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 2006FA0000930Rib · crackedTHE HORIZONTAL STABILIZER RIB (RT SIDE) LOCATED UNDER THE ROLLER BRACKET HAD A CRACK IN IT. THIS ITEM IS COVERED UNDER COMMUNIQUÉ NR 70.Sep 20, 2006 · N939GP · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006319Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RIGHT INBOARD HORIZONTAL STABILIZER NOSE RIB STRUCTURE (PART NUMBER 45A21085-004) WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINEDSep 14, 2006 · N466CW · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006318Fairing · bentTHE CREW REPORTED THAT THE IB TOP END OF THE LT ENGINE THRUST REVERSER FAIRING WAS BENT UP AT A 45 DEGREE ANGLE, AND THE BOTTOM WAS BENT DOWN APPROXIMATELY ONE INCH WHERE THE THRUST REVERSER ROD IS HITTING THE FAIRING. MAINTENANCE DISCOVERED THAT THE LT THRUSSep 10, 2006 · N434LX · Beech 400A · Engine Thrust ReverserSDR 2006FA0000952Line · chafedDURING A SCHEDULED INSPECTION FOUND PN 128580101-1, BRAKE LINE ASSY CHAFE DAMAGED BY EXCESS LENGTH CABIN FLOOR PANEL ATTACH SCREW AS DESCRIBED IN MFG SB 53-3511. REPAIR REQUIRED SPLICING IN OF NEW BRAKE LINE SEGMENT IAW SB 53-3511. HAVE FOUND THIS CONDITION Sep 8, 2006 · N785TA · Beech 400A · Landing Gear Brake SystemSDR DJFA2006316Line · chafedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A (D) LEVEL INSPECTION A BRAKE RETURN LINE WAS FOUND TO BE CHAFING FROM A SCREW THAT SECURES THE CENTER COCKPIT TO CABIN FLOORBOARD. INSPECTION AND REPAIR OF THIS AREA IS OUTLINED IN MFG SB 53-3511. THE CSep 8, 2006 · N715TA · Beech 400A · Hydraulic System, MainSDR CA060906013Engine · flamed out(CAN) THE AIRCRAFT ENTERED RAIN AND TURBULENCE AT 40K FEET AND THE ENGINE FLAMED OUT. ENGINE ANTI-ICE AND CONTINUOUS IGNITION HAD NOT BEEN SELECTED. THE ENGINE WAS SUCCESSFULLY RE-STARTED AT 28K FEET. MFG WILL MONITOR THE INVESTIGATION OF THIS EVENT AND WILSep 7, 2006 · Beech 400A · Engine (Turbine/Turboprop)SDR DJFA2006312Bulb · blownKDSM - KTEB WHEN THE LANDING GEAR WAS EXTENDED FOR LANDING IN KTEB THE CREW DID NOT RECEIVE THE GEAR POSITION INDICATION FOR THE RIGHT MAIN GEAR. AN ALTERNATE GEAR EXTENSION WAS PERFORMED AND THE AIRCRAFT WAS LANDED IN KTEB WITHOUT FURTHER INCIDENT. MAINTENSep 5, 2006 · N462LX · Beech 400A · Landing Gear Position and WarningSDR DJFA2006313Hydraulic Line · chafedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A C-LEVEL INSPECTION A BRAKE LINE WAS FOUND TO BE CHAFING FROM A SCREW THAT SECURES THE CENTER COCKPIT TO CABIN FLOORBOARD. INSPECTION AND REPAIR OF THIS AREA IS OUTLINED IN BEECHCRAFT SERVICE BULLETIN 53-Sep 4, 2006 · N785TA · Beech 400A · Landing Gear Brake SystemSDR DJFA2006309Thrust Reverser · activatedWHILE LEVELING OUT AT 10,000 FEET, CREW HEARD A BUMP WHILE THE AIRCRAFT YAWED TO THE RT. NO ABNORMAL INDICATIONS WERE RECEIVED IN THE COCKPIT. CREW ACTIVATED EMERGENCY STOW BUTTON AFTER DETERMINING THAT RT THRUST REVERSER HAD PARTIALLY DEPLOYED. AFTER REACHAug 30, 2006 · N795TA · Beech 400A · Engine Thrust ReverserSDR DJFA2006307Printed Ckt Board · shortedKRWI - WHILE ON CLIMBOUT THE NR 1 INVERTER FAILED AND WAS FOLLOWED BY PUNGENT FUMES FROM THE LOWER CIRCUIT BREAKER PANEL. THE AIRCRAFT WAS RETURNED TO KRWI WHERE AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND CONTACTS A2 AND A1 OF THE K5 RELAY ON PRINTED Aug 27, 2006 · N898TA · Beech 400A · AC InverterSDR 2006FA0000891Power Supply · inoperativeDURING SCHEDULED 12 MONTH/200 HR INSPECTION OF AIRCRAFT SERVICES EMERGENCY LIGHTING SYS INSTALLED UNDER STS ST00344AT FOUND AFT POWER INSTALLED UNDER STC ST00344AT FOUND AFT POWER SUPPLY TO HAVE NO OUTPUT. VERIFIED POWER SUPPLY RECEIVING BATTERY CHARGING VOLTAug 24, 2006 · N45RK · Beech 400A · Emergency LightingSDR DXTA200601563Downlock Switch · faultyON GEAR EXTENSION HAD INDICATION OF LT AND RT MAINS ONLY NO NOSE INDICATION. PERFORMED THE LANDING GEAR NOT DOWN AND LOCKED CHECKLIST AFTER CYCLING THE GEAR AGAIN. LANDED NORMALLY. NOSE GEAR INDICATED GREEN AFTER LANDING. REPLACED NOSE GEAR DOWN LOCK SWITCH WAug 19, 2006 · N131QS · Beech 400A · Landing Gear Position and WarningSDR DJFA2006306Downlock Switch · faultyKSLC - KOMA THE CREW DID NOT RECEIVE THE RIGHT MAIN GEAR DOWN AND LOCKED INDICATION WHEN THE GEAR WAS EXTENDED WHILE ON APPROACH FOR LANDING IN KOMA. WHEN THE LIGHT WAS TESTED IT OPERATED NORMALLY. AN EMERGENCY GEAR EXTENSION WAS PERFORMED AND A FLY-BY PASTAug 17, 2006 · N480LX · Beech 400A · Landing Gear Position and WarningSDR DJFA2006305Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RT IB HORIZONTAL STABILIZER NOSE RIB STRUCTURE AND BOTH LT AND RT RIB BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IAug 14, 2006 · N795TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DXTA200601553Air Duct · odorDURING FLIGHT FROM SLC TO COS, HAD A BURNING SMELL IN COCKPIT AND CABIN WHEN ENG AND WING ANTI-ICE WAS TURNED ON, SMELL WAS STRONGER IN CABIN. FELT SIDE PANEL IN CABIN BUT THEY WERE NOT EXCESSIVELY WARM. M2B: INSPECTED WING ANTI ICE DUCTS FOR CONDITION AND LAug 13, 2006 · N114QS · Beech 400A · Air Distribution SystemSDR 800GF081206Switch · malfunctionedLANDING GEAR DID NOT COME DOWN WHEN SELECTED. PERFORMED EMERGANCE EXTEND AND LANDED WITH NO PROBLEMS. FOUND SWITCH IN GEAR CONTROLLER INTERMITTENTERLY HAVING HIGH RESISTANCE. (K)Aug 12, 2006 · N800GF · Beech 400A · Landing Gear Retraction/Extension SystemSDR DJFA2006302Water Separator · blockedKATL - KBED DURING FLIGHT AT A REDUCED POWER SETTING OF 88% N1 A PASSENGER REPORTED SMELLING SMOKE IN THE CABIN AREA. AN EMERGENCY WAS DECLARED BY THE CREW AND THE AIRCRAFT WAS DIVERTED TO KRDU WHEN AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE REPLACED THE CAug 12, 2006 · N417LX · Beech 400A · Humidity Control SystemSDR DJFA2006299Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE LEFT AND RIGHT INBOARD HORIZONTAL STABILIZER BEARING SUPPORT RIBS WERE FOUND CRACKED NEXT TO THE SIDE ROLLER BRACKET. DETAILED INSPECTION INSTRUCTIONS OF THIS Aug 3, 2006 · N446CW · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006298Link Assy · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING AN (A) LEVEL INSPECTION, THE LT LOWER THRUST REVERSER BUCKET IDLER LINK ASSY WAS FOUND CRACKED. THE LT THRUST REVERSER LOWER BUCKET IDLER LINK ASSY WAS REPLACED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.Aug 2, 2006 · N447LX · Beech 400A · Engine Thrust ReverserSDR DJFA2006296Wire Harness · false activationKAPA - KAPA, WHILE IN CRUISE FLIGHT AT 34,000 FT THE RT THRUST REVERSER DEPLOY LIGHT ILLUMINATED. AFTER THE CREW PUSHED THE EMERGENCY STOW BUTTON, THE LIGHT REMAINED ILLUMINATED. WHILE DESCENDING FROM 29,000 FT TO RETURN TO KAPA, A "POP" SOUND WAS HEARD ANDAug 2, 2006 · N466CW · Beech 400A · Engine Thrust ReverserSDR DJFA2006297Bracket · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING AD 2002-01-23 A CRACK WAS DISCOVERED ON THE LT ENGINE CARRY THROUGH MOUNT BRACKET. THE LT ENGINE WAS REMOVED, AND THE LT AFT CARRY THROUGH BRACKET WAS REPLACED REFERENCING RAYTHEON ENGINEERING DRAWING 128-Aug 1, 2006 · N447LX · Beech 400A · Engine Mount SectionSDR 2006FA0000832Switch · damagedDURING SCHEDULED INSPECTION, FOUND LANDING GEAR WARNING HORN WOULD NOT OPERATE WITH LT POWER LEVER RETARDED. FOUND THROTTLE QUADRANT SWITCHES S25 AND S26 TO HAVE HIGH INTERNAL RESISTANCE. REPLACED SWITCHES AND ADJUSTED AS REQUIRED IAW MM. LANDING GEAR WARNIJul 26, 2006 · N334SR · Beech 400A · Landing Gear SelectorSDR DJFA2006292Buss Bar · arcedKSFB TRIP THE CREW REPORTED THAT UPON STARTING THE RIGHT ENGINE ALL POWER TO THE AIRCRAFT FAILED EXCEPT FOR STANDBY POWER. A GROUND POWER UNIT WAS CONNECTED AND SUFFICIENT VOLTAGE WAS SUPPLIED. WHEN RECYCLING THE POWER SWITCHES, THE AIRCRAFT WOULD BEGIN TO BRJul 24, 2006 · N497CW · Beech 400A · Electrical Power System WiringSDR DJFA2006290Switch · intermittentTRIP ID NR 1049878 WHILE CLIMBING THROUGH FL 280 THE CREW HEARD A (CLUNK) IN THE CENTER CONSOLE AND THE RT THRUST REVERSER DEPLOY ANNUNCIATOR ILLUMINATED. THRUST REVERSER EMERGENCY STOW SWITCH WAS PUSHED AND THRUST REVERSER CONTROL CIRCUIT BREAKER WAS PULLEDJul 20, 2006 · N749TA · Beech 400A · Engine Thrust ReverserSDR DJFA2006289Bulb · blownKMRY - KOAK. AFTER THE LANDING GEAR WERE EXTENDED FOR LANDING THE RIGHT MAIN GEAR DOWN INDICATION DID NOT ILLUMINATE. THE CREW PERFORMED A GO-AROUND SO THEY COULD VERIFY GEAR POSITION BEFORE LANDING. NO GEAR WARNING HORN, AND NO RED GEAR HANDLE LIGHT WERE RJul 20, 2006 · N709TA · Beech 400A · Landing Gear Position and WarningSDR 2006FA0000833Brake · seizedDURING INITIAL TAKEOFF ROLL, FOLLOWING POSITIVE PARKING BRAKE RELEASE CHECK, LT MAIN WHEEL BRAKE LOCKED-UP. TAKEOFF ABORTED DUE TO SLOW ACCELERATION, POOR DIRECTIONAL CONTROL. UNABLE TO MOVE AIRCRAFT UNTIL RT BRAKE APPLIED AND RELEASED, THEN TAXI-IN NORMAL. Jul 18, 2006 · N476LX · Beech 400A · Landing Gear Brake SystemSDR DJFA2006288Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER BRACKET INSPECTION THE LEFT INBOARD HORIZONTAL STABILIZER NOSE RIB STRUCTURE WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN BEECHJET COMMUNIJul 18, 2006 · N456CW · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006287Thrust Reverser · brokenTHE CREW REPORTED THAT AFTER LANDING THE RIGHT THRUST REVERSER DID NOT DEPLOY. BOTH ARM AND UNLOCK LIGHTS ILLUMINATED BUT THE DEPLOY LIGHT DID NOT. DURING THE POST FLIGHT INSPECTION A BROKEN THRUST REVERSER DRIVER ARM WAS FOUND AND THE FAIRING WAS BUCKLED. Jul 18, 2006 · N410CW · Beech 400A · Engine Thrust ReverserSDR DJFA2006285Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION AS PART OF THE A LEVEL INSPECTION THE LT IB HORIZONTAL STABILIZER NOSE RIB STRUCTURE WAS FOUND CRACKED NEXT TO THE SIDE ROLLER BRACKET. DETAILED INSPECTION INSTRUCJul 16, 2006 · N787TA · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006284Arm · brokenDURING A PREFLIGHT INSPECTION THE CREW DISCOVERED THE LT OB BOTTOM THRUST REVERSER ARM WAS BROKEN AND HANGING DOWN AND THE TOP ARM ROD COVER WAS BENT UP. MAINTENANCE REPLACED THE THRUST REVERSER ASSEMBLY. SYSTEM OPERATIONAL CHECKS WERE SATISFACTORY AND NO LEJul 16, 2006 · N740TA · Beech 400A · Engine Thrust ReverserSDR DXTA200601497Downlock Switch · out of adjustWHEN LANDING WAS LOWERED ON APPROACH RIGHT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE. CYCLED GEAR TWICE AND RIGHT GEAR GREEN LIGHT ILLUMINATED. RED LIGHT IN GEAR HANDLE WAS OUT. INSTALLED NEW LT MAIN GEAR DOWN LOCK SWITCH AND ADJUSTED IAW HAWKER 400XP MM 32-Jul 13, 2006 · N119QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200601492Wire Harness · damagedWHEN LANDING GEAR WAS LOWERED ON APPROACH IN YYZ RIGHT GEAR GREEN LIGHT DID NOT ILLUMINATE. CYCLED GEAR WITH SAME INDICATIONS. EXECUTED A MISSED APPROACH AND BEFORE GEAR WAS RAISED RIGHT GEAR GREEN LIGHT ILLUMINATED. LEFT LANDING GEAR DOWN FOR SECOND APPROAJul 12, 2006 · N119QS · Beech 400A · Landing Gear System WiringSDR DXTA200601495Proximity Switch · malfunctionedGREEN RIGHT MAIN GEAR LANDING LT DID NOT ILLUMINATE. LIGHT BULB WAS OPERATIVE. RAN CHECKLIST AND MADE NORMAL LANDING. REPLACED RT MLG DOWNLOCK SWITCH WITH NEW. OPS CHECKED GOOD IAW HAWKER 400XP MM 32-10-00.Jul 12, 2006 · N116QS · Beech 400A · Landing Gear Position and WarningSDR DJFA2006283Arm · brokenDURING A PREFLIGHT INSPECTION THE CREW DISCOVERED THE LEFT INBOARD THRUST REVERSER ARM BELOW THE FAIRING WAS BROKEN. MAINTENANCE REPLACED THE THRUST REVERSER ASSEMBLY ON THE NR 1 ENGINE. NO DISCREPANCIES WERE NOTED DURING GROUND OPERATIONAL AND EMERGENCY STOJul 8, 2006 · N436LX · Beech 400A · Engine Thrust ReverserSDR MFG2006F00001Engine · flamed outWHILE ON A PART 91 LEG WITH CREW ONLY AT AN ALTITUDE OF 40,000 FT, THE AC ENTERED TURBULENCE AND RAIN AND THE LT ENGINE FLAMED OUT. THE CREW PUT ON THEIR OXYGEN MASKS FOR PRECAUTIONARY PURPOSE AND CONTACTED ATC TO GO TO A LOWER ALTITUDE. AT AN ALTITUDE OF 28Jul 7, 2006 · N418GJ · Beech 400A · Engine (Turbine/Turboprop)SDR DJFA2006278Anti-Skid Sys · inoperativeWHILE SLOWING THROUGH APPROX 10 -15 KTS ON ROLLOUT, LOST BRAKING ACTION. ANTI-SKID SYS WAS SELECTED OFF, BRAKES RETURNED IMMEDIATELY. ONCE AC WAS SLOWED TO TAXI SPEED ANTI-SKID (ABS) SYS WAS SELECTED BACK ON AND BRAKES WERE AVAILABLE. MAINT ISSUED MEL 32-1 Jun 30, 2006 · N709TA · Beech 400A · Brake Anti-Skid SectionSDR DXTA200601461Downlock · malfunctionedLT MAIN GEAR GREEN IND LIGHT DOES NOT ILLUMINATE WITH GEAR EXTENDED. LIGHT TEST GOOD. NO RED GEAR HANDLE LIGHT AND NO GEAR WARNING HORN WITH FLAPS EXTENDED IN FLIGHT. REMOVED AND REPLACED GEAR DOWN AND LOCKED LIGHT ASSY AND PERFORMED OPS CHECK IAW HAWKER 4Jun 29, 2006 · N119QS · Beech 400A · Landing Gear Position and WarningSDR DJFA2006277Odor · detectedKPDX - KSAN THE CREW REPORTED A BRIEF ELECTRICAL BURNING ODOR IN THE COCKPIT WHILE EN ROUTE. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. AN INSPECTION AND OPERATIONAL CHECK OF THE AVIONICS SYSTEM AND OTHER ELECTRICAL COMPONENTS WAS PERFORMED WHILE ELECTJun 29, 2006 · N453CW · Beech 400A · Air Distribution SystemSDR DJFA2006274Brake · malfunctionedCREW REPORTED THAT FOLLOWING LANDING THE CO-PILOTS SIDE BRAKES FAILED COMPLETELY, AND WHEN THE PILOT APPLIED THE BRAKES, BRAKES SEEMED TO GRAB AND WERE INCONSISTENT. THE LEFT BRAKE HUNG UP AND DRAGGED. BRAKING WAS RETURNED TO NORMAL AFTER THE ANTI-SKID SYSTEJun 29, 2006 · N434LX · Beech 400A · Landing Gear Brake SystemSDR DJFA2006276Engine · leakingKSFB - KHPN THE CREW REPORTED A SMELL OF BURNING OIL OR A BLEED AIR ODOR FILLED THE COCKPIT AND CABIN ON TAKEOFF. THE ODOR CONTINUED DURING ALL POWER CHANGES AND WHILE VARIOUS POSITIONS OF THE ENVIRONMENTAL CONTROL SYSTEM WERE SELECTED. THE AIRCRAFT WAS DIVEJun 28, 2006 · N410CW · Beech 400A · Turbine Engine Oil SystemSDR DJFA2006273Downlock Switch · out of adjustCREW REPORTED ON APPROACH NOSE GEAR INDICATION WAS NOT RECEIVED AFTER LANDING GEAR WERE SELECTED DOWN. LIGHT DID ILLUMINATE WHEN TESTED. ON 3 MILE FINAL AURAL WARNING OF -GEAR TOO LOW- WAS RECEIVED. A GO-AROUND PAST TOWER WAS MADE SO THE TOWER COULD CHECK GJun 27, 2006 · N462LX · Beech 400A · Landing Gear Position and WarningSDR DJFA2006271Control Valve · faultyTHE CREW REPORTED THAT THE CABIN TEMPERATURE WAS EXTREMELY HOT AND WAS DIFFICULT TO REGULATE WITH CABIN CONTROLS IN BOTH MANUAL AND AUTOMATIC MODE SETTINGS. THE SYSTEM WAS EMITTING A BURNT RUBBER SMELL INTO THE COCKPIT AND CABIN AREAS. WHEN THE COCKPIT TEMPEJun 25, 2006 · N478LX · Beech 400A · Cabin Temperature ControllerSDR DXTA200601455Pitot System · obstructedABORTED TAKEOFF DUE TO SPLIT IN AIRSPEED INDICATIONS. LEFT : HUNG AT 80KTS. RIGHT : READ 100 KTS. INSPECTED LT PITOT PROBE FOR BLACKAGE. NO VISUAL SIGN OF BLOCKAGE NOTED. CONNECTED PITOT TESTER TO LT PITOT TUBE AT ADC. APPLIED PRESSURE AND REMOVED BUG FRJun 24, 2006 · N108QS · Beech 400A · Pitot/Static SystemSDR DJFA2006270Odor · detectedTHE CREW DETECTED A BURNING ODOR IN THE CABIN AND COCKPIT APPROXIMATELY THREE MINUTES AFTER SELECTING THE WING ANTI-ICING SYSTEM. FOLLOWING LANDING THE RIGHT SIDEWALL IN THE CABIN WAS STILL VERY HOT AND THE ODOR WAS STILL PRESENT WITH THE CABIN TABLE EXTENDEDJun 22, 2006 · N482LX · Beech 400A · Air Distribution SystemSDR DJFA2006286Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER BRACKET INSPECTION BOTH THE LEFT AND RIGHT INBOARD HORIZONTAL STABILIZER ROLLER BRACKET RIB STRUCTURES AND BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF TJun 21, 2006 · N440CW · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006275Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT A VERTICAL STABILIZER SUPPORT RIB WAS FOUND CRACKED. SUPPORT RIB PART NUMBER 45A23324-003 WAS REPLACED REFERENCING THE BEECHJET 400A STRUCTURAL REPAIR MANUAL.Jun 21, 2006 · N898TA · Beech 400A · Vertical Stabilizer, Spar/RibSDR 2006FA0000650Antenna · debondedINVESTIGATED PILOT REPORT OF LOSS OF NR 1 AND NR 2 VHF COMMUNICATION RADIOS WHEN FLYING IN PRECIPITATION. IAW P-STATIC TESTING FOUND POOR NR 1 AND NR 2 VHF ANTENNAS BONDS TO FUSELAGE. CLEANED, REBONDED AND REINSTALLED ANTENNAS. ALSO INSTALLED LT FUEL VENT LJun 20, 2006 · N731TA · Beech 400A · VHF Communications SystemSDR DJFA2006269Valve · defectiveON T/O CREW NOTED A BURNING BLEED AIR ODOR UNTIL AIRCRAFT WAS LEVELED 23,000 FT. IN DESCENT SAME SMELL WAS PRESENT. INSPECTED BLEED AIR COMPONENTS, DISCOVERED CONNECTOR FOR FLOW INCREASING VALVE NOT HOOKED UP. CONNECTOR INSTALLED. NO DISCREPANCIES DURING GJun 20, 2006 · N410CW · Beech 400A · Pressure Regulator/Outflow ValveSDR DXTA200601445Landing Gear · malfunctionedAFTER GEAR HANDLE WAS SELECTED UP, GREEN NOSE INDICATION REMAINED ILLUMINATED, IT SOUNDED LIKE THE NOSE GEAR WAS STILL DOWN. LANDING WAS UNEVENTFUL. JACKED AIRCRAFT, INSP NLG AREA. OPERATED GEAR CYCLE 15 TIMES. OPENED NLG DOORS, DISCONNECTED DRAG STRUT. IJun 19, 2006 · N145QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR DJFA2006267Coalescer Bag · dirtyTHE CREW REPORTED THAT A BURNING BLEED AIR SMELL WAS COMING INTO THE COCKPIT ON TAKEOFF BUT HAD DISSIPATED ENTIRELY AFTER ROTATION. BOTH COCKPIT AND CABIN HEAT WAS SET AT FULL COLD. MAINTENANCE CLEANED THE WATER SEPARATOR SOCK. SYSTEM OPERATIONAL CHECKS WERJun 18, 2006 · N410CW · Beech 400A · Humidity Control System
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