# Service difficulty reports: N3292M A list on [N3292M](https://openairdocs.org/aircraft/N3292M.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR HYIA20231219001](https://openairdocs.org/sdr/HYIA20231219001.md): Spar Cap · corroded · Dec 19, 2023 · N3292M · Cessna 402C · Wing Spar > DURING MAINTENANCE AN AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE RH AFT LOWER OUTBOARD SPAR CAP, OEM P/N: 5122041-24. THIS CORROSION IS LOCATED ON THE FORWARD FACE OF THE VERTICAL LEG AT APPROXIMATE RWS 229.71. THIS CORROSION MEASURES APPROXIMATELY.020 - [SDR HYIA20200512001](https://openairdocs.org/sdr/HYIA20200512001.md): Ignition Unit · burned out · May 8, 2020 · N3292M · Cessna 402C · Heating System > PILOT REPORTED A NOXIOUS SMELL DURING FLIGHT, AND NOTED THE HEATER DID NOT FEEL LIKE IT WAS PERFORMING. MAINTENANCE INSPECTED AND FOUND THE HEATER IGNITION UNIT TO BE BURNT OUT. REPLACED THE UNIT WITH NO FURTHER DEFECTS NOTED. - [SDR HYIA20191014001](https://openairdocs.org/sdr/HYIA20191014001.md): Fitting · corroded · Oct 11, 2019 · N3292M · Cessna 402C · Wing, Attach Fittings > WHILE PERFORMING SPECIAL INSPECTION 402-22 IAW INSPECTION PROGRAM MANUAL, AND MM 5-20-01, CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT WING'S, FORWARD SPAR'S, UPPER, AFT, WING FITTING (P/N 082255-45). THIS CORROSION IS ON THE UPPER HORIZONTAL FLANGE OF THE FI - [SDR HYIA2018101515001](https://openairdocs.org/sdr/HYIA2018101515001.md): Connector · damaged · Oct 11, 2018 · N3292M · Cessna 402C · Auto Flight System Wiring > PILOT REPORTED SMOKE IN COCKPIT AND THE AUTOPILOT SYSTEM CIRCUIT BREAKER POPPED. MX PERFORMED INITIAL INSPECTION AND FOUND THE AUTOPILOT INTERFACE CONNECTOR DAMAGED. THE SYSTEM WAS PLACED ON MEL, FURTHER DETAILS WILL BE PROVIDED IF ADDITIONAL FAILED PARTS ARE - [SDR HYIA20160818075](https://openairdocs.org/sdr/HYIA20160818075.md): Exhaust Valve · damaged · Aug 15, 2016 · N3292M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160818074](https://openairdocs.org/sdr/HYIA20160818074.md): Exhaust Valve · damaged · Aug 15, 2016 · N3292M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160803037](https://openairdocs.org/sdr/HYIA20160803037.md): Exhaust Valve · damaged · Jul 7, 2016 · N3292M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160803036](https://openairdocs.org/sdr/HYIA20160803036.md): Exhaust Valve · damaged · Jul 7, 2016 · N3292M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160803035](https://openairdocs.org/sdr/HYIA20160803035.md): Exhaust Valve · damaged · Jul 7, 2016 · N3292M · Cessna 402C · Reciprocating Engine Cylinder Section > CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20151124003](https://openairdocs.org/sdr/HYIA20151124003.md): Flap · out of rig · Nov 21, 2015 · N3292M · Cessna 402C · Trailing Edge Flap Control System > PILOT REPORTED ACFT ROLLS TO THE RT WHEN FLAPS ARE 15 DEGREES EXTENDED. INSPECTED & FOUND AN ASYMMETRICAL CONDITION WITH FLAPS. RIGGED FLAPS IAW MM CHAPTER 27. - [SDR HYIA11072015001](https://openairdocs.org/sdr/HYIA11072015001.md): Beam · cracked · Nov 5, 2015 · N3292M · Cessna 402C · Nacelle/Pylon, Main Frame > DURING SCHEDULED INSPECTION THE LT NACELLE CROSSOVER BEAM ASSEMBLY WAS FOUND TO BE CRACKED AT OTBD LOWER U CHANNEL. REMOVAL OF CROSSOVER BEAM ASSEMBLY, DETAILED VISUAL INSPECTION OF SURROUNDING STRUCTURE FOR ADDITIONAL DEFECTS & INSTALLATION OF NEW BEAM ASSEM - [SDR HYIA20150413001](https://openairdocs.org/sdr/HYIA20150413001.md): Unknown · odor · Apr 10, 2015 · N3292M · Cessna 402C · Air Distribution System > PILOT REPORTED FUEL ODOR IN CABIN. INSPECTED BOTH WINGS, FUEL TANKS, STRAINERS, FUEL LINES, NOSE COMPARTMENT & FUSELAGE. NO DEFECTS FOUND. - [SDR HYIA201419003](https://openairdocs.org/sdr/HYIA201419003.md): Unknown · odor · Dec 18, 2014 · N3292M · Cessna 402C · Air Distribution System > HEAVY FUEL SMELL IN CABIN. INSPECTED THE CABIN, BOTH WINGS & NOSE BAGGAGE COMPARTMENT FOR ANY EVIDENCE OF FUEL LEAK. NO DEFECTS NOTED. - [SDR HYIA20130124002](https://openairdocs.org/sdr/HYIA20130124002.md): Spar · damaged · Jan 24, 2013 · N3292M · Cessna 402C · Fuselage Main, Structure > DURING A REGULARLY SCHEDULED MX EVENT, DAMAGE WAS DISCOVERED ON THE REAR SPAR WEBS IN BOTH FORWARD AND AFT POSITIONS. DAMAGE WAS MAPPED AND SENT. REPAIRS WERE CARRIED OUT IAW REPAIR PLANS SUPPLIED AND SUBSTANTIATED. - [SDR HYIA20140414014](https://openairdocs.org/sdr/HYIA20140414014.md): Drag Brace · cracked · Jul 10, 2012 · N3292M · 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 HYIA20140415058](https://openairdocs.org/sdr/HYIA20140415058.md): Drag Brace · cracked · May 16, 2011 · N3292M · 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 HYIAN3292M](https://openairdocs.org/sdr/HYIAN3292M.md): Separator · frozen · Jan 10, 2009 · N3292M · Cessna 402C · Engine Oil Indicating System > AIRCRAFT OVERNIGHTED IN TEMPS WELL BELOW ZERO, WITHOUT PROPER PREHEAT. AFTER TAKEOFF, BREATHER SYSTEM BLOCKED UP FROM FREEZING MOISTURE. AT APPROXIMATELY 1000 AGL, THE LEFT ENGINE OIL PRESSURE BEGAN TO RISE ABOVE THE GREEN ARC. AS CREW BEGAN TO SHUT DOWN EN - [SDR HYIA3292M](https://openairdocs.org/sdr/HYIA3292M.md): Beam · cracked · Dec 22, 2008 · N3292M · Cessna 402C · Nacelle/Pylon, Main Frame > RIGHT ENGINE'S INBOARD ENGINE BEAM IS CRACKED AT THE AFT UPPER WEB 0NE HALF OF AN INCH. REMOVAL AND REPLACEMENT OF THE ENGINE BEAM. - [SDR GNB2005F00005](https://openairdocs.org/sdr/GNB2005F00005.md): Control Cable · worn · Jun 28, 2005 · N3292M · Cessna 402C · Aileron Control System > WEAR FROM BLENDING DUE TO SOFTER MATERIAL USED IN NEW STYLE CABLE. - [SDR GNB2005F00002](https://openairdocs.org/sdr/GNB2005F00002.md): Cable · frayed · Apr 3, 2005 · N3292M · Cessna 402C · Landing Gear Steering System > DURING INSPECTION, FOUND RT NOSE STEERING CABLE BLENDED AND FRAYED AT PULLEY. NEW MFG CABLES (STANLESS STEEL) LAST ONLY FRACTION OF TIME AS OLD STYLE CABLES. HAS BECOME MUCH MORE COMMON OCCURRANCE. (K) - [SDR 99ZZZX538](https://openairdocs.org/sdr/99ZZZX538.md): Slinger · missing · Jan 6, 1999 · N3292M · Cessna 402C · Magneto/Distributor > DURING PHASE INSPECTION, DIQSCOVERED L.E. LEFT MAGNETO HAD OIL INTERNALLY. DISSAMBLED MAGNETO IAW OM. FOUND OIL SLINGER WAS NOT INSTALLED. ## 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 = 'N3292M' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N3292M/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.