82 FR 27219 - Airworthiness Directives; Bombardier, Inc., Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 82, Issue 113 (June 14, 2017)

Page Range		27219-27221
FR Document		2017-09846

We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc., Model CL-600-2A12 (CL-601 Variant) and CL- 600-2B16 (CL-601-3A, CL-601-3R, and CL-604 Variants) airplanes. This proposed AD was prompted by a determination that the bushing holes on the engine mount rib might not conform to the engineering drawings and that certain inspections of the engine mount rib must be included in the airworthiness limitations section (ALS) of the Instructions for Continued Airworthiness (ICA). This proposed AD would require revising the maintenance or inspection program to incorporate certain airworthiness limitation items (ALIs). We are proposing this AD to address the unsafe condition on these products.

Federal Register, Volume 82 Issue 113 (Wednesday, June 14, 2017)

[Federal Register Volume 82, Number 113 (Wednesday, June 14, 2017)]
[Proposed Rules]
[Pages 27219-27221]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2017-09846]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-0338; Directorate Identifier 2016-NM-153-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-600-2A12 (CL-601 Variant) and CL-
600-2B16 (CL-601-3A, CL-601-3R, and CL-604 Variants) airplanes. This 
proposed AD was prompted by a determination that the bushing holes on 
the engine mount rib might not conform to the engineering drawings and 
that certain inspections of the engine mount rib must be included in 
the airworthiness limitations section (ALS) of the Instructions for 
Continued Airworthiness (ICA). This proposed AD would require revising 
the maintenance or inspection program to incorporate certain 
airworthiness limitation items (ALIs). We are proposing this AD to 
address the unsafe condition on these products.

DATES: We must receive comments on this proposed AD by July 31, 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.

[[Page 27220]]

    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 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-
0338; 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: Aziz Ahmed, Aerospace Engineer, 
Airframe and Mechanical Systems Branch, ANE-171, New York Aircraft 
Certification Office (ACO), FAA, 1600 Stewart Avenue, Suite 410, 
Westbury, NY 11590; telephone 516-228-7329; fax 516-794-5531.

SUPPLEMENTARY INFORMATION: 

Comments Invited

    We invite 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-2017-0338; 
Directorate Identifier 2016-NM-153-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-
2015-09R1, dated June 29, 2015 (referred to after this as the Mandatory 
Continuing Airworthiness Information, or ``the MCAI''), to correct an 
unsafe condition for certain Bombardier, Inc., Model CL-600-2A12 (CL-
601 Variant), and CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604 
Variants) airplanes. The MCAI states:

    The aeroplane manufacturer has determined that the bushing holes 
on the engine mount rib may not conform to the engineering drawings. 
Non-conforming bushing holes could increase loading on adjacent 
fasteners, resulting in premature fatigue cracking of the engine 
mount rib.
    In addition, it was also discovered that the inspection 
requirements for the engine mount rib were not listed in the 
Airworthiness Limitations Section of the Instructions for Continued 
Airworthiness.
    Failure of the engine mount rib could compromise the structural 
integrity of the engine mount and could lead to subsequent 
detachment of an engine.
    A new Time Limits/Maintenance Checks (TLMC) Airworthiness 
Limitations (AWL) task is introduced to ensure that any fatigue 
cracking of the engine mount rib is detected and corrected.
    The original issue of this [Canadian] AD mandated the 
incorporation of a new TLMC AWL task [into the maintenance or 
inspection program, as applicable].
    Revision 1 of this [Canadian] AD is issued to remove model CL-
600-1A11 (600) aeroplanes from the Applicability section of the 
[Canadian] AD since this model was incorrectly included in the 
original issue.

    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-
0338.

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.
    This AD requires revisions to certain operator maintenance 
documents to include new actions (e.g., inspections). Compliance with 
these actions is required by 14 CFR 91.403(c). For airplanes that have 
been previously modified, altered, or repaired in the areas addressed 
by this proposed AD, the operator may not be able to accomplish the 
actions described in the revisions. In this situation, to comply with 
14 CFR 91.403(c), the operator must request approval for an alternative 
method of compliance under the provisions of paragraph (i)(1) of this 
proposed AD. The request should include a description of changes to the 
required actions that will ensure the continued damage tolerance of the 
affected structure.

Costs of Compliance

    We estimate that this proposed AD affects 129 airplanes of U.S. 
registry.
    We estimate the following costs to comply with this proposed AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Revision of maintenance or inspection   1 work-hour x $85 per                 $0             $85         $10,965
 program.                                hour = $85.
----------------------------------------------------------------------------------------------------------------

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

[[Page 27221]]

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

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-2017-0338; Directorate Identifier 
2016-NM-153-AD.

(a) Comments Due Date

    We must receive comments by July 31, 2017.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to the Bombardier, Inc., airplanes identified in 
paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in 
any category.
    (1) Bombardier, Inc., Model CL-600-2A12 (CL-601) airplanes, 
having serial numbers (S/Ns) 3001 through 3066 inclusive.
    (2) Bombardier, Inc., Model CL-600-2B16 (CL-601-3A and CL-601-3R 
Variants) airplanes, having S/Ns 5001 through 5194 inclusive.
    (3) Bombardier, Inc., Model CL-600-2B16 (CL-604 Variant) 
airplanes, having S/Ns 5301 through 5665 inclusive, and 5701 and 
subsequent.

(d) Subject

    Air Transport Association (ATA) of America Code 05, Periodic 
inspections.

(e) Reason

    This AD was prompted by a determination that the bushing holes 
on the engine mount rib may not conform to the engineering drawings 
and that certain inspections of the engine mount rib must be 
included in the airworthiness limitations section (ALS) of the 
Instructions for Continued Airworthiness (ICA). We are issuing this 
AD to detect and correct failure of an engine mount rib. Failure of 
an engine mount rib could compromise the structural integrity of the 
engine mount and could lead to subsequent detachment of an engine.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Maintenance or Inspection Program Revision

    Within 60 days after the effective date of this AD: Revise the 
maintenance or inspection program, as applicable, to incorporate 
maintenance tasks, in accordance with a method approved by the 
Manager, New York Aircraft Certification Office (ACO), ANE-170, FAA.

    Note 1 to paragraph (g) of this AD:  Applicable information on 
tasks required by paragraph (g) of this AD can be found in Chapter 5 
of Time Limits/Maintenance Checks (TLMC) Manual PSP 601-5 (for Model 
CL-600-2A12 (CL-601 Variant) airplanes), TLMC Manual PSP 601A-5 (for 
CL-600-2B16 (CL-601-3A and CL-601-3R Variants) airplanes), TLMC 
Manual CL-604 (for Model CL-600-2B16 (CL-604 Variant) airplanes, S/
Ns 5301 through 5665 inclusive), and TLMC Manual CL-605 (for Model 
CL-600-2B16 (CL-604 Variant) airplanes, S/Ns 5701 and subsequent).

(h) No Alternative Actions and/or Intervals

    After the maintenance or inspection program has been revised as 
required by paragraph (g) of this AD, no alternative actions (e.g., 
inspections) and/or intervals may be used, unless the actions and/or 
intervals are approved as an alternative method of compliance (AMOC) 
in accordance with the procedures specified in paragraph (i)(1) of 
this AD.

(i) 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.
    (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-2015-09R1, dated June 29, 
2015, 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-2017-0338.
    (2) For more information about this AD, contact Aziz Ahmed, 
Aerospace Engineer, Airframe and Mechanical Systems Branch, ANE-171, 
New York Aircraft Certification Office (ACO), FAA, 1600 Stewart 
Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7329; fax 
516-794-5531.

    Issued in Renton, Washington, on May 8, 2017.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2017-09846 Filed 6-13-17; 8:45 am]
 BILLING CODE 4910-13-P

Federal Register / Vol. 82, No. 113 / Wednesday, June 14, 2017 / Proposed Rules 27219

38. The DHS/ALL–025 Law Enforcement the subject of a record to impede the (i) From subsection (g)(1) (Civil Remedies)
Authority in Support of the Protection of investigation, to tamper with witnesses or to the extent that the system is exempt from
Property Owned or Occupied by the evidence, and to avoid detection or other specific subsections of the Privacy Act.
Department of Homeland Security system of apprehension. Amendment of the records Dated: June 8, 2017.
records consists of electronic and paper could interfere with ongoing investigations Jonathan R. Cantor,
records and will be used by DHS and its and law enforcement activities and would
components. The DHS/ALL–025 Law impose an unreasonable administrative Acting Chief Privacy Officer, Department of
Enforcement Authority in Support of the burden by requiring investigations to be Homeland Security.
Protection of Property Owned or Occupied continually reinvestigated. In addition, [FR Doc. 2017–12253 Filed 6–13–17; 8:45 am]
by the Department of Homeland Security permitting access and amendment to such BILLING CODE 9110–9B–P
system is a repository of information held by information could disclose security-sensitive
DHS in connection with its several and information that could be detrimental to
varied missions and functions, including: homeland security.
The enforcement of civil and criminal laws; (c) From subsection (e)(1) (Relevancy and DEPARTMENT OF TRANSPORTATION
investigations, inquiries, and proceedings Necessity of Information) because in the
there under; and national security and course of investigations into potential Federal Aviation Administration
intelligence activities. The DHS/ALL–025 violations of federal law, the accuracy of
Law Enforcement Authority in Support of the information obtained or introduced 14 CFR Part 39
Protection of Property Owned or Occupied occasionally may be unclear, or the
by the Department of Homeland Security information may not be strictly relevant or [Docket No. FAA–2017–0338; Directorate
system contains information that is collected necessary to a specific investigation. In the Identifier 2016–NM–153–AD]
by, on behalf of, in support of, or in
interests of effective law enforcement, it is RIN 2120–AA64
cooperation with DHS and its components
appropriate to retain all information that may
and may contain personally identifiable
aid in establishing patterns of unlawful Airworthiness Directives; Bombardier,
information collected by other federal, state,
activity. Inc., Airplanes
local, tribal, foreign, or international
(d) From subsection (e)(2) (Collection of
government agencies. The Secretary of
Information from Individuals) because AGENCY: Federal Aviation
Homeland Security, pursuant to 5 U.S.C.
requiring that information be collected from Administration (FAA), DOT.
552a(j)(2), has exempted this system from the
the subject of an investigation would alert the
following provisions of the Privacy Act: 5 ACTION: Notice of proposed rulemaking
subject to the nature or existence of the
U.S.C. 552a(c)(3), (c)(4); (d); (e)(1), (e)(2), (NPRM).
investigation, thereby interfering with that
(e)(3), (e)(4)(G), (e)(4)(H), (e)(4)(I), (e)(5),
investigation and related law enforcement
(e)(8); (f), (g)(1). Additionally, the Secretary SUMMARY: We propose to adopt a new
of Homeland Security, pursuant to 5 U.S.C. activities.
(e) From subsection (e)(3) (Notice to airworthiness directive (AD) for certain
552a(k)(1), (k)(2), and (k)(5), has exempted Bombardier, Inc., Model CL–600–2A12
this system from the following provisions of Subjects) because providing such detailed
information could impede law enforcement (CL–601 Variant) and CL–600–2B16
the Privacy Act: 5 U.S.C. 552a(c)(3); (d);
(e)(1), (e)(4)(G), (e)(4)(H), (e)(4)(I); and (f). by compromising the existence of a (CL–601–3A, CL–601–3R, and CL–604
When a record received from another system confidential investigation or reveal the Variants) airplanes. This proposed AD
has been exempted in that source system identity of witnesses or confidential was prompted by a determination that
under 5 U.S.C. 552a(j)(2), DHS will claim the informants. the bushing holes on the engine mount
same exemptions for those records that are (f) From subsections (e)(4)(G), (e)(4)(H), rib might not conform to the engineering
claimed for the original primary systems of and (e)(4)(I) (Agency Requirements) and (f)
drawings and that certain inspections of
records from which they originated and (Agency Rules), because portions of this
system are exempt from the individual access
the engine mount rib must be included
claims any additional exemptions set forth in the airworthiness limitations section
here. Exemptions from these particular provisions of subsection (d) for the reasons
noted above, and therefore DHS is not (ALS) of the Instructions for Continued
subsections are justified, on a case-by-case
basis to be determined at the time a request required to establish requirements, rules, or Airworthiness (ICA). This proposed AD
is made, for the following reasons: procedures with respect to such access. would require revising the maintenance
(a) From subsection (c)(3) and (4) Providing notice to individuals with respect or inspection program to incorporate
(Accounting for Disclosures) because release to the existence of records pertaining to them certain airworthiness limitation items
of the accounting of disclosures could alert in the system of records or otherwise setting (ALIs). We are proposing this AD to
the subject of an investigation of an actual or up procedures pursuant to which individuals address the unsafe condition on these
potential criminal, civil, or regulatory may access and view records pertaining to
products.
violation to the existence of that investigation themselves in the system would undermine
and reveal investigative interest on the part investigative efforts and reveal the identities DATES: We must receive comments on
of DHS as well as the recipient agency. of witnesses, and potential witnesses, and this proposed AD by July 31, 2017.
Disclosure of the accounting would therefore confidential informants. ADDRESSES: You may send comments,
present a serious impediment to law (g) From subsection (e)(5) (Collection of
Information) because with the collection of
using the procedures found in 14 CFR
enforcement efforts and/or efforts to preserve
information for law enforcement purposes, it 11.43 and 11.45, by any of the following
national security. Disclosure of the
accounting would also permit the individual is impossible to determine in advance what methods:
who is the subject of a record to impede the information is accurate, relevant, timely, and • Federal eRulemaking Portal: Go to
investigation, to tamper with witnesses or complete. Compliance with subsection (e)(5) http://www.regulations.gov. Follow the
evidence, and to avoid detection or would preclude DHS agents from using their instructions for submitting comments.
apprehension, which would undermine the investigative training and exercise of good • Fax: 202–493–2251.
entire investigative process. judgment to both conduct and report on • Mail: U.S. Department of
mstockstill on DSK30JT082PROD with PROPOSALS

(b) From subsection (d) (Access to Records) investigations. Transportation, Docket Operations, M–
because access to the records contained in (h) From subsection (e)(8) (Notice on 30, West Building Ground Floor, Room
this system of records could inform the Individuals) because compliance would
W12–140, 1200 New Jersey Avenue SE.,
subject of an investigation of an actual or interfere with DHS’s ability to obtain, serve,
potential criminal, civil, or regulatory and issue subpoenas, warrants, and other law Washington, DC 20590.
violation to the existence of that investigation enforcement mechanisms that may be filed • Hand Delivery: Deliver to Mail
and reveal investigative interest on the part under seal and could result in disclosure of address above between 9 a.m. and 5
of DHS or another agency. Access to the investigative techniques, procedures, and p.m., Monday through Friday, except
records could permit the individual who is evidence. Federal holidays.

VerDate Sep<11>2014 17:21 Jun 13, 2017 Jkt 241001 PO 00000 Frm 00003 Fmt 4702 Sfmt 4702 E:\FR\FM\14JNP1.SGM 14JNP1

Federal Register / Vol. 82, No. 113 / Wednesday, June 14, 2017 / Proposed Rules 27221

because it addresses an unsafe condition (2) Bombardier, Inc., Model CL–600–2B16 accordance with 14 CFR 39.19, send your
that is likely to exist or develop on (CL–601–3A and CL–601–3R Variants) request to your principal inspector or local
products identified in this rulemaking airplanes, having S/Ns 5001 through 5194 Flight Standards District Office, as
inclusive. appropriate. If sending information directly
action.
(3) Bombardier, Inc., Model CL–600–2B16 to the ACO, send it to ATTN: Program
Regulatory Findings (CL–604 Variant) airplanes, having S/Ns 5301 Manager, Continuing Operational Safety,
through 5665 inclusive, and 5701 and FAA, New York ACO, 1600 Stewart Avenue,
We determined that this proposed AD subsequent. Suite 410, Westbury, NY 11590; telephone
would not have federalism implications 516–228–7300; fax 516–794–5531. Before
under Executive Order 13132. This (d) Subject using any approved AMOC, notify your
proposed AD would not have a Air Transport Association (ATA) of appropriate principal inspector, or lacking a
substantial direct effect on the States, on America Code 05, Periodic inspections. principal inspector, the manager of the local
the relationship between the national flight standards district office/certificate
(e) Reason holding district office.
Government and the States, or on the
This AD was prompted by a determination (2) Contacting the Manufacturer: For any
distribution of power and
that the bushing holes on the engine mount requirement in this AD to obtain corrective
responsibilities among the various rib may not conform to the engineering actions from a manufacturer, the action must
levels of government. drawings and that certain inspections of the be accomplished using a method approved
For the reasons discussed above, I engine mount rib must be included in the by the Manager, New York ACO, ANE–170,
certify this proposed regulation: airworthiness limitations section (ALS) of the FAA; or Transport Canada Civil Aviation
1. Is not a ‘‘significant regulatory Instructions for Continued Airworthiness (TCCA); or Bombardier, Inc.’s TCCA Design
action’’ under Executive Order 12866; (ICA). We are issuing this AD to detect and Approval Organization (DAO). If approved by
2. Is not a ‘‘significant rule’’ under the correct failure of an engine mount rib. Failure the DAO, the approval must include the
DOT Regulatory Policies and Procedures of an engine mount rib could compromise the DAO-authorized signature.
(44 FR 11034, February 26, 1979); structural integrity of the engine mount and
(j) Related Information
3. Will not affect intrastate aviation in could lead to subsequent detachment of an
Alaska; and engine. (1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) Canadian
4. Will not have a significant (f) Compliance Airworthiness Directive CF–2015–09R1,
economic impact, positive or negative, dated June 29, 2015, for related information.
Comply with this AD within the
on a substantial number of small entities compliance times specified, unless already This MCAI may be found in the AD docket
under the criteria of the Regulatory done. on the Internet at http://www.regulations.gov
Flexibility Act. by searching for and locating Docket No.
(g) Maintenance or Inspection Program FAA–2017–0338.
List of Subjects in 14 CFR Part 39 Revision (2) For more information about this AD,
Air transportation, Aircraft, Aviation Within 60 days after the effective date of contact Aziz Ahmed, Aerospace Engineer,
safety, Incorporation by reference, this AD: Revise the maintenance or Airframe and Mechanical Systems Branch,
Safety. inspection program, as applicable, to ANE–171, New York Aircraft Certification
incorporate maintenance tasks, in accordance Office (ACO), FAA, 1600 Stewart Avenue,
The Proposed Amendment with a method approved by the Manager, Suite 410, Westbury, NY 11590; telephone
New York Aircraft Certification Office (ACO), 516–228–7329; fax 516–794–5531.
Accordingly, under the authority
ANE–170, FAA. Issued in Renton, Washington, on May 8,
delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part Note 1 to paragraph (g) of this AD: 2017.
Applicable information on tasks required by Michael Kaszycki,
39 as follows:
paragraph (g) of this AD can be found in
Acting Manager, Transport Airplane
Chapter 5 of Time Limits/Maintenance
PART 39—AIRWORTHINESS Directorate, Aircraft Certification Service.
Checks (TLMC) Manual PSP 601–5 (for
DIRECTIVES Model CL–600–2A12 (CL–601 Variant) [FR Doc. 2017–09846 Filed 6–13–17; 8:45 am]
airplanes), TLMC Manual PSP 601A–5 (for BILLING CODE 4910–13–P
■ 1. The authority citation for part 39
CL–600–2B16 (CL–601–3A and CL–601–3R
continues to read as follows: Variants) airplanes), TLMC Manual CL–604
Authority: 49 U.S.C. 106(g), 40113, 44701. (for Model CL–600–2B16 (CL–604 Variant) ENVIRONMENTAL PROTECTION
airplanes, S/Ns 5301 through 5665 inclusive),
§ 39.13 [Amended] and TLMC Manual CL–605 (for Model CL–
AGENCY
■ 2. The FAA amends § 39.13 by adding 600–2B16 (CL–604 Variant) airplanes, S/Ns
40 CFR Part 52
the following new airworthiness 5701 and subsequent).
directive (AD): [EPA–R06–OAR–2015–0833; FRL–9962–49–
(h) No Alternative Actions and/or Intervals Region 6]
Bombardier, Inc.: Docket No. FAA–2017– After the maintenance or inspection
0338; Directorate Identifier 2016–NM–
program has been revised as required by Approval and Promulgation of
153–AD.
paragraph (g) of this AD, no alternative Implementation Plans; Texas; Clean
(a) Comments Due Date actions (e.g., inspections) and/or intervals Air Act Requirements for Vehicle
We must receive comments by July 31, may be used, unless the actions and/or Inspection and Maintenance and
2017. intervals are approved as an alternative
Nonattainment New Source Review
method of compliance (AMOC) in
(b) Affected ADs accordance with the procedures specified in AGENCY: Environmental Protection
None. paragraph (i)(1) of this AD. Agency (EPA).
mstockstill on DSK30JT082PROD with PROPOSALS

(c) Applicability (i) Other FAA AD Provisions ACTION: Proposed rule.
This AD applies to the Bombardier, Inc., The following provisions also apply to this SUMMARY: Pursuant to the Federal Clean
airplanes identified in paragraphs (c)(1), AD:
(1) Alternative Methods of Compliance
Air Act (CAA or Act), the
(c)(2), and (c)(3) of this AD, certificated in
any category. (AMOCs): The Manager, New York ACO, Environmental Protection Agency (EPA)
(1) Bombardier, Inc., Model CL–600–2A12 ANE–170, FAA, has the authority to approve is proposing to approve a State
(CL–601) airplanes, having serial numbers (S/ AMOCs for this AD, if requested using the Implementation Plan (SIP) revision
Ns) 3001 through 3066 inclusive. procedures found in 14 CFR 39.19. In submitted by the State of Texas for the

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Document Created: 2017-06-14 01:23:32
Document Modified: 2017-06-14 01:23:32

Category		Regulatory Information
Collection		Federal Register
sudoc Class		AE 2.7: GS 4.107: AE 2.106:
Publisher		Office of the Federal Register, National Archives and Records Administration
Section		Proposed Rules
Action		Notice of proposed rulemaking (NPRM).
Dates		We must receive comments on this proposed AD by July 31, 2017.
Contact		Aziz Ahmed, Aerospace Engineer, Airframe and Mechanical Systems Branch, ANE-171, New York Aircraft Certification Office (ACO), FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7329; fax 516-794-5531.
FR Citation		82 FR 27219
RIN Number		2120-AA64
CFR Associated		Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

82 FR 27219 - Airworthiness Directives; Bombardier, Inc., Airplanes

DEPARTMENT OF TRANSPORTATIONFederal Aviation Administration

Federal Register Volume 82, Issue 113 (June 14, 2017)

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration