N9897Y

Valid Registration

1962 CHAMPION 7GCB

N9897Y is a 1962 CHAMPION 7GCB registered to CLINE BRAXTON L in WASILLA, AK. Its FAA registration status is Valid. It has 3 NTSB accident records on file. 3 Airworthiness Directives may apply.

Registration Details

N-Number
N9897Y
Serial Number
7GCB-117
Manufacturer
CHAMPION
Model
7GCB
Year
1962
Registration Status
Valid
Airworthiness Date
1968-06-14
Owner
CLINE BRAXTON L
Owner City
WASILLA
Owner State
AK

The CHAMPION 7GCB is registered with the FAA under N-number N9897Y. This airframe was manufactured in 1962. Its manufacturer serial number is 7GCB-117. The aircraft was issued its airworthiness certificate on 1968-06-14. The current registered owner is CLINE BRAXTON L, based in WASILLA, AK. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2007-07-10

King Salmon, AK, USA

Accident — Champion 7GCB (NTSB ANC07LA064)

No injuries reported2003-06-28

PILOT POINT, AK, USA

Accident — Champion 7GCB (NTSB ANC03LA063)

Minor injuries1992-05-29

SNOW LAKE, AK, USA

Accident — CHAMPION 7GCB (NTSB ANC92LA082)

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

N9897Y has been involved in 3 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. N9897Y 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 N9897Y

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

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