82_FR_57622 82 FR 57390 - Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

82 FR 57390 - Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 82, Issue 232 (December 5, 2017)

Page Range57390-57392
FR Document2017-26039

We propose to supersede Airworthiness Directive (AD) 2017-02- 07 for Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model MBB-BK 117 C-2 and Model MBB-BK 117 D-2 helicopters. AD 2017-02-07 currently requires a repetitive inspection and a one-time torque of each hydraulic module plate assembly attachment point (attachment point). Since we issued AD 2017-02-07, a terminating action has been developed to address the unsafe condition. This proposed AD would retain the initial inspection and torque requirements of AD 2017-02-07 and require replacing the attachment point hardware. The actions of this proposed AD are intended to prevent an unsafe condition on these products.

Federal Register, Volume 82 Issue 232 (Tuesday, December 5, 2017)
[Federal Register Volume 82, Number 232 (Tuesday, December 5, 2017)]
[Proposed Rules]
[Pages 57390-57392]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2017-26039]



[[Page 57390]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-1123; Product Identifier 2017-SW-013-AD]
RIN 2120-AA64


Airworthiness Directives; Airbus Helicopters Deutschland GmbH 
Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to supersede Airworthiness Directive (AD) 2017-02-
07 for Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model 
MBB-BK 117 C-2 and Model MBB-BK 117 D-2 helicopters. AD 2017-02-07 
currently requires a repetitive inspection and a one-time torque of 
each hydraulic module plate assembly attachment point (attachment 
point). Since we issued AD 2017-02-07, a terminating action has been 
developed to address the unsafe condition. This proposed AD would 
retain the initial inspection and torque requirements of AD 2017-02-07 
and require replacing the attachment point hardware. The actions of 
this proposed AD are intended to prevent an unsafe condition on these 
products.

DATES: We must receive comments on this proposed AD by February 5, 
2018.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Docket: Go to http://www.regulations.gov. Follow the online instructions for sending your 
comments electronically.
     Fax: 202-493-2251.
     Mail: Send comments to the U.S. Department of 
Transportation, Docket Operations, M-30, West Building Ground Floor, 
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590-0001.
     Hand Delivery: Deliver to the ``Mail'' address between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.

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-2017-
1123; or in person at the Docket Operations Office between 9 a.m. and 5 
p.m., Monday through Friday, except Federal holidays. The AD docket 
contains this proposed AD, the European Aviation Safety Agency (EASA) 
AD, the economic evaluation, any comments received and other 
information. The street address for the Docket Operations Office 
(telephone 800-647-5527) is in the ADDRESSES section. Comments will be 
available in the AD docket shortly after receipt.
    For service information identified in this proposed 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.airbushelicopters.com/techpub. You may review service 
information at the FAA, Office of the Regional Counsel, Southwest 
Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177.

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: 

Comments Invited

    We invite you to participate in this rulemaking by submitting 
written comments, data, or views. We also invite comments relating to 
the economic, environmental, energy, or federalism impacts that might 
result from adopting the proposals in this document. The most helpful 
comments reference a specific portion of the proposal, explain the 
reason for any recommended change, and include supporting data. To 
ensure the docket does not contain duplicate comments, commenters 
should send only one copy of written comments, or if comments are filed 
electronically, commenters should submit only one time.
    We will file in the docket all comments that we receive, as well as 
a report summarizing each substantive public contact with FAA personnel 
concerning this proposed rulemaking. Before acting on this proposal, we 
will consider all comments we receive on or before the closing date for 
comments. We will consider comments filed after the comment period has 
closed if it is possible to do so without incurring expense or delay. 
We may change this proposal in light of the comments we receive.

Discussion

    We issued AD 2017-02-07, Amendment 39-18786 (82 FR 10267, February 
10, 2017) (2017-02-07) for Airbus Helicopters Model MBB-BK 117 C-2 
helicopters, serial numbers up to and including 9750, and Model MBB-BK 
117 D-2 helicopters, serial numbers up to and including 20110, with a 
hydraulic module plate assembly part number B291M0003103 with a single 
locking attachment point installed. AD 2017-02-07 requires a repetitive 
inspection and a one-time torque of the attachment points. The actions 
in AD 2017-02-07 are intended to prevent failure of an attachment 
point, loss of the hydraulic module plate, and subsequent loss of 
control of the helicopter.
    EASA, which is the Technical Agent for the Member States of the 
European Union, issued EASA AD No. 2015-0210R1, Revision 1, dated 
October 28, 2015 (2015-0210R1), to correct an unsafe condition for 
Airbus Helicopters Model MBB-BK117 C-2, MBB-BK117 C-2e, MBB-BK117 D-2, 
and MBB-BK117 D-2m helicopters. EASA advised that the hydraulic plate 
assembly on certain MBB-BK117 models has four attachment points on the 
fuselage secured by a single locking mechanism. According to EASA, a 
design reassessment revealed stiffness of the hydraulic plate may be 
insufficient to withstand the in-service loads in the event one of the 
four single locking attachment points fails. EASA stated that if this 
condition is not detected and corrected, it may lead to loss of the 
hydraulic module plate and possible loss of control of the helicopter. 
Therefore, the EASA AD required a repetitive inspection and one-time 
torque tightening of the attachment points in accordance with Airbus 
Helicopters' service information.
    EASA considered its AD an interim action and stated further AD 
action may follow. EASA subsequently revised AD 2015-0210R1 and issued 
AD No. 2015-0210R2, dated December 2, 2016 (2015-0210R2), to exclude 
from the applicability helicopters with an improved double locking 
attachment mechanism that is not subject to the unsafe condition.

Actions Since AD 2017-02-07 Was Issued

    Since we issued AD 2017-02-07, Airbus Helicopters revised its 
service information to add procedures to modify single locking 
attachment mechanisms to double locking attachment mechanisms. EASA 
subsequently superseded AD 2015-0210R2 with AD No. 2017-0047, dated 
March 13, 2017, to require installation of double locking attachments.

FAA's Determination

    These helicopters have been approved by the aviation authority of 
Germany

[[Page 57391]]

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 its AD. We are 
proposing this AD because we evaluated all known relevant information 
and determined that an unsafe condition is likely to exist or develop 
on other products of the same type design.

Related Service Information Under 1 CFR Part 51

    We reviewed Airbus Helicopters Alert Service Bulletin (ASB) No. ASB 
MBB-BK117 C-2-29A-003 for Model MBB-BK 117 C-2 helicopters and ASB No. 
ASB MBB-BK117 D-2-29A-001 for Model MBB-BK 117 D-2 helicopters, both 
Revision 2 and both dated February 1, 2017. Until the attachment points 
are modified with double locking attachment mechanisms, this service 
information specifies a repetitive visual inspection for condition and 
correct installation of the attachment points and replacing the 
affected parts if there is a crack. This service information also 
specifies a tightening torque check after the initial inspection and 
replacing the affected parts if torque cannot be applied. This revision 
of the service information also specifies procedures to replace the 
single locking attachment hardware with double locking attachment 
hardware.
    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.

Other Related Service Information

    We also reviewed Airbus Helicopters ASB No. ASB MBB-BK117 C-2-29A-
003 for Model MBB-BK 117 C-2 helicopters and ASB No. ASB MBB-BK117 D-2-
29A-001 for Model MBB-BK 117 D-2 helicopters, both Revision 1 and both 
dated October 14, 2016. Revision 1 of this service information contains 
the same visual inspection and torque tightening check procedures as 
Revision 2. However, Revision 2 of this service information adds the 
procedures to replace the single locking attachment hardware with 
double locking attachment hardware.

Proposed AD Requirements

    This proposed AD would require, within 100 hours time-in-service 
(TIS), unless already done within the last 100 hours TIS, performing a 
visual inspection of each attachment point of the hydraulic module 
plate assembly for a crack and proper installation, and applying torque 
to the nuts of each attachment point. This proposed AD would also 
require, within 300 hours TIS, replacing each single locking attachment 
point mechanism with a double locking attachment point mechanism.

Differences Between This Proposed AD and the EASA AD

    The EASA AD specifies performing the visual inspection of each 
attachment point at intervals not exceeding 400 flight hours. This 
proposed AD would not require a repetitive inspection. This proposed AD 
would require the replacement of each single locking attachment point 
mechanism with a double locking attachment point mechanism within 300 
hours TIS instead, which would make subsequent inspections unnecessary.

Costs of Compliance

    We estimate that this proposed AD would affect 134 helicopters of 
U.S. Registry. We estimate that operators may incur the following costs 
in order to comply with this AD. We estimate the cost of labor at $85 
per work-hour. Visually inspecting the four attachment points would 
take about 0.75 work-hour for an estimated cost of $64 per helicopter 
and $8,576 for the U.S. fleet. Inspecting the torque of the four 
attachment points would take about 0.25 work-hour for an estimated cost 
of $21 per helicopter and $2,814 for the U.S. fleet. Replacing any of 
the attachment point parts would take a minimal amount of time and 
parts would cost about $48 per attachment point. Installing four double 
locking attachment point mechanisms would take a minimal amount of time 
and parts would cost about $400 per helicopter and $53,600 for the U.S. 
fleet.
    According to Airbus Helicopters service information, some of the 
costs of this proposed 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 products identified in this 
rulemaking action.

Regulatory Findings

    We determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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 this proposed regulation:
    1. Is not a ``significant regulatory action'' under Executive Order 
12866;
    2. Is not a ``significant rule'' under the 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 proposed 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.

The Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 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 removing Airworthiness Directive (AD) 
2017-02-07, Amendment 39-18786 (82 FR 10267, February 10, 2017), and 
adding the following new AD:

Airbus Helicopters Deutschland GmbH: Docket No. FAA-2017-1123; 
Product Identifier 2017-SW-013-AD.

[[Page 57392]]

(a) Applicability

    This AD applies to Model MBB-BK 117 C-2 helicopters, serial 
numbers up to and including 9750, and Model MBB-BK 117 D-2 
helicopters, serial numbers up to and including 20110, with a 
hydraulic module plate assembly part number B291M0003103 with a 
single locking attachment point installed, certificated in any 
category.

(b) Unsafe Condition

    This AD defines the unsafe condition as failure of a hydraulic 
module plate assembly attachment point (attachment point). This 
condition could result in loss of the hydraulic module plate and 
subsequent loss of control of the helicopter.

(c) Affected ADs

    This AD supersedes 2017-02-07, Amendment 39-18786 (82 FR 10267, 
February 10, 2017).

(d) Comments Due Date

    We must receive comments by February 5, 2018.

(e) 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.

(f) Required Actions

    (1) Within 100 hours time-in-service (TIS):
    (i) Visually inspect the split pins, castellated nuts, plugs, 
nuts, and hexagon bolts of each attachment point for a crack and for 
proper installation by following the Accomplishment Instructions, 
paragraphs 3.B.1.3.a. through 3.B.1.3.d., of Airbus Helicopters 
Alert Service Bulletin (ASB) No. ASB MBB-BK117 C-2-29A-003 (ASB MBB-
BK117 C-2-29A-003) or Airbus Helicopters ASB No. ASB MBB-BK117 D-2-
29A-001 (ASB MBB-BK117 D-2-29A-001), both Revision 2 and both dated 
February 1, 2017, as applicable to your model helicopter. Replace 
any part that has a crack before further flight. If the split pins, 
castellated nuts, or hexagon bolts are not as depicted in Figure 2 
of ASB MBB-BK117 C-2-29A-003 or ASB MBB-BK117 D-2-29A-001, before 
further flight, properly install them.
    (ii) Apply a torque of 9 to 10 Nm to the left-hand and right-
hand nuts of each attachment point. If a torque of 9 to 10 Nm cannot 
be applied, replace the affected nut before further flight.
    (2) Within 300 hours TIS:
    (i) Replace each forward single locking attachment hardware with 
double locking attachment hardware by following the Accomplishment 
Instructions, paragraphs 3.B.3.3. through 3.B.3.6. on page 11 of ASB 
MBB-BK117 C-2-29A-003 or ASB MBB-BK117 D-2-29A-001, as applicable to 
your model helicopter, except you are not required to discard old 
parts.
    (ii) Replace each aft single locking attachment hardware with 
double locking attachment hardware by following the Accomplishment 
Instructions, paragraphs 3.B.3.1. through 3.B.3.3. on page 13 of ASB 
MBB-BK117 C-2-29A-003 or ASB MBB-BK117 D-2-29A-001, as applicable to 
your model helicopter, except you are not required to discard old 
parts.

(g) Credit for Previous Actions

    Actions accomplished before the effective date of this AD in 
accordance with the procedures specified in AD 2017-02-07, Amendment 
39-18786 (82 FR 10267, February 10, 2017) or Airbus Helicopters ASB 
No. ASB MBB-BK117 C-2-29A-003 or ASB No. ASB MBB-BK117 D-2-29A-001, 
both Revision 1 and both dated October 14, 2016, are considered 
acceptable for compliance with the corresponding actions specified 
in paragraph (f)(1) of this AD.

(h) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Safety Management Section, 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.

(i) Additional Information

    (1) Airbus Helicopters ASB No. ASB MBB-BK117 C-2-29A-003 and ASB 
No. ASB MBB-BK117 D-2-29A-001, both Revision 1 and both dated 
October 14, 2016, which are not incorporated by reference, contain 
additional information about the subject of this AD. For 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.airbushelicopters.com/techpub. You may review a copy of the 
service information at the FAA, Office of the Regional Counsel, 
Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 
76177.
    (2) The subject of this AD is addressed in European Aviation 
Safety Agency (EASA) AD No. 2017-0047, dated March 13, 2017. You may 
view the EASA AD on the Internet at http://www.regulations.gov in 
the AD Docket.

(j) Subject

    Joint Aircraft Service Component (JASC) Code: 2900, Hydraulic 
Power System.

    Issued in Fort Worth, Texas, on November 17, 2017.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification 
Service.
[FR Doc. 2017-26039 Filed 12-4-17; 8:45 am]
 BILLING CODE 4910-13-P



                                                  57390                 Federal Register / Vol. 82, No. 232 / Tuesday, December 5, 2017 / Proposed Rules

                                                  DEPARTMENT OF TRANSPORTATION                            European Aviation Safety Agency                       and including 9750, and Model MBB–
                                                                                                          (EASA) AD, the economic evaluation,                   BK 117 D–2 helicopters, serial numbers
                                                  Federal Aviation Administration                         any comments received and other                       up to and including 20110, with a
                                                                                                          information. The street address for the               hydraulic module plate assembly part
                                                  14 CFR Part 39                                          Docket Operations Office (telephone                   number B291M0003103 with a single
                                                  [Docket No. FAA–2017–1123; Product                      800–647–5527) is in the ADDRESSES                     locking attachment point installed. AD
                                                  Identifier 2017–SW–013–AD]                              section. Comments will be available in                2017–02–07 requires a repetitive
                                                                                                          the AD docket shortly after receipt.                  inspection and a one-time torque of the
                                                  RIN 2120–AA64                                             For service information identified in               attachment points. The actions in AD
                                                                                                          this proposed rule, contact Airbus                    2017–02–07 are intended to prevent
                                                  Airworthiness Directives; Airbus                                                                              failure of an attachment point, loss of
                                                                                                          Helicopters, 2701 N. Forum Drive,
                                                  Helicopters Deutschland GmbH                                                                                  the hydraulic module plate, and
                                                                                                          Grand Prairie, TX 75052; telephone
                                                  Helicopters                                                                                                   subsequent loss of control of the
                                                                                                          (972) 641–0000 or (800) 232–0323; fax
                                                  AGENCY: Federal Aviation                                (972) 641–3775; or at http://                         helicopter.
                                                  Administration (FAA), DOT.                              www.airbushelicopters.com/techpub.                       EASA, which is the Technical Agent
                                                                                                          You may review service information at                 for the Member States of the European
                                                  ACTION: Notice of proposed rulemaking
                                                                                                          the FAA, Office of the Regional Counsel,              Union, issued EASA AD No. 2015–
                                                  (NPRM).
                                                                                                          Southwest Region, 10101 Hillwood                      0210R1, Revision 1, dated October 28,
                                                  SUMMARY:   We propose to supersede                      Pkwy., Room 6N–321, Fort Worth, TX                    2015 (2015–0210R1), to correct an
                                                  Airworthiness Directive (AD) 2017–02–                   76177.                                                unsafe condition for Airbus Helicopters
                                                  07 for Airbus Helicopters Deutschland                                                                         Model MBB–BK117 C–2, MBB–BK117
                                                                                                          FOR FURTHER INFORMATION CONTACT:    Matt              C–2e, MBB–BK117 D–2, and MBB–
                                                  GmbH (Airbus Helicopters) Model                         Fuller, Senior Aviation Safety Engineer,
                                                  MBB–BK 117 C–2 and Model MBB–BK                                                                               BK117 D–2m helicopters. EASA advised
                                                                                                          Safety Management Section, Rotorcraft                 that the hydraulic plate assembly on
                                                  117 D–2 helicopters. AD 2017–02–07                      Standards Branch, FAA, 10101
                                                  currently requires a repetitive                                                                               certain MBB–BK117 models has four
                                                                                                          Hillwood Pkwy., Fort Worth, TX 76177;                 attachment points on the fuselage
                                                  inspection and a one-time torque of                     telephone (817) 222–5110; email
                                                  each hydraulic module plate assembly                                                                          secured by a single locking mechanism.
                                                                                                          matthew.fuller@faa.gov.                               According to EASA, a design
                                                  attachment point (attachment point).
                                                                                                          SUPPLEMENTARY INFORMATION:                            reassessment revealed stiffness of the
                                                  Since we issued AD 2017–02–07, a
                                                  terminating action has been developed                   Comments Invited                                      hydraulic plate may be insufficient to
                                                  to address the unsafe condition. This                                                                         withstand the in-service loads in the
                                                                                                             We invite you to participate in this               event one of the four single locking
                                                  proposed AD would retain the initial                    rulemaking by submitting written
                                                  inspection and torque requirements of                                                                         attachment points fails. EASA stated
                                                                                                          comments, data, or views. We also                     that if this condition is not detected and
                                                  AD 2017–02–07 and require replacing                     invite comments relating to the
                                                  the attachment point hardware. The                                                                            corrected, it may lead to loss of the
                                                                                                          economic, environmental, energy, or                   hydraulic module plate and possible
                                                  actions of this proposed AD are                         federalism impacts that might result
                                                  intended to prevent an unsafe condition                                                                       loss of control of the helicopter.
                                                                                                          from adopting the proposals in this                   Therefore, the EASA AD required a
                                                  on these products.                                      document. The most helpful comments                   repetitive inspection and one-time
                                                  DATES: We must receive comments on                      reference a specific portion of the                   torque tightening of the attachment
                                                  this proposed AD by February 5, 2018.                   proposal, explain the reason for any                  points in accordance with Airbus
                                                  ADDRESSES: You may send comments by                     recommended change, and include                       Helicopters’ service information.
                                                  any of the following methods:                           supporting data. To ensure the docket                    EASA considered its AD an interim
                                                     • Federal eRulemaking Docket: Go to                  does not contain duplicate comments,                  action and stated further AD action may
                                                  http://www.regulations.gov. Follow the                  commenters should send only one copy                  follow. EASA subsequently revised AD
                                                  online instructions for sending your                    of written comments, or if comments are               2015–0210R1 and issued AD No. 2015–
                                                  comments electronically.                                filed electronically, commenters should               0210R2, dated December 2, 2016 (2015–
                                                     • Fax: 202–493–2251.                                 submit only one time.                                 0210R2), to exclude from the
                                                     • Mail: Send comments to the U.S.                       We will file in the docket all                     applicability helicopters with an
                                                  Department of Transportation, Docket                    comments that we receive, as well as a                improved double locking attachment
                                                  Operations, M–30, West Building                         report summarizing each substantive                   mechanism that is not subject to the
                                                  Ground Floor, Room W12–140, 1200                        public contact with FAA personnel                     unsafe condition.
                                                  New Jersey Avenue SE., Washington,                      concerning this proposed rulemaking.
                                                  DC 20590–0001.                                          Before acting on this proposal, we will               Actions Since AD 2017–02–07 Was
                                                     • Hand Delivery: Deliver to the                      consider all comments we receive on or                Issued
                                                  ‘‘Mail’’ address between 9 a.m. and 5                   before the closing date for comments.                    Since we issued AD 2017–02–07,
                                                  p.m., Monday through Friday, except                     We will consider comments filed after                 Airbus Helicopters revised its service
                                                  Federal holidays.                                       the comment period has closed if it is                information to add procedures to
                                                                                                          possible to do so without incurring                   modify single locking attachment
                                                  Examining the AD Docket
                                                                                                          expense or delay. We may change this                  mechanisms to double locking
                                                    You may examine the AD docket on                      proposal in light of the comments we
sradovich on DSK3GMQ082PROD with PROPOSALS




                                                                                                                                                                attachment mechanisms. EASA
                                                  the Internet at http://                                 receive.                                              subsequently superseded AD 2015–
                                                  www.regulations.gov by searching for                                                                          0210R2 with AD No. 2017–0047, dated
                                                  and locating Docket No. FAA–2017–                       Discussion
                                                                                                                                                                March 13, 2017, to require installation
                                                  1123; or in person at the Docket                          We issued AD 2017–02–07,                            of double locking attachments.
                                                  Operations Office between 9 a.m. and 5                  Amendment 39–18786 (82 FR 10267,
                                                  p.m., Monday through Friday, except                     February 10, 2017) (2017–02–07) for                   FAA’s Determination
                                                  Federal holidays. The AD docket                         Airbus Helicopters Model MBB–BK 117                     These helicopters have been approved
                                                  contains this proposed AD, the                          C–2 helicopters, serial numbers up to                 by the aviation authority of Germany


                                             VerDate Sep<11>2014   18:01 Dec 04, 2017   Jkt 244001   PO 00000   Frm 00008   Fmt 4702   Sfmt 4702   E:\FR\FM\05DEP1.SGM   05DEP1


                                                                        Federal Register / Vol. 82, No. 232 / Tuesday, December 5, 2017 / Proposed Rules                                              57391

                                                  and are approved for operation in the                   attachment point. This proposed AD                    promoting safe flight of civil aircraft in
                                                  United States. Pursuant to our bilateral                would also require, within 300 hours                  air commerce by prescribing regulations
                                                  agreement with Germany, EASA, its                       TIS, replacing each single locking                    for practices, methods, and procedures
                                                  technical representative, has notified us               attachment point mechanism with a                     the Administrator finds necessary for
                                                  of the unsafe condition described in its                double locking attachment point                       safety in air commerce. This regulation
                                                  AD. We are proposing this AD because                    mechanism.                                            is within the scope of that authority
                                                  we evaluated all known relevant                                                                               because it addresses an unsafe condition
                                                                                                          Differences Between This Proposed AD
                                                  information and determined that an                                                                            that is likely to exist or develop on
                                                                                                          and the EASA AD
                                                  unsafe condition is likely to exist or                                                                        products identified in this rulemaking
                                                  develop on other products of the same                      The EASA AD specifies performing                   action.
                                                  type design.                                            the visual inspection of each attachment
                                                                                                          point at intervals not exceeding 400                  Regulatory Findings
                                                  Related Service Information Under 1                     flight hours. This proposed AD would                    We determined that this proposed AD
                                                  CFR Part 51                                             not require a repetitive inspection. This             would not have federalism implications
                                                     We reviewed Airbus Helicopters Alert                 proposed AD would require the                         under Executive Order 13132. This
                                                  Service Bulletin (ASB) No. ASB MBB–                     replacement of each single locking                    proposed AD would not have a
                                                  BK117 C–2–29A–003 for Model MBB–                        attachment point mechanism with a                     substantial direct effect on the States, on
                                                  BK 117 C–2 helicopters and ASB No.                      double locking attachment point                       the relationship between the national
                                                  ASB MBB–BK117 D–2–29A–001 for                           mechanism within 300 hours TIS                        Government and the States, or on the
                                                  Model MBB–BK 117 D–2 helicopters,                       instead, which would make subsequent                  distribution of power and
                                                  both Revision 2 and both dated                          inspections unnecessary.                              responsibilities among the various
                                                  February 1, 2017. Until the attachment                                                                        levels of government.
                                                  points are modified with double locking                 Costs of Compliance
                                                                                                                                                                  For the reasons discussed, I certify
                                                  attachment mechanisms, this service                        We estimate that this proposed AD                  this proposed regulation:
                                                  information specifies a repetitive visual               would affect 134 helicopters of U.S.                    1. Is not a ‘‘significant regulatory
                                                  inspection for condition and correct                    Registry. We estimate that operators                  action’’ under Executive Order 12866;
                                                  installation of the attachment points and               may incur the following costs in order                  2. Is not a ‘‘significant rule’’ under the
                                                  replacing the affected parts if there is a              to comply with this AD. We estimate the               DOT Regulatory Policies and Procedures
                                                  crack. This service information also                    cost of labor at $85 per work-hour.                   (44 FR 11034, February 26, 1979);
                                                  specifies a tightening torque check after               Visually inspecting the four attachment                 3. Will not affect intrastate aviation in
                                                  the initial inspection and replacing the                points would take about 0.75 work-hour                Alaska to the extent that it justifies
                                                  affected parts if torque cannot be                      for an estimated cost of $64 per                      making a regulatory distinction; and
                                                  applied. This revision of the service                   helicopter and $8,576 for the U.S. fleet.               4. Will not have a significant
                                                  information also specifies procedures to                Inspecting the torque of the four                     economic impact, positive or negative,
                                                  replace the single locking attachment                   attachment points would take about                    on a substantial number of small entities
                                                  hardware with double locking                            0.25 work-hour for an estimated cost of               under the criteria of the Regulatory
                                                  attachment hardware.                                    $21 per helicopter and $2,814 for the                 Flexibility Act.
                                                     This service information is reasonably               U.S. fleet. Replacing any of the                        We prepared an economic evaluation
                                                  available because the interested parties                attachment point parts would take a                   of the estimated costs to comply with
                                                  have access to it through their normal                  minimal amount of time and parts                      this proposed AD and placed it in the
                                                  course of business or by the means                      would cost about $48 per attachment                   AD docket.
                                                  identified in the ADDRESSES section.                    point. Installing four double locking
                                                                                                          attachment point mechanisms would                     List of Subjects in 14 CFR Part 39
                                                  Other Related Service Information
                                                                                                          take a minimal amount of time and parts                 Air transportation, Aircraft, Aviation
                                                     We also reviewed Airbus Helicopters                  would cost about $400 per helicopter                  safety, Incorporation by reference,
                                                  ASB No. ASB MBB–BK117 C–2–29A–                          and $53,600 for the U.S. fleet.                       Safety.
                                                  003 for Model MBB–BK 117 C–2                               According to Airbus Helicopters
                                                  helicopters and ASB No. ASB MBB–                        service information, some of the costs of             The Proposed Amendment
                                                  BK117 D–2–29A–001 for Model MBB–                        this proposed AD may be covered under                   Accordingly, under the authority
                                                  BK 117 D–2 helicopters, both Revision                   warranty, thereby reducing the cost                   delegated to me by the Administrator,
                                                  1 and both dated October 14, 2016.                      impact on affected individuals. We do                 the FAA proposes to amend 14 CFR part
                                                  Revision 1 of this service information                  not control warranty coverage by Airbus               39 as follows:
                                                  contains the same visual inspection and                 Helicopters. Accordingly, we have
                                                  torque tightening check procedures as                   included all costs in our cost estimate.              PART 39—AIRWORTHINESS
                                                  Revision 2. However, Revision 2 of this                                                                       DIRECTIVES
                                                  service information adds the procedures                 Authority for This Rulemaking
                                                  to replace the single locking attachment                  Title 49 of the United States Code                  ■ 1. The authority citation for part 39
                                                  hardware with double locking                            specifies the FAA’s authority to issue                continues to read as follows:
                                                  attachment hardware.                                    rules on aviation safety. Subtitle I,                     Authority: 49 U.S.C. 106(g), 40113, 44701.
                                                                                                          section 106, describes the authority of
                                                  Proposed AD Requirements                                the FAA Administrator. ‘‘Subtitle VII:                § 39.13    [Amended]
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                                                    This proposed AD would require,                       Aviation Programs,’’ describes in more                ■ 2. The FAA amends § 39.13 by
                                                  within 100 hours time-in-service (TIS),                 detail the scope of the Agency’s                      removing Airworthiness Directive (AD)
                                                  unless already done within the last 100                 authority.                                            2017–02–07, Amendment 39–18786 (82
                                                  hours TIS, performing a visual                            We are issuing this rulemaking under                FR 10267, February 10, 2017), and
                                                  inspection of each attachment point of                  the authority described in ‘‘Subtitle VII,            adding the following new AD:
                                                  the hydraulic module plate assembly for                 Part A, Subpart III, Section 44701:                   Airbus Helicopters Deutschland GmbH:
                                                  a crack and proper installation, and                    General requirements.’’ Under that                        Docket No. FAA–2017–1123; Product
                                                  applying torque to the nuts of each                     section, Congress charges the FAA with                    Identifier 2017–SW–013–AD.



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                                                  57392                 Federal Register / Vol. 82, No. 232 / Tuesday, December 5, 2017 / Proposed Rules

                                                  (a) Applicability                                       model helicopter, except you are not required         DEPARTMENT OF THE TREASURY
                                                    This AD applies to Model MBB–BK 117 C–                to discard old parts.
                                                  2 helicopters, serial numbers up to and                                                                       Alcohol and Tobacco Tax and Trade
                                                                                                          (g) Credit for Previous Actions
                                                  including 9750, and Model MBB–BK 117 D–                                                                       Bureau
                                                  2 helicopters, serial numbers up to and                   Actions accomplished before the effective
                                                  including 20110, with a hydraulic module                date of this AD in accordance with the                27 CFR Parts 24 and 27
                                                  plate assembly part number B291M0003103                 procedures specified in AD 2017–02–07,
                                                  with a single locking attachment point                  Amendment 39–18786 (82 FR 10267,                      [Docket No. TTB–2016–0014; Notice No.
                                                  installed, certificated in any category.                February 10, 2017) or Airbus Helicopters              168A; Re: Notice No. 168, T.D. TTB–147,
                                                                                                                                                                and T.D. TTB 147A]
                                                  (b) Unsafe Condition                                    ASB No. ASB MBB–BK117 C–2–29A–003 or
                                                                                                          ASB No. ASB MBB–BK117 D–2–29A–001,                    RIN 1513–AC31
                                                     This AD defines the unsafe condition as
                                                  failure of a hydraulic module plate assembly            both Revision 1 and both dated October 14,
                                                  attachment point (attachment point). This               2016, are considered acceptable for                   Implementation of Statutory
                                                  condition could result in loss of the                   compliance with the corresponding actions             Amendments Requiring the
                                                  hydraulic module plate and subsequent loss              specified in paragraph (f)(1) of this AD.             Modification of the Definition of Hard
                                                  of control of the helicopter.                                                                                 Cider; Delayed Compliance Date for
                                                                                                          (h) Alternative Methods of Compliance
                                                                                                                                                                the Hard Cider Tax Class Labeling
                                                  (c) Affected ADs                                        (AMOCs)
                                                                                                                                                                Statement Requirement; Reopening of
                                                     This AD supersedes 2017–02–07,                         (1) The Manager, Safety Management                  Comment Period
                                                  Amendment 39–18786 (82 FR 10267,                        Section, FAA, may approve AMOCs for this
                                                  February 10, 2017).                                     AD. Send your proposal to: Matt Fuller,               AGENCY: Alcohol and Tobacco Tax and
                                                  (d) Comments Due Date                                   Senior Aviation Safety Engineer, Safety               Trade Bureau, Treasury.
                                                                                                          Management Section, Rotorcraft Standards              ACTION: Notice of proposed rulemaking
                                                    We must receive comments by February 5,
                                                  2018.                                                   Branch, FAA, 10101 Hillwood Pkwy., Fort               and reopening of comment period.
                                                                                                          Worth, TX 76177; telephone (817) 222–5110;
                                                  (e) Compliance                                          email 9-ASW-FTW-AMOC-Requests@faa.gov.                SUMMARY:   On January 23, 2017, the
                                                     You are responsible for performing each                (2) For operations conducted under a 14             Alcohol and Tobacco Tax and Trade
                                                  action required by this AD within the                   CFR part 119 operating certificate or under           Bureau (TTB) published a temporary
                                                  specified compliance time unless it has                 14 CFR part 91, subpart K, we suggest that            rule, T.D. TTB–147, Implementation of
                                                  already been accomplished prior to that time.           you notify your principal inspector, or               Statutory Amendments Requiring the
                                                  (f) Required Actions                                    lacking a principal inspector, the manager of         Modification of the Definition of Hard
                                                                                                          the local flight standards district office or         Cider, that amended its regulations to
                                                     (1) Within 100 hours time-in-service (TIS):
                                                     (i) Visually inspect the split pins,                 certificate holding district office before            implement changes made to the
                                                  castellated nuts, plugs, nuts, and hexagon              operating any aircraft complying with this            definition of ‘‘hard cider’’ in the Internal
                                                  bolts of each attachment point for a crack and          AD through an AMOC.                                   Revenue Code of 1986 by the Protecting
                                                  for proper installation by following the                                                                      Americans from Tax Hikes Act (PATH
                                                                                                          (i) Additional Information
                                                  Accomplishment Instructions, paragraphs                                                                       Act) of 2015. The amended regulations
                                                  3.B.1.3.a. through 3.B.1.3.d., of Airbus                   (1) Airbus Helicopters ASB No. ASB MBB–            included a requirement that the
                                                  Helicopters Alert Service Bulletin (ASB) No.            BK117 C–2–29A–003 and ASB No. ASB                     statement ‘‘Tax class 5041(b)(6)’’ appear
                                                  ASB MBB–BK117 C–2–29A–003 (ASB MBB–                     MBB–BK117 D–2–29A–001, both Revision 1                on the container of any wine for which
                                                  BK117 C–2–29A–003) or Airbus Helicopters                and both dated October 14, 2016, which are            the hard cider tax rate is claimed if the
                                                  ASB No. ASB MBB–BK117 D–2–29A–001                       not incorporated by reference, contain
                                                  (ASB MBB–BK117 D–2–29A–001), both                                                                             wine is removed from wine premises or
                                                                                                          additional information about the subject of           customs custody on or after January 1,
                                                  Revision 2 and both dated February 1, 2017,             this AD. For service information identified in
                                                  as applicable to your model helicopter.                                                                       2018. Concurrent with the temporary
                                                                                                          this AD, contact Airbus Helicopters, 2701 N.          rule, TTB published Notice of Proposed
                                                  Replace any part that has a crack before
                                                  further flight. If the split pins, castellated          Forum Drive, Grand Prairie, TX 75052;                 Rulemaking No. 168 requesting
                                                  nuts, or hexagon bolts are not as depicted in           telephone (972) 641–0000 or (800) 232–0323;
                                                                                                                                                                comments on the regulatory
                                                  Figure 2 of ASB MBB–BK117 C–2–29A–003                   fax (972) 641–3775; or at http://
                                                                                                                                                                amendments made by T.D. TTB–147. In
                                                  or ASB MBB–BK117 D–2–29A–001, before                    www.airbushelicopters.com/techpub. You
                                                                                                                                                                response to a comment received from a
                                                  further flight, properly install them.                  may review a copy of the service information
                                                                                                                                                                cider industry trade association, TTB, in
                                                     (ii) Apply a torque of 9 to 10 Nm to the             at the FAA, Office of the Regional Counsel,
                                                  left-hand and right-hand nuts of each                                                                         a temporary rule published elsewhere in
                                                                                                          Southwest Region, 10101 Hillwood Pkwy.,
                                                  attachment point. If a torque of 9 to 10 Nm                                                                   this issue of the Federal Register, is
                                                                                                          Room 6N–321, Fort Worth, TX 76177.
                                                  cannot be applied, replace the affected nut                (2) The subject of this AD is addressed in
                                                                                                                                                                now delaying the compliance date for
                                                  before further flight.                                  European Aviation Safety Agency (EASA) AD
                                                                                                                                                                the hard cider tax class labeling
                                                     (2) Within 300 hours TIS:
                                                                                                          No. 2017–0047, dated March 13, 2017. You
                                                                                                                                                                requirement by one year, until January
                                                     (i) Replace each forward single locking                                                                    1, 2019. In this document, TTB is
                                                  attachment hardware with double locking                 may view the EASA AD on the Internet at
                                                                                                          http://www.regulations.gov in the AD Docket.          requesting comments on that delayed
                                                  attachment hardware by following the                                                                          compliance date, and we are also re-
                                                  Accomplishment Instructions, paragraphs                 (j) Subject                                           opening the comment period for Notice
                                                  3.B.3.3. through 3.B.3.6. on page 11 of ASB
                                                  MBB–BK117 C–2–29A–003 or ASB MBB–                         Joint Aircraft Service Component (JASC)             No. 168 for an additional 60 days to
                                                  BK117 D–2–29A–001, as applicable to your                Code: 2900, Hydraulic Power System.                   request comments on the regulatory
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                                                  model helicopter, except you are not required                                                                 amendments described in T.D. TTB–
                                                                                                            Issued in Fort Worth, Texas, on November
                                                  to discard old parts.                                                                                         147.
                                                                                                          17, 2017.
                                                     (ii) Replace each aft single locking                                                                       DATES: Comments on the delayed
                                                  attachment hardware with double locking                 Lance T. Gant,
                                                  attachment hardware by following the                    Director, Compliance & Airworthiness
                                                                                                                                                                compliance date referenced in this
                                                  Accomplishment Instructions, paragraphs                 Division, Aircraft Certification Service.             document (Notice No. 168A) are due on
                                                  3.B.3.1. through 3.B.3.3. on page 13 of ASB                                                                   or before February 5, 2018. The
                                                                                                          [FR Doc. 2017–26039 Filed 12–4–17; 8:45 am]
                                                  MBB–BK117 C–2–29A–003 or ASB MBB–                                                                             comment period for the proposed rule,
                                                                                                          BILLING CODE 4910–13–P
                                                  BK117 D–2–29A–001, as applicable to your                                                                      Notice No. 168, published on January


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Document Created: 2017-12-04 23:44:30
Document Modified: 2017-12-04 23:44:30
CategoryRegulatory Information
CollectionFederal Register
sudoc ClassAE 2.7:
GS 4.107:
AE 2.106:
PublisherOffice of the Federal Register, National Archives and Records Administration
SectionProposed Rules
ActionNotice of proposed rulemaking (NPRM).
DatesWe must receive comments on this proposed AD by February 5, 2018.
ContactMatt 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 Citation82 FR 57390 
RIN Number2120-AA64
CFR AssociatedAir Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

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