# Service difficulty reports: Cessna 310R

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

Newest first. General aviation reporting is voluntary.

Page 1 of 11 · 518 reports

- [SDR 2026FA0000607](https://openairdocs.org/sdr/2026FA0000607.md): Skin · cracked · Jul 28, 2026 · N1342G · Cessna 310R · Wing, Plate/Skin
  > LEFT AND RIGHT UPPER WING SKIN CRACKS PER CESSNA MEB08-3.
- [SDR 2026FA0000606](https://openairdocs.org/sdr/2026FA0000606.md): Rib · cracked · Jul 28, 2026 · N1342G · Cessna 310R · Fuselage, Landing Gear Attach Fittings
  > LEFT AND RIGHT MAIN LANDING GEAR SIDE BRACE RIBS CRACKED PER CESSNA ME76-2
- [SDR 2026FA0000605](https://openairdocs.org/sdr/2026FA0000605.md): Bellcrank · cracked · Jul 28, 2026 · N1342G · Cessna 310R · Landing Gear Steering System
  > CRACKED NOSE GEAR STEERING BELL CRANK. (OLD STYLE BELL CRANKS FREQUENTLY)
- [SDR 2026FA0000433](https://openairdocs.org/sdr/2026FA0000433.md): Alternator · inoperative · May 27, 2026 · N506DR · Cessna 310R · AC Generator-Alternator
  > THE PILOT REPORTED THE LH ALTERNATOR FAILURE LIGHT ILLUMINATED IN FLIGHT, WITH THE LH ALTERNATOR INDICATING NO ELECTRICAL OUTPUT. THE ALTERNATOR WAS INSTALLED ON 05/20/2025 AT AN AIRFRAME TOTAL TIME OF 4939.8 HOURS AND WAS REMOVED AS INOPERATIVE ON 05/14/2026.
- [SDR 2026FA0000257](https://openairdocs.org/sdr/2026FA0000257.md): Attach Bolt · sheared · Apr 6, 2026 · N310AC · Cessna 310R · Main Landing Gear
  > EXPERIENCED A RIGHT MAIN GEAR COLLAPSE DURING LANDING ROLLOUT. FURTHER EXAMINATION OF THE COLLAPSE IDENTIFIED A BOLT AND THE BELLCRANK HAVING SHEARED/BROKEN.
- [SDR 7RKR2024043001](https://openairdocs.org/sdr/7RKR2024043001.md): Muffler · separated · Apr 29, 2024 · N1274G · Cessna 310R · Engine Noise Suppressor
  > DURING VISUAL INSPECTION PRIOR TO MAINTENANCE RH MUFFLER OF LH ENGINE WAS FOUND TO BE COMPLETELY SEPARATED FROM FORWARD PIVOT ADAPTER TUBE AT TUBE-TO-MUFFLER WELD. THE WELD HAD FAILED THE COMPLETE CIRCUMFERENCE OF THE MUFFLER-TUBE JOINT. THERE WAS EVIDENC
- [SDR W59R15956](https://openairdocs.org/sdr/W59R15956.md): Bearing · failed · Sep 29, 2022 · N310LA · Cessna 310R · Propeller Governor
  > LEFT ENGINE ON AIRCRAFT WOULD NOT MAKE RPM OR CYCLE PROPELLER. BA59 BEARING FOUND IN LEFT ENGINE GOVERNOR, THIS UNIT THE RIGHT ENGINE PROPELLER GOVERNOR REMOVED TO INSPECT AS PRECAUTION AND TO COMPLY WITH AD 2020-19-06 AND MCCAULEY ASB273C. THIS GOVERNOR
- [SDR W59R15971](https://openairdocs.org/sdr/W59R15971.md): Bearing · failed · Sep 29, 2022 · N310LA · Cessna 310R · Propeller Governor
  > ENGINE WOULD NOT MAKE RED LINE RPM OR CYCLE. GOVERNOR REMOVED, DRIVE GEAR WOULD NOT TURN. GOVERNOR DISASSEMBLED AND FOUND BA59 BEARING FAILED AS DESCRIBED IN AD 2020-19-06 AND MCCAULEY ASB273C. GOVERNOR OVERHAULED 30/NOV/2017 USING A NEW MCCAULEY A20107 IDLER
- [SDR 2021FA0000344](https://openairdocs.org/sdr/2021FA0000344.md): None · broken · Nov 21, 2021 · N2738B · Cessna 310R · Landing Gear System
  > RIGHT MAIN GEAR COLLAPSE ON LANDING. DOWNLOCK BELLCRANK, PN 5041001-11, WAS FOUND TO BE BROKEN.
- [SDR MLJA20210000250](https://openairdocs.org/sdr/MLJA20210000250.md): Hsi · out of limits · Aug 21, 2021 · N3284M · Cessna 310R · Attitude and Direction Data System
  > UPON DEPARTURE THE HSI SHOWED 60 DEGREES OFF ACTUAL HEADING. RE-SLAVE ATTEMPT UNSUCCESSFUL. NOTIFIED ATC AND RETURNED TO FIELD. LANDED WITHOUT INCIDENT. RE-CENTERED HSI. OPERATIONAL CHECK SATISFACTORY.
- [SDR W1XA20210614](https://openairdocs.org/sdr/W1XA20210614.md): Engine · failed · Jun 14, 2021 · N196TC · Cessna 310R · Engine (Reciprocating)
  > PILOT DEPARTED KANE, WHILE CLIMBING THROUGH 2,700', LEFT ENGINE DEVELOPED A VIBRATION. WHILE SCANNING ENGINE INSTRUMENTS HE NOTICED THE LEFT ENGINE OIL PRESSURE WAS AT ZERO PSI. PILOT TURNED AROUND TO RETURN TO KANE AIRPORT AND BEGAN ENGINE SHUT DOWN PROCEDURE
- [SDR CSLR20200314991](https://openairdocs.org/sdr/CSLR20200314991.md): Line · corroded · Mar 14, 2020 · N712CP · Cessna 310R · Heating System
  > PASSENGER IN CO PILOT SEAT NOTICED FUEL SMELL IN FLIGHT WITH COMBUSTION HEATER OPERATIONAL.HEATER WAS SECURED AND FUEL SMELL WENT AWAY.PILOT LEFT COMBUSTION HEATER SECURED AND AIRCRAFT WAS BROUGHT IN FOR INSPECTION. LOWER RIGHT UPHOLSTERY PANEL WAS REMOVED TO
- [SDR IKBR202002119093](https://openairdocs.org/sdr/IKBR202002119093.md): Tube · corroded · Jan 22, 2020 · N312CS · Cessna 310R · Trailing Edge Flap Control System
  > WHILE REPLACING THE FLAP CONTROL CABLES WE FOUND THE TUBE ASSY P/N 0862100-57 CORRODED AROUND THE INBOARD END. INSTALLED NEW ROD ASSY.
- [SDR IKBR201912129089](https://openairdocs.org/sdr/IKBR201912129089.md): Control Cable · broken · Nov 26, 2019 · N312CS · Cessna 310R · Trailing Edge Flap Control System
  > THIS IS THE PILOTS REPORT OF THE INCIDENT; WHILE AT 200' AGL ON FINAL APPROACH, THE RIGHT FLAPS ON THE C310R BEING FLOWN BECAME DISCONNECTED AND BLEW TO TRAIL. A SUDDEN RIGHT ROLL AND RIGHT YAW WAS FELT, WHICH WAS CORRECTED WITH NEAR FULL LEFT AILERON AND LEF
- [SDR 2020FA0000015](https://openairdocs.org/sdr/2020FA0000015.md): Bellcrank · failed · Nov 12, 2019 · N98904 · Cessna 310R · Nose/Tail Landing Gear
  > PILOT PLACED GEAR HANDLE IN THE DOWN POSITION, LOUD BANG, ALL 3 GEAR DOWN LIGHTS ILLUMINATED AND PILOT LANDED WITHOUT ISSUE. AFTER SHUT DOWN NOTICED LINKAGE HANGING FROM NOSE WHEEL WELL. THE NOSE GEAR TORQUE TUBE ADJUST INBD P/N 0842104-3 HAD FAILED AND THE
- [SDR 2020FA0000014](https://openairdocs.org/sdr/2020FA0000014.md): Pump · failed · Nov 12, 2019 · N6832Y · Cessna 310R · Vacuum Distribution System
  > VACUUM PUMP FAILED IN LESS THAN 10 HOURS OPERATION. PROBABLY CAUSED BY DE-ICE CONTROL. VALVE RELIEF PRESSURE SET AT 5 PSI, SHOULD BE SET AT 1.5 PSI TO PREVENT OVERWORKING VACUUM PUMP.
- [SDR 2019FA0000350](https://openairdocs.org/sdr/2019FA0000350.md): Bellcrank · broken · Oct 6, 2019 · N4941A · Cessna 310R · Landing Gear Retraction/Extension System
  > WHILE ON APPROACH TO LAND ANOTHER PILOT IN AN AIRPLANE HOLDING SHORT OF THE RUNWAY NOTICED THE RIGHT MAIN LANDING GEAR APPEARED TO NOT BE DOWN AND LOCKED AND NOTIFIED THE TOWER. THE PILOT OF THE 310 HEARD THE CALL AND ABORTED THE LANDING APPROACH AND PROCEEDED
- [SDR CA190521016](https://openairdocs.org/sdr/CA190521016.md): Engine · vibration · May 17, 2019 · Cessna 310R · Engine (Turbine/Turboprop)
  > (CAN) L/H ENGINE VIBRATION DURING RUN-UP (TC# 20190521016)
- [SDR N4CA2019012100002](https://openairdocs.org/sdr/N4CA2019012100002.md): Bellcrank · broken · Jan 17, 2019 · N71NC · Cessna 310R · Landing Gear Retraction/Extension System
  > BELLCRANK FORK ASSEMBLY BROKE WHILE EXTENDING THE LANDING GEAR FOR LANDING CAUSING THE NOSE GEAR TO NOT EXTEND. AIRCRAFT LANDED WITH MAIN GEAR ONLY.
- [SDR W1X2018F00000](https://openairdocs.org/sdr/W1X2018F00000.md): Torque Tube · failed · Jul 10, 2018 · N196TC · Cessna 310R · Landing Gear Retraction/Extension System
  > RIGHT MAIN LANDING GEAR COLLAPSED AFTER LANDING. PILOT MADE A LEFT TURN CAUSING RIGHT GEAR TO COLLAPSE. INSPECTION FOUND THE TORQUE TUBE BRACKET ASSEMBLY BROKEN AT THE PIVOT BEARING, CAUSING THE DOWN LOCK TENSION TO BE NONEXISTENT. FAILURE OF THE TORQUE RUB
- [SDR W1XA201806200001](https://openairdocs.org/sdr/W1XA201806200001.md): Gasket · collapsed · Jun 20, 2018 · N77RG · Cessna 310R · Reciprocating Engine Cylinder Section
  > AFTER TAKE OFF AND IN CLIMB OUT, THE TOWER REPORTED SMOKE TRAILING THE LEFT ENGINE. RETURNED TO DEPARTURE WITHOUT INCIDENT. REMOVED COWL AND FOUND OIL DRIPPING FROM THE NR 3 CYLINDER. FOUND THE GASKET ON THE NR 3 CYLINDER HAD COLLAPSED IN UPPER RIGHT CORNER.
- [SDR 2018FA0000087](https://openairdocs.org/sdr/2018FA0000087.md): Regulator · malfunctioned · Jan 8, 2018 · N68310 · Cessna 310R · AC Inverter
  > DETERMINED THE LEFT ALTERNATOR WAS OVERCHARGING THE SYSTEM RESULTING IN TRIPPING OF THE OVERVOLTAGE RELAY, DRAINING OF THE AIRCRAFT BATTERY, AND LOSS OF ELECTRICAL POWER. POSSIBLE CONTRIBUTING FACTORS TO THE LOSS OF POWER, SUNLIGHT ON THE INSTALLED LOW VOLTAG
- [SDR 7ILA2018F00000](https://openairdocs.org/sdr/7ILA2018F00000.md): Electrical Sys · failed · Jan 3, 2018 · N68310 · Cessna 310R · Electrical Power System
  > AIRCRAFT EXPERIENCED ELECTRICAL SYSTEM FAILURE RESULTING IN PILOT PERFORMING EMERGENCY LANDING.
- [SDR 2017FA0000119](https://openairdocs.org/sdr/2017FA0000119.md): Bellcrank · cracked · Mar 18, 2017 · N4258C · Cessna 310R · Landing Gear Door Retract Section
  > POST FLIGHT INSPECTION DISCOVERED RIGHT INBOARD MAIN LANDING GEAR DOOR IN THE OPEN POSITION. FOUND CRACKED BELLCRANK. NO ADVERSE EFFECTS NOTICED DURING THE PREVIOUS FLIGHT. NO ADDITIONAL NOISE OR VIBRATION. NO OBVIOUS CAUSE NOTED FOR FAILURE.REPLACED BELLCRA
- [SDR 20171212006](https://openairdocs.org/sdr/20171212006.md): Distributor Gear · worn · Dec 8, 2016 · N98904 · Cessna 310R · Magneto/Distributor
  > RIGHT ENGINE STARTED RUNNING A BIT ROUGH. VISUALLY INSPECTED MAGNETOS AND REMOVED RIGHT MAGNETO FOR INSPECTION. DISCOVERED WORN DISTRIBUTOR GEAR. REPLACED MAGNETO WITH OVERHAULED UNIT OF SAME TYPE.
- [SDR 7IL2016F00000](https://openairdocs.org/sdr/7IL2016F00000.md): Bellcrank · broken · Jul 27, 2016 · N80FA · Cessna 310R · Landing Gear Door Retract Section
  > PILOT REPORTED ENCOUNTERING SEVERE TURBULENCE UPON APPROACH TO LANDING. UPON RETURN TO BASE, PILOT NOTICED THAT RT INNER GEAR DOOR WAS HANGING OPEN. UPON FURTHER INSPECTION, FOUND BELLCRANK BROKEN, PN 08411066.
- [SDR 2015FA0000066](https://openairdocs.org/sdr/2015FA0000066.md): Seal · blew out · Feb 19, 2015 · Cessna 310R · Reciprocating Engine Front Section
  > ICE BUILDUP ON VENT TUBE CAUSED CRANKCASE PRESSURES TO INCREASE AND CRANKSHAFT SEAL TO PUSH ON RETAINERS TILL FAILURE. FLIGHT WAS AT NIGHT AND LEAK WAS NOT NOTICED TILL AFTER ACFT LANDED. THE ENGINE LOST 7 QUARTS OF OIL OF ITS 12 QUART OIL CAPACITY.
- [SDR MLJ2015F00000](https://openairdocs.org/sdr/MLJ2015F00000.md): Skin · damaged · Feb 5, 2015 · N3284M · Cessna 310R · Fuselage Main, Plate/Skin
  > PILOT WAS DISPATCHED TODAY TO PICK UP MECHANICS AND SPARE TIRE. UPON ARRIVAL PILOT WENT TO RESTROOM AND WHEN HE RETURNED, MECHANICS WERE LOADING THE ACFT. PILOT NOTED DAMAGE TO SKIN BELOW BAGGAGE DOOR BUT WAS UNSURE IF IT WAS NEW DUE TO DARKNESS AND PSA MECH
- [SDR CA150107011](https://openairdocs.org/sdr/CA150107011.md): Magneto · failed · Jan 7, 2015 · Cessna 310R · Magneto/Distributor
  > (CAN) DURING 200HR INSPECTION OIL LEAK NOTICED ON LH SIDE OF ENGINE. AFTER CLEANING AREA WAS DETERMINED THAT IT WAS THE LH MAG GASKET LEAKING. MAGNETO WAS REMOVED AND MOUNTING FLANGE WAS FOUND TO BE BROKEN. BROKEN AT THE POINT THE HOLD DOWN PLATE IS USED TO HO
- [SDR XIRA2014121200001](https://openairdocs.org/sdr/XIRA2014121200001.md): Rod End · broken · Dec 12, 2014 · N101G · Cessna 310R · Landing Gear Retraction/Extension System
  > ROD END BROKE, UPLOCK COULD NOT RELEASE, CAUSING DAMAGE TO GEAR SYSTEM AND STRUCTURE. AGE IS THOUGHT TO BE THE CAUSE.
- [SDR 2014FA0000144](https://openairdocs.org/sdr/2014FA0000144.md): Injector · dirty · Mar 3, 2014 · N37250 · Cessna 310R · Fuel Injector Nozzle
  > PILOT REPORTED ROUGH RUNNING ENGINE AND MADE PRECAUTIONARY LANDING. PILOT WAS ABLE TO INFORM MAINTENANCE OF THE CYLINDERS THAT WERE HAVING ISSUES FROM THE ENGINE MONITOR INDICATION. MAINTENANCE FOUND SMALL AMOUNTS OF DIRT IN THE INJECTORS OF THE AFFECTED CYL
- [SDR 2013FA0000366](https://openairdocs.org/sdr/2013FA0000366.md): Screw · broken · Jun 17, 2013 · N310LA · Cessna 310R · Landing Gear Retraction/Extension System
  > AN ADJUSTMENT SCREW, WHICH IS PART OF THE RT MAIN GEAR DOWN LOCK ASSEMBLY, FAILED. THIS ALLOWED THE MAIN GEAR BRACE ASSY TO RETURN FROM A DOWN AND LOCKED (OVERCENTER) POSITION AND THE GEAR TO FOLD UP UNDER NORMAL GROUND OPERATIONS.
- [SDR 2013FA0000220](https://openairdocs.org/sdr/2013FA0000220.md): Line · leaking · Mar 21, 2013 · N617AX · Cessna 310R · Aircraft Fuel Distribution System
  > PILOT REPORTED FUEL ODOR IN CABIN. AFTER INSPECTION, IT WAS DETERMINED THAT THE RIGID FUEL CROSSFEED LINES THAT RUN THROUGH THE FUSELAGE, INSIDE THE MAIN SPAR BOX, HAD CORRODED INTERNALLY RESULTING IN FUEL POOLING IN THE LOWER SPAR BOX. THIS OCCURRED IN OCT
- [SDR CA130218012](https://openairdocs.org/sdr/CA130218012.md): Lifter · failed · Jan 23, 2013 · Cessna 310R · Reciprocating Engine Power Section
  > (CAN) ENGINE WAS REMOVED FOR REPAIR AFTER FINDING METAL IN THE FILTER. IT WAS DISCOVERED THAT THE 6 INTAKE LIFTERS WERE FAILED OR FAILING. THESE LIFTERS WERE PART OF A NEW CAMSHAFT AND LIFTER KIT. THESE LIFTERS WERE MFG JUST BEFORE MANDATORY SB 09-8A. AWD. 2
- [SDR FSEA2012F00059](https://openairdocs.org/sdr/FSEA2012F00059.md): Control Handle · burned · Feb 14, 2012 · N815AC · Cessna 310R · Landing Gear Selector
  > LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. LANDING GEAR WAS MANUALLY EXTENDED TO FULL DOWN POSITION WITH 3 GREEN INDICATIONS. ON RETURN TO MX FACILITY, ACFT WAS PLACED ON JACKS AND LANDING GEAR FUNCTIONED NORMALLY. THIS PROBLEM OCCURRED APPROX 10 MONTH PR
- [SDR CA120202004](https://openairdocs.org/sdr/CA120202004.md): Support Beam · cracked · Feb 2, 2012 · Cessna 310R · Engine Mount Section
  > (CAN) RIGHT ENGINE SUPPORT BEAMS INSPECTED IAW INSPECTION OPERATION 35 DURING ENGINE REPLACEMENT A2 CM. CRACK WAS FOUND VISUALLY BELOW THE FRONT INBD MOUNT ATTACHMENT BOLT HOLE. ENGINE SUPPORT BEAM REPLACED WITH NEW.
- [SDR 2011FA0000683](https://openairdocs.org/sdr/2011FA0000683.md): Skin · cracked · Oct 14, 2011 · N87397 · Cessna 310R · Wing, Plate/Skin
  > A CRACK OF APPROX 8-9 INCHES WAS FOUND IN UPPER INBD RT WING SKIN AND A 6-7 INCH CRACK FOUND IN UPPER INBD OF LT WING SKIN. THIS CRACK WAS LOCATED ON INTERIOR SIDE OF BOTH WING NACELLE LOCKERS, UNDERNEATH THE CARPET, AT INBD SIDE OF RIB WHICH SUPPORTS UPPER M
- [SDR 2011FA0000585](https://openairdocs.org/sdr/2011FA0000585.md): Crankshaft · broken · Jul 27, 2011 · N18BK · Cessna 310R · Reciprocating Engine Power Section
  > ACFT LANDED AT AIRPORT WITH RT PROPELLER FEATHERED. PILOT STATED ENGINE QUIT SUDDENLY ABOUT 15 MILES NORTH OF AIRPORT. PILOT AUTHORIZED INSP TO DETERMINE PROBLEM. GROUND PERSONEL COULD NOT TURN ENGINE OVER WITH PROPELLER. OIL DRAINED AND FILTER INSPECTED. OIL
- [SDR CA110725008](https://openairdocs.org/sdr/CA110725008.md): Engine · failed · Jul 22, 2011 · Cessna 310R · Engine (Reciprocating)
  > (CAN) AFTER TAKING OFF AND IN CLIMB, PILOT FELT SLIGHT VIBRATION IN LT SIDE OF ACFT. HE CHECKED HIS ENGINE GAUGES AND NOTED THAT THE LT ENGINE HAD NO OIL PRESSURE. HE SHUT DOWN THE LT ENGINE, FEATHERED THE PROP AND RETURNED TO THE AIRPORT. THE ACFT WAS PULLED
- [SDR CA101004011](https://openairdocs.org/sdr/CA101004011.md): Control Cable · frayed · Oct 1, 2010 · Cessna 310R · Trailing Edge Flap Control System
  > ON COMING INTO LAND, THE FLAPS WERE LOWERED TO 15 DEGREES, THE ACFT MADE A ROLL TO THE LT. PILOT CORRECTED AND LANDED WITHOUT INCIDENT. AME INSPECTED THE FLAP SYS AND FOUND THE RT FLAP RETURN CABLE HAD STARTED TO FRAY. WHEN THE FLAPS WERE LOWERED TO 15 DEGR
- [SDR 2010FA0001135](https://openairdocs.org/sdr/2010FA0001135.md): Cylinder · cracked · Aug 18, 2010 · N1203W · Cessna 310R · Reciprocating Engine Cylinder Section
  > (WS9R) CYLINDER CRACKED FROM INJECTOR PORT TO SPARK PLUG BOSS.
- [SDR 2010FA0000960](https://openairdocs.org/sdr/2010FA0000960.md): Line · cracked · Aug 18, 2010 · N3694G · Cessna 310R · Windshield/Door Rain/Ice Removal
  > DURING REPAIR OF THE WINDSHIELD DE-ICE (ALCOHOL) SYSTEM, FOUND MANIFOLD SUPPLY LINE CRACKED AND SPRAYING ATOMIZED ALCOHOL ONTO COMBUSITON HEATER ASSY. FAILURE RESULTING IN FIRE AND POSSIBLE EXPLOSION IN EVENT OF USING DE-ICE SYSTEM WHILE HEATER ON. FOUND LIN
- [SDR CA100809007](https://openairdocs.org/sdr/CA100809007.md): Heater · corroded · May 13, 2010 · Cessna 310R · Fuel Heater
  > PILOTS REPORT SMELL OF RAW FUEL ON DESCENT/APPROACH FROM HEATER. MX CHECKED VARIOUS TIMES BUT COULD NOT DUPLICATE. INSP REVEALED FUEL LINE RUNNING DOWN RT WALL AT CO-PILOT FEET AREA AND VENT SEEPING FUEL OUT OF AREA OF CORROSION ON LINE.
- [SDR CA090320004](https://openairdocs.org/sdr/CA090320004.md): Tube · split · Mar 19, 2009 · Cessna 310R · Tire Tube
  > (CAN) AFTER LANDING, PILOT NOTICED ACFT DRAGGING TO ONE SIDE. ACFT WAS STOPPED, PILOT GOT OUT AND NOTICED LT TIRE WAS FLAT. MX WENT OUT AND REPLACED WHEEL ASSY. ACFT BROUGHT BACK TO HANGAR. TIRE WAS DISASSEMBLED, THE TUBE HAD SPLIT ON THE JOINT LINE. NO REASO
- [SDR 2008FA0000911](https://openairdocs.org/sdr/2008FA0000911.md): Rod End · cracked · Dec 1, 2008 · N77RG · Cessna 310R · Landing Gear Retraction/Extension System
  > PILOT REPORTED NO LT GEAR DOWN LIGHT AND ALSO HEARD A LOUD BANG WHEN GEAR WAS RETRACTED. PILOT DID SEVERAL FLYBYS FOR MECHANICS ON GROUND, GEAR APPEARED TO BE DOWN. PILOT LANDED WITHOUT INCIDENT AND STOPPED ON RUNWAY. GEAR WAS NOT COMPLETELY LOCKED. GEAR WA
- [SDR W1X2008F00000](https://openairdocs.org/sdr/W1X2008F00000.md): Bellcrank · broken · May 23, 2008 · N5338C · Cessna 310R · Nose/Tail Landing Gear
  > FAILURE OF NOSE GEAR TO EXTEND, FOUND BELLCRANK ON GEAR BOX BROKEN. (K)
- [SDR 7AA2008F00000](https://openairdocs.org/sdr/7AA2008F00000.md): Bolt · sheared · Dec 13, 2007 · N310SA · Cessna 310R · Horizontal Stabilizer Structure
  > WHILE PREPARING AIRCRAFT FOR HORIZONTAL STABILIZER REMOVAL, THE 4 BOLTS THAT ATTACH THE HORIZONTAL STABILIZER TO THE AFT FUSELAGE ALL SHEARED WITH MINIMAL EFFORT WHEN THEY WERE BEING REMOVED. THERE ARE STANDARD AIRCRAFT BOLTS, AN5-6A. (K)
- [SDR 2007FA0000956](https://openairdocs.org/sdr/2007FA0000956.md): Bracket · inoperative · Sep 19, 2007 · N5338C · Cessna 310R · Wing, Attach Fittings
  > THE RT MAIN LANDING GEAR WOULD NOT RETRACT INTO WHEEL WELL. PILOT REPORTED LOUD BANG HEARD AFTER RETRACTING OF GEAR. WHEN EXTENDING THE GEAR FOR LANDING, THE RT GEAR WOULD NOT INDICATE GREEN BUT WAS VISUALLY CONFIRMED DOWN. PILOT LANDED WITHOUT INCIDENT AND
- [SDR CA070927001](https://openairdocs.org/sdr/CA070927001.md): Wheel · broken · Aug 31, 2007 · Cessna 310R · Wheel/Ski/Float
  > (CAN) DURING MAINT THE RT MAIN WAS FOUND WITH PART OF THE BEAD MISSING, PILOT SAID THE WHEEL WAS OK PRIOR TO DEPARTURE AND LANDING NORMAL. TOWER ADVISED AND CREW SENT OUT FOR INSP, NO PIECES FOUND. (TC NR 20070927001)
- [SDR 2007FA0000550](https://openairdocs.org/sdr/2007FA0000550.md): Bellcrank · broken · Jun 21, 2007 · N1771G · Cessna 310R · Landing Gear Retraction/Extension System
  > LT MAIN GEAR BELLCRANK ASSY BROKE IN MARCH OF 2007. THE PART WAS REPLACED BY A USED SERVICABLE PART WHICH LASTED APPROXIMATLY 58 HRS. THEN FAILED AT THE SAME LOCATION ON THE PART.

Next page: https://openairdocs.org/model/cessna-310r/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 = '310R'
ORDER BY difficulty_date DESC
```

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

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