N205PA

Valid Registration

1976 BELL 206B

N205PA is a 1976 BELL 206B registered to RIDGELINE ENTERPRISES LLC in TWIN FALLS, ID. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 13 Airworthiness Directives may apply.

Registration Details

N-Number
N205PA
Serial Number
1996
Manufacturer
BELL
Model
206B
Year
1976
Registration Status
Valid
Airworthiness Date
1976-06-07
Owner
RIDGELINE ENTERPRISES LLC
Owner City
TWIN FALLS
Owner State
ID

The BELL 206B is registered with the FAA under N-number N205PA. This airframe was manufactured in 1976. Its manufacturer serial number is 1996. The aircraft was issued its airworthiness certificate on 1976-06-07. The current registered owner is RIDGELINE ENTERPRISES LLC, based in TWIN FALLS, ID. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

Minor injuries2023-06-03

Filer, ID, USA

Accident — BELL 206B (NTSB WPR23LA214)

Serious injuries1988-11-14

PANAMA CITY, PA

Accident — AIRBUS INDUSTRIE A-300B4-203 (NTSB MIA89WA071)

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

N205PA 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. N205PA 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 N205PA

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

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