airworthiness · Rule · Final rule; request for comments. · Published 2012-05-29 · Effective 2012-05-29 · 77 FR 31483
Document
Document number
2012-13034
Federal Register citation
77 FR 31483
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Gulfstream Aerospace Corporation
Publication date
2012-05-29
Effective date
2012-05-29
FAA docket
Docket No. FAA-2012-0494
Abstract
We are adopting a new airworthiness directive (AD) for all Gulfstream Aerospace Corporation Model G-1159, G-1159A, and G-1159B airplanes. This AD requires, for certain airplanes, a measurement to determine the clearance (gap) of the exposed rounded portion of the doubler and clothespin fitting at the wing-to-fuselage attachment, and repair if necessary. This AD also requires, for certain other airplanes, determining if a certain aircraft service change has been incorporated, and for affected airplanes, a measurement to determine the clearance (gap) of the exposed rounded portion of the doubler and clothespin fitting at the wing-to-fuselage attachment, and repair if necessary. This AD was prompted by a report of an improper structural modification that had excessive gaps in the wing-to-fuselage attachment fittings. We are issuing this AD to detect and correct excessive gaps in the wing-to-fuselage attachment fittings, which could result in reduced structural integrity at the wing-to-fuselage attachment and consequent separation of the wing from the airplane.