Federal Register / Vol. 81, No. 16 / Tuesday, January 26, 2016 / Rules and Regulations 4163 

Estimated Number of Responses per 

Respondent: 13.78. 

Estimated Total Annual Burden on 

Respondents: 252,432.64 hours. See the 

table below for estimated total annual 

burden for each type of respondent. 

STATE AGENCIES

CFR Action Number of 

respondents 

Frequency 

per 

respondent 

Total annual 

responses 

Burden hours 

per response 

Total 

burden 

hours 

Previous 

submission 

total hours 

Difference 

due to 

program 

changes 

Difference 

due to 

adjustments 

272.2 ......... Program Activity Statement 

(FNS 366B).

53 4 212 15 3,180 950.29 2,229.71 0.00 

272.16 ....... NDNH—Applicant/Recipient 

Screening.

53 1 9,158,240 0.017 155,690.08 0.00 155,690.08 0.00 

272.16 ....... NDNH—Verification of Match 53 1 1,237,600 0.03 37,128 0.00 37,128.00 0.00 

272.16 ....... NDNH—Notice of Adverse 

Action or Notice of Denial.

53 1 495,040 0.03 14,851.20 0.00 14,851.20 0.00 

Total .. ............................................... 53 .................... 10,891,092 0.019359792 210,849.28 950.29 209,898.99 0.00 

HOUSEHOLDS

CFR Action Number of 

respondents 

Frequency 

per 

respondent 

Total annual 

responses 

Burden 

hours per 

response 

Total 

burden 

hours 

Previous 

submission 

total hours 

Difference 

due to 

program 

changes 

Difference 

due to 

adjustments 

272.16 ....... NDNH—Request for Contact 891,072 1 891,072 0.03 26,732.16 0.00 26,732.16 0.00 

272.16 ....... NDNH—Notice of Adverse 

Action or Notice of Denial.

495,040 1 495,040 0.03 14,851.20 0.00 14,851.20 0.00 

Total .. ............................................... 891,072 .................... 1,386,112 0.03 41,583.36 0.00 41,583.36 0.00 

E-Government Act Compliance 

The Department is committed to 

complying with the E-Government Act 

of 2002 to promote the use of the 

Internet and other information 

technologies to provide increased 

opportunities for citizen access to 

Government information and services, 

and for other purposes. 

List of Subjects in 7 CFR Part 272 

Civil rights, Supplemental Nutrition 

Assistance Program, Grant programs— 

social programs, Reporting and 

recordkeeping requirements. 

Accordingly, 7 CFR part 272 is 

amended as follows: 

PART 272—REQUIREMENTS FOR 

PARTICIPATING STATE AGENCIES 

■ 1. The authority citation for part 272 

continues to read as follows: 

Authority: 7 U.S.C. 2011–2036. 

■ 2. In § 272.2, revise paragraphs 

(c)(1)(ii) and (e)(2)(ii) to read as follows: 

§ 272.2 Plan of operation. 

* * * * * 

(c) * * * 

(1) * * * 

(ii) The Program Activity Statement, 

to be submitted quarterly (unless 

otherwise directed by FNS), solicits a 

summary of Program activity for the 

State agency’s operations during the 

preceding reporting period. 

* * * * * 

(e) * * * 

(2) * * * 

(ii) The Program Activity Statement 

shall be submitted quarterly (unless 

otherwise directed by FNS) based on the 

Federal fiscal year. 

* * * * * 

■ 3. Add § 272.16 to read as follows: 

§ 272.16 National Directory of New Hires. 

(a) General. Each State agency shall 

establish a system to verify applicant 

employment data for the determination 

of SNAP eligibility and correct benefit 

amount. 

(b) Data source. States shall use the 

U.S. Department of Health and Human 

Service (HHS) National Directory of 

New Hires (NDNH) and enter into a 

computer matching agreement with 

HHS pursuant to the authority in 42 

U.S.C. 653(j)(10). 

(c) Use of match data. In accordance 

with the procedural requirements and 

privacy protections required for 

computer data matching at 5 U.S.C. 

552a(p), States shall provide a system 

for: 

(1) Comparing identifiable 

information about each adult household 

member against data from the NDNH. 

States must, at minimum, match 

household members against new hire 

data available in the database. States 

shall make the comparison of matched 

data at the time of application and 

recertification. 

(2) The reporting of instances where 

there is a match; 

(3) The independent verification of 

match hits to determine their accuracy; 

(4) Notice to the household of match 

results; 

(5) An opportunity for the household 

to respond to the match prior to an 

adverse action to deny, reduce, or 

terminate benefits; and 

(6) The establishment and collection 

of claims as appropriate. 

Dated: January 14, 2016. 

Audrey Rowe, 

Administrator, Food and Nutrition Service. 

[FR Doc. 2016–01402 Filed 1–25–16; 8:45 am] 

BILLING CODE 3410–30–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–1281; Directorate 

Identifier 2014–NM–241–AD; Amendment 

39–18346; AD 2015–25–08] 

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 777 airplanes. Paragraph (i)(4) of 

the regulatory text contains a reference 

to a nonexistent paragraph. This 

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4164 Federal Register / Vol. 81, No. 16 / Tuesday, January 26, 2016 / Rules and Regulations 

document corrects that error. In all other 

respects, the original document remains 

the same. 

DATES: This final rule is effective 

January 28, 2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of January 28, 2016 (80 FR 80234, 

December 24, 2015). 

ADDRESSES: For service information 

identified in this final rule, contact 

Boeing Commercial Airplanes, 

Attention: Data & Services Management, 

P.O. Box 3707, MC 2H–65, Seattle, WA 

98124–2207; telephone 206–544–5000, 

extension 1; fax 206–766–5680; Internet 

https://www.myboeingfleet.com. You 

may view this referenced service 

information at the FAA, Transport 

Airplane Directorate, 1601 Lind Avenue 

SW., Renton, WA. For information on 

the availability of this material at the 

FAA, call 425–227–1221. It is also 

available on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

1281. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

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 AD, the regulatory 

evaluation, any comments received, and 

other information. The address for the 

Docket Office (phone: 800–647–5527) is 

Docket Management Facility, 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: Eric 

Lin, Aerospace Engineer, Airframe 

Branch, ANM–120S, FAA, Seattle 

Aircraft Certification Office (ACO), 1601 

Lind Avenue SW., Renton, WA 98057– 

3356; phone: 425–917–6412; fax: 425– 

917–6590; email: Eric.Lin@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Airworthiness Directive 2015–25–08, 

Amendment 39–18346 (80 FR 80234, 

December 24, 2015), currently requires 

repetitive inspections for any crack in 

the aft webs of the radial lap splices of 

the aft pressure bulkhead, and, if 

necessary, corrective actions, for all The 

Boeing Company Model 777 airplanes. 

Need for the Correction 

As published, paragraph (i)(4) of the 

regulatory text contains a reference to a 

nonexistent paragraph. Paragraph (i)(4) 

of the AD incorrectly references 

paragraph ‘‘(l)(4)(ii)’’; however, the 

correct reference is paragraph 

‘‘(i)(4)(ii).’’ 

Related Service Information Under 1 

CFR Part 51 

We reviewed Boeing Alert Service 

Bulletin 777–53A0078, dated December 

5, 2014. This service information 

describes procedures for inspections of 

the lap splices in the web of the aft 

pressure bulkhead for cracking, and 

corrective actions. This service 

information is reasonably available 

because the interested parties have 

access to it through their normal course 

of business or by the means identified 

in the ADDRESSES section. 

Correction of Publication 

This document corrects an error and 

correctly adds the AD as an amendment 

to section 39.13 of the Federal Aviation 

Regulations (14 CFR 39.13). Although 

no other part of the preamble or 

regulatory information has been 

corrected, we are publishing the entire 

rule in the Federal Register. 

The effective date of this AD remains 

January 28, 2016. 

Since this action only corrects a 

paragraph reference, it has no adverse 

economic impact and imposes no 

additional burden on any person. 

Therefore, we have determined that 

notice and public 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): 

2015–25–08 The Boeing Company: 

Amendment 39–18346; Docket No. 

FAA–2015–1281; Directorate Identifier 

2014–NM–241–AD. 

(a) Effective Date 

This AD becomes effective on January 28, 

2016. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all The Boeing 

Company Model 777–200, –200LR, –300, 

–300ER, and 777F series airplanes, 

certificated in any category. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 53, Fuselage. 

(e) Unsafe Condition 

This AD was prompted by an evaluation by 

the design approval holder indicating that 

the lap splices of the aft pressure bulkhead 

webs are subject to widespread fatigue 

damage on aging Model 777 airplanes that 

have accumulated at least 38,000 total flight 

cycles. We are issuing this AD to detect and 

correct fatigue cracking in the aft webs of the 

radial lap splices of the aft pressure 

bulkhead; such cracking could result in 

reduced structural integrity of the airplane, 

decompression of the cabin, and collapse of 

the floor structure. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Inspection of Lap Splice in the Web of the 

Aft Pressure Bulkhead 

Except as required by paragraph (h) of this 

AD: At the times specified in paragraph 1.E., 

‘‘Compliance,’’ of Boeing Alert Service 

Bulletin 777–53A0078, dated December 5, 

2014, do a medium frequency eddy current 

inspection for any cracking in the aft webs 

of the radial lap splices of the aft pressure 

bulkhead, in accordance with the 

Accomplishment Instructions of Boeing Alert 

Service Bulletin 777–53A0078, dated 

December 5, 2014. Repeat the inspection 

thereafter at intervals not to exceed 8,400 

flight cycles from the previous inspection. If 

any crack is found during any inspection 

required by this AD, do the applicable 

corrective actions, in accordance with the 

Accomplishment Instructions of Boeing Alert 

Service Bulletin 777–53A0078, dated 

December 5, 2014. If a corrective action 

described in Boeing Alert Service Bulletin 

777–53A0078, dated December 5, 2014, 

specifies to contact Boeing for appropriate 

action: Before further flight, repair using a 

method approved in accordance with the 

procedures specified in paragraph (i) of this 

AD. 

(h) Exception to Service Information 

Specifications 

Where Boeing Alert Service Bulletin 777– 

53A0078, dated December 5, 2014, specifies 

a compliance time ‘‘after the original issue 

date of this service bulletin,’’ this AD 

requires compliance within the specified 

compliance time after the effective date of 

this AD. 

(i) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle Aircraft 

Certification Office (ACO), FAA, has the 

authority to approve AMOCs for this AD, if 

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Federal Register / Vol. 81, No. 16 / Tuesday, January 26, 2016 / Rules and Regulations 4165 

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 ACO, send it to the 

attention of the person identified in 

paragraph (j) of this AD. Information may be 

emailed to: 9–ANM-Seattle-ACO–AMOCRequests@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. 

(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 

Commercial Airplanes Organization 

Designation Authorization (ODA) that has 

been authorized by the Manager, Seattle 

ACO, 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. 

(4) For service information that contains 

steps that are labeled as Required for 

Compliance (RC), the provisions of 

paragraphs (i)(4)(i) and (i)(4)(ii) of this AD 

apply. 

(i) The steps labeled as RC, including 

substeps under an RC step and any figures 

identified in an RC step, must be done to 

comply with the AD. An AMOC is required 

for any deviations to RC steps, including 

substeps and identified figures. 

(ii) Steps not labeled as RC may be 

deviated from using accepted methods in 

accordance with the operator’s maintenance 

or inspection program without obtaining 

approval of an AMOC, provided the RC steps, 

including substeps and identified figures, can 

still be done as specified, and the airplane 

can be put back in an airworthy condition. 

(j) Related Information 

For more information about this AD, 

contact Eric Lin, Aerospace Engineer, 

Airframe Branch, ANM–120S, FAA, Seattle 

ACO, 1601 Lind Avenue SW., Renton, WA 

98057–3356; phone: 425–917–6412; fax: 425– 

917–6590; email: Eric.Lin@faa.gov. 

(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. 

(3) The following service information was 

approved for IBR on January 28, 2016 (80 FR 

80234, December 24, 2015). 

(i) Boeing Alert Service Bulletin 777– 

53A0078, dated December 5, 2014. 

(ii) Reserved. 

(4) For service information identified in 

this AD, contact Boeing Commercial 

Airplanes, Attention: Data & Services 

Management, P. O. Box 3707, MC 2H–65, 

Seattle, WA 98124–2207; telephone 206– 

544–5000, extension 1; fax 206 766 5680; 

Internet https://www.myboeingfleet.com. 

(5) You may view this service information 

at FAA, Transport Airplane Directorate, 1601 

Lind Avenue SW., Renton, WA. For 

information on the availability of this 

material at the FAA, call 425–227–1221. 

(6) 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, call 

202–741–6030, or go to: http://www.archives.

gov/federal-register/cfr/ibr-locations.html. 

Issued in Renton, Washington, on January 

19, 2016. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2016–01441 Filed 1–25–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–3585; Directorate 

Identifier 2015–NE–22–AD; Amendment 39– 

18384; AD 2015–28–01] 

RIN 2120–AA64 

Airworthiness Directives; Engine 

Alliance Turbofan Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Engine Alliance (EA) GP7270 turbofan 

engines. This AD was prompted by the 

manufacturer informing us that the 

inspection criteria and repair 

procedures in the maintenance manual 

for aft bolt holes of the high-pressure 

compressor (HPC) cone shaft on the 

affected engines is incorrect. This AD 

requires inspection of the HPC cone 

shaft and repair of affected parts, if 

needed. We are issuing this AD to 

prevent failure of the HPC cone shaft, 

which could lead to uncontained engine 

failure and damage to the airplane. 

DATES: This AD is effective March 1, 

2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of March 1, 2016. 

ADDRESSES: For service information 

identified in this AD, contact Engine 

Alliance, 400 Main St., East Hartford, 

CT 06108, M/S 169–10, phone: 800– 

565–0140; email: help24@pw.utc.com; 

Internet: sp.engineallianceportal.com. 

You may view this service information 

at the FAA, Engine & Propeller 

Directorate, 1200 District Avenue, 

Burlington, MA. For information on the 

availability of this material at the FAA, 

call 781–238–7125. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

3585; 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 AD, the regulatory 

evaluation, any comments received, and 

other information. The address for the 

Docket Office (phone: 800–647–5527) is 

Document Management Facility, 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: Kyle 

Gustafson, Aerospace Engineer, Engine 

& Propeller Directorate, FAA, 1200 

District Avenue, Burlington, MA 01803; 

phone: 781–238–7183; fax: 781–238– 

7199; email: kyle.gustafson@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to certain EA GP7270 turbofan 

engines. The NPRM published in the 

Federal Register on October 1, 2015 (80 

FR 59081). The NPRM was prompted by 

the manufacturer informing us that the 

inspection criteria and repair 

procedures in the maintenance manual 

for aft bolt holes of the HPC cone shaft, 

also referred to as the ‘‘HPC forward 

stubshaft,’’ for the affected engines is 

incorrect. The NPRM proposed to 

require inspection of the HPC cone shaft 

and repair of affected parts, if needed. 

We are issuing this AD to prevent 

failure of the HPC cone shaft, which 

could lead to uncontained engine failure 

and damage to the airplane. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. The 

following presents the comments 

received on the NPRM (80 FR 59081, 

October 1, 2015) and the FAA’s 

response to each comment. 

Request To Add Engine Models 

EA requested that we expand the 

applicability to include the GP7272 and 

GP7277 engine models. 

We disagree. There are no GP7272 or 

GP7277 engines in service nor have any 

been delivered. New engines would be 

delivered with corrected service 

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