airworthiness · Rule · Final rule. · Published 2016-09-08 · Effective 2016-10-13 · 81 FR 61983
Document
Document number
2016-21288
Federal Register citation
81 FR 61983
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Fokker Services B.V.
Publication date
2016-09-08
Effective date
2016-10-13
FAA docket
Docket No. FAA-2016-6665
Abstract
We are adopting a new airworthiness directive (AD) for all Fokker Services B.V. Model F28 Mark 0070 and 0100 airplanes. This AD was prompted by an aileron-wing flutter analysis finding that, when a hydraulic aileron actuator is not powered while at least one aileron flutter damper is inoperative (latent failure), the maximum speed currently defined in the airplane flight manual (AFM) is insufficient to meet the required safety margin. This AD requires revising the AFM to include procedures to follow in the event of a hydraulic system failure and abnormal flight control behavior. We are issuing this AD to ensure that the flightcrew has procedures to follow in the event of a hydraulic system failure and abnormal flight control behavior. If not corrected, this condition could lead to aileron flutter and possible reduced control of the airplane.