Airworthiness Directives; Airbus Industrie Model A310 and A300- 600 Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 1994-01-05 · Effective 1994-01-20 · 59 FR 507
Document
Document number
94-21
Federal Register citation
59 FR 507
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Airbus Industrie Model A310 and A300- 600 Series
Publication date
1994-01-05
Effective date
1994-01-20
FAA docket
Federal Register: January 5, 1994
Abstract
This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) T93-24-51 that was sent previously to all known U.S. owners and operators of all Airbus Model A310 and A300-600 series airplanes by individual telegrams. This AD requires repetitive operational tests of feel and limitation computers (FLC) 1 and 2. This amendment is prompted by a report that the pitch control on a Model A300-600 series airplane operated with stiffness. The actions specified by this AD are intended to prevent stiff operation of the pitch control and undetected loss of rudder travel limitation function.