83_FR_39157 83 FR 39004 - Airworthiness Directives; Bell Helicopter Textron Canada Limited Helicopters

83 FR 39004 - Airworthiness Directives; Bell Helicopter Textron Canada Limited Helicopters

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 83, Issue 153 (August 8, 2018)

Page Range39004-39007
FR Document2018-16637

We propose to supersede airworthiness directive (AD) 2015-22- 02 for Bell Helicopter Textron Canada Limited (Bell) Model 429 helicopters. AD 2015-22-02 requires inspecting the tail rotor (TR) pitch link assemblies. This proposed AD would retain the inspections of AD 2015-22-02 and would require replacing certain pitch link bearings. Since we issued AD 2015-22-02, Bell has introduced a new design bearing. The actions of this proposed AD are intended to prevent an unsafe condition on these products.

Federal Register, Volume 83 Issue 153 (Wednesday, August 8, 2018)
[Federal Register Volume 83, Number 153 (Wednesday, August 8, 2018)]
[Proposed Rules]
[Pages 39004-39007]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2018-16637]


=======================================================================
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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0722; Product Identifier 2017-SW-104-AD
RIN 2120-AA64


Airworthiness Directives; Bell Helicopter Textron Canada Limited 
Helicopters

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to supersede airworthiness directive (AD) 2015-22-
02 for Bell Helicopter Textron Canada Limited (Bell) Model 429 
helicopters. AD 2015-22-02 requires inspecting the tail rotor (TR) 
pitch link assemblies. This proposed AD would retain the inspections of 
AD 2015-22-02 and would require replacing certain pitch link bearings. 
Since we issued AD 2015-22-02, Bell has introduced a new design 
bearing. 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 October 9, 2018.

ADDRESSES: You may send comments by any of the following methods:

[[Page 39005]]

     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-2018-
0722; 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 proposed AD, the Transport Canada AD, the economic evaluation, any 
comments received, and other information. The street address for Docket 
Operations (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 final rule, contact Bell 
Helicopter Textron Canada Limited, 12,800 Rue de l'Avenir, Mirabel, 
Quebec J7J1R4; telephone (450) 437-2862 or (800) 363-8023; fax (450) 
433-0272; or at http://www.bellcustomer.com/files/. 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.

FOR FURTHER INFORMATION CONTACT: David Hatfield, Aviation Safety 
Engineer, Safety Management Section, Rotorcraft Standards Branch, FAA, 
10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222-5110; 
email david.hatfield@faa.gov.

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 2015-22-02, Amendment 39-18306 (80 FR 65618, October 
27, 2015) (AD 2015-22-02), for Bell Model 429 helicopters with a TR 
pitch link assembly part number (P/N) 429-112-101 or 429-112-103 
installed. AD 2015-22-02 requires repetitively inspecting each inboard 
and outboard TR pitch link assembly for axial or radial bearing play 
every 50 hours time-in-service (TIS), performing a dimensional 
inspection of the TR pitch link if there is axial or radial bearing 
play, and replacing the TR pitch link before further flight if there is 
any wear beyond allowable limits. AD 2015-22-02 was prompted by 
Emergency AD No. CF-2015-16, dated July 2, 2015, and Emergency AD No. 
CF-2015-16R1, dated August 6, 2015, issued by Transport Canada, to 
correct an unsafe condition for Bell Model 429 helicopters. Transport 
Canada advised of several occasions where the TR pitch link spherical 
bearings experienced early and accelerated wear.

Actions Since AD 2015-22-02 Was Issued

    Since we issued AD 2015-22-02, Transport Canada has issued AD No. 
CF-2015-16R2, dated April 17, 2017, which supersedes AD CF-2015-16R1. 
According to Transport Canada, Bell has reported that the TR pitch link 
assembly can be rotated during the 50-hour inspections to extend the 
serviceability life of the bearings. Transport Canada AD No. CF-2015-
16R2 requires modified inspection procedures for the spherical bearings 
and requires replacing the TR pitch link bearings (or the TR pitch link 
assembly) with spherical bearings manufactured after January 12, 2015. 
Transport Canada AD No. CF-2015-16R2 also requires re-identifying TR 
pitch link assemblies with a different P/N after installing the new 
bearings. We propose to issue this AD to make similar changes.

FAA's Determination

    These helicopters have been approved by the aviation authority of 
Canada and are approved for operation in the United States. Pursuant to 
our bilateral agreement with Canada, Transport Canada, its technical 
representative, has notified us of the unsafe condition described in 
the Transport Canada AD. We are proposing this AD because we evaluated 
all information provided by Transport Canada and determined the unsafe 
condition exists and is likely to exist or develop on other products of 
the same type design.

Related Service Information

    Bell has issued Alert Service Bulletin No. 429-15-16, Revision B, 
dated June 15, 2016. This service information contains procedures for 
repetitively inspecting the TR pitch link assembly until it is upgraded 
by replacing the TR pitch link bearings.

AD Requirements

    This proposed AD would require performing a dimensional inspection 
of the spherical bearings for axial and radial play and inspecting the 
TR pitch link assembly sealant for pin holes, voids, and excessive 
thickness. These inspections would be required within 50 hours TIS and 
thereafter at intervals not exceeding 50 hours TIS.
    This proposed AD would also require replacing any spherical bearing 
manufactured before January 13, 2015, that has exceeded 250 hours TIS 
or that has an unknown number of hours TIS, and re-identifying the P/N 
of the TR pitch link assembly.

Differences Between This Proposed AD and the Transport Canada AD

    The Transport Canada AD requires the bearing inspection within 10 
hours TIS or before exceeding 60 hours TIS since new, whichever occurs 
later. This proposed AD would require the bearing inspection within 50 
hours TIS. The Transport Canada AD also requires replacing certain 
bearings within 200 hours TIS after the initial bearing inspection or 
within 250 hours TIS since new, whichever occurs first. This proposed 
AD would require replacing the bearing within 200 hours of the initial 
inspection or at the next 50 hour TIS inspection if the hours TIS of a 
pitch link assembly exceed 250 hours TIS or are unknown.

Interim Action

    We consider this proposed AD to be an interim action. If final 
action is later

[[Page 39006]]

identified, we might consider further rulemaking then.

Costs of Compliance

    We estimate that this proposed AD would affect 85 helicopters of 
U.S. Registry. We estimate that operators may incur the following costs 
in order to comply with this proposed AD. At an average labor rate of 
$85 per hour, inspecting the TR pitch link assemblies would require 2 
work-hours for a cost of $170 per helicopter and $14,450 for the U.S. 
fleet per inspection cycle. Replacing both spherical bearings in each 
TR pitch link assembly would require 3 work-hours, and required parts 
would cost $3,088, for a cost of $3,343 per helicopter and $284,155 for 
the U.S. fleet.
    According to Bell's 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 
Bell. 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 will not have federalism 
implications under Executive Order 13132. This proposed AD will not 
have a substantial direct effect on the States, on the relationship 
between the national Government and the States, or on the distribution 
of power and responsibilities among the various levels of government.
    For the reasons discussed, I certify that this proposed regulation:
    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 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) 
2015-22-02, Amendment 39-18306 (80 FR 65618, October 27, 2015), and 
adding the following new AD:

Bell Helicopter Textron Canada Limited: Docket No. FAA-2018-0722; 
Product Identifier 2017-SW-104-AD.

(a) Applicability

    This AD applies to Model 429 helicopters with a pitch link 
assembly part number (P/N) 429-012-112-101, 429-012-112-103, 429-
012-112-101FM, or 429-012-112-103FM installed, certificated in any 
category.

(b) Unsafe Condition

    This AD defines the unsafe condition as a worn pitch link. This 
condition, if not corrected, could result in pitch link failure and 
subsequent loss of control of the helicopter.

(c) Affected ADs

    This AD replaces AD 2015-22-02, Amendment 39-18306 (80 FR 65618, 
October 27, 2015).

(d) Comments Due Date

    We must receive comments by October 9, 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 50 hours time-in-service (TIS) and thereafter at 
intervals not to exceed 50 hours TIS:
    (i) Perform a dimensional inspection of each inboard and 
outboard pitch link assembly for axial and radial bearing play. With 
a 10X or higher power magnifying glass, inspect the bearing liner 
for a crack, deterioration of the liner, and extrusion of the liner 
from the plane. If there is axial or radial play that exceeds 
allowable limits, or if there is a crack, deterioration of the 
liner, or extrusion of the liner, before further flight, replace the 
bearing.
    (ii) Inspect the pitch link assembly sealant for pin holes and 
voids and to determine if the sealant thickness is 0.025 inch (0.64 
mm) or less, extends over the roll staked lip by 0.030 inch (0.76 
mm) or more, and is clear of the bearing ball. If there is a pin 
hole or void, or if the sealant exceeds 0.026 inch (0.66 mm), does 
not extend over the roll staked lip by 0.030 inch (0.76 mm) or more, 
or is not clear of the bearing ball, before further flight, replace 
the bearing.
    (2) For pitch link assembly part number (P/N) 429-012-112-101, 
429-012-112-103, 429-012-112-101FM, and 429-012-112-103FM, within 
200 hours TIS following the initial inspection required by paragraph 
(f)(1) of this AD, or if the hours TIS of a pitch link assembly 
exceed 250 hours TIS or are unknown, at the next 50 hour TIS 
inspection required by paragraph (f)(1) of this AD:
    (i) Replace each bearing P/N 429-312-107-103 with a date of 
manufacture before January 13, 2015, with a bearing P/N 429-312-107-
103 that was manufactured on or after January 13, 2015.
    (ii) Using a white permanent fine point marker or equivalent, 
re-identify the pitch link assembly:
    (A) Re-identify P/N 429-012-112-101 and 429-012-112-101FM as 
429-012-112-111FM.
    (B) Re-identify P/N 429-012-112-103 and 429-012-112-103FM as 
429-012-112-113FM.
    (iii) Apply a coating of DEVCON 2-TON (C-298) or equivalent over 
the new P/N.

(g) Special Flight Permits

    Special flight permits are prohibited.

(h) 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: 
David Hatfield, Aviation Safety Engineer, Safety Management Section, 
Rotorcraft Standards Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, 
TX 76177; telephone (817) 222-5110; email 9-ASW-FTW-AMOC-Requests@faa.gov.
    (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.

[[Page 39007]]

(i) Additional Information

    (1) Bell Alert Service Bulletin No. 429-15-16, Revision B, dated 
June 15, 2016, which is not incorporated by reference, contains 
additional information about the subject of this AD. For service 
information identified in this AD, contact Bell Helicopter Textron 
Canada Limited, 12,800 Rue de l'Avenir, Mirabel, Quebec J7J1R4; 
telephone (450) 437-2862 or (800) 363-8023; fax (450) 433-0272; or 
at http://www.bellcustomer.com/files/. 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 Transport Canada AD 
No. CF-2015-16R2, dated April 17, 2017. You may view the Transport 
Canada AD on the internet at http://www.regulations.gov in the AD 
Docket.

(j) Subject

    Joint Aircraft Service Component (JASC) Code: 6720 Tail Rotor 
Control System.

    Issued in Fort Worth, Texas, on July 23, 2018.
Scott A. Horn,
Deputy Director for Regulatory Operations, Compliance & Airworthiness 
Division, Aircraft Certification Service.
[FR Doc. 2018-16637 Filed 8-7-18; 8:45 am]
BILLING CODE 4910-13-P



                                               39004                Federal Register / Vol. 83, No. 153 / Wednesday, August 8, 2018 / Proposed Rules

                                               information collection. The NCUA may                    Affairs, Office of Management and                     List of Subjects in 12 CFR Part 702
                                               not conduct or sponsor, and the                         Budget, Attention: Desk Officer for                     Credit unions, Reporting and
                                               respondent is not required to respond                   NCUA, New Executive Office Building,                  recordkeeping requirements.
                                               to, an information collection unless it                 Room 10235, Washington, DC 20503, or
                                               displays a currently valid Office of                    email at                                                By the National Credit Union
                                               Management and Budget (OMB) control                     OIRA_Submission,@OMB.EOP.gov.                         Administration Board on August 2, 2018.
                                               number.                                                   Submission of comments. The NCUA                    Gerard Poliquin,
                                                 The proposed changes to part 702                      considers comments by the public on                   Secretary of the Board.
                                               would increase the asset size of credit                 this proposed collection of information                  For the reasons discussed above, the
                                               unions identified as complex from                       in:                                                   Board proposes to further amend 12
                                               greater than $100 million to greater than                 • Evaluating whether the proposed                   CFR part 702, as amended in a final rule
                                               $500 million. This change would reduce                  collection of information is necessary                at 80 FR 66625 (Oct. 29, 2015), effective
                                               the number of credit unions who must                    for the proper performance of the                     January 1, 2019, as follows:
                                               comply with recordkeeping                               functions of the NCUA, including
                                               requirements prescribed by § 702.101(b).                whether the information will have a                   PART 702—CAPITAL ADEQUACY
                                               Therefore, the burden cleared under                     practical use;
                                               OMB number 3133–0191 will be revised                      • Evaluating the accuracy of the                    ■ 1. The authority citation for part 702
                                               to reflect the reduction in the number of               NCUA’s estimate of the burden of the                  continues to read as follows:
                                               respondents.50                                          proposed collection of information,                       Authority: 12 U.S.C. 1766(a), 1790d.
                                                 Title of Information Collection:                      including the validity of the
                                               Prompt Corrective Action—Risk-Based                     methodology and assumptions used;                     § 702.103    [Amended]
                                               Capital.                                                  • Enhancing the quality, usefulness,
                                                 OMB Control Number: 3133–0191.                                                                              ■  2. Amend § 702.103 by removing the
                                                                                                       and clarity of the information to be                  words ‘‘one hundred million dollars
                                                 Affected Public: Private Sector: Not-                 collected; and
                                               for-profit institutions—Complex Credit                                                                        ($100,000,000)’’ and add in their place
                                                                                                         • Minimizing the burden of collection               ‘‘five hundred million dollars
                                               Unions.                                                 of information on those who are to
                                                 Estimated Number of Respondents:                                                                            ($500,000,000).’’
                                                                                                       respond, including through the use of
                                               531.                                                                                                          [FR Doc. 2018–16888 Filed 8–7–18; 8:45 am]
                                                                                                       appropriate automated, electronic,
                                                 Estimated Number of Responses per                                                                           BILLING CODE 7535–01–P
                                                                                                       mechanical, or other technological
                                               Respondent: 1.
                                                                                                       collection techniques or other forms of
                                                 Estimated Hours per Response: 40.
                                                 Estimated Total Annual Burden                         information technology; e.g., permitting
                                                                                                       electronic submission of responses.                   DEPARTMENT OF TRANSPORTATION
                                               Hours: 21,240.
                                                 By exempting credit unions with                       Executive Order 13132                                 Federal Aviation Administration
                                               assets between $100 million and $500
                                                                                                         Executive Order 13132 encourages
                                               million, the NCUA estimates that the                                                                          14 CFR Part 39
                                                                                                       independent regulatory agencies to
                                               burden under this proposed rule would                                                                         [Docket No. FAA–2018–0722; Product
                                                                                                       consider the impact of their actions on
                                               be 41,040 fewer hours.                                                                                        Identifier 2017–SW–104–AD
                                                 The Board invites comment on (a)                      state and local interests. The NCUA, an
                                               whether the collections of information                  independent regulatory agency as                      RIN 2120–AA64
                                               are necessary for the proper                            defined in 44 U.S.C. 3502(5), voluntarily
                                               performance of the agency’s function,                   complies with the principles of the                   Airworthiness Directives; Bell
                                               including practical utility; (b) the                    executive order to adhere to                          Helicopter Textron Canada Limited
                                               accuracy of estimates of the burden of                  fundamental federalism principles. This               Helicopters
                                               the information collections, including                  proposed rule reduces the number of
                                                                                                       federally insured natural-person credit               AGENCY: Federal Aviation
                                               the validity of the methodology and                                                                           Administration (FAA), Department of
                                               assumptions used; (c) ways to enhance                   unions, including federally insured,
                                                                                                       state-chartered natural-person credit                 Transportation (DOT).
                                               the quality, utility, and clarity of the                                                                      ACTION: Notice of proposed rulemaking
                                               information being collected, and (d)                    unions that would be subject to the 2015
                                                                                                       Final Rule. It may have, to some degree,              (NPRM).
                                               ways to minimize the burden of the
                                               information collection on respondents,                  a direct effect on the states, on the
                                                                                                       relationship between the national                     SUMMARY:    We propose to supersede
                                               including through the use of automated                                                                        airworthiness directive (AD) 2015–22–
                                               collection techniques or other forms of                 government and the states, or on the
                                                                                                       distribution of power and                             02 for Bell Helicopter Textron Canada
                                               information technology.                                                                                       Limited (Bell) Model 429 helicopters.
                                                 All comments are a matter of public                   responsibilities among the various
                                                                                                       levels of government. It does not,                    AD 2015–22–02 requires inspecting the
                                               record. Comments regarding the                                                                                tail rotor (TR) pitch link assemblies.
                                               information collection requirements of                  however, rise to the level of material
                                                                                                       impact for purposed of Executive Order                This proposed AD would retain the
                                               this rule should be sent to (1) Dawn                                                                          inspections of AD 2015–22–02 and
                                               Wolfgang, NCUA PRA Clearance                            13132.
                                                                                                                                                             would require replacing certain pitch
                                               Officer, National Credit Union                          Assessment of Federal Regulations and                 link bearings. Since we issued AD
                                               Administration, 1775 Duke Street, Suite                 Policies on Families                                  2015–22–02, Bell has introduced a new
amozie on DSK3GDR082PROD with PROPOSALS




                                               5080, Alexandria, Virginia 22314, or Fax                                                                      design bearing. The actions of this
                                                                                                         The NCUA has determined that this
                                               No. 703–519–8572, or Email at                                                                                 proposed AD are intended to prevent an
                                                                                                       proposed rule will not affect family
                                               PRAcomments@ncua.gov and the (2)                                                                              unsafe condition on these products.
                                                                                                       well-being within the meaning of
                                               Office of Information and Regulatory                                                                          DATES: We must receive comments on
                                                                                                       section 654 of the Treasury and General
                                                 50 Proposed revisions to OMB control number           Government Appropriations Act, 1999,                  this proposed AD by October 9, 2018.
                                               3133–0191 have been submitted to OMB for                Public Law 105–277, 112 Stat. 2681                    ADDRESSES: You may send comments by
                                               approval in accordance with 5 CFR 1320.11.              (1998).                                               any of the following methods:


                                          VerDate Sep<11>2014   18:59 Aug 07, 2018   Jkt 244001   PO 00000   Frm 00023   Fmt 4702   Sfmt 4702   E:\FR\FM\08AUP1.SGM   08AUP1


                                                                    Federal Register / Vol. 83, No. 153 / Wednesday, August 8, 2018 / Proposed Rules                                             39005

                                                 • Federal eRulemaking Docket: Go to                   commenters should send only one copy                  new bearings. We propose to issue this
                                               http://www.regulations.gov. Follow the                  of written comments, or if comments are               AD to make similar changes.
                                               online instructions for sending your                    filed electronically, commenters should
                                                                                                                                                             FAA’s Determination
                                               comments electronically.                                submit only one time.
                                                 • Fax: 202–493–2251.                                     We will file in the docket all                       These helicopters have been approved
                                                 • Mail: Send comments to the U.S.                     comments that we receive, as well as a                by the aviation authority of Canada and
                                               Department of Transportation, Docket                    report summarizing each substantive                   are approved for operation in the United
                                               Operations, M–30, West Building                         public contact with FAA personnel                     States. Pursuant to our bilateral
                                               Ground Floor, Room W12–140, 1200                        concerning this proposed rulemaking.                  agreement with Canada, Transport
                                               New Jersey Avenue SE, Washington, DC                    Before acting on this proposal, we will               Canada, its technical representative, has
                                               20590–0001.                                             consider all comments we receive on or                notified us of the unsafe condition
                                                 • Hand Delivery: Deliver to the                       before the closing date for comments.                 described in the Transport Canada AD.
                                               ‘‘Mail’’ address between 9 a.m. and 5                   We will consider comments filed after                 We are proposing this AD because we
                                               p.m., Monday through Friday, except                     the comment period has closed if it is                evaluated all information provided by
                                               Federal holidays.                                       possible to do so without incurring                   Transport Canada and determined the
                                                                                                       expense or delay. We may change this                  unsafe condition exists and is likely to
                                               Examining the AD Docket                                                                                       exist or develop on other products of the
                                                                                                       proposal in light of the comments we
                                                  You may examine the AD docket on                     receive.                                              same type design.
                                               the internet at http://                                                                                       Related Service Information
                                               www.regulations.gov by searching for                    Discussion
                                               and locating Docket No. FAA–2018–                                                                               Bell has issued Alert Service Bulletin
                                                                                                          We issued AD 2015–22–02,
                                               0722; or in person at Docket Operations                                                                       No. 429–15–16, Revision B, dated June
                                                                                                       Amendment 39–18306 (80 FR 65618,
                                               between 9 a.m. and 5 p.m., Monday                                                                             15, 2016. This service information
                                                                                                       October 27, 2015) (AD 2015–22–02), for
                                               through Friday, except Federal holidays.                                                                      contains procedures for repetitively
                                                                                                       Bell Model 429 helicopters with a TR
                                               The AD docket contains this proposed                                                                          inspecting the TR pitch link assembly
                                                                                                       pitch link assembly part number (P/N)
                                               AD, the Transport Canada AD, the                                                                              until it is upgraded by replacing the TR
                                                                                                       429–112–101 or 429–112–103 installed.
                                               economic evaluation, any comments                                                                             pitch link bearings.
                                                                                                       AD 2015–22–02 requires repetitively
                                               received, and other information. The                    inspecting each inboard and outboard                  AD Requirements
                                               street address for Docket Operations                    TR pitch link assembly for axial or
                                               (telephone 800–647–5527) is in the                                                                               This proposed AD would require
                                                                                                       radial bearing play every 50 hours time-              performing a dimensional inspection of
                                               ADDRESSES section. Comments will be                     in-service (TIS), performing a
                                               available in the AD docket shortly after                                                                      the spherical bearings for axial and
                                                                                                       dimensional inspection of the TR pitch                radial play and inspecting the TR pitch
                                               receipt.                                                link if there is axial or radial bearing
                                                  For service information identified in                                                                      link assembly sealant for pin holes,
                                                                                                       play, and replacing the TR pitch link                 voids, and excessive thickness. These
                                               this final rule, contact Bell Helicopter                before further flight if there is any wear
                                               Textron Canada Limited, 12,800 Rue de                                                                         inspections would be required within
                                                                                                       beyond allowable limits. AD 2015–22–                  50 hours TIS and thereafter at intervals
                                               l’Avenir, Mirabel, Quebec J7J1R4;                       02 was prompted by Emergency AD No.
                                               telephone (450) 437–2862 or (800) 363–                                                                        not exceeding 50 hours TIS.
                                                                                                       CF–2015–16, dated July 2, 2015, and                      This proposed AD would also require
                                               8023; fax (450) 433–0272; or at http://                 Emergency AD No. CF–2015–16R1,
                                               www.bellcustomer.com/files/. You may                                                                          replacing any spherical bearing
                                                                                                       dated August 6, 2015, issued by                       manufactured before January 13, 2015,
                                               review the referenced service                           Transport Canada, to correct an unsafe
                                               information at the FAA, Office of the                                                                         that has exceeded 250 hours TIS or that
                                                                                                       condition for Bell Model 429                          has an unknown number of hours TIS,
                                               Regional Counsel, Southwest Region,                     helicopters. Transport Canada advised
                                               10101 Hillwood Pkwy., Room 6N–321,                                                                            and re-identifying the P/N of the TR
                                                                                                       of several occasions where the TR pitch               pitch link assembly.
                                               Fort Worth, TX 76177.                                   link spherical bearings experienced
                                               FOR FURTHER INFORMATION CONTACT:                        early and accelerated wear.                           Differences Between This Proposed AD
                                               David Hatfield, Aviation Safety                                                                               and the Transport Canada AD
                                               Engineer, Safety Management Section,                    Actions Since AD 2015–22–02 Was
                                                                                                       Issued                                                  The Transport Canada AD requires
                                               Rotorcraft Standards Branch, FAA,                                                                             the bearing inspection within 10 hours
                                               10101 Hillwood Pkwy., Fort Worth, TX                       Since we issued AD 2015–22–02,                     TIS or before exceeding 60 hours TIS
                                               76177; telephone (817) 222–5110; email                  Transport Canada has issued AD No.                    since new, whichever occurs later. This
                                               david.hatfield@faa.gov.                                 CF–2015–16R2, dated April 17, 2017,                   proposed AD would require the bearing
                                               SUPPLEMENTARY INFORMATION:                              which supersedes AD CF–2015–16R1.                     inspection within 50 hours TIS. The
                                                                                                       According to Transport Canada, Bell has               Transport Canada AD also requires
                                               Comments Invited                                        reported that the TR pitch link assembly              replacing certain bearings within 200
                                                  We invite you to participate in this                 can be rotated during the 50-hour                     hours TIS after the initial bearing
                                               rulemaking by submitting written                        inspections to extend the serviceability              inspection or within 250 hours TIS
                                               comments, data, or views. We also                       life of the bearings. Transport Canada                since new, whichever occurs first. This
                                               invite comments relating to the                         AD No. CF–2015–16R2 requires                          proposed AD would require replacing
                                               economic, environmental, energy, or                     modified inspection procedures for the                the bearing within 200 hours of the
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                                               federalism impacts that might result                    spherical bearings and requires                       initial inspection or at the next 50 hour
                                               from adopting the proposals in this                     replacing the TR pitch link bearings (or              TIS inspection if the hours TIS of a
                                               document. The most helpful comments                     the TR pitch link assembly) with                      pitch link assembly exceed 250 hours
                                               reference a specific portion of the                     spherical bearings manufactured after                 TIS or are unknown.
                                               proposal, explain the reason for any                    January 12, 2015. Transport Canada AD
                                               recommended change, and include                         No. CF–2015–16R2 also requires re-                    Interim Action
                                               supporting data. To ensure the docket                   identifying TR pitch link assemblies                    We consider this proposed AD to be
                                               does not contain duplicate comments,                    with a different P/N after installing the             an interim action. If final action is later


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                                               39006                Federal Register / Vol. 83, No. 153 / Wednesday, August 8, 2018 / Proposed Rules

                                               identified, we might consider further                     2. Is not a ‘‘significant rule’’ under              (f) Required Actions
                                               rulemaking then.                                        DOT Regulatory Policies and Procedures                   (1) Within 50 hours time-in-service (TIS)
                                                                                                       (44 FR 11034, February 26, 1979);                     and thereafter at intervals not to exceed 50
                                               Costs of Compliance
                                                                                                         3. Will not affect intrastate aviation in           hours TIS:
                                                  We estimate that this proposed AD                    Alaska to the extent that it justifies                   (i) Perform a dimensional inspection of
                                               would affect 85 helicopters of U.S.                     making a regulatory distinction; and                  each inboard and outboard pitch link
                                               Registry. We estimate that operators                      4. Will not have a significant                      assembly for axial and radial bearing play.
                                               may incur the following costs in order                                                                        With a 10X or higher power magnifying glass,
                                                                                                       economic impact, positive or negative,
                                               to comply with this proposed AD. At an                                                                        inspect the bearing liner for a crack,
                                                                                                       on a substantial number of small entities             deterioration of the liner, and extrusion of
                                               average labor rate of $85 per hour,                     under the criteria of the Regulatory                  the liner from the plane. If there is axial or
                                               inspecting the TR pitch link assemblies                 Flexibility Act.                                      radial play that exceeds allowable limits, or
                                               would require 2 work-hours for a cost of                  We prepared an economic evaluation                  if there is a crack, deterioration of the liner,
                                               $170 per helicopter and $14,450 for the                 of the estimated costs to comply with                 or extrusion of the liner, before further flight,
                                               U.S. fleet per inspection cycle.                        this proposed AD and placed it in the                 replace the bearing.
                                               Replacing both spherical bearings in                    AD docket.                                               (ii) Inspect the pitch link assembly sealant
                                               each TR pitch link assembly would                                                                             for pin holes and voids and to determine if
                                               require 3 work-hours, and required parts                List of Subjects in 14 CFR Part 39                    the sealant thickness is 0.025 inch (0.64 mm)
                                               would cost $3,088, for a cost of $3,343                   Air transportation, Aircraft, Aviation              or less, extends over the roll staked lip by
                                               per helicopter and $284,155 for the U.S.                                                                      0.030 inch (0.76 mm) or more, and is clear
                                                                                                       safety, Incorporation by reference,
                                                                                                                                                             of the bearing ball. If there is a pin hole or
                                               fleet.                                                  Safety.                                               void, or if the sealant exceeds 0.026 inch
                                                  According to Bell’s service
                                                                                                       The Proposed Amendment                                (0.66 mm), does not extend over the roll
                                               information some of the costs of this                                                                         staked lip by 0.030 inch (0.76 mm) or more,
                                               proposed AD may be covered under                          Accordingly, under the authority                    or is not clear of the bearing ball, before
                                               warranty, thereby reducing the cost                     delegated to me by the Administrator,                 further flight, replace the bearing.
                                               impact on affected individuals. We do                   the FAA proposes to amend 14 CFR part                    (2) For pitch link assembly part number
                                               not control warranty coverage by Bell.                  39 as follows:                                        (P/N) 429–012–112–101, 429–012–112–103,
                                               Accordingly, we have included all costs                                                                       429–012–112–101FM, and 429–012–112–
                                               in our cost estimate.                                   PART 39—AIRWORTHINESS                                 103FM, within 200 hours TIS following the
                                                                                                       DIRECTIVES                                            initial inspection required by paragraph (f)(1)
                                               Authority for This Rulemaking                                                                                 of this AD, or if the hours TIS of a pitch link
                                                  Title 49 of the United States Code                   ■ 1. The authority citation for part 39               assembly exceed 250 hours TIS or are
                                               specifies the FAA’s authority to issue                  continues to read as follows:                         unknown, at the next 50 hour TIS inspection
                                                                                                                                                             required by paragraph (f)(1) of this AD:
                                               rules on aviation safety. Subtitle I,                       Authority: 49 U.S.C. 106(g), 40113, 44701.           (i) Replace each bearing P/N 429–312–107–
                                               section 106, describes the authority of                                                                       103 with a date of manufacture before
                                               the FAA Administrator. ‘‘Subtitle VII:                  § 39.13   [Amended]
                                                                                                                                                             January 13, 2015, with a bearing P/N 429–
                                               Aviation Programs,’’ describes in more                  ■ 2. The FAA amends § 39.13 by                        312–107–103 that was manufactured on or
                                               detail the scope of the Agency’s                        removing Airworthiness Directive (AD)                 after January 13, 2015.
                                               authority.                                              2015–22–02, Amendment 39–18306 (80                       (ii) Using a white permanent fine point
                                                  We are issuing this rulemaking under                 FR 65618, October 27, 2015), and                      marker or equivalent, re-identify the pitch
                                               the authority described in ‘‘Subtitle VII,              adding the following new AD:                          link assembly:
                                               Part A, Subpart III, Section 44701:                                                                              (A) Re-identify P/N 429–012–112–101 and
                                                                                                       Bell Helicopter Textron Canada Limited:
                                               General requirements.’’ Under that                                                                            429–012–112–101FM as 429–012–112–
                                                                                                            Docket No. FAA–2018–0722; Product
                                               section, Congress charges the FAA with                                                                        111FM.
                                                                                                            Identifier 2017–SW–104–AD.
                                                                                                                                                                (B) Re-identify P/N 429–012–112–103 and
                                               promoting safe flight of civil aircraft in                                                                    429–012–112–103FM as 429–012–112–
                                                                                                       (a) Applicability
                                               air commerce by prescribing regulations                                                                       113FM.
                                               for practices, methods, and procedures                    This AD applies to Model 429 helicopters
                                                                                                       with a pitch link assembly part number                   (iii) Apply a coating of DEVCON 2–TON
                                               the Administrator finds necessary for                                                                         (C–298) or equivalent over the new P/N.
                                                                                                       (P/N) 429–012–112–101, 429–012–112–103,
                                               safety in air commerce. This regulation                 429–012–112–101FM, or 429–012–112–                    (g) Special Flight Permits
                                               is within the scope of that authority                   103FM installed, certificated in any category.
                                               because it addresses an unsafe condition                                                                        Special flight permits are prohibited.
                                               that is likely to exist or develop on                   (b) Unsafe Condition
                                                                                                                                                             (h) Alternative Methods of Compliance
                                               products identified in this rulemaking                    This AD defines the unsafe condition as a           (AMOCs)
                                               action.                                                 worn pitch link. This condition, if not
                                                                                                       corrected, could result in pitch link failure            (1) The Manager, Safety Management
                                               Regulatory Findings                                     and subsequent loss of control of the                 Section, Rotorcraft Standards Branch, FAA,
                                                                                                       helicopter.                                           may approve AMOCs for this AD. Send your
                                                 We determined that this proposed AD                                                                         proposal to: David Hatfield, Aviation Safety
                                               will not have federalism implications                   (c) Affected ADs                                      Engineer, Safety Management Section,
                                               under Executive Order 13132. This                          This AD replaces AD 2015–22–02,                    Rotorcraft Standards Branch, FAA, 10101
                                               proposed AD will not have a substantial                 Amendment 39–18306 (80 FR 65618, October              Hillwood Pkwy., Fort Worth, TX 76177;
                                               direct effect on the States, on the                     27, 2015).                                            telephone (817) 222–5110; email 9-ASW-
                                               relationship between the national                                                                             FTW-AMOC-Requests@faa.gov.
                                                                                                       (d) Comments Due Date
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                                               Government and the States, or on the                                                                             (2) For operations conducted under a 14
                                                                                                         We must receive comments by October 9,              CFR part 119 operating certificate or under
                                               distribution of power and                                                                                     14 CFR part 91, subpart K, we suggest that
                                                                                                       2018.
                                               responsibilities among the various                                                                            you notify your principal inspector, or
                                               levels of government.                                   (e) Compliance                                        lacking a principal inspector, the manager of
                                                 For the reasons discussed, I certify                     You are responsible for performing each            the local flight standards district office or
                                               that this proposed regulation:                          action required by this AD within the                 certificate holding district office, before
                                                 1. Is not a ‘‘significant regulatory                  specified compliance time unless it has               operating any aircraft complying with this
                                               action’’ under Executive Order 12866;                   already been accomplished prior to that time.         AD through an AMOC.



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                                                                    Federal Register / Vol. 83, No. 153 / Wednesday, August 8, 2018 / Proposed Rules                                             39007

                                               (i) Additional Information                                • Federal eRulemaking Docket: Go to                 does not contain duplicate comments,
                                                  (1) Bell Alert Service Bulletin No. 429–15–          http://www.regulations.gov. Follow the                commenters should send only one copy
                                               16, Revision B, dated June 15, 2016, which              online instructions for sending your                  of written comments, or if comments are
                                               is not incorporated by reference, contains              comments electronically.                              filed electronically, commenters should
                                               additional information about the subject of               • Fax: 202–493–2251.                                submit only one time.
                                               this AD. For service information identified in            • Mail: Send comments to the U.S.                      We will file in the docket all
                                               this AD, contact Bell Helicopter Textron                                                                      comments that we receive, as well as a
                                               Canada Limited, 12,800 Rue de l’Avenir,
                                                                                                       Department of Transportation, Docket
                                               Mirabel, Quebec J7J1R4; telephone (450)                 Operations, M–30, West Building                       report summarizing each substantive
                                               437–2862 or (800) 363–8023; fax (450) 433–              Ground Floor, Room W12–140, 1200                      public contact with FAA personnel
                                               0272; or at http://www.bellcustomer.com/                New Jersey Avenue SE, Washington, DC                  concerning this proposed rulemaking.
                                               files/. You may review a copy of the service            20590–0001.                                           Before acting on this proposal, we will
                                               information at the FAA, Office of the                     • Hand Delivery: Deliver to the                     consider all comments we receive on or
                                               Regional Counsel, Southwest Region, 10101               ‘‘Mail’’ address between 9 a.m. and 5                 before the closing date for comments.
                                               Hillwood Pkwy., Room 6N–321, Fort Worth,                p.m., Monday through Friday, except                   We will consider comments filed after
                                               TX 76177.                                                                                                     the comment period has closed if it is
                                                  (2) The subject of this AD is addressed in           Federal holidays.
                                               Transport Canada AD No. CF–2015–16R2,                                                                         possible to do so without incurring
                                                                                                       Examining the AD Docket                               expense or delay. We may change this
                                               dated April 17, 2017. You may view the
                                               Transport Canada AD on the internet at                    You may examine the AD docket on                    proposal in light of the comments we
                                               http://www.regulations.gov in the AD Docket.            the internet at http://                               receive.
                                               (j) Subject
                                                                                                       www.regulations.gov by searching for                  Discussion
                                                                                                       and locating Docket No. FAA–2018–
                                                  Joint Aircraft Service Component (JASC)                                                                       We issued AD 2016–25–19,
                                                                                                       0669; or in person at Docket Operations
                                               Code: 6720 Tail Rotor Control System.                                                                         Amendment 39–18745 (81 FR 95854,
                                                                                                       between 9 a.m. and 5 p.m., Monday
                                                 Issued in Fort Worth, Texas, on July 23,              through Friday, except Federal holidays.              December 29, 2016) (AD 2016–25–19),
                                               2018.                                                   The AD docket contains this proposed                  for Airbus Helicopters Model AS350B3
                                               Scott A. Horn,                                          AD, the European Aviation Safety                      and EC130B4 helicopters with the
                                               Deputy Director for Regulatory Operations,              Agency (EASA) AD, the economic                        ARRIEL 2B1 engine with the two-
                                               Compliance & Airworthiness Division,                    evaluation, any comments received and                 channel Full Authority Digital Engine
                                               Aircraft Certification Service.                                                                               Control (FADEC) and with new twist
                                                                                                       other information. The street address for
                                               [FR Doc. 2018–16637 Filed 8–7–18; 8:45 am]              Docket Operations (telephone 800–647–                 grip modification (MOD) 073254 (for the
                                               BILLING CODE 4910–13–P                                  5527) is in the ADDRESSES section.                    Model AS350B3 helicopter) or MOD
                                                                                                       Comments will be available in the AD                  073773 (for the Model EC130B4
                                                                                                       docket shortly after receipt.                         helicopter). AD 2016–25–19 requires
                                               DEPARTMENT OF TRANSPORTATION                              For service information identified in               repetitively inspecting the wiring,
                                                                                                       this proposed rule, contact Airbus                    performing an insulation test, inspecting
                                               Federal Aviation Administration                                                                               the pilot and copilot throttle twist grip
                                                                                                       Helicopters, 2701 N. Forum Drive,
                                                                                                       Grand Prairie, TX 75052; telephone                    controls, and testing the pilot and
                                               14 CFR Part 39                                                                                                copilot throttle twist grip controls for
                                                                                                       (972) 641–0000 or (800) 232–0323; fax
                                               [Docket No. FAA–2018–0669; Product                      (972) 641–3775; or at http://                         proper functioning. AD 2016–25–19 was
                                               Identifier 2017–SW–041–AD]                              www.helicopters.airbus.com/website/                   prompted by AD No. 2013–0191–E,
                                                                                                       en/ref/Technical-Support_73.html. You                 dated August 22, 2013 (EASA AD 2013–
                                               RIN 2120–AA64
                                                                                                       may review service information at the                 0191–E), issued by EASA, which is the
                                               Airworthiness Directives; Airbus                        FAA, Office of the Regional Counsel,                  Technical Agent for the Member States
                                               Helicopters (Previously Eurocopter                      Southwest Region, 10101 Hillwood                      of the European Union. EASA advised
                                               France)                                                 Pkwy, Room 6N–321, Fort Worth, TX                     that the switches in the engine ‘‘IDLE’’
                                                                                                       76177.                                                or ‘‘FLIGHT’’ control system could be
                                               AGENCY: Federal Aviation                                                                                      affected by the corrosive effects of a salt-
                                               Administration (FAA), DOT.                              FOR FURTHER INFORMATION CONTACT:                      laden atmosphere, which could lead to
                                               ACTION: Notice of proposed rulemaking                   George Schwab, Aviation Safety                        engine power loss. EASA AD 2013–
                                               (NPRM).                                                 Engineer, Safety Management Section,                  0191–E required repetitive inspections
                                                                                                       Rotorcraft Standards Branch, FAA,                     for corrosion, application of corrosion
                                               SUMMARY:   We propose to supersede                      10101 Hillwood Pkwy., Fort Worth, TX                  protection on the switches, and testing
                                               Airworthiness Directive (AD) 2016–25–                   76177; telephone (817) 222–5110; email
                                               19 for Airbus Helicopters (previously                                                                         of the insulation and switches of the
                                                                                                       george.schwab@faa.gov.                                engine idle and flight control system.
                                               Eurocopter France) Model AS350B3 and
                                                                                                       SUPPLEMENTARY INFORMATION:                            The actions required in AD 2016–25–19
                                               EC130B4 helicopters. AD 2016–25–19
                                               requires inspecting the pilot’s and co-                 Comments Invited                                      are intended to prevent unintended
                                               pilot’s throttle twist for proper                                                                             touchdown to the ground at a flight-idle
                                                                                                          We invite you to participate in this               power setting during a practice
                                               operation. This proposed AD would                       rulemaking by submitting written
                                               retain the requirements of AD 2016–25–                                                                        autorotation, damage to the helicopter,
                                                                                                       comments, data, or views. We also                     and injury to occupants.
                                               19 and add certain model helicopters to                 invite comments relating to the
                                               the applicability. The actions of this                                                                        Actions Since AD 2016–25–19 Was
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                                                                                                       economic, environmental, energy, or
                                               proposed AD are intended to address                     federalism impacts that might result                  Issued
                                               the unsafe condition on these                           from adopting the proposals in this                     Since we issued AD 2016–25–19,
                                               helicopters.                                            document. The most helpful comments                   EASA issued AD No. 2017–0052, dated
                                               DATES: We must receive comments on                      reference a specific portion of the                   March 24, 2017, which superseded
                                               this proposed AD by October 9, 2018.                    proposal, explain the reason for any                  EASA AD No. 2013–0191–E, dated
                                               ADDRESSES: You may send comments by                     recommended change, and include                       August 22, 2013. EASA advised that
                                               any of the following methods:                           supporting data. To ensure the docket                 Airbus Helicopters had added


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Document Created: 2018-08-08 02:04:59
Document Modified: 2018-08-08 02:04:59
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 October 9, 2018.
ContactDavid Hatfield, 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 Citation83 FR 39004 
RIN Number2120-AA64
CFR AssociatedAir Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

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