[Federal Register Volume 65, Number 195 (Friday, October 6, 2000)]
[Rules and Regulations]
[Pages 59710-59711]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 00-25684]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 99-NM-26-AD; Amendment 39-11902; AD 2000-19-01]
RIN 2120-AA64
Airworthiness Directives; Bombardier Model CL-600-1A11 (CL-600)
and CL-600-2A12 (CL-601) Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
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SUMMARY: 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
[[Page 59711]]
acceptable method of compliance that involves installation of a new
revision to the AFM.
DATES: Effective October 25, 2000.
FOR FURTHER INFORMATION CONTACT: James E. Delisio, Aerospace Engineer,
Airframe and Propulsion Branch, ANE-171, FAA, New York Aircraft
Certification Office, 10 Fifth Street, Third Floor, Valley Stream, New
York 11581; telephone (516) 256-7521; fax (516) 568-2716.
SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 2000-19-01,
amendment 39-11902, applicable to certain Bombardier Model CL-600-1A11
(CL-600) and CL-600-2A12 (CL-601) series airplanes, was published in
the Federal Register on September 20, 2000 (65 FR 56780). That 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. That 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, that AD
provides for an acceptable method of compliance that involves
installation of a new revision to the AFM.
As published, paragraph (d) of the existing AD specifies that
installation of a specific AFM revision is acceptable for compliance
with the requirements of paragraphs (a) and (b) of that AD. The FAA
inadvertently did not specify that installation of a specific AFM
revision is also acceptable for compliance with the requirements of
paragraph (c) of that AD.
Since no other part of the regulatory information has been changed,
the final rule is not being republished.
The effective date of this AD remains October 25, 2000.
Sec. 39.13 [Corrected]
On page 56782, in the second column, paragraph (d) of AD 2000-19-01
is corrected to read as follows:
* * * * *
(d) For all airplanes: Installation of the AFM revision specified
in either paragraph (d)(1) or (d)(2) of this AD, as applicable, is
acceptable for compliance with the requirements of paragraphs (a), (b),
and (c) of this AD, as applicable.
(1) Bombardier Model CL-600-1A11 (CL-600) AFM Revisions A84 and 76,
both dated February 7, 2000; or
(2) Bombardier Model CL600-2A12 (CL-601) AFM Revisions 45, 48, 50,
and 86, all dated February 7, 2000.
* * * * *
Issued in Renton, Washington, on October 2, 2000.
Donald L. Riggin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 00-25684 Filed 10-5-00; 8:45 am]
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