← FAA Federal Register actions

Airworthiness Directives; Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) Series Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 2004-12-20 · Effective 2005-01-04 · 69 FR 75830

Document

Document number
04-27507
Federal Register citation
69 FR 75830
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2004-12-20
Effective date
2005-01-04
FAA docket
Docket No. FAA-2004-19862

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) series airplanes. This AD requires revising the airplane flight manual to provide the flightcrew with procedures and limitations for operating an airplane with out-of-tolerance angle of attack (AOA) transducers. This AD also requires repetitive linearity tests of the AOA transducers, and corrective action if necessary. This AD is prompted by a report of premature wear of the potentiometers in AOA transducers having a certain part number. We are issuing this AD to prevent a delay in the stall computer commands for stall warning, stick shaker, and stick pusher operation, due to premature wear of the potentiometers of the AOA transducers, which may cause the airplane to enter a stall condition, and result in loss of control of the airplane.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown