N186AC

Valid Registration

1994 AMERICAN CHAMPION AIRCRAFT 8GCBC

N186AC is a 1994 AMERICAN CHAMPION AIRCRAFT 8GCBC registered to HARTMAN JAMES R TRUSTEE in EVERETT, WA. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 4 Airworthiness Directives may apply.

Registration Details

N-Number
N186AC
Serial Number
369-94
Manufacturer
AMERICAN CHAMPION AIRCRAFT
Model
8GCBC
Year
1994
Registration Status
Valid
Airworthiness Date
1994-09-21
Owner
HARTMAN JAMES R TRUSTEE
Owner City
EVERETT
Owner State
WA

The AMERICAN CHAMPION AIRCRAFT 8GCBC is registered with the FAA under N-number N186AC. This airframe was manufactured in 1994. Its manufacturer serial number is 369-94. The aircraft was issued its airworthiness certificate on 1994-09-21. The current registered owner is HARTMAN JAMES R TRUSTEE, based in EVERETT, WA. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2007-01-04

Buckley, WA, USA

Accident — American Champion (ACAC) 8GCBC (NTSB SEA07CA042)

No injuries reported2004-02-13

Sunburg, MN, USA

Accident — American Champion (ACAC) 8GCBC (NTSB CHI04LA072)

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

N186AC 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

4 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. N186AC may be affected by 4 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.

+3 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 N186AC

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

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