airworthiness · Rule · Final rule. · Published 2014-08-01 · Effective 2014-09-05 · 79 FR 44663
Document
Document number
2014-17468
Federal Register citation
79 FR 44663
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2014-08-01
Effective date
2014-09-05
FAA docket
Docket No. FAA-2014-0228
Abstract
We are adopting a new airworthiness directive (AD) for all Airbus Model A330-200 Freighter, A330-200 and -300, and A340-200, -300, -500, and -600 series airplanes. This AD was prompted by reassessment of an unsafe condition related to MZ-type spoiler servo-controls (SSCs) that did not remain locked in the retracted position (hydraulic locking function) after manual depressurization of the corresponding hydraulic circuit. This reassessment resulted in the determination that performing repetitive operational tests of all SSC types is necessary. This AD requires repetitive operational tests of the hydraulic locking function on each SSC installed on the blue or yellow hydraulic circuits, and replacing any affected SSC with a serviceable SSC. We are issuing this AD to detect and correct loss of the hydraulic locking function during take-off, which, in combination with one inoperative engine, could result in reduced controllability of the airplane.