[Federal Register Volume 82, Number 134 (Friday, July 14, 2017)]
[Proposed Rules]
[Pages 32501-32503]
[FR Doc No: 2017-14373]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-0671; Directorate Identifier 2016-SW-072-AD]
RIN 2120-AA64

Airworthiness Directives; Airbus Helicopters (Previously
Eurocopter France)

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: We propose to supersede Airworthiness Directive (AD) 2009-25-
07 for Airbus Helicopters Model EC120B helicopters. AD 2009-25-07
currently requires amending the rotorcraft flight manual supplement
(RFMS) and pre-flight checking the emergency flotation gear before each
flight over water. Since we issued AD 2009-25-07, Airbus Helicopters
developed a terminating action and identified an additional part-
numbered emergency floatation gear part with the unsafe condition. This
proposed AD would retain the requirements of AD 2009-25-07, expand the
applicability, and add a terminating action for the repetitive
inspections. The actions of this proposed AD are intended to correct
the unsafe condition on these helicopters.

DATES: We must receive comments on this proposed AD by September 12,
2017.

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:<PHONE_NUMBER>.
     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-
0671; 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<PHONE_NUMBER>) 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<PHONE_NUMBER> or<PHONE_NUMBER>; fax<PHONE_NUMBER>; or at
http://www.airbushelicopters.com/Web site/technical-expert/. 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: George Schwab, Aviation Safety
Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 10101
Hillwood Pkwy, Fort Worth, TX 76177; telephone<PHONE_NUMBER>; email
<EMAIL_ADDRESS>
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

    On November 18, 2009, we issued AD 2009-25-07, Amendment 39-16126
(74 FR 65682, December 11, 2009) for Eurocopter France (now Airbus
Helicopters) Model EC120B helicopters with an Emergency Floatation Gear
lighting and ancillary control unit (LACU), part number (P/N) 040101AB,
installed. AD 2009-25-07 requires amending the Limitations section of
the RFMS to prohibit flight over water if the ``float arm'' pushbutton
does not remain lit, conducting a pilot check to determine whether the
``float arm'' pushbutton remains lit before any flight over water, and
placarding the ``float arm'' pushbutton as inoperative if the
functional check is unsuccessful.
    AD 2009-25-07 was prompted by AD No. 2008-0177-E, dated September
19, 2008 (AD 2008-0177-E), issued by EASA, which is the Technical Agent
for the Member States of the European Union, to correct an unsafe
condition for Model EC120B helicopters. EASA advises that operators
reported reliability issues with the LACU emergency flotation ``float
arm'' latching pushbuttons, used to arm the emergency flotation gear,
including failure of the light to illuminate properly. AD 2008-0177-E
states the unsafe condition may be due to the bonding of the
pushbuttons and requires a repetitive, in-flight functional test of the
float arm pushbutton before flight overwater. AD 2008-0177-E further
prohibits overwater flight if the pushbutton fails to latch in the
depressed position. Those actions are intended to prohibit flight over
water if a functional test indicates that the emergency flotation gear
cannot be armed, which would preclude deployment of the floats in an
emergency water ditching, resulting in subsequent damage to the
helicopter and injury to occupants.

Actions Since AD 2009-25-07 Was Issued

    Since we issued AD 2009-25-07, EASA has issued AD No. 2016-0180,
dated September 13, 2016 (AD 2016-0180), which superseded AD 2008-0177-
E. EASA advises that Airbus Helicopters has designed an improved
latching pushbutton, which when installed becomes a terminating action
for the repetitive functional checks of the float arm pushbuttons. EASA
also states that LACU P/N 040101BA is equipped with the same faulty
pushbutton and must be included in the applicability.

    We have also determined that the ``Emergency Floatation Gear LACU''
as identified in AD 2009-25-07 is more correctly described as an LACU.
Therefore we use the term ``LACU'' in this proposed AD.

FAA's Determination

    These helicopters have been approved by the aviation authority of
France and are approved for operation in the United States. Pursuant to
our bilateral agreement with France, 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

    We reviewed Airbus Helicopters Emergency Alert Service Bulletin No.
04A007, Revision 1, dated June 30, 2016 (EASB), for Airbus Helicopters
Model EC120B helicopters. The EASB describes procedures for a pre-
flight check of the float arm pushbutton while arming the emergency
flotation gear and prohibits operators from flight over water if the
float arm pushbutton fails.
    We also reviewed Airbus Helicopters Alert Service Bulletin No.
EC120-31A008, dated June 30, 2016 (ASB), for Airbus Helicopters Model
EC 120B helicopters. The ASB describes procedures for replacing the
float arm pushbutton with a new design pushbutton and for re-labeling
the modified LACU with a new P/N label.

Proposed AD Requirements

    This proposed AD would retain the RFMS amendment and repetitive
functional check requirements of AD 2009-25-07. This proposed AD would
add LACU P/N 040101BA to the applicability paragraph, require replacing
the float arm pushbutton P/N 045004A111A with float arm pushbutton P/N
304-2500-00 within 300 hours time-in-service (TIS), and prohibit
installing float arm pushbutton P/N 045004A111A on any helicopter.
Replacing the float arm pushbutton would be a terminating action for
the repetitive functional checks prior to flight overwater.
    An owner/operator (pilot) may perform the functional check required
by this AD and must enter compliance with that paragraph into the
helicopter maintenance records in accordance with 14 CFR 43.9(a)(1)
through (4) and 91.417(a)(2)(v). A pilot may perform this check because
it involves only a functional check to determine whether the emergency
flotation gear has been armed and can be performed equally well by a
pilot or a mechanic. This check is an exception to our standard
maintenance regulations.
    This proposed AD would also revise the term ``emergency flotation
gear lighting and ancillary control unit'' in the applicability
paragraph to ``lighting and ancillary control unit'' for technical
accuracy.

Differences Between This Proposed AD and the EASA AD

    The EASA AD requires installing the LACU float arm pushbutton
within 13 months; the proposed AD would require the installation within
300 hours TIS.

Costs of Compliance

    We estimate that this proposed AD would affect 53 helicopters of
U.S. Registry.
    We estimate that operators may incur the following costs in order
to comply with this AD. At an average labor rate of $85 per hour, the
cost of revising the limitations section of the RFMS and of the pre-
flight functional check is negligible. Replacing the float arm
pushbutton would require about 2 work-hours, and required parts would
cost about $311, for a cost per helicopter of $481 and a total cost of
$25,493 to the U.S. fleet.

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)
2009-25-07, Amendment 39-16126 (74 FR 65682, December 11, 2009), and
adding the following new AD:

Airbus Helicopters (Previously Eurocopter France): Docket No. FAA-
2017-0671; Directorate Identifier 2016-SW-072-AD.

(a) Applicability

    This AD applies to Airbus Helicopters (previously Eurocopter
France) Model EC120B helicopters, certificated in any category, with
a Lighting and Ancillary Control Unit (LACU) part-number (P/N)
040101AB or 040101BA with a float arm pushbutton P/N 045004A111A
installed.

(b) Unsafe Condition

    This AD defines the unsafe condition as failure of a ``float
arm'' pushbutton, which could result in inoperative floats being
used in an emergency water ditching, causing damage to the
helicopter or injury to occupants.

(c) Affected ADs

    This AD supersedes AD 2009-25-07, Amendment 39-16126 (74 FR
65682, December 11, 2009).

(d) Comments Due Date

    We must receive comments by September 12, 2017.

(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) Before further flight, amend the EC120B Rotorcraft Flight
Manual Supplement (RFMS) for the emergency flotation gear Aerazur,
by inserting a copy of this AD into the Limitations section of the
RFMS or by making pen and ink changes to that section to add the
information in figure 1 to paragraph (f)(1) of this AD:
[GRAPHIC] [TIFF OMITTED] TP13JY17.002

    (2) Before each flight over water:
    (i) Perform a functional check to determine whether flight over
water is permitted under the Limitations section in paragraph (f)(1)
of this AD. For purposes of this AD, ``flight over water'' means
flight beyond the power-off gliding distance from shore. ``Shore''
is an area of land adjacent to the water and above the high water
mark but does not include land area that is intermittently under
water. The actions required by this paragraph may be performed by
the owner/operator (pilot) holding at least a private pilot
certificate, and must be entered into the aircraft records showing
compliance with this AD in accordance with 14 CFR 43.9 (a)(1)
through (4) and 14 CFR 91.417(a)(2)(v). The record must be
maintained as required by 14 CFR 91.417, 121.380, or 135.439.
    (ii) If the LACU fails the functional check required by
paragraph (f)(2)(i) of this AD, place a placard over the ``float
arm'' pushbutton that reads ``INOP.''
    (3) Within 300 hours time-in-service, replace float arm
pushbutton P/N 045004A111A with float arm pushbutton P/N 304-2500-
00. Installing float arm pushbutton P/N 304-2500-00 is terminating
action for the functional check and placard required by paragraphs
(f)(2)(i) and (f)(2)(ii) of this AD.
    (4) Do not install float arm pushbutton P/N 045004A111A on any
helicopter.

(g) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Safety Management Group, FAA, may approve AMOCs
for this AD. Send your proposal to: George Schwab, Aviation Safety
Engineer, Safety Management Group, Rotorcraft Directorate, FAA,
10101 Hillwood Pkwy, Fort Worth, TX 76177; telephone<PHONE_NUMBER>;
email<EMAIL_ADDRESS>    (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.

(h) Additional Information

    (1) Airbus Helicopters Emergency Alert Service Bulletin No.
04A007, Revision 1, dated June 30, 2016, and Airbus Helicopters
Alert Service Bulletin No. EC120-31A008, dated June 30, 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<PHONE_NUMBER> or<PHONE_NUMBER>; fax
(972) 641-3775; or at http://www.airbushelicopters.com/website/technical-expert/. 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. 2016-0180, dated September 13, 2016. You
may view the EASA AD on the Internet at http://www.regulations.gov
in the AD Docket.

(i) Subject

    Joint Aircraft Service Component (JASC) Code: 2560 Emergency
Equipment.

    Issued in Fort Worth, Texas, on June 28, 2017.
Scott A. Horn,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 2017-14373 Filed 7-13-17; 8:45 am]
 BILLING CODE 4910-13-P