# Service difficulty reports: N6813J A list on [N6813J](https://openairdocs.org/aircraft/N6813J.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR HYIA20260818001](https://openairdocs.org/sdr/HYIA20260818001.md): Switch · faulty · Aug 16, 2026 · N6813J · Cessna 402C · Landing Gear Retraction/Extension System > PILOT REPORTED THE LANDING GEAR EXTENDED BY ITSELF WITH GEAR HANDLE IN UP POSITION. MAINTENANCE INSPECTED LANDING GEAR SELECTOR SWITCH, NO DEFECTS FOUND. THE SWITCH WAS REPLACED AS A PRECAUTION, WITH NO FURTHER DEFECTS NOTED. - [SDR HYIA20221215001](https://openairdocs.org/sdr/HYIA20221215001.md): Circuit Breaker · failed · Dec 8, 2022 · N6813J · Cessna 402C · Light System Wiring > PILOT REPORTED SMOKE OBSERVED FROM SIDE PANEL. MAINTENANCE INSPECTED ANTI-COLLISION CIRCUIT BREAKER SWITCH AND WIRING, FOUND SWITCH INOP AND WIRE INSULATION BURNT ON LOAD SIDE OF SWITCH. REPAIRED DAMAGED ANTI-COLLISION LIGHT SWITCH WIRE IAW 402C WDM CHAPTER 20 - [SDR HYIA20190128001](https://openairdocs.org/sdr/HYIA20190128001.md): Rib · cracked · Jan 25, 2019 · N6813J · Cessna 402C · Wing, Rib/Bulkhead > DURING MAINTENANCE A CRACK WAS DISCOVERED ON THE LEFT HAND CLOSEOUT RIB LOCATED AT LEFT WING STATION 106.79. THIS CRACK STARTS AT A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT TRUNION SUPPORT AND EXTENDS FORWARD APPROXIMATELY.900 IN. THIS RIB WILL - [SDR HYIA2017010500001](https://openairdocs.org/sdr/HYIA2017010500001.md): Engine · shutdown · Jan 2, 2018 · N6813J · Cessna 402C · Engine (Turbine/Turboprop) > PILOT REPORTED THE RIGHT ENGINE SHUTDOWN IN FLIGHT. OPEN - [SDR HYIA20171117001](https://openairdocs.org/sdr/HYIA20171117001.md): Torque Tube · failed · Nov 16, 2017 · N6813J · Cessna 402C · Rudder Control System > WHILE IN CRUISE, THE RT RUDDER PEDAL WENT TO THE FLOOR, FULL FORWARD. THE PILOT DID NOT HAVE ANY RUDDER AUTHORITY, BUT THE AIRCRAFT REMAINED IN STRAIGHT AND LEVEL FLIGHT. DIVERTED AND LANDED SAFELY WITH NO ISSUES. THE AIRCRAFT WAS UNABLE TO TAXI FROM THE RU - [SDR HYIA20170705001](https://openairdocs.org/sdr/HYIA20170705001.md): Fitting · cracked · Jul 5, 2017 · N6813J · Cessna 402C · Nacelle/Pylon, Attach Fittings > WHILE PREPPING THE LOWER NACELLE SKIN FOR SID 57-10-16 NDT INSPECTION, TWO CRACKS WERE IDENTIFIED IN THE LT OUTBOARD NACELLE FITTING. - [SDR HYIA20170503001](https://openairdocs.org/sdr/HYIA20170503001.md): Cylinder · broken · Apr 28, 2017 · N6813J · Cessna 402C · Reciprocating Engine Cylinder Section > PILOT REPORTED SHUDDERING AND VIBRATION FROM LEFT ENGINE. UPON INSPECTION MAINTENANCE FOUND THE CYLINDER ROTOCOIL BROKEN. CYLINDER WAS REPLACED, ADDITIONAL DETAILS TO BE CONVEYED UPON TEARDOWN ANALYSIS. - [SDR HYIA20140414025](https://openairdocs.org/sdr/HYIA20140414025.md): Drag Brace · cracked · Oct 19, 2012 · N6813J · Cessna 402C · Landing Gear Retraction/Extension System > AT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A - [SDR HYIA20140414007](https://openairdocs.org/sdr/HYIA20140414007.md): Drag Brace · cracked · Aug 11, 2011 · N6813J · Cessna 402C · Landing Gear Retraction/Extension System > AT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A - [SDR HYIA20140415065](https://openairdocs.org/sdr/HYIA20140415065.md): Drag Brace · cracked · Jul 8, 2011 · N6813J · Cessna 402C · Landing Gear Retraction/Extension System > AT SCHEDULED INSPECTION, NLG DRAG BRACE, PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAW - [SDR HYIA20140415052](https://openairdocs.org/sdr/HYIA20140415052.md): Drag Brace · cracked · Apr 18, 2011 · N6813J · Cessna 402C · Landing Gear Retraction/Extension System > AT SCHEDULED INSPECTION, NLG DRAG BRACE, OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE - [SDR HYIA6813J1024](https://openairdocs.org/sdr/HYIA6813J1024.md): Resistor · burned · Oct 24, 2010 · N6813J · Cessna 402C · Air Conditioning System Wiring > CREW REPORTED, IN CRUISE, STRONG ELECTRIAL SMELL IN COCKPIT. CREW DIVERTED. MX INSPECTED ACFT, R & R OVERHEATED CABIN HEATER FAN HIGH - LOW RESISTOR. SYS CHECKS OK. ACFT RELEASED BACK TO SERVICE. - [SDR 1356813112207](https://openairdocs.org/sdr/1356813112207.md): Fitting · leaking · Nov 22, 2007 · N6813J · Cessna 402C · Heating System > PILOT NOTICED FUEL SMELL IN COCKPIT DURING HEATER START UP AND SHUT DOWN, WHEN BRINGING AIRCRAFT TO FLEET CENTER AT END OF NIGHT. MAINTENANCE FOUND PUMP OUTLET FITTING LEAKING. MAINTENANCE TIGHTENED FUEL PUMP OUTLET FITTING AND AS A PRECAUTIONARY MEASURE REM - [SDR 135N6813JLENG](https://openairdocs.org/sdr/135N6813JLENG.md): Connecting Rod · destroyed · Aug 22, 2006 · N6813J · Cessna 402C · Reciprocating Engine Power Section > PILOT REPORTED RPM/POWER LOSS, SHUT ENGINE AS A PRECAUTIONARY MEASURE, RETURNED TO DEPARTURE AIRPORT. - [SDR 1350606N6813J](https://openairdocs.org/sdr/1350606N6813J.md): Circuit Breaker · defective · Aug 17, 2006 · N6813J · Cessna 402C · Electrical Power System > AVIONICS CIRCUIT BREAKER FAILED IN THE ON POSITION. - [SDR 13500527N6813](https://openairdocs.org/sdr/13500527N6813.md): Circuit Board · defective · Aug 6, 2006 · N6813J · Cessna 402C · Electrical Power System > CREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH. - [SDR HYI2003F00020](https://openairdocs.org/sdr/HYI2003F00020.md): Liner · damaged · Nov 11, 2003 · N6813J · Cessna 402C · Landing Gear Brake System > AFTER LANDING, ON ROLLOUT, AIRCRAFT STARTED VEERING TO THE LEFT. CREW WAS UNABLE TO STRAIGHTEN OR TURN RIGHT EVEN WITH DIFFERENTIAL POWER OR RT RUDDER. AIRCRAFT WAS SHUTDOWN ON RUNWAY. TOWED TO HANGER. MECHANIC UNABLE TO DUPLICATE CONDITION, REMOVED AND RE - [SDR HYI2001F00002](https://openairdocs.org/sdr/HYI2001F00002.md): Master Switch · inoperative · Oct 8, 2001 · N6813J · Cessna 402C · DC Power Distribution System > CREW REPORTED AVIONICS MASTER SWITCH INOPERATIVE ON PREFLIGHT. MAINTENANCE REMOVED AND REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE. (PTRS-2001B5540) ## 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 n_number = 'N6813J' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N6813J/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.