AD 2021-09-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | BD-500-1A10 BD-500-1A11 | Airworthiness Directives; Airbus Canada Limited Partnership (Type Certificate Previously Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Airplanes |
| aircraft | Bombardier | Various | Airworthiness Directives; Airbus Canada Limited Partnership (Type Certificate Previously Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Canada Limited Partnership (Type Certificate Previously Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Airplanes |
Unsafe Condition
The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to certain Airbus Canada Limited Partnership Model BD-500-1A10 and BD-500-1A11 airplanes. As published, two references to a Transport Canada Civil Aviation (TCCA) AD number specified in the regulatory text are incorrect. This document corrects those errors. In all other respects, the original document remains the same.
Affected Aircraft
Airbus Canada Limited Partnership (Type Certificate Previously Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Model BD-500-1A10 and BD-500-1A11 airplanes, certificated in any category, as identified in Transport Canada Civil Aviation (TCCA) AD CF-2021-10, dated March 18, 2021 (TCCA AD CF-2021-10)
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to certain Airbus Canada Limited Partnership Model BD-500-1A10 and BD-500-1A11 airplanes. As published, two references to a Transport Canada Civil Aviation (TCCA) AD number specified in the regulatory text are incorrect. This document corrects those errors. In all other respects, the original document remains the same.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to Airbus Canada Limited Partnership (type
certificate previously held by C Series Aircraft Limited Partnership
(CSALP); Bombardier, Inc.) Model BD-500-1A10 and BD-500-1A11
airplanes, certificated in any category, as identified in Transport
Canada Civil Aviation (TCCA) AD CF-2021-10, dated March 18, 2021
(TCCA AD CF-2021-10).
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 86, Number 79 (Tuesday, April 27, 2021)]
[Rules and Regulations]
[Pages 22111-22113]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2021-08760]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-0313; Project Identifier MCAI-2021-00348-T;
Amendment 39-21516; AD 2021-09-03]
RIN 2120-AA64
Airworthiness Directives; Airbus Canada Limited Partnership (Type
Certificate Previously Held by C Series Aircraft Limited Partnership
(CSALP); Bombardier, Inc.) Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
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SUMMARY: The FAA is correcting an airworthiness directive (AD) that was
published in the Federal Register. That AD applies to certain Airbus
Canada Limited Partnership Model BD-500-1A10 and BD-500-1A11 airplanes.
As published, two references to a Transport Canada Civil Aviation
(TCCA) AD number specified in the regulatory text are incorrect. This
document corrects those errors. In all other respects, the original
document remains the same.
DATES: This correction is effective May 4, 2021. The effective date of
AD 2021-09-03 remains May 4, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of May 4, 2021
(86 FR 20266, April 19, 2021).
The date by which FAA must receive comments on this AD remains June
3, 2021.
ADDRESSES: For material incorporated by reference (IBR) in this AD,
contact TCCA, Transport Canada National
[[Page 22112]]
Aircraft Certification, 159 Cleopatra Drive, Nepean, Ontario K1A 0N5,
Canada; telephone 888-663-3639; email <a href="/cdn-cgi/l/email-protection#d09194fd939e90a4b3feb7b3feb3b1"><span class="__cf_email__" data-cfemail="d9989df49a9799adbaf7bebaf7bab8">[email protected]</span></a>; internet <a href="https://tc.canada.ca/en/aviation">https://tc.canada.ca/en/aviation</a>. You may view this IBR material at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200 South
216th St., Des Moines, WA. For information on the availability of this
material at the FAA, call 206-231-3195. It is also available in the AD
docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for
and locating Docket No. FAA-2021-0313.
Examining the AD Docket
You may examine the AD docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2021-
0313; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this final rule, any comments received, and other information. The
address for Docket Operations is U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Deep Gaurav, Aerospace Engineer,
Airframe and Propulsion Section, FAA, New York ACO Branch, 1600 Stewart
Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7300; fax 516-
794-5531; email <a href="/cdn-cgi/l/email-protection#5f66723e292c7231263e3c30723c302c1f393e3e71383029"><span class="__cf_email__" data-cfemail="2b12064a5d580645524a4844064844586b4d4a4a054c445d">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION: AD 2021-09-03, Amendment 39-21516 (86 FR
20266, April 19, 2021) (AD 2021-09-03), requires repetitive
replacements of the emergency locator transmitter (ELT) antenna and
repetitive inspections for damage of the exterior fuselage skin around
the ELT antenna attachment area, as specified in TCCA AD CF-2021-10,
dated March 18, 2021 (TCCA AD CF-2021-10). That AD applies to certain
Airbus Canada Limited Partnership Model BD-500-1A10 and BD-500-1A11
airplanes.
Need for the Correction
As published, the TCCA AD number specified in paragraphs (h)(1) and
(2) of the regulatory text of AD 2021-09-03 is incorrectly identified
as ``TCCA AD CF-2020-10,'' where the correct identification is ``TCCA
AD CF-2021-10.''
Related Service Information Under 1 CFR Part 51
TCCA AD CF-2021-10 describes procedures for repetitive replacements
of the ELT antenna with a new ELT antenna and repetitive inspections of
the exterior fuselage skin around the ELT antenna attachment area for
damage (including cracking). This material is reasonably available
because the interested parties have access to it through their normal
course of business or by the means identified in the ADDRESSES section.
Correction of Publication
This document corrects multiple errors and correctly adds the AD as
an amendment to 14 CFR 39.13. Although no other part of the preamble or
regulatory information has been corrected, the FAA is publishing the
entire rule in the Federal Register.
The effective date of this AD remains May 4, 2021.
Since this action only corrects references to a TCCA AD number, it
has no adverse economic impact and imposes no additional burden on any
person. Therefore, the FAA has determined that notice and public
procedures are unnecessary.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Correction
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration amends part 39 of
the Federal Aviation Regulations (14 CFR part 39) as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Corrected]
0
2. The FAA corrects Sec. 39.13 by revising the following airworthiness
directive to read:
2021-09-03 Airbus Canada Limited Partnership (Type Certificate
Previously Held by C Series Aircraft Limited Partnership (CSALP);
Bombardier, Inc.): Amendment 39-21516; Docket No. FAA-2021-0313;
Project Identifier MCAI-2021-00348-T.
(a) Effective Date
This airworthiness directive (AD) becomes effective May 4, 2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Canada Limited Partnership (type
certificate previously held by C Series Aircraft Limited Partnership
(CSALP); Bombardier, Inc.) Model BD-500-1A10 and BD-500-1A11
airplanes, certificated in any category, as identified in Transport
Canada Civil Aviation (TCCA) AD CF-2021-10, dated March 18, 2021
(TCCA AD CF-2021-10).
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.
(e) Reason
This AD was prompted by reports of the failure of emergency
locator transmitter (ELT) antennas. The FAA is issuing this AD to
address ELT antenna failure, which can lead to the loss of the ELT
antenna and the development of fuselage cracks that can result in an
inability to maintain cabin pressure.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, TCCA AD CF-2021-10.
(h) Exception to TCCA AD CF-2021-10
(1) Where TCCA AD CF-2021-10 refers to its effective date, this
AD requires using the effective date of this AD.
(2) Where TCCA AD CF-2021-10 refers to hours air time, this AD
requires using flight hours.
(3) If any damage is found as a result of the inspections
required by this AD, repairs must be done before further flight.
(i) Special Flight Permit
Special flight permits may be issued in accordance with 14 CFR
21.197 and 21.199 to operate the airplane to a location where the
airplane can be modified (if the operator elects to do so), provided
no passengers are onboard.
(j) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York ACO Branch, FAA, has the authority to approve AMOCs for this
AD, if requested using the procedures found in 14 CFR 39.19. In
accordance with 14 CFR 39.19, send your request to your principal
inspector or responsible Flight Standards Office, as appropriate. If
sending information directly to the manager of the certification
office, send it to ATTN: Program Manager, Continuing Operational
Safety, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300; fax 516-794-5531. Before
using any approved AMOC, notify your
[[Page 22113]]
appropriate principal inspector, or lacking a principal inspector,
the manager of the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, New York ACO
Branch, FAA; or TCCA; or Airbus Canada Limited Partnership's TCCA
Design Approval Organization (DAO). If approved by the DAO, the
approval must include the DAO-authorized signature.
(k) Related Information
For more information about this AD, contact Deep Gaurav,
Aerospace Engineer, Airframe and Propulsion Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7300; fax 516-794-5531; email <a href="/cdn-cgi/l/email-protection#9aa3b7fbece9b7f4e3fbf9f5b7f9f5e9dafcfbfbb4fdf5ec"><span class="__cf_email__" data-cfemail="c7feeaa6b1b4eaa9bea6a4a8eaa4a8b487a1a6a6e9a0a8b1">[email protected]</span></a>.
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(3) The following service information was approved for IBR on
May 4, 2021 (86 FR 20266, April 19, 2021).
(i) Transport Canada Civil Aviation (TCCA) AD CF-2021-10, dated
March 18, 2021.
(ii) [Reserved]
(4) For TCCA AD CF-2021-10, contact TCCA, Transport Canada
National Aircraft Certification, 159 Cleopatra Drive, Nepean,
Ontario K1A 0N5, Canada; telephone 888-663-3639; email <a href="/cdn-cgi/l/email-protection#6a2b2e4729242a1e09440d0944090b"><span class="__cf_email__" data-cfemail="9bdadfb6d8d5dbeff8b5fcf8b5f8fa">[email protected]</span></a>; internet <a href="https://tc.canada.ca/en/aviation">https://tc.canada.ca/en/aviation</a>.
(5) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th St., Des Moines, WA. For information on the availability
of this material at the FAA, call 206-231-3195. This material may be
found in the AD docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-
2021-0313.
(6) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, email <a href="/cdn-cgi/l/email-protection#c1a7a4a5b3a4a6efada4a6a0ad81afa0b3a0efa6aeb7"><span class="__cf_email__" data-cfemail="6b0d0e0f190e0c45070e0c0a072b050a190a450c041d">[email protected]</span></a>, or go to: <a href="https://www.archives.gov/federal-register/cfr/ibr-locations.html">https://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued on April 22, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2021-08760 Filed 4-23-21; 11:15 am]
BILLING CODE 4910-13-P
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Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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