Airworthiness Directives; Pilatus Aircraft Ltd. Model PC-7 Airplanes
airworthiness · Rule · Final rule. · Published 2000-01-12 · Effective 2000-03-03 · 65 FR 1767
Document
Document number
00-498
Federal Register citation
65 FR 1767
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Pilatus
Publication date
2000-01-12
Effective date
2000-03-03
FAA docket
Docket No. 99-CE-61-AD
Abstract
This amendment supersedes Airworthiness Directive (AD) 98-08- 07, which currently requires replacing the rudder and elevator pivot arms with parts of improved design on certain Pilatus Aircraft Ltd. (Pilatus) Model PC-7 airplanes. This AD requires replacing the rudder and elevator pivot arms with parts that have been improved since issuance of AD 98-08-07. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified by this AD are intended to prevent failure of the elevator and rudder caused by fatigue cracking of the pivot arms, which could result in reduced airplane controllability and possible loss of control of the airplane.