Beech 400A

Service difficulty reports · 1,397

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  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 DJFA2007039Rib · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE DISCOVERED A CRACK IN A VERTICAL STABILIZER RIB ABOVE THE ELEVATOR BELLCRANK MOUNTING BRACKET. CRACK WAS .5" LONG AND TERMINATED TO A TOOLING HOLE. CRACK WAS REPAIRED IAW ENGINEERING DATA.Mar 30, 2007 · N789TA · Beech 400A · Vertical Stabilizer, Spar/RibSDR DJFA2007038Trim Switch · stickingTRIP NR 1160942 CREW REPORTED ROLL TRIM RUNAWAY. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. MAINTENANCE FOUND THE ROLL TRIM SWITCH STUCK. THE SWITCH WAS REPLACED.Mar 30, 2007 · N455CW · Beech 400A · Aileron Tab Control SystemSDR DJFA2007037Starter Gen · vibratesTRIP NR 1161270 CREW REPORTED SEVERE AIRFRAME VIBRATION COMING FROM THE RT SIDE. DECISION WAS MADE TO DIVERT. MAINTENANCE DISCOVERED THE RT STARTER GENERATOR AS CAUSE OF THE VIBRATION; POSSIBLE BEARING FAILURE OR WARPED STATOR ASSEMBLY. THE GENERATOR WAS REMar 29, 2007 · N454LX · Beech 400A · Starter-GeneratorSDR DJFA2007036Frame · crackedDURING A SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACK IN THE NR 1 ENGINE AFT NACELLE SUPPORT FRAME. THE CRACK WAS ABOUT .25 INCH, LOCATED ON THE IB SIDE JUST FWD OF THE TR AND JUST ABOVE THE PYLON AT ABOUT THE 0930 POSITION LOOKING AFT. CRACK WAS REPAIREDMar 28, 2007 · N785TA · Beech 400A · Nacelle/Pylon, Frame/Spar/RibSDR DXTA200702048Oil System · overtempON TAKEOFF, NOTICED YAW JUST BEFORE ROTATION. NORMAL TAKEOFF. WHEN LEVEL AT 3000 FT - 200KTS NOTICED RT ENGINE OIL TEMP IN RED. REDUCED THRUST OIL TEMP OUT OF RED, LANDED. FOUND RIGHT ENGINE OIL TEMP/PRESS GAUGE INCORRECT. REMOVED RIGHT ENGINE OIL TEMP/PRESMar 25, 2007 · N142QS · Beech 400A · Turbine Engine Oil SystemSDR DJFA2007034Annunciator · inoperativeTRIP NR 1154624 - CREW REPORTED NO GREEN GEAR DOWN AND LOCKED LIGHTS. CREW ACCOMPLISHED EMERGENCY GEAR EXTENSION AND DECLARED EMERGENCY. MAINTENANCE DISCOVERED THE LANDING GEAR INDICATOR CAPSULE INOPERATIVE. THE CAPSULE WAS REPLACED.Mar 22, 2007 · N467LX · Beech 400A · Landing Gear Position and WarningSDR DJFA2007033Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION, THE LT AND RT IB HORIZONTAL STABILIZER, BOTH LT AND RT RIBS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 7Mar 22, 2007 · N741TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2007032Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION, THE LT AND RT IB HORIZONTAL STABILIZER, BOTH LT AND RT RIBS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 7Mar 22, 2007 · N789TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA200702040Unknown · odorUNIDENTIFIED ENVIROMENTAL SYSTEM ODOR BEGAN ENTERING THE CABIN PASSING 7000 FT WITH THE THROTTLES NEAR IDLE IN DESCENT. VISUALLY INSPECTED RT AND LT ENGINE INTAKE AND EXHAUST, NO DISCREPANCIES WERE NOTED. GAINED ACCESS TO THE REFRIGERATION UNIT AND VISUALLY IMar 21, 2007 · N161QS · Beech 400A · Air Distribution SystemSDR DJFA2007031Pin · missingUPON INSPECTION OF THE RT MAIN LANDING GEAR MAINTENANCE DISCOVERED THE UPPER TORQUE LINK PIVOT PIN WAS MISSING ITS RETAINING PIN. THE PIVOT PIN HAD SLID OUT ABOUT .5 INCHES. ADDITIONALLY, IT APPEARS THAT THE GEAR HAS NOT BEEN PROPERLY LUBRICATED. AIRCRAFT Mar 21, 2007 · N471LX · Beech 400A · Main Landing GearSDR 40675Actuator · inoperativeDIFFICULTY OCCURED UPON DESCENT. PILOT RECIEVED A WARNING PITCH TRIM WAS NOT SYNCRONIZED WITH AUTOPILOT SYSTEM AND TO PREPARE FOR RESISTANCE WHEN AUTOPILOT IS DISCONNECTED. PITCH TRIM ACTUATOR WAS FOUND INOPERATIVE IN THE EMERGENCY MODE/AUTOPILOT MODE. REPLMar 20, 2007 · N790SS · Beech 400A · Stabilizer Position IndicatingSDR M40675Actuator · inoperativeDIFFICULTY OCCURRED UPON DESCENT. PILOT RECEIVED A WARNING PITCH TRIM WAS NOT SYNCHRONIZED WITH AUTOPILOT SYSTEM AND TO PREPARE FOR RESISTANCE WHEN AUTOPILOT IS DISCONNECTED. PITCH TRIM ACTUATOR WAS FOUND INOPERATIVE IN THE EMERGENCY MODE/AUTOPILOT MODE. REPLAMar 20, 2007 · N790SS · Beech 400A · Stabilizer Control SystemSDR DJFA2007030Downlock Switch · out of rigON ROLLOUT, AFTER LANDING, THE LT MAIN GEAR COLLAPSED. INITIAL INSPECTION REVEALED THE LT DOWN LOCK SWITCH OUT OF RIG AND THE OVER CENTER PIVOT JOINT APPEARED TO BE BINDING DUE TO LACK OF LUBRICATION. THE AIRCRAFT HAS NOT REACHED ITS FIRST SCHEDULED MAINTENANMar 16, 2007 · N466LX · Beech 400A · Landing Gear Position and WarningSDR DXTA200702023Landing Gear · inoperativeCOULD NOT GET RT MAIN GEAR LIGHT USED ALTERNATE GEAR EXTENSION. TROUBLESHOT SYSTEM AND FOUND RT MLG DOWNLOCK SWITCH TO BE SHORTED AND NOT REPORTING POSITION. REMOVED AND INSTALLED NEW SWITCH IAW HAWKER 400XP MM 32-60-00. OPS CHECK OF SYSTEM SHOWS NORMAL OPERAMar 15, 2007 · N131QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR DJFA2007028Reservoir · emptyTRIP NR 1153226, ON LANDING, CREW REPORTED HYDRAULIC LOW ANNUNCIATOR ILLUMINATED AND LOSS OF HYDRAULIC PRESSURE. EMERGENCY BRAKING WAS USED. MAINTENANCE DICOVERED HYDRAULIC RESERVOIR EMPTY. MAINTENANCE DISCOVERED THE HYDRAULIC PRESSURE LINE ON THE RIGHT HANDMar 9, 2007 · N790TA · Beech 400A · Hydraulic Reservoir, MainSDR 2007FA032201Servo · malfunctionedDIFFICULTY OCCURRED UPON DESCENT. PILOT DISENGAGED AUTO-PILOT AND FELT RESISTANCE IN THE ELEVATOR CONTROL SYSTEM. ON INSPECTION OF THE SYSTEM THE AUTO-PILOT ACTUATOR WAS FOUND PARTIALLY ENGAGED. UNIT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THIS AMar 8, 2007 · N188JF · Beech 400A · Auto Flight SystemSDR DJFA2007027Unknown · unknownTRIP NR 1152283/ CREW REPORTED AT FLIGHT LEVEL 380 IN CLEAR SKYS AND SMOOTH AIR A LOUD NOISE SOUNDED AND RANG OUT THROUGHOUT THE AIRCRAFT. AIRCRAFT PITCHED DOWN MOMENTARILY AND CREW DISENGAGED THE AP AFTER WHICH THE AIRCRAFT RETURNED TO NORMAL LEVEL FLIGHT. Mar 8, 2007 · N454LX · Beech 400A · Flight Control SystemSDR DJFA2007026Inlet · crackedDURING A SCHEDULED MAINTENANCE EVENT MAINTENANCE FOUND A CRACK ON THE RT ENGINE INLET RING AT THE 12 O'CLOCK POSITION. THE CRACK IS ABOUT .25 INCH LONG. MAINTENANCE REPLACED THE INLET.Mar 6, 2007 · N686TA · Beech 400A · Engine Air Intake SystemSDR DXTA200701998Engine · surgesAFTER LEVEL OFF FOLLOWING AN UNRESTRICTED CLIMB TO FL 380, LT ENGINE BEGAN TO SURGE +- 2 PERCENT N1 (APPROX). ENGINE SYNC-ON. EGT, N2 AND FUEL FLOW WERE ALSO FLUXUATING WITH FUEL FLOW =- 50 TO 75 PSI. ENGINE SYNC TURNED OFF WITH NO CHANGE (STILL FLUXUATING). BMar 4, 2007 · N149QS · Beech 400A · Engine (Turbine/Turboprop)SDR DXTA200701992Uplock Switch · malfunctionedRED LIGHT ON GEAR HANDLE REMAINS ON AFTER GEAR RETRACTION. JACKED AIRCRAFT PERFORMED GEAR RETRACT TEST MAIN GEAR INBD DOORS DID NOT CLOSE. TROUBLSHOT SYSTEM & FOUND RIGHT GEAR UPLOCK SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH & PERFORMED NUMEROUS GEAR SWINGSMar 3, 2007 · N122QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200701987Door · out of rigUPON GEAR RETRACTION RED LIGHT ON GEAR HANDLE REMAINS ON. DRAGGING NOISE HEARD FROM COCKPIT. SOUNDS LIKE GEAR DOORS DID NOT CLOSE. JACKED AIRCRAFT AND CONNECTED MULE AND GROUND POWER UNIT. PERFORMED GEAR CYCLE AND FOUND RIGGING OF NOSE GEAR DOORS PREVENTING NMar 2, 2007 · N122QS · Beech 400A · Landing Gear Door Retract SectionSDR DXTA200701982Unknown · warning lightUPON GEAR RETRACTION AFTER MISSED APPROACH IN KASE. RED LIGHT ON GEAR HANDLE REMAINED ON. DRAGGING NOISE DURING REMAINDER OF FLIGHT TO GRAND JUNCTIONS. GEAR EXTENSION WAS NORMAL. JACKED AIRCRAFT. PERFORMED 15 FAULT FREE GEAR SWINGS IAW 400A MM 32-00-00. NO DEMar 1, 2007 · N122QS · Beech 400A · Landing Gear SystemSDR 2007FA0000279Uplock · out of adjustFLIGHT CREW REPORTED RED LANDING GEAR HANDLE WARNING LIGHT STAYING ILLUMINATED AFTER GEAR RETRACTION. LANDING GEAR CYCLED SEVERAL TIMES, HANDLE WARNING LIGHT STAYED ILLUMINATED. FOUND NOSE LANDING GEAR UPLOCK NOT FULLY ENGAGING ADJUSTED NOSE LANDING GEAR UPLFeb 28, 2007 · N123QS · Beech 400A · Nose/Tail Landing GearSDR DXTA200701976Speed Brake · slowON APPROACH HAD A UNCOMMANDED TURN TO THE RT WITH SPEED BRAKES EXTENDED. AIRCRAFT WAS AT APPROACH SPEED. CHECKED LEFT AND RIGHT SPOILER CABLE TENSIONS FOUND NORMAL AT 82 FOUND IAW HAWKER 400XP M.M. CH 27-60-00 CHART 201. FOUND LEFT SIDE SPEEDBRAKE EXTENDING Feb 28, 2007 · N131QS · Beech 400A · Drag Control SystemSDR DJFA2007025Arm · crackedDURING A SCHEDULED MAINTENANCE EVENT, MAINTENANCE DISCOVERED A LARGE CRACK ON THE UPPER OB THRUST REVERSER ARM OF THE LT ENGINE. SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.Feb 28, 2007 · N408CW · Beech 400A · Engine Thrust ReverserSDR DXTA200701967Warning Light · illuminatedRED LIGHT ON GEAR HANDLE REMAINS ON WHEN GEAR IS RETRACTED. GEAR WAS CYCLED AND RED LIGHT REMAINED ILLUMINATED.Feb 26, 2007 · N123QS · Beech 400A · Landing Gear Position and WarningSDR DJFA2007023Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STABILIZER, THE RT RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. MAINTENANCE REFeb 25, 2007 · N755TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2007022Skin · crackedDURING A SCHEDULED MAINTENANCE EVENT, MAINTENANCE DISCOVERED A CRACK ON THE RH ELEVATOR LOWER SKIN APPROX. 9.5 INCHES FROM THE INBD END. THE CRACK TRANSECTS A RIVET HOLE FROM LEFT TO RIGHT AND IS APPROX .75" IN LENGTH. THE ELEVATOR WAS REPLACED.Feb 22, 2007 · N417LX · Beech 400A · Elevator, Plate/SkinSDR DIXA200700001Electrical Sys · odorFLIGHT CREW REPORTED HEARING A POPPING SOUND FROM BEHIND THE COCKPIT LT SIDEWALL AREA FOLLOWED BY A SLIGHT ELECTRICAL ODOR FOR A PERIOD OF 15 SECONDS. NO SYSTEMS WERE AFFECTED AS ALL WERE OPERATING NORMALLY FOR THE DURATION OF THE FLIGHT (1.2 HRS). MFG AIRCRAFFeb 22, 2007 · N314TL · Beech 400A · Electrical Power System WiringSDR DJFA2007021Intake · crackedDURING A SCHEDULED MAINTENANCE EVENT MAINTENANCE FOUND A CRACK ON THE ENGINE INLET RING AT THE 12 OCLOCK POSITION. THE CRACK WAS APPROX .67 INCH LONG AND TRANSECTED THE SCREW HOLE FROM THE AFT EDGE OF THE RING. MAINTENANCE IS REPLACING THE INLET RING. THE SFeb 19, 2007 · N465LX · Beech 400A · Engine Air Intake SystemSDR CA070314016Engine · vibration(CAN) ENGINE EXHIBITED HEAVY VIBRATION DURING CRUISE AND WAS SHUTDOWN IN FLIGHT. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED. (TC NR 20070314016)Feb 15, 2007 · Beech 400A · Engine (Turbine/Turboprop)SDR DXTA200701948Uplock Switch · malfunctionedRED LIGHT ON GEAR HANDLE REMAINS ON WHEN GEAR IS RETRACTED. GEAR WAS CYCLED ONE TIME AND RED LIGHT STILL DID NOT GO OUT. GEAR IS O.K. WHEN GEAR IS SELECTED DOWN.FOUND LEFT MAIN GEAR UPLOCK SWITCH READING HIGH RESISTANCE. REMOVED AND REPLACED SWITCH READING HIFeb 15, 2007 · N123QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200701937Seal · bindingAFTER CRUISING AT FL360 FOR APPROX. 90 MINUTES, UPON BEING CLEARED FOR DESCENT LEFT THROTTLE STUCK @ 97.0 N1, THROTTLE WOULD NOT BUDGE. FINALLY OUT OF FL240 IT CAME FREE & OPERATED NORMALLY. TEMP WAS -10 RAT. REMOVED OLD SEALS REPLACED WTH NEW. LUBED TELESCOPFeb 13, 2007 · N142QS · Beech 400A · Engine (Turbine/Turboprop)SDR DJFA2007019Seal · leakingTRIP NR 1141843 CREW REPORTED A NOXIOUS OILY SMELL WHEN ENGINE IS AT HIGH POWER SETTINGS CONTINUING THROUGH CLIMB THEN DISSIPATING DURING CRUISE. MAINTENANCE FOUND BROWN RESIDUE INTO BLEED DUCT WITH SOME CRYSTALLIZATION AND SUSPECTS LEAKING AT CENTRIFUGAL COMFeb 13, 2007 · N898TA · Beech 400A · Turbine Engine Compressor SectionSDR DXTA200701942Brake Assy · unknownBOTH SIDES BRAKES HAVE A LOT OF TRAVEL WITH NO BRAKING THEN IT BRAKES HARD TURNING TO ONE SIDE. AFTER BLEEDING THE BRAKES WITH THE HYDRAULIC MULE AND CHECKING THE MASTER CYLINDER RESERVOIR, TAXI CHECKED AND FOUND THE BRAKES TO BE OPERATING NORMALLY IAW HAWKER Feb 11, 2007 · N161QS · Beech 400A · Landing Gear Brake SystemSDR DXTA200701944Downlock Switch · inoperativeRT MLG DOWN AND LOCKED LIGHT DID NOT ILLUMINATE WHEN GEAR SELECTED DOWN. RAN THE CHECKLIST, ALTERNATE GEAR EXTENSION PROCEDURE WAS NOT NECESSARY. LANDED WITHOUT INCIDENT AND THE LIGHT CAME BACK ON STEADY AFTER TOUCH DOWN. REPLACED RH MAIN GEAR DOWN LOCK SWITCHFeb 9, 2007 · N145QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200701924Indicator · intermittentBOTH LT AND RT MAIN GEAR INDICATOR LIGHTS WERE INTERMITTENT AND AT TIMES WOULD NOT ILLUMINATE AT ALL WHEN GEAR WAS SELECTED DOWN, ALL OTHER INDICATIONS WERE, CORRECT. ACCOMPLISHED CHECKLIST AND LANDED NORMALLY ALTERNATE GEAR EXTENSION WAS NOT USED. TROUBLESHOTFeb 8, 2007 · N125QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200701922Indicator · no indicationWHEN GEAR WAS PLACED IN DOWN POSITION. THE RT GREEN R DID NOT ILLUMINATE. OHMED OUT GEAR INDICATOR HARNESS NO DEFECTS WERE NOTED. ACCESSED CONNECTOR P272 IN R/H WHEEL WELL OHMED OUT DOWN LOCK SWITCH FOUND HIGH RESISTANCE THROUGH CLOSED CONTACTS ON SWITCH. NOTFeb 8, 2007 · N120QS · Beech 400A · Landing Gear Position and WarningSDR DJFA2007017Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STABILIZER, THE RT RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. SDR WILL BE UPFeb 7, 2007 · N790TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2007015Hmu · malfunctionedTRIP NR 1136187, CREW REPORTED WHILE CLIMBING THROUGH FL260 THEY NOTICED A YAW OF THE AIRCRAFT AND DISCOVERED THE LT ENGINE HAD ROLLED BACK TO 62 PERCENT N1. THEY TURNED THE ENGINE ANTI-ICE ON AND TURNED THE EEC OFF AND PUSHED THROTTLES FORWARD WITH NO IMPROVFeb 5, 2007 · N755TA · Beech 400A · Fuel Controlling SystemSDR DEBD624B0207Bolt · brokenA WHEEL THRU BOLT BROKE WHILE BEING TORQUED DURING WHEEL REASSEMBLY AFTER A TIRE CHANGE.Feb 2, 2007 · N624B · Beech 400A · Wheel/Ski/FloatSDR DXTA200701905Brake Assy · malfunctionedBRAKES DO NOT WORK UNTIL MAXIMUM FORCE IS APPLIED (ON BOTH SIDES). HYDRAULIC PRESSURE NORMAL AND NO LIGHTS. PERFORMED VISUAL INSPECTION OF BRAKE ASSEMBLIES, MASTER CYLINDERS, MIXING & ANTISKID VALVES AND ASSOCIATED LINES. NO DEFECTS OR LEAKAGE FOUND. VERIFIEDFeb 1, 2007 · N161QS · Beech 400A · Landing Gear Brake SystemSDR BUE2007F00001Computer · faultedSTICK SHAKER ACTIVATED SHORTLY AFTER ROTATION, STAYED ACTIVATED UNTIL 240KIAS. INDICATOR AND ANGLE OF ATTACK (AOA) INDEXER READ NORMAL. FLAPS WERE AT 10 DEGREES, LANDING GEAR WAS DOWN. AOA HEAT WAS SELECTED. AIRCRAFT HAD DEICE FLUID APPLIED. INSP OF EMPENJan 30, 2007 · N9PW · Beech 400A · Stall Warning SystemSDR DXTA200701889Landing Gear · unknownAFTER T/O THE LANDING GEAR HANDLE LIGHT REMAINED ILLUMINATED. AIRSPEED WAS KEPT BELOW 190 KTS AND SLIGHT VIBRATION FELT. UPON EXTENSION LIGHT EXTINGUISHED AMD 3 GREEN LIGHTS. JACKED ACFT., INSPECTED MLG, NO FAULTS FOUND. PERFORMED 10 GEAR CYCLES, NO FAULTS NJan 29, 2007 · N142QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR DJFA2007012Servo · bindingTRIP NR 1132520 AFTER LANDING CREW REPORTED THAT WITH THE YAW DAMPER ENGAGED RUDDER PEDDALS WERE VERY STIFF. MAINTENANCE DISCOVERED THE RUDDER SERVO CLUTCH STICKING. THE MOUNT WAS REPLACED AND THE CABLE TENSIONS ADJUSTED.Jan 24, 2007 · N798TA · Beech 400A · Autopilot Main ServoSDR DJFA20070011Wire Harness · chafedTRIP NR 1130219 ON TAKEOFF ROLL CREW NOTED FLUCTUATION IN ELECTRICAL SYSTEM FOLLOWED BY EMERGENCY BUS FAIL AND BATT CUTOFF CAUTION LIGHTS. TAKEOFF WAS ABORTED. MAINTENANCE DISCOVERED WIRE HARNESS ROUTED ON LT SIDE OF THE AIRCRAFT RUNS OVER THE PILOTS PFD ANDJan 18, 2007 · N715TA · Beech 400A · Electrical Power System WiringSDR DJFA2007009Support Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LT IB HORIZONTAL STABILIZER RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. SDR WILL BE UPDATED UPJan 15, 2007 · N482LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2007010Antenna · brokenTRIP NR 1129456 ON REPO, CREW NOTICED A LOUD NOISE COMING FROM THE REAR OF THE AIRCRAFT AT FL030 AND 250 KTS. ON LANDING, MAINTENANCE DISCOVERED A LARGE PORTION OF THE NR 2 VHF ANTENNA HAD BROKEN OFF AND DEPARTED THE AIRCRAFT, THE FLIGHT PHONE ANTENNA WAS DAMAJan 15, 2007 · N768TA · Beech 400A · VHF Communications SystemSDR DJFA2007008Unknown · odorTRIP NR 1129156 CREW NOTED BURNING ODOR FROM LAV AREA DURING CLIMB ENROUTE. AIRCRAFT DIVERTED. MAINTENANCE PERFORMED NUMEROUS GROUND RUNS WITH CREW ON BOARD AND WAS UNABLE TO DUPLICATE THE DISCREPANCY.Jan 15, 2007 · N469LX · Beech 400A · Air Distribution SystemSDR DXTA200701855Reservoir · underservicedON TAXI OUT, RT BRAKE PEDAL, CAPT, PRESSED TO FLOOR. NO PRESSURE OR BRAKING ACTION. LT PEDAL HAD PRESSURE BUT ALSO NO BRAKING ACTION. APPLIED EMER BRAKE TO STOP. OPS CHECKED BRAKES, FOUND TO BE SPONGY. PERFORMED PILOT AND COPILOT BRAKE SYSTEM BLEEDING (BLEED Jan 14, 2007 · N149QS · Beech 400A · Hydraulic Reservoir, Main
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