# Service difficulty reports: Textron 510

A list on [Textron 510](https://openairdocs.org/model/textron-510.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 88 reports

- [SDR O9IA20260730167](https://openairdocs.org/sdr/O9IA20260730167.md): Oil System · malfunctioned · Jul 30, 2026 · N171AA · Cessna 510 · Engine Oil Indicating System
  > RT ENG OIL PRESSURE DROPPED TO 0 ON APPROACH INTO HIO FROM PAE. PRESSURE JUMPED UP INTO GREEN & SPIKED INTO RED & STAYED THERE. ENG THEN SHUTDOWN INFLT ON APPROACH. PILOT DECLARED AN EMERGENCY & LANDED WITHOUT INCIDENT. MAINT CHKD OIL LEVEL ON ENGS & BOTH W
- [SDR 2026FA0000133](https://openairdocs.org/sdr/2026FA0000133.md): Pressure Switch · leaking · Feb 18, 2026 · N79SG · Cessna 510 · Aircraft Fuel Distribution System
  > REPEATED FAILURE OF FUEL PRESSURE SWITCH P/N: 9912033-2 CAUSING FUEL TO LEAK FROM THE WEEP HOLE OF THE SWITCH BODY. FUEL THEN LEAKS INTO THE COWLING. FAILURES INCLUDE SWITCH S/N'S: 13646, 13661, 13262 ALL FAILURES HAVE OCCURRED WITHIN A 12-MONTH PERIOD OF 01/2
- [SDR 2025FA0000087](https://openairdocs.org/sdr/2025FA0000087.md): Windshield · fractured · Jan 30, 2025 · N4PG · Cessna 510 · Flight Compartment Windows
  > THE OUTER (GLASS) PANE OF THE PILOT SIDE WINDSHIELD FRACTURED DURING CLIMB OUT THROUGH FL180. THE INNER (ACRYLIC) PANE AND PRIMARY STRUCTURE OF THE WINDSHIELD WAS FULLY INTACT AND UNDAMAGED.
- [SDR 2023FA0000284](https://openairdocs.org/sdr/2023FA0000284.md): Sensor · failed · Apr 20, 2023 · N510PX · Cessna 510 · Engine Oil Indicating System
  > LOSS OF OIL PRESSURE INDICATION ON LEFT ENGINE. ACTUAL PROBLEM WAS A BAD PRESSURE SENSOR. SINGLE POINT OF FAILURE. THERE IS NO BACK UP TO THIS INDICATION.
- [SDR 2023FA0000186](https://openairdocs.org/sdr/2023FA0000186.md): Shuttle Valve · unserviceable · Mar 26, 2023 · N88CH · Cessna 510 · Landing Gear Retraction/Extension System
  > DURING TAKEOFF, THE CREW REPORTED THE RH GEAR DOWN/LOCKED (GREEN) LIGHT DID NOT EXTINGUISH AND THE TRANSIT LIGHT STAYED ON. THE CREW FOLLOWED THE AFM PROCEDURE AND RESET AND ATTEMPTED A SECOND GEAR RETRACTION WITH NO SUCCESS. MX PERFORMED MULTIPLE GEAR SWINGS
- [SDR 2021FA0000012](https://openairdocs.org/sdr/2021FA0000012.md): Starter Gen · detached · Jan 8, 2021 · N22EM · Cessna 510 · Starter-Generator
  > RIGHT ENGINE STARTER GENERATOR FAILED IN FLIGHT AND WAS SEVERED FROM THE ENGINE. THE FRONT OF THE STARTER/GENERATOR WAS STILL ATTACHED TO THE GEARBOX AND THE UNIT WAS HANGING BY ITS WIRING AND COOLING BOOT. THE GEAR BOX WAS CRACKED DURING THIS EVENT AND WILL
- [SDR JGVR20200218001](https://openairdocs.org/sdr/JGVR20200218001.md): Bellcrank · wrong part · Feb 18, 2020 · N91FP · Cessna 510 · Aileron Control System
  > DURING A DOCUMENT 16 INSPECTION FOUND AILERON WING CABLES TO BE WORN REQUIRING REPLACEMENT. AFTER THE REPLACEMENT OF THE AILERON WING CABLES AND DURING THE RIGGING OF THE R/H AILERON IT WAS FOUND THAT THE AILERON COULD NOT BE RIGGED TO THE REQUIRED 2 DEGREES
- [SDR CA190604007](https://openairdocs.org/sdr/CA190604007.md): Warning Message · illuminated · May 23, 2019 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) PILOT REPORTED ITT SPIKE INTO THE YELLOW RANGE DURING TAKE-OFF ON THE RIGHT HAND ENGINE. THE TAKE-OFF WAS ABORTED BEFORE AIRCRAFT LEAVE THE GROUND AND RETURNED TO BACK RAMP FOR TROUBLESHOOTING.
- [SDR 11FA2019070100001](https://openairdocs.org/sdr/11FA2019070100001.md): Engine · malfunctioned · May 23, 2019 · N820UT · Cessna 510 · Engine (Turbine/Turboprop)
  > ITT SPIKE NR 2 ENGINE EXCEEDED REDLINE. ENGINE AND FADEC REMOVED AND SENT TO PWC FOR TEARDOWN INSPECTION.
- [SDR 11FA2019070100002](https://openairdocs.org/sdr/11FA2019070100002.md): Unknown · malfunctioned · May 20, 2019 · N820UT · Cessna 510 · Engine EGT/TIT Indicating System
  > ITT SPIKE IN THE CLIMB FOR UNKNOWN REASONS. MANUALLY ADJUSTED POWER SETTING AND NORMAL OPERATIONS RESUMED.
- [SDR CA190524003](https://openairdocs.org/sdr/CA190524003.md): Housing · damaged · May 13, 2019 · Cessna 510 · Turbine Engine Compressor Section
  > (CAN) DURING TAKE-OFF ROLL CREW NOTICED ENGINE HIGH ITT AT RED BAND. AIRCRAFT RETURNED TO ITS ORIGINAL DEPARTURE AND LANDED UNEVENTFULLY. TROUBLESHOOTING IS ONGOING. (TC# 20190524003)
- [SDR NI6R201805220048](https://openairdocs.org/sdr/NI6R201805220048.md): Controller · malfunctioned · May 22, 2018 · N223PW · Cessna 510 · Cabin Pressure Controller
  > PILOT REPORTED THAT DURING CLIMB CABIN PRESSURE INCREASED TO OVER 8 PSI, AND WOULD NOT DECREASE. AIRCRAFT RETURNED TO THE AIRPORT AND USED THE MANUAL DEPRESSURIZATION SWITCH TO DEPRESSURIZE THE CABIN. VISUAL INSPECTIONS WERE CONDUCTED OF THE PRESSURIZATION S
- [SDR 2017FA0000225](https://openairdocs.org/sdr/2017FA0000225.md): Cable · worn · May 31, 2017 · N620WB · Cessna 510 · Aileron Control System
  > FOUND LEFT AILERON LOWER WING CABLE RUBBING NEAR WS 273 FAIRLEAD. REPLACED THE LEFT AILERON LOWER WING CABLE IAW MM 27-10-00.
- [SDR 2017FA0000224](https://openairdocs.org/sdr/2017FA0000224.md): Cable · worn · May 31, 2017 · N620WB · Cessna 510 · Aileron Control System
  > FOUND LEFT AILERON LOWER WING CABLE RUBBING NEAR WS 273 FAIRLEAD. REPLACED THE LEFT AILERON LOWER WING CABLE FROM OUTBOARD SECTOR TO TURNBUCKLE IAW MM 27-10-00.
- [SDR CNQ4N510BK052017](https://openairdocs.org/sdr/CNQ4N510BK052017.md): Precooler · ruptured · May 15, 2017 · N510BK · Cessna 510 · Pneumatic Distribution System
  > AFTER TAKE OFF, OPERATOR REPORTED THE LEFT ENGINE DUCT OVERHEAT ANNUNCIATOR ILLUMINATED. THE OPERATOR REDUCED THE ENGINE POWER SETTINGS, LANDED BACK TO DEPARTURE. INVESTIGATION REVEALED THE LEFT ENGINE BLEED AIR PRE-COOLER HAD RUPTURED CAUSING THE DUCT OVER
- [SDR 2016FA0000244](https://openairdocs.org/sdr/2016FA0000244.md): Regulator · leaking · Mar 15, 2016 · N397CM · Cessna 510 · Crew Oxygen System
  > OXYGEN BOTTLE RECEIVED FROM REPAIR SHOP FOR FITMENT TO AIRCRAFT. ON FITMENT OF OXYGEN BOTTLE ASSY DURING 30 MINUTE LEAK TEST IAW MM, REV 12, 35-10-00, REV 8, 6, B 11A. LEAK DETECTED FROM PRESSURE REGULATOR ON/OFF VALVE. PART REMOVED FROM AIRCRAFT AND RETURN
- [SDR CA160216013](https://openairdocs.org/sdr/CA160216013.md): Oil System · low pressure · Feb 12, 2016 · Cessna 510 · Turbine Engine Oil System
  > (CAN) THE FLIGHT CREW OBSERVED A RED INDICATION ON THE NR 2 ENGINE OIL PRESSURE DISPLAY. THE FLIGHT CREW ACTIONED THE ABNORMAL PROCEDURES CHECKLIST, DETERMINED IT WAS A FAULTY INDICATION AND CONTINUED WITH THE DESCENT. WHILE ON LEFT BASE TO RUNWAY 35, THE MAST
- [SDR O9IA20160205001](https://openairdocs.org/sdr/O9IA20160205001.md): Downlock Switch · out of tolerance · Feb 3, 2016 · N910GF · Cessna 510 · Landing Gear Position and Warning
  > NORMAL FLIGHT, GEAR RETRACTED NORMALLY UPON DEPARTURE. UPON ARRIVAL ESTABLISHED IN THE DOWNWIND SLOWED BELOW 185 & PUT FLAPS TO TO & APP ABEAM THE NRS, LOWERED THE GEAR & ONLY GOT DOWN & LOCKED INDICATIONS FOR THE MAINS, NO NOSE WHEEL. BROKE OUT OF THE PATTE
- [SDR CA160204007](https://openairdocs.org/sdr/CA160204007.md): Transducer · failed · Feb 2, 2016 · Cessna 510 · Engine Oil Indicating System
  > (CAN) TRANSDUCERS SEEM TO HAVE A SHORT LIFE LIMIT AND GIVE IRRATIC, FALSE INDICATIONS WHEN THEY FAIL IN FLIGHT.
- [SDR 2016FA0000019](https://openairdocs.org/sdr/2016FA0000019.md): Actuator · failed · Jan 12, 2016 · N510J · Cessna 510 · Landing Gear Actuator
  > DURING APPROACH, THE LANDING GEAR WAS SELECTED DOWN AND THE LT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE AND GEAR UNSAFE WAS ILLUMINATED. THE GEAR WAS CYCLED 2 ADDITIONAL TIMES WITH NO CHANGE. THE PILOT USED THE PROCEDURES ON THE EMERGENCY CHECKLIST AND USED
- [SDR YGJA201512290001](https://openairdocs.org/sdr/YGJA201512290001.md): Control Cable · worn · Dec 29, 2015 · N417G · Cessna 510 · Aileron Control System
  > WHILE PERFORMING A DOC 1 INSPECTION, 450 HR INTERVAL, THE RT LOWER INBD AILERON CABLE WAS FOUND WORN AT THE FAIRLEAD. THE WEAR WAS MORE THAN 50 PERCENT WHICH REQUIRES REPLACEMENT.
- [SDR CA151030010](https://openairdocs.org/sdr/CA151030010.md): Oil System · pressure loss · Oct 25, 2015 · Cessna 510 · Engine Oil Indicating System
  > (CAN) DURING TAXI BEFORE TAKEOFF FOR A TEST FLIGHT AFTER MAINTENANCE, THE PILOT RECEIVED A NR 2 ENGINE OIL PRESSURE LOW WARNING. TAKEOFF WAS ABORTED AND THE ACFT TAXIED BACK TO SERVICE CENTER. TROUBLESHOOTING IS ON-GOING.
- [SDR CA151015014](https://openairdocs.org/sdr/CA151015014.md): Engine · malfunctioned · Oct 9, 2015 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) DURING FLIGHT IN CRUISE AT FL380 IN ICE CONDITION, A RED X INDICATION APPEARED IN THE OIL PRESSURE INDICATION. PILOT FOLLOWED PILOT OPERATING HANDBOOK ABNORMAL PROCEDURE AND FOUND NO FURTHER ABNORMALITIES INDICATIONS. PILOT TRIED RESETTING EEC. NO EFFECT
- [SDR ON0A2015FA0000542](https://openairdocs.org/sdr/ON0A2015FA0000542.md): Starter Gen · failed · Oct 9, 2015 · N30NF · Cessna 510 · Starter-Generator
  > LEFT ENGINE GENERATOR FAILED IN FLIGHT, CREW RECEIVED GENERATOR FAIL CAS AND FELT VIBRATION THROUGH THE AIRFRAME.
- [SDR CA150925003](https://openairdocs.org/sdr/CA150925003.md): Engine · power loss · Sep 4, 2015 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) THE PILOT REPORTED THAT AFTER NOTICING AN INCREASING IN RAT INDICATION AND A DECREASING IN THE RATE OF CLIMB,BOTH ENGINES ROLLED BACK. "NORMALLY THE ENGINE ROLL BACK IS PREDATED BY A T2 HEATER FAIL L/R. BUT WAS NOT THE CASE. SINCE THE RATE OF CLIMB WAS V
- [SDR CA150911006](https://openairdocs.org/sdr/CA150911006.md): Engine · power loss · Sep 3, 2015 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) THE LT ENGINE HAD A UNCOMMANDED POWER ROLL BACK. NO T2 HTR CAS MESSAGE APPEARED. IT OCCURRED DURING CLIMB IN IMC, SUPER MOIST, LIGHT ICE, AROUND FL270.
- [SDR 2015FA0000325](https://openairdocs.org/sdr/2015FA0000325.md): Circuit Board · failed · Jul 16, 2015 · N511TP · Cessna 510 · Landing Gear System Wiring
  > PILOT FOR ACFT INFORMED THE TOWER THAT HE HAD NO POSITIVE GEAR DOWN AND LOCKED INDICATION, THE TOWER DECLARED AN EMEMERGENCY LANDING. PILOT SELECTED GEAR DOWN AND HAD NO GREEN LIGHT INDICATION FOR DOWN AND LOCKED. HE BLEW GEAR AND STILL HAD NO LIGHT DOWN AND
- [SDR 2GYR2015FA0000247](https://openairdocs.org/sdr/2GYR2015FA0000247.md): Cable · displaced · May 29, 2015 · N620WB · Cessna 510 · Aileron Control System
  > WHILE IN THE PROCESS OF PERFORMING AN INSPECTION ON ACFT. FOUND IN THE RT WING, AILERON WING SECTOR AREA, THE CABLE COMPLETELY OFF THE PULLEY. THE REFERENCE FOR THIS PULLEY IS 27-10-00, FG. 3, IT 50, PN S3504-4.5. LOW FRICTION PULLEY, RT.
- [SDR 2015FA0000186](https://openairdocs.org/sdr/2015FA0000186.md): Control Cable · worn · May 8, 2015 · Cessna 510 · Aileron Control System
  > AILERON CABLES INSTALLED ALONG THE REAR WING SPAR PASS THROUGH THE WING RIBS WITH FAIR LEADS. EVERY 450 HOUR INSPECTION OF THE ACFT REVEAL THESE CABLES ARE WORN BEYOND LIMITS AND REQUIRE REPLACEMENT. THE CABLES ARE CHAFING ON THE FAIR LEADS DUE TO INSUFFICIENT
- [SDR SBBA20150501001](https://openairdocs.org/sdr/SBBA20150501001.md): Transducer · defective · Apr 25, 2015 · N510KZ · Cessna 510 · Engine Oil Pressure
  > WHILE IN CRUISE FLIGHT THE LT ENG OIL PRESS INDICATIONS BEGAN TO FLUCTUATE ENOUGH TO TRIP THE MASTER WARNING SYS. PILOT FOLLOWED AFM PROCEDURES & BROUGHT ENG TO IDLE. THIS DID NOT HELP THE INDICATIONS, THE ENG WAS SHUT DOWN AS AN AFM REQUIREMENT. TROUBLESHO
- [SDR CA150205007](https://openairdocs.org/sdr/CA150205007.md): Carbon Seal · leaking · Jan 26, 2015 · Cessna 510 · Turbine Engine Oil System
  > (CAN) DURING FLIGHT, THE OIL PRESSURE DROPPED TO THE LOW SIDE, AND THE PILOT REDUCED POWER TO IDLE, BUT DID NOT SHUT IT DOWN. THE TROUBLESHOOTING REVEALED THE SIGHT GLASS WAS EMPTY UPON CHECKING, AND THE OIL FILTER BYPASS INDICATOR WAS POPPED. THE CARBON PARTI
- [SDR CA150205003](https://openairdocs.org/sdr/CA150205003.md): Engine · malfunctioned · Jan 22, 2015 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) PILOT REPORTED THAT DURING THE DESCENT, WHEN PASSING FL250, THEY HEARD A NOISE ON THE ENGINE NR 2, WHILE BOTH ENGINES WHERE BELOW CRUISE POWER. THE AIRCRAFT DIVERTED. DURING THE TROUBLESHOOTING, BOTH ENGINE SPOOLS (LOW AND HIGH POWER) ROTATED NORMALLY. A
- [SDR CA141202020](https://openairdocs.org/sdr/CA141202020.md): Oil System · empty · Nov 20, 2014 · Cessna 510 · Turbine Engine Oil System
  > (CAN) DURING FLIGHT THE PILOT NOTICED OIL PRESSURE FLUCTUATING. THE PILOT ELECTED TO START DESCENT AND THE PRESSURE CONTINUED DECREASING INTO THE RED BAND. THE PILOT THEN SHUT THE ENGINE DOWN, AND DECLARED AN EMERGENCY WHERE HE PERFORMED AN UNEVENTFUL SINGLE E
- [SDR CA141202014](https://openairdocs.org/sdr/CA141202014.md): Warning Message · illuminated · Nov 15, 2014 · Cessna 510 · Engine Indicating System
  > (CAN) LEFT ENGINE CONTROL AMBER MESSAGE ILLUMINATED IN THE DECENT. THROTTLE RETARDED TO IDLE BUT ENGINE REMAINED AT 55% UNTIL PASSING THROUGH 4,000FT. WARNING REMAINED UNTIL POWER CYCLED ON THE GROUND. THE AIRCRAFT IS AWAITING DOWNLOAD ANALYSIS.
- [SDR CA141202013](https://openairdocs.org/sdr/CA141202013.md): Engine · power loss · Nov 14, 2014 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) WHILE ENROUTE AT ABOUT FL300 IN POOR WEATHER AND CONSTANT ICING CONDITIONS, BOTH ENGINES POWER ROLLBACK. THE LT ENGINE RECOVERED BUT SUFFERED SIGNIFICANT FLUCTUATIONS. THE PILOT WANTED TO CLIMB HIGHER BUT THE ACFT WOULD NOT RESPOND, CHOSE TO DESCEND AND
- [SDR 2014FA0000587](https://openairdocs.org/sdr/2014FA0000587.md): Engine · malfunctioned · Oct 3, 2014 · N510BK · Cessna 510 · Engine (Turbine/Turboprop)
  > RT ENGINE SHUTDOWN AT FL370 FOR AN HOUR AT CRUISE WITH NO ISSUE. STARTED TO CLIMB, AND ABOUT 2-3 MINUTES LATER AT ABOUT 39,500" HAD THE RT ENGINE OIL TEMPERATURE CLIMB HIGH, REDUCED POWER. IT KEPT CLIMBING AFTER STABILIZING FOR A SHORT BIT EACH TIME THE P
- [SDR CA141020010](https://openairdocs.org/sdr/CA141020010.md): Belt · failed · Oct 2, 2014 · Cessna 510 · Cabin Cooling System
  > (CAN) AIR CONDITIONING SYSTEM DRIVE BELT FAILED AT ONLY 279.2 HRS TTAF.
- [SDR CA140915014](https://openairdocs.org/sdr/CA140915014.md): Starter Gen · failed · Sep 6, 2014 · Cessna 510 · Starter-Generator
  > (CAN) NR 2 ENGINE STARTER GENERATOR FAILED DURING FLIGHT AND WAS CASUING ENGINE VIBRATION. UPON INSPECTION FOLLOWING REMOVAL THE STARTER GENERATOR WAS FOUND TO HAVE INTERNAL BEARING FAILURE CAUSING THE VIBRATION.
- [SDR CA140630003](https://openairdocs.org/sdr/CA140630003.md): Engine · failed · Jun 13, 2014 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) THE PILOT HEARD A LOUD NOISE FOLLOWED BY ENGINE PARAMETERS GOING INTO THE RED BAND. UPON INITIATING ENGINE SHUTDOWN, HEARD ANOTHER LOUD NOISE FOLLOWED BY SMOKE IN THE COCKPIT. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPL
- [SDR 2014FA0000360](https://openairdocs.org/sdr/2014FA0000360.md): Uplock Switch · intermittent · Jun 3, 2014 · N759SB · Cessna 510 · Landing Gear Retraction/Extension System
  > DURING APPROACH, GEAR WAS SELECTED DOWN AND INDICATED 3 GREEN AND THE RED GEAR UNSAFE LIGHT WAS ON. GEAR WAS RETRACTED AND GEAR INDICATION WAS NORMAL ALL LIGHTS EXTINGUISHED. A SECOND APPROACH WAS ATTEMPTED AND WHEN GEAR DOWN WAS SELECTED THE INDICATION WAS 3
- [SDR CNQR201307181381](https://openairdocs.org/sdr/CNQR201307181381.md): Wire · broken · Jul 15, 2013 · N264CA · Cessna 510 · Landing Gear Position and Warning
  > AFTER TAKEOFF AND GEAR RETRACTED, DID NOT GET A GEAR RETRACTED INDICATION. GEAR CYCLED SEVERAL TIMES WITH NO CHANGE IN INDICATION. A WIRE WAS FOUND BROKEN ON THE NOSE DOWNLOCK SWITCH.
- [SDR CA130408009](https://openairdocs.org/sdr/CA130408009.md): Wire · damaged · Apr 3, 2013 · Cessna 510 · Window System Wiring
  > (CAN) ON A RECENT TRIP, THE PILOT NOTED PRIOR TO TAKEOFF A CAS MESSAGE DISPLAYING LT WINDSHIELD HEAT FAILURE. ACFT RETURNED TO THE RAMP AND FURTHER INVESTIGATION WAS CARRIED OUT SUSPECTING A BAD WINDSHIELD HEAT CONTROLLER. PLANS WERE TO SWAP THE 2 CONTROLLER
- [SDR 2013F00039](https://openairdocs.org/sdr/2013F00039.md): Bearing · failed · Feb 24, 2013 · N91FP · Cessna 510 · Starter-Generator
  > LEFT ENGINE STARTER/GEN FAILED. REAR BEARING FAILURE.
- [SDR 2013F00038](https://openairdocs.org/sdr/2013F00038.md): Bearing · failed · Dec 6, 2012 · N91FP · Cessna 510 · Starter-Generator
  > RIGHT ENGINE STARTER/GEN FAILED. REAR BEARING FAILURE.
- [SDR CA121105015](https://openairdocs.org/sdr/CA121105015.md): Engine · odor · Oct 23, 2012 · Cessna 510 · Turbine Engine Oil System
  > (CAN) FOLLOWING T/O, THE CREW REPORTED A STRONG BURNING SMELL FOLLOWED BY BLUE TINGED SMOKE. ENGINES INDICATIONS WERE FOUND NORMAL. THE PILOT REQUESTED A PRIORITY RETURN TO THE DEPARTURE AIRPORT AND THE A/C LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTIONS SHOW
- [SDR 2012FA0000652](https://openairdocs.org/sdr/2012FA0000652.md): Ferrule · cracked · Sep 26, 2012 · N949JB · Cessna 510 · Trailing Edge Flap Control System
  > DURING A SCHEDULED INSPECTION, THE FERRULE ON THE RT FLAP FLEX SHAFT OUTER HOUSING WAS FOUND CRACKED. CRACK WAS ON THE END WHERE THE CABLE ATTACHES TO THE FLAP ACTUATOR.
- [SDR 2012FA0000647](https://openairdocs.org/sdr/2012FA0000647.md): Duct · delaminated · Sep 26, 2012 · N949JB · Cessna 510 · Turbine Engine Bypass Section
  > AFT BYPASS DUCT WAS FOUND DELAMINATED DURING A SCHEDULED INSPECTION.
- [SDR CA120903005](https://openairdocs.org/sdr/CA120903005.md): Engine · vibration · Aug 28, 2012 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) DURING FLIGHT, THE PILOT FELT SUDDEN HEAVY VIBRATIONS WITH A RISING ENGINE TEMPERATURE. THE ENGINE WAS SHUTDOWN AND SECURED BEFORE AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED. POST FLIGHT INSPECTION FOUND SEIZED TURBINES. THE ENGINE WILL BE R
- [SDR CA120821003](https://openairdocs.org/sdr/CA120821003.md): Engine · vibration · Aug 12, 2012 · Cessna 510 · Engine (Turbine/Turboprop)
  > (CAN) APPROXIMATELY 30 MIN AFTER DEPARTURE, THE PILOT FELT A SMALL VIBRATION. 10 MINUTES LATER, THE FOLLOWING CAS MESSAGE WAS SEEN: GEN OFF L. AFTER ANOTHER 45 MIN, DURING APPROACH TO LFPB, OIL PRESSURE RAISED AND THEN DECREASED TO 0 PSI. ENGINE WAS SHUTDOWN
- [SDR CA120814006](https://openairdocs.org/sdr/CA120814006.md): Pushrod · undertorqued · Aug 10, 2012 · Cessna 510 · Elevator Control System
  > (CAN) DURING THE 36 MONTH CHECK THE AREA OF THE ELEVATOR CONTROL SYS SECTOR AND HORN WAS ACCESSED FOR THE FIRST TIME SINCE THE ACFT WAS NEW AND IT WAS FOUND THE BOLTS WERE NOT TORQUED CORRECTLY AND THAT BOTH THE BOLTS COULD BE SLID BACK AND FORTH IN THE ROD AN

Next page: https://openairdocs.org/model/textron-510/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 = '510'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/textron-510/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.