81 FR 36452 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 109 (June 7, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 109 (June 7, 2016)
| Page Range | 36452-36454 | |
| FR Document | 2016-12842 |
[Federal Register Volume 81, Number 109 (Tuesday, June 7, 2016)] [Rules and Regulations] [Pages 36452-36454] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-12842] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-3987; Directorate Identifier 2015-NM-066-AD; Amendment 39-18544; AD 2016-11-17] 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 a report of wire chafing caused by a left wing spoiler actuator wire not having enough separation from a certain bracket when the spoiler is in the deployed position. This AD requires measuring the separation between a certain electro-mechanical actuator wire of the left wing, spoiler 4, and the support bracket of the flap variable camber trim unit; and related investigative and corrective actions if necessary. We are issuing this AD to detect and correct wire chafing. Such chafing could result in an electrical short and potential fire in a flammable fluid leakage zone and possible loss of several functions essential for safe flight. DATES: This AD is effective July 12, 2016. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of July 12, 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. It is also available on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015- 3987. 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- 3987; 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: Sean J. Schauer, Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057- 3356; phone: 425-917-6479; fax: 425-917-6590; email: sean.schauer@faa.gov. 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 Model 787-8 airplanes. The NPRM published in the Federal Register on October 19, 2015 (80 FR 63132) (``the NPRM''). The NPRM was prompted by a report of insufficient clearance and wire chafing between the wiring to the number 4 spoiler electro-mechanical actuator and a bracket of the flap variable camber trim unit with the spoiler fully deployed. The NPRM proposed to require measuring the separation between a certain electro-mechanical actuator wire of the left wing, spoiler 4, and the support bracket of the flap variable camber trim unit, and related investigative and corrective actions if necessary. We are issuing this AD to detect and correct wire chafing. Such chafing could result in an electrical short and potential fire in a flammable fluid leakage zone and possible loss of several functions essential for safe flight. Comments We gave the public the opportunity to participate in developing this AD. The following presents the comments received on the NPRM and the FAA's response to each comment. Support for the NPRM United Airlines stated that it agrees with the NPRM, has completed the actions specified in Boeing Alert Service Bulletin B787-81205- SB270024-00, Issue 001, dated September 24, 2014, and has no technical findings/issues to report. [[Page 36453]] We acknowledge United Airlines' comment. An anonymous commenter stated that it is in the airplane manufacturer's best interest to address the faulty wire as soon as possible as this safety issue may have an impact on profits because of the impact to the company's image. We agree with the commenter in so much as the identified unsafe condition needs to be addressed on the affected airplanes. No change to this final rule was requested. Request To Clarify the Issue That Prompted the NPRM Boeing requested that we revise the Discussion section of the NPRM to clarify that the safety issue was prompted by a report of wire chafing caused by insufficient clearance between the wiring to the number 4 spoiler electro-mechanical actuator and a bracket of the flap variable camber trim unit with the spoiler fully deployed. We agree with Boeing's statement regarding the action that prompted this AD. We have revised the Discussion section of this final rule accordingly. Conclusion We reviewed the relevant data, considered the comments received, and determined that air safety and the public interest require adopting this AD as proposed, except for minor editorial changes. We have determined that these minor changes:Are consistent with the intent that was proposed in the NPRM for correcting the unsafe condition; and Do not add any additional burden upon the public than was already proposed in the NPRM. Related Service Information Under 1 CFR Part 51 We reviewed Boeing Alert Service Bulletin B787-81205-SB270024-00, Issue 001, dated September 24, 2014. The service information describes procedures for accomplishing the following actions. Measuring the separation between the electro-mechanical actuator wire W801182 of the left wing, spoiler 4, and the support bracket of the flap variable camber trim unit. Related investigative actions and corrective actions such as doing a general visual inspection for chafing of the electro- mechanical actuator wire W801182 of the left wing, spoiler 4; adjusting the electro-mechanical actuator wire W801182 of the left wing, spoiler 4; and replacing the electro-mechanical actuator wire W801182 of the left wing, spoiler 4. 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 12 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 product operators ---------------------------------------------------------------------------------------------------------------- Measurement............................... 6 work-hours x $85 per hour = $510 $510 $6,120 ---------------------------------------------------------------------------------------------------------------- We estimate the following costs to do any necessary replacements that would be required based on the results of the inspection. We have no way of determining the number of aircraft that might need this replacement: On-Condition Costs ---------------------------------------------------------------------------------------------------------------- Cost per Action Labor cost Parts cost product ---------------------------------------------------------------------------------------------------------------- Related investigative and corrective 2 work-hours x $85 per hour = $170 $24 $194 actions. ---------------------------------------------------------------------------------------------------------------- According to the manufacturer, all 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 the 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, (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. [[Page 36454]] 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): 2016-11-17 The Boeing Company: Amendment 39-18544 ; Docket No. FAA- 2015-3987; Directorate Identifier 2015-NM-066-AD. (a) Effective Date This AD is effective July 12, 2016. (b) Affected ADs None. (c) Applicability This AD applies to certain The Boeing Company Model 787-8 airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin B787-81205-SB270024-00, Issue 001, dated September 24, 2014. (d) Subject Air Transport Association (ATA) of America Code 24, Electrical power. (e) Unsafe Condition This AD was prompted by a report of wire chafing caused by a left wing spoiler actuator wire not having enough separation from a certain bracket when the spoiler is in the deployed position. We are issuing this AD to detect and correct wire chafing; such chafing could result in an electrical short and potential fire in a flammable fluid leakage zone and possible loss of several functions essential for safe flight. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Wire Separation Measurement, Related Investigative Actions, and Corrective Actions Within 24 months after the effective date of this AD: Measure the separation between the electro-mechanical actuator wire W801182 of the left wing, spoiler 4, and the support bracket of the flap variable camber trim unit, and do all applicable related investigative and corrective actions, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin B787- 81205-SB270024-00, Issue 001, dated September 24, 2014. Do all applicable related investigative and corrective actions before further flight. (h) 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 (i) of this AD. Information may be emailed to: 9-ANM-Seattle-ACO-AMOC-Requests@faa.gov. (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. (i) Related Information For more information about this AD, contact Sean J. Schauer, Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle ACO, 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917-6479; fax: 425-917-6590; email: sean.schauer@faa.gov. (j) 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-SB270024-00, Issue 001, dated September 24, 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 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 May 20, 2016. Victor Wicklund, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-12842 Filed 6-6-16; 8:45 am] BILLING CODE 4910-13-P
![36452 Federal Register / Vol. 81, No. 109 / Tuesday, June 7, 2016 / Rules and Regulations
approval of an AMOC, provided the RC steps, DEPARTMENT OF TRANSPORTATION and locating Docket No. FAA–2015–
including substeps and identified figures, can 3987; or in person at the Docket
still be done as specified, and the airplane Federal Aviation Administration Management Facility between 9 a.m.
can be put back in an airworthy condition. and 5 p.m., Monday through Friday,
(l) Related Information
14 CFR Part 39 except Federal holidays. The AD docket
[Docket No. FAA–2015–3987; Directorate contains this AD, the regulatory
(1) For more information about this AD, evaluation, any comments received, and
contact Kevin Nguyen, Aerospace Engineer, Identifier 2015–NM–066–AD; Amendment
39–18544; AD 2016–11–17] other information. The address for the
Propulsion Branch, ANM–140S, FAA, Seattle Docket Office (phone: 800–647–5527) is
ACO, 1601 Lind Avenue SW., Renton, WA RIN 2120–AA64 Docket Management Facility, U.S.
98057–3356; phone: 425–917–6501; fax: 425– Department of Transportation, Docket
917–6590; email: kevin.nguyen@faa.gov. Airworthiness Directives; The Boeing
Operations, M–30, West Building
(2) Service information identified in this Company Airplanes
Ground Floor, Room W12–140, 1200
AD that is not incorporated by reference is
AGENCY: Federal Aviation New Jersey Avenue SE., Washington,
available at the addresses specified in
Administration (FAA), DOT. DC 20590.
paragraphs (m)(3) and (m)(4) of this AD.
ACTION: Final rule. FOR FURTHER INFORMATION CONTACT:
(m) Material Incorporated by Reference Sean J. Schauer, Aerospace Engineer,
(1) The Director of the Federal Register SUMMARY: We are adopting a new Systems and Equipment Branch, ANM–
approved the incorporation by reference airworthiness directive (AD) for certain 130S, FAA, Seattle Aircraft Certification
(IBR) of the service information listed in this The Boeing Company Model 787–8 Office (ACO), 1601 Lind Avenue SW.,
paragraph under 5 U.S.C. 552(a) and 1 CFR airplanes. This AD was prompted by a Renton, WA 98057–3356; phone: 425–
part 51. report of wire chafing caused by a left 917–6479; fax: 425–917–6590; email:
(2) You must use this service information wing spoiler actuator wire not having sean.schauer@faa.gov.
as applicable to do the actions required by enough separation from a certain SUPPLEMENTARY INFORMATION:
this AD, unless the AD specifies otherwise. bracket when the spoiler is in the
deployed position. This AD requires Discussion
(i) Boeing Special Attention Service
Bulletin 777–54–0028, Revision 1, dated measuring the separation between a We issued a notice of proposed
December 10, 2013. certain electro-mechanical actuator wire rulemaking (NPRM) to amend 14 CFR
(ii) Boeing Special Attention Service of the left wing, spoiler 4, and the part 39 by adding an AD that would
Bulletin 777–71–0055, Revision 1, dated support bracket of the flap variable apply to certain The Boeing Company
April 15, 2015. camber trim unit; and related Model 787–8 airplanes. The NPRM
(iii) Airworthiness Limitation 54–AWL–01, investigative and corrective actions if published in the Federal Register on
‘‘Forward Strut Drain Line,’’ as specified in necessary. We are issuing this AD to October 19, 2015 (80 FR 63132) (‘‘the
Section D.4, Pratt and Whitney Forward Strut detect and correct wire chafing. Such NPRM’’). The NPRM was prompted by
Drain Line, dated March 2014, of the Boeing chafing could result in an electrical a report of insufficient clearance and
777 Maintenance Planning Data Document short and potential fire in a flammable wire chafing between the wiring to the
Section 9, Airworthiness Limitations and fluid leakage zone and possible loss of number 4 spoiler electro-mechanical
Certification Maintenance Requirements, several functions essential for safe actuator and a bracket of the flap
D622W001–9, dated October 2014. flight. variable camber trim unit with the
(3) For Boeing service information spoiler fully deployed. The NPRM
DATES: This AD is effective July 12,
identified in this AD, contact Boeing proposed to require measuring the
2016.
Commercial Airplanes, Attention: Data & separation between a certain electro-
The Director of the Federal Register
Services Management, P.O. Box 3707, MC mechanical actuator wire of the left
approved the incorporation by reference
2H–65, Seattle, WA 98124–2207; telephone wing, spoiler 4, and the support bracket
of a certain publication listed in this AD
206–544–5000, extension 1; fax 206–766– of the flap variable camber trim unit,
as of July 12, 2016.
5680; Internet https:// and related investigative and corrective
www.myboeingfleet.com. ADDRESSES: For service information actions if necessary. We are issuing this
(4) You may view this service information identified in this final rule, contact AD to detect and correct wire chafing.
at the FAA, Transport Airplane Directorate, Boeing Commercial Airplanes, Such chafing could result in an
1601 Lind Avenue SW., Renton, WA. For Attention: Data & Services Management, electrical short and potential fire in a
information on the availability of this P.O. Box 3707, MC 2H–65, Seattle, WA flammable fluid leakage zone and
material at the FAA, call 425–227–1221. 98124–2207; telephone 206–544–5000, possible loss of several functions
(5) You may view this service information extension 1; fax 206–766–5680; Internet essential for safe flight.
that is incorporated by reference at the https://www.myboeingfleet.com. You
National Archives and Records may view this referenced service Comments
Administration (NARA). For information on information at the FAA, Transport We gave the public the opportunity to
the availability of this material at NARA, call Airplane Directorate, 1601 Lind Avenue participate in developing this AD. The
202–741–6030, or go to: http:// SW., Renton, WA. For information on following presents the comments
www.archives.gov/federal-register/cfr/ibr- the availability of this material at the received on the NPRM and the FAA’s
locations.html. FAA, call 425–227–1221. It is also response to each comment.
Issued in Renton, Washington, on May 20, available on the Internet at http://
www.regulations.gov by searching for Support for the NPRM
2016.
jstallworth on DSK7TPTVN1PROD with RULES
and locating Docket No. FAA–2015– United Airlines stated that it agrees
Victor Wicklund, with the NPRM, has completed the
3987.
Acting Manager, Transport Airplane actions specified in Boeing Alert Service
Directorate, Aircraft Certification Service. Examining the AD Docket Bulletin B787–81205–SB270024–00,
[FR Doc. 2016–12599 Filed 6–6–16; 8:45 am] You may examine the AD docket on Issue 001, dated September 24, 2014,
BILLING CODE 4910–13–P the Internet at http:// and has no technical findings/issues to
www.regulations.gov by searching for report.
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![36454 Federal Register / Vol. 81, No. 109 / Tuesday, June 7, 2016 / Rules and Regulations
Adoption of the Amendment (h) Alternative Methods of Compliance Issued in Renton, Washington, on May 20,
(AMOCs) 2016.
Accordingly, under the authority (1) The Manager, Seattle Aircraft Victor Wicklund,
delegated to me by the Administrator, Certification Office (ACO), FAA, has the Acting Manager, Transport Airplane
the FAA amends 14 CFR part 39 as authority to approve AMOCs for this AD, if Directorate, Aircraft Certification Service.
follows: requested using the procedures found in 14 [FR Doc. 2016–12842 Filed 6–6–16; 8:45 am]
CFR 39.19. In accordance with 14 CFR 39.19, BILLING CODE 4910–13–P
PART 39—AIRWORTHINESS send your request to your principal inspector
DIRECTIVES or local Flight Standards District Office, as
appropriate. If sending information directly
to the manager of the ACO, send it to the DEPARTMENT OF COMMERCE
■ 1. The authority citation for part 39
continues to read as follows: attention of the person identified in
paragraph (i) of this AD. Information may be Office of the Secretary
Authority: 49 U.S.C. 106(g), 40113, 44701. emailed to: 9-ANM-Seattle-ACO-AMOC-
Requests@faa.gov. 15 CFR Part 6
§ 39.13 [Amended]
(2) Before using any approved AMOC, [Docket No. 160523449–6449–01]
■ 2. The FAA amends § 39.13 by adding notify your appropriate principal inspector,
or lacking a principal inspector, the manager RIN 0605–AA44
the following new airworthiness
of the local flight standards district office/
directive (AD): certificate holding district office. Civil Monetary Penalty Adjustments for
2016–11–17 The Boeing Company: (3) An AMOC that provides an acceptable Inflation
Amendment 39–18544 ; Docket No. level of safety may be used for any repair
FAA–2015–3987; Directorate Identifier required by this AD if it is approved by the AGENCY: Office of the Chief Financial
2015–NM–066–AD. Boeing Commercial Airplanes Organization Officer and Assistant Secretary for
Designation Authorization (ODA) that has Administration, Department of
(a) Effective Date
been authorized by the Manager, Seattle Commerce.
This AD is effective July 12, 2016. ACO, to make those findings. For a repair ACTION: Interim final rule with request
(b) Affected ADs method to be approved, the repair must meet for comments.
the certification basis of the airplane, and the
None. approval must specifically refer to this AD. SUMMARY: This interim final rule is
(c) Applicability (i) Related Information being issued to adjust for inflation each
This AD applies to certain The Boeing For more information about this AD, civil monetary penalty (CMP) provided
Company Model 787–8 airplanes, certificated contact Sean J. Schauer, Aerospace Engineer, by law within the jurisdiction of the
in any category, as identified in Boeing Alert Systems and Equipment Branch, ANM–130S, Department of Commerce (Commerce
Service Bulletin B787–81205–SB270024–00, FAA, Seattle ACO, 1601 Lind Avenue SW., Department). The Federal Civil
Issue 001, dated September 24, 2014. Renton, WA 98057–3356; phone: 425–917– Penalties Inflation Adjustment Act of
(d) Subject 6479; fax: 425–917–6590; email: 1990, as amended by the Debt
sean.schauer@faa.gov. Collection Improvement Act of 1996
Air Transport Association (ATA) of
America Code 24, Electrical power. (j) Material Incorporated by Reference and the Federal Civil Penalties Inflation
Adjustment Act Improvements Act of
(e) Unsafe Condition (1) The Director of the Federal Register
2015, requires the head of each agency
approved the incorporation by reference
This AD was prompted by a report of wire (IBR) of the service information listed in this to adjust for inflation its CMP levels in
chafing caused by a left wing spoiler actuator paragraph under 5 U.S.C. 552(a) and 1 CFR effect as of November 2, 2015, under a
wire not having enough separation from a part 51. revised methodology effective for 2016
certain bracket when the spoiler is in the (2) You must use this service information which provides for initial catch up
deployed position. We are issuing this AD to adjustments for inflation in 2016, and
as applicable to do the actions required by
detect and correct wire chafing; such chafing
this AD, unless the AD specifies otherwise. under a revised methodology for each
could result in an electrical short and
(i) Boeing Alert Service Bulletin B787– year thereafter. The revised
potential fire in a flammable fluid leakage
81205–SB270024–00, Issue 001, dated methodologies provide for the
zone and possible loss of several functions
September 24, 2014. improvement of the effectiveness of
essential for safe flight.
(ii) Reserved. CMPs and to maintain their deterrent
(f) Compliance (3) For Boeing service information
effect. The initial catch up adjustment
Comply with this AD within the identified in this AD, contact Boeing
Commercial Airplanes, Attention: Data &
for inflation of a CMP in 2016 shall not
compliance times specified, unless already exceed 150 percent of the amount of the
done. Services Management, P.O. Box 3707, MC
2H–65, Seattle, WA 98124–2207; telephone CMP on the date of enactment of the
(g) Wire Separation Measurement, Related 206–544–5000, extension 1; fax 206–766– Federal Civil Penalties Inflation
Investigative Actions, and Corrective 5680; Internet https:// Adjustment Act Improvements Act of
Actions www.myboeingfleet.com. 2015 (November 2, 2015). The initial
Within 24 months after the effective date (4) You may view this service information catch up adjustments for inflation to
of this AD: Measure the separation between at the FAA, Transport Airplane Directorate, CMPs are required to be published
the electro-mechanical actuator wire 1601 Lind Avenue SW., Renton, WA. For through an interim final rule not later
W801182 of the left wing, spoiler 4, and the information on the availability of this than July 1, 2016, and the adjustments
support bracket of the flap variable camber material at the FAA, call 425–227–1221. for inflation shall take effect not later
jstallworth on DSK7TPTVN1PROD with RULES
trim unit, and do all applicable related (5) You may view this service information
than August 1, 2016. For each year
investigative and corrective actions, in that is incorporated by reference at the
accordance with the Accomplishment National Archives and Records thereafter, the adjustments for inflation
Instructions of Boeing Alert Service Bulletin Administration (NARA). For information on to CMPs shall take effect not later than
B787–81205–SB270024–00, Issue 001, dated the availability of this material at NARA, call January 15. These adjustments for
September 24, 2014. Do all applicable related 202–741–6030, or go to: http:// inflation apply only to CMPs with a
investigative and corrective actions before www.archives.gov/federal-register/cfr/ibr- dollar amount, and will not apply to
further flight. locations.html. CMPs written as functions of violations.
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Document Created: 2018-02-08 07:31:28
Document Modified: 2018-02-08 07:31:28
| 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 July 12, 2016. | |
| Contact | Sean J. Schauer, Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057- 3356; phone: 425-917-6479; fax: 425-917-6590; email: [email protected] | |
| FR Citation | 81 FR 36452 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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