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PROPOSED AD BOMBARDIER, INC.: Docket No. FAA-2017-0477; Directorate Identifier 2016-NM-112-AD.
(a) COMMENTS DUE DATE

    We must receive comments by July 6, 2017.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to Bombardier, Inc., Model CL-600-2B16 (CL-601-3A,  CL
    -601-3R, and CL-604 Variants) airplanes, certificated in any category,
    serial numbers 5702  through 5705 inclusive,  5707, 5709, 5710,  5712,
    5714, 5715,  5718, 5719,  5722, 5723,  5725, 5727,  5728, 5731 through
    5733 inclusive, 5735, 5736, 5740, 5742, 5743, 5745, 5746, 5748 through
    5750  inclusive,  5752  through  5754  inclusive,  5756  through  5758
    inclusive, 5760 through 5762  inclusive, 5764 through 5766  inclusive,
    5768 through 5770 inclusive, 5772 through 5774 inclusive, 5776 through
    5780 inclusive, 5782 through  5787 inclusive, 5790, 5791,  5793, 5794,
    5796, 5797, 5799, 5800, 5802, 5803, 5805 through 5814 inclusive, 5816,
    5818 through 5820 inclusive, 5823 through 5829 inclusive, 5831 through
    5853 inclusive, 5856, 5857, 5859 through 5863 inclusive, 5865  through
    5874  inclusive,  5876  through  5881  inclusive,  5883  through  5888
    inclusive, 5890 through 5894  inclusive, 5896 through 5898  inclusive,
    5900 through 5906 inclusive, 5908 through 5911 inclusive, 5913 through
    5938  inclusive,  5940  through  5947  inclusive,  5949  through  5980
    inclusive, 5982 through 5985 inclusive, 5987, and 5988.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 35, Oxygen.

(e) REASON

    This AD was prompted by a report indicating that the lanyard length of
    the passenger drop down  oxygen masks is too  long. The length of  the
    oxygen  mask  lanyard  might  cause the  safety  pin  tethered  to the
    opposite  end of  the lanyard  to remain  engaged in  the oxygen  flow
    mechanism when  the mask  is pulled  to the  passenger's face.  We are
    issuing this AD to prevent  improper oxygen flow functionality to  the
    passenger oxygen masks in the event of an emergency.

(f) COMPLIANCE

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

(g) REPLACEMENT OF OXYGEN MASK LANYARDS

    Within 2,400 flight hours or 60 months,  whichever occurs first  after
    the effective date  of this AD,  replace the existing  lanyards in the
    passenger oxygen box assemblies  with lanyards of the  correct length,
    in  accordance  with  the  Accomplishment  Instructions  of Bombardier
    Service Bulletin 605-35-003, Revision 02, dated April 18, 2016.

(h) CREDIT FOR PREVIOUS ACTIONS

    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 Bombardier Service Bulletin 605-35-003, dated January
    28, 2016;  or  Bombardier  Service Bulletin  605-35-003,  Revision 01,
    dated February 10, 2016.

(i) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs):  The Manager, New York Air-
    craft Certification Office (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.

(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  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 Airworthiness Directive CF-2016-15,  dated June 1, 2016,  for
    related information. 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-2017-0477.

(2) For more information about this AD,  contact Cesar A. Gomez, Aerospace
    Engineer,  Airframe and Mechanical Systems Branch,  ANE-171,  FAA, New
    York ACO, 1600 Stewart Avenue, Ste 410, Westbury, NY 11590;  telephone
    516-228-7318; fax 516-794-5531.

(3) For  service information identified  in this AD,  contact  Bombardier,
    Inc., 400 Cote-Vertu Road West, Dorval, Quebec H4S 1Y9, Canada;  tele-
    phone 514-855-5000;  fax 514-855-7401;  email thd.crj@aero.bombardier.
    com; Internet http://www.bombardier.com. You may view this service in-
    formation 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.

Issued in Renton,  Washington, on May 12, 2017.  Michael  Kaszycki, Acting
Manager, Transport Airplane Directorate, Aircraft Certification Service.

DATES: We must receive comments on this proposed AD by July 6, 2017.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-0477; Directorate Identifier 2016-NM-112-AD]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc., Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for
certain Bombardier, Inc., Model CL-600-2B16 (CL-601-3A, CL-601-3R, and
CL-604 Variants) airplanes. This proposed AD was prompted by a report
indicating that the lanyard length of the passenger drop down oxygen
masks is too long. This proposed AD would require replacing the
existing oxygen mask lanyards with lanyards of the correct length. We
are proposing this AD to address the unsafe condition on these
products.

DATES: We must receive comments on this proposed AD by July 6, 2017.

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 http://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 Cote-Vertu Road West, Dorval, Quebec
H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855-7401; email
thd.crj@aero.bombardier.com; 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.

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-
0477; 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 proposed 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.
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Cesar A. Gomez, Aerospace Engineer,
Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft
Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury,
NY 11590; telephone 516-228-7318; fax 516-794-5531.

SUPPLEMENTARY INFORMATION:

Comments Invited

We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include "Docket No. FAA-2017-0477;
Directorate Identifier 2016-NM-112-AD" at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD based on those comments.

We will post all comments we receive, without change, to http://www.
regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this proposed AD.

Discussion

Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian Airworthiness Directive CF-
2016-15, dated June 1, 2016 (referred to after this as the Mandatory
Continuing Airworthiness Information, or "the MCAI"), to correct an
unsafe condition for certain Bombardier, Inc., Model CL-600-2B16 (CL-
601-3A, CL-601-3R, and CL-604 Variants) airplanes. The MCAI states:

Bombardier (BA) has determined that the lanyard length of the
passenger drop down oxygen masks is too long and may cause the
safety pin tethered to the opposite end of the lanyard to remain
engaged in the oxygen flow mechanism when the mask is pulled to the
passenger's face. In an emergency situation where oxygen is
required, it is possible that certain passengers may not receive
oxygen supply due to the increased length of the lanyard.

[Bombardier] has issued service bulletin (SB) 605-35-003 to
replace the existing lanyards in the passenger oxygen box assemblies
with lanyards of the correct length. Incorporation of this
[Bombardier service bulletin] will restore the proper oxygen flow
functionality to the passenger oxygen masks in the event of an
emergency.

This [Canadian] AD mandates the incorporation of [Bombardier
service bulletin] 605-35-003.

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-2017-0477.

Related Service Information Under 1 CFR Part 51

Bombardier, Inc., issued Service Bulletin 605-35-003, Revision 02,
dated April 18, 2016. This service information describes procedures for
replacing the existing oxygen mask lanyards with lanyards of the
correct length. 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 and Requirements of This Proposed AD

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 pertinent information and determined an unsafe condition
exists and is likely to exist or develop on other products of the same
type design.

Costs of Compliance

We estimate that this proposed AD affects 120 airplanes of U.S.
registry.

We estimate the following costs to comply with this proposed AD:

Estimated Costs

Action
Labor cost
Parts cost
Cost per product
Cost on U.S. operators
Replacement 4 work-hours x $85 per hour = $340 Not available
$340
$40,800

According to the manufacturer, some of the costs of this proposed
AD may be covered under warranty, thereby reducing the cost impact on
affected individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all 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.

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 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. 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.

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):