Cessna A188B

Service difficulty reports · 57

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 = 'A188B'
  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 CA960328010Camshaft · spalled(CAN) DURING INSPECTION AND UPON DISMANTLING, #5 AND #1 EXHAUST LOBE, AND #3 AND #4 INTAKE LOBES ON CAMSHAFT WERE SPALLED. THE LIFTERS CONTACTING THE SPALLED LOBES WERE ALSO SPALLED. #2 EXHAUST LIFTER, #4 EXHAUST LIFTER AND #6 INTAKE LIFTER WERE CORROSIVELY PIFeb 28, 1996 · Cessna A188B · Reciprocating Engine Power SectionSDR CA960328009Camshaft · spalled(CAN) DURING INSPECTION AND UPON DISMANTLING, #3 & #4 INTAKE LOBES, #5 EXHAUST LOBE, AND #5 & #6 INTAKE LOBES ON CAMSHAFT WERE SPALLED. TWO LOBES WERE SPALLED OVER ENTIRE FACE AND TWO WERE SPALLED ONLY IN THE CENTRE. TWO LIFTERS WERE CORRODED BADLY. ALL MAIN BFeb 28, 1996 · Cessna A188B · Reciprocating Engine Power SectionSDR 96ZZZX2160Cylinder · separatedCYLINDER HEAD SEPARATED FROM BARREL ON TAKEOFF CAUSING CONSIDERABLE DAMAGE TO AIRCRAFT, NO INJURIES. DURING REPAIR OF ACFT AND ANNUAL INSP, FOUND ENGINE BAFFLE SEAL MATERIAL EXTREMELY DETERIORATED AND IN A DEFECTIVE CONDITION AND CHT PROBE IN WRONG CYLINDER PAug 19, 1995 · N731VX · Cessna A188B · Reciprocating Engine Cylinder SectionSDR 95ZZZX3261Muffler · shroud failedSHROUD MISSING FROM EXHAUST SYSTEM MUFFLER WHICH CAUSED MUFFLER TO HEAT UP ENOUGH TO BURN A HOLE IN IT. BURNED UP INTAKE AIR FILTER WHICH WAS INDUCED INTO ENGINE CAUSING ENGINE FAILURE.Jun 13, 1995 · N4916Q · Cessna A188B · Engine Noise SuppressorSDR 96ZZZX5266Bolt · crackedDURING ATTEMPT TO REMOVE CYLINDERS FROM ENGINE CASE, FOUND HOLD DOWN NUTS HAD BEEN OVERTORQUED AND HAD TO BE DRILLED TO BE REMOVED. FOUND MAIN JOURNAL WEB CRACKS IN CYLINDERS NR 4 AND NR 6. SUBMITTER BELIEVES HOLD DOWN NUTS OVERTORQUE TO BE A FACTOR IN CASE May 5, 1995 · N8999G · Cessna A188B · Reciprocating Engine Power SectionSDR 96ZZZX5265Bolt · crackedDURING ATTEMPT TO REMOVE CYLINDERS FROM ENGINE CASE, FOUND HOLD DOWN NUTS HAD BEEN OVERTORQUED AND HAD TO BE DRILLED TO BE REMOVED. FOUND MAIN JOURNAL WEB CRACKS IN CYLINDERS NR 4 AND NR 6. SUBMITTER BELIEVES HOLD DOWN NUTS OVERTORQUE TO BE A FACTOR IN CASE May 5, 1995 · N8999G · Cessna A188B · Reciprocating Engine Power SectionSDR 95ZZZX3328Adjusting Nut · missingINJECTOR ARRIVED WITH NO FUEL FLOW. UPON PUTTING IT ON FLOW BENCH USING NORMAL FLOW PROCEDURES, WAS UNABLE TO GET FUEL FLOW. REMOVED HEX BRASS NUT FROM REGULATOR. THE RETAINING AND FLOW ADJUSTING NUT WAS MISSING. RECOMMEND ALL FLOW BENCH OPERATORS SHOULD BApr 6, 1995 · N4854R · Cessna A188B · Fuel Control/Reciprocating Engines
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