[Federal Register Volume 88, Number 132 (Wednesday, July 12, 2023)]
[Proposed Rules]
[Pages 44235-44237]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-14468]



[[Page 44235]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1399; Project Identifier MCAI-2022-01533-E]
RIN 2120-AA64


Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG 
(Type Certificate Previously Held by Rolls-Royce plc) 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) 
2020-15-07, which applies to certain Rolls-Royce Deutschland Ltd & Co 
KG (RRD) (type certificate previously held by Rolls-Royce plc) Model 
RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19, RB211-524G3-T-19, 
RB211-524H2-19, RB211-524H2-T-19, RB211-524H-36, and RB211-524H-T-36 
engines. AD 2020-15-07 requires replacement of the low-pressure turbine 
(LPT) stage 1 disk with part number (P/N) UL37606, UL37607, UL37608, 
UL37722 or UL37790, installed. Since the FAA issued AD 2020-15-07, RRD 
determined that additional LPT stage 1 disks are affected by the unsafe 
condition, and updated the Aircraft Maintenance Manual (AMM) to add new 
component life limits. This proposed AD would retain the requirement to 
replace the LPT stage 1 disk and would include additional LPT stage 1 
disks, 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 28, 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-2023-1399; 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 that is proposed for IBR 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-2023-1399.
     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-2023-1399; Project Identifier 
MCAI-2022-01533-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 2020-15-07, Amendment 39-21170 (85 FR 43682, July 
20, 2020), (AD 2020-15-07), for RRD Model B211-524G2-19, RB211-524G2-T-
19, RB211-524G3-19, RB211-524G3-T-19, RB211-524H2-19, RB211-524H2-T-19, 
RB211-524H-36, and RB211-524H-T-36 engines with LPT stage 1 disks, part 
number (P/N) UL37606, UL37607, UL37608, UL37722 or UL37790, installed. 
AD 2020-15-07 was prompted by an MCAI originated by EASA, which is the 
Technical Agent for the Member States of the European Union. EASA 
issued EASA AD 2020-0059, dated March 17, 2020 (EASA AD 2020-0059), to 
address an unsafe condition identified as an updated analysis by the 
engine manufacturer indicating that certain part-numbered and serial-
numbered LPT stage 1 disks that have undergone rework could fail before 
the current published life limits.
    AD 2020-15-07 requires replacement of the LPT stage 1 disk before 
it reaches its new Declared Safe Cycle Limit (DSCL) or within 25 flight 
cycles after the effective date of AD 2020-15-07, whichever occurs 
later. The FAA issued AD 2020-15-07 to prevent failure of the LPT stage 
1 disk.

Actions Since AD 2020-15-07 Was Issued

    Since the FAA issued AD 2020-15-07, EASA superseded EASA AD 2020-
0059 and issued EASA AD 2022-0237, dated December 2, 2022 (EASA AD 
2022-0237) (referred to after this as the MCAI). The MCAI states that 
further investigation by the manufacturer identified additional part 
numbered LPT stage 1 disks affected by the unsafe

[[Page 44236]]

condition. As a result of this finding, RRD published revised service 
information, which includes the additional affected LPT stage 1 disk 
part numbers.
    The FAA is proposing this AD to prevent failure of the LPT stage 1 
disk. This condition, if not addressed, could result in uncontained 
release of high-energy debris from the engine, in-flight shutdown of 
the engine, damage to the engine, and damage to the airplane.
    You may examine the MCAI in the AD docket at regulations.gov under 
Docket No. FAA-2023-1399.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed EASA AD 2022-0237, which specifies procedures for 
replacement of the LPT stage 1 disk and reducing the DSCL for LPT stage 
1 disks. 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 this 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 on other products of the same type design.

Proposed AD Requirements in This NPRM

    This proposed AD would retain none of the requirements of AD 2020-
15-07. This proposed AD would include additional LPT stage 1 disks and 
require accomplishing the actions specified in the MCAI described 
previously, except for any differences identified as exceptions in the 
regulatory text of this proposed.

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 2022-0237 
in the FAA final rule. This proposed AD would, therefore, require 
compliance with EASA AD 2022-0237 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 and 
compliance times,'' compliance with this AD requirement is not limited 
to the section titled ``Required Action(s) and Compliance Time(s)'' in 
EASA AD 2022-0237. Service information required by the EASA AD for 
compliance will be available at regulations.gov under Docket No. FAA-
2023-1399 after the FAA final rule is published.

Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would 
affect 18 engines installed on airplanes of U.S. registry.
    The FAA estimates the following costs to comply with this proposed 
AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Remove and replace LPT stage 1 disk...  120 work-hours x $85 per         $30,000         $40,200        $723,600
                                         hour = $10,200.
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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 
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 2020-15-07, Amendment 39-21170 (85 
FR 43682, July 20, 2020); and
0
b. Adding the following new airworthiness directive:


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Rolls-Royce Deutschland Ltd. & Co. KG: Docket No. FAA-2023-1399; 
Project Identifier MCAI-2022-01533-E.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) by August 28, 2023.

(b) Affected ADs

    This AD replaces AD 2020-15-07, Amendment 39-21170 (85 FR 43682, 
July 20, 2020).

(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, RB211-524H2-19, RB211-524H2-T-19, RB211-524H-36, and RB211-
524H-T-36 engines.

(d) Subject

    Joint Aircraft System Component (JASC) Code 7250, Turbine 
Section.

(e) Unsafe Condition

    This AD was prompted by an updated analysis by the engine 
manufacturer, which indicates certain part-numbered and serial-
numbered low-pressure turbine (LPT) stage 1 disks that have 
undergone rework could fail before the current published life 
limits. The FAA is issuing this AD to prevent failure of the LPT 
stage 1 disk. The unsafe condition, if not addressed, could result 
in uncontained release of high-energy debris from the engine, in-
flight shutdown of the engine, damage to the engine, 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 paragraphs (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 
2022-0237, dated December 2, 2022 (EASA AD 2022-0237).

(h) Exceptions to EASA AD 2022-0237

    (1) Where EASA AD 2022-0237 refers to its effective date, this 
AD requires using the effective date of this AD.
    (2) This AD does not adopt the Remarks paragraph of EASA AD 
2022-0237.

(i) 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 of the certification office, 
send it to the attention of the person identified in paragraph (j) 
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.

(j) 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].

(k) 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 2022-0237, dated 
December 2, 2022.
    (ii) [Reserved]
    (3) For EASA AD 2022-0237 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 June 30, 2023.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness 
Division, Aircraft Certification Service.

[FR Doc. 2023-14468 Filed 7-11-23; 8:45 am]
BILLING CODE 4910-13-P


