Airworthiness Directives; Saab Model SAAB 2000 Airplanes
airworthiness · Rule · Final rule. · Published 2005-08-23 · Effective 2005-09-27 · 70 FR 49173
Document
Document number
05-16456
Federal Register citation
70 FR 49173
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Saab Model SAAB 2000
Publication date
2005-08-23
Effective date
2005-09-27
FAA docket
Docket No. FAA-2005-21341
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Saab Model SAAB 2000 airplanes. This AD requires an inspection for cracking of the fastener holes in the front and rear spars, a modification of the fastener holes of the front and rear spars and the rear spar web, and related investigative/corrective actions if necessary. This AD is prompted by a report of cracking of certain fastener holes in the lower spar cap of the rear spar and in the lower skin at the front spar. We are issuing this AD to prevent cracking of the front and rear spars, which could result in fuel leakage and consequent reduced structural integrity of the wing structure.