# Service difficulty reports: N2615G A list on [N2615G](https://openairdocs.org/aircraft/N2615G.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR HYIA20231031002](https://openairdocs.org/sdr/HYIA20231031002.md): Gps · failed · Oct 27, 2023 · N2615G · Cessna 402C · Global Positioning System > PILOT REPORTED THE GARMIN 430 STOPPED WORKING, SCREEN WENT BLANK AND NOTED ELECTRICAL BURNING SMELL. MAINTENANCE REPLACED THE GPS 430W UNIT IN ACCORDANCE WITH GARMIN 430W INSTALLATION MANUAL WITH NO FURTHER DEFECTS NOTED. - [SDR HYIA20170512001](https://openairdocs.org/sdr/HYIA20170512001.md): Pump · leaking · May 9, 2017 · N2615G · Cessna 402C · Heating System > PILOT REPORTED FUEL SMELL IN CABIN WITH HEATER RUNNING. UPON INSPECTION, MAINTENANCE DETERMINED TO BE FROM LEAKING HEATER FUEL PUMP THAT WAS DRAINING FROM HEATER VENT LINE. REPLACED FUEL PUMP WITH NO FURTHER DEFECTS NOTED. - [SDR HYIA20161209001](https://openairdocs.org/sdr/HYIA20161209001.md): Gasket · leaking · Dec 8, 2016 · N2615G · Cessna 402C · Heating System > PILOT REPORTED FUEL ODOR IN CABIN WITH HEATER TURNED ON. MAINTENANCE REPLACED THE HEATER FUEL FILTER BOWL GASKET. FURTHER DETAILS ABOUT THE CONDITION OF THE GASKET WILL BE ADDED ONCE THE MECHANIC WHO REPLACED THE GASKET IS BACK TO WORK. - [SDR HYIA20160912132](https://openairdocs.org/sdr/HYIA20160912132.md): Exhaust Valve · damaged · Sep 8, 2016 · N2615G · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160912131](https://openairdocs.org/sdr/HYIA20160912131.md): Exhaust Valve · damaged · Sep 8, 2016 · N2615G · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160812070](https://openairdocs.org/sdr/HYIA20160812070.md): Exhaust Valve · damaged · Aug 8, 2016 · N2615G · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160812069](https://openairdocs.org/sdr/HYIA20160812069.md): Exhaust Valve · damaged · Aug 8, 2016 · N2615G · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160812068](https://openairdocs.org/sdr/HYIA20160812068.md): Exhaust Valve · damaged · Aug 8, 2016 · N2615G · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160803034](https://openairdocs.org/sdr/HYIA20160803034.md): Exhaust Valve · damaged · Jul 7, 2016 · N2615G · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20150914001](https://openairdocs.org/sdr/HYIA20150914001.md): Axle · broken · Sep 11, 2015 · N2615G · Cessna 402C · Main Landing Gear Strut/Axle/Truck > ON TAXI OUT, PILOT REPORTED THE RT MAIN WHEEL BROKEN. PERFORMED VISUAL INSPECTION ON RT MLG & FOUND THE RT MLG AXLE BROKEN & MAIN TIRE WITH DAMAGE. R & R THE RT MLG LOWER BARREL IAW MM CHAPTER 32-10-00. OPERATIONS CHECKED GOOD. R & R RT MLG WHEEL ASSEMBLY - [SDR HYIA20140422111](https://openairdocs.org/sdr/HYIA20140422111.md): Fuel Line · cracked · Apr 20, 2014 · N2615G · Cessna 402C · Aircraft Fuel Distribution System > PILOT REPORTED FUEL SMELL IN COCKPIT. FOUND A FUEL LINE FROM THE RT ENG FIREWALL TO THE RT FUEL BOWL LEAKING. THE LINE WAS REPLACED, OPERATIONAL & LEAK CHECK WERE PERFORMED WITH NO DEFECTS NOTED. - [SDR HYIA20140421110](https://openairdocs.org/sdr/HYIA20140421110.md): Drain Line · loose · Apr 18, 2014 · N2615G · Cessna 402C · Aircraft Fuel Distribution System > A PAX REPORTED A FUEL SMELL IN THE CABIN AFTER TAKEOFF. TIGHTENED THE DRAIN LINE ON THE RT FUEL AUXILIARY PUMP & PERFORMED A PRESS TEST, NO DEFECTS NOTED. - [SDR HYIA03142014001](https://openairdocs.org/sdr/HYIA03142014001.md): Spar Cap · corroded · Mar 12, 2014 · N2615G · Cessna 402C · Wing Spar > DURING ROUTINE SCHEDULED INSPECTION, AREAS OF CORROSION WERE FOUND AT LT & RT LWR WING SPAR CAP STRAPS PREVIOUSLY INSTALLED VIA CESSNA SK402-47 ON 04/16/2003 TO SATISFY REQUIREMENT OF CESSNA MEB02-5 & AD2005-12-13. THE CORRECTIVE ACTION TO REMEDIATE CONDITION - [SDR HYIA20140415078](https://openairdocs.org/sdr/HYIA20140415078.md): Drag Brace · cracked · Aug 16, 2012 · N2615G · 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 HYIA20140415039](https://openairdocs.org/sdr/HYIA20140415039.md): Drag Brace · cracked · Mar 25, 2011 · N2615G · 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 HYIA20090122001](https://openairdocs.org/sdr/HYIA20090122001.md): Selector Valve · sticking · Jan 22, 2009 · N2615G · Cessna 402C · Fuel Selector/Shut-Off Valve > LEFT AND RIGHT ENGINES AND LOST POWER, LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND IT WAS FOUND THE LEFT FUEL SELECTOR VALVE WAS STICKING SELECTOR WAS LUBED AND EXERCISED OPERATIONAL CHECK GOOD. AIRCRAFT WAS RELEASED. - [SDR N2615G](https://openairdocs.org/sdr/N2615G.md): Line · fractured · Oct 1, 2007 · N2615G · Cessna 402C · Heating System > DURING TAXI, PILOT TURNED ON CABIN HEATER. WHEN NO HEAT APPEARED PRESENT, PILOT TURNED OFF HEATER. AT THIS POINT A SMALL FIRE IGNITED IN THE HEATER BAY. PILOT SECURED THE AIRCRAFT AND EXITED THE AIRCRAFT. THE FIRE WAS EXTINGUISHED WITH MINIMAL DAMAGE TO TH - [SDR HYI2006F00003](https://openairdocs.org/sdr/HYI2006F00003.md): Uplock Switch · failed · Dec 2, 2005 · N2615G · Cessna 402C · Landing Gear Retraction/Extension System > CREW REPORTED LT MAIN GEAR DID NOT FULLY RETRACT WITH HEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE LT UPLOCK MICROSWITCH, GEAR SWING CHECKS, OK. AIRCRAFT RELEASED FOR SERVICE. (K) - [SDR HYI2006F00002](https://openairdocs.org/sdr/HYI2006F00002.md): Uplock Switch · failed · Dec 2, 2005 · N2615G · Cessna 402C · Landing Gear Position and Warning > CREW REPORTED GEAR UNSAFE LIGHT REMAINTED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE LT UPLOCK MICROSWITCH, GEAR SWING CHECKS, OK. AIRCRAFT RELEASED FOR SERVICE. (K) - [SDR HYI2006F00001](https://openairdocs.org/sdr/HYI2006F00001.md): Uplock Switch · failed · Dec 2, 2005 · N2615G · Cessna 402C · Landing Gear Position and Warning > CREW REPORTED GEAR UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE ATTEMPTED TO REMOVE AND REPLACE THE LT HAND UP LOCK MICROSWITCH, 3 SWITCHES FAILED (BAD FROM STOCK) BEFORE INSTALLING A SERVICABLE UNIT, GEAR SWING CHECKS, OK. AIRCRAFT R - [SDR HYI2006F00000](https://openairdocs.org/sdr/HYI2006F00000.md): Uplock Switch · failed · Dec 2, 2005 · N2615G · Cessna 402C · Landing Gear Retraction/Extension System > CREW REPORTED GEAR UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE LT UP LOCK MICROSWITCH, GEAR SWING CHECKS, OK. AIRCRAFT RELEASED FOR SERVICE. (K) - [SDR HYI2005F00000](https://openairdocs.org/sdr/HYI2005F00000.md): Circuit Breaker · failed · Aug 23, 2004 · N2615G · Cessna 402C · Light System Wiring > ON SHORT FINAL, CREW REPORTED SMELL OF SMOKE, TO REDUCE LOAD ALL LIGHTS WERE TURNED OFF, SMELL DISSIPATED. MECHANIC FOUND ANTI COLLISION WIRING DAMAGED NEAR C/B PANEL AND CIRCUIT BREAKER FAILED. REPAIRED WIRING, REPLACED BREAKER AND RETURNED AIRCRAFT TO SERV - [SDR 2004F00274](https://openairdocs.org/sdr/2004F00274.md): Wire · failed · Aug 23, 2004 · N2615G · Cessna 402C · Light System Wiring > ON SHORT FINAL, CREW REPORTED ODOR OF SMOKE, TO REDUCE LOAD ALL LIGHTS WERE TURNED OFF. ODOR DISSIPATED. MAINTENANCE FOUND ANTI COLLISION WIRING DAMAGED NEAR C/B PANEL ON CIRCUIT BREAKER FAILED. REPAIRED WIRING REPLACED BREAKER AND RETURNED AIRCRAFT TO SERVICE ## 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 = 'N2615G' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N2615G/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.