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Airworthiness Directives; Bombardier Model CL-600-1A11 (CL-600) and CL-600-2A12 (CL-601) Series Airplanes

airworthiness · Rule · Final rule; correction. · Published 2000-10-06 · Effective 2000-10-25 · 65 FR 59710

Document

Document number
00-25684
Federal Register citation
65 FR 59710
Type
Rule
Action
Final rule; correction.
Category
airworthiness
Manufacturer
Bombardier Model CL-600-1A11 (CL-600) and CL-600-2A12 (CL-601) Series
Publication date
2000-10-06
Effective date
2000-10-25
FAA docket
Docket No. 99-NM-26-AD

Abstract

This document corrects a typographical error that appeared in airworthiness directive (AD) AD 2000-19-01 that was published in the Federal Register on September 20, 2000 (65 FR 56780). The typographical error resulted in failure to reference an acceptable method of compliance for a certain requirement. This AD is applicable to certain Bombardier Model CL-600-1A11 (CL-600) and CL-600-2A12 (CL-601) series airplanes. This AD requires modification of the main landing gear (MLG) brake units and inboard MLG wheels; and a revision to the Airplane Flight Manual (AFM) to include the increased cooling times for the modified brakes. This AD allows, for certain cases, removal of the inboard and/or outboard wheel discs by installation of a placard to limit airplane operation on the ground and a revision to the AFM to include information for operating the airplane with the wheel discs removed. Additionally, this AD provides for an acceptable method of compliance that involves installation of a new revision to the AFM.

Source

Authoritative
Federal Register document
Machine
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