Pratt & Whitney JT15D-5

Service difficulty reports · 953

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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 engine_model_key = 'JT15D5'
  ORDER BY difficulty_date DESC"

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SDR DJFA20120711001Unknown · odorDURING FLIGHT, CREW REPORTED HEARING A POPPING SOUND, FOLLOWED BY A BURNING ODOR. THE ODOR DISSIPATED AFTER A SHORT TIME AND THE ACFT LANDED SAFELY AT DESTINATION. MX WAS UNABLE TO FIND ANY DISCREPANCIES. DISCREPANCY HAS NOT REPEATED.Jul 11, 2012 · N429LX · Beech 400A · Air Distribution SystemSDR CA120709001Engine · flamed out(CAN) IT WAS REPORTED THAT DURING FLIGHT AT 45,000 FT BOTH ENGINES FLAMED OUT AND RE-LIT IN-FLIGHT. FURTHER COMMUNICATION WITH THE OWNER REVEALED THAT BOTH ENGINES WERE NOT RUNNING WHEN THE ACFT LANDED. THE CREW PERFORMED A DEAD STICK LANDING SAFELY. TROULBJun 29, 2012 · Beech 400A · Engine (Turbine/Turboprop)SDR CA120628012Wheel Half · cracked(CAN) ON A BASE INSPECTION, MAINTENANCE FOUND THE RT MAIN WHEEL PRESSURE WAS LOW AT 40 PSI. THEY REPLACED WHEEL ASSY WITH REPAIRED UNIT. IT WAS INFLATED IT TO RATED PRESSURE AND THE ACFT WAS RELEASED FOR SERVICE. ON DISASSEMBLY BY PERSONS IN THE COMPONENT SHOPJun 26, 2012 · Cessna 560XL · Wheel/Ski/FloatSDR 2012FA0000451Gasket · wrong partENGINE FIRE LIGHT CAME ON DURING FLIGHT, DUE TO A GASKET LISTED IN THE MFG IPC BEING INCORRECT.Jun 23, 2012 · N997EA · Cessna 560CESSNA · Engine Bleed Air SystemSDR 9JLA2012071704219Motor · overheatedTHE CREW REPORTED THE AIR CONDITIONING SYSTEM INOPERATIVE. TROUBLESHOOTING FOUND THE AIR CONDITIONER COMPRESSOR MOTOR DEFECTIVE. A MODIFIED MOTOR WAS INSTALLED. OPS CHECKS GOOD.Jun 20, 2012 · N314TL · Beech 400A · Cabin Compressor SystemSDR 9JLA201271904219Motor · defectiveCREW REPORTED THAT THE AIR CONDITIONING WAS INOPERATIVE. TROUBLESHOOTING IDENTIFIED THE AIR CON COMPRESSOR MOTOR AS DEFECTIVE. A MODIFIED MOTOR WAS INSTALLED, FUNCTIONAL CHECKED SATISFACTORY.Jun 20, 2012 · N314TL · Beech 400A · Cabin Compressor SystemSDR DJFA20120501010Rib · crackedDURING SCHDULED INSPECTION, MX FOUND 12 RIBS CRACKED IN THE HORIZONTAL STAB. CRACKS WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 12 RIBS WERE REPMay 1, 2012 · N413LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR CA120319004Link · corroded(CAN) DISCOLOR ON BOLT AND BUSHING FOUND ON ROUTINE INSPECTION. FURTHER INSPECTION OUTSIDE THE SCOPE OF ORIGINAL INSPECTION REVEALED CORROSION ON PRESSED FIT BUSHING. THE CORROSION HAD GONE THROUGH THE BUSHING AND MADE A VISABLE HOLE. CORROSION WAS ALSO IDENTMar 16, 2012 · Cessna 560CESSNA · Engine Thrust ReverserSDR CA120312003Fuel Control · malfunctioned(CAN) DURING TAXI-OUT, 1 ENGINE ROLLED BACK TO SUB-IDLE AND SEEMED TO HUNG. THE ENGINE WAS SHUTDOWN AND LARGE AMOUNT OF SMOKE APPEARED IN THE BACK. STREAM OF FUEL POOLED UNDER THE ENGINE. ACFT WAS TOWED BACK TO ORIGIN. GROUND TECH CONFIRMED FUEL LEAKING FRFeb 27, 2012 · Beech 400A · Fuel Control/Turbine EnginesSDR DXTA2012030804910Fuel Control · flamed outLEFT ENGINE FLAME OUT OR HUNG START, DURING EFC TEST. BOTH ENGINES STARTED NORMALLY ON GPU POWER. BOTH ENGINES FUNCTIONED NORMALLY OUT OF THE RAMP AREA. REPLACED THE LT ENGINE FUEL PUMP AND FUEL CONTROL IAW MM 73-20-00. LEAK AND OPS CHECKED GOOD.Feb 26, 2012 · N106QS · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)SDR CA120222004Connector · loose(CAN) DURING DECENT, AIRCREW TRIED TO EXTEND LANDING GEAR BY PUTTING LANDING GEAR HANDLE IN DOWN POSITION, LANDING GEAR FALIED TO EXTEND. PILOT THEN JIGGLED HANDLE, LANDING GEAR EXTENDED WITH A DOWN AND LOCKED POSITION. PILOT LANDED ACFT WITH NO FURTHER ISSUFeb 13, 2012 · Cessna 560CESSNA · Landing Gear System WiringSDR DJFA01302012009Inverter · failedON APPROACH FOR LANDING, CREW REPORTED HEARING A SOUND LIKE A SPARK FOLLOWED BY AN ELECTRICAL BURNING SMELL AND NR1 INVERTER FAILURE INDICATION. ACFT LANDED SAFELY. MAINTENANCE FOUND THE NR 1 INVERTER FAILED AND THE "AC SELECT" SWITCH MALFUNCTIONING. BOTH Jan 30, 2012 · N429LX · Beech 400A · AC InverterSDR CA120115009Fuel Control · malfunctioned(CAN) AS POWER WAS APPLIED FOR T/O, THE ENGINES COULD NOT ACHIEVE T/O POWER FOR THE DAY IN EEC MODE. REQUIRED THRUST COULD BE ACHIEVED IN MANUAL MODE. TROUBLESHOOTING LED TO THE REPLACEMENT OF BOTH ENGINE`S FUEL CONTROL BEFORE THE ACFT WAS RETURNED TO SERVICEDec 21, 2011 · Raythn 400ARAYTHEON · Fuel Control/Turbine EnginesSDR CA111201002Engine · damaged(CAN) DURING FLIGHT, THE NR 2 ENGINE SURGED WITH A RAISE IN TEMPERATURE. THE PILOT REDUCED THROTTLE AND WITHIN 15 SEC., THE ENGINE LOST POWER. THE ENGINE WAS SHUT DOWN AND THE FLIGHT WAS DIVERTED TO HOME BASE WHERE AND UNEVENTFUL SINGLE ENGINE LANDING WAS MADENov 27, 2011 · Beech 400A · Engine (Turbine/Turboprop)SDR HVJA2011F00210Tire · failedLT MAIN TIRE WAS PUNCTURED WHEN IT ENCOUNTERED UNKNOWN FOD CAUSING THE TIRE TO COMPLETELY DEFLATE ON LANDING. THE ACFT WAS ABLE TO MAINTAIN BRAKING CONTROL AND SAFELY TAXI OFF THE RUNWAY. SIGNIFICANT HEAT WAS DEVELOPED IN THE BRAKING ACTION AND CAUSED 2 OF THOct 4, 2011 · N933AC · Beech 400BEECH · TireSDR 2011F00204Tire · separatedFLIGHT CREW NOTED ABNORMAL BRAKING AND CONTROL ON LANDING, ACFT CLEARED RUNWAY AND STOPPED ON RAMP WITH NO INCIDENT. FOUND LT MAIN TIRE FLAT WITH TREAD MISSING, NO OTHER ACFT DAMAGE NOTED. MX INSPECTED ACFT, AND REPLACED TIRE AND WHEEL ASSY. MX FOUND TREAD Sep 24, 2011 · N26PA · Beech 400A · TireSDR CA110921001Bearing · failed(CAN) ENGINE WAS SENT FOR A SCHEDULED O/H. DISASSEMBLY OF ENGINE REVEALED THAT THE ENGINE HAD METAL CONTAMINATION IN THE OIL FILTER AND OIL FILTER HSG. THE SOURCE OF THE METAL CONTAMINATION WAS THE DUPLEX BEARING ON THE AGB INPUT DRIVE GEAR WHICH HAD A THOUSep 20, 2011 · Engine (Turbine/Turboprop)SDR 2011F00201Engine · making metalDURING ENGINE MINOR INSP, SENT OIL FILTER TO LAB FOR ROUTINE ANALYSIS, LAB REPORTED METAL IN OIL. CONTACTED MFG FOR EVALUATION, MFG INSTRUCTED TO INSTALL NEW OIL AND FILTER, PERFORM GROUND RUN FOR 1 HOUR, AND SEND FILTER OUT FOR REPEAT ANALYSIS. SECOND ANALYSSep 13, 2011 · N26PA · Beech 400A · Engine (Turbine/Turboprop)SDR CVGA112501Engine · power lossDESCENDING THROUGH 16,000FT WITH 68% N1/SIDE AND ENGINE ANIT-ICE ON, THE RIGHT ENGINE ROLLED BACK TO 42% N1. HEARD BANGING FROM THE RIGHT ENGINE THAT LASTED 3 OR 4 SECONDS WITH ABOUT 5 BANGS. THEN THE ENGINE RETURNED TO THE ORIGINAL POWER SETTING.Sep 7, 2011 · N511VB · Beech 400A · Engine (Turbine/Turboprop)SDR DJFA20110905001Oil System · leakingFLIGHT CREW NOTED A BURNING SMELL AFTER TAKEOFF, FOLLOWED BY VISIBLE SMOKE IN THE AFT PASSENGER CABIN (NO PASSENGERS WERE ONBOARD). ACFT RETURNED TO THE DEPARTURE AIRPORT AND LANDED SAFELY. MAINTENANCE TECHNICIANS CONFIRMED OIL SMELL COMING FROM THE RT ENGISep 5, 2011 · N426FL · Beech 400A · Turbine Engine Oil SystemSDR CA110826005Switch · failed(CAN) ON APPROACH, PILOT SELECTED GEAR DOWN AND DID NOT GET NOSE DOWNLOCK INDICATION. ACFT RETURNED TO DEPARTURE AND RECYCLED LANDING GEAR DOWN, STILL DID NOT GET DOWNLOCK INDICATION. CREW ALERTED ATC AND PROCEEDED WITH EMERGENCY GEAR DOWN PROCEDURES. STILLAug 23, 2011 · Cessna 560CESSNA · Landing Gear Retraction/Extension SystemSDR CA110617001Bearing Cage · crackedENGINEERING INVESTIGATION REPORT. CONFIRMED THAT ENGINE DID HAVE METAL CONTAMINATION OF THE OIL SYS. THE SOURCE OF METAL CONTAMINATION WAS THE NR 3 BEARING (PN 3107493-01, S/N FC153527) WHICH HAD A THROUGH GOING CRACK ON THE ROLLER CAGE. THE CRACK ALLOWED THJun 16, 2011 · Turbine SectionSDR CA110615003Bearing Cage · crackedDURING EIR JT15D 2011-006, WAS ABLE TO CONFIRM THAT ENGINE DID HAVE METAL CONTAMINATION OF THE OIL SYS. THE SOURCE OF METAL CONTAMINATION WAS THE NR 3 BEARING WHICH HAD A CRACK ON CAGE WHICH ALLOWED THE ADJACENT ROLLER ELEMENT TO TURN SIDEWAYS WITHIN THE POCKJun 14, 2011 · Turbine SectionSDR CA110613004Turbine Blades · damagedVIBRATIONS/IFSD DURING CLIMB THROUGH FL260, SUDDEN VIBRATIONS WERE FELT. LT ENGINE VIBRATION WENT TO FULL SCALE. WHEN ENGINE WAS SELECTED TO IDLE, VIBRATIONS DECREASED. PRECAUTIONARY SHUTDOWN WAS PERFORMED AND AN UNEVENTFUL SINGLE-ENGINE LANDING WAS ACCOMPLIJun 5, 2011 · Raythn 400ARAYTHEON · Turbine SectionSDR I5WA20110629Fuel Control · failedRT ENGINE SURGING WITH FLUCTUATIONS IN N1, N2, AND FUEL FLOWJun 1, 2011 · N205CM · Cessna 560CESSNA · Fuel Control/Turbine EnginesSDR CA110711009Warning Light · illuminated(CAN) ABORTED T/O, ON T/O ROLL AT APPROXIMATELY 25 KTS, THE ENGINE ELECTRONIC FUEL CONTROL, EFC, LIGHT CAME ON AT APPROX 97 PERCENT N1. THE PILOT ABORTED T/O. TROUBLESHOOTING IS ON-GOING.Jun 1, 2011 · Beech 400A · Fuel Controlling SystemSDR BTA2011F00000O-Ring · brokenACFT DEPARTED, ENROUTE, PILOT NOTED LT ENG OIL PRESSURE FALLING, PILOT MONITORED OIL PRESSURE AND AFTER A FEW MINUTES, HE NOTED THE OIL PRESSURE WAS STILL FALLING. THE PILOT SHUT DOWN THE LT ENGINE AND DECLARED AN EMERGENCY LANDING. AFTER LANDING, MX TROUBLEMay 2, 2011 · N560CF · Cessna 560CESSNA · Turbine Engine Oil SystemSDR BTA2011F00001O-Ring · brokenACFT DEPARTED, PILOT NOTED LT ENGINE OIL PRESSURE FALLING, PILOT MONITORED OIL PRESSURE AND AFTER A FEW MINUTES HE NOTED THE OIL PRESSURE WAS STILL FALLING. THE PILOT SHUT DOWN THE LT ENGINE AND DECLARED AN EMERGENCY LANDING. AFTER LANDING, HAD REPAIR STATIOMay 2, 2011 · N560CF · Cessna 560CESSNA · Turbine Engine Oil SystemSDR 2011F00077Light · inoperativeITT INDICATOR BACKLIGHT INOPERATIVE, REMOVED AND REPLACED INDICATOR.Apr 23, 2011 · N570EJ · Cessna 560CESSNA · Engine EGT/TIT Indicating SystemSDR 2011F00076Light · inoperativeORDERED IN A SECOND WARRANTY EXCHANGE UNIT FROM ACFT MFG AND WERE SENT A REPLACEMENT GAUGE 4/23/2011, SN 346KA. THE UNIT WAS O/H REF W/O 0372457 BUT WHEN INSTALLED NONE OF THE BACKLIGHTING WORKED AND THE FAULT WAS IN THE UNIT.Apr 22, 2011 · N570EJ · Cessna 560CESSNA · Engine EGT/TIT Indicating SystemSDR 2011F00075Indicator · inoperativeORDERED IN A WARRANTY EXCHANGE UNIT FROM ACFT MFG AND WERE SENT A REPLACEMENT GAUGE 2/22/2011, SN 864BA. THIS UNIT WAS O/H REF WO 0364333 BUT WHEN INSTALLED, THE LOWER HALF OF THE BACKLIGHTING IAW INOPERATIVE. TROUBLESHOT THE BACKLIGHTING WIRING AND DETERMINApr 21, 2011 · N570EJ · Cessna 560CESSNA · Engine EGT/TIT Indicating SystemSDR CA110413008Indication Sys · malfunctioned(CAN) ABORTED T/O, THE PILOT ABORTED DUE TO BOTH ENGINES BEING 0.1 PERCENT BELOW TARGET N1 SPEED. POST EVENT PERFORMANCE ENGINE RUN UPS WERE SATISFACTORY AND THE ACFT WAS RETURNED TO SERVICE. EXTENT OF TROUBLESHOOTING PERFORMED IS UNKNOWN AT THIS TIME.Apr 4, 2011 · Engine Indicating SystemSDR 2011FA0000142O-Ring · pinchedCREW EXPERIENCED LT ENGINE OIL PRESSURE FLUCTUATING. UPON COMPLETING EMERGENCY CHECK LIST OIL PRESSURE DROPPED BELOW 20PSI AND ENGINE WAS SHUT DOWN. SUBSEQUENT INSPECTION REVEALED A PINCHED O-RING IN THE MAIN ENGINE OIL FILTER HOUSING. O-RING WAS REPLACED ANDFeb 22, 2011 · N406T · Beech 400BEECH · Engine Oil System (Airframe Furnished)SDR 2011FA0000106Bearing · brokenCREW NOTICED A VIBRATION IN CRUISE. IDENTIFIED ELECTRICAL POWER LOSS IN RT STARTER/GENERATOR. I SOLATED STARTER/GENERATOR. NO FURTHER PROBLEMS EXPERIENCED DURING THE FLIGHT. RESEARCH REVEALED THE STARTER/GENERATOR, O/H, HAD THE SAME FAILURE PRIOR TO BEING OFeb 15, 2011 · N628CK · Cessna 560CESSNA · Starter-GeneratorSDR 2011F00000AIndicator · failedTHE ENGINE ITT GAUGE FAILED AND A REPLACEMENT WAS INSTALLED THIS UNIT WAS O/H REF WO 0363688. AFTER 122.4 HOURS THE UNIT STARTED TO CAUSE THE ASSOCIATED "RT ITT" CIRCUIT BREAKER TO TRIP. THE FAULT WAS DETERMINED TO BE BEING CAUSED BY THE UNIT. Feb 12, 2011 · N570EJ · Cessna 560CESSNA · Engine EGT/TIT Indicating SystemSDR 2011FA0000073Lamp · failedRT RECOGNITION LAMP DISCOVERED FAILED DURING POST FLIGHT INSP. REPLACED LAMP AND DISCOVERED FAILED LAMP WAS DEFECTIVE. LAMP SOLDER JOINT FAILURE AT MOUNTING FLANGE. CAUSED FAILURE OF LAMP ASSY, ARCING, OVERHEATING, AND DISPLACEMENT OF LAMP CORE. FAILURE APFeb 8, 2011 · N628CK · Cessna 560CESSNA · Exterior LightingSDR CA110208010Engine · failed(CAN) IFSD/INABILITY TO MODULATE THRUST DURING TAKE OFF, PILOT HEARD A BUZZING NOISE. PILOT ELECTED TO CONTINUE TO FL180. ONCE AT CRUISE AT FL180, PILOT MODULATED LH ENGINE POWER LEVER AND THE AND ENGINE ROLLED BACK TO FLIGHT IDLE POWER. THE PILOT DECLARED EMEJan 28, 2011 · Raythn 400ARAYTHEON · Powerplant SystemSDR CA110125010Engine · flamed out(CAN) FLAMEOUT ON LANDING ROLLOUT, WHILE STOWING THE THRUST REVERSERS, THE NR 1 ENGINE FLAMED OUT. WHILE TAXIING CLEAR OF RUNWAY, THE ENGINE RE-LIT WITHOUT INPUT FROM CREW. TROUBLESHOOTING IS ON-GOING.Jan 17, 2011 · Raythn 400ARAYTHEON · Engine (Turbine/Turboprop)SDR ISYA20110106Engine · failedDURING CLIMBOUT, NOTICED A MASTER CAUTION LIGHT FLASH. THEN A FEW SECONDS LATER IT DID IT AGAIN, LOOKED ALL AROUND AND SAW NOTHING. THEN IT CAME ON AND STAYED ON AND IT WAS THE RT OIL PRESSURE LIGHT. LOOKED AT THE GAUGE AND THE NEEDLE WAS IN THE RED. WENT TOJan 3, 2011 · N8283C · Beech 400A · Engine (Turbine/Turboprop)SDR DXTA2011010304385Line · leakingOUT OF 4000 FT THE LT ENG FIRE LIGHT CAME ON, PULLED POWER TO IDLE AND LIGHT WENT OUT. LANDED WITH NO OTHER LIGHTS. REMOVED COWLING AND INSPECTED ENGINE FOR HOT STAB. NO DAMAGE NOTED RAN ENG AND FOUND INBD BLEED AIR LINE LEAKING. INSTALLED NEW LINE ASSY IJan 2, 2011 · N316QS · Cessna 560XL · Pneumatic Distribution SystemSDR DBCA201101020001Starter Gen · failedWHEN PREPARING TO DEPART BZN NR 1 ENGINE WOULD NOT SPOOL. TROUBLESHOOTING BY MAINTENANCE FOUND STARTER/GENERATOR HAD FAILED. REPLACED STARTER/GENERATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD.Jan 2, 2011 · N95GK · Beech 400A · Starter-GeneratorSDR DXTA2010122204371Landing Gear · failedABORTED TAKEOFF, DUE TO LT MLG FAILURE AT 80KTS. ACCELERATION TO 80KTS APPEARED NORMAL UNTIL 80KTS, THEN ACCELERATION IMPAIRED & DIRECTIONAL CONTROL EFFECTED. IMMEDIATELY ABORTED TAKE OFF & IT TOOK A LOT OF RT BRAKING TO KEEP THE ACFT FROM DEPARTING RUNWAY. Dec 20, 2010 · N149QS · Raythn 400ARAYTHEON · Main Landing GearSDR DXTA2010121904368Fuel Cell · leakingDURING CLIMB, FUEL OBSERVED LEAKING FROM UNDER LT WING. FUEL WAS TRANSFERRING FROM FUSELAGE TANKS AND WING FUEL GAUGES, INDICATED FULL LEVELS. DURING DESCENT, FUEL LEAKAGE APPEARED TO STOP, APPROX 15 MINUTES AFTER INITIAL DISCOVERY OF LEAK. INSTALLED NEW PILDec 17, 2010 · N140QS · Raythn 400ARAYTHEON · Fuel StorageSDR DXTA2010121904367Uplock · out of adjustON GEAR RETRACTION, ALL 3 GREEN DOWN & LOCK LIGHTS EXTINGUISHED. RED GEAR UNSAFE LIGHT IN GEAR HANDLE REMAINED ILLUMINATED. GEAR SELECTED DOWN & ALL LIGHTS SHOWED PROPER INDICATIONS. JACKED ACFT AND APPLIED HYD POWER, CYCLED LANDING GEAR AND WAS ABLE TO DUPLIDec 16, 2010 · N142QS · Raythn 400ARAYTHEON · Landing Gear Retraction/Extension SystemSDR DXTA2010120904356Stabilizer · failedHORIZ STAB FAILED IN FLIGHT IN ICING CONDITIONS. RESET CIRCUIT BREAKER HORIZONTAL STAB PROTECT, COMPLIED WITH GROUND TEST OF HORIZONTAL STAB HEAT SYS IAW MM 30-12-00-201. GROUND CHECKED GOOD.Dec 8, 2010 · N141QS · Raythn 400ARAYTHEON · Stabilizer Control SystemSDR DXTA2010120604355Warning Light · false activationAFTER GEAR RETRACTION RED GEAR UNSAFE LIGHTS ON GEAR HANDLE REMAINED ILLUMINATED. DURING APPROACH GEAR EXTENSION WAS NORMAL AND RED UNSAFE LIGHTS EXTINGUISHED. COULD NOT DUPLICATE DISCEPANCY. CLEANED ALL UPLOCK AND DOOR SWITCHES AND INSPECTED SWITCH WIRING HDec 6, 2010 · N149QS · Raythn 400ARAYTHEON · Landing Gear Position and WarningSDR DXTA2010120304344Brake Sys · malfunctionedON LANDING, WHEN APPLYING BRAKES, BOTH PEDALS WERE HARD AND THERE WAS NO BRAKING ACTION UNTIL AFTER THE ACFT SLOWED BELOW 60KNTS. BRAKES WORKED NORMAL WITH THE ANTI-SKID OFF DURING TAXI. COULD NOT DUPLICATED DISCREPANCY. ALL WORK PERFORMED IAW MM 32-40-03 ANDec 2, 2010 · N120QS · Raythn 400ARAYTHEON · Landing Gear Brake SystemSDR DJFA2010037Control Cable · severedDURING CRUISE FLIGHT, THE CREW NOTED THE FLAP ASSYMETRY LIGHT AND MASTER CAUTION LIGHT ILLUMINATED. DURING TROUBLESHOOTING MX FOUND THE LT AND RT FWD FLAP CABLES SEVERELY CORRODED AND SEVERED AT THE MID BELL CRANK FERRULE. MX REPLACED BOTH CABLES.Dec 2, 2010 · N447LX · Beech 400A · Trailing Edge Flap Control SystemSDR DXTA2010120204340Mixing Valve · malfunctionedDURING LANDING ROLLOUT COPILOT BRAKES PERFORMED ABNORMALLY; SEVERAL PUMPS REGAINED PRESSURE. DURING TAXI STEADY BRAKING RESULTED IN DECREASING PRESSURE WITH LT PEDAL REACHING FLOOR. REPLACED LEFT MIXER VALVE IAW MM 32-40-00. OPS AND LEAK CHECKED GOOD.Nov 30, 2010 · N139QS · Raythn 400ARAYTHEON · Landing Gear Brake SystemSDR DJFA2010036Power Supply · failedACFT DIVERTED, DUE TO SMOKE SMELL IN COCKPIT. EMERGENCY WAS DECLARED. MX EVALUATED AND CONFIRMED "BURNED ELECTRICAL" ODOR FROM ALTITUDE AWARENESS PANEL. ALSO FOUND INSTRUMENT LIGHT POWER SUPPLY OUTPUT AT 118VAC. R & R THE INSTRUMENT LIGHT POWER SUPPLY AND Nov 27, 2010 · N443LX · Beech 400A · Instrument System Wiring
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