# N402BF: 1976 Cessna 402B, registration cancelled 2009-08-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 24, 2009 - Status when cancelled: Triennial form not returned - 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: 402B-1076 - Year built: 1976 - Type of aircraft: Fixed wing multi engine - Engine type: Reciprocating - Airworthiness: Standard, normal - Airworthiness date: June 28, 1976 - Certificate issued: October 6, 2005 - Last registry action: October 21, 2008 - Mode S code: A4B42E - Owner when cancelled: [D+A Investments LLC](https://openairdocs.org/faa-owner/D+A%20INVESTMENTS%20LLC) - Location: [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque) - Owner type: Corporation - Owner's area on the map: 35.1378° N, 106.6425° W: Placed by OpenAirDocs at the center of ZIP code 87107, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N402BF - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=402BF - Page: https://openairdocs.org/deregistered/N402BF-2009-08-24 From the FAA registry file of October 29, 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 (10) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR N3B2007F00002](https://openairdocs.org/sdr/N3B2007F00002), Sep 10, 2007: BELLCRANK. BROKEN. LT MAIN LANDING COLLAPSED ON LANDING. IT APPEARS THAT BELLCRANK ASSEMBLY, PN 50410015 FAILED DURING EXTENSION CYCLE. (K) - [SDR 20010514CW008](https://openairdocs.org/sdr/20010514CW008), Apr 18, 2001: EXHAUST PIPE. DAMAGED. WHILE ON FINAL APPROACH, THE PILOT REPORTED A LOSS OF MANIFOLD PRESSURE WITH THE RIGHT ENGINE. IT WAS FOUND THAT THERE WAS A HOLE APPROX 1.5 X 3.0 INCHES IN THE - [SDR 20000803SH006](https://openairdocs.org/sdr/20000803SH006), Jul 12, 2000: CONTROL CABLE. BROKEN. ASG/LIT - WHILE EN ROUTE AND ON APPROACH AT ABOUT 500 AGL, PILOT EXPERIENCED A FLAP SYSTEM FAILURE UPON DEPLOYMENT OF THE FLAPS, ONLY THE LT SIDE CAME DOWN. THI - [SDR 98ZZZX1994](https://openairdocs.org/sdr/98ZZZX1994), Apr 20, 1998: CRANKCASE STUD. BROKEN. DURING THE COURSE OF A 100-HOUR INSPECTION, THE MECHANIC NOTICED THE LEFT ENGINE, NR 1 CYLINDER, MOST FORWARD UPPER STUD HAD BROKEN OFF FLUSH WITH THE CYLINDER - [SDR 97ZZZX2612](https://openairdocs.org/sdr/97ZZZX2612), May 19, 1997: CYLINDER. LEAKS. DURING 50-HOUR INSPECTION, MECH TURNED PROP AND NOTICED A 'HISSING' SOUND EMITTING FROM NR 4 CYLINDER ON LT ENGINE. UPON CLOSER INSP, THE HISS WAS DETERMINED TO - [SDR 97ZZZX2108](https://openairdocs.org/sdr/97ZZZX2108), May 1, 1997: RIB. CRACKED. DURING A 100 HOUR INSPECTION, MECHANIC NOTICED CRACK IN THE WING SKIN IN MOST AFT OTBD SECTION OF LT WING. MECHANIC ALSO OBSERVED 2 RIVETS SHEARED THAT ATTACH T - [SDR 97ZZZX2107](https://openairdocs.org/sdr/97ZZZX2107), May 1, 1997: BRACKET. RIVET SHEARED. DURING A 100 HOUR INSPECTION, MECHANIC NOTICED CRACK IN THE WING SKIN IN MOST AFT OTBD SECTION OF LT WING. MECHANIC ALSO OBSERVED 2 RIVETS SHEARED THAT ATTACH T - [SDR 97ZZZX2106](https://openairdocs.org/sdr/97ZZZX2106), May 1, 1997: BRACKET. RIVET SHEARED. DURING A 100 HOUR INSPECTION, MECHANIC NOTICED CRACK IN THE WING SKIN IN MOST AFT OTBD SECTION OF LT WING. MECHANIC ALSO OBSERVED 2 RIVETS SHEARED THAT ATTACH T - [SDR 97ZZZX2105](https://openairdocs.org/sdr/97ZZZX2105), May 1, 1997: BRACKET. RIVET SHEARED. DURING A 100 HOUR INSPECTION, MECHANIC NOTICED CRACK IN THE WING SKIN IN MOST AFT OTBD SECTION OF LT WING. MECHANIC ALSO OBSERVED 2 RIVETS SHEARED THAT ATTACH T - [SDR 97ZZZX2104](https://openairdocs.org/sdr/97ZZZX2104), May 1, 1997: SKIN. CRACKED. DURING A 100 HOUR INSPECTION, MECHANIC NOTICED CRACK IN THE WING SKIN IN MOST AFT OTBD SECTION OF LT WING. MECHANIC ALSO OBSERVED 2 RIVETS SHEARED THAT ATTACH T ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DEN07LA156](https://openairdocs.org/ntsb/DEN07LA156), Sep 10, 2007: Cessna 402B (N402BF), Hobbs, NM, substantial damage. Probable cause: The failure of the left main landing gear down lock due to overload causing the main landing gear to collapse. ## 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. - [Accident 20070910019549A](https://openairdocs.org/incident/20070910019549A), Sep 10, 2007: Cessna 402B (N402BF), Hobbs, NM, Substantial damage. (-23) On September 10, 2007, at approximately 0938 MDT, N402BF, a Cessna model CE-402B, was on short final for runway 13 at Lea County Regional Airport (khob)… ## Other aircraft with N402BF - [Registered now](https://openairdocs.org/aircraft/N402BF): Cessna 402B, S/N 402B1010, built 1975 --- 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.