# N4165G: 1976 Cessna 402B, registration cancelled 2026-07-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 21, 2026 - Exported to: Bahamas - Status when cancelled: Valid registration - Airframe: [Cessna 402B](https://openairdocs.org/model/cessna-402b) (registry code 207590P) - Engine: [Continental TSIO-520 series](https://openairdocs.org/engine/continental-tsio-520-series) (registry code 17040) - Data sheets: [TCDS A7CE](https://openairdocs.org/tcds/A7CE), [TCDS E8CE](https://openairdocs.org/tcds/E8CE) (OpenAirDocs) - Serial number: 402B1212 - Year built: 1976 - Type of aircraft: Fixed wing multi engine - Engine type: Reciprocating - Airworthiness: Standard, normal - Airworthiness date: December 18, 1976 - Certificate issued: May 12, 2025 - Last registry action: October 3, 2025 - Mode S code: A4ED78 - Owner when cancelled: [Delaware Aircraft Trust LLC Trustee](https://openairdocs.org/faa-owner/DELAWARE%20AIRCRAFT%20TRUST%20LLC%20TRUSTEE) - Location: [New Castle, DE](https://openairdocs.org/faa-place/DE/New%20Castle) - Owner type: LLC - Owner's area on the map: 39.6466° N, 75.6048° W: Placed by OpenAirDocs at the center of ZIP code 19720, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N4165G - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=4165G - Page: https://openairdocs.org/deregistered/N4165G-2026-07-21 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 (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR XGNA2020F00000](https://openairdocs.org/sdr/XGNA2020F00000), Nov 4, 2019: CONTROLLER. INOPERATIVE. RIGHT ENGINE WILL NOT MAINTAIN CORRECT MANIFOLD PRESSURE. - [SDR XGN2011F00006](https://openairdocs.org/sdr/XGN2011F00006), Jan 18, 2011: CYLINDER HEAD. CRACKED. NR 2 CYLINDER CRACKED BETWEEN THE FINS AFT OF THE FUEL INJECTOR BY THE INTAKE VALVE AND WAS LEAKING FUEL. THIS CYLINDER, THECYLINDER HEAD WAS MFG WITH THE METAL - [SDR XGN2011F00005](https://openairdocs.org/sdr/XGN2011F00005), Jan 18, 2011: CYLINDER HEAD. CRACKED. NR 1 CYLINDER CRACKED BETWEEN THE FINS AFT OF THE FUEL INJECTOR BY THE INTAKE VALVE AND WAS LEAKING FUEL. THIS CYLINDER, THECYLINDER HEAD WAS MFG WITH THE METAL - [SDR XGN2011F00004](https://openairdocs.org/sdr/XGN2011F00004), Jan 18, 2011: CYLINDER HEAD. CRACKED. NR 4 CYLINDER CRACKED BETWEEN THE FINS AFT OF THE FUEL INJECTOR BY THE INTAKE VALVE AND WAS LEAKING FUEL. THIS CYLINDER, THECYLINDER HEAD WAS MFG WITH THE METAL - [SDR XGN2011F00003](https://openairdocs.org/sdr/XGN2011F00003), Jan 18, 2011: CYLINDER. CRACKED. NR 1 CYLINDER CRACKED BETWEEN THE FINS AFT OF THE FUEL INJECTOR BY THE INTAKE VALVE AND WAS LEAKING FUEL. THIS CYLINDER THAT THE CYLINDER HEAD WAS MFG WITH THE - [SDR XGNA2011F00002](https://openairdocs.org/sdr/XGNA2011F00002), Jan 18, 2011: CYLINDER. CRACKED. NR 2 CYLINDER CRACKED BETWEEN THE FINS AFT OF THE FUEL INJECTOR BY THE INTAKE VALVE AND WAS LEAKING FUEL. THIS CYLINDER THAT THE CYLINDER HEAD WAS MFG WITH THE - [SDR XGNA2011F00001](https://openairdocs.org/sdr/XGNA2011F00001), Jan 18, 2011: CYLINDER. CRACKED. NR 4 CYLINDER CACKED BETWEEN THE FINS AFT OF THE FUEL INJECTOR BY THE INTAKE VALVE AND WAS LEAKING FUEL. THIS CYLINDER THAT THE CYLINDER HEAD WAS MFG WITH THE M - [SDR XGN2008F00012](https://openairdocs.org/sdr/XGN2008F00012), Aug 1, 2008: CYLINDER. CRACKED. REV 3, E=SERIES CYLINDER, CRACKED. (K) - [SDR XGN2008F00010](https://openairdocs.org/sdr/XGN2008F00010), 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 2007FA0001027](https://openairdocs.org/sdr/2007FA0001027), Nov 8, 2007: CYLINDER HEAD. CRACKED. CRACKED CYL HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. (K) - [SDR 2007FA0001026](https://openairdocs.org/sdr/2007FA0001026), Nov 8, 2007: CYLINDER HEAD. CRACKED. CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECT IN MFG PROCESS. (K) - [SDR 2007FA0001025](https://openairdocs.org/sdr/2007FA0001025), Nov 8, 2007: CYLINDER HEAD. CRACKED. CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECT IN MFG PROCESS. (K) - [SDR 2007FA0001024](https://openairdocs.org/sdr/2007FA0001024), Nov 8, 2007: CYLINDER HEAD. CRACKED. CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR1, NR3. DEFECT IN MFG PROCESS. (K) - [SDR 2007FA0001028](https://openairdocs.org/sdr/2007FA0001028), Nov 7, 2007: CYLINDER HEAD. CRACKED. CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR1, NR3. DEFECT IN MFG PROCESS. (K) - [SDR XGN2007F00010](https://openairdocs.org/sdr/XGN2007F00010), Dec 26, 2006: CYLINDER. CRACKED. CRACKED CYLINDER HEAD. (K) - [SDR XGN2007F00000](https://openairdocs.org/sdr/XGN2007F00000), Dec 26, 2006: CYLINDER HEAD. CRACKED. CRACKED CYLINDER HEAD. (K) - [SDR XGN2006F00058](https://openairdocs.org/sdr/XGN2006F00058), Mar 3, 2006: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR XGN2006F00030](https://openairdocs.org/sdr/XGN2006F00030), Mar 3, 2006: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR XGN2005F00001](https://openairdocs.org/sdr/XGN2005F00001), May 4, 2005: CYLINDER HEAD. CRACKED. THIS CYLINDER WAS INSTALLED AS A SERVICEABLE CYLINDER 135.5 HOURS AGO. THE CRACK WAS FOUND DURING A 100 HR INSPECTION COMPRESSION CHECK. (K) - [SDR XGN2006F00028](https://openairdocs.org/sdr/XGN2006F00028), Apr 4, 2005: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR XGN2006F00029](https://openairdocs.org/sdr/XGN2006F00029), Feb 8, 2005: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR XGN2006F00027](https://openairdocs.org/sdr/XGN2006F00027), Dec 21, 2004: CYLINDER. CRACKED. CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K) - [SDR XGN2004F00002](https://openairdocs.org/sdr/XGN2004F00002), Jan 22, 2004: SAFETY SWITCH. INOPERATIVE. NOSE GEAR LIGHT WOULD NOT ILLUMINATE AND THE GEAR WARNING HORN WAS GOING OFF ON APPROACH. PILOT DID A FLY BY THE TOWER TO VERIFY NOSE GEAR DOWN. AIRCRAFT LANDED ## FAA accident and incident reports (3) 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 19910919045909I](https://openairdocs.org/incident/19910919045909I), Sep 19, 1991: Cessna 402B (N4165G), Charlotte, NC, Minor damage. Right gear collapsed on landing rollout. Had safe light. Left gear swiveled when mounting pin failed. - [Incident 19840814059189I](https://openairdocs.org/incident/19840814059189I), Aug 14, 1984: Cessna 402B (N4165G), Albany, NY. Left engine failed en route. Landed at nearest airport. Found broken ring and a hole in #3 piston. - [Incident 19810512034779I](https://openairdocs.org/incident/19810512034779I), May 12, 1981: Cessna 402CESSNA (N4165G), Hyannis, MA, No damage. Passengers shipped a wet cell battery as checked baggage. Acid spill in cargo compartment. Minor acid burn to pilot --- 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.