# Service difficulty reports: Cessna 310L

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

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 60 reports

- [SDR 2021FA0000105](https://openairdocs.org/sdr/2021FA0000105.md): Bolt · sheared · Apr 1, 2021 · N2249M · Cessna 310L · Main Landing Gear Strut/Axle/Truck
  > DURING THE LANDING PORTION OF OUR FLIGHT ON THE ROLL OUT THE RIGHT GEAR COLLAPSE UNDERNEATH THE AIRPLANE. UPON FURTHER INSPECTION IT WAS DETERMINED THAT THE BOLT HOLDING THE FOLLOWING SIDE BRACE AND DOWN LOCK SHEARD CAUSING THE RIGHT SIDE BRACE LOCK LINK ASSE
- [SDR 2015FA0000307](https://openairdocs.org/sdr/2015FA0000307.md): Tube · bent · Jun 16, 2015 · N2215F · Cessna 310L · Landing Gear Retraction/Extension System
  > LANDING GEAR WAS SELECTED DOWN AND EXTENDED AND THE PILOT FELT A STRANGE "CLUNK" UNDER HIS FEET. THE PILOT DID NOT GET A "GREEN" DOWN-AND-LOCKED INDICATION FOR THE NOSE GEAR. TOWER CONFIRMED NOSE GEAR WAS NOT DOWN. THE NOSE GEAR COLLAPSED UPON LANDING. SUB
- [SDR 2011FA0000389](https://openairdocs.org/sdr/2011FA0000389.md): Idler Assy · broken · Jun 20, 2011 · N3275X · Cessna 310L · Landing Gear Retraction/Extension System
  > ON TAKEOFF; GEAR RETRACT; GEAR MOTOR DID NOT SHUT OFF IN TIME CAUSING NOSE GEAR TO BE RETRACTED FARTHER THAN RIGGING ALLOWED; IDLER ASSY (BELLCRANK) PN 0842102-2 BROKE AT BOLT HOLE FOR AFT PUSH PULL TUBE. THIS CAUSED NOSE GEAR TO BE UNCONTROLLED REGARDING EXT
- [SDR 2009FA0000545](https://openairdocs.org/sdr/2009FA0000545.md): Combust Chamber · wrong part · Jun 22, 2009 · Cessna 310L · Heating System
  > HEATER (PN 96C62, SN 9660906) RECEIVED FOR OVERHAUL. HEATER WAS PREVIOUSLY OVERHAULED AND HAS A REPAIR STATION DATA PLATE. UPON INSPECTION, HEATER HAS WRONG COMBUSTION TUBE INSTALLED. WRONG COMBUSTION TUBE REQUIRED COMBUSTION HEAD THAT IS NOT CALLED FOR IN T
- [SDR 2009FA0000544](https://openairdocs.org/sdr/2009FA0000544.md): Combust Chamber · wrong part · Jun 22, 2009 · Cessna 310L · Heating System
  > HEATER (PN 96C62, SN 9660906) RECEIVED FOR OVERHAUL. HEATER WAS PREVIOUSLY OVERHAULED AND HAS THE REPAIR STATION DATA PLATE. UPON INSP, HEATER HAS WRONG COMBUSTION TUBE INSTALLED. WRONG COMBUSTION TUBE REQUIRED COMBUSTION HEAD THAT IS NOT CALLED FOR IN THE 96
- [SDR 2008FA0000065](https://openairdocs.org/sdr/2008FA0000065.md): Wheel Half · cracked · Aug 24, 2007 · N63EL · Cessna 310L · Wheel/Ski/Float
  > UPON CHANGING A TIRE ON A CLEVELAND WHEEL ASSEMBLY ON ABOVE AIRCRAFT IT WAS DISCOVERED THAT THE PORTION OF THE WHEEL HALF THAT HOLDS THE BEARING RACE WAS CRACKING. IT HAD CRACKED OVER 180 DEGREES AROUND THE AXLE OPENING, WHICH COULD HAVE EVENTUALLY HAD A SERIO
- [SDR CA040311001](https://openairdocs.org/sdr/CA040311001.md): Switch · broken · Mar 10, 2004 · Cessna 310L · Landing Gear Position and Warning
  > (CAN) UPON APPROACH THE LANDING GEAR WAS SELECTED DOWN WITH NO GREEN LIGHT DOWN AND LOCKED INDICATION ON THE RT GEAR. THE GEAR WAS CYCLED, THE MANUAL EXTENSION WAS PERFORMED ALL WITH THE SAME RESULT. THE AIRCRAFT LANDED UNEVENTFULLY AND UPON INVESTIGATION TH
- [SDR CA031127011](https://openairdocs.org/sdr/CA031127011.md): Bulkhead · cracked · Nov 25, 2003 · Cessna 310L · Fuselage Main, Bulkhead
  > (CAN) DURING THE 100 HOUR INSPECTION PLAY WAS NOTICED IN THE NOSE GEAR AREA. UPON INSPECTION THE LT NOSE SECTION BULKHEAD WAS FOUND TO BE CRACKED VERTICALLY THROUGH THE CENTER OF THE LIGHTENING HOLE. DOUBLER PATCHES WERE INSTALLED AND RIVETED INTO PLACE AND
- [SDR CA030520005](https://openairdocs.org/sdr/CA030520005.md): Spring · broken · May 20, 2003 · Cessna 310L · Landing Gear Retraction/Extension System
  > (CAN) DURING WALK-AROUND PRIOR TO FLIGHT, PIC NOTICED DOWNLOCK SPRING HANGING FROM ONE ATTACH POINT AND UPON INSPECTION WAS FOUND BROKEN AT ATTACH POINT ABOUT 1/2 AN INCH ABOVE SPRING BODY. SPRING WAS REPLACED NEW.
- [SDR CA030506001](https://openairdocs.org/sdr/CA030506001.md): Actuator · cracked · Apr 28, 2003 · Cessna 310L · Landing Gear Door Actuator
  > (CAN) AT 160 KTS DID NOT GET DOWN LOCKED IND ON RT MAIN. GEAR WAS SEL UP, TOP OF TRAVEL, GRINDING NOISE WAS HEARD. GEAR SELECT WAS PLACED IN NEUTRAL, GEAR WAS HAND-CRANKED DOWN, A/C LANDED. RT MAIN GEAR DOOR WAS OPEN ABOUT 6 IN FROM NORMAL CLOSED GEAR DOWN PO
- [SDR CA030219004](https://openairdocs.org/sdr/CA030219004.md): Piston · cracked · Feb 19, 2003 · Cessna 310L · Main Landing Gear Strut/Axle/Truck
  > (CAN) DURING COMPLETE REMOVAL AND NDT OF ALL LANDING GEAR PARTS BOTH LT & RT MAIN GEAR PISTON AND AXLE ASSEMBLIES (P/N S 5041000-77 & 5041000-76 RESPECTIVELY) WERE FOUND CRACKED AT THE SMALLER OF THE TWO TORQUE LINK ATTACH LUGS.THE RT WAS REPLACED WITH A USED
- [SDR CA021118003](https://openairdocs.org/sdr/CA021118003.md): Torque Tube · cracked · Nov 13, 2002 · Cessna 310L · Landing Gear Retraction/Extension System
  > (CAN) ON T/O, A CLUNK HEARD NEAR END OF MLG TRAVEL DURING RETRACTION. NO DIFFERECE IN FLT CONTROL. PILOTS INFORMED RT MLG HANGING. MLG SELECTED DOWN STEEP BANKS & YAWS PERFORMED TO GET RT MLG LOCKED. NO DOWN & LOCKED IND EVIDENT, A/C LANDED UNEVENTFULL
- [SDR CA021118004](https://openairdocs.org/sdr/CA021118004.md): Spring · broken · Nov 13, 2002 · Cessna 310L · Landing Gear Position and Warning
  > (CAN) SUBSEQUENT TO THE RT MAIN GEAR FAILURE TO LOCK AND FINDING THE TORQUE TUBE CRACKED, THE DOWNLOCK SPRING WAS ALSO BROKEN. HAD THIS SPRING BEEN INTACT THE GEAR WOULD HAVE FREE-FALLEN DOWN AND LOCKED. THERE IS NO RIGGING OR ADJUSTMENT ON THESE SPRINGS. BO
- [SDR 2002FA0000196](https://openairdocs.org/sdr/2002FA0000196.md): Bellcrank · broken · Feb 1, 2002 · N510V · Cessna 310L · Landing Gear Retraction/Extension System
  > AFTER REPLACING BROKEN SQUAT SWITCH, CONDUCTED ROUTINE RETRACTION TEST TO CHECK FUNCTION OF GEAR. MAINS RETRACTED NORMALLY, NOSE GEAR STARTED TO RETRACT AND THEN BOUND UP. BEFORE LANDING GEAR LEVER COULD BE MOVED TO NEUTRAL POSITION, LOUD BANG AND MOVEMENT OF
- [SDR AUS20020003](https://openairdocs.org/sdr/AUS20020003.md): Door · misinstalled · Jan 2, 2002 · Cessna 310L · Emergency Exits
  > (AUS) EMERGENCY EXIT INCORRECTLY INSTALLED. ONLY TWO OF THREE LATCHING PINS ENGAGED. EMERGENCY RELEASE CABLE LOOPED AND THE TWO LATCHING PINS WERE FITTED BACKWARDS. IT WOULD HAVE BEEN IMPOSSIBLE FOR THE EMERGENCY EXIT TO BE RELEASED.
- [SDR 2001FA0000341](https://openairdocs.org/sdr/2001FA0000341.md): Plate · wrong part · Aug 22, 2001 · N2209F · Cessna 310L · Engine Oil Cooler
  > ENGINE HAD LOST OIL PRESSURE DURING FLIGHT. AFTER A SAFE LANDING IT WAS DETERMINED THAT THE OIL HAD LEAKED OUT FROM THE BETWEEN THE OIL COOLER PLATE AND THE ENGINE. THE OIL COOLER PLATE ATTACHMENT NUTS WERE FOUND TO BE LOOSE. THE GASKET BETWEEN THE PLATE AN
- [SDR CA001207020](https://openairdocs.org/sdr/CA001207020.md): Tube · cracked · Nov 23, 2000 · Cessna 310L · Landing Gear Retraction/Extension System
  > (CAN) WHILE PERFORMING FLT TEST, GEAR SELECTED DOWN AND OVERSHOOT PERFORMED. GEAR SELECTED UP SUCCESSFULLY. A/C RE-JOINED CCT & ON APPROACH GEAR SELECTED DOWN WITH GREEN LIGHTS INDICATING GOOD MAINS BUT NOTHING ON NOSE. UPON LDG THROTTLES WERE PULLED BACK & ID
- [SDR CA000928019](https://openairdocs.org/sdr/CA000928019.md): Rack · chafed · Aug 30, 2000 · Cessna 310L · Instrument Panel
  > (CAN) UPON PERFORMING FLAIR DURING LANDING, THE PILOTS NOTICED THE ELEVATOR CONTROLS WERE FEELING A LITTLE STIFF. UPON MAINTENANCE INVESTIGATION, FOUND THE RADIO IN THE CENTER INSTRUMENT PANEL (RADIO RACK) WERE SETTING DOWN AND MAKING CONTACT WITH THE CONTROL
- [SDR 20000720SH009](https://openairdocs.org/sdr/20000720SH009.md): Tube · failed · Feb 7, 2000 · N867MF · Cessna 310L · Landing Gear Retraction/Extension System
  > ON APPROACH AFTER LOWERING GEAR, PILOT NOTICED NOSE GEAR NOT DOWN AND LOCKED. PILOT MADE NOSE-UP LANDING. FURTHER INSPECTION REVEALED EYELET OF TUBE ASSY HAD FAILED. (X)
- [SDR 20000720SH008](https://openairdocs.org/sdr/20000720SH008.md): Tube · failed · Feb 7, 2000 · N867MF · Cessna 310L · Landing Gear Retraction/Extension System
  > ON APPROACH AFTER LOWERING GEAR, PILOT NOTICED NOSE GEAR NOT DOWN AND LOCKED. PILOT MADE NOSE-UP LANDING. FURTHER INSPECTION REVEALED EYELET OF TUBE ASSY HAD FAILED. (X)
- [SDR 20000925SH010](https://openairdocs.org/sdr/20000925SH010.md): Brace · failed · Jun 7, 1999 · N3210 · Cessna 310L · Landing Gear Retraction/Extension System
  > AFTER LANDING, DURING ROLL-OUT, RIGHT MAIN LANDING GEAR SIDE BRACE EXPERIENCED CATASTROPHIC FAILURE RESULTING IN THE COLLAPSE OF THE RIGHT MAIN GEAR. THE ATTACHMENT LOBE ON THE SIDE BRACE FRACTURED. (X)
- [SDR 99ZZZX2233](https://openairdocs.org/sdr/99ZZZX2233.md): Control Cable · failed · Apr 26, 1999 · N2215F · Cessna 310L · Power Lever
  > THROTTLE CABLE FAILED WHILE IN-FLIGHT. DEFECT DISCOVERED AT FIRST ATTEMPT TO REDUCE POWER FOR DESCENT. INNER CONTROL CABLE FAILED (SEPARATED) AT SWAGED TERMINAL END AT ENGINE. UNABLE TO CONTROL POWER OUTPUT OF ENGINE. THIS ASSEMBLY CANNOT BE VISUALLY INSPEC
- [SDR CA990318039](https://openairdocs.org/sdr/CA990318039.md): Windshield · cracked · Feb 26, 1999 · Cessna 310L · Flight Compartment Windows
  > (CAN) CRACKED AND CRAZED WINDSHIELD REPLACED. NO INCIDENTS IN FLIGHT HISTORY REPORTED.
- [SDR 99ZZZX1216](https://openairdocs.org/sdr/99ZZZX1216.md): Tube Assy · broken · Jan 24, 1999 · N73NR · Cessna 310L · Landing Gear Retraction/Extension System
  > DRIVE TUBE FOR NOSE GEAR SYSTEM BROKE AT LANDING GEAR ACTUATOR DUE STRESS OF DRIVE TUBE.
- [SDR 98ZZZX1717](https://openairdocs.org/sdr/98ZZZX1717.md): Wire · broken · Apr 13, 1998 · N3304X · Cessna 310L · Landing Gear System Wiring
  > LANDING GEAR DID NOT COME DOWN DUE TO A BROKEN WIRE TO MASTER SOLENOID. REPLACED WIRE WITH NEW AND WILL REPLACE ALL WIRING ON MASTER SIDE DUE TO AGE.
- [SDR AU980422](https://openairdocs.org/sdr/AU980422.md): Bulkhead · cracked · Apr 9, 1998 · Cessna 310L · Fuselage Main, Bulkhead
  > (AUS) FORWARD FUSELAGE BULKHEAD AND BRACKET AT LOCATED AT STN 27.25 CRACKED. BULKHEAD SUPPORTS THE PULLEYS FOR THE NOSE WHEEL STEERING CABLE. PART TC: 6,445.
- [SDR AU980462](https://openairdocs.org/sdr/AU980462.md): Line · sludged · Feb 27, 1998 · Cessna 310L · Engine Oil Pressure
  > (AUS) DURING FLIGHT, THE RT ENGINE GAUGE DISPLAYED LOW OIL PRESSURE. ENGINE GROUND RUN WITH A CALIBRATED OIL PRESSURE GAUGE PLUMBED INTO SYSTEM WAS CARRIED OUT WITH NO FAULT FOUND. SUSPECTING IT COULD HAVE BEEN A SLUDGE PROBLEM IN THE PRESSURE LINE BETWEEN T
- [SDR 97ZZZX4502](https://openairdocs.org/sdr/97ZZZX4502.md): Bracket · cracked · Oct 9, 1997 · N2239F · Cessna 310L · Landing Gear Steering System
  > ON DEPLOYMENT OF LANDING GEAR NOSE, WHEEL STUCK 60 DEGREES TO LEFT OF CENTER. PERFORMED GEAR SWING, FOUND ATTACH BRACKETS FOR STEERING BELLCRANK CRACKED. REPLACED BRACKETS. GEAR RETRACTION NORMAL.
- [SDR 97ZZZX4501](https://openairdocs.org/sdr/97ZZZX4501.md): Bracket · cracked · Oct 9, 1997 · N2239F · Cessna 310L · Landing Gear Steering System
  > ON DEPLOYMENT OF LANDING GEAR NOSE, WHEEL STUCK 60 DEGREES TO LEFT OF CENTER. PERFORMED GEAR SWING, FOUND ATTACH BRACKETS FOR STEERING BELLCRANK CRACKED. REPLACED BRACKETS. GEAR RETRACTION NORMAL.
- [SDR AU970693](https://openairdocs.org/sdr/AU970693.md): Mount · worn · Jun 19, 1997 · Cessna 310L · Engine Mount Section
  > (AUS) RH ENGINE RH REAR ENGINE MOUNT LANDS WORN EXCESSIVELY. SEE MDR97/0685 FOR DEFECT ON RH ENGINE LH REAR MOUNT FAILURE
- [SDR AU970692](https://openairdocs.org/sdr/AU970692.md): Diode · inoperative · Jun 19, 1997 · Cessna 310L · Battery/Charger System
  > (AUS) BATTERY MASTER SYSTEM DIODE INOPERATIVE.
- [SDR AU970691](https://openairdocs.org/sdr/AU970691.md): Alternator · inoperative · Jun 19, 1997 · Cessna 310L · DC Generator-Alternator
  > (AUS) ALTERNATOR EMERGENCY FIELD SYSTEM INOPERATIVE. SEE MDR 97/0682FOR ADDITIONAL INFORMATION.
- [SDR AU970690](https://openairdocs.org/sdr/AU970690.md): Nut · loose · Jun 19, 1997 · Cessna 310L · Mixture Control
  > (AUS) ENGINE MIXTURE CONTROL CABLE OUTER SHEATH NUT NOT ATTACHED
- [SDR AU970689](https://openairdocs.org/sdr/AU970689.md): Bracket · separated · Jun 19, 1997 · Cessna 310L · Engine Air Intake System
  > (AUS) ENGINE ALTERNATE AIR DOOR BRACKET SEPARATED AND INGESTED INTO ENGINE
- [SDR AU970688](https://openairdocs.org/sdr/AU970688.md): Cylinder · damaged · Jun 19, 1997 · Cessna 310L · Reciprocating Engine Cylinder Section
  > (AUS) NO2 AND NO6 CYLINDERS DAMAGED BY INGESTION OF SEPARATED ALTERNATE AIR DOOR BRACKET. PERSONNEL/MAINTENANCE ERROR.
- [SDR AU970682](https://openairdocs.org/sdr/AU970682.md): Electrical Sys · faulty · Jun 19, 1997 · Cessna 310L · Electrical Power System
  > (AUS) AIRCRAFT EXPERIENCED ELECTRICAL PROBLEMS. FIBREGLASS PROTECTIVE SHIELD OVER LH AND RH FIELD FUSES ON THE LH FIREWALL HAD CHAFED THROUGH THE LH ALTERNATOR FIELD CABLE. PERSONNEL/MAINTENANCEERROR
- [SDR AU970428](https://openairdocs.org/sdr/AU970428.md): Striker · cracked · Apr 26, 1997 · Cessna 310L · Landing Gear Position and Warning
  > (AUS) RH MAIN LANDING GEAR MICROSWITCH STRIKER ARM CRACKED AND SEPARATED FROM SWITCH
- [SDR AU970505](https://openairdocs.org/sdr/AU970505.md): Headset · damaged · Apr 20, 1997 · Cessna 310L · Audio Integrating System
  > (AUS) HEADSET LEAD MELTED DUE TO SHORT CIRCUIT BETWEEN CO-PILOTS PHONEJACK AND INSTRUMENT LIGHTING WIRE
- [SDR AU970687](https://openairdocs.org/sdr/AU970687.md): Exit Door · sealed · Mar 11, 1997 · Cessna 310L · Emergency Exits
  > (AUS) EMERGENCY EXIT DOOR SEALED CLOSED. SEALANT HAD TO BE CUT TO ALLOW THE EXIT TO BE REMOVED. AD/GEN/37 LAST CARRIED OUT ON THE 15TH OCTOBER 1996. PERSONNEL/MAINTENANCE ERROR.
- [SDR AU970686](https://openairdocs.org/sdr/AU970686.md): Door · loose · Mar 11, 1997 · Cessna 310L · Engine Air Intake System
  > (AUS) ENGINE ALTERNATE AIR DOOR BRACKET LOOSE AND INCORRECTLY RIGGED
- [SDR AU970685](https://openairdocs.org/sdr/AU970685.md): Mount · broken · Mar 11, 1997 · Cessna 310L · Engine Mount Section
  > (AUS) RH ENGINE REAR ENGINE MOUNT RUBBER BROKEN.
- [SDR AU970679](https://openairdocs.org/sdr/AU970679.md): Plate · damaged · Mar 11, 1997 · Cessna 310L · Nose/Tail Landing Gear Attach Section
  > (AUS) NOSE LANDING GEAR FACE PLATE DAMAGED
- [SDR 97ZZZX1154](https://openairdocs.org/sdr/97ZZZX1154.md): Tube Assy · broken · Feb 25, 1997 · N3285X · Cessna 310L · Landing Gear Retraction/Extension System
  > TUBE MAY BECOME BENT DUE TO HIGH AIR SPEED WHEN GEAR IS EXTENDED. AFTER INITIAL BENDING, TUBE WILL FLEX WITH EACH CYCLE EVENTUALLY BREAKING. THIS TUBE IS HARD TO INSPECT DUE TO THE LOCATION IN THE A/C. SUBMITTER SUGGESTED TUBE BE REMOVED AND INSPECTED EACH
- [SDR EY2R9601302](https://openairdocs.org/sdr/EY2R9601302.md): Cylinder · corroded · Dec 1, 1996 · Cessna 310L · Propeller Assembly
  > CYLINDER FOUND WITH CORROSION.
- [SDR EY2R9601301](https://openairdocs.org/sdr/EY2R9601301.md): Cylinder · corroded · Dec 1, 1996 · Cessna 310L · Propeller Assembly
  > CYLINDER FOUND WITH CORROSION.
- [SDR AU961083](https://openairdocs.org/sdr/AU961083.md): Spinner Blkhd · cracked · Jul 31, 1996 · Cessna 310L · Propeller Spinner Section
  > (AUS) PROPELLER SPINNER BULKHEAD CRACKED FROM ATTACHMENT SCREW HOLES - SUSPECT CRACKS HAD EXISTED FOR SOME TIME - INVESTIGATION FOUND THAT THE DOUBLER ASSEMBLY PNO 0895008-4 HAD NOT BEEN FITTED - PERSONNEL/MAINTENANCE ERROR
- [SDR AU961082](https://openairdocs.org/sdr/AU961082.md): Switch · dirty · Jul 26, 1996 · Cessna 310L · Landing Gear Position and Warning
  > (AUS) RH MAIN LANDING GEAR DOWNLOCK MICROSWITCH DIRTY
- [SDR AU961081](https://openairdocs.org/sdr/AU961081.md): Torque Tube · failed · Jul 18, 1996 · Cessna 310L · Landing Gear Retraction/Extension System
  > (AUS) LH MAIN LANDING GEAR RETRACTION SYSTEM TORQUE TUBE SPLIT - INBOARD LANDING GEAR DOOR ACTUATING ROD ROD-END PNO 5045025-1MISSING FROM MLG RETRACTION LINKAGE IDLER BELLCRANK PNO 0841106-5DUE TO LOSS OF TORQUE OF THE ATTACHMENT NUT
- [SDR EY2R9601555](https://openairdocs.org/sdr/EY2R9601555.md): Blade · damaged · Jun 1, 1996 · Cessna 310L · Propeller Blade Section
  > BLADE SN K77739YS, SCRATCH IN THREADS
- [SDR AU960737](https://openairdocs.org/sdr/AU960737.md): O-Ring · wrong part · May 24, 1996 · Cessna 310L · Propeller Assembly
  > (AUS) PROPELLER CONTAINED THE FOLLOWING FAULTS:- 1. INCORRECT RETENTION NUT 'O' RINGS FITTED2. RETENTION NUT NOT TORQUED 3. NO MOLY KOTE LUBRICANT ON FERRULE THREADS OR BLADE THREADS4. OLD TYPE PRESSURE LATCH STILL FITTED - SHOULD HAVE BEENREPLACED WITH LATEST

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

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

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