# Service difficulty reports: Beech 65-A80 A list on [Beech 65-A80](https://openairdocs.org/model/beech-65-a80.md). Newest first. General aviation reporting is voluntary. - [SDR BEMA2019072900001](https://openairdocs.org/sdr/BEMA2019072900001.md): Intake Valve · broken · Jul 23, 2019 · N131BA · Beech 65A80 · Reciprocating Engine Cylinder Section > THE #1 CYLINDER INDUCTION VALVE FAILED IN FLIGHT. THE PROBLEM WAS NOT DETECTED UNTIL THE PILOT DID HIE POST FLIGHT WALK AROUND. THE VALVE BROKE IN HALF AT THE NARROW SPOT WERE THE VALVE KEEPERS ARE. THE VALVE PART NUMBER IS 17A23937, AND CONTROL NUMBER FOR THE - [SDR WX52008F00000](https://openairdocs.org/sdr/WX52008F00000.md): Shaft · worn · May 16, 2008 · N6AQ · Beech 65A80 · Nose/Tail Landing Gear > NLG WOULD NOT DEPLOY ON APP TO LANDING. AFTER NLG REMOVAL IT WAS DISCOVERED THA THE NLG ACTUATOR DRIVE SHAFT (PN 50-820218) INTERNAL SPLINE WAS WORN AND SHEARED. LUBE POINTS ON DRIVE SHAFT TO LUBE SPLINES TO REDUCE WEAR. (K) - [SDR 2008FA0000353](https://openairdocs.org/sdr/2008FA0000353.md): Shaft · lack of lube · May 16, 2008 · N6AQ · Beech 65A80 · Landing Gear Actuator > NOSE LANDING GEAR WOULD NOT DEPLOY ON APPROACH TO LANDING. AFTER NLG REMOVAL, IT WAS DISCOVERED THAT THE NLG ACTUATOR DRIVE SHAFT PN 50820218 INTERNAL SPLINE WAS WORN AND SHEARED. LUBE POINTS ON DRIVE SHAFT TO LUBE SPLINES TO REDUCE WEAR. (K) - [SDR 2006F00012](https://openairdocs.org/sdr/2006F00012.md): Actuator · failed · Feb 14, 2006 · N55SA · Beech 65A80 · Landing Gear Actuator > PILOT SELECTED GEAR DOWN FOR LANDING AND HAD NO NOSE INDICATION. HE PERFORMED A LOW LEVEL PASS AND GROUND PERSONNEL DETERMINED THAT THE NOSE GEAR WAS NOT IN THE DOWN AND LOCKED POSITION. A GEAR UP LANDING WAS MADE WITH MINOR DAMAGE TO THE AIRCRAFT. FURTHER INS - [SDR 20010206CW006](https://openairdocs.org/sdr/20010206CW006.md): Exhaust Valve · broken · Jan 11, 2001 · N134BA · Beech 65A80 · Reciprocating Engine Cylinder Section > EXHAUST VALVE BROKEN IN HALF. - [SDR 20000720SH006](https://openairdocs.org/sdr/20000720SH006.md): Fitting · cracked · Jul 6, 2000 · N70348 · Beech 65A80 · Empennage Flight Control Surfaces, Attach Fittings > FOUND CRACK RUNNING FROM.25 INCH MOUNTING HOLE TO EDGE OF PART. POSSIBLE CAUSE WAS OVERTORQUE OF FITTING TO ELEVATOR BELLCRANK ATTACH BOLT. FITTING TIES ELEVATOR TORQUE TUBE TO BELLCRANK ASSEMBLY. (X) - [SDR 2000ZZZX32](https://openairdocs.org/sdr/2000ZZZX32.md): Shaft · failed · Dec 16, 1999 · N95LL · Beech 65A80 · Engine Starter > STARTER DRIVE SHAFT TWISTED OFF ABOUT.1250 INCH FORWARD OF KEY SLOT - EVEN WITH FORWARD EDGE OF DRIVEN GEAR ON SHAFT/BENDIX. - [SDR 97ZZZX5175](https://openairdocs.org/sdr/97ZZZX5175.md): Pump Adapter · cracked · Nov 25, 1997 · N95LL · Beech 65A80 · Reciprocating Engine Rear Section > FOUND HYDRAULIC PUMP ADAPTER WITH CRACKED MOUNT FLANGE. SUBMITTER STATED WILL CRACK AROUND ANY OF THE 4 HOLD-DOWN FLANGES. - [SDR 97ZZZX3172](https://openairdocs.org/sdr/97ZZZX3172.md): Pump Adapter · cracked · Jun 24, 1997 · N95LL · Beech 65A80 · Hydraulic Pump (Electric/Engine), Main > THE HYDRAULIC PUMP ADAPTER CRACKS AND EVENTUALLY BREAKS AT THE ATTACH POINT TO ACCESSORY CASE. - [SDR 97ZZZX758](https://openairdocs.org/sdr/97ZZZX758.md): Boot · lead broken · Dec 27, 1996 · N95LL · Beech 65A80 · Propeller Deice Boot Section > THE LEADS ARE BREAKING 12 INCHES FROM THE TERMINALS. THE LEAD IS REQUIRED TO BEND IN THIS AREA. SUBMITTER STATED THIS IS THE 10TH BOOT WHICH HAS FAILED IN THIS AREA IN THE LAST FIVE WEEKS. - [SDR 97ZZZX751](https://openairdocs.org/sdr/97ZZZX751.md): Drive Assy · failed · Dec 23, 1996 · N134BA · Beech 65A80 · Trailing Edge Flap Actuator > SOMETHING WITHIN THE 90 DEGREE DRIVE ASSY FAILED WHICH MADE THE FLAP FAIL TO EXTEND OR RETRACT. THE ACTUATOR WAS OH 20.6 HRS AGO. - [SDR 96ZZZX6092](https://openairdocs.org/sdr/96ZZZX6092.md): Deice Boot · wires break · Dec 4, 1996 · N55SA · Beech 65A80 · Propeller Deice Boot Section > PROP DE-ICE BOOT OTB, INB, AND GRD WIRES BREAK 12 INCHES FROM THE TERMINALS. THE LEAD IS REQUIRED TO BEND IN THIS AREA. THIS IS THE 8TH BOOT WHICH HAS FAILED IN THIS AREA IN THE LAST TWO WEEKS. - [SDR EY2R9601155](https://openairdocs.org/sdr/EY2R9601155.md): Bearing · corroded · Oct 1, 1996 · Beech 65A80 · Propeller Assembly > SPLIT BEARING FOUND CORRODED. - [SDR EY2R9601045](https://openairdocs.org/sdr/EY2R9601045.md): Blade · corroded · Oct 1, 1996 · Beech 65A80 · Propeller Blade Section > BLADE, SN 111092, FOUND CORRODED. - [SDR EY2R9601044](https://openairdocs.org/sdr/EY2R9601044.md): Blade · corroded · Oct 1, 1996 · Beech 65A80 · Propeller Blade Section > BLADE, SN A20549, FOUND CORRODED. - [SDR EY2R9601043](https://openairdocs.org/sdr/EY2R9601043.md): Blade · corroded · Oct 1, 1996 · Beech 65A80 · Propeller Blade Section > BLADE, SN B69968, FOUND CORRODED. - [SDR EY2R9601041](https://openairdocs.org/sdr/EY2R9601041.md): Pilot Tube · corroded · Oct 1, 1996 · Beech 65A80 · Propeller Assembly > R & R PILOT TUBES - [SDR EY2R9601040](https://openairdocs.org/sdr/EY2R9601040.md): Pilot Tube · corroded · Oct 1, 1996 · Beech 65A80 · Propeller Assembly > R & R PILOT TUBES ## 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 = '65A80' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/beech-65-a80/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.