Federal Register / Vol. 85, No. 240 / Monday, December 14, 2020 / Rules and Regulations 80589 

§ 121.301 What size standards and 

affiliation principles are applicable to 

financial assistance programs? 

* * * * * 

(f) * * * 

(4) Affiliation based on identity of 

interest. Affiliation arises when there is 

an identity of interest between close 

relatives, as defined in 13 CFR 120.10, 

with identical or substantially identical 

business or economic interests (such as 

where the close relatives operate 

concerns in the same or similar industry 

in the same geographic area). Where 

SBA determines that interests should be 

aggregated, an individual or firm may 

rebut that determination with evidence 

showing that the interests deemed to be 

one are in fact separate. 

(5) Affiliation based on franchise and 

license agreements. The restraints 

imposed on a franchisee or licensee by 

its franchise or license agreement 

generally will not be considered in 

determining whether the franchisor or 

licensor is affiliated with an applicant 

franchisee or licensee provided the 

applicant franchisee or licensee has the 

right to profit from its efforts and bears 

the risk of loss commensurate with 

ownership. SBA will only consider the 

franchise or license agreements of the 

applicant concern. 

* * * * * 

■ 23. Amend § 121.302 by revising 

paragraphs (a) and (b) to read as follows: 

§ 121.302 When does SBA determine the 

size status of an applicant? 

(a) The size status of an applicant for 

SBA financial assistance is determined 

as of the date the application for 

financial assistance is accepted for 

processing by SBA, except for 

applications under the Preferred 

Lenders Program (PLP), the Disaster 

Loan program, the SBIC program, and 

the New Markets Venture Capital 

(NMCV) program. 

(b) For the Preferred Lenders Program, 

size is determined as of the date of 

approval of the loan by the Preferred 

Lender. 

* * * * * 

Jovita Carranza, 

Administrator. 

[FR Doc. 2020–26450 Filed 12–11–20; 8:45 am] 

BILLING CODE 8026–03–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2020–1031; Project 

Identifier AD–2020–00846–T; Amendment 

39–21334; AD 2020–24–04] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Airplanes 

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. That 

AD applies to all The Boeing Company 

Model 787–8, 787–9, and 787–10 

airplanes. As published, the regulatory 

text of the AD included errors in certain 

references to the airplane flight manual 

(AFM) that is required to be revised. 

This document corrects those errors. In 

all other respects, the original document 

remains the same. 

DATES: This correction is effective 

December 18, 2020. The effective date of 

AD 2020–24–04 remains December 18, 

2020. 

ADDRESSES: You may examine the AD 

docket at https://www.regulations.gov; 

or in person at the Docket Management 

Facility 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: 

Frank Carreras, Aerospace Engineer, 

Systems and Equipment Section, FAA, 

Seattle ACO Branch, 2200 South 216th 

St., Des Moines, WA 98198; phone and 

fax: 206–231–3539; email: 

frank.carreras@faa.gov. 

SUPPLEMENTARY INFORMATION: As 

published, Airworthiness Directive 

2020–24–04, Amendment 39–21334 (85 

FR 77991, December 3, 2020), requires 

revising the existing AFM to incorporate 

procedures for conducting an approach 

with a localizer-based navigation aid, 

monitoring localizer raw data, calling 

out any significant deviations, and 

performing an immediate go around if 

the airplane has not intercepted the 

final approach course as shown by the 

localizer deviation. AD 2020–24–04 

applies to all The Boeing Company 

Model 787–8, 787–9, and 787–10 

airplanes. 

As published, the regulatory text 

included errors in certain references to 

the AFM that is required to be revised. 

The location of the AFM text to be 

revised is incorrectly identified as the 

‘‘Limitations section’’; the correct 

location is the ‘‘Operating Procedures 

chapter.’’ In addition, the figure 

incorrectly identified the heading of the 

AFM text as ‘‘Operating Instructions’’; 

the correct heading is ‘‘Autopilot Flight 

Director System—Operating 

Instructions.’’ 

Correction of Publication 

This document corrects an error and 

correctly adds the AD as an amendment 

to 14 CFR 39.13. Although no other part 

of the preamble or regulatory 

information has been corrected, the 

FAA is publishing the entire rule in the 

Federal Register. 

The effective date of this AD remains 

December 18, 2020. 

Since this action only corrects errors 

in certain AFM references, it has no 

adverse economic impact and imposes 

no additional burden on any person. 

Therefore, the FAA has determined that 

notice and public comment procedures 

are unnecessary. 

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) 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 adding 

the following new airworthiness 

directive (AD): 

2020–24–04 The Boeing Company: 

Amendment 39–21334; Docket No. 

FAA–2020–1031; Project Identifier AD– 

2020–00846–T. 

(a) Effective Date 

This AD is effective December 18, 2020. 

(b) Affected ADs 

None. 


jbell on DSKJLSW7X2PROD with RULES
80590 Federal Register / Vol. 85, No. 240 / Monday, December 14, 2020 / Rules and Regulations 

(c) Applicability 

This AD applies to all The Boeing 

Company Model 787–8, 787–9, and 787–10 

airplanes, certificated in any category. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 22, Auto flight. 

(e) Unsafe Condition 

This AD was prompted by reports 

indicating that the autopilot flight director 

system (AFDS) failed to transition to the 

instrument landing system localizer (LOC) 

beam after the consistent localizer capture 

function in the flight control modules 

initiated a transition to capture LOC during 

approach. The FAA is issuing this AD to 

address the AFDS failing to transition, which 

could result in localizer overshoot leading to 

glideslope descent on the wrong heading. 

Combined with a lack of flight deck effects 

for a consistent localizer capture mode 

failure, this condition could result in a 

controlled flight into terrain. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Revise the Airplane Flight Manual (AFM) 

Within 14 days after the effective date of 

this AD, revise the Operating Procedures 

chapter of the existing AFM and applicable 

corresponding operational procedures to 

incorporate the procedures specified in figure 

1 to paragraph (g) of this AD. Revising the 

existing AFM to include the changes 

specified in paragraph (g) of this AD may be 

done by inserting a copy of figure 1 to 

paragraph (g) of this AD into the existing 

AFM. 

(h) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle ACO 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 (i) of this 

AD. Information may be emailed to: 9-ANMSeattle-ACO-AMOC-Requests@faa.gov. 

(2) Before using any approved AMOC, 

notify your appropriate principal inspector, 

or lacking a principal inspector, the manager 

of the responsible Flight Standards Office. 

(3) An AMOC that provides an acceptable 

level of safety may be used for any repair, 

modification, or alteration required by this 

AD if it is approved by The Boeing Company 

Organization Designation Authorization 

(ODA) that has been authorized by the 

Manager, Seattle ACO Branch, FAA, to make 

those findings. To be approved, the repair 

method, modification deviation, or alteration 

deviation must meet the certification basis of 

the airplane, and the approval must 

specifically refer to this AD. 

(i) Related Information 

For more information about this AD, 

contact Frank Carreras, Aerospace Engineer, 

Systems and Equipment Section, FAA, 

Seattle ACO Branch, 2200 South 216th St., 

Des Moines, WA 98198; phone and fax: 206– 

231–3539; email: frank.carreras@faa.gov. 

(j) Material Incorporated by Reference 

None. 

Issued on December 9, 2020. 

Ross Landes, 

Deputy Director for Regulatory Operations, 

Compliance & Airworthiness Division, 

Aircraft Certification Service. 

[FR Doc. 2020–27507 Filed 12–10–20; 11:15 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2020–1117; Project 

Identifier MCAI–2020–01429–E; Amendment 

39–21361; AD 2020–26–06] 

RIN 2120–AA64 

Airworthiness Directives; Technify 

Motors GmbH (Type Certificate 

Previously Held by Thielert Aircraft 

Engines GmbH) Reciprocating Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for certain 

Technify Motors GmbH TAE 125–02–99 

and TAE 125–02–114 model 

reciprocating engines. This AD was 

prompted by a report of a defective 

turbocharger hose discovered on an 

airplane during a pre-flight inspection. 

This AD requires the removal and 

replacement of the affected turbocharger 

hose. The FAA is issuing this AD to 

address the unsafe condition on these 

products. 

DATES: This AD is effective December 

29, 2020. 

The FAA must receive comments on 

this AD by January 28, 2021. 

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 

https://www.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. 

For service information identified in 

this final rule, contact Continental 

Aerospace Technologies GmbH, 

Platanenstrasse 14, 09356 Sankt 

Egidien, Germany; phone: +49 37204 

696 0; email: support@

continentaldiesel.com; website: 

www.continentaldiesel.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 


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