# Service difficulty reports: Cessna 310Q

A list on [Cessna 310Q](https://openairdocs.org/model/cessna-310q.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 146 reports

- [SDR 2015FA0000159](https://openairdocs.org/sdr/2015FA0000159.md): Washer · missing · Mar 27, 2015 · N69HB · Cessna 310Q · Aileron Control System
  > RIGHT AILERON CONTROL PUSHROD FOUND MISSING WASHERS, ITEM 62 IN IPC PRINTOUT. THESE ACT AS SPACERS, AND WHEN MISSING CAUSE THE STRUCTURE TO SQUEEZE TOGETHER CAUSING AILERON SKIN WRINKLING AND POSSIBLE DAMAGE.
- [SDR 2014FA0000295](https://openairdocs.org/sdr/2014FA0000295.md): Heater · fire · Mar 8, 2014 · N69980 · Cessna 310Q · Heating System
  > NOSE COMPARTMENT WAS DISCOLORED, PAINT BLISTERED, EVIDENCE OF A FIRE IN THE COMPARTMENT.
- [SDR ESMR2013122001](https://openairdocs.org/sdr/ESMR2013122001.md): Window · departed · Dec 19, 2013 · N69728 · Cessna 310Q · Emergency Exits
  > THE EMERGENCY EXIT WINDOW, WHICH IS THE PILOT'S SIDE WINDOW, DEPARTED THE AIRCRAFT IN CRUISE FLIGHT AT 4,500 FEET. THE WINDOW DID NOT STRIKE ANY AIRCRAFT STRUCTURE OR CONTROL SURFACE. THE AIRCRAFT FLEW NORMALLY AND THE PILOT DID NOT EXPERIENCE ANY OTHER DIFFIC
- [SDR 2013FA0000039](https://openairdocs.org/sdr/2013FA0000039.md): Isolator · failed · Jan 19, 2013 · N466Q · Cessna 310Q · Engine Mount Section
  > DURING INSPECTION FOUND LT ENGINE, LT FORWARD AND LT REAR ENGINE MOUNT ISOLATOR DEFORMED, SAGGING AND JUMPED OUT OF AIRFRAME MOUNT. ALLOWS ENGINE TO SAG AND INTAKE MANIFOLD, AND EXHAUST PIPE TO CONTACT ACFT STRUCTURE. LT FORWARD ISOLATOR HAD BEEN INSTALLED
- [SDR EAVR20110816001](https://openairdocs.org/sdr/EAVR20110816001.md): Cylinder Head · cracked · Aug 15, 2011 · N316RA · Cessna 310Q · Reciprocating Engine Cylinder Section
  > AIRCRAFT LEVELED OFF FROM CRUISE CLIMB. ACFT WAS ALLOWED TO ACCELERATE TO CRUISE SPEED. POWER WAS SET TO CRUISE POWER SETTINGS OF 23/23 IN MP AND 2300/2300 RPM. FUEL FLOW WAS SET AT 12/12 GPH. APPROX 10 MINUES LATER, A SLIGHT JOLT WAS FELT WITH A CONTINUED SL
- [SDR MLJG20010613](https://openairdocs.org/sdr/MLJG20010613.md): Piston · broken · Jun 13, 2011 · N790DM · Cessna 310Q · Reciprocating Engine Power Section
  > WHEN REMOVING RT ENGINE NR 4 CYLINDER DUE TO A CRACK, NR 4 PISTON SKIRT FOUND BROKE OFF AT THE 4TH RING LAND. ENGINE THEN REMOVED FROM ACFT FOR TEAR-DOWN INSPECTION. I HAVE FOUND BROKEN PISTON SKIRTS ON THIS PARTICULAR ACFT ON 3 DIFFERENT ENGINES.
- [SDR 2011F00142](https://openairdocs.org/sdr/2011F00142.md): Mount · damaged · Jun 13, 2011 · N790DM · Cessna 310Q · Engine Mount Section
  > LEFT AND RIGHT ENGINE, BOTH FRONT MOUNT UPPER HALVES COMPRESSED EXCESSIVELY. THE LT FRONT MOUNT ON THE LT AND RT ENGINE WERE EXPOSING.2500" OF INNER BARREL. SUBSEQUENTLY, THE LT ENGINE NR 6 CYLINDER HEADER TUBE RUBBED THE ENGINE BEAM EXTENSION. IT HAS NOT BE
- [SDR 2010FA0000268](https://openairdocs.org/sdr/2010FA0000268.md): Downlock · lack of lube · Mar 24, 2010 · N5LH · Cessna 310Q · Landing Gear Retraction/Extension System
  > RT LANDING GEAR FAILED TO FULLY EXTEND AND LOCK. THE RT DOWNLOCK PN 5041018-1 SEIZED DUE TO LACK OF LUBRICATION. THE DOWN LOCK ROD END PN KWBS WAS ALSO SEIZED FOR THE SAME REASON. THE WEIGHT OF THE ACFT ON THE PARTIALLY EXTENDED GEAR PULLED THE BELLCRANK BRA
- [SDR 2009FA0000746](https://openairdocs.org/sdr/2009FA0000746.md): Cylinder Head · broken · Aug 24, 2009 · N316RA · Cessna 310Q · Reciprocating Engine Cylinder Section
  > CYLINDER HEAD SEPARATED FROM BARREL.
- [SDR 2008FA0000623](https://openairdocs.org/sdr/2008FA0000623.md): Skin · cracked · Sep 5, 2008 · N100EL · Cessna 310Q · Wing, Plate/Skin
  > FOUND CRACK IN UPPER WING SKIN AS DESCRIBED IN SB MEB08-3. CRACK EXTENDS 4 INCHES FORE AND AFT PARALLEL TO LT WING MAIN LANDING GEAR ASIDE BRACE WING RIB NR 502210451 OB FLANGE. CRACK IS APPROXIMATELY CENTERED IN MLG WHEEL WELL OPENING. CRACK WAS FOUND VISUAL
- [SDR MLJ2008F00000](https://openairdocs.org/sdr/MLJ2008F00000.md): Piston · failed · Jan 14, 2008 · N790DM · Cessna 310Q · Reciprocating Engine Cylinder Section
  > THE LT ENGINE WAS EXHIBITING LOW OIL PRESSURE. THE OIL FILTER WAS PULLED, CUT OPEN, AND INSPECTED. A SIGNIFICANT AMOUNT OF METAL WAS FOUND. THE ENGINE WAS THEN TORN DOWN FOR FURTHER INSPECTION. CHUNKS OF PISTON SKIRTING WAS FOUND IN THE OIL PAN, NR 2 PISTO
- [SDR 2007FA0000908](https://openairdocs.org/sdr/2007FA0000908.md): Stop · broken · Sep 19, 2007 · N20SS · Cessna 310Q · Landing Gear Retraction/Extension System
  > PILOT HAD NO LT GEAR DOWN INDICATION. HE CYCLED GEAR WITH NO SUBSEQUENT GEAR DOWN INDICATION. HE ATTEMPTED MANUAL EXTENSION, CRANKED TO THE MECHANICAL STOP IN THE GEARBOX AND BROKE THE STOP. BELLCRANK CONTINUED PAST DOWN AND THEN WENT PARTIALLY (UP). GEAR
- [SDR MLJ2006F00000](https://openairdocs.org/sdr/MLJ2006F00000.md): Clevis Pin · missing · Oct 17, 2006 · N790DM · Cessna 310Q · Landing Gear Doors
  > COTTER PIN CAME OUT OF CLEVIS PIN ITEM NR 5 OR CLEVIS PIN FAILED ATTACHING NOSE GEAR DOOR PUSH PULL TUBE TO THE EYE BOLT ON THE LT NOSE GEAR DOOR. ON TAKE OFF THE LT GEAR DOOR BLEW SHUT. WHEN GEAR WAS RETRACTED THE NOSE GEAR JAMMED HALF WAY UP, BREAKING BELL
- [SDR 2006FA0000925](https://openairdocs.org/sdr/2006FA0000925.md): Spar Cap · corroded · Sep 17, 2006 · N69704 · Cessna 310Q · Wing Spar
  > DURING THE ANNUAL INSPECTION, FOUND UPPER AND LOWER REAR SPAR DAMAGE ON THIS AIRCRAFT. THIS DAMAGE IS DUE TO CORROSION ON THE UPPER AND LOWER REAR SPAR CAPS. THE UPPER REAR SPAR CAP DAMAGE IS LOCATED ON THE FORWARD SIDE OF THE REAR SPAR CAP EXTENDING IB FROM
- [SDR 2006FA0000907](https://openairdocs.org/sdr/2006FA0000907.md): Motor · failed · Aug 22, 2006 · N7940Q · Cessna 310Q · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT EXTEND ELECTRICALLY ON APPROACH. OPERATIONS NORMAL WHEN LANDING GEAR EXTENDED WITH MANUAL EMERGENCY EXTENSION SYS. FOUND LANDING GEAR ACTUATOR MOTOR INOPERATIVE. WOULD MAKE NOISE BUT NOT ROTATE. REPLACED MOTOR WITH OVERHAULED REPLACEM
- [SDR CA060821002](https://openairdocs.org/sdr/CA060821002.md): Wire Harness · wrong part · Aug 15, 2006 · Cessna 310Q · Propeller Feathering/Reversing
  > (CAN) HARNESS TOO SHORT WOULD NOT ALLOW PROPELLER TO FEATHER. PILOT COULD NOT FEATHER LT OR RT PROPELLERS DURING TRAINING FLIGHT. WRONG PROPELLER DEICE WIRING HARNESSES FOUND INSTALLED AND REPLACED WITH CORRECT P/N D5855-1. (TC NR 20060821002)
- [SDR 2006FA0000753](https://openairdocs.org/sdr/2006FA0000753.md): Torque Tube · damaged · Jul 18, 2006 · N119RS · Cessna 310Q · Rudder Structure
  > RT RUDDER TORQUE TUBE RIPPED AT RUDDER CABLE BRACKET. INSPECT THIS AREA NEXT TO WELD. (K)
- [SDR CA060602003](https://openairdocs.org/sdr/CA060602003.md): Throttle Cable · broken · Jun 2, 2006 · Cessna 310Q · Fuel Control/Reciprocating Engines
  > (CAN) DOING UPPER AIR WORK, IT WAS NOTICED THEIR WAS NO THROTTLE RESPONSE FROM RT ENGINE. THE ENGINE WAS RUNING NORMAL SO THE CREW RETURNED TO AIRPORT AND DID A NORMAL LANDING AND SHUTDOWN OF ENGINE ON TOUCHDOWN. MAINTENANCE FOUND THE THROTTLE CABLE BROKEN AT
- [SDR AU510001703](https://openairdocs.org/sdr/AU510001703.md): Bellcrank · sheared · Dec 12, 2005 · Cessna 310Q · Nose/Tail Landing Gear
  > NOSE LANDING GEAR IDLER BELLCRANK SHEARED AT THE TWO BOLT HOLES FOR THE FORWARD AND AFT PUSH-PULL TUBES. SUSPECT CAUSED BY WORN UPLOCK.
- [SDR 2005FA0000890](https://openairdocs.org/sdr/2005FA0000890.md): Cylinder · cracked · Jun 1, 2005 · N1249G · Cessna 310Q · Reciprocating Engine Cylinder Section
  > FOUND CASE CRACKED BEYOND REPAIR AT NR 1 CYLINDER, FOUND 2 THRU BOLTS SHEARED AND 5 CYLINDER STUDS BROKEN ON NR 1 CYLINDER. THRU BOLTS DEFECTIVE CAUSING A CHAIN REACTION IN SHEARING CYLINDER STUDS. SINCE CYLINDER WAS NO LONGER SEATED SQUARELY TO THE CASE, TH
- [SDR CA050224005](https://openairdocs.org/sdr/CA050224005.md): Clamp · obstructed · Feb 15, 2005 · Cessna 310Q · Aileron Control System
  > (CAN) WHEN THE AILERON CONTROL WAS MOVED TO THE EXTREME LT, THE CONTROL WOULD OCCASIONALLY CATCH MOMENTARILY AND THEN RELEASE. UPON FURTHER EXAMINATION OF THE AILERON CONTROL SYSTEM, THE AUTOPILOT CLAMP ON THE LT AILERON CABLE WAS FOUND TO BE CATCHING ON THE D
- [SDR 2004FA0000387](https://openairdocs.org/sdr/2004FA0000387.md): Adapter · backed out · May 7, 2004 · N3310D · Cessna 310Q · Fuel Injector Nozzle
  > 2 FUEL INJECTION NOZZLE ADAPTERS BACKED OUT WITH FUEL NOZZLES.
- [SDR AUS20040134](https://openairdocs.org/sdr/AUS20040134.md): Torque Tube · broken · Jan 14, 2004 · Cessna 310Q · Landing Gear Retraction/Extension System
  > (AUS) LT MAIN LANDING GEAR TORQUE TUBE BROKEN.
- [SDR T0DR200300002](https://openairdocs.org/sdr/T0DR200300002.md): Fairlead · broken · Aug 9, 2003 · N122E · Cessna 310Q · Rudder Control System
  > RUDDER JAMMED UPON ROTATION. (RUDDER SYS JAM) CHECKLIST. ALL KNOWN SYSTEMS SUSPECTED OF HAVING BRG ON RUDDER SYS. ALL OTHER FLIGHT CONTROL SYS OPERATED NORMALLY AND AC CONTROL WAS NEVER IN DOUBT. EMERG WAS DECLARED, 2 TOWER FLY-BYS WERE EXECUTED TO ALLOW TO
- [SDR 2003F00331](https://openairdocs.org/sdr/2003F00331.md): Screw · broken · May 29, 2003 · N589DM · Cessna 310Q · Main Landing Gear Attach Section
  > ON LANDING ROLLOUT AT 30 KNOTS, THE RIGHT MAIN LANDING GEAR COLLAPSED CAUSING RIGHT PROP TO STRIKE THE GROUND. THE ADJUSTMENT SCREW PN 0841111-1 BROKE. A SPAS PN QUERY SHOWED NO OTHER ACCIDENTS OR INCIDENTS.
- [SDR 2004FA0000096](https://openairdocs.org/sdr/2004FA0000096.md): Bearing · failed · May 25, 2003 · N3310D · Cessna 310Q · Nose/Tail Landing Gear
  > NOSE GEAR STRUT JAMMED AT NORMAL EXTENSION. ON RETRACTION NOSE GEAR JAMS ON NOSE GEAR DOOR HINGES AND CAUSES NOSE GEAR BELLCRANK TO BREAK. ACTUAL PROBLEM IS DUE TO STRUT UPPER BEARING FAILURE, BUT COULD EASILY BE MISDIAGNOSED AS A DEFECTIVE BELLCRANK. IT IS
- [SDR CA030324003](https://openairdocs.org/sdr/CA030324003.md): Bellcrank · cracked · Mar 10, 2003 · Cessna 310Q · Landing Gear Steering System
  > (CAN) UPON INSPECTION, FOUND STEERING BELLCRANK CRACKED IN RADIUS, SEVERAL LOCATIONS. NOTE: THE NEW BELLCRANK INSTALLED IS A HEAVIER UNIT.
- [SDR 2003F00103](https://openairdocs.org/sdr/2003F00103.md): Line · failed · Dec 20, 2002 · N591DM · Cessna 310Q · Fuel Flow Indicating
  > FULE LEAK IN COCKPIT, PILOT DECLARED EMERGENCY AND RETURNED TO FARMINGTON, NM AIRPORT. RIGHT FUEL FLOW GAUGE INDICATION WENT TO ZERO. REMOVED AND REPLACED RIGHT FUEL FLOW GAUGE PRESSURE LINE P/N CM2944-2-18.
- [SDR 2002FA0001385](https://openairdocs.org/sdr/2002FA0001385.md): Bellcrank · broken · Aug 14, 2002 · N120SA · Cessna 310Q · Landing Gear Retraction/Extension System
  > UPON GEAR EXTENSION, BELLCRANK FAILED. ALL ATTEMPTS TO EXTEND NOSE GEAR FAILED. AIRCRAFT LANDED WITH NOSE GEAR AT 45 DEGREE ANGLE. DAMAGE TO NOSE GEAR AREA.
- [SDR EA42002F00000](https://openairdocs.org/sdr/EA42002F00000.md): Valve · broken · Jan 2, 2002 · N100CP · Cessna 310Q · Vacuum Distribution System
  > RUBBER FLAPPER BROKE OFF AND BLOCKED VACUUM INLET FROM RIGHT VACUUM PUMP. THEN RIGHT ENGINE WAS OPERATED ALONE, BOTH FAIL INDICATORS WERE OUT AND VACUUM INDICATED (0)ZERO. WHEN LEFT ENGINE WAS OPERATED ALONE BOTH INDICATORS WERE IN AND VACUUM INDICATED 5.0
- [SDR 2002FA0000089](https://openairdocs.org/sdr/2002FA0000089.md): Strut · broken · Nov 19, 2001 · N8TC · Cessna 310Q · Entrance Stairs
  > MAINTENANCE PERSONNEL ATTEMPTED TO BOARD AIRCRAFT WHEN MOUNTING STEP STRUT ASSEMBLY BROKE AWAY. WELD ASSEMBLY (PN 0811946-23) FAILED COMPLETELY AT UPPER STEP. INDICATIONS OF A PRE EXISTING CRACK AROUND ONE THIRD OF THE CIRCUMFERENCE OF THE TUBE. NO SIGNS OF
- [SDR CA011105006](https://openairdocs.org/sdr/CA011105006.md): Link Rod · disconnected · Oct 1, 2001 · Cessna 310Q · Fuel Control/Turbine Engines
  > (CAN) ON APPROACH PILOT NOTICED ROUGHNESS FROM LEFT ENGINE AND UPON LANDING REPORTED THAT THE LEFT ENGINE WOULD NOT IDLE UNLESS MIXTURE PULLED BACK HALFWAY. INSPECTION REVEALED THAT THE COTTER PIN WHICH HOLD THE MIXTURE INTERCONNECT ROD TO THE THROTTLE VALVE H
- [SDR 20010502CW002](https://openairdocs.org/sdr/20010502CW002.md): Throttle Control · broken · Apr 11, 2001 · N121LA · Cessna 310Q · Power Lever
  > DURING APPROACH FOR LANDING, RIGHT ENGINE THROTTLE CONTROL MOVEMENT HAD NO RESPONSE IN ENGINE POWER. CONTROL FELT NORMAL. ENGINE FEATHERED AND AIRCRAFT MADE A NORMAL LANDING. INSPECTION REVEALED THROTTLE CABLE BROKE ABOUT 12 INCHES AFT OF THROTTLE ASSEMBLY.
- [SDR BJ3RE000007](https://openairdocs.org/sdr/BJ3RE000007.md): Exhaust Valve · worn · Feb 26, 2001 · N69604 · Cessna 310Q · Reciprocating Engine Cylinder Section
  > DURING AN IRAN INSPECTION, IT WAS NOTICED THAT THE AMOUNT OF VALVE SHOWING ABOVE THE KEEPER WAS LESS ON ONE CYINDER THAN ON THE OTHERS. UPON DISASSEMBLY IT WAS FOUND THAT #3 CYLINDER EXHAUST VALVE WAS 1/16TH INCH SHORTER THAN THE OTHER VALVES. A SLIGHT MUSHRO
- [SDR 20001207SH016](https://openairdocs.org/sdr/20001207SH016.md): Torque Tube · cracked · Nov 21, 2000 · N8TC · Cessna 310Q · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, PILOT ADVISED BY GROUND OBSERVERS, LT MLG STILL DOWN. GEAR CYCLED SEVERAL TIMES, GROUND OBSERVERS REPORTED LT MAIN GEAR STILL DOWN. GEAR SELECTED DOWN, SAFE LANDING. INSP SHOWED LT M/G TORQUE TUBE, PN 5045010-19, CRACKED, FAILED. CRACK APPEA
- [SDR 20001011SH005](https://openairdocs.org/sdr/20001011SH005.md): Pump · failed · Oct 7, 2000 · N69572 · Cessna 310Q · Fuel Boost Pump
  > DURING FLIGHT, PILOT NOTICED LEFT LANDING LIGHT CIRCUIT BREAKER OPEN. AFTER LANDING, INSP FOUND LEFT TIP TANK FUEL TRANSFER PUMP P/N 476411 FAILED ELECTRICALLY. PUMP SHOWED SIGNS OF HEAT AND ARCING ON OUTSIDE OF CASE FROM INTERNAL FAILURE. THIS PUMP IS WIR
- [SDR 20000912SH024](https://openairdocs.org/sdr/20000912SH024.md): Trunnion · failed · Aug 25, 2000 · N8403F · Cessna 310Q · Main Landing Gear Strut/Axle/Truck
  > AFTER LANDING AND WHILE TURNING LEFT OFF OF RUNWAY ONTO TAXIWAY, RIGHT GEAR COLLAPSED. FOUND RIGHT GEAR TRUNNION UPPER BARREL TO BELLCRANK CASTING FAILED AND THE LOWER SIDE LINK SEPARATED AT ADJUSTMENT BOLT. POSSIBLE CAUSE: LOWER SIDE LINK ADJUSTMENT BOLT S
- [SDR CA990915072](https://openairdocs.org/sdr/CA990915072.md): Camshaft · spalling · Sep 9, 1999 · Cessna 310Q · Reciprocating Engine Power Section
  > (CAN) SEVERE SPALLNG OF REAR CAM LOBE.
- [SDR 99ZZZX3174](https://openairdocs.org/sdr/99ZZZX3174.md): Hub · misrepaired · Aug 6, 1999 · Cessna 310Q · Propeller Hub Section
  > THE HUB WAS DEEMED UNAIRWORTHY DUE TO IMPROPER PROCEDURES WHEN MODIFYING THE RETENTION NUTS DURING C/W AD NOTE 95-24-05R1.
- [SDR 99ZZZX2757](https://openairdocs.org/sdr/99ZZZX2757.md): Pump · failed · Jul 13, 1999 · N69980 · Cessna 310Q · Fuel Boost Pump
  > MAIN FUEL TRANSFER PUMP IN RIGHT WING FAILED DUE TO SHORTING OF POSITIVE WIRE TO GROUNDING SHIELDED WIRE. FAILURE OCCURRED IN FLIGHT. SUBMITTER STATED CAUSE UNKNOWN.
- [SDR 99ZZZX2127](https://openairdocs.org/sdr/99ZZZX2127.md): Exit · misinstalled · Apr 29, 1999 · N1562T · Cessna 310Q · Emergency Exits
  > WHILE INSPECTING AIRCRAFT FOR FERRY FLIGHT, FOUND EMERGENCY EXIT WAS SEALED SHUT AND THERE WAS NO EVIDENCE, IT HAD EVER BEEN TESTED AS REQUIRED ON 100-HOUR/ANNUAL INSPECTIONS. RETURNED AIRCRAFT TO CUSTOMER AS IS. CUSTOMER/OPERATOR ADVISED EMERGENCY EXIT NEED
- [SDR 99ZZZX1941](https://openairdocs.org/sdr/99ZZZX1941.md): Duct · failed · Apr 28, 1999 · N100TG · Cessna 310Q · Engine Air Intake System
  > DURING TAKEOFF, EXPERIENCED LOSS OF POWER ON THE ELFT ENGINE. WHEN THE POWER LEVER WAS REDUCED, THE ENGINE WANTED TO RUN BETTER. AN UNEVENTFUL LANDING WAS MADE. THE 4.25 INCH DUCT FROM THE WING LEADING EDGE TO THE ENGINE COMPARTMENT WAS DETERIORATED AND ONE
- [SDR AU990444](https://openairdocs.org/sdr/AU990444.md): Trunnion · cracked · Apr 16, 1999 · Cessna 310Q · Nose/Tail Landing Gear Attach Section
  > (AUS) NOSE LANDING GEAR TRUNNION CRACKED IN ONE PIVOT AS INDICATED IN AAC1-108.
- [SDR 99ZZZX1947](https://openairdocs.org/sdr/99ZZZX1947.md): Filter · leaking · Apr 12, 1999 · N69622 · Cessna 310Q · Reciprocating Engine Oil System
  > ROUTINE OIL CHANGE, FILTER STARTED LEAKING AT BASE. LOOKS LIKE CRACK OR SMALL PERFORATIONS WHERE HOUSING IS CRIMPED/WELDED TO END PLATE. INSPECTED INVENTORY, NONE OTHERS FOUND. (KEYSTONE AERIAL SURVEYS).
- [SDR 99ZZZX2079](https://openairdocs.org/sdr/99ZZZX2079.md): Bracket · damaged · Mar 23, 1999 · N1312G · Cessna 310Q · Elevator Control System
  > BOLT HOLES THROUGH BRACKETS, WHICH SUPPORT ELEVATOR BELLCRANK, ELONGATED FORWARD. NOTED DURING ANNUAL INSPECTION. POSSIBLE CAUSE IS TENSION EXERTED ON BRACKETS BY CABLE TENSION AND CONSTANT FORWARD STRESS CAUSED BY USE OF THE ELEVATORS.
- [SDR 99ZZZX2078](https://openairdocs.org/sdr/99ZZZX2078.md): Bracket · damaged · Mar 23, 1999 · N1312G · Cessna 310Q · Elevator Control System
  > BOLT HOLES THROUGH BRACKETS, WHICH SUPPORT ELEVATOR BELLCRANK, ELONGATED FORWARD. NOTED DURING ANNUAL INSPECTION. POSSIBLE CAUSE IS TENSION EXERTED ON BRACKETS BY CABLE TENSION AND CONSTANT FORWARD STRESS CAUSED BY USE OF THE ELEVATORS.
- [SDR 99ZZZX1411](https://openairdocs.org/sdr/99ZZZX1411.md): Torque Tube · cracked · Mar 5, 1999 · N69836 · Cessna 310Q · Landing Gear Retraction/Extension System
  > RT AND LT MLG TORQUE TUBES WERE REMOVED DURING INSTALLATION OF SK414-8E. BOTH WERE FOUND CRACKED AT THE WELD AREA FOR THE FORK BOLT BOSS.
- [SDR 99ZZZX1410](https://openairdocs.org/sdr/99ZZZX1410.md): Torque Tube · cracked · Mar 5, 1999 · N69836 · Cessna 310Q · Landing Gear Retraction/Extension System
  > RT AND LT MLG TORQUE TUBES WERE REMOVED DURING INSTALLATION OF SK414-8E. BOTH WERE FOUND CRACKED AT THE WELD AREA FOR THE FORK BOLT BOSS.
- [SDR 98ZZZX4246](https://openairdocs.org/sdr/98ZZZX4246.md): Wheel · damaged · Oct 27, 1998 · N88LT · Cessna 310Q · Wheel/Ski/Float
  > WHILE REPLACING TIRE, RIGHT INBOARD WHEEL HALF BEARING CONE WAS FOUND LOOSE IN HUB. PERSONS UNKNOWN HAD PREVIOUSLY ATTEMPTED TO STAKE CONE IN PLACE. WHEEL HALF WAS REJECTED DUE TO OVERSIZE BORE AND DAMAGE FROM STAKING ATTEMPT. SUBMITTER STATED CAUSE AS IMPR
- [SDR 98ZZZX4245](https://openairdocs.org/sdr/98ZZZX4245.md): Stringer · corroded · Oct 27, 1998 · N88LT · Cessna 310Q · Wing, Longeron/Stringer
  > DURING ANNUAL INSPECTION, STRING IN LEFT WING UPPER SKIN NACELLE AREA STA 80.0L WAS FOUND WITH EXFOLIATION CORROSION. INBOARD 8 INCHES OF STRINGER WAS REPLACED.

Next page: https://openairdocs.org/model/cessna-310q/reports.md?page=2

## 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 = '310Q'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-310q/reports

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