Official Federal Register HTML source
AD 2021-26-13
Published 2021-12-23 · Document 2021-27628
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
- 2022-01-27
- 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 (Type
Certificate previously held by Rolls-Royce plc) (RRD) 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 model turbofan 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:
- Trent 1000-A2
- Trent 1000-AE2
- Trent 1000-C2
- Trent 1000-CE2
- Trent 1000-D2
- 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
None.
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 January 27, 2022.
(b) Affected ADs
(b) Affected ADs
None.
(c) Applicability
(c) Applicability
This AD applies to Rolls-Royce Deutschland Ltd & Co KG (Type
Certificate previously held by Rolls-Royce plc) (RRD) 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 model turbofan 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,
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 AD 2020-0241,
dated November 5, 2020 (EASA AD 2020-0241).
(h) Exceptions to EASA AD 2020-0241
(h) Exceptions to EASA AD 2020-0241
(1) The requirements specified in paragraphs (1) and (2) of EASA
AD 2020-0241 are not required by this AD.
(2) Where EASA AD 2020-0241 requires compliance from its
effective date, this AD requires using the effective date of this
AD.
(3) Paragraph (3) of EASA AD 2020-0241 specifies revising the
approved airworthiness maintenance program within 12 months after
its effective date, but this AD requires revising the existing
approved continuous airworthiness maintenance program within 90 days
after the effective date of this AD.
(4) This AD does not mandate compliance with the ``Remarks''
section of EASA AD 2020-0241.
(i) No Reporting Requirement
(i) No Reporting Requirement
Although the service information referenced in EASA AD 2020-0241
specifies to submit certain information to the manufacturer, this AD
does not include that requirement.
(j) Alternative Methods of Compliance (AMOCs)
(j) 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
ECO Branch, send it to the attention of the person identified in
paragraph (k) of this AD. Information may be emailed to: [email protected].
(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.
(k) Related Information
(k) Related Information
For more information about this AD, contact Kevin M. Clark,
Aviation Safety Engineer, ECO Branch, FAA, 1200 District Avenue,
Burlington, MA 01803; phone: (781) 238-7088; fax: (781) 238-7199;
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 (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 this AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) AD 2020-0241,
dated November 5, 2020.
(ii) [Reserved]
(3) For EASA AD 2020-0241, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; phone: +49 221 8999 000; email:
[email protected]. You may find this EASA AD on the EASA website at
https://ad.easa.europa.eu.
(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 material 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 https://www.archives.gov/federal-register/cfr/ibr-locations.html.