Rule2022-05525
Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters
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
March 15, 2022
Effective
March 30, 2022
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Deutschland GmbH (AHD) Model MBB-BK 117 C-2 and MBB-BK 117 D-2 helicopters. This AD was prompted by a report of erroneous or partial installation of the seat belt restraint system. This AD requires inspecting certain seats, as specified in a European Union Aviation Safety Agency (EASA) 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 50 (Tuesday, March 15, 2022)</title>
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[Federal Register Volume 87, Number 50 (Tuesday, March 15, 2022)]
[Rules and Regulations]
[Pages 14385-14388]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-05525]
========================================================================
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. 50 / Tuesday, March 15, 2022 / Rules
and Regulations
[[Page 14385]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0278; Project Identifier MCAI-2021-01437-R;
Amendment 39-21979; AD 2022-06-13]
RIN 2120-AA64
Airworthiness Directives; Airbus Helicopters Deutschland GmbH
(AHD) Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Airbus Helicopters Deutschland GmbH (AHD) Model MBB-BK 117 C-2
and MBB-BK 117 D-2 helicopters. This AD was prompted by a report of
erroneous or partial installation of the seat belt restraint system.
This AD requires inspecting certain seats, as specified in a European
Union Aviation Safety Agency (EASA) AD, which is incorporated by
reference. The FAA is issuing this AD to address the unsafe condition
on these products.
DATES: This AD becomes effective March 30, 2022.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of March 30,
2022.
The FAA must receive comments on this AD by April 29, 2022.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to <a href="https://www.regulations.gov">https://www.regulations.gov</a>. Follow the instructions for submitting comments.
<bullet> Fax: (202) 493-2251.
<bullet> Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
<bullet> Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For EASA material incorporated by reference (IBR) in this final
rule, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany;
telephone +49 221 8999 000; email <a href="/cdn-cgi/l/email-protection#d59491a695b0b4a6b4fbb0a0a7baa5b4fbb0a0"><span class="__cf_email__" data-cfemail="9fdedbecdffafeecfeb1faeaedf0effeb1faea">[email protected]</span></a>; internet
www.easa.europa.eu. You may find this IBR material on the EASA website
at <a href="https://ad.easa.europa.eu">https://ad.easa.europa.eu</a>. For Mecaer Aviation Group (MAG) service
information identified in this final rule, contact Mecaer Aviation
Group, Via dell'Artigianato 1, Monteprandone 63076 Ascoli Piceno,
Italy; telephone (+39) 0735-7091; email <a href="/cdn-cgi/l/email-protection#72111305321f17111317005c111d1f"><span class="__cf_email__" data-cfemail="482b293f08252d2b292d3a662b2725">[email protected]</span></a>; or at
<a href="http://www.mecaer.com">www.mecaer.com</a>. You may view this material at the FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321,
Fort Worth, TX 76177. For information on the availability of this
material at the FAA, call (817) 222-5110. Service information that is
IBRed 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-2022-0278.
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-2022-0278; 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
EASA AD, supplemental type certificates (STCs), any comments received,
and other information. The street address for Docket Operations is
listed above. Comments will be available in the AD docket shortly after
receipt.
FOR FURTHER INFORMATION CONTACT: Antariksh Shetty, Aerospace Engineer,
Airframe & Propulsion Section, New York ACO Branch, Compliance &
Airworthiness Division, FAA, 1600 Stewart Avenue, Suite 410, Westbury,
NY 11590; telephone (516) 228-7300; email <a href="/cdn-cgi/l/email-protection#5b62763a2d287635223a3834763834281b3d3a3a753c342d"><span class="__cf_email__" data-cfemail="2c15014d5a5f0142554d4f43014f435f6c4a4d4d024b435a">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2021-0287, dated December 21, 2021,
and corrected January 26, 2022 (EASA AD 2021-0287), to correct an
unsafe condition for Airbus Helicopters Deutschland GmbH (AHD),
formerly Eurocopter Deutschland GmbH; and Airbus Helicopters Inc.,
formerly American Eurocopter LLC, Model MBB-BK117 C-2, D-2, and D-3
helicopters, all serial numbers, if modified in accordance with EASA
STC 10038915 or STC 10055175. The equivalent FAA STCs for Model MBB-
BK117 C-2 and MBB-BK117 D-2 helicopters are STC SR03130NY and STC
SR03703NY, respectively. Currently, there are no equivalent FAA STCs or
any other forms of FAA design approval to install an affected seat on
Model MBB-BK117 D-3 helicopters. Accordingly, this modification does
not affect U.S. registered MBB-BK117 D-3 helicopters, so this AD does
not include that model in the applicability.
This AD was prompted by a report of erroneous or partial
installation of the seat belt restraint system. The FAA is issuing this
AD to ensure proper installation of the seat belt restraint system. See
EASA AD 2021-0287 for additional background information.
Related Service Information Under 1 CFR Part 51
EASA AD 2021-0287 requires a one-time inspection of the affected
seats and depending on the results, corrective action or marking the
affected seat ``inoperative.''
The FAA also reviewed Mecaer Aviation Group Mandatory Service
Bulletin No. SB-EC1-010, Revision A, dated December 30, 2021 (SB-EC1-
010, Rev A). SB-EC1-010, Rev A identifies affected part-numbered and
serial-numbered pilot, co-pilot, and passenger (passenger cabin) seats,
and specifies procedures for inspecting the affected seats for proper
assembly and corrective action if there is a deviation.
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.
Other Related Service Information
The FAA reviewed B/E Aerospace Fischer Component Maintenance Manual
With Illustrated Parts List, 25-24-19, Revision D, dated September 10,
2018. This service information specifies
[[Page 14386]]
procedures for maintenance, repair, disassembly, and assembly of an
affected crew (pilot or co-pilot) seat.
The FAA also reviewed Fischer+Entwicklungen Component Maintenance
Manual With Illustrated Parts List, 25-24-29, Revision C, dated January
09, 2013. This service information specifies procedures for
maintenance, repair, disassembly, and assembly of an affected common
(passenger or passenger cabin) seat.
FAA's Determination
These helicopters have been approved by EASA and are approved for
operation in the United States. Pursuant to the FAA's bilateral
agreement with the European Union, EASA, its technical representative,
has notified the FAA of the unsafe condition described in its AD. The
FAA is issuing this AD after evaluating all pertinent information and
determining that the unsafe condition exists and is likely to exist or
develop on other helicopters of the same type designs.
Requirements of This AD
This AD requires accomplishing the actions specified in EASA AD
2021-0287, described previously, as incorporated by reference, except
for any differences identified as exceptions in the regulatory text of
this AD and except as discussed under ``Differences Between this AD and
EASA AD 2021-0287.''
Explanation of Required Compliance Information
In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA developed a process to use some civil aviation
authority (CAA) ADs as the primary source of information for compliance
with requirements for corresponding FAA ADs. The FAA has been
coordinating this process with manufacturers and CAAs. As a result,
EASA AD 2021-0287 will be incorporated by reference in this FAA final
rule. This AD would, therefore, require compliance with EASA AD 2021-
0287 in its entirety through that incorporation, except for any
differences identified as exceptions in the regulatory text of this AD.
Using common terms that are the same as the heading of a particular
section in EASA AD 2021-0287 does not mean that operators need comply
only with that section. For example, where the AD requirement refers to
``all required actions and compliance times,'' compliance with this AD
requirement is not limited to the section titled ``Required Action(s)
and Compliance Time(s)'' in EASA AD 2021-0287. Service information
referenced in EASA AD 2021-0287 for compliance will be available at
<a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No.
FAA-2022-0278.
Differences Between This AD and EASA AD 2021-0287
EASA AD 2021-0287 includes Model MBB-BK 117 D-3 helicopters in the
applicability, whereas this AD does not. This AD requires renumbering
certain figures in SB-EC1-010, Rev A, for the purposes of this AD,
whereas EASA AD 2021-0287 does not. Where the service information
referenced in EASA AD 2021-0287 specifies to contact ``MAG DOA
(<a href="/cdn-cgi/l/email-protection#ff9c9e88bf929a9c9e9a8dd19c9092"><span class="__cf_email__" data-cfemail="b0d3d1c7f0ddd5d3d1d5c29ed3dfdd">[email protected]</span></a>) to receive instructions,'' this AD requires repair
done in accordance with certain approved methods instead.
Where the service information referenced in EASA AD 2021-0287
specifies, ``17. Make available items C (q.ty 2) and D (q.ty 2) (ref.
Figure 18), for each affected seat,'' this AD requires installing new
(zero total hours time-in-service) nuts and hex head screws (bolts).
Lastly, the service information referenced in EASA AD 2021-0287
specifies to submit certain information to the manufacturer; this AD
does not include that requirement.
Justification for Immediate Adoption and Determination of the Effective
Date
Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5
U.S.C. 551 et seq.) authorizes agencies to dispense with notice and
comment procedures for rules when the agency, for ``good cause,'' finds
that those procedures are ``impracticable, unnecessary, or contrary to
the public interest.'' Under this section, an agency, upon finding good
cause, may issue a final rule without providing notice and seeking
comment prior to issuance. Further, section 553(d) of the APA
authorizes agencies to make rules effective in less than thirty days,
upon a finding of good cause.
An unsafe condition exists that requires the immediate adoption of
this AD without providing an opportunity for public comments prior to
adoption. The FAA has found that the risk to the flying public
justifies foregoing notice and comment prior to adoption of this rule
because seat belt restraint systems are critical for flight crew and
occupant safety. The improper installation of the seat belt restraint
system, if not corrected, could result in serious injury to the seat
occupant during various operations including inclement weather,
autorotations, hard landings, and emergency or forced landings. In
light of this, the required actions of this AD must be accomplished
within 3 months or 50 hours time-in-service, whichever occurs first.
This is a short compliance time for these high usage helicopters, some
of which could reach these hours within 60 calendar days. Therefore,
the compliance time for the required actions is shorter than the time
necessary for the public to comment and for publication of the final
rule. Accordingly, notice and opportunity for prior public comment are
impracticable and contrary to the public interest pursuant to 5 U.S.C.
553(b)(3)(B).
In addition, the FAA finds that good cause exists pursuant to 5
U.S.C. 553(d) for making this amendment effective in less than 30 days,
for the same reasons the FAA found good cause to forego notice and
comment.
Comments Invited
The FAA invites you to send any written data, views, or arguments
about this final rule. Send your comments to an address listed under
ADDRESSES. Include ``Docket No. FAA-2022-0278; Project Identifier MCAI-
2021-01437-R'' at the beginning of your comments. The most helpful
comments reference a specific portion of the final rule, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this final rule because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
<a href="https://www.regulations.gov">https://www.regulations.gov</a>, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact received about this final rule.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this AD contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this AD, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket
[[Page 14387]]
of this AD. Submissions containing CBI should be sent to Antariksh
Shetty, Aerospace Engineer, Airframe & Propulsion Section, New York ACO
Branch, Compliance & Airworthiness Division, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone (516) 228-7300; email <a href="/cdn-cgi/l/email-protection#c4fde9a5b2b7e9aabda5a7abe9a7abb784a2a5a5eaa3abb2"><span class="__cf_email__" data-cfemail="95acb8f4e3e6b8fbecf4f6fab8f6fae6d5f3f4f4bbf2fae3">[email protected]</span></a>. Any commentary that the FAA receives that is not
specifically designated as CBI will be placed in the public docket for
this rulemaking.
Regulatory Flexibility Act
The requirements of the Regulatory Flexibility Act (RFA) do not
apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt
a rule without prior notice and comment. Because the FAA has determined
that it has good cause to adopt this rule without prior notice and
comment, RFA analysis is not required.
Costs of Compliance
The FAA estimates that this AD affects 3 helicopters of U.S.
Registry. Labor rates are estimated at $85 per work-hour. Based on
these numbers, the FAA estimates the following costs to comply with
this AD.
Inspecting the seat belt restraint system for a cabin seat takes up
to 1 work-hour for an estimated cost of up to $85 per cabin seat and up
to $2,040 for the U.S. fleet.
If required, reworking the seat belt restraint system for a cabin
seat takes up to 1 work-hour and parts cost up to $95 for an estimated
cost of up to $180 per cabin seat and up to $4,320 for the U.S. fleet.
Inspecting the seat belt restraint system for a pilot/co-pilot seat
takes up to 2 work-hours for an estimated cost of up to $170 per pilot/
co-pilot seat and up to $1,020 for the U.S. fleet.
If required, reworking the seat belt restraint system for a pilot/
co-pilot seat takes up to 2 work-hours with a negligible parts cost for
an estimated cost of up to $170 per pilot/co-pilot seat and up to
$1,020 for the U.S. fleet. The FAA has no way of determining the costs
pertaining to any necessary repairs that are required to be done with
an approved method.
The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some of the costs of this AD
may be covered under warranty, thereby reducing the cost impact on
affected operators.
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, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866, and
(2) Will not affect intrastate aviation in Alaska
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:
AD 2022-06-13 Airbus Helicopters Deutschland GmbH (AHD): Amendment
39-21979; Docket No. FAA-2022-0278; Project Identifier MCAI-2021-
01437-R.
(a) Effective Date
This airworthiness directive (AD) is effective March 30, 2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Helicopters Deutschland GmbH (AHD)
Model MBB-BK 117 C-2 and MBB-BK 117 D-2 helicopters, certificated in
any category, modified by Supplemental Type Certificate (STC)
SR03130NY, or STC SR03703NY.
(d) Subject
Joint Aircraft Service Component (JASC) Code: 2500, Cabin
Equipment/Furnishings.
(e) Unsafe Condition
This AD was prompted by a report of erroneous or partial
installation of the seat belt restraint system. The FAA is issuing
this AD to ensure proper installation of the seat belt restraint
system. The unsafe condition, if not addressed, could prevent proper
operation of the seat belt restraint system, resulting in subsequent
injury to the seat occupant.
(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, European Union Aviation Safety Agency (EASA) AD
2021-0287, dated December 21, 2021, and corrected January 26, 2022
(EASA AD 2021-0287).
(h) Exceptions to EASA AD 2021-0287
(1) Where EASA AD 2021-0287 requires compliance in terms of
flight hours, this AD requires using hours time-in-service (TIS).
(2) Where EASA AD 2021-0287 refers to its effective date, this
AD requires using the effective date of this AD.
(3) Where paragraph (1) of EASA AD 2021-0287 specifies to
``inspect each affected part in accordance with the instructions of
the SB,'' this AD requires inspecting each affected part by
following the procedures in Mecaer Aviation Group Mandatory Service
Bulletin No. SB-EC1-010, Revision A, dated December 30, 2021 (SB-
EC1-010, Rev A). Except for the purposes of this AD, consider Figure
16 on page 16 of SB-EC1-010, Rev A, as Figure 18 and consider
Figures 17 and 18 on page 17 of SB-EC1-010, Rev A, as Figures 19 and
20, respectively.
Note 1 to paragraph (h)(3): SB-EC1-010, Rev A refers to a
passenger seat as a passenger seat and passenger cabin seat; a seat
belt as a seat belt and safety belt; and a bolt as a hex head screw
and hex head bolt.
(4) Where the service information referenced in paragraph (2) of
EASA AD 2021-0287 specifies to ``contact MAG to receive missing
parts/materials, if any,'' this AD requires replacing the missing
parts and materials but does not require contacting MAG to receive
the missing parts or materials.
(5) Where the service information referenced in paragraph (2) of
EASA AD 2021-0287 specifies contacting ``MAG DOA (<a href="/cdn-cgi/l/email-protection#04676573446961676561762a676b69"><span class="__cf_email__" data-cfemail="accfcddbecc1c9cfcdc9de82cfc3c1">[email protected]</span></a>) to
receive instructions,''
[[Page 14388]]
this AD requires repair done in accordance with a method approved by
the Manager, General Aviation & Rotorcraft Section, International
Validation Branch, FAA; or EASA; or Airbus Helicopters' EASA Design
Organization Approval (DOA). If approved by the DOA, the approval
must include the DOA-authorized signature.
(6) Where the service information referenced in paragraph (2) of
EASA AD 2021-0287 specifies, ``17. Make available items C (q.ty 2)
and D (q.ty 2) (ref. Figure 18), for each affected seat,'' this AD
requires installing new (zero total hours TIS) nuts and hex head
screws.
(7) This AD does not mandate compliance with the ``Remarks''
section of EASA AD 2021-0287.
(i) No Reporting Requirement
Although the service information referenced in EASA AD 2021-0287
specifies to submit certain information to the manufacturer, this AD
does not include that requirement.
(j) Alternative Methods of Compliance (AMOCs)
(1) The Manager, International Validation 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 local Flight
Standards District Office, as appropriate. If sending information
directly to the manager of the International Validation Branch, send
it to the attention of the person identified in paragraph (k) of
this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#88b1a5c9dedba5c9c1daa5bfbbb8a5c9c5c7cbc8eee9e9a6efe7fe"><span class="__cf_email__" data-cfemail="0e37234f585d234f475c23393d3e234f43414d4e686f6f20696178">[email protected]</span></a>.
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(k) Related Information
For more information about this AD, contact Antariksh Shetty,
Aerospace Engineer, Airframe & Propulsion Section, New York ACO
Branch, Compliance & Airworthiness Division, FAA, 1600 Stewart
Avenue, Suite 410, Westbury, NY 11590; telephone (516) 228-7300;
email <a href="/cdn-cgi/l/email-protection#7e47531f080d5310071f1d11531d110d3e181f1f50191108"><span class="__cf_email__" data-cfemail="e5dcc8849396c88b9c84868ac8868a96a5838484cb828a93">[email protected]</span></a>.
(l) 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 the AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) AD 2021-0287,
dated December 21, 2021, and corrected January 26, 2022.
(ii) Mecaer Aviation Group Mandatory Service Bulletin No. SB-
EC1-010, Revision A, dated December 30, 2021.
(3) For EASA AD 2021-0287, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#0f4e4b7c4f6a6e7c6e216a7a7d607f6e216a7a"><span class="__cf_email__" data-cfemail="3071744370555143511e5545425f40511e5545">[email protected]</span></a>; internet www.easa.europa.eu. You may find the
EASA material on the EASA website at <a href="https://ad.easa.europa.eu">https://ad.easa.europa.eu</a>. For
Mecaer Aviation Group service information identified in this AD,
contact Mecaer Aviation Group (MAG), Via dell'Artigianato 1,
Monteprandone 63076 Ascoli Piceno, Italy; telephone (+39) 0735-7091;
email <a href="/cdn-cgi/l/email-protection#4e2d2f390e232b2d2f2b3c602d2123"><span class="__cf_email__" data-cfemail="17747660577a72747672653974787a">[email protected]</span></a>; or at <a href="http://www.mecaer.com">www.mecaer.com</a>.
(4) You may view this service information at the FAA, Office of
the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room
6N-321, Fort Worth, TX 76177. For information on the availability of
this material at the FAA, call (817) 222-5110.
(5) 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#93f5e1bdfafde0e3f6f0e7fafcfdd3fdf2e1f2bdf4fce5"><span class="__cf_email__" data-cfemail="ef899dc186819c9f8a8c9b868081af818e9d8ec1888099">[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 March 10, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2022-05525 Filed 3-11-22; 4:15 pm]
BILLING CODE 4910-13-P
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