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Timestamp: 2020-01-26 17:41:29
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Matched Legal Cases: ['art 39', 'art 39', 'art 39', 'art 39', 'ART 39', 'art 39']

[Docket No. FAA ; Product Identifier 2018-NE-01-AD; Amendment ; AD ] - PDF Free Download
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1 [Federal Register Volume 83, Number 144 (Thursday, July 26, 2018)] [Rules and Regulations] [Pages ] From the Federal Register Online via the Government Publishing Office [ [FR Doc No: ] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA ; Product Identifier 2018-NE-01-AD; Amendment ; AD ] 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 all General Electric Company (GE) GEnx-1B engines. This AD was prompted by a report of a center vent tube (CVT) failure leading to a loss of oil pressure and subsequent in-flight engine shutdown. This AD requires removal of an affected extension duct and replacing it with a part eligible for installation. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective August 30, ADDRESSES: For service information identified in this final rule, contact General Electric Company, GE Aviation, Room 285, 1 Neumann Way, Cincinnati, OH 45215; phone: ; You may view this service information at the FAA, Engine and Propeller Standards Branch, 1200 District Avenue, Burlington, MA. For information on the availability of this material at the FAA, call It is also available on the internet at by searching for and locating Docket No. FAA Examining the AD Docket You may examine the AD docket on the internet at by searching for and locating Docket No. FAA ; or in person at Docket Operations 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 Docket Operations (phone: ) is U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC
2 FOR FURTHER INFORMATION CONTACT: Herman Mak, Aerospace Engineer, ECO Branch, FAA, 1200 District Ave., Burlington, MA 01803; phone: ; fax: ; 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 GE GEnx-1B engines. The NPRM published in the Federal Register on April 30, 2018 (83 FR 18747). The NPRM was prompted by a report of a CVT failure leading to a loss of oil pressure and subsequent in-flight engine shutdown. During the event, the CVT failed due to oil leaking into the fan mid shaft, resulting in coking on the seal assembly and overpressurization of the CVT. The NPRM proposed to require removal of an affected extension duct and replacing it with a part eligible for installation. We are issuing this AD to address the unsafe condition on these products. Comments We gave the public the opportunity to participate in developing this final rule. We have considered the comments received. The Air Line Pilots Association and United Airlines supported the NPRM. 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 Service Bulletin (SB) R01, dated August 21, The SB describes procedures for replacing air/oil extension ducts, P/N 2332M85P01 or 2331M25G03, with an extension duct eligible for installation. Costs of Compliance We estimate that this AD affects 97 engines installed on airplanes of U.S. registry. We estimate the following costs to comply with this AD: Replacement of Extension Duct Estimated Costs Action Labor cost Parts cost Authority for This Rulemaking 4 work-hours $85 per hour = $340 2 Cost per product Cost on U.S. operators $16,270 $16,610 $1,611,170 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.
3 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. This AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to engines, propellers, and associated appliances to the Manager, Engine and Propeller Standards Branch, Policy and Innovation Division. Regulatory Findings This AD will not have federalism implications under Executive Order 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: PART 39 AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, [Amended] 2. The FAA amends by adding the following new airworthiness directive (AD): 3
4 FAA Aviation Safety AIRWORTHINESS DIRECTIVE General Electric Company: Amendment ; Docket No. FAA ; Product Identifier 2018-NE-01-AD. (a) Effective Date This AD is effective August 30, (b) Affected ADs None. (c) Applicability This AD applies to General Electric Company (GE) GEnx-1B64, -1B64/P1, -1B64/P2, -1B67, - 1B67/P1, -1B67/P2, -1B70, -1B70/75/P1, -1B70/75/P2, -1B70/P1, -1B70/P2, -1B70C/P1, - 1B70C/P2, -1B74/75/P1, and -1B74/75/P2 engines with air/oil extension duct, part number (P/N) 2332M85P01 or 2331M25G03, installed. (d) Subject Joint Aircraft System Component (JASC) Code 7250, Turbine Section. (e) Unsafe Condition This AD was prompted by reports of a center vent tube (CVT) failure. We are issuing this AD to prevent failure of the CVT. The unsafe condition, if not addressed, could result in failure of one or more engines, loss of thrust control, and loss of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Action At the next engine shop visit after the effective date of this AD, remove air/oil extension ducts, P/N 2332M85P01 or 2331M25G03, and replace with a part eligible for installation. (h) Definition For the purpose of this AD, an engine shop visit is the induction of an engine into the shop for maintenance involving the separation of pairs of major mating engine case flanges, except for the following situations, which do not constitute an engine shop visit: (1) Separation of engine flanges solely for the purposes of transportation of the engine without subsequent maintenance. 4
5 (2) Separation of engine flanges solely for the purpose of replacing the fan or propulsor without subsequent maintenance. (i) Installation Prohibition After the effective date of this AD, do not install an air/oil extension duct, P/N 2332M85P01 or 2331M25G03, into a fan mid shaft assembly. (j) Alternative Methods of Compliance (AMOCs) (1) The Manager, ECO Branch, FAA, has the authority to approve AMOCs for this AD if requested using the procedures found in 14 CFR 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 certification office, send it to the attention of the person identified in paragraph (k) of this AD. You may your request to: (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. (k) Related Information For more information about this AD, contact Herman Mak, Aerospace Engineer, ECO Branch, FAA, 1200 District Ave., Burlington, MA 01803; phone: ; fax: ; (l) Material Incorporated by Reference None. Issued in Burlington, Massachusetts, on July 19, Karen M. Grant, Acting Manager, Engine and Propeller Standards Branch, Aircraft Certification Service. 5