preamble attached >>>
ADs updated daily at www.Tdata.com
PROPOSED AD BELL TEXTRON CANADA LIMITED (TYPE CERTIFICATE PREVIOUSLY HELD BY BELL HELICOPTER TEXTRON CANADA LIMITED): Docket No. FAA-2021-0575; Project Identifier MCAI-2020-00545-R.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive (AD)  by
    September 7, 2021.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD  applies to  Bell  Textron Canada  Limited  (type certificate
    previously held by Bell  Helicopter Textron Canada Limited)  Model 429
    helicopters,  certificated  in  any  category,  serial  numbers  57001
    through 57210 inclusive, 57212 through 57344 inclusive, 57346  through
    57371 inclusive, 57374 through 57377 inclusive, and 57380.

(d) SUBJECT

    Joint Aircraft Service Component (JASC) Code: 6700, Rotorcraft  Flight
    Control.

(e) UNSAFE CONDITION

    This  AD  was  prompted by  reports  of  incorrectly staked  spherical
    bearings in  the directional  control bellcrank  assembly. The  FAA is
    issuing this AD  to address incorrectly  staked spherical bearings  in
    the directional  control bellcrank  assembly. This  condition, if  not
    addressed,  could result  in wear  or elongation  of the  bore in  the
    bellcrank,  which  could  result  in  reduced  helicopter  directional
    control.

(f) COMPLIANCE

    Comply  with this  AD within  the compliance  times specified,  unless
    already done.

(g) REQUIRED INSPECTION AND CORRECTIVE ACTIONS

    Within 25  hours time-in-service  (TIS) or  90 days,  whichever occurs
    first after the effective date  of this AD: Inspect the  lower surface
    of the spherical bearing on the directional control bellcrank assembly
    to  determine  if  it  is  properly  staked,  in  accordance  with the
    Accomplishment Instructions, Part  I, step 7.,  of Bell Alert  Service
    Bulletin 429-19-50, Revision B,  dated December 19, 2019  (BASB 429-19
    -50, Revision B). After the inspection, before further flight, do  the
    applicable action required by paragraph (g)(1) or (2) of this AD.

(1) If  the lower  surface of  the spherical  bearing is improperly staked
    (any discrepancy is found e.g., the witness marks are not present  and
    intact or the  staked lip is  not uniform along  the chamfer): Inspect
    the  bore  in the  bellcrank  assembly for  excessive  wear (including
    mechanical  or   corrosion  damage   that  exceed   0.001  inch  (0.03
    millimeter)  maximum depth  for \1/4\  of the  circumference, and  any
    cracking); in accordance with the Accomplishment Instructions, Part I,
    steps 10. through 13., of BASB 429-19-50, Revision B, and depending on
    the  findings,  do  the  applicable  actions  required  by   paragraph
    (g)(1)(i) or (ii) of this AD before further flight.

(i) If the bore in the  bellcrank assembly shows signs of excessive  wear:
    Repair the bellcrank, including re-identifying the bellcrank  assembly
    part number, in accordance with the Accomplishment Instructions,  Part
    II, steps 1. through 13., of BASB 429-19-50, Revision B.

(ii) If the bore diameter  is within 0.001 inch (0.03  millimeter) maximum
     depth  for  \1/4\  of  the  circumference:  Install  a  new spherical
     bearing, in accordance with the Accomplishment Instructions, Part II,
     steps 4. through 12., of BASB 429-19-50, Revision B.

(2) If  the lower  surface of  the spherical  bearing is  properly staked:
    Inspect the upper surface of the spherical bearing on the  directional
    control bellcrank assembly to determine  if it is properly staked,  in
    accordance with the Accomplishment Instructions, Part I, steps 8.  and
    9., of BASB 429-19-50, Revision  B, and depending on the  findings, do
    the applicable actions required by paragraph (g)(2)(i) or (ii) of this
    AD before further flight.

(i) If  the spherical  bearing is  properly staked:  No further  action is
    required by this AD.

(ii) If the spherical bearing  is not properly staked (any  discrepancy is
     found  e.g., the  witness marks  are not  present and  intact or  the
     staked lip is not uniform along the chamfer): Inspect the bore in the
     bellcrank  assembly  for  excessive  wear  (including  mechanical  or
     corrosion damage  that exceed  0.001 inch  (0.03 millimeter)  maximum
     depth  for  \1/4\  of  the  circumference,  and  any  cracking),   in
     accordance with  the Accomplishment  Instructions, Part  I, steps 10.
     through 13.,  of BASB  429-19-50, Revision  B, and  depending on  the
     findings,   do   the  applicable   actions   required  by   paragraph
     (g)(2)(ii)(A) or (B) of this AD before further flight.

(A) If the bore in the  bellcrank assembly shows signs of excessive  wear:
    Repair the bellcrank, including re-identifying the bellcrank  assembly
    part number, in accordance  with the Accomplishment Instruction,  Part
    II, steps 1. through 13., of BASB 429-19-50, Revision B.

(B) If the  bore diameter is  within 0.001 inch  (0.03 millimeter) maximum
    depth for \1/4\ of the circumference: Install a new spherical bearing,
    in accordance with the Accomplishment Instructions, Part II, steps  4.
    through 12., of BASB 429-19-50, Revision B.

(h) REQUIRED POST REPAIR INSPECTIONS

    For  any  helicopter  on  which the  bellcrank  has  been  repaired as
    required by paragraphs (g)(1)(i)  or (g)(2)(ii)(A) of this  AD: Within
    100 hours  TIS after  the repair,  and thereafter  at intervals not to
    exceed  100 hours  TIS, inspect  the lower  surface of  the  spherical
    bearing  to  determine  if  it  has  moved,  in  accordance  with  the
    Accomplishment Instructions,  Part III,  step 7.,  of BASB  429-19-50,
    Revision B.  If the  spherical bearing  has moved  (is loose):  Before
    further  flight,  inspect  the  bore  in  the  bellcrank  assembly  to
    determine if the diameter  exceeds 0.6283 inch (15.9588  millimeters),
    in accordance with the Accomplishment Instructions, Part III, steps 8.
    through 11., of BASB 429-19-50, Revision B.

(1) If the diameter of the  bore in the bellcrank assembly exceeds  0.6283
    inch  (15.9588  millimeters):   Before  further  flight   replace  the
    bellcrank assembly.

(2) If the diameter of the bore in the bellcrank assembly does not  exceed
    0.6283 inch (15.9588 millimeters): Before further flight install a new
    spherical bearing in accordance with the Accomplishment  Instructions,
    Part II, steps 4. through 12., of BASB 429-19-50, Revision B.

(i) TERMINATING ACTION

    Replacement of a bellcrank assembly  with a new part (never  installed
    on a  helicopter or  has accumulated  zero hours  TIS) is  terminating
    action for the requirements of this AD for that helicopter only.

(j) CREDIT FOR PREVIOUS ACTIONS

    This paragraph provides credit  for actions required by  paragraph (g)
    of this AD, if those actions were performed before the effective  date
    of  this  AD using  the  service information  identified  in paragraph
    (j)(1) or (2) of this AD.

(1) Bell Alert Service Bulletin 429-19-50, dated November 27, 2019.

(2) Bell Alert Service Bulletin  429-19-50, Revision A, dated December  2,
    2019.

(k) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The Manager, International  Validation Branch, FAA, has  the authority
    to approve AMOCs for this AD, if requested using the procedures  found
    in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to
    your principal inspector or local Flight Standards District Office, as
    appropriate. If  sending information  directly to  the manager  of the
    International  Validation  Branch, send  it  to the  attention  of the
    person identified in paragraph (l)(1)  of this AD. Information may  be
    emailed to: 9-AVS-AIR-730-AMOC@faa.gov.

(2) Before  using  any approved  AMOC, notify  your appropriate  principal
    inspector, or lacking a principal inspector, the manager of the  local
    flight standards district office/certificate  holding district office.

(l) RELATED INFORMATION

(1) For more information about this AD, contact Andrea Jimenez,  Aerospace
    Engineer, COS Program  Management Section, Operational  Safety Branch,
    Compliance &  Airworthiness Division,  FAA, 1600  Stewart Ave.,  Suite
    410,  Westbury,  NY  11590; telephone  (516)  228-7330;  email andrea.
    jimenez@faa.gov.

(2) For service  information identified in  this AD, contact  Bell Textron
    Canada  Limited,  12,800 Rue  de  l'Avenir, Mirabel,  Quebec  J7J 1R4,
    Canada;  telephone  1-450-437-2862  or  1-800-363-8023;  fax 1-450-433
    -0272;      email      productsupport@bellflight.com;      or       at
    https://www.bellflight.com/support/contact-support. You may view  this
    referenced  service information  at the  FAA, Office  of the  Regional
    Counsel, Southwest  Region, 10101  Hillwood Pkwy.,  Room 6N-321,  Fort
    Worth, TX 76177. For information on the availability of this  material
    at the FAA, call (817) 222-5110.

(3) The subject of this AD is addressed in Transport Canada AD CF-2020-11,
    dated April  16, 2020.  You may  view the  Transport Canada  AD on the
    internet at https://www.regulations.gov in Docket No. FAA-2021-0575.

Issued  on July  15, 2021.  Ross Landes,  Deputy Director  for  Regulatory
Operations, Compliance  & Airworthiness  Division, Aircraft  Certification
Service.

DATES: The  FAA must  receive comments  on this  proposed AD  September 7,
2021.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


14 CFR Part 39

[Docket No. FAA-2021-0575; Project Identifier MCAI-2020-00545-R]
RIN 2120-AA64

Airworthiness Directives; Bell Textron Canada Limited (Type
Certificate Previously Held by 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 Textron Canada Limited (type certificate previously
held by Bell Helicopter Textron Canada Limited) (Bell) Model 429
helicopters. This proposed AD was prompted by reports of incorrectly
staked spherical bearings in the directional control bellcrank
assembly. This proposed AD would require a one-time inspection of the
lower surface of the spherical bearing in the directional control
bellcrank assembly to determine if it is properly staked and, depending
on the findings, applicable corrective actions. For certain
helicopters, this proposed AD would also require repetitive inspections
and, depending on the findings, applicable corrective actions. This
proposed AD would also provide a terminating action for the repetitive
inspections. The FAA is proposing this AD to address the unsafe
condition on these products.

DATES: The FAA must receive comments on this proposed AD September 7, 2021.

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 between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays.

For service information identified in this NPRM, contact Bell
Textron Canada Limited, 12,800 Rue de l'Avenir, Mirabel, Quebec J7J
1R4, Canada; telephone 1-450-437-2862 or 1-800-363-8023; fax 1-450-433-
0272; email productsupport@bellflight.com; or at
https://www.bellflight.com/support/contact-support.

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. For
information on the availability of this material at the FAA, call (817)
222-5110.

Examining the AD Docket


You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0575; 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 NPRM, the
Transport Canada AD, any comments received, and other information. The
street address for Docket Operations is listed above.

FOR FURTHER INFORMATION CONTACT: Andrea Jimenez, Aerospace Engineer,
COS Program Management Section, Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY
11590; telephone (516) 228-7330; email andrea.jimenez@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 ADDRESSES. Include "Docket No. FAA-2021-0575; Project Identifier
MCAI-2020-00545-R" 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 proposal 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 agency 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
Andrea Jimenez, Aerospace Engineer, COS Program Management Section,
Operational Safety Branch, Compliance & Airworthiness Division, FAA,
1600 Stewart Ave., Suite 410, Westbury, NY 11590; telephone (516) 228-
7330; email andrea.jimenez@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.

Background


Transport Canada, which is the aviation authority for Canada, has
issued Canadian AD CF-2020-11, dated April 16, 2020 (Transport Canada
AD CF-2020-11), to correct an unsafe
condition for Bell Textron Canada Limited (Bell) Model 429 helicopters,
serial numbers 57001 through 57210, 57212 through 57344, 57346 through
57371, 57374 through 57377, and 57380. Transport Canada advises that
there are reports of incorrectly staked spherical bearings in the
directional control bellcrank assembly. This condition, if not
addressed, could result in wear or elongation of the bore in the
bellcrank, which could result in reduced helicopter directional
control.

Accordingly, Transport Canada AD CF-2020-11 requires a one-time
inspection to determine if a spherical bearing is properly staked in
the directional control bellcrank assembly, and, depending on the
findings, replacement of the spherical bearing with a new spherical
bearing, repair of an affected bellcrank assembly and repetitive
inspections of that repaired bellcrank assembly, or replacement of the
affected bellcrank assembly with a serviceable part. Transport Canada
AD CF-2020-11 also provides terminating actions for the requirements of
the Canadian AD.

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
the FAA's bilateral agreement with Canada, Transport Canada, its
technical representative, has notified the FAA of the unsafe condition
described in its AD. The FAA is proposing this AD after evaluating all
known relevant information and determining that the unsafe condition
described previously is likely to exist or develop on other helicopters
of the same type design.

Related Service Information Under 1 CFR Part 51


The FAA reviewed Bell Alert Service Bulletin 429-19-50, Revision B,
dated December 19, 2019. This service information specifies procedures
for an initial inspection of the lower surface of the spherical bearing
in the directional control bellcrank assembly to determine if it is
properly staked, additional inspections, and corrective actions. The
corrective actions include installation of a new spherical bearing,
repair (including re-identification of the bellcrank assembly part
number), and replacement of the bellcrank assembly. The additional
inspections include an inspection of the upper surface of the spherical
bearing in the directional control bellcrank assembly to determine if
it is properly staked, an inspection of the bore in the bellcrank
assembly for excessive wear (including mechanical or corrosion damage
that exceed 0.001 inch (0.03 millimeter) maximum depth for \1/4\ of the
circumference, and any cracking); and, for any helicopter with a
bellcrank assembly that is repaired, repetitive inspections of the
lower surface of the spherical bearing to determine if it has moved.

This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in the ADDRESSES section.

Other Related Service Information


The FAA also reviewed Bell Alert Service Bulletin 429-19-50, dated
November 27, 2019; and Revision A, dated December 2, 2019. Bell Alert
Service Bulletin 429-19-50, dated November 27, 2019, specifies
procedures for an initial inspection of the spherical bearing in the
directional control bellcrank assembly to determine if it is properly
staked and replacement of the spherical bearing with a new spherical
bearing if it is determined that the spherical bearing was not properly
staked.

Bell Alert Service Bulletin 429-19-50, Revision A, dated December
2, 2019, specifies procedures for an initial inspection of the lower
surface of the spherical bearing in the directional control bellcrank
assembly to determine if it is properly staked, additional inspections,
and corrective actions. The corrective actions include installation of
a new spherical bearing. The additional inspections include an
inspection of the upper surface of the spherical bearing in the
directional control bellcrank assembly to determine if it is properly
staked, and an inspection of the bore in the bellcrank assembly for
excessive wear.

Proposed AD Requirements in This NPRM


This proposed AD would require accomplishing the actions specified
in the service information already described.

Costs of Compliance


The FAA estimates that this AD, if adopted as proposed, would
affect 120 helicopters of U.S. registry. The FAA estimates the
following costs to comply with this proposed AD:

Estimated Costs

ACTION
LABOR COST
PARTS COST
COST PER PRODUCT
COST ON U.S. OPERATORS
Inspection 1 work-hour x $85 per hour = $85 per inspection cycle
$0
$85
$10,200

The FAA estimates the following costs to do any necessary actions
that would be required based on the results of the proposed inspection.
The agency has no way of determining the number of helicopters that
might need these actions:

On-Condition Costs

ACTION
LABOR COST
PARTS COST
COST PER PRODUCT
Replacement Spherical Bearing 7 work-hours x $85 per hour = $595.
$56
$651.
Repair/replacement Bellcrank 4 work-hours x $85 per hour = $340.
2,856
3,196.
Repetitive Inspections 1 work-hour x $85 per hour= $85 per inspection cycle
0
85 per inspection cycle.

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, I certify this proposed regulation:

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

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

(3) Would 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: