# Service difficulty reports: N763EA A list on [N763EA](https://openairdocs.org/aircraft/N763EA.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR HYIA20240607001](https://openairdocs.org/sdr/HYIA20240607001.md): Fitting · cracked · Jun 5, 2024 · N763EA · Cessna 402C · Nacelle/Pylon, Attach Fittings > DURING SCHEDULED NONDESTRUCTIVE TESTING AS NOTED IN CESSNA SUPPLEMENTAL INSPECTION DOCUMENT (SID) 57-10-16, A CRACK WAS DISCOVERED ON THE LEFT HAND OUTBOARD NACELLE FITTING (OEM P/N: 5292029-31) THIS CRACK MEASURES APPROXIMATELY.104 INCHES LONG ON THE LOWER O - [SDR HYIA20210222001](https://openairdocs.org/sdr/HYIA20210222001.md): Fitting · cracked · Feb 22, 2021 · N763EA · Cessna 402C · Nacelle/Pylon, Attach Fittings > DURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE LEFT HAND INBOARD NACELLE FITTING. (P/N: 5292029-21) THIS CRACK MEASURES APPROXIMATELY.145 INCHES LONG ON THE INBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACKS F - [SDR HYIA20210202001](https://openairdocs.org/sdr/HYIA20210202001.md): Fitting · corroded · Feb 2, 2021 · N763EA · Cessna 402C · Fuselage, Wing Attach Fittings > DURING MAINTENANCE AN AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT HAND LOWER FUSELAGE ATTACH FITTING (P/N: 0811350-10) ON N763EA. THIS CORROSION MEASURES APPROXIMATELY.390 INCHES TALL,.429 WIDE, AND HAS A MAXIMUM DEPTH OF.056. IT IS LOCATED ON THE - [SDR HYIA20200911001](https://openairdocs.org/sdr/HYIA20200911001.md): Attach Fitting · cracked · Sep 10, 2020 · N763EA · Cessna 402C · Nacelle/Pylon, Attach Fittings > WHILE PERFORMING THE LIGHTED BOROSCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02R2 TO SATISFY AD2017-10-19, A CRACK WAS IDENTIFIED ON THE OUTBOARD RADIUS OF THE RIGHT HAND INBOARD NACELLE ATTACH FITTING (P/N: 5292029-22). THIS CRACK MEASURES APPRO - [SDR HYIA2019032700000](https://openairdocs.org/sdr/HYIA2019032700000.md): Spar Cap · corroded · Mar 27, 2019 · N763EA · Cessna 402C · Wing Spar > DURING MAINTENANCE CORROSION WAS DISCOVERED ON THE OUTBOARD LEFT LOWER SPAR CAP (P/N: 5122041-23) THIS CORROSION IS LOCATED ON THE BOTTOM OF THE HORIZONTAL LEG BETWEEN LWS 119.29 AND 106.79. THE DEEPEST MEASUREMENT MEASURES APPROXIMATELY.050 INCHES DEEP AT AP - [SDR HYIA20190107001](https://openairdocs.org/sdr/HYIA20190107001.md): Intake Valve · damaged · Jan 5, 2019 · N763EA · Cessna 402C · Reciprocating Engine Cylinder Section > PILOT REPORTED RIGHT ENGINE SHUDDERED, THEN STARTED RUNNING ROUGH IN FLIGHT. PRELIMINARY INSPECTION FOUND DAMAGE TO THE NR 1 INTAKE VALVE, DAMAGE TO THE NR 1 AND NR 5 PISTON HEADS AND THE NR 5 CYLINDER INTAKE LIFTER SLEEVE EXTRUDING FROM LIFTER TUBE IN CRANK C - [SDR HYIA20171113001](https://openairdocs.org/sdr/HYIA20171113001.md): Cylinder · damaged · Nov 8, 2017 · N763EA · Cessna 402C · Reciprocating Engine Cylinder Section > AT CRUISE POWER SETTING, CREW REPORTED A ROUGH RUNNING RT ENGINE ALONG WITH A CONTINUOUS MODERATE VIBRATION THROUGHOUT RANGE OF POWER SETTINGS. THE FLIGHT DIVERTED AND LANDED SAFELY. INSPECTION REVEALED THE NR 6 CYLINDER AND PISTON ASSEMBLY WERE SEVERELY DA - [SDR HYIA201205170004](https://openairdocs.org/sdr/HYIA201205170004.md): Spar · damaged · May 16, 2012 · N763EA · Cessna 402C · Fuselage Main, Frame > DURING A MX EVENT, DAMAGE WAS DISCOVERED ON THE AFT CARRY THROUGH SPAR STRUCTURE. DAMAGE INCLUDES FWD UPPER SPAR WEB FLANGE CRACKS AND MISSING MATERIAL AT SAME LOCATION. PREVIOUS EFFORTS IN REPAIRING THIS AREA HAVE RESULTED IN ADDITIONAL FASTENER LOCATIONS PE - [SDR HYIA20140415048](https://openairdocs.org/sdr/HYIA20140415048.md): Drag Brace · cracked · Apr 13, 2011 · N763EA · 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 HYIA763EAREV 1](https://openairdocs.org/sdr/HYIA763EAREV%201.md): Line · ruptured · Jun 28, 2009 · N763EA · Cessna 402C · Hydraulic System, Main > DURING INITIAL CLIMB OUT, HYD FLOW LIGHTS ILLUMINATED. LANDING GEAR CYCLED WITH NO EFFECT. EMERGENCY DECLARED, GEAR EXTENDED BY USE OF EMERGENCY EXTENSION SYS. MX REMOVED AND REPLACED HYD LINE IN RT STUB WING AREA. OPS CHECK AND LEAK CHECK PERFORMED. ACFT - [SDR HYIA20090628001](https://openairdocs.org/sdr/HYIA20090628001.md): Hydraulic Line · ruptured · Jun 28, 2009 · N763EA · Cessna 402C · Hydraulic System, Main > DURING INITIAL CLIMB OUT, HYDRAULIC FLOW LIGHTS ILLUMINATED. LANDING GEAR CYCLED WITH NO EFFECT. EMERGENCY DECLARED GEAR EXTENDED BY USE OF EMERGENCY EXTENSION SYSTEM MAINTENANCE REMOVED AND REPLACED HYDRAULIC LINE IN RIGHT STUB WING AREA. OPERATIONAL C - [SDR HYIA763EA](https://openairdocs.org/sdr/HYIA763EA.md): Bolt · unserviceable · Mar 20, 2009 · N763EA · Cessna 402C · Engine (Reciprocating) > CREW REPORTED RIGHT ALTERNATOR INOPERATIVE. MAINTENANCE REMOVED ALTERNATOR AND FOUND ALTERNATOR DRIVE GEAR ATTACH BOLTS SHEARED. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE. - [SDR 135763022008](https://openairdocs.org/sdr/135763022008.md): Turbocharger · failed · Feb 17, 2008 · N763EA · Cessna 402C · Exhaust Turbocharger > THE MANIFOLD PRESSURE DROPPED TO AMBIENT AND OIL PRESSURE DECREASED SHORTLY THERE AFTER. PILOT PERFORMED PRECAUTIONARY ENGINE SHUT DOWN. MAINTENANCE INSPECTED ENGINE AND FOUND BAD TURBOCHARGER AND REPLACED. MAINTENANCE PERFORMED PRECAUTIONARY OIL FILTER, AN - [SDR 1350532763EA](https://openairdocs.org/sdr/1350532763EA.md): Master Switch · inoperative · May 28, 2006 · N763EA · Cessna 402C · Navigation System > CREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH. - [SDR HYI2003F00021](https://openairdocs.org/sdr/HYI2003F00021.md): Torque Tube · failed · Nov 5, 2003 · N763EA · Cessna 402C · Rudder Control System > ON TAKE OFF ROLL, RIGHT RUDDER PEDAL FAILED. MECHANIC FOUND RUDDER PEDAL TORQUE TUBE FAILED AT POST WELD. REMOVED AND REPLACED TORQUE TUBE AND RETURNED AIRCRAFT TO SERVICE. - [SDR HYI2001F00008](https://openairdocs.org/sdr/HYI2001F00008.md): Drag Brace · cracked · Nov 6, 2001 · N763EA · Cessna 402C · Landing Gear Retraction/Extension System > REGULAR SCHEDULED INSPECTION, FOUND NOSE GEAR DRAG BRACE CRACKED AT ACTUATOR ATTACH LUG. MECHANIC REMOVED AND REPLACED NOSE GEAR DRAG BRACE.(K) - [SDR 96ZZZX5231](https://openairdocs.org/sdr/96ZZZX5231.md): Hook · failed · Aug 9, 1996 · N763EA · Cessna 402C · Landing Gear Retraction/Extension System > UPLOCK HOOK FAILED. UNABLE TO DETERMINE THE OLD PART NUMBER IN CESSNA PARTS BOOK. INSTALLED NEW STEEL HOOK, P/N 5141312-2. SUBMITTER STATED THIS HOOK (STEEL) IS THE WAY TO GO. THE STOCK PART DELIVERED (THIN ALUMINUM) AND THE ONE SUPPLIED BY SERVICE KITS (T ## 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 = 'N763EA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N763EA/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.