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. Prices of

new books are listed in the first FEDERAL

REGISTER issue of each week.

Rules and Regulations Federal Register

69111 

Vol. 80, No. 216 

Monday, November 9, 2015 

OFFICE OF MANAGEMENT AND 

BUDGET 

2 CFR Part 200 

Guidance for Reporting and Use of 

Information Concerning Recipient 

Integrity and Performance; Corrections 

AGENCY: Executive Office of the 

President, Office of Management and 

Budget. 

ACTION: Correcting amendments. 

SUMMARY: The Office of Management 

and Budget (OMB) is correcting the final 

guidance that appeared in the Federal 

Register on July 22, 2015 (80 FR 43301). 

OMB is amending the guidance to make 

technical corrections where necessary. 

The final guidance is revised to reflect 

that due to the 14 day delay of the 

publically available information entered 

into the OMB-designated integrity and 

performance system accessible through 

SAM (currently the Federal Awardee 

Performance and Integrity Information 

System (FAPIIS)), Federal awarding 

agencies should review the non-public 

segment of the system when conducting 

their risk review as described in the 

guidance. This will ensure that Federal 

awarding agencies have the most 

current information available when 

completing the review. 

DATES: Effective date: November 9, 

2015. 

The applicability date of the final 

guidance remains January 1, 2016. 

FOR FURTHER INFORMATION CONTACT: 

Rhea Hubbard, Office of Federal 

Financial Management, rhubbard@

omb.eop.gov, or via telephone at (202) 

395–3993. 

SUPPLEMENTARY INFORMATION: On July 

22, 2015 (80 FR 43301), OMB issued a 

number of changes to Title 2 of the Code 

of Federal Regulations (2 CFR part 180 

and 2 CFR part 200). These changes 

provided guidance to Federal agencies 

to implement Section 872 of the Duncan 

Hunter National Defense Authorization 

Act for Fiscal Year 2009. As Section 872 

required, OMB and the General Services 

Administration (GSA) have established 

an integrity and performance system 

that includes governmentwide data with 

specified information related to the 

integrity and performance of entities 

awarded Federal grants and contracts. 

This is the second set of corrections. 

The first set of corrections was 

published in the Federal Register on 

July 30, 2015 (80 FR 45395) to advance 

the effective date to July 30, 2015 and 

reflect that the applicability date is 

January 1, 2016. This set of corrections 

reflects that Federal awarding agencies 

should check the non-public segment of 

the OMB-designated integrity and 

performance system accessible through 

SAM when conducting their risk 

review. 

List of Subjects in 2 CFR Part 200 

Accounting, Auditing, Colleges and 

universities, State and local 

governments, Grant programs, Grants 

administration, Hospitals, Indians, 

Nonprofit organizations, Reporting and 

recordkeeping requirements. 

Mark Reger, 

Deputy Controller. 

Under the authority of the Chief 

Financial Officer Act of 1990 (31 U.S.C. 

503), the Office of Management and 

Budget amends 2 CFR part 200 by 

making the following correcting 

amendments: 

PART 200—UNIFORM 

ADMINISTRATIVE REQUIREMENTS, 

COST PRINCIPLES, AND AUDIT 

REQUIREMENTS FOR FEDERAL 

AWARDS 

■ 1. The authority citation for part 200 

continues to read as follows: 

Authority: 31 U.S.C. 503. 

§ 200.205 [Amended] 

■ 2. Amend § 200.205 paragraph (a)(2) 

by removing ‘‘publicly available 

information in’’ and adding, in its place 

‘‘non-public segment of’’. 

[FR Doc. 2015–28441 Filed 11–6–15; 8:45 am] 

BILLING CODE 3110–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–3969; Directorate 

Identifier 2014–SW–010–AD; Amendment 

39–18318; AD 2015–23–02] 

RIN 2120–AA64 

Airworthiness Directives; Agusta 

S.p.A. Helicopters 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for Agusta 

S.p.A. (Agusta) Model AB412 

helicopters. This AD requires inspecting 

the filters installed on the pressure lines 

of utility hydraulic systems for metal 

particles. This AD is prompted by a 

report of a pump failure on the 

hydraulic external hoist caused by metal 

particles. These actions are intended to 

detect metal particles in the filter of the 

pressure line and prevent the pumps’ 

failure, which could lead to a hoisting 

accident and injury to persons. 

DATES: This AD becomes effective 

November 24, 2015. 

We must receive comments on this 

AD by January 8, 2016. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Docket: Go to 

http://www.regulations.gov. Follow the 

online instructions for sending your 

comments electronically. 

• Fax: 202–493–2251. 

• Mail: Send comments to the U.S. 

Department of Transportation, Docket 

Operations, M–30, West Building 

Ground Floor, Room W12–140, 1200 

New Jersey Avenue SE., Washington, 

DC 20590–0001. 

• Hand Delivery: Deliver to the 

‘‘Mail’’ address between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

locating Docket No. FAA–2015–3969 or 

in person at the Docket Operations 

Office between 9 a.m. and 5 p.m., 


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69112 Federal Register / Vol. 80, No. 216 / Monday, November 9, 2015 / Rules and Regulations 

Monday through Friday, except Federal 

holidays. The AD docket contains this 

AD, the European Aviation Safety 

Agency (EASA) AD, and other 

information. The street address for the 

Docket Operations Office (telephone 

800–647–5527) is in the ADDRESSES

section. Comments will be available in 

the AD docket shortly after receipt. 

For service information identified in 

this AD, contact AgustaWestland, 

Product Support Engineering, Via del 

Gregge, 100, 21015 Lonate Pozzolo (VA) 

Italy, ATTN: Maurizio D’Angelo; 

telephone 39–0331–664757; fax 39– 

0331–664680; or at http://

www.agustawestland.com/technicalbulletins. You may review the 

referenced service information at the 

FAA, Office of the Regional Counsel, 

Southwest Region, 10101 Hillwood 

Pkwy., Room 6N–321, Fort Worth, TX 

76177. 

FOR FURTHER INFORMATION CONTACT: Matt 

Wilbanks, Aviation Safety Engineer, 

Regulations and Policy Group, 

Rotorcraft Directorate, FAA, 10101 

Hillwood Pkwy., Fort Worth, TX 76177; 

email matt.wilbanks@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not provide you with notice and 

an opportunity to provide your 

comments prior to it becoming effective. 

However, we invite you to participate in 

this rulemaking by submitting written 

comments, data, or views. We also 

invite comments relating to the 

economic, environmental, energy, or 

federalism impacts that resulted from 

adopting this AD. The most helpful 

comments reference a specific portion of 

the AD, explain the reason for any 

recommended change, and include 

supporting data. To ensure the docket 

does not contain duplicate comments, 

commenters should send only one copy 

of written comments, or if comments are 

filed electronically, commenters should 

submit them only one time. We will file 

in the docket all comments that we 

receive, as well as a report summarizing 

each substantive public contact with 

FAA personnel concerning this 

rulemaking during the comment period. 

We will consider all the comments we 

receive and may conduct additional 

rulemaking based on those comments. 

Discussion 

EASA, which is the Technical Agent 

for the Member States of the European 

Union, issued EASA AD No. 2014– 

0063–E, dated March 12, 2014, to 

correct an unsafe condition for Agusta 

Model AB412 helicopters. EASA 

advises that during a hoist operation, a 

pressure line pump part number (P/N) 

1–8072 Rev. A failed on a Model AB412 

helicopter. Preliminary investigations 

reveal that unusual wear of an internal 

subcomponent generated metal 

particles, which caused the pump to 

fail, EASA advises. The root cause of 

this wear has not been determined. 

This condition, if not detected and 

corrected, could lead to future pump 

failures, resulting in hoisting accidents 

and injuries. As a result, EASA requires 

repetitive inspections of the pump’s 

filter for metal particles and 

replacement of the pressure line pump 

if particles exist. EASA advises that its 

AD is an interim action and that further 

AD action may follow, depending on the 

outcome of the investigations. 

FAA’s Determination 

These helicopters have been approved 

by the aviation authority of Italy and are 

approved for operation in the United 

States. Pursuant to our bilateral 

agreement with Italy, EASA, its 

technical representative, has notified us 

of the unsafe condition described in the 

EASA AD. We are issuing this AD 

because we evaluated all information 

provided by EASA and determined the 

unsafe condition exists and is likely to 

exist or develop on other helicopters of 

these same type designs. 

Related Service Information 

AgustaWestland has issued Bollettino 

Tecnico No. 412–140, dated March 11, 

2014 (BT), for Model AB412 helicopters 

with a hydraulic external hoist P/N 

BL10300–60 installed. The BT notes 

that Agusta received a report that pump 

P/N 1–8072 Rev. A failed during a hoist 

operation on a Model AB412 helicopter 

due to metal particles generated by 

unusual wear of an internal 

subcomponent. The BT calls for 

inspecting the filter installed on the 

external hoist’s pressure line for metal 

particles. The BT notes that an 

investigation is underway to determine 

the failure’s root causes and that the BT 

could be updated. 

AD Requirements 

This AD requires, within 10 hours 

time-in-service (TIS) and thereafter at 

intervals not to exceed 25 hours TIS, 

inspecting to determine whether metal 

particles are in the filter installed on the 

pressure line of the utility hydraulic 

system. If there are any metal particles, 

this AD requires, before the next flight, 

flushing the utility hydraulic system, 

replacing the filter with an airworthy 

filter, and replacing the pressure line 

pump with an airworthy pressure line 

pump. 

Interim Action 

We consider this AD to be an interim 

action. The design approval holder is 

investigating the root cause for the 

unsafe condition identified in this AD. 

Once the investigation is completed, we 

might consider additional rulemaking. 

Costs of Compliance 

There are no costs of compliance with 

this AD because there are no helicopters 

with this type certificate on the U.S. 

Registry. 

FAA’s Justification and Determination 

of the Effective Date 

There are no helicopters with this 

type certificate are on the U.S. Registry. 

Therefore, we believe it is unlikely that 

we will receive any adverse comments 

or useful information about this AD 

from U.S. Operators. 

Since an unsafe condition exists that 

requires the immediate adoption of this 

AD, we determined that notice and 

opportunity for public comment before 

issuing this AD are unnecessary because 

there are none of these helicopters on 

the U.S. Registry and that good cause 

exists for making this amendment 

effective in less than 30 days. 

Authority for This Rulemaking 

Title 49 of the United States Code 

specifies the FAA’s authority to issue 

rules on aviation safety. Subtitle I, 

section 106, describes the authority of 

the FAA Administrator. ‘‘Subtitle VII: 

Aviation Programs,’’ describes in more 

detail the scope of the Agency’s 

authority. 

We are issuing this rulemaking under 

the authority described in ‘‘Subtitle VII, 

Part A, Subpart III, Section 44701: 

General requirements.’’ Under that 

section, Congress charges the FAA with 

promoting safe flight of civil aircraft in 

air commerce by prescribing regulations 

for practices, methods, and procedures 

the Administrator finds necessary for 

safety in air commerce. This regulation 

is within the scope of that authority 

because it addresses an unsafe condition 

that is likely to exist or develop on 

products identified in this rulemaking 

action. 

Regulatory Findings 

We determined that this AD will not 

have federalism implications under 

Executive Order 13132. This AD will 

not have a substantial direct effect on 

the States, on the relationship between 

the national Government and the States, 

or on the distribution of power and 


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Federal Register / Vol. 80, No. 216 / Monday, November 9, 2015 / Rules and Regulations 69113 

responsibilities among the various 

levels of government. 

For the reasons discussed, I certify 

that this AD: 

1. Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866; 

2. Is not a ‘‘significant rule’’ under 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979); 

3. Will not affect intrastate aviation in 

Alaska to the extent that it justifies 

making a regulatory distinction; and 

4. Will not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends 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 [Amended] 

■ 2. The FAA amends § 39.13 by adding 

the following new airworthiness 

directive (AD): 

2015–23–02 Agusta S.p.A.: Amendment 39– 

18318; Docket No. FAA–2015–3969; 

Directorate Identifier 2014–SW–010–AD. 

(a) Applicability 

This AD applies to Model AB412 

helicopters with a hydraulic external hoist 

part number BL10300–60 installed, 

certificated in any category. 

(b) Unsafe Condition 

This AD defines the unsafe condition as 

failure of a hydraulic external hoist pressure 

line pump. This condition, if not detected 

and prevented, could result in loss of 

hydraulic pressure and subsequent injury to 

persons being lifted in the hoist. 

(c) Effective Date 

This AD becomes effective November 24, 

2015. 

(d) Compliance 

You are responsible for performing each 

action required by this AD within the 

specified compliance time unless it has 

already been accomplished prior to that time. 

(e) Required Actions 

Within 10 hours time-in-service (TIS) and 

thereafter at intervals not to exceed 25 hours 

TIS: 

(1) Inspect the hydraulic external hoist 

pressure line filter for metal particles. 

(2) If there are any metal particles, before 

further flight, flush the utility hydraulic 

system, replace the pressure line pump, and 

replace the filter. 

(f) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Safety Management 

Group, FAA, may approve AMOCs for this 

AD. Send your proposal to: Matt Wilbanks, 

Aviation Safety Engineer, Regulations and 

Policy Group, Rotorcraft Directorate, FAA, 

10101 Hillwood Pkwy., Fort Worth, TX 

76177; email 9-asw-ftw-amoc-requests@

faa.gov. 

(2) For operations conducted under a 14 

CFR part 119 operating certificate or under 

14 CFR part 91, subpart K, we suggest that 

you notify your principal inspector, or 

lacking a principal inspector, the manager of 

the local flight standards district office or 

certificate holding district office, before 

operating any aircraft complying with this 

AD through an AMOC. 

(g) Additional Information 

(1) AgustaWestland Bollettino Tecnico No. 

412–140, dated March 11, 2014, which is not 

incorporated by reference, contains 

additional information about the subject of 

this AD. For service information identified in 

this AD, contact AgustaWestland, Product 

Support Engineering, Via del Gregge, 100, 

21015 Lonate Pozzolo (VA) Italy, ATTN: 

Maurizio D’Angelo; telephone 39–0331– 

664757; fax 39–0331–664680; or at http://

www.agustawestland.com/technicalbulletins. You may review a copy of the 

service information at the FAA, Office of the 

Regional Counsel, Southwest Region, 10101 

Hillwood Pkwy., Room 6N–321, Fort Worth, 

TX 76177. 

(2) The subject of this AD is addressed in 

European Aviation Safety Agency (EASA) AD 

No. 2014–0063–E, dated March 12, 2014. You 

may view the EASA AD on the Internet at 

http://www.regulations.gov by searching for 

and locating it in Docket No. FAA–2015– 

3969. 

(h) Subject 

Joint Aircraft Service Component (JASC) 

Code: 2550, Cargo Compartments. 

Issued in Fort Worth, Texas, on October 30, 

2015. 

James A. Grigg, 

Acting Assistant Manager, Rotorcraft 

Directorate, Aircraft Certification Service. 

[FR Doc. 2015–28314 Filed 11–6–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–3224; Directorate 

Identifier 2015–CE–026–AD; Amendment 

39–18290; AD 2015–20–11] 

RIN 2120–AA64 

Airworthiness Directives; SchemppHirth Flugzeugbau GmbH Gliders 

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 certain Schempp-Hirth 

Flugzeugbau GmbH Models Duo Discus 

and Duo Discus T gliders. The Model 

Duo Discus gliders were incorrectly 

referenced as powered sailplanes in the 

Applicability section. This document 

corrects that error and refers to both 

models as just gliders as in previous 

ADs. In all other respects, the original 

document remains the same; however 

we are publishing the entire rule in the 

Federal Register. 

DATES: This final rule is effective 

November 18, 2015. 

ADDRESSES: You may examine the AD 

docket on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

3224; 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: Jim 

Rutherford, Aerospace Engineer, FAA, 

Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4165; fax: (816) 

329–4090; email: jim.rutherford@

faa.gov. 

SUPPLEMENTARY INFORMATION: 

Airworthiness Directive 2015–20–11, 

Amendment 39–18290 (80 FR 61722, 

October 14, 2015), currently requires 

inspecting and replacing the airbrake 

bell crank and the airbrake drive funnels 

and inspecting the airbrake control 

system for proper clearance and making 

necessary adjustments. 


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