Cessna T210M

Service difficulty reports · 110

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 = 'T210M'
  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 96ZZZX705Cylinder · failedTHE NORMAL LIFE OF THIS CYLINDER IS AT 1,500 HOURS TCO. THIS ONE LASTED 1,043 HOURS. THIS PREMATURE WEAR FAILURE SEEMS TO BE AN UNFORTUNATE TREND FOR CERMICHROME CYLINDERS. SUBMITTER RECOMMENDS NORMAL OPERATIONS WATCHING ENGINE PARAMETERS AND FREQUENT OIL CJan 23, 1996 · N7398M · Cessna T210M · Reciprocating Engine Cylinder SectionSDR 96ZZZX707Bracket · bentDURING CERTAIN LOADING CONDITIONS, THE T210 CAN PRODUCE A NOSE WHEEL SHIMMEY THAT ALLOWS THIS BRACKET TO BEND OUT OF POSITION. SUBMITTER RECOMMENDS A PRE-FLIGHT INSPECTION FOR PROPER ENGAGEMENT OF SWITCH.Jan 1, 1996 · N6611C · Cessna T210M · Landing Gear Retraction/Extension SystemSDR 96ZZZX258Gauges · errorsFUEL GAUGES HAVE INACCURATE READINGS CAUSING MISFUELING OF AIRCRAFT AND FUEL STARVATION. SUBMITTER RECOMMENDS GAUGES BE CHECKED FOR ACCURACY AT INSPECTIONS. IF INACCURATE GAUGES ARE PRESENT, REPLACE THEM WITH REBUILT UNITS OR THE NEW KIT OFFERED BY CESSNA.Nov 16, 1995 · N6508B · Cessna T210M · Fuel Quantity IndicatorSDR 95ZZZX6548Piston · failedLOST OIL PRESSURE AND MADE FORCE LANDING, NO DAMAGE TO AIRCRAFT, PILOT OR PASSENGERS. FOUND PISTON FAILED.Nov 13, 1995 · N6591M · Cessna T210M · Reciprocating Engine Cylinder SectionSDR 95ZZZX6547Magneto · coil failedMAG FAILURE TRACED TO BAD COIL.Nov 13, 1995 · N6591M · Cessna T210M · Magneto/DistributorSDR 95ZZZX5232Hose · failedNOSE GEAR DOOR OPEN HOSE PARTED FROM FITTING AFTER GEAR DOWN MODE WAS SELECTED. MAIN LANDING GEAR WOULD NOT LOCK DOWN. HYDRAULIC HOSE AS LISTED LOST ALL HYDRAULIC FLUID SO THE MAIN GEAR WOULD NOT HAVE PRESSURE TO LOCK INTO DOWN POSITION. EMERGENCY LANDING WSep 15, 1995 · N6597B · Cessna T210M · Landing Gear Door Retract SectionSDR 95ZZZX5706Hub · excess corrosionINSPECTION FOUND PROPELLER SLOW TO OPERATE. EXCESSIVE RUST, CORROSION, AND CONDENSATION FOUND INSIDE. OHC PROPELLER AT RECOMMENED TBO.Sep 7, 1995 · N761HS · Cessna T210M · Propeller Hub SectionSDR 95ZZZX5598Crankcase · crackedCRACK IN THE CRANKCASE ON THE FORWARD LOWER PORTION OF NR 5 CYLINDER, RUNNING THROUGH THE LOWER FORWARD CYLINDER MOUNTING STUD.Aug 16, 1995 · N6994B · Cessna T210M · Reciprocating Engine Power SectionSDR 95ZZZX3813Line · crackedHYDRAULIC FLUID WAS PUMPED OVERBOARD WHEN THE GEAR DOOR CLOSE LINE CRACKED JUST BELOW THE TUBING FLARE WHERE IT COMES OUT OF THE HYDRAULIC PUMP.Jun 28, 1995 · N732MZ · Cessna T210M · Hydraulic System, MainSDR 95ZZZX3228Uplock Switch · defectiveAFTER TAKEOFF AND GEAR UP SELECTED, NO 'UP' LIGHT AND THE POWER PACK CONTINUED TO RUN. CREW SELECTED GEAR DOWN WITH NO PROBLEMS. MAINTENANCE PERSONNEL INSPECTED AND FOUND THE LT MLG UPLOCK SWITCH MOUNTING JAM NUT HAD BACKED OFF LOOSENING THE SWITCH CAUSING TJun 2, 1995 · N7072 · Cessna T210M · Landing Gear Position and Warning
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