← FAA Federal Register actions

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

airworthiness · Rule · Final rule. · Published 2003-11-07 · Effective 2003-12-12 · 68 FR 63013

Document

Document number
03-27668
Federal Register citation
68 FR 63013
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2003-11-07
Effective date
2003-12-12
FAA docket
Docket No. 2002-NM-157-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model CL-600-1A11 (CL-600), CL-600- 2A12 (CL-601), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) series airplanes. This amendment requires revising the airplane flight manual to provide the flightcrew with procedures and limitations for operating the airplane with out-of-tolerance angle of attack (AOA) transducers. This amendment also requires, among other actions, measuring the vane angles and voltage of the AOA transducers; reworking the AOA transducer assemblies; repetitive measurements of the resistance of both AOA transducers; and follow-on and corrective actions, as applicable. This action is necessary to prevent flat spots on the potentiometers of the AOA transducers due to wear, which may cause a delay in the commands for stall warning, stick shaker, and stick pusher operation. This action is intended to address the identified unsafe condition.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown