82 FR 26580 - Airworthiness Directives; General Electric Company Turbofan Engines
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 109 (June 8, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 109 (June 8, 2017)
| Page Range | 26580-26582 | |
| FR Document | 2017-11781 |
[Federal Register Volume 82, Number 109 (Thursday, June 8, 2017)] [Rules and Regulations] [Pages 26580-26582] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-11781] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2017-0016; Directorate Identifier 2016-NE-31-AD; Amendment 39-18917; AD 2017-12-02] RIN 2120-AA64 Airworthiness Directives; General Electric Company Turbofan Engines AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain General Electric Company (GE) GEnx-1B64, -1B64/P1, -1B64/P2, -1B67, - 1B67/P1, -1B67/P2, -1B70, -1B70/P1, -1B70/P2, -1B70/75/P1, -1B70/75/P2, -1B70C/P1, -1B70C/P2, -1B74/75/P1, -1B74/75/P2, -1B76A/P2 turbofan engines. This AD was prompted by a fracture of the fuel manifold which led to an in-flight shutdown of the engine. This AD requires replacement of the outer left side signal fuel manifold with a part eligible for installation. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective July 13, 2017. ADDRESSES: For service information identified in this final rule, contact General Electric Company, GE-Aviation, Room 285, 1 Neumann Way, Cincinnati, OH 45215, phone: 513-552-3272; fax: 513-552-3329; email: [email protected]. You may view this service information at the FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA. For information on the availability of this material at the FAA, call 781-238-7125. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017- 0016. 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-2017- 0016; 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 final rule, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (phone: 800-647-5527) is Document Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building [[Page 26581]] Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Christopher McGuire, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781- 238-7120; fax: 781-238-7199; 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 GEnx-1B64, -1B64/P1, - 1B64/P2, -1B67, -1B67/P1, -1B67/P2, -1B70, -1B70/P1, -1B70/P2, -1B70/ 75/P1, -1B70/75/P2, -1B70C/P1, -1B70C/P2, -1B74/75/P1, -1B74/75/P2, - 1B76A/P2 engines with outer left side signal fuel manifold, part number (P/N) 2403M46G01, and CAGE code 05813, installed. The NPRM published in the Federal Register on February 28, 2017 (82 FR 12070) (``the NPRM''). The NPRM was prompted by a fracture of the fuel manifold which led to an in-flight shutdown of the engine. The NPRM proposed to require replacement of the outer left side signal fuel manifold with a part eligible for installation. We are issuing this AD to prevent fracture of the fuel manifold, engine fire, and damage to the airplane. Comments We gave the public the opportunity to participate in developing this final rule. The following presents the comments received on the NPRM and the FAA's response to each comment. Request To Reduce Compliance Time The Air Line Pilots Association (ALPA) requested that the FAA reduce the compliance time in this AD from 12 months to 60 days. ALPA commented that the service bulletin (SB) recommends replacement of the left side signal fuel manifold within 60 days of issuance of the SB. We disagree. Our risk assessment of the potential for additional fuel manifold fractures indicates that 12 months represents an acceptable level of risk for replacement of the affected fuel manifolds. We did not change this AD. Request To Withdraw NPRM United Airlines (United) requested that the NPRM be withdrawn. United commented that they have already accomplished the requirements of this AD and removed all affected parts from stock. United noted that GE has reported that this issue has been resolved by all operators. United indicated that this AD will therefore only generate unnecessary work. We disagree. This AD includes an installation prohibition that prevents any non-conforming parts from being re-installed into engines. Without this prohibition, a non-conforming part could be installed into an engine and re-enter service. We did not change this AD. Request To Revise Applicability Japan Airlines (JAL) requested that the applicability of this AD be revised so that it lists affected engine serial numbers instead of applicable engines with the affected part installed. JAL indicated that GE no longer delivers engines with the affected parts installed. We disagree. This AD includes an installation prohibition to prevent the affected outer left side signal fuel manifold from being re-installed in any engine. By defining applicability according to the affected engine with the outer left side signal fuel manifold, P/N 2403M46G01, and CAGE code 05813, installed, we ensure that all the affected parts are removed from service and not re-installed in any engine. We did not change this AD. Request To Clarify Compliance Using SB JAL commented that they believe the AD should allow replacement of the affected outer left side signal fuel manifold using GE GEnx-1B SB 73-0053 R00, dated November 15, 2016. We agree. This AD does not specify which service material to use when replacing the outer left side signal fuel manifold. This AD lists GE service bulletins, including GEnx-1B SB 73-0053 R00, dated November 15, 2016, as guidance when inspecting, repairing, and replacing the outer left side signal fuel manifold. Therefore, this AD already allows use of GEnx-1B SB 73-0053 R00 when complying with this AD. We did not change this AD. Request That AD Not Apply to New Engines JAL requested that newly-delivered engines, which are not covered by GEnx-1B SB 73-0053 R00, dated November 15, 2016, should be considered as ``not applicable to this AD.'' We partially agree. We agree that this AD does not apply to new engines that do not have the affected fuel manifold installed. We disagree with changing the applicability of this AD because we do not want to allow an affected part to be installed later on a new engine. We did not change this AD. Support for the NPRM GE expressed support for the NPRM as written. Conclusion We reviewed the relevant data, considered the comments received, and determined that air safety and the public interest require adopting this final rule as proposed. Related Service Information We reviewed GE GEnx-1B SB 73-0051 R00, dated November 4, 2016; GE GEnx-1B SB 73-0052 R00, dated October 28, 2016; and GE GEnx-1B SB 73- 0053 R00, dated November 15, 2016. These SBs describe, respectively, procedures for inspecting, repairing, and replacing the outer left side signal fuel manifold, part number 2403M46G01, and CAGE code 05813. Costs of Compliance We estimate that this AD affects 109 engines installed on 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 of fuel manifold.......... 2 work-hours x $85 per $16,000 $16,170 $1,762,530 hour = $170. ---------------------------------------------------------------------------------------------------------------- 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, [[Page 26582]] 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 to the extent that it justifies making a regulatory distinction, 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): 2017-12-02 General Electric Company: Amendment 39-18917; Docket No. FAA-2017-0016; Directorate Identifier 2016-NE-31-AD. (a) Effective Date This AD is effective July 13, 2017. (b) Affected ADs None. (c) Applicability This AD applies to all GEnx-1B64, -1B64/P1, -1B64/P2, -1B67, - 1B67/P1, -1B67/P2, -1B70, 1B70/P1, -1B70/P2, -1B70/75/P1, -1B70/75/ P2, -1B70C/P1, -1B70C/P2, -1B74/75/P1, -1B74/75/P2, -1B76A/P2 engines with outer left side signal fuel manifold, part number (P/N) 2403M46G01, and CAGE code 05813, installed. (d) Subject Joint Aircraft System Component (JASC) Code 7313, Fuel Injector Nozzle. (e) Unsafe Condition This AD was prompted by fracture of the fuel manifold which led to an in-flight shutdown of the engine. We are issuing this AD to prevent fracture of the fuel manifold, engine fire, and damage to the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (1) Inspect the outer left side signal fuel manifold, P/N 2403M46G01 and CAGE code 05813, to determine if the part has additional marking ``XB,'' ``INS,'' or ``KB'' adjacent to part number. If the part is marked with ``XB,'' ``INS,'' or ``KB,'' then no further action is required. (2) For parts without additional marking ``XB,'' ``INS,'' or ``KB'' adjacent to the part number, within 12 months after the effective date of this AD, replace the outer left side signal fuel manifold with a part eligible for installation. (g) Installation Prohibition After the effective date of this AD, do not install an outer left side signal fuel manifold, P/N 2403M46G01, and CAGE code 05813, onto an engine, unless additional marking ``XB,'' ``INS,'' or ``KB'' is adjacent to the part number. (h) Alternative Methods of Compliance (AMOCs) The Manager, Engine Certification Office, FAA, may approve AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make your request. You may email your request to: [email protected]. (i) Related Information (1) For more information about this AD, contact Christopher McGuire, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7120; fax: 781-238-7199; email: [email protected]. (2) GE GEnx-1B Service Bulletin (SB) 73-0051 R00, dated November 4, 2016; GE GEnx-1B SB 73-0052 R00, dated October 28, 2016; and GE GEnx-1B SB 73-0053 R00, dated November 15, 2016, can be obtained from GE using the contact information in paragraph (i)(3) of this AD. These SBs, respectively, describe procedures for inspecting, repairing, and replacing the outer left side signal fuel manifold. (3) For service information identified in this AD, contact General Electric Company, GE-Aviation, Room 285, 1 Neumann Way, Cincinnati, OH 45215, phone: 513-552-3272; fax: 513-552-3329; email: [email protected]. (4) You may view this service information at the FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA. For information on the availability of this material at the FAA, call 781-238-7125. (j) Material Incorporated by Reference None. Issued in Burlington, Massachusetts, on May 30, 2017. Robert J. Ganley, Acting Manager, Engine & Propeller Directorate, Aircraft Certification Service. [FR Doc. 2017-11781 Filed 6-7-17; 8:45 am] BILLING CODE 4910-13-P
![26580 Federal Register / Vol. 82, No. 109 / Thursday, June 8, 2017 / Rules and Regulations
We are issuing this rulemaking under (a) Effective Date DEPARTMENT OF TRANSPORTATION
the authority described in Subtitle VII, This AD is effective July 13, 2017.
Part A, Subpart III, Section 44701: Federal Aviation Administration
‘‘General requirements.’’ Under that (b) Affected ADs
section, Congress charges the FAA with None. 14 CFR Part 39
promoting safe flight of civil aircraft in (c) Applicability [Docket No. FAA–2017–0016; Directorate
air commerce by prescribing regulations Identifier 2016–NE–31–AD; Amendment 39–
for practices, methods, and procedures This AD applies to General Electric
18917; AD 2017–12–02]
the Administrator finds necessary for Company (GE) CF6–80C2L1F turbofan
engines with a high-pressure turbine (HPT) RIN 2120–AA64
safety in air commerce. This regulation
spacer/impeller, part number (P/N)
is within the scope of that authority Airworthiness Directives; General
1539M12P02, installed.
because it addresses an unsafe condition Electric Company Turbofan Engines
that is likely to exist or develop on (d) Subject
products identified in this rulemaking Joint Aircraft System Component (JASC) AGENCY: Federal Aviation
action. Code 7250, Turbine/Turboprop Engine— Administration (FAA), DOT.
Turbine Section. ACTION: Final rule.
Regulatory Findings
This AD will not have federalism (e) Unsafe Condition SUMMARY: We are adopting a new
implications under Executive Order This AD was prompted by a reduction in airworthiness directive (AD) for certain
13132. This AD will not have a the life limit of the affected engines, which General Electric Company (GE) GEnx–
substantial direct effect on the States, on is the result of a revised operating profile. We 1B64, –1B64/P1, –1B64/P2, –1B67,
the relationship between the national are issuing this AD to prevent failure of the –1B67/P1, –1B67/P2, –1B70, –1B70/P1,
government and the States, or on the HPT spacer/impeller, uncontained release of –1B70/P2, –1B70/75/P1, –1B70/75/P2,
distribution of power and the HPT spacer/impeller, damage to the –1B70C/P1, –1B70C/P2, –1B74/75/P1,
responsibilities among the various engine, and damage to the airplane. –1B74/75/P2, –1B76A/P2 turbofan
levels of government. (f) Compliance
engines. This AD was prompted by a
For the reasons discussed above, I fracture of the fuel manifold which led
Comply with this AD within the to an in-flight shutdown of the engine.
certify that this AD: compliance times specified, unless already
(1) Is not a ‘‘significant regulatory This AD requires replacement of the
done. outer left side signal fuel manifold with
action’’ under Executive Order 12866, After the effective date of this AD, replace
a part eligible for installation. We are
(2) Is not a ‘‘significant rule’’ under the HPT spacer/impeller, P/N 1539M12P02,
issuing this AD to address the unsafe
DOT Regulatory Policies and Procedures before it exceeds 18,000 flight cycles since
condition on these products.
(44 FR 11034, February 26, 1979), new.
DATES: This AD is effective July 13,
(3) Will not affect intrastate aviation (g) Installation Prohibition
in Alaska to the extent that it justifies 2017.
After the effective date of this AD, do not ADDRESSES: For service information
making a regulatory distinction, and
install an HPT spacer/impeller, P/N identified in this final rule, contact
(4) Will not have a significant 1539M12P02, onto any engine, or return to
economic impact, positive or negative, General Electric Company, GE-Aviation,
service any engine with an HPT spacer/
on a substantial number of small entities Room 285, 1 Neumann Way, Cincinnati,
impeller, P/N 1539M12P02, installed, if the
under the criteria of the Regulatory HPT spacer/impeller exceeds 18,000 flight
OH 45215, phone: 513–552–3272; fax:
Flexibility Act. cycles since new.
513–552–3329; email: geae.aoc@ge.com.
You may view this service information
List of Subjects in 14 CFR Part 39 (h) Alternative Methods of Compliance at the FAA, Engine & Propeller
(AMOCs) Directorate, 1200 District Avenue,
Air transportation, Aircraft, Aviation
safety, Incorporation by reference, The Manager, Engine Certification Office, Burlington, MA. For information on the
Safety. FAA, may approve AMOCs for this AD. Use availability of this material at the FAA,
the procedures found in 14 CFR 39.19 to call 781–238–7125. It is also available
Adoption of the Amendment make your request. You may email your on the internet at http://
Accordingly, under the authority request to: ANE-AD-AMOC@faa.gov. www.regulations.gov by searching for
delegated to me by the Administrator, (i) Related Information and locating Docket No. FAA–2017–
the FAA amends 14 CFR part 39 as 0016.
For more information about this AD,
follows: contact Herman Mak, Aerospace Engineer, Examining the AD Docket
Engine Certification Office, FAA, Engine & You may examine the AD docket on
PART 39—AIRWORTHINESS
Propeller Directorate, 1200 District Avenue,
DIRECTIVES the Internet at http://
Burlington, MA 01803; phone: 781–238–
www.regulations.gov by searching for
7147; fax: 781–238–7199; email:
■ 1. The authority citation for part 39 and locating Docket No. FAA–2017–
herman.mak@faa.gov.
continues to read as follows: 0016; or in person at the Docket
Authority: 49 U.S.C. 106(g), 40113, 44701. (j) Material Incorporated by Reference Management Facility between 9 a.m.
None. and 5 p.m., Monday through Friday,
asabaliauskas on DSKBBXCHB2PROD with RULES
§ 39.13 [Amended] except Federal holidays. The AD docket
Issued in Burlington, Massachusetts, on
■ 2. The FAA amends § 39.13 by adding contains this final rule, the regulatory
May 23, 2017.
the following new airworthiness evaluation, any comments received, and
Carlos A. Pestana, other information. The address for the
directive (AD): Acting Manager, Engine & Propeller
2017–11–15 General Electric Company: Docket Office (phone: 800–647–5527) is
Directorate, Aircraft Certification Service. Document Management Facility, U.S.
Amendment 39–18914; Docket No.
FAA–2016–9490; Directorate Identifier [FR Doc. 2017–11780 Filed 6–7–17; 8:45 am] Department of Transportation, Docket
2016–NE–26–AD. BILLING CODE 4910–13–P Operations, M–30, West Building
VerDate Sep<11>2014 16:16 Jun 07, 2017 Jkt 241001 PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 E:\FR\FM\08JNR1.SGM 08JNR1](https://thefederalregister.org/doc/82_FR_26689/page/1.svg)
![26582 Federal Register / Vol. 82, No. 109 / Thursday, June 8, 2017 / Rules and Regulations
Part A, Subpart III, Section 44701: (b) Affected ADs (3) For service information identified in
‘‘General requirements.’’ Under that None. this AD, contact General Electric Company,
section, Congress charges the FAA with GE-Aviation, Room 285, 1 Neumann Way,
(c) Applicability Cincinnati, OH 45215, phone: 513–552–3272;
promoting safe flight of civil aircraft in
This AD applies to all GEnx–1B64, –1B64/ fax: 513–552–3329; email: geae.aoc@ge.com.
air commerce by prescribing regulations (4) You may view this service information
for practices, methods, and procedures P1, –1B64/P2, –1B67, –1B67/P1, –1B67/P2,
–1B70, 1B70/P1, –1B70/P2, –1B70/75/P1, at the FAA, Engine & Propeller Directorate,
the Administrator finds necessary for 1200 District Avenue, Burlington, MA. For
–1B70/75/P2, –1B70C/P1, –1B70C/P2,
safety in air commerce. This regulation –1B74/75/P1, –1B74/75/P2, –1B76A/P2 information on the availability of this
is within the scope of that authority engines with outer left side signal fuel material at the FAA, call 781–238–7125.
because it addresses an unsafe condition manifold, part number (P/N) 2403M46G01, (j) Material Incorporated by Reference
that is likely to exist or develop on and CAGE code 05813, installed.
None.
products identified in this rulemaking
(d) Subject Issued in Burlington, Massachusetts, on
action.
Joint Aircraft System Component (JASC) May 30, 2017.
Regulatory Findings Code 7313, Fuel Injector Nozzle. Robert J. Ganley,
This AD will not have federalism (e) Unsafe Condition Acting Manager, Engine & Propeller
implications under Executive Order This AD was prompted by fracture of the Directorate, Aircraft Certification Service.
13132. This AD will not have a fuel manifold which led to an in-flight [FR Doc. 2017–11781 Filed 6–7–17; 8:45 am]
substantial direct effect on the States, on shutdown of the engine. We are issuing this BILLING CODE 4910–13–P
the relationship between the national AD to prevent fracture of the fuel manifold,
government and the States, or on the engine fire, and damage to the airplane.
distribution of power and (f) Compliance DEPARTMENT OF HOMELAND
responsibilities among the various SECURITY
Comply with this AD within the
levels of government.
compliance times specified, unless already
For the reasons discussed above, I done. U.S. Customs and Border Protection
certify that this AD: (1) Inspect the outer left side signal fuel
(1) Is not a ‘‘significant regulatory manifold, P/N 2403M46G01 and CAGE code DEPARTMENT OF THE TREASURY
action’’ under Executive Order 12866, 05813, to determine if the part has additional
(2) Is not a ‘‘significant rule’’ under marking ‘‘XB,’’ ‘‘INS,’’ or ‘‘KB’’ adjacent to 19 CFR Part 12
DOT Regulatory Policies and Procedures part number. If the part is marked with ‘‘XB,’’
‘‘INS,’’ or ‘‘KB,’’ then no further action is [CBP Dec. No. 17–04]
(44 FR 11034, February 26, 1979),
(3) Will not affect intrastate aviation required. RIN 1515–AE22
(2) For parts without additional marking
in Alaska to the extent that it justifies
‘‘XB,’’ ‘‘INS,’’ or ‘‘KB’’ adjacent to the part Merchandise Produced by Convict,
making a regulatory distinction, and number, within 12 months after the effective
(4) Will not have a significant Forced, or Indentured Labor;
date of this AD, replace the outer left side
economic impact, positive or negative, signal fuel manifold with a part eligible for
Conforming Amendment and Technical
on a substantial number of small entities installation. Corrections
under the criteria of the Regulatory AGENCY: U.S. Customs and Border
(g) Installation Prohibition
Flexibility Act. Protection, Department of Homeland
After the effective date of this AD, do not
List of Subjects in 14 CFR Part 39 install an outer left side signal fuel manifold, Security; Department of the Treasury.
P/N 2403M46G01, and CAGE code 05813, ACTION: Final rule.
Air transportation, Aircraft, Aviation
onto an engine, unless additional marking
safety, Incorporation by reference, ‘‘XB,’’ ‘‘INS,’’ or ‘‘KB’’ is adjacent to the part SUMMARY: This document amends the
Safety. number. U.S. Customs and Border Protection
Adoption of the Amendment regulations to reflect section 910 of the
(h) Alternative Methods of Compliance
(AMOCs)
Trade Facilitation and Trade
Accordingly, under the authority Enforcement Act of 2015 by removing
delegated to me by the Administrator, The Manager, Engine Certification Office, the ‘‘consumptive demand’’ clause from
the FAA amends 14 CFR part 39 as FAA, may approve AMOCs for this AD. Use
the procedures found in 14 CFR 39.19 to
the regulations concerning the
follows: prohibition on the importation of
make your request. You may email your
request to: ANE-AD-AMOC@faa.gov. merchandise produced by convict,
PART 39—AIRWORTHINESS
forced, or indentured labor. It also
DIRECTIVES (i) Related Information updates the regulations to reflect the
(1) For more information about this AD, correct name of the agency and includes
■ 1. The authority citation for part 39 contact Christopher McGuire, Aerospace
continues to read as follows: a minor procedural change with regard
Engineer, Engine Certification Office, FAA, to the filing of proof of admissibility.
Authority: 49 U.S.C. 106(g), 40113, 44701. Engine & Propeller Directorate, 1200 District
Avenue, Burlington, MA 01803; phone: 781– DATES: This final rule is effective on
§ 39.13 [Amended] 238–7120; fax: 781–238–7199; email: June 8, 2017.
■ 2. The FAA amends § 39.13 by adding chris.mcguire@faa.gov. FOR FURTHER INFORMATION CONTACT:
(2) GE GEnx-1B Service Bulletin (SB) 73– Thomas Kendrick, Trade Remedy Law
the following new airworthiness
asabaliauskas on DSKBBXCHB2PROD with RULES
0051 R00, dated November 4, 2016; GE Enforcement Directorate, Office of
directive (AD): GEnx–1B SB 73–0052 R00, dated October 28, Trade, Thomas.Kendrick@dhs.gov, (202)
2017–12–02 General Electric Company: 2016; and GE GEnx–1B SB 73–0053 R00,
863–6057.
Amendment 39–18917; Docket No. dated November 15, 2016, can be obtained
FAA–2017–0016; Directorate Identifier from GE using the contact information in SUPPLEMENTARY INFORMATION:
2016–NE–31–AD. paragraph (i)(3) of this AD. These SBs, I. Background
respectively, describe procedures for
(a) Effective Date inspecting, repairing, and replacing the outer Section 307 of the Tariff Act of 1930,
This AD is effective July 13, 2017. left side signal fuel manifold. as amended (19 U.S.C. 1307) prohibits
VerDate Sep<11>2014 16:16 Jun 07, 2017 Jkt 241001 PO 00000 Frm 00012 Fmt 4700 Sfmt 4700 E:\FR\FM\08JNR1.SGM 08JNR1](https://thefederalregister.org/doc/82_FR_26689/page/3.svg)
Document Created: 2018-11-14 10:06:50
Document Modified: 2018-11-14 10:06:50
| 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 13, 2017. | |
| Contact | Christopher McGuire, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781- 238-7120; fax: 781-238-7199; email: [email protected] | |
| FR Citation | 82 FR 26580 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
2025 Federal Register | Disclaimer | Privacy Policy
USC | CFR | eCFR