Beech E95

Service difficulty reports · 17

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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 = 'E95'
  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 CA110416001Landing Gear · deteriorated(CAN) THE SWITCH KEY WAY IS SUCH THAT THE CENTER TERMINAL IS VERY CLOSE TO STRUCTURE. THE INSULATING TAPE THAT WAS INSTALLED DETERIORATED ALLOWING THE SCREW HEAD TO CONTACT STRUCTURE AND SHORT OUT THE LANDING GEAR RELAY C/B.Apr 14, 2011 · Beech E95 · Main Landing GearSDR CA090918005Cylinder · cracked(CAN) DURING THE CRUISE PORTION OF FLIGHT, THE RT ENG BEGAN RUNNING VERY ROUGH. CREW REDUCED POWER SETTING ON RT ENGINE AND CONTINUED ON TO DESTINATION. UPON ARRIVAL, AN INSP REVEALED A CRACKED CYL AND LEAKING OIL ON INSIDE OF THE COWLING. MX REPLACED THE CYSep 10, 2009 · Beech E95 · Reciprocating Engine Cylinder SectionSDR CA070322011Window · broken(CAN) IN CRUISE FLIGHT, AT 6000 FT, THE MAJORITY OF THE LT SIDE COCKPIT WINDOW DEPARTED THE AC. THE AC BEING CLOSE TO ITS INTENDED DESTINATION CONTINUED ON AND LANDED WITHOUT INCIDENT. A FLIGHT PERMIT WAS ISSUED AND THE AIRCRAFT FLOWN TO MAIN BASE FOR EVALUATIMar 22, 2007 · Beech E95 · Flight Compartment WindowsSDR CA061025007Control Cable · defective(CAN) AFTER A ROUTINE TRAINING FLIGHT THE PILOT REPORTED THAT THE RT PROP CONTROL WAS VERY STIFF AND SPRINGY AND THE PROP WAS SLOW TO FEATHER. THE CONTROL WAS DISCONNECTED FROM THE GOVERNOR AND THE DEFECT WAS CONFIRMED TO BE THE CONTROL CABLE. THE TTSN FOR THESep 30, 2006 · Beech E95 · Propeller Feathering/ReversingSDR CA061025006Spar · cracked(CAN) DUING INSPECTION IAW FAA AD 90-08-14 AND SB53-2269 REV 2 SHORT CRACKS WERE VISUALLY FOUND EMINATING FROM 2 HUCK BOLT LOCATIONS ON THE LT FORWARD WING SPAR CARRY THROUGH WEB FACE. CRACKS WERE CONFIRMED BY LPI. REPAIRED IAW MFG FAA APPROVED DRAWING 58-4000May 2, 2006 · Beech E95 · Wing SparSDR CA990311002Switch · failed(CAN) AFTER LEFT ENGINE WAS STARTED AND DURING THE MAG DROP TEST, ELECTRICAL SMELL WAS DETECTED AND ARCING COULD BE HEARD. THE MAGNETO SWITCH WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. A SUBSEQUENT INSPECTION OF A MAGNETO SWITCH REVEALED THAT IT WAS Dec 8, 1998 · Beech E95 · Ignition SwitchingSDR CA980602058Motor · failed(CAN) LANDING GEAR FAILED TO EXTEND USING THE NORMAL ELECTRICAL EXTENSION SYSTEM. THE LANDING GEAR WAS EXTENDED MANUALLY AND AIRCRAFT LANDED WITHOUT INCIDENT AFTER CONFIRMATION GEAR DOWN AND LOCKED. SUBSEQUENT INVESTIGATION REVEALED THE LANDING GEAR ELECTRICApr 17, 1998 · Beech E95 · Landing Gear Retraction/Extension SystemSDR CA980311005Motor · failed(CAN) LANDING GEAR FAILED TO COMPLETELY RETRACT AFTER TAKEOFF. GEAR SELECTED DOWN AND NO MOVEMENT. GEAR RESELECTED UPN AND GEAR CIRCUIT BREAKER POPPED. FLY BY INDICATED GEAR DOWN. AIRCRAFT LANDED. GEAR RETRACT MOTOR REPLACED. ARMATURE BADLY ERODED, BRUSHES SHOMar 1, 1998 · Beech E95 · Main Landing Gear Attach SectionSDR CA970904034Stud · sheared(CAN) ON DAILY INSPECTION THE UPPER FORWARD CYLINDER BASE STUD ON THE NR2 CYLINDER WAS FOUND SHEARED OFF. THE STUD WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Sep 1, 1997 · Beech E95 · Reciprocating Engine Power SectionSDR CA960909026Bracket · slipped(CAN) AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT, THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. A SUBSEQUENT INSPECTION REVEALED THAT THE LANDING GEAR SAFETY SWITCH HAD SLIPPED THUS NOT ACTUATING THE SWITCH WHEN THE GEAR WAS FULLY EXTENDED. THE SAFSep 4, 1996 · Beech E95 · Landing Gear Position and WarningSDR 96ZZZX4811Resistor · burnedA RESISTOR IN CABIN HEATER OVERHEAT WARNING SYSTEM FAILED AND BURNED CAUSING SMOKE IN THE CABINAug 30, 1996 · N729EM · Beech E95 · Heating SystemSDR CA960826044Crankcase · cracked(CAN) DURING A SCHEDULED INSPECTION A CRACK WAS FOUND ON THE RH ENGINE BETWEEN #2 AND #4 CYLINDERS, APPROXIMATELY 4" LONG PROPAGATING FROM THE #4 CYLINDER FLANGE. THE ENGINE WAS REPLACED.Jul 31, 1996 · Beech E95 · Reciprocating Engine Power SectionSDR CA960709003Bushing · oversized(CAN) RIGHT HAND MAIN LANDING GEAR BUSHING PURCHASED NEW FROM BEECHCRAFT FOUND TO BE OUTSIDE THE TOLERANCE OF THE MAINTENANCE MANUAL. THE BUSHING WAS RETURNED FOR A CREDIT.Jun 26, 1996 · Beech E95 · Main Landing Gear Strut/Axle/TruckSDR CA960515002Static Sensor · leak(CAN) PIEZO STATIC SENSOR HOUSING LEAKING IN EXCESS OF LIMITSMay 7, 1996 · Beech E95 · Pitot/Static SystemSDR CA960321012Alternator · shorted field(CAN)DURING CLIMB BOTH ALTERNATORS WENT OFF LINE. AN INSPECTION REVEALED THAT THE RIGHT HAND COOLING FAN HAD SEPARATED FROM THE ALTERNATOR AND SOME OF THE PIECES WERE FOUND INSIDE THE ALTERNATOR THUS SHORTING THE FIELD. THE SHORTED FIELD CAUSED A VOLTAGE REGULMar 20, 1996 · Beech E95 · DC Generator-AlternatorSDR CA960212015Vane · stuck(CAN)ON TAKEOFF THE LEFT HAND ENGINE WOULD NOT DEVELOP FULL POWER. INSPECTION REVEALED THE ALTERNATE AIR DOOR CABLE TO BE OUT OF RIG, CAUSING THE AFT VANE TO JAM IF THE CONTROL CABLE WAS PUSHED TOO FAR TOWARDS THE FILTER POSITION. THE ALTERNATE AIR CONTROL WASFeb 9, 1996 · Beech E95 · Engine Air Intake SystemSDR CA960212013Vane · frozen(CAN)DURING TAKEOFF ROLL A LEFT YAW WAS NOTICED AND ONCE AIRBORNE THE FUEL FLOW AND MANIFOLD PRESSURE ON THE LEFT ENGINE WAS NOTED TO BE LOW. THE ALTERNATE AIR CONTROL WAS NOTED IN THE HEAT POSITION. WHEN THE ALTERNATE AIR WAS RETURNED TO THE FILTER POSITION Feb 5, 1996 · Beech E95 · Engine Air Intake System
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