[Federal Register Volume 88, Number 131 (Tuesday, July 11, 2023)]
[Proposed Rules]
[Pages 44075-44077]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-14587]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1410; Project Identifier MCAI-2022-01517-E]
RIN 2120-AA64


Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG 
Engines

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD) 
2013-26-10, which applies to certain Rolls-Royce Deutschland Ltd & Co 
KG (RRD) Model RB211-524G2-19, RB211-524G3-19, RB211-524H-36, and 
RB211-524H2-19 engines. AD 2013-26-10 requires a one-time reduction in 
the cyclic life of certain high-pressure compressor (HPC) rotor stage 1 
and stage 2 disks, and removal of disks that exceed the reduced cycle 
life. Since the FAA issued AD 2013-26-10, the manufacturer has revised 
the engine time limits manual (TLM), introducing new and more 
restrictive instructions. This proposed AD would require revisions to 
the airworthiness limitations section (ALS) of the operator's existing 
approved engine maintenance or inspection program, as applicable, as 
specified in a European Union Aviation Safety Agency (EASA) AD, which 
is proposed for incorporation by reference (IBR). The FAA is proposing 
this AD to address the unsafe condition on these products.

DATES: The FAA must receive comments on this NPRM by August 25, 2023.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to regulations.gov. Follow 
the instructions for submitting comments.
     Fax: (202) 493-2251.
     Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE, Washington, DC 20590.
     Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2023-1410; 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 NPRM, the mandatory continuing airworthiness 
information (MCAI), any comments received, and other information. The 
street address for Docket Operations is listed above.
    Material Incorporated by Reference:
     For service information identified in this NPRM, 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. It is also 
available at regulations.gov under Docket No. FAA-2023-1410.
     You may view this service information 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.

FOR FURTHER INFORMATION CONTACT: Sungmo Cho, Aviation Safety Engineer, 
FAA, 2200 South 216th Street, Des Moines, WA 98198; phone: (781) 238-
7241; email: [email protected].

SUPPLEMENTARY INFORMATION:

Comments Invited

    The FAA invites you to send any written relevant data, views, or 
arguments about this proposal. Send your comments to an address listed 
under ADDRESSES. Include ``Docket No. FAA-2023-1410; Project Identifier 
MCAI-2022-01517-E'' at the beginning of your comments. The most helpful 
comments reference a specific portion of the proposal, explain the 
reason for any recommended change, and include supporting data. The FAA 
will consider all comments received by the closing date and may amend 
the proposal because of those comments.
    Except for Confidential Business Information (CBI) as described in 
the following paragraph, and other information as described in 14 CFR 
11.35, the FAA will post all comments received, without change, to 
regulations.gov, including any personal information you provide. The 
agency will also post a report summarizing each substantive verbal 
contact received about this NPRM.

Confidential Business Information

    CBI is commercial or financial information that is both customarily 
and actually treated as private by its owner. Under the Freedom of 
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public 
disclosure. If your comments responsive to this NPRM contain commercial 
or financial information that is customarily treated as private, that 
you actually treat as private, and that is relevant or responsive to 
this NPRM, it is important that you clearly designate the submitted 
comments as CBI. Please mark each page of your submission containing 
CBI as ``PROPIN.'' The FAA will treat such marked submissions as 
confidential under the FOIA, and they will not be placed in the public 
docket of this NPRM. Submissions containing CBI should be sent to 
Sungmo Cho, Aviation Safety Engineer, FAA, 2200 South 216th Street, Des 
Moines, WA 98198. Any commentary that the FAA receives which is not 
specifically designated as CBI will be placed in the public docket for 
this rulemaking.

Background

    The FAA issued AD 2013-26-10, Amendment 39-17719 (79 FR 1315, 
January 8, 2014) (AD 2013-26-10), for all RRD Model RB211-524G2-19, 
RB211-524G3-19, RB211-524H-36, and RB211-524H2-19 engines. AD 2013-26-
10 was prompted by an MCAI originated by EASA, which is the Technical 
Agent for the Member States of the European Union. EASA issued

[[Page 44076]]

EASA AD 2013-0246, dated October 10, 2013, to correct an unsafe 
condition identified as part failure and consequent release of high-
energy debris, possibly resulting in damage to the airplane.
    AD 2013-26-10 requires a one-time reduction in the cyclic life of 
certain HPC stage 1 and stage 2 disks and removal of disks that exceed 
the reduced cycle life from service. The agency issued AD 2013-26-10 to 
prevent the failure of certain life-limited parts, which could result 
in uncontained engine damage and damage to the airplane.

Actions Since AD 2013-26-10 Was Issued

    Since the FAA issued AD 2013-26-10, EASA superseded EASA AD 2013-
0246 and issued EASA AD 2022-0232, dated November 28, 2022 (EASA AD 
2022-0232) (referred to after this as the MCAI). The MCAI states that 
the ALS for RB211-524G/H engines, which is approved by EASA, is defined 
and published in TLM T-211(524)-7RR, and that these airworthiness 
limitations have been identified as mandatory for continued 
airworthiness. The MCAI also states that since the original issue of 
TLM T-211(524)-7RR, updated thresholds and intervals were introduced 
for newly designed parts. EASA AD 2013-0246 was issued to require 
implementation of the reduced cyclic life limit and replacement of HPC 
stage 1 and 2 disks before exceeding their life limit. The MCAI also 
states that the manufacturer published a revised engine TLM since EASA 
AD 2013-0246 was issued, introducing new and more restrictive 
instructions. The ALS defined in the revised engine TLM also adds RRD 
Model RB211-524G2-T-19, RB211-524G3-T-19, RB211-524H-T-36, and RB211-
524H2-T-19 engines to the list of affected engines.
    You may examine the MCAI in the AD docket at regulations.gov under 
Docket No. FAA-2023-1410.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed EASA AD 2022-0232, which specifies instructions 
for accomplishing the actions specified in the applicable TLM, 
including performing maintenance tasks, replacing life-limited parts, 
and revising the existing approved maintenance or inspection program, 
as applicable, by incorporating the limitations, tasks, and associated 
thresholds and intervals described in the TLM. This material is 
reasonably available because the interested parties have access to it 
through their normal course of business or by the means identified in 
ADDRESSES.

FAA's Determination

    These products have been approved by the aviation authority of 
another country, and are approved for operation in the United States. 
Pursuant to the FAA's bilateral agreement with the State of Design 
Authority, it has notified the FAA of the unsafe condition described in 
the MCAI described above. The FAA is issuing this NPRM after 
determining that the unsafe condition described previously is likely to 
exist or develop in other products of the same type design.

Proposed AD Requirements in This NPRM

    This proposed AD would retain none of the requirements of AD 2013-
26-10. This proposed AD would require revising the existing approved 
engine maintenance or inspection program, as applicable, to incorporate 
new and more restrictive airworthiness limitations, which are specified 
in EASA AD 2022-0232 described previously, except for any differences 
identified as exceptions in the regulatory text of this AD and as 
discussed under ``Differences Between this Proposed AD and the MCAI.''

Explanation of Required Compliance Information

    In the FAA's ongoing efforts to improve the efficiency of the AD 
process, the FAA developed a process to use some civil aviation 
authority (CAA) ADs as the primary source of information for compliance 
with requirements for corresponding FAA ADs. The FAA has since 
coordinated with other manufacturers and CAAs to use this process. As a 
result, the FAA proposes to incorporate by reference EASA AD 2022-0232 
in the FAA final rule. This proposed AD would, therefore, require 
compliance with EASA AD 2022-0232 in its entirety through that 
incorporation, except for any differences identified as exceptions in 
the regulatory text of this proposed AD. Using common terms that are 
the same as the heading of a particular section in the EASA AD does not 
mean that operators need comply only with that section. For example, 
where the AD requirement refers to ``all required actions within the 
compliance times,'' compliance with this AD requirement is not limited 
to the section titled ``Required Action(s) and Compliance Time(s)'' in 
EASA AD 2022-0232. Service information required by the EASA AD for 
compliance will be available at regulations.gov by searching for and 
locating Docket No. FAA-2023-1410 after the FAA final rule is 
published.

Difference Between This Proposed AD and the MCAI

    Where paragraph (3) of EASA AD 2022-0232 specifies revising the 
approved Aircraft Maintenance Programme within 12 months after the 
effective date of EASA AD 2022-0232, this proposed AD would require 
revising the ALS of the existing approved engine maintenance or 
inspection program, as applicable, within 90 days after the effective 
date of this AD.

Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would 
affect 22 engines installed on airplanes of U.S. registry.
    The FAA estimates the following costs to comply with this proposed 
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 of the existing        1 work-hours x $85 per               $0              $85           $1,870
 approved engine maintenance or        hour = $85.
 inspection program.
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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 44077]]

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

    The FAA determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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 the proposed 
regulation:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Would not affect intrastate aviation in Alaska, and
    (3) Would 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 Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 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(g), 40113, 44701.


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by:
0
a. Removing Airworthiness Directive 2013-26-10, Amendment 39-17719 (79 
FR 1315, January 8, 2014); and
0
b. Adding the following new airworthiness directive:

Rolls-Royce Deutschland Ltd & Co KG: Docket No. FAA-2023-1410; 
Project Identifier MCAI-2022-01517-E.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) by August 25, 2023.

(b) Affected ADs

    This AD replaces AD 2013-26-10, Amendment 39-17719 (79 FR 1315, 
January 8, 2014).

(c) Applicability

    This AD applies to Rolls-Royce Deutschland Ltd & Co KG (RRD) 
Model RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19, RB211-524G3-
T-19, RB211-524H-36, RB211-524H-T-36, RB211-524H2-19, and RB211-
524H2-T-19 engines.

(d) Subject

    Joint Aircraft System Component (JASC) Code 7230, Turbine Engine 
Compressor Section.

(e) Unsafe Condition

    This AD was prompted by the manufacturer revising the engine 
time limits manual, introducing new and more restrictive 
instructions. The FAA is issuing this AD to prevent failure of 
certain life-limited parts. The unsafe condition, if not addressed, 
could result in uncontained engine damage and damage to the 
airplane.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(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 
2022-0232, dated November 28, 2022 (EASA AD 2022-0232).

(h) Exceptions to EASA AD 2022-0232

    (1) Where EASA AD 2022-0232 defines the AMP as the approved 
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 2022-0232 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 2022-0232.
    (4) This AD does not require compliance with paragraph (2) of 
EASA AD 2022-0232.
    (5) Where paragraph (3) of EASA AD 2022-0232 specifies revising 
the approved Aircraft Maintenance Programme within 12 months after 
the effective date of EASA AD 2022-0232, this AD requires revising 
the airworthiness limitations section (ALS) of the existing approved 
engine maintenance or inspection program, as applicable, within 90 
days after the effective date of this AD.
    (6) This AD does not require compliance with paragraph (4) of 
EASA AD 2022-0232.
    (7) This AD does not require compliance with paragraph (5) of 
EASA AD 2022-0232.
    (8) This AD does not adopt the Remarks paragraph of EASA AD 
2022-0232.

(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 2022-0232.

(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 
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].
    (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

    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].

(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 the AD specifies otherwise.
    (i) European Union Aviation Safety Agency AD 2022-0232, dated 
November 28, 2022.
    (ii) [Reserved]
    (3) For EASA AD 2022-0232, 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.
    (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.

    Issued on July 6, 2023.
Michael Linegang,
Acting Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2023-14587 Filed 7-10-23; 8:45 am]
BILLING CODE 4910-13-P