N2583F

Valid Registration

CHAMPION 7ECA

N2583F is a CHAMPION 7ECA registered to CHATWELL TERRY D in FORT WORTH, TX. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 3 Airworthiness Directives may apply.

Registration Details

N-Number
N2583F
Serial Number
214
Manufacturer
CHAMPION
Model
7ECA
Year
—
Registration Status
Valid
Airworthiness Date
1965-05-19
Owner
CHATWELL TERRY D
Owner City
FORT WORTH
Owner State
TX

The CHAMPION 7ECA is registered with the FAA under N-number N2583F. Its manufacturer serial number is 214. The aircraft was issued its airworthiness certificate on 1965-05-19. The current registered owner is CHATWELL TERRY D, based in FORT WORTH, TX. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2004-08-29

Williams, AZ, USA

Accident — Champion 7ECA (NTSB LAX04CA307)

No injuries reported1997-07-09

SONORA, TX, USA

Accident — Bellanca 7ECA (NTSB FTW97LA260)

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

N2583F 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

3 found
AD E9-25258Effective: 2009-10-29

Airworthiness Directives; American Champion Aircraft Corp. Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes

We are adopting a new airworthiness directive (AD) for all American Champion Aircraft Corp. Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC airplanes, manufactured prior to 1989 and equipped with folding rear seat backs. This AD requires inspection of the rear seat back hinge areas for cracking and excessive elongation of the rear seat hinge bolt hole and, if cracking or excessive elongation is found, replacement of the rear seat frame. We are issuing this AD to detect and correct cracking of the rear seat back hinge area and excessive elongation of the rear seat hinge bolt hole, either of which could result in failure of the seat back. This failure could lead to a rear- seated pilot or passenger inadvertently interfering with the control stick while attempting to not roll to the rear of the airplane upon seat back failure. Consequently, this failure could result in loss of control.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N2583F may be affected by 3 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.

+2 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 N2583F

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

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