82_FR_23250 82 FR 23153 - Airworthiness Directives; Embraer S.A. Airplanes

82 FR 23153 - Airworthiness Directives; Embraer S.A. Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 82, Issue 97 (May 22, 2017)

Page Range23153-23156
FR Document2017-10136

We are revising an earlier notice of proposed rulemaking (NPRM) to supersede an Airworthiness Directive (AD) for all Embraer S.A. Model ERJ 190-100 STD, -100 LR, and -100 IGW airplanes; and Model ERJ 190-200 STD, -200 LR, and -200 IGW airplanes. This action revises the NPRM by adding a requirement to revise the maintenance or inspection program, as applicable, to incorporate new airworthiness limitations and adding certain airplanes to the applicability. We are proposing this airworthiness directive (AD) to address the unsafe condition on these products. Since these actions impose an additional burden over those proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.

Federal Register, Volume 82 Issue 97 (Monday, May 22, 2017) 
[Federal Register Volume 82, Number 97 (Monday, May 22, 2017)]
[Proposed Rules]
[Pages 23153-23156]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2017-10136]


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Proposed Rules
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains notices to the public of 
the proposed issuance of rules and regulations. The purpose of these 
notices is to give interested persons an opportunity to participate in 
the rule making prior to the adoption of the final rules.

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Federal Register / Vol. 82, No. 97 / Monday, May 22, 2017 / Proposed 
Rules

[[Page 23153]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0008; Directorate Identifier 2013-NM-076-AD]
RIN 2120-AA64


Airworthiness Directives; Embraer S.A. Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Supplemental notice of proposed rulemaking (SNPRM); reopening 
of comment period.

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

SUMMARY: We are revising an earlier notice of proposed rulemaking 
(NPRM) to supersede an Airworthiness Directive (AD) for all Embraer 
S.A. Model ERJ 190-100 STD, -100 LR, and -100 IGW airplanes; and Model 
ERJ 190-200 STD, -200 LR, and -200 IGW airplanes. This action revises 
the NPRM by adding a requirement to revise the maintenance or 
inspection program, as applicable, to incorporate new airworthiness 
limitations and adding certain airplanes to the applicability. We are 
proposing this airworthiness directive (AD) to address the unsafe 
condition on these products. Since these actions impose an additional 
burden over those proposed in the NPRM, we are reopening the comment 
period to allow the public the chance to comment on these proposed 
changes.

DATES: The comment period for the NPRM published in the Federal 
Register on February 3, 2014 (79 FR 6106), is reopened.
    We must receive comments on this SNPRM 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: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday 
through Friday, except Federal holidays.
    For service information identified in this SNPRM, contact Embraer 
S.A., Technical Publications Section (PC 060), Av. Brigadeiro Faria 
Lima, 2170--Putim--12227-901 S[atilde]o Jose dos Campos--SP--BRASIL; 
telephone +55 12 3927-5852 or +55 12 3309-0732; fax +55 12 3927-7546; 
email distrib@embraer.com.br; Internet http://www.flyembraer.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-2014-
0008; 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 SNPRM, the regulatory evaluation, any comments received, 
and other information. The street address for the Docket 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: Ana Martinez Hueto, Aerospace 
Engineer, International Branch, ANM-116, Transport Airplane 
Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; 
telephone 425-227-1622; fax 425-227-1320.

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-2014-0008; 
Directorate Identifier 2013-NM-076-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of this SNPRM. We will 
consider all comments received by the closing date and may amend this 
SNPRM 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 SNPRM.

Discussion

    On November 13, 2012, we issued AD 2012-23-09, Amendment 39-17265 
(77 FR 73270, December 10, 2012) (``AD 2012-23-09''). AD 2012-23-09 
requires actions intended to address an unsafe condition on all Embraer 
S.A. Model ERJ 190-100 STD, -100 LR, and -100 IGW airplanes; and Model 
ERJ 190-200 STD, -200 LR, and -200 IGW airplanes.
    We issued an NPRM to amend 14 CFR part 39 by adding an AD to 
supersede AD 2012-23-09 that would apply to all Embraer S.A. Model ERJ 
190-100 STD, -100 LR, and -100 IGW airplanes; and Model ERJ 190-200 
STD, -200 LR, and -200 IGW airplanes. The NPRM published in the Federal 
Register on February 3, 2014 (79 FR 6106). The NPRM was prompted by a 
determination that more restrictive maintenance requirements and 
airworthiness limitations were necessary. The NPRM proposed to require 
a revision to the maintenance or inspection program to incorporate new 
inspection tasks and their respective thresholds and intervals.

Actions Since the NPRM was Issued

    Since we issued the NPRM, a new revision of the airworthiness 
limitations section (ALS) of the EMBRAER ERJ 190/195 Maintenance Review 
Board Report (MRBR) was issued, which contains more restrictive 
airworthiness limitations. The Ag[ecirc]ncia Nacional de 
Avia[ccedil][atilde]o Civil (ANAC), which is the aviation authority for 
Brazil, has issued Brazilian Airworthiness Directive 2016-04-01, 
effective April 4, 2016 (referred to after this as the Mandatory 
Continuing Airworthiness Information, or ``the MCAI''), to correct an 
unsafe condition on certain Embraer S.A. Model ERJ 190-100 STD, -100 
LR, -100 IGW, and -100 ECJ airplanes; and

[[Page 23154]]

Model ERJ 190-200 STD, -200 LR, and -200 IGW airplanes. The MCAI 
states:

    This [Brazilian] AD was prompted by a determination that 
existing maintenance requirements and airworthiness limitations are 
inadequate to ensure the structural integrity of the airplane. We 
are issuing this [Brazilian] AD to prevent failure of certain system 
components, which could result in reduced structural integrity [and 
system reliability] of the airplane.

    The required action is revising the maintenance or inspection 
program, as applicable, to incorporate the airworthiness limitations.
    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-2014-
0008.

Related Service Information Under 1 CFR Part 51

    Embraer S.A. has issued Appendix A--Airworthiness Limitations, Part 
1--Certification Maintenance Requirements, Part 2--Airworthiness 
Limitation Inspections--Structures, Part 3--Fuel System Limitation 
Items, and Part 4--Life-Limited Items, of the EMBRAER ERJ 190/195 
Maintenance Review Board Report (MRBR), MRB-1928, Revision 9, dated 
August 14, 2015 (``MRB-1928, Revision 9''). This service information 
describes airworthiness limitations (Part 1, Part 2, Part 3, and Part 4 
in Appendix A--Airworthiness Limitations of MRB-1928, Revision 9, make 
up the airworthiness limitations).
    Embraer S.A. has also issued Temporary Revision 9-1, dated October 
27, 2015, to Appendix A--Airworthiness Limitations, of MRB-1928, 
Revision 9, which provides revised airworthiness limitation inspections 
and life limited items due to new structural provisions for Live TV and 
Connectivity System.
    In addition, Embraer S.A. has issued Temporary Revision 9-3, dated 
October 27, 2015, to Appendix A--Airworthiness Limitations, of MRB-
1928, Revision 9, which updates the life limitations of certain main 
landing gear and nose landing gear components.
    Embraer S.A. has also issued Appendix A, Airworthiness Limitation, 
of the EMBRAER ERJ 190-100 ECJ Maintenance Planning Guide (MPG), MPG-
2928, Revision 4, dated July 14, 2014 (``MPG-2928, Revision 4''). This 
service information describes airworthiness limitations (Part 1, 
Certification Maintenance Requirements, Part 2, Airworthiness 
Limitation Inspections--Structures, Part 3, Fuel System Limitation 
Items, and Part 4, Life Limited Items, of the MPG make up the 
airworthiness limitations).
    Embraer S.A. has also issued Temporary Revision 4-2, dated February 
13, 2015, to Appendix A, Part 2, of MPG-2928, Revision 4, which 
describes detailed inspections for the upper doubler at the forward 
passenger door cutout.
    Furthermore, Embraer S.A. has issued Temporary Revision 4-3, dated 
October 30, 2015, to Appendix A, Part 4, of MPG-2928, Revision 4, which 
updates the life limitations of certain main landing gear and nose 
landing components.
    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.

Comments

    We gave the public the opportunity to participate in developing 
this proposed AD. We received no comments on the NPRM or on the 
determination of the cost to the public.

FAA's Determination and Requirements of This SNPRM

    This proposed AD would require revisions to certain operator 
maintenance documents to include new actions (e.g., inspections) and 
Critical Design Configuration Control Limitations (CDCCLs). Compliance 
with these actions and CDCCLs 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 according to paragraph 
(k)(1) of this proposed AD. The request should include a description of 
changes to the required inspections that will ensure the continued 
damage tolerance of the affected structure.
    Notwithstanding any other maintenance or operational requirements, 
components that have been identified as airworthy or installed on the 
affected airplanes before accomplishing the revision of the airplane 
maintenance or inspection program specified in this proposed AD, do not 
need to be reworked in accordance with the CDCCLs. However, once the 
airplane maintenance or inspection program has been revised as required 
by this proposed AD, future maintenance actions on these components 
must be done in accordance with the CDCCLs.
    Certain changes described above expand the scope of the NPRM. As a 
result, we have determined that it is necessary to reopen the comment 
period to provide additional opportunity for the public to comment on 
this SNPRM.

Costs of Compliance

    We estimate that this SNPRM affects 83 airplanes of U.S. registry.
    The actions that are required by AD 2012-23-09 and retained in this 
SNPRM take about 1 work-hour per product, at an average labor rate of 
$85 per work-hour. Required parts cost about $0 per product. Based on 
these figures, the estimated cost of the actions that were required by 
AD 2012-23-09 is $85 per product.
    We also estimate that it would take about 1 work-hour per product 
to comply with the new basic requirements of this SNPRM. The average 
labor rate is $85 per work-hour. Required parts would cost about $0 per 
product. Based on these figures, we estimate the cost of this SNPRM on 
U.S. operators to be $7,055, or $85 per product.

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;

[[Page 23155]]

    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 removing Airworthiness Directive (AD) 
2012-23-09, Amendment 39-17265 (77 FR 73270, December 10, 2012), and 
adding the following new airworthiness directive (AD):

Embraer S.A.: Docket No. FAA-2014-0008; Directorate Identifier 2013-
NM-076-AD.

(a) Comments Due Date

    We must receive comments by July 6, 2017.

(b) Affected ADs

    This AD replaces AD 2012-23-09, Amendment 39-17265 (77 FR 73270, 
December 10, 2012) (``AD 2012-23-09'').

(c) Applicability

    This AD applies to Embraer S.A. Model ERJ 190-100 STD, -100 LR, 
-100 ECJ, and -100 IGW airplanes; and Model ERJ 190-200 STD, -200 
LR, and -200 IGW airplanes; certificated in any category; serial 
numbers 19000002, 19000004, 19000006 through 19000213 inclusive, 
19000215 through 19000276 inclusive, 19000278 through 19000466 
inclusive, 19000468 through 19000525 inclusive, and 19000527 through 
19000696 inclusive.

(d) Subject

    Air Transport Association (ATA) of America Codes 27, Flight 
controls; 28, Fuel; 52, Doors; 53, Fuselage; 54, Nacelles/pylons; 
55, Stabilizers; 57, Wings; 71, Powerplant; and 78, Exhaust.

(e) Reason

    This AD was prompted by a determination that more restrictive 
airworthiness limitations are necessary. We are issuing this AD to 
detect and correct fatigue cracking of structural components and to 
prevent failure of certain system components; these conditions could 
result in reduced structural integrity and system reliability of the 
airplane.

(f) Compliance

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

(g) Retained Revision of the Maintenance Program, With No Changes

    For Model ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 
190-200 STD, ERJ 190-200 LR, and ERJ 190-200 IGW airplanes: This 
paragraph restates the actions required by paragraph (h) of AD 2012-
23-09, with no changes. Within 90 days after January 14, 2013 (the 
effective date of AD 2012-23-09), revise the maintenance program to 
incorporate the tasks specified in Part 2--Airworthiness Limitation 
Inspections (ALI)--Structures, of Appendix A, Airworthiness 
Limitations (AL), of the EMBRAER 190 Maintenance Review Board 
Report, MRB-1928, Revision 5, dated November 11, 2010; and EMBRAER 
Temporary Revision (TR) 5-1, dated February 11, 2011, to Part 2--
Airworthiness Limitation Inspections (ALI)--Structures, of Appendix 
A, Airworthiness Limitations (AL), of the EMBRAER 190 Maintenance 
Review Board Report, MRB-1928, Revision 5, dated November 11, 2010; 
with the thresholds and intervals stated in these documents. The 
initial compliance times for the tasks are stated in the 
``Implementation Plan'' section of Appendix A, Airworthiness 
Limitations (AL), of the EMBRAER 190 Maintenance Review Board 
Report, MRB-1928, Revision 5, dated November 11, 2010.

(h) Retained No Alternative Actions or Intervals, With New Exception

    This paragraph restates the actions required by paragraph (i) of 
AD 2012-23-09, with a new exception. After accomplishing the 
revision required by paragraph (g) of this AD, no alternative 
actions (e.g., inspections) or intervals, may be used, unless the 
actions or intervals are approved as an alternative method of 
compliance (AMOC) in accordance with the procedures specified in 
paragraph (k)(1) of this AD, and except as required by paragraph (i) 
of this AD.

(i) New Requirements of This AD: Revision of the Maintenance or 
Inspection Program

    (1) For Model ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, 
ERJ 190-200 STD, ERJ 190-200 LR, and ERJ 190-200 IGW airplanes: 
Within 90 days after the effective date of this AD, revise the 
maintenance or inspection program, as applicable, to incorporate the 
tasks specified in Part 2--Airworthiness Limitation Inspections--
Structures, of Appendix A--Airworthiness Limitations, of the EMBRAER 
190/195 Maintenance Review Board Report, MRB-1928, Revision 9, dated 
August 14, 2015 (``MRB-1928, Revision 9''); EMBRAER Temporary 
Revision 9-1, dated October 27, 2015, to Part 2--Airworthiness 
Limitation Inspections--Structures, and Part 4--Life Limited Items, 
of Appendix A, Airworthiness Limitations, of MRB-1928, Revision 9; 
and EMBRAER Temporary Revision 9-3, dated October 27, 2015, to Part 
2--Airworthiness Limitation Inspections--Structures, of Appendix A, 
Airworthiness Limitations, of MRB-1928, Revision 9; with the 
thresholds and intervals stated in these documents. The initial 
compliance times for the tasks are at the later of the times 
specified in paragraphs (i)(1)(i) and (i)(1)(ii) of this AD. Doing 
the revision required by this paragraph terminates the revision 
required by paragraph (g) of this AD.
    (i) Within the applicable times specified in MRB-1928, Revision 
9; EMBRAER Temporary Revision 9-1, dated October 27, 2015, to Part 
2--Airworthiness Limitation Inspections--Structures, and Part 4--
Life Limited Items, of Appendix A, Airworthiness Limitations, of 
MRB-1928, Revision 9; and EMBRAER Temporary Revision 9-3, dated 
October 27, 2015, to Part 2--Airworthiness Limitation Inspections--
Structures, of Appendix A, Airworthiness Limitations, of MRB-1928, 
Revision 9. Where tasks are listed in both MRB-1928, Revision 9, and 
a temporary revision, the compliance times in the temporary revision 
take precedence.
    (ii) Within 90 days or 600 flight cycles after the effective 
date of this AD, whichever occurs later.
    (2) For Model ERJ 190-100 ECJ airplanes: Within 90 days after 
the effective date of this AD, revise the maintenance or inspection 
program, as applicable, to incorporate the tasks specified in Part 
1, Certification Maintenance Requirements, Part 2, Airworthiness 
Limitation Inspections--Structures, Part 3, Fuel System Limitation 
Items, and Part 4, Life Limited Items, of Appendix A, Airworthiness 
Limitation, of the EMBRAER ERJ 190-100 ECJ Maintenance Planning 
Guide, MPG-2928, Revision 4, dated July 14, 2014; EMBRAER Temporary 
Revision (TR) 4-2, dated February 13, 2015, and EMBRAER TR 4-3, 
dated October 30, 2015; with the thresholds and intervals stated in 
these documents. The initial compliance times for the tasks are at 
the later of the times specified in paragraphs (i)(2)(i) and 
(i)(2)(ii) of this AD.
    (i) Within the applicable times specified in Part 1, 
Certification Maintenance Requirements, Part 2, Airworthiness 
Limitation Inspections--Structures, Part 3, Fuel System Limitation 
Items, and Part 4, Life Limited Items, of Appendix A, Airworthiness 
Limitation, of the EMBRAER ERJ 190-100 ECJ Maintenance Planning 
Guide, MPG-2928, Revision 4, dated July 14, 2014; EMBRAER TR 4-2, 
dated February 13, 2015; and EMBRAER TR 4-3, dated October 30, 2015. 
Where tasks are listed in both MPG-2928, Revision 4, and a temporary 
revision, the compliance times in the temporary revision take 
precedence.
    (ii) Within 90 days or 600 flight cycles after the effective 
date of this AD, whichever occurs later.

(j) No Alternative Actions, Intervals, and/or Critical Design 
Configuration Control Limitations (CDCCLs)

    After accomplishment of the revision required by paragraph (i) 
of this AD, no alternative actions (e.g., inspections), intervals, 
and/or CDCCLs may be used unless the actions, intervals, and/or 
CDCCLs are

[[Page 23156]]

approved as an AMOC in accordance with the procedures specified in 
paragraph (k)(1) of this AD.

(k) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Branch, ANM-116, Transport Airplane Directorate, 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 International Branch, send it to the attention of 
the person identified in paragraph (l)(2) of this AD. Information 
may be emailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. 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: As of the effective date of 
this AD, 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, International Branch, ANM-116, Transport 
Airplane Directorate, FAA; or the Ag[ecirc]ncia Nacional de 
Avia[ccedil][atilde]o Civil (ANAC); or ANAC's authorized Designee. 
If approved by the ANAC Designee, the approval must include the 
Designee's authorized signature.

(l) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) Brazilian Airworthiness Directive 2016-04-01, effective April 
4, 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-2014-0008.
    (2) For more information about this AD, contact Ana Martinez 
Hueto, Aerospace Engineer, International Branch, ANM-116, Transport 
Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-
3356; telephone 425-227-1622; fax 425-227-1320.
    (3) For service information identified in this AD, contact 
Embraer S.A., Technical Publications Section (PC 060), Av. 
Brigadeiro Faria Lima, 2170--Putim--12227-901 S[atilde]o Jose dos 
Campos--SP--BRASIL; telephone +55 12 3927-5852 or +55 12 3309-0732; 
fax +55 12 3927-7546; email distrib@embraer.com.br; Internet http://www.flyembraer.com. 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.

    Issued in Renton, Washington, on May 8, 2017.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2017-10136 Filed 5-19-17; 8:45 am]
 BILLING CODE 4910-13-P

23153 Proposed Rules Federal Register Vol. 82, No. 97 Monday, May 22, 2017 This section of the FEDERAL REGISTER • Mail: U.S. Department of your comments. We specifically invite contains notices to the public of the proposed Transportation, Docket Operations, M– comments on the overall regulatory, issuance of rules and regulations. The 30, West Building Ground Floor, Room economic, environmental, and energy purpose of these notices is to give interested W12–140, 1200 New Jersey Avenue SE., aspects of this SNPRM. We will persons an opportunity to participate in the Washington, DC 20590. consider all comments received by the rule making prior to the adoption of the final rules. • Hand Delivery: U.S. Department of closing date and may amend this Transportation, Docket Operations, M– SNPRM based on those comments. 30, West Building Ground Floor, Room We will post all comments we DEPARTMENT OF TRANSPORTATION W12–140, 1200 New Jersey Avenue SE., receive, without change, to http:// Washington, DC, between 9 a.m. and 5 www.regulations.gov, including any Federal Aviation Administration p.m., Monday through Friday, except personal information you provide. We Federal holidays. will also post a report summarizing each 14 CFR Part 39 For service information identified in substantive verbal contact we receive this SNPRM, contact Embraer S.A., about this SNPRM. [Docket No. FAA–2014–0008; Directorate Technical Publications Section (PC Identifier 2013–NM–076–AD] 060), Av. Brigadeiro Faria Lima, 2170— Discussion RIN 2120–AA64 Putim—12227–901 São Jose dos On November 13, 2012, we issued AD Campos—SP—BRASIL; telephone +55 2012–23–09, Amendment 39–17265 (77 Airworthiness Directives; Embraer S.A. 12 3927–5852 or +55 12 3309–0732; fax FR 73270, December 10, 2012) (‘‘AD Airplanes +55 12 3927–7546; email distrib@ 2012–23–09’’). AD 2012–23–09 requires embraer.com.br; Internet http:// actions intended to address an unsafe AGENCY: Federal Aviation www.flyembraer.com. You may view condition on all Embraer S.A. Model Administration (FAA), DOT. this referenced service information at ERJ 190–100 STD, –100 LR, and –100 ACTION: Supplemental notice of the FAA, Transport Airplane IGW airplanes; and Model ERJ 190–200 proposed rulemaking (SNPRM); Directorate, 1601 Lind Avenue SW., STD, –200 LR, and –200 IGW airplanes. reopening of comment period. Renton, WA. For information on the We issued an NPRM to amend 14 CFR availability of this material at the FAA, part 39 by adding an AD to supersede SUMMARY: We are revising an earlier call 425–227–1221. AD 2012–23–09 that would apply to all notice of proposed rulemaking (NPRM) Embraer S.A. Model ERJ 190–100 STD, to supersede an Airworthiness Directive Examining the AD Docket –100 LR, and –100 IGW airplanes; and (AD) for all Embraer S.A. Model ERJ You may examine the AD docket on Model ERJ 190–200 STD, –200 LR, and 190–100 STD, –100 LR, and –100 IGW the Internet at http:// –200 IGW airplanes. The NPRM airplanes; and Model ERJ 190–200 STD, www.regulations.gov by searching for published in the Federal Register on –200 LR, and –200 IGW airplanes. This and locating Docket No. FAA–2014– February 3, 2014 (79 FR 6106). The action revises the NPRM by adding a 0008; or in person at the Docket NPRM was prompted by a requirement to revise the maintenance Management Facility between 9 a.m. determination that more restrictive or inspection program, as applicable, to and 5 p.m., Monday through Friday, maintenance requirements and incorporate new airworthiness except Federal holidays. The AD docket airworthiness limitations were limitations and adding certain airplanes contains this SNPRM, the regulatory necessary. The NPRM proposed to to the applicability. We are proposing evaluation, any comments received, and require a revision to the maintenance or this airworthiness directive (AD) to other information. The street address for inspection program to incorporate new address the unsafe condition on these the Docket Office (telephone: 800–647– inspection tasks and their respective products. Since these actions impose an 5527) is in the ADDRESSES section. thresholds and intervals. additional burden over those proposed Comments will be available in the AD in the NPRM, we are reopening the docket shortly after receipt. Actions Since the NPRM was Issued comment period to allow the public the FOR FURTHER INFORMATION CONTACT: Ana Since we issued the NPRM, a new chance to comment on these proposed Martinez Hueto, Aerospace Engineer, revision of the airworthiness limitations changes. International Branch, ANM–116, section (ALS) of the EMBRAER ERJ 190/ DATES: The comment period for the Transport Airplane Directorate, FAA, 195 Maintenance Review Board Report NPRM published in the Federal 1601 Lind Avenue SW., Renton, WA (MRBR) was issued, which contains Register on February 3, 2014 (79 FR 98057–3356; telephone 425–227–1622; more restrictive airworthiness 6106), is reopened. fax 425–227–1320. limitations. The Agência Nacional de We must receive comments on this SUPPLEMENTARY INFORMATION: Aviação Civil (ANAC), which is the SNPRM by July 6, 2017. aviation authority for Brazil, has issued Comments Invited nlaroche on DSK30NT082PROD with PROPOSALS ADDRESSES: You may send comments, Brazilian Airworthiness Directive 2016– using the procedures found in 14 CFR We invite you to send any written 04–01, effective April 4, 2016 (referred 11.43 and 11.45, by any of the following relevant data, views, or arguments about to after this as the Mandatory methods: this proposed AD. Send your comments Continuing Airworthiness Information, • Federal eRulemaking Portal: Go to to an address listed under the or ‘‘the MCAI’’), to correct an unsafe http://www.regulations.gov. Follow the ADDRESSES section. Include ‘‘Docket No. condition on certain Embraer S.A. instructions for submitting comments. FAA–2014–0008; Directorate Identifier Model ERJ 190–100 STD, –100 LR, –100 • Fax: 202–493–2251. 2013–NM–076–AD’’ at the beginning of IGW, and –100 ECJ airplanes; and VerDate Sep<11>2014 12:41 May 19, 2017 Jkt 241001 PO 00000 Frm 00001 Fmt 4702 Sfmt 4702 E:\FR\FM\22MYP1.SGM 22MYP1

23154 Federal Register / Vol. 82, No. 97 / Monday, May 22, 2017 / Proposed Rules Model ERJ 190–200 STD, –200 LR, and Embraer S.A. has also issued result, we have determined that it is –200 IGW airplanes. The MCAI states: Temporary Revision 4–2, dated necessary to reopen the comment period This [Brazilian] AD was prompted by a February 13, 2015, to Appendix A, Part to provide additional opportunity for determination that existing maintenance 2, of MPG–2928, Revision 4, which the public to comment on this SNPRM. requirements and airworthiness limitations describes detailed inspections for the are inadequate to ensure the structural upper doubler at the forward passenger Costs of Compliance integrity of the airplane. We are issuing this door cutout. We estimate that this SNPRM affects [Brazilian] AD to prevent failure of certain Furthermore, Embraer S.A. has issued 83 airplanes of U.S. registry. system components, which could result in Temporary Revision 4–3, dated October The actions that are required by AD reduced structural integrity [and system 30, 2015, to Appendix A, Part 4, of reliability] of the airplane. 2012–23–09 and retained in this MPG–2928, Revision 4, which updates SNPRM take about 1 work-hour per The required action is revising the the life limitations of certain main product, at an average labor rate of $85 maintenance or inspection program, as landing gear and nose landing per work-hour. Required parts cost applicable, to incorporate the components. about $0 per product. Based on these airworthiness limitations. This service information is reasonably figures, the estimated cost of the actions You may examine the MCAI in the available because the interested parties that were required by AD 2012–23–09 is AD docket on the Internet at http:// have access to it through their normal $85 per product. www.regulations.gov by searching for course of business or by the means We also estimate that it would take and locating Docket No. FAA–2014– identified in the ADDRESSES section. about 1 work-hour per product to 0008. Comments comply with the new basic Related Service Information Under 1 requirements of this SNPRM. The We gave the public the opportunity to CFR Part 51 average labor rate is $85 per work-hour. participate in developing this proposed Embraer S.A. has issued Appendix Required parts would cost about $0 per AD. We received no comments on the A—Airworthiness Limitations, Part 1— product. Based on these figures, we NPRM or on the determination of the Certification Maintenance estimate the cost of this SNPRM on U.S. cost to the public. Requirements, Part 2—Airworthiness operators to be $7,055, or $85 per Limitation Inspections—Structures, Part FAA’s Determination and Requirements product. 3—Fuel System Limitation Items, and of This SNPRM Authority for This Rulemaking Part 4—Life-Limited Items, of the This proposed AD would require EMBRAER ERJ 190/195 Maintenance revisions to certain operator Title 49 of the United States Code Review Board Report (MRBR), MRB– maintenance documents to include new specifies the FAA’s authority to issue 1928, Revision 9, dated August 14, 2015 actions (e.g., inspections) and Critical rules on aviation safety. Subtitle I, (‘‘MRB–1928, Revision 9’’). This service Design Configuration Control section 106, describes the authority of information describes airworthiness Limitations (CDCCLs). Compliance with the FAA Administrator. ‘‘Subtitle VII: limitations (Part 1, Part 2, Part 3, and these actions and CDCCLs is required by Aviation Programs,’’ describes in more Part 4 in Appendix A—Airworthiness 14 CFR 91.403(c). For airplanes that detail the scope of the Agency’s Limitations of MRB–1928, Revision 9, have been previously modified, altered, authority. make up the airworthiness limitations). or repaired in the areas addressed by We are issuing this rulemaking under Embraer S.A. has also issued this proposed AD, the operator may not the authority described in ‘‘Subtitle VII, Temporary Revision 9–1, dated October be able to accomplish the actions Part A, Subpart III, Section 44701: 27, 2015, to Appendix A— described in the revisions. In this General requirements.’’ Under that Airworthiness Limitations, of MRB– situation, to comply with 14 CFR section, Congress charges the FAA with 1928, Revision 9, which provides 91.403(c), the operator must request promoting safe flight of civil aircraft in revised airworthiness limitation approval for an alternative method of air commerce by prescribing regulations inspections and life limited items due to compliance according to paragraph for practices, methods, and procedures new structural provisions for Live TV (k)(1) of this proposed AD. The request the Administrator finds necessary for and Connectivity System. should include a description of changes safety in air commerce. This regulation In addition, Embraer S.A. has issued to the required inspections that will is within the scope of that authority Temporary Revision 9–3, dated October ensure the continued damage tolerance because it addresses an unsafe condition 27, 2015, to Appendix A— of the affected structure. that is likely to exist or develop on Airworthiness Limitations, of MRB– Notwithstanding any other products identified in this rulemaking 1928, Revision 9, which updates the life maintenance or operational action. limitations of certain main landing gear requirements, components that have Regulatory Findings and nose landing gear components. been identified as airworthy or installed Embraer S.A. has also issued on the affected airplanes before We determined that this proposed AD Appendix A, Airworthiness Limitation, accomplishing the revision of the would not have federalism implications of the EMBRAER ERJ 190–100 ECJ airplane maintenance or inspection under Executive Order 13132. This Maintenance Planning Guide (MPG), program specified in this proposed AD, proposed AD would not have a MPG–2928, Revision 4, dated July 14, do not need to be reworked in substantial direct effect on the States, on 2014 (‘‘MPG–2928, Revision 4’’). This accordance with the CDCCLs. However, the relationship between the national nlaroche on DSK30NT082PROD with PROPOSALS service information describes once the airplane maintenance or Government and the States, or on the airworthiness limitations (Part 1, inspection program has been revised as distribution of power and Certification Maintenance required by this proposed AD, future responsibilities among the various Requirements, Part 2, Airworthiness maintenance actions on these levels of government. Limitation Inspections—Structures, Part components must be done in For the reasons discussed above, I 3, Fuel System Limitation Items, and accordance with the CDCCLs. certify this proposed regulation: Part 4, Life Limited Items, of the MPG Certain changes described above 1. Is not a ‘‘significant regulatory make up the airworthiness limitations). expand the scope of the NPRM. As a action’’ under Executive Order 12866; VerDate Sep<11>2014 12:41 May 19, 2017 Jkt 241001 PO 00000 Frm 00002 Fmt 4702 Sfmt 4702 E:\FR\FM\22MYP1.SGM 22MYP1

Federal Register / Vol. 82, No. 97 / Monday, May 22, 2017 / Proposed Rules 23155 2. Is not a ‘‘significant rule’’ under the of certain system components; these October 27, 2015, to Part 2—Airworthiness DOT Regulatory Policies and Procedures conditions could result in reduced structural Limitation Inspections—Structures, of (44 FR 11034, February 26, 1979); integrity and system reliability of the Appendix A, Airworthiness Limitations, of 3. Will not affect intrastate aviation in airplane. MRB–1928, Revision 9; with the thresholds and intervals stated in these documents. The Alaska; and (f) Compliance initial compliance times for the tasks are at 4. Will not have a significant Comply with this AD within the the later of the times specified in paragraphs economic impact, positive or negative, compliance times specified, unless already (i)(1)(i) and (i)(1)(ii) of this AD. Doing the on a substantial number of small entities done. revision required by this paragraph under the criteria of the Regulatory terminates the revision required by paragraph (g) Retained Revision of the Maintenance Flexibility Act. Program, With No Changes (g) of this AD. (i) Within the applicable times specified in List of Subjects in 14 CFR Part 39 For Model ERJ 190–100 STD, ERJ 190–100 MRB–1928, Revision 9; EMBRAER Air transportation, Aircraft, Aviation LR, ERJ 190–100 IGW, ERJ 190–200 STD, ERJ Temporary Revision 9–1, dated October 27, 190–200 LR, and ERJ 190–200 IGW airplanes: 2015, to Part 2—Airworthiness Limitation safety, Incorporation by reference, This paragraph restates the actions required Safety. Inspections—Structures, and Part 4—Life by paragraph (h) of AD 2012–23–09, with no Limited Items, of Appendix A, Airworthiness The Proposed Amendment changes. Within 90 days after January 14, Limitations, of MRB–1928, Revision 9; and 2013 (the effective date of AD 2012–23–09), EMBRAER Temporary Revision 9–3, dated Accordingly, under the authority revise the maintenance program to October 27, 2015, to Part 2—Airworthiness delegated to me by the Administrator, incorporate the tasks specified in Part 2— Limitation Inspections—Structures, of the FAA proposes to amend 14 CFR part Airworthiness Limitation Inspections (ALI)— Appendix A, Airworthiness Limitations, of 39 as follows: Structures, of Appendix A, Airworthiness MRB–1928, Revision 9. Where tasks are Limitations (AL), of the EMBRAER 190 listed in both MRB–1928, Revision 9, and a PART 39—AIRWORTHINESS Maintenance Review Board Report, MRB– temporary revision, the compliance times in DIRECTIVES 1928, Revision 5, dated November 11, 2010; the temporary revision take precedence. and EMBRAER Temporary Revision (TR) 5– (ii) Within 90 days or 600 flight cycles after ■ 1. The authority citation for part 39 1, dated February 11, 2011, to Part 2— the effective date of this AD, whichever continues to read as follows: Airworthiness Limitation Inspections (ALI)— occurs later. Structures, of Appendix A, Airworthiness (2) For Model ERJ 190–100 ECJ airplanes: Authority: 49 U.S.C. 106(g), 40113, 44701. Limitations (AL), of the EMBRAER 190 Within 90 days after the effective date of this Maintenance Review Board Report, MRB– AD, revise the maintenance or inspection § 39.13 [Amended] 1928, Revision 5, dated November 11, 2010; program, as applicable, to incorporate the ■ 2. The FAA amends § 39.13 by with the thresholds and intervals stated in tasks specified in Part 1, Certification removing Airworthiness Directive (AD) these documents. The initial compliance Maintenance Requirements, Part 2, 2012–23–09, Amendment 39–17265 (77 times for the tasks are stated in the Airworthiness Limitation Inspections— FR 73270, December 10, 2012), and ‘‘Implementation Plan’’ section of Appendix Structures, Part 3, Fuel System Limitation adding the following new airworthiness A, Airworthiness Limitations (AL), of the Items, and Part 4, Life Limited Items, of EMBRAER 190 Maintenance Review Board directive (AD): Report, MRB–1928, Revision 5, dated Appendix A, Airworthiness Limitation, of the EMBRAER ERJ 190–100 ECJ Maintenance Embraer S.A.: Docket No. FAA–2014–0008; November 11, 2010. Planning Guide, MPG–2928, Revision 4, Directorate Identifier 2013–NM–076–AD. (h) Retained No Alternative Actions or dated July 14, 2014; EMBRAER Temporary (a) Comments Due Date Intervals, With New Exception Revision (TR) 4–2, dated February 13, 2015, We must receive comments by July 6, 2017. This paragraph restates the actions and EMBRAER TR 4–3, dated October 30, required by paragraph (i) of AD 2012–23–09, 2015; with the thresholds and intervals stated (b) Affected ADs with a new exception. After accomplishing in these documents. The initial compliance This AD replaces AD 2012–23–09, the revision required by paragraph (g) of this times for the tasks are at the later of the times Amendment 39–17265 (77 FR 73270, AD, no alternative actions (e.g., inspections) specified in paragraphs (i)(2)(i) and (i)(2)(ii) December 10, 2012) (‘‘AD 2012–23–09’’). or intervals, may be used, unless the actions of this AD. or intervals are approved as an alternative (i) Within the applicable times specified in (c) Applicability Part 1, Certification Maintenance method of compliance (AMOC) in This AD applies to Embraer S.A. Model accordance with the procedures specified in Requirements, Part 2, Airworthiness ERJ 190–100 STD, –100 LR, –100 ECJ, and paragraph (k)(1) of this AD, and except as Limitation Inspections—Structures, Part 3, –100 IGW airplanes; and Model ERJ 190–200 required by paragraph (i) of this AD. Fuel System Limitation Items, and Part 4, STD, –200 LR, and –200 IGW airplanes; Life Limited Items, of Appendix A, certificated in any category; serial numbers (i) New Requirements of This AD: Revision Airworthiness Limitation, of the EMBRAER 19000002, 19000004, 19000006 through of the Maintenance or Inspection Program ERJ 190–100 ECJ Maintenance Planning 19000213 inclusive, 19000215 through (1) For Model ERJ 190–100 STD, ERJ 190– Guide, MPG–2928, Revision 4, dated July 14, 19000276 inclusive, 19000278 through 100 LR, ERJ 190–100 IGW, ERJ 190–200 STD, 2014; EMBRAER TR 4–2, dated February 13, 19000466 inclusive, 19000468 through ERJ 190–200 LR, and ERJ 190–200 IGW 2015; and EMBRAER TR 4–3, dated October 19000525 inclusive, and 19000527 through airplanes: Within 90 days after the effective 30, 2015. Where tasks are listed in both 19000696 inclusive. date of this AD, revise the maintenance or MPG–2928, Revision 4, and a temporary inspection program, as applicable, to revision, the compliance times in the (d) Subject incorporate the tasks specified in Part 2— temporary revision take precedence. Air Transport Association (ATA) of Airworthiness Limitation Inspections— (ii) Within 90 days or 600 flight cycles after America Codes 27, Flight controls; 28, Fuel; Structures, of Appendix A—Airworthiness the effective date of this AD, whichever 52, Doors; 53, Fuselage; 54, Nacelles/pylons; Limitations, of the EMBRAER 190/195 occurs later. nlaroche on DSK30NT082PROD with PROPOSALS 55, Stabilizers; 57, Wings; 71, Powerplant; Maintenance Review Board Report, MRB– 1928, Revision 9, dated August 14, 2015 (j) No Alternative Actions, Intervals, and/or and 78, Exhaust. (‘‘MRB–1928, Revision 9’’); EMBRAER Critical Design Configuration Control (e) Reason Temporary Revision 9–1, dated October 27, Limitations (CDCCLs) This AD was prompted by a determination 2015, to Part 2—Airworthiness Limitation After accomplishment of the revision that more restrictive airworthiness Inspections—Structures, and Part 4—Life required by paragraph (i) of this AD, no limitations are necessary. We are issuing this Limited Items, of Appendix A, Airworthiness alternative actions (e.g., inspections), AD to detect and correct fatigue cracking of Limitations, of MRB–1928, Revision 9; and intervals, and/or CDCCLs may be used unless structural components and to prevent failure EMBRAER Temporary Revision 9–3, dated the actions, intervals, and/or CDCCLs are VerDate Sep<11>2014 12:41 May 19, 2017 Jkt 241001 PO 00000 Frm 00003 Fmt 4702 Sfmt 4702 E:\FR\FM\22MYP1.SGM 22MYP1

23156 Federal Register / Vol. 82, No. 97 / Monday, May 22, 2017 / Proposed Rules approved as an AMOC in accordance with DEPARTMENT OF TRANSPORTATION and locating Docket No. FAA–2017– the procedures specified in paragraph (k)(1) 0477; or in person at the Docket of this AD. Federal Aviation Administration Management Facility between 9 a.m. (k) Other FAA AD Provisions and 5 p.m., Monday through Friday, The following provisions also apply to this 14 CFR Part 39 except Federal holidays. The AD docket AD: [Docket No. FAA–2017–0477; Directorate contains this proposed AD, the (1) Alternative Methods of Compliance Identifier 2016–NM–112–AD] regulatory evaluation, any comments (AMOCs): The Manager, International received, and other information. The Branch, ANM–116, Transport Airplane RIN 2120–AA64 street address for the Docket Operations Directorate, FAA, has the authority to office (telephone 800–647–5527) is in approve AMOCs for this AD, if requested Airworthiness Directives; Bombardier, using the procedures found in 14 CFR 39.19. the ADDRESSES section. Comments will Inc., Airplanes In accordance with 14 CFR 39.19, send your be available in the AD docket shortly request to your principal inspector or local AGENCY: Federal Aviation after receipt. Flight Standards District Office, as Administration (FAA), DOT. FOR FURTHER INFORMATION CONTACT: appropriate. If sending information directly ACTION: Notice of proposed rulemaking Cesar A. Gomez, Aerospace Engineer, to the International Branch, send it to the attention of the person identified in (NPRM). Airframe and Mechanical Systems paragraph (l)(2) of this AD. Information may Branch, ANE–171, FAA, New York SUMMARY: We propose to adopt a new Aircraft Certification Office (ACO), 1600 be emailed to: 9-ANM-116-AMOC- REQUESTS@faa.gov. Before using any airworthiness directive (AD) for certain Stewart Avenue, Suite 410, Westbury, approved AMOC, notify your appropriate Bombardier, Inc., Model CL–600–2B16 NY 11590; telephone 516–228–7318; fax principal inspector, or lacking a principal (CL–601–3A, CL–601–3R, and CL–604 516–794–5531. inspector, the manager of the local flight Variants) airplanes. This proposed AD standards district office/certificate holding was prompted by a report indicating SUPPLEMENTARY INFORMATION: district office. that the lanyard length of the passenger Comments Invited (2) Contacting the Manufacturer: As of the drop down oxygen masks is too long. effective date of this AD, for any requirement We invite you to send any written in this AD to obtain corrective actions from This proposed AD would require replacing the existing oxygen mask relevant data, views, or arguments about a manufacturer, the action must be this proposed AD. Send your comments accomplished using a method approved by lanyards with lanyards of the correct the Manager, International Branch, ANM– length. We are proposing this AD to to an address listed under the 116, Transport Airplane Directorate, FAA; or address the unsafe condition on these ADDRESSES section. Include ‘‘Docket No. the Agência Nacional de Aviação Civil products. FAA–2017–0477; Directorate Identifier (ANAC); or ANAC’s authorized Designee. If 2016–NM–112–AD’’ at the beginning of approved by the ANAC Designee, the DATES: We must receive comments on your comments. We specifically invite approval must include the Designee’s this proposed AD by July 6, 2017. comments on the overall regulatory, authorized signature. ADDRESSES: You may send comments, economic, environmental, and energy (l) Related Information using the procedures found in 14 CFR aspects of this proposed AD. We will (1) Refer to Mandatory Continuing 11.43 and 11.45, by any of the following consider all comments received by the Airworthiness Information (MCAI) Brazilian methods: closing date and may amend this Airworthiness Directive 2016–04–01, • Federal eRulemaking Portal: Go to proposed AD based on those comments. effective April 4, 2016, for related http://www.regulations.gov. Follow the We will post all comments we information. This MCAI may be found in the instructions for submitting comments. receive, without change, to http:// AD docket on the Internet at http:// • Fax: 202–493–2251. www.regulations.gov, including any www.regulations.gov by searching for and • Mail: U.S. Department of personal information you provide. We locating Docket No. FAA–2014–0008. Transportation, Docket Operations, M– (2) For more information about this AD, will also post a report summarizing each contact Ana Martinez Hueto, Aerospace 30, West Building Ground Floor, Room substantive verbal contact we receive Engineer, International Branch, ANM–116, W12–140, 1200 New Jersey Avenue SE., about this proposed AD. Transport Airplane Directorate, FAA, 1601 Washington, DC 20590. Lind Avenue SW., Renton, WA 98057–3356; • Hand Delivery: Deliver to Mail Discussion telephone 425–227–1622; fax 425–227–1320. address above between 9 a.m. and 5 Transport Canada Civil Aviation (3) For service information identified in p.m., Monday through Friday, except this AD, contact Embraer S.A., Technical (TCCA), which is the aviation authority Federal holidays. for Canada, has issued Canadian Publications Section (PC 060), Av. Brigadeiro For service information identified in Faria Lima, 2170—Putim—12227–901 São Airworthiness Directive CF–2016–15, Jose dos Campos—SP—BRASIL; telephone this NPRM, contact Bombardier, Inc., dated June 1, 2016 (referred to after this +55 12 3927–5852 or +55 12 3309–0732; fax 400 Côte-Vertu Road West, Dorval, as the Mandatory Continuing +55 12 3927–7546; email distrib@ Québec H4S 1Y9, Canada; telephone Airworthiness Information, or ’’the embraer.com.br; Internet http:// 514–855–5000; fax 514–855–7401; email MCAI’’), to correct an unsafe condition www.flyembraer.com. You may view this thd.crj@aero.bombardier.com; Internet for certain Bombardier, Inc., Model CL– service information at the FAA, Transport http://www.bombardier.com. You may Airplane Directorate, 1601 Lind Avenue SW., 600–2B16 (CL–601–3A, CL–601–3R, and view this referenced service information CL–604 Variants) airplanes. The MCAI Renton, WA. For information on the at the FAA, Transport Airplane availability of this material at the FAA, call states: 425–227–1221. Directorate, 1601 Lind Avenue SW., nlaroche on DSK30NT082PROD with PROPOSALS Renton, WA. For information on the Bombardier (BA) has determined that the Issued in Renton, Washington, on May 8, lanyard length of the passenger drop down availability of this material at the FAA, 2017. oxygen masks is too long and may cause the call 425–227–1221. safety pin tethered to the opposite end of the Michael Kaszycki, Examining the AD Docket lanyard to remain engaged in the oxygen flow Acting Manager, Transport Airplane mechanism when the mask is pulled to the Directorate, Aircraft Certification Service. You may examine the AD docket on passenger’s face. In an emergency situation [FR Doc. 2017–10136 Filed 5–19–17; 8:45 am] the Internet at http:// where oxygen is required, it is possible that BILLING CODE 4910–13–P www.regulations.gov by searching for certain passengers may not receive oxygen VerDate Sep<11>2014 12:41 May 19, 2017 Jkt 241001 PO 00000 Frm 00004 Fmt 4702 Sfmt 4702 E:\FR\FM\22MYP1.SGM 22MYP1


Document Created: 2018-11-08 08:50:19
Document Modified: 2018-11-08 08:50:19
CategoryRegulatory Information
CollectionFederal Register
sudoc ClassAE 2.7:
GS 4.107:
AE 2.106:
PublisherOffice of the Federal Register, National Archives and Records Administration
SectionProposed Rules
ActionSupplemental notice of proposed rulemaking (SNPRM); reopening of comment period.
DatesThe comment period for the NPRM published in the Federal Register on February 3, 2014 (79 FR 6106), is reopened.
ContactAna Martinez Hueto, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1622; fax 425-227-1320.
FR Citation82 FR 23153 
RIN Number2120-AA64
CFR AssociatedAir Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety
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