Federal Register / Vol. 80, No. 58 / Thursday, March 26, 2015 / Proposed Rules 15947 

(2) The report has been prepared in 

accordance with all applicable statutory 

or regulatory requirements, and 

(3) The information is true, accurate, 

and complete to the best of signatories’ 

knowledge and belief. 

(c) Distribution. The Corporation must 

distribute the signed report of condition 

to all its shareholders within 90 days of 

its fiscal year-end. The Corporation 

must provide us one paper and one 

electronic copy of every signed report 

within 5 days of signing. If the report is 

the same as that filed with the SEC, the 

Corporation may instead provide the 

signed reports to us only in electronic 

form and simultaneous with filing the 

report with the SEC. 

(1) The Corporation must publish a 

copy of each report of condition on its 

Web site within 3 business days of filing 

the report with us. The report must 

remain on the Web site until the next 

report is posted. When the reports are 

the same as those filed with the SEC, 

electronic links to the SEC filings Web 

site, EDGAR, may be used in satisfaction 

of this requirement. 

(2) Upon receiving a request for an 

annual report of condition from a 

stockholder, investor, or the public, the 

Corporation must promptly provide the 

requester the most recent signed annual 

report issued in compliance with this 

section. 

§ 655.15 Interim reports, notices, and 

proxy statements. 

(a) The Corporation must provide to 

us one paper and one electronic copy of 

every interim report, notice, and proxy 

statement filed with the SEC within 1 

business day of filing the item with the 

SEC, including all papers and 

documents that are a part of the report, 

notice, or statement. 

(b) The Corporation must publish a 

copy of each interim report, notice, and 

proxy statement on its Web site within 

5 business days of filing the 

document(s) with the SEC. The interim 

report, notice, or proxy statement must 

remain on the Web site for 6 months or 

until the next annual report of condition 

is posted, whichever is later. Electronic 

links to the SEC filings Web site, 

EDGAR, may be used in satisfaction of 

this requirement. 

Subpart C—Reports Relating to 

Securities Activities of the Federal 

Agricultural Mortgage Corporation 

§ 655.20 Securities not registered under 

the Securities Act. 

The Corporation must make special 

filings with OSMO for securities either 

issued or guaranteed by the Corporation 

that are not registered under the 

Securities Act. These filings include, 

but are not limited to: 

(a) One paper and one electronic copy 

of any offering circular, private 

placement memorandum, or 

information statement prepared in 

connection with the securities offering 

at or before the time of the securities 

offering. 

(b) For securities backed by qualified 

loans as defined in section 8.0(9)(A) of 

the Act, one paper and one electronic 

copy of the following within 1 business 

day of the finalization of the transaction: 

(1) The private placement memoranda 

for securities sold to investors; and 

(2) The pooling and servicing 

agreement when the security is 

purchased by the Corporation as 

authorized by section 8.6(g) of the Act. 

(c) For securities backed by qualified 

loans as defined in section 8.0(9)(B) of 

the Act, the Corporation must provide 

summary information on such securities 

issued during each calendar quarter in 

the form prescribed by us. Such 

summary information must be provided 

with each report of condition and 

performance filed pursuant to § 621.12, 

and at such other times as OSMO may 

require. 

§ 655.21 Filings and communications with 

the U.S. Treasury, the SEC, and NYSE. 

(a) The Corporation must send us one 

paper and one electronic copy of every 

filing made with U.S. Treasury, the SEC, 

or NYSE, including financial statements 

and related schedules, exhibits, and 

other documents that are a part of the 

filing. Such copies must be filed with us 

no later than 1 business day after any 

U.S. Treasury, SEC, or NYSE filing. If 

the filing is one addressed in subpart B 

of this part, no action under this 

paragraph is required. 

(b) The Corporation must send us, 

within 3 business days and according to 

instructions provided by us, copies of 

all substantive correspondence between 

the Corporation and the U.S. Treasury, 

the SEC, or NYSE. 

(c) The Corporation must notify us 

within 1 business day if it becomes 

exempt or claims exemption from any 

filing requirements of the Securities Act. 

Dated: March 19, 2015. 

Dale L. Aultman, 

Secretary, Farm Credit Administration Board. 

[FR Doc. 2015–06755 Filed 3–25–15; 8:45 am] 

BILLING CODE 6705–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–0249; Directorate 

Identifier 2014–NM–174–AD] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to supersede 

Airworthiness Directive (AD) 2012–18– 

05, which applies to The Boeing 

Company Model DC–9–10, DC–9–20, 

DC–9–30, DC–9–40, and DC–9–50 series 

airplanes; and Model DC–9–81 (MD– 

81), DC–9–82 (MD–82), DC–9–83 (MD– 

83), DC–9–87 (MD–87), MD–88, and 

MD–90–30 airplanes; equipped with a 

center wing fuel tank and Boeing 

original equipment manufacturerinstalled auxiliary fuel tanks. AD 2012– 

18–05 currently requires adding design 

features to detect electrical faults and to 

detect a pump running in an empty fuel 

tank. Since we issued AD 2012–18–05, 

we have determined that it is necessary 

to clarify the actions for airplanes on 

which the auxiliary fuel tanks are 

removed. This proposed AD would 

allow certain actions as optional 

methods of compliance. We are 

proposing this AD to reduce the 

potential of ignition sources inside fuel 

tanks, which, in combination with 

flammable fuel vapors, could result in 

fuel tank explosions and consequent 

loss of the airplane. 

DATES: We must receive comments on 

this proposed AD by May 11, 2015. 

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 

http://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 proposed AD, contact Boeing 

Commercial Airplanes, Attention: Data 

& Services Management, 3855 

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15948 Federal Register / Vol. 80, No. 58 / Thursday, March 26, 2015 / Proposed Rules 

Lakewood Boulevard, MC D800–0019, 

Long Beach, CA 90846–0001; telephone 

206–544–5000, extension 2; fax 206– 

766–5683; 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– 

0249. 

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– 

0249; 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 proposed AD, the 

regulatory evaluation, any comments 

received, and other information. The 

street address for the Docket Office 

(phone: 800–647–5527) is in the 

ADDRESSES section. Comments will be 

available in the AD docket shortly after 

receipt. 

FOR FURTHER INFORMATION CONTACT: Se ́rj 

Harutunian, Aerospace Engineer, 

Propulsion Branch, ANM–140L, FAA, 

Los Angeles Aircraft Certification Office 

(ACO), 3960 Paramount Boulevard, 

Lakewood, CA 90712–4137; phone: 

562–627–5254; fax: 562–627–5210; 

email: serj.harutunian@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to send any written 

relevant data, views, or arguments about 

this proposed AD. Send your comments 

to an address listed under the 

ADDRESSES section. Include ‘‘Docket No. 

FAA–2015–0249; Directorate Identifier 

2014–NM–174–AD’’ at the beginning of 

your comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of this proposed AD. We will 

consider all comments received by the 

closing date and may amend this 

proposed AD because of those 

comments. 

We will post all comments we 

receive, without change, to http://

www.regulations.gov, including any 

personal information you provide. We 

will also post a report summarizing each 

substantive verbal contact we receive 

about this proposed AD. 

Discussion 

On August 6, 2012, we issued AD 

2012–18–05, Amendment 39–17181 (77 

FR 54793, September 6, 2012), for The 

Boeing Company Model DC–9–10, DC– 

9–20, DC–9–30, DC–9–40, and DC–9–50 

series airplanes; and Model DC–9–81 

(MD–81), DC–9–82 (MD–82), DC–9–83 

(MD–83), DC–9–87 (MD–87), MD–88, 

and MD–90–30 airplanes; equipped 

with a center wing fuel tank and Boeing 

original equipment manufacturerinstalled auxiliary fuel tanks. AD 2012– 

18–05 requires adding design features to 

detect electrical faults and to detect a 

pump running in an empty fuel tank. 

AD 2012–18–05 resulted from fuel 

system reviews conducted by the 

manufacturer. We issued AD 2012–18– 

05 to reduce the potential of ignition 

sources inside fuel tanks, which, in 

combination with flammable fuel 

vapors, could result in fuel tank 

explosions and consequent loss of the 

airplane. 

Actions Since AD 2012–18–05, 

Amendment 39–17181 (77 FR 54793, 

September 6, 2012) Was Issued 

Since we issued AD 2012–18–05, 

Amendment 39–17181 (77 FR 54793, 

September 6, 2012), we have 

determined that it is necessary to clarify 

the actions for airplanes on which the 

auxiliary fuel tanks are removed. In 

addition, The Boeing Company has 

issued new service information for 

Model DC–9–81 (MD–81), DC–9–82 

(MD–82), DC–9–83 (MD–83), DC–9–87 

(MD–87), and Model MD–88 airplanes; 

and Model MD–90–30 airplanes, which 

provides a method of compliance for the 

actions required by AD 2012–18–05. 

Boeing has not yet issued corresponding 

service information for Boeing Model 

DC–9–10, DC–9–20, DC–9–30, DC–9–40, 

and DC–9–50 series airplanes. The 

applicability of AD 2012–18–05 has not 

changed in this proposed AD. 

Related Service Information Under 1 

CFR Part 51 

We reviewed Boeing Service Bulletin 

MD80–28–228, dated September 27, 

2013; and Boeing Service Bulletin 

MD90–28–013, dated September 27, 

2013. The service information describes 

procedures for installing GFI relays that 

change fuel pump system wiring, 

installing a low fuel pressure indication 

system, and revising the inspection or 

maintenance program to include new 

limitations. 

We have also reviewed Appendixes B, 

C, and D of Boeing Special Compliance 

Item Report MDC–92K9145, Revision M, 

dated February 5, 2013, which includes 

Critical Design Configuration Control 

Limitations (CDCCLs), Airworthiness 

Limitations Instructions (ALIs), and 

short-term extensions. 

Boeing Service Bulletin MD80–28– 

228, dated September 27, 2013, specifies 

prior or concurrent accomplishment of 

the following concurrent service 

information. 

• Boeing MD–80 Service Bulletin 28– 

53, Revision 1, dated April 16, 1992, 

which describes procedures for 

installing a low fuel pressure indication 

system. 

• Boeing MD–80 Service Bulletin 28– 

63, Revision 2, dated April 8, 1992, 

which describes procedures for 

installing a low fuel pressure indication 

inhibit system. 

This service information is reasonably 

available; see ADDRESSES for ways to 

access this service information. 

Clarification of the Requirements for 

the Design Features 

In paragraph (c) of this proposed AD, 

we have added the text ‘‘for airplanes on 

which auxiliary fuel tanks are removed, 

the AD action specified for the auxiliary 

fuel tanks are not required’’ to clarify 

that the actions specified in this AD for 

the auxiliary fuel tanks are not required 

when the auxiliary fuel tanks are 

removed, but the AD actions for the 

center fuel tanks still apply. 

Revised Compliance Time 

We have determined that it is 

appropriate to allow additional time to 

accomplish the design features and 

requirements specified in this proposed 

AD. Therefore, we have added a 

compliance time of ‘‘within 42 months 

after the effective date of this AD’’ to 

paragraph (g) of this proposed AD. We 

have determined that this extension of 

the compliance time will provide an 

acceptable level of safety. 

FAA’s Determination 

We are proposing this AD because we 

evaluated all the relevant information 

and determined the unsafe condition 

described previously is likely to exist or 

develop in other products of these same 

type designs. 

Proposed AD Requirements 

This proposed AD would retain all 

requirements of AD 2012–18–05, 

Amendment 39–17181 (77 FR 54793, 

September 6, 2012). This proposed AD 

would clarify the actions for airplanes 

on which the auxiliary fuel tanks are 

removed, that the actions specified for 

the auxiliary fuel tanks are not required. 

This proposed AD would also provide 

certain methods of compliance for the 

actions restated from AD 2012–18–05 

(one option is accomplishing the actions 

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Federal Register / Vol. 80, No. 58 / Thursday, March 26, 2015 / Proposed Rules 15949 

specified in the service information 

described previously, including revising 

the inspection or maintenance program, 

as applicable, to include new 

limitations; the other option is installing 

a supplemental type certificate (STC)). 

This proposed AD specifies to revise 

certain operator maintenance 

documents to include new actions (e.g., 

inspections) and CDCCLs. Compliance 

with these actions and CDCCLs is 

required by 14 CFR 91.403(c). For 

airplanes that have been previously 

modified, altered, or repaired in the 

areas addressed by this proposed AD, 

the operator may not be able to 

accomplish the actions described in the 

revisions. In this situation, to comply 

with 14 CFR 91.403(c), the operator 

must request approval for an alternative 

method of compliance according to 

paragraph (l) of this proposed AD. The 

request should include a description of 

changes to the required actions and 

CDCCLs that will ensure the continued 

operational safety of the airplane. 

Costs of Compliance 

We estimate that this proposed AD 

affects 809 airplanes of U.S. registry. 

We estimate the following costs to 

comply with this proposed AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Installing design features for airplanes with center wing and 

auxiliary tanks (263 airplanes), using a method approved 

by the FAA [retained actions from AD 2012-18-05, 

Amendment 39-17181 (77 FR 54793, September 6, 

2012)].

50 work-hours × $85 per hour 

= $4,250.

$35,000 $39,250 $10,322,750 

Installing design features for airplanes with center wing tank 

(546 airplanes), using a method approved by the FAA [retained actions from AD 2012–18–05, Amendment 

39-17181 (77 FR 54793, September 6, 2012)].

35 work-hours × $85 per hour 

= $2,975.

17,000 19,975 10,906,350 

ESTIMATED COSTS: NEW OPTIONAL ACTIONS FOR INSTALLING DESIGN FEATURES

Action Labor cost Parts cost Cost per 

product 

For airplanes with center wing and auxiliary tanks, using service information specified in paragraph (h) of this proposed AD (including revising the maintenance/inspection program).250 work-hours × $85 per hour = 

$21,250.

$69,000 $90,250 

For airplanes with center wing tank, using service information specified 

in paragraph (h) of this proposed AD (including revising the maintenance/inspection program).

110 work-hours × $85 = 9,350 ........ 30,000 39,350 

Installing STC specified in paragraph (i) of this proposed AD .................. 35 work-hours × $85 per hour = 

$2,975.

17,000 19,975 

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 have determined that this 

proposed AD would not have federalism 

implications under Executive Order 

13132. This proposed AD would 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 

responsibilities among the various 

levels of government. 

For the reasons discussed above, I 

certify that the proposed regulation: 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866, 

(2) Is not a ‘‘significant rule’’ under 

the DOT Regulatory Policies and 

Procedures (44 FR 11034, February 26, 

1979), 

(3) Will not affect intrastate aviation 

in Alaska, 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. 

The Proposed Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA proposes to amend 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 

removing Airworthiness Directive (AD) 

2012–18–05, Amendment 39–17181 (77 

FR 54793, September 6, 2012), and 

adding the following new AD: 

The Boeing Company: Docket No. FAA– 

2015–0249; Directorate Identifier 2014 

NM–174–AD. 

(a) Comments Due Date 

The FAA must receive comments on this 

AD action by May 11, 2015. 

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15950 Federal Register / Vol. 80, No. 58 / Thursday, March 26, 2015 / Proposed Rules 

(b) Affected ADs 

This AD replaces AD 2012–18–05, 

Amendment 39–17181 (77 FR 54793, 

September 6, 2012). 

(c) Applicability 

This AD applies to The Boeing Company 

airplanes identified in paragraphs (c)(1) 

through (c)(8) of this AD, certificated in any 

category, and equipped with center wing fuel 

tanks and Boeing original equipment 

manufacturer-installed auxiliary fuel tanks. 

For airplanes on which the auxiliary fuel 

tanks have been removed, the actions 

specified for the auxiliary fuel tanks are not 

required. 

(1) Model DC–9–11, DC–9–12, DC–9–13, 

DC–9–14, DC–9–15, and DC–9–15F airplanes. 

(2) Model DC–9–21 airplanes. 

(3) Model DC–9–31, DC–9–32, DC–9–32 

(VC–9C), DC–9–32F, DC–9–33F, DC–9–34, 

DC–9–34F, and DC–9–32F (C–9A, C 9B) 

airplanes. 

(4) Model DC–9–41 airplanes. 

(5) Model DC–9–51 airplanes. 

(6) Model DC–9–81 (MD–81), DC–9–82 

(MD–82), DC–9–83 (MD–83), and DC–9–87 

(MD–87) airplanes. 

(7) Model MD–88 airplanes. 

(8) Model MD–90–30 airplanes. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 28, Fuel. 

(e) Unsafe Condition 

This AD was prompted by fuel system 

reviews conducted by the manufacturer. We 

are issuing this AD to reduce the potential of 

ignition sources inside fuel tanks, which, in 

combination with flammable fuel vapors, 

could result in fuel tank explosions and 

consequent loss of the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Retained Criteria for Operation 

This paragraph restates the actions 

required by paragraph (g) of AD 2012–18–05, 

Amendment 39–17181 (77 FR 54793, 

September 6, 2012), with a new compliance 

time. Except as provided by paragraphs (h) 

and (i) of this AD: As of 42 months after the 

effective date of this AD, no person may 

operate any airplane affected by this AD 

unless an amended type certificate or 

supplemental type certificate that 

incorporates the design features and 

requirements described in paragraphs (g)(1) 

and (g)(2) of this AD has been approved by 

the Manager, Los Angeles Aircraft 

Certification Office (ACO), FAA, and those 

design features are installed on the airplane. 

(1) Each electrically powered fuel pump 

installed in the center wing tank or auxiliary 

fuel tank must have a protective device 

installed to detect electrical faults that can 

cause arcing and burn through the fuel pump 

housing. The same device must shut off the 

pump by automatically removing electrical 

power from the pump when such faults are 

detected. When a fuel pump is shut off as the 

result of detection of an electrical fault, the 

device must stay latched off until the fault is 

cleared through maintenance action and 

verified that the pump and the electrical 

power feed are safe for operation. 

(2) Additional design features must be 

installed to detect when any center wing tank 

or auxiliary fuel tank pump is running in an 

empty fuel tank. The prospective pump 

shutoff system must shut off each pump no 

later than 60 seconds after the fuel tank is 

emptied. The pump shutoff system design 

must preclude undetected running of a fuel 

pump in an empty tank, after the pump was 

commanded off manually or automatically. 

(h) New: Optional Methods of Compliance 

For Model DC–9–81 (MD–81), DC–9–82 

(MD–82), DC–9–83 (MD–83), DC–9–87 (MD– 

87), and Model MD–88 airplanes; and Model 

MD–90–30 airplanes: In lieu of doing the 

requirements of paragraph (g) of this AD, do 

the applicable actions specified in 

paragraphs (h)(1), (h)(2), and (h)(3) of this 

AD. 

(1) For Model DC–9–81 (MD–81), DC–9–82 

(MD–82), DC–9–83 (MD–83), DC–9–87 (MD– 

87), and Model MD–88 airplanes: Do the 

applicable actions specified in paragraphs 

(h)(1)(i), (h)(1)(ii), and (h)(1)(iii) of this AD. 

(i) For all airplanes identified in paragraph 

(h)(1) of this AD: Within the compliance time 

specified in paragraph (g) of this AD, install 

ground fault interrupter (GFI) relays, in 

accordance with the Accomplishment 

Instructions of Boeing Service Bulletin 

MD80–28–228, dated September 27, 2013. 

(ii) For airplanes identified in Boeing MD– 

80 Service Bulletin 28–53, Revision 1, dated 

April 16, 1992: Prior to or concurrently with 

accomplishing the action specified in 

paragraph (h)(1)(i) of this AD, install a low 

fuel pressure indication system, in 

accordance with the Accomplishment 

Instructions of Boeing MD–80 Service 

Bulletin 28–53, Revision 1, dated April 16, 

1992. 

(iii) For airplanes identified in Boeing MD– 

80 Service Bulletin 28–63, Revision 2, dated 

April 8, 1992: Prior to or concurrently with 

accomplishing the action specified in 

paragraph (h)(1)(i) of this AD, install a low 

fuel pressure indication inhibition system, in 

accordance with the Accomplishment 

Instructions of Boeing MD–80 Service 

Bulletin 28–63, Revision 2, dated April 8, 

1992. 

(2) For Model MD–90–30 airplanes: Within 

the compliance time specified in paragraph 

(g) of this AD, install brackets and mod block 

rails, and install GFI relays, in accordance 

with the Accomplishment Instructions of 

Boeing Service Bulletin MD90–28–013, dated 

September 27, 2013. 

(3) For all airplanes: Within 30 days after 

accomplishing the actions required by 

paragraph (h)(1) or (h)(2) of this AD or within 

30 days after the effective date of this AD, 

whichever occurs later, revise the 

maintenance or inspection program, as 

applicable, to incorporate the Critical Design 

Configuration Control Limitations (CDCCLs), 

Airworthiness Limitations Instructions 

(ALIs), and short-term extensions specified in 

Appendixes B, C, and D of Boeing Special 

Compliance Item Report MDC–92K9145, 

Revision M, dated February 5, 2013. The 

initial compliance time for accomplishing the 

actions specified in the ALIs is at the later 

of the times in paragraphs (h)(3)(i) and 

(h)(3)(ii) of this AD. Doing the revision of the 

maintenance or inspection program, as 

applicable, required by this paragraph 

terminates the requirements in paragraphs (g) 

and (h) of AD 2008–11–15, Amendment 39– 

15538 (73 FR 30746, May 29, 2008). 

(i) At the applicable time specified in in 

Appendix C of Boeing Special Compliance 

Item Report MDC–92K9145, Revision M, 

dated February 5, 2013, except as provided 

by Appendix D, of Boeing Special 

Compliance Item Report MDC–92K9145, 

Revision M, dated February 5, 2013. 

(ii) Within 30 days after accomplishing the 

actions required by paragraph (h)(1) or (h)(2) 

of this AD, or within 30 days after the 

effective date of this AD, whichever occurs 

later. 

(i) New: Optional Universal Fault 

Interrupter (UFI) Installation 

In lieu of doing the requirements of 

paragraph (g) of this AD, within the 

compliance time specified in paragraph (g) of 

this AD install a TDG Aerospace Inc. UFI 

using a method approved in accordance with 

the procedures specified in paragraph (l) of 

this AD. 

Note 1 to paragraph (i) of this AD: TDG 

Aerospace STC ST02502LA ([http://

rgl.faa.gov/Regulatory_and_Guidance_

Library/rgstc.nsf/0/

4d132827a425d7de86257cd3004dfc02/

$FILE/ST02502LA.pdf)] provides additional 

guidance for installing the TDG UFI. 

(j) No Alternative Actions, Intervals, and 

CDCCLs 

After the maintenance or inspection 

program, as applicable, has been revised as 

required by paragraph (h)(3) of this AD, no 

alternative actions (e.g., inspections), 

intervals, or CDCCLs may be used unless the 

actions, intervals, or CDCCLs are approved as 

an alternative method of compliance (AMOC) 

in accordance with the procedures specified 

in paragraph (l) of this AD. 

(k) Credit for Previous Actions 

This paragraph provides credit for the 

actions specified in paragraphs (h)(1)(ii) and 

(h)(1)(iii) of this AD, if those actions were 

performed before the effective date of this AD 

using any of the service information specified 

in paragraph (k)(1), (k)(2), or (k)(3) of this AD. 

(1) Boeing MD–80 Service Bulletin 28–53, 

dated April 8, 1991. 

(2) Boeing MD–80 Service Bulletin 28–63, 

dated, June 14, 1991. 

(3) Boeing MD–80 Service Bulletin 28–63, 

Revision 1, dated July 19, 1991. 

(l) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Los Angeles Aircraft 

Certification Office (ACO), 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 local Flight Standards District Office, as 

appropriate. If sending information directly 

to the manager of the ACO, send it to the 

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Federal Register / Vol. 80, No. 58 / Thursday, March 26, 2015 / Proposed Rules 15951 

attention of the person identified in 

paragraph (m)(1) of this AD. Information may 

be emailed to: 9-ANM-LAACO-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 

required by this AD if it is approved by the 

Boeing Commercial Airplanes Organization 

Designation Authorization (ODA) that has 

been authorized by the Manager, Los Angeles 

ACO, to make those findings. For a repair 

method to be approved, the repair must meet 

the certification basis of the airplane, and the 

approval must specifically refer to this AD. 

(4) AMOCs approved for AD 2012–18–05, 

Amendment 39–17181 (77 FR 54793, 

September 6, 2012), are approved as AMOCs 

for the corresponding provisions of this AD. 

(m) Related Information 

(1) For more information about this AD, 

contact Se ́rj Harutunian, Aerospace Engineer, 

Propulsion Branch, ANM–140L, FAA, Los 

Angeles Aircraft Certification Office (ACO), 

3960 Paramount Boulevard, Lakewood, CA 

90712–4137; phone: 562–627–5254; fax: 562– 

627–5210; email: serj.harutunian@faa.gov. 

(2) For service information identified in 

this AD, contact Boeing Commercial 

Airplanes, Attention: Data & Services 

Management, 3855 Lakewood Boulevard, MC 

D800–0019, Long Beach, CA 90846–0001; 

telephone 206–544–5000, extension 2; fax 

206–766–5683; 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. 

Issued in Renton, Washington, on February 

11, 2015. 

Jeffrey E. Duven, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2015–06745 Filed 3–25–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF JUSTICE 

28 CFR Part 16 

[CPCLO Order No. 004–2014] 

Privacy Act of 1974; Implementation 

AGENCY: Department of Justice. 

ACTION: Notice of proposed rulemaking. 

SUMMARY: As described in the notice 

section of this issue of the Federal 

Register, the Department of Justice 

(Department or DOJ) has published a 

notice of a new Department-wide 

Privacy Act system of records, 

‘‘Department of Justice, Giglio 

Information Files,’’ JUSTICE/DOJ–017. 

This system has been established to 

enable DOJ investigative agencies to 

collect and maintain records of potential 

impeachment information and to 

disclose such information to DOJ 

prosecuting offices in order to ensure 

that prosecutors receive sufficient 

information to meet their obligations 

under Giglio v. United States, 405 U.S. 

150 (1972), as well as to enable DOJ 

prosecuting offices to maintain records 

of potential impeachment information 

obtained from DOJ investigative 

agencies, other federal agencies, and 

state and local agencies and to disclose 

such information in accordance with the 

Giglio decision. For the reasons 

provided below, the Department 

proposes to amend its Privacy Act 

regulations by establishing an 

exemption for records in this system 

from certain provisions of the Privacy 

Act pursuant to 5 U.S.C. 552a(j) and (k). 

DATES: Comments must be received by 

April 27, 2015. 

ADDRESSES: Address all comments to 

the Privacy Analyst, Office of Privacy 

and Civil Liberties, National Place 

Building, 1331 Pennsylvania Avenue 

NW., Suite 1000, Washington, DC 

20530, or by facsimile to (202) 307– 

0693. To ensure proper handling, please 

reference the CPCLO Order Number on 

your correspondence. You may review 

an electronic version of the proposed 

rule at http://www.regulations.gov, and 

you may also comment by using that 

Web site’s comment form for this 

regulation. Please include the CPCLO 

Order Number in the subject box. 

Please note that the Department is 

requesting that electronic comments be 

submitted before midnight Eastern Time 

on the day the comment period closes 

because this is when http://

www.regulations.gov terminates the 

public’s ability to submit comments. 

Commenters in time zones other than 

Eastern Time may want to consider this 

so that their electronic comments are 

received. All comments sent via regular 

or express mail will be considered 

timely if postmarked on or before the 

day the comment period closes. 

Posting of Public Comments: Please 

note that all comments received are 

considered part of the public record and 

made available for public inspection 

online at http://www.regulations.gov 

and in the Department’s public docket. 

Such information includes personally 

identifying information (such as your 

name, address, etc.) voluntarily 

submitted by the commenter. 

If you want to submit personally 

identifying information (such as your 

name, address, etc.) as part of your 

comment, but do not want it to be 

posted online or made available in the 

public docket, you must include the 

phrase ‘‘PERSONALLY IDENTIFYING 

INFORMATION’’ in the first paragraph 

of your comment. You must also place 

all the personally identifying 

information you do not want posted 

online or made available in the public 

docket in the first paragraph of your 

comment and identify what information 

you want redacted. 

If you want to submit confidential 

business information as part of your 

comment, but do not want it to be 

posted online or made available in the 

public docket, you must include the 

phrase ‘‘CONFIDENTIAL BUSINESS 

INFORMATION’’ in the first paragraph 

of your comment. You must also 

prominently identify confidential 

business information to be redacted 

within the comment. If a comment has 

so much confidential business 

information that it cannot be effectively 

redacted, all or part of that comment 

may not be posted online or made 

available in the public docket. 

Personally identifying information 

and confidential business information 

identified and located as set forth above 

will be redacted and the comment, in 

redacted form, will be posted online and 

placed in the Department’s public 

docket file. Please note that the Freedom 

of Information Act applies to all 

comments received. If you wish to 

inspect the agency’s public docket file 

in person by appointment, please see 

the FOR FURTHER INFORMATION CONTACT

paragraph. 

FOR FURTHER INFORMATION CONTACT: 

Tricia Francis, Executive Office for 

United States Attorneys, FOIA/Privacy 

Act Staff, 600 E Street NW., Suite 7300, 

Washington, DC 20530, or by facsimile 

at (202) 252–6047. 

SUPPLEMENTARY INFORMATION: In the 

notices section of this issue of the 

Federal Register, the Department of 

Justice has published a system of 

records notice for the system entitled, 

‘‘Department of Justice Giglio 

Information Files,’’ JUSTICE/DOJ–017. 

This Department-wide system notice 

replaces the notice for the system 

entitled, ‘‘United States Attorney’s 

Office, Giglio Information Files,’’ 

JUSTICE/USA–018, 65 FR 75308 (Dec. 

1, 2000). That system of records was 

exempt from certain provisions of the 

Privacy Act pursuant to 5 U.S.C. 552a(j) 

and (k). Those exemptions are codified 

in the Code of Federal Regulations 

(CFR) section for Exemption of United 

States Attorneys Systems (28 CFR 

16.81(g) and (h)). The Department is 

now proposing to establish a new CFR 

section for exemptions of the JUSTICE/ 

DOJ–017 system (28 CFR 16.136) and to 

mstockstill on DSK4VPTVN1PROD with PROPOSALS