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 

### 89878

Vol. 81, No. 239

Tuesday, December 13, 2016

**DEPARTMENT OF AGRICULTURE**

**Agricultural Marketing Service**

**7 CFR Parts 1150, 1160, 1205, 1206, 1207, 1208, 1209, 1210, 1212, 1214,**  **1215, 1216, 1217, 1218, 1219, 1222, 1230, 1250, and 1260** 

**[Document Number AMS–DA–16–0101]**

**Provisions for Removing Commodity Research and Promotion Board**  **Members and Staff**

**AGENCY :**  Agricultural Marketing Service, USDA.

**ACTION :**  Extension of comment period.

**SUMMARY :**  Notice is hereby given that the comment period on proposed amendments to the provisions for removal of board and council members or staff of the research and promotion orders—or the regulations under the orders—overseen by the Agricultural Marketing Service (AMS) is extended to December 23, 2016. The proposed rule would provide uniform authority for the U.S. Department of Agriculture (USDA) to initiate action to remove board members and staff who fail to perform their duties or who engage in dishonest actions or willful misconduct. Such action is necessary to ensure the boards can continue to fulfill their intended purposes with minimal disruption.

**DATES :**  Comments must be received by December 23, 2016.

**ADDRESSES :**  Interested persons are invited to submit written comments concerning this proposed rule. Comments should be submitted on the internet at: http://www.regulations.gov. Written comments may also be sent to Laurel L. May, Senior Marketing Specialist, Order Formulation and Enforcement Division, USDA/AMS/ Dairy Program, 1400 Independence Avenue SW., Room 2967–S—Stop 0231, Washington, DC 20250–0231; facsimile: 202–690–0552. All comments should reference the document number and the date and page number of this issue and the November 23, 2016, issue of the Federal Register, and will be made available for public inspection in the above office during regular business hours, or may be viewed at: http:// www.regluations.gov. Please be advised that the identity of the individuals or entities submitting the comments will be made public on the internet at the address provided above.

**FOR FURTHER INFORMATION CONTACT :**  Laurel L. May, Senior Marketing Specialist, USDA/AMS/Dairy Program, telephone 202–690–1366, or email Laurel.May@ams.usda.gov; or Whitney Rick, Director; Promotion, Research, and Planning Division; USDA/AMS/Dairy Program; telephone 202–720–6961; or email Whitney.Rick@ams.usda.gov.

**SUPPLEMENTARY INFORMATION :**  A proposed rule was published in the Federal Register on November 23, 2016 (81 FR 84510). The proposed rule would amend the orders and/or rules and regulations for 19 of the 22 national commodity research and promotion programs overseen by AMS by providing uniform authority for USDA to initiate action as necessary to remove board and council members or their staff employees to preserve program integrity and mitigate damage from illegal or inappropriate behavior. Currently, most of AMS’s 22 research and promotion programs specify provisions for removing board and council members or their staff employees when they are unwilling or unable to perform their duties properly or when they engage in prohibited or illegal activities or other willful misconduct. However, removal authority is inconsistent across all of the programs, which impairs AMS’s ability to provide uniform oversight of the programs and their assets. The 15-day comment period provided in the proposed rule closes December 8, 2016.

USDA received letters from several of the affected programs requesting that the comment period be extended. The letters expressed concern that the original comment period was insufficient to allow commenters to adequately evaluate the impacts of the proposal and develop appropriate
comments.

Authority: This document is issued under 19 of the commodity research and promotion orders established under the following acts: Beef Promotion and Research Act of 1985 (7 U.S.C. 2901–2911); Commodity Promotion, Research, and Information Act of 1996 (7 U.S.C. 7411–7425); Cotton Research and Promotion Act of 1966 (7 U.S.C. 2101–2118); Dairy Production Stabilization Act of 1983 (7 U.S.C. 4501–4514); Egg Research and Consumer Information Act of 1974 (7 U.S.C. 2701–2718); Fluid Milk Promotion Act of 1990 (7 U.S.C. 6401–6417); Hass Avocado Promotion, Research, and Information Act of 2000 (U.S.C. 7801–7813); Mushroom Promotion, Research, and Consumer Information Act of 1990 (7 U.S.C. 6101– 6112); Popcorn Promotion, Research, and Consumer Information Act of 1996 (7 U.S.C. 7481–7491); Pork Promotion, Research, and Consumer Information Act of 1985 (7 U.S.C. 4801–4819); Potato Research and Promotion Act of 1971 (7 U.S.C. 2611–2627); and Watermelon Research and Promotion Act (7 U.S.C. 4901–4916). These acts are collectively referred to as ‘‘commodity research and promotion laws’’ or ‘‘acts.’’

Dated: December 7, 2016. Bruce Summers, Associate Administrator, Agricultural Marketing Service.

[FR Doc. 2016–29852 Filed 12–12–16; 8:45 am]

**BILLING CODE 3410–02–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2016–4220; Directorate Identifier 2015–NM–076–AD]** 

**RIN 2120–AA64**

**Airworthiness Directives; BAE Systems (Operations) Limited**  **Airplanes**

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

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

**SUMMARY :**  We are revising an earlier proposal to supersede Airworthiness Directive (AD) 2011–24–06. AD 2011– 24–06 applies to all BAE Systems (Operations) Limited Model Bae 146– 100A, –200A, and –300A airplanes; and Model Avro 146–RJ70A, 146–RJ85A, and 146–RJ100A airplanes. This action revises the NPRM by adding airplanes to the applicability. We are proposing this AD to address the unsafe condition on these products. Since these actions impose an additional burden over those proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.


### 89879 Federal Register / Vol. 81, No. 239 / Tuesday, December 13, 2016 / Proposed Rules

**DATES :**  We must receive comments on this SNPRM by January 27, 2017.

**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 SNPRM, contact BAE Systems (Operations) Limited, Customer Information Department, Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United Kingdom; telephone +44 1292 675207; fax +44 1292 675704; email RApublications@ baesystems.com ; Internet http:// www.baesystems.com/Businesses/ RegionalAircraft/index.htm. 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–2016– 4220; 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 (telephone: 800–647–5527) is in the

**ADDRESSES** section. Comments will be available in the AD docket shortly after receipt.

**FOR FURTHER INFORMATION CONTACT :**  Todd Thompson, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 425–227–1175; 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–2016–4220; Directorate Identifier 2015–NM–076–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

On November 8, 2011, we issued AD 2011–24–06, Amendment 39–16870 (76 FR 73477, November 29, 2011) (‘‘AD 2011–24–06’’). AD 2011–24–06 requires actions intended to address an unsafe condition on all BAE Systems (Operations) Limited Model BAe 146 series airplanes; and Model Avro 146– RJ series airplanes.

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD to supersede AD 2011–24–06 that would apply to all BAE Systems (Operations) Limited Model Avro 146–RJ series airplanes. The NPRM published in the Federal Register on March 8, 2016 (81 FR 12044) (‘‘the NPRM’’). The NPRM was prompted by a determination that new or revised structural inspection requirements are necessary. The NPRM proposed to require revising the maintenance or inspection program, as applicable, to incorporate new or revised structural inspection requirements.

Actions Since Previous NPRM Was Issued

Since we issued the NPRM, we have determined that the applicability should include BAE Systems (Operations) Limited Model BAe 146 series airplanes.

The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA Airworthiness Directive 2014–0071, dated March 19, 2014 (referred to after this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for all BAE Systems (Operations) Limited Model BAe 146 series and Avro 146–RJ series airplanes. The MCAI states:

The BAe 146/AVRO 146–RJ Aircraft Maintenance Manual (AMM) includes the Chapters as listed in Appendix 1 of this [EASA] AD. Compliance with these chapters has been identified as a mandatory action for continued airworthiness and EASA AD 2012–0004 was issued to require operators to comply with those instructions.

Since that [EASA] AD was issued, BAE Systems (Operations) Ltd revised the AMM (Revision 107), introducing a new defined life limit for the Fire Bottle Cartridge Firing Unit into Chapter 05–10–15. Subsequently, Revision 108 of the AMM introduced in Chapter 05–20–00 inspection tasks for repairs applied to fatigue critical structures and also introduced a new Chapter 05–20–07 to provide Structural Repair Manual (SRM) references for these tasks, applicable to repairs accomplished after the publication of AMM Revision 108. Finally, AMM Revision 111 introduced safe life limitations into Chapter 05–10–15 for rollers of main landing gear and door up-locks.

Furthermore, Section 6 of the Maintenance Review Board Report (MRBR) Document MRB 146–01, Issue 2, Revision 18 was published (as referenced in Chapter 05–20– 01 of the AMM) to correct discrepancies in inspection tasks for a number of Structurally Important Items (SIIs). Grace periods for these revised inspection tasks are included in BAE Systems (Operations) Ltd Inspection Service Bulletin (ISB) ISB.53–237.

Failure to comply with the new and more restrictive tasks and limitations referenced above could result in an unsafe condition.

For the reasons described above, this [EASA] AD retains the requirements of EASA AD 2012–0004, which is superseded, and requires implementation of the maintenance tasks and/or airworthiness limitations as specified in the defined parts of Chapter 05 of the AMM at Revision 112.

The unsafe condition is fatigue cracking of certain structural elements, which could adversely affect the structural integrity of the airplane. 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–2016–
4220.

Comments

We gave the public the opportunity to participate in developing this proposed AD. We considered the comment received. Request To Revise the Applicability

Neptune Aviation Services requested that we revise the applicability to include BAE Systems (Operations) Limited Model BAe 146–100A, –200A, and –300A airplanes. The commenter stated that these airplanes are in the applicability of AD 2011–24–06.

We agree that BAE Systems (Operations) Limited BAe 146–100A, –200A, and –300A airplanes should be in the applicability in order to address the identified unsafe condition for those airplanes. We have revised paragraph (c) of this proposed AD accordingly.


### 89880 Federal Register / Vol. 81, No. 239 / Tuesday, December 13, 2016 / Proposed Rules

FAA’s Determination and Requirements of This SNPRM

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 these same type designs.

Certain changes described above expand the scope of the NPRM. 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 SNPRM.

This proposed AD requires revisions to certain operator maintenance documents to include new actions ( e.g., inspections) and critical design configuration control limitations (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 (k)(1) of this proposed AD. The request should include a description of changes to the required actions that will ensure the continued damage tolerance of the affected structure. Costs of Compliance

We estimate that this SNPRM affects 2 airplanes of U.S. registry.

The actions required by AD 2011–24– 06 and retained in this proposed AD take about 3 work-hours per product, atan average labor rate of $85 per workhour. Based on these figures, the estimated cost of the actions that are required by AD 2011–24–06 is $255 per product.

We also estimate that it would take about 1 work-hour 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 this proposed AD on U.S. operators to be $170, or $85 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 removing Airworthiness Directive (AD) 2011–24–06, Amendment 39–16870 (76 FR 73477, November 29, 2011), and adding the following new AD:
BAE Systems (Operations) Limited: Docket No. FAA–2016–4220; Directorate Identifier 2015–NM–076–AD.

(a) Comments Due Date

We must receive comments by January 27,
2017.
(b) Affected ADs

This AD replaces AD 2011–24–06, Amendment 39–16870 (76 FR 73477, November 29, 2011) (‘‘AD 2011–24–06’’).
(c) Applicability

This AD applies to BAE Systems (Operations) Limited Model BAe 146–100A, –200A, and –300A airplanes; and Model Avro 146–RJ70A, 146–RJ85A, and 146– RJ100A airplanes; certificated in any category; all serial numbers.
(d) Subject

Air Transport Association (ATA) of America Code 05, Periodic Inspections.

(e) Reason

This AD was prompted by a determination that new or revised structural inspection requirements are necessary. We are issuing this AD to detect and correct fatigue cracking of certain structural elements, which could adversely affect the structural integrity of the airplane.
(f) Compliance

Comply with this AD within the compliance times specified, unless already done.
(g) Retained Airworthiness Limitations Revisions of the Shock Absorber Assemblies, With No Changes

This paragraph restates the requirements of paragraph (j) of AD 2011–24–06, with no changes. Within 90 days after January 3, 2012 (the effective date of AD 2011–24–06), revise the maintenance program, by incorporating Subject 05–10–15, ‘‘Aircraft Equipment Airworthiness Limitations’’ of Chapter 05, ‘‘Time Limits/Maintenance Checks,’’ of the BAE Systems (Operations) Limited BAe 146 Series/Avro 146–RJ Series Aircraft Maintenance Manual (AMM), Revision 104, dated April 15, 2011, to remove life limits on shock absorber assemblies, but not the individual shock absorber components, amend life limits on main landing gear (MLG) up-locks and door up-locks, and to introduce and amend life limits on MLG components. Accomplishing the actions required by paragraph (i) of this AD terminates the actions required by this paragraph.

(h) Retained No Alternative Actions, Intervals, and/or Critical Design Configuration Control Limitations (CDCCLs), With No Changes

This paragraph restates the requirements of paragraph (k) of AD 2011–24–06, with no changes. Except as specified in paragraph (i) of this AD: After accomplishing the revision required by paragraph (g) of this AD, no


### 89881 Federal Register / Vol. 81, No. 239 / Tuesday, December 13, 2016 / Proposed Rules

alternative actions ( e.g., inspections), intervals, and/or CDCCLs may be used, unless the actions, intervals, and/or CDCCLs are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (k)(1) of this AD.
(i) New Revise Maintenance Program or Inspection Program

Within 90 days after the effective date of this AD: Revise the maintenance or inspection program, as applicable, to incorporate new and revised limitations, tasks, thresholds, and intervals using a method approved by the Manager, International Branch, ANM–116, Transport Airplane Directorate, FAA. Accomplishing the actions required by this paragraph terminates the actions required by paragraph (g) of this AD.

Note 1 to paragraph (i) of this AD: An additional source of guidance for the actions specified in paragraph (i) of this AD can be found in BAe 146/AVRO 146–RJ Airplane Maintenance Manual, Revision 112, dated October 15, 2013.

Note 2 to paragraph (i) of this AD: An additional source of guidance for the actions specified in paragraph (i) of this AD can be found in Corrosion Prevention Control Program (CPCP) Document No. CPCP–146– 01, Revision 4, dated September 15, 2010.

Note 3 to paragraph (i) of this AD: An additional source of guidance for the actions specified in paragraph (i) of this AD can be found in Supplemental Structural Inspections Document (SSID) Document No. SSID–146–01, Revision 2, dated August 15,

2012.

Note 4 to paragraph (i) of this AD: An additional source of guidance for the actions specified in paragraph (i) of this AD can be found in Maintenance Review Board Report Document No. MRB 146–01, Issue 2, Revision 19, dated August 2012.

Note 5 to paragraph (i) of this AD: An additional source of guidance for the actions specified in paragraph (i) of this AD can be found in BAE Systems (Operations) Limited Inspection Service Bulletin ISB.53–237, Revision 1, dated April 2, 2013.

(j) New No Alternative Actions, Intervals, and/or CDCCLs

After accomplishment of the revision required by paragraph (i) of this AD, no alternative actions ( e.g., inspections), intervals, and/or CDCCLs may be used, unless the actions, intervals, and/or CDCCLs are approved as an AMOC in accordance with the procedures specified in paragraph (k)(1) of this AD.

(k) 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: Todd Thompson, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone 425–227–1175; 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.

(2) Contacting the Manufacturer: As of the effective date of this AD, 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 the European Aviation Safety Agency (EASA); or BAE Systems (Operations) Limited’s EASA Design Organization Approval (DOA). If approved by the DOA,the approval must include the DOAauthorized signature.

(l) Related Information

(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2014–0071, dated March 19, 2014, 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–

2016–4220.

(2) For service information identified in this AD, contact BAE Systems (Operations) Limited, Customer Information Department, Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United Kingdom; telephone +44 1292 675207; fax +44 1292 675704; email RApublications@ baesystems.com; Internet http:// www.baesystems.com/Businesses/ RegionalAircraft/index.htm. 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 10, 2016. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.

[FR Doc. 2016–28060 Filed 12–12–16; 8:45 am]

**BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION** 

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2015–7529; Directorate Identifier 2014–NM–207–AD]** 

**RIN 2120–AA64**

**Airworthiness Directives; Bombardier, Inc. Airplanes** 

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

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

**SUMMARY :**  We are revising an earlier proposal to supersede Airworthiness Directive (AD) 2014–16–02 for certain Bombardier, Inc. Model CL–600–1A11 (CL–600) airplanes. This action revises the notice of proposed rulemaking (NPRM) by reducing the compliance time to modify the thrust reversers, and adding new modification procedures. We are proposing this AD to address the unsafe condition on these products. Since these actions impose an additional burden over those 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 SNPRM by January 27, 2017.

**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 SNPRM, contact Bombardier, Inc., 400 Co ˆ te-Vertu Road West, Dorval, Que  ́bec H4S 1Y9, Canada; Widebody Customer Response Center North America; toll-free telephone number 1–866–538–1247 or direct-dial telephone number 1–514–855–2999; fax 514–855–7401; email ac.yul@ aero.bombardier.com; Internet http:// www.bombardier.com. You may view