Beech 58P

Service difficulty reports · 123

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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 aircraft_model_key = '58P'
  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 2017FA0000368Clutch · brokenFOUND FWU SEIZED. DISASSEMBLY FOUND CLUTCH CAGE BROKE BETWEEN SPRAGS IN TWO PLACES.Apr 6, 2017 · N58TR · Beech 58P · Main Rotor GearboxSDR 2016FA0000218Downlock Arm · brokenSTARBOARD DOWNLOCK ARM ON THE NOSE GEAR FAILED UPON LANDING CAUSING SIGNIFICANT DAMAGE TO ACFT. POST FLIGHT INSPECTON SHOWED THE WELD AT THE BALL JOINT APEARED TO HAVE FAILED.Apr 10, 2016 · N58JC · Beech 58P · Nose/Tail Landing GearSDR 2015FA0000024Separator · crackedPILOT REPORTED LT ENGINE OIL PRESSURE PROBLEMS, LANDED WITHOUT INCIDENT. VISUAL INSPECTION BY MECHANIC FOUND THE LT ENGINE AIR/OIL SEPARATOR HAD DEVELOPED A CRACK IN THE SEPARATOR CAUSING A OIL LEAK, THE ENGINE WAS NOT RUN OUT OF OIL, THE SEPARATOR WAS REPLACJan 23, 2015 · N58VB · Beech 58P · Turbine Engine Oil SystemSDR FAA20140220000090Pump · inoperativeLEFT INSTRUMENT AIR PUMP FAILED.Feb 4, 2014 · N58LP · Beech 58P · Pneumatic Distribution SystemSDR FAA20140220000089Pump · inoperativeRIGHT INSTRUMENT AIR PUMP FAILED.Feb 4, 2014 · N58LP · Beech 58P · Pneumatic Distribution SystemSDR 2014FA0000061Cylinder · low pressureDURING ANNUAL INSPECTION, PERFORMED A DIFFERENTIAL COMPRESSION CHECK. FOUND NR 6 CYLINDER COMPRESSION 32 PSI/80 PSI. COMPRESSION LEAK PAST EXHAUST VALVE. REMOVED CYLINDER ASSY AND SENT TO MFG FOR REPAIRS.Jan 15, 2014 · N58LP · Beech 58P · Reciprocating Engine Cylinder SectionSDR 2014FA0000060Pump · low pressureOWNER REPORTED LT FUEL PRESSURE WAS LOW WHEN OPERATING BOOST PUMP. TESTED FUEL PRESSURE, FOUND PRESSURE LOW. PUMP REMOVED. FUEL SYS COMPONENTS WERE INSPECTED AND NO EVIDENCE OF DEBRIS OR CONTAMINATION WAS FOUND.Jan 15, 2014 · N58LP · Beech 58P · Fuel Boost PumpSDR 2014FA0000059Pump · inoperativeDURING AN ANNUAL INSPECTION, FOUND LEFT INSTRUMENT AIR PUMP INOPERATIVE. REMOVED PUMP, FOUND DRIVE COUPLING SHEARED. FOUND PUMP VANE DEBRIS IN PRESSURE SIDE AIR HOSE. SINCE O/H, ALL FILTERS WERE REPLACED WITH NEW WHEN PUMP WAS INSTALLED.Jan 15, 2014 · N58LP · Beech 58P · Independent InstrumentsSDR 2013FA0000280Mount · erodedDURING LT AND RT ENGINE CHANGE THE LT AND RT ENGINE MOUNT TRUSSES WERE INSPECTED. SEVERE HEAT EROSION WAS FOUND ON THE LT BEAM BELOW THE FWD INDUCTION AIR BOX MOUNT BRACKET. THIS AREA IS NEAR THE LT EXHAUST ELBOW. BOTH MOUNTS SHOW THE SAME AMOUNT OF EROSIONApr 10, 2013 · N58LP · Beech 58P · Engine Mount SectionSDR 2012FA0000812Cylinder · crackedDURING ROUTINE MX, FUEL STAINING WAS FOUND ON THE NR 5 CYLINDER HEAD. FURTHER INSPECTION FOUND A SMALL CRACK APPROX .6250". CYLINDER WAS REMOVED AND SENT FOR INSPECTION. OVERHAULED CYLINDER WAS INSTALLED.Dec 8, 2012 · N53MT · Beech 58P · Reciprocating Engine Cylinder SectionSDR 2012FA0000657Fuel Cell · debondedFLOATS AND FUEL CELLS, NEWLY MFG INBD L/E TANK , REPLACES OEM CELL PN 60-921057-3. NEWLY INSTALLED 1-6-12. LOW POINT DRAIN NIPPLE INTERNAL REINFORCEMENT DEBONDED, ALLOWING COMPLETE DRAINING OF LT WING FUEL LOAD. ACFT WAS ON GROUND AT TIME OF INCIDENT. RECOJul 18, 2012 · N3864U · Beech 58P · Fuel StorageSDR 2012FA0000102Cylinder · crackedLT ENGINE CYLINDER FOUND TO BE CRACKED AT FUEL INJECTOR NOZZLE HOLE. NEW CYLINDERS WERE INSTALLED AT ENGINE O/H.Feb 9, 2012 · N58TB · Beech 58P · Reciprocating Engine Cylinder SectionSDR 2011FA0000269Leg Assy · brokenACFT LANDED WITH NOSE LANDING GEAR IN THE UNLOCKED POSITION. THE PILOT REPORTED ON TAKEOFF THAT THE ACFT HAD A SEVERE VIBRATION AT APPROX 85 KNT, CONTINUED FLIGHT AND A SECOND ACFT VERIFIED THAT THE NLG WAS "FLOPPING AROUND", CONTINUED THE FLIGHT TO BURN OFF Mar 31, 2011 · N6752X · Beech 58P · Nose/Tail Landing GearSDR 2011FA0000039Mount · damagedUPON REMOVAL, AN INSPECTION OF THE MOUNT WAS PERFORMED. DAMAGE WAS FOUND ON THE INBD MAIN SUPPORT CHANNEL. APPROX 10-12 INCHES FWD OF WHERE THE MOUNT ATTACHES TO THE FIREWALL. DAMAGE WAS ON THE INSIDE UPPER PART OF CHANNEL WITH A GROVE WORN APPROX .2500" INJan 3, 2011 · N79AP · Beech 58P · Engine Mount SectionSDR 2010FA0000207Distributor Blk · looseCUSTOMER HAD INTERMITTENT ROUGH ENGINE THAT FINALLY HAD FAILED MAGNETO. DISASSEMBLED & FOUND DISTRIBUTOR GEAR AXEL WAS LOOSE IN BLOCK AND TOWER CONTACTS WERE GROUND OFF. REPLACED DISTRIBUTOR BLOCK AND LARGE GEAR. MAGNETO WAS O/H 250 PRIOR ON 11-1-2004.Feb 16, 2010 · N491WM · Beech 58P · Magneto/DistributorSDR 2009FA0000289Cylinder · crackedFOUND (2) ECI CYLINDERS CRACKED ARE CRACKED BETWEEN THE 17TH AND 18TH FIN AS LOOKING AT CYLINDER INSTALLED FROM THE BARREL TO THE HEAD. IN THE EXHAUST CHAMBER AREA. FOUND BY DOING COMPRESSION. LET ENGINE COOL OFF AND SOAP LEAK TEST. REMOVED THE REMAINING CMar 16, 2009 · N6408Q · Beech 58P · Reciprocating Engine Cylinder SectionSDR 2009FA0000290Cylinder · crackedFOUND (2) ECI CYLINDERS CRACKED. CYLINDERS ARE CRACKED BETWEEN THE 17TH AND 18TH FIN AS LOOKING AT CYLINDER INSTALLED FROM THE BARREL TO THE HEAD, IN THE EXHAUST CHAMBER AREA. FOUND BY DOING COMPRESSION. LET ENGINE COOL OFF AND SOAP LEAK TEST. REMOVED THE Mar 15, 2009 · N6408Q · Beech 58P · Reciprocating Engine Cylinder SectionSDR 2007FA0000247Clamp · failedLT ENGINE REPORTED TO BE ROUGH RUNNING. INDUCTION HOSE CLAMP(P/N-RAM 1170-2)FAILED; ALLOWING INDUCTION COUPLER(P/N-632323) TO SEPARATE FROM INDUCTION TUBE. THIS INDUCTION LEAK OCCURRED BETWEEN THE Y AND INTAKE TUBES TO CYLINDERS NR 2, NR 4 AND NR 6.Feb 27, 2007 · N25RL · Beech 58P · Engine Air Intake SystemSDR EY2R0079965Hub · corrodedCORROSION ON PROPELLER HUB.Apr 21, 2006 · Beech 58P · Propeller Hub SectionSDR 0079965AHub · corrodedPROPELLER HUB HAS INTERNAL AND EXTERNAL CORROSIONApr 4, 2006 · Beech 58P · Propeller Hub SectionSDR 2005FA0001480Clamp · looseIN CRUISE FLIGHT, 2500 RPM, 35 HG, PILOT NOTED L/ENGINE LOST POWER. PILOT FEATHERED PROPELLER AND POWERED ENGINE. MAINT NOTED INTERCOOLER DUCT, PN 102-389003-3 LOOSE AT DUCT SERV CLAMP WAS LOOSE, DUCT WAS PARTIALLY DETACHED. REPLACED DUCT, RUNUP OK. (K)Oct 18, 2005 · N6677L · Beech 58P · Pneumatic Distribution SystemSDR 2005FA0001210Motor · failedFLAP CIRCUIT BREAKER POPS WHEN RETRACTING FLAPS. FOUND FLAPS GOING OVER TRAVEL IN DOWN DIRECTION, PROBABLY OVERLOADING CAUSING OVERLOADING OF FLAP MOTOR. FOUND MOTOR COILS SHOW SIGNS OF OVERHEATING. MFG HAS SUPERSEDED MOTOR TO NEW MOTOR. (K)Aug 11, 2005 · N80LM · Beech 58P · Trailing Edge Flap Control SystemSDR BHA01RSWindow · departedWHILE IN FLIGHT, PILOTS LEFT SIDE WINDOW CRACKED AND DEPARTED AIRCRAFT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.Nov 28, 2003 · N6047S · Beech 58P · Flight Compartment WindowsSDR 2003FA0000972Crossover Tube · chafedDURING A PHASE INSPECTION, THE LEFT CROSSOVER TUBE WAS POUND CHAFED BY THE ENGINE MOUNT TRUSS (PN 102-910026-131). THE CHAFING WAS APPROXIMATELY HALFWAY THROUGH THE WALL THICKNESS. WE HAVE A SPECIAL INSPECTION TO CHECK THE HEATSHIELD FOR CHATING IN THIS SAMEAug 22, 2003 · N153Z · Beech 58P · Engine Collector/Tailpipe/NozzleSDR CA030903007Valve · leaking(CAN) PN 6524323A1M (FLOW DIVIDED) LEAKING FUEL AFTER ENGINE SHUT DOWN/NEW PART INSTALLED.Aug 12, 2003 · Beech 58P · Engine Fuel DistributionSDR PG0306889Skin · crackedCRACK FOUND ON TOP SIDE OF LEFT HAND ELEVATOR, JUST FORWARD OF OUTBOARD END OF TRIM TAB. CRACK EXTENDS FORWARD INBOARD FOR APPROXIMATELY THREE INCHES.May 19, 2003 · N981SS · Beech 58P · Elevator, Plate/SkinSDR 2003FA0000086Bearing · looseDURING CRUISE POWER SETTING IN FLIGHT. RT ENGINE RPM FLUX 100-200 RPM AND MANIFOLD PRESSURE FLUX 1 INCH TO 2 INCH. DURING GROUND RUN TO TROUBLESHOOT SYSTEM ENGINE RPM WOULD SUDDENLY DROP 200-400 RPM. AT CRUISE SETTING. PERFORMED MAGNETO CHECK. LT MAG FAILJan 15, 2003 · N135Z · Beech 58P · Magneto/DistributorSDR 2002FA0001348Magneto · lack of lubeELECTROSYSTEMS DISTRIBUTOR BLOCK FAILED ON TAKEOFF ROLL APPROXIMATELY 10 HOURS AFTER INSTALLATION. IT APPEARS THAT THE OIL LIGHT BEARING THAT THE ROTOR SHAFT RIDES IN WAS NOT PROPERLY OIL BEFORE INSTALLATION. THE PART WAS INSTALLED IN THE LEFT MAGNETO ON THE LNov 26, 2002 · N112RS · Beech 58P · Magneto/DistributorSDR DP02002F00000Control Unit · failedNEW ENGINE INSTALLED FROM FACTORY. ENGINE DRIVER PUMP PRESSURES ADJUSTED IAW MFG MM. ENGINE FUEL FLOWS WOULD NOT REACH SPECIFIED VALUE OF 32.4 TO 34.1 GPH. IAW SD. ENGINE CHT AND TLT HOT. MFG RECOMMEDED INCREASING UNMETERED PRESSURE 5 PSI BEYOND THEIR PUBLSep 4, 2002 · N146Z · Beech 58P · Power LeverSDR 2002FA0001078Throttle Control · bindingPILOT REPORTED BINDING OF LEFT ENGINE THROTTLE. INVESTIGATION REVEALED GALLING OF MIXTURE ADJUSTMENT ROD WHERE IT ATTACHES TO THE THROTTLE LEVER, WITH A SIGNIFICANT AMOUNT OF TRANSFER OF METAL FROM THE LEVER TO THE ROD, PREVENTING FULL THROTTLE MOVEMENT. THISep 4, 2002 · N146Z · Beech 58P · Power LeverSDR UAO2002F00000Truss · brokenDURING A PHASE INSPECTION IT WAS NOTED THAT THE EXHAUST HEATSHIELD FORWARD OF THE TURBO COMPRESSOR HAD CHAFED AN AREA .1875 INCH X .3125 INCH THROUGH THE ENGINE MOUNT TRUSS. THIS WAS CAUSED BY THE HEATSHIELD MOUNT BREAKING ALLOWING THE HEATSHIELD TO DROP ONTOAug 27, 2002 · N145Z · Beech 58P · Engine Mount SectionSDR 2002FA0001059Panel · shortedPANEL ON SWITCH PANEL LIGHTING SHORTED WHICH MADE THE INVERTER EMITTED SMOKE INTO THE COCKPIT. BOTH PARTS WERE REPLACED WITH NEW PARTS FROM MFG.Aug 27, 2002 · N68BB · Beech 58P · Instrument PanelSDR 2002FA0000456Adapter · failedPILOT REPORTED ENGINE WOULD NOT START. FOUND THAT PROP WOULD NOT TURN BACKWARDS. REPLACED STARTER ADAPTER WITH A REBUILT AND OPS CHECKED OK. THIS IS THE SECOND ADAPTER REPLACED ON THIS ENGINE. THE FIRST ONE FAILED ON A FACTORY REBUILT/ZERO TIME ENGINE WITH 40Apr 8, 2002 · Beech 58P · Engine StarterSDR FEG2002F00000Line · chafedENGINE OIL FOUND LEAKING FROM WING ROOT/FUSELAGE JUNCTION AT LEADING EDGE. LEADING EDGE REMOVED. FOUND ALUMINUM OIL PRESSURE GAUGE LINE CHAFFED THROUGH FROM CONTACT WITH INBOARD RIB OF 102-100026-602 LEADING EDGE FAIRING ASSEMBLY. RECOMMEND INSPECTING OIL PFeb 20, 2002 · N153Z · Beech 58P · Engine Oil Indicating SystemSDR 2001FA0000520Skin · crackedLOWER INBOARD LEADING EDGE SKIN CRACKED BETWEEN FUEL TANK DRAIN FITTING HOLE AND REAR EDGE OF SKIN. CRACK IS THROUGH AND AREA APPROXIMATELY 2 INCHES WIDE THAT HAS NO RIVET CONNECTING SKIN TO FRONT SPAR STRUCTURE. NORMAL FLEXING OF WING APPEARS TO BE STRESSINOct 31, 2001 · N145Z · Beech 58P · Wing, Plate/SkinSDR 2001FA0000519Skin · crackedFOUND ONE INCH LONG CRACK IN AFT UPPER FUSELAGE SKIN AT BASE OF VERTICAL FIN. CRACK STARTS AT LEFT FORWARD STABILIZER SPAR EXTENSION CUTOUT AND EXTENDS UPWARD. SUSPECT LACK OF PROPER RADIUS IN CORNER OF CUTOUT CREATED A STRESS RISER WHICH CAUSED THE SKIN TO Oct 31, 2001 · N145Z · Beech 58P · Fuselage Main, Plate/SkinSDR 2001FA0000518Rivet · brokenRIVET HEAD MISSING ON EXTENSION FITTING OF VERTICAL STABILIZER FORWARD SPAR JUST ABOVE AREA WHERE SPAR IS BOLTED TO FUSELAGE BULKHEAD. THERE IS NO EVIDENCE OF CORROSION OR CRACKING OF STRUCTURE IMMEDIATELY SURROUNDING RIVET LOCATION. RIVET APPEARS TO HAVE FAOct 31, 2001 · N145Z · Beech 58P · Vertical StabilizerSDR 2001FA0000398Throttle Cable · chafedPILOT COMPLAINED, RIGHT THROTTLE VERY STIFF, THROTTLE HAD BEEN REPLACED FOUR MONTHS EARLIER FOR SAME REASON. UPON REMOVAL IT WAS DISCOVERED THAT THE CABLE, WHICH WAS COVERED WITH FIRE SLEEVE, HAD BEEN CHAFFING ON THE LOWER PART OF THE TURBOCHARGER COMPRESSOR Sep 28, 2001 · N145Z · Beech 58P · Power LeverSDR 2001FA0000333Tire · failedNOSE TIRE FAILED AND NOSE GEAR COLLAPSED.Sep 2, 2001 · N582TA · Beech 58P · TireSDR FD62001F00000Strobe · burned outPRIOR TO ROLLOUT, PILOT ACTIVATED THE PULSELIGHT SWITCH. AS HE WAS ON ROLLOUT, THERE WAS SMOKE IN THE CABIN. PILOT ABORTED TAKEOFF AND THE AIRCRAFT WAS TAKEN TO MAINTENANCE. THE TECH FOUND THE INSTALLATION NOT TO BE IAW THE STC INSTALLATION INSTRUCTIONS. (TAug 22, 2001 · N162Z · Beech 58P · Exterior LightingSDR 20010425CW010Filter · chippedPILOT REPORTED LOW OIL PRESSURE AND HIGH TEMPERATURES. INVESTIGATION REVEALED METAL PIECES HOLDING OPEN THE OIL TEMPERATURE CONTROL VALVE. THE METAL PIECES WERE TRACED TO THE OIL FILTER. UPON REMOVING THE TOP FROM THE OIL FILTER WE OBSERVED PIECES MISSING FMar 22, 2001 · N1563L · Beech 58P · Reciprocating Engine Oil SystemSDR 20010328CW006Window · failedAIRCRAFT HAD BEEN CRUISING AT FL240 FOR 1 HOUR PLUS TEMP-40 DEGREE. ON DESCENT OUT OF FL200 THE LEFT MID CABIN WINDOW BLEW OUT OF AIRCRAFT, CABIN DEPRESSURIZATION. PILOT CONTINUED DESCENT TO LOWER ALTITUDE AND LANDED WITHOUT FURTHER INCIDENT. WINDOWS WEW INFeb 22, 2001 · N40PG · Beech 58P · Passenger Compartment WindowsSDR 20010223CW005Probe · brokenCUSTOMER REPORTED NR1 EGT ON HIS GEM 1200, INOPERATIVE. UPON REMOVAL OF EGT PROBE, ABOUT HALF OF THE PROBE TIP WAS BROKEN OFF AND MISSING. THE ONLY PATH OF EXIT IS THROUGH THE TURBO CHARGER. FURTHER INSPECTION OF THE TURBO CHARGER REVEALED FOD DAMAGE TO THEJan 23, 2001 · N4269S · Beech 58P · Engine EGT/TIT Indicating SystemSDR 20000920SH007Hinge · misinstalledOUTER HINGE ATTACHMENT SCREWS ON THE LOWER SIDE WERE HOT. INSTALLED THROUGH THE HINGE ASSEMBLY, BUT THROUGH THE SKIN ONLY. SCREWS WERE HELD IN BY THE SKIN AND BACKSIDE OF COCKED HINGE. PROBLEM WAS DISCOVERED FROM RESPONSE TO BEECH MAINTENANCE ALERT MA00-03,Sep 8, 2000 · N249CR · Beech 58P · AileronsSDR 20000811SH011Coupling · separatedUPON INVESTIGATION OF AN ALTERNATOR FAILURE, DISCOVERED THE ELASTOMER COUPLING HAD COME APART SENDING A LARGE AMOUNT OF RED RUBBER PARTICLES INTO THE ENGINE CRANKCASE AND OIL SYSTEM. THE OIL FILTER WAS INSPECTED AND FOUND TO BE CONTAMINATED WITH THIS DEBRIS. Jul 24, 2000 · N120Z · Beech 58P · Alternator-Generator DriveSDR 20000811SH010Rod End · wornDURING LANDING GEAR INSPECTION, PORTION OF PHASE INSPECTION, AN AMOUNT OF BRASS SHAVINGS WERE OBSERVED UNDER THE RT MAIN GEAR BRAKE ASSY ROD END WHERE IT ATTACHES TO THE ACTUATOR ASSY. THE ROD END WAS DISCOVERED TO BE SEVERELY WORN. BOTH (ACTUATOR END) ROD EJul 24, 2000 · N133Z · Beech 58P · Landing Gear ActuatorSDR 20000828SH023Line · misalignedPILOT WAS UNABLE TO OBTAIN FULL RICH FUEL MIXTURE ON LEFT ENGINE. UPON INSPECTION BY MAINTENANCE, THE MIXTURE CONTROLLER LINKAGE WAS FOUND OBSTRUCTED FROM REACHING FULL TRAVEL BY THE DRY AIR PUMP PRESSURE AIR LINE. THE PRESSURE AIR LINE WAS CORRECTLY ROUTED Jul 22, 2000 · N163Z · Beech 58P · Vacuum Distribution SystemSDR 20000828SH022Nut · missingWHILE PERFORMING A VISUAL INSPECTION OF LEFT ENGINE, DISCOVERED THE FREON COMPRESSOR BRACKET ASSY MISSING THE NUT THAT RETAINS THE IDLER SHEAVE ARM RETAINING BOLT. THE SHEAVE ASSY WAS BEING HELD TO THE COMPRESSOR BRACKET BY BELT TENSION ONLY AND EVENTUALLY WOJul 22, 2000 · N163Z · Beech 58P · Air Conditioning SystemSDR 20000628SH002Hinge · failedREAR HINGE CASTING FAILED HALFWAY ALONG ARM OF RADIUS, PN 35/815016/7 WHILE APPROACH TO LAND: POSSIBLE CAUSE IS WEAR IN THE FRONT HINGE PIVOT BRACKET BOLT HOLES WHICH COULD CAUSE VIBRATION. INSPECT BOTH FRONT AND REAR BOLT HOLES FOR WEAR ALIGNMENT BY DISCONNJun 16, 2000 · N79AP · Beech 58P · Landing Gear DoorsSDR 20001031SH018Injector · leakingWHILE IN-FLIGHT, A FUEL SMELL ENTERED THE CABIN. FUEL WAS LEAKING AT ALL 6 INJECTORS BETWEEN PIPE THREADS AND CYLINDER. ALL INJECTORS WERE SEALED PER CONTINENTAL SM. NEXT FLIGHT STILL LEAKING. INJECTORS RESEALED WITH LOCTITE 569 PER CONTINENTAL. (X)May 19, 2000 · N144Z · Beech 58P · Fuel Injector Nozzle
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