N271MA

Valid Registration

2003 AMERICAN CHAMPION AIRCRAFT 7GCAA

N271MA is a 2003 AMERICAN CHAMPION AIRCRAFT 7GCAA registered to EARTHBOUND AVIATION GROUP LLC in WILMINGTON, DE. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 2 Airworthiness Directives may apply.

Registration Details

N-Number
N271MA
Serial Number
475-2003
Manufacturer
AMERICAN CHAMPION AIRCRAFT
Model
7GCAA
Year
2003
Registration Status
Valid
Airworthiness Date
2003-07-24
Owner
EARTHBOUND AVIATION GROUP LLC
Owner City
WILMINGTON
Owner State
DE

The AMERICAN CHAMPION AIRCRAFT 7GCAA is registered with the FAA under N-number N271MA. This airframe was manufactured in 2003. Its manufacturer serial number is 475-2003. The aircraft was issued its airworthiness certificate on 2003-07-24. The current registered owner is EARTHBOUND AVIATION GROUP LLC, based in WILMINGTON, DE. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

Fatal injuries1988-11-16

CHICAGO, IL, USA

Accident — MITSUBISHI MU-2B-60 (NTSB CHI89FA026)

No injuries reported1987-07-02

KANSAS CITY, MO, USA

Accident — MITSUBISHI MU-2B-60 (NTSB MKC87FA130)

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

N271MA 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

2 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. N271MA may be affected by 2 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.

+1 more Airworthiness Directive 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 N271MA

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

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