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2018-07-09 BOMBARDIER, INC.: Amendment 39-19240; Docket No. FAA-2017-0810; Product Identifier 2017-NM-045-AD.
(a) EFFECTIVE DATE

    This AD is effective May 14, 2018.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to the airplanes identified  in paragraphs (c)(1), (c)
    (2), and (c)(3) of this AD, certificated in any category, all certifi-
    cated models.

(1) Bombardier, Inc.,  Model CL-600-2C10  (Regional Jet Series 700, 701, &
    702) airplanes, serial numbers 10001 through 10344 inclusive.

(2) Bombardier, Inc, Model CL-600-2D15 (Regional Jet Series 705) and Model
    CL-600-2D24 (Regional Jet Series 900) airplanes,  serial numbers 15001
    through 15382 inclusive.

(3) Bombardier, Inc.,  Model  CL-600-2E25 (Regional Jet Series 1000)  air-
    planes, serial numbers 19001 through 19044 inclusive.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 25, Equipment/furnish-
    ings.

(e) REASON

    This AD was prompted by a report of a smoke-in-cabin event  due  to  a
    non-sustaining electrical fire.  We are issuing this AD  to prevent an
    electrical short of a bonding jumper wire that may result in in-flight
    smoke or fire events, as well as failure of avionics equipment, due to
    possible water spray or leakage from a damaged water supply line.

(f) COMPLIANCE

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

(g) PROTECTIVE SLEEVE INSTALLATION

(1) For  airplanes  on  which  the actions specified in Bombardier Service
    Bulletin 670BA-25-101, dated December 17, 2015; or Bombardier  Service
    Bulletin 670BA-25-101,  Revision A,  dated October 31, 2016,  have not
    been done, as of  the effective date of  this AD: Within 6,600  flight
    hours or  36 months  after the  effective date  of this  AD, whichever
    occurs first, install protective  sleeves on the bonding  jumper wires
    of affected galleys and lavatories,  in accordance with Part A through
    Part E, as applicable of the Accomplishment Instructions of Bombardier
    Service Bulletin 670BA-25-101, Revision B, dated January 12, 2017.

(2) For  airplanes  on which the actions specified  in  Bombardier Service
    Bulletin 670BA-25-101, dated December 17, 2015;  or Bombardier Service
    Bulletin 670BA-25-101, Revision A,  dated October 31, 2016,  have been
    done,  as of the effective date of this AD:  Within 6,600 flight hours
    or  36 months after the effective date  of this AD,  whichever  occurs
    first,  inspect,  and  if required,  install protective sleeves on the
    bonding jumper wires of affected galleys and lavatories, in accordance
    with Part F of the Accomplishment Instructions  of  Bombardier Service
    Bulletin 670BA-25-101, Revision B, dated January 12, 2017.

(h) 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
    corrective  actions   from  a   manufacturer,  the   action  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.

(i) RELATED INFORMATION

(1) Refer   to   Mandatory  Continuing  Airworthiness  Information  (MCAI)
    Canadian AD CF-2016-20R1, dated February 3, 2017, for related informa-
    tion. This MCAI may be found in the AD docket on the internet at http:
    //www.regulations.gov by searching for  and  locating  Docket No. FAA-
    2017-0810.

(2) For more information about this AD contact Assata Dessaline, Aerospace
    Engineer, Avionics and Administrative Services Section,  FAA, New York
    ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;  tele-
    phone: 516-228-7301; fax: 516-794-5531.

(j) 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 Service Bulletin 670BA-25-101, Revision B dated January 12,
    2017.

(ii) Reserved.

(3) For service information identified  in  this  AD,  contact Bombardier,
    Inc.,  400 Cote  Vertu  Road  West,  Dorval,  Quebec 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:   ac.yul@aero.bombardier.com;   internet:   http://www.
    bombardier.com.

(4) 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.

(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  Des Moines, Washington,  on March 20, 2018.  Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification Service

FOR FURTHER INFORMATION CONTACT:  Assata  Dessaline,  Aerospace  Engineer,
Avionics and Administrative Services Section,  FAA,  New York  ACO Branch,
1600 Stewart Avenue,  Suite 410,  Westbury, NY 11590;  telephone: 516-228-
7301; fax: 516-794-5531.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-0810; Product Identifier 2017-NM-045-AD; Amendment
39-19240; AD 2018-07-09]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc., Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Bombardier, Inc., Model CL-600-2C10 (Regional Jet Series 700, 701, &
702), Model CL-600-2D15 (Regional Jet Series 705), Model CL-600-2D24
(Regional Jet Series 900), and Model CL-600-2E25 (Regional Jet Series
1000) airplanes. This AD was prompted by a report of a smoke-in-cabin
event due to a non-sustaining electrical fire. This AD requires
installation of protective sleeves on the bonding jumper wires of
affected galleys and lavatories. We are issuing this AD to address the
unsafe condition on these products.

DATES: This AD is effective May 14, 2018.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of May 14,
2018.

ADDRESSES: For service information identified in this final rule,
contact Bombardier, Inc., 400 Cote Vertu Road West, Dorval,
Quebec 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: ac.yul@aero.bombardier.com;
internet: http://www.bombardier.com. You may view this referenced
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. It is also available on the internet at http://www.
regulations.gov by searching for and locating Docket No. FAA-2017-0810.

Examining the AD Docket

You may examine the AD docket on the internet at http://www.regulations.gov
by searching for and locating Docket No. FAA-2017-0810;
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 Office (telephone:
800-647-5527) is 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 20590.

FOR FURTHER INFORMATION CONTACT: Assata Dessaline, Aerospace Engineer,
Avionics and Administrative Services Section, FAA, New York ACO Branch,
1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone: 516-228-
7301; 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), Model CL-600-
2D15 (Regional Jet Series 705), Model CL-600-2D24 (Regional Jet Series
900), and Model CL-600-2E25 (Regional Jet Series 1000) airplanes. The
NPRM published in the Federal Register on September 13, 2017 (82 FR
42953) (``the NPRM''). The NPRM was prompted by a report of a smoke-in-
cabin event due to a non-sustaining electrical fire. The NPRM proposed
to require installation of protective sleeves on the bonding jumper
wires of affected galleys and lavatories. We are issuing this AD to
prevent an electrical short of a bonding jumper wire that may result in
in-flight smoke or fire events, as well as failure of avionics
equipment, due to possible water spray or leakage from a damaged water
supply line.
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian AD CF-2016-20R1, dated
February 3, 2017 (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), Model CL-600-2D15 (Regional Jet Series 705),
Model CL-600-2D24 (Regional Jet Series 900), and Model CL-600-2E25
(Regional Jet Series 1000) airplanes. The MCAI states:

A CRJ900 aeroplane reported a smoke in cabin event due to a non-
sustaining electrical fire. The source of smoke was traced to a
burnt heated water supply line behind the #2 Galley. The surrounding
insulation was also found burnt.
The root cause of this electrical fire was an electrical short
between an un-insulated bonding jumper and a terminal block carrying
115 volts AC. The circuit resistance was high enough and the circuit
breakers that protect the wiring did not trip open.
Electrical short of a bonding jumper may result in in-flight
smoke or fire events as well as failure of avionics equipment due to
possible water spray or leakage from a damaged water supply line.
The likelihood of this happening is increased by the removal and
installation of the galley or lavatory during maintenance, allowing
the bonding jumper to become wedged under the terminal block.
* * * * *
Revision 1 of this [Canadian] AD is issued to mandate [the
installation of protective sleeves on the galley and lavatory
bonding jumper wires in accordance with] Bombardier Service Bulletin
(SB) 670BA-25-101 Revision B dated 12 January 2017. * * *

You may examine the MCAI in the AD docket on the internet at http://www.
regulations.gov by searching for and locating Docket No. FAA-2017-0810.

Comments

We gave the public the opportunity to participate in developing
this final rule. We considered the comment received. The Air Line
Pilots Association, International supported the NPRM.

Conclusion

We reviewed the relevant data, considered the comment received, and
determined that air safety and the public interest require adopting
this AD as proposed except for minor editorial changes. We have
determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM for correcting the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

Bombardier, Inc., has issued Service Bulletin 670BA-25-101,
Revision B, dated January 12, 2017. The service information describes
procedures for installation of protective sleeves on the bonding jumper
wires of affected galleys and lavatories. 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.

Costs of Compliance

We estimate that this AD affects 544 airplanes of U.S. registry.
We estimate the following costs to comply with this AD:

Estimated Costs

Action Labor cost Parts cost Cost per product Cost on U.S. operators
Install protective sleeves 10 work-hours x $85 per hour = $850 Negligible $850 $462,400

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.
This AD is issued in accordance with authority delegated by the
Executive Director, Aircraft Certification Service, as authorized by
FAA Order 8000.51C. In accordance with that order, issuance of ADs is
normally a function of the Compliance and Airworthiness Division, but
during this transition period, the Executive Director has delegated the
authority to issue ADs applicable to transport category airplanes to
the Director of the System Oversight Division.

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.

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

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):