81360 Federal Register / Vol. 76, No. 249 / Wednesday, December 28, 2011 / Rules and Regulations 

PART 301—DOMESTIC QUARANTINE 

NOTICES 

Accordingly, we are adopting as a 

final rule, without change, the interim 

rule that amended 7 CFR part 301 and 

that was published at 76 FR 52543– 

52544 on August 23, 2011. 

Done in Washington, DC, this 19th day of 

December 2011. 

Kevin Shea, 

Acting Administrator, Animal and Plant 

Health Inspection Service. 

[FR Doc. 2011–33204 Filed 12–27–11; 8:45 am] 

BILLING CODE 3410–34–P 

DEPARTMENT OF AGRICULTURE 

Food Safety and Inspection Service 

9 CFR Parts 332 and 381 

[Docket No. FSIS–2008–0039] 

RIN 0583–AD37 

Cooperative Inspection Programs: 

Interstate Shipment of Meat and 

Poultry Products; Correction 

AGENCY: Food Safety and Inspection 

Service, USDA. 

ACTION: Correcting amendments. 

SUMMARY: This document corrects 

typographical errors in the final 

regulations establishing a new voluntary 

cooperative program under which 

certain very small and small State– 

inspected establishments will be eligible 

to ship meat and poultry products in 

interstate commerce. The final rule was 

published in the Federal Register on 

May 2, 2011, and became effective on 

July 1, 2011. 

DATES: December 28, 2011. 

FOR FURTHER INFORMATION CONTACT: 

Charles Williams, Acting Director, 

Policy Issuance Division, Office of 

Policy and Program Development, Food 

Safety and Inspection Service, U.S. 

Department of Agriculture, Washington, 

DC 20250; (202) 720–5627; Fax (202) 

690–0486. 

SUPPLEMENTARY INFORMATION: 

Background 

On May 2, 2011, FSIS published in 

the Federal Register, the final rule, 

‘‘Cooperative Inspection Programs; 

Interstate Shipment of Meat and Poultry 

Products’’ (76 FR 24714). The final rule 

amended the Federal meat and poultry 

products inspection regulations to 

establish a new cooperative inspection 

program under which State-inspected 

establishments with 25 or fewer 

employees on average will be permitted 

ship meat and poultry products in 

interstate commerce. Two of the 

instructions for amending the 

regulations created typographical errors 

in the resulting regulatory language. The 

amendments in this document correct 

those errors. 

List of Subjects 

9 CFR Part 332 

Grant programs-agriculture, 

Intergovernmental relations, Meat 

inspection. 

9 CFR Part 381 

Grant programs-agriculture, 

Intergovernmental relations, Poultry and 

poultry products. 

Accordingly, 9 CFR parts 332 and 381 

are corrected by making the following 

correcting amendments: 

PART 332—SELECTED 

ESTABLISHMENTS; COOPERATIVE 

PROGRAM FOR INTERSTATE 

SHIPMENT OF CARCASSES, PARTS 

OF CARCASSES, MEAT, AND MEAT 

FOOD PRODUCTS 

■ 1. The authority citation for part 332 

continues to read as follows: 

Authority: 21 U.S.C. 601–695; 7 U.S.C. 

138–138i, 450, 1901–1906; 7 CFR 2.7, 2.18, 

2.53. 

§ 332.3 [Amended] 

■ 2. Amend § 332.3 as follows: 

■ a. In paragraph (c)(7) remove ‘‘and’’ 

after the semicolon. 

■ b. In paragraph (c)(8) remove the 

period at the end of the paragraph and 

add ‘‘; and’’ in its place. 

PART 381—POULTRY PRODUCTS 

INSPECTION REGULATIONS 

■ 3. The authority citation for part 381 

continues to read: 

Authority: 21 U.S.C. 451–472; 7 CFR 2.18, 

2.53. 

§ 381.513 [Amended] 

■ 4. Amend § 381.513 as follows: 

■ a. In paragraph (c)(7) remove ‘‘and’’ 

after the semicolon. 

■ b. In paragraph (c)(8) remove the 

period at the end of the paragraph and 

add ‘‘; and’’ in its place. 

Done in Washington, DC, on: December 19, 

2011. 

Alfred V. Almanza, 

Administrator. 

[FR Doc. 2011–32877 Filed 12–27–11; 8:45 am] 

BILLING CODE 3410–DM–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 25 

[Docket No. FAA–2011–1172: Special 

Conditions No. 25–453–SC] 

Special Conditions: Gulfstream 

Aerospace LP (GALP) Model G280 

Airplane, Operation Without Normal 

Electrical Power 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final special conditions. 

SUMMARY: These special conditions are 

issued for the Gulfstream Aerospace LP 

(GALP) Model G280 airplane. This 

airplane will have a novel or unusual 

design feature associated with operation 

without normal electrical power. The 

applicable airworthiness regulations do 

not contain adequate or appropriate 

safety standards for this design feature. 

These special conditions contain the 

additional safety standards that the 

Administrator considers necessary to 

establish a level of safety equivalent to 

that established by the existing 

airworthiness standards. 

DATES: Effective Date: The effective date 

of these special conditions is December 

20, 2011. 

FOR FURTHER INFORMATION CONTACT: 

Nazih Khaouly, Transport Airplane 

Directorate, Aircraft Certification 

Service, 1601 Lind Avenue SW., 

Renton, Washington 98057–3356; 

telephone (425) 227–2432; facsimile 

(425) 227–1149. 

SUPPLEMENTARY INFORMATION: 

Background 

On March 30, 2006, GALP applied for 

a type certificate for their new Model 

G280 airplane. The Model G280 will 

have a novel or unusual design feature 

associated with operation without 

normal electrical power. 

Type Certification Basis 

Under the provisions of Title 14, Code 

of Federal Regulations (14 CFR) 21.17, 

GALP must show that the Model G280 

airplane meets the applicable provisions 

of part 25 as amended by Amendments 

25–1 through 25–117. 

If the Administrator finds that the 

applicable airworthiness regulations 

(i.e., 14 CFR part 25) do not contain 

adequate or appropriate safety standards 

for the Model G280 airplane because of 

a novel or unusual design feature, 

special conditions are prescribed under 

the provisions of § 21.16. 

Special conditions are initially 

applicable to the model for which they 

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Federal Register / Vol. 76, No. 249 / Wednesday, December 28, 2011 / Rules and Regulations 81361 

are issued. Should the type certificate 

for that model be amended later to 

include any other model that 

incorporates the same novel or unusual 

design feature, the special conditions 

would also apply to the other model. 

In addition to the applicable 

airworthiness regulations and special 

conditions, the Model G280 airplane 

must comply with the fuel-vent and 

exhaust-emission requirements of part 

34 and the noise-certification 

requirements of part 36; and the FAA 

must issue a finding of regulatory 

adequacy under § 611 of Public Law 92– 

574, the ‘‘Noise Control Act of 1972.’’ 

The FAA issues special conditions, as 

defined in 14 CFR 11.19, in accordance 

with § 11.38, and they become part of 

the type-certification basis under 

§ 21.17(a)(2). 

Novel or Unusual Design Features 

The Model G280 airplane will 

incorporate the following novel or 

unusual design features: 

The Model G280 airplane is equipped 

with electrical and electronic systems 

that control critical functions and 

systems. Examples of these include the 

electronic displays, rudder, brakes, 

spoilers, flaps, and electronic engine 

controls. The Model G280 electricalpower generation and distribution 

architecture is equipped with an 

auxiliary power unit (APU) and is not 

equipped with a Ram Air Turbine (RAT) 

generator. The loss of all electrical 

power to certain functions and systems 

impacts the airplane’s ability to land 

safely. Therefore, these special 

conditions are issued to retain the level 

of safety intended by the current 

§ 25.1351(d). 

Discussion 

The Model G280 airplane requires a 

continuous source of electrical power 

for continued safe flight and landing. 

The current regulation in § 25.1351(d), 

‘‘Operation without normal electrical 

power,’’ states that the airplane must be 

operated safely in visual-flight-rules 

conditions, for a period of not less than 

five minutes, with the normal electrical 

power (electrical power sources 

excluding the battery) inoperative. This 

rule was structured around a traditional 

design utilizing mechanical controls for 

flight systems while the crew took time 

to sort out the electrical failure, start 

engine(s) if necessary, and re-establish 

some of the electrical-power-generation 

capability. 

To maintain the same level of safety 

associated with traditional designs, the 

Model G280 airplane electrical-system 

design must not be time-limited in its 

operation. It should be noted that 

service experience has shown that the 

loss of all electrical power, which is 

generated by the airplane’s engine 

generators or APU is not extremely 

improbable. Thus, it must be 

demonstrated that the airplane can 

continue through safe flight and landing 

(including steering and braking on 

ground for airplanes using steer/brakeby-wire) with the use of its emergency 

electrical-power systems. These 

emergency electrical-power systems 

must be able to power loads that are 

required for continued safe flight and 

landing. 

Discussion of Comments 

Notice of proposed special conditions 

no. 25–11–17–SC for the GALP Model 

G280 airplanes was published in the 

Federal Register on October 27, 2011 

(76 FR 66660). No comments were 

received, and the special conditions are 

adopted as proposed. 

Applicability 

As discussed above, these special 

conditions are applicable to the GALP 

Model G280 airplane. Should GALP 

apply at a later date for a change to the 

type certificate to include another 

model incorporating the same novel or 

unusual design feature, the special 

conditions would apply to that model as 

well. 

Under standard practice, the effective 

date of final special conditions would 

be 30 days after the date of publication 

in the Federal Register; however, as the 

certification date for the GALP Model 

G280 airplane is imminent, the FAA 

finds good cause to make these special 

conditions effective upon issuance. 

Conclusion 

This action affects only certain novel 

or unusual design features on the GALP 

Model G280 airplane. It is not a rule of 

general applicability and it affects only 

the applicant who applied to the FAA 

for approval of these features on the 

airplane. 

List of Subjects in 14 CFR Part 25 

Aircraft, Aviation safety, Reporting 

and recordkeeping requirements. 

The authority citation for these 

special conditions is as follows: 

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

44702, 44704. 

The Special Conditions 

Accordingly, pursuant to the 

authority delegated to me by the 

Administrator, the following special 

conditions are issued as part of the typecertification basis for GALP Model G280 

airplanes. The special conditions are 

issued in lieu of 14 CFR 25.1351(d) and 

are required to ensure that the airplane 

has sufficient electrical power for 

continued safe flight and landing. 

1. The applicant must show by test or 

a combination of test and analysis that 

the airplane is capable of continued safe 

flight and landing with all normal 

electrical power sources inoperative, as 

prescribed by paragraphs (1)(a) and 

(1)(b) below. 

For purposes of this special condition, 

normal sources of electrical-power 

generation do not include any alternate 

power sources such as a battery, ram-air 

turbine (RAT), or independent power 

systems such as the flight-control 

permanent-magnet generating system. 

In showing capability for continued 

safe flight and landing, consideration 

must be given to systems capability, 

effects on crew workload and operating 

conditions, and the physiological needs 

of the flightcrew and passengers for the 

longest diversion time for which 

approval is sought. 

a. Common-cause failures, cascading 

failures, and zonal physical threats must 

be considered in showing compliance 

with this requirement. 

b. The ability to restore operation of 

portions of the electrical-power 

generation and distribution system may 

be considered if it can be shown that 

unrecoverable loss of those portions of 

the system is extremely improbable. An 

alternative source of electrical power 

must be provided for the time required 

to restore the minimum electricalpower-generation capability required for 

safe flight and landing. Unrecoverable 

loss of all engines may be excluded 

when showing that unrecoverable loss 

of critical portions of the electrical 

system is extremely improbable. 

Unrecoverable loss of all engines is 

covered in special condition 2, below, 

and thus may be excluded when 

showing compliance with this 

requirement. 

2. Regardless of any electricalgeneration and distribution-system 

recovery capability shown under special 

condition 1, above, sufficient electricalsystem capability must be provided to: 

a. Allow time to descend, with all 

engines inoperative, at the speed that 

provides the best glide slope, from the 

maximum operating altitude to the 

altitude at which the soonest possible 

engine restart could be accomplished, 

and 

b. Subsequently allow multiple start 

attempts of the engines and APU. This 

capability must be provided in addition 

to the electrical capability required by 

existing part 25 requirements related to 

operation with all engines inoperative. 

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81362 Federal Register / Vol. 76, No. 249 / Wednesday, December 28, 2011 / Rules and Regulations 

3. The airplane emergency electricalpower system must be designed to 

supply: 

a. Electrical power required for 

immediate safety, which must continue 

to operate without the need for crew 

action following the loss of the normal 

electrical power, for a duration 

sufficient to allow reconfiguration to 

provide a non-time-limited source of 

electrical power. 

b. Electrical power required for 

continued safe flight and landing for the 

maximum diversion time. 

4. If APU-generated electrical power 

is used in satisfying the requirements of 

these special conditions, and if reaching 

a suitable runway upon which to land 

is beyond the capacity of the battery 

systems, then the APU must be able to 

be started under any foreseeable flight 

condition prior to the depletion of the 

battery or the restoration of normal 

electrical power, whichever occurs first. 

Flight tests must demonstrate this 

capability at the most critical condition. 

a. It must be shown that the APU will 

provide adequate electrical power for 

continued safe flight and landing. 

b. The Airplane Flight Manual (AFM) 

must incorporate non-normal 

procedures that direct the pilot to take 

appropriate actions to activate the APU 

after loss of normal engine-driven 

generated electrical power. 

As a part of showing compliance with 

these special conditions, the tests by 

which loss of all normal electrical 

power is demonstrated must also take 

into account the following: 

1. The failure condition should be 

assumed to occur during night 

instrument meteorological conditions 

(IMC), at the most critical phase of the 

flight, relative to the worst possible 

electrical-power distribution and 

equipment-loads-demand condition. 

2. After the un-restorable loss of 

normal engine generator power, the 

airplane-engine-restart capability must 

be provided and operations continued 

in IMC. 

3. It should be demonstrated that the 

aircraft is capable of continued safe 

flight and landing. The length of time 

must be computed based on the 

maximum diversion-time capability for 

which the airplane is being certified. 

Consideration for airspeed reductions 

resulting from the associated failure or 

failures must be made. 

4. The airplane must provide 

adequate indication of loss of normal 

electrical power to direct the pilot to the 

non-normal procedures, and the AFM 

must incorporate non-normal 

procedures that will direct the pilot to 

take appropriate actions. 

Issued in Renton, Washington, on 

December 20, 2011. 

K.C. Yanamura, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2011–33281 Filed 12–27–11; 8:45 am] 

BILLING CODE 4910–13–P 

JOINT BOARD FOR THE 

ENROLLMENT OF ACTUARIES 

20 CFR Part 901 

[TD 9517] 

RIN 1545–BC82 

Regulations Governing the 

Performance of Actuarial Services 

Under the Employee Retirement 

Income Security Act of 1974; 

Correction 

AGENCY: Joint Board for the Enrollment 

of Actuaries. 

ACTION: Correction to final regulations. 

SUMMARY: This document contains 

corrections to final regulations (TD 

9517) that were published in the 

Federal Register on Thursday, March 

31, 2011 (76 FR 17762) relating to the 

enrollment of actuaries. 

DATES: This correction is effective on 

December 28, 2011, and is applicable on 

March 31, 2011. 

FOR FURTHER INFORMATION CONTACT: 

Patrick McDonough, Executive Director, 

Joint Board for the Enrollment of 

Actuaries, at (202) 622–8229 (not a tollfree number). 

SUPPLEMENTARY INFORMATION: 

Background 

The final regulations (TD 9517) that 

are the subject of this correction are 

under section 3042 of the Employee 

Retirement Income Security Act of 1974 

(88 Stat. 829), Public Law 93–406 

(ERISA). 

Need for Correction 

As published, final regulations (TD 

9517) contain errors that may prove to 

be misleading and are in need of 

clarification. 

Correction of Publication 

Accordingly, the publication of the 

final regulations (TD 9517) which were 

the subject of FR Doc. 2011–7573 is 

corrected as follows: 

On page 17762, column 1, in the 

preamble, under the paragraph heading 

‘‘Paperwork Reduction Act’’, last 

paragraph of the column, fourth line, 

the language ‘‘901.11(f)(2)(D), 

901.11(f)(2)(G) and (H),’’ is corrected to 

read ‘‘901.11(f)(2)(i)(D), 

901.11(f)(2)(i)(G) and (H),’’. 

Guy R. Traynor, 

Acting Chief, Publications and Regulations 

Branch, Legal Processing Division, Associate 

Chief Counsel, (Procedure and 

Administration). 

[FR Doc. 2011–33197 Filed 12–27–11; 8:45 am] 

BILLING CODE 4810–25–P 

JOINT BOARD FOR THE 

ENROLLMENT OF ACTUARIES 

20 CFR Part 901 

[TD 9517] 

RIN 1545–BC82 

Regulations Governing the 

Performance of Actuarial Services 

Under the Employee Retirement 

Income Security Act of 1974; 

Correction 

AGENCY: Joint Board for the Enrollment 

of Actuaries. 

ACTION: Correcting amendment. 

SUMMARY: This document describes 

correcting amendments to final 

regulations (TD 9517) relating to the 

enrollment of actuaries. These 

regulations were published in the 

Federal Register on Thursday, March 

31, 2011 (76 FR 17762). 

DATES: This correction is effective on 

December 28, 2011, and is applicable on 

March 31, 2011. 

FOR FURTHER INFORMATION CONTACT: 

Patrick McDonough, Executive Director, 

Joint Board for the Enrollment of 

Actuaries, at (202) 622–8229 (not a tollfree number). 

SUPPLEMENTARY INFORMATION: 

Background 

The final regulations (TD 9517) that 

are the subject of this correction are 

under section 3042 of the Employee 

Retirement Income Security Act of 1974 

(88 Stat. 829), Public Law 93–406 

(ERISA). 

Need for Correction 

As published, final regulations (TD 

9517) contain errors that may prove to 

be misleading and are in need of 

clarification. 

List of Subjects in 20 CFR Part 901 

Administrative practice and 

procedure, Pensions. 

Correction of Publication 

Accordingly, 20 CFR part 901 is 

corrected by making the following 

correcting amendments: 

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