Beech 95

Service difficulty reports · 17

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 2023FA0000816Rod End · severedFORWARD RUDDER TRIM TAB CONTROL ROD END BROKE. UN CONTROLLED RUDDER TAB CAUSED SEVERE OSCILLATIONS RESULTING IN WINDSHIELD SEPARATED FROM THE AIRCRAFT.Nov 17, 2023 · N2024C · Beech 95 · Rudder Tab Control SystemSDR 2021FA0000346None · noneDURING 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 REMAININGNov 28, 2021 · N677Q · Beech 95 · Landing Gear Retraction/Extension SystemSDR 2012FA0000500Rod End · separatedTHE ROD END, PN HMXL6FG, CONNECTED TO GEAR RETRACT ROD, SEPARATED AT THAT CONNECTION CAUSING THE NOSE GEAR TO COLLAPSE DURING THE LANDING ROLL OUT.Jul 3, 2012 · N275EC · Beech 95 · Nose/Tail Landing GearSDR 2010FA0000296Line · splitDURING 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.Apr 7, 2010 · N59LS · Beech 95 · Reciprocating Engine Oil SystemSDR CA061117004Cylinder Head · cracked(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)Nov 4, 2006 · Beech 95 · Reciprocating Engine Cylinder SectionSDR 2005FA0000089Armature · failedTHE 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 Dec 2, 2004 · N21JC · Beech 95 · AC Generator-AlternatorSDR CA030506006Wire · failed(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 CRACKMar 14, 2003 · Beech 95 · Flight Control System WiringSDR 2001F00165Arm · crackedDURING 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 CRAJun 27, 2001 · Beech 95 · Nose/Tail Landing Gear Strut/AxleSDR 2001FA0000067Arm · crackedUPON 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.May 3, 2001 · N2765Y · Beech 95 · Nose/Tail Landing Gear Strut/AxleSDR 2000ZZZX379Spring · brokenLOW 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 TJan 11, 2000 · N2051C · Beech 95 · Propeller Controlling SystemSDR AU990914Nut · cracked(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.Sep 2, 1999 · Beech 95 · Propeller AssemblySDR 99ZZZX1886Sector Gear · failedDURING 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 SWIApr 10, 1999 · N21JC · Beech 95 · Landing Gear ActuatorSDR 98ZZZX2116Skin · chafedDURING 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 BMay 13, 1998 · N21JC · Beech 95 · Wing, Plate/SkinSDR 98ZZZX2115Skin · chafedDURING 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 BMay 13, 1998 · N21JC · Beech 95 · Wing, Plate/SkinSDR 96ZZZX1965Mount · crackedMAIN 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.Mar 18, 1996 · Beech 95 · Engine Mount SectionSDR CA960509202Ribs · bent(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 ).Mar 8, 1996 · Beech 95 · Wing, Rib/BulkheadSDR 95ZZZX3325Screw · brokenDURING 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 OFJun 1, 1995 · Beech 95 · Propeller Blade Section
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