N2238U

Valid Registration

1968 BRANTLY B-2B

N2238U is a 1968 BRANTLY B-2B registered to HEWITT ROBERT E in BYBEE, TN. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 1 Airworthiness Directive may apply.

Registration Details

N-Number
N2238U
Serial Number
479
Manufacturer
BRANTLY
Model
B-2B
Year
1968
Registration Status
Valid
Airworthiness Date
1968-02-02
Owner
HEWITT ROBERT E
Owner City
BYBEE
Owner State
TN

The BRANTLY B-2B is registered with the FAA under N-number N2238U. This airframe was manufactured in 1968. Its manufacturer serial number is 479. The aircraft was issued its airworthiness certificate on 1968-02-02. The current registered owner is HEWITT ROBERT E, based in BYBEE, TN. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2003-03-08

Zelienople, PA, USA

Accident — Brantly Helicopter B-2B (NTSB NYC03LA063)

No injuries reported1999-08-15

HUDSON, MI, USA

Accident — Brantly Helicopter B-2B (NTSB CHI99LA292)

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

N2238U 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

1 found
AD 06-3536Effective: 2006-04-17

Airworthiness Directives; Brantly International, Inc. Model B-2, B-2A, and B-2B Helicopters

This amendment adopts a new airworthiness directive (AD) for the specified Brantly International, Inc. (Brantly) model helicopters. This action requires certain inspections and measurements of the upper tail rotor vertical gearbox (gearbox), vertical shaft (shaft) and shaft housing (housing) and their associated parts; and of the intermediate gear box bushing (bushing). This amendment is prompted by an accident and an incident report of fatigue cracking of a shaft. The actions specified in this AD are intended to prevent fatigue cracking of a shaft, failure of a shaft, and subsequent loss of control of the helicopter.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N2238U may be affected by 1 directive. 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.

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Get the complete history for N2238U

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

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