Rule2023-04869
Airworthiness Directives; General Electric Company Turbofan Engines
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
March 10, 2023
Effective
March 27, 2023
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain General Electric Company (GE) GE90-110B1 and GE90-115B model turbofan engines. This AD was prompted by a manufacturer investigation which discovered that florescent penetrant inspections (FPI) were not performed on the dovetail pressure face of certain high-pressure compressor (HPC) rotor spools at overhaul. This AD requires FPI of the affected HPC rotor stage 7-9 spool and, depending on the results of the inspection, replacement with a part eligible for installation. The FAA is issuing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 88 Issue 47 (Friday, March 10, 2023)</title>
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[Federal Register Volume 88, Number 47 (Friday, March 10, 2023)]
[Rules and Regulations]
[Pages 14871-14874]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2023-04869]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-0423; Project Identifier AD-2022-01525-E;
Amendment 39-22366; AD 2023-04-19]
RIN 2120-AA64
Airworthiness Directives; General Electric Company Turbofan
Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
[[Page 14872]]
ACTION: Final rule; request for comments.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain General Electric Company (GE) GE90-110B1 and GE90-115B model
turbofan engines. This AD was prompted by a manufacturer investigation
which discovered that florescent penetrant inspections (FPI) were not
performed on the dovetail pressure face of certain high-pressure
compressor (HPC) rotor spools at overhaul. This AD requires FPI of the
affected HPC rotor stage 7-9 spool and, depending on the results of the
inspection, replacement with a part eligible for installation. The FAA
is issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective March 27, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of March 27,
2023.
The FAA must receive comments on this AD by April 24, 2023.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to <a href="http://regulations.gov">regulations.gov</a>. Follow
the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
<bullet> Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> by
searching for and locating Docket No. FAA-2023-0423; 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, any
comments received, and other information. The street address for Docket
Operations is listed above.
Material Incorporated by Reference
<bullet> 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; email:
<a href="/cdn-cgi/l/email-protection#305146595144595f5e1e565c555544434540405f4244700c5110584255560d" http: ge.com">ge.com</a>">aviation.fleetsupport@<a href="http://ge.com">ge.com</a></a>.
<bullet> You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 1200
District Avenue, Burlington, MA 01803. For information on the
availability of this material at the FAA, call (817) 222-5110. It is
also available at <a href="http://regulations.gov">regulations.gov</a> by searching for and locating Docket
No. FAA-2023-0423.
FOR FURTHER INFORMATION CONTACT: Stephen Elwin, Aviation Safety
Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803;
phone: (781) 238-7236; email: <a href="/cdn-cgi/l/email-protection#12416677627a777c3c5e3c577e657b7c527473733c757d64"><span class="__cf_email__" data-cfemail="55062130253d303b7b197b1039223c3b153334347b323a23">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
The FAA received a report that a GE overhaul shop internal
investigation found that several HPC rotor stage 7-9 spools were
shipped to operators prior to a final FPI being performed on the
dovetail pressure face. A final FPI is performed to confirm that any
linear indications have been removed, as indications on the HPC rotor
stage 7-9 spool may potentially propagate and eventually lead to
failure of the HPC rotor stage 7-9 spool. This condition, if not
addressed, could result in an in-flight shutdown, damage to the engine,
and damage to the airplane. The FAA is issuing this AD to address the
unsafe condition on these products.
FAA's Determination
The FAA is issuing this AD because the agency has determined the
unsafe condition described previously is likely to exist or develop in
other products of the same type design.
Related Service Information Under 1 CFR Part 51
The FAA reviewed GE GE90-100 Service Bulletin 72-0905 R00, dated
July 25, 2022. This service information specifies procedures for
performing a piece-part inspection of the affected HPC rotor stage 7-9
spools. 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 ADDRESSES.
AD Requirements
This AD requires, at the next shop visit after the effective date
of this AD, performing an FPI of each affected HPC rotor stage 7-9
spool and, depending on the results of the inspection, replacement with
a part eligible for installation.
Justification for Immediate Adoption and Determination of the Effective
Date
Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5
U.S.C. 551 et seq.) authorizes agencies to dispense with notice and
comment procedures for rules when the agency, for ``good cause,'' finds
that those procedures are ``impracticable, unnecessary, or contrary to
the public interest.'' Under this section, an agency, upon finding good
cause, may issue a final rule without providing notice and seeking
comment prior to issuance. Further, section 553(d) of the APA
authorizes agencies to make rules effective in less than thirty days,
upon a finding of good cause.
The FAA has found the risk to the flying public justifies waiving
notice and comment prior to adoption of this rule because no domestic
operators use this product. It is unlikely that the FAA will receive
any adverse comments or useful information about this AD from any U.S.
operator. Accordingly, notice and opportunity for prior public comment
are unnecessary, pursuant to 5 U.S.C. 553(b)(3)(B). In addition, for
the foregoing reason(s), the FAA finds that good cause exists pursuant
to 5 U.S.C. 553(d) for making this amendment effective in less than 30
days.
Comments Invited
The FAA invites you to send any written data, views, or arguments
about this final rule. Send your comments to an address listed under
ADDRESSES. Include ``FAA-2023-0423 Project Identifier AD-2022-01525-E''
at the beginning of your comments. The most helpful comments reference
a specific portion of the final rule, explain the reason for any
recommended change, and include supporting data. The FAA will consider
all comments received by the closing date and may amend this final rule
because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
<a href="http://regulations.gov">regulations.gov</a>, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this final rule.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this AD contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this AD, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA
[[Page 14873]]
will treat such marked submissions as confidential under the FOIA, and
they will not be placed in the public docket of this AD. Submissions
containing CBI should be sent to Stephen Elwin, Aviation Safety
Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803.
Any commentary that the FAA receives which is not specifically
designated as CBI will be placed in the public docket for this
rulemaking.
Regulatory Flexibility Act
The requirements of the Regulatory Flexibility Act (RFA) do not
apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt
a rule without prior notice and comment. Because FAA has determined
that it has good cause to adopt this rule without prior notice and
comment, RFA analysis is not required.
Costs of Compliance
The FAA estimates that this AD affects 0 engines installed on
airplanes of U.S. registry.
The FAA estimates the following costs to comply with this AD:
Estimated Costs
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Cost per Cost on U.S.
Action Labor cost Parts cost product operators
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Perform an FPI of the HPC rotor stage 5 work-hours x $85 per $0 $425 $0
7-9 spool. hour = $425.
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The FAA estimates the following costs to do any necessary
replacements that would be required based on the results of the
inspection. The agency has no way of determining the number of aircraft
that might need these replacements:
On-Condition Costs
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Cost per
Action Labor cost Parts cost product
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Replace the HPC rotor stage 7-9 spool......... 40 work-hours x $85 per hour = $1,183,200 $1,186,600
$3,400.
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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.
The FAA is 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, and
(2) Will not affect intrastate aviation in Alaska.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
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:
2023-04-19 General Electric Company: Amendment 39-22366; Docket No.
FAA-2023-0423; Project Identifier AD-2022-01525-E.
(a) Effective Date
This airworthiness directive (AD) is effective March 27, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to General Electric Company (GE) GE90-110B1 and
GE90-115B model turbofan engines with an installed high-pressure
compressor (HPC) rotor stage 7-9 spool with part number (P/N)
2032M23G01, P/N 2032M23G02, P/N 2676M00G01, or P/N 2676M00G02, and a
serial number listed in paragraph 4., Appendix--A, Table 1 of GE
GE90-100 Service Bulletin (SB) 72-0905 R00, dated July 25, 2022 (GE
SB 72-0905).
(d) Subject
Joint Aircraft System Component (JASC) Code 7230, Turbine Engine
Compressor Section.
(e) Unsafe Condition
This AD was prompted by a manufacturer investigation which
revealed that florescent penetrant inspections (FPI) were not
performed on the dovetail pressure face of certain HPC rotor stage
7-9 spools at overhaul. The FAA is issuing this AD to prevent the
failure of the HPC rotor stage 7-9 spool. The unsafe condition, if
not addressed, could result in an in-flight shutdown, damage to the
engine, and damage to the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
(1) At the next engine shop visit after the effective date of
this AD, perform an FPI of the dovetail pressure face of the
affected HPC rotor stage 7-9 spool in accordance with the
[[Page 14874]]
Accomplishment Instructions, paragraph 3.A.(1)(a) of GE SB 72-0905.
(2) If, during the FPI required by paragraph (g)(1) of this AD,
the HPC rotor stage 7-9 spool does not meet the part serviceability
criteria in the Accomplishment Instructions, paragraph 3.A.(1)(a) of
GE SB 72-0905, before further flight, replace the compressor rotor
stage 7-9 spool 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
separation of pairs of major mating engine flanges, except for the
following situations, which do not constitute an engine shop visit:
(i) Separation of engine flanges solely for the purposes of
transportation of the engine without subsequent maintenance; or
(ii) Separation of engine flanges solely for the purpose of
replacing the fan or propulsor without subsequent maintenance.
(i) 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
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
certification office, send it to the attention of the person
identified in paragraph (j) of this AD and email it to: <a href="/cdn-cgi/l/email-protection#a9e8e7ec84e8ed84e8e4e6eae9cfc8c887cec6df"><span class="__cf_email__" data-cfemail="7938373c54383d543834363a391f1818571e160f">[email protected]</span></a>.
(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 Stephen Elwin,
Aviation Safety Engineer, ECO Branch, FAA, 1200 District Avenue,
Burlington, MA 01803; phone: (781) 238-7236; email:
<a href="/cdn-cgi/l/email-protection#510225342139343f7f1d7f143d26383f113730307f363e27"><span class="__cf_email__" data-cfemail="782b0c1d08101d165634563d140f1116381e1919561f170e">[email protected]</span></a>.
(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) GE GE90-100 Service Bulletin 72-0905 R00, dated July 25,
2022.
(ii) [Reserved]
(3) For GE service information identified in this AD, contact
General Electric Company, 1 Neumann Way, Cincinnati, OH 45215;
phone: (513) 552-3272; email: <a href="/cdn-cgi/l/email-protection#87e6f1eee6f3eee8e9a9e1ebe2e2f3f4f2f7f7e8f5f3c7e6e2a9bbe6a7eff5e2e1ba" http: ge.com">ge.com</a>">aviation.fleetsupport@ae.<a href="http://ge.com">ge.com</a></a>;
website: <a href="http://ge.com">ge.com</a>.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 1200
District Avenue, Burlington, MA 01803. For information on the
availability of this material at the FAA, call (817) 222-5110.
(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, email: <a href="/cdn-cgi/l/email-protection#680e1a4601061b180d0b1c0107062806091a09460f071e"><span class="__cf_email__" data-cfemail="b8deca96d1d6cbc8dddbccd1d7d6f8d6d9cad996dfd7ce">[email protected]</span></a>, or go to: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued on February 25, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-04869 Filed 3-9-23; 8:45 am]
BILLING CODE 4910-13-P
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