Beech 58

Service difficulty reports · 1,000

Newest first. General aviation reporting is voluntary.

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 = '58'
  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 BSYA200500024Door · openON DEPARTURE, COCKPIT DOOR CAME OPEN. AIRCRAFT THEN RETURNED TO DEPARTURE. MAINTENANCE LUBED AND ADJUSTED UPPER HOOK ASSY, OPS CHECKS GOOD.Nov 25, 2005 · N3695V · Beech 58 · Passenger/Crew DoorsSDR 2005FA0001574Pneumatic System · contaminatedDURING PROLONGED PERIODS OF OPERATION IN HEAVY PRECIPITATION CONSIDERABLE AMOUNTS OF WATER INTO THE PNEUMATIC SYSTEM. INSP OF PNEUMATIC SYS REVEALED LARGE AMOUNTS OF WATER BEING PASSED THROUGH DEICE BOOT EJECTOR, FURTHER DISASSEMBLY INSP REVEALED SEVERAL OUNCNov 23, 2005 · N3214H · Beech 58 · Pneumatic Distribution SystemSDR 2005F00110Pneumatic System · contaminatedDURING PROLINGED PERIODS OF OPERATION IN HEAVY PRECIPITATION CONSIDERABLE AMOUNTS OF WATER ENTER INTO THE PNEUMATIC SYSTEM. INSP OF PNEUMATIC SYS REVEALED LARGE AMOUNTS OF WATER BEING PASSED THROUGH DEICE BOOT EJECTOR, FURTHER DISASSEMBLY INSP REVEALED SEVERANov 23, 2005 · N401BC · Beech 58 · Pneumatic Distribution SystemSDR 2005FA0001573Pneumatic System · contaminatedDURING PROLONGED PERIODS OF OPERATION IN HEAVY PRECIPITATION CONSIDERABLE AMOUNTS OF WATER ENTER INTO THE PNEUMATIC SYSTEM. INSP OF PNEUMATIC SYS REVEALED LARGE AMOUNTS OF WATER BEING PASSED THROUGH DEICE BOOT EJECTOR, FURTHER DISASSEMBLY INSP REVEALED SEVERANov 23, 2005 · N1065B · Beech 58 · Pneumatic Distribution SystemSDR 2005FA0001572Pneumatic System · contaminatedDURING PROLONGED PERIODS OF OPERATION IN HEAVY PRECIPITATION CONSIDERABLE AMOUNTS OF WATER ENTER INTO THE PNEUMATIC SYSTEM. INSP OF PNEUMATIC SYS REVEALED LG AMOUNTS OF WATER BEING PASSED THROUGH DEICE BOOT EJECTOR, FURTHER DISASSEMBLY INSP REVEALED SEVERAL ONov 23, 2005 · N3267N · Beech 58 · Pneumatic Distribution SystemSDR BSYA200500022Door · openON CLIMBOUT OF LCK, COCKPIT DOOR CAME OPEN. RETURNED TO LCK, LANDED, CLOSED DOOR CORRECTLY AND CONTINUED ON WITH FLIGHT.Nov 22, 2005 · N3695V · Beech 58 · Passenger/Crew DoorsSDR BSYA2005019Transponder · brokenAIRCRAFT TOOK OFF, COULD NOT TRANSMITT FROM EITHER COMM. RADIO. FOUND PILOTS PUSH TO TALK SWITCH BROKEN, CO-PILOTS PUSH TO TALK DID WORK AND THERE WAS A HAND MIC IN GLOVE BOX. AIRCRAFT ALSO HAD A MODE (C) PROBLEM. AIRCRAFT RETURMED TO DEPARTURE, NR 1 TRANSPONov 15, 2005 · N1859K · Beech 58 · Communications SystemSDR Z4TA20050005Engine · seizedPILOT WAS IN CRUISE FLIGHT. HEARD POP AND NOTICED RT ENGINE WAS WINDMILLING. FEATHERED PROPELLER. ATTEMPTED RESTART BUT WAS UNSUCCESSFUL. LANDED AT ALTERNATE FIELD. ON GROUND, DISCOVERED RT ENGINE PROPELLER WOULD NOT TURN - SEIZED.Nov 10, 2005 · N95KM · Beech 58 · Engine (Reciprocating)SDR BSYA200500029Squat Switch · inoperativeON TAKEOFF, PILOT SELECTED GEAR UP NOTHING HAPPENED, THEN ELECTED TO RETURN. MAINTENANCE JACKED AIRCRAFT CLEANED AND LUBED SQUAT SWITCH. OPS CHECKED GOOD.Nov 8, 2005 · N78RE · Beech 58 · Landing Gear Position and WarningSDR BSYR200500028Actuator · frozenON TAKEOFF, ELEVATOR TRIM FROZE UP, RETURNED. MAINTENANCE CHANGED LT TRIM TAB ACTUATOR OPS CHECKED GOOD.Nov 6, 2005 · N4098S · Beech 58 · Elevator Tab Control SystemSDR BSYA200500016Door · unsecureCOCKPIT DOOR POPPED OPEN AFTER TAKEOFF, RETURNED AND LANDED PROPERLY, SECURED DOOR AND CONTINUED WITH FLIGHT.Oct 26, 2005 · N297AT · Beech 58 · Fixed Inner DoorsSDR 2005FA0001466Linkage · jammedDURING POWER APPLICATION FOR TOUCH AND GO, UNABLE TO ADVANCE THROTTLE ON RT ENGINE. FOUND THE LOWER NUT WHICH SECURES THE PHENOLIC BLOCK FOR THE ANTI-RETRACT CAM TO THE THROTTLE LINKAGE ROD HAD COME OFF, ALLOWING THE BLOCK TO SEPARATE FROM THE LINKAGE ROD. DUOct 21, 2005 · N879JN · Beech 58 · Power LeverSDR FFKA2005106Hub · shearedALTERNATOR HUB ASSEMBLY SHEARED (DESIGNED TO DO THIS) AND/OR BECAME OBLONG AND THEN SHEARED THE SHAFT OF THE ALTERNATOR ALLOWING IT TO COME IN CONTACT WITH THE CRANKSHAFT AND CONTAMINATING THE OIL WITH METAL.Oct 19, 2005 · N11HW · Beech 58 · DC Generating SystemSDR 1005FAA001Strobe · damagedWING TIP STROBE UNIT FLASH TUBE. SOLDER JOINT BETWEEN PIN COMING OUT OF FLASH TUBE AND END CAP IS FAILING DUE TO SOLDER BEAD BEING GROUND FLAT AFTER ATTACHMENT DURING MANUFACTURE. MULTIPLE FAILURES - CONDITION EXISTS ON NEW UNITS.Oct 18, 2005 · N3694K · Beech 58 · Exterior LightingSDR 2005FA0001435Bellcrank · fracturedTHE CO-PILOTS RUDDER/STEERING BELLCRANK FRACTURED AT THE CENTER CONNECTING POINT CAUSING A LACK OF NOSE WHEEL STEERING ON THE CO-PILOTS SIDE.Oct 14, 2005 · N555ND · Beech 58 · Landing Gear Steering SystemSDR XGN2006F00044Cylinder · crackedFOUND CYLINDER HEAD CRACKED IN THE EXHAUST SIDE DURING A 50 HR INSPECTION. THIS IS AN ON GOING PROBLEM WITH THE CYLINDERS. (K)Oct 11, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2005F00014Cylinder · crackedFOUND CYLINDER HEAD CRACKED IN THE EXHAUST SIDE DURING A 50 HOUR INSPECTION. THIS IS AN ON GOING PROBLEM WITH THE ECI CYLINDER. (K)Oct 11, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR BSYA200500014Tach Generator · inoperativeRIGHT ENGINE TACHOMETER QUIT AFTER TAKEOFF OUT OF MKE. AIRCRAFT RETURNED TO MKE. REMOVED AND REPLACED TACH GENERATOR, OPS CHECKS GOOD.Oct 7, 2005 · N9044V · Beech 58 · Indicating/Recording SystemSDR BSYA200500013Latch · lack of lubeCOCKPIT DOOR CAME OPEN AFTER TAKEOFF. RETURNED TO TEB. MAINTENANCE LUBED DOOR LATCHES AND CABLE OPS CHECKS GOOD.Oct 6, 2005 · N297AT · Beech 58 · Fixed Inner DoorsSDR XGN2006F00048Cylinder · crackedFOUND CRACKED CYLINDER HEAD AT 50 HR INSPECTION. DUE TO THE FREQUENCY OF THE NUMBER OF CYLINDERS WE ARE FINDING CRACKED, WE DO A COMPRESSION CHECK EACH 50 HRS. (K)Oct 5, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2005FA0001468Fuel Cell · failedWHILE ENROUTE, PILOT EXPERIENCED TOTAL LOSS OF REMAINING FUEL IN RT WING. DURING FLIGHT WITHOUT WARNING. SUBSEQUENTLY RT ENGINE EXPERIENCED UNCOMMANDED SHUTDOWN DUE TO FUEL STARVATION. LARGE QUANTITY OF FUEL LOST IN SHORT TIME. PILOT LANDED, TROUBLESHOT ACOct 2, 2005 · N92DD · Beech 58 · Fuel StorageSDR Z4TA20050004Housing · crackedPILOT REPORTED ABNORMAL OIL LOSS FOR RIGHT ENGINE. ALSO, OIL TRAIL ON LOWER RT WING. UPON INSPECTION, FOUND NR 6 CYLINDER FORWARD PUSH ROD HOUSING CRACKED, ALLOWING OIL TO DRAIN INTO LOWER COWL. REPLACED HOUSING.Sep 19, 2005 · N95KM · Beech 58 · Reciprocating Engine Cylinder SectionSDR Z4TA20050003Housing · crackedPILOT REPORTED ABNORMAL OIL LOSS FOR RIGHT ENGINE. ALSO, OIL TRAIL ON LOWER RT WING. UPON INSPECTION, FOUND NR 6 CYLINDER FORWARD PUSH ROD HOUSING CRACKED, ALLOWING OIL TO DRAIN INTO LOWER COWL. REPLACED HOUSING.Sep 19, 2005 · N95KM · Beech 58 · Reciprocating Engine Cylinder SectionSDR Z4TA20050002Housing · crackedPILOT REPORTED ABNORMAL OIL LOSS FOR RIGHT ENGINE. ALSO, OIL TRAIL ON LOWER RT WING. UPON INSPECTION, FOUND NR 6 CYLINDER FORWARD PUSH ROD HOUSING CRACKED, ALLOWING OIL TO DRAIN INTO LOWER COWL. REPLACED PART.Sep 19, 2005 · N95KM · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2006F00045Cylinder · crackedCYLINDER HEAD CRACKS FOUND AT 50 HR INSPECTION. DUE TO THE FREQUENCY OF THE NR OF CYLINDERS WE ARE FINDING CRACKED, WE DO A COMPRESSION CHECK EACH 50 HOURS. (K)Sep 6, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR BSYA200500012Engine · failedAIRCRAFT WAS ENROUTE FROM BDL TO PHL WHEN HE SEEN SPARKS AND LOST ALL OIL PRESSURE, THEN DIVERTED TO TEB DECLARED AN EMERGENCY, LANDED NO PROBLEMS. FOUND NR 2 ROD THRU ENGINE CASE. CAUSE UNKNOWN AT THIS TIME, R&R ENGINEJul 21, 2005 · N9044V · Beech 58 · Engine (Reciprocating)SDR AU510001440Relay · failed(AUS) LANDING GEAR RETRACTION SYSTEM DYNAMIC RELAY FAULTY.(OTHER CAUSE: HIGH HOURS ) (CASA# 510001440)Jul 6, 2005 · Beech 58 · Landing Gear Retraction/Extension SystemSDR 2005FA0000933Washer · improper partWHILE PERFORMING SB WHICH INCLUDES PROPELLER, REMOVING THE MOUNTING PLATE FROM THE SLIP RING, FOUND THAT THE WASHERS USED TO HOLD THESE ITEMS TOGETHER ARE TOO WIDE AND SCORED, THE PROP HUB. WERE ABLE TO POLISH OUT THE SCOPE MARKS ON THE HUB AND MODIFY THE WASJun 16, 2005 · N21YM · Beech 58 · Propeller SystemSDR CA050630003Shaft · worn(CAN) NLG DOOR RETRACT SHAFT ASSEMBLY PREMATURE WEAR (160 CYCLES) NEW AIRCRAFT (2005). INSTALLED PRODUCT IMPROVEMENT KIT NR 36-8005-3 SUGGEST KIT BE INCORPORATED AT PRODUCTION (KIT REPLACES PIN THAT TRACKS INCAM WITH A ROLLER).Jun 13, 2005 · Beech 58 · Landing Gear Retraction/Extension SystemSDR S002368Starter · seizedTHIS STARTER SIEZED DURING START CAUSING SIEZURE AND SEVERE DAMAGE TO THE ENGINE ACCESSORY GEARBOX STATER ADAPTER.Jun 8, 2005 · N3101B · Beech 58 · Starter-GeneratorSDR AU510001611Cam · missingLANDING GEAR WARNING HORN FAILED TO OPERATE WHEN THROTTLES CLOSED. INVESTIGATION FOUND NO SWITCHES, BRACKETS OR ROLLERS IN WARNING SYSTEM. LT ENGINE FCU WARNING SYSTEM ACTIVATING CAM MISSING. NO WIRING FITTED FORWARD OF THE FIREWALL. PERSONNEL/MAINTENANCE Jun 6, 2005 · Beech 58 · Landing Gear Position and WarningSDR AU510001610Landing Gear · out of adjustNOSE LANDING GEAR RETRACTION SYSTEM MISRIGGED. NLG FAILED TO FULLY RETRACT INTO THE WHEEL WELL, LEAVING THE DOORS WIDE OPEN AND THE NOSEWHEEL HANGING OUT BY APPROXIMATELY 127MM TO 152.4MM (5IN TO 6IN). NLG WAS CORRECTLY RIGGED IN THE DOWN POSITION.Jun 6, 2005 · Beech 58 · Nose/Tail Landing GearSDR FFKR103Relay · burned outPILOT REPORTED THAT THE LANDING GEAR STOPPED RETRACTING DURING NORMAL OPERATION. MAINTENANCE INSPECTED LANDING GEAR SYSTEM AND FOUND THE L/G RELAY TO BE INOP CAUSING THE LANDING GEAR MOTOR TO CONTINUE TO OPERATE CAUSING IT TO FAIL AS WELL. REPLACED BOTH PARTJun 3, 2005 · N11HW · Beech 58 · Landing Gear Retraction/Extension SystemSDR SFO2005F00002Bolt · looseWHILE PERFORMING A SCHEDULED INSPECTION, 3 OF THE 4 ENGINE MOUNT (CUSHION) BOLTS WERE FOUND LOOSE. 2 REQUIRED 1 FULL TURN TO TIGHTEN, AND THE 3RD TOOK ALMOST 2 TURNS TO TIGHTEN. THE SELF LOCKING FEATURE OF THE NUTS WAS CHECKED AND APPEARED TO BE OK. IT CAN May 25, 2005 · N917SF · Beech 58 · Engine Mount SectionSDR 2005FA0000844Bulkhead · crackedBULKHEAD CRACKED AT TOP PORTION AT JOGGLED AREA BELOW AFT HORIZONTAL ATTACH BRACKET/SPAR CRACK TO BE ABOUT .2500 INCH ON RT, ABOUT 1 INCH ON LT, CAUSE PROBABLY DUE TO HIGH AIRFRAME TT AND FATIGUE. (SW01200504562) (K)May 17, 2005 · N8245H · Beech 58 · Fuselage Main, BulkheadSDR XGN2005F00005Cylinder · crackedCYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HOUR INSPECTION. WE ARE USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. WE ARE DOING COMPRESSION CHECKS EACH 50 HOURS. 3 CRACKED CYLINDERS WMay 4, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2005F00004Cylinder · crackedCYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HOUR INSPECTION. WE ARE USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. WE ARE DOING COMPRESSION CHECKS EACH 50 HOURS. 3 CRACKED CYLINDERS WMay 4, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2005F00003Cylinder · crackedCYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HOUR INSPECTION. ARE USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. WE ARE DOING COMPRESSION CHECKS EACH 50 HOURS. 3 CRACKED CYLINDERS WEREMay 4, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR 2005FA0000735Gasket · out of positionTHE MATERIAL THE UPPER AND LOWER GASKETS ARE NOW MADE OF IS MUCH SOFTER THAN THE ORIGINAL DESIGN. THEY TEND TO COMPRESS AND SLIDE OUT FROM UNDER THE STRAINER WALL INTO THE CENTER OF THE FUEL STRAINER BODY AND BEGAN TO LEAK FUEL. THE STRAINER HOUSING IS NOT MMay 4, 2005 · N4488Q · Beech 58 · Aircraft Fuel Filter/StrainerSDR 2005FA0000788Distributor Gear · burnedDURING DISASSEMBLY OF MAGNETO FOR 500 HR INTERNAL INSPECTION, FOUND DISTRIBUTOR FINGER ON DISTRIBUTOR GEAR SEVERELY BURNED WITH MATERIAL MISSING. FOUND MAGNETO INTERNAL TIMING 2 TEETH OFF FROM SPECIFIED. SUSPECT INCORRECT INTERNAL TIMING CAUSED A LARGE GAP BMay 2, 2005 · N2224D · Beech 58 · Magneto/DistributorSDR 2005FA0000643Spar · crackedWHERE HORIZONTAL STAB SPAR ATTACHES. THE BULKHEAD IS CUT AWAY, TO ALLOW THIS, AND IS FORMED BY JOGGLE BEND. SIDE TO SIDE. AT THIS JOGGLE, IT IS CRACKED, FORE AND AFT, TO INCLUDE BOTH BULKHEAD AND FORMER. (SW01200504216) (K)Apr 27, 2005 · N8117V · Beech 58 · Fuselage Main, StructureSDR XGN2006F00047Cylinder · crackedCYLINDER HEAD CRACKED, FOUND DURING 100 HR INSPECTION. THIS IS AN ON GOING PROBLEM THAT WE ARE FINDING IN OUT FLEET OF AIRCRAFT. (K)Apr 26, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2006F00046Cylinder · crackedCYLINDERS WERE FOUND DURING COMPRESSION CHECK AT THE 100 HR INSPECTION. USING A SOAP SOLUTION TO DETECT CRACKS IN THE EXHAUST SIDE OF THE CYLINDER WHILE DOING A COMPRESSION CHECK. DOING COMPRESSION CHECKS EACH 50 HRS. 3 CRACKED CYLINDERS WERE FOUND ON THE Apr 26, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR XGN2005F00002Cylinder Head · crackedCYLINDER HEAD CRACKED. FOUND DURING 100 HR INSPECTION. THIS IS AN ONGOING PROBLEM THAT WE ARE FINDING IN OUR FLEET OF AIRCRAFT. (K)Apr 26, 2005 · N577W · Beech 58 · Reciprocating Engine Cylinder SectionSDR BSYA200500009Light · looseON APPROACH INTO CMH PILOT SAID HE HAD NO GEAR DOWN AND LOCK LIGHT. DID A FLY-BY PAST CONTROL TOWER AND MAINTENANCE PERSONAL ON GROUND CONFIRMED GEAR DOORS WHERE CLOSED AND GEAR LOOK DOWN AND LOCKED. LANDED AIRCRAFT NO PROBLEMS. MAINTENANCE JACKED AIRCRAFT,Apr 21, 2005 · N400RP · Beech 58 · Landing Gear Position and WarningSDR SFO2005F00000Spar · crackedDURING ANNUAL INSP, CRACKS WERE NOTED IN FWD CARRY-THRU SPAR WEB. LOCATED AT LT UPPER OB MOST HUCK BOLTS (2 EA) ON FWD SIDE OF CARRY-THRU ASSY. HEAD SIDE OF UPPER HUCK BOLT IS INACCESSIBLE FOR VIEWING WITHOUT WING REMOVAL. LWR HUCK BOLT IS ACCESSIBLE, NO MOApr 14, 2005 · N37SF · Beech 58 · Wing SparSDR BSYA200500007Motor · malfunctionedON APPROACH INTO BNA, PILOT SELECTED GEAR DOWN AND NOTHING HAPPENED. PILOT PULLED GEAR CIRCUIT BREAKER AND HAND CRANKED GEAR DOWN, LANDED NO PROBLEM. MAINTENANCE JACKED A/C RESET CIRCUIT BREAKER GEAR OPERATED NORMALLY. CHANGED GEAR MOTOR AND DYNAMIC BREAK REApr 14, 2005 · N33DK · Beech 58 · Landing Gear Retraction/Extension SystemSDR 2005FA0000607Rib · crackedDURING SCHEDULED ANNUAL INSPECTION, FOUND LT WING BATT RIB AFT ANGLE AT IB MLG DOOR AFT ATTACH POINT CRACKED. HAVE NOTED SIMILAR CRACKING IN OTHER LOW-TIME RAC MODEL 58 AIRCRAFT. CRACKING SEEMS TO BE RELATED TO INSTALLATION OF MACHINED ALUMINUM DOORS THAT REApr 1, 2005 · N128WS · Beech 58 · Wing, Rib/BulkheadSDR 2005FA0000869Impulse Coupling · looseDURING ANNUAL INSPECTION, COMPLY WITH 500 HR MAGNETO INTERNAL INSPECTION, WHICH INCLUDES THE IMPULSE COUPLING IAW MFG SB. ONE IMPULSE COUPLING WAS FOUND TO BE VERY LOOSE, DUE TO LOOSE RIVETS, WOULD HAVE FAILED SOON. FAILURE OF THIS TYPE CAN CAUSE EXTENSIVE DMar 22, 2005 · N815P · Beech 58 · Magneto/DistributorSDR Z4TA20050001Element · shortedDURING GROUND RUN, DISCOVERED RIGHT ENGINE OIL TEMP WOULD NOT REACH GREEN RANGE. REPLACED OIL TEMP SENDER AND SYSTEM OPS CK OK. OIL TEMP SENDER BULB ALLOWED OIL TO LEAK INTO ELECTRICAL CONNECTION CAVITY, THUS SHORTING THE CONNECTION.Mar 3, 2005 · N95KM · Beech 58 · Engine Oil Temperature
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