N4262Y

Valid Registration

1965 BELL 47G-4A

N4262Y is a 1965 BELL 47G-4A registered to SWIFT HORSE WJ LLC in FREDERICKSBURG, TX. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 5 Airworthiness Directives may apply.

Registration Details

N-Number
N4262Y
Serial Number
7674
Manufacturer
BELL
Model
47G-4A
Year
1965
Registration Status
Valid
Airworthiness Date
1982-01-27
Owner
SWIFT HORSE WJ LLC
Owner City
FREDERICKSBURG
Owner State
TX

The BELL 47G-4A is registered with the FAA under N-number N4262Y. This airframe was manufactured in 1965. Its manufacturer serial number is 7674. The aircraft was issued its airworthiness certificate on 1982-01-27. The current registered owner is SWIFT HORSE WJ LLC, based in FREDERICKSBURG, TX. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

Minor injuries2001-08-11

Strathmore, CA, USA

Accident — Bell 47G-4A (NTSB LAX01LA276)

Minor injuries1983-02-03

FIVE POINTS, CA, USA

Accident — BELL 47G4 (NTSB LAX83FA087)

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

N4262Y 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

5 found
AD E9-13563Effective: 2009-06-12

Airworthiness Directives; Bell Helicopter Textron, Inc. Model 47, 47B, 47B3, 47D, 47D1, 47E, 47G, 47G-2, 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G-3B-1, 47G-3B-2, 47G-3B-2A, 47G-4, 47G-4A, 47G-5, 47G-5A, 47H-1, 47J, 47J-2, 47J-2A, and 47K Helicopters

This amendment adopts a new airworthiness directive (AD) for the specified Bell Helicopter Textron, Inc. (Bell) helicopters. This action requires visually inspecting each main rotor blade box beam clip (clip) for correct installation. This amendment is prompted by a report of a main rotor blade with an incorrectly installed clip. The actions specified in this AD are intended to prevent a main rotor blade spar crack as a result of an incorrectly installed clip, loss of a main rotor 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. N4262Y may be affected by 5 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.

+4 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 N4262Y

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

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