Daher TBM 700

Service difficulty reports · 131

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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 = 'TBM700'
  ORDER BY difficulty_date DESC"

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SDR 2013FA0000281Insert · looseINBD FLAP CARRIAGE INSERTS HAVE LOOSENED UP UNDER NORMAL USE. COULD POSSIBLY LEAD TO FLAP CARRIAGE ATTACHMENT FAILURE DURING FLAP DEPLOYMENT WITH SUBSEQUENT LOSS OF FLAP OR WORSE. REQUIRES REPAIR TO FLAP END AND INSTALLATION OF NEW FLAP CARRIAGE INSERTS. THMar 13, 2013 · N700WK · Socata TBM700 · Trailing Edge FlapsSDR 2012FA0000754Rod End · failedPILOT REPORTED UNUSUAL SOUND DURING LOWERING THE LANDING GEAR. WHEN PILOT FLARED FOR LANDING, ON TOUCHDOWN THE RT WING CONTACTED THE GROUND. THE RT MLG ACTUATOR ROD END SEPARATING FROM THE ACTUATOR BALL JOINT CAUSING THE LANDING GEAR TO COLLAPSE. REPLACEDSep 7, 2012 · N850ZM · Socata TBM700 · Landing Gear Retraction/Extension SystemSDR 2012FA0000489Bridal Cable · disengagedON CLIMBOUT, PILOT ENGAGED AUTOPILOT AND ACFT BEGAN TO PITCH UP AND CLIMB. AUTOPILOT WAS DISENGAGED AND CONTROL WAS MAINTAINED. PILOT AGAIN ENGAGED AUTOPILOT AND ACFT ROLLED TO THE LEFT. PILOT DISENGAGED AUTOPILOT AND AGAIN GAINED CONTROL, DELCLARED AN EMERJul 19, 2012 · N854MA · Socata TBM700 · Auto Flight System WiringSDR CA120723001Oil System · malfunctioned(CAN) THE PILOT REPORTED THAT THE OIL PRESSURE HAS DECREASED STEADILY FOR THE PAST 4 FLIGHTS, ENDING VERY CLOSE TO THE YELLOW BAND IN CRUISE ON THE LAST FLIGHT. THE TORQUE ALSO WENT DOWN ON THE LAST FLIGHT, THE PILOT COULD ACTUALLY FEEL IT. AFTER LANDING, THJul 10, 2012 · Socata TBM700 · Engine Oil PressureSDR 2012FA0000425Stop · brokenDURING ANNUAL INSPECTION FOUND LT SECONDARY RUDDER STOP BROKEN. CABLE TENSION CHECK, OK. RUDDER PEDALS STOP PINS CHECKED OK, RUDDER PEDALS STOPS CHECKED OK. THIS ACFT IS NORMALLY PARKED IN HANGER AT HOME STATION. POSSIBLE CAUSE IS WIND OR BLAST FROM ACFT WMay 14, 2012 · N70LT · Socata TBM700 · Rudder StructureSDR 2012FA0000081Fuel Control · failedDURING RUNUP, PROP FEATHER CHECK CONDUCTED NORMALLY. WHEN ADVANCING POWER LEVER TO DO A PROP OVERSPEED TEST, COULD NOT REACH 1900 RPM WITH POWER LEVER FORWARD. HIGHEST RPM ACHIEVED WAS 1700. SHUTDOWN AND RESTART. DURING THE START, AT LOW IDLE, FLAMES SHOTJan 31, 2012 · N701QD · Socata TBM700 · Fuel Control/Turbine EnginesSDR CA120129001Fuel Control · failed(CAN) WHILE PREPARING FOR THE SCHEDULED NIGHT FLIGHTS, AFTER NORMAL ENGINE START, WHILE RUNNING UP TO PERFORM THE FEATHERING CHECK, THE ENGINE COULD ONLY ACHIEVE 1700 RPM ON THE PROPELLER WHERE 1900 RPM SHOULD HAVE BEEN AVAILABLE WITH THROTTLE FULL FORWARD. FLJan 13, 2012 · Socata TBM700 · Fuel Control/Turbine EnginesSDR CA111019003Engine · fod(CAN) DURING CRUISE, THE PILOT HEARD A LOUD NOISE WHICH WAS FOLLOWED BY ENGINE POWER LOSS. THE USE OF THE EMERGENCY POWER LEVER RESULTED IN ONLY 5 PERCENT TORQUE WITH HIGH ENGINE TEMPERATURE. HE DECLARED AN EMERGENCY AND FLEW ACFT TO AIRPORT WHERE AN EVENTFUOct 7, 2011 · Socata TBM700 · Engine (Turbine/Turboprop)SDR 2011FA0000708Fork · brokenDURING PRE-INSPECTION GROUND RUN, FOUND CO-PILOT LT BRAKE PEDAL NOT IN PROPER POSITION AND UNABLE TO APPLY BRAKE. FOUND LT BRAKE FORK BROKEN AT THREADED SHAFT. FOUND BEARING WAS STIFF, CLEANED AND LUBED BEARING ALL OTHER BEARINGS WERE CHECKED AND FOUND OK.Oct 5, 2011 · N123ZC · Socata TBM700 · Landing Gear Brake SystemSDR 2011FA0000369Buss Bar · crackedON DOING A COMPRESSOR/POWER RECOVERY WASH AT MAINTENANCE SHOP. THE GPU PLUG, GROUNDING SHUNT BURNED AND BROKEN IN HALF. THIS IS THE SECOND TIME THIS HAS HAPPENED. THERE IS NO LIMITAION ON GPU USE.Jun 16, 2011 · N378FC · Socata TBM700 · Electrical Power System WiringSDR 2011FA0000329Gasket · separatedPROPELLER OVERSPEED GOVERNOR TO ENGINE PAD GASKET FAILED CAUSING LOSS OF OIL.May 26, 2011 · N175JB · Socata TBM700 · Propeller GovernorSDR 2011FA0000235Tee Fitting · obstructedFUEL PRESSURE INDICATION WENT OT -0- INFLIGHT. `FUEL PRESSURE LOW, ANNUNCIATOR REMAINED UNLIT. NO OPERATIONAL PROBLEMS NOTED. CLEANED ORIFICE IN PLUMBING TEE, ADJACENT TO FUEL PRESSURE TRANSDUCER, AND NORMAL INDICATION WAS RESTORED. THIS IS A RECURRING DIFMar 28, 2011 · N700KP · Socata TBM700 · Aircraft Fuel Distribution SystemSDR 2010FA0000931Control Cable · brokenPERFORMED NORMAL START, NOTED LOW IDLE LOW, MOVED CONDITION LEVER TO HIGH IDLE WITH NO RESPONSE FROM ENGINE, TRIED SEVERAL TIMES & HAD NO RESPONSE. PERFORMED ENGINE SHUTDOWN. MOVED CONDITION LEVER IN COCKPIT WHILE 2ND PERSON WATCHED MOVEMENT ON FCU. MOVEMENTSep 1, 2010 · N843BH · Socata TBM700 · Engine ControlsSDR 2010FA0000527Bracket · crackedATTEMPTING TO START USING A GPU, GPU WAS WORKING NORMAL AND HAD LIGHT OFF OF THE FUEL, ELECTRIC SYS WENT DEAD. THEN IT CAME BACK ON, CONTINUING TO TURN THE STARTER. QUICKLY TURNED OFF THE IGNITION SWITCH AND FUEL CUTOFF. NO HOT START, TEMPS GOT UP HIGH 300'S.Jun 7, 2010 · N378FC · Socata TBM700 · Fuselage Main, Attach FittingsSDR 2010FA0000585Shutoff Valve · intermittent((X1IR)) ACFT OWNER COMPLAINED OF PRESSURIZATION PROBLEM AT FL 290 WHERE THE CABIN PRESSURE WOULD INTERMITTENTLY DROP FROM 6.2 TO 4.0 UPON INVESTIGATION, FOUND THE ACFT DID NOT SWITCH FROM 3.0 TO 2.5 BLEED AIR. CAUSE IS DETERMINED, DUE TO THE SHUTOFF VALVE HNov 6, 2009 · N850GS · Socata TBM700 · Pressure Regulator/Outflow ValveSDR 2009FA0000623Shaft · fracturedDURING START ATTEMPT, THE POWER SECTION DID NOT ROTATE WHEN THE NG REACHED 13 PERCENT. START WAS ABORTED AND PROPELLER TURNED BY HAND. A NOISE WAS HEARD FROM THE EXHAUST STACK AND DRAGGING/BINDING WAS FELT. POWER SECTION WAS REMOVED AND SENT FOR TROUBLESHOJul 10, 2009 · N708PW · Socata TBM700 · Turbine SectionSDR CA080814007Wheel Half · cracked(CAN) DURING LANDING ROLL, PILOT NOTICED ABNORMAL "FEEL" OF ACFT AND STEERING. DISCOVERED FLAT TIRE ON RT MAIN WHEEL. ACFT RECOVERED FROM RUNWAY. DISASSEMBLED WHEEL AND PERFORMED DYE PENETRANT INSP ON WHEEL HALVES. CRACK INDICATION VERY EVIDENT IN INNER BEAD Aug 14, 2008 · Socata TBM700 · Wheel/Ski/FloatSDR 2008FA0000069Hinge · crackedHINGE FOUND CRACKED IN AREA OF CONCERN IDENTIFIED IN AD 99-07-11, PREVIOUS INSPECTION 100 HOURS EARLIER SHOWED NO SIGN OF CRACKING.Jan 23, 2008 · N800GS · Socata TBM700 · Horizontal Stabilizer StructureSDR 2007FA0000329Fitting · corrodedDURING A 6000HR/10 YEAR CORROSION INSPECTION AD2007-06-11 WAS BEING COMPLIED IAW AD AND MANDATORY SB70-104, AMENDMENT 2. AFTER COMPLETING THE PENETRANT INSPECTION, NO CRACKS WERE DETECTED IN THE SPECIFIED AREAS HOWEVER THE FITTINGS LISTED IN BLOCK 5 WERE REMOApr 6, 2007 · N704QD · Socata TBM700 · Horizontal Stabilizer StructureSDR 2007FA0000328Fitting · crackedDURING A 6000HR/10 YEAR CORROSION INSPECTION AD2007-06-11 WAS BEING COMPLIED IAW AD AND MANDATORY SB70-=104, AMENDMENT 2. AFTER COMPLETING THE PENETRANT INSPECTION NO CRACKS WERE DETECTED IN THE SPECIFIED AREAS HOWEVER THE FITTINGS LISTED IN BLOCK 5 WERE REMOApr 6, 2007 · N704QD · Socata TBM700 · Rudder/Tab, Attach FittingsSDR CA061219022Engine · leaking(CAN) IN FLIGHT THE ENGINE OIL TEMPERATURE INCREASED ACCOMPANIED BY A LOSS OF OIL PRESSURE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METAL CONTAMINATION OF THE OIL SYSTEM, INTERNAL OIL LEAKAGE AND SEIZURE OF THE REDUCTION GEAR BOX. Sep 25, 2006 · Socata TBM700 · Turbine Engine Oil SystemSDR CA061103004Oil System · overtemp(CAN) IN FLIGHT ENGINE OIL TEMPERATURE WAS SEEN TO INCREASE ACCOMPANIED BY A DROP IN OIL PRESSURE. THE ENGINE WAS SHUTDOWN IN FLIGHT. POST FLIGHT INSPECTION REVEALED DEBRIS IN THE ENGINE OIL SYSTEM AND EVIDENSE OF OIL LEAKAGE FROM THE ENGINE DRAIN. MFG WILLSep 25, 2006 · Socata TBM700 · Turbine Engine Oil SystemSDR CA061006020Engine · seized(CAN) ENGINE OIL TEMPERATURE WAS SEEN TO INCREASE IN FLIGHT ACCOMPANIED BY A LOSS OF OIL PRESSURE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED OIL IN THE ENGINE DRAINS AND SEIZURE OF THE POWER SECTION. MFG WILL INVESTIGATE THE EVENT ANSep 25, 2006 · Socata TBM700 · Engine (Turbine/Turboprop)SDR 1MAC06Cable · frayedFRAYED ELEVATOR TRIM CABLE FOUND DURING 100 HR INSPECTION IN AFT FUSELAGE ACCESS PANEL.Apr 10, 2006 · N930MA · Socata TBM700 · Elevator Tab Control SystemSDR CA060327003Line · contaminatedDURING BIANNUAL ALTIMETER SYSTEM TEST AND INSPECTION PILOTS ALTIMETER AND VSI RESPONDED ERRATICALLY TO INCREASING/DECREASING PRESSURE. WATER DROPLETS WERE FOUND IS PILOTS STATIC SYSTEM BETWEEN NR 1 LEFT STATIC VENT AND Y CONNECTION TO RIGHT VENT.Mar 24, 2006 · Socata TBM700 · Pitot/Static SystemSDR 2006FA0000248Attach Bracket · crackedDURING A 6000 HOUR INSPECTION, THE LT AND RT WING TIP ASSEMBLIES WERE REMOVED TO FACILITATE FURTHER INSPECTION OF THE AILERON SYSTEM. AFTER REMOVAL OF THE TIPS THE INSPECTING TECHNICIAN NOTED CRACKS IN BOTH THE LT AND RT AILERON OB ATTACH POINTS. THE BRACKETFeb 21, 2006 · N701QD · Socata TBM700 · Wing, Attach FittingsSDR 2006FA0000247Support Bracket · crackedDURING A 6000 HOUR INSPECTION, THE LT AND RT WING TIP ASSEMBLIES WERE REMOVED TO FACILITATE FURTHER INSPECTION OF THE AILERON SYSTEM. AFTER REMOVAL OF THE TIPS THE INSPECTING TECHNICIAN NOTED CRACKS IN BOTH THE LT AND RT AILERON OB ATTACH POINTS. THE BRACKETFeb 21, 2006 · N701QD · Socata TBM700 · Wing, Attach FittingsSDR 2006FA0000246Attach Bracket · crackedDURING A ROUTINE PHASE INSPECTION, THE LT WING TIP ASSY WAS REMOVED TO FACILITATE FURTHER INSPECTION OF THE AILERON CABLE. AFTER REMOVAL OF THE TIP, THE INSPECTING TECHNICIAN NOTICED A CRACK IN AT THE OB ATTACH POINT. THE BRACKET WAS REMOVED AND INSPECTED WIFeb 21, 2006 · N703QD · Socata TBM700 · Wing, Attach FittingsSDR 2006FA0000169Electrical Box · overheatedDURING THE START SEQUENCE WHEN THE PILOT SELECTED THE START POSITION THE STARTER WOULD NOT RESPOND. THE PILOT COULD HEAR THE SOUND OF RELAY CONTACTS BUT THE STARTER WOULD NOT RESPOND. THE AIRCRAFT WAS EXAMINED BY A LINE TECHNICIAN WHO REPORTED THE ELECTRICALFeb 10, 2006 · N704QD · Socata TBM700 · Engine Starting System WiringSDR 2006FA0000126Flap · excess playFLAP SN SC279 WAS REMOVED FROM SERVICE FOR LOOSE ATTACHMENT INSERTS ON THE IB END RIB. THE FLAP ATTACH CARRIAGE WAS DISCOVERED LOOSE DURING A ROUTINE DAILY PPOST FLIGHT INSPECTION, WHERE PLAY WAS NOTED BETWEEN THE FLAP ATTACH CARRIAGE AND THE IB FLAP END RIB.Jan 26, 2006 · N704QD · Socata TBM700 · Trailing Edge FlapsSDR 2005FA0000345Actuator · frozenAFTER THE AIRCRAFT HAD BEEN LEFT OUT IN THE RAIN, THE PREVIOUS DAY, THE AC WAS FLOWN. UPON HAND FLYING THE AIRCRAFT TO ALTITUDE, THE PILOT REPORTED THA THE TRIM WHEEL BECAME INCREASINGLY MORE DIFFICULT TO MOVE AS HE ENTERED FREEZING LEVELS. AT OAT -8 THE TRIFeb 22, 2005 · N883CA · Socata TBM700 · Elevator Tab Control SystemSDR 2004FA0000736Fork · bentLT RUDDER PEDAL WENT TO FLOOR ON TAXI OUT. FOUND FORK END SHEARED AT JAM NUT. WHEN BOLT AND CASTLE NUT WERE REMOVED, CASTLE NUT WAS EXTREMELY TIGHT AND BOLT COULD NOT ROTATE. THIS COULD BE CAUSE OF THE PROBLEM. RUDDER PEDAL NUT AND BOLT ON OTHER RUDDER PEDSep 13, 2004 · N220MA · Socata TBM700 · Rudder Control SystemSDR 2005FA0000288Rib · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUCAug 9, 2004 · Socata TBM700 · Trailing Edge FlapsSDR 2005FA0000287Carriage · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR METAL CARRIAGE ASSY (PN TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUAug 9, 2004 · Socata TBM700 · Trailing Edge FlapsSDR 2005FA0000286Rib · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUAug 9, 2004 · Socata TBM700 · Trailing Edge FlapsSDR 2005FA0000285Rib · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUAug 9, 2004 · Socata TBM700 · Trailing Edge FlapsSDR 2005FA0000284Rib · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUAug 9, 2004 · Socata TBM700 · Trailing Edge FlapsSDR 2005FA0000283Rib · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUAug 9, 2004 · Socata TBM700 · Trailing Edge FlapsSDR 2005FA0000282Rib · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUAug 9, 2004 · Socata TBM700 · Trailing Edge FlapsSDR 2005FA0000281Rib · failedTHE BONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSEMBLY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS Aug 9, 2004 · Socata TBM700 · Trailing Edge FlapsSDR 2003FA0000680Turnbuckle · unsafetiedDURING THE FIRST ONE HUNDRED HOUR INSPECTION OF THIS AIRCRAFT THE AFT TURNBUCKLE FOR THE RUDDER SYSTEM, AS VIEWED THROUGH ACCESS DOOR 311, HAD FIVE THREADS EXPOSED ON LOWER END AND FOUR THREADS EXPOSED ON UPPER END. BOTH ENDS WERE SAFETIED WITH CLIPS. CLOSE May 30, 2003 · N459MA · Socata TBM700 · Rudder Control SystemSDR FCPR20030010Autopilot Sys · malfunctionedPILOT REPORTED THAT WHILE FLYING IN IMC CONDITIONS WITH AUTO PILOT ENGAGED IN HEADING MODE, HE COMMANDED A COURSE CHANGE AND THE AUTOPILOT PERFORMED A TURN IN THE OPPOSITE DIRECTION. CONDUCTED AT P-STATIC TEST AND FOUND SEVERAL STATIC WICKS NOT BONDED CORRECTMay 6, 2003 · N700PX · Socata TBM700 · Autopilot SystemSDR 2003FA0000412Valve · leakingAIRCRAFT ARRIVED WITH AN OXYGEN LEAK. THE ALTIMETRIC VALVE WAS REPLACED. THE REPLACEMENT VALVE ALSO LEAKED. THE THIRD VALVE INSTALLED DIDN`T LEAK IN THE OFF POSITION BUT WHEN THE PASSENGER OXYGEN WAS TURNED ON DEPLOYING THE MASKS THE VALVE LEAKED FROM THE Mar 21, 2003 · N700RK · Socata TBM700 · Passenger Oxygen SystemSDR TBM700Blade · failedEXPERIENCED A TOTAL POWER FAILURE WHILE DESCENDING FROM FL250 TO FL240. PILOT MADE A SUCCESSFUL DEAD STICK LANDING. INSPECTION OF THE ENG REVEALED A CATASTROPHIC FAILURE OF A COMPRESSOR TURBINE BLADE WHICH RESULTED IN A COMPLETE ENGINE STOPPAGE AND LOCKING UPFeb 21, 2003 · N12WY · Socata TBM700 · Turbine Engine Compressor SectionSDR 2002FA0001384Bearing · failedA/C EXPERIENCED SUDDEN POWER LOSS & ENG STOPPAGE, AND A EMERGENCY LANDING FROM FL245. NO EXTERNAL OIL LEAKS, AND OIL LEVEL WAS DOWN 3 QUARTS FROM FULL. INSPECT OF THE POWER TURBINE SHOWED FOD AND A SMALL AMOUNT OF MELTED METAL IN THE DUCT. PROP SHAFT COULD Dec 12, 2002 · N12WY · Socata TBM700 · Turbine Engine Compressor SectionSDR S5656Seat Belt · failedREF. SAIB NO.CE-02-44 DATED SEPTEMBER 4, 2002 PREBUY ON AIRCRAFT CHECK, ALL CABIN AND COCKPIT SEAT BELTS COULD BE PULLED APART WITH A SLIGHT PULL OR TUG. WOULD NOT STAY ENGAGED RECOMMEND REPLACEMENT OF ALL BELTS WITH NEWER STYLENov 20, 2002 · N700PP · Socata TBM700 · Flight Compartment EquipmentSDR CA021204004Sleeve · cracked(CAN) MAG PARTICAL INSPECTION FOUND CRACK INDICATION ON THE B476 SLEEVE UNIT AT THE SLOTTED END ABOUT 1/8 INCH LONG. HARTZELL SERVICE BULLETIN 61235 INCORPORATED.Nov 14, 2002 · Socata TBM700 · Propeller Feathering/ReversingSDR CA021204003Dowel Pin · broken(CAN) DURING OVERHAUL A BROKEN COUNTERWEIGHT DOWEL PIN WAS DISCOVERED. NEW INSTALLED.Nov 14, 2002 · Socata TBM700 · Propeller Blade SectionSDR CA021204002Bolt · failed(CAN) DURING PROPELLER OVERHAUL, BOLT PN A2431 WAS MAGNAFLUXED AND FOUND A CRACK INDICATION RUNNING LENGTH WISE ON THE BOLT THREADS. NEW BOLT INSTALLED.Nov 14, 2002 · Socata TBM700 · Propeller AssemblySDR 2002FA0001198Seat Belt · failedSEAT BELT BUCKLE CAME APART WITH A SIMPLE JERK TEST. WITH A STEADY PULL ON THE SEAT BELTS THE BELTS HOLD OK. ALL BELTS IN THE AIRCRAFT DID THE SAME THING. SEAT BELTS ARE MANUFACTURED BY ANJOU AERONAUTIQUE, THERE IS A SOCATA SERVICE LETTER SL70-027 THAT INFOct 17, 2002 · N700SP · Socata TBM700 · Passenger Compartment Equipment
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