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PROPOSED AD BELL HELICOPTER TEXTRON CANADA LIMITED: Docket No. FAA-2020-0860; Product Identifier 2019-SW-005-AD.
(a) COMMENTS DUE DATE

    The FAA must receive comments by November 16, 2020.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies  to Bell Helicopter  Textron Canada Limited  Model 429
    helicopters,  certificated  in  any  category,  serial  numbers  57001
    through 57351 inclusive.

(d) SUBJECT

    Joint Aircraft Service Component (JASC) Code 6200, Main rotor system.

(e) REASON

    This AD was prompted by the  introduction of a new life limit  for the
    centrifugal force bearing (CFB). The FAA is issuing this AD to address
    a CFB remaining in service beyond its fatigue life. Failure to observe
    the CFB  life limit  could result  in excessive  vibration and loss of
    control of the helicopter.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) REQUIRED ACTIONS

    For each CFB  having part number  429-310-003-103 (the affected  CFB):
    Within 50 hours time-in-service, determine the accumulated  retirement
    index number (RIN). For purposes of this AD, count 1 RIN each time one
    or both engines are started. If any affected CFB has accumulated 8,000
    or more total RIN, before further flight, remove the affected CFB from
    service. If  any affected  CFB has  accumulated less  than 8,000 total
    RIN, create a component history card or equivalent record indicating a
    life limit of 8,000 total  RIN. Thereafter, continue to count  RIN and
    record the  life limit  of the  affected CFB  on its component history
    card or  equivalent record  and remove  the affected  CFB from service
    before accumulating 8,000 total RIN.

(h) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The Manager, Rotorcraft Standards Branch,  FAA,  may approve AMOCs for
    this AD.  Send your proposal to: Matt Fuller, AD Program Manager, Con-
    tinued  Operational  Safety  Branch,  Airworthiness  Products Section,
    General Aviation and Rotorcraft Unit,  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, notify your principal inspector or
    lacking  a  principal  inspector,  the  manager  of  the  local flight
    standards  district  office or  certificate  holding district  office,
    before operating any aircraft complying with this AD through an AMOC.

(i) RELATED INFORMATION

(1) Bell Model 429  Maintenance Planning Information BHT-429-MPI,  Chapter
    4, Airworthiness Limitations Schedule,  DMC-429-A-04-00-00-00A-288A-A,
    Issue  1,  dated  January 10, 2019,   which  is  not  incorporated  by
    reference,  contains additional information  about the subject of this
    AD. For service information identified in this AD,  contact Bell Heli-
    copter 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  https://www.bellcustomer.com.  You may view 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 CF-2019-03,
    dated January 31, 2019.  This Transport Canada AD  may be found in the
    AD docket on the internet at https://www.regulations.gov  by searching
    for and locating Docket No. FAA-2020-0860.

Issued on September 25, 2020.  Lance T. Gant, Director,  Compliance & Air-
worthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments  on this proposed AD  by November 16,
2020.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0860; Product Identifier 2019-SW-005-AD]
RIN 2120-AA64

Airworthiness Directives; Bell Helicopter Textron Canada Limited
Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Bell Helicopter Textron Canada Limited Model 429
helicopters. This proposed AD was prompted by the introduction of a new
life limit for the centrifugal force bearing (CFB). This proposed AD
would require determining the accumulated retirement index number (RIN)
and removing each affected CFB from service before it accumulates 8,000
total RIN. The FAA is proposing this AD to address the unsafe condition
on these products.

DATES: The FAA must receive comments on this proposed AD by November
16, 2020.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:

Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the
instructions for submitting comments.

Fax: 202-493-2251.

Mail: U.S. Department of Transportation, Docket Operations, M-30, West
Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE,
Washington, DC 20590.

Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.

For service information identified in this NPRM, contact Bell
Helicopter Textron Canada Limited, 12,800 Rue de l'Avenir, Mirabel,
Quebec J7J 1R4; telephone 450-437-2862 or 800-363-8023; fax 450-433-
0272; or at https://www.bellcustomer.com. You may view this service
information at the FAA, Office of the Regional Counsel, Southwest
Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177.

Examining the AD Docket

You may examine the AD docket on the internet at https://www.regulations.
gov by searching for and locating Docket No. FAA-2020-0860;
or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this AD, the Transport Canada Civil Aviation (TCCA) AD, any comments
received, and other information. The street address for Docket
Operations is listed above. Comments will be available in the AD docket
shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Matt Fuller, AD Program Manager,
Continued Operational Safety Branch, Airworthiness Products Section,
General Aviation and Rotorcraft Unit, FAA, 10101 Hillwood Pkwy., Fort
Worth, TX 76177; telephone 817-222-5110; email matthew.fuller@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under the ADDRESSES section. Include "Docket No. FAA-2020-0860;
Product Identifier 2019-SW-005-AD" at the beginning of your comments.
The most helpful comments reference a specific portion of the proposal,
explain the reason for any recommended change, and include supporting
data. The FAA will consider all comments received by the closing date
and may amend this NPRM because of those comments.

Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
https://www.regulations.gov, including any personal information you
provide. The FAA will also post a report summarizing each substantive
verbal contact received about this NPRM.

Confidential Business Information

CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as "PROPIN." The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to Matt
Fuller, AD Program Manager, Continued Operational Safety Branch,
Airworthiness Products Section, General Aviation and Rotorcraft Unit,
FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222-
5110; email matthew.fuller@faa.gov. Any commentary that the FAA
receives which is not specifically designated as CBI will be placed in
the public docket for this rulemaking.

Discussion

TCCA, which is the aviation authority for Canada, issued Transport
Canada AD CF-2019-03, dated January 31, 2019 (referred to after this as
the Mandatory Continuing Airworthiness Information, or "the MCAI"),
to correct an unsafe condition for certain Bell Helicopter Textron
Canada Limited Model 429 helicopters. TCCA advises that an
airworthiness limitations schedule document introduces a new life limit
for CFB part number (P/N) 429-310-003-103, a component that was not
previously included. Failure to observe the CFB life limit could result
in excessive vibration and loss of control of the helicopter.

You may examine the MCAI in the AD docket on the internet at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2020-0860.

Other Related Service Information

Bell Helicopter has issued Bell Model 429 Maintenance Planning
Information BHT-429-MPI, Chapter 4, Airworthiness Limitations Schedule,
DMC-429-A-04-00-00-00A-288A-A, Issue 1, dated January 10, 2019. This
service information describes new maintenance requirements and
airworthiness limitations.

FAA's Determination

This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to the FAA's bilateral agreement with the State of Design Authority,
the FAA has been notified of the unsafe condition described in the MCAI
and service information referenced above. The FAA is proposing this AD
after evaluating all the relevant information and determining the
unsafe condition described previously is likely to exist or develop on
other products of the same type design.

Proposed Requirements of This NPRM

This proposed AD would require, for each CFB having P/N 429-310-
003-103, determining the accumulated RIN and removing the CFB from
service before it accumulates 8,000 total RIN. If the new life limit
has not been reached, this proposed AD would require creating a
component history card or equivalent record indicating the new life
limit and removing the CFB from service before reaching the new life
limit.

Costs of Compliance

The FAA estimates that this proposed AD affects 85 helicopters of
U.S. registry. The FAA estimates the following costs to comply with
this proposed AD:

Estimated Costs for Required Actions

Labor cost
Parts cost
Cost per helicopter
Cost on U.S. operators
28 work-hours x $85 per hour = $2,380 $42,576 ($10,644 per bearing x 4 blades)
$44,956
$3,821,260

Authority for This Rulemaking

Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.

The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.

Regulatory Findings

The FAA 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 above, I certify this proposed regulation:

(1) Is not a "significant regulatory action" under Executive
Order 12866,

(2) Will not affect intrastate aviation in Alaska, and

(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

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

The 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

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]

2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):