83 FR 49791 - Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 83, Issue 192 (October 3, 2018)

Page Range		49791-49793
FR Document		2018-21342

We are adopting a new airworthiness directive (AD) for Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model MBB-BK 117 C-2 and MBB-BK 117 D-2 helicopters. This AD requires altering and re- identifying the overhead panel shock mount assembly (shock mount). This AD was prompted by the manufacturer's stress recalculations. The actions of this AD are intended to correct an unsafe condition on these products.

Federal Register, Volume 83 Issue 192 (Wednesday, October 3, 2018)

[Federal Register Volume 83, Number 192 (Wednesday, October 3, 2018)]
[Rules and Regulations]
[Pages 49791-49793]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2018-21342]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0517; Product Identifier 2017-SW-098-AD; Amendment 
39-19443; AD 2018-20-09]
RIN 2120-AA64


Airworthiness Directives; Airbus Helicopters Deutschland GmbH 
Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for Airbus 
Helicopters Deutschland GmbH (Airbus Helicopters) Model MBB-BK 117 C-2 
and MBB-BK 117 D-2 helicopters. This AD requires altering and re-
identifying the overhead panel shock mount assembly (shock mount). This 
AD was prompted by the manufacturer's stress recalculations. The 
actions of this AD are intended to correct an unsafe condition on these 
products.

DATES: This AD is effective November 7, 2018.
    The Director of the Federal Register approved the incorporation by 
reference of certain documents listed in this AD as of November 7, 
2018.

ADDRESSES: For service information identified in this final rule, 
contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 
75052; telephone (972) 641-0000 or (800) 232-0323; fax (972) 641-3775; 
or at http://www.helicopters.airbus.com/website/en/ref/Technical-Support_73.html. You may review the referenced service information at 
the FAA, Office of the Regional Counsel, Southwest Region, 10101 
Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. It is also available 
on the internet at http://www.regulations.gov by searching for and 
locating Docket No. FAA-2018-0517.

Examining the AD Docket

    You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0517; 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 AD, the European Aviation Safety Agency (EASA) AD, any 
incorporated-by-reference service information, the economic evaluation, 
any comments received, and other information. The street address for 
Docket Operations (phone: 800-647-5527) 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: Matt Fuller, Senior Aviation Safety 
Engineer, Safety Management Section, Rotorcraft Standards Branch, FAA, 
10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222-5110; 
email [email protected].

SUPPLEMENTARY INFORMATION:

Discussion

    On June 7, 2018, at 83 FR 26387, the Federal Register published our 
notice of proposed rulemaking (NPRM), which proposed to amend 14 CFR 
part 39 by adding an AD that would apply to Airbus Helicopters Model 
MBB-BK 117 C-2 and Model MBB-BK 117 D-2 helicopters with an overhead 
panel shock mount assembly part number (P/N) B246M2035102 or P/N 
B246M2036101 installed. The NPRM proposed to require installing a 
retaining plate on the shock mount and re-identifying the shock mount 
by changing the last three digits of the P/N to -966. The NPRM also 
proposed prohibiting the installation of shock

[[Page 49792]]

mount P/N B246M2035102 and P/N B246M2036101 on any helicopter. The 
proposed requirements were intended to prevent failure of a shock 
mount, which could result in detachment of the overhead panel and 
injury to occupants during an emergency landing.
    The NPRM was prompted by AD No. 2017-0026, dated February 14, 2017, 
issued by EASA, which is the Technical Agent for the Member States of 
the European Union, to correct an unsafe condition for Airbus 
Helicopters Model MBB-BK 117 C-2, MBB-BK117 C-2e, MBB-BK 117 D-2, and 
MBB-BK117 D-2m helicopters. EASA advises that a recent stress 
calculation identified that the shock mount may not withstand 
certification crash loads. EASA states that this condition, if not 
corrected, could lead to the overhead panel disconnecting during an 
emergency landing and injuring occupants. Accordingly, the EASA AD 
requires modifying and re-identifying the shock mounts.

Comments

    We gave the public the opportunity to participate in developing 
this AD, but we did not receive any comments on the NPRM.

FAA's Determination

    These helicopters have been approved by the aviation authority of 
Germany and are approved for operation in the United States. Pursuant 
to our bilateral agreement with Germany, EASA, its technical 
representative, has notified us of the unsafe condition described in 
the EASA AD. We are issuing this AD because we evaluated all 
information provided by EASA and determined the unsafe condition exists 
and is likely to exist or develop on other helicopters of these same 
type designs and that air safety and the public interest require 
adopting the AD requirements as proposed.

Differences Between This AD and the EASA AD

    The EASA AD applies to Model MBB-BK117 D-2m helicopters, whereas 
this AD does not since the Model MBB-BK117 D-2m is not FAA type-
certificated. This AD also does not include the Model MBB-BK117 C-2(e) 
in the applicability section because it is a marketing designation and 
not an FAA type-certificated model. However, this AD applies to those 
helicopters, as they are Model MBB-BK117 C-2 helicopters. The EASA AD 
specifies particular helicopter serial numbers (S/Ns) that may not be 
required to complete some of the requirements of the AD since the 
specified S/Ns were manufactured with shock mounts not affected by the 
unsafe condition. This AD does not specify particular S/Ns.

Related Service Information Under 1 CFR Part 51

    Airbus Helicopters has issued Alert Service Bulletin (ASB) MBB-
BK117 C-2-24A-015 for Model MBB-BK117 C-2 helicopters and ASB MBB-BK117 
D-2-24A-004 for Model MBB-BK117 D-2 helicopters, both Revision 0 and 
dated September 14, 2016. This service information contains procedures 
for altering the shock mounts by installing retaining plates and re-
identifying the shock mounts by changing the last three digits of the 
P/N to -966.
    This service information 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

    We estimate that this AD affects 144 helicopters of U.S. Registry. 
We estimate that operators may incur the following costs in order to 
comply with this AD. Labor costs are estimated at $85 per work-hour.
    Installing retaining plates and re-identifying the four shock 
mounts takes about 3 work-hours and parts cost about $184 for a total 
estimated cost of $439 per helicopter and $63,216 for the U.S. fleet.
    According to Airbus Helicopter's service information, some of the 
costs of this AD may be covered under warranty, thereby reducing the 
cost impact on affected individuals. We do not control warranty 
coverage by Airbus Helicopters. Accordingly, we have included all costs 
in our 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.
    We are 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 helicopters 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) Is not a ``significant rule'' under DOT Regulatory Policies and 
Procedures (44 FR 11034, February 26, 1979);
    (3) Will not affect intrastate aviation in Alaska to the extent 
that it justifies making a regulatory distinction; and
    (4) 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.
    We prepared an economic evaluation of the estimated costs to comply 
with this AD and placed it in the AD docket.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of 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):

2018-20-09 Airbus Helicopters Deutschland GmbH: Amendment 39-19443; 
Docket No. FAA-2018-0517; Product Identifier 2017-SW-098-AD.

(a) Applicability

    This AD applies to Model MBB-BK 117 C-2 and Model MBB-BK 117 D-2 
helicopters, certificated in any category, with an overhead panel 
shock mount assembly part number (P/N) B246M2035102 or P/N 
B246M2036101 installed.

    Note 1 to paragraph (a) of this AD: Helicopters with an MBB-
BK117 C-2e designation are Model MBB-BK117 C-2 helicopters.


[[Page 49793]]



(b) Unsafe Condition

    This AD defines the unsafe condition as failure of an overhead 
panel shock mount assembly (shock mount). This condition could 
result in detachment of the overhead panel and injury to occupants 
during an emergency landing.

(c) Effective Date

    This AD becomes effective November 7, 2018.

(d) Compliance

    You are responsible for performing each action required by this 
AD within the specified compliance time unless it has already been 
accomplished prior to that time.

(e) Required Actions

    (1) Within 300 hours time-in-service:
    (i) Install a retaining plate on each shock mount by following 
the Accomplishment Instructions, paragraphs 3.B.2.1. through 
3.B.2.4, of Airbus Helicopters Alert Service Bulletin (ASB) MBB-
BK117 C-2-24A-015, Revision 0, dated September 14, 2016 (ASB MBB-
BK117 C-2-24A-015), or ASB MBB-BK117 D-2-24A-004, Revision 0, dated 
September 14, 2016 (ASB MBB-BK117 D-2-24A-004), as applicable to 
your model helicopter.
    (ii) Re-identify shock mount P/N B246M2035102 as P/N 
B246M2035966 and shock mount P/N B246M2036101 as P/N B246M2036966 
using permanent ink. When the ink is dry, apply varnish over the P/
N.
    (iii) Re-install each shock mount.
    (2) After the effective date of this AD, do not install a shock 
mount P/N B246M2035102 or P/N B246M2036101 on any helicopter.

(f) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Safety Management Section, Rotorcraft Standards 
Branch, FAA, may approve AMOCs for this AD. Send your proposal to: 
Matt Fuller, Senior Aviation Safety Engineer, Safety Management 
Section, Rotorcraft Standards Branch, FAA, 10101 Hillwood Pkwy., 
Fort Worth, TX 76177; telephone (817) 222-5110; email [email protected].
    (2) For operations conducted under a 14 CFR part 119 operating 
certificate or under 14 CFR part 91, subpart K, we suggest that you 
notify your principal inspector, or lacking a principal inspector, 
the manager of the local flight standards district office or 
certificate holding district office, before operating any aircraft 
complying with this AD through an AMOC.

(g) Additional Information

    The subject of this AD is addressed in European Aviation Safety 
Agency (EASA) AD No. 2017-0026, dated February 14, 2017. You may 
view the EASA AD on the internet at http://www.regulations.gov in 
Docket No. FAA-2018-0517.

(h) Subject

    Joint Aircraft Service Component (JASC) Code: 2400, Electrical 
Power System.

(i) 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) Airbus Helicopters Alert Service Bulletin (ASB) MBB-BK117 C-
2-24A-015, Revision 0, dated September 14, 2016.
    (ii) Airbus Helicopters ASB MBB-BK117 D-2-24A-004, Revision 0, 
dated September 14, 2016.
    (3) For Airbus Helicopters service information identified in 
this AD, contact Airbus Helicopters, 2701 N Forum Drive, Grand 
Prairie, TX 75052; telephone (972) 641-0000 or (800) 232-0323; fax 
(972) 641-3775; or at http://www.helicopters.airbus.com/website/en/ref/Technical-Support_73.html.
    (4) You may view this service information at 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, call (202) 741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Fort Worth, Texas, on September 24, 2018.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification 
Service.
[FR Doc. 2018-21342 Filed 10-2-18; 8:45 am]
BILLING CODE 4910-13-P

Federal Register / Vol. 83, No. 192 / Wednesday, October 3, 2018 / Rules and Regulations 49791

(h) No Alternative Actions or Intervals paragraph under 5 U.S.C. 552(a) and 1 CFR of certain documents listed in this AD
After the maintenance or inspection part 51. as of November 7, 2018.
program has been revised as required by (2) You must use this service information
ADDRESSES: For service information
paragraph (g) of this AD, no alternative as applicable to do the actions required by
this AD, unless this AD specifies otherwise. identified in this final rule, contact
actions (e.g., inspections) or intervals may be
(i) Chapter 5–40, Airworthiness Airbus Helicopters, 2701 N Forum
used unless the actions or intervals are
approved as an alternative method of Limitations, DGT 113872, Revision 24, dated Drive, Grand Prairie, TX 75052;
compliance (AMOC) in accordance with the July 2017, of the Dassault Falcon 50/50EX telephone (972) 641–0000 or (800) 232–
procedures specified in paragraph (j)(1) of Maintenance Manual. 0323; fax (972) 641–3775; or at http://
this AD. (ii) Reserved. www.helicopters.airbus.com/website/
(3) For service information identified in
(i) Terminating Actions for Other ADs this AD, contact Dassault Falcon Jet
en/ref/Technical-Support_73.html. You
Corporation, Teterboro Airport, P.O. Box may review the referenced service
(1) Accomplishing the actions required by information at the FAA, Office of the
paragraph (g) of this AD terminates all 2000, South Hackensack, NJ 07606;
requirements of AD 2017–09–03. telephone 201–440–6700; internet http:// Regional Counsel, Southwest Region,
(2) Accomplishing the actions required by www.dassaultfalcon.com. 10101 Hillwood Pkwy., Room 6N–321,
(4) You may view this service information Fort Worth, TX 76177. It is also
paragraph (g) of this AD terminates all
at the FAA, Transport Standards Branch, available on the internet at http://
requirements of AD 2010–26–05 and AD
2200 South 216th St., Des Moines, WA. For
2012–02–18 for the Dassault Aviation Model www.regulations.gov by searching for
information on the availability of this
MYSTERE-FALCON 50 airplanes specified in
material at the FAA, call 206–231–3195. and locating Docket No. FAA–2018–
those ADs. (5) You may view this service information 0517.
(j) Other FAA AD Provisions that is incorporated by reference at the
Examining the AD Docket
National Archives and Records
The following provisions also apply to this
Administration (NARA). For information on You may examine the AD docket on
AD:
the availability of this material at NARA, call the internet at http://
(1) Alternative Methods of Compliance 202–741–6030, or go to: http://
(AMOCs): The Manager, International www.regulations.gov by searching for
www.archives.gov/federal-register/cfr/ibr- and locating Docket No. FAA–2018–
Section, Transport Standards Branch, FAA, locations.html.
has the authority to approve AMOCs for this 0517; or in person at Docket Operations
AD, if requested using the procedures found Issued in Des Moines, Washington, on between 9 a.m. and 5 p.m., Monday
in 14 CFR 39.19. In accordance with 14 CFR September 21, 2018. through Friday, except Federal holidays.
39.19, send your request to your principal John P. Piccola, The AD docket contains this AD, the
inspector or local Flight Standards District Acting Director, System Oversight Division, European Aviation Safety Agency
Office, as appropriate. If sending information Aircraft Certification Service. (EASA) AD, any incorporated-by-
directly to the International Section, send it [FR Doc. 2018–21343 Filed 10–2–18; 8:45 am]
to the attention of the person identified in reference service information, the
paragraph (k)(2) of this AD. Information may BILLING CODE 4910–13–P economic evaluation, any comments
be emailed to: 9-ANM-116-AMOC- received, and other information. The
REQUESTS@faa.gov. Before using any street address for Docket Operations
approved AMOC, notify your appropriate DEPARTMENT OF TRANSPORTATION (phone: 800–647–5527) is U.S.
principal inspector, or lacking a principal Department of Transportation, Docket
inspector, the manager of the local flight Federal Aviation Administration
Operations, M–30, West Building
standards district office/certificate holding Ground Floor, Room W12–140, 1200
district office. 14 CFR Part 39
New Jersey Avenue SE, Washington, DC
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain corrective
[Docket No. FAA–2018–0517; Product 20590.
Identifier 2017–SW–098–AD; Amendment FOR FURTHER INFORMATION CONTACT: Matt
actions from a manufacturer, the action must
39–19443; AD 2018–20–09]
be accomplished using a method approved Fuller, Senior Aviation Safety Engineer,
by the Manager, International Section, RIN 2120–AA64 Safety Management Section, Rotorcraft
Transport Standards Branch, FAA; or the Standards Branch, FAA, 10101
European Aviation Safety Agency (EASA); or Airworthiness Directives; Airbus Hillwood Pkwy., Fort Worth, TX 76177;
Dassault Aviation’s EASA Design Helicopters Deutschland GmbH telephone (817) 222–5110; email
Organization Approval (DOA). If approved by Helicopters
the DOA, the approval must include the
matthew.fuller@faa.gov.
DOA-authorized signature. AGENCY: Federal Aviation SUPPLEMENTARY INFORMATION:
Administration (FAA), DOT. Discussion
(k) Related Information
ACTION: Final rule.
(1) Refer to Mandatory Continuing On June 7, 2018, at 83 FR 26387, the
Airworthiness Information (MCAI) EASA SUMMARY: We are adopting a new Federal Register published our notice of
Airworthiness Directive 2018–0026, dated airworthiness directive (AD) for Airbus proposed rulemaking (NPRM), which
January 30, 2018, for related information. Helicopters Deutschland GmbH (Airbus proposed to amend 14 CFR part 39 by
This MCAI may be found in the AD docket
on the internet at http://www.regulations.gov
Helicopters) Model MBB–BK 117 C–2 adding an AD that would apply to
by searching for and locating Docket No. and MBB–BK 117 D–2 helicopters. This Airbus Helicopters Model MBB–BK 117
FAA–2018–0394. AD requires altering and re-identifying C–2 and Model MBB–BK 117 D–2
(2) For more information about this AD, the overhead panel shock mount helicopters with an overhead panel
contact Tom Rodriguez, Aerospace Engineer, assembly (shock mount). This AD was shock mount assembly part number
International Section, Transport Standards prompted by the manufacturer’s stress (P/N) B246M2035102 or P/N
Branch, FAA, 2200 South 216th St., Des recalculations. The actions of this AD B246M2036101 installed. The NPRM
daltland on DSKBBV9HB2PROD with RULES

Moines, WA 98198; telephone and fax 206– are intended to correct an unsafe proposed to require installing a
231–3226. condition on these products. retaining plate on the shock mount and
(l) Material Incorporated by Reference DATES: This AD is effective November 7, re-identifying the shock mount by
(1) The Director of the Federal Register 2018. changing the last three digits of the P/
approved the incorporation by reference The Director of the Federal Register N to –966. The NPRM also proposed
(IBR) of the service information listed in this approved the incorporation by reference prohibiting the installation of shock

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49792 Federal Register / Vol. 83, No. 192 / Wednesday, October 3, 2018 / Rules and Regulations

mount P/N B246M2035102 and P/N shock mounts not affected by the unsafe helicopters identified in this rulemaking
B246M2036101 on any helicopter. The condition. This AD does not specify action.
proposed requirements were intended to particular S/Ns.
Regulatory Findings
prevent failure of a shock mount, which
Related Service Information Under 1 This AD will not have federalism
could result in detachment of the
CFR Part 51 implications under Executive Order
overhead panel and injury to occupants
during an emergency landing. Airbus Helicopters has issued Alert 13132. This AD will not have a
The NPRM was prompted by AD No. Service Bulletin (ASB) MBB–BK117 C– substantial direct effect on the States, on
2017–0026, dated February 14, 2017, 2–24A–015 for Model MBB–BK117 C–2 the relationship between the national
issued by EASA, which is the Technical helicopters and ASB MBB–BK117 D–2– government and the States, or on the
Agent for the Member States of the 24A–004 for Model MBB–BK117 D–2 distribution of power and
European Union, to correct an unsafe helicopters, both Revision 0 and dated responsibilities among the various
condition for Airbus Helicopters Model September 14, 2016. This service levels of government.
MBB–BK 117 C–2, MBB–BK117 C–2e, information contains procedures for For the reasons discussed above, I
MBB–BK 117 D–2, and MBB–BK117 D– altering the shock mounts by installing certify that this AD:
2m helicopters. EASA advises that a retaining plates and re-identifying the (1) Is not a ‘‘significant regulatory
recent stress calculation identified that shock mounts by changing the last three action’’ under Executive Order 12866;
the shock mount may not withstand digits of the P/N to –966. (2) Is not a ‘‘significant rule’’ under
certification crash loads. EASA states This service information is reasonably DOT Regulatory Policies and Procedures
that this condition, if not corrected, available because the interested parties (44 FR 11034, February 26, 1979);
could lead to the overhead panel have access to it through their normal (3) Will not affect intrastate aviation
disconnecting during an emergency course of business or by the means in Alaska to the extent that it justifies
landing and injuring occupants. identified in the ADDRESSES section. making a regulatory distinction; and
Accordingly, the EASA AD requires (4) Will not have a significant
modifying and re-identifying the shock Costs of Compliance economic impact, positive or negative,
mounts. We estimate that this AD affects 144 on a substantial number of small entities
helicopters of U.S. Registry. We estimate under the criteria of the Regulatory
Comments Flexibility Act.
that operators may incur the following
We gave the public the opportunity to costs in order to comply with this AD. We prepared an economic evaluation
participate in developing this AD, but Labor costs are estimated at $85 per of the estimated costs to comply with
we did not receive any comments on the work-hour. this AD and placed it in the AD docket.
NPRM.
Installing retaining plates and re- List of Subjects in 14 CFR Part 39
FAA’s Determination identifying the four shock mounts takes
Air transportation, Aircraft, Aviation
These helicopters have been approved about 3 work-hours and parts cost about
safety, Incorporation by reference,
by the aviation authority of Germany $184 for a total estimated cost of $439
Safety.
and are approved for operation in the per helicopter and $63,216 for the U.S.
United States. Pursuant to our bilateral fleet. Adoption of the Amendment
agreement with Germany, EASA, its According to Airbus Helicopter’s Accordingly, under the authority
technical representative, has notified us service information, some of the costs of delegated to me by the Administrator,
of the unsafe condition described in the this AD may be covered under warranty, the FAA amends 14 CFR part 39 as
EASA AD. We are issuing this AD thereby reducing the cost impact on follows:
because we evaluated all information affected individuals. We do not control
provided by EASA and determined the warranty coverage by Airbus PART 39—AIRWORTHINESS
unsafe condition exists and is likely to Helicopters. Accordingly, we have DIRECTIVES
exist or develop on other helicopters of included all costs in our cost estimate.
these same type designs and that air ■ 1. The authority citation for part 39
Authority for This Rulemaking continues to read as follows:
safety and the public interest require
adopting the AD requirements as Title 49 of the United States Code Authority: 49 U.S.C. 106(g), 40113, 44701.
proposed. specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I, § 39.13 [Amended]
Differences Between This AD and the section 106, describes the authority of ■ 2. The FAA amends § 39.13 by adding
EASA AD the FAA Administrator. Subtitle VII: the following new airworthiness
The EASA AD applies to Model Aviation Programs, describes in more directive (AD):
MBB–BK117 D–2m helicopters, whereas detail the scope of the Agency’s
2018–20–09 Airbus Helicopters
this AD does not since the Model MBB– authority. Deutschland GmbH: Amendment 39–
BK117 D–2m is not FAA type- We are issuing this rulemaking under 19443; Docket No. FAA–2018–0517;
certificated. This AD also does not the authority described in Subtitle VII, Product Identifier 2017–SW–098–AD.
include the Model MBB–BK117 C–2(e) Part A, Subpart III, Section 44701:
(a) Applicability
in the applicability section because it is ‘‘General requirements.’’ Under that
a marketing designation and not an FAA section, Congress charges the FAA with This AD applies to Model MBB–BK 117 C–
type-certificated model. However, this promoting safe flight of civil aircraft in 2 and Model MBB–BK 117 D–2 helicopters,
certificated in any category, with an overhead
AD applies to those helicopters, as they air commerce by prescribing regulations
daltland on DSKBBV9HB2PROD with RULES

panel shock mount assembly part number (P/
are Model MBB–BK117 C–2 helicopters. for practices, methods, and procedures N) B246M2035102 or P/N B246M2036101
The EASA AD specifies particular the Administrator finds necessary for installed.
helicopter serial numbers (S/Ns) that safety in air commerce. This regulation Note 1 to paragraph (a) of this AD:
may not be required to complete some is within the scope of that authority Helicopters with an MBB–BK117 C–2e
of the requirements of the AD since the because it addresses an unsafe condition designation are Model MBB–BK117 C–2
specified S/Ns were manufactured with that is likely to exist or develop on helicopters.

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Federal Register / Vol. 83, No. 192 / Wednesday, October 3, 2018 / Rules and Regulations 49793

(b) Unsafe Condition (i) Material Incorporated by Reference certain frame (FR) angle fitting. This AD
This AD defines the unsafe condition as (1) The Director of the Federal Register requires, depending on airplane
failure of an overhead panel shock mount approved the incorporation by reference of configuration, a modification of certain
assembly (shock mount). This condition the service information listed in this angle fitting attachment holes; repetitive
could result in detachment of the overhead paragraph under 5 U.S.C. 552(a) and 1 CFR inspections for cracking of certain holes
panel and injury to occupants during an part 51. of the internal lower angle fitting web,
emergency landing. (2) You must use this service information
certain holes of the internal lower angle
as applicable to do the actions required by
(c) Effective Date this AD, unless the AD specifies otherwise. fitting horizontal splicing, the aft bottom
This AD becomes effective November 7, (i) Airbus Helicopters Alert Service panel, and a certain junction area; and
2018. Bulletin (ASB) MBB–BK117 C–2–24A–015, related investigative and corrective
Revision 0, dated September 14, 2016. actions if necessary. We are issuing this
(d) Compliance (ii) Airbus Helicopters ASB MBB–BK117 AD to address the unsafe condition on
You are responsible for performing each D–2–24A–004, Revision 0, dated September these products.
action required by this AD within the 14, 2016.
DATES: This AD is effective November 7,
specified compliance time unless it has (3) For Airbus Helicopters service
information identified in this AD, contact 2018.
already been accomplished prior to that time. The Director of the Federal Register
Airbus Helicopters, 2701 N Forum Drive,
(e) Required Actions Grand Prairie, TX 75052; telephone (972) approved the incorporation by reference
(1) Within 300 hours time-in-service: 641–0000 or (800) 232–0323; fax (972) 641– of certain publications listed in this AD
(i) Install a retaining plate on each shock
3775; or at http:// as of November 7, 2018.
www.helicopters.airbus.com/website/en/ref/ The Director of the Federal Register
mount by following the Accomplishment
Technical-Support_73.html. approved the incorporation by reference
Instructions, paragraphs 3.B.2.1. through
(4) You may view this service information of a certain other publication listed in
3.B.2.4, of Airbus Helicopters Alert Service at FAA, Office of the Regional Counsel,
Bulletin (ASB) MBB–BK117 C–2–24A–015, this AD as of December 19, 2005 (70 FR
Southwest Region, 10101 Hillwood Pkwy.,
Revision 0, dated September 14, 2016 (ASB Room 6N–321, Fort Worth, TX 76177. For 69056, November 14, 2005).
MBB–BK117 C–2–24A–015), or ASB MBB– information on the availability of this ADDRESSES: For service information
BK117 D–2–24A–004, Revision 0, dated material at the FAA, call (817) 222–5110. identified in this final rule, contact
September 14, 2016 (ASB MBB–BK117 D–2– (5) You may view this service information Airbus SAS, Airworthiness Office—
24A–004), as applicable to your model that is incorporated by reference at the EAW, Rond-Point Emile Dewoitine No:
helicopter. National Archives and Records 2, 31700 Blagnac Cedex, France;
(ii) Re-identify shock mount P/N Administration (NARA). For information on telephone +33 5 61 93 36 96; fax +33 5
B246M2035102 as P/N B246M2035966 and the availability of this material at NARA, call
shock mount P/N B246M2036101 as P/N (202) 741–6030, or go to: http://
61 93 44 51; email account.airworth-
B246M2036966 using permanent ink. When www.archives.gov/federal-register/cfr/ibr- eas@airbus.com; internet http://
the ink is dry, apply varnish over the P/N. locations.html. www.airbus.com. You may view this
(iii) Re-install each shock mount. service information at the FAA,
Issued in Fort Worth, Texas, on September
(2) After the effective date of this AD, do 24, 2018.
Transport Standards Branch, 2200
not install a shock mount P/N South 216th St., Des Moines, WA. For
Lance T. Gant,
B246M2035102 or P/N B246M2036101 on information on the availability of this
any helicopter. Director, Compliance & Airworthiness material at the FAA, call 206–231–3195.
Division, Aircraft Certification Service.
(f) Alternative Methods of Compliance It is also available on the internet at
[FR Doc. 2018–21342 Filed 10–2–18; 8:45 am]
(AMOCs) http://www.regulations.gov by searching
BILLING CODE 4910–13–P
for and locating Docket No. FAA–2018–
(1) The Manager, Safety Management
Section, Rotorcraft Standards Branch, FAA,
0497.
may approve AMOCs for this AD. Send your DEPARTMENT OF TRANSPORTATION Examining the AD Docket
proposal to: Matt Fuller, Senior Aviation
Safety Engineer, Safety Management Section, You may examine the AD docket on
Federal Aviation Administration
Rotorcraft Standards Branch, FAA, 10101 the internet at http://
Hillwood Pkwy., Fort Worth, TX 76177; www.regulations.gov by searching for
14 CFR Part 39
telephone (817) 222–5110; email 9-ASW- and locating Docket No. FAA–2018–
FTW-AMOC-Requests@faa.gov. [Docket No. FAA–2018–0497; Product 0497; or in person at Docket Operations
(2) For operations conducted under a 14 Identifier 2017–NM–140–AD; Amendment between 9 a.m. and 5 p.m., Monday
CFR part 119 operating certificate or under 39–19418; AD 2018–19–18] through Friday, except Federal holidays.
14 CFR part 91, subpart K, we suggest that RIN 2120–AA64 The AD docket contains this final rule,
you notify your principal inspector, or the regulatory evaluation, any
lacking a principal inspector, the manager of Airworthiness Directives; Airbus SAS comments received, and other
the local flight standards district office or Airplanes information. The address for Docket
certificate holding district office, before Operations (phone: 800–647–5527) is
operating any aircraft complying with this AGENCY: Federal Aviation
U.S. Department of Transportation,
AD through an AMOC. Administration (FAA), Department of
Docket Operations, M–30, West
(g) Additional Information
Transportation (DOT).
Building Ground Floor, Room W12–140,
ACTION: Final rule.
The subject of this AD is addressed in 1200 New Jersey Avenue SE,
European Aviation Safety Agency (EASA) AD SUMMARY: We are adopting a new Washington, DC 20590.
No. 2017–0026, dated February 14, 2017. You airworthiness directive (AD) for certain FOR FURTHER INFORMATION CONTACT: Dan
daltland on DSKBBV9HB2PROD with RULES

may view the EASA AD on the internet at Airbus SAS Model A300 B4–603, B4– Rodina, Aerospace Engineer,
http://www.regulations.gov in Docket No. International Section, Transport
620, and B4–622 airplanes; Model A300
FAA–2018–0517.
B4–600R series airplanes; Model A300 Standards Branch, FAA, 2200 South
(h) Subject C4–605R Variant F airplanes; and Model 216th St., Des Moines, WA 98198;
Joint Aircraft Service Component (JASC) A300 F4–605R airplanes. This AD was telephone and fax 206–231–3225.
Code: 2400, Electrical Power System. prompted by reports of cracking on a SUPPLEMENTARY INFORMATION:

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Document Created: 2018-10-03 02:29:56
Document Modified: 2018-10-03 02:29:56

Category		Regulatory Information
Collection		Federal Register
sudoc Class		AE 2.7: GS 4.107: AE 2.106:
Publisher		Office of the Federal Register, National Archives and Records Administration
Section		Rules and Regulations
Action		Final rule.
Dates		This AD is effective November 7, 2018.
Contact		Matt Fuller, Senior Aviation Safety Engineer, Safety Management Section, Rotorcraft Standards Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222-5110; email [email protected]
FR Citation		83 FR 49791
RIN Number		2120-AA64
CFR Associated		Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

83 FR 49791 - Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

DEPARTMENT OF TRANSPORTATIONFederal Aviation Administration

Federal Register Volume 83, Issue 192 (October 3, 2018)

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration