Airworthiness Directives; Bombardier, Inc., Airplanes, 12659-12662 [2018-05014]

Download as PDF Federal Register / Vol. 83, No. 57 / Friday, March 23, 2018 / Rules and Regulations E-Government Act Compliance RHS is committed to complying with the E-Government Act, 44 U.S.C. 3601 et seq., to promote the use of the internet and other information technologies to provide increased opportunities for citizen access to Government information and services, and for other purposes. amozie on DSK30RV082PROD with RULES Non-Discrimination Policy In accordance with Federal civil rights law and U.S. Department of Agriculture (USDA) civil rights regulations and policies, the USDA, its Agencies, offices, and employees, and institutions participating in or administering USDA programs are prohibited from discriminating based on race, color, national origin, religion , sex, gender identity (including gender expression), sexual orientation, disability, age, marital status, family/ parental status, income derived from a public assistance program, political beliefs, or reprisal or retaliation for prior civil rights activity, in any program or activity conducted or funded by USDA (not all bases apply to all programs). 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Submit your completed form or letter to USDA by: (1) Mail: U.S. Department of Agriculture, Office of the Assistant Secretary for Civil Rights, 1400 Independence Avenue SW, Washington, DC 20250–9410; (2) Fax: (202)690–7442; or (3) Email: program.intake@usda.gov. USDA is an equal opportunity provider, employer, and lender. implemented by Regulation Z of the Federal Reserve System, and with RESPA as implemented by Regulation X of the Department of Housing and Urban Development. In 2010, Congress signed into law the Dodd-Frank Wall Street Reform and Consumer Protection Act (Dodd-Frank Act). The Dodd-Frank Act directed the Consumer Financial Protection Bureau (CFPB) to integrate the mortgage loan disclosures under TILA and RESPA Sections 4 and 5. The CFPB’s TRID rule requires easier-to-use mortgage disclosure forms that clearly lay out the terms of a mortgage for a homebuyer; the rule consolidated the four disclosures required under TILA and RESPA into two forms: A Loan Estimate and a Closing Disclosure. With the TRID rule’s effective date of October 3, 2015 (80 FR 43911), which modified 12 CFR parts 1024 and 1026, 7 CFR part 1940, subpart I, has become functionally obsolete since it refers to outdated processes, forms, and governing bodies. Through this direct final action, this functionally obsolete regulation will be eliminated to avoid confusion and possible noncompliance on the part of Agency staff; and the RHS programs’ guidance will cite the TRID rule as the standard to follow. The TRID rule contains comprehensive instructions on its subject matter. By citing the CFPB’s requirements regarding mortgage disclosures in its guidance, it is the Agency’s objective to ensure that any future changes are immediately and accurately incorporated by reference. List of Subjects in 7 CFR Part 1940 Agriculture, Environmental protection, Flood plains, Grant programs—agriculture, Grant programs—housing and community development, Loan programs— agriculture, Loan programs—housing and community development, Low and moderate-income housing, Reporting and recordkeeping requirements, Rural areas, Truth in lending. For the reasons stated in the preamble, chapter XVIII, title 7 of the Code of Federal Regulations, is amended as follows: PART 1940—GENERAL I. Background 1. The authority citation for part 1940 continues to read as follows: 7 CFR part 1940, subpart I, provides instruction for compliance with TILA as Authority: 5 U.S.C. 301; 7 U.S.C. 1989; and 42 U.S.C. 1480. VerDate Sep<11>2014 16:24 Mar 22, 2018 Jkt 244001 ■ PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 12659 Subpart I—[Remove and Reserved] 2. Remove and reserve subpart I, consisting of §§ 1940.401 through 1940.406. ■ Dated: March 1, 2018. Anne C. Hazlett, Assistant to the Secretary, Rural Development. Dated: March 8, 2018. Bill Northey, Under Secretary, Farm Production and Conservation. [FR Doc. 2018–05999 Filed 3–22–18; 8:45 am] BILLING CODE 3410–XV–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2017–0495; Product Identifier 2017–NM–017–AD; Amendment 39–19222; AD 2018–06–02] RIN 2120–AA64 Airworthiness Directives; Bombardier, Inc., Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: We are adopting a new airworthiness directive (AD) for all Bombardier, Inc., Model CL–600–2B19 (Regional Jet Series 100 & 440), Model CL–600–2C10 (Regional Jet Series 700, 701, & 702), Model CL–600–2D15 (Regional Jet Series 705), and Model CL–600–2D24 (Regional Jet Series 900) airplanes. This AD was prompted by development of a modification to prevent uncommanded rudder movement during flight. This AD requires modifying the wiring harness of the yaw damper control system. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective April 27, 2018. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of April 27, 2018. ADDRESSES: For service information identified in this final rule, contact ˆ Bombardier, Inc., 400 Cote-Vertu Road ´ West, Dorval, Quebec H4S 1Y9, Canada; Widebody Customer Response Center North America toll-free telephone 1– 866–538–1247 or direct-dial telephone 1–514–855–2999; fax 514–855–7401; email ac.yul@aero.bombardier.com; internet: https://www.bombardier.com. SUMMARY: E:\FR\FM\23MRR1.SGM 23MRR1 12660 Federal Register / Vol. 83, No. 57 / Friday, March 23, 2018 / Rules and Regulations You may view this referenced service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. It is also available on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2017– 0495. Examining the AD Docket You may examine the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2017– 0495; 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 AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (telephone 800–647– 5527) is Docket Management Facility, U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE, Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Cesar Gomez, Aerospace Engineer, Airframe and Mechanical Systems Section, New York ACO Branch, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516– 228–7318; fax 516–794–5531. SUPPLEMENTARY INFORMATION: amozie on DSK30RV082PROD with RULES Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to all Bombardier, Inc., Model CL–600–2B19 (Regional Jet Series 100 & 440), Model CL–600–2C10 (Regional Jet Series 700, 701, & 702), Model CL–600– 2D15 (Regional Jet Series 705), and Model CL–600–2D24 (Regional Jet Series 900) airplanes. The NPRM published in the Federal Register on May 31, 2017 (82 FR 24897) (‘‘the NPRM’’). The NPRM was prompted by development of a modification to prevent uncommanded rudder movement during flight. The NPRM proposed to require modifying the wiring harness of the yaw damper control system. We are issuing this AD to prevent uncommanded rudder movement and consequent loss of the ability to control the airplane. Transport Canada Civil Aviation (TCCA), which is the aviation authority for Canada, has issued Canadian Airworthiness Directive CF–2017–06, effective February 14, 2017 (referred to after this as the Mandatory Continuing VerDate Sep<11>2014 16:24 Mar 22, 2018 Jkt 244001 Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for all Bombardier, Inc., Model CL–600– 2B19 (Regional Jet Series 100 & 440), Model CL–600–2C10 (Regional Jet Series 700, 701, & 702), Model CL–600– 2D15 (Regional Jet Series 705), and Model CL–600–2D24 (Regional Jet Series 900) airplanes. The MCAI states: [Canadian] AD CF–2013–13 was issued on 28 May 2013 [related to FAA AD 2013–14– 11, Amendment 39–17516 (78 FR 44871, July 25, 2013) (‘‘AD 2013–14–11’’)] to mandate the introduction of an emergency procedure to the Aeroplane Flight Manual to address the uncommanded rudder movement. Since the original issue of [Canadian] AD CF–2013–13, Bombardier Aerospace has developed a wiring modification for the yaw damper control system to prevent uncommanded movement of the rudder [and consequent loss of the ability to control the airplane]. This [Canadian] AD mandates the wiring modification for the yaw damper control system * * *. You may examine the MCAI in the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–20**– ****. Comments We gave the public the opportunity to participate in developing this AD. The following presents the comments received on the NPRM and the FAA’s response to each comment. Support for the NPRM The Air Line Pilots Association, International (ALPA), agreed with the intent of the NPRM. Request To Clarify Credit for Certain Service Information SkyWest Airlines and Ahmad Lababidi asked that we revise paragraph (h) of the proposed AD to clarify the credit language for accomplishing the engineering orders in conjunction with the referenced service information. Ahmad Lababidi stated that Service Non-Incorporated Engineering Order (SNIEO) K601R50211 S02, dated October 31, 2014, was issued for certain airplane configurations where the wire connector was changed from pin type to socket type. The commenters added that SNIEOs K601R50211 S03, dated April 21, 2015, and S04, dated April 24, 2015, were issued to clarify certain splicing, capping, and stowing locations, and to reduce the work hours for accomplishing the actions specified in the service bulletin. The commenters added that it is not necessary to do the engineering orders in conjunction with the referenced service information. SkyWest reported accomplishing the PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 modification on some airplanes using only the applicable service bulletin without any reference to the SNIEOs specified in paragraph (h) of the proposed AD. We agree with the commenters’ requests for the reasons provided. We have revised paragraphs (h)(1)(i) and (h)(1)(ii) of this AD to remove reference to the SNIEOs, which are not required to be used in conjunction with the referenced service information. Request To Revise Parts Installation Limitations Paragraph Air Wisconsin asked that we revise paragraph (i) of the proposed AD (Parts Installation Limitations) to exclude parts on which the actions in the referenced service information have been done. We acknowledge the commenter’s request. However, paragraph (i) of this AD already prohibits installation of a yaw damper actuator . . . ‘‘unless it has been modified in accordance with the applicable service information specified in table 1 to paragraph (g) of this AD.’’ Since existing language meets the intent of the commenter’s request, we have not changed this AD in this regard. Conclusion We reviewed the relevant data, considered the comments received, and determined that air safety and the public interest require adopting this AD with the changes described previously, and minor editorial changes. We have determined that these minor changes: • Are consistent with the intent that was proposed in the NPRM for correcting the unsafe condition; and • Do not add any additional burden upon the public than was already proposed in the NPRM. We also determined that these changes will not increase the economic burden on any operator or increase the scope of this AD. Related Service Information Under 1 CFR Part 51 Bombardier has issued Service Bulletin 601R–22–017, Revision C, dated May 11, 2016; and Service Bulletin 670BA–22–007, Revision A, dated February 16, 2016. This service information describes procedures for modifying the wiring harness of the yaw damper control system. These documents are distinct since they apply to different airplane models. 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. E:\FR\FM\23MRR1.SGM 23MRR1 Federal Register / Vol. 83, No. 57 / Friday, March 23, 2018 / Rules and Regulations Costs of Compliance We estimate that this AD affects 1,006 airplanes of U.S. registry. 12661 We estimate the following costs to comply with this AD: ESTIMATED COSTS Action Labor cost Parts cost Cost per product Wiring modification ............ 5 work-hours × $85 per hour = $425 ........................... Up to $39 .... Up to $464 .. According to the manufacturer, some of the costs of this AD may be covered under warranty, thereby reducing the cost impact on affected individuals. We do not control warranty coverage for affected individuals. As a result, we have included all costs in our cost estimate. Authority for This Rulemaking amozie on DSK30RV082PROD with RULES 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. This AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to transport category VerDate Sep<11>2014 16:24 Mar 22, 2018 Jkt 244001 airplanes to the Director of the System Oversight Division. Regulatory Findings We determined that this AD will not have federalism implications under Executive Order 13132. This AD will 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 this AD: 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. § 39.13 Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: ■ [Amended] 2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD): ■ 2018–06–02 Bombardier, Inc.: Amendment 39–19222; Docket No. FAA–2017–0495; Product Identifier 2017–NM–017–AD. (a) Effective Date This AD is effective April 27, 2018. (b) Affected ADs None. (c) Applicability This AD applies to all Bombardier, Inc., Model CL–600–2B19 (Regional Jet Series 100 & 440), Model CL–600–2C10 (Regional Jet Series 700, 701, & 702), Model CL–600–2D15 (Regional Jet Series 705), and Model CL–600– 2D24 (Regional Jet Series 900) airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 22, Auto Flight. (e) Reason This AD was prompted by development of a modification to prevent uncommanded rudder movement during flight. We are issuing this AD to prevent uncommanded rudder movement and consequent loss of the ability to control the airplane. Comply with this AD within the compliance times specified, unless already done. (g) Modification Within 6,600 flight hours or 36 months after the effective date of this AD, whichever occurs first: Modify the wiring harness of the yaw damper control system, in accordance with the applicable service information specified in table 1 to paragraph (g) of this AD. Authority: 49 U.S.C. 106(g), 40113, 44701. Frm 00005 Fmt 4700 Sfmt 4700 Up to $466,784. (f) Compliance Adoption of the Amendment PO 00000 Cost on U.S. operators E:\FR\FM\23MRR1.SGM 23MRR1 Federal Register / Vol. 83, No. 57 / Friday, March 23, 2018 / Rules and Regulations (h) Credit for Previous Actions (1) This paragraph provides credit for actions required by paragraph (g) of this AD for Model CL–600–2B19 (Regional Jet Series 100 & 440) airplanes, if those actions were performed before the effective date of this AD using the service information specified in paragraph (h)(1)(i), (h)(1)(ii), or (h)(1)(iii) of this AD. (i) Bombardier Service Bulletin 601R–22– 017, dated September 24, 2014. (ii) Bombardier Service Bulletin 601R–22– 017, Revision A, dated February 26, 2015. (iii) Bombardier Service Bulletin 601R–22– 017, Revision B, dated July 16, 2015. (2) This paragraph provides credit for actions required by paragraph (g) of this AD for Model CL–600–2C10 (Regional Jet Series 700, 701, & 702), Model CL–600–2D15 (Regional Jet Series 705), and Model CL–600– 2D24 (Regional Jet Series 900) airplanes, if those actions were performed before the effective date of this AD using Bombardier Service Bulletin 670BA–22–007, dated October 15, 2014. amozie on DSK30RV082PROD with RULES (i) Parts Installation Limitations As of 24 months after the effective date of this AD, no person may install, on any airplane, a yaw damper actuator having part number 622–9968–001, unless it has been modified in accordance with the applicable service information specified in table 1 to paragraph (g) of this AD. (j) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, New York ACO Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the New York ACO, send it to ATTN: Program Manager, Continuing Operational Safety, New York ACO Branch, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516–228– 7300; fax 516–794–5531. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight VerDate Sep<11>2014 16:24 Mar 22, 2018 Jkt 244001 standards district office/certificate holding district office. (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, New York ACO Branch, FAA; or Transport Canada Civil Aviation (TCCA); or Bombardier, Inc.’s TCCA Design Approval Organization (DAO). If approved by the DAO, the approval must include the DAO-authorized signature. (k) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) Canadian Airworthiness Directive CF–2017–06, effective February 14, 2017, for related information. This MCAI may be found in the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2017–0495. (2) For more information about this AD, contact Cesar Gomez, Aerospace Engineer, Airframe and Mechanical Systems Section, New York ACO Branch, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516–228–7318; fax 516–794–5531. (3) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (l)(3) and (l)(4) of this AD. (l) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. (i) Bombardier Service Bulletin 601R–22– 017, Revision C, dated May 11, 2016. (ii) Bombardier Service Bulletin 670BA– 22–007, Revision A, dated February 16, 2016. (3) For service information identified in ˆ this AD, contact Bombardier, Inc., 400 Cote´ Vertu Road West, Dorval, Quebec H4S 1Y9, Canada; Widebody Customer Response Center North America toll-free telephone 1– 866–538–1247 or direct-dial telephone 1– 514–855–2999; fax 514–855–7401; email ac.yul@aero.bombardier.com; internet: https://www.bombardier.com. (4) You may view this service information at the FAA, Transport Standards Branch, PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: https:// www.archives.gov/federal-register/cfr/ibrlocations.html. Issued in Renton, Washington, on March 2, 2018. Michael Kaszycki, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018–05014 Filed 3–22–18; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF HOMELAND SECURITY Coast Guard 33 CFR Part 165 [Docket No. USCG–2018–0063] RIN 1625–AA00 Safety Zone: Juan Benitez Fireworks Display, San Francisco, CA Coast Guard, DHS. Temporary final rule. AGENCY: ACTION: The Coast Guard is establishing a temporary moving safety zone in the navigable waters of the San Francisco Bay near Point Cavallo in support of the Juan Benitez Fireworks Display on March 24, 2018. This safety zone is established to ensure the safety of participants and spectators from the dangers associated with pyrotechnics. Unauthorized persons or vessels are prohibited from entering into, transiting through, or remaining in the safety zone without permission of the Captain of the Port or their designated representative. DATES: This rule is effective from 9:00 a.m. to 8:40 p.m. on March 24, 2018. SUMMARY: E:\FR\FM\23MRR1.SGM 23MRR1 ER23MR18.021</GPH> 12662

Agencies

[Federal Register Volume 83, Number 57 (Friday, March 23, 2018)]
[Rules and Regulations]
[Pages 12659-12662]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-05014]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-0495; Product Identifier 2017-NM-017-AD; Amendment 
39-19222; AD 2018-06-02]
RIN 2120-AA64


Airworthiness Directives; Bombardier, Inc., Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for all 
Bombardier, Inc., Model CL-600-2B19 (Regional Jet Series 100 & 440), 
Model CL-600-2C10 (Regional Jet Series 700, 701, & 702), Model CL-600-
2D15 (Regional Jet Series 705), and Model CL-600-2D24 (Regional Jet 
Series 900) airplanes. This AD was prompted by development of a 
modification to prevent uncommanded rudder movement during flight. This 
AD requires modifying the wiring harness of the yaw damper control 
system. We are issuing this AD to address the unsafe condition on these 
products.

DATES: This AD is effective April 27, 2018.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of April 27, 
2018.

ADDRESSES: For service information identified in this final rule, 
contact Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval, 
Qu[eacute]bec H4S 1Y9, Canada; Widebody Customer Response Center North 
America toll-free telephone 1-866-538-1247 or direct-dial telephone 1-
514-855-2999; fax 514-855-7401; email [email protected]; 
internet: https://www.bombardier.com.

[[Page 12660]]

You may view this referenced service information at the FAA, Transport 
Standards Branch, 2200 South 216th St., Des Moines, WA. For information 
on the availability of this material at the FAA, call 206-231-3195. It 
is also available on the internet at https://www.regulations.gov by 
searching for and locating Docket No. FAA-2017-0495.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2017-
0495; 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 AD, the regulatory evaluation, any comments received, and 
other information. The street address for the Docket Office (telephone 
800-647-5527) is Docket Management Facility, U.S. Department of 
Transportation, Docket Operations, M-30, West Building Ground Floor, 
Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Cesar Gomez, Aerospace Engineer, 
Airframe and Mechanical Systems Section, New York ACO Branch, FAA, 1600 
Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7318; 
fax 516-794-5531.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 by adding an AD that would apply to all Bombardier, Inc., Model 
CL-600-2B19 (Regional Jet Series 100 & 440), Model CL-600-2C10 
(Regional Jet Series 700, 701, & 702), Model CL-600-2D15 (Regional Jet 
Series 705), and Model CL-600-2D24 (Regional Jet Series 900) airplanes. 
The NPRM published in the Federal Register on May 31, 2017 (82 FR 
24897) (``the NPRM''). The NPRM was prompted by development of a 
modification to prevent uncommanded rudder movement during flight. The 
NPRM proposed to require modifying the wiring harness of the yaw damper 
control system. We are issuing this AD to prevent uncommanded rudder 
movement and consequent loss of the ability to control the airplane.
    Transport Canada Civil Aviation (TCCA), which is the aviation 
authority for Canada, has issued Canadian Airworthiness Directive CF-
2017-06, effective February 14, 2017 (referred to after this as the 
Mandatory Continuing Airworthiness Information, or ``the MCAI''), to 
correct an unsafe condition for all Bombardier, Inc., Model CL-600-2B19 
(Regional Jet Series 100 & 440), Model CL-600-2C10 (Regional Jet Series 
700, 701, & 702), Model CL-600-2D15 (Regional Jet Series 705), and 
Model CL-600-2D24 (Regional Jet Series 900) airplanes. The MCAI states:

    [Canadian] AD CF-2013-13 was issued on 28 May 2013 [related to 
FAA AD 2013-14-11, Amendment 39-17516 (78 FR 44871, July 25, 2013) 
(``AD 2013-14-11'')] to mandate the introduction of an emergency 
procedure to the Aeroplane Flight Manual to address the uncommanded 
rudder movement.
    Since the original issue of [Canadian] AD CF-2013-13, Bombardier 
Aerospace has developed a wiring modification for the yaw damper 
control system to prevent uncommanded movement of the rudder [and 
consequent loss of the ability to control the airplane].
    This [Canadian] AD mandates the wiring modification for the yaw 
damper control system * * *.

    You may examine the MCAI in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-20**-
****.

Comments

    We gave the public the opportunity to participate in developing 
this AD. The following presents the comments received on the NPRM and 
the FAA's response to each comment.

Support for the NPRM

    The Air Line Pilots Association, International (ALPA), agreed with 
the intent of the NPRM.

Request To Clarify Credit for Certain Service Information

    SkyWest Airlines and Ahmad Lababidi asked that we revise paragraph 
(h) of the proposed AD to clarify the credit language for accomplishing 
the engineering orders in conjunction with the referenced service 
information. Ahmad Lababidi stated that Service Non-Incorporated 
Engineering Order (SNIEO) K601R50211 S02, dated October 31, 2014, was 
issued for certain airplane configurations where the wire connector was 
changed from pin type to socket type. The commenters added that SNIEOs 
K601R50211 S03, dated April 21, 2015, and S04, dated April 24, 2015, 
were issued to clarify certain splicing, capping, and stowing 
locations, and to reduce the work hours for accomplishing the actions 
specified in the service bulletin. The commenters added that it is not 
necessary to do the engineering orders in conjunction with the 
referenced service information. SkyWest reported accomplishing the 
modification on some airplanes using only the applicable service 
bulletin without any reference to the SNIEOs specified in paragraph (h) 
of the proposed AD.
    We agree with the commenters' requests for the reasons provided. We 
have revised paragraphs (h)(1)(i) and (h)(1)(ii) of this AD to remove 
reference to the SNIEOs, which are not required to be used in 
conjunction with the referenced service information.

Request To Revise Parts Installation Limitations Paragraph

    Air Wisconsin asked that we revise paragraph (i) of the proposed AD 
(Parts Installation Limitations) to exclude parts on which the actions 
in the referenced service information have been done.
    We acknowledge the commenter's request. However, paragraph (i) of 
this AD already prohibits installation of a yaw damper actuator . . . 
``unless it has been modified in accordance with the applicable service 
information specified in table 1 to paragraph (g) of this AD.'' Since 
existing language meets the intent of the commenter's request, we have 
not changed this AD in this regard.

Conclusion

    We reviewed the relevant data, considered the comments received, 
and determined that air safety and the public interest require adopting 
this AD with the changes described previously, and minor editorial 
changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the 
NPRM for correcting the unsafe condition; and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM.
    We also determined that these changes will not increase the 
economic burden on any operator or increase the scope of this AD.

Related Service Information Under 1 CFR Part 51

    Bombardier has issued Service Bulletin 601R-22-017, Revision C, 
dated May 11, 2016; and Service Bulletin 670BA-22-007, Revision A, 
dated February 16, 2016. This service information describes procedures 
for modifying the wiring harness of the yaw damper control system. 
These documents are distinct since they apply to different airplane 
models. 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.

[[Page 12661]]

Costs of Compliance

    We estimate that this AD affects 1,006 airplanes of U.S. registry.
    We estimate the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                                  Cost on U.S.
             Action                    Labor cost            Parts cost      Cost per product      operators
----------------------------------------------------------------------------------------------------------------
Wiring modification............  5 work-hours x $85 per  Up to $39........  Up to $464.......  Up to $466,784.
                                  hour = $425.
----------------------------------------------------------------------------------------------------------------

    According to the manufacturer, some of the costs of this AD may be 
covered under warranty, thereby reducing the cost impact on affected 
individuals. We do not control warranty coverage for affected 
individuals. As a result, we have included all costs in our cost 
estimate.

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.
    This AD is issued in accordance with authority delegated by the 
Executive Director, Aircraft Certification Service, as authorized by 
FAA Order 8000.51C. In accordance with that order, issuance of ADs is 
normally a function of the Compliance and Airworthiness Division, but 
during this transition period, the Executive Director has delegated the 
authority to issue ADs applicable to transport category airplanes to 
the Director of the System Oversight Division.

Regulatory Findings

    We determined that this AD will not have federalism implications 
under Executive Order 13132. This AD will 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 this AD:
    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.

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive (AD):

2018-06-02 Bombardier, Inc.: Amendment 39-19222; Docket No. FAA-
2017-0495; Product Identifier 2017-NM-017-AD.

(a) Effective Date

    This AD is effective April 27, 2018.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all Bombardier, Inc., Model CL-600-2B19 
(Regional Jet Series 100 & 440), Model CL-600-2C10 (Regional Jet 
Series 700, 701, & 702), Model CL-600-2D15 (Regional Jet Series 
705), and Model CL-600-2D24 (Regional Jet Series 900) airplanes, 
certificated in any category.

(d) Subject

    Air Transport Association (ATA) of America Code 22, Auto Flight.

(e) Reason

    This AD was prompted by development of a modification to prevent 
uncommanded rudder movement during flight. We are issuing this AD to 
prevent uncommanded rudder movement and consequent loss of the 
ability to control the airplane.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Modification

    Within 6,600 flight hours or 36 months after the effective date 
of this AD, whichever occurs first: Modify the wiring harness of the 
yaw damper control system, in accordance with the applicable service 
information specified in table 1 to paragraph (g) of this AD.

[[Page 12662]]

[GRAPHIC] [TIFF OMITTED] TR23MR18.021

(h) Credit for Previous Actions

    (1) This paragraph provides credit for actions required by 
paragraph (g) of this AD for Model CL-600-2B19 (Regional Jet Series 
100 & 440) airplanes, if those actions were performed before the 
effective date of this AD using the service information specified in 
paragraph (h)(1)(i), (h)(1)(ii), or (h)(1)(iii) of this AD.
    (i) Bombardier Service Bulletin 601R-22-017, dated September 24, 
2014.
    (ii) Bombardier Service Bulletin 601R-22-017, Revision A, dated 
February 26, 2015.
    (iii) Bombardier Service Bulletin 601R-22-017, Revision B, dated 
July 16, 2015.
    (2) This paragraph provides credit for actions required by 
paragraph (g) of this AD for Model CL-600-2C10 (Regional Jet Series 
700, 701, & 702), Model CL-600-2D15 (Regional Jet Series 705), and 
Model CL-600-2D24 (Regional Jet Series 900) airplanes, if those 
actions were performed before the effective date of this AD using 
Bombardier Service Bulletin 670BA-22-007, dated October 15, 2014.

(i) Parts Installation Limitations

    As of 24 months after the effective date of this AD, no person 
may install, on any airplane, a yaw damper actuator having part 
number 622-9968-001, unless it has been modified in accordance with 
the applicable service information specified in table 1 to paragraph 
(g) of this AD.

(j) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, New 
York ACO Branch, FAA, has the authority to approve AMOCs for this 
AD, if requested using the procedures found in 14 CFR 39.19. In 
accordance with 14 CFR 39.19, send your request to your principal 
inspector or local Flight Standards District Office, as appropriate. 
If sending information directly to the manager of the New York ACO, 
send it to ATTN: Program Manager, Continuing Operational Safety, New 
York ACO Branch, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 
11590; telephone 516-228-7300; fax 516-794-5531. 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: 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, New York ACO 
Branch, FAA; or Transport Canada Civil Aviation (TCCA); or 
Bombardier, Inc.'s TCCA Design Approval Organization (DAO). If 
approved by the DAO, the approval must include the DAO-authorized 
signature.

(k) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) Canadian Airworthiness Directive CF-2017-06, effective 
February 14, 2017, for related information. This MCAI may be found 
in the AD docket on the internet at https://www.regulations.gov by 
searching for and locating Docket No. FAA-2017-0495.
    (2) For more information about this AD, contact Cesar Gomez, 
Aerospace Engineer, Airframe and Mechanical Systems Section, New 
York ACO Branch, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 
11590; telephone 516-228-7318; fax 516-794-5531.
    (3) Service information identified in this AD that is not 
incorporated by reference is available at the addresses specified in 
paragraphs (l)(3) and (l)(4) of this AD.

(l) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless this AD specifies otherwise.
    (i) Bombardier Service Bulletin 601R-22-017, Revision C, dated 
May 11, 2016.
    (ii) Bombardier Service Bulletin 670BA-22-007, Revision A, dated 
February 16, 2016.
    (3) For service information identified in this AD, contact 
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval, 
Qu[eacute]bec H4S 1Y9, Canada; Widebody Customer Response Center 
North America toll-free telephone 1-866-538-1247 or direct-dial 
telephone 1-514-855-2999; fax 514-855-7401; email 
[email protected]; internet: https://www.bombardier.com.
    (4) You may view this service information at the FAA, Transport 
Standards Branch, 2200 South 216th St., Des Moines, WA. For 
information on the availability of this material at the FAA, call 
206-231-3195.
    (5) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, call 202-741-6030, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on March 2, 2018.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2018-05014 Filed 3-22-18; 8:45 am]
BILLING CODE 4910-13-P
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