Airworthiness Directives; Raytheon Aircraft Company Models 58P and 58TC Airplanes
airworthiness · Rule · Final rule. · Published 2007-10-11 · Effective 2007-11-15 · 72 FR 57850
Document
Document number
E7-19888
Federal Register citation
72 FR 57850
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Raytheon
Publication date
2007-10-11
Effective date
2007-11-15
FAA docket
Docket No. FAA-2005-21175
Abstract
The FAA adopts a new airworthiness directive (AD) for certain Raytheon Aircraft Company (RAC) Models 58P and 58TC airplanes that were used as lead airplanes by the United States Forest Service (USFS). This AD establishes new limits for the structural life of the airframe (wing, fuselage, empennage, and associated structure) through the incorporation of a supplement to the Limitations Section of the pilot's operating handbook and airplane flight manual (POH/AFM). This AD results from the FAA's analysis and determination that the operational history and usage of the affected airplanes requires a reduction in the structural life limit to 4,500 hours time-in-service (TIS) for the airframe (wing, fuselage, empennage, and associated structure). We are issuing this AD to prevent structural failure of the airframe (wing, fuselage, empennage, or associated structure) based on the operational history and usage of the affected airplanes. Such failure could lead to loss of control.