSURE WAS INDICATING TOO HIGH. THE HIGH HYDRAULIC SYSTEM PRESSURE CHECKLIST REQUIRES A NO FLAP LANDING AND USE OF EMERGENCY BRAKES TO STOP THE AIRCRAFT. EMERGENCY DECLARED. DUE TO IT'S LONGER RUNWAY LENGTH, ACFTAug 12, 2005 · N440CW · Beech 400A · Hydraulic Power System WiringSDR DJFA2005128Circuit Board · intermittentON VISUAL APPROACH GEAR WAS SELECTED DOWN, NO GEAR MOVEMENT. APPROACH WAS MISSED, GEAR SELECTED UP. EMERGENCY DECLARED, ACFT RETURNED. ON RETURN GEAR LEVER WAS CYCLED SEVERAL TIMES WITH NO GEAR MOVEMENT. ON APPROACH GEAR SELECTED DOWN & APPROX 5 SEC GEAR EAug 10, 2005 · N457CW · Beech 400A · Landing Gear System WiringSDR 800GF080905Warning Horn · activatedTAKEOFF CONFIGURATION WARNING HORN SOUNDED ON TAKEOFF ROLL, THE CREW ABORTED THE TAKEOFF. ONCE CLEAR OF THE RUNWAY THE TAKEOFF CONFIGURATION WAS CHECKED AND RESET, WITH NO FURTHER PROBLEM.Aug 9, 2005 · N800GF · Beech 400A · Stabilizer Position IndicatingSDR DJFA2005127Line · rupturedON LANDING ROLL AS THE A/C SLOWED THROUGH 55 KTS BRAKE PRESSURE WAS LOST AND THE THRUST REVERSERS WOULD NOT DEPLOY. THE EMERGENCY BRAKES WERE APPLIED TO STOP THE A/C. AT THAT POINT, THE HYD PRESSURE WAS INDICATING ZERO. WHILE AWAITING PARKING INSTRUCTIONS, Aug 7, 2005 · N708TA · Beech 400A · Hydraulic System, MainSDR DJFA2005126Sump · openKSGR - KHOU DURING CLIMB THE CREW NOTICED FUEL LEAKING FROM THE RIGHT WING TIP. THE FUEL WAS COMING FROM TWO AREAS. THE FIRST BEING THE WING TIP AREA WHICH PRODUCED A FIVE FOOT VAPOR TRAIL. THE SECOND AREA WAS FROM THE SPOILER, ABOUT ONE FOOT IN FROM THE OUAug 6, 2005 · N792TA · Beech 400A · Fuel StorageSDR DJFA2005125Master Cylinder · leakingTHE CREW REPORTED UPON LANDING, THERE WERE NO BRAKES. USED THE EMERGENCY BRAKE SYSTEM TO STOP THE AIRCRAFT. THE CREW TRIED THE NORMAL BRAKES AFTER ROLLOUT ONTO THE TAXIWAY AND THE BRAKES WERE AVAILABLE BUT WERE JERKY. MAINTENANCE FOUND THE PILOTS RIGHT MASAug 3, 2005 · N793TA · Beech 400A · Master Cylinder/Brake ValveSDR DJFA2005123Actuator · unserviceableTHE CREW REPORTED, AFTER LEVELING OFF AT 11,000 FT, ATTEMPTED TO TRIM THE NOSE OF THE A/C DOWN. WHILE PASSING 200 KTS, IT WAS NOTED THAT NO FURTHER TRIM WAS AVAILABLE AND THE CREW HAD REDUCED POWER. THE CO-PILOT HAD ATTEMPTED TO TRIM THE NOSE DOWN WITH THE Aug 2, 2005 · N708TA · Beech 400A · Elevator Tab Control SystemSDR 2005FA0001138Pressure Switch · failedRT WING OVERPRESSURE ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT. FOUND S128 PRESSURE SWITCH TO HAVE CONTINUITY WITH NO PRESSURE SWITCH TO HAVE CONTINUITY WITH NO PRESSURE APPLIED. REPLACED SWITCH ASSY WITH NEW UNIT IAW MM, OPERATIONS NORMAL. (K)Aug 1, 2005 · N432CW · Beech 400A · Fuel Quantity IndicatorSDR DJFA2005122Downlock Switch · false indicationON APPROACH, CREW RECEIVED 2 GREEN & NO RED GEAR INDICATIONS. NLG LIGHT WOULD NOT ILLUMINATE, BUT LIGHT WOULD TEST. NO CHANGE IN GEAR DOWN INDICATION WHEN CREW CYCLED MLG TWICE. TOWER HAD CONFIRMED NLG DOWN DURING A LOW APPROACH, BUT AURAL "TOO LOW GEAR" WAJul 28, 2005 · N898TA · Beech 400A · Landing Gear Position and WarningSDR AJC2005F00009Valve · failedAIR RETURNED DUE TO AIR CONDITIONING FAIL LIGHT ILLUMINATED AND CABIN REVERTED TO EMERGENCY PRESSURIZATION MODE. AIRCRAFT ISSUED SPECIAL FLIGHT PERMIT, FOR MAINTENANE AT SERVICE CENTER. MAINTENANCE FOUND THE CABIN TEMPERATURE CONTROL VALVE TO BE DEFECTIVE. RJul 27, 2005 · N127BW · Beech 400A · Cabin Temperature Control SystemSDR DXTA200500859Transmitter · inoperativeAFTER TAKEOFF, AFTER SELECTING FLAPS 0 " FLAP ASSM " ANNUNICATOR ILLUMINATED. FLYING PILOT NOTICED NO CONTROL PROBLEMS. ANNUNICATOR EVENTULLY EXTINGUISHED. TROUBLESHOT SYSTEM AS PER WDM IN 400 XP MM CM 27-50-00, REMOVED AND REPLACED LT AND RT FLAP POSITIONJul 18, 2005 · N117QS · Beech 400A · Trailing Flap Position Indicating SystemSDR DJFA2005121Downlock Switch · out of adjustTHE CREW REPORTED THAT THE NOSE WHEEL DID NOT INDICATE DOWN WHEN THE GEAR WAS EXTENDED FOR LANDING IN KDAL. THE LIGHT DID ILLUMINATE WHEN TESTED. WHEN THE FLAPS WERE EXTENDED TO 30 DEGREES, AND THE THROTTLES REDUCED TO IDLE THE GEAR WARNING HORN DID NOT SOUNJul 18, 2005 · N731TA · Beech 400A · Landing Gear Position and WarningSDR DXTA200500844Bulb · burned outLOWERED GEAR HANDLE AND ONLY LEFT MAIN GEAR ILLUMINATED DOWN. RAN GEAR EXTENSION CHECKLIST AND STILL ONLY INDICATED LEFT MAIN DOWN. LANDING WAS UNEVENTFUL. REPLACED INDICATOR LIGHT BULBS WITH NEW AND PERFORMED LANDING GEAR RETRACTION TEST IAW HAWKER 400XP MJul 17, 2005 · N115QS · Beech 400A · Landing Gear Position and WarningSDR ERYR682DCable · brokenFLAP FOLLOW-UP CABLE WAS DISCOVERED CORRODED AND BROKEN IN HALF DURING AN INSPECTION.Jul 15, 2005 · N746TA · Beech 400A · Trailing Edge Flap Control SystemSDR 2005FA0000960Cable · brokenFLAP FOLLOW-UP CABLE WAS DISCOVERED CORRODED AND BROKEN IN HALF DURING AN INSPECTION.Jul 15, 2005 · N746TA · Beech 400A · Trailing Edge Flap Control SystemSDR DXTA200500824Connector · corrodedON APPROACH INTO ASE FLAPS LOCKED UP AT 10 DEGREES. DIVERTED TO GJT FOR LANDING AT FLAPS 10. TROUBLESHOT FAULT BY OPENING THROTTLE QUAD AND CLEANED, LUBED. INSPECTION FLAP LEVER AND FOUND NO FAULT. INSPECTED 10 DEG FLAP SWITCH AND ACTUATOR SWITCH. BOTH CHJul 8, 2005 · N117QS · Beech 400A · Trailing Edge Flap Control SystemSDR DJFA2005120Landing Gear · unwanted deployWHILE IN CRUISE FLT AT FL 260 AT 300 KTS, NLG DROPPED OUT OF WW. CREW SLOWED A/C TO BELOW 200 KTS AND REQUESTED A LOWER ALT. L/G WAS CYCLED UP AND ALL GEAR REMAINED RETRACTED. A/C WAS LANDED W/O FURTHER INCIDENT. GEAR WAS INSPECTED FOLLOWING LANDING AND A Jul 3, 2005 · N749TA · Beech 400A · Landing Gear Retraction/Extension System
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