# Service difficulty reports: Cessna T310Q A list on [Cessna T310Q](https://openairdocs.org/model/cessna-t310q.md). Newest first. General aviation reporting is voluntary. - [SDR 2020FA0000451](https://openairdocs.org/sdr/2020FA0000451.md): Tube · broken · Oct 20, 2020 · N28409 · Cessna T310Q · Landing Gear Retraction/Extension System > IN PREPARATION FOR SLOW FLIGHT DURING A COMMERCIAL PILOT CHECK RIDE, LANDING GEAR EXTENSION WAS ACCOMPLISHED. AN UNUSUAL YAW WAS EXPERIENCED WITH UNUSUAL NOISE FROM THE LEFT MAIN LANDING GEAR. THE LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. GEAR WAS RE - [SDR 2008FA0000411](https://openairdocs.org/sdr/2008FA0000411.md): Rod End · broken · Jun 12, 2008 · N7044Q · Cessna T310Q · Landing Gear Retraction/Extension System > AFTER TAKEOFF, WHEN RETRACTING GEAR, PILOT HEARD LOUD CRACK. NOSE GEAR WOULD NOT RETRACT. AIRCRAFT LANDED WITH NOSE GEAR TRAILING AFT. NOSE GEAR COLLAPLSED ON LANDING. INSPECTION REVEALED ROD END UNDER PILOT`S FLOOR THAT CONNECTS NOSE GEAR RETRACT ROD TO B - [SDR 2007FA0000713](https://openairdocs.org/sdr/2007FA0000713.md): Cylinder · leaking · Jul 31, 2007 · N7714Q · Cessna T310Q · Reciprocating Engine Cylinder Section > WHILE PERFORMING OTHER MAINTENANCE A FUEL STAIN WAS NOTICED BETWEEN THE SECOND AND THIRD COOLING FIN AFT OF THE FUEL INJECTOR ON THE NR 6 CYLINDER OF THE RT ENGINE. THIS CONDITION PROMPTED A CLOSER INSPECTION OF THE ENGINE RESULTING IN THE DISCOVERY OF SIMILA - [SDR 2007FA0000625](https://openairdocs.org/sdr/2007FA0000625.md): Bellcrank · failed · Jun 22, 2007 · N372CC · Cessna T310Q · Landing Gear Retraction/Extension System > FAILED DUE TO MECHANICAL OVERLOAD, NOSE GEAR JAMMED. (K) - [SDR 2006FA0001058](https://openairdocs.org/sdr/2006FA0001058.md): Pitot Line · corroded · Oct 18, 2006 · N87JV · Cessna T310Q · Pitot/Static System > DURING A ROUTINE PITOT/STATIC TEST, FOUND THAT THE PITOT SYSTEM WAS LEAKING BEYOND LIMITS. THE LEAKAGE WAS DETERMINED TO BE IN THE TUBING FROM THE PITOT TUBE TO THE FORWARD CABIN BULKHEAD FITTING. UPON REMOVING THE TUBE (PN 0800106-379) SEVERE CORROSION WAS - [SDR HXR2004F00000](https://openairdocs.org/sdr/HXR2004F00000.md): Adc · malfunctioned · Sep 21, 2004 · N767RR · Cessna T310Q · Air Data Computer > ADC AND ALTIMETER READING 2000 FT DIFFERENCE. - [SDR 2004FA0000853](https://openairdocs.org/sdr/2004FA0000853.md): Rod End · broken · Jul 9, 2004 · N27KC · Cessna T310Q · Nose/Tail Landing Gear > THE AIRCRAFT DEPARTED. A LARGE NOISE WAS HEARD, COULD NOT EXTEND NOSE GEAR. LANDED WITH AN UNSAFE NOSE GEAR UP, NOSE GEAR COLLAPSED ON LANDING CAUSING DAMAGE. THE ROD END FAILED ON TUBE ASSY. NOTE: THIS IS A COMMON PROBLEM ON THE AK. (SW05200408481) - [SDR DYT2003F00000](https://openairdocs.org/sdr/DYT2003F00000.md): Bellcrank · broken · Jan 10, 2003 · N8108G · Cessna T310Q · Nose/Tail Landing Gear > PILOT REPORTED BANG COMING FROM UNDER HIS FEET WHEN GEAR WAS RETRACTED. WHEN GEAR WAS EXTENDED THE NOSE GEAR DID NOT LOCK. AIRCRAFT LANDED AND NOSE GEAR COLLAPSED. INVESTIGATION FOUND THAT NOSE GEAR IDLER BELLCRANK, BROKEN. - [SDR 2003FA0000036](https://openairdocs.org/sdr/2003FA0000036.md): Bellcrank · broken · Jan 8, 2003 · N8108G · Cessna T310Q · Landing Gear Retraction/Extension System > THE IDLER BELLCRANK FOR THE NOSE GEAR RETRACTION LINKAGE BROKE WHEN THE LANDING GEAR WAS SELECTED TO THE UP POSITION. PILOT WAS UNABLE TO EXTEND THE NOSE GEAR. UPON LANDING THE NOSE GEAR RETRACTED INTO THE WHEEL WELL. INSPECTION REVEALED THAT THE IDLER BELL - [SDR CA030211008](https://openairdocs.org/sdr/CA030211008.md): Actuator · failed · Jan 7, 2003 · Cessna T310Q · Landing Gear Actuator > (CAN) CJ0701 ACTUATOR TAB IS A SMALL METAL TAB THAT FITS ON PORT GEAR DOWN SWITCH. TAB FAILED DUE TO METAL FATIGUE CAUSING INTERMITTENT GEAR SAFE LIGHT ON PORT SIDE. - [SDR 2002FA0001085](https://openairdocs.org/sdr/2002FA0001085.md): Clamp · cracked · Jul 22, 2002 · N650PC · Cessna T310Q · Engine Collector/Tailpipe/Nozzle > THIS CLAMP ATTACHES TAILPIPE TO TURBOCHARGER OUTLET. DURING COMPLIANCE WITH AD2000-1-16 FOUND CLAMP SPLIT AT THE APEX OF THE "V" AROUND 4.75" TO 5.0" OF CIRCUMFERENCE. PER AD2000-1-16 THIS CLAMP IS NOT LIFE-LIMITED. - [SDR 20010312CW010](https://openairdocs.org/sdr/20010312CW010.md): Bracket · cracked · Jan 25, 2001 · N7542Q · Cessna T310Q · Exterior Lighting > AC WAS IN THE HANGAR FOR 50 HOUR INSPECTION. STROBE LIGHTS WERE TURNED ON AND AN EXPLOSION DAMAGED THE LEFT WING TIP TANK. FWD FAIRING WAS BLOWN APART BY AN EXPLOSION. FOUND THE FWD TANK ACCESS PANEL SPOT WELDS FOR THE NAV/STROBE LIGHT BRACKETS WERE CRACKED, - [SDR 20000427SH031](https://openairdocs.org/sdr/20000427SH031.md): Hub · cracked · Mar 21, 2000 · N7542Q · Cessna T310Q · Propeller Hub Section > PART CRACKED FROM GREASE FITTING HOLE ACROSS BACK OF HUB TO OPPOSITE SIDE. SENT TO HARTZEL PROPELLER FOR EVALUATION. (X) - [SDR 20000427SH030](https://openairdocs.org/sdr/20000427SH030.md): Hub · cracked · Mar 21, 2000 · N7542Q · Cessna T310Q · Propeller Hub Section > RAM A/C ENGINE AND PROPELLER MODIFICATIONS PER STC NR SA 4011SW. (X) - [SDR 2000ZZZX225](https://openairdocs.org/sdr/2000ZZZX225.md): Fitting · unapproved part · Nov 29, 1999 · N767RR · Cessna T310Q · Wing Miscellaneous Structure > NOTE: FITTING WAS STEEL SUBMITTER STATED FITTING LOOKED HOMEMADE. INSTALLED FORGED NEW CORRECT CESSNA PART MADE FORM ALUMINUM. PART TOTAL TIME UNKNOWN. - [SDR 2000ZZZX224](https://openairdocs.org/sdr/2000ZZZX224.md): Deice System · inoperative · Nov 29, 1999 · N767RR · Cessna T310Q · Airfoil Anti/De-ice System > NOTED THAT DE-ICE FOR VERTICAL STABILIZER INOPERATIVE. FURTHER INVESTIGATION REVEALS HOSES TIED OFF. REPLACED HOSES, PATCHED BOOT. OPS CHECKED, WORKS FINE. TOATL TIME AT INSTALLATION UNKNOWN. - [SDR EY2R9600334](https://openairdocs.org/sdr/EY2R9600334.md): Blade · corroded · Feb 1, 1996 · Cessna T310Q · Propeller Blade Section > BLADE, SN F45244YS, FOUND CORRODED. - [SDR EY2R9600333](https://openairdocs.org/sdr/EY2R9600333.md): Blade · corroded · Feb 1, 1996 · Cessna T310Q · Propeller Blade Section > BLADE, SN F45225YS, FOUND CORRODED. - [SDR EY2R9600332](https://openairdocs.org/sdr/EY2R9600332.md): Blade · corroded · Feb 1, 1996 · Cessna T310Q · Propeller Blade Section > BLADE, SN F45471YS, FOUND CORRODED. - [SDR EY2R9600331](https://openairdocs.org/sdr/EY2R9600331.md): Hub · corroded · Feb 1, 1996 · Cessna T310Q · Propeller Hub Section > HUB FOUND CORRODED. - [SDR EY2R9600326](https://openairdocs.org/sdr/EY2R9600326.md): Hub · corroded · Feb 1, 1996 · Cessna T310Q · Propeller Hub Section > HUB FOUND CORRODED. - [SDR EY2R9600322](https://openairdocs.org/sdr/EY2R9600322.md): Ferrule · corroded · Feb 1, 1996 · Cessna T310Q · Propeller Assembly > CORROSION FOUND ON FERRULE. - [SDR EY2R9600320](https://openairdocs.org/sdr/EY2R9600320.md): Feather Cylinder · corroded · Feb 1, 1996 · Cessna T310Q · Propeller Assembly > FEATHER CYLINDER FOUND WITH CORROSION. - [SDR EY2R9600317](https://openairdocs.org/sdr/EY2R9600317.md): Retain Bearing · corroded · Feb 1, 1996 · Cessna T310Q · Propeller Assembly > RETAIN BEARING FOUND CORRODED. - [SDR 95ZZZX3227](https://openairdocs.org/sdr/95ZZZX3227.md): Exhaust Riser · hole burned · Jun 1, 1995 · N7584Q · Cessna T310Q · Engine Collector/Tailpipe/Nozzle > DURING DEPARTURE CLIMB, THE EXHAUST RISER ON THE LEFT ENGINE NR 2 CYLINDER DEVELOPED A HOLE ON THE LOWER SIDE. PRIOR TO THE FAILURE OF THE PART IT APPEARED TO BE IN GOOD CONDITION. DURING THE PRECEDING FEW HOURS OF FLIGHT THE AIRCRAFT WAS USED FOR FLIGHT TRA ## 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 = 'T310Q' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/cessna-t310q/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.