Beech C90A

Service difficulty reports · 461

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 = 'C90A'
  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 CA960214012Flux Valve · oil soaked(CAN)AIRCRAFT COMPASS SYSTEM REPORTED UNRELIABLE. EXAMINATION OF COMPASS COMPONENTS AND WIRING REVEALED THAT THE FLUX VALVE WAS SATURATED WITH INSTRUMENT OIL. COLLINS CONFIRMED THAT THE LOSS OF OIL COULD R ESULT IN FAILURE OF THE COMPONENT. FLUX VALVE WAS REPLFeb 8, 1996 · Beech C90A · Directional Gyro and Indicating SystemSDR 96ZZZX1251Bearing Cone · failedOUTER BEARING CONE (BEARING CLOSEST TO AXLE NUT) BROKE CAUSING THE ROLLER BEARINGS AND BEARING CAGE TO SEPARATE FROM THE BEARING CONE ASSY. THIS ALLOWED RT MAIN WHEEL TO WORK ITS WAY OFF AXLE AND SEPARATE FROM THE ACFT ON TAKEOFF. THE AXLE NUT, COTTER PIN, SDec 29, 1995 · N494JY · Beech C90A · Main Landing Gear Strut/Axle/TruckSDR 96ZZZX555Shaft · crackedFLAP ACTUATOR SHAFT WAS FOUND CRACKED THE ENTIRE LENGTH OF THE SHAFT. CAUSE OF CRACK IS UNKNOWN. THE FLAP MOTOR AND GEAR BOX ASSY WERE ALSO FOUND TO BE WORN AT THIS SAME TIME.Dec 20, 1995 · N8156Z · Beech C90A · Trailing Edge Flap ActuatorSDR CA960110006De-Ice Duct · cracked(CAN)EXHAUST STACK CRACKING WHERE COWL ANTI-ICE TUBE ATTACHES TO THE MAIN EXHAUST STACK.Dec 5, 1995 · Beech C90A · Engine Collector/Tailpipe/NozzleSDR 95ZZZX6025Balance Weight · screw looseDURING INSPECTION, ONE NAS 14411 SCREW WAS FOUND MISSING FROM THE RT ELEVATOR BALANCE WEIGHT WHICH SECURES THE BALANCE WEIGHT TO THE ELEVATOR. A TORQUE CHECK OF THE REMAINING THREE SCREWS FOUND ALL OF THEM LOOSE. IN ADDITION, THE ELEVATOR BALANCE WEIGHT SCRESep 18, 1995 · N476JA · Beech C90A · Elevator StructureSDR 95ZZZX4600Bolt · missingLEFT MAIN LANDING GEAR ASSEMBLY COLLAPSED ON LANDING. THE LOWER DRAG LINK TO STRUT ASSEMBLY BOLT WAS MISSING. IT IS NOT CLEAR WHY THE BOLT WAS MISSING. THE BOLT WAS PRESENT 9 HOURS AND 28 LANDINGS PRIOR.Aug 11, 1995 · N490JT · Beech C90A · Landing Gear Retraction/Extension SystemSDR 95ZZZX3585Wheel · crackedTHIS PART NUMBER WHEEL HALF CRACKED ON LEFT AND RIGHT MAIN WHEELS. THIS SAME PART NUMBER WHEEL HALF FOUND CRACKED ON ANOTHER AIRCRAFT LAST WEEK.Jul 6, 1995 · N1564P · Beech C90A · Wheel/Ski/FloatSDR 95ZZZX3143Bearing · missing needlesDURING THE FLAP DRIVE INSPECTION AND LUBRICATION EVENT, FOUND THAT THE NEEDLE BEARINGS WERE MISSING FROM THE BEARING HOUSING AT THE WORN GEAR UPPER BEARING. ONLY THE BEARING SHELL WAS INSTALLED. THERE WAS NO EVIDENCE IN THE GEARBOX OF THE MISSING NEEDLE BEAMay 31, 1995 · N484JA · Beech C90A · Trailing Edge Flap ActuatorSDR 95ZZZX2955Exhaust Stack · brokeRIGHT ENGINE, LEFT EXHAUST STACK, ELBOW FOR HEATED LIP BROKE OFF. SECOND TIME IN 150 HOURS. PROPELLER PREVIOUSLY BALANCED BEFORE PROBLEMS STARTED. MINOR DAMAGE TO COWLING.May 31, 1995 · N415P · Beech C90A · Engine Collector/Tailpipe/NozzleSDR 95ZZZX3193Indicator · case brokenUPON INSTALLATION IN THE ACFT - BACK OF THE UNIT CAME OFF IN THE TECHNICIAN'S HANDS. FURTHER INVESTIGATION FOUND THAT BLACK ELECTRICAL TAPE WAS COVERING BROKEN OUT INSTRUMENT CASE MOUNTING HOLES FOR THE REAR PLATE. THE ONLY THING HOLDING THE INSTRUMENT TOGETMay 30, 1995 · N477JA · Beech C90A · Turn and Bank/Rate of Turn IndicatorSDR 95ZZZX1868Side Brace · corrodedDURING PRIMARY INSPECTION, THE RIGHT MAIN GEAR SIDE BRACE WAS FOUND CORRODED. WHAT APPEARED TO BE A BLACK SPOT .0625 INCH IN DIAMETER, AFTER PROBING, BECAME .25 INCH HOLE. THE CORROSION HAD STARTED INTERNALLY AND HAD EATEN THROUGH. THE CORROSION WAS ON THE Feb 24, 1995 · N1552G · Beech C90A · Main Landing Gear
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