81 FR 11687 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 44 (March 7, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 44 (March 7, 2016)
| Page Range | 11687-11689 | |
| FR Document | 2016-04679 |
[Federal Register Volume 81, Number 44 (Monday, March 7, 2016)] [Proposed Rules] [Pages 11687-11689] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-04679] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-3992; Directorate Identifier 2015-NM-075-AD] RIN 2120-AA64 Airworthiness Directives; The Boeing Company Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 787-8 airplanes. This proposed AD was prompted by a report that a captain's seat moved uncommanded during a landing rollout due to a failure in the seat horizontal actuator. This proposed AD would require repetitive tests of the captain and first officer seat assemblies for proper operation, and corrective action if necessary. This proposed AD would also require installing new captain and first officer seat assemblies, which would terminate the repetitive tests. We are proposing this AD to prevent a seat actuator clutch failure, which could result in a loss of seat locking and uncommanded motion of the captain's or first officer's seat; uncommanded seat movement could result in reduced controllability of the airplane. DATES: We must receive comments on this proposed AD by April 21, 2016. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments. Fax: 202-493-2251. Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590. Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. [[Page 11688]] For service information identified in this NPRM, 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. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-3992. 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-2016- 3992; 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 Office (phone: 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Brandon Lucero, Aerospace Engineer, Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917-6572; fax: 425-917-6590. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2016-3992; Directorate Identifier 2015-NM-075-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 because of 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 This proposed AD was prompted by a report that a captain's seat moved uncommanded during a landing rollout due to a failure in the seat horizontal actuator. Investigation found press fit clutch pins in the actuator could migrate loose when subjected to repeated dynamic impact loading from clutch re-engagement when the manual horizontal control lever is released with the seat still moving on the tracks. The clutch pins can migrate loose, overturn, and force clutch plate separation, resulting in degraded or failed seat locking. We are proposing this AD to prevent a seat actuator clutch failure, which could result in a loss of seat locking and uncommanded motion of the captain's or first officer's seat; uncommanded seat movement could result in reduced controllability of the airplane. Related Service Information Under 1 CFR Part 51 We reviewed Boeing Alert Service Bulletin B787-81205-SB250054-00, Issue 001, dated December 19, 2014. This service information provides procedures for installation of new captain and first officer seat assemblies, a test of the captain and first officer seat assemblies, and corrective action 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. FAA's Determination We are proposing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of the same type design. Proposed AD Requirements This proposed AD would require accomplishing the actions specified in the service information described previously. For information on the procedures and compliance times, see this service information at http://www.regulations.gov by searching for and locating Docket No. FAA-2016- 3992. The phrase ``corrective actions'' is used in this proposed AD. ``Corrective actions'' are actions that correct or address any condition found. Corrective actions in an AD could include, for example, repairs. Costs of Compliance We estimate that this proposed AD affects 18 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost on U.S. Action Labor cost Parts cost Cost per product operators ---------------------------------------------------------------------------------------------------------------- Operational test................. 2 work-hours x $85 $0................. $170 per test cycle $3060 per hour = $170 per test cycle. Seat assembly installation....... 3 work-hours x $85 $15,141 per seat x 30,537 to replace 549,666 per hour = $255 to 2 seats = $30,282. two seats. replace two seats. ---------------------------------------------------------------------------------------------------------------- We estimate the following costs to do any necessary corrective actions that would be required based on the results of the proposed operational tests. We have no way of determining the number of aircraft that might need these actions: On-Condition Costs ---------------------------------------------------------------------------------------------------------------- Cost per Action Labor cost Parts cost product ---------------------------------------------------------------------------------------------------------------- Replacement of captain seat vertical actuator. 2 work-hours x $85 per hour = $7,500 $7,670 $170. Replacement of captain seat horizontal 2 work-hours x $85 per hour = 7,500 7,670 actuator. $170. Replacement of first officer seat vertical 2 work-hours x $85 per hour = 7,500 7,670 actuator. $170. Replacement of first officer seat horizontal 2 work-hours x $85 per hour = 7,500 7,670 actuator. $170. ---------------------------------------------------------------------------------------------------------------- [[Page 11689]] 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): The Boeing Company: Docket No. FAA-2016-3992; Directorate Identifier 2015-NM-075-AD. (a) Comments Due Date We must receive comments by April 21, 2016. (b) Affected ADs None. (c) Applicability This AD applies to The Boeing Company Model 787-8 airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin B787-81205-SB250054-00, Issue 001, dated December 19, 2014. (d) Subject Air Transport Association (ATA) of America Code 25, Equipment/ furnishings. (e) Unsafe Condition This AD was prompted by a report that a captain's seat moved uncommanded during a landing rollout due to a failure in the seat horizontal actuator. We are issuing this AD to prevent a seat actuator clutch failure, which could result in a loss of seat locking and uncommanded motion of the captain's or first officer's seat; uncommanded seat motion could result in reduced controllability of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Repetitive Tests of Captain and First Officer Seat Assembly Operation Within 1,000 flight hours after the effective date of this AD, test the operation of the captain and first officer seat assemblies and do all applicable corrective actions, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin B787- 81205-SB250054-00, Issue 001, dated December 19, 2014. Do all applicable corrective actions before further flight. Repeat the operational test thereafter at intervals not to exceed 1,000 flight hours until the installation required by paragraph (h) of this AD is done. (h) New Seat Installation Within 72 months after the effective date of this AD, do the actions specified in paragraphs (h)(1) and (h)(2) of this AD, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin B787-81205-SB250054-00, Issue 001, dated December 19, 2014. Installing the seat specified in paragraph (h)(1) or (h)(2) of this AD is terminating action for the repetitive operational tests required by paragraph (g) of this AD for that seat only. (1) Install new captain seat assembly, part number (P/N) 3A380- 0007-01-7. (2) Install new first officer seat assembly, P/N 3A380-0008-01- 7. (i) Alternative Methods of Compliance (AMOCs) (1) The Manager, Seattle Aircraft Certification Office, ANM- 150S, 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 (j)(1) of this AD. (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 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 ACO, to make those findings. For a repair method to be approved, the repair 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 (i)(4)(i) and (i)(4)(ii) of this AD, 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. (j) Related Information (1) For more information about this AD, contact Brandon Lucero, Aerospace Engineer, Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917-6572; fax: 425-917-6590. (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 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 February 23, 2016. Dionne Palermo, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-04679 Filed 3-4-16; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 81, No. 44 / Monday, March 7, 2016 / Proposed Rules 11687
ACTION: Proposed rulemaking; notice of Energy, Office of Electricity Delivery Issued in Washington, DC, on February 29,
public meeting. and Energy Reliability, Mailstop OE–20, 2016.
Room 8G–017, 1000 Independence Meghan Conklin,
SUMMARY: This document announces Avenue SW., Washington, DC 20585; or Deputy Assistant Secretary, Office of
that the U.S. Department of Energy Electricity Delivery and Energy Reliability.
oeregs@hq.doe.gov.
(DOE) will hold a public workshop to [FR Doc. 2016–04986 Filed 3–4–16; 8:45 am]
discuss the proposed rule for the SUPPLEMENTARY INFORMATION: On BILLING CODE 6450–01–P
coordination of federal authorizations February 2, 2016, DOE published a
for electric transmission facilities for the proposed rule in the Federal Register
Integrated Interagency Pre-application (81 FR 5383) to provide a process for the DEPARTMENT OF TRANSPORTATION
(IIP) process. The public workshop will timely coordination of Federal
include a presentation describing the authorizations for proposed Federal Aviation Administration
proposed rule and will allow for transmission facilities pursuant to
questions and comments about and on section 216(h) of the FPA (16 U.S.C. 14 CFR Part 39
the rule. 824p(h)). The rule would establish an [Docket No. FAA–2016–3992; Directorate
DATES: The public workshop will be early pre-application process (the Identifier 2015–NM–075–AD]
held on March 22, 2016, beginning at Integrated Interagency Pre-application
1:00 p.m. Eastern Time. Written (IIP) process) in support of this RIN 2120–AA64
comments are welcome before or after coordination and the selection of a
the workshop and should be submitted Airworthiness Directives; The Boeing
NEPA lead agency. The proposed Company Airplanes
prior to the end of the public comment regulations provide a framework for
period for the proposed rule (April 4, DOE to facilitate early cooperation and AGENCY: Federal Aviation
2016). Administration (FAA), DOT.
exchange of environmental information
ADDRESSES: The meeting will be held required to site qualified electric ACTION: Notice of proposed rulemaking
via webinar and conference call. The transmission facilities. These activities (NPRM).
webinar invitation, phone number, and would occur prior to an applicant filing
instructions on how to register and log SUMMARY: We propose to adopt a new
a request for authorization with Federal airworthiness directive (AD) for certain
in to the webinar will be available at: permitting agencies. The proposed
http://energy.gov/oe/downloads/notice- The Boeing Company Model 787–8
regulations also provide an opportunity airplanes. This proposed AD was
proposed-rulemaking-integrated- for non-Federal agencies (tribal, state, or
interagency-pre-application-process-iip- prompted by a report that a captain’s
local governments) to coordinate seat moved uncommanded during a
electric.
separate non-Federal permitting and landing rollout due to a failure in the
You may submit comments, identified
by RIN 1901–AB36, by any of the environmental reviews with those of the seat horizontal actuator. This proposed
following methods: Federal permitting agencies. This AD would require repetitive tests of the
1. Follow the instructions for document announces the public captain and first officer seat assemblies
submitting comments on the Federal workshop described in the proposed for proper operation, and corrective
eRulemaking Portal at http:// rule. action if necessary. This proposed AD
www.regulations.gov. Members of the public are welcome to would also require installing new
2. Send email to oeregs@hq.doe.gov. pre-register for the webinar if they captain and first officer seat assemblies,
Include RIN 1901–AB36 in the subject would like to make oral statements which would terminate the repetitive
line of the email. Please include the full during the specified period for public tests. We are proposing this AD to
body of your comments in the text of the prevent a seat actuator clutch failure,
comment. To pre-register to provide
message or as an attachment. which could result in a loss of seat
public comments, please email oeregs@
3. Address postal mail to U.S. locking and uncommanded motion of
hq.doe.gov. In the email, please indicate
Department of Energy, Office of the captain’s or first officer’s seat;
your name, organization (if appropriate), uncommanded seat movement could
Electricity Delivery and Energy citizenship, and contact information. If
Reliability, Mailstop OE–20, Room 8G– result in reduced controllability of the
you would like to receive further airplane.
017, 1000 Independence Avenue SW.,
information on the proposed rule or IIP
Washington, DC 20585. DATES: We must receive comments on
Due to potential delays in the delivery process, please include your email
address in your pre-registration email. this proposed AD by April 21, 2016.
of postal mail, we encourage ADDRESSES: You may send comments,
respondents to submit comments An audio recording and written using the procedures found in 14 CFR
electronically to ensure timely receipt. transcript of the public workshop, and 11.43 and 11.45, by any of the following
This notice, a transcript of the public any comments that DOE receives during methods:
workshop, and any comments that DOE the workshop, will be made available • Federal eRulemaking Portal: Go to
receives on the proposed rulemaking after the webinar on the DOE Web site http://www.regulations.gov. Follow the
will be made available on the DOE Web at http://energy.gov/oe/downloads/ instructions for submitting comments.
site at http://energy.gov/oe/downloads/ notice-proposed-rulemaking-integrated- • Fax: 202–493–2251.
notice-proposed-rulemaking-integrated- • Mail: U.S. Department of
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interagency-pre-application-process-iip-
interagency-pre-application-process-iip- electric. You may request a hardcopy of Transportation, Docket Operations, M–
electric. You may request a hardcopy of the workshop transcript or comments be 30, West Building Ground Floor, Room
the workshop transcript or comments be sent to you via postal mail by contacting W12–140, 1200 New Jersey Avenue SE.,
sent to you via postal mail by contacting DOE’s Office of Electricity Delivery and Washington, DC 20590.
the DOE’s Office of Electricity Delivery
Energy Reliability. • Hand Delivery: Deliver to Mail
and Energy Reliability. address above between 9 a.m. and 5
FOR FURTHER INFORMATION CONTACT: Julie p.m., Monday through Friday, except
A. Smith, Ph.D., U.S. Department of Federal holidays.
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![Federal Register / Vol. 81, No. 44 / Monday, March 7, 2016 / Proposed Rules 11689
Authority for This Rulemaking § 39.13 [Amended] (i) Alternative Methods of Compliance
(AMOCs)
Title 49 of the United States Code ■ 2. The FAA amends § 39.13 by adding
specifies the FAA’s authority to issue (1) The Manager, Seattle Aircraft
the following new airworthiness Certification Office, ANM–150S, FAA, has
rules on aviation safety. Subtitle I, directive (AD): the authority to approve AMOCs for this AD,
section 106, describes the authority of The Boeing Company: Docket No. FAA– if requested using the procedures found in 14
the FAA Administrator. Subtitle VII: 2016–3992; Directorate Identifier 2015– CFR 39.19. In accordance with 14 CFR 39.19,
Aviation Programs, describes in more NM–075–AD. send your request to your principal inspector
detail the scope of the Agency’s or local Flight Standards District Office, as
authority. (a) Comments Due Date appropriate. If sending information directly
We are issuing this rulemaking under We must receive comments by April 21, to the manager of the ACO, send it to the
the authority described in Subtitle VII, 2016. attention of the person identified in
Part A, Subpart III, Section 44701: paragraph (j)(1) of this AD.
(b) Affected ADs (2) Before using any approved AMOC,
‘‘General requirements.’’ Under that notify your appropriate principal inspector,
None.
section, Congress charges the FAA with or lacking a principal inspector, the manager
promoting safe flight of civil aircraft in (c) Applicability of the local flight standards district office/
air commerce by prescribing regulations This AD applies to The Boeing Company certificate holding district office.
for practices, methods, and procedures Model 787–8 airplanes, certificated in any (3) An AMOC that provides an acceptable
the Administrator finds necessary for category, as identified in Boeing Alert level of safety may be used for any repair
safety in air commerce. This regulation Service Bulletin B787–81205–SB250054–00, required by this AD if it is approved by the
is within the scope of that authority Issue 001, dated December 19, 2014. Boeing Commercial Airplanes Organization
Designation Authorization (ODA) that has
because it addresses an unsafe condition (d) Subject been authorized by the Manager, Seattle
that is likely to exist or develop on Air Transport Association (ATA) of ACO, to make those findings. For a repair
products identified in this rulemaking America Code 25, Equipment/furnishings. method to be approved, the repair must meet
action. the certification basis of the airplane, and the
(e) Unsafe Condition approval must specifically refer to this AD.
Regulatory Findings This AD was prompted by a report that a (4) For service information that contains
We determined that this proposed AD captain’s seat moved uncommanded during a steps that are labeled as Required for
would not have federalism implications landing rollout due to a failure in the seat Compliance (RC), the provisions of
under Executive Order 13132. This horizontal actuator. We are issuing this AD paragraphs (i)(4)(i) and (i)(4)(ii) of this AD,
proposed AD would not have a to prevent a seat actuator clutch failure, apply.
which could result in a loss of seat locking (i) The steps labeled as RC, including
substantial direct effect on the States, on substeps under an RC step and any figures
and uncommanded motion of the captain’s or
the relationship between the national first officer’s seat; uncommanded seat motion identified in an RC step, must be done to
Government and the States, or on the could result in reduced controllability of the comply with the AD. An AMOC is required
distribution of power and airplane. for any deviations to RC steps, including
responsibilities among the various substeps and identified figures.
levels of government. (f) Compliance (ii) Steps not labeled as RC may be
For the reasons discussed above, I Comply with this AD within the deviated from using accepted methods in
certify this proposed regulation: compliance times specified, unless already accordance with the operator’s maintenance
(1) Is not a ‘‘significant regulatory done. or inspection program without obtaining
approval of an AMOC, provided the RC steps,
action’’ under Executive Order 12866, (g) Repetitive Tests of Captain and First including substeps and identified figures, can
(2) Is not a ‘‘significant rule’’ under Officer Seat Assembly Operation still be done as specified, and the airplane
the DOT Regulatory Policies and Within 1,000 flight hours after the effective can be put back in an airworthy condition.
Procedures (44 FR 11034, February 26, date of this AD, test the operation of the
1979), (j) Related Information
captain and first officer seat assemblies and
(3) Will not affect intrastate aviation do all applicable corrective actions, in (1) For more information about this AD,
in Alaska; and accordance with the Accomplishment contact Brandon Lucero, Aerospace Engineer,
(4) Will not have a significant Instructions of Boeing Alert Service Bulletin Cabin Safety and Environmental Systems
economic impact, positive or negative, B787–81205–SB250054–00, Issue 001, dated Branch, ANM–150S, FAA, Seattle Aircraft
December 19, 2014. Do all applicable Certification Office (ACO), 1601 Lind Avenue
on a substantial number of small entities SW., Renton, WA 98057–3356; phone: 425–
under the criteria of the Regulatory corrective actions before further flight.
Repeat the operational test thereafter at 917–6572; fax: 425–917–6590.
Flexibility Act. (2) For service information identified in
intervals not to exceed 1,000 flight hours
List of Subjects in 14 CFR Part 39 until the installation required by paragraph this AD, contact Boeing Commercial
(h) of this AD is done. Airplanes, Attention: Data & Services
Air transportation, Aircraft, Aviation Management, P.O. Box 3707, MC 2H–65,
safety, Incorporation by reference, (h) New Seat Installation Seattle, WA 98124–2207; telephone 206–
Safety. Within 72 months after the effective date 544–5000, extension 1; fax 206–766–5680;
of this AD, do the actions specified in Internet https://www.myboeingfleet.com. You
The Proposed Amendment paragraphs (h)(1) and (h)(2) of this AD, in may view this service information at the
Accordingly, under the authority accordance with the Accomplishment FAA, Transport Airplane Directorate, 1601
Instructions of Boeing Alert Service Bulletin Lind Avenue SW., Renton, WA. For
delegated to me by the Administrator,
B787–81205–SB250054–00, Issue 001, dated information on the availability of this
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the FAA proposes to amend 14 CFR part material at the FAA, call 425–227–1221.
39 as follows: December 19, 2014. Installing the seat
specified in paragraph (h)(1) or (h)(2) of this Issued in Renton, Washington, on February
PART 39—AIRWORTHINESS AD is terminating action for the repetitive 23, 2016.
operational tests required by paragraph (g) of Dionne Palermo,
DIRECTIVES this AD for that seat only.
Acting Manager, Transport Airplane
(1) Install new captain seat assembly, part
■ 1. The authority citation for part 39 Directorate, Aircraft Certification Service.
number (P/N) 3A380–0007–01–7.
continues to read as follows: (2) Install new first officer seat assembly, [FR Doc. 2016–04679 Filed 3–4–16; 8:45 am]
Authority: 49 U.S.C. 106(g), 40113, 44701. P/N 3A380–0008–01–7. BILLING CODE 4910–13–P
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Document Created: 2018-02-02 15:08:02
Document Modified: 2018-02-02 15:08:02
| 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 April 21, 2016. | |
| Contact | Brandon Lucero, Aerospace Engineer, Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917-6572; fax: 425-917-6590. | |
| FR Citation | 81 FR 11687 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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