Rule2022-22331
Airworthiness Directives; Airbus Canada Limited Partnership (Type Certificate Previously Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Airplanes
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
October 21, 2022
Effective
November 25, 2022
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Canada Limited Partnership Model BD-500-1A10 and BD-500- 1A11 airplanes. This AD was prompted by the discovery that overwing emergency exit door (OWEED) handle covers were difficult to open on some airplanes. This AD requires replacing the existing OWEED handle cover brackets with newly designed OWEED handle cover brackets and installing placards regarding this replacement, as specified in a Transport Canada Civil Aviation (TCCA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 87 Issue 203 (Friday, October 21, 2022)</title>
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[Federal Register Volume 87, Number 203 (Friday, October 21, 2022)]
[Rules and Regulations]
[Pages 63933-63935]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-22331]
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Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
========================================================================
Federal Register / Vol. 87, No. 203 / Friday, October 21, 2022 /
Rules and Regulations
[[Page 63933]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0393; Project Identifier MCAI-2021-01249-T;
Amendment 39-22131; AD 2022-16-02]
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.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Airbus Canada Limited Partnership Model BD-500-1A10 and BD-500-
1A11 airplanes. This AD was prompted by the discovery that overwing
emergency exit door (OWEED) handle covers were difficult to open on
some airplanes. This AD requires replacing the existing OWEED handle
cover brackets with newly designed OWEED handle cover brackets and
installing placards regarding this replacement, as specified in a
Transport Canada Civil Aviation (TCCA) AD, which is incorporated by
reference. The FAA is issuing this AD to address the unsafe condition
on these products.
DATES: This AD is effective November 25, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of November 25,
2022.
ADDRESSES: For material incorporated by reference (IBR) in this AD,
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#3170751c727f7145521f56521f5250"><span class="__cf_email__" data-cfemail="a7e6e38ae4e9e7d3c489c0c489c4c6">[email protected]</span></a>; internet <a href="https://tc.canada.ca/en/aviation">https://tc.canada.ca/en/aviation</a>.
You may view this 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 at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2022-
0393.
Examining the AD Docket
You may examine the AD docket at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by
searching for and locating Docket No. FAA-2022-0393; 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, the
mandatory continuing airworthiness information (MCAI), 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: Gabriel Kim, Aerospace Engineer,
Mechanical Systems and Administrative Services Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7300; email <a href="/cdn-cgi/l/email-protection#b48d99d5c2c799dacdd5d7db99d7dbc7f4d2d5d59ad3dbc2"><span class="__cf_email__" data-cfemail="9da4b0fcebeeb0f3e4fcfef2b0fef2eeddfbfcfcb3faf2eb">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
TCCA, which is the aviation authority for Canada, has issued TCCA
AD CF-2021-39, dated November 10, 2021 (TCCA AD CF-2021-39) (also
referred to as the MCAI), to correct an unsafe condition for certain
Airbus Canada Limited Partnership Models BD-500-1A10 and BD-500-1A11
airplanes.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain Airbus Canada
Limited Partnership Model BD-500-1A10 and BD-500-1A11 airplanes. The
NPRM published in the Federal Register on April 6, 2022 (87 FR 19815).
The NPRM was prompted by the discovery that OWEED handle covers were
difficult to open on some airplanes. An investigation revealed that
brackets of certain OWEED handle covers are prone to flexure, thus
increasing the force necessary to remove the OWEED handle cover beyond
design requirements. As a result, the OWEED handle covers must be
removed in order to access the emergency exit, which could delay
passenger evacuation. The NPRM proposed to require replacing the
existing OWEED handle cover brackets with newly designed OWEED handle
cover brackets and installing a placard regarding this replacement, as
specified in TCCA AD CF-2021-39.
The FAA is issuing this AD to address the increased force necessary
to remove the OWEED handle cover to access the emergency exit, which
could hinder passenger evacuation in emergency. See the MCAI for
additional background information.
Discussion of Final Airworthiness Directive
Comments
The FAA received a comment from an individual who supported the
NPRM without change.
The FAA also received a comment from Delta Airlines (DAL). The
following presents that comment received on the NPRM and the FAA's
response.
Request To Clarify Part Numbers for the SB Incorporation Placard
DAL found that the SB Incorporation Placard is identified as two
different part numbers, CDPL604-5 and CDPL604-5-F493000-25-01, in
Safran Service Bulletin F493000-25-01, Revision 1, dated September 17,
2020, which is referenced in TCCA AD CF-2021-39. The Safran component
maintenance manual (CMM) states ``true part number is CDPL604-5-
F493000-25-01, added by service bulletin F493000-25-01'' in the
nomenclature for part number ``CDPL604-5F49300'' described as
``placard, service bulletin incorporation (bonded).'' The Safran CMM
has another part number that begins with ``CDPL604-5,'' but with a
different suffix. The service bulletin does not state the full true
part number CDPL604-5-F493000-25-01. DAL requested that paragraph (h)
of the proposed AD be revised to add an Exception that clarifies the
part numbers.
The FAA partially agrees with the request. The FAA agrees that two
part numbers, CDPL604-5 and CDPL604-5-F493000-25-01, were identified
for the SB Incorporation Placard, and that both
[[Page 63934]]
part numbers are correct and represent the same part. However, the FAA
disagrees with the need to revise paragraph (h) of this AD to provide
further clarification of the part numbers. The replacement kit includes
the correct placard for installation. This AD has not been changed with
regard to this request.
Conclusion
The FAA reviewed the relevant data, considered the comments
received, and determined that air safety requires adopting this AD as
proposed. Except for minor editorial changes, and any other changes
described previously, this AD is adopted as proposed in the NPRM. None
of the changes will increase the economic burden on any operator.
Accordingly, the FAA is issuing this AD to address the unsafe condition
on these products.
Related Service Information Under 1 CFR Part 51
TCCA AD CF-2021-39 specifies procedures for replacing the existing
OWEED handle cover brackets with newly designed OWEED handle cover
brackets and installing placards regarding this replacement.
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.
Costs of Compliance
The FAA estimates that this AD affects 21 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
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3 work-hours x $85 per hour = $255........................... $40 $295 $6,195
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According to the manufacturer, some or all of the costs of this AD
may be covered under warranty, thereby reducing the cost impact on
affected individuals. The FAA does not control warranty coverage for
affected individuals. As a result, the FAA has included all known costs
in the cost estimate.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 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 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2022-16-02 Airbus Canada Limited Partnership (Type Certificate
Previously Held by C Series Aircraft Limited Partnership (CSALP);
Bombardier, Inc.): Amendment 39-22131; Docket No. FAA-2022-0393;
Project Identifier MCAI-2021-01249-T.
(a) Effective Date
This airworthiness directive (AD) is effective November 25,
2022.
(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-2021-39, dated November 10, 2021
(TCCA AD CF-2021-39).
(d) Subject
Air Transport Association (ATA) of America Code 52, Doors.
(e) Unsafe Condition
This AD was prompted by discovery that overwing emergency exit
door (OWEED) handle covers were difficult to open on some airplanes.
An investigation revealed that brackets of certain OWEED handle
covers are prone to flexure, thus increasing the force necessary to
remove the OWEED handle cover beyond design requirements. The FAA is
proposing this AD to address the increased force necessary to remove
the OWEED handle cover to access the emergency exit, which could
hinder passenger evacuation in an emergency.
(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-2021-39.
(h) Exception to TCCA AD CF-2021-39
Where TCCA AD CF-2021-39 refers to its effective date, this AD
requires using the effective date of this AD.
[[Page 63935]]
(i) Additional 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 the attention of the person identified in
paragraph (j) of this AD. Information may be emailed to: ATTN:
Program Manager, Continuing Operational Safety, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7300. Before using any approved AMOC, notify your
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.
(j) Related Information
For more information about this AD, contact Gabriel Kim,
Aerospace Engineer, Mechanical Systems and Administrative Services
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300; email <a href="/cdn-cgi/l/email-protection#142d39756267397a6d75777b39777b67547275753a737b62"><span class="__cf_email__" data-cfemail="ba8397dbccc997d4c3dbd9d597d9d5c9fadcdbdb94ddd5cc">[email protected]</span></a>.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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.
(i) Transport Canada Civil Aviation (TCCA) AD CF-2021-39, dated
November 10, 2021.
(ii) [Reserved]
(3) For TCCA AD CF-2021-39, contact 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#b1f0f59cf2fff1c5d29fd6d29fd2d0"><span class="__cf_email__" data-cfemail="6021244d232e2014034e07034e0301">[email protected]</span></a>; internet
<a href="https://tc.canada.ca/en/aviation">https://tc.canada.ca/en/aviation</a>.
(4) You may view this 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.
(5) You may view this material 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#5335217d3a3d20233630273a3c3d133d3221327d343c25"><span class="__cf_email__" data-cfemail="a6c0d488cfc8d5d6c3c5d2cfc9c8e6c8c7d4c788c1c9d0">[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 July 22, 2022.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022-22331 Filed 10-20-22; 8:45 am]
BILLING CODE 4910-13-P
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