# Service difficulty reports: Cessna 414

A list on [Cessna 414](https://openairdocs.org/model/cessna-414.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 234 reports

- [SDR 2025F00273](https://openairdocs.org/sdr/2025F00273.md): Support · corroded · Nov 26, 2025 · N86VS · Cessna 414 · Vertical Stabilizer Miscellaneous Structure
  > DURING A PREFLIGHT WALKAROUND, SURFACE CORROSION WAS OBSERVED ON THE VERTICAL STABILIZER AFT SECTION. AFTER CLOSER INSPECTION SEVERE DELAMINATION WAS SEEN ON THE AFT VERTICAL SUPPORT ANGLES AND AFT STAB BULKHEAD SECTION. THE RUDDER TRIM TAB BRACKET ALSO HAD SI
- [SDR KISA202602050001](https://openairdocs.org/sdr/KISA202602050001.md): Angle · corroded · Nov 25, 2025 · N86VS · Cessna 414 · Vertical Stabilizer Miscellaneous Structure
  > DURING A PREFLIGHT WALK AROUND CORROSION WAS OBSERVED ON THE AFT SPAR ANGLE CHANNEL OF THE VERTICAL STABILIZER. UPON FURTHER INVESTIGATION SIGNIFICANT INTERGRANULAR CORROSION WAS FOUND RESULTING IN EXFOLIATION OF THE SURFACE OT THE SPAR ANGLE. THIS RESULTED IN
- [SDR 2021FA0000079](https://openairdocs.org/sdr/2021FA0000079.md): Oxygen System · leaking · Mar 9, 2021 · Cessna 414 · Oxygen System
  > AIRCRAFT OWNER REPORTED HISSING SOUND ABOVE CABIN HEADLINER WHEN CABIN OXYGEN CONTROL WAS TURNED ON. PRESSURIZED OXYGEN SYSTEM AND CONFIRMED LOUD HISSING SOUND COMING FROM HEADLINER BETWEEN FIRST ROW OF PASSENGER SEATS. USED BORESCOPE TO INSPECT THE AREA, AND
- [SDR 2018FA0000375](https://openairdocs.org/sdr/2018FA0000375.md): Trim Tab · cracked · Sep 15, 2018 · N414AC · Cessna 414 · Elevator, Tab Structure
  > DURING ANNUAL/100 INSPECTION, SURFACE CORROSION WAS OBSERVED NEAR AND ON THE ATTACHMENT SCREWS FOR THE ELEVATOR TRIM TAB HORN (P/N: 0831000-50). CORROSION WAS CLEANED. CRACKS WERE OBSERVED IN THE AFT TWO SCREW HOLES ON THE TOP SURFACE OF THE ELEVATOR TRIM TAB.
- [SDR 2018FA0000340](https://openairdocs.org/sdr/2018FA0000340.md): Fork · broken · Jun 23, 2018 · N3758C · Cessna 414 · Nose/Tail Landing Gear
  > NOSE GEAR WOULD NOT LOCK IN DOWN POSITION UPON LANDING.
- [SDR 2RM2017F00001](https://openairdocs.org/sdr/2RM2017F00001.md): Lifter · spalled · Oct 17, 2017 · N414AW · Cessna 414 · Reciprocating Engine Power Section
  > ENGINE WAS DISASSEMBLED FOR PROP STRIKE INSPECTION. FOUND LIFTERS BEGINNING TO SPALL AND WERE REPLACED WITH NEW LIFTERS AT THIS TIME TO PREVENT DAMAGE TO CAMSHAFT. LIFTERS WERE INSTALLED IN MAY OF 2010 AND HAVE 303.7 HOURS SINCE NEW.
- [SDR 2RM2017F00000](https://openairdocs.org/sdr/2RM2017F00000.md): Lifter · spalled · Oct 17, 2017 · N414AW · Cessna 414 · Reciprocating Engine Power Section
  > ENGINE WAS DISASSEMBLED FOR PROP STRIKE INSPECTION. FOUND LIFTERS BEGINNING TO SPALL AND WERE REPLACED WITH NEW LIFTERS AT THIS TIME TO PREVENT DAMAGE TO CAMSHAFT. LIFTERS WERE INSTALLED IN MAY OF 2010 AND HAVE 303.7 HOURS SINCE NEW.
- [SDR 2017FA0000379](https://openairdocs.org/sdr/2017FA0000379.md): Beam · corroded · Mar 17, 2017 · N620CA · Cessna 414 · Engine Mount Section
  > WHILE REMOVING THE TURBO CHARGER, NOTICED SEVERAL RIVET HEADS MISSING ON THE DOUBLER FOR THE TALL PIPE SUPPORT CLAMP. ON FURTHER INVESTIGATION, IT WAS DISCOVERED THAT THE DOUBLER WAS PUSHED UP FROM CORROSION. THE TALL PIPE SUPPORT WAS REMOVED AND THE ENGIN
- [SDR 2016FA0000239](https://openairdocs.org/sdr/2016FA0000239.md): Bellcrank · broken · May 13, 2016 · Cessna 414 · Landing Gear Retraction/Extension System
  > ON LANDING ROLLOUT, THE LT MAIN GEAR COLLAPSED. 1 OF THE LOWER EARS OF THE LT LANDING GEAR RETRACTION BELLCRANK WAS SHEARED AND NOT FOUND. THE BELLCRANK CAME OFF THE DOWNLOCK PIN. ALSO THE UPPER ATTACH BOLT SHEARED AND 1 OF THE ATTACHMENT EARS OF THE UPPER
- [SDR 4MCA2015F00094](https://openairdocs.org/sdr/4MCA2015F00094.md): Magneto · malfunctioned · Aug 4, 2015 · N999RK · Cessna 414 · Magneto/Distributor
  > ATC KEPT ACFT AT 3000 FT FOR APPROXIMATELY 15 MINUTES. DURING THIS TIME, KEPT FULL POWER AND MIXTURE FULL RICH, WAS EXPECTING A CLIMB TO FILED ALTITUDE. AFTER ABOUT 15 MINUTES, SET POWER TO CRUISE SETTING AND LEANED MIXTURE. A FEW MINUTES LATER, WAS TOLD T
- [SDR 7IL2015F00008](https://openairdocs.org/sdr/7IL2015F00008.md): Bulkhead · cracked · Jan 16, 2015 · N490KM · Cessna 414 · Propeller Spinner Section
  > WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND SPINNER REAR BULKHEAD CRACKED. BULKHEAD SN DY-1863.
- [SDR 7IL2015F00007](https://openairdocs.org/sdr/7IL2015F00007.md): Bracket · cracked · Jan 16, 2015 · N490KM · Cessna 414 · Landing Gear Doors
  > WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND RT REAR INNER GEAR DOOR ATTACH BRACKETS CRACKED AT INBD BOLT HOLE. BRACKET WAS STILL SECURED BY REMAINING MOUNT TABS. SIMILAR BRACKETS ARE USED ON FWD SIDE OF GEAR DOOR AS WELL AS LT GEAR DOOR, NO DAMAGE FOUN
- [SDR 7IL2015F00006](https://openairdocs.org/sdr/7IL2015F00006.md): Bracket · cracked · Jan 16, 2015 · N490KM · Cessna 414 · Landing Gear Doors
  > WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND RT REAR INNER GEAR DOOR ATTACH BRACKETS CRACKED AT INBD BOLT HOLE. BRACKET WAS STILL SECURED BY REMAINING MOUNT TABS. SIMILAR BRACKETS ARE USED ON FWD SIDE OF GEAR DOOR AS WELL AS LT GEAR DOOR, NO DAMAGE FOUN
- [SDR 7IL2015F00005](https://openairdocs.org/sdr/7IL2015F00005.md): Cylinder Head · cracked · Jan 16, 2015 · N490KM · Cessna 414 · Reciprocating Engine Cylinder Section
  > WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS: NR 3 LOCATION, SN60652-27, NR 5 LOCATION, SN 60652-25, NR 4 LOCATION, SN 606652-23. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED
- [SDR 7IL2015F00004](https://openairdocs.org/sdr/7IL2015F00004.md): Cylinder Head · cracked · Jan 16, 2015 · N490KM · Cessna 414 · Reciprocating Engine Cylinder Section
  > WHILE PERFORMING 100 HR INSPECTION OF AIRCRAFT, FOUND CRACKS IN CYLINDERS: NR 3 LOCATION, SN60652-27, NR 5 LOCATION, SN 60652-25, NR 4 LOCATION, SN 606652-23. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUN
- [SDR 7IL2015F00003](https://openairdocs.org/sdr/7IL2015F00003.md): Cylinder Head · cracked · Jan 16, 2015 · N490KM · Cessna 414 · Reciprocating Engine Cylinder Section
  > WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS: NR 3 LOCATION, SN60652-27, NR 5 LOCATION, SN 60652-25, NR 4 LOCATION, SN 606652-23. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED
- [SDR 7IL2015F00002](https://openairdocs.org/sdr/7IL2015F00002.md): Cylinder Head · cracked · Jan 16, 2015 · N490KM · Cessna 414 · Reciprocating Engine Cylinder Section
  > WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS NR 3 LOCATION, SN64015-16, NR 5 LOCATION, SN64016-17, NR 6 LOCATION, SN 63936-02. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED OTB
- [SDR 7ILA2015F00001](https://openairdocs.org/sdr/7ILA2015F00001.md): Cylinder Head · cracked · Jan 16, 2015 · N490KM · Cessna 414 · Reciprocating Engine Cylinder Section
  > WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS NR 3 LOCATION, SN 64015-16, NR 5 LOCATION, SN 64016-17, NR 6 LOCATION, SN 63936-02. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED O
- [SDR 7ILA2015F00000](https://openairdocs.org/sdr/7ILA2015F00000.md): Cylinder Head · cracked · Jan 16, 2015 · N490KM · Cessna 414 · Reciprocating Engine Cylinder Section
  > WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS NR 3 LOCATION, SN64015-16, NR 5 LOCATION, SN64016-17, NR 6 LOCATION, SN 63936-02. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED OTB
- [SDR 2014FA0000541](https://openairdocs.org/sdr/2014FA0000541.md): Cylinder · burst · Aug 10, 2014 · N698D · Cessna 414 · Propeller Assembly
  > PROPELLER CYLINDER C3550 BURST FROM OIL PRESSURE, PROBABLE FROM GOVERNOR. GOVERNOR MUST BE TESTED BEFORE PROPELLER REINSTALLED. PROPELLER HUB SERIAL 700239. REJECTED DUE TO FORCE PUT ON SCREW HOLES.
- [SDR 2014FA0000156](https://openairdocs.org/sdr/2014FA0000156.md): Landing Gear · collapsed · Mar 13, 2014 · N606PP · Cessna 414 · Main Landing Gear
  > LEFT MLG COLLAPSED ON LANDING ROLLOUT.
- [SDR 2013FA0000741](https://openairdocs.org/sdr/2013FA0000741.md): Pivot Assy · failed · Dec 5, 2013 · N2694H · Cessna 414 · Flight Compartment Equipment
  > PIVOT ARM SUPPORTING THE PILOT SEAT BACK FAILED DURING TAXI, ALLOWING SEAT BACK TO PARTIALLY RECLINE. SPECIFIC INSPECTION FOR CRACKS AND CORROSION ON THE SEAT PIVOT ARMS RECOMMENDED. THERE WAS EVIDENCE OF CRACK/CORROSION THAT MAY HAVE CAUSED THE FAILURE.
- [SDR CA130826006](https://openairdocs.org/sdr/CA130826006.md): Bellcrank · sheared · Aug 22, 2013 · Cessna 414 · Landing Gear Door Retract Section
  > (CAN) AFTER FLIGHT, IT WAS NOTED THAT THE RT INBD MLG DOOR WAS HANGING OPEN. NO NOISE WAS HEARD IN FLIGHT DURING EXTENSION AND RETRACTION AND THE LANDING GEAR SYS FUNCTIONED NORMALLY. IT WAS FOUND THAT THE IDLER BELLCRANK THAT CONTROLS THE DOOR MOVEMENT HAD
- [SDR CA130410019](https://openairdocs.org/sdr/CA130410019.md): Tach Generator · failed · Apr 9, 2013 · Cessna 414 · Engine RPM Indicating System
  > (CAN) DURING TAKEOFF, NON FLYING PILOT NOTED THE CO-PILOTS ENGINE RPM, TACH, INDICATOR LT NEEDLE DROPPING FROM TAKEOFF RPM TO ZERO WITH NO CHANGE IN ENGINE PERFORMANCE. PRIMARY FLIGHT DISPLAY TACHOMETER INDICATION REMAINED UNCHANGED. INSPECTION DETERMINED THA
- [SDR 2013FA0000469](https://openairdocs.org/sdr/2013FA0000469.md): Trunnion · cracked · Apr 5, 2013 · N37480 · Cessna 414 · Fuselage, Landing Gear Attach Fittings
  > NLG LT TRUNNION LUG FAILED UPON LANDING.
- [SDR CA121112006](https://openairdocs.org/sdr/CA121112006.md): Cylinder · cracked · Nov 7, 2012 · Cessna 414 · Reciprocating Engine Cylinder Section
  > (CAN) DURING TROUBLESHOOTING, DIFFERENTIAL COMPRESSION TEST AND CYLINDER LEAKAGE TEST. FOUND CYLINDER LEAKING AIR FROM AREA OF COOLING FINS ON THE EXHAUST PORT. VISUAL INSPECTION FOUND INTERNAL CRACK EXHAUST PORT OF CYLINDER WITH EXHAUST REMOVED.
- [SDR CA121112005](https://openairdocs.org/sdr/CA121112005.md): Cylinder · cracked · Nov 7, 2012 · Cessna 414 · Reciprocating Engine Cylinder Section
  > (CAN) DURING TROUBLESHOOTING, DIFFERENTIAL COMPRESSION TEST AND CYLINDER LEAKAGE TEST, FOUND CYLINDER LEAKING AIR FROM AREA OF COOLING FINS ON THE EXHAUST PORT. BOROSCOPE INSPECTION FOUND INTERNAL CRACK IN THE HEAD OF THE CYLINDER.
- [SDR CA121112004](https://openairdocs.org/sdr/CA121112004.md): Antenna · intermittent · Oct 24, 2012 · Cessna 414 · Global Positioning System
  > (CAN) DURING FLIGHT PILOT HAD LOSS OF ALL GPS NAVIGATION TO THE GARMIN 430W, GARMIN 530W AND THE GARMIN G600 SYS. SYSTEM REVERTED TO DEAD, RECONNING MODE. TROUBLESHOOTING DETERMINED THE GARMIN GA-35 WAAS GPS ANTENNA FOR THE GARMIN 430W FAILED CAUSING AN OSCI
- [SDR J7B2012F00000](https://openairdocs.org/sdr/J7B2012F00000.md): Bearing · worn · Mar 1, 2012 · N4243C · Cessna 414 · Exhaust Turbocharger
  > SHORTLY AFTER DEPARTURE, A MINOR FLUCTUATION OF MANIFOLD PRESSURE WAS OBSERVED ON THE RT ENGINE. THE ACFT RETURNED TO DEPARTURE WITHOUT INCIDENT. UPON INSPECTION IT WAS DISCOVERED THAT THE RT ENGINE TURBOCHARGER CENTER BEARING HAD EXCESSIVE WEAR CAUSING THE
- [SDR CA111026007](https://openairdocs.org/sdr/CA111026007.md): Skin · cracked · Oct 23, 2011 · Cessna 414 · Horizontal Stabilizer, Plate/Skin
  > (CAN) NUMEROURS SKIN CRACKS FOUND IN UPPER SKIN ON LT ELEVATOR AND LT HORIZONTAL STABILIZER.
- [SDR 2011FA0000684](https://openairdocs.org/sdr/2011FA0000684.md): Skin · cracked · Oct 14, 2011 · N414EL · Cessna 414 · Wing, Plate/Skin
  > AFTER FINDING SIMILAR ACFT WITH SIMILAR ISSUES, PERFORMED A VISUAL INSP OF BOTH RT AND LT UPPER INBD RT WING SKIN AND LT WING SKIN FROM WHEEL WELL AREA AND NOTED CRACKS IN SKIN, (APPROX 2-3 INCHES IN LENGTH), IN AREA OF RIB THAT ATTACHES UPPER MLG SIDE BRACE S
- [SDR CA110429001](https://openairdocs.org/sdr/CA110429001.md): Connecting Rod · broken · Dec 8, 2010 · Cessna 414 · Reciprocating Engine Power Section
  > (CAN) TWO CONNECTING RODS BROKEN. SCRAP CRANKCASE BROKEN. SCRAP CAMSHAFT BROKEN - SCRAP OIL SUMP, SCRAP PISTON BROKEN.
- [SDR CA101112006](https://openairdocs.org/sdr/CA101112006.md): Turbine · stuck · Nov 12, 2010 · Cessna 414 · Exhaust Turbocharger
  > (CAN) ON TAKEOFF, THE NR 2 ENGINE WOULD NOT DEVELOP FULL POWER. THE TURBOCHARGER HOT SIDE TURBINE WAS RUBBING ON THE TURBO HOUSING, PREVENTING IT SPINNING. THE TURBO WAS REPLACED.
- [SDR CA091116007](https://openairdocs.org/sdr/CA091116007.md): Skin · cracked · Nov 13, 2009 · Cessna 414 · Wing, Plate/Skin
  > (CAN) DURING AN INSP, THE UPPER WING SKIN WAS FOUND CRACKED. THE CRACK WAS LOCATED AT THE AFT ATTACHMENT POINT OF THE MAIN FUEL TIP TANK. THE CRACK WAS 3/4 OF AN INCH IN LENGTH JUST FWD OF THE AFT WING SPAR. 2 RIVETS THAT GO THROUGH THE OTBD AILERON ATTACH BRA
- [SDR J7B2009F00000](https://openairdocs.org/sdr/J7B2009F00000.md): Cylinder Head · separated · May 20, 2009 · N4243C · Cessna 414 · Reciprocating Engine Cylinder Section
  > WHILE IN FLIGHT, AT CRUISE POWER, A LOSS OF MANIFOLD PRESSURE AND ENGINE ROUGHNESS WAS EXPERIENCED. THE ENGINE WAS SHUTDOWN. A NORMAL LANDING WAS MADE AT THE INTENDED DESTINATION. INSP REVEALED THAT NR 2 CYLINDER HEAD HAD SEPARATED. NO STRUCTURAL DAMAGE OC
- [SDR CA090403002](https://openairdocs.org/sdr/CA090403002.md): Connecting Rod · worn · Mar 17, 2009 · Cessna 414 · Reciprocating Engine Power Section
  > (CAN) PISTON PIN BUSHING FAILED DUE TO LACK OF LUBRICATION. ENG DISMANTLED AND FAILURE DETERMINED TO BE CASUED BY SEALANT BLOCKING THE PISTON COOLING JET TO NR 2 CYLINDER. THE PROBLEM SEEMED TO BE CAUSED BY THE USE OF EXCESSIVE SEALANT (POSSIBLY LOCKTITE 515)
- [SDR 2009FA0000014](https://openairdocs.org/sdr/2009FA0000014.md): Arm · broken · Dec 10, 2008 · N52CS · Cessna 414 · Landing Gear Position and Warning
  > ON LANDING, THE PILOT SELECTED THE GEAR DOWN AND NEVER GOT A GREEN DOWN AND LOCK LIGHT IN THE CABIN FOR THE RT MAIN GEAR. THE GEAR DOWNLOCK MICRO-SWITCH ACTUATOR ARM WAS BROKEN AND WOULD NOT ACTUATE THE MICRO-SWITCH. THESE ACTUATOR ARMS SEEM TO GET WEAK OVER
- [SDR A6WA200840624](https://openairdocs.org/sdr/A6WA200840624.md): Support · cracked · Dec 1, 2008 · N414AW · Cessna 414 · Fuselage Main, Attach Fittings
  > AFT COMPARTMENT RT HYDRAULIC SUPPORT AT FS 718 FOUND CRACKED IN AFT LOWER CORNER. AFT COMPARTMENT RT HYDRAULIC SUPPORT AT FS 718 ON AFT LOWER CORNER REPAIRED IAW CRJ200 REO 601R-53-62-031 REV A.
- [SDR CA080410009](https://openairdocs.org/sdr/CA080410009.md): Cylinder Head · cracked · Mar 12, 2008 · Cessna 414 · Reciprocating Engine Cylinder Section
  > PILOT FLYING IN CRUISE FLIGHT, WHEN HE HEARD A POP AND EXPERIENCED LOSS OF ENGINE POWER. FEATHERED PROPELLER AND LANDED AT NEAREST AIRPORT. ENGINE CYLINDER REPLACED.
- [SDR CA071004006](https://openairdocs.org/sdr/CA071004006.md): Cable · broken · Oct 1, 2007 · Cessna 414 · Mixture Control
  > (CAN) DURING THE ENGINE RUN-UP, THE RT ENGINE DID NOT RESPOND TO MIXTURE CONTROL. THE MIXTURE CONTROL CABLE WAS FOUND BROKEN UNDER THE ENGINE CONTROL PEDISTAL. THE BRAKE WAS INSIDE THE CONTROL CABLE HOUSING AND COULD NOT BE SEEN WITH ANY INSPECTION. (TC NR 200
- [SDR 2007FA0000749](https://openairdocs.org/sdr/2007FA0000749.md): Exhaust Pipe · cracked · Aug 29, 2007 · N22MG · Cessna 414 · Engine Collector/Tailpipe/Nozzle
  > DURING COMPLIANCE WITH AD 2000-01-16 THE TAIL PIPE ON THE RT ENGINE WAS FOUND WITH A 6 INCH CRACK. THE LAST INSPECTION WAS 40 HRS PRIOR.
- [SDR 2007FA0000396](https://openairdocs.org/sdr/2007FA0000396.md): Switch · stuck · Apr 30, 2007 · N42SG · Cessna 414 · Navigation System
  > AVIONICS MASTER SWITCH STUCK IN THE ON POSITION AD 2005-20-25 WAS PREVIOUSL COMPLIED WITH AND DID NOT APPLY. DATE CODE OF THE SWITCH WAS 7647. THERE WAS NO BURNING SMELL WHEN THE SWITCH BECAME STUCK. (K)
- [SDR 155SW112206](https://openairdocs.org/sdr/155SW112206.md): Exhaust Stack · cracked · Nov 22, 2006 · N155SW · Cessna 414 · Engine Collector/Tailpipe/Nozzle
  > APPROXIMATELY 5 MINUTES AFTER TAKEOFF FROM ST MARY'S COUNTY, MD (2W6) EN ROUTE TO CLARKSBURG, WV (KCKB), THE PILOT NOTICED AN UNUSUAL SOUND COMING FROM THE LEFT ENGINE. THE PILOT THEN NOTICED THE LEFT MANIFOLD PRESSURE BEGIN TO DROP TO APPROXIMATELY 28 INCHES
- [SDR CA061123006](https://openairdocs.org/sdr/CA061123006.md): Cap · cracked · Nov 20, 2006 · Cessna 414 · Nacelle/Pylon Miscellaneous Structure
  > (CAN) CRACK NOTED AT LT NACELLE CANTED BULKHEAD CAP. CAP REPAIRED. (TC NR 20061123006)
- [SDR 155SW111506](https://openairdocs.org/sdr/155SW111506.md): Pump · leaking · Nov 15, 2006 · N155SW · Cessna 414 · Vacuum Distribution System
  > APPROXIMATELY 40 MINUTES INTO A FLIGHT FROM CLARKSBURG, WV (KCKB) TO ST. MARY'S COUNTY, MD (2W6), OIL WAS OBSERVED ON THE RIGHT ENGINE NACELLE STARTING AT THE VENT ON TOP OF THE NACELLE AND EXTENDING BACK TO THE TRAILING EDGE. AS A PRECAUTIONARY MEASURE, THE
- [SDR 2006FA0000622](https://openairdocs.org/sdr/2006FA0000622.md): Skin · cracked · Jun 22, 2006 · N414JS · Cessna 414 · Wing, Plate/Skin
  > DURING AN ANNUAL INSPECTION, A CRACK WAS FOUND ON THE RT WING SKIN AT THE OB AILERON ATTACH POINT, WHICH IS ALSO THE MAIN FUEL TANK AFT ATTACH POINT. UPON FURTHER INSPECTION OF AREA, THE RIVETS THAT ATTACH THE AILERON SUPPORT TO THE REAR SPAR WERE FOUND SHEARE
- [SDR 2006FA0000621](https://openairdocs.org/sdr/2006FA0000621.md): Skin · cracked · Jun 22, 2006 · N414JS · Cessna 414 · Wing, Plate/Skin
  > DURING AN ANNUAL INSPECTION, A CRACK WAS FOUND ON THE RT WING SKIN AT THE OB AILERON ATTACH POINT, WHICH IS ALSO THE MAIN FUEL TANK AFT ATTACH POINT. UPON FURTHER INSPECTION OF AREA, THE RIVETS THAT ATTACH THE AILERON SUPPORT TO THE REAR SPAR WERE FOUND SHEARE
- [SDR 2006FA0000498](https://openairdocs.org/sdr/2006FA0000498.md): Cylinder · cracked · May 11, 2006 · N710US · Cessna 414 · Reciprocating Engine Cylinder Section
  > DURING DECENT TO AIRPORT, PILOT REPORTED RT ENGINE STARTED HAVING EXCESSIVE VIBRATION. NO OTHER MAJOR ENGINE INDICATIONS WERE NOTED. AFTER LANDING, A MAGNETO CHECK WAS CONDUCTED AND NO DESCREPANCIES WERE FOUND. UPON REMOVAL OF COWLING, RT ENGINE NR 6 CYLIND
- [SDR 2006FA0000493](https://openairdocs.org/sdr/2006FA0000493.md): Fitting · cracked · May 4, 2006 · N352TS · Cessna 414 · Wing, Attach Fittings
  > DURING ANNUAL INSP FOUND LT STUB WING AFT SPAR, UPPER FITTING CRACKED AT OB BOLT HOLE. FOUND NO CORROSION OR STRESS IN SURROUNDING AREAS. SUSPECT BOLT WAS OVERTORQUED. (K)
- [SDR 2006FA0000202](https://openairdocs.org/sdr/2006FA0000202.md): Turbocharger · disintegrated · Feb 21, 2006 · N4243C · Cessna 414 · Exhaust Turbocharger
  > TURBOCHARGER CAME APART INTERNALLY RESULTING IN LOSS OF MANIFOLD PRESSURE AND ENGINE METAL CONTAMINATION. ENGINE REMOVED FROM SERVICE. (K)

Next page: https://openairdocs.org/model/cessna-414/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 = '414'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-414/reports

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