Official Federal Register HTML source
AD 2023-21-08
Published 2023-11-14 · Document 2023-25099
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
- 2023-12-19
- Source acquired
- 2026-09-28
- PDF corroboration
- Not verified in this HTML-only batch
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Applicability wording in this source
(c) Applicability
This AD applies to Rolls-Royce Deutschland Ltd & Co KG (RRD)
Model Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE,
Trent 1000-D, Trent 1000-E, Trent 1000-G, and Trent 1000-H engines.
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:
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 2021-21-13, Amendment 39-21773 (86 FR 64066,
November 17, 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 December 19,
2023.
(b) Affected ADs
(b) Affected ADs
This AD replaces AD 2021-21-13, Amendment 39-21773 (86 FR 64066,
November 17, 2021).
(c) Applicability
(c) Applicability
This AD applies to Rolls-Royce Deutschland Ltd & Co KG (RRD)
Model Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE,
Trent 1000-D, Trent 1000-E, Trent 1000-G, and Trent 1000-H engines.
(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.
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 critical rotating parts, which 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
2022-0259, dated December 20, 2022 (EASA AD 2022-0259).
(h) Exceptions to EASA AD 2022-0259
(h) Exceptions to EASA AD 2022-0259
(1) Where EASA AD 2022-0259 defines the AMP as the Aircraft
Maintenance Programme, which contains the tasks on the basis of
which the scheduled maintenance is conducted to ensure the
continuing airworthiness of each operated engine, this AD defines
the AMP as the Aircraft Maintenance Program, which contains the
tasks of which the operator or the owner ensures the continuing
airworthiness of each operated airplane.
(2) Where EASA AD 2022-0259 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 2022-0259.
(4) This AD does not require compliance with paragraph (2) of
EASA AD 2022-0259.
(5) Where paragraph (3) of EASA AD 2022-0259 specifies revising
the approved Aircraft Maintenance Programme within 12 months after
the effective date of EASA AD 2022-0259, this AD requires revising
the airworthiness limitations section of the existing approved
maintenance or inspection program, as applicable, within 90 days
after the effective date of this AD.
(6) This AD does not adopt the ``Remarks'' paragraph of EASA AD
2022-0259.
(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 2022-0259.
(j) Alternative Methods of Compliance (AMOCs)
(j) Alternative Methods of Compliance (AMOCs)
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 responsible
Flight Standards 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 (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, 2200 South 216th Street, Des Moines, WA 98198;
phone: (781) 238-7241; email: [email protected].
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(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 (EASA) AD 2022-0259,
dated December 20, 2022.
(ii) [Reserved]
(3) For EASA AD 2022-0259, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; phone: +49 221 8999 000; email:
[email protected]; website: easa.europa.eu. You may find this EASA
AD on the EASA website at ad.easa.europa.eu.
(4) You may view this service information at 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. This material may be found
in the AD docket at regulations.gov under Docket No. FAA-2023-1490.
(5) You may view this material at the National Archives and
Records Administration (NARA). For information on the availability
of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email [email protected].