Egg Products Inspection Regulations; Correction

• Citation: 86 FR 60549
• Record Number: 2021-23703
• Published date: 03 November 2021
• Section: Rules and Regulations
• Court: Food Safety And Inspection Service

This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents.

Rules and Regulations Federal Register

60549

Vol. 86, No. 210

Wednesday, November 3, 2021

DEPARTMENT OF AGRICULTURE

Food Safety and Inspection Service

9 CFR Part 590

[Docket No. FSIS–2005–0015]

RIN 0583–AC58

Egg Products Inspection Regulations;

Correction

AGENCY

: Food Safety and Inspection

Service, Department of Agriculture

(USDA).

ACTION

: Correcting amendment.

SUMMARY

: The Food Safety and

Inspection Service (FSIS) is correcting

its regulations requiring official plants

that process egg products (herein also

referred to as ‘‘egg products plants’’ or

‘‘plants’’) to develop and implement

Hazard Analysis and Critical Control

Point (HACCP) Systems and Sanitation

Standard Operating Procedures

(Sanitation SOPs) and to meet other

sanitation requirements consistent with

FSIS’ meat and poultry regulations.

DATES

: This correction is effective

November 3, 2021, except for

amendatory instructions 3 and 5, which

are effective October 31, 2022.

FOR FURTHER INFORMATION CONTACT

:

Victoria Levine, Program Analyst, Office

of Policy and Program Development by

telephone at (202) 690–3184.

SUPPLEMENTARY INFORMATION

: FSIS is

making changes to the egg products

inspection regulations because plants

that have not already implemented

HACCP will continue to need to meet

the times and temperatures contained in

Table 1 of 9 CFR 590.530 and the times

and temperatures found in 9 CFR

590.536 until the HACCP regulations

become effective on October 31, 2022.

List of Subjects in 9 CFR Part 590

Eggs and egg products, Exports, Food

grades and standards, Food labeling,

Imports, Reporting and recordkeeping

requirements.

For the reasons set out in the

preamble, 9 CFR part 590 is corrected by

making the following correcting

amendments:

PART 590—INSPECTION OF EGGS

AND EGG PRODUCTS (EGG

PRODUCTS INSPECTION ACT)

■1. The authority citation for part 590

continues to read as follows:

Authority: 21 U.S.C. 1031–1056; 7 CFR

2.18, 2.53.

■2. Add § 590.530 to read as follows:

§ 590.530 Liquid egg cooling.

(a) through (b) [Reserved]

(c) The cooling and temperature

requirements for liquid egg products

shall be as specified in Table 1 to this

section.

T

ABLE

1

TO

§ 590.530—M

INIMUM

C

OOLING AND

T

EMPERATURE

R

EQUIREMENTS FOR

L

IQUID

E

GG

P

RODUCTS

[Unpasterurized product temperature within 2 hours from time of breaking]

Product

Liquid (other

than salt

product) to be

held

8 hours or less

Liquid (other

than salt

product) to be

held in excess

of

8 hours

Liquid salt

product Temperature within 2 hours after

pasteurization Temperature within 3 hours after

stabilization

Whites (not to be

stabilized). 55 °F or lower ... 45 °F or lower ... .......................... 45 °F or lower.

Whites (to be sta-

bilized). 70 °F or lower ... 55 °F or lower ... .......................... 55 °F or lower ............................. (

1

).

All other product

(except product

with 10 percent

or more salt

added).

45 °F or lower ... 40 °F or lower ... .......................... If to be held 8 hours or less

45 °F or lower. If to be held in

excess of 8 hours, 40 °F or

lower.

If to be held 8 hours or less,

45 °F or lower. If to be held in

excess of 8 hours, 40 °F or

lower.

Liquid egg prod-

uct with 10 per-

cent or more

salt added.

.......................... .......................... If to be held 30

hours or less,

65 °F or

lower. If to be

held in ex-

cess of 30

hours, 45 °F

or lower.

65 °F or lower

2

.

1

Stabilized liquid whites shall be dried as soon as possible after removal of glucose. The storage of stabilized liquid whites shall be limited to

that necessary to provide a continuous operation.

2

The cooling process shall be continued to assure that any salt product to be held in excess of 24 hours is cooled and maintained at 45 °F or

lower.

(d) Upon written request and under

such conditions as may be prescribed by

the National Supervisor, liquid cooling

and holding temperatures not otherwise

provided for in this section may be

approved.

(e) through (g) [Reserved]

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60550

Federal Register / Vol. 86, No. 210 / Wednesday, November 3, 2021 / Rules and Regulations

§ 590.530 [Removed]

■3. Effective October 31, 2022, remove

§ 590.530.

§ 590.536 [Amended]

■4. Add § 590.536 to read as follows:

§ 590.536 Freezing operations.

(a) [Reserved]

(b)(1) Nonpasteurized egg products

which are to be frozen shall be solidly

frozen or reduced to a temperature of

10 °F or lower within 60 hours from

time of breaking.

(2) Pasteurized egg products which

are to be frozen shall be solidly frozen

or reduced to a temperature of 10 °F or

lower within 60 hours from time of

pasteurization.

(3) The temperature of the products

not solidly frozen shall be taken at the

center of the container to determine

compliance with this section.

(c) through (e) [Reserved]

§ 590.536 [Removed]

■5. Effective October 31, 2022, remove

§ 590.536.

Done at Washington, DC.

Theresa Nintemann,

Deputy Administrator.

[FR Doc. 2021–23703 Filed 11–2–21; 8:45 am]

BILLING CODE 3410–DM–P

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA–2021–0836; Project

Identifier MCAI–2020–01629–E; Amendment

39–21759; AD 2021–20–21]

RIN 2120–AA64

Airworthiness Directives; GE Aviation

Czech s.r.o. (Type Certificate

Previously Held by WALTER Engines

a.s., Walter a.s., and MOTORLET a.s.)

Turboprop Engines

AGENCY

: Federal Aviation

Administration (FAA), DOT.

ACTION

: Final rule; request for

comments.

SUMMARY

: The FAA is superseding

Airworthiness Directive (AD) 2018–16–

10 which applied to certain GE Aviation

Czech s.r.o. (GEAC) H80–200 model

turboprop engines. AD 2018–16–10

required an adjustment of the engine

push-pull control and replacement of

the beta switch to prevent the propeller

governor control from going to a

negative thrust position. This AD

requires an initial inspection and

adjustment of the engine push-pull

control and replacement of the beta

switch. This AD also requires inspection

and adjustment of the engine push-pull

control after any maintenance, repair or

modification that affects the push-pull

control and installation of an improved

push-pull control. This AD also expands

the applicability to include GEAC H85–

200 model turboprop engines with Avia

Propeller AV–725 propellers installed.

This AD was prompted by an accident

involving an Aircraft Industries (AI) L

410 UVP–E20 airplane caused by one

propeller going to a negative thrust

position during the landing approach.

The FAA is issuing this AD to address

the unsafe condition on these products.

DATES

: This AD is effective November

18, 2021.

The Director of the Federal Register

approved the incorporation by reference

of certain publications listed in this AD

as of November 18, 2021.

The FAA must receive any comments

on this AD by December 20, 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 GE Aviation

Czech s.r.o., Beranovy

´ch 65, 199 02

Praha 9, Letn

ˇany, Czech Republic;

phone: +420 222 538 111. 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 (781) 238–

7759. It is also available at https://

www.regulations.gov by searching for

and locating Docket No. FAA–2021–

0836.

Examining the AD Docket

You may examine the AD docket at

https://www.regulations.gov by

searching for and locating Docket No.

FAA–2021–0836; 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, the mandatory continuing

airworthiness information (MCAI), any

comments received, and other

information. The street address for the

Docket Operations is listed above.

FOR FURTHER INFORMATION CONTACT

:

Barbara Caufield, Aviation Safety

Engineer, ECO Branch, FAA, 1200

District Avenue, Burlington, MA 01803;

phone: (781) 238–7146; fax: (781) 238–

7199; email: barbara.caufield@faa.gov.

SUPPLEMENTARY INFORMATION

:

Background

The FAA issued AD 2018–16–10,

Amendment 39–19350 (83 FR 43742,

August 28, 2018) (AD 2018–16–10), for

certain GE Aviation Czech H80–200

model turboprop engines. AD 2018–16–

10 required replacement of the beta

switch and adjustment of the engine

push-pull control to prevent the

propeller governor control from going to

a negative thrust position. AD 2018–16–

10 resulted from an accident involving

an AI L 410 UVP–E20 airplane caused

by one propeller going to a negative

thrust position during the landing

approach. The FAA issued AD 2018–

16–10 to require engine modification to

prevent asymmetric thrust. The unsafe

condition, if not addressed, could result

in failure of the beta switch, loss of

engine thrust control, and reduced

control of the airplane.

Actions Since AD 2018–16–10 Was

Issued

Since the FAA issued AD 2018–16–

10, the European Union Aviation Safety

Agency (EASA), which is the Technical

Agent for the Member States of the

European Community, has issued EASA

AD 2020–0143, dated June 25, 2020, to

address an unsafe condition for the

specified products. The MCAI states:

In 2017, a fatal accident was reported of an

L 410 UVP–E20 aeroplane. The investigation

determined that there was an annunciation of

Beta mode on the right-hand engine, that the

propeller went inadvertently beyond the fine

pitch position and reached a negative thrust

position, and that the pitch lock system did

not intervene. The event occurred on

approach at a speed and altitude which did

not allow the flight crew to recover this

control system malfunction.

This condition, if not corrected, could lead

to reduced control or loss of control of the

aeroplane.

To address this unsafe condition, GEAC

issued the SB, providing inspection and

modification instructions, and EASA issued

AD 2018–0075 to require a one-time

inspection and adjustment of the engine

push-pull control and replacement of the

beta switch with an improved part.

Addressing the same unsafe condition at

aeroplane level, EASA also issued AD 2018–

0057, requiring modification of affected AI L

410 UVP–E20 and L 410 UVP–E20 CARGO

aeroplanes, if equipped with H80–200

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