This section of the FEDERAL REGISTER

contains notices to the public of the proposed

issuance of rules and regulations. The

purpose of these notices is to give interested

persons an opportunity to participate in the

rule making prior to the adoption of the final

rules.

Proposed Rules Federal Register

3139 

Vol. 79, No. 12 

Friday, January 17, 2014 

DEPARTMENT OF AGRICULTURE 

Agricultural Marketing Service 

7 CFR Part 1216 

[Document Number AMS–FV–13–0089] 

Peanut Promotion, Research and 

Information Order; Continuance 

Referendum 

AGENCY: Agricultural Marketing Service, 

Agriculture. 

ACTION: Referendum order. 

SUMMARY: This document directs that a 

referendum be conducted among 

eligible producers of peanuts to 

determine whether they favor 

continuance of the Peanut Promotion, 

Research and Information Order (Order). 

DATES: The referendum will be 

conducted from April 7 through April 

18, 2014. To vote in this referendum, 

producers must have paid assessments 

on peanuts produced during the 

representative period from January 1 

through December 31, 2013, and must 

currently be a peanut producer. 

ADDRESSES: Copies of the Order may be 

obtained from: Referendum Agent, 

Promotion and Economics Division 

(PED), Fruit and Vegetable Program 

(FVP), AMS, USDA, Stop 0244, Room 

1406–S, 1400 Independence Avenue 

SW., Washington, DC 20250–0244; 

telephone: (888) 720–9917 (toll free), 

(202) 720–9915 (direct line); facsimile: 

(202) 205–2800. 

FOR FURTHER INFORMATION CONTACT: 

Jeanette Palmer, Marketing Specialist, 

PED, FVP, AMS, USDA, Stop 0244, 

Room 1406–S, 1400 Independence 

Avenue SW., Washington, DC 20250– 

0244; telephone: (888) 720–9917 (toll 

free), (202) 720–9915 (direct line); 

facsimile: (202) 205–2800; or electronic 

mail: Jeanette.Palmer@ams.usda.gov. 

SUPPLEMENTARY INFORMATION: Pursuant 

to the Commodity Promotion, Research 

and Information Act of 1996 (7 U.S.C. 

7411–7425) (Act), it is hereby directed 

that a referendum be conducted to 

ascertain whether continuance of the 

Order is favored by producers of 

peanuts covered under the program. The 

Order is authorized under the Act. 

The representative period for 

establishing voter eligibility for the 

referendum shall be the period from 

January 1 through December 31, 2013. 

Persons who are currently producers of 

peanuts, and who produced peanuts 

and paid assessments during the 

representative period are eligible to 

vote. Persons who received an 

exemption from assessments for the 

entire representative period are 

ineligible to vote. The referendum shall 

be conducted by mail from April 7 

through April 18, 2014. 

Section 518 of the Act authorizes 

continuance referenda. Under section 

1216.82 of the Order, the U.S. 

Department of Agriculture (Department) 

must conduct a referendum every five 

years or when 10 percent or more of the 

eligible peanut producers petition the 

Secretary of Agriculture to hold a 

referendum to determine if persons 

subject to assessment favor continuance 

of the Order. The Department would 

continue the Order if continuance is 

approved by a simple majority of the 

producers voting in the referendum. 

In accordance with the Paperwork 

Reduction Act of 1995 (44 U.S.C. 

chapter 35), the referendum ballot has 

been approved by the Office of 

Management and Budget (OMB) and 

assigned OMB No. 0581–0093. It has 

been estimated that there are 

approximately 9,208 producers who 

will be eligible to vote in the 

referendum. It will take an average of 15 

minutes for each voter to read the voting 

instructions and complete the 

referendum ballot. 

Jeanette Palmer and Sonia Jimenez, 

PED, FVP, AMS, USDA, Stop 0244, 

Room 1406–S, 1400 Independence 

Avenue SW., Washington, DC 20250– 

0244, are designated as the referendum 

agents to conduct this referendum. The 

referendum procedures 7 CFR 1216.100 

through 1216.107, which were issued 

pursuant to the Act, shall be used to 

conduct the referendum. 

The referendum agents will mail the 

ballots to be cast in the referendum and 

voting instructions to all known 

producers prior to the first day of the 

voting period. Persons who are 

producers at the time of the referendum 

and who produced peanuts and paid 

assessments during the representative 

period are eligible to vote. Persons who 

received an exemption from 

assessments during the entire 

representative period are ineligible to 

vote. Any eligible producer who does 

not receive a ballot should contact the 

referendum agent no later than one 

week before the end of the voting 

period. Ballots must be received by the 

referendum agent, not later than close of 

business 4:30 p.m. Eastern time, April 

18, 2014, in order to be counted. 

List of Subjects in 7 CFR Part 1216 

Administrative practice and 

procedure, Advertising, Consumer 

information, Marketing agreements, 

Peanut promotion, Reporting and 

recordkeeping requirements. 

Authority: 7 U.S.C. 7411–7425 and 7 

U.S.C. 7401. 

Dated: January 10, 2014. 

Rex A. Barnes, 

Associate Administrator. 

[FR Doc. 2014–00773 Filed 1–16–14; 8:45 am] 

BILLING CODE 3410–02–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2007–28413; Directorate 

Identifier 2007–NE–25–AD] 

RIN 2120–AA64 

Airworthiness Directives; General 

Electric Company Turbofan Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to supersede 

airworthiness directives (ADs) 90–26– 

01, 91–20–02, and 2009–05–02, which 

apply to all General Electric Company 

(GE) CF6–80C2 and CF6–80E1 series 

turbofan engines. Since we issued ADs 

90–26–01, 91–20–02, and 2009–05–02, 

we received a report of an undercowl 

fire caused by a manifold high-pressure 

fuel leak, and several additional reports 

of fuel leaks. This proposed AD would 

require additional repetitive 

inspections, replacement of tube (block) 

clamp, and inspection of fuel manifolds 

for wear at each tube (block) clamp 

location. We are proposing this AD to 


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prevent failure of the fuel manifold, 

which could lead to uncontrolled 

engine fire, engine damage, and damage 

to the airplane. 

DATES: We must receive comments on 

this proposed AD by March 3, 2014. 

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 General 

Electric Company, GE Aviation, Room 

285, 1 Neumann Way, Cincinnati, OH 

45215; phone: 513–552–3272; email: 

geae.aoc@ge.com. You may view this 

service information at the FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, 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–2007– 

28413; 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: 

Kasra Sharifi, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, Burlington, MA. 01830; 

phone 781–238–7773; fax: 781–238– 

7199; email: kasra.sharifi@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–2007–28413; Directorate Identifier 

2007–NE–25–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 December 20, 1990, we issued AD 

90–26–01 (55 FR 49611, November 30, 

1990), for GE CF6–80C2 series turbofan 

engines. That AD requires replacing fuel 

manifold, part numbers (P/Ns) 

1303M31G04 and 1303M32G04, within 

30 calendar days after the effective date 

of the AD. That AD resulted from a 

report of an engine fire. 

On November 15, 1991, we issued AD 

91–20–02 (56 FR 55231, October 25, 

1991), for the same engines. That AD 

requires replacing fuel manifold, P/Ns 

1303M31G06, 1303M32G06, 

1303M31G07, 1303M32G07, 

1303M31G08, and 1303M32G08, at the 

next engine removal, but no later than 

June 30, 1993. That AD also resulted 

from a report of an engine fire. 

On March 31, 2009, we issued AD 

2009–05–02 (74 FR 8161, February 24, 

2009), for GE CF6–80C2 and CF6–80E1 

series turbofan engines with fuel 

manifolds, P/Ns 1303M31G12 and 

1303M32G12, installed in drainless fuel 

manifold assemblies. That AD requires 

removing the loop clamps that hold the 

fuel manifold to the compressor rear 

frame damper brackets, inspecting the 

fuel manifold for wear at each clamp 

location, and replacing the clamps with 

new zero-time parts. That AD also 

requires revising the Airworthiness 

Limitations Section to require repetitive 

fuel manifold inspection and loop 

clamp replacement. That AD resulted 

from reports of fuel leaks during engine 

operation. 

We issued these ADs to prevent 

failure of the fuel manifold, which 

could lead to uncontrolled engine fire, 

engine damage, and damage to the 

airplane. We are superseding these ADs 

to eliminate potentially confusing and 

contradictory requirements in these 

ADs. This proposed AD expands the 

inspection mandated by AD 2009–05–02 

and it expands the list of banned fuel 

manifolds mandated by AD 90–26–01 

and AD 91–20–02. 

Actions Since Previous ADs Were 

Issued 

Since we issued AD 90–26–01 (55 FR 

49611, November 30, 1990); AD 91–20– 

02 (56 FR 55231, October 25, 1991); and 

AD 2009–05–02 (74 FR 8161, February 

24, 2009); we received a report of an 

undercowl fire caused by a fuel 

manifold high-pressure fuel leak in 

engine model CF6–80C2, and several 

additional reports of fuel leaks; four in 

the CF6–80C2 and one in the CF6–80E1 

model engine. 

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 the same 

type design. 

Proposed AD Requirements 

This proposed AD would retain the 

requirements of AD 90–26–01 (55 FR 

49611, November 30, 1990); and AD 91– 

20–02 (56 FR 55231, October 25, 1991); 

to remove certain fuel manifold P/Ns, 

and the requirements of AD 2009–05–02 

(74 FR 8161, February 24, 2009); to 

inspect certain fuel manifold P/Ns and 

replace certain consumable 

components. This proposed AD would 

add a requirement to inspect an 

additional fuel manifold configuration 

and replacement of certain loop clamps. 

This proposed AD would also require 

repetitive inspection and replacement of 

tube (block) clamp, and inspection of 

the fuel manifold for wear at each tube 

(block) clamp location. This proposed 

AD would also require removing certain 

drainless fuel manifold assembly P/Ns 

from service. 

Costs of Compliance 

We estimate that this proposed AD 

would affect 1,126 engines installed on 

airplanes of U.S. registry. We also 

estimate that required parts cost about 

$34,894 per engine. We also estimate 

that is would take about 6 hours to 

accomplish the actions required by this 

AD. The average labor rate is $85 per 

hour. Based on these figures, we 

estimate the total cost of the proposed 

AD to U.S. operators to be $39,864,904. 

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, 


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Federal Register / Vol. 79, No. 12 / Friday, January 17, 2014 / Proposed Rules 3141 

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 proposed 

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 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. 

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: 

■ a. Removing airworthiness directive 

(AD) 90–26–01 (55 FR 49611, November 

30, 1990); AD 91–20–02 (56 FR 55231, 

October 25, 1991); and AD 2009–05–02 

(74 FR 8161, February 24, 2009); and 

■ b. Adding the following new AD: 

General Electric Company: Docket No. FAA– 

2007–28413; Directorate Identifier 2007– 

NE–25–AD. 

(a) Comments Due Date 

The FAA must receive comments on this 

AD action by March 3, 2014. 

(b) Affected ADs 

This AD supersedes AD 90–26–01 (55 FR 

49611, November 30, 1990); AD 91–20–02 

(56 FR 55231, October 25, 1991); and AD 

2009–05–02 (74 FR 8161, February 24, 2009). 

(c) Applicability 

This AD applies to all General Electric 

Company (GE) CF6–80C2 and CF6–80E1 

turbofan engines with fuel manifold, part 

numbers (P/Ns) 1303M31G04,1303M32G04, 

1303M31G06, 1303M32G06, 1303M31G07, 

1303M32G07, 1303M31G08, 

1303M32G08,1308M31G12, 1308M32G12, 

2420M70G01, and 2420M71G01, installed. 

(d) Unsafe Condition 

This AD was prompted by a report of an 

undercowl fire caused by a fuel manifold 

high-pressure fuel leak, and several 

additional reports of fuel leaks. We are 

issuing this AD to prevent failure of the fuel 

manifold, which could lead to uncontrolled 

engine fire, engine damage, and damage to 

the airplane. 

(e) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(1) Fuel Manifold Removal. 

(i) For CF6–80C2 and CF6–80E1 series 

engines, before further flight after the 

effective date of this AD, remove fuel 

manifold, P/Ns 1303M31G04, 1303M32G04, 

1303M31G06, 1303M32G06, 1303M31G07, 

1303M32G07, 1303M31G08, and 

1303M32G08, from service. 

(ii) For CF6–80C2 and CF6–80E1 series 

engines, at the next engine shop visit after 

effective date of this AD, remove fuel 

manifold, P/Ns 1303M31G12, 1303M32G12, 

2420M70G01, and 2420M71G01, from 

service. 

(2) Fuel Manifold, Loop Clamp, and Tube 

(Block) Clamp Inspection and Replacement— 

Drainless Assembly. 

(i) For CF6–80C2 series engines, with fuel 

manifold, P/N 1303M31G12 or 1303M32G12, 

installed, refer to Table 1 to paragraph (e) of 

this AD, accomplish the initial inspections of 

the fuel manifold and replacement of the 

loop clamps in accordance with paragraphs 

3.A and 3.D of GE Service Bulletin (SB) CF6– 

80C2 S/B 73–0326, Revision 4, dated 

December 23, 2009. 

(ii) For CF6–80C2 series engines, with fuel 

manifold, P/Ns 2420M70G01 or 

2420M71G01, installed, refer to Table 1 to 

paragraph (e) of this AD, accomplish the 

initial inspection of the fuel manifold and 

replacement of the loop clamps in 

accordance with paragraphs 3.C and 3.D of 

GE SB CF6–80C2 S/B 73–0326, Revision 4, 

dated December 23, 2009. 

(iii) For CF6–80E1 series engines, with fuel 

manifold, P/Ns 1303M31G12 or 

1303M32G12, installed, refer to Table 1 to 

paragraph (e) of this AD, accomplish the 

initial inspection of the fuel manifold and 

replacement of the loop clamps in 

accordance with paragraphs 3.A and 3.C of 

GE SB CF6–80E1 S/B 73–0061, Revision 4, 

dated December 23, 2009. 

(iv) For CF6–80E1 series engines, with fuel 

manifold P/Ns 2420M70G01 or 2420M71G01 

installed, refer to Table 1 to paragraph (e) of 

this AD, accomplish the initial inspection of 

the fuel manifold and replacement of the 

loop clamps in accordance with paragraphs 

3.B and 3.C of GE SB CF6–80E1 S/B 73–0061, 

Revision 4, dated December 23, 2009. 

(v) Thereafter, inspect fuel manifolds P/Ns 

1303M31G12, 1303M32G12, 2420M70G01, 

and 2420M71G01 installed, within every 

7,500 flight hours (FH) since the last 

inspection, in accordance with paragraphs 

(e)(2)(i) through (e)(2)(iv) of this AD. 

TABLE 1 TO PARAGRAPH (E)—FUEL MANIFOLD INSPECTION AND LOOP CLAMP REPLACEMENT AND INSPECTION CRITERIA

If: Then: 

1—If the engine was previously inspected using any of the following: 

• GE SB CF6–80C2 SB 73–0326 R04, Revision 4, dated December 23, 2009; Then inspect fuel manifold and replace clamps within 7,500 flight hours 

(FH) time-since-last-inspection (TSLI) or within 6 months after the effective date of this AD, whichever occurs first. 

• GE SB CF6–80C2 SB 73–0326, Revision 3, dated April 24, 

2009; 

• GE SB CF6–80E1 SB 73–0061 R04, Revision 4, dated December 23, 2009 or; 

• GE SB CF6–80E1 SB 73–0061, Revision 3, dated April, 24, 

2009. 

2—If the loop clamps installed at last shop visit were previously used 

or of unknown heritage or the engine was previously inspected using 

either of the following: 


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TABLE 1 TO PARAGRAPH (E)—FUEL MANIFOLD INSPECTION AND LOOP CLAMP REPLACEMENT AND INSPECTION CRITERIA— 

Continued 

If: Then: 

• GE CF6–80C2 SB 73–0326, Revision 2, dated August 30, 2007 

or earlier; 

Then inspect fuel manifold and replace clamps within 1,750 FH timesince-last-shop-visit or within 4 months after the effective date of this 

AD, whichever occurs first. 

• GE CF6–80E1 SB 73–0061, Revision 2, dated August 30, 2007 

or earlier. 

3—If the engine is a first-run engine, an engine with zero-time, or has 

new loop clamps previously installed on-wing or at shop visit.

Then inspect fuel manifold and replace clamps within 7,500 FH timesince-new or since zero-time that new loop clamps were installed. 

4—If the engine has already exceeded the 1,750 FH initial inspection 

threshold on the effective date of this AD but has fewer than 4,500 

flight hours TSLI.

Then inspect fuel manifold and replace clamps within 4,500 FH TSLI or 

4 months after the effective date of this AD, whichever occurs first. 

5—If the engine has already exceeded the 4,500 FH initial inspection 

threshold on the effective date of this AD.

Then inspect fuel manifold and replace clamps within 4 months after 

the effective date of this AD. 

(3) For CF6–80C2 series engines, with fuel 

manifold, P/Ns 1303M31G12, 1303M32G12, 

2420M70G01, or 2420M71G01, with tube 

(block) clamp, P/N 1153M26G15, refer to 

Table 2 to paragraph (e) of this AD, 

accomplish the initial inspection of the fuel 

manifold and tube (block) clamp, and 

replacement of the fuel manifold and tube 

(block) clamp, if required based on 

inspection results, in accordance with 

paragraph 3.A of GE SB CF6–80C2 S/B 73– 

0414, dated July 2, 2013. 

(4) For CF6–80E1 series engines, with fuel 

manifold, P/Ns 1303M31G12, 1303M32G12, 

2420M70G01, or 2420M71G01, with tube 

(block) clamp, P/N 1153M26G15, refer to 

Table 2 to paragraph (e) of this AD, 

accomplish the initial inspections of the fuel 

manifold and tube (block) clamp, and 

replacement of the fuel manifold and tube 

(block) clamp, if required based on 

inspection results, in accordance with 

paragraph 3.A of GE SB CF6–80E1 S/B 73– 

0121, dated July 2, 2013. 

(5) Thereafter, inspect fuel manifold, P/Ns 

1303M31G12, 1303M32G12, 2420M70G01, 

and 2420M71G01, within every 7,500 flight 

hours (FH) since the last inspection, in 

accordance with paragraphs (e)(3) and (e)(4) 

of this AD. 

TABLE 2 TO PARAGRAPH (E)—FUEL MANIFOLD AND TUBE (BLOCK) CLAMP INSPECTION AND REPLACEMENT CRITERIA

If: Then: 

1—If the engine is a first run engine or the engine was previously inspected using either of the following: 

• GE SB CF6–80C2 S/B 73–0414, dated July 2, 2013; Then inspect clamps and replace within 7,500 FH TSLI. 

• GE SB CF6–80E1 S/B 73–0121 dated July 02, 2013. 

2—If the engine has already exceeded the 7,500 FH initial inspection 

threshold on the effective date of this AD.

Then inspect clamps and replace within 3 months after the effective 

date of this AD. 

(f) Prohibition Statement 

After the effective date of this AD, do not 

install fuel manifold, P/Ns 1308M31G04, 

1303M32G04, 1303M31G06, 1303M32G06, 

1303M31G07, 1303M32G07, 1303M31G08, 

1303M32G08, 1308M31G12, 1308M32G12, 

2420M70G01, or 2420M71G01, on any 

engine. 

(g) Definition 

For the purpose of this AD, an engine shop 

visit is the induction of an engine into the 

shop for maintenance involving separation of 

pairs of major mating engine flanges (lettered 

flanges), except that the separation of engine 

flanges solely for the purposes of transporting 

the engine without subsequent engine 

maintenance does not constitute an engine 

shop visit. 

(h) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Engine Certification Office, 

FAA, may approve AMOCs for this AD. Use 

the procedures found in 14 CFR 39.19 to 

make your request. Previously approved 

AMOCs for AD 2009–05–02 (74 FR 8161, 

February 24, 2009) remain approved for the 

corresponding requirements of paragraphs 

(e)(1) through (e)(5) of this AD. 

(i) Related Information 

(1) For more information about this AD, 

contact Kasra Sharifi, Aerospace Engineer, 

Engine Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01830; 

phone 781–238–7773; fax: 781–238–7199; 

email: kasra.sharifi@faa.gov. 

(2) General Electric Service Bulletin (SB) 

CF6–80C2 S/B 73–0326, Revision 4, dated 

December 23, 2009, SB CF6–80E1 S/B 73– 

0061, Revision 4, dated December 23, 2009, 

SB CF6–80C2 S/B 73–0414, dated July 2, 

2013, and SB CF6–80E1 S/B 73–0121, dated 

July 2, 2013, pertain to the subject of this AD 

and can be obtained from GE using the 

contact information in paragraph (i)(3) of this 

AD. 

(3) For service information identified in 

this AD, contact General Electric Company, 

GE Aviation, Room 285, 1 Neumann Way, 

Cincinnati, OH 45215; phone: 513–552–3272; 

email: geae.aoc@ge.com. 

(4) You may view this service information 

at the FAA, Engine & Propeller Directorate, 

12 New England Executive Park, Burlington, 

MA. For information on the availability of 

this material at the FAA, call 781–238–7125. 

Issued in Burlington, Massachusetts, on 

December, 24, 2013. 

Frank P. Paskiewicz, 

Acting Director, Aircraft Certification Service. 

[FR Doc. 2014–00833 Filed 1–16–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF THE TREASURY 

Internal Revenue Service 

26 CFR Part 1 

[REG–154890–03] 

RIN 1545–BJ42 

Basis in Interests in Tax-Exempt 

Trusts 

AGENCY: Internal Revenue Service (IRS), 

Treasury. 

ACTION: Notice of proposed rulemaking. 

SUMMARY: This document contains 

proposed regulations that provide rules 

for determining a taxable beneficiary’s 

basis in a term interest in a charitable 

remainder trust upon a sale or other 

disposition of all interests in the trust to 


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