N231RL

Valid Registration

1974 BELL 206B

N231RL is a 1974 BELL 206B registered to NOR WES INC in CRESTON, IA. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 13 Airworthiness Directives may apply.

Registration Details

N-Number
N231RL
Serial Number
1324
Manufacturer
BELL
Model
206B
Year
1974
Registration Status
Valid
Airworthiness Date
1974-03-28
Owner
NOR WES INC
Owner City
CRESTON
Owner State
IA

The BELL 206B is registered with the FAA under N-number N231RL. This airframe was manufactured in 1974. Its manufacturer serial number is 1324. The aircraft was issued its airworthiness certificate on 1974-03-28. The current registered owner is NOR WES INC, based in CRESTON, IA. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

Fatal injuries2023-07-30

Denison, IA, USA

Accident — BELL 206B (NTSB CEN23LA342)

No injuries reported1995-12-18

INGLESIDE, TX, USA

Accident — Beech 200 (NTSB FTW96LA074)

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

N231RL 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. N231RL 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 N231RL

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

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