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Published 2000-10-06 · Federal Register document 00-25684

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

Publication 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 acceptable method of compliance that involves installation of a new revision to the AFM.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:00.616356+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2000-18aee3630151116d
Source row
results[451]
Raw source SHA-256
18aee3630151116d2fb3a6893673332fd0937cde18bc691722f3a802a62279eb

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2000-19-01
Effective date printed in this edition
Unknown

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Find all recorded historical references to AD 2000-19-01 · 0 printed reference observations in this pinned collection.

These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.

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They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.

Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: b692dc9450f16afd8e333a6e5457b074ae3612718fe913aee8a55c08a6a1c7a6. Source manifest: 067c52f15dae547fad6bec6d868017c004b20b060fd518a9f5291597efc6809a.

Official source · 2000-10-06

Publication text

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Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.

Read the complete official publication text
[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.

-----------------------------------------------------------------------

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]
BILLING CODE 4910-13-P


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Source SHA-256
846cc5fdb2247806645549a8aa238f27b692b5f6b657dc04072ef8a6a1e9f967
Text SHA-256
b692dc9450f16afd8e333a6e5457b074ae3612718fe913aee8a55c08a6a1c7a6

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