airworthiness · Rule · Final rule; removal of airworthiness directive (AD). · Published 2020-09-11 · Effective 2020-09-11 · 85 FR 56161
Document
Document number
2020-20001
Federal Register citation
85 FR 56161
Type
Rule
Action
Final rule; removal of airworthiness directive (AD).
Category
airworthiness
Manufacturer
Airbus
Publication date
2020-09-11
Effective date
2020-09-11
FAA docket
Docket No. FAA-2020-0463
Abstract
The FAA is removing AD 2015-17-01, which applied to certain Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350C, AS350D, AS350D1, AS355E, AS355F, AS355F1, AS355F2, AS355N, and AS355NP helicopters. AD 2015-17-01 required inspections of each tail rotor pitch horn assembly (pitch horn) for a crack, replacement of a cracked pitch horn, and a repetitive visual inspection of certain pitch horns. AD 2015-17-01 is no longer necessary because the cause of the unsafe condition has been removed from all affected helicopter models. Accordingly, the FAA is removing AD 2015-17-01.