82 FR 29019 - Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 122 (June 27, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 122 (June 27, 2017)
| Page Range | 29019-29021 | |
| FR Document | 2017-13357 |
[Federal Register Volume 82, Number 122 (Tuesday, June 27, 2017)] [Proposed Rules] [Pages 29019-29021] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-13357] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2017-0623; Directorate Identifier 2017-NM-024-AD] RIN 2120-AA64 Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for all Airbus Defense and Space S.A Model C-212-CB, C-212-CC, C-212-CD, C-212- CE, and C-212-DF airplanes. This proposed AD was prompted by reports of failures of the rudder pedal control system support. This proposed AD would require modifying the rudder pedal adjustment system. We are proposing this AD to address the unsafe condition on these products. DATES: We must receive comments on this proposed AD by August 11, 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, Airbus Defense and Space Services/Engineering Support, Avenida de Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; fax +34 91 585 31 27; email [email protected]. 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- 0623; 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: Shahram Daneshmandi, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone: 425-227-1112; fax: 425-227-1149. 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-2017-0623; Directorate Identifier 2017-NM-024-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 The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA Airworthiness Directive 2017-0036, dated February 21, 2017 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for all Airbus Defense and Space S.A Model C-212-CB, C-212-CC, C-212-CD, C-212-CE, and C-212- DF airplanes. The MCAI states: Failures were reported of the pedal control system support of CASA C-212 aeroplanes. Subsequent investigation revealed that the welding area of the affected support structure had broken. This condition, if not corrected, could lead to failure of the rudder control system, possibly resulting in reduced control of the aeroplane. [[Page 29020]] To address this potential unsafe condition, EADS-CASA issued Service Bulletin (SB) SB-212-27-0057 to provide modification instructions. For the reasons described above, this [EASA] AD requires modification of the rudder pedal adjustment system. 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- 0623. Related Service Information Under 1 CFR Part 51 We reviewed EADS CASA Service Bulletin SB-212-27-0057, dated May 21, 2014. This service information provides instructions for modifying the rudder pedal adjustment system. 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 42 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 ---------------------------------------------------------------------------------------------------------------- Modification....................... 9 work-hours x $85 per hour $5,683 $6,448 $270,816 = $765. ---------------------------------------------------------------------------------------------------------------- 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 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): Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.): Docket No. FAA-2017-0623; Directorate Identifier 2017-NM-024-AD. (a) Comments Due Date We must receive comments by August 11, 2017. (b) Affected ADs None. (c) Applicability This AD applies to all Airbus Defense and Space S.A Model C-212- CB, C-212-CC, C-212-CD, C-212-CE, and C-212-DF airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 27, Flight controls. (e) Reason This AD was prompted by reports of failures of the rudder pedal control system support and a determination that the welding area of the affected support structure had broken. We are issuing this AD to prevent failure of the rudder control system, which could result in reduced controllability of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Modification Within 12 months after the effective date of this AD: Modify the rudder pedal adjustment system, in accordance with the Accomplishment Instructions of EADS CASA Service Bulletin SB-212-27- 0057, dated May 21, 2014. (h) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the International Branch, send it to the attention of the person identified in paragraph (i)(2) of this AD. Information may be emailed to: [email protected]. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal [[Page 29021]] 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, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or EADS CASA's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (i) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2017-0036, dated February 21, 2017, 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-2017-0623. (2) For more information about this AD, contact Shahram Daneshmandi, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone: 425-227-1112; fax: 425-227-1149. Information may be emailed to: [email protected]. (3) For service information identified in this AD, contact Airbus Defense and Space Services/Engineering Support, Avenida de Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; fax +34 91 585 31 27; email [email protected]. 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 June 19, 2017. John P. Piccola, Jr., Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2017-13357 Filed 6-26-17; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 82, No. 122 / Tuesday, June 27, 2017 / Proposed Rules 29019
using the procedures found in 14 CFR 39.19. DEPARTMENT OF TRANSPORTATION and locating Docket No. FAA–2017–
In accordance with 14 CFR 39.19, send your 0623; or in person at the Docket
request to your principal inspector or local Federal Aviation Administration Management Facility between 9 a.m.
Flight Standards District Office, as and 5 p.m., Monday through Friday,
appropriate. If sending information directly 14 CFR Part 39 except Federal holidays. The AD docket
to the manager of the International Branch, contains this proposed AD, the
[Docket No. FAA–2017–0623; Directorate
send it to the attention of the person regulatory evaluation, any comments
Identifier 2017–NM–024–AD]
identified in paragraph (l)(2) of this AD. received, and other information. The
Information may be emailed to: 9-ANM-116- RIN 2120–AA64 street address for the Docket Operations
AMOC-REQUESTS@faa.gov. office (telephone 800–647–5527) is in
(i) Before using any approved AMOC, Airworthiness Directives; Airbus
the ADDRESSES section. Comments will
notify your appropriate principal inspector, Defense and Space S.A. (Formerly
be available in the AD docket shortly
or lacking a principal inspector, the manager Known as Construcciones
after receipt.
of the local flight standards district office/ Aeronauticas, S.A.) Airplanes
certificate holding district office. FOR FURTHER INFORMATION CONTACT:
AGENCY: Federal Aviation Shahram Daneshmandi, Aerospace
(ii) AMOCs approved previously for AD
Administration (FAA), DOT. Engineer, International Branch, ANM–
2014–22–08 are approved as AMOCs for the
corresponding provisions of paragraph (g) of ACTION: Notice of proposed rulemaking 116, Transport Airplane Directorate,
this AD. (NPRM). FAA, 1601 Lind Avenue SW., Renton,
(2) Contacting the Manufacturer: As of the WA 98057–3356; telephone: 425–227–
SUMMARY: We propose to adopt a new 1112; fax: 425–227–1149.
effective date of this AD, for any requirement
airworthiness directive (AD) for all
in this AD to obtain corrective actions from SUPPLEMENTARY INFORMATION:
Airbus Defense and Space S.A Model C–
a manufacturer, the action must be
212–CB, C–212–CC, C–212–CD, C–212– Comments Invited
accomplished using a method approved by
the Manager, International Branch, ANM–
CE, and C–212–DF airplanes. This
proposed AD was prompted by reports We invite you to send any written
116, Transport Airplane Directorate, FAA; or relevant data, views, or arguments about
the European Aviation Safety Agency
of failures of the rudder pedal control
system support. This proposed AD this proposed AD. Send your comments
(EASA); or Airbus’s EASA Design to an address listed under the
Organization Approval (DOA). If approved by would require modifying the rudder
ADDRESSES section. Include ‘‘Docket No.
the DOA, the approval must include the pedal adjustment system. We are
proposing this AD to address the unsafe FAA–2017–0623; Directorate Identifier
DOA-authorized signature. 2017–NM–024–AD’’ at the beginning of
condition on these products.
(l) Related Information your comments. We specifically invite
DATES: We must receive comments on
comments on the overall regulatory,
(1) Refer to Mandatory Continuing this proposed AD by August 11, 2017.
Airworthiness Information (MCAI) EASA
economic, environmental, and energy
ADDRESSES: You may send comments, aspects of this proposed AD. We will
Airworthiness Directive 2016–0092, dated using the procedures found in 14 CFR
May 13, 2016, for related information. This
consider all comments received by the
11.43 and 11.45, by any of the following closing date and may amend this
MCAI may be found in the AD docket on the methods:
Internet at http://www.regulations.gov by proposed AD based on those comments.
• Federal eRulemaking Portal: Go to We will post all comments we
searching for and locating Docket No. FAA–
http://www.regulations.gov. Follow the receive, without change, to http://
2017–0625.
instructions for submitting comments. www.regulations.gov, including any
(2) For more information about this AD,
• Fax: 202–493–2251. personal information you provide. We
contact Sanjay Ralhan, Aerospace Engineer,
• Mail: U.S. Department of will also post a report summarizing each
International Branch, ANM–116, Transport
Transportation, Docket Operations, M– substantive verbal contact we receive
Airplane Directorate, FAA, 1601 Lind
30, West Building Ground Floor, Room about this proposed AD.
Avenue SW., Renton, WA 98057–3356;
W12–140, 1200 New Jersey Avenue SE.,
telephone 425–227–1405; fax 425–227–1149. Discussion
Washington, DC 20590.
(3) For service information identified in
this AD, contact Airbus, Airworthiness
• Hand Delivery: Deliver to Mail The European Aviation Safety Agency
Office—EIAS, 1 Rond Point Maurice
address above between 9 a.m. and 5 (EASA), which is the Technical Agent
Bellonte, 31707 Blagnac Cedex, France;
p.m., Monday through Friday, except for the Member States of the European
telephone +33 5 61 93 36 96; fax +33 5 61 Federal holidays. Union, has issued EASA Airworthiness
93 44 51; email account.airworth-eas@ For service information identified in Directive 2017–0036, dated February 21,
airbus.com; Internet http://www.airbus.com. this NPRM, Airbus Defense and Space 2017 (referred to after this as the
You may view this service information at the Services/Engineering Support, Avenida Mandatory Continuing Airworthiness
FAA, Transport Airplane Directorate, 1601 de Aragón 404, 28022 Madrid, Spain; Information, or ‘‘the MCAI’’), to correct
Lind Avenue SW., Renton, WA. For telephone +34 91 585 55 84; fax +34 91 an unsafe condition for all Airbus
information on the availability of this 585 31 27; email Defense and Space S.A Model C–212–
material at the FAA, call 425–227–1221. MTA.TechnicalService@airbus.com. CB, C–212–CC, C–212–CD, C–212–CE,
You may view this referenced service and C–212–DF airplanes. The MCAI
Issued in Renton, Washington, on June 20, information at the FAA, Transport
2017. states:
pmangrum on DSK7TPTVN1PROD with PROPOSALS
Airplane Directorate, 1601 Lind Avenue
John P. Piccola, Jr., SW., Renton, WA. For information on Failures were reported of the pedal control
system support of CASA C–212 aeroplanes.
Acting Manager, Transport Airplane the availability of this material at the
Subsequent investigation revealed that the
Directorate, Aircraft Certification Service. FAA, call 425–227–1221. welding area of the affected support structure
[FR Doc. 2017–13365 Filed 6–26–17; 8:45 am] had broken.
Examining the AD Docket
BILLING CODE 4910–13–P This condition, if not corrected, could lead
You may examine the AD docket on to failure of the rudder control system,
the Internet at http:// possibly resulting in reduced control of the
www.regulations.gov by searching for aeroplane.
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![29020 Federal Register / Vol. 82, No. 122 / Tuesday, June 27, 2017 / Proposed Rules
To address this potential unsafe condition, 21, 2014. This service information Design Authority, we have been notified
EADS–CASA issued Service Bulletin (SB) provides instructions for modifying the of the unsafe condition described in the
SB–212–27–0057 to provide modification rudder pedal adjustment system. This MCAI and service information
instructions.
For the reasons described above, this
service information is reasonably referenced above. We are proposing this
[EASA] AD requires modification of the available because the interested parties AD because we evaluated all pertinent
rudder pedal adjustment system. have access to it through their normal information and determined an unsafe
course of business or by the means condition exists and is likely to exist or
You may examine the MCAI in the
identified in the ADDRESSES section. develop on other products of the same
AD docket on the Internet at http://
www.regulations.gov by searching for FAA’s Determination and Requirements type design.
and locating Docket No. FAA–2017– of This Proposed AD Costs of Compliance
0623.
This product has been approved by We estimate that this proposed AD
Related Service Information Under 1 the aviation authority of another
CFR Part 51 affects 42 airplanes of U.S. registry.
country, and is approved for operation
We reviewed EADS CASA Service in the United States. Pursuant to our We estimate the following costs to
Bulletin SB–212–27–0057, dated May bilateral agreement with the State of comply with this proposed AD:
ESTIMATED COSTS
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
Modification ..................................................... 9 work-hours × $85 per hour = $765 ............. $5,683 $6,448 $270,816
Authority for This Rulemaking 3. Will not affect intrastate aviation in 212–CD, C–212–CE, and C–212–DF airplanes,
Alaska; and certificated in any category.
Title 49 of the United States Code
specifies the FAA’s authority to issue 4. Will not have a significant (d) Subject
rules on aviation safety. Subtitle I, economic impact, positive or negative, Air Transport Association (ATA) of
section 106, describes the authority of on a substantial number of small entities America Code 27, Flight controls.
the FAA Administrator. ‘‘Subtitle VII: under the criteria of the Regulatory
(e) Reason
Aviation Programs,’’ describes in more Flexibility Act.
This AD was prompted by reports of
detail the scope of the Agency’s List of Subjects in 14 CFR Part 39 failures of the rudder pedal control system
authority. support and a determination that the welding
We are issuing this rulemaking under Air transportation, Aircraft, Aviation
area of the affected support structure had
the authority described in ‘‘Subtitle VII, safety, Incorporation by reference, broken. We are issuing this AD to prevent
Part A, Subpart III, Section 44701: Safety. failure of the rudder control system, which
General requirements.’’ Under that The Proposed Amendment could result in reduced controllability of the
section, Congress charges the FAA with airplane.
promoting safe flight of civil aircraft in Accordingly, under the authority
(f) Compliance
air commerce by prescribing regulations delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part Comply with this AD within the
for practices, methods, and procedures compliance times specified, unless already
the Administrator finds necessary for 39 as follows: done.
safety in air commerce. This regulation PART 39—AIRWORTHINESS (g) Modification
is within the scope of that authority DIRECTIVES Within 12 months after the effective date
because it addresses an unsafe condition
of this AD: Modify the rudder pedal
that is likely to exist or develop on ■ 1. The authority citation for part 39 adjustment system, in accordance with the
products identified in this rulemaking continues to read as follows: Accomplishment Instructions of EADS CASA
action. Service Bulletin SB–212–27–0057, dated May
Authority: 49 U.S.C. 106(g), 40113, 44701.
21, 2014.
Regulatory Findings
§ 39.13 [Amended] (h) Other FAA AD Provisions
We determined that this proposed AD
■ 2. The FAA amends § 39.13 by adding The following provisions also apply to this
would not have federalism implications
the following new airworthiness AD:
under Executive Order 13132. This
directive (AD): (1) Alternative Methods of Compliance
proposed AD would not have a
Airbus Defense and Space S.A. (Formerly (AMOCs): The Manager, International
substantial direct effect on the States, on Branch, ANM–116, FAA, has the authority to
the relationship between the national Known as Construcciones Aeronauticas,
S.A.): Docket No. FAA–2017–0623; approve AMOCs for this AD, if requested
Government and the States, or on the using the procedures found in 14 CFR 39.19.
Directorate Identifier 2017–NM–024–AD.
distribution of power and In accordance with 14 CFR 39.19, send your
responsibilities among the various (a) Comments Due Date request to your principal inspector or local
pmangrum on DSK7TPTVN1PROD with PROPOSALS
levels of government. We must receive comments by August 11, Flight Standards District Office, as
For the reasons discussed above, I 2017. appropriate. If sending information directly
certify this proposed regulation: to the manager of the International Branch,
(b) Affected ADs send it to the attention of the person
1. Is not a ‘‘significant regulatory identified in paragraph (i)(2) of this AD.
None.
action’’ under Executive Order 12866; Information may be emailed to: 9-ANM-116-
2. Is not a ‘‘significant rule’’ under the (c) Applicability AMOC-REQUESTS@faa.gov. Before using
DOT Regulatory Policies and Procedures This AD applies to all Airbus Defense and any approved AMOC, notify your appropriate
(44 FR 11034, February 26, 1979); Space S.A Model C–212–CB, C–212–CC, C– principal inspector, or lacking a principal
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![Federal Register / Vol. 82, No. 122 / Tuesday, June 27, 2017 / Proposed Rules 29021
inspector, the manager of the local flight Issued in Renton, Washington, on June 19, FOR FURTHER INFORMATION CONTACT:
standards district office/certificate holding 2017. Chanda McNeal (301) 492–4132 or
district office. John P. Piccola, Jr., Jamaca Mitchell (301) 492–4177.
(2) Contacting the Manufacturer: For any Acting Manager, Transport Airplane SUPPLEMENTARY INFORMATION:
requirement in this AD to obtain corrective Directorate, Aircraft Certification Service.
actions from a manufacturer, the action must [FR Doc. 2017–13357 Filed 6–26–17; 8:45 am] I. Background
be accomplished using a method approved BILLING CODE 4910–13–P In FR Doc. 2017–12130 of June 12,
by the Manager, International Branch, ANM– 2017 (82 FR 26885), there was an error
116, Transport Airplane Directorate, FAA; or
that is identified and corrected in the
the European Aviation Safety Agency
DEPARTMENT OF HEALTH AND Correction of Errors section of this
(EASA); or EADS CASA’s EASA Design
HUMAN SERVICES correction notice. The correction in this
Organization Approval (DOA). If approved by
document is effective as if it had been
the DOA, the approval must include the
Centers for Medicare & Medicaid included in the document published on
DOA-authorized signature.
Services June 12, 2017. Accordingly, the
(i) Related Information correction is effective (June 26, 2017).
(1) Refer to Mandatory Continuing 42 CFR Chapter IV II. Summary of Errors
Airworthiness Information (MCAI) EASA
Airworthiness Directive 2017–0036, dated Office of the Secretary On page 26886, we inadvertently
February 21, 2017, for related information. included the incorrect contact
This MCAI may be found in the AD docket 45 CFR Subtitle A information in the FOR FURTHER
on the Internet at http://www.regulations.gov INFORMATION CONTACT section. Therefore,
by searching for and locating Docket No. [CMS–9928–CN] we are correcting this error to provide
FAA–2017–0623. the public with the correct point of
(2) For more information about this AD, RIN 0938–ZB39 contact’s name and phone number for
contact Shahram Daneshmandi, Aerospace issues related to the June 12, 2017
Engineer, International Branch, ANM–116, Reducing Regulatory Burdens request for information notice.
Transport Airplane Directorate, FAA, 1601 Imposed by the Patient Protection and
Affordable Care Act & Improving III. Correction of Errors
Lind Avenue SW., Renton, WA 98057–3356;
telephone: 425–227–1112; fax: 425–227– Healthcare Choices To Empower In FR Doc. 2017–12130 of June 12,
1149. Information may be emailed to: 9- 2017 (82 FR 26885), make the following
AGENCY: Centers for Medicare &
ANM-116-AMOC-REQUESTS@faa.gov. correction.
Medicaid Services (CMS), HHS.
(3) For service information identified in On page 26886, in the first column,
ACTION: Request for information; under the FOR FURTHER INFORMATION
this AD, contact Airbus Defense and Space
Services/Engineering Support, Avenida de correction. CONTACT, the contact name and phone
Aragón 404, 28022 Madrid, Spain; telephone SUMMARY: This document corrects an number for ‘‘Vanessa Jones, (202) 690–
+34 91 585 55 84; fax +34 91 585 31 27; email error that appeared in the request for 700’’ is deleted and replaced with,
MTA.TechnicalService@airbus.com. You
information notice published in the ‘‘Chanda McNeal, (301) 492–4132, or
may view this service information at the
Federal Register on June 12, 2017 Jamaca Mitchell, (301) 492–4177.’’
FAA, Transport Airplane Directorate, 1601 Dated: June 21, 2017.
entitled ‘‘Reducing Regulatory Burdens
Lind Avenue SW., Renton, WA. For
Imposed by the Patient Protection and Ann C. Agnew,
information on the availability of this
Affordable Care Act & Improving Executive Secretary to the Department,
material at the FAA, call 425–227–1221.
Healthcare Choices to Empower.’’ Department of Health and Human Services.
DATES: This correction is effective June [FR Doc. 2017–13417 Filed 6–26–17; 8:45 am]
26, 2017. BILLING CODE 4120–01–P
pmangrum on DSK7TPTVN1PROD with PROPOSALS
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Document Created: 2018-11-14 10:15:14
Document Modified: 2018-11-14 10:15:14
| 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 August 11, 2017. | |
| Contact | Shahram Daneshmandi, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone: 425-227-1112; fax: 425-227-1149. | |
| FR Citation | 82 FR 29019 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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