# Service difficulty reports: Cessna T210L

A list on [Cessna T210L](https://openairdocs.org/model/cessna-t210l.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 78 reports

- [SDR 2024FA0000836](https://openairdocs.org/sdr/2024FA0000836.md): Seat · broken · Nov 12, 2024 · N74LC · Cessna T210L · Flight Compartment Equipment
  > DURING THE 200HR/ANNUAL INSPECTION IT WAS FOUND THAT BOTH CESSNA SK210-175A AND SK210-175B KITS THAT WERE INSTALLED TO COMPLY WITH CESSNA SB SEB07-5R2 WERE FOUND IN AN INOP CONDITION (BROKEN). THE SWIVEL ADAPTER THAT IS HELD ONTO THE REEL ASSEMBLY WITH 2 SMALL
- [SDR 2023FA0000305](https://openairdocs.org/sdr/2023FA0000305.md): Alternator · failed · May 13, 2023 · N4678Q · Cessna T210L · Alternator-Generator Drive
  > N4678Q, C210, DECLARED AN EMERGENCY DUE TO POSSIBLE ELECTRICAL ISSUE. THE FLIGHT LANDED SAFELY WITHOUT ISSUE.
- [SDR 2023FA0000267](https://openairdocs.org/sdr/2023FA0000267.md): Rod · broken · Apr 24, 2023 · N2092S · Cessna T210L · Standard Practices/Structures
  > ROD ASSEMBLY BROKE AT THE THREADED END OF THE ROD END.
- [SDR 2016FA0000584](https://openairdocs.org/sdr/2016FA0000584.md): Alternator · low voltage · Nov 15, 2016 · N93285 · Cessna T210L · AC Generator-Alternator
  > VOLT METER INDICATED A DISCHARGE AT 1000 RPM. NORMAL VOLT AT 1000RPM AS PER CHECK SHOULD BE 28.5+-5. VOLT METER INDICATED AT 1000 RPM 25.0 AMPS 37. AT 1700 RPM VOLT 27.8 AMPS 42, AT 2000 RPM V27.8 AMPS 39.
- [SDR 4DSR201411240001](https://openairdocs.org/sdr/4DSR201411240001.md): Control Unit · seized · Nov 24, 2014 · N93285 · Cessna T210L · Mixture Control
  > DURING 50 HOUR INSPECTION, MECHANIC FOUND THE MIXTURE CONTROL OPERATION TO BE VERY STIFF. FOUND THE MIXTURE CONTROL UNIT ON ENGINE SEIZED AND VERY HARD TO MOVE BY HAND, REPLACED.
- [SDR 2014FA0000560](https://openairdocs.org/sdr/2014FA0000560.md): Tube · failed · Jul 29, 2014 · N100BG · Cessna T210L · Aircraft Fuel Distribution System
  > ENROUTE, MANIFOLD PRESSURE DROPPED TO 24". INDUCTION TUBE FROM COMPRESSOR TO THROTTLEBODY FAILED WITH A 2" TO 3" HOLE ONLEFT SIDE BLEW OUT.
- [SDR 2013FA0000181](https://openairdocs.org/sdr/2013FA0000181.md): Hose · leaking · Mar 20, 2013 · N732JJ · Cessna T210L · Reciprocating Engine Oil System
  > FIRST GROUND RUN REVEALED A LEAKING OIL PRESSURE TO WASTGATE HOSE OR FITTING. REPLACED FITTING IN ENGINE WITH NEW STEEL FITTING. SECOND GROUND RUN, OIL LEAKED FROM HOSE AGAIN. AFTER SLIGHT ADDITIONAL TORQUE APPLIED AND THIRD GROUND RUN, THE HOSE WAS REPLACED
- [SDR R29R2012062001](https://openairdocs.org/sdr/R29R2012062001.md): Switch · loose · Jun 20, 2012 · N732BB · Cessna T210L · Landing Gear Position and Warning
  > PILOT REPORTED NO GEAR DOWN INDICATION UPON LOWERING THE LANDING GEAR HANDLE. IFE WAS DECLARED, GEAR WAS VISUALLY CONFIRMED DOWN BY GROUND CREW AND ACFT LANDED UNEVENTFULLY. IT WAS DISCOVERED THAT THE JAMB NUT THAT SECURES THE DOWN LOCK SWITCH HAD LOOSENED TO
- [SDR 2011FA0000805](https://openairdocs.org/sdr/2011FA0000805.md): Cylinder · fractured · Nov 15, 2011 · N732GS · Cessna T210L · Reciprocating Engine Cylinder Section
  > 6 NEW CYLINDERS WERE INSTALLED AUG 10, 2008 AT 2812 TOTAL TIME. THE CYLINDERS EXPERIENCED A FAILURE OF THE VALVE GUIDES ON 3 OF THE 6 AT 384 HOURS TIME IN SERVICE. ALL 3 FAILED VALVE GUIDES BROKE OFF AT THE INSERT POINT AND 1 COMPLETELY DISINTEGRATED, CONTAMIN
- [SDR 2009FA0000004](https://openairdocs.org/sdr/2009FA0000004.md): Bolt · failed · Dec 10, 2008 · N9426K · Cessna T210L · Reciprocating Engine Power Section
  > DURING CLIMB TO CRUISE ENGINE MADE A LOUD NOISE AND QUIT RUNNING, ENGINE REMAINED WINDMILLING TO LANDING. VISUAL INSP REVEALED NR 3 CYLINDER ROD BOLT MISSING, ROD CAP EXITED ENG THRU UPPER CASE, NO EVIDENCE OF OIL STARVATION.
- [SDR 2008FA0000546](https://openairdocs.org/sdr/2008FA0000546.md): Control Cable · defective · Jul 17, 2008 · N2423S · Cessna T210L · Trailing Edge Flap Control System
  > ORDERED NEW FLAP FOLLOW UP CABLE; TO REPLACED ORIGINAL CABLE WHICH HAD BECOME DEFECTIVE DUE TO NORMAL USAGE AND AGE.
- [SDR 2008FA0000499](https://openairdocs.org/sdr/2008FA0000499.md): Control Cable · defective · Jul 16, 2008 · N2423S · Cessna T210L · Trailing Edge Flap Control System
  > ORDERED NEW MFG FLAP FOLLOW UP CABLE; TO REPLACE ORIGINAL CABLE WHICH HAD BECOME DEFECTIVE DUE TO NORMAL USAGE AND AGE. THIS CABLE IS SIMILAR TO A THROTTLE CABLE WITH AN INSIDE CABLE WHICH SLIDES IN AN OUTSIDE HOUSING. UPON INSTALLATION, OF NEW MFG FLAP FOLL
- [SDR CA061019009](https://openairdocs.org/sdr/CA061019009.md): Spring · broken · Oct 18, 2006 · Cessna T210L · Magneto/Distributor
  > (CAN) NOTE THE SERIAL NUMBER ON THE ENGINE ON THIS FORM IS INCORRECT IT IS 217469-R. THE IMPULSE COUPLING SPRING WAS FOUND BROKEN. CUSTOMER HAD COMPLAINED OF ROUGH RUNNING CHECK MAG DROP, REMOVED MAGS AND INSPECTED. THE SPRINGS WERE BROKEN IN BOTH MAGNETOS,
- [SDR CA061109004](https://openairdocs.org/sdr/CA061109004.md): Bracket · loose · Sep 22, 2006 · Cessna T210L · Elevator Structure
  > (CAN) BRACKET P/N 1243019-2 FOUND LOOSE AGAINST TORQUE TUBE P/N 1234650-2. LOOSE FASTENERS REMOVED AND REPLACED. (TC NR 20061109004)
- [SDR AOC06001](https://openairdocs.org/sdr/AOC06001.md): Actuator · broken · Mar 16, 2006 · N57977 · Cessna T210L · Landing Gear Retraction/Extension System
  > UPON LANDING, THE NOSE LANDING GEAR COLLAPSED, CAUSING MAJOR DAMAGE TO THE PROPELLER AND DAMAGE TO THE NOSE SECTION OF THE AIRCRAFT. INSPECTION AFTER RECOVERY REVEALED THE THE BEARING END (P/N - 1280600-5) HAD BROKEN, ALSO SHEARING THE PINS (P/N - 1280209-1).
- [SDR AU510001486](https://openairdocs.org/sdr/AU510001486.md): Crankcase · damaged · Dec 12, 2005 · Cessna T210L · Reciprocating Engine Power Section
  > (AUS) CRANKCASE HOLED. LOSS OF POWER IN NR 4 AND NR 6 CYLINDERS. (CASA# 510001486)
- [SDR 2005FA0000697](https://openairdocs.org/sdr/2005FA0000697.md): Pressure Switch · failed · Dec 14, 2004 · N2164S · Cessna T210L · Hydraulic Indicating System
  > LANDING GEAR FAILED TO FULLY RETRACT AFTER TAKEOFF. FOUND THAT THE WIRE SOLDERED TO THE HYDRAULIC POWER PACK PRESSURE SWITCH HAD CORRODED BENEATH THE HEAT-SHRINK TUBING, NEAR THE SOLDER JOINT. SUSPECTED: THE MFG OF THE PRESSURE SWITCH ASSY USED ACID CORE SO
- [SDR CA040622005](https://openairdocs.org/sdr/CA040622005.md): Belt · failed · Jun 6, 2004 · Cessna T210L · Alternator-Generator Drive
  > (CAN) THE ALTERNATOR DRIVE BELT CAME OFF IN FLIGHT.
- [SDR 2004FA0000432](https://openairdocs.org/sdr/2004FA0000432.md): Pump · inoperative · May 21, 2004 · N93379 · Cessna T210L · Engine Fuel Pump
  > ENGINE DRIVEN FUEL PUMP NO METERED OR UN METERED FUEL PRESSURE WHILE ENGINE RUNNING. FUEL PUMP RECENTLY INSTALLED HAD 2.7 HOURS ON IT, AFTER OVERHAUL. INSTALLED NEWLY OVERHAULD PUMP. OPS CHECK GOOD. PROBABLE CAUSE OF PUMP FAILURE, UNKNOWN.
- [SDR 21200004](https://openairdocs.org/sdr/21200004.md): Autopilot Sys · defective · Feb 21, 2004 · N2084S · Cessna T210L · Autopilot System
  > AIRCRAFT PORPOISES WHILE IN ALTITUDE HOLD MODE. DISABLE ALTITUDE HOLD MODE. MAINTENANCE CONFIRMS DEFECTIVE UNIT BY MANUFACTURER. MANUFACTURER UNABLE TO SUPPLY REPLACEMENT PART.
- [SDR 2004FA0000198](https://openairdocs.org/sdr/2004FA0000198.md): Oil Cooler · cracked · Feb 4, 2004 · N732HN · Cessna T210L · Engine Oil Cooler
  > LOWER OB FLANGE OF ENGINE OIL COOLER IS CRACKED AND LEAKING.
- [SDR FPI2003F00015](https://openairdocs.org/sdr/FPI2003F00015.md): Mount · cracked · Dec 9, 2003 · N732HN · Cessna T210L · Engine Oil Cooler
  > TOP FORWARD MOUNT FLANGE CRACKED UNDER NORMAL OPERATION. TOP AT BOTTOM FLANGES ARE NOT TRUE.
- [SDR FPI2003F00014](https://openairdocs.org/sdr/FPI2003F00014.md): Oil Cooler · cracked · Nov 7, 2003 · N732HN · Cessna T210L · Engine Oil Cooler
  > BOTTOM COOLER TO ENGINE MOUNT EAR CRACKED. OCCURRED UNDER NORMAL OPERATION.
- [SDR B30R2003003](https://openairdocs.org/sdr/B30R2003003.md): Cylinder · cracked · Jun 2, 2003 · N732JF · Cessna T210L · Reciprocating Engine Cylinder Section
  > DURING ANNUAL ENGINE INSPECTION A MECHANIC NOTED BLUE FUEL STAIN IN THE AREA OF THE NR 1 CYLINDER FUEL DRAIN PORT. BLUE FUEL STAIN WAS REMOVED AND ENGINE FUEL SYSTEM WAS PRESSURIZED. AT THIS TIME FUEL STARTED TO DRIP FROM IN BETWEEN THE FIRST TWO COOLING FINS
- [SDR 2003FA0000032](https://openairdocs.org/sdr/2003FA0000032.md): Cowling · worn · Dec 31, 2002 · N11KR · Cessna T210L · Nacelle/Pylon, Plate/Skin
  > IT IS POSSIBLE THAT DUE TO NORMAL WEAR OF THE ENGINE COWL CAUSED CONTACT WITH THE NLG DOOR EDGE PREVENTING THE NLG FROM FULLY EXTENDING. IN ADDITION IT IS POSSIBLE THAT DUE TO THE INCORPORATION OF STC SA 5934SW, REMOVING HYDRAULIC POWER FROM THE NLG, ACTUATIO
- [SDR 2003FA0000000](https://openairdocs.org/sdr/2003FA0000000.md): Alternator · seized · Nov 26, 2002 · N2317G · Cessna T210L · AC Generator-Alternator
  > PILOT REPORTED THAT THE LOW VOLTAGE LIGHT ILLUMINATED ON TAXI. MECHANIC FOUND THAT THE ALTERNATOR HAD SEIZED AND THE BELT HAD BROKEN. WHEN THE ALTERNATOR WAS REMOVED, THE MECHANIC NOTED THAT THERE WAS A NOTICEABLE CATCH WHILE ROTATION THE PULLEY. ADDITIONAL
- [SDR DFJ2002F00000](https://openairdocs.org/sdr/DFJ2002F00000.md): Diode · defective · Oct 25, 2002 · N6864C · Cessna T210L · Aileron Control System
  > LANDING GEAR WOULD NOT EXTEND UNTIL STARTING SYSTEM WITH HAND PUMP. FOUND DEFECTIVE DIODE IN DOWN SIDE OF GEAR SELECTOR SWITCH TO CONTACTOR. DIODE LOOKED NORMAL AND HAD NO EXTERNAL DAMAGE.
- [SDR 2002FA0000990](https://openairdocs.org/sdr/2002FA0000990.md): Magneto · corroded · Aug 14, 2002 · N59132 · Cessna T210L · Magneto/Distributor
  > DURING MAINTENANCE, ITS WAS NOTED THAT THE MAGNETOS WERE HAVING TROUBLE HOLDING THEIR TIMING POSITIONS. RT MAGNETO WAS DISASSEMBLED AND FOUND THAT THE DRIVE AND DRIVEN GEARS HAD ROTTED TO THE POINT OF LOSING TEETH. NOTED THAT THE CARBON BUTTON THAT RIDES ON
- [SDR 2002FA0000989](https://openairdocs.org/sdr/2002FA0000989.md): Magneto · corroded · Aug 14, 2002 · N59132 · Cessna T210L · Magneto/Distributor
  > DURING MAINTENANCE, IT WAS NOTED THAT THE MAGNETOS WERE HAVING TROUBLE HOLDING THEIR TIMING POSITIONS. RT MAGNETO WAS DISASSEMBLED AND FOUND THAT THE DRIVE AND DRIVEN GEARS HAD ROTTED TO THE POINT OF LOSING TEETH. NOTED THAT THE CARBON BUTTON THAT RIDES ON T
- [SDR 11482](https://openairdocs.org/sdr/11482.md): Wheel · cracked · Jul 31, 2002 · N94148 · Cessna T210L · Wheel/Ski/Float
  > ON PRECAUTIONARY INSPECTION FOUND CRACKS AT WHEEL/HUB FLANGE MOUNTING BOLT HOLES ON BOTH WHEELS. REPLACED BOTH WHEELS WITH CLEVELAND TWO PIECE WHEELS. WE HAVE FOUND 6 OF THE SAME WHEEL(HUBS)CRACKED ON 172/182/210 CESSNA AIRCRAFT IN THE LAST WEEK. RECOMMEND IMM
- [SDR 2002FA0000588](https://openairdocs.org/sdr/2002FA0000588.md): Alternator · failed · Apr 22, 2002 · N1226M · Cessna T210L · AC Generator-Alternator
  > ALTERNATOR FAILED IN FLIGHT. PILOT SMELLED ELECTRICAL BURNING ODOR. FLIGHT COMPLETED WITHOUT INCIDENT. ALTERNATOR REPLACEMENT CORRECTED PROBLEM. THIS IS THE 2ND ALTERNATOR FAILURE ON THIS ENGINE WITHIN 300.7 HOURS. FAILED ALTERNATOR NOT DISASSEMBLED TO DE
- [SDR 2002FA0000214](https://openairdocs.org/sdr/2002FA0000214.md): Line · corroded · Feb 13, 2002 · N711PJ · Cessna T210L · Aircraft Fuel Distribution System
  > LINE DEVELOPED PINHOLE LEAK DUE TO CORROSION WHERE CABIN VENT SCEET HOSE RESTED ON TOP OF IT.
- [SDR 2001FA0000361](https://openairdocs.org/sdr/2001FA0000361.md): Rib · cracked · Sep 20, 2001 · N375AB · Cessna T210L · Wing, Rib/Bulkhead
  > LEFT WING RIB CRACKED WHERE LEFT FLAP BELLCRACK SUPPORT BRACKETS ARE MOUNTED, CRACK RUNS FROM INBOARD LOWER SUPPORT BRACKET RIVET HOLE APPROX. ONE(1) INCH IN LENGTH DOWN AND TO THE LEFT. PROBABLE CAUSE: FLAPS EXTENDED AT TOO HIGH OF AN AIRSPEED.
- [SDR NMO192](https://openairdocs.org/sdr/NMO192.md): Hose · failed · Sep 12, 2001 · N6721M · Cessna T210L · Landing Gear Retraction/Extension System
  > DURING LANDING, NOSE GEAR EXTENDED AND LOCKED, BUT MAIN GEAR DID NOT LOCK INTO PLACE. PILOT TRIED TO LOCK MAIN GEAR USING HAND HYDRAULIC PUMP WITH NO SUCCESS. AIRCRAFT LANDED WITH LOCKED NOSE GEAR AND COLLAPSED MAIN GEAR. SUFFERED DAMAGE TO REAR OF FUSELAGE, L
- [SDR 20010613CW002](https://openairdocs.org/sdr/20010613CW002.md): Control Cable · slipped · May 26, 2001 · N93344 · Cessna T210L · Trailing Edge Flap Control System
  > DURING 100 HR INSPECTION, FOUND FLAPS NOT WORKING PROPERLY, FOUND CONTROL PUSH/PULL CABLE OUTER HOUSING WHERE HOUSING IS CLAMPED, SLIPPING IN CLAMP BUSHING. ORDER NEW CABLE FROM CESSNA, IT WAS TOO SHORT, CALLED CESSNA AND FOUND THEIR STOCK WAS MANUFACTURED WR
- [SDR 20000821SH009](https://openairdocs.org/sdr/20000821SH009.md): Magneto · corroded · Aug 11, 2000 · N94203 · Cessna T210L · Magneto/Distributor
  > PRESSURIZED SLICK MAGNETOS ON CESSNA T210L. DURING ANNUAL, INSPECTED MAGS INTERNALLY FOR CONDITION. FOUND SEVERE MOISTURE-CASED CORROSION ALL AROUND INSIDE. MAGNETO MANUAL CALLS FOR INSPECTION OF 6200 SERIES EACH 100 HOURS, NOTHING FOUND FOR INSPECTION OF 6
- [SDR 20000821SH008](https://openairdocs.org/sdr/20000821SH008.md): Magneto · corroded · Aug 11, 2000 · N94203 · Cessna T210L · Magneto/Distributor
  > PRESSURIZED SLICK MAGNETOS ON CESSNA T210L. DURING ANNUAL, INSPECTED MAGS INTERNALLY FOR CONDITION. FOUND SEVERE MOISTURE-CASED CORROSION ALL AROUND INSIDE. MAGNETO MANUAL CALLS FOR INSPECTION OF 6200 SERIES EACH 100 HOURS, NOTHING FOUND FOR INSPECTION OF 6
- [SDR B3OR200000002](https://openairdocs.org/sdr/B3OR200000002.md): Skin Panel · loose · Jul 26, 2000 · N732JF · Cessna T210L · Fuselage Main, Plate/Skin
  > AIRCRAFT WAS TEST FLOWN DUE TO HIGH CO LEVEL DISCOVERED IN ANOTHER 210 SERIES FLEET AIRCRAFT. PILOTS FOUND UNACCEPTABLE LEVEL OF CO IN CABIN USING TOXIBEE CO DETECTOR. MAINTENANCE FOUND EXHAUST GASES ENTERING TAILCONE THROUGH VENT HOLE FOR STC SA71RM AIR CONDI
- [SDR CA000802024](https://openairdocs.org/sdr/CA000802024.md): Bracket · cracked · Jul 14, 2000 · Cessna T210L · Elevator Control System
  > (CAN) DURING THE INSPECTION OF THE STABILIZER, A CRACK WAS FOUND ON THE INBOARD LT STABILIZER BRACKET TO ELEVATOR P/N 1232624-1 ATTACHED TO THE SPAR. PROBLEM WAS REPAIRED.
- [SDR CA000802023](https://openairdocs.org/sdr/CA000802023.md): Solenoid · failed · Jul 14, 2000 · Cessna T210L · Landing Gear Retraction/Extension System
  > (CAN) AFTER TAKEOFF AND LANDING SELECTED UP AND LOCKED. LANDING GEAR CIRCUIT BREAKER TRIPPED. (PROBLEM RETURNED INTERMITTENTLY.) PROBLEM TRACED TO DEFECTIVE LANDING GEAR SOLENOID. SOLENOID REPLACED, PROBLEM SOLVED.
- [SDR 20000522SH016](https://openairdocs.org/sdr/20000522SH016.md): Riser · cracked · May 15, 2000 · N732JF · Cessna T210L · Engine Collector/Tailpipe/Nozzle
  > MAINTENANCE LOOKED AT ACFT BEFORE FLIGHT. COWLING WAS REMOVED AND EXHAUST SOOT WAS SEEN AROUND LOWER SIDE OF NR 4 CYLINDER. FURTHER INVESTIGATION REVEALED A CRACK AROUND THE EXHAUST RISER THAT WAS ABOUT 270 DEGREES AROUND THE PIPE. HEAT EXCHANGER PORTION OF
- [SDR 20000417SH016](https://openairdocs.org/sdr/20000417SH016.md): Link · cracked · Mar 13, 2000 · N6864C · Cessna T210L · Landing Gear Retraction/Extension System
  > DURING ROUTINE INSPECTION, FOUND UPPER TORQUE LINK CRACKED. SUBMITTER STATED THIS PART NUMBER LINK WAS FOUND CRACKED ON ANOTHER T210L IN THE SAME FLEET. (X)
- [SDR 99ZZZX2978](https://openairdocs.org/sdr/99ZZZX2978.md): Skin · cracked · Jul 1, 1999 · N4687Q · Cessna T210L · Wing, Plate/Skin
  > THE TRAILING EDGE OF THE AIRCRAFT WING INBOARD OF THE SPEED BRAKE LOCATION. THE DISTURBED AIR BEHIND THE EXTENDED SPEED BRAKES WAS WORKING THE TRAILING EDGE OF THE WING CAUSING CRACKS AROUND THE TRAILING EDGE ATTACHMENT RIVETS.
- [SDR 99ZZZX2772](https://openairdocs.org/sdr/99ZZZX2772.md): Reinforcement · cracked · Jun 25, 1999 · N61170 · Cessna T210L · Horizontal Stabilizer Structure
  > REINFORCEMENT P/N 1232623-2 NOTED AS CRACKED. THE AIRCRAFT HAD NOT HAD SE84-17 C/W, SO THE NEW BRACKETS ORDERED. IT WAS SUGGESTED CHANGE COULD BE DONE WITHOUT COMPLETELY REMOVING THE HORIZONTAL STABILIZER. SUBMITTER ELECTED TO REMOVE THE STABILIZER AND INSP
- [SDR 99ZZZX2771](https://openairdocs.org/sdr/99ZZZX2771.md): Fitting · loose · Jun 25, 1999 · N61170 · Cessna T210L · Horizontal Stabilizer Structure
  > REINFORCEMENT P/N 1232623-2 NOTED AS CRACKED. THE AIRCRAFT HAD NOT HAD SE84-17 C/W, SO THE NEW BRACKETS ORDERED. IT WAS SUGGESTED CHANGE COULD BE DONE WITHOUT COMPLETELY REMOVING THE HORIZONTAL STABILIZER. SUBMITTER ELECTED TO REMOVE THE STABILIZER AND INSP
- [SDR 99ZZZX1193](https://openairdocs.org/sdr/99ZZZX1193.md): Control Cable · malfunctioned · Mar 8, 1999 · N10419 · Cessna T210L · Trailing Edge Flap Control System
  > WHEN FLAP FOLLOW-UP CABLE IS INSTALLED IN AIRCRAFT, IT HAS AN INTERNAL BIND WHICH CAUSES THE BELLCRANK IN THE LEFT WING TO 'JERK' AS THE MOTION OF THE BELLCRANK OVERCOMES THE BINDING OF THE CABLE. THIS 'JERKING' CAUSES THE RIB TO WHICH THE BELLCRANK IS ATTACH
- [SDR 99ZZZX1195](https://openairdocs.org/sdr/99ZZZX1195.md): Reinforcement · cracked · Jan 18, 1999 · N93155 · Cessna T210L · Horizontal Stabilizer Structure
  > WHEN A 1 INCH LONG CRACK WAS NOTED ON ANOTHER T210 HORIZONTAL STABILIZER AFT SPAR, THIS AIRCRAFT WAS INSPECTED AND A CRACK WAS NOTED ON THE AFT SPAR REINFORCEMENT. WHEN THE STABILIZER WAS REMOVED, THE LEFT FORWARD FITTING (PN 0732601-5) WAS NOTED TO HAVE 4 OF
- [SDR 99ZZZX706](https://openairdocs.org/sdr/99ZZZX706.md): Battery Box · leaking · Jul 15, 1998 · N2259S · Cessna T210L · Battery Box Structure
  > DURING ANNUAL INSPECTION, BATTERY ACID WAS FOUND TO HAVE LEAKED INTO COCKPIT ONTO LEFT RUDDER PEDAL, ATTACHING TUBING, AND GENERAL AREA BELOW PEDAL. ACID HAD FLOWED THROUGH CORRODED RIVET HOLE ONTO SEAT FOR CABIN HEAT AND DRIPPED INTO FLOOR AREA. SUBMITTER B
- [SDR 98ZZZX2356](https://openairdocs.org/sdr/98ZZZX2356.md): Plunger · worn · Jun 13, 1998 · N732GR · Cessna T210L · Aircraft Fuel Filter/Strainer
  > FUEL STRAINER PLUNGER NIPPLE WEARING.
- [SDR 98ZZZX2037](https://openairdocs.org/sdr/98ZZZX2037.md): Cowling · mismanufactured · May 13, 1998 · N2317G · Cessna T210L · Engine Cowling System
  > THIS NEW COWL WAS PURCHASED FROM CESSNA AND IT HAS TWO PROBLEMS. 1. THE TOP LEADING EDGE IS TOO THICK IN PLACES (FILLER OR ADHESIVE) AND WILL NOT CONTOUR WITH EXISTING NOSE COWL. 2. ON THE AFT EDGE, THERE IS NOT ENOUGH MATERIAL, AN APPROXIMATE.25 INCH GA

Next page: https://openairdocs.org/model/cessna-t210l/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 = 'T210L'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-t210l/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.