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AD 94-15595

Published 1994-06-28 · 2 models · 2 US-registered tails affected · Federal Register

Airworthiness Directives; Canadair Model CL-600-1A11, -2A12, and -2B16 Series Airplanes Federal Register ↗

Abstract

This document revises an earlier proposed airworthiness directive (AD), applicable to certain Canadair Model CL-600-1A11, - 2A12, and -2B16 series airplanes, that would have required a test of the engine throttle quadrant to determine if the throttle lever bypasses the idle stop into the shut-off position, and modification of the throttle quadrant or replacement of the throttle quadrant with a modified unit. That proposal was prompted by reports of unintentional engine shutdown on certain of these airplanes. This action revises the proposed rule by requiring a different test and eventual replacement of the throttle quadrant. The actions specified by this proposed AD are intended to prevent inadvertent shutdown of an engine while the airplane is taxiing or in flight.

Applicability · by US fleet size

Compliance instructions

Required actions, compliance times, parts/serial numbers and methods of compliance are in the Federal Register publication — not paraphrased here. Read AD on Federal Register ↗