# Service difficulty reports: Beech 95

A list on [Beech 95](https://openairdocs.org/model/beech-95.md).

Newest first. General aviation reporting is voluntary.

- [SDR 2023FA0000816](https://openairdocs.org/sdr/2023FA0000816.md): Rod End · severed · Nov 17, 2023 · N2024C · Beech 95 · Rudder Tab Control System
  > FORWARD RUDDER TRIM TAB CONTROL ROD END BROKE. UN CONTROLLED RUDDER TAB CAUSED SEVERE OSCILLATIONS RESULTING IN WINDSHIELD SEPARATED FROM THE AIRCRAFT.
- [SDR 2021FA0000346](https://openairdocs.org/sdr/2021FA0000346.md): None · none · Nov 28, 2021 · N677Q · Beech 95 · Landing Gear Retraction/Extension System
  > DURING LANDING TOUCHDOWN RUSSELLVILLE, AR (RUE) THE NOSE LANDING GEAR COLLAPSED. INVESTIGATION REVEALED THE NOSE GEAR RETRACT DRAG BRACE P/N 002-820017-1 AT THE ATTACHMENT POINT FOR THE EXTENSION/RETRACTION PUSH PULL TUBE HAD BROKEN WITH THE ROD END REMAINING
- [SDR 2012FA0000500](https://openairdocs.org/sdr/2012FA0000500.md): Rod End · separated · Jul 3, 2012 · N275EC · Beech 95 · Nose/Tail Landing Gear
  > THE ROD END, PN HMXL6FG, CONNECTED TO GEAR RETRACT ROD, SEPARATED AT THAT CONNECTION CAUSING THE NOSE GEAR TO COLLAPSE DURING THE LANDING ROLL OUT.
- [SDR 2010FA0000296](https://openairdocs.org/sdr/2010FA0000296.md): Line · split · Apr 7, 2010 · N59LS · Beech 95 · Reciprocating Engine Oil System
  > DURING FLIGHT, SHUTDOWN THE RT ENGINE DUE TO OIL LOSS. AN INITIAL ASSESSMENT OF THE CAUSE WAS DUE TO THE ONE OF THE OIL LINE FROM THE OIL COOLER APPEARED TO SPLIT WHERE IT WAS ROUTED TO CLOSE TO AN EXHAUST MANIFOLD.
- [SDR CA061117004](https://openairdocs.org/sdr/CA061117004.md): Cylinder Head · cracked · Nov 4, 2006 · Beech 95 · Reciprocating Engine Cylinder Section
  > (CAN) DURING A ROUTINE 100 HOUR INSPECTION A CRACK WAS FOUND ON THE RH ENGINE #4 CYLINDER STARTING AT THE TOP SPARK PLUG HOLE AND CONTINUING DOWN TO THE EXHAUST PORT. THE CYLINDER WAS REMOVED AND REPLACED. (TC# 20061117004)
- [SDR 2005FA0000089](https://openairdocs.org/sdr/2005FA0000089.md): Armature · failed · Dec 2, 2004 · N21JC · Beech 95 · AC Generator-Alternator
  > THE GENERATOR WAS JUST O/H, WITHOUT DISASSEMBLING THE GENERATOR, LOOKING IN TO PULLEY SIDE, YOU COULD SEE THAT THE ARMATURE HAD PARTIALLY UNWOUND. TO THE POINT WHERE ONE ARMATURE WIRE WAS RUBBING LARGE AMOUNTS OF FIELD COVERING OFF. THIS CAUSED THE ARMATURE
- [SDR CA030506006](https://openairdocs.org/sdr/CA030506006.md): Wire · failed · Mar 14, 2003 · Beech 95 · Flight Control System Wiring
  > (CAN) THE AME INSTALLED THE COMPONENT (OVERHAULED JAN/02) DURING 2002-2003 WINTER MAINTENANCE. A FUNCTION CHECK OF THE UNIT REVEALED INTERMITTENT INDICATIONS. REMOVAL OF THE UNIT REVEALED THAT THERE WAS A BROKEN WIRE INTERNALLY. A PREVIOUSLY UNDISCOVERED CRACK
- [SDR 2001F00165](https://openairdocs.org/sdr/2001F00165.md): Arm · cracked · Jun 27, 2001 · Beech 95 · Nose/Tail Landing Gear Strut/Axle
  > DURING A RECENT INVESTIGATION OF AN INCIDENT OF A BEECH 95 THAT THE NOSE GEAR COLLAPSED ON ROLL OUT AFTER LANDING. IT WAS DISCOVERED THAT THE LANDING GEAR CRANK ARM PART NUMBER 35-825174 THAT ATTACHES TO THE LANDING GEAR TRANSMISSION BOX HAD CRACKED. THE CRA
- [SDR 2001FA0000067](https://openairdocs.org/sdr/2001FA0000067.md): Arm · cracked · May 3, 2001 · N2765Y · Beech 95 · Nose/Tail Landing Gear Strut/Axle
  > UPON LANDING ROLL-OUT THE NOSE GEAR COLLAPSED. THE CRACK ON THE SPLINE PORTION OF ARM CAUSED THE ARM TO FLEX AND OPEN CAUSING MATING GEARS TO SEPARATE AND THE NOSE GEAR TO COLLAPSE. PROBABLE CAUSE IS FATIGUE. REOCCURRING INSPECTIONS ARE RECOMMENDED.
- [SDR 2000ZZZX379](https://openairdocs.org/sdr/2000ZZZX379.md): Spring · broken · Jan 11, 2000 · N2051C · Beech 95 · Propeller Controlling System
  > LOW OIL PRESSURE DURING FLIGHT CAUSING PROPELLER TO GO TO LOW PITCH AND EVENTUALLY FEATHER. AIRCRAFT LANDED SAFELY AND AFTER TROUBLESHOOTING PROBLEM, FOUND BROKEN SPRING IN OIL PRESSURE RELIEF VALVE. INSTALLED NEW SPRING, ADJUSTED OIL PRESSURE AND RETURNED T
- [SDR AU990914](https://openairdocs.org/sdr/AU990914.md): Nut · cracked · Sep 2, 1999 · Beech 95 · Propeller Assembly
  > (AUS) PROPELLER RETENTION NUT CRACKED. EVIDENCE OF CRACK HIGHLIGHTED BY MARKER PEN. SUBMITTER SUSPECTED CRACK HAD BEEN FOUND PREVIOUSLY AND THE UNSERVICEABLE NUT HAD BEEN REUSED.
- [SDR 99ZZZX1886](https://openairdocs.org/sdr/99ZZZX1886.md): Sector Gear · failed · Apr 10, 1999 · N21JC · Beech 95 · Landing Gear Actuator
  > DURING ANNUAL INSPECTION GEAR OPERATION, ADJUSTED DOORS TO FIT TIGHTER, AND ACTUATOR SECTOR SHEARED TEETH. ACCORDING TO BEECH SHOP MANUAL AND OWNER'S MANUAL, IF GEAR ACTUATOR MOTOR FAILS TO SHUT OFF AFTER GEAR UP OR DOWN POSITIONS, ADJUST OR REPLACE LIMIT SWI
- [SDR 98ZZZX2116](https://openairdocs.org/sdr/98ZZZX2116.md): Skin · chafed · May 13, 1998 · N21JC · Beech 95 · Wing, Plate/Skin
  > DURING ANNUAL PREPARATIONS, FOUND BEHIND BOTH ENGINES THAT LOWER AFT NACELLES WERE CHAFING THROUGH WING SKIN JUST AFT OF FRONT SPAR FLANGE AND LEFT UNTREATED WOULD CHAFE INTO SPAR FLANGE. AIRCRAFT HAS 6,500 HOURS TTAF. NO LORD MOUNT DAMAGE, BUT SHOULD HAVE B
- [SDR 98ZZZX2115](https://openairdocs.org/sdr/98ZZZX2115.md): Skin · chafed · May 13, 1998 · N21JC · Beech 95 · Wing, Plate/Skin
  > DURING ANNUAL PREPARATIONS, FOUND BEHIND BOTH ENGINES THAT LOWER AFT NACELLES WERE CHAFING THROUGH WING SKIN JUST AFT OF FRONT SPAR FLANGE AND LEFT UNTREATED WOULD CHAFE INTO SPAR FLANGE. AIRCRAFT HAS 6,500 HOURS TTAF. NO LORD MOUNT DAMAGE, BUT SHOULD HAVE B
- [SDR 96ZZZX1965](https://openairdocs.org/sdr/96ZZZX1965.md): Mount · cracked · Mar 18, 1996 · Beech 95 · Engine Mount Section
  > MAIN DYNA FOCAL ATTACH RING TUBE AT TIME OF INSPECTION WAS FOUND TO HAVE CRACKS AT TOP RT ATTACH POINT AND AFT OF ATTACH PLATE APPROXIMATELY.75 INCH AND.50 INCH LONG. THIS MOUNT WAS TAGGED UNSERVICEABLE, RED TAG. REPLACEMENT OF UNIT WAS SUGGESTED.
- [SDR CA960509202](https://openairdocs.org/sdr/CA960509202.md): Ribs · bent · Mar 8, 1996 · Beech 95 · Wing, Rib/Bulkhead
  > (CAN) RIGHT WING RIBS AT W.S. 94.864, 108.281 AND 122.500 FOUND BENT AND BUCKLED UNDER THE UPPER WING SKIN. POSSIBLY CAUSED BY OVERPRESSURE OF FUEL IN AUXILIARY TANK (THERMAL EXPANSION).
- [SDR 95ZZZX3325](https://openairdocs.org/sdr/95ZZZX3325.md): Screw · broken · Jun 1, 1995 · Beech 95 · Propeller Blade Section
  > DURING DISASEMBLY, INNER CLAMP SCREW FOUND BROKEN OFF ON THE SHANK AT TOP THREAD, ENTERING CLAMP. SURFACE OF BREAK APPEARED CLEAN WITH A SMALL PIT ORIGINATING IN THE MIDDLE OF THE THREAD AREA. SUSPECT PIT WAS CAUSED BY MOISTURE CREEPING AROUND SOCKET HEAD OF

## 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 = '95'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/beech-95/reports

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