Proposed Rule2022-08822
Airworthiness Directives; Bombardier, Inc., Airplanes
Primary source
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Published
April 26, 2022
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to adopt a new airworthiness directive (AD) for all Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes. This proposed AD was prompted by reports that some oxygen box assemblies had their piston ejected during the mask deployment test. This proposed AD would require a one-time inspection of each passenger oxygen box dual manifold assembly to find and replace affected parts. This proposed AD would also prohibit installing affected parts. The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 87 Issue 80 (Tuesday, April 26, 2022)</title>
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[Federal Register Volume 87, Number 80 (Tuesday, April 26, 2022)]
[Proposed Rules]
[Pages 24476-24479]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-08822]
[[Page 24476]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0470; Project Identifier MCAI-2021-01002-T]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc., Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for all Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes.
This proposed AD was prompted by reports that some oxygen box
assemblies had their piston ejected during the mask deployment test.
This proposed AD would require a one-time inspection of each passenger
oxygen box dual manifold assembly to find and replace affected parts.
This proposed AD would also prohibit installing affected parts. 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 June 10,
2022.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to <a href="https://www.regulations.gov">https://www.regulations.gov</a>. Follow the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> 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.
<bullet> 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 Bombardier
Business Aircraft Customer Response Center, 400 C[ocirc]te-Vertu Road
West, Dorval, Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-2999;
email <a href="/cdn-cgi/l/email-protection#eb8a88c5929e87ab8a8e9984c5898486898a998f828e99c5888486"><span class="__cf_email__" data-cfemail="0564662b7c7069456460776a2b676a68676477616c60772b666a68">[email protected]</span></a>; internet <a href="https://www.bombardier.com">https://www.bombardier.com</a>.
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 at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by
searching for and locating Docket No. FAA-2022-0470; 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.
FOR FURTHER INFORMATION CONTACT: Elizabeth Dowling, Aerospace Engineer,
Mechanical Systems and Administrative Services Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7300; email <a href="/cdn-cgi/l/email-protection#f9c0d4988f8ad49780989a96d49a968ab99f9898d79e968f"><span class="__cf_email__" data-cfemail="8bb2a6eafdf8a6e5f2eae8e4a6e8e4f8cbedeaeaa5ece4fd">[email protected]</span></a>.
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-2022-0470; Project Identifier
MCAI-2021-01002-T'' 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 received, without change, to
<a href="https://www.regulations.gov">https://www.regulations.gov</a>, 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
Elizabeth Dowling, Aerospace Engineer, Mechanical Systems and
Administrative Services Section, FAA, New York ACO Branch, 1600 Stewart
Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7300; email <a href="/cdn-cgi/l/email-protection#9ea7b3ffe8edb3f0e7fffdf1b3fdf1eddef8ffffb0f9f1e8"><span class="__cf_email__" data-cfemail="3c05115d4a4f1152455d5f53115f534f7c5a5d5d125b534a">[email protected]</span></a>. 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 Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued TCCA AD CF-2021-30, dated September 7,
2021 (TCCA AD CF-2021-30) (also referred to after this as the Mandatory
Continuing Airworthiness Information, or the MCAI), to correct an
unsafe condition for all Bombardier, Inc., Model BD-700-1A10 and BD-
700-1A11 airplanes. You may examine the MCAI in the AD docket at
<a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No.
FAA-2022-0470.
This proposed AD was prompted by reports that some passenger oxygen
box dual manifold assemblies had their piston ejected during the mask
deployment test due to a non-conformity in manufacturing. The FAA is
proposing this AD to address a possible in-service piston ejection when
used for emergency descent, smoke, or fire that may result in a high
rate of oxygen leakage, which could prematurely deplete the oxygen for
all passengers. See the MCAI for additional background information.
Related Service Information Under 1 CFR Part 51
Bombardier, Inc., has issued the following service information.
<bullet> Service Bulletin 700-35-5004, Revision 02, dated August
27, 2021.
<bullet> Service Bulletin 700-35-5502, dated August 27, 2021.
<bullet> Service Bulletin 700-35-6004, Revision 05, dated August
27, 2021.
<bullet> Service Bulletin 700-35-6502, dated August 27, 2021.
This service information describes procedures for inspecting each
passenger oxygen box dual manifold assembly to find affected parts, and
replacing affected parts. These documents are distinct because they
apply to different airplane configurations.
This service information is reasonably available because the
interested parties have access to it through their normal
[[Page 24477]]
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 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 308 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
Estimated Costs for Required Actions
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Cost per Cost on U.S.
Labor cost Parts cost product operators
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1 work-hour x $85 per hour = $85............................. $0 $85 $26,180
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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 this on-condition action:
Estimated Costs of On-Condition Actions
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Labor cost Parts cost Cost per product
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Up to 34 work-hours x $85 Up to $1,700........ Up to $4,590.
per hour = $2,890.
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The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all of the costs of
this proposed AD may be covered under warranty, thereby reducing the
cost impact on affected operators.
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) 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
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 adding the following new airworthiness
directive:
Bombardier, Inc.: Docket No. FAA-2022-0470; Project Identifier MCAI-
2021-01002-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by June 10, 2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Bombardier, Inc., Model BD-700-1A10 and
BD-700-1A11 airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen.
(e) Unsafe Condition
This AD was prompted by reports that some passenger oxygen box
dual manifold had their piston ejected during the mask deployment
test due to a non-conformity in manufacturing. The FAA is issuing
this AD to address a possible in-service piston ejection when used
for emergency descent, smoke, or fire that may result in a high rate
of oxygen leakage, which could prematurely deplete the oxygen for
all passengers.
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(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Definition
An affected part is a passenger oxygen box assembly having a
dual manifold assembly having part number 100-009-39 and a lot and
serial number specified in figure 1 to paragraph (g) of this AD.
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[GRAPHIC] [TIFF OMITTED] TP26AP22.058
(h) Required Actions
Within the applicable compliance time specified in paragraph
(h)(1) or (2) of this AD: Inspect each passenger oxygen box dual
manifold assembly to determine if it is an affected part, as defined
in paragraph (g) of this AD, and replace any affected part in
accordance with paragraph 2.B. of the Accomplishment Instructions of
the applicable Bombardier service bulletin specified in figure 2 to
paragraph (h) of this AD. Replace any affected part before further
flight.
(1) For airplanes having serial numbers 9771, 9779, 9784, 9788
through 9824 inclusive, 9853 through 9857 inclusive, and 9859
through 9876 inclusive, within 4 months after the effective date of
this AD.
(2) For airplane having serial numbers 9877 through 9879
inclusive, and 60001 through 60042 inclusive, within 30 months after
the effective date of this AD.
[GRAPHIC] [TIFF OMITTED] TP26AP22.059
(i) Parts Installation Prohibition
As of the effective date of this AD, no person may install an
affected part as defined in paragraph (g) of this AD, on any
airplane.
(j) Credit for Previous Actions
This paragraph provides credit for actions required by paragraph
(h) of this AD, if those actions were performed before the effective
date of this AD using the service information specified in
paragraphs (j)(1) through (7) of this AD, as applicable.
(1) Bombardier Service Bulletin 700-35-5004, dated December 10,
2018.
(2) Bombardier Service Bulletin 700-35-5004, Revision 01, dated
November 29, 2019.
[[Page 24479]]
(3) Bombardier Service Bulletin 700-35-6004, dated December 10,
2018.
(4) Bombardier Service Bulletin 700-35-6004, Revision 01, dated
January 16, 2019.
(5) Bombardier Service Bulletin 700-35-6004, Revision 02, dated
April 5, 2019.
(6) Bombardier Service Bulletin 700-35-6004, Revision 03, dated
May 31, 2019.
(7) Bombardier Service Bulletin 700-35-6004, Revision 04, dated
November 29, 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 responsible Flight Standards 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. Before using any
approved AMOC, notify your appropriate principal inspector, or
lacking a principal inspector, the manager of the responsible Flight
Standards 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
Bombardier, Inc.'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) TCCA AD CF-2021-30, dated September 7, 2021, for related
information. This MCAI may be found in the AD docket on the internet
at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket
No. FAA-2022-0470.
(2) For more information about this AD, contact Elizabeth
Dowling, Aerospace Engineer, Mechanical Systems and Administrative
Services Section, FAA, New York ACO Branch, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone 516-228-7300; email <a href="/cdn-cgi/l/email-protection#b38a9ed2c5c09eddcad2d0dc9ed0dcc0f3d5d2d29dd4dcc5"><span class="__cf_email__" data-cfemail="053c28647376286b7c64666a28666a76456364642b626a73">[email protected]</span></a>.
(3) For service information identified in this AD, contact
Bombardier Business Aircraft Customer Response Center, 400
C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada;
telephone 514-855-2999; email <a href="/cdn-cgi/l/email-protection#c1a0a2efb8b4ad81a0a4b3aeefa3aeaca3a0b3a5a8a4b3efa2aeac"><span class="__cf_email__" data-cfemail="c5a4a6ebbcb0a985a4a0b7aaeba7aaa8a7a4b7a1aca0b7eba6aaa8">[email protected]</span></a>; internet
<a href="https://www.bombardier.com">https://www.bombardier.com</a>. 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.
Issued on April 20, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2022-08822 Filed 4-25-22; 8:45 am]
BILLING CODE 4910-13-C
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