80 FR 52939 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 80, Issue 170 (September 2, 2015)
Federal Aviation Administration
Federal Register Volume 80, Issue 170 (September 2, 2015)
| Page Range | 52939-52941 | |
| FR Document | 2015-21474 |
[Federal Register Volume 80, Number 170 (Wednesday, September 2, 2015)] [Rules and Regulations] [Pages 52939-52941] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-21474] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2014-0777; Directorate Identifier 2014-NM-088-AD; Amendment 39-18257; AD 2015-17-24] RIN 2120-AA64 Airworthiness Directives; The Boeing Company Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 787-8 airplanes. This AD was prompted by numerous reports of failures of the proximity sensor within the slat skew detection mechanism assembly (DMA) leading to slats up landing events. This AD requires replacing the slat skew DMAs with new slat skew DMAs, and marking the existing identification plates on the slat with the new part number. We are issuing this AD to prevent failure of the proximity sensor, which could result in the slats being shut down and a slats up high speed landing. This condition, in combination with abnormal landing conditions such as a short runway or adverse weather conditions, could result in a runway excursion. DATES: This AD is effective October 7, 2015. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of October 7, 2015. ADDRESSES: 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. It is also available on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014- 0777. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014- 0777; 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: Douglas Tsuji, Senior Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone: 425-917-6546; 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 certain The Boeing Company [[Page 52940]] Model 787-8 airplanes. The NPRM published in the Federal Register on November 28, 2014 (79 FR 70802). The NPRM was prompted by numerous reports of failures of the proximity sensor within the slat skew DMA leading to slats up landing events. The NPRM proposed to require replacing the slat skew DMAs with new slat skew DMAs, and marking the existing identification plates on the slat with the new part number. We are issuing this AD to prevent failure of the proximity sensor, which could result in the slats being shut down and a slats up high speed landing. This condition, in combination with abnormal landing conditions such as a short runway or adverse weather conditions, could result in a runway excursion. Comments We gave the public the opportunity to participate in developing this AD. The following presents the comments received on the NPRM (79 FR 70802, November 28, 2014) and the FAA's response to each comment. Support for the NPRM (79 FR 70802, November 28, 2014) United Airlines (UAL) stated that it supports the NPRM (79 FR 70802, November 28, 2014). Requests To Correct the Location of the Part Numbers Affected Boeing and UAL requested a correction of the location of the identified part numbers affected in paragraphs (h)(2) and (h)(3) of the proposed AD (79 FR 70802, November 28, 2014). UAL stated that the part numbers affected in paragraphs (h)(2) and (h)(3) of the proposed AD are the wing leading edge slat assemblies, not the DMA. Boeing also commented that the part numbers are for a complete slat assembly (structure with DMA installed) and not just the DMA. We agree with the request. The intent of this AD is to prohibit installation of a defective slat skew DMA. Boeing Alert Service Bulletin B787-81205-SB270021-00, Issue 001, dated March 20, 2014, provides instructions to modify the existing slat assembly by replacing the defective slat skew DMA and then marking the existing slat assembly identification plate with a new part number. Therefore, we have revised paragraphs (h)(2) and (h)(3) of this AD to remove the text ``slat skew DMA in'' and just refer to the existing part numbers of the slat assembly, which contain the defective slat skew DMA. 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:Are consistent with the intent that was proposed in the NPRM (79 FR 70802, November 28, 2014) for correcting the unsafe condition; and Do not add any additional burden upon the public than was already proposed in the NPRM (79 FR 70802, November 28, 2014). 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 We reviewed Boeing Alert Service Bulletin B787-81205-SB270021-00, Issue 001, dated March 20, 2014. The service information describes procedures for replacing the slat skew DMAs with new slat skew DMAs, and marking the existing identification plates on the slat with the new part number. 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. Costs of Compliance We estimate that this AD affects 15 airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Replacement....................... 11 work-hours X $85 per $0 $935 $14,025 hour = $935. ---------------------------------------------------------------------------------------------------------------- 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, (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: [[Page 52941]] 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): 2015-17-24 The Boeing Company: Amendment 39-18257 ; Docket No. FAA- 2014-0777; Directorate Identifier 2014-NM-088-AD. (a) Effective Date This AD is effective October 7, 2015. (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-SB270021-00, Issue 001, dated March 20, 2014. (d) Subject Air Transport Association (ATA) of America Code 27, Flight Controls. (e) Unsafe Condition This AD was prompted by numerous reports of failures of the proximity sensor within the slat skew detection mechanism assembly (DMA) leading to slats up landing events. We are issuing this AD to prevent failure of the proximity sensor, which could result in the slats being shut down and a slats up high speed landing. This condition, in combination with abnormal landing conditions such as a short runway or adverse weather conditions, could result in a runway excursion. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Replacement Within 24 months after the effective date of this AD: Replace the slat skew DMAs in slat number 5 and slat number 8 with new slat skew DMAs, and mark the existing identification plates on the slat with the new part number, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin B787-81205-SB270021- 00, Issue 001, dated March 20, 2014. (h) Parts Installation Prohibitions (1) As of the effective date of this AD, no person may install a slat skew DMA, part number P683A0001-03, on any airplane. (2) As of the effective date of this AD, no person may install on any airplane, a slat assembly number 5, having part number 145Z0201-11-8, 145Z0201-21-4, 145Z0201-21-3, 145Z0201-21-5, 145Z0201-21-8, 145Z0201-21-9, 145Z0201-31-1, or 145Z0201-33-1. (3) As of the effective date of this AD, no person may install on any airplane, a slat assembly number 8, having part number 145Z0201-12-8, 145Z0201-22-4, 145Z0201-22-3, 145Z0201-22-5, 145Z0201-22-8, 145Z0201-22-9, 145Z0201-32-1, or 145Z0201-34-1. (i) 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 (j) 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. (j) Related Information For more information about this AD, contact Douglas Tsuji, Senior Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone: 425-917-6546; fax: 425-917-6590; email: [email protected]. (k) 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 B787-81205-SB270021-00, Issue 001, dated March 20, 2014. (ii) Reserved. (3) For Boeing 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 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. (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 August 21, 2015. Kevin Hull, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2015-21474 Filed 9-1-15; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 80, No. 170 / Wednesday, September 2, 2015 / Rules and Regulations 52939
Bombardier Service Bulletin 84–32–118, (l) Material Incorporated by Reference number. We are issuing this AD to
dated April 8, 2014. (1) The Director of the Federal Register prevent failure of the proximity sensor,
Note 1 to paragraph (g) of this AD: Re- approved the incorporation by reference which could result in the slats being
installing the hand pump lever of the parking (IBR) of the service information listed in this shut down and a slats up high speed
brake to the right-hand side equipment bay paragraph under 5 U.S.C. 552(a) and 1 CFR landing. This condition, in combination
(Bombardier ModSum 4–113804) may be part 51. with abnormal landing conditions such
done at the operator’s discretion. (2) You must use this service information
as a short runway or adverse weather
as applicable to do the actions required by
(h) Optional Installation this AD, unless this AD specifies otherwise. conditions, could result in a runway
Incorporation of ModSum 4–113723 by re- (i) Bombardier Service Bulletin 84–32–99, excursion.
locating the hand pump lever of the parking Revision A, dated October 2, 2012. DATES: This AD is effective October 7,
brake from the right-hand side nacelle to the (ii) Bombardier Service Bulletin 84–32– 2015.
right-hand side equipment bay, in 118, dated April 8, 2014. The Director of the Federal Register
accordance with the Accomplishment (3) For service information identified in approved the incorporation by reference
Instructions of Bombardier Service Bulletin this AD, contact Bombardier, Inc., Q-Series
Technical Help Desk, 123 Garratt Boulevard,
of a certain publication listed in this AD
84–32–99, Revision A, dated October 2, 2012,
Toronto, Ontario M3K 1Y5, Canada; as of October 7, 2015.
is acceptable for compliance with the
modification specified in paragraph (g) of telephone 416–375–4000; fax 416–375–4539; ADDRESSES: For service information
this AD, provided the incorporation of email thd.qseries@aero.bombardier.com; identified in this AD, contact Boeing
ModSum 4–113723 is done within the Internet http://www.bombardier.com. Commercial Airplanes, Attention: Data
compliance time specified in paragraph (g) of (4) You may view this service information & Services Management, P.O. Box 3707,
this AD. at the FAA, Transport Airplane Directorate, MC 2H–65, Seattle, WA 98124–2207;
1601 Lind Avenue SW., Renton, WA. For telephone 206–544–5000, extension 1;
(i) Credit for Previous Actions information on the availability of this
material at the FAA, call 425–227–1221.
fax 206–766–5680; Internet https://
This paragraph provides credit for actions
(5) You may view this service information www.myboeingfleet.com. You may view
required by paragraph (h) of this AD, if those
actions were performed before the effective that is incorporated by reference at the this referenced service information at
date of this AD using Bombardier Service National Archives and Records the FAA, Transport Airplane
Bulletin 84–32–99, dated January 26, 2012, Administration (NARA). For information on Directorate, 1601 Lind Avenue SW.,
which is not incorporated by reference in this the availability of this material at NARA, call Renton, WA. For information on the
AD. 202–741–6030, or go to: http:// availability of this material at the FAA,
www.archives.gov/federal-register/cfr/ibr- call 425–227–1221. It is also available
(j) Other FAA AD Provisions locations.html. on the Internet at http://
The following provisions also apply to this Issued in Renton, Washington, on August www.regulations.gov by searching for
AD: 10, 2015.
(1) Alternative Methods of Compliance
and locating Docket No. FAA–2014–
Michael Kaszycki, 0777.
(AMOCs): The Manager, New York Aircraft
Certification Office (ACO), ANE–170, FAA, Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
Examining the AD Docket
has the authority to approve AMOCs for this
AD, if requested using the procedures found [FR Doc. 2015–20583 Filed 9–1–15; 8:45 am] You may examine the AD docket on
in 14 CFR 39.19. In accordance with 14 CFR BILLING CODE 4910–13–P
the Internet at http://
39.19, send your request to your principal www.regulations.gov by searching for
inspector or local Flight Standards District and locating Docket No. FAA–2014–
Office, as appropriate. If sending information DEPARTMENT OF TRANSPORTATION 0777; or in person at the Docket
directly to the ACO, send it to ATTN: Management Facility between 9 a.m.
Program Manager, Continuing Operational Federal Aviation Administration and 5 p.m., Monday through Friday,
Safety, FAA, New York ACO, 1600 Stewart except Federal holidays. The AD docket
Avenue, Suite 410, Westbury, NY 11590;
14 CFR Part 39 contains this AD, the regulatory
telephone 516–228–7300; fax 516–794–5531.
Before using any approved AMOC, notify [Docket No. FAA–2014–0777; Directorate
evaluation, any comments received, and
your appropriate principal inspector, or Identifier 2014–NM–088–AD; Amendment other information. The address for the
lacking a principal inspector, the manager of 39–18257; AD 2015–17–24] Docket Office (phone: 800–647–5527) is
the local flight standards district office/ Docket Management Facility, U.S.
certificate holding district office. The AMOC RIN 2120–AA64 Department of Transportation, Docket
approval letter must specifically reference Operations, M–30, West Building
this AD. Airworthiness Directives; The Boeing
Ground Floor, Room W12–140, 1200
(2) Contacting the Manufacturer: For any Company Airplanes
New Jersey Avenue SE., Washington,
requirement in this AD to obtain corrective DC 20590.
AGENCY: Federal Aviation
actions from a manufacturer, the action must
be accomplished using a method approved Administration (FAA), DOT. FOR FURTHER INFORMATION CONTACT:
by the Manager, New York ACO, ANE–170, ACTION: Final rule. Douglas Tsuji, Senior Aerospace
FAA; or Transport Canada Civil Aviation Engineer, Systems and Equipment
(TCCA); or Bombardier, Inc.’s TCCA Design SUMMARY: We are adopting a new Branch, ANM–130S, FAA, Seattle
Approval Organization (DAO). If approved by airworthiness directive (AD) for certain Aircraft Certification Office, 1601 Lind
the DAO, the approval must include the The Boeing Company Model 787–8 Avenue SW., Renton, WA 98057–3356;
DAO-authorized signature. airplanes. This AD was prompted by telephone: 425–917–6546; fax: 425–
asabaliauskas on DSK5VPTVN1PROD with RULES
(k) Related Information numerous reports of failures of the 917–6590; email: douglas.tsuji@faa.gov.
proximity sensor within the slat skew SUPPLEMENTARY INFORMATION:
Refer to Mandatory Continuing
Airworthiness Information (MCAI) Canadian
detection mechanism assembly (DMA)
leading to slats up landing events. This Discussion
Airworthiness Directive CF–2014–18, dated
June 19, 2014, for related information. This AD requires replacing the slat skew We issued a notice of proposed
MCAI may be found in the AD docket on the DMAs with new slat skew DMAs, and rulemaking (NPRM) to amend 14 CFR
Internet at http://www.regulations.gov/ marking the existing identification part 39 by adding an AD that would
#!documentDetail;D=FAA-2015-0680-0002. plates on the slat with the new part apply to certain The Boeing Company
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![Federal Register / Vol. 80, No. 170 / Wednesday, September 2, 2015 / Rules and Regulations 52941
PART 39—AIRWORTHINESS assembly number 8, having part number Issued in Renton, Washington, on August
DIRECTIVES 145Z0201–12–8, 145Z0201–22–4, 145Z0201– 21, 2015.
22–3, 145Z0201–22–5, 145Z0201–22–8, Kevin Hull,
■ 1. The authority citation for part 39 145Z0201–22–9, 145Z0201–32–1, or Acting Manager, Transport Airplane
continues to read as follows: 145Z0201–34-1. Directorate, Aircraft Certification Service.
Authority: 49 U.S.C. 106(g), 40113, 44701. (i) Alternative Methods of Compliance [FR Doc. 2015–21474 Filed 9–1–15; 8:45 am]
(AMOCs) BILLING CODE 4910–13–P
§ 39.13 [Amended]
(1) The Manager, Seattle Aircraft
■ 2. The FAA amends § 39.13 by adding Certification Office (ACO), FAA, has the
the following new airworthiness authority to approve AMOCs for this AD, if
DEPARTMENT OF TRANSPORTATION
directive (AD): requested using the procedures found in 14
Federal Aviation Administration
2015–17–24 The Boeing Company: CFR 39.19. In accordance with 14 CFR 39.19,
Amendment 39–18257 ; Docket No. send your request to your principal inspector
FAA–2014–0777; Directorate Identifier 14 CFR Part 39
or local Flight Standards District Office, as
2014–NM–088–AD. appropriate. If sending information directly [Docket No. FAA–2014–0779; Directorate
(a) Effective Date to the manager of the ACO, send it to the Identifier 2014–NM–052–AD; Amendment
attention of the person identified in 39–18260; AD 2015–18–02]
This AD is effective October 7, 2015.
paragraph (j) of this AD. Information may be RIN 2120–AA64
(b) Affected ADs emailed to: 9-ANM-Seattle-ACO-AMOC-
None. Requests@faa.gov. Airworthiness Directives; Lockheed
(2) Before using any approved AMOC, Martin Corporation/Lockheed Martin
(c) Applicability
notify your appropriate principal inspector, Aeronautics Company Airplanes
This AD applies to The Boeing Company or lacking a principal inspector, the manager
Model 787–8 airplanes, certificated in any AGENCY: Federal Aviation
of the local flight standards district office/
category, as identified in Boeing Alert
Service Bulletin B787–81205–SB270021–00, certificate holding district office. Administration (FAA), DOT.
Issue 001, dated March 20, 2014. (j) Related Information ACTION: Final rule; request for
(d) Subject
comments.
For more information about this AD,
Air Transport Association (ATA) of contact Douglas Tsuji, Senior Aerospace SUMMARY: We are adopting a new
America Code 27, Flight Controls. Engineer, Systems and Equipment Branch, airworthiness directive (AD) for all
ANM–130S, FAA, Seattle Aircraft Lockheed Martin Corporation/Lockheed
(e) Unsafe Condition
Certification Office, 1601 Lind Avenue SW., Martin Aeronautics Company Model
This AD was prompted by numerous Renton, WA 98057–3356; telephone: 425–
reports of failures of the proximity sensor 382, 382B, 382E, 382F, and 382G
917–6546; fax: 425–917–6590; email: airplanes. This AD requires replacing
within the slat skew detection mechanism
assembly (DMA) leading to slats up landing douglas.tsuji@faa.gov. the center wing box (CWB) and certain
events. We are issuing this AD to prevent (k) Material Incorporated by Reference outer wings. This AD was prompted by
failure of the proximity sensor, which could an evaluation by the design approval
result in the slats being shut down and a slats (1) The Director of the Federal Register
approved the incorporation by reference holder (DAH) indicating that the CWB
up high speed landing. This condition, in
combination with abnormal landing (IBR) of the service information listed in this and outer wings are subject to
conditions such as a short runway or adverse paragraph under 5 U.S.C. 552(a) and 1 CFR widespread fatigue damage (WFD). We
weather conditions, could result in a runway part 51. are issuing this AD to prevent fatigue
excursion. (2) You must use this service information cracking of the outer wings and the
(f) Compliance as applicable to do the actions required by lower surface of the CWB, which could
this AD, unless the AD specifies otherwise. result in reduced structural integrity of
Comply with this AD within the
compliance times specified, unless already (i) Boeing Alert Service Bulletin B787– the airplane.
done. 81205–SB270021–00, Issue 001, dated March DATES: This AD is effective September
20, 2014. 17, 2015.
(g) Replacement (ii) Reserved. The Director of the Federal Register
Within 24 months after the effective date (3) For Boeing service information approved the incorporation by reference
of this AD: Replace the slat skew DMAs in identified in this AD, contact Boeing of certain publications listed in this AD
slat number 5 and slat number 8 with new Commercial Airplanes, Attention: Data &
slat skew DMAs, and mark the existing as of September 17, 2015.
Services Management, P.O. Box 3707, MC We must receive comments on this
identification plates on the slat with the new
2H–65, Seattle, WA 98124–2207; telephone AD by October 19, 2015.
part number, in accordance with the
206–544–5000, extension 1; fax 206–766–
Accomplishment Instructions of Boeing Alert ADDRESSES: You may send comments,
Service Bulletin B787–81205–SB270021–00, 5680; Internet https://
www.myboeingfleet.com. using the procedures found in 14 CFR
Issue 001, dated March 20, 2014. 11.43 and 11.45, by any of the following
(4) You may view this referenced service
(h) Parts Installation Prohibitions information at the FAA, Transport Airplane methods:
(1) As of the effective date of this AD, no Directorate, 1601 Lind Avenue SW., Renton, • Federal eRulemaking Portal: Go to
person may install a slat skew DMA, part WA. For information on the availability of http://www.regulations.gov. Follow the
number P683A0001–03, on any airplane. this material at the FAA, call 425–227–1221. instructions for submitting comments.
asabaliauskas on DSK5VPTVN1PROD with RULES
(2) As of the effective date of this AD, no (5) You may view this service information • Fax: 202–493–2251.
person may install on any airplane, a slat
that is incorporated by reference at the • Mail: U.S. Department of
assembly number 5, having part number Transportation, Docket Operations, M–
National Archives and Records
145Z0201–11–8, 145Z0201–21–4, 145Z0201–
21–3, 145Z0201–21–5, 145Z0201–21–8, Administration (NARA). For information on 30, West Building Ground Floor, Room
145Z0201–21–9, 145Z0201–31-1, or the availability of this material at NARA, call W12–140, 1200 New Jersey Avenue SE.,
145Z0201–33-1. 202–741–6030, or go to: http:// Washington, DC 20590.
(3) As of the effective date of this AD, no www.archives.gov/federal-register/cfr/ibr- • Hand Delivery: U.S. Department of
person may install on any airplane, a slat locations.html. Transportation, Docket Operations, M–
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Document Created: 2018-02-26 10:10:58
Document Modified: 2018-02-26 10:10:58
| 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 | Rules and Regulations | |
| Action | Final rule. | |
| Dates | This AD is effective October 7, 2015. | |
| Contact | Douglas Tsuji, Senior Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone: 425-917-6546; fax: 425-917-6590; email: [email protected] | |
| FR Citation | 80 FR 52939 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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