[Federal Register Volume 81, Number 13 (Thursday, January 21, 2016)]
[Rules and Regulations]
[Pages 3297-3301]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-00630]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2015-1987; Directorate Identifier 2014-NM-240-AD;
Amendment 39-18377; AD 2016-01-17]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc. Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, &
702) airplanes. This AD was prompted by reports of cracked forward door
members of the inboard main landing gear (MLG) doors. This AD requires
repetitive inspections of the inboard MLG doors, repairs if necessary,
and replacement of the inboard MLG doors. This AD also provides
optional terminating action for the door replacement. We are issuing
this AD to prevent loss of an MLG door during flight, which could
result in damage to the airplane.
DATES: This AD becomes effective February 25, 2016.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of February 25,
2016.
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2015-1987; or in person at the
Docket Management Facility, U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC.
For service information identified in this AD, contact Bombardier,
Inc., 400 C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9,
Canada; telephone 514-855-5000; fax 514-855-7401; email
[email protected]; Internet http://www.bombardier.com. You
may view this referenced service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information
on the availability of this material at the FAA, call 425-227-1221. It
is also available on the Internet at http://www.regulations.gov by
searching for and locating Docket No. FAA-2015-1987.
FOR FURTHER INFORMATION CONTACT: Aziz Ahmed, Aerospace Engineer, ANE-
171, FAA, New York Aircraft Certification Office, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; phone 516-228-7329; fax 516-794-5531.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain Bombardier, Inc.
Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes. The
NPRM published in the Federal Register on June 30, 2015 (80 FR 37200).
The NPRM was prompted by reports of cracked forward door members of the
inboard MLG doors. The NPRM proposed to require repetitive inspections
of the inboard MLG doors, repairs if necessary, and replacement of the
inboard MLG doors. The NPRM also proposed optional terminating action
for the door replacement. We are issuing this AD to prevent loss of an
MLG door during flight, which could result in damage to the airplane.
[[Page 3298]]
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian Airworthiness Directive CF-
2014-42, dated December 12, 2014 (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-
2C10 (Regional Jet Series 700, 701, & 702) airplanes. The MCAI states:
Cases of inboard MLG doors with cracked door forward members
were found. A cracked inboard MLG door forward member could result
in door departure from the aeroplane. Loss of an MLG door during
flight could result in damage to the aeroplane and injury to persons
on the ground.
This [Canadian] AD mandates the repetitive inspection [and
corrective actions if necessary] and replacement of the inboard MLG
doors.
The repetitive inspection is a detailed inspection for damage
(including deformation, pulled or missing fasteners on the inner skins
and outer skin, and cracks) on the inner skins, outer skin, and the
forward member of the inboard MLG doors. Corrective actions include
repairing, removing, or replacing the inboard MLG door.
You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2015-1987-0002.
Comments
We gave the public the opportunity to participate in developing
this AD. The following presents the comment received on the NPRM (80 FR
37200, June 30, 2015) and the FAA's response to the comment.
Request To Revise Repair Instructions
Envoy Airlines requested that we revise the wording in paragraph
(i)(1)(ii)(A) of the proposed AD (80 FR 37200, June 30, 2015) to
clarify that removal of the MLG door is not required in all repair
situations. Envoy Airlines stated that Bombardier Service Bulletin
670BA-32-042, Revision A, dated July 2, 2014, including Appendixes A
and B, both dated November 5, 2013, specifies that repairs can be
accomplished with the door installed in some situations. Envoy Airlines
suggested that the text ``Repair and reinstall the door'' in paragraph
(i)(1)(ii)(A) of the proposed AD be reworded to specify ``repair the
door.''
We agree with the commenter's request to revise the repair
instructions. We have revised paragraph (i)(1)(ii)(A) of this AD by
removing the instructions to reinstall the door.
Clarification of Actions
We have clarified the inspection area in paragraph (g) of this AD
by specifying to inspect for damage on the inner skins, outer skin, and
the forward member of the inboard MLG doors.
Paragraph (i)(1)(ii)(A) of the proposed AD (80 FR 37200, June 30,
2015) specifies to do a repair ``if repair of the inboard MLG is
possible.'' We have revised paragraph (i)(1)(ii)(A) of this AD to
clarify the repair is done if it is possible to repair the inboard MLG
door in accordance with the Accomplishment Instructions of Bombardier
Service Bulletin 670BA-32-042, Revision A, dated July 2, 2014,
including Appendixes A and B, both dated November 5, 2013.
We have also revised paragraph (i)(1)(i) of this AD to specify that
clarify that removed damaged doors cannot be reinstalled, unless the
door is repaired prior to reinstallation and the actions specified in
paragraph (l) of this AD are done.
We have also clarified the actions required by paragraphs
(i)(1)(iii), (i)(2), (k)(1), and (k)(2)(i) of this AD by specifying
that where Bombardier Service Bulletin 670BA-32-043, Revision A, dated
November 13, 2014, specifies to contact the manufacturer for certain
instructions, this AD requires accomplishing those actions using a
method approved by the Manager, New York ACO, ANE-170, FAA; or TCCA; or
Bombardier, Inc.'s TCCA DAO.
We have also revised paragraph (m) of this AD to refer to the
latest revision of Bombardier Service Bulletin 670BA-32-043, dated July
2, 2014. The ``Pre SB Part Number'' column of Section M, Relationship
Chart, of Bombardier Service Bulletin 670BA-32-043, Revision A, dated
November 13, 2014, is the same as that in Bombardier Service Bulletin
670BA-32-043, dated July 2, 2014.
Conclusion
We reviewed the relevant data, considered the comment received, and
determined that air safety and the public interest require adopting
this AD with the changes described previously and minor editorial
changes. We have determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM (80 FR 37200, June 30, 2015) for correcting the unsafe condition;
and
Do not add any additional burden upon the public than was
already proposed in the NPRM (80 FR 37200, June 30, 2015).
We also determined that these changes will not increase the
economic burden on any operator or increase the scope of this AD.
Related Service Information Under 1 CFR Part 51
Bombardier has issued the following service information.
Bombardier Modification Summary Package IS670528200033,
Revision A-2, dated October 11, 2005. This service information
describes procedures for enlarging the forward and aft hinge cutouts of
the MLG inboard and outboard doors.
Bombardier Service Bulletin 670BA-32-040, Revision D,
dated July 2, 2014, including Appendix A, Revision A, dated July 2,
2014, and Appendix B, Revision B, dated July 2, 2014. This service
information describes procedures for increasing the clearances between
the MLG fairing and the MLG doors.
Bombardier Service Bulletin 670BA-32-040, Revision E,
dated November 13, 2014, including Appendix A, Revision A, dated July
2, 2014, and Appendix B, Revision B, dated July 2, 2014. This service
information describes procedures for increasing the clearances between
the MLG fairing and the MLG doors, and for enlarging the forward and
aft hinge cutouts of the MLG inboard and outboard doors.
Bombardier Service Bulletin 670BA-32-042, Revision A,
dated July 2, 2014, including Appendixes A and B, both dated November
5, 2013. This service information describes procedures for inspecting
and repairing the inboard MLG door inner skins, outer skin, and the
forward member.
Bombardier Service Bulletin 670BA-32-043, dated July 2,
2014; and Bombardier Service Bulletin 670BA-32-043, Revision A, dated
November 13, 2014. This service information describes procedures for
replacing the inboard MLG doors.
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 of this
AD.
Costs of Compliance
We estimate that this AD affects 269 airplanes of U.S. registry.
We estimate that it will take about 16 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work hour. Required parts will cost about $31,000 per
product. Based on these figures, we estimate the cost of this AD on
U.S. operators to be $8,704,840, or $32,360 per product.
[[Page 3299]]
In addition, we estimate that any necessary follow-on actions will
take up to 44 work-hours and require parts costing up to $31,000, for a
cost of up to $34,740 per product. We have no way of determining the
number of aircraft that might need these actions.
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.
We are 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
We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will 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 that this AD:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in Alaska; and
4. 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.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2015-1987; or in person at the
Docket Management Facility between 9 a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The AD docket contains this AD, the
regulatory evaluation, any comments received, and other information.
The street address for the Docket Operations office (telephone 800-647-
5527) is in the ADDRESSES section.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 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):
2016-01-17 Bombardier, Inc.: Amendment 39-18377; Docket No. FAA-
2015-1987; Directorate Identifier 2014-NM-240-AD.
(a) Effective Date
This AD becomes effective February 25, 2016.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc. Model CL-600-2C10 (Regional
Jet Series 700, 701, & 702) airplanes, certificated in any category,
serial numbers 10002 and subsequent, as identified in Bombardier
Service Bulletin 670BA-32-042, Revision A, dated July 2, 2014,
including Appendixes A and B, both dated November 5, 2013.
(d) Subject
Air Transport Association (ATA) of America Code 32, Landing
Gear.
(e) Reason
This AD was prompted by reports of cracked forward door members
of the inboard main landing gear (MLG) doors. We are issuing this AD
to prevent loss of an MLG door during flight, which could result in
damage to the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Repetitive Inspections
Within 660 flight hours or 12 months after the effective date of
this AD, whichever occurs first: Do a detailed inspection for damage
(including deformation, pulled or missing fasteners on the inner
skins and outer skin, and cracks) on the inner skins, outer skin,
and the forward member of the inboard MLG doors, in accordance with
the Accomplishment Instructions of Bombardier Service Bulletin
670BA-32-042, Revision A, dated July 2, 2014, including Appendixes A
and B, both dated November 5, 2013. Repeat the inspection thereafter
at intervals not to exceed 660 flight hours or 12 months, whichever
occurs first.
(h) Detailed Inspection Definition
For the purposes of this AD, a detailed inspection is an
intensive examination of a specific item, installation, or assembly
to detect damage, failure, or irregularity. Available lighting is
normally supplemented with a direct source of good lighting at an
intensity deemed appropriate. Inspection aids such as mirror,
magnifying lenses, etc., may be necessary. Surface cleaning and
elaborate procedures may be required.
(i) Corrective Actions
(1) If any damage is found on any inner skin or outer skin of
the inboard MLG door during any inspection required by paragraph (g)
of this AD: Before further flight, do the actions specified in
paragraph (i)(1)(i), (i)(1)(ii), or (i)(1)(iii) of this AD.
(i) Remove the damaged inboard MLG door, in accordance with the
Accomplishment Instructions of Bombardier Service Bulletin 670BA-32-
042, Revision A, dated July 2, 2014, including Appendixes A and B,
both dated November 5, 2013. A damaged inboard MLG door cannot be
reinstalled, unless the repair specified in paragraph (i)(1)(ii) of
this AD is done prior to reinstallation and the actions specified in
paragraph (l) of this AD are done at the times specified in
paragraph (l) of this AD.
(ii) Repair the door as specified in paragraph (i)(1)(ii)(A) or
(i)(1)(ii)(B) of this AD, as applicable.
(A) If it is possible to repair the inboard MLG door in
accordance with the Accomplishment Instructions of Bombardier
Service Bulletin 670BA-32-042, Revision A, dated July 2, 2014,
including Appendixes A and B, both dated November 5, 2013: Repair
the door, in accordance with the Accomplishment Instructions of
Bombardier Service Bulletin 670BA-32-042, Revision A, dated July 2,
2014, including Appendixes A and B, both dated November 5, 2013.
(B) If it is not possible to repair the inboard MLG door in
accordance with the Accomplishment Instructions of Bombardier
Service Bulletin 670BA-32-042, Revision A, dated July 2, 2014,
including Appendixes A and B, both dated November 5, 2013: Repair
using a method approved by the Manager, New York Aircraft
Certification Office (ACO), ANE-170, FAA; or Transport Canada Civil
Aviation (TCCA); or Bombardier, Inc.'s TCCA Design Approval
Organization (DAO).
(iii) Replace the inboard MLG door, in accordance with the
Accomplishment Instructions of Bombardier Service Bulletin 670BA-32-
043, Revision A, dated November 13, 2014, except, where Bombardier
Service Bulletin 670BA-32-043, Revision A, dated November 13, 2014,
specifies to contact the manufacturer for certain instructions, this
AD requires accomplishing those actions using a method approved by
the Manager, New York ACO, ANE-170, FAA; or TCCA; or Bombardier,
Inc.'s TCCA DAO.
[[Page 3300]]
(2) If any damage is found on the forward member of the inboard
MLG door during any inspection required by paragraph (g) of this AD:
Before further flight, replace the inboard MLG door, in accordance
with the Accomplishment Instructions of Bombardier Service Bulletin
670BA-32-043, Revision A, dated November 13, 2014, except, where
Bombardier Service Bulletin 670BA-32-043, Revision A, dated November
13, 2014, specifies to contact the manufacturer for certain
instructions, this AD requires accomplishing those actions using a
method approved by the Manager, New York ACO, ANE-170, FAA; or TCCA;
or Bombardier, Inc.'s TCCA DAO.
(j) Terminating Action
Within 6,600 flight hours or 36 months after the effective date
of this AD, whichever occurs first, except as provided by paragraph
(l) of this AD: Replace the inboard MLG doors, in accordance with
the Accomplishment Instructions of Bombardier Service Bulletin
670BA-32-043, Revision A, dated November 13, 2014; except, where
Bombardier Service Bulletin 670BA-32-043, Revision A, dated November
13, 2014, specifies to contact the manufacturer for certain
instructions, this AD requires accomplishing those actions using a
method approved by the Manager, New York ACO, ANE-170, FAA; or TCCA;
or Bombardier, Inc.'s TCCA DAO.
(1) Doing the MLG door replacement required by the introductory
text of paragraph (j) of this AD terminates the inspections required
by paragraph (g) of this AD for that MLG door.
(2) Doing the MLG door replacement required by the introductory
text of paragraph (j) of this AD does not terminate the actions
required by AD 2010-23-19, Amendment 39-16508 (75 FR 68695, November
9, 2010).
(k) Optional Actions for Compliance With Paragraph (j) of This AD
Doing any of the actions specified in paragraph (k)(1), (k)(2),
(k)(3), or (k)(4) of this AD is acceptable for compliance with the
requirements of paragraph (j) of this AD.
(1) Replacement of the inboard MLG door, in accordance with the
Accomplishment Instructions of Bombardier Service Bulletin 670BA-32-
043, Revision A, dated November 13, 2014, except, where Bombardier
Service Bulletin 670BA-32-043, Revision A, dated November 13, 2014,
specifies to contact the manufacturer for certain instructions, this
AD requires accomplishing those actions using a method approved by
the Manager, New York ACO, ANE-170, FAA; or TCCA; or Bombardier,
Inc.'s TCCA DAO; and enlargement of the forward and aft hinge
cutouts, in accordance with the procedures specified in Bombardier
Modification Summary Package IS670528200033, Revision A-2, dated
October 11, 2005.
(2) Installation of an inboard MLG door assembly with a part
number listed in the ``Post SB Part Number'' column of Section M,
Relationship Chart, of Bombardier Service Bulletin 670BA-32-043,
dated July 2, 2014, in accordance with a method specified in
paragraph (k)(2)(i) or (k)(2)(ii) of this AD.
(i) Do the installation in accordance with the Accomplishment
instructions of Bombardier Service Bulletin 670BA-32-043, dated July
2, 2014; or Bombardier Service Bulletin 670BA-32-043, Revision A
dated November 13, 2014; except, where Bombardier Service Bulletin
670BA-32-043, Revision A, dated November 13, 2014, specifies to
contact the manufacturer for certain instructions, this AD requires
accomplishing those actions using a method approved by the Manager,
New York ACO, ANE-170, FAA; or TCCA; or Bombardier, Inc.'s TCCA DAO.
(ii) Do the installation using a method approved by the Manager,
New York ACO, ANE-170, FAA; or TCCA; or Bombardier, Inc.'s TCCA DAO.
(3) Doing the actions specified in ``PART C--Installation of the
Inboard MLG Door Part Number CC670-10520-15 and Increase of the
Clearance Between the Left MLG Inboard-Door and the MLG Fairing''
and ``PART D--Installation of the Inboard MLG Door Part Number
CC670-10520-16 and Increase of the Clearance Between the Right MLG
Inboard-Door and the MLG Fairing'' of the Accomplishment
Instructions of Bombardier Service Bulletin 670BA-32-040, Revision
E, dated November 13, 2014, including Appendix A, Revision A, dated
July 2, 2014, and Appendix B, Revision B, dated July 2, 2014.
(4) Doing the actions specified in paragraphs (k)(4)(i) and
(k)(4)(ii) of this AD.
(i) Doing the actions specified in ``PART C--Installation of the
Inboard MLG Door Part Number CC670-10520-15 and Increase of the
Clearance Between the Left MLG Inboard-Door and the MLG Fairing''
and ``PART D--Installation of the Inboard MLG Door Part Number
CC670-10520-16 and Increase of the Clearance Between the Right MLG
Inboard-Door and the MLG Fairing'' of the Accomplishment
Instructions of Bombardier Service Bulletin 670BA-32-040, Revision
D, dated July 2, 2014, including Appendix A, Revision A, dated July
2, 2014, and Appendix B, Revision B, dated July 2, 2014.
(ii) Enlargement of the forward and aft hinge cutouts specified
in Bombardier Modification Summary Package IS670528200033, Revision
A-2, dated October 11, 2005.
(l) Optional Delay of MLG Door Replacement
If an MLG door is removed, the replacement required by paragraph
(j) of this AD can be delayed until the MLG door is reinstalled.
When the removed MLG door is reinstalled, the actions required by
paragraph (j) of this AD must be done at the time specified in
paragraph (j) of this AD.
(m) Parts Installation Prohibition
Upon completion of the actions specified in paragraph (j) or (k)
of this AD, no person may install an inboard MLG door assembly with
a part number listed in the ``Pre SB Part Number'' column of Section
M, Relationship Chart, of Bombardier Service Bulletin 670BA-32-043,
Revision A, dated November 13, 2014; on any airplane.
(n) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York ACO, ANE-170, 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 ACO, send it to ATTN: Program
Manager, Continuing Operational Safety, FAA, New York ACO, 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. The AMOC approval letter must
specifically reference this AD.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, New York ACO,
ANE-170, FAA; or TCCA; or Bombardier, Inc.'s TCCA DAO. If approved
by the DAO, the approval must include the DAO authorized signature.
(o) Special Flight Permits
Special flight permits, as described in Section 21.197 and
Section 21.199 of the Federal Aviation Regulations (14 CFR 21.197
and 21.199), are not allowed.
(p) Related Information
Refer to Mandatory Continuing Airworthiness Information (MCAI)
Canadian Airworthiness Directive CF-2014-42, dated December 12,
2014, for related information. This MCAI may be found in the AD
docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2015-1987-0002.
(q) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Modification Summary Package IS670528200033,
Revision A-2, dated October 11, 2005.
(ii) Bombardier Service Bulletin 670BA-32-040, Revision D, dated
July 2, 2014, including Appendix A, Revision A, dated July 2, 2014,
and Appendix B, Revision B, dated July 2, 2014.
(iii) Bombardier Service Bulletin 670BA-32-040, Revision E,
dated November 13, 2014, including Appendix A, Revision A, dated
July 2, 2014, and Appendix B, Revision B, dated July 2, 2014.
(iv) Bombardier Service Bulletin 670BA-32-042, Revision A, dated
July 2, 2014, including Appendixes A and B, both dated November 5,
2013.
(v) Bombardier Service Bulletin 670BA-32-043, dated July 2,
2014.
(vi) Bombardier Service Bulletin 670BA-32-043, Revision A, dated
November 13, 2014.
[[Page 3301]]
(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; telephone 514-855-5000; fax 514-855-
7401; email [email protected]; Internet http://www.bombardier.com.
(4) You may view this service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
425-227-1221.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on January 6, 2016.
Victor Wicklund,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2016-00630 Filed 1-20-16; 8:45 am]
BILLING CODE 4910-13-P