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PROPOSED AD AIRBUS CANADA LIMITED PARTNERSHIP (TYPE CERTIFICATE PREVIOUSLY HELD BY C SERIES AIRCRAFT LIMITED PARTNERSHIP (CSALP); BOMBARDIER, INC.): Docket No. FAA-2020-0971; Product Identifier 2020-NM-083-AD.
(a) COMMENTS DUE DATE

    The FAA must receive comments by December 14, 2020.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to Airbus Canada Limited Partnership (type certificate
    previously  held  by  C Series  Aircraft Limited Partnership  (CSALP);
    Bombardier, Inc.) airplanes,  certificated in any category, as identi-
    fied in paragraphs (c)(1) and (2) of this AD.

(1) Model BD-500-1A10 airplanes, serial numbers 50010 through 50018 inclu-
    sive, and 50020 through 50041 inclusive.

(2) Model BD-500-1A11 airplanes, serial numbers 55003 through 55016 inclu-
    sive, 55018 through 55054 inclusive, and 55056.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 28, Fuel.

(e) REASON

    This proposed AD was prompted by a report that threaded fuel couplings
    were incorrectly installed at final  assembly and in service. The  FAA
    is  issuing  this AD  to  address loose  fuel  couplings, which  could
    eventually  disconnect  and  could  lead  to  fuel  starvation  of the
    auxiliary power unit (APU) and pose a risk of fire.

(f) COMPLIANCE

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

(g) FUNCTIONAL TEST OF THE APU FUEL FEED LINE SHROUD

    Within 4,000 flight hours  after the effective date of this AD,  do an
    initial functional test of the APU fuel feed line shroud,  in  accord-
    ance with Part A  of the Accomplishment Instructions  of Airbus Canada
    Service Bulletin BD500-282009, Issue 003 dated August 14, 2020. There-
    after, repeat  the functional  test at  intervals not  to exceed 4,000
    flight hours.  If any functional test reveals a leak,  before  further
    flight, do the applicable actions  specified in paragraph (h) of  this
    AD.

(h) INSPECTION AND TORQUE OF APU FUEL FEED LINE SHROUD COUPLINGS

(1) Except as required  by paragraph (g)  of this AD:  Within 9,350 flight
    hours or within 56 months,  whichever occurs first after the effective
    date of this AD:  Do a general visual inspection  of the APU feed line
    shroud for any loose couplings,  and  tighten  any  loose couplings as
    applicable,  in accordance  with Part B of the Accomplishment Instruc-
    tions of Airbus Canada Service Bulletin BD500-282009, Issue 003, dated
    August 14, 2020.

(2) For airplanes  on which the inspection and tightening  of the APU fuel
    feed line shroud couplings was done  before the effective date of this
    AD,  in  accordance  with Part B of the Accomplishment Instructions of
    Airbus Canada Service Bulletin BD500-282009, Issue 001, dated December
    13, 2019:  Within 9,350 flight hours  or  56 months,  whichever occurs
    first after the effective date of this AD, do a general visual inspec-
    tion of the APU feed line shroud for any loose couplings between frame
    (FR) 63 and FR 80,  and tighten any loose couplings as applicable,  in
    accordance with Part C  of  the  Accomplishment Instructions of Airbus
    Canada Service Bulletin BD500-282009, Issue 003 dated August 14, 2020.

(i) TERMINATING ACTION FOR THE FUNCTIONAL TESTS

    The inspection and  tightening  of the APU fuel feed line shroud coup-
    lings as specified in paragraph (h)  of this AD  terminate the initial
    and repetitive functional tests of the APU fuel feed line shroud spec-
    ified in paragraph (g) of this AD.

(j) CREDIT FOR PREVIOUS ACTIONS

(1) 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  Airbus Canada Service Bulletin BD500-282009,  Issue
    001, dated December 13, 2019, or Airbus Canada Service Bulletin BD500-
    282009, Issue 002, dated March 18, 2020,  provided the functional test
    is repeated  at  intervals not to exceed 4,000 flight hours  from  the
    completion of those actions specified in paragraph (g) of this AD.

(2) This paragraph provides credit for actions required  by  paragraph (h)
    (1) of this AD,  if those actions were performed  before the effective
    date  of this  AD  using  Airbus Canada Service Bulletin BD500-282009,
    Issue 001, dated December 13, 2019.

(k) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs):  The Manager,  New York ACO
    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 certification office,  send
    it to ATTN: Program  Manager, Continuing Operational Safety,  FAA, New
    York ACO Branch, 1600 Stewart  Avenue, Suite 410, Westbury, NY  11590;
    telephone 516-228-7300;  fax 516-794-5531.  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.

(2) Contacting the Manufacturer:  For any requirement in this AD to obtain
    instructions   from   a  manufacturer,   the   instructions  must   be
    accomplished using  a method  approved by  the Manager,  New York  ACO
    Branch,  FAA; or  Transport Canada  Civil Aviation  (TCCA); or  Airbus
    Canada Limited Partnership's TCCA Design Approval Organization  (DAO).
    If approved by the DAO, the approval must include the DAO-  authorized
    signature.

(l) RELATED INFORMATION

(1) Refer   to   Mandatory  Continuing  Airworthiness  Information  (MCAI)
    Canadian AD CF-2020-14, dated April 30, 2020, for related information.
    This MCAI may be found in the AD docket  on the internet  at  https://
    www.regulations.gov by searching for and locating Docket No. FAA-2020-
    0971.

(2) For more information about this AD, contact Darren Gassetto, Aerospace
    Engineer, Mechanical Systems and Administrative Services Section, FAA,
    New York ACO Branch, 1600 Stewart Ave., Suite 410, Westbury, NY 11590;
    telephone 516-228-7323;  fax 516-794-5531;  email 9-avs-nyaco-cos@faa.
    gov.

(3) For service information identified  in this AD,  contact Airbus Canada
    Limited Partnership,  13100 Henri-Fabre Boulevard, Mirabel, Quebec J7N
    3C6, Canada; telephone 450-476-7676; email a220_crc@abc.airbus; inter-
    net http://a220world.airbus.com. You may view this service information
    at the FAA, Airworthiness Products Section, Operational Safety Branch,
    2200 South 216th St, Des Moines, WA. For information on the availabil-
    ity of this material at the FAA, call 206-231-3195.

Issued on October 22, 2020. Lance T Gant, Director, Compliance & Airworth-
iness Division, Aircraft Certification Service.

DATES: The FAA must receive comments  on this proposed AD  by December 14,
2020.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0971; Product Identifier 2020-NM-083-AD]
RIN 2120-AA64

Airworthiness Directives; Airbus Canada Limited Partnership (Type
Certificate Previously Held by C Series Aircraft Limited Partnership
(CSALP); Bombardier, Inc.) Airplanes

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 Airbus Canada Limited Partnership Model BD-500-1A10 and BD-
500-1A11 airplanes. This proposed AD was prompted by a report that
threaded fuel couplings were incorrectly installed at final assembly
and in service. This proposed AD would require repetitive functional
tests of the auxiliary power unit (APU) fuel feed line shroud, a
general visual inspection of the APU feed line shroud for any loose
couplings; and tightening any loose couplings, which would terminate
the repetitive functional tests. 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 December
14, 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 Airbus
Canada Limited Partnership, 13100 Henri-Fabre Boulevard, Mirabel,
Quebec J7N 3C6, Canada; telephone 450-476-7676; email
a220_crc@abc.airbus; internet http://a220world.airbus.com. You may view
this service information at the FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call 206-
231-3195.

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-
0971; 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, 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: Darren Gassetto, Aerospace Engineer,
Mechanical Systems and Administrative Services Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7323; fax 516-794-5531; email 9-avs-nyaco-cos@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-2020-0971; Project Identifier
AD 2020-NM-083" 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
the 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 we receive, 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 we receive about this proposed AD.

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
Darren Gassetto, Aerospace Engineer, Mechanical Systems and
Administrative Services Section, FAA, New York ACO Branch, 1600 Stewart
Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7323; fax 516-
794-5531; email 9-avs-nyaco-cos@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

Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian AD CF-2020-14, dated April
30, 2020 (referred to after this as the Mandatory Continuing
Airworthiness Information, or "the MCAI"), to correct an unsafe
condition for certain Airbus Canada Limited Partnership Model BD-500-
1A10 and BD-500-1A11 airplanes. 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-2020-0971.

This proposed AD was prompted by a report that threaded fuel
couplings were incorrectly installed at final assembly and in service.
The FAA is proposing this AD to address loose fuel couplings, which
could eventually disconnect and could lead to fuel starvation of the
APU and pose a risk of fire. See the MCAI for additional background
information.

Related Service Information Under 1 CFR part 51

Airbus Canada has issued Service Bulletin BD500-282009, Issue 003,
dated August 14, 2020. This service information describes procedures
for repetitive functional tests of the APU fuel feed line shroud, a
general visual inspection of the APU feed line shroud for any loose
couplings, and tightening of any loose couplings if necessary. The
inspection and tightening of the APU fuel feed line shroud couplings
terminates the repetitive functional tests of the APU fuel feed line
shroud. 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.

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
because the FAA evaluated all the relevant information and determined
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 accomplishing the actions specified
in the service information described previously.

Costs of Compliance

The FAA estimates that this proposed AD affects 22 airplanes 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 product
Cost on U.S. operators
Up to 42 work-hours x $85 per hour = Up to $3,570
$0
Up to $3,570
Up to $78,540

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

Estimated Costs of On-Condition Actions

Labor cost
Parts cost
Cost per product
8 work-hours x $85 per hour = $680
$0
$680

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):