# Service difficulty reports: N26632, cancelled Nov 15, 2025 A list on [N26632, cancelled Nov 15, 2025](https://openairdocs.org/deregistered/N26632-2025-11-15.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR HYIA20201124002](https://openairdocs.org/sdr/HYIA20201124002.md): Axle · cracked · Nov 23, 2020 · N26632 · Cessna 402C · Main Landing Gear Strut/Axle/Truck > THE PILOT REPORTED THAT AFTER LANDING, THE AXLE BROKE WHILE EXITING THE RUNWAY. MAINTENANCE INSPECTED AND FOUND THE RIGHT AXLE TO BE CRACKED. REMOVED AND REPLACED THE RIGHT LOWER BARREL AND AXLE ASSEMBLY. NO FURTHER DEFECTS NOTED. - [SDR HYIA20190716001](https://openairdocs.org/sdr/HYIA20190716001.md): Fitting · cracked · Jul 16, 2019 · N26632 · Cessna 402C · Nacelle/Pylon Miscellaneous Structure > DURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE OUTBOARD LEG OF THE LEFT HAND OUTBOARD NACELLE FITTING (P/N 5292029-09.) THIS CRACK MEASURES APPROXIMATELY.149 IN LENGTH, AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN MEL-5 - [SDR HYIA20190307002](https://openairdocs.org/sdr/HYIA20190307002.md): Fitting · cracked · Mar 6, 2019 · N26632 · Cessna 402C · Nacelle/Pylon Miscellaneous Structure > DURING NDT INSPECTION AS NOTED IN SID 57-10-16 A CRACK WAS IDENTIFIED ON THE RIGHT HAND INBOARD NACELLE FITTING (P/N: 5292029-22). THIS CRACK LOCATED ON THE LOWER LEG OF THE OUTBOARD SIDE OF THE FITTING MEASURES APPROXIMATELY.083" LONG AND IS CONSISTENT TO OT - [SDR HYIA20170828016](https://openairdocs.org/sdr/HYIA20170828016.md): Fitting · cracked · May 25, 2017 · N26632 · Cessna 402C · Nacelle/Pylon, Attach Fittings > DURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED.123 IN LENGTH. - [SDR HYIA20151223001](https://openairdocs.org/sdr/HYIA20151223001.md): Unknown · odor · Dec 18, 2015 · N26632 · Cessna 402C · Air Distribution System > PILOT REPORTED BURNING SMELL ON DESCENT, NO SMOKE, BUT WAS UNABLE TO IDENTIFY THE SOURCE. INSPECTED WIRING ON INSTRUMENT PANEL, SIDE CONSOLE & CO-PILOT CONSOLE. NO EVIDENCE OF BURNING FOUND AT THIS TIME. - [SDR HYIA20151203005](https://openairdocs.org/sdr/HYIA20151203005.md): Master Cylinder · malfunctioned · Dec 2, 2015 · N26632 · Cessna 402C · Master Cylinder/Brake Valve > PILOT REPORTED RT BRAKE FAILURE WHILE MAKING RIGHT 180 ON RUNWAY. LT MAIN GEAR EXITED RUNWAY. INSPECTED THE ACFT, NO DAMAGE NOTED. RE-SEALED RT MASTER CYLINDER, SERVICED & BLED. TAXI CHECKED GOOD. - [SDR HYIA2015072020150](https://openairdocs.org/sdr/HYIA2015072020150.md): Master Cylinder · low · Jul 15, 2015 · N26632 · Cessna 402C · Master Cylinder/Brake Valve > PILOT REPORTED ON LANDING, RT BRAKE PEDAL WENT TO THE FLOOR & APPLIED NO BRAKE PRESS. INSPECTED RT BRAKE SYS WITH NO DEFECTS OR LEAKS NOTED. SERVICED RT BRAKE MASTER CYLINDER WITH HYD FLUID IAW MM CH 32-40-00. OPERATIONALLY CHECKED GOOD. - [SDR HYIA03272015004](https://openairdocs.org/sdr/HYIA03272015004.md): Beam · cracked · Mar 27, 2015 · N26632 · Cessna 402C · Nacelle/Pylon Miscellaneous Structure > THE LT NACELLE OTBD ENG BEAM WAS FOUND TO BE CRACKED JUST FWD OF AFT ENG MOUNT, TRANSVERSE TO LENGTH OF BEAM, ACROSS UPPER FACE OF BEAM, DURING NDT PRESCRIBED WITHIN MEL-54-01. REMOVE BEAM ASSEMBLY, PERFORM DETAILED VISUAL INSPECTION OF SURROUNDING STRUCTURE - [SDR HYIA20140414041](https://openairdocs.org/sdr/HYIA20140414041.md): Drag Brace · cracked · Dec 28, 2012 · N26632 · 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 HYIA20121008001](https://openairdocs.org/sdr/HYIA20121008001.md): Wire Harness · out of position · Oct 3, 2012 · N26632 · Cessna 402C · Electrical Power System Wiring > ON LANDING, PILOT NOTED SPARKS ON THE RT ENGINE COWL. SHUTDOWN RT ENGINE ON LANDING. WHEN INSPECTED, DISCREPANCY WAS CLEARED BY REROUTING POWER WIRE HARNESS AND INSOLATED IT IAW STANDARD PRACTICE. - [SDR HYIA20140414023](https://openairdocs.org/sdr/HYIA20140414023.md): Drag Brace · cracked · Sep 18, 2012 · N26632 · 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 HYIA20140415071](https://openairdocs.org/sdr/HYIA20140415071.md): Drag Brace · cracked · Aug 12, 2011 · N26632 · 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 HYIA26632LSTRT](https://openairdocs.org/sdr/HYIA26632LSTRT.md): Relay · overheated · Oct 28, 2009 · N26632 · Cessna 402C · Engine Cranking > AFTER TAXI IN, ON SHUTDOWN, LT ENG CONTINUED TO CRANK UNTIL MASTER SWITCH WAS SHUTOFF. MX REMOVED AND REPLACED STUCK START RELAY AND REPLACED ASSOCIATED WIRING AS A PRECAUTIONARY MEASURE. SYS CHECKED OK, ACFT RELEASED BACK TO SERVICE. - [SDR HYIA26632](https://openairdocs.org/sdr/HYIA26632.md): Brake Sys · failed · Dec 15, 2008 · N26632 · Cessna 402C · Landing Gear Brake System > LEFT BRAKE FAILED DURING TAXI. MAINTENANCE INSPECTED BLED AND SERVICED LEFT BRAKE SYSTEM. - [SDR 135632112407](https://openairdocs.org/sdr/135632112407.md): Engine · failed · Nov 24, 2007 · N26632 · Cessna 402C · Engine (Reciprocating) > ON TAKEOFF FROM MAZ, AT 2400 FEET AND CLIMBING TO 3500 FEET, PILOT HEARD LOUD BOOM WITH RIGHT ENGINE SHUT DOWN AND PROPELLER FEATHERING. THE PILOT PERFORMED ENGINE FAILURE FLOW CHECK LIST AND RETURNED TO MAZ. PRELIMINARY INSPECTION SHOWS CATASTROPHIC FAILURE - [SDR 1350527N26632](https://openairdocs.org/sdr/1350527N26632.md): Circuit Breaker · defective · Jul 13, 2006 · N26632 · Cessna 402C · Electrical Power System > CREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH. - [SDR HYI2003F00003](https://openairdocs.org/sdr/HYI2003F00003.md): Clutch · failed · Mar 5, 2003 · N26632 · Cessna 402C · Engine Starter > CREW REPORTED LEFT ENGINE FAILED TO START. MECHANIC REMOVED AND REPLACED STARTER CLUTCH. ON INSPECTION OF REMOVED STARTER CLUTCH, MECHANIC FOUND DRIVE GEAR TOOTH SHEARED. RECOVERED SINGLE TOOTH FROM OIL PUMP. RETURNED AIRCRAFT TO SERVICE AFTER FURTHER INS ## 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 = 'N26632' AND deregistration_id = 'N26632-2025-11-15' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N26632-2025-11-15/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, except the copies of manufacturers’ service documents, which belong to their rights holders.