Airworthiness Directive

AD 2009-22-02 74 FR 55765

Federal Aviation Administration · 14 CFR part 39

FR document
E9-25258
Amendment
39-16053
Published
2009-10-29
Models covered
1
Last live check
2026-08-17
AD

2009-22-02

FR doc E9-25258 · 74 FR 55765

AD 2009-22-02Published 2009-10-29Effective 2009-12-03

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.

Full official abstract

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.

Applies to 1 model in our index