# Service difficulty reports: Cessna 310J A list on [Cessna 310J](https://openairdocs.org/model/cessna-310j.md). Newest first. General aviation reporting is voluntary. - [SDR 2023FA0000263](https://openairdocs.org/sdr/2023FA0000263.md): Roller · seized · May 15, 2023 · N3087L · Cessna 310J · Landing Gear Steering System > NOSE LANDING GEAR STRAIGHTENER CAM ROLLER PN CR10-1 SEIZED WHICH BENT THE NOSE LANDING GEAR STRAIGHTENER PN 0842000-58 BRACKET CAUSING NOSE LANDING GEAR TO BE UNABLE TO CENTER AAND UNABLE TO EXTEND OR RETRACT FULLY. AIRCRAFT LANDED WITH MLG RETRACTED AND NLG P - [SDR LCPR20220119001](https://openairdocs.org/sdr/LCPR20220119001.md): None · defective · Dec 27, 2021 · N3134L · Cessna 310J · Landing Gear Retraction/Extension System > AFTER INCIDENT ON 12/21/2021 AT KBCT. PER REQUEST AIRCRAFT WAS JACKED AND FUNCTIONAL CHECKS (GEAR SWINGS) WERE PERFORMED ON THE AIRCRAFT. AFTER MULTIPLE FUNCTIONAL CHECKS (GEAR SWINGS) IT WAS FOUND THAT THE NOSE GEAR WOULD NOT LOCK OUT AND A GRINDING NOISE WAS - [SDR 2007FA0000195](https://openairdocs.org/sdr/2007FA0000195.md): Limit Switch · failed · Jan 29, 2007 · N3091L · Cessna 310J · Landing Gear Actuator > UP LIMIT SWITCH FAILED ON LANDING GEAR ACTUATOR, CAUSING OVER EXTENSION OF NOSE GEAR SYSTEM. THIS CAUSED THE INTERMEDIATE TORQUE TUBE TO BEND. (K) - [SDR 2005FA0001244](https://openairdocs.org/sdr/2005FA0001244.md): Attach Fitting · corroded · May 16, 2005 · N700MA · Cessna 310J · Fuselage, Wing Attach Fittings > DURING THE ANNUAL INSPECTION, THE WING FITTING WAS FOUND TO BE CORRODED SO SEVERE THAT IT WAS ALMOST.2500 OF THE WAY THRU THE FITTING. PICTURES ENCLOSED THAT SHOW DAMAGE. FITTING WAS LOCATED ON THE LT SIDE, AFT TOP FITTING. (K) - [SDR 310EE](https://openairdocs.org/sdr/310EE.md): Support Bracket · broken · Aug 8, 2003 · N310EE · Cessna 310J · Fuselage Miscellaneous Structure > RH LANDING GEAR COLLAPSED ON LANDING. FOUND THAT THE UPPER BELLCRANK BRACKETT P/N 0811303-1 WHICH SUPPORTS AND GUIDES THE RT MAIN LANDING GEAR PUSH/PULL TUBES FROM GEAR BOX TO GEAR ASSEMBLY SEPERATED FROM BULKHEAD DUE TO MOUNTING RIVET FAILURE. THIS SEPERATION - [SDR 2003F00141](https://openairdocs.org/sdr/2003F00141.md): Switch · failed · Mar 13, 2003 · N308J · Cessna 310J · Landing Gear Position and Warning > ON APPROACH TO ELP THE PILOT DID NOT HAVE A GREEN LIGHT AFTER SELECTING GEAR DOWN. A FLY BY INDICATED GEAR APPEARED IN NORMAL DOWN POSITION. PILOT LANDED WITHOUT INCIDENT. THE LEFT HAND MICRO SWITCH PN 1SE3-3 FAILED INTERNALLY. REMOVED AND REPLACED SWITCH. - [SDR 2001FA0000595](https://openairdocs.org/sdr/2001FA0000595.md): Bushing · separated · Jul 10, 2001 · Cessna 310J · Main Landing Gear Strut/Axle/Truck > RIGHT MAIN LANDING GEAR UPPER AND LOWER TORQUE LINKS BECAME DISCONNECTED FROM EACH OTHER DURING TAKEOFF ROLL. IT APPEARS THAT A PRESSED IN BUSHING, SEPARATED FROM THE LOWER TORQUE LINK ALLOWING THE BOLT HEAD AND WASHER TO PASS THROUGH THE ENLARGED HOLE NORMAL - [SDR 2002FA0000045](https://openairdocs.org/sdr/2002FA0000045.md): Shimmy Dampener · damaged · Apr 3, 2001 · N63GG · Cessna 310J · Shimmy Damper > PILOT MADE A HARD LEFT TURN CAUSEING DAMAGE TO THE NOSE GEAR AREA. BENT ROD ON THE SHIMMY DAMPER CAUSING INTERNAL DAMAGE TO THE COMPONENT. - [SDR 20010412CW009](https://openairdocs.org/sdr/20010412CW009.md): Cylinder · leaking · Mar 1, 2001 · N515HW · Cessna 310J · Reciprocating Engine Cylinder Section > AIRCRAFT LANDED. OIL LEAKING FROM LEFT ENGINE. INSPECTION REVEALED NR 4 CYLINDER VALVE COVER BROKEN DUE TO VALVE ROCKER ASSEMBLY BROKEN FROM CYLINDER BOSS. PROBABLE CAUSE STUCK VALVE OR METAL FATIGUE AT BOSS. - [SDR 20000817SH012](https://openairdocs.org/sdr/20000817SH012.md): Hub · cracked · Jul 31, 2000 · N3141L · Cessna 310J · Propeller Hub Section > HUB CRACKED IN BOTH THREADED BLADE SOCKETS. PROPELLER WAS LEAKING, IN FOR RE-SEAL. (X) - [SDR 20000626SH003](https://openairdocs.org/sdr/20000626SH003.md): Spar · corroded · Jun 13, 2000 · N310J · Cessna 310J · Wing Spar > EXFOLIATION CORROSION AT LEAST.01 INCH TO.1250 INCH DEEP AND GROWING. SUBMITTER STATES THAT AIRCRAFT WAS BASED IN SAN FRANCISCO BAY AREA AND SALT AIR MAY HAVE CONDENSED INSIDE THE AIRCRAFT INSULATION AND DRIPPED DOWN ON THE FITTINGS. HOWEVER, SUBMITTER BEL - [SDR 20000626SH002](https://openairdocs.org/sdr/20000626SH002.md): Fitting · corroded · Jun 13, 2000 · N3079L · Cessna 310J · Wing, Attach Fittings > EXFOLIATION CORROSION AT LEAST.01 INCH TO.1250 INCH DEEP AND GROWING. SUBMITTER STATES THAT AIRCRAFT WAS BASED IN SAN FRANCISCO BAY AREA AND SALT AIR MAY HAVE CONDENSED INSIDE THE AIRCRAFT INSULATION AND DRIPPED DOWN ON THE FITTINGS. HOWEVER, SUBMITTER BEL - [SDR CA001005010](https://openairdocs.org/sdr/CA001005010.md): Downlock · misaligned · Apr 9, 2000 · Cessna 310J · Landing Gear Retraction/Extension System > (CAN) - RIGHT GEAR COLLAPSED AFTER LANDING. DOWNLOCK FOUND MISADJUSTED (TOO SHORT). DOWNLOCK BELLCRANK, SIDE BRACE LINK REPLACED. DOWNLOCK READJUSTED. (X) - [SDR CA990318038](https://openairdocs.org/sdr/CA990318038.md): Window · separated · Feb 23, 1999 · Cessna 310J · Emergency Exits > (CAN) AFTER T/F EMERGENCY WINDOW DEPARTED AIRCRAFT. UPON FURTHER INVESTIGATION, THE WINDOW SEPARATED FROM THE FRONT AND PROCEEDED TO PEEL BACKWARDS. THE EMERGENCY CABLE WAS NOT PULLED. THE REAR LOCKING PINS WERE BENT AND THE WINDOW TABS WERE RIPPED FROM THE - [SDR 98ZZZX983](https://openairdocs.org/sdr/98ZZZX983.md): Idler Gear · failed · Feb 23, 1998 · N3141L · Cessna 310J · Landing Gear Retraction/Extension System > IDLER IN NOSE GEAR RETRACT LINKAGE BROKE DURING RETRACTION DUE TO INTERFERENCE OF NOSE GEAR AND WHEELWELL DOORS. NOSE GEAR FAILED TO EXTEND DUE TO LOSS OF NITROGEN CHARGE IN STRUT. STRUT HAD BEEN OVERSERVICED WITH HYDRAULIC FLUID. WITH THE STRUT BEING OVERS - [SDR EY2R9600168](https://openairdocs.org/sdr/EY2R9600168.md): Hub · cracked · Dec 1, 1996 · Cessna 310J · Propeller Hub Section > PROP HUB ASSY CRACKED IN THREAD AREA - [SDR EY2R9600064](https://openairdocs.org/sdr/EY2R9600064.md): Hub · cracked · May 1, 1996 · Cessna 310J · Propeller Hub Section > PROP ASSY HUB CRACKED - [SDR AU960503](https://openairdocs.org/sdr/AU960503.md): Exhaust Valve · leaking · Apr 16, 1996 · Cessna 310J · Reciprocating Engine Cylinder Section > (AUS) ENGINE COMPRESSION LEAKAGE FROM EXHAUST VALVES ON ALL 6 CYLINDERS- FOUND DURING COMPRESSION CHECK IAW AD/ENG/4 AMDT 5 - ENGINECALENDER TIME SINCE OVERHAUL WAS 19 YEARS - [SDR 95ZZZX568](https://openairdocs.org/sdr/95ZZZX568.md): Mount · damaged · Jan 13, 1995 · N3192L · Cessna 310J · Engine Mount Section > NEW OWNER BROUGHT AIRCRAFT IN FOR PITOT HEAT PROBLEM. NOTICED LT ENGINE WAS SAGGING RELATIVE TO THE COWLING. FURTHER INSPECTION REVEALED THE FORWARD MOUNTS TO HAVE UNSEATED AND DROPPED IN THE SUPPORT STRUCTURE. THE RT ENGINE WAS CHECKED AND FOUND TO HAVE TH ## 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 = '310J' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/cessna-310j/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.