Airworthiness Directives; Bombardier, Inc. Airplanes
| Published date | 18 February 2020 |
| Citation | 85 FR 8768 |
| Record Number | 2020-03042 |
| Section | Proposed rules |
| Court | Federal Aviation Administration,Transportation Department |
Federal Register, Volume 85 Issue 32 (Tuesday, February 18, 2020)
[Federal Register Volume 85, Number 32 (Tuesday, February 18, 2020)]
[Proposed Rules]
[Pages 8768-8771]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-03042]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-0092; Product Identifier 2020-NM-001-AD]
RIN 2120-AA64
Airworthiness Directives; 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 Bombardier, Inc., Model CL-600-2B19 (Regional Jet Series
100 & 440) airplanes, Model CL-600-2C10 (Regional Jet Series 700, 701 &
702) airplanes, Model CL-600-2D15 (Regional Jet Series 705) airplanes,
and Model CL-600-2D24 (Regional Jet Series 900) airplanes; and all
Model CL-600-2C11 (Regional Jet Series 550) airplanes. This proposed AD
was prompted by reports of fractured rudder primary feel unit shafts; a
subsequent investigation determined that the fractures in the shafts
are consistent with fatigue damage. This proposed AD would require
replacement of the rudder primary feel unit shaft. 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 April 3,
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
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec
H4S 1Y9, Canada; Widebody Customer Response Center North America toll-
free telephone 1-866-538-1247 or direct-dial telephone 1-514-855-2999;
fax 514-855-7401; email [email protected]; internet http://www.bombardier.com. You may view this service information at the FAA,
Transport Standards 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-
0092; 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 regulatory evaluation, 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: Andrea Jimenez, Aerospace Engineer,
Airframe and Mechanical Systems Section, FAA, New York ACO Branch, 1600
Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7330;
fax 516-794-5531; email [email protected].
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-2020-0092;
Product Identifier 2020-NM-001-AD'' at the beginning of your comments.
The FAA specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this NPRM. The FAA will
consider all comments received by the closing date and may amend this
NPRM because of those comments.
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.
[[Page 8769]]
Discussion
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian AD CF-2019-42, dated November
8, 2019 (referred to after this as the Mandatory Continuing
Airworthiness Information, or ``the MCAI''), to correct an unsafe
condition for certain Bombardier, Inc., Model CL-600-2B19 (Regional Jet
Series 100 & 440) airplanes, Model CL-600-2C10 (Regional Jet Series
700, 701 & 702) airplanes, Model CL-600-2D15 (Regional Jet Series 705)
airplanes, and Model CL-600-2D24 (Regional Jet Series 900) airplanes;
and all Model CL-600-2C11 (Regional Jet Series 550) 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-
0092.
This proposed AD was prompted by reports of fractured rudder
primary feel unit shafts; a subsequent investigation determined that
the fractures in the shafts are consistent with fatigue damage. The FAA
is proposing this AD to address fractures of the rudder primary feel
unit shaft, which could result in a loss of feel in the yaw axis and
thereby impact the controllability of the airplane. See the MCAI for
additional background information.
Related Service Information Under 1 CFR Part 51
Bombardier has issued Service Bulletin 601R-27-166, dated April 5,
2019, and Service Bulletin 670BA-27-075, dated April 5, 2019. This
service information describes procedures for replacing the rudder
primary feel unit shaft that has part number 600-90251-1 with a new
shaft. These documents are distinct since they apply to different
airplane models. 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 our bilateral agreement with the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. We are proposing this AD because we
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 1,002 airplanes of
U.S. registry. The FAA estimates the following costs to comply with
this proposed AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
18 work-hours x $85 per hour = $1,530........................ $158 $1,688 $1,691,376
----------------------------------------------------------------------------------------------------------------
According to the manufacturer, some or all of the costs of this
proposed AD may be covered under warranty, thereby reducing the cost
impact on affected individuals. The FAA does not control warranty
coverage for affected individuals. As a result, the FAA has included
all known 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.
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 has 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
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 (AD):
Bombardier, Inc.: Docket No. FAA-2020-0092; Product Identifier 2020-
NM-001-AD.
(a) Comments Due Date
We must receive comments by April 3, 2020.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc. airplanes, certificated in
any category, as specified in paragraphs (c)(1) through (4) of this
AD.
[[Page 8770]]
(1) Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes,
serial number (S/N) 7003 through 7990 inclusive, and S/N 8000 and
subsequent.
(2) Model CL-600-2C10 (Regional Jet Series 700, 701 & 702)
airplanes, S/N 10002 through 10347 inclusive.
(3) Model CL-600-2D15 (Regional Jet Series 705) airplanes and
Model CL-600-2D24 (Regional Jet Series 900) airplanes, S/N 15001
through 15469 inclusive.
(4) Model CL-600-2C11 (Regional Jet Series 550) airplanes, all
serial numbers.
(d) Subject
Air Transport Association (ATA) of America Code 27, Flight
controls.
(e) Reason
This AD was prompted by reports of fractured rudder primary feel
unit shafts; a subsequent investigation determined that the
fractures in the shafts are consistent with fatigue damage. The FAA
is issuing this AD to address fractures of the rudder primary feel
unit shaft, which could result in a loss of feel in the yaw axis and
thereby impact the controllability of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Replacement
Within the compliance times specified in figure (1) to paragraph
(g) of this AD: Replace all rudder primary feel unit shafts that
have part number (P/N) 600-90251-1 with a new shaft, in accordance
with the Accomplishment Instructions of the Bombardier Service
Bulletin 601R-27-166, dated April 5, 2019; or Bombardier Service
Bulletin 670BA-27-075, dated April 5, 2019; as applicable. For Model
CL-600-2C11 (Regional Jet Series 550) airplanes, do the replacement
in accordance with the Accomplishment Instructions of Bombardier
Service Bulletin 670BA-27-075, dated April 5, 2019.
[GRAPHIC] [TIFF OMITTED] TP18FE20.052
(h) Parts Installation Prohibition
As of the effective date of this AD, no person may install a
rudder primary feel unit shaft, P/N 600-90251-1, on any airplane.
(i) 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
Bombardier, Inc.'s TCCA Design Approval Organization (DAO). If
approved by the DAO, the approval must include the DAO-authorized
signature.
(j) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) Canadian AD CF-2019-42, dated November 8, 2019, 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-2020-0092.
(2) For more information about this AD, contact Andrea Jimenez,
Aerospace Engineer, Airframe and Mechanical Systems Section, FAA,
New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 516-228-7330; fax 516-794-5531; email [email protected].
[[Page 8771]]
(3) For service information identified in this AD, contact
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval,
Qu[eacute]bec H4S 1Y9, Canada; Widebody Customer Response Center
North America toll-free telephone 1-866-538-1247 or direct-dial
telephone 1-514-855-2999; fax 514-855-7401; email
[email protected]; internet http://www.bombardier.com. You
may view this service information at the FAA, Transport Standards
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 February 11, 2020.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020-03042 Filed 2-14-20; 8:45 am]
BILLING CODE 4910-13-P
