Cessna 210-5

Service difficulty reports · 22

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 = '2105'
  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 2017FA0000170Wire Rope · brokenFAILURE 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.Apr 29, 2017 · N1748Z · Cessna 2105 · Flight Compartment EquipmentSDR 2013FA0000446Bracket · crackedBALANCE TUBE MOUNTING BRACKET CRACKED. TUBE CRACKED AT ONE END.Jul 5, 2013 · N205CL · Cessna 2105 · Fuselage Miscellaneous StructureSDR 2009FA0000330Bulkhead · crackedINSP PURSUANT TO AD-72-07-09 REVEALED A CRACK IN THE UPPER LT FLANGE AREA OF THE BULKHEAD. BULKHEAD WAS REPLACED. (K)Apr 1, 2009 · N8453Z · Cessna 2105 · Fuselage Main, BulkheadSDR CA071227003Bolt · broken(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)Oct 15, 2007 · Cessna 2105 · Nose/Tail Landing GearSDR 2006FA0000515Elt · failedELT 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)May 5, 2006 · N8197Z · Cessna 2105 · Emergency Locator BeaconSDR CA060228011Magneto · failedNR 1 CYLINDER NOT FIRING. TRACED BACK TO INTERNAL PROBLEM WITH MAGNETO, RETURNED FOR WARRANTY.Dec 5, 2005 · Cessna 2105 · Magneto/DistributorSDR CA060228012Oil Cooler · crackedOIL LEAK FROM OIL COOLER.Jul 2, 2005 · Cessna 2105 · Engine Oil CoolerSDR CA060228010Magneto · failedROUGHNESS ON STARTUP OF LT MAGNETO.Jun 21, 2005 · Cessna 2105 · Magneto/DistributorSDR AU510001732Bulkhead · cracked(AUS) FUSELAGE DOORPOST BULKHEAD CRACKED. FOUND DURING INSPECTION IAW AD/C205/21. (AD/SB DESC: AD/C205/21 ) (CASA NR 510001732)Feb 8, 2005 · Cessna 2105 · Fuselage Main, BulkheadSDR W322004F00000Yoke · crackedPILOT 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 PLADec 22, 2003 · N8298Z · Cessna 2105 · Control Column SectionSDR CA030305008Propeller · failed(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.Feb 17, 2003 · Cessna 2105 · Propeller Blade SectionSDR AUS20021364Valve Guide · unserviceable(AUS) NO2 CYLINDER EXHAUST VALVE GUIDE CARBON BUILDUP. EXHAUST VALVESEIZED IN GUIDE CAUSING PUSHROD TO BEND AND SHROUD TUBE TO BE BROKEN.Nov 22, 2002 · Cessna 2105 · Reciprocating Engine Cylinder SectionSDR 2002FA0000796Pump · failedENGINE 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 TMar 28, 2002 · N8130Z · Cessna 2105 · Engine Fuel PumpSDR 20010501CW005Wheel · crackedMAGNESIUM 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.Apr 17, 2001 · N8279Z · Cessna 2105 · Wheel/Ski/FloatSDR 20010410AP002Floorbeam · corrodedDURING 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 Feb 21, 2001 · N1825Z · Cessna 2105 · Fuselage Main, Floor BeamSDR CA000925033Crankcase · cracked(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)Aug 23, 2000 · Cessna 2105 · Reciprocating Engine Cylinder SectionSDR 20000831SH012Pump · leakingDURING 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 HEAAug 3, 2000 · N8260Z · Cessna 2105 · Fuel Control/Reciprocating EnginesSDR AU980999Piston Ring · broken(AUS) NR 2 AND NR 4 CYLINDER OIL CONTROL RINGS BROKEN. PART TC: 89.Aug 4, 1998 · Cessna 2105 · Reciprocating Engine Cylinder SectionSDR CA961018002Cylinder · head separated(CAN) HEAD BLOWN OFF CYLINDER.Sep 13, 1996 · Cessna 2105 · Reciprocating Engine Cylinder SectionSDR AU961186Angle · corroded(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 ANDPLATJun 12, 1996 · Cessna 2105 · Wing Miscellaneous StructureSDR CA960515004Static Sensor · leaking(CAN) PIEZO STATIC SENSOR HOUSING LEAKING IN EXCESS OF LIMITSMay 7, 1996 · Cessna 2105 · Pitot/Static SystemSDR 96ZZZX2295Static Port · leakingTHE 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. Apr 1, 1996 · N5875 · Cessna 2105 · Pitot/Static System
Back to Cessna 210-5