Rule2021-12482
Airworthiness Directives; Airbus 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
June 15, 2021
Effective
July 20, 2021
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Model EC155B1 helicopters. This AD was prompted by a report of difficulties when jettisoning the co-pilot door during non-scheduled maintenance. This AD requires a functional check of the pilot and co-pilot door jettisoning system and corrective actions if necessary, as specified in a European 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 86 Issue 113 (Tuesday, June 15, 2021)</title>
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[Federal Register Volume 86, Number 113 (Tuesday, June 15, 2021)]
[Rules and Regulations]
[Pages 31609-31611]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2021-12482]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-0314; Project Identifier MCAI-2020-00599-R;
Amendment 39-21592; AD 2021-12-05]
RIN 2120-AA64
Airworthiness Directives; Airbus Helicopters
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 Helicopters Model EC155B1 helicopters. This AD was
prompted by a report of difficulties when jettisoning the co-pilot door
during non-scheduled maintenance. This AD requires a functional check
of the pilot and co-pilot door jettisoning system and corrective
actions if necessary, as specified in a European 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 is effective July 20, 2021.
[[Page 31610]]
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of July 20,
2021.
ADDRESSES: For material incorporated by reference (IBR) in this AD,
contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany;
telephone +49 221 8999 000; email <a href="/cdn-cgi/l/email-protection#59181d2a193c382a38773c2c2b362938773c2c"><span class="__cf_email__" data-cfemail="5f1e1b2c1f3a3e2c3e713a2a2d302f3e713a2a">[email protected]</span></a>; internet
www.easa.europa.eu. You may find this material on the EASA website at
<a href="https://ad.easa.europa.eu">https://ad.easa.europa.eu</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. 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-2021-0314.
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-
0314; 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: Kathleen Arrigotti, Program Manager,
Large Aircraft Section, International Validation Branch, Compliance &
Airworthiness Division, FAA, 2200 South 216th St., Des Moines, WA
98198; telephone and fax 206-231-3218; email
<a href="/cdn-cgi/l/email-protection#adc6ccd9c5c1c8c8c383ccdfdfc4cac2d9d9c4edcbcccc83cac2db"><span class="__cf_email__" data-cfemail="452e24312d2920202b6b2437372c222a31312c052324246b222a33">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
The EASA (now European Union Aviation Safety Agency), which is the
Technical Agent for the Member States of the European Union, has issued
EASA AD 2015-0157, dated July 30, 2015 (EASA AD 2015-0157) (also
referred to as the Mandatory Continuing Airworthiness Information, or
the MCAI), to correct an unsafe condition for Airbus Helicopters Model
EC 155 B1 helicopters, all serial numbers delivered after manufacturing
before June 30, 2015, and equipped with a pilot or co-pilot door
jettisoning system in accordance with Airbus Helicopters Modification
POST MOD 0752C05, except helicopters on which Aircraft Maintenance
Manual (AMM) Task 52-11-00-712 was accomplished on both pilot and co-
pilot doors since the last crew door installation.
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
Helicopters Model EC155B1 helicopters. The NPRM published in the
Federal Register on April 22, 2021 (86 FR 21240). The NPRM was prompted
by a report of difficulties when jettisoning the co-pilot door during
non-scheduled maintenance. The NPRM proposed to require a functional
check of the pilot and co-pilot door jettisoning system and corrective
actions if necessary, as specified in an EASA AD.
The FAA is issuing this AD to address jamming of the affected door
jettisoning mechanism, which could reduce the ability of the flightcrew
to evacuate in the event of an emergency situation. See the MCAI for
additional background information.
Discussion of Final Airworthiness Directive
Comments
The FAA gave the public the opportunity to participate in
developing this final rule. The FAA received no comments on the NPRM or
on the determination of the cost to the public.
Conclusion
The FAA reviewed the relevant data and determined that air safety
and the public interest require adopting this final rule as proposed,
except for minor editorial changes. The FAA has determined that these
minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM.
Related Service Information Under 1 CFR Part 51
EASA AD 2015-0157 specifies procedures for doing a functional check
of the pilot and co-pilot door jettisoning system and corrective
actions. The corrective actions include greasing the tenons and
restoring the jettison system. 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 14 helicopters of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
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Cost per Cost on U.S.
Labor cost Parts cost product operators
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8 work-hours x $85 per hour = $680........................... $0 $680 $9,520
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The FAA estimates the following costs to do any necessary on-
condition action that would be required based on the results of any
required actions. The FAA has no way of determining the number of
helicopters that might need this on-condition action:
Estimated Costs of On-Condition Actions
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Cost per
Labor cost Parts cost product
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1 work-hour x $85 per hour = $85.............................................. $0 $85
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[[Page 31611]]
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:
2021-12-05 Airbus Helicopters: Amendment 39-21592; Docket No. FAA-
2021-0314; Project Identifier MCAI-2020-00599-R.
(a) Effective Date
This airworthiness directive (AD) is effective July 20, 2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Helicopters Model EC155B1 helicopters,
certificated in any category, all serial numbers manufactured before
June 30, 2015, and equipped with a pilot or co-pilot door
jettisoning system in accordance with Airbus Helicopters
modification POST MOD 0752C05, except helicopters on which Aircraft
Maintenance Manual (AMM) task 52-11-00-712 was accomplished on both
pilot and co-pilot doors since the last crew door installation.
(d) Subject
Joint Aircraft System Component (JASC) Code 5210, Passenger/Crew
Doors.
(e) Reason
This AD was prompted by a report of difficulties when
jettisoning the co-pilot door during non-scheduled maintenance. The
FAA is issuing this AD to address jamming of the affected door
jettisoning mechanism, which could reduce the ability of the
flightcrew to evacuate in the event of an emergency situation.
(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 Aviation Safety Agency (now European Union
Aviation Safety Agency) (EASA) AD 2015-0157, dated July 30, 2015
(EASA AD 2015-0157).
(h) Exceptions to EASA AD 2015-0157
(1) Where EASA AD 2015-0157 refers to its effective date, this
AD requires using the effective date of this AD.
(2) The ``Remarks'' section of EASA AD 2015-0157 does not apply
to this AD.
(3) Where EASA AD 2015-0157 refers to flight hours (FH), this AD
requires using hours time-in-service.
(4) Where paragraph (2) of EASA AD 2015-0157 provides an option
to contact Airbus Helicopters for approved instructions and
accomplish those instructions, for this AD, the option is to repair
the jettison system in accordance with FAA-approved procedures.
(5) Where the service information referenced in EASA AD 2015-
0157 specifies to ``speak to Airbus Helicopters,'' this AD requires
repairing the jettison system in accordance with FAA-approved
procedures.
(6) Where the service information referenced in EASA AD 2015-
0157 specifies to discard certain parts, this AD requires removing
the parts from service instead.
(i) 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 (j) of
this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#d6effb978085fb979f84fbe1e5e6fb979b999596b0b7b7f8b1b9a0"><span class="__cf_email__" data-cfemail="fac3d7bbaca9d7bbb3a8d7cdc9cad7bbb7b5b9ba9c9b9bd49d958c">[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.
(j) Related Information
For more information about this AD, contact Kathleen Arrigotti,
Program Manager, Large Aircraft Section, International Validation
Branch, Compliance & Airworthiness Division, FAA, 2200 South 216th
St., Des Moines, WA 98198; telephone and fax 206-231-3218; email
<a href="/cdn-cgi/l/email-protection#4922283d21252c2c2767283b3b202e263d3d20092f2828672e263f"><span class="__cf_email__" data-cfemail="d8b3b9acb0b4bdbdb6f6b9aaaab1bfb7acacb198beb9b9f6bfb7ae">[email protected]</span></a>.
(k) 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.
(i) European Aviation Safety Agency (EASA) AD 2015-0157, dated
July 30, 2015.
(ii) [Reserved]
(3) For EASA AD 2015-0157, contact the EASA, Konrad-Adenauer-
Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#fabbbe89ba9f9b899bd49f8f88958a9bd49f8f"><span class="__cf_email__" data-cfemail="9bdadfe8dbfefae8fab5feeee9f4ebfab5feee">[email protected]</span></a>; Internet www.easa.europa.eu. You may find this
EASA AD on the EASA website at <a href="https://ad.easa.europa.eu">https://ad.easa.europa.eu</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. 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-
2021-0314.
(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#dabcbfbea8bfbdf4b6bfbdbbb69ab4bba8bbf4bdb5ac"><span class="__cf_email__" data-cfemail="224447465047450c4e4745434e624c4350430c454d54">[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 May 27, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2021-12482 Filed 6-14-21; 8:45 am]
BILLING CODE 4910-13-P
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