# Service difficulty reports: Beech V35

A list on [Beech V35](https://openairdocs.org/model/beech-v35.md).

Newest first. General aviation reporting is voluntary.

- [SDR 2026FA0000631](https://openairdocs.org/sdr/2026FA0000631.md): Impulse Coupling · destroyed · Jul 8, 2026 · N231S · Beech V35 · Magneto/Distributor
  > THE PILOT/OWNER ATTEMPTED TO START THE PLANE. AFTER THE FIRST FAILED START, THE PROPELLER STOPPED SPINNING DURING THE SECOND ATTEMPTED START. THE PILOT ABORTED THE START AND ALERTED ME TO A GRINDING SOUND. UPON INSPECTING THE ENGINE, THE LEFT MAGNETO HOUSING H
- [SDR 2022FA0000215](https://openairdocs.org/sdr/2022FA0000215.md): Brake · corroded · Mar 19, 2022 · N2058W · Beech V35 · Landing Gear Brake System
  > RIGHT BRAKE FAILED ON ROLL OUT FROM LANDING, DEPARTED RUNWAY. NO DAMAGE TO AIRCRAFT. AIRCRAFT TOWED TO MAINTENANCE FACILITY. BRAKE LINE FROM RIGHT MASTER CYLINDER PASSING UNDER HEATING DUCT HOSE CLAMP (FORWARD CABIN, UNDER FLOOR BOARD) DEVELOPED LEAK FROM CORR
- [SDR 2019FA0000033](https://openairdocs.org/sdr/2019FA0000033.md): Control Cable · broken · Jan 5, 2019 · N3704Q · Beech V35 · Aileron Control System
  > DURING ANNUAL INSPECTION, FOUND RIGHT AILERON CABLE BROKEN AT SWAGED END BETWEEN SAFETY WIRE HOLE AND THREADED END. SAFETY WIRE WAS HOLDING IT TOGETHER.
- [SDR 2018FA0000470](https://openairdocs.org/sdr/2018FA0000470.md): Control Cable · corroded · Nov 1, 2018 · N9568Q · Beech V35 · Aileron Control System
  > DURING CRUSE ALTITUDE 7500FT, THERE WAS A LOSS OF AILERON CONTROL. THE AIRCRAFT DRIFTED TO THE RIGHT AND WAS CORRECTED BY ROLLING LEFT. THE PILOT THEN FELT SOMETHING BREAK AND THE RIGHT WING DROPPED. THE PILOT TURNED THE AILERON CONTROL YOKE TO THE LEFT, UNTI
- [SDR 2016FA0000316](https://openairdocs.org/sdr/2016FA0000316.md): Warning System · failed · Jun 29, 2016 · N149G · Beech V35 · Landing Gear Position and Warning
  > GEAR WARNING HORN FAILED TO SOUND DURING LANDING WITH GEAR UP.
- [SDR MAMR2015121600654](https://openairdocs.org/sdr/MAMR2015121600654.md): Housing · damaged · Dec 4, 2015 · N354DP · Beech V35 · Exhaust Turbocharger
  > TURBOCHARGER RECEIVED IN FOR INSPECTION, FOUND THE TURNINE HOUSING HAD DEVELOPED A GROWTH OR DEFORMITY IN THE CASTING. THIS DECREASED THE CLEARANCE BETWEEN THE TURBINE HOUSING AND THE TURBINE WHEEL CAUSING THE TURBO TO RUB/STICK. REPLACED THE TURBINE HOUSING
- [SDR 2015FA0000606](https://openairdocs.org/sdr/2015FA0000606.md): Housing · deformed · Nov 3, 2015 · N110CC · Beech V35 · Exhaust Turbocharger
  > TURBOCHARGER RECEIVED IN FOR INSPECTION. FOUND THE TURBINE HOUSING HAD DEVELOPED A GROWTH OR DEFORMITY IN THE CASTING. THIS DECREASED THE CLEARANCE BETWEEN THE TURBINE HOUSING AND TURBINE WHEEL CAUSING A SLIGHT RUB OR CLUNKING SOUND. REPLACED THE TURBINE HO
- [SDR 2015FA0000281](https://openairdocs.org/sdr/2015FA0000281.md): Throttle Arm · disconnected · Jun 22, 2015 · N54VK · Beech V35 · Power Lever
  > PRACTICING AN INSTRUMENT APPROACH INTO AIRPORT. PILOT FLYING WAS SLIGHTLY LOW ON A NON-PRECISION INSTRUMENT APPROACH. POWER SETTING WAS 15" MAP. APPLICATION OF FULL THROTTLE, DID NOT INCREASE MANIFOLD PRESSURE. AFTER SAFE LANDING ON RUNWAY WITH NO DAMAGE T
- [SDR 2013FA0000321](https://openairdocs.org/sdr/2013FA0000321.md): Worm Gear · mismanufactured · Jun 5, 2013 · Beech V35 · Landing Gear Retraction/Extension System
  > WORM GEAR RECEIVED FROM MFG. VISUAL INSPECTION REVEALED A "ROUGH" SURFACE FINISH ON GEAR FACE. CONFIRMED "OUT OF LIMITS".
- [SDR 2012FA0000295](https://openairdocs.org/sdr/2012FA0000295.md): Fitting · cracked · May 1, 2012 · N433S · Beech V35 · Elevator Control System
  > DURING INSPECTION AND REMOVAL OF TAIL CONE, FOUND RT ELEVATOR CONTROL FITTING CRACKED 75 PERCENT AROUND FITTING.
- [SDR 2011FA0000413](https://openairdocs.org/sdr/2011FA0000413.md): Lifter · spalled · Apr 20, 2011 · Beech V35 · Reciprocating Engine Cylinder Section
  > LIFTERS SPALLED, CAUSING A METAL CONTAMINATION IN THE ENGINE.
- [SDR 2011FA0000412](https://openairdocs.org/sdr/2011FA0000412.md): Lifter · spalled · Apr 20, 2011 · Beech V35 · Reciprocating Engine Cylinder Section
  > LIFTERS SPALLED, CAUSING A METAL CONTAMINATION IN THE ENGINE.
- [SDR 2010FA0000961](https://openairdocs.org/sdr/2010FA0000961.md): Gasket · loose · Aug 20, 2010 · N35UP · Beech V35 · Engine Air Intake System
  > GASKET CAME OFF THE AIR FILTER. THE ADHESIVE HAD FAILED LETTING THE GASKET GET LOOSE AND IT CAN BE SUCKED INTO THE ENGINE, SHUTTING IT DOWN. CALLED MFG AND TALKED TO REP ABOUT THIS.
- [SDR 2008FA0000436](https://openairdocs.org/sdr/2008FA0000436.md): Cylinder · cracked · May 6, 2008 · N2024W · Beech V35 · Reciprocating Engine Cylinder Section
  > CRACK VISIBLE AT NR 4 CYLINDER. CRACK APPEARS TO START AT CASTING ANOMALY, CONTINUES TO EDGE OF FINS, AND IS VISIBLE AT THE FIRST FOUR COOLING FINS. ALSO VERIFIED, THROUGH USE OF EDDY CURRENT, THAT THE CRACK CONTINUES TO THE SPARK PLUG HOLE. ALL OTHER CYLINDER
- [SDR 0000H2484](https://openairdocs.org/sdr/0000H2484.md): Line · chafed · Mar 18, 2008 · N363BC · Beech V35 · Aircraft Fuel Distribution System
  > FUEL LINE MOUNTED ON FIREWALL FABRICATED PER STC SA8676SW WAS CHAFING THE ENGINE TAILPIPE.
- [SDR 07N911KD01](https://openairdocs.org/sdr/07N911KD01.md): Spar · cracked · May 25, 2007 · N911K · Beech V35 · Rotorcraft Tail Boom
  > DURING DETAILED INSPECTION OF TAILBOOM VERTICAL SPAR AREA FOUND 2 EA CRACKS APPROX.7500 INCHES IN LENGTH AT THE 1:00 O'CLOCK AND 7:00 O'CLOCK POSITIONS ON THE SECOND LIGHTING HOLE DOWN FROM TAIL ROTOR GEARBOX MOUNT. SUSPECT CRACKS HAVE BEEN WORKING FOR SOME T
- [SDR 2007FA0000090](https://openairdocs.org/sdr/2007FA0000090.md): Control Cable · broken · Jan 2, 2007 · N767TM · Beech V35 · Elevator Control System
  > FOUND BROKEN STRANDS ON ELEVATOR CABLE BEHIND INSTRUMENT PANEL ABOUT 10 INCHES ABOVE THE (PN 535521242-13) BOBWEIGHT. (K)
- [SDR 2006FA0001229](https://openairdocs.org/sdr/2006FA0001229.md): Line · broken · Nov 22, 2006 · N205DB · Beech V35 · Reciprocating Engine Oil System
  > STARFLEX 193, LOW PRESSURE HOSE, LP MIL-H-50555 WAS USED TO CONNECT OIL COOLER TO FIREWALL FITTING. OIL PRESSURE WILL RUN BETWEEN 50-100 PSI IN LINE. HOSE BROKE AT FITTING AT OIL COOLER OUTLET, ALL OIL WAS PUMPED OUT OF ENGINE CAUSING ROD TO BE RAMMED THROU
- [SDR 2006FA0001207](https://openairdocs.org/sdr/2006FA0001207.md): Case · damaged · Nov 22, 2006 · N205DB · Beech V35 · Engine (Reciprocating)
  > ENGINE LT CASE, MALT DEVELOPED HOLE APPROX 6 INCHES X 4 INCHES AS ROD-PISTON APPEARS TO BE MISSING FOR NR 4 CYLINDER. ENGINE OPERATED: (104 HOURS - 2004), (14 HOURS - 2005), (12 HOURS - 2006). PROPELLER RECENTLY SHIMMED BLADE NR 3, RED DYE AROUND PROP SEAL.
- [SDR H8A2004F00000](https://openairdocs.org/sdr/H8A2004F00000.md): Motor · inoperative · May 21, 2004 · N2082W · Beech V35 · Landing Gear Actuator
  > PILOT REPORTED, COULD NOT LOWER GEAR ELECTRICALLY, PILOT PERFORMED EMERGENCY EXTENSION SUCESSIVELY. UPON INSPECTION OF LANDING GEAR FOUND MOTOR INOPERATIVE. BRUSHES WERE COMPLETELY WORN OUT, REPLACED MOTOR.
- [SDR 2003FA0000305](https://openairdocs.org/sdr/2003FA0000305.md): Pump · sheared · Mar 19, 2003 · N9486S · Beech V35 · Fuel Boost Pump
  > ENGINE QUIT DURING TAKEOFF. THE AIRCRAFT WAS SUBSTANTIALLY DAMAGED. INVESTIGATION REVEALED A SHEARED DRIVE SHAFT FOR THE ENGINE DRIVEN FUEL PUMP (INJECTOR PUMP). DISASSEMBLY REVEALED FOD (A SMALL PIECE OF WIRE) JAMMED IN THE ROTOR/VANE. FURTHER INVESTIGATIO
- [SDR 2002FA0001005](https://openairdocs.org/sdr/2002FA0001005.md): Bearing · failed · Aug 13, 2002 · N119RB · Beech V35 · AC Generator-Alternator
  > BEARING FAILURE IN ALTERNATOR CAUSED FAILURE OF CLUTCH ASSEMBLY.
- [SDR 2002FA0000328](https://openairdocs.org/sdr/2002FA0000328.md): Pump · failed · Mar 7, 2002 · Beech V35 · Fuel Boost Pump
  > FUEL PUMP WOULD NOT PRODUCE FUEL FLOW OR PRESSURE. ENGINE WOULD NOT IDLE BELOW 1000 RPM AND WOULD NOT PRODUCE POWER.
- [SDR 20000531SH018](https://openairdocs.org/sdr/20000531SH018.md): Nut · failed · May 11, 2000 · Beech V35 · Propeller Assembly
  > PENETRANT TESTING INDICATION IN O-RING AREA. (X)
- [SDR 20000531SH017](https://openairdocs.org/sdr/20000531SH017.md): Hub · cracked · May 11, 2000 · Beech V35 · Propeller Hub Section
  > EDDY CURRENT AND PENETRANT TESTING INDICATION IN THREAD AREA. (X)
- [SDR AU000328](https://openairdocs.org/sdr/AU000328.md): Filter · contaminated · May 4, 2000 · Beech V35 · Aircraft Fuel Filter/Strainer
  > (AUS) AIRFRAME FUEL FILTER CONTAMINATED BY AN UNKNOWN WHITE SUBSTANCE.
- [SDR 99ZZZX1933](https://openairdocs.org/sdr/99ZZZX1933.md): Control Cable · misinstalled · Apr 10, 1999 · N6264V · Beech V35 · Elevator Tab Control System
  > FOUND LEFT ELEVATOR TRIM TAB CONTROL CABLE IMPROPERLY INSTALLED. SUBMITTER STATED CABLE ENDS ARE NOT IDENTIFIED AND CAN BE EASILY INSTALLED IN WRONG POSITION CAUSING CABLE CHAFING AND INCORRECT TAB MOVEMENT.
- [SDR AU980488](https://openairdocs.org/sdr/AU980488.md): Crankcase · cracked · Mar 1, 1998 · Beech V35 · Reciprocating Engine Power Section
  > (AUS) AT ENGINE BULK STRIP, FOLLOWING THE SEPARATION OF NR 2 CYLINDER HEAD (REFER MDR 98/0488), A 127 MM (5 INCH) LONG CRACK WAS FOUND IN THE CRANKCASE RUNNING FROM THE MATING FACE BACKBONE FLANGE DOWN TO THE NR 2 CYLINDER PAD. THE CRACK WAS OBSCURED BY THE L
- [SDR AU980487](https://openairdocs.org/sdr/AU980487.md): Cylinder Head · separated · Mar 1, 1998 · Beech V35 · Reciprocating Engine Cylinder Section
  > (AUS) NR 2 CYLINDER HEAD SEPARATED FROM THE CYLINDER BARREL.
- [SDR 97ZZZX1930](https://openairdocs.org/sdr/97ZZZX1930.md): Uplock Cable · frayed · Apr 5, 1997 · N7586L · Beech V35 · Landing Gear Retraction/Extension System
  > DURING INSTALLATION OF OXYGEN SYSTEM, OBSERVED INBD END OF LEFT LANDING GEAR UPLOCK CABLE SEVERELY FRAYED AT THE TERMINAL END WHERE IT EXITS THE HOUSING: SUBMITTER SUSPECTS OLD AGE AND LACK OF LUBRICATION. SUBMITTER RECOMMENDS FREQUENT INSPECTION OF BOTH MLG
- [SDR 96ZZZX5952](https://openairdocs.org/sdr/96ZZZX5952.md): Rib · cracked · Nov 15, 1996 · N6238V · Beech V35 · Trailing Edge Flaps
  > DURING RE-SKIN OF HAIL DAMAGED FLAP, FOUND NOSE RIB AT ACTUATOR ATTACH POINT CRACKED. CRACK IS IN WEB OF RIB AT THE RELIEF OF THE CAP FORMATION, LOWER FORWARD. SUBMITTER STATED THIS IS NOT AN UNCOMMON FIND. THIS CAN ONLY BE DETECTED IF THE SKIN IS REMOVED.
- [SDR EY2R9600115](https://openairdocs.org/sdr/EY2R9600115.md): Hub · cracked · Oct 1, 1996 · Beech V35 · Propeller Hub Section
  > HUB CRACKED IN THREAD AREA
- [SDR 96ZZZX3767](https://openairdocs.org/sdr/96ZZZX3767.md): Fuel Selector · o-ring defective · Jul 10, 1996 · N2011W · Beech V35 · Fuel Selector/Shut-Off Valve
  > FUEL SELECTOR O-RING FOR THE RIGHT TANK FEED WAS RAISED BETWEEN THE SELECTOR BODY AND PLATE ALLOWING CONTINUOUS FEED OF FUEL FROM THE RIGHT TANK. THE FUEL SELECTOR WAS NOT DETERMINED TO BE A FACTOR IN THIS ACCIDENT.
- [SDR EY2R9600089](https://openairdocs.org/sdr/EY2R9600089.md): Hub · cracked · Jul 1, 1996 · Beech V35 · Propeller Hub Section
  > HUB CRACKED IN THREAD AREA
- [SDR EY2R9600839](https://openairdocs.org/sdr/EY2R9600839.md): Hub · corroded · Jun 1, 1996 · Beech V35 · Propeller Hub Section
  > HUB FOUND CORRODED.
- [SDR EY2R9600045](https://openairdocs.org/sdr/EY2R9600045.md): Hub · cracked · Apr 1, 1996 · Beech V35 · Propeller Hub Section
  > INSP FOUND HUB CRACKED
- [SDR 96ZZZX2380](https://openairdocs.org/sdr/96ZZZX2380.md): Blade · cracked · Mar 21, 1996 · N999ER · Beech V35 · Propeller Blade Section
  > BLADE DYE CHECKED IAW AD 68-13-02. NO CRACKS INDICATED. CHECKED OK. FOUND ONE INCH LONG CRACK IN BLADE, USING EDDY CURRENT, APPROXIMATELY.040 INCH DEEP. SUBMITTER SUGGESTED MAKING EDDY CURRENT INSPECTION MANDATORY.
- [SDR EY2R9600031](https://openairdocs.org/sdr/EY2R9600031.md): Hub · cracked · Mar 1, 1996 · Beech V35 · Propeller Hub Section
  > HUB CRACKED IN THREAD AREA
- [SDR AU960481](https://openairdocs.org/sdr/AU960481.md): Spar Cap · corroded · Feb 12, 1996 · Beech V35 · Wing Spar
  > (AUS) RH WING LOWER SPAR CAP CORRODED
- [SDR EY2R9601367](https://openairdocs.org/sdr/EY2R9601367.md): Hub · mis drilled · Jan 1, 1996 · Beech V35 · Propeller Hub Section
  > PROP ASSY HUB DRILLED PAST.152
- [SDR EY2R9600209](https://openairdocs.org/sdr/EY2R9600209.md): Hub · corroded · Jan 1, 1996 · Beech V35 · Propeller Hub Section
  > PROP HUB ASSY IS CORRODED
- [SDR 95ZZZX6158](https://openairdocs.org/sdr/95ZZZX6158.md): Hub · corroded · Oct 24, 1995 · N5915S · Beech V35 · Propeller Hub Section
  > PROPELLER WAS LAST OVERHAULED 7-21-91. WAS SENT IN FOR OVERHAUL. AFTER TEAR DOWN AND CLEANING, FOUND TO HAVE EXCESSIVE CORROSION ON THE HUB PILOT TUBES AND AROUND THE HUB SPIDER ARMS INBOARD OF THE BEARINGS SEAT. CORROSION ON THE SPIDER ARMS COULD RESULT IN
- [SDR 95ZZZX6017](https://openairdocs.org/sdr/95ZZZX6017.md): Air Filter · defective · Oct 13, 1995 · N5421U · Beech V35 · Engine Air Intake System
  > AD95-03-02 SHOULD INCLUDE THIS BRACKETT, BA7210, AS WE FOUND THE GASKET MOVED FROM PROPER POSITION.
- [SDR 95ZZZX2435](https://openairdocs.org/sdr/95ZZZX2435.md): Piston · failed · Jan 30, 1995 · N9516Q · Beech V35 · Reciprocating Engine Cylinder Section
  > PISTON SKIRT FAILED AT LOWER RING LAND ON THRUST SIDE. DEBRIS EXTENSIVELY DAMAGED CRANKCASE, CRANKSHAFT, CAMSHAFT, RODS, ADJACENT PISTONS AND CYLINDERS. ALSO, THE ENTIRE OIL SYSTEM WAS CONTAMINATED.

## 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 = 'V35'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/beech-v35/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.