# Service difficulty reports: Beech 58P

A list on [Beech 58P](https://openairdocs.org/model/beech-58p.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 123 reports

- [SDR 2017FA0000368](https://openairdocs.org/sdr/2017FA0000368.md): Clutch · broken · Apr 6, 2017 · N58TR · Beech 58P · Main Rotor Gearbox
  > FOUND FWU SEIZED. DISASSEMBLY FOUND CLUTCH CAGE BROKE BETWEEN SPRAGS IN TWO PLACES.
- [SDR 2016FA0000218](https://openairdocs.org/sdr/2016FA0000218.md): Downlock Arm · broken · Apr 10, 2016 · N58JC · Beech 58P · Nose/Tail Landing Gear
  > STARBOARD 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.
- [SDR 2015FA0000024](https://openairdocs.org/sdr/2015FA0000024.md): Separator · cracked · Jan 23, 2015 · N58VB · Beech 58P · Turbine Engine Oil System
  > PILOT 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 REPLAC
- [SDR FAA20140220000090](https://openairdocs.org/sdr/FAA20140220000090.md): Pump · inoperative · Feb 4, 2014 · N58LP · Beech 58P · Pneumatic Distribution System
  > LEFT INSTRUMENT AIR PUMP FAILED.
- [SDR FAA20140220000089](https://openairdocs.org/sdr/FAA20140220000089.md): Pump · inoperative · Feb 4, 2014 · N58LP · Beech 58P · Pneumatic Distribution System
  > RIGHT INSTRUMENT AIR PUMP FAILED.
- [SDR 2014FA0000061](https://openairdocs.org/sdr/2014FA0000061.md): Cylinder · low pressure · Jan 15, 2014 · N58LP · Beech 58P · Reciprocating Engine Cylinder Section
  > DURING 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.
- [SDR 2014FA0000060](https://openairdocs.org/sdr/2014FA0000060.md): Pump · low pressure · Jan 15, 2014 · N58LP · Beech 58P · Fuel Boost Pump
  > OWNER 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.
- [SDR 2014FA0000059](https://openairdocs.org/sdr/2014FA0000059.md): Pump · inoperative · Jan 15, 2014 · N58LP · Beech 58P · Independent Instruments
  > DURING 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.
- [SDR 2013FA0000280](https://openairdocs.org/sdr/2013FA0000280.md): Mount · eroded · Apr 10, 2013 · N58LP · Beech 58P · Engine Mount Section
  > DURING 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 EROSION
- [SDR 2012FA0000812](https://openairdocs.org/sdr/2012FA0000812.md): Cylinder · cracked · Dec 8, 2012 · N53MT · Beech 58P · Reciprocating Engine Cylinder Section
  > DURING 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.
- [SDR 2012FA0000657](https://openairdocs.org/sdr/2012FA0000657.md): Fuel Cell · debonded · Jul 18, 2012 · N3864U · Beech 58P · Fuel Storage
  > FLOATS 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. RECO
- [SDR 2012FA0000102](https://openairdocs.org/sdr/2012FA0000102.md): Cylinder · cracked · Feb 9, 2012 · N58TB · Beech 58P · Reciprocating Engine Cylinder Section
  > LT ENGINE CYLINDER FOUND TO BE CRACKED AT FUEL INJECTOR NOZZLE HOLE. NEW CYLINDERS WERE INSTALLED AT ENGINE O/H.
- [SDR 2011FA0000269](https://openairdocs.org/sdr/2011FA0000269.md): Leg Assy · broken · Mar 31, 2011 · N6752X · Beech 58P · Nose/Tail Landing Gear
  > ACFT 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
- [SDR 2011FA0000039](https://openairdocs.org/sdr/2011FA0000039.md): Mount · damaged · Jan 3, 2011 · N79AP · Beech 58P · Engine Mount Section
  > UPON 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" IN
- [SDR 2010FA0000207](https://openairdocs.org/sdr/2010FA0000207.md): Distributor Blk · loose · Feb 16, 2010 · N491WM · Beech 58P · Magneto/Distributor
  > CUSTOMER 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.
- [SDR 2009FA0000289](https://openairdocs.org/sdr/2009FA0000289.md): Cylinder · cracked · Mar 16, 2009 · N6408Q · Beech 58P · Reciprocating Engine Cylinder Section
  > FOUND (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 C
- [SDR 2009FA0000290](https://openairdocs.org/sdr/2009FA0000290.md): Cylinder · cracked · Mar 15, 2009 · N6408Q · Beech 58P · Reciprocating Engine Cylinder Section
  > FOUND (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
- [SDR 2007FA0000247](https://openairdocs.org/sdr/2007FA0000247.md): Clamp · failed · Feb 27, 2007 · N25RL · Beech 58P · Engine Air Intake System
  > LT 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.
- [SDR EY2R0079965](https://openairdocs.org/sdr/EY2R0079965.md): Hub · corroded · Apr 21, 2006 · Beech 58P · Propeller Hub Section
  > CORROSION ON PROPELLER HUB.
- [SDR 0079965A](https://openairdocs.org/sdr/0079965A.md): Hub · corroded · Apr 4, 2006 · Beech 58P · Propeller Hub Section
  > PROPELLER HUB HAS INTERNAL AND EXTERNAL CORROSION
- [SDR 2005FA0001480](https://openairdocs.org/sdr/2005FA0001480.md): Clamp · loose · Oct 18, 2005 · N6677L · Beech 58P · Pneumatic Distribution System
  > IN 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)
- [SDR 2005FA0001210](https://openairdocs.org/sdr/2005FA0001210.md): Motor · failed · Aug 11, 2005 · N80LM · Beech 58P · Trailing Edge Flap Control System
  > FLAP 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)
- [SDR BHA01RS](https://openairdocs.org/sdr/BHA01RS.md): Window · departed · Nov 28, 2003 · N6047S · Beech 58P · Flight Compartment Windows
  > WHILE IN FLIGHT, PILOTS LEFT SIDE WINDOW CRACKED AND DEPARTED AIRCRAFT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.
- [SDR 2003FA0000972](https://openairdocs.org/sdr/2003FA0000972.md): Crossover Tube · chafed · Aug 22, 2003 · N153Z · Beech 58P · Engine Collector/Tailpipe/Nozzle
  > DURING 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 SAME
- [SDR CA030903007](https://openairdocs.org/sdr/CA030903007.md): Valve · leaking · Aug 12, 2003 · Beech 58P · Engine Fuel Distribution
  > (CAN) PN 6524323A1M (FLOW DIVIDED) LEAKING FUEL AFTER ENGINE SHUT DOWN/NEW PART INSTALLED.
- [SDR PG0306889](https://openairdocs.org/sdr/PG0306889.md): Skin · cracked · May 19, 2003 · N981SS · Beech 58P · Elevator, Plate/Skin
  > CRACK FOUND ON TOP SIDE OF LEFT HAND ELEVATOR, JUST FORWARD OF OUTBOARD END OF TRIM TAB. CRACK EXTENDS FORWARD INBOARD FOR APPROXIMATELY THREE INCHES.
- [SDR 2003FA0000086](https://openairdocs.org/sdr/2003FA0000086.md): Bearing · loose · Jan 15, 2003 · N135Z · Beech 58P · Magneto/Distributor
  > DURING 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 FAIL
- [SDR 2002FA0001348](https://openairdocs.org/sdr/2002FA0001348.md): Magneto · lack of lube · Nov 26, 2002 · N112RS · Beech 58P · Magneto/Distributor
  > ELECTROSYSTEMS 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 L
- [SDR DP02002F00000](https://openairdocs.org/sdr/DP02002F00000.md): Control Unit · failed · Sep 4, 2002 · N146Z · Beech 58P · Power Lever
  > NEW 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 PUBL
- [SDR 2002FA0001078](https://openairdocs.org/sdr/2002FA0001078.md): Throttle Control · binding · Sep 4, 2002 · N146Z · Beech 58P · Power Lever
  > PILOT 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. THI
- [SDR UAO2002F00000](https://openairdocs.org/sdr/UAO2002F00000.md): Truss · broken · Aug 27, 2002 · N145Z · Beech 58P · Engine Mount Section
  > DURING 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 ONTO
- [SDR 2002FA0001059](https://openairdocs.org/sdr/2002FA0001059.md): Panel · shorted · Aug 27, 2002 · N68BB · Beech 58P · Instrument Panel
  > PANEL ON SWITCH PANEL LIGHTING SHORTED WHICH MADE THE INVERTER EMITTED SMOKE INTO THE COCKPIT. BOTH PARTS WERE REPLACED WITH NEW PARTS FROM MFG.
- [SDR 2002FA0000456](https://openairdocs.org/sdr/2002FA0000456.md): Adapter · failed · Apr 8, 2002 · Beech 58P · Engine Starter
  > PILOT 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 40
- [SDR FEG2002F00000](https://openairdocs.org/sdr/FEG2002F00000.md): Line · chafed · Feb 20, 2002 · N153Z · Beech 58P · Engine Oil Indicating System
  > ENGINE 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 P
- [SDR 2001FA0000520](https://openairdocs.org/sdr/2001FA0000520.md): Skin · cracked · Oct 31, 2001 · N145Z · Beech 58P · Wing, Plate/Skin
  > LOWER 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 STRESSIN
- [SDR 2001FA0000519](https://openairdocs.org/sdr/2001FA0000519.md): Skin · cracked · Oct 31, 2001 · N145Z · Beech 58P · Fuselage Main, Plate/Skin
  > FOUND 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
- [SDR 2001FA0000518](https://openairdocs.org/sdr/2001FA0000518.md): Rivet · broken · Oct 31, 2001 · N145Z · Beech 58P · Vertical Stabilizer
  > RIVET 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 FA
- [SDR 2001FA0000398](https://openairdocs.org/sdr/2001FA0000398.md): Throttle Cable · chafed · Sep 28, 2001 · N145Z · Beech 58P · Power Lever
  > PILOT 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
- [SDR 2001FA0000333](https://openairdocs.org/sdr/2001FA0000333.md): Tire · failed · Sep 2, 2001 · N582TA · Beech 58P · Tire
  > NOSE TIRE FAILED AND NOSE GEAR COLLAPSED.
- [SDR FD62001F00000](https://openairdocs.org/sdr/FD62001F00000.md): Strobe · burned out · Aug 22, 2001 · N162Z · Beech 58P · Exterior Lighting
  > PRIOR 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. (T
- [SDR 20010425CW010](https://openairdocs.org/sdr/20010425CW010.md): Filter · chipped · Mar 22, 2001 · N1563L · Beech 58P · Reciprocating Engine Oil System
  > PILOT 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 F
- [SDR 20010328CW006](https://openairdocs.org/sdr/20010328CW006.md): Window · failed · Feb 22, 2001 · N40PG · Beech 58P · Passenger Compartment Windows
  > AIRCRAFT 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 IN
- [SDR 20010223CW005](https://openairdocs.org/sdr/20010223CW005.md): Probe · broken · Jan 23, 2001 · N4269S · Beech 58P · Engine EGT/TIT Indicating System
  > CUSTOMER 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 THE
- [SDR 20000920SH007](https://openairdocs.org/sdr/20000920SH007.md): Hinge · misinstalled · Sep 8, 2000 · N249CR · Beech 58P · Ailerons
  > OUTER 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,
- [SDR 20000811SH011](https://openairdocs.org/sdr/20000811SH011.md): Coupling · separated · Jul 24, 2000 · N120Z · Beech 58P · Alternator-Generator Drive
  > UPON 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.
- [SDR 20000811SH010](https://openairdocs.org/sdr/20000811SH010.md): Rod End · worn · Jul 24, 2000 · N133Z · Beech 58P · Landing Gear Actuator
  > DURING 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 E
- [SDR 20000828SH023](https://openairdocs.org/sdr/20000828SH023.md): Line · misaligned · Jul 22, 2000 · N163Z · Beech 58P · Vacuum Distribution System
  > PILOT 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
- [SDR 20000828SH022](https://openairdocs.org/sdr/20000828SH022.md): Nut · missing · Jul 22, 2000 · N163Z · Beech 58P · Air Conditioning System
  > WHILE 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 WO
- [SDR 20000628SH002](https://openairdocs.org/sdr/20000628SH002.md): Hinge · failed · Jun 16, 2000 · N79AP · Beech 58P · Landing Gear Doors
  > REAR 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 DISCONN
- [SDR 20001031SH018](https://openairdocs.org/sdr/20001031SH018.md): Injector · leaking · May 19, 2000 · N144Z · Beech 58P · Fuel Injector Nozzle
  > WHILE 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)

Next page: https://openairdocs.org/model/beech-58p/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/model/beech-58p/reports

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