Published 2011-08-03 · Federal Register document C1-2011-17402
Airworthiness Directives; Bombardier, Inc. Model CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604 Variants) Airplanes
Publication summary
No summary was recorded in this metadata source.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:36.067984+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2011-e3661fa6ab35b428
- Source row
- results[214]
- Raw source SHA-256
- e3661fa6ab35b428e6e5ee3716d50c22e985c092328ad8ce2f0f440b962ae0cd
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2011-09-09
- Effective date printed in this edition
- Unknown
This correction is a separate source edition; it is not counted as a new adopted rule.
No adopted-clause structure was recorded for this source edition. Read the complete text; no applicability conclusion has been inferred.
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2011-09-09 · 0 printed reference observations in this pinned collection.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.
Why these observations are shown
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-1.2.0. Text SHA-256: cac62af2752e0009ed2c0360490fb4529c05cddf240cd698873dfcf88e1bbfad. Source manifest: 9746c88c23dbb64ad18fb573e5d6aa76976fb4537a70c3c1393a22342951b21d.
Official source · 2011-08-03
Publication text
This is the complete recorded text of this dated publication.
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 76, Number 149 (Wednesday, August 3, 2011)]
[Rules and Regulations]
[Pages 46597-46598]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: C1-2011-17402]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-1307; Directorate Identifier 2010-NM-049-AD;
Amendment 39-16671; AD 2011-09-09]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc. Model CL-600-2A12 (CL-
601) and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604 Variants)
Airplanes
Correction
In rule document 2011-17402 appearing on page 41653-41657, in the
issue of Friday, July 15, 2011, make the following correction:
[[Page 46598]]
39--AIRWORTHINESS DIRECTIVES
Sec. 39.13 [Corrected]
On page 41655, in the second table, Table 2--Initial Compliance
Times for Airworthiness Limitations Tasks, a fourth column title was
inadvertently printed above the words ``Within 240 Flight hours after
the effective date of this AD.'' The table should appear as set forth
below.
Table 2--Initial Compliance Times for Airworthiness Limitations Tasks
----------------------------------------------------------------------------------------------------------------
----------------------------------------------------------------------------------------------------------------
Bombardier, Inc. model-- Task(s)-- Initial compliance time (whichever occurs later)--
----------------------------------------------------------------------------------------------------------------
CL-600-2A12 (CL-601) airplanes, 30-11-00-101, Wing Anti- Prior to the Within 240 flight hours
serial numbers 3001 through 3066 icing. accumulation of 4,800 after the effective
inclusive; and CL-600-2B16 (CL- total flight hours; or date of this AD.
601-3A and CL-601-3R Variants) within 4,800 flight
airplanes, serial numbers 5001 hours after
through 5194 inclusive; on which accomplishing Task 30-
Bombardier Service Bulletin 601- 11-06-204 in Section 5-
0590 has been accomplished. 20-15 of the applicable
Time Limits/Maintenance
Checks manual specified
in table 1 of this AD;
whichever occurs later.
CL-600-2A12 (CL-601) airplanes, 30-11-00-102, Wing Anti- Prior to the Within 240 flight hours
serial numbers 3001 through 3066 icing. accumulation of 4,800 after the effective
inclusive; and CL-600-2B16 (CL- total flight hours; or date of this AD.
601-3A and CL-601-3R Variants) within 4,800 flight
airplanes, serial numbers 5001 hours after
through 5194 inclusive; on which accomplishing Task 30-
Bombardier Service Bulletin 601- 13-00-205 in Section 5-
0590 has been accomplished. 20-15 of the applicable
Time Limits/Maintenance
Checks manual specified
in table 1 of this AD;
whichever occurs later.
CL-600-2B16 (CL-604 Variants) 30-11-00-101, Detailed Prior to the Within 320 flight hours
airplanes, serial numbers 5301 Inspection of the Wing accumulation of 6,400 after the effective
through 5665 inclusive. Anti-Ice Duct Piccolo- total flight hours; date of this AD.
Tube, and 36-21-00-101, except for airplanes
Functional Test of the having 6,400 total
Leading Edge Thermal flight hours or more as
Switches. of the effective date
of this AD on which the
task has not been
accomplished: prior to
the next scheduled
6,400 flight hour task
inspection or prior to
the next scheduled
accomplishment of Task
57-10-00-208 in the
applicable Time Limits/
Maintenance Checks
manual specified in
table 1 of this AD,
whichever occurs first.
CL-600-2B16 (CL-604 Variants) 30-11-00-101, Detailed Prior to the Within 320 flight hours
airplanes, serial numbers 5701 Inspection of the Wing accumulation of 6,400 after the effective
and subsequent. Anti-Ice Duct Piccolo- total flight hours. date of this AD.
Tube, and 36-21-00-101,
Functional Test of the
Leading Edge Thermal
Switches.
----------------------------------------------------------------------------------------------------------------
[FR Doc. C1-2011-17402 Filed 7-28-11; 8:45 am]
BILLING CODE 1505-01-D
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:07:52.617192+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- ac2222df3a7f85901aa7cd02ce92150d8d87b18aff90a923281bf4f30359045b
- Text SHA-256
- cac62af2752e0009ed2c0360490fb4529c05cddf240cd698873dfcf88e1bbfad
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.