Rule2025-03987
Airworthiness Directives; General Electric Company 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 13, 2025
Effective
April 17, 2025
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is adopting a new airworthiness directive (AD) for all General Electric Company (GE) Model CT7-2E1 engines. This AD was prompted by a revised analysis using an updated stress model, which calculated that the actual life limit of the CT7-2E1 stage 2 turbine aft cooling plate is less than the current life limit. This AD requires revision of the airworthiness limitations section (ALS) of the existing CT7-2E1 engine maintenance manual (EMM) and the operator's existing approved maintenance program or inspection program, as applicable, to incorporate a reduced life limit for this part. The FAA is issuing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 90 Issue 48 (Thursday, March 13, 2025)</title>
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[Federal Register Volume 90, Number 48 (Thursday, March 13, 2025)]
[Rules and Regulations]
[Pages 11896-11897]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2025-03987]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-2547; Project Identifier AD-2024-00334-E;
Amendment 39-22987; AD-2025-05-15]
RIN 2120-AA64
Airworthiness Directives; General Electric Company Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
General Electric Company (GE) Model CT7-2E1 engines. This AD was
prompted by a revised analysis using an updated stress model, which
calculated that the actual life limit of the CT7-2E1 stage 2 turbine
aft cooling plate is less than the current life limit. This AD requires
revision of the airworthiness limitations section (ALS) of the existing
CT7-2E1 engine maintenance manual (EMM) and the operator's existing
approved maintenance program or inspection program, as applicable, to
incorporate a reduced life limit for this part. The FAA is issuing this
AD to address the unsafe condition on these products.
DATES: This AD is effective April 17, 2025.
ADDRESSES:
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2024-2547; 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 address for Docket Operations is 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: Barbara Caufield, Aviation Safety
Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198 ; phone:
(781) 238-7146; email: <a href="/cdn-cgi/l/email-protection#7c1e1d0e1e1d0e1d521f1d091a151910183c1a1d1d521b130a"><span class="__cf_email__" data-cfemail="bbd9dac9d9dac9da95d8daceddd2ded7dffbdddada95dcd4cd">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to all GE Model CT7-2E1
engines. The NPRM published in the Federal Register on December 5, 2024
(89 FR 96618). The NPRM was prompted by a revised analysis using an
updated stress model, which calculated that the actual life limit of
the GE Model CT7-2E1 engine stage 2 turbine aft cooling plate is less
than the current life limit. In the NPRM, the FAA proposed to require
revision of the ALS of the existing CT7-2E1 EMM and the operator's
existing approved maintenance program or inspection program, as
applicable, to incorporate a reduced life limit for the stage 2 turbine
aft cooling plate part number 5166T27P01. The FAA is issuing this AD to
address the unsafe condition on these products.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the costs.
Conclusion
The FAA reviewed the relevant data and determined that air safety
requires adopting this AD as proposed. Accordingly, the FAA is issuing
this AD to address the unsafe condition on these products. Except for
minor editorial changes, this AD is adopted as proposed in the NPRM.
Costs of Compliance
The FAA estimates that this AD affects eight CT7-2E1 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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Revise the ALS........................... 1 work-hour x $85 per hour $0 $85 $680
= $85.
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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
[[Page 11897]]
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) Will not affect intrastate aviation in Alaska, and
(3) 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.
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(f), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2025-05-15 General Electric Company: Amendment 39-22987; Docket No.
FAA-2024-2547; Project Identifier AD-2024-00334-E.
(a) Effective Date
This airworthiness directive (AD) is effective April 17, 2025.
(b) Affected ADs
None.
(c) Applicability
This AD applies to General Electric Company (GE) Model CT7-2E1
engines.
(d) Subject
Joint Aircraft System Component (JASC) Code 7200, Engine
(Turbine/Turboprop).
(e) Unsafe Condition
This AD was prompted by a revised analysis using an updated
stress model, which calculated that the actual life limit of the
CT7-2E1 stage 2 turbine aft cooling plate is less than the current
life limit. The FAA is issuing this AD to prevent failure of the
stage 2 aft turbine cooling plate. The unsafe condition, if not
addressed, could result in an uncontained failure, release of high-
energy debris, damage to the engine, damage to the airplane, and
loss of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Within 30 days after the effective date of this AD, revise the
airworthiness limitations section of the existing engine maintenance
manual or instructions for continued airworthiness, and the
operator's existing approved maintenance program or inspection
program, as applicable, by replacing the 6,100 cycle life limit with
the new life limit of 3,100 cycles for the stage 2 aft turbine
cooling plate part number 5166T27P01.
(h) Provisions for Alternative Actions or Intervals
After the action required by paragraph (g) of this AD has been
done, no alternative actions, including life limits, are allowed
unless they are approved as specified in the provisions of paragraph
(i) of this AD.
(i) Alternative Methods of Compliance (AMOCs)
(1) The Manager, AIR-520 Continued Operational Safety 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 AIR-520 Continued
Operational Safety Branch, send it to the attention of the person
identified in paragraph (j) of this AD. Information may be emailed
to: <a href="/cdn-cgi/l/email-protection#3475797b77745255551a535b42"><span class="__cf_email__" data-cfemail="2c6d61636f6c4a4d4d024b435a">[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) Additional Information
For more information about this AD, contact Barbara Caufield,
Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines,
WA 98198; phone: (781) 238-7146; email: <a href="/cdn-cgi/l/email-protection#5a383b28383b283b74393b2f3c333f363e1a3c3b3b743d352c"><span class="__cf_email__" data-cfemail="bbd9dac9d9dac9da95d8daceddd2ded7dffbdddada95dcd4cd">[email protected]</span></a>.
(k) Material Incorporated by Reference
None.
Issued on March 7, 2025.
Peter A. White,
Deputy Director, Integrated Certificate Management Division, Aircraft
Certification Service.
[FR Doc. 2025-03987 Filed 3-12-25; 8:45 am]
BILLING CODE 4910-13-P
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