# N3211K: not currently registered

- Registered now: No (not in the FAA registry file). The mark may be reserved or free to assign
- Earlier aircraft: 2
- Last cancelled: April 17, 2012
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=3211K
- Page: https://openairdocs.org/aircraft/N3211K

## Aircraft that carried N3211K

- [Cancelled 2012-04-17](https://openairdocs.org/deregistered/N3211K-2012-04-17): Bell 206L-3, S/N 51126, built 1985. Exported to Indonesia. Owner: [Air Center Helicopters Inc](https://openairdocs.org/faa-owner/AIR%20CENTER%20HELICOPTERS%20INC), [Ft Worth, TX](https://openairdocs.org/faa-place/TX/Ft%20Worth)
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N3211K-undated): Globe GC-1B, S/N 1204, built 1946. Owner: [Glove Aircraft Corp](https://openairdocs.org/faa-owner/GLOVE%20AIRCRAFT%20CORP), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth)

## NTSB investigations on N3211K (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 FTW94LA071](https://openairdocs.org/ntsb/FTW94LA071), Jan 20, 1994: Bell 206L-3 (N3211K), Cascade, CO, substantial damage. Probable cause: THE PILOT'S IMPROPER IN-FLIGHT PLANNING WHICH RESULTED IN THE AIRCRAFT'S YAW PERFORMANCE BEING EXCEEDED. A FACTOR WAS THE HIGH DENSITY ALTITUDE.

## FAA accident and incident reports on N3211K (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 19940120000639A](https://openairdocs.org/incident/19940120000639A), Jan 20, 1994: Bell 206L3 (N3211K), Cascade, CO, Substantial damage. Made slow pass over pikes peak. Lost tail rotor effectiveness. Spun into peak. Rolled over. Photo flight.

---
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.