Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes
airworthiness · Rule · Final rule. · Published 2001-11-15 · Effective 2002-01-07 · 66 FR 57364
Document
Document number
01-28571
Federal Register citation
66 FR 57364
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Reims Aviation S.A. Model F406
Publication date
2001-11-15
Effective date
2002-01-07
FAA docket
Docket No. 99-CE-28-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that applies to certain Reims Aviation S.A. (Reims) Model F406 airplanes. This AD requires you to repetitively inspect the canted rib upper cap in the center wing carry-through area for cracks, and, if cracks are found, immediately repair the cracks or modify this area depending on the extent of any cracks found. This AD also requires you to modify the canted rib upper cap at a certain time period as terminating action for the repetitive inspections. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by this AD are intended to detect and correct cracks in the canted rib upper cap in the center wing carry-through area, which could result in structural failure of the wing with possible loss of control of the airplane.