# Service difficulty reports: Beech 58

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

Newest first. General aviation reporting is voluntary.

Page 1 of 20 · 1,000 reports

- [SDR 2026FA0000145](https://openairdocs.org/sdr/2026FA0000145.md): Fuel Line · cracked · Feb 9, 2026 · N747PH · Beech 58 · Aircraft Fuel Distribution System
  > DURING A ROUTINE OIL CHANGE, FOUND TWO FUEL INJECTION LINES WITH CRACKED SOLDER JOINTS AND WERE SPRAYING FUEL IN-FLIGHT. INJECTION LINES WERE IN CYLINDERS NR 1 AND NR 4.
- [SDR 2025F00224](https://openairdocs.org/sdr/2025F00224.md): Piston · separated · Sep 16, 2025 · N96GB · Beech 58 · Propeller Hub Section
  > PISTON CYLINDER BECAME SEPARATED FROM THE HUB. IT APPEARS THAT THE THREADS STRIPPED OUT OF THE HUB ABOUT 1/8 INCH. AT THIS TIME WE ARE SENDING TO H&S PROPELLER IN MICHIGAN FOR AN DETAILED TEAR DOWN INSPECTION REPORT TO DETERMINE THE FAILURE.
- [SDR 2024FA0000862](https://openairdocs.org/sdr/2024FA0000862.md): Alternator · inoperative · Nov 4, 2024 · N5ZR · Beech 58 · DC Generator-Alternator
  > PILOT EXPERIENCED LH ALTERNATOR FAILURE IN FLIGHT. TURNED LH ALTERNATOR SELECTOR TO OFF POSITION. SHORTLY AFTER, THE G1000 AVIONICS SYSTEM STARTED TO GO OUT. PILOT DECLARED EMERGENCY AND LANDED AT ROLLA NATIONAL (KVIH). SUSPECTED THE PILOT NEGLECTED TO MOVE LH
- [SDR XGNA20240223002](https://openairdocs.org/sdr/XGNA20240223002.md): Rib · cracked · Feb 19, 2024 · N577W · Beech 58 · Horizontal Stabilizer, Spar/Rib
  > 1 5/8-INCH CRACK ORIGINATING FROM THE FORWARD END OF LOWER FLANGE OF THE AFT INBOARD RIB. CRACK EXTENDS BEYOND THE FIRST RIVET OF FLANGE THEN SPLITS INTO 2 CRACKS WITH ONE ALMOST TO THE SECOND RIVET AND THE SECOND MOVING TOWARD THE RADIUS OF THE BEND IN THE FL
- [SDR XGNA20240219001](https://openairdocs.org/sdr/XGNA20240219001.md): Rib · cracked · Feb 19, 2024 · N577W · Beech 58 · Horizontal Stabilizer, Spar/Rib
  > 2 3/16-INCH CRACK IN AFT END OF LOWER FLANGE OF INBOARD FORWARD RIB. CRACKED THROUGH FIRST 3 RIVETS THEN, INTO RADIUS OF FLANGE JUST STARTING UPWARD INTO THE WEB OF RIB.
- [SDR XGNA202402150005](https://openairdocs.org/sdr/XGNA202402150005.md): Rib · cracked · Feb 14, 2024 · N577W · Beech 58 · Horizontal Stabilizer, Spar/Rib
  > TWO CRACKS IN INBOARD FORWARD RIB OF LEFT HORIZONTAL STABILIZER AT STA 00.000..25-INCH CRACK ORIGINATING FROM THE EDGE OF THE UPPER AFT FLANGE INTO THE FIRST RIVET. 2.5-INCH CRACK ORIGINATING FROM THE EDGE OF THE LOWER AFT FLANGE THROUGH THE FIRST 3 RIVETS, J
- [SDR XGNA2024021500006](https://openairdocs.org/sdr/XGNA2024021500006.md): Channel · cracked · Feb 14, 2024 · N577W · Beech 58 · Horizontal Stabilizer Structure
  > .25-INCH CRACK INTO FIRST RIVET IN LOWER FLANGE OF FRONT SPAR CHANNEL AT HORIZONTAL STABILIZER STA 00.000.
- [SDR XGNA202402150004](https://openairdocs.org/sdr/XGNA202402150004.md): Rib · cracked · Feb 14, 2024 · N577W · Beech 58 · Horizontal Stabilizer, Spar/Rib
  > CRACK 1.0 INCH IN LENGTH IN FORWARD LOWER FLANGE OF AFT INBOARD RIB AT HORIZONTAL STABILIZER STA 00.000. CRACK FROM AFT END OF FLANGE THROUGH THE FIRST RIVET AND THEN SPLITTING OFF INTO 2 CRACKS WITH THE MAIN CRACK ALMOST INTO THE SECOND RIVET AND THE OTHER CR
- [SDR XGNA202402150001](https://openairdocs.org/sdr/XGNA202402150001.md): Rib · cracked · Feb 14, 2024 · Beech 58 · Horizontal Stabilizer, Spar/Rib
  > TWO CRACKS IN INBOARD FORWARD RIB OF LEFT HORIZONTAL STABILIZER AT STA 00.000..25-INCH CRACK IN UPPER AFT FLANGE INTO THE FIRST RIVET. 2.5-INCH CRACK IN LOWER AFT FLANGE THROUGH 3 RIVETS, JUST BEGINNING TO TURN UPWARDS INTO THE WEB OF THE RIB.
- [SDR XGNA2024021500003](https://openairdocs.org/sdr/XGNA2024021500003.md): Gusset · cracked · Jan 31, 2024 · N2064V · Beech 58 · Horizontal Stabilizer Structure
  > 1 5/8 INCH CRACK IN LOWER RADIUS OF AFT SPAR GUSSET OF LEFT HORIZONTAL STABILIZER STA 00.000.
- [SDR XGNA2064VRIB](https://openairdocs.org/sdr/XGNA2064VRIB.md): Rib · cracked · Jan 31, 2024 · N2064V · Beech 58 · Horizontal Stabilizer, Spar/Rib
  > 2 INCH CRACK THROUGH 3 RIVETS IN LOWER AFT FLANGE OF FORWARD INBOARD RIB OF LEFT HORIZONTAL STABILIZER AT STA 00.000.
- [SDR XGNA202402130002](https://openairdocs.org/sdr/XGNA202402130002.md): Gusset · cracked · Jan 31, 2024 · N2064V · Beech 58 · Horizontal Stabilizer Structure
  > 1.58 INCH CRACK IN LOWER RADIUS OF AFT SPAR GUSSET AT STA 00.000 OF LEFT HORIZONTAL STABILIZER.
- [SDR XGNA2024021300001](https://openairdocs.org/sdr/XGNA2024021300001.md): Rib · cracked · Jan 31, 2024 · N2064V · Beech 58 · Horizontal Stabilizer, Spar/Rib
  > LEFT HORIZONTAL STABILIZER FORWARD INBOARD RIB AT HORIZONTAL STAB STA 00.000 CRACKED THROUGH 3 RIVETS IN THE LOWER FLANGE AND RADIUS OF FLANGE.
- [SDR XGNA2024021500002](https://openairdocs.org/sdr/XGNA2024021500002.md): Channel · cracked · Jan 2, 2024 · N36673 · Beech 58 · Horizontal Stabilizer Structure
  > 1/2-INCH CRACK IN LOWER INBOARD FLANGE RADIUS OF FORWARD SPAR CHANNEL OF LEFT HORIZONTAL STABILIZER AT STA 00.000.
- [SDR XGNA 202402130001](https://openairdocs.org/sdr/XGNA%20202402130001.md): Channel · cracked · Jan 2, 2024 · N36673 · Beech 58 · Horizontal Stabilizer Structure
  > .5 INCH CRACK IN LOWER INBOARD FLANGE RADIUS OF FORWARD SPAR CHANNEL OF LEFT HORIZONTAL STABILIZER.
- [SDR XGNA2024021336673](https://openairdocs.org/sdr/XGNA2024021336673.md): Channel · cracked · Jan 2, 2024 · N36673 · Beech 58 · Horizontal Stabilizer Structure
  > 1/2" CRACK IN LOWER FLANGE RADIUS OF FRONT SPAR CHANNEL OF LEFT HORIZONTAL STABILIZER.
- [SDR XGN2024F00000](https://openairdocs.org/sdr/XGN2024F00000.md): Channel · cracked · Jan 2, 2024 · N36673 · Beech 58 · Horizontal Stabilizer Structure
  > 1/2" CRACK IN LOWER FLANGE RADIUS OF FRONT SPAR CHANNEL OF LEFT HORIZONTAL STABILIZER.
- [SDR 2023FA0000674](https://openairdocs.org/sdr/2023FA0000674.md): Motor · seized · Oct 18, 2023 · N889FT · Beech 58 · Landing Gear Retraction/Extension System
  > LANDING GEAR MOTOR SEIZED IN GEAR TRANSIT AND WOULD NOT EXTEND GEAR. PREVENTED MANUAL EXTENSION BY HAND CRANK. GEAR MOTOR FILLED COCKPIT WITH SMOKE. AIRCRAFT LANDED WITH LANDING GEAR NOT LOCKED AND SUFFERED LANDING GEAR COLLAPSE AND PROP STRIKE. LANDING GEAR M
- [SDR 2023FA0000579](https://openairdocs.org/sdr/2023FA0000579.md): Nut · backed out · Sep 30, 2023 · N686FR · Beech 58 · Engine Mount Section
  > NOTICED A LOSS OF FUEL PRESSURE EN ROUTE. ELECTED TO LAND AT NEAREST SUITABLE AIRPORT. FOUND THAT THE MIXTURE CABLE SUPPORT NUT HAD BACKED OFF AND ALLOWED THE CABLE TO PULL THE MIXTURE ARM TOWARDS LEAN, RESULTING IN PARTIAL LOSS OF POWER.
- [SDR Q5QA20230525005](https://openairdocs.org/sdr/Q5QA20230525005.md): Magneto · damaged · May 25, 2023 · N14JH · Beech 58 · Magneto/Distributor
  > DURING A PRE-TAKE OFF MAGNETO CHECK THE PILOT OBSERVED HIS #2 ENGINE RIGHT MAGNETO HAD A 1100 RPM DROP AND WAS FAILING HIS MAGNETO CHECK. THE PILOT THEN RETURNED THE BEECH BARON 58 TO MAINTENANCE. THE MAINTENANCE TEAM COMPLETED A RUN-UP OF THE AIRCRAFT CONFIRM
- [SDR Q5QA20230222003](https://openairdocs.org/sdr/Q5QA20230222003.md): Doubler · cracked · Feb 20, 2023 · Beech 58 · Fuselage Main, Bulkhead
  > DURING AN INSPECTION OF THE TAIL SECTION OF N36TA, THE AFT-MOST FUSELAGE BULKHEAD ASSEMBLY, FS 272.0, WAS NOTED CRACKED AT THE LEFT LOWER AND RIGHT LOWER RADII ONLY ON THE DOUBLER P/N 002-440024-11 (SEE ATTACHED PHOTO).
- [SDR Q5QA20230215001](https://openairdocs.org/sdr/Q5QA20230215001.md): Bulkhead · cracked · Feb 15, 2023 · N2143J · Beech 58 · Fuselage Main, Bulkhead
  > DURING AN INSPECTION OF THE TAIL SECTION OF N2143J, THE AFT-MOST FUSELAGE BULKHEAD ASSEMBLY, FS 272.0, WAS NOTED CRACKED AT THE LEFT LOWER AND RIGHT LOWER RADII.
- [SDR 2022FA0000741](https://openairdocs.org/sdr/2022FA0000741.md): Crankshaft · cracked · Dec 6, 2022 · N7293R · Beech 58 · Reciprocating Engine Power Section
  > OIL LEAK, TROUBLESHOT AND FOUND CRANKSHAFT, PROPELLER FLANGE CRACKED 1/2 WAY AROUND CIRCUMFERENCE. ENGINE IS NEW WITH 13.6 HOURS ON IT.
- [SDR 2022FA0000282](https://openairdocs.org/sdr/2022FA0000282.md): Propeller · active · Jun 9, 2022 · N78KL · Beech 58 · Propeller Blade Section
  > PROPELLER BLADE BROKE OFF AT END OF DE-ICE BOOT 16 INCH FROM ROOT
- [SDR Q5QA20220324004](https://openairdocs.org/sdr/Q5QA20220324004.md): Brush Block · broken · Mar 24, 2022 · N36TA · Beech 58 · Alternator-Generator Drive
  > THE PILOT REPORTED LH ALTERNATOR WAS INOPERATIVE. THE PILOT LANDED AT AN ALTERNATIVE AIRPORT WITHOUT INCIDENT. A TECHNICIAN'S INSPECTION DISCLOSED THAT THE ALTERNATOR BRUSH ASSEMBLY HAD ONE BRAIDED LEAD BROKEN AT THE TERMINAL BLOCK. THE BRUSH ASSEMBLY WAS R
- [SDR Q5QA20220127001](https://openairdocs.org/sdr/Q5QA20220127001.md): Piston Pin · broken · Jan 27, 2022 · N96WE · Beech 58 · Engine (Reciprocating)
  > DURING A CYLINDER CHANGE FOUND THE PISTON PIN ALUMINUM END CAP PLUG WAS BROKEN IN TWO PIECES. THERE WAS NO ABNORMAL WEAR ON THE CONNECTING ROD PISTON PIN BUSHING, AND THE BUSHING DIMENSIONS ARE WITHIN SPEC. NO METAL CONTAMINATION WAS FOUND IN THE FILTER OR ENG
- [SDR Q5QA20211102005](https://openairdocs.org/sdr/Q5QA20211102005.md): Pcb · shorted · Nov 2, 2021 · N36TA · Beech 58 · Flight Control System Wiring
  > PILOT EXPERIENCED A FLAP FAILURE ON APPROACH FOR LANDING. THE FLAPS WOULD NOT EXTEND PAST 0 DEGREES AND THE FLAP MOTOR CIRCUIT BREAKER WAS TRIPPED. THE PILOT LANDED WITHOUT FURTHER INCIDENT. TROUBLESHOOTING DISCLOSED THAT THE MOTOR HAD A BURNED ELECTRICAL S
- [SDR XGNA2021052500013](https://openairdocs.org/sdr/XGNA2021052500013.md): Spar · cracked · May 25, 2021 · N36673 · Beech 58 · Fuselage Main, Structure
  > DURING A VISUAL INSPECTION REQUIRED BY AD 90-08-14 SPAR CARRY THRU INSPECTION CRACKS WERE FOUND RADIATING FROM THE OUTBOARD UPPER HUCKBOLT HOLE OUTWARD ON THE FORWARD LEFT AND RIGHT HAND FORWARD SPAR. THESE CRACKS WERE FOUND ABOVE THE INSPECTION AREA REQUIRED
- [SDR XGNA2021050500012](https://openairdocs.org/sdr/XGNA2021050500012.md): Landing Gear · malfunctioned · May 4, 2021 · N36673 · Beech 58 · Nose/Tail Landing Gear
  > DURING DEPARTURE OF FLIGHT # GTX487 FROM ADS TO ELP, AND AFTER GEAR RETRACTION OUR DIRECTOR OF OPERATION'S VISUALLY OBSERVED THAT THE NOSE GEAR DOORS HAD NOT RETRACTED. HE CONTACTED ADS GROUND TO HAVE THEM CONTACT REGIONAL APPROACH TO CONTACT THE PILOT OF FLIG
- [SDR Q5QA2021030501](https://openairdocs.org/sdr/Q5QA2021030501.md): Magneto · failed · Mar 5, 2021 · N2143J · Beech 58 · Magneto/Distributor
  > PILOT NOTED ON RUN-UP THAT THE #2 ENGINE LH MAGNETO WAS MISFIRING. THE MAGNETO WAS REPLACED WITH NO FURTHER INCIDENT. TROUBLESHOOTING DISCLOSED THE MAGNETO POINT GAP HAD APPARENTLY SHIFTED AND THE INTERNAL MAGNETO TIMING WAS SUBSTANTIALLY OUT OF LIMITS. IN
- [SDR XGNA2021052500012](https://openairdocs.org/sdr/XGNA2021052500012.md): Spar · cracked · Feb 15, 2021 · N577W · Beech 58 · Fuselage Main, Structure
  > DURING A VISUAL INSPECTION REQUIRED BY AD 90-08-14 SPAR CARRY THRU INSPECTION CRACKS WERE FOUND RADIATING FROM THE OUTBOARD UPPER HUCKBOLT HOLE OUTWARD ON THE FORWARD AND AFT SIDES OF THE LEFT HAND FORWARD SPAR. THESE CRACKS WERE FOUND ABOVE THE INSPECTION ARE
- [SDR XGNA2020111800009](https://openairdocs.org/sdr/XGNA2020111800009.md): Motor · failed · Nov 18, 2020 · N36673 · Beech 58 · Landing Gear Retraction/Extension System
  > DURING APPROACH PILOT ATTEMPTED TO EXTEND THE LANDING GEAR. HE HAD NO VISUAL INDICATION THE GEAR WAS DOWN. HE ABORTED THE APPROACH, FLEW BY THE TOWER TO VERIFY GEAR WAS NOT EXTENDED. HE THEN PROCEEDED EAST OF KADS TO TROUBLESHOOT LANDING GEAR. HE WAS ABLE
- [SDR XGNA2020050600007](https://openairdocs.org/sdr/XGNA2020050600007.md): Door · unsecure · May 6, 2020 · N36673 · Beech 58 · Cargo/Baggage Doors
  > ON 06 MAY, 2020 AT APPROXIMATELY 7:20AM EDT WHILE OPERATING GTX502, PILOT HAD TO ABORT THE TAKEOFF ROLL AT KIAD, RWY 19C DUE TO AN UNSECURED NOSE BAGGAGE DOOR ON N36673. AFTER ABORTING THE TAKEOFF PILOT NOTIFIED TOWER OF THE ABORTED TAKEOFF DUE TO THE UNSECUR
- [SDR Q5QA202001140301](https://openairdocs.org/sdr/Q5QA202001140301.md): Wheel Half · cracked · Jan 3, 2020 · N36TA · Beech 58 · Wheel/Ski/Float
  > LINE PERSONNEL NOTED A WOBBLE IN THE LEFT MAIN WHEEL WHILE TOWING THE AIRCRAFT OUT OF THE HANGAR. FURTHER INSPECTION DISCLOSED A VERY LARGE CIRCUMFERENTIAL CRACK ON THE OUTBOARD WHEEL HALF INSIDE OF THE TIRE BEAD AREA.
- [SDR XGNA201912160001](https://openairdocs.org/sdr/XGNA201912160001.md): Switch · out of adjust · Dec 13, 2019 · N6573K · Beech 58 · Landing Gear Position and Warning
  > DURING APPROACH TO LANDING, GEAR FAILED TO SHOW THREE GREEN, NOSE GEAR LIGHT FLICKERED. PILOT EXECUTED A GO AROUND AND RECYCLED GEAR. PILOT THEN REPORTED GETTING THREE GREEN GEAR DOWN AND LOCK INDICATION. LANDED WITHOUT INCIDENT. MAINTENANCE REPORTED THEY FOUN
- [SDR 2020FA0000018](https://openairdocs.org/sdr/2020FA0000018.md): Arm · broken · Oct 6, 2019 · N9LT · Beech 58 · Nose/Tail Landing Gear
  > NOSE LANDING GEAR UP/DOWN SWITCH ACTUATING ARM BROKEN AT PIVOTING BOLT.
- [SDR Q5QA20190815243](https://openairdocs.org/sdr/Q5QA20190815243.md): Spar Web · cracked · Aug 15, 2019 · N202P · Beech 58 · Wing Spar
  > REAR SPAR CARRY THROUGH IS CRACKED.THE CRACK RADIATES FROM THE LOWER RIGHT MOST OUTBOARD FASTENER OF THE FUSELAGE REAR WING ATTACH FITTING. THE LENGTH OF THE CRACK IS APPROXIMATELY 5/16" AND CAN BE SEEN WITHOUT MAGNIFICATION. THE CRACK WAS CONFIRMED WITH EDDY
- [SDR Q6MR201908123003](https://openairdocs.org/sdr/Q6MR201908123003.md): Engine · shutdown · Aug 4, 2019 · N484WW · Beech 58 · Engine (Turbine/Turboprop)
  > PILOT REPORTED LEFT ENGINE SHUT DOWN IN CRUISE FLIGHT. PILOT RETURNED TO DEPARTURE AIRPORT. MAINTENANCE INSPECTED THE ENGINE INCLUDING FUEL SYSTEM AND IGNITION SYSTEM. RAN ENGINE ON GROUND. ENGINE STARTED AND RAN WITH NO DEFECTS. COULD NOT DUPLICATE ISSUE.
- [SDR 2019FA0000157](https://openairdocs.org/sdr/2019FA0000157.md): Gasket · cracked · May 23, 2019 · N592WT · Beech 58 · Engine Fuel Distribution
  > ENGINE FUEL INLET SCREEN GASKETS SPLITTING, CAUSING A FUEL LEAK. WE BELIEVE THIS TO HAVE BEEN A BAD BATCH OF GASKETS. ON THIS PARTICULAR AIRPLANE, NEW GASKETS WERE INSTALLED ON 4/2. PILOT REPORTED TO US THAT THE LEFT GASKET WAS LEAKING ON 4/26. RIGHT SIDE WAS
- [SDR 2019FA0000126](https://openairdocs.org/sdr/2019FA0000126.md): Battery · failed · Apr 22, 2019 · N27DQ · Beech 58 · Battery/Charger System
  > UPON ENGAGING LT ENGINE STARTER, AIRCRAFT SUFFERED COMPLETE BATTERY ELECTRICAL BUS FAILURE. RIGHT ENGINE WAS RUNNING WITH BATTERY MASTER SWITCH ON. THE POSITION OF THE RT ALTERNATOR SWITCH IS UNKNOWN. TROUBLESHOOTING OF THE ISSUE FOUND THAT ONE OF THE 2 12V
- [SDR 2020FA0000087](https://openairdocs.org/sdr/2020FA0000087.md): Fork · cracked · Feb 18, 2019 · N638LD · Beech 58 · Propeller Controlling System
  > CRACK FOUND ON PITCH CHANGE FORK DURING MAGNETO PARTICLE INSPECTION. THE CRACK IS APPROXIMATELY 0.125 INCHES LONG AND IS LOCATED ON THE BOTTOM CORNER OF THE BLOCK SLOT. CRACK MAY HAVE FORMED DUE TO SERVICE FATIGUE. THERE IS NO EVIDENCE OF ABNORMAL LOAD OR O
- [SDR Q5QA2018122808](https://openairdocs.org/sdr/Q5QA2018122808.md): Stringer · cracked · Dec 7, 2018 · N910SA · Beech 58 · Wing, Longeron/Stringer
  > INSPECTION DISCLOSED WING STRINGER ON LOWER RH WING WAS CRACKED INBOARD AND OUTBOARD OF RIB AT W.S 108.5
- [SDR 2018FA0000502](https://openairdocs.org/sdr/2018FA0000502.md): Bladder · contaminated · Dec 4, 2018 · N951MB · Beech 58 · Fuel Storage
  > ON G58 BARON S/N TH-2474, OPERATOR STARTED NOTING CONTINUALLY CLOUDY SUMP FUEL FROM LEFT INBOARD SUMP, APPROXIMATELY 100 HOURS AFTER AIRCRAFT WAS DELIVERED NEW WITH RELIABLE FUELING LOCATION. FUEL SAMPLE WAS SENT TO BEECH FOR ANALYSIS. SUBSTANCE WAS DETERMINED
- [SDR 2020FA0000085](https://openairdocs.org/sdr/2020FA0000085.md): Switch · failed · Nov 30, 2018 · N882MT · Beech 58 · Light System Wiring
  > THESE ARE THE NEW SWITCHES CALL FOR IN AD2008-13-17 AND SB 24-3807. THESE NEW SWITCHES HAVE A HIGHER FAILURE RATE COMPARED TO OEM PART.
- [SDR Q5QA2018122809](https://openairdocs.org/sdr/Q5QA2018122809.md): Spar · cracked · Sep 14, 2018 · N1065B · Beech 58 · Trailing Edge Flaps
  > INSPECTION DISCLOSED LEFT FLAP SPAR WAS CRACKED ALONG UPPER FLANGE CORNER AT OUTBOARD FLAP TRACK BRACKETRY.
- [SDR VRXR20180822002](https://openairdocs.org/sdr/VRXR20180822002.md): Stud · pulled · Aug 8, 2018 · N858PB · Beech 58 · Manifold Pressure (MP) Indicating
  > STUD PULLED OUT OF TACH DRIVE HOUSING COVER ALLOWING OIL TO LEAK OUT ONTO EXHAUST CAUSING SMOKE AND THE FLIGHT TO RETURN TO THE AIRPORT IMMEDIATELY AFTER TAKEOFF. THE THREADS WERE PULLED OUT POSSIBLY FROM REPETITIVELY REMOVING BRACKET FROM THE Y PIPE DURING
- [SDR 17GR2018071701](https://openairdocs.org/sdr/17GR2018071701.md): Pressure Switch · defective · Jul 17, 2018 · N747DW · Beech 58 · Air Conditioning System
  > SWITCH FAILED BLOCKING VOLTAGE TO COMPRESSOR CLUTCH. DID NOT BLOW FUSE ASSOCIATED WITH SWITCH CIRCUIT.
- [SDR Q5QA201807131007](https://openairdocs.org/sdr/Q5QA201807131007.md): Wire · broken · Jul 10, 2018 · N910SA · Beech 58 · Electrical Power System Wiring
  > THE LT ALTERNATOR WAS REMOVED FOR ROUTINE INSPECTIONS. AFTER REMOVING THE COVER FROM THE BACK OF THE ALTERNATOR, THE TECHNICIAN NOTED SOME GREEN DISCOLORATION ON ONE OF THE DIODES. FURTHER INVESTIGATION DISCLOSED THE DIODE WIRE WAS BROKEN OFF OF THE DIODE BA
- [SDR Q5QA201807131006](https://openairdocs.org/sdr/Q5QA201807131006.md): Drive Coupling · worn · Jul 10, 2018 · N910SA · Beech 58 · AC Generator-Alternator
  > DURING A ROUTINE INSPECTION OF THE ALTERNATOR DRIVE HUB, THE INSPECTOR NOTED THE CASTELLATED NUT RETAINING THE DRIVE HUB WAS LOOSE (THE COTTER PIN THROUGH THE CASTELLATED NUT WAS STILL IN PLACE). INSPECTION AFTER REMOVAL OF THE DRIVE HUB ASSEMBLY DISCLOSED EX
- [SDR Q5QA2018070605](https://openairdocs.org/sdr/Q5QA2018070605.md): Alternator · defective · Jul 6, 2018 · N36TA · Beech 58 · DC Generator-Alternator
  > PILOT REPORTED LT ALTERNATOR WAS INTERMITTENT (INDICATOR LIGHT WAS FLASHING). INSPECTION DISCLOSED A CRACKED SOLDER JOINT ON THE ALTERNATOR AT THE BASE OF THE A+ OUTPUT TERMINAL.

Next page: https://openairdocs.org/model/beech-58/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 = '58'
ORDER BY difficulty_date DESC
```

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

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