U/A Canada PT6A-41

Service difficulty reports · 717

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Query with SQL
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 = 'PT6A41'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CIEA200700002Resistor · burnedSHUTDOWN THE ENGINES, NOTICED LIGHT SMOKE COMING FROM UNDER INSTRUMENT PANEL & AN ODOR LIKE ELECTRICAL BURNING. MAINT INSPECTED AC & WHEN MASTER SWITCH WAS TURNED ON, A RESISTOR MOUNTED TO FWD BULKHEAD UNDER PILOTS INSTRUMENT PANEL FOUND TO BE GLOWING RED & EApr 6, 2007 · N60PD · Beech 200BEECH · Passenger Compartment LightingSDR CA070409006Drag Brace · failed(CAN) AC WAS DISCOVERD OUTSIDE HANGER WITH THE LT MLG COLLAPSED. THE FAULT OF THE PROBLEM WAS THE LT MLG DRAG BRACE. IT WAS REPLACED RECENTLY WHEN A SIMILIAR INCIDENT OCCURED TO THE RT MLG DRAG BRACE CAUSING THE LT MLG TO COLLAPSE WHILE BEING TOWED. DAMAGE CAApr 5, 2007 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR 2007FA0000381Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE, REMOVED LT ENGINE EXHAUST STACK TO FACILITATE INSPECTING THE EXHAUST DUCT. FOUND CRACK FOLLOWING THE CIRCUMFERENCE OF THE SKI SLOPE. THE EXHAUST DUCT HAD SB 3380 COMPLIED WITH 514 HOURS EARLIER.POWER SECTION WAS REMOVED Apr 4, 2007 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR CA070409003Selector Valve · leaking(CAN) VALVE WAS OVERHAULED BY VENDOR. AFTER OVERHAUL IT WAS INSTALLED IN THE AIRCRAFT. AFTER 2 HOURS OF OPERATION A LEAK DEVELOPED. THE VALVE WAS REMOVED AND DISTRIBUTION MANIFOLD DISASSEMBLED. WHEN CHECKING THE IPC IT WAS NOTED THAT AT OVERHAUL, THE OVERHAUL Apr 4, 2007 · Beech 200BEECH · Hydraulic System, MainSDR CA070327001Boot · arced(CAN) PILOTS REPORTED THAT THE IB LEADING EDGE DEICE BOOT WAS NOT FUNCTIONING. THE DEICE SYSTEM WAS TESTED AND THE SNAG WAS CONFIRMED. WHEN THE LEADING EDGE WAS REMOVED TO CHECK THE BOOT SYSTEM EVIDENCE OF SEVERE ARCING WAS FOUND IN THE VICINITY OF THE STARMar 26, 2007 · Beech 200BEECH · Airfoil Anti/De-ice SystemSDR CA070312010Cotter Pin · misinstalled(CAN) ON DESCENT FROM 21000 FEET, THE RT POWER LEVER WAS PULLED BACK BUT THE ENGINE DID NOT RESPOND TO THE COMMAND. ENGINE WAS THEN SHUTDOWN TO PREVENT OVERTORQUING. ON INSPECTION OF FCU LINKAGES, MECHANICS FOUND THE COTTER PIN GOING THROUGH INPUT SHAFT AFT Mar 7, 2007 · Beech 200BEECH · Fuel Controlling SystemSDR K5L2007F00000Windshield · failedWHEN IN CRUISE FLIGHT AT FL210 AND -42 DEGREES C, THE INNER PANE ON THE CO-PILOTS WINDSHIELD SHATTERED. NO PIECES BROKE LOOSE AND NORMAL DESCENT AND SAFE LANDING WERE MADE AT KLEB. THERE WAS NO LOSS OF CABIN PRESSURE. LAST INSPECTION WAS 3 MONTH AND 100 HOUMar 6, 2007 · N636B · Beech A200 · Flight Compartment WindowsSDR CA070514022Tube · fractured(CAN) DURING SPRAYING OPERATIONS, THE ENGINE LOST POWER RESULTING IN A FORCED LANDING. SUBSEQUENT INSPECTION REVEALED A FRACTURED FUEL CONTROL P3 DELIVERY LINE. (TC NR 20070514022)Feb 22, 2007 · Ayres S2RHGT65 · Engine Fuel DistributionSDR 2007FA0000145Exhaust Duct · crackedWHILE PERFORMING SCHEDULED MAINTENANCE, REMOVED LT ENGINE EXHAUST STACKS TO FACILITATE INSPECTING THE EXHAUST DUCT. FOUND A 14 INCH CRACK FOLLOWING THE CIRCUMFERENCE OF THE SKI SLOPE WITH A 3 INCHES CRACK PROPAGATING LONGITUDELY AT THE 10 O'CLOCK POSITION FROFeb 15, 2007 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR 2007FA0000435Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE. EXHAUST DUCT SB HAD BEEN COMPLIED WITH 422 HOURS PRIOR. POWER SECTION WAS REMOVED FOR REPAIR.Feb 9, 2007 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR CA070219006Fcu · faulty(CAN) DURING GROUND RUN, RT POWER LEVER FOUND NOT CONTOLLING FCU. INSPECTED THROTLE LEVER LINKAGES AND CABLE TO FCU AND NO FAULTS FOUND. AFTER TROUBLESHOOTING WITH MFG TECH SUPPORT, SUSPECTED FAULTY FUEL CONTROL UNIT. FCU HAS BEEN REPLACED AND FAULT ELIMINATEDFeb 8, 2007 · Beech 200BEECH · Fuel Control/Turbine EnginesSDR CIEA200700001Pressure Panel · crackedDURING INSPECTION OF THE AIRCRAFT TO EVALUATE A PRESSURIZATION LEAK, THE PANEL BEHIND THE REAR SPAR WAS FOUND TO BE CRACKED IN THE LOWER RADIUS AREA. THERE WAS A CRACK APPROXIMATELY 4 INCHES LONG NEAR THE CENTER LINE OF THE AIRCRAFT. THE AIRCRAFT SKIN WAS NOJan 24, 2007 · N520MC · Beech 200BEECH · Fuselage Main, BulkheadSDR CA070126010Bearing · disintegrated(CAN) BEARING WITHIN RT ENGINE AIR CONDITIONING COMPRESSOR DRIVE PULLEY DISINTEGRATED WHICH GREATLY CAUSED FURTHER HARM TO ITS ASSOCIATED PARTS. THE QUILL SHAFT, COMPRESSOR DRIVE PULLEY, COMPRESSOR MOUNT ASSEMBLY, DRIVE SUPPORT, BEARING SHIMS AND SPACER, AND Jan 23, 2007 · Beech 200BEECH · Cabin Compressor SystemSDR CA070122008Drag Link · failed(CAN) AFTER SCHEDULED MAINTENANCE THE AIRCRAFT WAS REMOVED FROM THE HANGER AND WAS TOWED TO THE FUEL PUMPS TO BE LEAK CHECKED. AFTER TOWING THE AIRCRAFT ABOUT 500 FEET THE RT MLG COLLAPSED CAUSING DAMAGE TO THE RT MAIN LANDING GEAR AND DOORS, WING TIP, CARGO PJan 20, 2007 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR ZFD2007F00000Pump · malfunctionedPILOT STATED THAT THE LT FUEL PRESSURE WOULD GO TO ZERO IF THE ELECTRIC PUMPS WERE TURNED OFF. FOUND AIRFRAME MFG INSTALLED ENGINE DRIVEN PUMP INOPERATIVE.. THE PUMP DRIVE WAS FOUND TO BE SLIPPING. INSPECTED THE PUMP AND NO OTHER DEFECTS WERE NOTED. THE PUJan 16, 2007 · N94EW · Piper PA42 · Engine Fuel PumpSDR CA070115017Stiffener · cracked(CAN) SPECIAL INSP NR53 WAS COMPLETED IAW MM 5-20-05, WHICH INVOLVES THE FOLLOWING: AFT FUSELAGE AREA AND REAR PRESSURE BULKHEAD. INSPECT THE ENTIRE FWD AND AFT SIDE OF THE REAR PRESSURE BULKHEAD FOR CRACKS AND LOOSE OR MISSING RIVETS. CHECKED OXYGEN BOTTLEJan 12, 2007 · Beech 200BEECH · Fuselage Main, BulkheadSDR CA070111018Shaft · cracked(CAN) THE NOSE GEAR ACTUATOR WAS REMOVED TO PERFORM AN END PLAY CHECK. THE NOSE GEAR RETRACT DRIVE SPROCKET AND SHAFT (PN 50-820218-11) ASSEMBLY WAS REMOVED FOR CLEANING. INSPECTION OF THE DRIVE SPROCKET AND SHAFT FOUND THAT A CRACK HAD FORMED ON THE END DIAMJan 9, 2007 · Beech 200BEECH · Landing Gear ActuatorSDR CA070105006Windshield · cracked(CAN) DURING PRESSURIZED FLIGHT THE LT WINDSHIELD CRACKED IN SEVERAL PLACES ALL ALONG THE IB SECTION OF THE WINDOW. THE WINDOW WAS ORIGINALLY A REPAIRED WINDOW AND WAS INSTALLED FOR 1512.9HRS/1450CYCLES BEFORE FAILING. (TC NR 20070105006)Jan 4, 2007 · Beech 200BEECH · Flight Compartment WindowsSDR CA070118005Sense Line · broken(CAN) P3 TUBE SUDDENLY BROKEN WHILE AIRCRAFT WAS IN CLIMB. ENGINE FAIL TO IDLE, ENGINE WAS SHUTDOWN BY THE CREW. AIRCRAFT RETURN TO DEPARTURE AIRPORT WITHOUT OTHER DIFFICULTY. (TC NR 20070118005)Jan 3, 2007 · Beech 200BEECH · Fuel Controlling SystemSDR CA070209010Tube · fractured(CAN) ON CLIMB, ENGINE POWER REDUCED TO IDLE UNCOMMANDED. THE ENGINE WAS SHUTDOWN IN FLIGHT. INSPECTION REVEALED A FRACTURED FCU P3 DELIVERY TUBE. (TC NR 20070209010)Jan 3, 2007 · Beech 200BEECH · Fuel Control/Turbine EnginesSDR CA061229001Motor · unserviceable(CAN) WHEN LANDING GEAR ONLY EXTENDED HALFWAY. EMERGENCY EXTENSION USED TO EXTEND TO LANDING CONFIGURATION. MOTOR WAS INSTALLED AS AN OVERHAULED UNIT 4.4 HRS PRIOR TO FAILURE. C/B WAS FOUND TRIPPED UNDER CABIN FLOOR. BREAKER RESET AND GEAR CYCLED. MOTOR WAS Dec 27, 2006 · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR CA061219026Turbine Blades · failed(CAN) IN CRUISE THE ENGINE EMITTED A LOUD NOISE AND FLAMED OUT. SUBSEQUENT INSPECTION REVEALED FRACTURED TURBINE BLADES AND VANES AND A PUNCTURED GAS GENERATOR CASE. LIGHT IMPACT DAMAGE WAS FOUND ON THE AIRCRAFT WING LEADING EDGE AND FUSELAGE WINDOWS. MFG WNov 28, 2006 · Beech 200BEECH · Turbine SectionSDR QZN2006F00000Actuator · failedNOSE GEAR ACTUATOR SLIPPING INTERNALLY CAUSING NOSE GEAR TO BE OUT OF SEQUENCE WITH MAIN GEAR. FAILED AFTER INSERVICE 306.6 HR, 269 LANDINGS. (K)Nov 16, 2006 · N500CR · Beech 200BEECH · Landing Gear ActuatorSDR CA061116006Skin · cracked(CAN) CABIN BOTTOM SKIN FOUND CRACKED ADJACENT TO ROTATING BEACON DOME MOUNTING. REPAIR DRAWING REQUESTED. (TC NR 20061116006)Nov 16, 2006 · Beech 200BEECH · Fuselage Main, Plate/SkinSDR F222007F00000Compressor · stalledPILOT REPORTED FLAMES MOMENTARILY COMING FROM THE LT AND RT ENGINE EXHAUST STACKS. THE PILOT DECIDED TO LAND AT AN AIRPORT THAT WE ALSO SERVE AS AN AIR AMBULANCE AND SWAP PLANES TIL THE CAUSE COULD BE DETERMINED. THE PILOT REPORTED IT TO MAINTENANCE AS A COMNov 15, 2006 · N988CC · Beech 200BEECH · Turbine Engine Compressor SectionSDR CIEA200600009Fire Warning · false activationDURING CRUISE FLIGHT IN THE LATE EVENING, THE RT ENGINE FIRE WARNING LIGHT ILLUMINATED IN FLIGHT. THE FIGHT CREW CHANGED DIRECTION OF FLIGHT TO DETERMINE IF THE SUNLIGHT MIGHT BE CREATING A PROBLEM WITH THE PHOTOCELL. THE FIRE LIGHT DID NOT EXTINGUISH. THE Nov 10, 2006 · N5ST · Beech 200BEECH · Fire DetectionSDR 2006F00050Windscreen · failedON A LEG, ENROUTE, AT CRUISE ALTITUDE OF FL250, THE INNER PANE OF THE RT WINDSCREEN SHATTERED, THE CREW THEN LANDED AT THE NEAREST SUITABLE AIRPORT (ERI), WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRIED BACK, WHERE THE WINDSCREEN WAS REPLACED WITH P/N 101-3Oct 21, 2006 · N942CE · Beech B200 · Flight Compartment WindowsSDR 2006F00051Windscreen · failedON A LEG, AT CRUISE ALTITUDE OF FL250, THE INNER PANE OF THE RT WINDSCREEN SHATTERED, THE CREW THEN LANDED AT THE NEAREST SUITABLE AIRPORT (ERI), WITHOUT FURTHER INCEDENT. THE AIRCRAFT WAS FERRIED BACK TO DEPARTURE WERE THE WINDSCREEN WAS REPLACED WITH P/N 101Oct 21, 2006 · N942CE · Beech B200 · Flight Compartment WindowsSDR 2006FA0001150Lock Plate · misinstalledDURING POST ACCIDENT INSPECTION OF RT AND LT MAIN LANDING GEAR DRAG LEGS, LOCK PLATES WERE FOUND MOUNTED WITH THE BEVEL AT THE NOSE OF THE PLATE FACING UP. INSPECTION OF 5 OTHER AC FOUND THE BEVEL FACING DOWN. REVIEW OF CURRENT REPS COMPONENT MM IS INCONCLUSOct 17, 2006 · N528WG · Beech 200BEECH · Landing Gear Retraction/Extension SystemSDR CA061019002Frame · cracked(CAN) SPECIAL INSPECTION 50 WAS COMPLETED AS PER RAYTHEON MM 5-20-05, WHICH INVOLVES THE FOLLOWING: FRAME WEB FS 179 THROUGH FS 271 INSPECT THE FRAME WEBS FOR CRACKS FROM THE LIGHTNING HOLES AND STRINGER CUTOUTS. THE FRAMES SHOULD BE INSPECTED FROM THE LOWEOct 13, 2006 · Beech 200BEECH · Fuselage Main, FrameSDR CA060926003Windshield · cracked(CAN) IN HOLDING PATTERN AT 9,000 FT/-2C/WINDSHIELD HEAT ON LOW; OUTER PANE OF WINDSHIELD CRACKED FOR NO APPARENT REASON. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. NO EVIDENCE OF BIRD STRIKE OR FOREIGN OBJECT DAMAGE NOTED. (TC NR 20060926003)Sep 21, 2006 · Beech 200BEECH · Flight Compartment WindowsSDR CA060921005Wire · contaminated(CAN) CREW HAD A FIRE WARNING LIGHT COME ON IN FLIGHT, CREW FOLLOWED PROCEDURES AND TURNED THE AIRCRAFT 90 DEGREES TO RULE OUT LIGHT POSSIBLY TRIPPING DETECTORS AND LIGHT REMAINED ON. NO SIGN OF FIRE WAS NOTED VISUALLY ON WING NOR ON THE GLANCE OF INSTRUMENTATSep 19, 2006 · Beech 200BEECH · Fire Protection System WiringSDR SX4A0609001Planetary Gear · brokenGEAR BOX FAILURE ON NR1 ENGINE JUST AFTER TAKE OFF, INDICATED BY CHIP DETECTOR LIGHT.Sep 8, 2006 · N485R · Beech 200BEECH · Turbine Engine Reduction GearSDR SX4A0609002Planetary Gear · brokenGEARBOX FAILURE ON NR 1 ENGINE JUST AFTER TAKE OFF, INDICATED BY CHIP DETECTOR LIGHT.Sep 8, 2006 · N485R · Beech 200BEECH · Turbine Engine Reduction GearSDR SX4A200609002Planetary Gear · brokenGEARBOX FAILURE ON NR 1 ENGINE JUST AFTER TAKE OFF, INDICATED BY CHIP DETECTOR LIGHT.Sep 8, 2006 · N485R · Beech 200BEECH · Turbine Engine Reduction GearSDR 2007FA0000441Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE.POWER SECTION WAS REMOVED FOR REPAIR.Sep 8, 2006 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR 2007FA0000376Exhaust Duct · crackedWHILE PERFORMING SCHEDULED MAINTENANCE,REMOVED LT ENGINE EXHAUST STACK TO FACILITATE INSPECTING THE EXHAUST DUCT. FOUND CRACK FOLLOWING THE CIRCUMFERENCE OF THE SKI SLOPE. THE EXHAUST DUCT HAD PWA SB 3380 COMPLIED WITH 431 HOURS EARLIER. POWER SECTION WAS REMSep 7, 2006 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR 2007FA0000407Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE.POWER SECTION WAS REMOVED FOR REPAIR.Sep 4, 2006 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR 2007FA0000424Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE.POWER SECTION WAS REMOVED FOR REPAIR.Aug 20, 2006 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR CA060928004Torque Knee · cracked(CAN) DURING A ROUTINE INSPECTION THE LT UPPER TORQUE KNEE WAS FOUND CRACKED. THE TORQUE KNEE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. SEE ATTACHED PICTURES. (TC NR 20060928004)Aug 17, 2006 · Beech 200BEECH · Main Landing GearSDR 2007FA0000409Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE.POWER SECTION WAS REMOVED FOR REPAIR.Aug 12, 2006 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR CA060810005Transmitter · failed(CAN) ON TAKEOFF RT TORQUE TRANSMITTER WAS READING HIGH AIRCRAFT RETURNED AIRPORT. AIRCRAFT ELECTRICAL POWER TURNED OFF AND TORQUE INDICATOR WENT TO ZERO. A GROUND RUN WAS ACCOMPLISHED AND TORQUE INDICATION WAS NORMAL AT HIGH AND LOW POWER SETTINGS. AIRCRAFT RAug 6, 2006 · Beech 200BEECH · Engine BMEP/Torque IndicatingSDR 2006FA0000740Exhaust Duct · crackedEXHAUST DUCT ASSY CRACKED AND MISSING PARTS.Aug 4, 2006 · N22932 · Grumav G21A · Engine Collector/Tailpipe/NozzleSDR 2007FA0000432Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE.THE EXHAUST DUCT SB 3380 HAD BEEN COMPLIED WITH 515.2 HOURS PRIOR.POWER SECTION WAS REMOVED FOR REPAIR.Jul 5, 2006 · Beech 200BEECH · Engine Collector/Tailpipe/NozzleSDR CA060629007Outflow Valve · failed(CAN) THE AIRCRAFT EXPERIENCED A LEAK DOWN OF CABIN PRESSURE. THE TROUBLE WAS TRACED TO THE FLOW CONTROL PACK UNITS. BOTH CONTROL UNITS WERE REPLACED WITH OVERHAULED UNITS. THE UNITS THAT WERE INSTALLED NEVER PROVIDED ENOUGH FLOW FOR PRESURIZATION, HEATING Jun 20, 2006 · Beech 200BEECH · Pressure Regulator/Outflow ValveSDR CA060606011Line · leaking(CAN) WHILE APPLYING TAKEOFF POWER THE PILOTS NOTICED SMOKE IN THE CABIN AND ABORTED THE TAKEOFF WITHOUT INCIDENT. DURING INVESTIGATION MAINTENANCE DISCOVERVED THAT A RECENTLY REPLACED OIL PRESSURE LINE TO THE TORQUE TRANSMITTER MANIFOLD WAS LEAKING AT THE FLAJun 5, 2006 · Beech 200BEECH · Turbine Engine Oil SystemSDR CA060529009Pump · failed(CAN) MAINTENANCE INSPECTED THE AIRCRAFT, FOUND MAIN 60A CB TRIPPED RESET CB AND SYSTEM APPEARED TO FUNCTION NORMAL FURTHER INVESTIGATION FOUND HYDRAULIC PUMP WOULD INTERMITTENTLY (ONLY OCCUR ON FIRST SYSTEM POWER UP) INTERNALLY BYPASS CAUSING LOW PRESSURE OMay 18, 2006 · Beech 200BEECH · Hydraulic Pump (Electric/Engine), MainSDR 2006FA0000449Light · burned outFLUORESCENT LIGHT ASSY FAILED AND DISPERSED SMOKE IN CABIN. POWER SUPPLY GOT HOT AND DAMAGED ADJACENT INSULATION. LIGHT ASSY WAS REPLACED WITH FACTORY NEW.May 1, 2006 · N800HA · Beech 200BEECH · Passenger Compartment LightingSDR 2006FA0000450Light · burned outFLUORESCENT LIGHT ASSY FAILED AND DISPERSED SMOKE IN CABIN. POWER SUPPLY GOT HOT AND DAMAGED ADJACENT INSULATION. LIGHT ASSY WAS REPLACED WITH FACTORY NEW.May 1, 2006 · N800HA · Beech 200BEECH · Passenger Compartment LightingSDR CA060403019Engine · failedTHE ENGINE WAS REPORTED TO HAVE EXPERIENCED AN INFLIGHT SHUTDOWN. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS ON THE ENGINE CHIP DETECTOR. P&WC WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.Apr 29, 2006 · Beech 200BEECH · Engine (Turbine/Turboprop)
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