Official Federal Register HTML source
AD 2026-10-21
Published 2026-06-04 · Document 2026-11179
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
- 2026-07-09
- 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 all Rolls-Royce Deutschland Ltd & Co KG Model
Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent
1000-H3, Trent 1000-J3, Trent 1000-K3, Trent 1000-L3, Trent 1000-M3,
Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3, and Trent 1000-R3
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-AE3
- Trent 1000-CE3
- Trent 1000-D3
- Trent 1000-G3
- Trent 1000-J3
- Trent 1000-K3
- Trent 1000-L3
- Trent 1000-M3
- Trent 1000-N3
- Trent 1000-P3
- Trent 1000-Q3
- Trent 1000-R3
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 2023-26-04, Amendment 39-22647 (89 FR 251,
January 3, 2024).
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 July 9, 2026.
(b) Affected ADs
(b) Affected ADs
This AD replaces AD 2023-26-04, Amendment 39-22647 (89 FR 251,
January 3, 2024).
(c) Applicability
(c) Applicability
This AD applies to all Rolls-Royce Deutschland Ltd & Co KG Model
Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent
1000-H3, Trent 1000-J3, Trent 1000-K3, Trent 1000-L3, Trent 1000-M3,
Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3, and Trent 1000-R3
engines.
(d) Subject
(d) Subject
Joint Aircraft System Component (JASC) Code 7500, Engine Bleed
Air System.
(e) Unsafe Condition
(e) Unsafe Condition
This AD was prompted by a determination that a new set of on-
wing initial and repetitive visual inspections of the intermediate-
pressure stage 8 (IP8) and high-pressure stage 3 (HP3) air transfer
tubes for cracking, damage, or air leakage wear are necessary, and
consequently the inspection interval for the repetitive in-shop
visual inspections of the front bearing housing IP8 air feed tubes
may be increased. The FAA is issuing this AD to prevent failure of
the IP8 and HP3 air transfer tubes and front bearing housing IP8 air
feed tubes. The unsafe condition, if not addressed, could affect the
engine internal cooling and sealing flows, resulting in failure of
the IP8 air transfer tubes, HP3 air transfer tubes, and front
bearing housing IP8 air feed tubes, with consequent damage to the
engine and reduced control 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) and (i) of this AD: Perform
all required actions within the compliance times specified in, and
in accordance with, European Union Aviation Safety Agency (EASA) AD
2025-0176, dated August 7, 2025 (EASA AD 2025-0176).
(h) Exceptions to EASA AD 2025-0176
(h) Exceptions to EASA AD 2025-0176
(1) Where EASA AD 2025-0176 refers to its effective date, this
AD requires using the effective date of this AD.
(2) This AD does not adopt the ``Remarks'' section of EASA AD
2025-0176.
(i) No Reporting Requirement
(i) No Reporting Requirement
Although the service material referenced in EASA AD 2025-0176
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, 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, 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].
(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) Additional Information
(k) Additional Information
For more information about this AD, contact Alexis Whitaker,
Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines,
WA 98198; phone: (516) 228-7309; 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 material listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this material as applicable to do the actions
required by this AD, unless the AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) AD 2025-0176,
dated August 7, 2025.
(ii) [Reserved]
[[Page 33607]]
(3) For EASA material identified in this AD, 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 material on the EASA website at ad.easa.europa.eu.
(4) You may view this material 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 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].