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and the service information specified in paragraphs (p)(1)(i) through (p)(1)(vi) of this AD, for related information.

(i) Airbus Mandatory Service Bulletin A310–57–2082, Revision 03, dated November 15, 2010.

(ii) Airbus Service Bulletin A310–57–2081, dated June 11, 2002.

(iii) Airbus Service Bulletin A310–57– 2081, Revision 03, dated October 13, 2010.

(iv) Airbus Service Bulletin A310–57– 2082, dated June 11, 2002.

(v) Airbus Repair Instruction R573–49237, Revision D, dated July 16, 2003.

(vi) Airbus Repair Instruction R573–49243, Revision C, dated July 16, 2003.

(2) For service information identified in this AD, contact Airbus SAS–EAW (Airworthiness Office), 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51; email account.airworth-eas@ airbus.com; Internet http://www.airbus.com. You may review copies of the 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 January 20, 2013. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.

[FR Doc. 2013–02448 Filed 2–4–13; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2012–0270; Directorate Identifier 2011–NM–113–AD]** 

**RIN 2120–AA64**

**Airworthiness Directives; Fokker Services B.V. Airplanes** 

**AGENCY :**  Federal Aviation Administration (FAA), DOT.

**ACTION :**  Supplemental notice of proposed rulemaking (NPRM); reopening of comment period.

**SUMMARY :**  We are revising an earlier proposed airworthiness directive (AD) for all Fokker Services B.V. Model F.27 Mark 050 airplanes, and Model F.28 Mark 0070 and 0100 airplanes. That NPRM proposed to require inspecting and, if necessary, adjusting, the torque values of nuts on circuit breakers, contactors, and terminal blocks of the electrical power center (EPC) and battery relay panel. This proposed AD would also require inspecting to determine if certain parts are installed, and installing the parts if necessary. This action revises that NPRM by adding a previously omitted terminal block to the required actions. We are proposing this AD to detect and correct loose nuts, which could result in arcing and potentially an onboard fire, possibly resulting in damage to the airplane and injury to occupants or maintenance personnel. Since these actions impose an additional burden over that proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.

**DATES :**  We must receive comments on this proposed AD by March 22, 2013.

**ADDRESSES :**  You may send comments 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: U.S. Department of Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.

For service information identified in this proposed AD, contact Fokker Services B.V., Technical Services Dept., P.O. Box 231, 2150 AE Nieuw-Vennep, the Netherlands; telephone +31 (0)252– 627–350; fax +31 (0)252–627–211; email technicalservices.fokkerservices @stork.com; Internet http:// www.myfokkerfleet.com. You may review copies of the 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.
Examining the AD Docket

You may examine the AD docket on the Internet at http:// www.regulations.gov; or in person at the Docket Operations office 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 Operations office (telephone (800) 647–5527) is in the **ADDRESSES** section. Comments will be available in the AD docket shortly after receipt.

**FOR FURTHER INFORMATION CONTACT :**  Tom Rodriguez, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, Washington 98057–3356; telephone (425) 227–1137; fax (425) 227–1149.

**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–2012–0270; Directorate Identifier 2011–NM–113–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 based on 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

We proposed to amend 14 CFR part 39 with an earlier NPRM for the specified products, which was published in the Federal Register on March 21, 2012 (77 FR 16486). That earlier NPRM proposed to require actions intended to address the unsafe condition for the products listed above.

Since that NPRM (77 FR 16486, March 21, 2012) was issued, we have determined that an additional terminal block used in some Model F.28 Mark 0100 airplanes needs to be included in the required actions proposed in the earlier NPRM. European Aviation Safety Agency (EASA) has issued Airworthiness Directive 2012–0050, dated March 27, 2012 (referred to after this as ‘‘the MCAI’’), to add that terminal block to their required actions. The MCAI states:

In December 1989, Fokker issued Service Bulletin (SB) SBF50–24–A013 and SBF100– 24–A011 (both Alert Bulletins) to instruct operators to inspect and adjust several torque values of bus bars and contactors in the EPC. The Civil Aviation Authority of The Netherlands (CAA–NL, formerly RLD) issued AD (BLA) 89–159 and BLA 89–157 respectively (both now at issue 2), to require operators of the affected aeroplanes to comply with the instructions of these SB’s.

Since those [Dutch] ADs were issued, several operators reported finding loose nuts on contactors in the EPC of Fokker 50/60 aeroplanes in post-SBF50–24–A013 configuration and on Fokker 70/100 aeroplanes in post-SBF100–24–A011 configuration. In some cases, the findings included damaged (burned) contactors.

This condition, if not detected and corrected, could lead to arcing and, in


### 8059 Federal Register / Vol. 78, No. 24 / Tuesday, February 5, 2013 / Proposed Rules

combination with other factors, to an onboard fire, possibly resulting in damage to the aeroplane and injury to occupants or maintenance personnel. EASA issued AD 2011–0083 [referenced in the earlier FAA NPRM (77 FR 16486, March 21, 2012)] to address this unsafe condition.

After that [EASA] AD was issued, it was noticed that terminal block TB4906A, used in some Fokker 100 aeroplanes, was missing from the list of affected terminal blocks, as specified in Fokker SBF100–24–043. To correct this oversight, Fokker Services issued Revision 1 of SBF100–24–043, adding terminal block TB4906A.

For the reasons described above, this [EASA] AD retains the requirements of EASA AD 2011–0083, which is superseded, and for F28 Mark 0100 aeroplanes, adds required action for the missing terminal block TB4906A by making reference to SBF100– 24–043 Revision 1. The required actions include doing a general visual inspection to determine if either the lock washer, flat washer and nut, or locking nut and flat washer, are installed; installing a new lock washer or self-locking nut, if necessary; and applying torque inspection lacquer. You may obtain further information by examining the MCAI in the AD docket.

Relevant Service Information

Fokker Services B.V. has issued Service Bulletin SBF100–24–043, Revision 1, dated December 15, 2011 (for Model F.28 Mark 0070 and 0100 airplanes). The actions described in this service information are intended to correct the unsafe condition identified in the MCAI.

Comments

We gave the public the opportunity to comment on the earlier NPRM (77 FR 16486, March 21, 2012). We received no comments on that NPRM or on the determination of the cost to the public. FAA’s Determination and Requirements of This Proposed AD

This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are proposing this AD because we evaluated all pertinent information and determined an unsafe condition exists and is likely to exist or develop on other products of the same type design.

Certain changes described above expand the scope of the earlier NPRM (77 FR 16486, March 21, 2012). As a result, we have determined that it is necessary to reopen the comment period to provide additional opportunity for the public to comment on this proposed AD. Difference Between the Proposed AD and the MCAI

The MCAI specifies credit for actions done according to Fokker Service Bulletin SBF100–24–043, dated February 10, 2011, which does not include inspecting the additional terminal block part number. This proposed AD does not specify such credit because we determined that inspecting for the additional terminal block more properly meets the intent of this proposed AD. This difference has been coordinated with EASA.
Costs of Compliance

Based on the service information, we estimate that this proposed AD would affect about 4 products of U.S. registry. We also estimate that it would take about 5 work-hours per product to comply with the basic requirements of this proposed AD. The average labor rate is $85 per work-hour. Based on these figures, we estimate the cost of the proposed AD on U.S. operators to be $1,700, or $425 per product.

In addition, we estimate that any necessary follow-on actions would take about 4 work-hours and require parts costing $25, for a cost of $365 per product. We have no way of determining the number of products that may need these actions.
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 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 this 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.

We prepared a regulatory evaluation of the estimated costs to comply with this proposed AD and placed it in the AD docket.
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 adding the following new AD:

Fokker Services B.V.: Docket No. FAA– 2012–0270; Directorate Identifier 2011–
NM–113–AD.

(a) Comments Due Date

We must receive comments by March 22,

2013.
(b) Affected ADs

None.
(c) Applicability

This AD applies to all Fokker Services B.V. Model F.27 Mark 050 airplanes, and Model F.28 Mark 0070 and 0100 airplanes, certificated in any category.
(d) Subject

Air Transport Association (ATA) of America Code 24: Electric power.

(e) Reason

This AD was prompted by reports of loose nuts on contactors in the electrical power center (EPC), and in some cases, burned contactors. We are issuing this AD to detect and correct loose nuts, which could result in


### 8060 Federal Register / Vol. 78, No. 24 / Tuesday, February 5, 2013 / Proposed Rules

arcing and potentially an onboard fire, possibly resulting in damage to the airplane and injury to occupants or maintenance personnel.
(f) Compliance

You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
(g) Actions

Within 24 months after the effective date of this AD, do the actions specified in paragraphs (g)(1), (g)(2), and (g)(3) of this AD.

(1) Do a torque check of the nuts and circuit breakers, contactors, and terminal blocks of the EPC and battery relay panel, as applicable, and do all applicable adjustments of the torque values, in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF50–24–032, including Fokker Manual Change Notification— Maintenance Documentation MCNM–F50– 072, dated February 10, 2011 (for Model F.27 Mark 050 airplanes); or the Accomplishment Instructions of Fokker Service Bulletin SBF100–24–043, Revision 1, dated December 15, 2011 (for Model F.28 Mark 0070 and 0100 airplanes). Do all applicable adjustments before further flight.

(2) Do a general visual inspection of the contacts and nuts on circuit breakers, contactors, and terminal blocks of the EPC and battery relay panel to determine if either the lock washer, flat washer and nut, or locking nut and flat washer are installed, and do all applicable installations; in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF50–24–032, including Fokker Manual Change Notification—Maintenance Documentation MCNM–F50–072, dated February 10, 2011 (for Model F.27 Mark 050 airplanes); or the Accomplishment Instructions of Fokker Service Bulletin SBF100–24–043, Revision 1, dated December 15, 2011 (for Model F.28 Mark 0070 and 0100 airplanes). Do all applicable installations before further flight.

(3) Before further flight after accomplishing any check required by paragraph (g)(1) of this AD or any inspection required by paragraph (g)(2) of this AD: Apply torque inspection lacquer, in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF50–24–032, including Fokker Manual Change Notification— Maintenance Documentation MCNM–F50– 072, dated February 10, 2011 (for Model F.27 Mark 050 airplanes); or the Accomplishment Instructions of Fokker Service Bulletin SBF100–24–043, Revision 1, dated December 15, 2011 (for Model F.28 Mark 0070 and 0100 airplanes).

(h) Other FAA AD Provisions

The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM–116, Transport Airplane Directorate, 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 International Branch, send it to ATTN: Tom Rodriguez, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, Washington 98057– 3356; telephone (425) 227–1137; fax (425) 227–1149. Information may be emailed to: 9- ANM-116-AMOC-REQUESTS@faa.gov. 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. The AMOC approval letter must specifically reference this AD.

(2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved.Corrective actions are considered FAAapproved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service.

(i) Related Information

Refer to MCAI European Aviation Safety Agency Airworthiness Directive 2012–0050, dated March 27, 2012, and the service information specified in paragraphs (i)(1) and (i)(2) of this AD, for related information.

(1) Fokker Service Bulletin SBF50–24–032, including Fokker Manual Change Notification—Maintenance Documentation MCNM–F50–072, dated February 10, 2011.

(2) Fokker Service Bulletin SBF100–24– 043, Revision 1, dated December 15, 2011 (for Model F.28 Mark 0070 and 0100 airplanes).

(3) For service information identified in this AD, contact Fokker Services B.V., Technical Services Dept., P.O. Box 231, 2150 AE Nieuw-Vennep, the Netherlands; telephone +31 (0)252–627–350; fax +31 (0)252–627–211; email technicalservices.fokkerservices@stork.com;
Internet http://www.myfokkerfleet.com . You may review copies of the 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 January
25, 2013. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service.

[FR Doc. 2013–02451 Filed 2–4–13; 8:45 am]

**BILLING CODE 4910–13–P DEPARTMENT OF THE TREASURY** 

**Internal Revenue Service**

**26 CFR Part 1**

**[REG–106918–08]**

**RIN 1545–BH89**

**Treatment of Grantor of an Option on a Partnership Interest** 

**AGENCY :**  Internal Revenue Service (IRS), Treasury.

**ACTION :**  Notice of proposed rulemaking.

**SUMMARY :**  This document contains proposed regulations relating to the tax treatment of noncompensatory options and convertible instruments issued by a partnership. Specifically, the proposed regulations expand the characterization rule measurement events to include certain transfers of interests in theissuing partnership and other lookthrough entities, and provide additional guidance in determining the character of the grantor’s gain or loss as a result of a closing transaction with respect to, or a lapse of, an option on a partnership interest. The proposed regulations will affect partnerships that issue noncompensatory options, the partners of such partnerships, and the holders of such options.

**DATES :**  Written or electronic comments and requests for a public hearing must be received by May 6, 2013.

**ADDRESSES :**  Send submissions to: CC:PA:LPD:PR (REG–106918–08), room 5203, Internal Revenue Service, PO Box 7604, Ben Franklin Station, Washington,DC 20044. Submissions may be handdelivered Monday through Friday between the hours of 8 a.m. and 4 p.m. to CC:PA:LPD:PR (REG–106918–08), Courier’s Desk, Internal Revenue Service, 1111 Constitution Avenue NW., Washington, DC, or sent electronically via the Federal eRulemaking Portal at www.regulations.gov (IRS REG–106918– 08).

**FOR FURTHER INFORMATION CONTACT :**  Concerning the proposed regulations under § 1.761–3, Benjamin Weaver at (202) 622–3050; concerning the proposed regulations under § 1.1234–3, Shawn Tetelman at (202) 622–3930; concerning submissions of comments and requests for a public hearing, Oluwafunmilayo (Funmi) Taylor, (202) 622–7180 (not toll free numbers).

**SUPPLEMENTARY INFORMATION :**  Background

This document contains proposed amendments to 26 CFR part 1 under sections 761 and 1234 of the Internal Revenue Code (Code). On January 22,