# N5421M: 1970 Cessna 402B, registration cancelled 2015-04-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 2, 2015 - Status when cancelled: Registration expired - Airframe: [Cessna 402B](https://openairdocs.org/model/cessna-402b) (registry code 207590P) - Engine: [Continental IO-520 series](https://openairdocs.org/engine/continental-io-520-series) (registry code 17032) - Data sheets: [TCDS A7CE](https://openairdocs.org/tcds/A7CE), [TCDS E5CE](https://openairdocs.org/tcds/E5CE) (OpenAirDocs) - Serial number: 402B0021 - Year built: 1970 - Type of aircraft: Fixed wing multi engine - Engine type: Reciprocating - Airworthiness: Standard, normal - Airworthiness date: May 28, 1970 - Certificate issued: July 24, 2001 - Last registry action: March 29, 2012 - Mode S code: A6E1E1 - Owner when cancelled: [Gta Air Inc](https://openairdocs.org/faa-owner/GTA%20AIR%20INC) - Location: [Addison, TX](https://openairdocs.org/faa-place/TX/Addison) - Owner type: Corporation - Owner's area on the map: 32.9600° N, 96.8372° W: Placed by OpenAirDocs at the center of ZIP code 75001, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N5421M - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=5421M - Page: https://openairdocs.org/deregistered/N5421M-2015-04-02 From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Cessna 402B: https://openairdocs.org/model/cessna-402b.md ## Service difficulty reports (17) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR XGN2008F00008](https://openairdocs.org/sdr/XGN2008F00008), Jul 23, 2008: CYLINDER. CRACKED. CRACKED BETWEEN FIN NR 1 AND FIN NR 3 AFT OF THE INJECTOR. MFG REV 3 E SERIES CYLINDER. ALL DEFECTIVE. (K) - [SDR XGN2008F00007](https://openairdocs.org/sdr/XGN2008F00007), Jul 23, 2008: CYLINDER. CRACKED. CRACKED BETWEEN FIN NR 1 AND FIN NR 3 AFT OF THE INJECTOR. MFG REV E SERIES CYLINDER. ALL DEFECTIVE. - [SDR XGN2008F00006](https://openairdocs.org/sdr/XGN2008F00006), Jul 23, 2008: CYLINDER. CRACKED. CRACKED BETWEEN FIN NR 1 AND FIN NR 3 AFT OF THE INJECTOR. ECI REV 3 E SERIES CYLINDER. ALL DEFECTIVE. (K) - [SDR 2008FA0000260](https://openairdocs.org/sdr/2008FA0000260), Feb 27, 2008: CYLINDER. CRACKED. CRACKED BETWEEN FIN NR1-3, BEHIND INJECTOR. DEFECTIVE PRODUCT. (K) - [SDR XGN2008F00005](https://openairdocs.org/sdr/XGN2008F00005), Feb 27, 2008: CYLINDER. CRACKED. CYLINDER CRACKED BETWEEN NR 1-3 FIN BEHIND INJECTOR, DEFECTIVE PRODUCT. (K) - [SDR XGN2008F00004](https://openairdocs.org/sdr/XGN2008F00004), Feb 27, 2008: CYLINDER. CRACKED. CYLINDER CRACKED BEHIND NR 1-3 FIN BY FUEL INJECTOR, DEFECTIVE PRODUCT. (K) - [SDR XGN2008F00003](https://openairdocs.org/sdr/XGN2008F00003), Feb 27, 2008: CYLINDER. CRACKED. CYLINDER CRACKED BETWEEN FIN NR1-3 BEHIND INJECTOR, DEFECTIVE PRODUCT. (K) - [SDR XGN2005F00006](https://openairdocs.org/sdr/XGN2005F00006), Jun 14, 2005: CYLINDER. CRACKED. THIS CYLINDER WAS IN THE NR 6 POSITION AND IS A TYPE (X) HEAD. THIS CRACKED VYLINDER HEAD WAS FOUND AT THE 100 HOUR INSPECTION. WE ARE FINDING SIGNS OF AIR LEAK - [SDR XGN2006F00035](https://openairdocs.org/sdr/XGN2006F00035), Jun 4, 2005: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR XGN2006F00057](https://openairdocs.org/sdr/XGN2006F00057), Apr 24, 2005: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR XGN2006F00036](https://openairdocs.org/sdr/XGN2006F00036), Apr 18, 2005: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR XGN2006F00056](https://openairdocs.org/sdr/XGN2006F00056), Apr 5, 2005: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR XGN2006F00034](https://openairdocs.org/sdr/XGN2006F00034), Apr 5, 2005: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR XGN2006F00033](https://openairdocs.org/sdr/XGN2006F00033), Mar 5, 2005: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR XGN2006F00032](https://openairdocs.org/sdr/XGN2006F00032), Mar 2, 2005: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR XGN2006F00031](https://openairdocs.org/sdr/XGN2006F00031), Nov 1, 2004: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR 2008F00023](https://openairdocs.org/sdr/2008F00023), Oct 7, 2004: PUSHROD. FAILED. ENGINE HAD MANIFOLD AND FUEL PRESSURE VARIATION IN FLT, THE ACFT BEGAN TO VIBRATE AND THE PILOT SHUTDOWN ENGINE. THE NR 1 AND NR 2 ROD`S FAILED AND SEPARATED FR ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19990407015309I](https://openairdocs.org/incident/19990407015309I), Apr 7, 1999: Cessna 402B (N5421M), Dallas, TX, Minor damage. Pilot and check airman were completing check ride iaw FAR 135.293. Pilot turned off 13L and was taxiing back to base and reached for flap handle and pulled… --- 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.