Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 2004-04-26 · Effective 2004-05-17 · 69 FR 22392
Document
Document number
04-9115
Federal Register citation
69 FR 22392
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Cessna
Publication date
2004-04-26
Effective date
2004-05-17
FAA docket
Docket No. 2004-CE-09-AD
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. This AD requires you to inspect any upper and lower wing strut attach fitting nut for existence of the corresponding cotter pin and do any necessary corrective action. This AD is the result of a report of one airplane having loose and improperly tied nuts on the wing struts upper attachment bolts. We are issuing this AD to detect and correct loose and improperly tied nuts on the wing struts, which could result in an attachment nut coming off the bolt. This could lead to the failure of the wing structure with consequent loss of control of the airplane.