### 74720 Federal Register / Vol. 80, No. 229 / Monday, November 30, 2015 / Proposed Rules

2 79 FR 32172.

3 80 FR 7980.

4 80 FR 32046. and International Operations regulations. 2 In that document we published a chart, listing the Agencies’ regulations in the 12 categories included in the EGRPRA review. The comment period for this Federal Register document closed on September 2, 2014. On February 13, 2015, we published a Federal Register document asking for public comment on three additional categories—Banking Operations; Capital; and the Community Reinvestment Act. 3 The comment period for the second Federal Register document closed on May 14, 2015. On June 5, 2015, the Agencies published a third Federal Register document asking for public comment on three additional categories—Consumer Protection; Directors, Officers and Employees; and Money Laundering. 4 This third Federal Register document announced that the Agencies’ expanded the scope of the EGRPRA review to cover newly issued regulations. The comment period for the third document closed on September 3, 2015. Before the end of the year, the Agencies intend to issue the final Federal Register document, requesting comment on regulations in the last three categories—Rules of Procedure; Safety and Soundness; and Securities, as well as on any other final rules not covered by one of the prior Federal Register documents. In addition, to be as inclusive as possible, the Agencies will invite comment during the comment period for the fourth document on any Agency rule that is issued in final form before the end of the year. Finally, as noted in prior documents, the Agencies will continue to accept comments on any rules included in the prior Federal Register documents for which we have already sought comment during the open comment period in the final Federal Register document.

Dated: November 18, 2015. Thomas J. Curry, Comptroller of the Currency.

By order of the Board of Governors of the Federal Reserve System, November 19, 2015. Robert deV. Frierson, Secretary of the Board.

Dated: November 18, 2015. Robert E. Feldman, Executive Secretary, Federal Deposit Insurance Corporation.
[FR Doc. 2015–30247 Filed 11–27–15; 8:45 am]

**BILLING CODE 4810–33–P; 6210–01–P; 6714–01–P DEPARTMENT OF TRANSPORTATION** 

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2015–6542; Directorate Identifier 2015–NM–038–AD]** 

**RIN 2120–AA64**

**Airworthiness Directives; Embraer S.A. Airplanes** 

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

**ACTION :**  Notice of proposed rulemaking (NPRM).

**SUMMARY :**  We propose to adopt a new airworthiness directive (AD) for all Embraer S.A. Model ERJ 170 airplanes; and all Embraer S.A. Model ERJ 190– 100 STD, –100 LR, –100 IGW, –200 STD, –200 LR, and –200 IGW airplanes. This proposed AD was prompted byreports of cracks in certain engine lowstage bleed check valves. This proposed AD would require replacing the air management system (AMS) controller operation program of the AMS controller processor boards, and replacement of the current low-stage bleed check valve and associated seals. We are proposing this AD to prevent failure of the low-stage bleed check valve, which could result in dual engine in-flight shutdown.

**DATES :**  We must receive comments on this proposed AD by January 14, 2016.

**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: 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 Embraer S.A., Technical Publications Section (PC 060), Av. Brigadeiro Faria Lima, 2170– Putim–12227–901 Sa  ̃ o Jose dos Campos–SP–BRASIL; telephone +55 12 3927–5852 or +55 12 3309–0732; fax +55 12 3927–7546; email distrib@ embraer.com.br; Internet http:// www.flyembraer.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. 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– 6542; 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 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 :**  Ana Martinez Hueto, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 425–227–1622; 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–2015–6542; Directorate Identifier 2015–NM–038–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

The Age ˆncia Nacional de Aviac

 ̧ a  ̃ o Civil (ANAC), which is the aviation authority for Brazil, has issued Brazilian Airworthiness Directive 2015–02–02, dated March 6, 2015 (referred to after this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for Embraer S.A. Model ERJ 190–100 STD, –100 LR, –100 IGW, –200 STD, –200 LR, and –200 IGW airplanes. The MCAI states:


### 74721 Federal Register / Vol. 80, No. 229 / Monday, November 30, 2015 / Proposed Rules

This [Brazilian] AD was prompted by reports of cracks in some engine low-stage bleed check valves having part number (P[/ ]N) 1001447–6. Further analysis hasdetermined that if a new (zero hour) lowstage bleed check valve P/N 1001447–6 is installed in an airplane already equipped with the Air Management System (AMS) controller processor boards containing the AMS Controller Operational Program version Black Label 13, or a later version, premature cracking on the petals of the low-stage bleed check valve is not expected to occur. We are issuing this [Brazilian] AD to prevent the possibility of a dual engine in-flight shutdown due to low-stage bleed check valve failure.

The required action is replacement of the AMS controller operation program of the AMS controller processor boards, and replacement of the low-stage bleed check valves and associated seals. You may examine the MCAI in the AD docket on the Internet at http:// www.regulations.gov by searching for and locating Docket No. FAA–2015–
6542.

Related Service Information Under 1 CFR Part 51

Embraer has issued Service Bulletin 190–36–0023, Revision 03, dated September 24, 2014, which describesprocedures for replacing the engine lowstage bleed check valves. Embraer has also issued Service Bulletin 190–21– 0041, Revision 02, dated July 30, 2013, which describe procedures for replacing the AMS controller operation program of the AMS controller processor boards. This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the **ADDRESSES** section of this NPRM.

Differences Between the MCAI and This Proposed AD

The applicability of paragraph (g) of this proposed AD is limited to airplanes identified in Embraer Service Bulletin 190–21–0041, Revision 02, dated July 30, 2013. The MCAI did not include this limitation. We have included this limitation because Model ERJ 190 airplanes with serial number (S/N) 19000587, S/N 19000589, S/N 19000593 and subsequent have a modification incorporated at the factory equivalent to the modification required by this AD.

Also, this proposed AD includes all Embraer S.A. Model ERJ 170–100 LR, –100 STD, –100 SE, and –100 SU airplanes; and Model ERJ 170–200 LR, –200 SU, and –200 STD airplanes, because of an additional proposed requirement in paragraph (j)(1) of this AD, which is related to installation of used low-stage bleed check valves having P/N 001447–6 on Model ERJ 170 airplanes. ANAC is considering future rulemaking to include a similar requirement. 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. Costs of Compliance

We estimate that this proposed AD affects 197 airplanes of U.S. registry.

We also estimate that it would take about 4 work-hours per product to comply with the basic requirements of this proposed AD. The average labor rate is $85 per work-hour. Required parts would cost about $638 per product. Based on these figures, we estimate the cost of this proposed AD on U.S. operators to be $192,666, or $978 per product. 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. 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 airworthiness directive (AD):

Embraer S.A.: Docket No. FAA–2015–6542; Directorate Identifier 2015–NM–038–AD.
(a) Comments Due Date

We must receive comments by January 14,
2016.
(b) Affected ADs

None. (c) Applicability

This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.

(1) All Embraer S.A. Model ERJ 170–100 LR, –100 STD, –100 SE, and –100 SU airplanes; and Model ERJ 170–200 LR, –200 SU, and –200 STD airplanes.

(2) All Embraer S.A. Model ERJ 190–100 STD, –100 LR, –100 IGW, –200 STD, –200 LR, and –200 IGW airplanes.
(d) Subject

Air Transport Association (ATA) of America Code 36, Pneumatic.

(e) Reason

This AD was prompted by reports of cracks in certain engine low-stage bleed check valves. We are issuing this AD to prevent failure of the low-stage bleed check valve, which could result in dual engine in-flight shutdown.


### 74722 Federal Register / Vol. 80, No. 229 / Monday, November 30, 2015 / Proposed Rules

(f) Compliance

Comply with this AD within the compliance times specified, unless already done.
(g) Modification

For Embraer S.A. Model ERJ 190 airplanes identified in Embraer Service Bulletin 190– 21–0041, Revision 02, dated July 30, 2013, within 3 months after the effective date of this AD, replace the Hamilton Sundstrand air management system (AMS) controller operation program of the AMS controller processor boards, as specified in paragraph (g)(1) or (g)(2) of this AD.

(1) Replace with a new, improved program, in accordance with the Accomplishment Instructions of Embraer Service Bulletin 190– 21–0041, Revision 02, dated July 30, 2013.

(2) Replace with a version of the Hamilton Sundstrand AMS controller operation program approved after August 31, 2012, using a method approved by the Manager, International Branch, ANM–116, Transport Airplane Directorate, FAA; Age ˆ ncia Nacional de Aviac

 ̧ a  ̃ o Civil (ANAC); or ANAC’s authorized Designee.
(h) Valve Replacement

For Embraer S.A. Model ERJ 190 airplanes identified in Embraer Service Bulletin 190– 21–0041, Revision 02, dated July 30, 2013, within 3 months after the effective date of this AD, and after accomplishment of the actions required by paragraph (g) of this AD: Replace the check valve and associated seals of the left-hand and right-hand engine bleed system with a check valve identified in paragraph (i) of this AD, and new seals, in accordance with the Accomplishment Instructions of Embraer Service Bulletin 190– 36–0023, Revision 03, dated September 24,
2014.
(i) Allowed Valves

When complying with paragraph (h) of this AD, the low-stage bleed check valves having P/N 1001447–6, and associated seals, arereplaced with new ones (zero-hour). Lowstage bleed check valves having P/N 1001447–6 that can be demonstrated with logged hours only on ERJ–170 aircraft and/ or on ERJ–190 aircraft equipped with the AMS Controller Operational Program version Black Label 13, or a later version, can be used instead of new ones (zero-hour).
(j) Parts Installation Limitation

(1) For Model ERJ 170–100 STD, –100 LR, –100SU, –100SE, –200 STD, –200 LR, and –200 SU airplanes: No person may install on any airplane a low-stage bleed check valve having P/N 1001447–6 that was installed on any Model ERJ 190–100 STD, –100 LR, –100 IGW, –200 STD, –200 LR, or –200 IGW airplane, any serial number except 190– 00587, 190–00589, and 190–00593 and subsequent, prior to accomplishment of paragraph (g) of this AD.

(2) For Model ERJ 190–100 STD, –100 LR, –100IGW, –200 STD, –200 LR, and –200 IGW airplanes: No person may install on any airplane on which the actions of paragraph (g) of this AD have been done, a low-stage bleed check valve having P/N 1001447–6 that was previously installed on any Model ERJ 190–100 STD, –100 LR, –100 IGW, –200 STD, –200 LR, or –200 IGW airplane, any serial number except 190–00587, 190–00589, 190– 00593 and subsequent, prior to accomplishment of paragraph (g) of this AD.
(k) Credit for Previous Actions

(1) This paragraph provides credit for actions required by paragraph (g) of this AD, if those actions were performed before the effective date of this AD using the service information identified in paragraph (k)(1)(i) or (k)(1)(ii) of this AD. This service information is not incorporated by reference in this AD.

(i) Embraer Service Bulletin 190–21–0041, dated September 27, 2012.

(ii) Embraer Service Bulletin 190–21–0041, Revision 01, dated December 20, 2012.

(2) This paragraph provides credit for actions required by paragraph (h) of this AD, if those actions were performed before the effective date of this AD using the service information identified in paragraph (k)(2)(i), (k)(2)(ii), or (k)(2)(iii) of this AD. This service information is not incorporated by reference in this AD.

(i) Embraer Service Bulletin 190–36–0023, dated July 22, 2013.

(ii) Embraer Service Bulletin 190–36–0023, Revision 01, dated September 3, 2013.

(iii) Embraer Service Bulletin 190–36– 0023, Revision 02, dated April 30, 2014.
(l) 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: Ana Martinez Hueto, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 425–227–1622; 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) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Branch, ANM– 116, Transport Airplane Directorate, FAA; or ANAC; or ANAC’s authorized Designee. If approved by the ANAC Designee, the approval must include the Designee’s authorized signature.
(m) Related Information

(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) Brazilian Airworthiness Directive 2015–02–02, dated March 6, 2015, for related information. This MCAI may be found in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA–
2015–6542.

(2) For service information identified in this AD, contact Embraer S.A., Technical Publications Section (PC 060), Av. Brigadeiro Faria Lima, 2170 – Putim – 12227–901 Sa  ̃ o Jose dos Campos – SP – BRASIL; telephone +55 12 3927–5852 or +55 12 3309–0732; fax +55 12 3927–7546; email distrib@ embraer.com.br; Internet http:// www.flyembraer.com. You may view this 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 November 20, 2015. Jeffrey E. Duven, Manager, Transport Airplane Directorate, Aircraft Certification Service.

[FR Doc. 2015–30224 Filed 11–27–15; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2015–1014; Directorate Identifier 2015–NE–14–AD]** 

**RIN 2120–AA64**

**Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Turbofan**  **Engines**

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

**ACTION :**  Proposed rule; withdrawal.

**SUMMARY :**  The FAA is withdrawing a notice of proposed rulemaking (NPRM). The NPRM proposed a new airworthiness directive (AD) that had applied to all Rolls-Royce Deutschland Ltd & Co KG (RRD) Tay 650–15 and Tay 651–54 turbofan engines. The proposed action would have required reducingthe cyclic life limits for certain highpressure turbine (HPT) disks. Accordingly, we withdraw the proposed rule.

**DATES :**  The proposed rule published in the Federal Register on June 8, 2015 (80 FR 32315, June 8, 2015) is withdrawn as of November 30, 2015.

**FOR FURTHER INFORMATION CONTACT :**  Philip Haberlen, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; phone: 781–238–7770; fax: 781–238– 7199; email: philip.haberlen@faa.gov

. **SUPPLEMENTARY INFORMATION :**  The FAA proposed to amend 14 CFR part 39 with