Official Federal Register HTML source
AD 2023-12-21
Published 2023-07-11 · Document 2023-14584
This is a dated source edition. Current legal effect, aircraft applicability, installed configuration and compliance remain unknown. It has not been promoted as a regulatory determination or qualified as paid-report evidence.
- Effective date printed in this source
- 2023-08-15
- Source acquired
- 2026-09-28
- PDF corroboration
- Not verified in this HTML-only batch
Open the official complete publication · Find this AD number in the FAA catalog
Applicability wording in this source
(c) Applicability
This AD applies to Rolls-Royce Deutschland Ltd & Co KG Model
Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent
1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2,
Trent 1000-K2, and Trent 1000-L2 engines, all serial numbers.
Serial numbers, installed parts, exceptions and service-document requirements have not been evaluated. An engine model mentioned here is not evidence that an aircraft has that engine installed.
Fully written literal labels recorded in this clause:
- Trent 1000-A2
- Trent 1000-AE2
- Trent 1000-C2
- Trent 1000-CE2
- Trent 1000-E2
- Trent 1000-G2
- Trent 1000-H2
- Trent 1000-J2
- Trent 1000-K2
- Trent 1000-L2
This literal index is partial. Shorthand, ranges and broken lines have not been expanded or repaired.
Historical relationship wording
(b) Affected ADs
This AD replaces AD 2021-26-13, Amendment 39-21872 (86 FR 72840,
December 23, 2021).
This wording records what this edition said at publication. It does not determine current supersession or current independent burden.
Recorded rule paragraphs
These exact source paragraphs include conditions and maintenance wording. They are not a conclusion that work applies to, or was completed on, an individual aircraft. Referenced manufacturer service documents are link-only and are not mirrored.
(a) Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective August 15, 2023.
(b) Affected ADs
(b) Affected ADs
This AD replaces AD 2021-26-13, Amendment 39-21872 (86 FR 72840,
December 23, 2021).
(c) Applicability
(c) Applicability
This AD applies to Rolls-Royce Deutschland Ltd & Co KG Model
Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent
1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2,
Trent 1000-K2, and Trent 1000-L2 engines, all serial numbers.
(d) Subject
(d) Subject
Joint Aircraft System Component (JASC) Code 7200, Engine
(Turbine/Turboprop).
(e) Unsafe Condition
(e) Unsafe Condition
This AD was prompted by the manufacturer revising the engine
Time Limits Manual life limits of certain critical rotating parts,
updating the direct accumulation counting data files, and updating
certain maintenance tasks. The FAA is issuing this AD to prevent the
failure of critical rotating parts. 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
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
(g) Required Actions
Except as specified in paragraph (h) of this AD: Perform all
required actions within the compliance times specified in, and in
accordance with, European Union Aviation Safety Agency (EASA) AD
2022-0210, dated October 17, 2022 (EASA AD 2022-0210).
(h) Exceptions to EASA AD 2022-0210
(h) Exceptions to EASA AD 2022-0210
(1) Where EASA AD 2022-0210 defines the AMP as the approved
Aircraft Maintenance Programme on the basis of which the operator or
the owner ensures the continuing airworthiness of each operated
engine, this AD defines the AMP as the Aircraft Maintenance Program
on the basis of which the operator or the owner ensures the
continuing airworthiness of each operated airplane.
(2) Where EASA AD 2022-0210 refers to its effective date, this
AD requires using the effective date of this AD.
(3) This AD does not require compliance with paragraph (1) of
EASA AD 2022-0210.
(4) This AD does not require compliance with paragraph (2) of
EASA AD 2022-0210.
(5) Where paragraph (3) of EASA AD 2022-0210 specifies revising
the approved AMP within 12 months after the effective date of EASA
AD 2022-0210, this AD requires revising the existing approved
maintenance or inspection program, as applicable, and airworthiness
limitations section within 90 days after the effective date of this
AD.
(6) This AD does not adopt the ``Remarks'' paragraph of EASA AD
2022-0210.
(i) Provisions for Alternative Actions and Intervals
(i) Provisions for Alternative Actions and Intervals
After performing the actions required by paragraph (g) of this
AD, no alternative actions and associated thresholds and intervals,
including life limits, are allowed unless they are approved as
specified in the provisions of the ``Ref. Publications'' section of
EASA AD 2022-0210.
[[Page 44042]]
(j) Alternative Methods of Compliance (AMOCs)
(j) Alternative Methods of Compliance (AMOCs)
The Manager, International Validation 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 responsible Flight
Standards 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 and email to: [email protected]. 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) Additional Information
(k) Additional Information
For more information about this AD, contact Sungmo Cho, Aviation
Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; phone: (781) 238-7241; email: [email protected].
(l) Material Incorporated by Reference
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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) European Union Aviation Safety Agency AD 2022-0210, dated
October 17, 2022.
(ii) [Reserved]
(3) For EASA AD 2022-0210, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; phone: +49 221 8999 000; email:
[email protected]; website: easa.europa.eu. This EASA AD may be
found in the AD docket at regulations.gov under Docket No. FAA-2023-
0437.
(4) You may view this service information at the 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: [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.