# Service difficulty reports: Cessna 210E A list on [Cessna 210E](https://openairdocs.org/model/cessna-210e.md). Newest first. General aviation reporting is voluntary. - [SDR 4S42020F00002](https://openairdocs.org/sdr/4S42020F00002.md): Doubler · cracked · Jun 18, 2019 · N404BN · Cessna 210E · Fuselage Main, Structure > THE 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 DET - [SDR Q06E2014FA0000368](https://openairdocs.org/sdr/Q06E2014FA0000368.md): Actuator · inoperative · May 16, 2014 · N2318F · Cessna 210E · Landing Gear Actuator > ACTUATOR 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. - [SDR 2013FA0000300](https://openairdocs.org/sdr/2013FA0000300.md): Saddle · cracked · May 21, 2013 · N4963U · Cessna 210E · Main Landing Gear > THE 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 D - [SDR 2013FA0000299](https://openairdocs.org/sdr/2013FA0000299.md): Saddle · cracked · May 21, 2013 · N4963U · Cessna 210E · Main Landing Gear > THE 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 T - [SDR 2006FA0000448](https://openairdocs.org/sdr/2006FA0000448.md): Fcu · worn · Apr 14, 2006 · Cessna 210E · Fuel Control/Reciprocating Engines > FOUND SHAFT AND LINKAGE EXCESSIVELY WORN. HAD COMPLETE ASSEMBLY OVERHAULED. (K) - [SDR 2005FA0001198](https://openairdocs.org/sdr/2005FA0001198.md): Wedge · broken · Jul 9, 2005 · N4933U · Cessna 210E · Power Lever > CABLE 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) - [SDR 2005FA0000656](https://openairdocs.org/sdr/2005FA0000656.md): Saddle · cracked · Apr 23, 2005 · N4934U · Cessna 210E · Main Landing Gear > REPLACED 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) - [SDR 2004FA0000516](https://openairdocs.org/sdr/2004FA0000516.md): Arm · inoperative · May 19, 2004 · N4916U · Cessna 210E · Landing Gear Door Retract Section > NOSE 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 - [SDR 2002FA0001399](https://openairdocs.org/sdr/2002FA0001399.md): Nut · loose · Dec 4, 2002 · N95PY · Cessna 210E · Reciprocating Engine Oil System > LARGE 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. - [SDR 2002FA0001125](https://openairdocs.org/sdr/2002FA0001125.md): Saddle · cracked · Sep 14, 2002 · N2398F · Cessna 210E · Main Landing Gear Attach Section > BOTH MLG SADDLES WERE FOUND TO BE CRACKED IAW AD. PREVIOUS INSPECTION WAS 132 HOURS BEFORE THIS INSPECTION. - [SDR 2002FA0001115](https://openairdocs.org/sdr/2002FA0001115.md): O-Ring · leaking · Sep 13, 2002 · N2398F · Cessna 210E · Landing Gear Actuator > AIRCRAFT 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. - [SDR 97ZZZX4443](https://openairdocs.org/sdr/97ZZZX4443.md): Door Sill · cracked · Oct 2, 1997 · N2393F · Cessna 210E · Fuselage Miscellaneous Structure > DURING 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 ENTRY - [SDR 96ZZZX4729](https://openairdocs.org/sdr/96ZZZX4729.md): Hose · deteriorated · Aug 19, 1996 · N4931U · Cessna 210E · Engine Fuel Distribution > FUEL 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. - [SDR AU960946](https://openairdocs.org/sdr/AU960946.md): Stud · sheared · Jul 5, 1996 · Cessna 210E · Reciprocating Engine Power Section > (AUS) NO5 CYLINDER BASE STUD (1OFF) SHEARED OFF - STUD WAS FOUND IN BOTTOM COWL - [SDR CA960612018](https://openairdocs.org/sdr/CA960612018.md): Hydpower Pack · contaminated · Jun 6, 1996 · Cessna 210E · Hydraulic Pump (Electric/Engine), Main > (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. - [SDR 95ZZZX6918](https://openairdocs.org/sdr/95ZZZX6918.md): Power Pack Valve · failed · Sep 8, 1995 · N2331F · Cessna 210E · Hydraulic Pump (Electric/Engine), Main > PILOT 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, BYPASSING - [SDR 95ZZZX3951](https://openairdocs.org/sdr/95ZZZX3951.md): Bearing · failed · Jul 25, 1995 · N4974U · Cessna 210E · Propeller Hub Section > BEARING 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. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/model/cessna-210e/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.