Federal Register / Vol. 87, No. 40 / Tuesday, March 1, 2022 / Rules and Regulations 11289 

that the issuance of the Bulletin does 

not impose any new or revise any 

existing recordkeeping, reporting, or 

disclosure requirements on covered 

entities or members of the public that 

would be collections of information 

requiring approval by the Office of 

Management and Budget under the 

Paperwork Reduction Act. 

Rohit Chopra, 

Director, Consumer Financial Protection 

Bureau. 

[FR Doc. 2022–04266 Filed 2–28–22; 8:45 am] 

BILLING CODE 4810–AM–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2021–0259; Project 

Identifier AD–2020–01128–E; Amendment 

39–21900; AD 2022–02–03] 

RIN 2120–AA64 

Airworthiness Directives; CFM 

International, S.A. Turbofan Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: The FAA is correcting an 

airworthiness directive (AD) that 

published in the Federal Register. The 

AD applies to CFM International, S.A. 

CFM56–3 and CFM56–7B model 

turbofan engines with certain accessory 

gearbox assembly (AGB) not equipped 

with a dynamic oil seal assembly in the 

handcranking pad. As published, the 

part numbers (P/Ns) listed in paragraph 

(i)(2)(i) are incorrect. This document 

corrects that error. In all other respects, 

the original document remains the 

same; however, for clarity, the FAA is 

publishing the entire rule in the Federal 

Register. 

DATES: This correction is effective 

March 22, 2022. The effective date of 

AD 2022–02–03 remains March 22, 

2022. 

ADDRESSES: For service information 

identified in this final rule, contact CFM 

International, S.A., Aviation Operations 

Center, 1 Neumann Way, M/D Room 

285, Cincinnati, OH 45125; phone: (877) 

432–3272; email: fleetsupport@ge.com. 

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. It is also available 

at https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2021–0259. 

Examining the AD Docket 

You may examine the AD docket at 

https://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2021–0259, 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 

final rule, any comments received, and 

other information. The address for 

Docket Operations is U.S. Department of 

Transportation, Docket Operations, 

M–30, West Building Ground Floor, 

Room W12–140, 1200 New Jersey 

Avenue SE, Washington, DC 20590. 

FOR FURTHER INFORMATION CONTACT: 

Kevin Clark, Aviation Safety Engineer, 

ECO Branch, FAA, 1200 District 

Avenue, Burlington, MA 01803; phone: 

(781) 238–7088; fax: (781) 238–7199; 

email: kevin.m.clark@faa.gov. 

SUPPLEMENTARY INFORMATION: AD 2022– 

02–03, 39–21961 (87 FR 8402, February 

15, 2022) (AD 2022–02–03), requires 

independent inspection to verify reinstallation of the AGB handcranking 

pad cover after maintenance. AD 2022– 

02–03 also requires the replacement of 

the affected AGB with a part eligible for 

installation as a terminating action to 

the inspection requirement. 

Need for the Correction 

As published, the P/Ns listed in 

paragraph (i)(2)(i) of the AD, which 

defines a part eligible for installation, 

are incorrect. The P/Ns were incorrectly 

listed as 340–046–503–0, 340–046–504– 

0, and 340–046–505–0. The correct P/Ns 

are 335–300–103–0, 335–300–105–0, 

335–300–106–0, 335–300–107–0, 335– 

300–108–0, 335–300–109–0, and 335– 

300–110–0. 

Although no other part of the 

preamble or regulatory information has 

been corrected, for clarity, the FAA is 

publishing the entire rule in the Federal 

Register. 

The effective date of this AD remains 

March 22, 2022. 

Good Cause for Adoption Without Prior 

Notice 

Section 553(b)(3)(B) of the 

Administrative Procedure Act (APA) (5 

U.S.C. 551 et seq.) authorizes agencies 

to dispense with notice and comment 

procedures for rules when the agency 

for ‘‘good cause’’ finds that those 

procedures are ‘‘impracticable, 

unnecessary, or contrary to the public 

interest.’’ Under this section, an agency, 

upon finding good cause, may issue a 

final rule without providing notice and 

seeking comment prior to issuance. 

Further, section 553(d) of the APA 

authorizes agencies to make rules 

effective in less than thirty days, upon 

a finding of good cause. 

The FAA has found that the risk to 

the flying public justifies foregoing 

notice and comment prior to adoption of 

this rule because this action corrects 

P/Ns that were correctly identified in a 

notice of proposed rulemaking, which 

published in the Federal Register on 

May 3, 2021 (86 FR 23301). 

Accordingly, notice and opportunity for 

prior public comment are unnecessary 

pursuant to 5 U.S.C. 553(b). 

In addition, the FAA finds that good 

cause exists pursuant to 5 U.S.C. 553(d) 

for making this amendment effective in 

less than 30 days, for the same reasons 

the FAA found good cause to forego 

notice and comment. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Correction 

Accordingly, pursuant to the 

authority delegated to me by the 

Administrator, the Federal Aviation 

Administration amends part 39 of the 

Federal Aviation Regulations (14 CFR 

part 39) by correcting 87 FR 8402, 

(February 15, 2022), beginning at page 

8405, column 2 as follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Corrected] 

■ 2. The FAA amends § 39.13 by: 

■ a. Removing airworthiness directive 

2013–26–01, Amendment 39–17710 (78 

FR 79295, December 30, 2013); and 

■ b. Adding the following new 

airworthiness directive: 

2022–02–03 CFM International, S.A.: 

Amendment 39–21900; Docket No. 

FAA–2021–0259; Project Identifier AD– 

2020–01128–E. 

(a) Effective Date 

This airworthiness directive (AD) is 

effective March 22, 2022. 

(b) Affected ADs 

This AD replaces AD 2013–26–01, 

Amendment 39–17710 (78 FR 79295, 

December 30, 2013). 

(c) Applicability 

This AD applies to CFM International, S.A. 

CFM56–3 and CFM56–7B model turbofan 

engines equipped with an accessory gearbox 

(AGB) assembly with the following part 

numbers (P/Ns): 

(1) For CFM56–3, CFM56–3B, and CFM56– 

3C model turbofan engines, AGB P/N: 335– 


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11290 Federal Register / Vol. 87, No. 40 / Tuesday, March 1, 2022 / Rules and Regulations 

300–103–0, 335–300–105–0, 335–300–106–0, 

335–300–107–0, 335–300–108–0, 335–300– 

109–0, or 335–300–110–0, installed. 

(2) For CFM56–7B20, CFM56–7B20/2, 

CFM56–7B20/3, CFM56–7B22, CFM56– 

7B22/2, CFM56–7B22/3, CFM56–7B22/3B1, 

CFM56–7B22/B1, CFM56–7B24, CFM56– 

7B24/2, CFM56–7B24/3, CFM56–7B24/3B1, 

CFM56–7B24/B1, CFM56–7B26, CFM56– 

7B26/2, CFM56–7B26/3, CFM56–7B26/3B1, 

CFM56–7B26/3B2, CFM56–7B26/3B2F, 

CFM56–7B26/3F, CFM56–7B26/B1, CFM56– 

7B26/B2, CFM56–7B27, CFM56–7B27/2, 

CFM56–7B27/3, CFM56–7B27/3B1, CFM56– 

7B27/3B1F, CFM56–7B27/3B3, CFM56– 

7B27/3F, CFM56–7B27/B1, and CFM56– 

7B27/B3 model turbofan engines, AGB P/N: 

340–046–503–0, 340–046–504–0, or 340– 

046–505–0, installed. 

(3) For CFM56–7B27A, CFM56–7B27A/3, 

or CFM56–7B27AE model turbofan engines, 

AGB P/N: 340–188–601–0, 340–188–603–0, 

or 340–188–605–0, installed. 

(d) Subject 

Joint Aircraft System Component (JASC) 

Code 7260, Turbine Engine Accessory Drive. 

(e) Unsafe Condition 

This AD was prompted by a dual engine 

loss of oil event and 42 prior events of total 

loss of engine oil during flight. The FAA is 

issuing this AD to prevent loss of engine oil 

while in flight. The unsafe condition, if not 

addressed, could result in engine failure, loss 

of thrust control, reduced control of the 

aircraft, and damage to the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Required Actions 

(1) After the effective date of this AD, after 

any maintenance that involves removal and 

re-installation of the AGB handcranking pad 

cover, perform an independent inspection to 

verify re-installation of the AGB 

handcranking pad cover; or 

(2) Prior to the next removal of the AGB 

handcranking pad cover from the engine, 

insert the independent inspection required 

by paragraph (g)(1) of this AD as a required 

inspection item in the existing approved 

continuous airworthiness maintenance 

program for the aircraft. 

(h) Mandatory Terminating Action 

As a mandatory terminating action to the 

requirements of paragraph (g) of this AD: 

(1) For affected CFM56–3, CFM56–3B, and 

CFM56–3C model turbofan engines, at the 

next engine shop visit, or before December 

31, 2026, whichever occurs first after the 

effective date of this AD, replace the affected 

AGB with a part eligible for installation. 

(2) For affected CFM56–7B model turbofan 

engines, except for CFM56–7B27A, CFM56– 

7B27A/3, and CFM56–7B27AE model 

turbofan engines, at the next engine shop 

visit, or before December 31, 2024, whichever 

occurs first after the effective date of this AD, 

replace the affected AGB with a part eligible 

for installation. 

(i) Definition 

(1) For the purpose of this AD, an ‘‘engine 

shop visit’’ is the induction of an engine into 

the shop for maintenance involving the 

separation of pairs of major mating engine 

case flanges, except for the following 

situations, which do not constitute an engine 

shop visit: 

(i) Separation of engine flanges solely for 

the purposes of transportation of the engine 

without subsequent maintenance; or 

(ii) Separation of engine flanges solely for 

the purpose of replacing the fan or propulsor 

without subsequent maintenance. 

(2) For the purpose of this AD, for affected 

CFM56–3, CFM56–3B, and CFM56–3C model 

turbofan engines, a part eligible for 

installation is: 

(i) An AGB with a P/N other than 335– 

300–103–0, 335–300–105–0, 335–300–106–0, 

335–300–107–0, 335–300–108–0, 335–300– 

109–0, 335–300–110–0; or 

(ii) An AGB that, using an FAA-approved 

procedure, has been re-worked with a 

dynamic oil seal in the handcranking pad 

cover assembly and re-identified with a new 

P/N not listed in paragraph (i)(2)(i) of this 

AD. 

Note 1 to paragraph (i)(2)(ii): Procedures to 

install a dynamic oil seal in the 

handcranking pad cover assembly can be 

found in CFM International SB CFM56–3 

S/B 72–1129, Revision 7, dated May 6, 2020. 

(3) For the purpose of this AD, for affected 

CFM56–7B model turbofan engines, except 

for CFM56–7B27A, CFM56–7B27A/3, and 

CFM56–7B27AE model turbofan engines, a 

part eligible for installation is: 

(i) An AGB with a P/N other than 340– 

046–503–0, 340–046–504–0, or 340–046– 

505–0; or 

(ii) An affected AGB that, using an FAAapproved procedure, has been re-worked 

with a dynamic oil seal in the handcranking 

pad cover assembly and re-identified with a 

new P/N not listed in paragraph (i)(3)(i) of 

this AD. 

Note 2 to paragraph (i)(3)(ii): Procedures to 

install a dynamic oil seal in the 

handcranking pad cover assembly can be 

found in CFM International SB CFM56–7B 

S/B 72–0879, Revision 7, dated February 10, 

2021, CFM56–7B S/B 72–0564, Revision 9, 

dated December 3, 2021, or CFM56–7B S/B 

72–1071, initial issue, dated December 3, 

2021. 

(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 certification office, 

send it to the attention of the person 

identified in paragraph (k) of this AD. You 

may email your request to: ANE-AD-AMOC@

faa.gov. 

(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 

For more information about this AD, 

contact Kevin Clark, Aviation Safety 

Engineer, ECO Branch, FAA, 1200 District 

Avenue, Burlington, MA 01803; phone: (781) 

238–7088; fax: (781) 238–7199; email: 

kevin.m.clark@faa.gov. 

(l) Material Incorporated by Reference 

None. 

Issued on February 23, 2022. 

Derek Morgan, 

Acting Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2022–04149 Filed 2–28–22; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 95 

[Docket No. 31417; Amdt. No. 564] 

IFR Altitudes; Miscellaneous 

Amendments 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This document adopts 

miscellaneous amendments to the 

required IFR (instrument flight rules) 

altitudes and changeover points for 

certain Federal airways, jet routes, or 

direct routes for which a minimum or 

maximum en route authorized IFR 

altitude is prescribed. This regulatory 

action is needed because of changes 

occurring in the National Airspace 

System. These changes are designed to 

provide for the safe and efficient use of 

the navigable airspace under instrument 

conditions in the affected areas. 

DATES: 0901 UTC, effective March 24, 

2022. 

FOR FURTHER INFORMATION CONTACT: 

Thomas J. Nichols, Flight Procedures 

and Airspace Group, Flight 

Technologies and Procedures Division, 

Flight Standards Service, Federal 

Aviation Administration. Mailing 

Address: FAA Mike Monroney 

Aeronautical Center, Flight Procedures 

and Airspace Group, 6500 South 

MacArthur Blvd., Registry Bldg. 29 

Room 104, Oklahoma City, OK 73125. 

Telephone: (405) 954–4164. 

SUPPLEMENTARY INFORMATION: This 

amendment to part 95 of the Federal 

Aviation Regulations (14 CFR part 95) 

amends, suspends, or revokes IFR 

altitudes governing the operation of all 

aircraft in flight over a specified route 

or any portion of that route, as well as 

the changeover points (COPs) for 


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