AD 2013-23-18

Airworthiness directive · Variable bypass valve (VBV) actuator fuel supply tube · General Electric GE90-110B1 and GE90-115B

Effective
January 7, 2014
Published
December 3, 2013 · 78 FR 72567–72568
Issued
November 14, 2013
Models
GE90-110B1, GE90-115B
Data sheet
TCDSE00049EN
Registered aircraft
143 matched by model
Product
Engine
Amendment
39-17673
Docket
FAA-2013-0499
Project
2013-NE-20-AD
Issued as
Final rule

Unofficial copy from the Federal Register XML, document 2013-28866. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.

On this page

Summary

We are adopting a new airworthiness directive (AD) for certain General Electric Company (GE) GE90-110B1 and -115B turbofan engines. This AD was prompted by multiple events of a leaking variable bypass valve (VBV) actuator fuel supply tube. This AD requires replacement of this VBV actuator fuel supply tube with a part eligible for installation. We are issuing this AD to prevent failure of the affected fuel supply tube, fuel leakage, engine fire, and damage to the airplane.

The airworthiness directive

2013-23-18 General Electric Company: Amendment 39-17673; Docket No. FAA-2013-0499; Directorate Identifier 2013-NE-20-AD.

(a) Effective Date

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This AD is effective January 7, 2014.

(b) Affected ADs

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None.

(c) Applicability

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This AD applies to General Electric Company (GE) GE90-110B1 and -115B turbofan engines with variable bypass valve (VBV) actuator fuel supply tube, part number (P/N) 2165M22P01, installed.

(d) Unsafe Condition

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This AD was prompted by multiple events of a leaking VBV actuator fuel supply tube. We are issuing this AD to prevent failure of the affected fuel supply tube, fuel leakage, engine fire, and damage to the airplane.

(e) Compliance

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(1) Comply with this AD within the compliance times specified, unless already done.

(2) At the next shop visit, after the effective date of this AD, replace the VBV actuator fuel supply tube, P/N 2165M22P01, with a part eligible for installation.

(f) Definition

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For the purpose of this AD, a shop visit is the induction of an engine into the shop for maintenance or overhaul. The separation of engine flanges solely for the purposes of transporting the engine without subsequent engine maintenance does not constitute an engine shop visit.

(g) Installation Prohibition

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After the effective date of this AD, do not install any VBV actuator fuel supply tube, P/N 2165M22P01, onto any engine.

(h) Alternative Methods of Compliance (AMOCs)

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The Manager, Engine Certification Office, FAA, may approve AMOCs for this AD. Use the procedures in 14 CFR 39.19 to make your request.

(i) Related Information

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For more information about this AD, contact Jason Yang, Aerospace Engineer, Engine Certification Office, FAA, 12 New England Executive Park, Burlington, MA 01803; phone: 781-238-7747; fax: 781-238-7199; email: jason.yang@faa.gov.

(j) Material Incorporated by Reference

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None.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

DatesPage 1

This AD is effective January 7, 2014.

For further information contactPage 1

Jason Yang, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; phone: 781-238-7747; fax: 781-238-7199; email: jason.yang@faa.gov.

DiscussionPage 1

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to the specified products. The NPRM published in the Federal Register on July, 25, 2013 (78 FR 44899, July 25, 2013). The NPRM proposed to require replacement of the affected VBV actuator fuel supply tube, part number 2165M22P01, with a part eligible for installation.

CommentsPage 1

We gave the public the opportunity to participate in developing this AD. The following presents the comments received on the proposal and the FAA's response to each comment.

Agreement With the Proposed ADPage 1

The Boeing Company and FedEx Express agreed with the AD as proposed.

Request To Change the Compliance TimePage 1

GE requested that we change the compliance time in this AD from “at the next shop visit, after the effective date of this AD” to “as soon as possible without effect on revenue service, but before April 1, 2014.” No justification was provided for the change.

We do not agree. Replacement of the VBV actuator fuel supply tube at the next shop visit maintains an acceptable level of safety for the fleet, based on safety risk analysis. We have no data to support that a more aggressive replacement schedule is required to maintain that acceptable level of safety. We did not change the AD.

ConclusionPage 1

We reviewed the relevant data, considered the comments received, and determined that air safety and the public interest require adopting this AD as proposed.

Costs of CompliancePage 2

We estimate that this AD will affect about 59 engines installed on airplanes of U.S. registry. We also estimate that it will take about eight hours per engine to replace the VBV actuator fuel supply tube. The cost of this part is about $14,310. The average labor rate is $85 per hour. Based on these figures, we estimate the cost of this AD on U.S. operators to be $884,410.

Authority for This RulemakingPage 2

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 findingsPage 2

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 if 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.

Adoption of the AmendmentPage 2

Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

Adoption of the amendmentPage 2

1. The authority citation for part 39 continues to read as follows:

2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD):

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 143

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Boeing143 aircraft
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Registered aircraft by year built: 139 aircraft
20053
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20119
201215
201310
20145
20154
20164
201715
20187
20199
20207
20216
20223
20237
20241
20255
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4 with no year recorded

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