[Federal Register Volume 80, Number 251 (Thursday, December 31, 2015)]
[Rules and Regulations]
[Pages 81738-81742]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-32596]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2015-0683; Directorate Identifier 2014-NM-196-AD;
Amendment 39-18355; AD 2015-26-07]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: We are adopting a new airworthiness directive (AD) for all The
Boeing Company Model 767-200, -300, and -300F series airplanes. This AD
was prompted by a finding that certain barrel nuts installed at the
vertical fin may be subject to stress corrosion and cracking. This AD
requires either repetitive inspections of vertical fin barrel nuts for
corrosion or a magnetic check to identify certain barrel nuts, and
corrective actions if necessary. We are issuing this AD to detect and
correct corroded and loose barrel nuts that attach the vertical fin to
body section 48; this condition could result in reduced structural
integrity of the vertical fin attachment joint, loss of the vertical
fin, and consequent loss of controllability of the airplane.
DATES: This AD is effective February 4, 2016.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of February 4,
2016.
ADDRESSES: For service information identified in this final rule,
contact Boeing Commercial Airplanes, Attention: Data & Services
Management, P.O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone
206-544-5000, extension 1; fax 206-766-5680; Internet https://www.myboeingfleet.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-2015-
0683; 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 AD, the regulatory evaluation, any comments received, and
other information. The address for the Docket Office (phone: 800-647-
5527) is 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 20590.
FOR FURTHER INFORMATION CONTACT: Wayne Lockett, Aerospace Engineer,
Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office
(ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917-
6447; fax: 425-917-6590; email: [email protected].
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 all The Boeing Company
Model 767-200, -300, and -300F series airplanes. The NPRM published in
the Federal Register on April 10, 2015 (80 FR 19248). The NPRM was
prompted by a finding that certain barrel nuts installed at the
vertical fin may be subject to stress corrosion and cracking. The NPRM
proposed to require either
[[Page 81739]]
repetitive inspections of vertical fin barrel nuts for corrosion or a
magnetic check to identify certain barrel nuts, and corrective actions
if necessary. We are issuing this AD to detect and correct corroded and
loose barrel nuts that attach the vertical fin to body section 48; this
condition could result in reduced structural integrity of the vertical
fin attachment joint, loss of the vertical fin, and consequent loss of
controllability of the airplane.
Comments
We gave the public the opportunity to participate in developing
this AD. The following presents the comments received on the NPRM (80
FR 19248, April 10, 2015) and the FAA's response to each comment.
Request To Revise Applicability
Boeing and Air New Zealand requested that additional clarification
be added to paragraph (c) of the proposed AD (80 FR 19248, April 10,
2015). Boeing stated that this addition will add clarity because there
is an existing AD (AD 2003-10-11, Amendment 39-13156 (68 FR 28703, May
27, 2003)) of a similar subject that covers only Boeing Model 767
airplanes, line numbers 1 through 574 inclusive. Boeing requested we
clarify that Boeing Alert Service Bulletin 767-53A0261, dated August
12, 2014, addresses only Boeing Model 767 airplanes with line numbers
575 through 681 inclusive. Air New Zealand asked whether the NPRM would
supersede AD 2003-10-11.
We agree to provide clarification. Only Model 767 airplanes with
line numbers 575 through 681 inclusive are affected by this AD. Some
proposed requirements overlap with the requirements of AD 2003-10-11,
Amendment 39-13156 (68 FR 28703, May 27, 2003). We have therefore
revised the applicability of this AD to specify airplanes identified in
Boeing Alert Service Bulletin 767-53A0261, dated August 12, 2014, which
limits the applicability to line numbers 575 through 681 inclusive.
Request To Add Clarification About the Previous Replacement of
Discovered H-11 Barrel Nuts With Inconel Alternatives
Boeing stated that operators may have already replaced discovered
H-11 barrel nuts with Inconel alternatives. Boeing requested that we
revise the NPRM (80 FR 19248, April 10, 2015) to specify the
``Compliance Time Exceptions'' noted in paragraph 1.E., ``Compliance,''
of Boeing Alert Service Bulletin 767-53A0261, dated August 12, 2014.
Those ``exceptions'' would specify that no further action is required
at the vertical stabilizer attachment point, provided the following
conditions are met:
The vertical stabilizer attachment barrel nut has been
inspected;
No H-11 steel barrel nut was found during the inspection;
and
Any replacement barrel nut is either a drawing
configuration barrel nut made from an alternative material to H-11
steel; or a barrel nut made from alternative material to H-11 steel
approved by the FAA or by a Boeing Company Authorized Representative.
We do not agree with the request because paragraph (g) of this AD
already makes reference to paragraph 1.E., ``Compliance,'' of Boeing
Alert Service Bulletin 767-53A0261, dated August 12, 2014, which lists
the compliance time exceptions. We have not changed this AD regarding
this issue.
Request To Clarify Terminating Action for Repetitive Inspections and
Replacement
United Parcel Service (UPS) requested that we provide terminating
action similar to that provided in paragraph (i) of AD 2013-18-02,
Amendment 39-17575 (78 FR 57049, September 17, 2013).
We agree with the commenter's request. The NPRM (80 FR 19248, April
10, 2015) is not clear whether the repetitive inspections are
terminated by replacement with an Inconel barrel nut or by a finding of
no H-11 steel barrel nut installed. Replacing a barrel nut at an
attachment point location with a new Inconel barrel nut in accordance
with Part 5 of Boeing Alert Service Bulletin 767-53A0261, dated August
12, 2014, terminates the inspections and replacement required by
paragraph (g) of this AD for that attachment point location only. In
addition, if no H-11 steel barrel nut is found installed at an
attachment point location, the repetitive inspections and replacement
required by paragraph (g) of this AD are terminated for that attachment
location only. We have added a new paragraph (h) to this AD to clarify
the terminating action and redesignated the subsequent paragraphs
accordingly.
Request For Clarification of Barrel Nuts To Be Replaced
UPS requested that we provide clarification of paragraph
(g)(1)(ii)(B) of the proposed AD (80 FR 19248, April 10, 2015). UPS
stated that its interpretation of paragraph (g)(1)(ii)(B) of the
proposed AD is that replacement of only H-11 steel barrel nuts is
required, although it appears that all barrel nuts are to be replaced,
even if the installed barrel nuts are Inconel or other approved barrel
nuts.
We agree that clarification is necessary. Operators are required to
do all actions specified in either paragraph (g)(1) or (g)(2) of this
AD. Paragraph (g)(1) of this AD is only an internal and external
detailed inspection of the barrel nuts and does not provide a method
for determination of the material of the barrel nuts. Paragraph (g)(2)
of this AD provides the method to determine if the material of the
barrel nuts is H-11 steel.
Therefore, if operators have chosen to do the internal and external
inspections along with the torque check specified in paragraph (g)(1)
of this AD, and have not chosen to do the magnetic check specified in
paragraph (g)(2) of this AD, then they have not determined the material
of the barrel nuts. For airplanes on which the material of the barrel
nuts has not been determined, the requirement is to replace all barrel
nuts, as required by paragraph (g)(1)(ii)(B) of this AD.
Operators choosing to do the magnetic check specified in paragraph
(g)(2) of this AD would have determined the material of the barrel
nuts, and may replace only H-11 steel barrel nuts, as required by
paragraph (g)(2)(i)(B)(2) of this AD.
Operators are not permitted to mix actions from paragraphs (g)(1)
and (g)(2) of this AD. Operators may, however, submit requests for
approval of an alternative method of compliance (AMOC) to the
requirements of paragraph (g) of this AD along with justification of an
equivalent level of safety. We have not changed this AD regarding this
issue.
Request For Clarification of Compliance Time
UPS requested that we provide an exception to the initial
inspection thresholds of the ``last Torque Check Inspection'' specified
in paragraph 1.E., ``Compliance,'' of Boeing Alert Service Bulletin
767-53A0261, dated August 12, 2014. The specified compliance time is
the later of 24 months after issuance of the service information or 36
months after the last torque check inspection specified in Task 53-734-
00, ``Internal, Special Detailed, Vertical Stabilizer Attach Bolt, of
Section 2, ``Structural Maintenance Requirements,'' of the Boeing Model
767 Maintenance Planning Document. The commenter understands that the
most recent accomplishment of Task 53-734-00 must be done prior to the
effective date of this AD. The commenter added that if the initial
inspection required by paragraph (g)(1) or (g)(2) of the proposed AD
(80 FR 19248, April 10, 2015) is
[[Page 81740]]
done from the most recent accomplishment of Task 53-734-00 and that
accomplishment occurs after the effective date of this AD, the time
limits given in paragraphs (g)(1)(ii)(B) and (g)(2)(i)(B)(2) of this
proposed AD may be exceeded (i.e., will have already passed).
We agree with the commenter's request and rationale regarding
providing an exception to the specified initial inspection threshold.
We have redesignated paragraph (h) of the proposed AD (80 FR 19248,
April 10, 2015) as paragraph (i)(1) of this AD and added new paragraph
(i)(2) to this AD to provide a compliance time exception to address the
issue described by the commenter. If the most recent accomplishment of
Task 53-734-00 occurs after the effective date of this AD, then
operators still have to comply with the requirements of paragraph
(g)(1) or (g)(2) of this AD.
Request For Clarification of Effect of Winglets on Accomplishment of
the Proposed Actions
Aviation Partners Boeing stated that accomplishing the supplemental
type certificate (STC) ST01920SE (http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/59027F43B9A7486E86257B1D006591EE) does not affect the actions specified
in the NPRM (80 FR 19248, April 10, 2015).
We agree with the commenter's statement. We have redesignated
paragraph (c) of the proposed AD (80 FR 19248, April 10, 2015) as
paragraph (c)(1) of this AD, and added new paragraph (c)(2) to this AD
to state that installation of STC ST01920SE (http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/59027F43B9A7486E86257B1D006591EE) does not affect the ability to
accomplish the actions required by this AD. Therefore, for airplanes on
which STC ST01920SE (http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/59027F43B9A7486E86257B1D006591EE) is installed, a ``change in product''
AMOC approval request is not necessary to comply with the requirements
of 14 CFR 39.17.
Conclusion
We reviewed the relevant data, considered the comments received,
and determined that air safety and the public interest require adopting
this AD with the changes described previously and minor editorial
changes. We have determined that these minor changes:
[Agr]re consistent with the intent that was proposed in
the NPRM (80 FR 19248, April 10, 2015) for correcting the unsafe
condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM (80 FR 19248, April 10, 2015).
We also determined that these changes will not increase the
economic burden on any operator or increase the scope of this AD.
Related Service Information Under 1 CFR Part 51
Boeing has issued Alert Service Bulletin 767-53A0261, dated August
12, 2014. The service information describes procedures for repetitive
internal and external detailed inspections of the barrel nut holes and
sealant for cracked/damaged sealant, corrosion, or a cracked/broken
barrel nut, and replacement of the barrel nut with a new Inconel barrel
nut if necessary. The service information also describes procedures for
repetitive torque checks on each affected vertical fin attachment bolt,
or, alternatively, a magnetic check to identify H-11 steel barrel nuts,
and replacement with a new Inconel barrel nut if necessary.
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.
Costs of Compliance
We estimate that this AD affects 38 airplanes of U.S. registry. We
estimate the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost on U.S.
Action Labor cost Parts cost Cost per product operators
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Option 1: Detailed inspections 4 work-hours x $85 (\1\) Up to $482,661 per Up to $18,341,118.
and torque check. per hour = $340 inspection cycle.
per inspection
cycle.
Option 2: Magnetic check........ 4 work-hours x $85 $0 $340............... $12,920.
per hour = $340.
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\1\ For the torque check, operators may choose to rent a special tool, with rental costs up to $482,321.
We estimate that replacing any barrel nut would take 1 work-hour,
at an average labor rate of $85 per work-hour. We have received no
definitive data that would enable us to provide cost estimates for the
cost of replacement parts. We have no way of determining the number of
aircraft that might need these replacements.
According to the manufacturer, some of the costs of this AD may be
covered under warranty, thereby reducing the cost impact on affected
individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all available costs in our
cost estimate.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
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,
[[Page 81741]]
(2) Is not a ``significant rule'' under 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):
2015-26-07 The Boeing Company: Amendment 39-18355; Docket No. FAA-
2015-0683; Directorate Identifier 2014-NM-196-AD.
(a) Effective Date
This AD is effective February 4, 2016.
(b) Affected ADs
None.
(c) Applicability
(1) This AD applies to The Boeing Company Model 767-200, -300, -
300F series airplanes, certificated in any category, as identified
in Boeing Alert Service Bulletin 767-53A0261, dated August 12, 2014.
(2) Installation of Supplemental Type Certificate (STC)
ST01920SE (http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/59027F43B9A7486E86257B1D006591EE) does not affect the
ability to accomplish the actions required by this AD. Therefore,
for airplanes on which STC ST01920SE (http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/59027F43B9A7486E86257B1D006591EE) is installed, a ``change in
product'' alternative method of compliance (AMOC) approval request
is not necessary to comply with the requirements of 14 CFR 39.17.
(d) Subject
Air Transport Association (ATA) of America Code 53, Fuselage.
(e) Unsafe Condition
This AD was prompted by a finding that certain barrel nuts
installed at the vertical fin may be subject to stress corrosion and
cracking. We are issuing this AD to detect and correct corroded and
loose barrel nuts that attach the vertical fin to body section 48;
this condition could result in reduced structural integrity of the
vertical fin attachment joint, loss of the vertical fin, and
consequent loss of controllability of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Inspection
For airplanes identified in Boeing Alert Service Bulletin 767-
53A0261, dated August 12, 2014: Do the actions specified in
paragraph (g)(1) or (g)(2) of this AD, in accordance with the
Accomplishment Instructions of Boeing Alert Service Bulletin 767-
53A0261, dated August 12, 2014. Signs of corrosion include, but are
not limited to, sealant cracks, sealant bulging, powder residue, and
cracked barrel nuts.
(1) At the applicable time specified in paragraph 1.E.,
``Compliance,'' of Boeing Alert Service Bulletin 767-53A0261, dated
August 12, 2014, except as provided by paragraph (i) of this AD: Do
internal and external detailed inspections of the barrel nuts and
sealant for signs of corrosion, and do a torque check of the
vertical stabilizer attachment bolts for loose barrel nuts.
(i) If corrosion or any loose barrel nut is found at any
attachment point location, before further flight, replace the barrel
nut with a new Inconel barrel nut.
(ii) If no corrosion or loose barrel nut is found at any
attachment point location, do the actions specified in paragraphs
(g)(1)(ii)(A) and (g)(1)(ii)(B) of this AD.
(A) Repeat the inspections and torque check thereafter at
intervals not to exceed 18 months until the replacement specified in
paragraph (g)(1)(ii)(B) of this AD is done at that attachment point
location.
(B) Within 36 months after the effective date of this AD,
replace all barrel nuts with new Inconel barrel nuts.
(2) At the applicable time specified in paragraph 1.E.,
``Compliance,'' of Boeing Alert Service Bulletin 767-53A0261, dated
August 12, 2014, except as provided by paragraph (i) of this AD: Do
a magnetic check to identify H-11 steel barrel nuts.
(i) If any H-11 steel barrel nut is found at any attachment
point location, before further flight, do an internal and external
detailed inspection of the barrel nut holes and sealant for signs of
corrosion, and do a torque check of the vertical stabilizer
attachment bolts for loose barrel nuts.
(A) If corrosion or any loose barrel nut is found, before
further flight, replace the barrel nut with a new Inconel barrel
nut.
(B) If no corrosion or loose barrel nut is found, do the actions
specified in paragraphs (g)(2)(i)(B)(1) and (g)(2)(i)(B)(2) of this
AD.
(1) Repeat the inspections and torque check thereafter at
intervals not to exceed 18 months until the replacement specified in
paragraph (g)(2)(i)(B)(2) of this AD is done at that attachment
point location.
(2) Within 36 months after the effective date of this AD,
replace all H-11 steel barrel nuts with new Inconel barrel nuts.
(ii) If no H-11 steel barrel nut is found at all attachment
point locations, no further work is required by this paragraph.
(h) Terminating Action for Repetitive Inspections and Replacement
(1) Replacing a barrel nut at an attachment point location with
a new Inconel barrel nut, in accordance with Part 5 of Boeing Alert
Service Bulletin 767-53A0261, dated August 12, 2014, terminates the
inspections and replacement required by paragraph (g) of this AD for
that attachment point location only.
(2) If no H-11 steel barrel nut is found installed at an
attachment point location, the repetitive inspections and
replacement required by paragraph (g) of this AD are terminated for
that attachment location only.
(i) Exception to Service Information Specifications
(1) Where Boeing Alert Service Bulletin 767-53A0261, dated
August 12, 2014, specifies a compliance time ``after the Original
Issue date of this Service Bulletin,'' this AD requires compliance
within the specified compliance time after the effective date of
this AD.
(2) Where Boeing Alert Service Bulletin 767-53A0261, dated
August 12, 2014, specifies a compliance time after the ``last Torque
Check Inspection'' in accordance with Task 53-734-00, ``Internal,
Special Detailed, Vertical Stabilizer Attach Bolt, of Section 2,
Structural Maintenance Requirements,'' of the Boeing Model 767
Maintenance Planning Document, that compliance time only applies if
the most recent accomplishment of Task 53-734-00 occurred on or
before the effective date of this AD.
(j) Parts Installation Prohibition
As of the effective date of this AD, no person may install an H-
11 steel barrel nut on the vertical stabilizer of any airplane.
(k) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Seattle Aircraft Certification Office (ACO),
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 ACO, send it to the
attention of the person identified in paragraph (l)(1) of this AD.
Information may be emailed to: [email protected].
(2) 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.
(3) An AMOC that provides an acceptable level of safety may be
used for any repair, modification, or alteration required by this AD
if it is approved by the Boeing Commercial Airplanes Organization
Designation Authorization (ODA) that has been authorized by the
Manager, Seattle
[[Page 81742]]
ACO, to make those findings. To be approved, the repair method,
modification deviation, or alteration deviation must meet the
certification basis of the airplane, and the approval must
specifically refer to this AD.
(4) For service information that contains steps that are labeled
as Required for Compliance (RC), the provisions of paragraphs
(k)(4)(i) and (k)(4)(ii) apply.
(i) The steps labeled as RC, including substeps under an RC step
and any figures identified in an RC step, must be done to comply
with the AD. An AMOC is required for any deviations to RC steps,
including substeps and identified figures.
(ii) Steps not labeled as RC may be deviated from using accepted
methods in accordance with the operator's maintenance or inspection
program without obtaining approval of an AMOC, provided the RC
steps, including substeps and identified figures, can still be done
as specified, and the airplane can be put back in an airworthy
condition.
(l) Related Information
(1) For more information about this AD, contact Wayne Lockett,
Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft
Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-
3356; phone: 425-917-6447; fax: 425-917-6590; email:
[email protected].
(2) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management,
P.O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone 206-544-
5000, extension 1; fax 206-766-5680; Internet https://www.myboeingfleet.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.
(m) 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 the AD specifies otherwise.
(i) Boeing Alert Service Bulletin 767-53A0261, dated August 12,
2014.
(ii) Reserved.
(3) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Data & Services Management,
P.O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone 206-544-
5000, extension 1; fax 206-766-5680; Internet https://www.myboeingfleet.com.
(4) You may view this service information at 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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on December 9, 2015.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2015-32596 Filed 12-30-15; 8:45 am]
BILLING CODE 4910-13-P