N3211N

Valid Registration

1984 BELL 206B

N3211N is a 1984 BELL 206B registered to TUMBLEWEED LEASING CO INC in SALT LAKE CITY, UT. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 13 Airworthiness Directives may apply.

Registration Details

N-Number
N3211N
Serial Number
3808
Manufacturer
BELL
Model
206B
Year
1984
Registration Status
Valid
Airworthiness Date
1984-10-11
Owner
TUMBLEWEED LEASING CO INC
Owner City
SALT LAKE CITY
Owner State
UT

The BELL 206B is registered with the FAA under N-number N3211N. This airframe was manufactured in 1984. Its manufacturer serial number is 3808. The aircraft was issued its airworthiness certificate on 1984-10-11. The current registered owner is TUMBLEWEED LEASING CO INC, based in SALT LAKE CITY, UT. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2014-02-05

Bountiful, UT, USA

Accident — BELL 206 (NTSB WPR14LA113)

No injuries reported1993-03-16

DALLAS, TX, USA

Accident — BELL 206B (NTSB FTW93TA#03)

Severity reflects injuries to people involved, not damage to the aircraft. A “no injuries” accident can still involve significant aircraft damage.

N3211N has been involved in 2 NTSB accidents since 1982. Each record above includes the date, location, severity, and NTSB summary. Buyers should review the full accident narratives and verify repairs in the aircraft's logbooks before purchase.

Applicable Airworthiness Directives

13 found
AD 2011-4465Effective: 2011-03-10

Airworthiness Directives; Bell Helicopter Textron Canada Limited (BHTC) Model 206A, 206B, 206L, 206L-1, 206L-3, 206L-4, 222, 222B, 222U, 230, 407, 427, and 430 Helicopters

This document publishes in the Federal Register an amendment adopting Emergency Airworthiness Directive (AD) 2010-26-51, which was sent previously to all known U.S. owners and operators of the specified model helicopters by individual letters. This AD also supersedes existing AD 2009-08-03. This AD is prompted by another incident in which the tail rotor blade (blade) tip weight separated from a blade during flight causing vibration. This unsafe condition led to the determination that additional blades could be affected and should be added to the applicability. The actions specified by this AD are intended to prevent loss of the blade tip weight, loss of a blade, and subsequent loss of control of the helicopter.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N3211N may be affected by 13 directives. All applicable ADs must be complied with for the aircraft to remain legally airworthy. Buyers should verify AD compliance in the aircraft's logbooks before purchase.

+12 more Airworthiness Directives found for this aircraft

Full list, with effective dates and links to the official Federal Register documents, is included in the paid report.

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Get the complete history for N3211N

Full accident narratives, all Airworthiness Directives, ownership chain, and a downloadable PDF.

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