Cessna 210E

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 = '210E'
  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 4S42020F00002Doubler · crackedTHE FOLLOWING IS THE INFORMATION FOR THE FAA FORM 8010-4 MALFUNCTION OR DEFECT REPORT REFERENCE CRACKS IN THE MLG ACTUATOR BULKHEAD DOUBLERS ON CESSNA 210E SN 21058705 N404BN TOTAL TIME AIRFRAME IS 5455.8 HOURS. AFTER RESEARCH OF THE ACFT LOG BOOKS IT WAS DETJun 18, 2019 · N404BN · Cessna 210E · Fuselage Main, StructureSDR Q06E2014FA0000368Actuator · inoperativeACTUATOR FAILED TO PROVIDE FUNCTION, GEAR UNLOCK FAILED AND WAS FORCED OVER LOCK, INCORRECT PARTS FOUND INSTALLED IN ACTUATOR, ACTUATOR RECEIVED BY INSTALLING AGENCY FOLLOWING O/H BY REPAIR STATION.May 16, 2014 · N2318F · Cessna 210E · Landing Gear ActuatorSDR 2013FA0000300Saddle · crackedTHE LT AND RT MAIN GEAR SADDLES WERE REPLACED 3-14-1977 AT TACH 1448.0. IAW AD76-14-07R2 AND SE75-26 THEY WERE DUE FOR A DY PENETRANT CHECK 1300 HRS LATER. THE DYE PENETRENT CHECK WAS DONE 42HRS EARLY TO CONINCIDE WITH OTHER MAINTENANCE. BOTH SADDLES WERE DMay 21, 2013 · N4963U · Cessna 210E · Main Landing GearSDR 2013FA0000299Saddle · crackedTHE LT AND RT MAIN GEAR SADDLES WERE REPLACED 3-14-1977 AT TACH 1448.0 IAW AD76-14-07R2 AND SE75-26 THEY WERE DUE FOR A DY PENETRANT CHECK 1300 HRS LATER. THE DYE PENETRENT CHECK WAS DONE 42HRS EARLY TO CONINCIDE WITH OTHER MX. BOTH SADDLES WERE DISCOVERED TMay 21, 2013 · N4963U · Cessna 210E · Main Landing GearSDR 2006FA0000448Fcu · wornFOUND SHAFT AND LINKAGE EXCESSIVELY WORN. HAD COMPLETE ASSEMBLY OVERHAULED. (K)Apr 14, 2006 · Cessna 210E · Fuel Control/Reciprocating EnginesSDR 2005FA0001198Wedge · brokenCABLE BROKE AT THE S3 WEDGE WHERE THE BARREL END CONNECTS TO THE INTERNAL CABLE. THIS AREA IS NOT VISIBLE AS THERE IS AN INTERNAL SLEEVE THAT COVERS THE CABLE IN THIS AREA. ( CE07200516270) (K)Jul 9, 2005 · N4933U · Cessna 210E · Power LeverSDR 2005FA0000656Saddle · crackedREPLACED BOTH MLG SADDLES AT ANNUAL INSP. BOTH WERE FOUND TO HAVE HAIR LINE CRACKS IN RADIUS ABOVE IB V-BOLT HOLE USING DYE PENETRANT INSPECTION METHOD. (K)Apr 23, 2005 · N4934U · Cessna 210E · Main Landing GearSDR 2004FA0000516Arm · inoperativeNOSE GEAR ON THIS AC WOULD NOT EXTEND DURING NORMAL, SUBSEQUENT EMERG L/G EXTEND PROCEDURE. UPON JACKING AC, FREEING NOSE GEAR, IT WAS DISCOVERED NOSE L/G DOOR ACTUATION ARM AND ROLLER ASSY WAS POSITIONED ON AFT SIDE OF NOSE GEAR FORK. WHEN WEIGHT OF AC WAS May 19, 2004 · N4916U · Cessna 210E · Landing Gear Door Retract SectionSDR 2002FA0001399Nut · looseLARGE LOCKNUT ON OIL FILTER ADAPTER CAME LOOSE AND OIL WENT OVERBOARD AND THE ENGINE SEIZED. THE AIRCRAFT LANDED IN A FIELD. THE SAFETY WIRE WAS STILL ATTACHED.Dec 4, 2002 · N95PY · Cessna 210E · Reciprocating Engine Oil SystemSDR 2002FA0001125Saddle · crackedBOTH MLG SADDLES WERE FOUND TO BE CRACKED IAW AD. PREVIOUS INSPECTION WAS 132 HOURS BEFORE THIS INSPECTION.Sep 14, 2002 · N2398F · Cessna 210E · Main Landing Gear Attach SectionSDR 2002FA0001115O-Ring · leakingAIRCRAFT LANDED WITH MAIN LANDING GEAR UP AND NOSE GEAR DOWN. CAUSE OF INCIDENT WAS A FAILED ORING IN NOSE LANDING GEAR ACTUATOR. LEAK RATE DEPLETED RESEVOIR AND WAS TOO GREAT FOR HAND PUMP VOLUME. MM HAS NO REPLACEMENT SCHEDULE FOR THESE ORINGS.Sep 13, 2002 · N2398F · Cessna 210E · Landing Gear ActuatorSDR 97ZZZX4443Door Sill · crackedDURING INSPECTION, REMOVED CHROME TRIM OVER DOOR SILL, FOUND REAR CORNER BROKEN ACROSS TOP. TRIM NOT USUALLY REMOVED FOR INSPECTION. SUBMITTER STATED POSSIBLE CAUSE, HARD LANDING. CLOSER INSPECTION REVEALS SOME PREVIOUS RIVETS REPLACED IN AREA, NO LOG ENTRYOct 2, 1997 · N2393F · Cessna 210E · Fuselage Miscellaneous StructureSDR 96ZZZX4729Hose · deterioratedFUEL HOSES NON-OPERATONAL FOR 3 YEARS ALLOWING NON-PRESSURE SIDE OF FUEL HOSES TO DRY OUT AND INSIDE OF HOSE TO DETERIORATE. SMALL PIECES OF RUBBER HOSE BROKE OFF AND CLOGGED FUEL LINES IN FUEL INJECTION SYSTEM.Aug 19, 1996 · N4931U · Cessna 210E · Engine Fuel DistributionSDR AU960946Stud · sheared(AUS) NO5 CYLINDER BASE STUD (1OFF) SHEARED OFF - STUD WAS FOUND IN BOTTOM COWLJul 5, 1996 · Cessna 210E · Reciprocating Engine Power SectionSDR CA960612018Hydpower Pack · contaminated(CAN) THE HYDRAULIC RESERVOIR WAS FOUND TO BE CONTAMINATED WITH A FILM OF SLUDGE. FURTHER INVESTIGATION FOUND TEFLON TAPE ON THE VARIOUS FITTINGS AND TEFLON CONTAMINATION THROUGHOUT THE UNIT.Jun 6, 1996 · Cessna 210E · Hydraulic Pump (Electric/Engine), MainSDR 95ZZZX6918Power Pack Valve · failedPILOT ATTEMPTED TO LOWER LANDING GEAR. PILOT WAS UNABLE TO LOWER LANDING GEAR USING NORMAL OR EMERGENCY PROCEDURES WHICH RESULTED IN A GEAR-UP LANDING. FURTHER INVESTIGATION REVEALED THAT POWER PACK SECONDARY RELIEF VALVE WAS STUCK OPEN, THEREFORE, BYPASSINGSep 8, 1995 · N2331F · Cessna 210E · Hydraulic Pump (Electric/Engine), MainSDR 95ZZZX3951Bearing · failedBEARING RACE BROKE, A PIECE ABOUT .3750 INCH CAME LOOSE AND WENT THROUGH HUB CAUSING DAMAGE. PROPELLER WAS OVERHAULED 5 YEARS PRIOR AND 415 HOURS TSO. THIS CONDITION WAS FOUND DURING OVERHAUL. ENTIRE HUB WAS CONDEMNED.Jul 25, 1995 · N4974U · Cessna 210E · Propeller Hub Section
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