Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes, 36707-36710 [2015-15615]
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Federal Register / Vol. 80, No. 123 / Friday, June 26, 2015 / Rules and Regulations
(g) A notification that the Recipient has
passed vetting does not constitute any other
approval under this award.
Alternate I. When subrecipients will be
subject to vetting, add the following
paragraphs to the basic award term:
(h) When the prime recipient anticipates
that it will require prior approval for a
subaward in accordance with 2 CFR
200.308(c)(6) the subaward is subject to
vetting. The prospective subrecipient must
submit a USAID Partner Information Form,
USAID Form 500–13, to the vetting official
identified in paragraph (c) of this provision.
The agreement officer must not approve a
subaward to any organization that has not
passed vetting when required.
(i) The recipient agrees to incorporate the
substance of paragraphs (a) through (i) of this
award term in all first tier subawards under
this award.
Alternate II. When specific classes of
services are subject to vetting, add the
following paragraph:
(j) Prospective contractors at any tier
providing the following classes of services
lllllllllllllllllllll
lllllllllllllllllllll
lllllllllllllllllllll
must pass vetting. Recipients must not
procure these services until they receive
confirmation from the vetting official that the
prospective contractor has passed vetting.
(End of award term)
Angelique M. Crumbly,
Assistant Administrator, Bureau for
Management.
[FR Doc. 2015–15017 Filed 6–25–15; 8:45 am]
BILLING CODE 6116–02–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2015–1986; Directorate
Identifier 2012–NM–100–AD; Amendment
39–18188; AD 2015–13–01]
RIN 2120–AA64
Airworthiness Directives; ATR–GIE
´
Avions de Transport Regional
Airplanes
Examining the AD Docket
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for
comments.
AGENCY:
We are adopting a new
airworthiness directive (AD) for certain
´
ATR–GIE Avions de Transport Regional
Model ATR42–500 and ATR72–212A
airplanes. This AD requires inspection
of the affected control systems rods and,
depending on findings, a replacement of
the affected rods. This AD was
prompted by reports of non-conformity
of certain control rods, which could
wreier-aviles on DSK5TPTVN1PROD with RULES
SUMMARY:
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14:06 Jun 25, 2015
Jkt 235001
result in failure of the control rods. We
are issuing this AD to detect and correct
failure of an affected control rod, which,
under certain circumstances, could
result in reduced control of the airplane.
DATES: This AD becomes effective July
13, 2015.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of July 13, 2015.
We must receive comments on this
AD by August 10, 2015.
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
https://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 AD, contact ATR–GIE Avions de
´
´
Transport Regional, 1, Allee Pierre
Nadot, 31712 Blagnac Cedex, France;
telephone +33 (0) 5 62 21 62 21; fax +33
(0) 5 62 21 67 18; email
continued.airworthiness@atr.fr; Internet
https://www.aerochain.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. It is also available
on the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2015–
1986.
You may examine the AD docket on
the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2015–
1986; or in person at the Docket
Operations office between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays. The AD docket
contains this AD, the regulatory
evaluation, any comments received, and
other information. The street address for
the Docket Operations office (telephone
800–647–5527) is in the ADDRESSES
section. Comments will be available in
the AD docket shortly after receipt.
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36707
Tom
Rodriguez, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA
98057–3356; telephone 425–227–1137;
fax 425–227–1149.
SUPPLEMENTARY INFORMATION:
FOR FURTHER INFORMATION CONTACT:
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 2012–0064, dated April 20,
2012 (referred to after this as the
Mandatory Continuing Airworthiness
Information, or ‘‘the MCAI’’), to correct
an unsafe condition for Model ATR42–
500 and ATR72–212A airplanes. The
MCAI states:
Prompted by the findings that led to
publication of EASA AD 2010–0063–E,
additional quality investigation showed that
the non-conformity of certain control rods,
which was due to incorrect polishing during
the rod manufacturing process, could also
affect other flight control rods [and could
result in failure of the control rods].
These other potentially non-conforming
control rods are installed on elevator
controls, rudder pedal assemblies and rudder
tab controls of certain ATR aeroplanes.
This condition, if not detected and
corrected, could lead to failure of an affected
control rod which, under certain
circumstances, could result in reduced
control of the aeroplane.
As a result of further investigations, other
batches have been incriminated, in addition
to the ones identified by EASA AD 2010–
0063–E, and new safety analyses also
indicate the need for replacement of the rods
(within an adapted compliance time), which
had passed the check required by EASA AD
2010–0063–E. Consequently, EASA AD
2010–0063–E is superseded by this new AD.
For the reasons described above, this
[EASA] AD requires a one-time inspection of
the affected control systems rods and,
depending on findings, replacement of the
affected rods.
You may examine the MCAI on the
Internet at https://www.regulations.gov
by searching for and locating Docket No.
FAA–2015–1986.
Related Service Information Under 1
CFR Part 51
ATR–GIE Avions de Transport
´
Regional (ATR) has issued the following
service information.
• ATR Service Bulletin ATR42–27–
0104, Revision 01, dated August 30,
2011.
• ATR Service Bulletin ATR42–27–
0105, Revision 01, dated August 30,
2011.
• ATR Service Bulletin ATR72–27–
1065, Revision 02, dated August 30,
2011.
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Federal Register / Vol. 80, No. 123 / Friday, June 26, 2015 / Rules and Regulations
• ATR Service Bulletin ATR72–27–
1066, Revision 01, dated August 30,
2011.
This service information describes
procedures for the inspection of affected
control systems rods and, depending on
findings, a replacement of the affected
rods. 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 of this AD.
FAA’s Determination and Requirements
of This 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 issuing this
AD because we evaluated all pertinent
information and determined the unsafe
condition exists and is likely to exist or
develop on other products of the same
type designs.
There are no products of this type
currently registered in the United States;
however, this rule is necessary to ensure
that the described unsafe condition is
addressed if any of these products are
placed on the U.S. Register in the future.
wreier-aviles on DSK5TPTVN1PROD with RULES
Differences Between This AD and the
MCAI or Service Information
The actions specified in paragraph (4)
of the MCAI, for rudder pedals that have
been inspected according to EASA AD
2010–0063–E, dated April 1, 2010, is
not included in this AD because the
those actions were not required by any
FAA AD.
Although the MCAI requires using a
certain repair manual to repair certain
conditions, paragraph (i) of this AD
requires repair using a method approved
by the Manager, International Branch,
ANM–116, Transport Airplane
Directorate, FAA; or the European
Aviation Safety Agency (EASA); or
ATR–GIE Avions de Transport
´
Regional’s EASA Design Organization
Approval (DOA).
FAA’s Determination of the Effective
Date
Since there are currently no domestic
operators of this product, notice and
opportunity for public comment before
issuing this AD are unnecessary.
Comments Invited
This AD is a final rule that involves
requirements affecting flight safety, and
we did not precede it by notice and
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opportunity for public comment. We
invite you to send any written relevant
data, views, or arguments about this AD.
Send your comments to an address
listed under the ADDRESSES section.
Include ‘‘Docket No. FAA–2015–1986;
Directorate Identifier 2012–NM–100–
AD’’ at the beginning of your comments.
We specifically invite comments on the
overall regulatory, economic,
environmental, and energy aspects of
this AD. We will consider all comments
received by the closing date and may
amend this AD based on those
comments.
We will post all comments we
receive, without change, to https://
www.regulations.gov, including any
personal information you provide. We
will also post a report summarizing each
substantive verbal contact we receive
about this AD.
Costs of Compliance
Currently, there are no affected
airplanes on the U.S. Register. However,
if an affected airplane is imported and
placed on the U.S. Register in the future,
we estimate that it will take about 1
work-hour per product to comply with
the basic requirements of this AD. The
average labor rate is $85 per work-hour.
Required parts will cost $0 per product.
Based on these figures, we estimate the
cost of this AD on U.S. operators to be
$85 per product.
Paperwork Reduction Act
A federal agency may not conduct or
sponsor, and a person is not required to
respond to, nor shall a person be subject
to penalty for failure to comply with a
collection of information subject to the
requirements of the Paperwork
Reduction Act unless that collection of
information displays a current valid
OMB control number. The control
number for the collection of information
required by this AD is 2120–0056. The
paperwork cost associated with this AD
has been detailed in the Costs of
Compliance section of this document
and includes time for reviewing
instructions, as well as completing and
reviewing the collection of information.
Therefore, all reporting associated with
this AD is mandatory. Comments
concerning the accuracy of this burden
and suggestions for reducing the burden
should be directed to the FAA at 800
Independence Ave. SW., Washington,
DC 20591, ATTN: Information
Collection Clearance Officer, AES–200.
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
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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 AD will not
have federalism implications under
Executive Order 13132. This AD will
not have a substantial direct effect on
the States, on the relationship between
the national government and the States,
or on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
2. Is not a ‘‘significant rule’’ under the
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in
Alaska; and
4. Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
■
2015–13–01 ATR–GIE Avions de Transport
´
Regional: Amendment 39–18188. Docket
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Federal Register / Vol. 80, No. 123 / Friday, June 26, 2015 / Rules and Regulations
No. FAA–2015–1986; Directorate
Identifier 2012–NM–100–AD.
(a) Effective Date
This AD becomes effective July 13, 2015.
(b) Affected ADs
None.
(c) Applicability
This AD applies to airplanes specified in
paragraphs (c)(1) and (c)(2) of this AD,
certificated in any category.
´
(1) ATR–GIE Avions de Transport Regional
Model ATR42–500 airplanes having
manufacturer serial number (MSN) 671
through 815 inclusive, except MSN 811.
´
(2) ATR–GIE Avions de Transport Regional
Model ATR72–212A airplanes having MSN
769 through 914 inclusive, except MSN 826,
905, 908, and 911.
(d) Subject
Air Transport Association (ATA) of
America Code 27, Flight Controls.
(e) Reason
This AD was prompted by reports of nonconformity of certain control rods, which
could result in failure of the control rods. We
are issuing this AD to detect and correct
failure of an affected control rod, which,
under certain circumstances, could result in
reduced control of the airplane.
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(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Elevator Control Rod Inspection
For airplanes identified in ATR Service
Bulletin ATR42–27–0105, Revision 01, dated
August 30, 2011; or ATR72–27–1066,
Revision 01, dated August 30, 2011; as
applicable to airplane model: Within 6
months after the effective date of this AD,
inspect all four elevator control rods having
part number (P/N) S27381930–004 and P/N
S27381831–006 for batch number
identification, in accordance with the
Accomplishment Instructions of ATR Service
Bulletin ATR42–27–0105, Revision 01, dated
August 30, 2011; or ATR Service Bulletin
ATR72–27–1066, Revision 01, dated August
30, 2011, as applicable to airplane model. A
review of airplane maintenance records is
acceptable in lieu of this inspection, if the
batch number can be conclusively
determined from that review. Replace any
affected rod, including any rod with an
unreadable batch number, at the applicable
time specified in paragraph (g)(1) or (g)(2) of
this AD, in accordance with ATR Service
Bulletin ATR42–27–0105, Revision 01, dated
August 30, 2011; or ATR72–27–1066,
Revision 01, dated August 30, 2011; as
applicable to airplane model.
(1) If only one rod is affected: Replace it
within 10 days after the inspection.
(2) If two or more rods are affected: Replace
all rods before further flight, except that
replacement of one of the affected rods may
be deferred for 10 days.
(h) Rudder Pedal Rod Inspection
For airplanes identified in ATR Service
Bulletin ATR42–27–0104, Revision 01, dated
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August 30, 2011; or ATR Service Bulletin
ATR72–27–1065, Revision 02, dated August
30, 2011; as applicable to airplane model:
Inspect all four rudder pedal rods having P/
N S2728116400000 for batch number
identification, in accordance with the
Accomplishment Instructions of ATR Service
Bulletin ATR42–27–0104, Revision 01, dated
August 30, 2011; or ATR Service Bulletin
ATR72–27–1065, Revision 02, dated August
30, 2011; as applicable to airplane model. For
any affected rudder pedal rod, including any
rod with an unreadable batch number, before
further flight, check the rod diameter using
a special tool, in accordance with ATR
Service Bulletin ATR42–27–0104, Revision
01, dated August 30, 2011; or ATR Service
Bulletin ATR72–27–1065, Revision 02, dated
August 30, 2011; as applicable to airplane
model.
(1) If, during the diameter check, the rod
passes through the tool, replace the rod
before further flight.
(2) If, during the diameter check, the rod
does not pass through the tool, replace the
rod within 5,000 flight hours after the
diameter check.
(i) Rudder Tab Control Rod Inspection
For airplanes identified in paragraph (c) of
this AD, except for airplanes having MSNs
671, 673, and 769 through 784 inclusive:
Within 24 months after the effective date of
this AD, inspect the rudder tab control rod
P/N S27281929–002 for batch number
identification, using a method approved by
the Manager, International Branch, ANM–
116, Transport Airplane Directorate, FAA; or
the European Aviation Safety Agency
´
(EASA); or Avions de Transport Regional
(ATR)’s EASA Design Organization Approval
(DOA). If the rudder tab control rod belongs
to batch number 2107267 or 2120855, or if
the batch number is unreadable: Before
further flight, replace the rod with a
serviceable rod using a method approved by
the Manager, International Branch, ANM–
116, Transport Airplane Directorate, FAA; or
EASA; or ATR’s EASA DOA.
Note 1 to paragraph (i) of this AD: ATR 42/
72 Aircraft Maintenance Manual (AMM)/Job
Instruction Cards (JIC) 27–20–00 DVI 1000
and AMM/JIC 27–21–42 RAI 10000 are
additional sources of guidance for
accomplishment of the rudder tab control rod
inspection.
(j) Reporting Requirement
Submit a report of the rod inspection and
check required by paragraphs (g) and (h) of
this AD at the applicable compliance time
specified in paragraph (j)(1) of this AD, in
accordance with the instructions specified in
paragraph (j)(2) of this AD.
(1) Submit the report at the applicable time
specified in paragraph (j)(1)(i) or (j)(1)(ii) of
this AD.
(i) If the inspection or check was done on
or after the effective date of this AD: Submit
the report within 30 days after the inspection
or check.
(ii) If the inspection or check was done
before the effective date of this AD: Submit
the report within 30 days after the effective
date of this AD.
(2) Submit the report (including no
findings) to ATR using the Accomplishment
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36709
Report form provided in the service
information identified in paragraph (j)(2)(i),
(j)(2)(ii), (j)(2)(iii), or (j)(2)(iv) of this AD; as
applicable to airplane model.
(i) ATR Service Bulletin ATR42–27–0104,
Revision 01, dated August 30, 2011.
(ii) ATR Service Bulletin ATR42–27–0105,
Revision 01, dated August 30, 2011.
(iii) ATR Service Bulletin ATR72–27–1065,
Revision 02, dated August 30, 2011.
(iv) ATR Service Bulletin ATR72–27–1066,
Revision 01, dated August 30, 2011.
(3) Send the report to ATR–GIE Avions de
´
´
Transport Regional, 1, Allee Pierre Nadot,
31712 Blagnac Cedex, France; telephone +33
(0) 5 62 21 62 21; fax +33 (0) 5 62 21 67 18;
email techdesk@atr.fr.
(k) Credit for Previous Actions
This paragraph provides credit for the
actions required by paragraphs (g) and (h) of
this AD, if those actions were performed
before the effective date of this AD using the
applicable service information specified in
paragraphs (k)(1) through (k)(5) of this AD.
These documents are not incorporated by
reference in this AD.
(1) ATR Service Bulletin ATR42–27–0104,
dated December 17, 2010.
(2) ATR Service Bulletin ATR42–27–0105,
dated February 17, 2011.
(3) ATR Service Bulletin ATR72–27–1065,
dated April 15, 2010.
(4) ATR Service Bulletin ATR72–27–1065,
Revision 01, dated December 17, 2010.
(5) ATR Service Bulletin ATR72–27–1066,
dated February 17, 2011.
(l) 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 International Branch, send it to ATTN:
Tom Rodriguez, Aerospace Engineer,
International Branch, ANM–116, Transport
Airplane Directorate, FAA, 1601 Lind
Avenue SW., Renton, WA 98057–3356;
telephone 425–227–1137; fax 425–227–1149.
Information may be emailed to: 9-ANM-116AMOC-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. The AMOC approval letter
must specifically reference this AD.
(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 ATR–GIE Avions de Transport
´
Regional’s EASA Design Organization
Approval (DOA). If approved by the DOA,
the approval must include the DOAauthorized signature.
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Federal Register / Vol. 80, No. 123 / Friday, June 26, 2015 / Rules and Regulations
(3) Reporting Requirements: A federal
agency may not conduct or sponsor, and a
person is not required to respond to, nor
shall a person be subject to a penalty for
failure to comply with a collection of
information subject to the requirements of
the Paperwork Reduction Act unless that
collection of information displays a current
valid OMB Control Number. The OMB
Control Number for this information
collection is 2120–0056. Public reporting for
this collection of information is estimated to
be approximately 5 minutes per response,
including the time for reviewing instructions,
completing and reviewing the collection of
information. All responses to this collection
of information are mandatory. Comments
concerning the accuracy of this burden and
suggestions for reducing the burden should
be directed to the FAA at: 800 Independence
Ave. SW., Washington, DC 20591, Attn:
Information Collection Clearance Officer,
AES–200.
Issued in Renton, Washington, on June 17,
2015.
Michael Kaszycki,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
(m) Related Information
AGENCY:
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA
Airworthiness Directive 2012–0064, dated
April 20, 2012, for related information. You
may examine the MCAI on the Internet at
https://www.regulations.gov by searching for
and locating Docket No. FAA–2015–1986.
(2) Service information identified in this
AD that is not incorporated by reference is
available at the addresses specified in
paragraphs (n)(3) and (n)(4) of this AD.
wreier-aviles on DSK5TPTVN1PROD with RULES
(n) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(i) ATR Service Bulletin ATR42–27–0104,
Revision 01, dated August 30, 2011.
(ii) ATR Service Bulletin ATR42–27–0105,
Revision 01, dated August 30, 2011.
(iii) ATR Service Bulletin ATR72–27–1065,
Revision 02, dated August 30, 2011.
(iv) ATR Service Bulletin ATR72–27–1066,
Revision 01, dated August 30, 2011.
(3) For service information identified in
this AD, contact ATR–GIE Avions de
´
´
Transport Regional, 1, Allee Pierre Nadot,
31712 Blagnac Cedex, France; telephone +33
(0) 5 62 21 62 21; fax +33 (0) 5 62 21 67 18;
email continued.airworthiness@atr.fr;
Internet https://www.aerochain.com.
(4) 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.
(5) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
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[FR Doc. 2015–15615 Filed 6–25–15; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2014–0524; Directorate
Identifier 2014–NM–042–AD; Amendment
39–18189; AD 2015–13–02]
RIN 2120–AA64
Airworthiness Directives; Bombardier,
Inc. Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
We are adopting a new
airworthiness directive (AD) for certain
Bombardier, Inc. Model DHC–8–400
series airplanes. This AD was prompted
by reports of corrosion in the low-rate
discharge tubes of the fire protection
system leading to the forward baggage
compartment, and perforation of one or
more tubes. This AD requires repetitive
checks for leakage of the discharge tubes
of the fire protection system. This AD
also mandates eventual replacement of
all existing aluminum tube assemblies
with new, improved corrosion-resistant
stainless steel tube assemblies. We are
issuing this AD to prevent perforation of
the low-rate discharge tubes, which
could result in insufficient fire
extinguishing agent reaching the
forward baggage compartment in the
event of a fire, which could result in
damage to the airplane and injury to the
occupants.
DATES: This AD becomes effective July
31, 2015
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of July 31, 2015.
ADDRESSES: You may examine the AD
docket on the Internet at https://
www.regulations.gov/
#!docketDetail;D=FAA-2014-0524 or in
person at the Docket Management
Facility, U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE.,
Washington, DC.
For service information identified in
this AD, contact Bombardier, Inc., QSUMMARY:
PO 00000
Frm 00018
Fmt 4700
Sfmt 4700
Series Technical Help Desk, 123 Garratt
Boulevard, Toronto, Ontario M3K 1Y5,
Canada; telephone 416–375–4000; fax
416–375–4539; email thd.qseries@
aero.bombardier.com; Internet https://
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. It is also available
on the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2014–
0524.
FOR FURTHER INFORMATION CONTACT:
Fabio Buttitta, Aerospace Engineer,
Airframe and Mechanical Systems
Branch, ANE–171, FAA, New York
Aircraft Certification Office (ACO), 1600
Stewart Avenue, Suite 410, Westbury,
NY 11590; telephone 516–228–7303; fax
516–794–5531.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to certain Bombardier, Inc. Model
DHC–8–400 series airplanes. The NPRM
published in the Federal Register on
August 13, 2014 (79 FR 47384).
Transport Canada Civil Aviation
(TCCA), which is the aviation authority
for Canada, has issued Canadian
Airworthiness Directive CF–2014–06,
dated January 21, 2014 (referred to after
this as the Mandatory Continuing
Airworthiness Information, or ‘‘the
MCAI’’), to correct an unsafe condition
for the specified products. The MCAI
states:
Corrosion has been reported in the fire
protection system low rate discharge tubes
leading to the forward baggage compartment.
In some cases, this has led to perforation of
one or more tubes.
Perforation of forward baggage
compartment fire protection system tubes
may result in decreased effectiveness of the
fire protection system in the event of a fire
in the forward baggage compartment.
This [Canadian] AD mandates a repetitive
integrity check of the forward baggage
compartment fire protection system tube
assemblies, and the replacement of
aluminum forward baggage compartment fire
protection tube assemblies with corrosion
resistant stainless steel (CRES) tubes.
The unsafe condition is perforation of
the low-rate discharge tubes, which
could result in insufficient fire
extinguishing agent reaching the
forward baggage compartment and
reduce the capability of the fire
protection system to extinguish fires,
possibly resulting in damage to the
E:\FR\FM\26JNR1.SGM
26JNR1
]]>Agencies
[Federal Register Volume 80, Number 123 (Friday, June 26, 2015)]
[Rules and Regulations]
[Pages 36707-36710]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-15615]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2015-1986; Directorate Identifier 2012-NM-100-AD;
Amendment 39-18188; AD 2015-13-01]
RIN 2120-AA64
Airworthiness Directives; ATR-GIE Avions de Transport
R[eacute]gional Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
ATR-GIE Avions de Transport R[eacute]gional Model ATR42-500 and ATR72-
212A airplanes. This AD requires inspection of the affected control
systems rods and, depending on findings, a replacement of the affected
rods. This AD was prompted by reports of non-conformity of certain
control rods, which could result in failure of the control rods. We are
issuing this AD to detect and correct failure of an affected control
rod, which, under certain circumstances, could result in reduced
control of the airplane.
DATES: This AD becomes effective July 13, 2015.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of July 13,
2015.
We must receive comments on this AD by August 10, 2015.
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 https://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 AD, contact ATR-GIE
Avions de Transport R[eacute]gional, 1, All[eacute]e Pierre Nadot,
31712 Blagnac Cedex, France; telephone +33 (0) 5 62 21 62 21; fax +33
(0) 5 62 21 67 18; email continued.airworthiness@atr.fr; Internet
https://www.aerochain.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. It is also available on the
Internet at https://www.regulations.gov by searching for and locating
Docket No. FAA-2015-1986.
Examining the AD Docket
You may examine the AD docket on the Internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2015-
1986; or in person at the Docket Operations office between 9 a.m. and 5
p.m., Monday through Friday, except Federal holidays. The AD docket
contains this AD, the regulatory evaluation, any comments received, and
other information. The street address for the Docket 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: Tom Rodriguez, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137;
fax 425-227-1149.
SUPPLEMENTARY INFORMATION:
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 2012-0064, dated April 20, 2012 (referred to
after this as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for Model ATR42-500 and
ATR72-212A airplanes. The MCAI states:
Prompted by the findings that led to publication of EASA AD
2010-0063-E, additional quality investigation showed that the non-
conformity of certain control rods, which was due to incorrect
polishing during the rod manufacturing process, could also affect
other flight control rods [and could result in failure of the
control rods].
These other potentially non-conforming control rods are
installed on elevator controls, rudder pedal assemblies and rudder
tab controls of certain ATR aeroplanes.
This condition, if not detected and corrected, could lead to
failure of an affected control rod which, under certain
circumstances, could result in reduced control of the aeroplane.
As a result of further investigations, other batches have been
incriminated, in addition to the ones identified by EASA AD 2010-
0063-E, and new safety analyses also indicate the need for
replacement of the rods (within an adapted compliance time), which
had passed the check required by EASA AD 2010-0063-E. Consequently,
EASA AD 2010-0063-E is superseded by this new AD.
For the reasons described above, this [EASA] AD requires a one-
time inspection of the affected control systems rods and, depending
on findings, replacement of the affected rods.
You may examine the MCAI on the Internet at https://www.regulations.gov
by searching for and locating Docket No. FAA-2015-1986.
Related Service Information Under 1 CFR Part 51
ATR-GIE Avions de Transport R[eacute]gional (ATR) has issued the
following service information.
ATR Service Bulletin ATR42-27-0104, Revision 01, dated
August 30, 2011.
ATR Service Bulletin ATR42-27-0105, Revision 01, dated
August 30, 2011.
ATR Service Bulletin ATR72-27-1065, Revision 02, dated
August 30, 2011.
[[Page 36708]]
ATR Service Bulletin ATR72-27-1066, Revision 01, dated
August 30, 2011.
This service information describes procedures for the inspection of
affected control systems rods and, depending on findings, a replacement
of the affected rods. 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
of this AD.
FAA's Determination and Requirements of This 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 issuing this AD because we
evaluated all pertinent information and determined the unsafe condition
exists and is likely to exist or develop on other products of the same
type designs.
There are no products of this type currently registered in the
United States; however, this rule is necessary to ensure that the
described unsafe condition is addressed if any of these products are
placed on the U.S. Register in the future.
Differences Between This AD and the MCAI or Service Information
The actions specified in paragraph (4) of the MCAI, for rudder
pedals that have been inspected according to EASA AD 2010-0063-E, dated
April 1, 2010, is not included in this AD because the those actions
were not required by any FAA AD.
Although the MCAI requires using a certain repair manual to repair
certain conditions, paragraph (i) of this AD requires repair using a
method approved by the Manager, International Branch, ANM-116,
Transport Airplane Directorate, FAA; or the European Aviation Safety
Agency (EASA); or ATR-GIE Avions de Transport R[eacute]gional's EASA
Design Organization Approval (DOA).
FAA's Determination of the Effective Date
Since there are currently no domestic operators of this product,
notice and opportunity for public comment before issuing this AD are
unnecessary.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not precede it by notice and opportunity for public
comment. We invite you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
the ADDRESSES section. Include ``Docket No. FAA-2015-1986; Directorate
Identifier 2012-NM-100-AD'' at the beginning of your comments. We
specifically invite comments on the overall regulatory, economic,
environmental, and energy aspects of this AD. We will consider all
comments received by the closing date and may amend this AD based on
those comments.
We will post all comments we receive, without change, to https://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this AD.
Costs of Compliance
Currently, there are no affected airplanes on the U.S. Register.
However, if an affected airplane is imported and placed on the U.S.
Register in the future, we estimate that it will take about 1 work-hour
per product to comply with the basic requirements of this AD. The
average labor rate is $85 per work-hour. Required parts will cost $0
per product. Based on these figures, we estimate the cost of this AD on
U.S. operators to be $85 per product.
Paperwork Reduction Act
A federal agency may not conduct or sponsor, and a person is not
required to respond to, nor shall a person be subject to penalty for
failure to comply with a collection of information subject to the
requirements of the Paperwork Reduction Act unless that collection of
information displays a current valid OMB control number. The control
number for the collection of information required by this AD is 2120-
0056. The paperwork cost associated with this AD has been detailed in
the Costs of Compliance section of this document and includes time for
reviewing instructions, as well as completing and reviewing the
collection of information. Therefore, all reporting associated with
this AD is mandatory. Comments concerning the accuracy of this burden
and suggestions for reducing the burden should be directed to the FAA
at 800 Independence Ave. SW., Washington, DC 20591, ATTN: Information
Collection Clearance Officer, AES-200.
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 AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in Alaska; and
4. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
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):
2015-13-01 ATR-GIE Avions de Transport R[eacute]gional: Amendment
39-18188. Docket
[[Page 36709]]
No. FAA-2015-1986; Directorate Identifier 2012-NM-100-AD.
(a) Effective Date
This AD becomes effective July 13, 2015.
(b) Affected ADs
None.
(c) Applicability
This AD applies to airplanes specified in paragraphs (c)(1) and
(c)(2) of this AD, certificated in any category.
(1) ATR-GIE Avions de Transport R[eacute]gional Model ATR42-500
airplanes having manufacturer serial number (MSN) 671 through 815
inclusive, except MSN 811.
(2) ATR-GIE Avions de Transport R[eacute]gional Model ATR72-212A
airplanes having MSN 769 through 914 inclusive, except MSN 826, 905,
908, and 911.
(d) Subject
Air Transport Association (ATA) of America Code 27, Flight
Controls.
(e) Reason
This AD was prompted by reports of non-conformity of certain
control rods, which could result in failure of the control rods. We
are issuing this AD to detect and correct failure of an affected
control rod, which, under certain circumstances, could result in
reduced control of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Elevator Control Rod Inspection
For airplanes identified in ATR Service Bulletin ATR42-27-0105,
Revision 01, dated August 30, 2011; or ATR72-27-1066, Revision 01,
dated August 30, 2011; as applicable to airplane model: Within 6
months after the effective date of this AD, inspect all four
elevator control rods having part number (P/N) S27381930-004 and P/N
S27381831-006 for batch number identification, in accordance with
the Accomplishment Instructions of ATR Service Bulletin ATR42-27-
0105, Revision 01, dated August 30, 2011; or ATR Service Bulletin
ATR72-27-1066, Revision 01, dated August 30, 2011, as applicable to
airplane model. A review of airplane maintenance records is
acceptable in lieu of this inspection, if the batch number can be
conclusively determined from that review. Replace any affected rod,
including any rod with an unreadable batch number, at the applicable
time specified in paragraph (g)(1) or (g)(2) of this AD, in
accordance with ATR Service Bulletin ATR42-27-0105, Revision 01,
dated August 30, 2011; or ATR72-27-1066, Revision 01, dated August
30, 2011; as applicable to airplane model.
(1) If only one rod is affected: Replace it within 10 days after
the inspection.
(2) If two or more rods are affected: Replace all rods before
further flight, except that replacement of one of the affected rods
may be deferred for 10 days.
(h) Rudder Pedal Rod Inspection
For airplanes identified in ATR Service Bulletin ATR42-27-0104,
Revision 01, dated August 30, 2011; or ATR Service Bulletin ATR72-
27-1065, Revision 02, dated August 30, 2011; as applicable to
airplane model: Inspect all four rudder pedal rods having P/N
S2728116400000 for batch number identification, in accordance with
the Accomplishment Instructions of ATR Service Bulletin ATR42-27-
0104, Revision 01, dated August 30, 2011; or ATR Service Bulletin
ATR72-27-1065, Revision 02, dated August 30, 2011; as applicable to
airplane model. For any affected rudder pedal rod, including any rod
with an unreadable batch number, before further flight, check the
rod diameter using a special tool, in accordance with ATR Service
Bulletin ATR42-27-0104, Revision 01, dated August 30, 2011; or ATR
Service Bulletin ATR72-27-1065, Revision 02, dated August 30, 2011;
as applicable to airplane model.
(1) If, during the diameter check, the rod passes through the
tool, replace the rod before further flight.
(2) If, during the diameter check, the rod does not pass through
the tool, replace the rod within 5,000 flight hours after the
diameter check.
(i) Rudder Tab Control Rod Inspection
For airplanes identified in paragraph (c) of this AD, except for
airplanes having MSNs 671, 673, and 769 through 784 inclusive:
Within 24 months after the effective date of this AD, inspect the
rudder tab control rod P/N S27281929-002 for batch number
identification, using a method approved by the Manager,
International Branch, ANM-116, Transport Airplane Directorate, FAA;
or the European Aviation Safety Agency (EASA); or Avions de
Transport R[eacute]gional (ATR)'s EASA Design Organization Approval
(DOA). If the rudder tab control rod belongs to batch number 2107267
or 2120855, or if the batch number is unreadable: Before further
flight, replace the rod with a serviceable rod using a method
approved by the Manager, International Branch, ANM-116, Transport
Airplane Directorate, FAA; or EASA; or ATR's EASA DOA.
Note 1 to paragraph (i) of this AD: ATR 42/72 Aircraft
Maintenance Manual (AMM)/Job Instruction Cards (JIC) 27-20-00 DVI
1000 and AMM/JIC 27-21-42 RAI 10000 are additional sources of
guidance for accomplishment of the rudder tab control rod
inspection.
(j) Reporting Requirement
Submit a report of the rod inspection and check required by
paragraphs (g) and (h) of this AD at the applicable compliance time
specified in paragraph (j)(1) of this AD, in accordance with the
instructions specified in paragraph (j)(2) of this AD.
(1) Submit the report at the applicable time specified in
paragraph (j)(1)(i) or (j)(1)(ii) of this AD.
(i) If the inspection or check was done on or after the
effective date of this AD: Submit the report within 30 days after
the inspection or check.
(ii) If the inspection or check was done before the effective
date of this AD: Submit the report within 30 days after the
effective date of this AD.
(2) Submit the report (including no findings) to ATR using the
Accomplishment Report form provided in the service information
identified in paragraph (j)(2)(i), (j)(2)(ii), (j)(2)(iii), or
(j)(2)(iv) of this AD; as applicable to airplane model.
(i) ATR Service Bulletin ATR42-27-0104, Revision 01, dated
August 30, 2011.
(ii) ATR Service Bulletin ATR42-27-0105, Revision 01, dated
August 30, 2011.
(iii) ATR Service Bulletin ATR72-27-1065, Revision 02, dated
August 30, 2011.
(iv) ATR Service Bulletin ATR72-27-1066, Revision 01, dated
August 30, 2011.
(3) Send the report to ATR-GIE Avions de Transport
R[eacute]gional, 1, All[eacute]e Pierre Nadot, 31712 Blagnac Cedex,
France; telephone +33 (0) 5 62 21 62 21; fax +33 (0) 5 62 21 67 18;
email techdesk@atr.fr.
(k) Credit for Previous Actions
This paragraph provides credit for the actions required by
paragraphs (g) and (h) of this AD, if those actions were performed
before the effective date of this AD using the applicable service
information specified in paragraphs (k)(1) through (k)(5) of this
AD. These documents are not incorporated by reference in this AD.
(1) ATR Service Bulletin ATR42-27-0104, dated December 17, 2010.
(2) ATR Service Bulletin ATR42-27-0105, dated February 17, 2011.
(3) ATR Service Bulletin ATR72-27-1065, dated April 15, 2010.
(4) ATR Service Bulletin ATR72-27-1065, Revision 01, dated
December 17, 2010.
(5) ATR Service Bulletin ATR72-27-1066, dated February 17, 2011.
(l) 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 International
Branch, send it to ATTN: Tom Rodriguez, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137;
fax 425-227-1149. 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. The AMOC approval letter must
specifically reference this AD.
(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 ATR-GIE Avions de
Transport R[eacute]gional's EASA Design Organization Approval (DOA).
If approved by the DOA, the approval must include the DOA-authorized
signature.
[[Page 36710]]
(3) Reporting Requirements: A federal agency may not conduct or
sponsor, and a person is not required to respond to, nor shall a
person be subject to a penalty for failure to comply with a
collection of information subject to the requirements of the
Paperwork Reduction Act unless that collection of information
displays a current valid OMB Control Number. The OMB Control Number
for this information collection is 2120-0056. Public reporting for
this collection of information is estimated to be approximately 5
minutes per response, including the time for reviewing instructions,
completing and reviewing the collection of information. All
responses to this collection of information are mandatory. Comments
concerning the accuracy of this burden and suggestions for reducing
the burden should be directed to the FAA at: 800 Independence Ave.
SW., Washington, DC 20591, Attn: Information Collection Clearance
Officer, AES-200.
(m) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive 2012-0064, dated April 20, 2012,
for related information. You may examine the MCAI on the Internet at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2015-1986.
(2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (n)(3) and (n)(4) of this AD.
(n) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) ATR Service Bulletin ATR42-27-0104, Revision 01, dated
August 30, 2011.
(ii) ATR Service Bulletin ATR42-27-0105, Revision 01, dated
August 30, 2011.
(iii) ATR Service Bulletin ATR72-27-1065, Revision 02, dated
August 30, 2011.
(iv) ATR Service Bulletin ATR72-27-1066, Revision 01, dated
August 30, 2011.
(3) For service information identified in this AD, contact ATR-
GIE Avions de Transport R[eacute]gional, 1, All[eacute]e Pierre
Nadot, 31712 Blagnac Cedex, France; telephone +33 (0) 5 62 21 62 21;
fax +33 (0) 5 62 21 67 18; email continued.airworthiness@atr.fr;
Internet https://www.aerochain.com.
(4) 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.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on June 17, 2015.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2015-15615 Filed 6-25-15; 8:45 am]
BILLING CODE 4910-13-P
