Cessna 340A

Service difficulty reports · 369

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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 = '340A'
  ORDER BY difficulty_date DESC"

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SDR 2006FA0000467Cylinder · crackedAT 400 HR TSO FOUND CYLINDER NR 4 CRACKED AT THE HEAD 5 FINS BACK TOWARD THE BARREL FROM THE TOP SPARK PLUG. CRACK GOES FROM THE EXHAUST VALVE SEAT TO THE TOP SPARK PLUG HOLE ON THE INSIDE OF THE CYLINDER. AD 04-08-10 DID NOT APPLY BY CLY. SN 13516-4 AND COApr 10, 2006 · N984MW · Cessna 340A · Reciprocating Engine Cylinder SectionSDR 2006FA0000405Bellcrank · crackedDURING ANNUAL INSPECTION FOUND NOSE GEAR STEERING BELLCRANK ASSY #5942001-1 CRACKED LEFT AND RIGHT SIDES AT PIVOT RADIOUS. NEW REPLACEMENT PART WITH SAME PART NUMBER OBTAINED FROM CESSNA AIRCRAFT IS MADE MUCH HEAVIER WITH ADDITIONAL MATERIAL IN CRACK PRONE AREMar 31, 2006 · N340JY · Cessna 340A · Landing Gear Steering SystemSDR 2006FA0000404Bellcrank · crackedDURING ANNUAL INSPECTION FOUND NOSE GEAR STEERING BELLCRANK ASSY #5942001-1 CRACKED LEFT AND RIGHT SIDES AT PIVOT RADIOUS. NEW REPLACEMENT PART WITH SAME PART NUMBER OBTAINED FROM CESSNA AIRCRAFT IS MADE MUCH HEAVIER WITH ADDITIONAL MATERIAL IN CRACK PRONE AREMar 31, 2006 · N340JY · Cessna 340A · Landing Gear Steering SystemSDR 2006FA0000333Bulkhead · corrodedDURING 500 HR. VISUAL INSPECTION PER AD2000-01-16 PARA (D) FOUND LEFT ENGINE AFT CANTED BULKHEAD NR 5695005-11 AND SUPPORT DOUBLER NR 5695005-6 CORRODED AND HEAT DAMAGED COMPLETELY THROUGH STRUCTURE. DAMAGE LOCATED NEAR OB SECTION ABOVE EXHAUST ELBOW CUT OUT Mar 27, 2006 · N340JY · Cessna 340A · Nacelle/Pylon, Bulkhead/FirewallSDR 2006FA0000332Bulkhead · corrodedDURING 500 HR. VISUAL INSPECTION PER AD2000-01-16 PARA (D) FOUND LEFT ENGINE AFT CANTED BULKHEAD #5695005-11 AND SUPPORT DOUBLER #5695005-6 CORRODED AND HEAT DAMAGED COMPLETELY THROUGH STRUCTURE. DAMAGE LOCATED NEAR OUTBOARD SECTION ABOVE EXHAUST ELBOW CUT OUMar 27, 2006 · N340JY · Cessna 340A · Nacelle/Pylon, Bulkhead/FirewallSDR 2005FA0000980Pan · crackedAFT PAN ASSY IN TAIL CRACKED. THIS IS A RECURRING ISSUE WITH OUT FLEET. PROBABLE CAUSE IS EXCESS FLEX IN TAIL. RECOMMEND CLOSER INSPECTION DURING 100 HR/ANNUAL INSPECTIONS. (GL21200502750) (K)Jun 14, 2005 · N340AX · Cessna 340A · Fuselage Miscellaneous StructureSDR 2005FA0000994Line · corrodedDURING ANNUAL INSPECTION FOUND FUEL STAINS ON CROSSFEED LINE UNDER CABIN FLOOR PANEL. FOUND CROSSFEED LINE CORRODED THROUGH. LINE WAS LEAKING AT A CORRODED AREA. THERE WAS NOTHING TOUCHING FUEL LINE. (GL21200502745) (K)Jun 9, 2005 · N98560 · Cessna 340A · Aircraft Fuel Distribution SystemSDR 2005FA0000642Pan · crackedDURING ANNUAL INSPECTION, TECH WAS INSPECTING TAIL SECTION. PAN IS ATTACHED TO A BULKHEAD WHICH ARE THE PRIMARY STRUCTURE (AFT) FOR THE HORIZONTAL AND VERTICAL STABILIZERS. TAIL FLEX IS TRANSFERRING TO THIS ASSY AND IS CAUSING CRACKS ON THE RADIUS. (K)Apr 12, 2005 · N234PS · Cessna 340A · Vertical Stabilizer, Attach FittingsSDR 2005FA0000641Pan · crackedDURING ANNUAL INSPECTION TECHNICIAN WAS INSPECTING TAIL SECTION. THE PAN (AFT) IS ATTACHED TO BULKHEAD WHICH ARE PRIMARY STRUCTURE (AFT) FOR HORIZONTAL AND VERTICAL STABILIZER. TAIL FLEX IS TRANSFERRING TO THIS ASSY AND IS CAUSING CRACKS IN THE RADIUS. (K)Apr 12, 2005 · N98560 · Cessna 340A · Vertical Stabilizer, Attach FittingsSDR 2004FA0000631Clamp · crackedWHILE DOING THE EXHAUST AD2000-01-16, THE ONE PIECE V CLAMP THAT HOLDS THE EXHAUST TO THE TURBO WAS FOUND CRACKED APPROX 50 PERCENT AROUND, REPLACED CLAMP AND LEAK CHECKED OK. THE CRACKED CLAMP DID NOT APPEAR TO BE OVER TORQUED.Jun 23, 2004 · N346FS · Cessna 340A · Engine Collector/Tailpipe/NozzleSDR BHA07RSGovernor · malfunctionedDURING CRUISE, AT AN ALTITUDE OF 10,000 FEET, THE PILOT NOTICED A REDUCTION IN MANIFOLD PRESSURE AND POWER FOR THE LEFT ENGINE. THE LEFT PROPELLER STARTED TO FEATHER. THE PILOT SHUT DOWN THE LEFT ENGINE AND LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. POST FLIJun 3, 2004 · N115BH · Cessna 340A · Propeller GovernorSDR 2004F00148Governor · making metalDURING CRUISE, AT AN ALTITUDE OF 10,000 FEET, THE PILOT NOTICED A REDUCTION IN MANIFOLD PRESSURE AND POWER FOR THE RIGHT ENGINE. THE RIGHT PROPELLER STARTED TO FEATHER. THE PILOT SHUT DOWN THE RIGHT ENGINE AND LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. POST Jun 2, 2004 · N115BH · Cessna 340A · Propeller GovernorSDR 2004FA0000653Line · corrodedOIL PRESSURE HARD LINES LEAKING OIL UNDER CABIN FLOOR AFT OF PILOTS AND COPILOTS SEATS. LINES MAKE A 90 DEGREE TURN FORWARD AND CONTACT CABIN DUCTWORK. LINE CORRODED AND APPROXIMATELY 2-3 QUARTS OF OIL DISCOVERED IN CABIN BELOW FLOOR.Apr 20, 2004 · N68245 · Cessna 340A · Turbine Engine Oil SystemSDR AW42004F00000Valve · brokenDURING CRUISE, THE EGT INDICATION FOR THE NR 2 CYL OF THE RT ENGINE DROPPED TO ZERO. THIS WAS ACCOMPANIED BY VIBRATION, SLIGHT LOSS OF MANIFOLD PRESSURE AND A SLIGHT DECREASE IN THE CHT AND EGT INDICATIONS FOR CYLINDERS NR 4 AND NR 5. RETURNED TO DEPARTURE BMar 23, 2004 · N3911G · Cessna 340A · Reciprocating Engine Cylinder SectionSDR 2004F00107Stud · looseDURING CLIMB OUT, THE PILOT NOTICED THE RIGHT ENGINE OIL PRESSURE GAGE INDICATING A SIGNIFICANT INCREASE IN PRESSURE. WHEN THE RIGHT ENGINE STARTED TO RUN ROUGH THE ENGINE WAS SECURED AND THE PROPELLER WAS FEATHERED AS A PRECAUTION. THE AIRCRAFT RETURNED TO Mar 10, 2004 · N114BH · Cessna 340A · Engine (Reciprocating)SDR BHA03RSEngine · damagedDURING FLIGHT, RT ENGINE OIL PRESSURE GAGE INDICATED A SIGNIFICANT INCREASE IN PRESSURE. RT ENGINE DAMAGE OCCURRED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.Feb 23, 2004 · N114BH · Cessna 340A · Engine (Reciprocating)SDR 2004FA0000173Downlock Switch · failedLANDING GEAR WOULD NOT EXTEND, FOUND LANDING GEAR ACTUATOR DOWN LIMIT SWITCH STUCK IN GEAR DOWN POSITION. PERIODIC REPLACEMENT OF SWITCH WOULD BE THE ONLY WAY TO PREVENT REOCURRENCE. THE SWITCH IS A SEALED UNIT AND CANNOT BE INSPECTED INTERNALLY. (GL1720040Jan 22, 2004 · N356D · Cessna 340A · Landing Gear Position and WarningSDR CA040203009Fork · cracked(CAN) CRACK FOUND IN FORK CASTING ON LT SIDE OF TUBE BORE. DISASSEMBLY REVEALED FORK CRACKED COMPLETELY THROUGH LT SIDE OF BORE.Jan 16, 2004 · Cessna 340A · Nose/Tail Landing GearSDR N6P2003F00001Cylinder · crackedCYLINDER NR 1 CRACKED IN THE HEAD AREA NEAR THE EXHAUST SIDE OF THE HEAD. NR 6 CYLINDER IS SUBJECT TO A SB. NR 03-7. THIS CALLS FOR REPLACEMENT OF CERTAIN CYLINDERS MANUFACTURED BETWEEN 9/1/2002 AND 4/21/2003. THIS CYLINDER IS NOT SUBJECT TO THAT BULLENTINNov 5, 2003 · N340AB · Cessna 340A · Reciprocating Engine Cylinder SectionSDR 2003FA0001104Switch · failedAFTER LANDING WHILE TAXING BACK, THE PILOT RETRACTED THE FLAPS. THE UP MICRO SWITCH FAILED TO STOP THE FLAPS AT THEIR UP LIMIT. BOTH CHAINS ATTACHED TO THE FLAP CABLES WERE BROKEN OR DAMAGED. SEVERAL OPERATING RODS WERE DAMAGED AND A PULLEY WAS PULLED OUT OOct 14, 2003 · N340FP · Cessna 340A · Trailing Flap Position Indicating SystemSDR 2003FA0000931Spark Plug · separatedPILOT REPORTED ENGINE ROUGHNESS ON APPROACH AND LOSS OF RIGHT ENGINE NR 3 CYLINDER EGT INDICATION. AIRCRAFT LANDED WITH OUT INCIDENT. INSPECTION REVEALED NR 3 CYLINDER LOWER SPARK PLUG HAD SEPERATED INTO TWO PIECES BETWEEN THE GASKET SURFACE AND THE WRENCH HEXSep 12, 2003 · N6827Z · Cessna 340A · Spark Plug/IgniterSDR LV02003F00000Rib · bentDURING ANNUAL INSPECTION, NOTICED LT ENGINE HUNG LOWER THAN RT. AFTER FURTHER INVESTIGATION, FOUND LT WING RIB (PN 08220009) AT W.S. 63.45 BENT AND DISTORTED. JUST AFT OF FORWARD WING SPAR ALONG WITH OTER MEMBERS IN GEARWELL AREA. SK4148E HAD BEEN PREVIOUSLMay 28, 2003 · N32PT · Cessna 340A · Wing, Rib/BulkheadSDR N6P2003F00000Bolt · brokenDURING REPAIR OF THE TAXI LIGHT WIRES, WHILE REMOVEING THE NUT FROMT HE BOLT ATTACHING AN ADEL CLAMP WHICH HOLES THE WIRE HARNESS TO THE NOSE GEAR SISSORS, AT THE SCISSORS PIVOT POINT, THE BOLT BROKE IN HALF DURING REMOVAL. LOG BOOK RESEARCH INDICATES PREVIOUMay 14, 2003 · N340AB · Cessna 340A · Nose/Tail Landing GearSDR 2003FA0000475Bracket · brokenDURING ANNUAL INSPECTION, ELEVATOR CONTROL SYS HAD EXCESSIVE FREE PLAY. FOUND BRACKETS WERE BROKEN. THESE BRACKETS SUPPORT ELEVATOR BELLCRANK IN TAIL SECTION. BOTH BRACKETS WERE MISSING THREE RIVETS EACH ON THE VERTICAL ANGLE THAT ATTACH RESPECTIVE BRACKET May 13, 2003 · N12315 · Cessna 340A · Elevator Control SystemSDR 2003FA0000585Bolt · bentDURING INSPECTION DISCOVERED ELEVATOR PIVOT BOLT TO BE BENT. REMOVED AND REPLACED BOLT WITH NEW AN4-14. CAUSE COULD BE ATTRIBUTED TO GUST LOCK NOT BEING INSTALLED AND ELEVATOR MOVEMENTS WHILE AIRCRAFT ARE PARKED ON THE RAMP.May 10, 2003 · N98585 · Cessna 340A · Elevator StructureSDR FJC4285Bolt · bentDURING INSPECTION OF THE ELEVATOR SYSTEM THE TECHNICIAN DISCOVERED THE ELEVATOR BELLCRANK BOLT BENT. WE HAVE FOUND SEVERAL BENT IN OUR FLEET, AND WOULD SUGGEST THAT ALL OPERATORS HAVE THE BOLT AND BEARING INSPECTED AS SOON AS POSSIBLE.Apr 11, 2003 · N234PS · Cessna 340A · Elevator Control SystemSDR CTU2003F00004Bolt · bentAFTER FAILURE OF BOLT PRIOR TO FLIGHT OPERATOR CHOSE TO PERFORM INSPECTION OF OTHER 340 AIRCRAFT IN FLEET. BOLT MUST BE REMOVED FOR INSPECTION. THIS BOLT IS THE ELEVATOR BOLT, CRANK PIVOT BOLT. IT ALSO HAS A BEARING WHICH IS SOMETIMES WORN AS WELL.Apr 10, 2003 · N340FR · Cessna 340A · FastenersSDR AUS20030586Slip Joint · cracked(AUS) RT ENGINE EXHAUST SYSTEM SLIP COUPLING CRACKED IN AREA NEAR TRANSITION DUCT.Apr 8, 2003 · Cessna 340A · Engine Collector/Tailpipe/NozzleSDR 2003FA0000011Pump · leakingLOSS OF OIL AND OIL PRESSURE ON RT ENGINE. TROUBLESHOT FOUND LEAKING FROM VACUUM PUMP BASE. REMOVED VACUUM PUMP. FOUND PIECES OF OLD GASKET STILL ATTACHED TO MOUNTING PAD WITH A NEW GASKET INSTALLED. CLEANED MOUNTING BASE, INSTALLED NEW VACUUM PUMP GASKET Dec 3, 2002 · N356D · Cessna 340A · Vacuum Distribution SystemSDR 2002FA0001319Flange · crackedTHE ATTACHING FLANGES BETWEEN THE EXHAUST WYE AND WASTE GATE ELBOW CRACKED ON BOTH PARTS.Oct 16, 2002 · N28RG · Cessna 340A · Engine Collector/Tailpipe/NozzleSDR 2002FA0001318Flange · brokenTHE ATTACHING FLANGES BETWEEN THE EXHAUST WYE AND WASTE GATE ELBOW CRACKED ON BOTH PARTS.Oct 16, 2002 · N28RG · Cessna 340A · Engine Collector/Tailpipe/NozzleSDR 2002FA0001170Bellcrank · brokenRIGHT MAIN LANDING GEAR COLLAPSED ON ROLLOUT AFTER TOUCHDOWN. INITIAL INSPECTION REVEALED OUTBOARD MAIN LANDING GEAR RETRACTION LINK (PN 504100112) SEPARATED FROM RIGHT MAIN LANDING GEAR STRUT AT ITS TWO ATTACH POINTS. BOTH BREAKS APPEAR TO BE INSTANTANEOUS Sep 26, 2002 · N340FS · Cessna 340A · Main Landing Gear Attach SectionSDR CTU2003F00000Bolt · bentAFTER FAILURE OF BOLT PRIOR TO FLIGHT MAINTENANCE FACILITY PERFORMED INSPECTION OF BOLT WHICH THE ELEVATOR BELLCRANK ROTATION. BOLT MUST BE REMOVED FOR PROPER INSPECTION. BOLTS HAVE BOTH STRESSED AND BENT. MANUFACTURER SHOULD HAVE BOLT OF LARGER SIZE INSTALAug 16, 2002 · N98560 · Cessna 340A · FastenersSDR MW22002F00000Crankshaft · brokenCRANKSHAFT BROKEN IN TWO PIECES AT NR 3 ROD CHEEK.Jul 15, 2002 · N3963G · Cessna 340A · Reciprocating Engine Power SectionSDR AUS20020519Line · chafed(AUS) LT ENGINE OIL PRESSURE INDICATOR LINE LOCATED IN THE STUB WING ADJACENT TO THE NACELLE WORN THROUGH IN SEVERAL PLACES BY CONTACT WITH THE LH ENGINE BLEED AIR DUCT.May 24, 2002 · Cessna 340A · Engine Oil PressureSDR D682002F00000Magneto · seizedOWNER-PILOT REPORTED BAD MAGNETO CHECK. RIGHT ENGINE LEFT MAGNETO INVESTIGATION FOUND LEFT MAGNETO WAS SEIZED AND COULD NOT BE TURNED BY HAND. PREVIOUSLY IT WAS THE RIGHT MAGNETO. REASON FOR MAG SEIZING IS EXCESSIVE HEAT, ALSO BEING PRESSURIZED. NO LOGS May 17, 2002 · N340KG · Cessna 340A · Magneto/DistributorSDR 2002F00458Downlock Switch · brokenLT MLG DOWN LIGHT FAILED TO ILLUMINATE ON APPROACH. EMERGENCY GEAR SYSTEM ACTIVATED. AIRCRAFT LANDED SAFELY AT MAIN BASE. FOUND LT MLG DOWNLOCK SWITCH ACTUATOR BROKEN.May 9, 2002 · N118BH · Cessna 340A · Landing Gear Position and WarningSDR 2002FA0000452Cylinder · failedIN FLIGHT, PILOT NOTICED REDUCTION IN MANIFOLD PRESSURE. PILOT DESCENDED WHEN COMPLETE FAILURE AND SEPARATION OF THE NR 4 CYLINDER ON THE LEFT ENGINE OCCURRED. CYLINDER HEAD SEPARATED FROM BARREL. ENGINE WAS SECURED AND SHUT DOWN. PROP WAS FEATHERED. THE Mar 22, 2002 · N234PS · Cessna 340A · Reciprocating Engine Cylinder SectionSDR IC1D213KChannel · crackedAIRCRAFT PAN CHANNEL JUST BELOW HORIZONTAL STABILIZER AFT SPAR ON EMPENAGE STRUCTURE HAS (NR 2)-.7500 INCH CRACKS IN RADIUSED AREAS. CRACKS WERE FOUND ON ANNUAL INSPECTION PROBABLE CAUSE UNKNOWN STRESS. RECOMMENDATION: DETAILED INSPECTION AT ANNUAL INSPECTIONFeb 12, 2002 · N324WA · Cessna 340A · Fuselage Miscellaneous StructureSDR 2002FA0000226Beam · corrodedFOUND RT OUTBOARD ENGINE BEAM CORRODED BEYOND LIMIT, CANTED BULKHEAD WAS ALSO CORRODED BEYOND LIMITS. SUGGEST SHORTER INTERVAL BETWEEN INSPECTIONS.Feb 6, 2002 · N2696U · Cessna 340A · Engine Mount SectionSDR 2002FA0000174Exhaust Pipe · crackedPILOT OBSERVED RT FUEL QUANTITY INDICATOR FAILED, THEN RT FUEL TRANSFER LIGHT ON AND RT LANDING LIGHT CIRCUIT BREAKER POPPED. AFTER FLIGHT, VISUAL INSPECTION OF THE RT ENGINE NACELLE IDENTIFIED A BURN THROUGH NACELLE SKIN ADJACENT TO THE RT ENGINE OVERBOARD TJan 23, 2002 · N340WT · Cessna 340A · Engine Collector/Tailpipe/NozzleSDR 2002FA0000130Valve · faultyREPLACED DEFECTIVE SURFACE DEICE CONTROL VALVE WITH NEW 2H48-14 S/N 2AU 29. ON RUN CHECK FOUND SYSTEM TO HAVE UNCOMMANDED SURFACE DEICE ACTIVATION. CHECKED SYSTEM AND FOUND NEW VALVE LEAKING FROM FAULTY ASSEMBLY AT RIVETED TOP CAP WHERE SOLENOID IS ATTACHED.Jan 23, 2002 · N340SV · Cessna 340A · Airfoil Anti/De-ice SystemSDR 2001F00758Clamp · crackedNEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS.Dec 10, 2001 · N114BH · Cessna 340A · Engine Collector/Tailpipe/NozzleSDR 2001F00764Clamp · crackedNEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS.Dec 7, 2001 · N118BH · Cessna 340A · Engine Collector/Tailpipe/NozzleSDR CRJ2002F00000Shuttle Valve · failed"INOP BTN" ON VAC GAGE WOULD NOT COME OUT WITH ONE ENG SHUT DOWN. REMOVED MAINFOLD, ONE CK VLV WOULD NOT SEAL. CLEANED VLV WITH ALCOHOL AND FUNC TESTED. REINSTALLED VLV AND FUNC TEST WAS OK. INOP BTN FAILED. REPLACED MANIFOLD PN 1H510. FUNC TEST SHOWED Dec 1, 2001 · N5421J · Cessna 340A · Airfoil Anti/De-ice SystemSDR 2001FA0000661Coupling · shearedPNEUMATIC PUMP COUPLING SHEARED AFTER 230.7 HOURS OF OPERATION.Nov 20, 2001 · N2741R · Cessna 340A · Vacuum Distribution SystemSDR OKT2001F00000Relay · failedLANDING GEAR FAILED TO RETRACT AFTER TAKEOFF, AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOT LANDING GEAR SYSTEM AND FOUND LANDING GEAR RELAY TO BE INOPERATIVE. PROBABLE CAUSE FOUND TO BE CYCLIC TIME OF PART. LANDING GEAR FUNCTIONAL CHECK SATISFACTORY AT PREVNov 20, 2001 · N2670H · Cessna 340A · Landing Gear Retraction/Extension SystemSDR 2001F00763Clamp · crackedNEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS.Nov 9, 2001 · N118BH · Cessna 340A · Engine Collector/Tailpipe/NozzleSDR 2001FA0000531Screw · brokenDOWNLOCK ADJUSTING SCREW BROKE FOR REASONS UNKNOWN.THIS ALLOWED LEFT MAIN GEAR TO LOSE DOWNLOCK TENSION. LEFT MAIN LANDING GEAR RETRACTED UNTIL IT STOPPED AGAINST INBOARD GEAR DOOR. THIS ALLOWED PROP TO HIT THE GROUND AND DAMAGE TO LEFT FLAPS OCCURED.Nov 8, 2001 · N115BH · Cessna 340A · Landing Gear Retraction/Extension SystemSDR 2001FA0000545Magneto · corrodedPILOT NOTED INTERMITTENT ROUGH ENGINE AND FLUCTUATING EGT. DURING SUBSEQUENT TROUBLE SHOOTING, NOTED ONLY ONE IMPULSE COUPLING SOUND. WHEN PULLING ENGINE THROUGH WITH SPARK PLUGS OUT AND TIMING WAS WAY OFF. UPON REMOVAL FOUND THAT COULD BARELY TURN THE MAGOct 25, 2001 · N340KG · Cessna 340A · Magneto/Distributor
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