# Service difficulty reports: Cessna 210-5 A list on [Cessna 210-5](https://openairdocs.org/model/cessna-210-5.md). Newest first. General aviation reporting is voluntary. - [SDR 2017FA0000170](https://openairdocs.org/sdr/2017FA0000170.md): Wire Rope · broken · Apr 29, 2017 · N1748Z · Cessna 2105 · Flight Compartment Equipment > FAILURE OF SECONDARY SEAT STOP INSTALLED PER SEB07-5. PILOT WAS UNABLE TO SLIDE THE SEAT AFT TO EXIT THE AIRCRAFT. INSPECTION DETERMINED THAT THE WIRE ROPE USED IN THE ACTUATOR MECHANISM FAILED AT THE CRIMPED END FITTING THAT ATTACHES TO THE SEAT. - [SDR 2013FA0000446](https://openairdocs.org/sdr/2013FA0000446.md): Bracket · cracked · Jul 5, 2013 · N205CL · Cessna 2105 · Fuselage Miscellaneous Structure > BALANCE TUBE MOUNTING BRACKET CRACKED. TUBE CRACKED AT ONE END. - [SDR 2009FA0000330](https://openairdocs.org/sdr/2009FA0000330.md): Bulkhead · cracked · Apr 1, 2009 · N8453Z · Cessna 2105 · Fuselage Main, Bulkhead > INSP PURSUANT TO AD-72-07-09 REVEALED A CRACK IN THE UPPER LT FLANGE AREA OF THE BULKHEAD. BULKHEAD WAS REPLACED. (K) - [SDR CA071227003](https://openairdocs.org/sdr/CA071227003.md): Bolt · broken · Oct 15, 2007 · Cessna 2105 · Nose/Tail Landing Gear > (CAN) WHILE TAXING ON BUSH STRIP, NOSE GEAR AFT DRAG STRUT BOLT BROKE AND WORKED OUT CAUSING NOSE GEAR TO FOLD FWD. (TC NR 20071227003) - [SDR 2006FA0000515](https://openairdocs.org/sdr/2006FA0000515.md): Elt · failed · May 5, 2006 · N8197Z · Cessna 2105 · Emergency Locator Beacon > ELT FAILED UPON INSPECTION AFTER 12 MONTHS OF SERVICE, DID NOT TRANSMIT THROUGH ANTENNA, LIGHT WENT ON INDICATING FUNCTION. THIS IS THE 3RD FAILURE ON UNITS NEWER THAN ONE YEAR OLD, IN 1.5 YEARS IN OUR SHOP. (K) - [SDR CA060228011](https://openairdocs.org/sdr/CA060228011.md): Magneto · failed · Dec 5, 2005 · Cessna 2105 · Magneto/Distributor > NR 1 CYLINDER NOT FIRING. TRACED BACK TO INTERNAL PROBLEM WITH MAGNETO, RETURNED FOR WARRANTY. - [SDR CA060228012](https://openairdocs.org/sdr/CA060228012.md): Oil Cooler · cracked · Jul 2, 2005 · Cessna 2105 · Engine Oil Cooler > OIL LEAK FROM OIL COOLER. - [SDR CA060228010](https://openairdocs.org/sdr/CA060228010.md): Magneto · failed · Jun 21, 2005 · Cessna 2105 · Magneto/Distributor > ROUGHNESS ON STARTUP OF LT MAGNETO. - [SDR AU510001732](https://openairdocs.org/sdr/AU510001732.md): Bulkhead · cracked · Feb 8, 2005 · Cessna 2105 · Fuselage Main, Bulkhead > (AUS) FUSELAGE DOORPOST BULKHEAD CRACKED. FOUND DURING INSPECTION IAW AD/C205/21. (AD/SB DESC: AD/C205/21) (CASA NR 510001732) - [SDR W322004F00000](https://openairdocs.org/sdr/W322004F00000.md): Yoke · cracked · Dec 22, 2003 · N8298Z · Cessna 2105 · Control Column Section > PILOT REPORTED THAT DURING LANDING FLARE, THE YOKE SNAPPED RESULTING IN A GO AROUND. AFTER INITIAL INSPECTION, YOKE WAS FOUND CRACKED COMPLETELY THROUGH ON UPPER LEFT HAND CORNER. YOKE MATERIAL APPEARS TO MANUFACTURED FROM PLASTIC, SUGGEST REMOVAL OF ALL PLA - [SDR CA030305008](https://openairdocs.org/sdr/CA030305008.md): Propeller · failed · Feb 17, 2003 · Cessna 2105 · Propeller Blade Section > (CAN) FACTORY NEW PROPELLER STC SA00920CH. ONLY OBTAIN 2300 RPM STATIC, SHOULD BE 2600 RPM. FOUND BLADE LOW END STOPS INCORRECTLY SET.- PROP RETURNED TO OBTAIN NEEDED 2600 RPM. ERROR IN ENGINEERING APPROVAL AT MCCAULEY INCORRECT BLADE ANGLES. - [SDR AUS20021364](https://openairdocs.org/sdr/AUS20021364.md): Valve Guide · unserviceable · Nov 22, 2002 · Cessna 2105 · Reciprocating Engine Cylinder Section > (AUS) NO2 CYLINDER EXHAUST VALVE GUIDE CARBON BUILDUP. EXHAUST VALVESEIZED IN GUIDE CAUSING PUSHROD TO BEND AND SHROUD TUBE TO BE BROKEN. - [SDR 2002FA0000796](https://openairdocs.org/sdr/2002FA0000796.md): Pump · failed · Mar 28, 2002 · N8130Z · Cessna 2105 · Engine Fuel Pump > ENGINE LOST POWER, AIRCRAFT LANDED OFF AIRPORT. FOUND FUEL CONTAMINATION AND FUEL PUMP PRESSURE RELIEF VALVE STUCK. AD841001, WAS SIGNED OFF BUT FUEL HEADER TNKS WERE CONTAMINATED AND NO DRAIN VALVES HAD BEEN INSTALLED. CUSTOMER WAS NOTIFIED THAT PUMP HAD T - [SDR 20010501CW005](https://openairdocs.org/sdr/20010501CW005.md): Wheel · cracked · Apr 17, 2001 · N8279Z · Cessna 2105 · Wheel/Ski/Float > MAGNESIUM 5.00-5 TYPE III WHEEL HALVES. FOUND CRACKS ADJAVENT TO THRU BOLT BOSSES AT PERIMETER ON BOTH WHEEL HALVES. POSSIBLE CAUSES, HARD LANDINGS OR OVER TORQUING. - [SDR 20010410AP002](https://openairdocs.org/sdr/20010410AP002.md): Floorbeam · corroded · Feb 21, 2001 · N1825Z · Cessna 2105 · Fuselage Main, Floor Beam > DURING ANNUAL INSPECTION DISCOVERED SEVERE INTERGRANULAR CORROSION ON LEFT 4 INCHES OF ANGLE. CORROSION OCCURED PRIMARILY WHERE.25 IN. HI-SHEAR RIVITS ATTACH ANGLE TO BULKHEAD AND WING LIFT STRUT ATTACH FITTING. ANGLE WAS LESS THAN HALF ORIGINAL THICKNESS - [SDR CA000925033](https://openairdocs.org/sdr/CA000925033.md): Crankcase · cracked · Aug 23, 2000 · Cessna 2105 · Reciprocating Engine Cylinder Section > (CAN) OIL LEAK TRACED TO CYLINDER HOLD DOWN AREA OF NR 2 CYLINDER. LARGE CRACK FROM 3 O''CLOCK POSITION. NR 2 CYLINDER UP TO 11 O''CLOCK. (X) - [SDR 20000831SH012](https://openairdocs.org/sdr/20000831SH012.md): Pump · leaking · Aug 3, 2000 · N8260Z · Cessna 2105 · Fuel Control/Reciprocating Engines > DURING POST-FLIGHT SECURING OF ACFT, PILOT NOTICED FUEL DRIPPING FROM LT COWL FLAP OPENING. INVEST REVEALED FUEL COMING FROM ENGINE DRAIN LINE TRACED TO THE FUEL INJECTION PUMP. SELECTING THE OFF POSITION OF THE FUEL SELECTOR VALVE RELIEVED THE FUEL TANK HEA - [SDR AU980999](https://openairdocs.org/sdr/AU980999.md): Piston Ring · broken · Aug 4, 1998 · Cessna 2105 · Reciprocating Engine Cylinder Section > (AUS) NR 2 AND NR 4 CYLINDER OIL CONTROL RINGS BROKEN. PART TC: 89. - [SDR CA961018002](https://openairdocs.org/sdr/CA961018002.md): Cylinder · head separated · Sep 13, 1996 · Cessna 2105 · Reciprocating Engine Cylinder Section > (CAN) HEAD BLOWN OFF CYLINDER. - [SDR AU961186](https://openairdocs.org/sdr/AU961186.md): Angle · corroded · Jun 12, 1996 · Cessna 2105 · Wing Miscellaneous Structure > (AUS) DURING INSPECTION OF LH AND RH WINGS MISSING RIVET HEADS WERE FOUND ON THE WING UPPER SKIN THROUGH THE MAIN SPAR INBOARD TOP CAP - FOLLOWING REMOVAL AND DISASSEMBLY OF THE WINGS THE SEVERE EXFOLIATION CORROSION WAS FOUND ON THE FOLLOWING ANGLES ANDPLAT - [SDR CA960515004](https://openairdocs.org/sdr/CA960515004.md): Static Sensor · leaking · May 7, 1996 · Cessna 2105 · Pitot/Static System > (CAN) PIEZO STATIC SENSOR HOUSING LEAKING IN EXCESS OF LIMITS - [SDR 96ZZZX2295](https://openairdocs.org/sdr/96ZZZX2295.md): Static Port · leaking · Apr 1, 1996 · N5875 · Cessna 2105 · Pitot/Static System > THE SEALANT BETWEEN STATIC PORT AND SKIN OF AIRCRAFT HAD TURNED TO POWDER MAKING A LEAK IN THE STATIC SYTSEM. DRILLED RIVETS OUT OF STATIC PORT, SEALED WITH PR-1422 SEALANT. STARTED STATIC CHECK AGAIN, GOT UP TO 11,000 FEET AND A SEVERE LEAK STARTED AGAIN. ## 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 = '2105' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/cessna-210-5/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.