Airworthiness Directives; Bombardier, Inc. Airplanes, 8145-8147 [2020-02837]

Download as PDF Federal Register / Vol. 85, No. 30 / Thursday, February 13, 2020 / Rules and Regulations agreement or contract, inspect any actions undertaken under the agreement or contract, and collect information necessary to evaluate agreement or contract performance, as specified in the agreement or contract. The NRCS representative will attempt to contact the applicant or participant prior to exercising this provision. § 1464.43 Equitable relief. (a) If a participant relied upon the advice or action of NRCS and did not know, or have reason to know, that the action or advice was improper or erroneous, the participant may be eligible for equitable relief under 7 CFR part 635; however, the financial or technical liability for any action by a participant that was taken based on the advice of a TSP will remain with the TSP and will not be assumed by NRCS. (b) If a participant has been found in violation of a program requirement through failure to comply fully with that requirement, the participant may be eligible for equitable relief under 7 CFR part 635. § 1464.44 Offsets and assignments. (a) Except as provided in paragraph (b) of this section, any payment or portion thereof to any person, legal entity, joint operation, or Indian Tribe will be made without regard to questions of title to the payment under State law and without regard to any claim or lien against the crop, or proceeds thereof, in favor of the owner or any other creditor except agencies of the U.S. Government. The regulations governing offsets and withholdings found at part 1403 of this chapter will apply to contract payments. (b) Any person, legal entity, Indian Tribe, eligible entity, or other party entitled to any cash payment under this program may assign the right to receive such cash payments, in whole or in part. jbell on DSKJLSW7X2PROD with RULES § 1464.45 Misrepresentation and scheme or device. (a) A person, legal entity, joint operation, or Indian Tribe that is determined to have erroneously represented any fact affecting a program determination made in accordance with this part will not be entitled to payments under RCPP and must refund to NRCS all RCPP payments, plus interest, determined in accordance with part 1403 of this chapter. (b) A participant will lose all interest in all contracts or agreements with NRCS and will refund to NRCS all payments, plus interest determined in accordance with part 1403 of this chapter, received by such participant with respect to all contracts and VerDate Sep<11>2014 17:58 Feb 12, 2020 Jkt 250001 agreements if it is determined that the participant has knowingly: (1) Adopted any scheme or device that tends to defeat the purpose of the program; (2) Made any fraudulent representation to NRCS; (3) Adopted any scheme or device for the purpose of depriving any tenant or sharecropper of the payments to which such person would otherwise be entitled under the program; or (4) Misrepresented any fact affecting a program determination. (c) If NRCS determines that a participant has violated the terms of a program contract, a lead partner has violated the terms of a partnership agreement, or a lead partner or nonlead partner has violated the terms of a supplemental agreement, NRCS may determine that the severity of the violation renders the participant, lead partner, or nonlead partner, respectively, ineligible for future NRCS conservation program consideration in accordance with applicable suspension and debarment regulations. § 1464.46 Environmental credits for conservation improvements. NRCS recognizes that environmental benefits will be achieved by implementing eligible activities funded through RCPP, and a participant may obtain environmental credits as a result of implementing additional eligible activities through an environmental service market if one of the purposes of the market is the facilitation of additional conservation benefits that are consistent with the purposes of a program contract or supplemental agreement. NRCS asserts no direct or indirect interest on these credits. However, NRCS retains the authority to ensure that operation and maintenance (O&M) requirements for RCPP-funded eligible activities are met. Where the non-RCPP funded additional eligible activities may impact the land under a program contract or supplemental agreement, producers and participants are highly encouraged to request an O&M compatibility determination from NRCS prior to entering into any environmental credit agreements. Matthew Lohr, Chief, Natural Resources Conservation Service. Robert Stephenson, Executive Vice President, Commodity Credit Corporation. [FR Doc. 2020–01812 Filed 2–12–20; 8:45 am] BILLING CODE 3410–16–P PO 00000 Frm 00015 Fmt 4700 Sfmt 4700 8145 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2019–0714; Product Identifier 2019–NM–103–AD; Amendment 39–21021; AD 2019–26–10] RIN 2120–AA64 Airworthiness Directives; Bombardier, Inc. Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). AGENCY: ACTION: Final rule. The FAA is adopting a new airworthiness directive (AD) for all Bombardier, Inc., Model CL–600–2C10 (Regional Jet Series 700, 701 & 702) airplanes; Model CL–600–2D15 (Regional Jet Series 705) airplanes; Model CL–600–2D24 (Regional Jet Series 900) airplanes; and Model CL– 600–2E25 (Regional Jet Series 1000) airplanes. This AD was prompted by a report of incorrectly installed flight compartment door edge protection plates on both sides of the upper decompression panel. This AD requires revising the existing maintenance or inspection program, as applicable, to incorporate a functional check of the flight compartment door decompression latches. The FAA is issuing this AD to address the unsafe condition on these products. SUMMARY: This AD is effective March 19, 2020. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of March 19, 2020. DATES: For service information identified in this final rule, contact Bombardier, Inc., 400 Coˆte Vertu Road West, Dorval, Que´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 ac.yul@aero.bombardier.com; internet https://www.bombardier.com. 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. It is also available on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2019– 0714. ADDRESSES: E:\FR\FM\13FER1.SGM 13FER1 jbell on DSKJLSW7X2PROD with RULES 8146 Federal Register / Vol. 85, No. 30 / Thursday, February 13, 2020 / Rules and Regulations 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–2019– 0714; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this final rule, the regulatory evaluation, any comments received, and other information. The address for Docket Operations is 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: Aziz Ahmed, Aerospace Engineer, Airframe and Propulsion Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516–228–7329; fax 516–794– 5531; email 9-avs-nyaco-cos@faa.gov. SUPPLEMENTARY INFORMATION: issuing this AD to address incorrect installation of the flight compartment door edge protection plates on both sides of the flight compartment door upper decompression panel. This condition, if not corrected, could result in the inability of the flight compartment door upper decompression panel to open during a rapid decompression event. This inability to relieve the pressure in the flight compartment may compromise the structural integrity of the bulkhead between the flight compartment and the passenger cabin. See the MCAI for additional background information. Discussion Transport Canada Civil Aviation (TCCA), which is the aviation authority for Canada, has issued Canadian AD CF–2019–20R1, dated May 31, 2019 (referred to after this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for all Bombardier, Inc., Model CL–600–2C10 (Regional Jet Series 700, 701 & 702) airplanes; Model CL–600–2D15 (Regional Jet Series 705) airplanes; Model CL–600–2D24 (Regional Jet Series 900) airplanes; and Model CL–600–2E25 (Regional Jet Series 1000) airplanes. 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–2019–0714. The FAA 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–600–2C10 (Regional Jet Series 700, 701 & 702) airplanes; Model CL–600– 2D15 (Regional Jet Series 705) airplanes; Model CL–600–2D24 (Regional Jet Series 900) airplanes; and Model CL– 600–2E25 (Regional Jet Series 1000) airplanes. The NPRM published in the Federal Register on October 9, 2019 (84 FR 54051). The NPRM was prompted by a report of incorrectly installed flight compartment door edge protection plates on both sides of the upper decompression panel. The NPRM proposed to require revising the existing maintenance or inspection program, as applicable, to incorporate a functional check of the flight compartment door decompression latches. The FAA is The FAA reviewed the relevant data, considered the comment received, and determined that air safety and the public interest require adopting this final rule as proposed, except for minor editorial changes. The FAA has determined that these minor changes: • Are consistent with the intent that was proposed in the NPRM for addressing the unsafe condition; and • Do not add any additional burden upon the public than was already proposed in the NPRM. VerDate Sep<11>2014 17:58 Feb 12, 2020 Jkt 250001 Comments The FAA gave the public the opportunity to participate in developing this final rule. The FAA has considered the comment received. Victor Oscilowicz indicated his support for the NPRM. Conclusion Related Service Information Under 1 CFR Part 51 Bombardier, Inc., has issued Task 251700–202, ‘‘Functional Check of the Flight Compartment Door Decompression Latches,’’ of Section 1, ‘‘Systems and Power Plant Program,’’ Subject 1–25, ‘‘Equipment and Furnishings,’’ of the Bombardier Model CL–600–2C10, CL–600–2D15, CL–600– 2D24, and CL–600–2E25 Series 700/ 705/900/1000 Maintenance Review Board Report, Maintenance Requirements Manual—Part 1, Volume 1, CSP B–053, Revision 18, dated July 25, 2018. This service information describes a functional check of the flight compartment door decompression latches. 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. Costs of Compliance The FAA estimates that this AD affects 522 airplanes of U.S. registry. PO 00000 Frm 00016 Fmt 4700 Sfmt 4700 The FAA estimates the following costs to comply with this AD: The FAA has determined that revising the existing maintenance or inspection program takes an average of 90 workhours per operator, although the FAA recognizes that this number may vary from operator to operator. In the past, the FAA has estimated that this action takes 1 work-hour per airplane. Since operators incorporate maintenance or inspection program changes for their affected fleet(s), the FAA has determined that a per-operator estimate is more accurate than a perairplane estimate. Therefore, the FAA estimates the total cost per operator to be $7,650 (90 work-hours × $85 per work-hour). 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. The FAA is 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 and associated appliances to the Director of the System Oversight Division. Regulatory Findings 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. E:\FR\FM\13FER1.SGM 13FER1 Federal Register / Vol. 85, No. 30 / Thursday, February 13, 2020 / Rules and Regulations For the reasons discussed above, I certify that this AD: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866, (2) Will not affect intrastate aviation in Alaska, and (3) 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. flight compartment door upper decompression panel to open during a rapid decompression event. This inability to relieve the pressure in the flight compartment may compromise the structural integrity of the bulkhead between the flight compartment and the passenger cabin. 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. (f) Compliance Comply with this AD within the compliance times specified, unless already done. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. (g) Maintenance or Inspection Program Revision Within 30 days after the effective date of this AD, revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in Task 251700–202, ‘‘Functional Check of the Flight Compartment Door Decompression Latches,’’ of Section 1, ‘‘Systems and Power Plant Program,’’ Subject 1–25, ‘‘Equipment and Furnishings,’’ of the Bombardier Model CL– 600–2C10, CL–600–2D15, CL–600–2D24, and CL–600–2E25 Series 700/705/900/1000 Maintenance Review Board Report, Maintenance Requirements Manual—Part 1, Volume 1, CSP B–053, Revision 18, dated July 25, 2018. The initial compliance time for doing the task is within 8,000 flight hours after this task is incorporated into the existing maintenance or inspection program, or within 30 days after the effective date of this AD, whichever occurs later. Repeat the task thereafter at intervals not to exceed 8,000 flight hours. (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) Canadian AD CF–2019–20R1, dated May 31, 2019, 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–2019–0714. (2) For more information about this AD, contact Aziz Ahmed, Aerospace Engineer, Airframe and Propulsion Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516–228–7329; fax 516–794–5531; email 9avs-nyaco-cos@faa.gov. 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 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): ■ 2019–26–10 Bombardier, Inc.: Amendment 39–21021; Docket No. FAA–2019–0714; Product Identifier 2019–NM–103–AD. (a) Effective Date This AD is effective March 19, 2020. (b) Affected ADs None. (c) Applicability This AD applies to the airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, all serial numbers. (1) Bombardier, Inc., Model CL–600–2C10 (Regional Jet Series 700, 701 & 702) airplanes. (2) Bombardier, Inc., Model CL–600–2D15 (Regional Jet Series 705) airplanes. (3) Bombardier, Inc., Model CL–600–2D24 (Regional Jet Series 900) airplanes. (4) Bombardier, Inc., Model CL–600–2E25 (Regional Jet Series 1000) airplanes. (d) Subject Air Transport Association (ATA) of America Code 25, Equipment/furnishings. jbell on DSKJLSW7X2PROD with RULES 8147 (e) Reason This AD was prompted by a report of incorrectly installed flight compartment door edge protection plates on both sides of the upper decompression panel. The FAA is issuing this AD to address incorrect installation of the flight compartment door edge protection plates on both sides of the flight compartment door upper decompression panel. This condition, if not corrected, could result in the inability of the VerDate Sep<11>2014 17:58 Feb 12, 2020 Jkt 250001 (h) No Alternative Actions or Intervals After the existing maintenance or inspection program has been revised as required by paragraph (g) of this AD, no alternative actions (e.g., inspections) or intervals may be used unless the actions and intervals are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (i)(1) of this AD. (i) 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 certification office, send it to ATTN: Program Manager, Continuing Operational Safety, FAA, New York ACO Branch, 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, PO 00000 Frm 00017 Fmt 4700 Sfmt 9990 (j) Related Information (k) 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) Task 251700–202, ‘‘Functional Check of the Flight Compartment Door Decompression Latches,’’ of Section 1, ‘‘Systems and Power Plant Program,’’ Subject 1–25, ‘‘Equipment and Furnishings,’’ of the Bombardier Model CL–600–2C10, CL–600–2D15, CL–600–2D24, and CL–600–2E25 Series 700/705/900/1000 Maintenance Review Board Report, Maintenance Requirements Manual—Part 1, Volume 1, CSP B–053, Revision 18, dated July 25, 2018. (ii) [Reserved] (3) For service information identified in this AD, contact Bombardier, Inc., 400 Coˆte Vertu Road West, Dorval, Que´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 ac.yul@aero.bombardier.com; 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, email fedreg.legal@nara.gov, or go to: https:// www.archives.gov/federal-register/cfr/ibrlocations.html. Issued on January 3, 2020. John P. Piccola, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2020–02837 Filed 2–12–20; 8:45 am] BILLING CODE 4910–13–P E:\FR\FM\13FER1.SGM 13FER1

Agencies

[Federal Register Volume 85, Number 30 (Thursday, February 13, 2020)]
[Rules and Regulations]
[Pages 8145-8147]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-02837]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0714; Product Identifier 2019-NM-103-AD; Amendment 
39-21021; AD 2019-26-10]
RIN 2120-AA64


Airworthiness Directives; Bombardier, Inc. Airplanes

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

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all 
Bombardier, Inc., Model CL-600-2C10 (Regional Jet Series 700, 701 & 
702) airplanes; Model CL-600-2D15 (Regional Jet Series 705) airplanes; 
Model CL-600-2D24 (Regional Jet Series 900) airplanes; and Model CL-
600-2E25 (Regional Jet Series 1000) airplanes. This AD was prompted by 
a report of incorrectly installed flight compartment door edge 
protection plates on both sides of the upper decompression panel. This 
AD requires revising the existing maintenance or inspection program, as 
applicable, to incorporate a functional check of the flight compartment 
door decompression latches. The FAA is issuing this AD to address the 
unsafe condition on these products.

DATES: This AD is effective March 19, 2020.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of March 19, 
2020.

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. 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. It is also available on the 
internet at https://www.regulations.gov by searching for and locating 
Docket No. FAA-2019-0714.

[[Page 8146]]

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-2019-
0714; or in person at Docket Operations between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays. The AD docket contains 
this final rule, the regulatory evaluation, any comments received, and 
other information. The address for Docket Operations is 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: Aziz Ahmed, Aerospace Engineer, 
Airframe and Propulsion Section, FAA, New York ACO Branch, 1600 Stewart 
Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7329; fax 516-
794-5531; email [email protected].

SUPPLEMENTARY INFORMATION:

Discussion

    Transport Canada Civil Aviation (TCCA), which is the aviation 
authority for Canada, has issued Canadian AD CF-2019-20R1, dated May 
31, 2019 (referred to after this as the Mandatory Continuing 
Airworthiness Information, or ``the MCAI''), to correct an unsafe 
condition for all Bombardier, Inc., Model CL-600-2C10 (Regional Jet 
Series 700, 701 & 702) airplanes; Model CL-600-2D15 (Regional Jet 
Series 705) airplanes; Model CL-600-2D24 (Regional Jet Series 900) 
airplanes; and Model CL-600-2E25 (Regional Jet Series 1000) airplanes. 
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-2019-
0714.
    The FAA 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-600-2C10 (Regional Jet Series 700, 701 & 702) airplanes; Model 
CL-600-2D15 (Regional Jet Series 705) airplanes; Model CL-600-2D24 
(Regional Jet Series 900) airplanes; and Model CL-600-2E25 (Regional 
Jet Series 1000) airplanes. The NPRM published in the Federal Register 
on October 9, 2019 (84 FR 54051). The NPRM was prompted by a report of 
incorrectly installed flight compartment door edge protection plates on 
both sides of the upper decompression panel. The NPRM proposed to 
require revising the existing maintenance or inspection program, as 
applicable, to incorporate a functional check of the flight compartment 
door decompression latches. The FAA is issuing this AD to address 
incorrect installation of the flight compartment door edge protection 
plates on both sides of the flight compartment door upper decompression 
panel. This condition, if not corrected, could result in the inability 
of the flight compartment door upper decompression panel to open during 
a rapid decompression event. This inability to relieve the pressure in 
the flight compartment may compromise the structural integrity of the 
bulkhead between the flight compartment and the passenger cabin. See 
the MCAI for additional background information.

Comments

    The FAA gave the public the opportunity to participate in 
developing this final rule. The FAA has considered the comment 
received. Victor Oscilowicz indicated his support for the NPRM.

Conclusion

    The FAA reviewed the relevant data, considered the comment 
received, and determined that air safety and the public interest 
require adopting this final rule as proposed, except for minor 
editorial changes. The FAA has determined that these minor changes:
     Are consistent with the intent that was proposed in the 
NPRM for addressing the unsafe condition; and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

    Bombardier, Inc., has issued Task 251700-202, ``Functional Check of 
the Flight Compartment Door Decompression Latches,'' of Section 1, 
``Systems and Power Plant Program,'' Subject 1-25, ``Equipment and 
Furnishings,'' of the Bombardier Model CL-600-2C10, CL-600-2D15, CL-
600-2D24, and CL-600-2E25 Series 700/705/900/1000 Maintenance Review 
Board Report, Maintenance Requirements Manual--Part 1, Volume 1, CSP B-
053, Revision 18, dated July 25, 2018. This service information 
describes a functional check of the flight compartment door 
decompression latches. 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.

Costs of Compliance

    The FAA estimates that this AD affects 522 airplanes of U.S. 
registry. The FAA estimates the following costs to comply with this AD:
    The FAA has determined that revising the existing maintenance or 
inspection program takes an average of 90 workhours per operator, 
although the FAA recognizes that this number may vary from operator to 
operator. In the past, the FAA has estimated that this action takes 1 
work-hour per airplane. Since operators incorporate maintenance or 
inspection program changes for their affected fleet(s), the FAA has 
determined that a per-operator estimate is more accurate than a per-
airplane estimate. Therefore, the FAA estimates the total cost per 
operator to be $7,650 (90 work-hours x $85 per work-hour).

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.
    The FAA is 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 and 
associated appliances to the Director of the System Oversight Division.

Regulatory Findings

    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.

[[Page 8147]]

    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Will not affect intrastate aviation in Alaska, and
    (3) 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):

2019-26-10 Bombardier, Inc.: Amendment 39-21021; Docket No. FAA-
2019-0714; Product Identifier 2019-NM-103-AD.

(a) Effective Date

    This AD is effective March 19, 2020.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to the airplanes identified in paragraphs (c)(1) 
through (4) of this AD, certificated in any category, all serial 
numbers.
    (1) Bombardier, Inc., Model CL-600-2C10 (Regional Jet Series 
700, 701 & 702) airplanes.
    (2) Bombardier, Inc., Model CL-600-2D15 (Regional Jet Series 
705) airplanes.
    (3) Bombardier, Inc., Model CL-600-2D24 (Regional Jet Series 
900) airplanes.
    (4) Bombardier, Inc., Model CL-600-2E25 (Regional Jet Series 
1000) airplanes.

(d) Subject

    Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.

(e) Reason

    This AD was prompted by a report of incorrectly installed flight 
compartment door edge protection plates on both sides of the upper 
decompression panel. The FAA is issuing this AD to address incorrect 
installation of the flight compartment door edge protection plates 
on both sides of the flight compartment door upper decompression 
panel. This condition, if not corrected, could result in the 
inability of the flight compartment door upper decompression panel 
to open during a rapid decompression event. This inability to 
relieve the pressure in the flight compartment may compromise the 
structural integrity of the bulkhead between the flight compartment 
and the passenger cabin.

(f) Compliance

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

(g) Maintenance or Inspection Program Revision

    Within 30 days after the effective date of this AD, revise the 
existing maintenance or inspection program, as applicable, to 
incorporate the information specified in Task 251700-202, 
``Functional Check of the Flight Compartment Door Decompression 
Latches,'' of Section 1, ``Systems and Power Plant Program,'' 
Subject 1-25, ``Equipment and Furnishings,'' of the Bombardier Model 
CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 Series 700/
705/900/1000 Maintenance Review Board Report, Maintenance 
Requirements Manual--Part 1, Volume 1, CSP B-053, Revision 18, dated 
July 25, 2018. The initial compliance time for doing the task is 
within 8,000 flight hours after this task is incorporated into the 
existing maintenance or inspection program, or within 30 days after 
the effective date of this AD, whichever occurs later. Repeat the 
task thereafter at intervals not to exceed 8,000 flight hours.

(h) No Alternative Actions or Intervals

    After the existing maintenance or inspection program has been 
revised as required by paragraph (g) of this AD, no alternative 
actions (e.g., inspections) or intervals may be used unless the 
actions and intervals are approved as an alternative method of 
compliance (AMOC) in accordance with the procedures specified in 
paragraph (i)(1) of this AD.

(i) 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 certification 
office, send it to ATTN: Program Manager, Continuing Operational 
Safety, FAA, New York ACO Branch, 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.

(j) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) Canadian AD CF-2019-20R1, dated May 31, 2019, 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-2019-0714.
    (2) For more information about this AD, contact Aziz Ahmed, 
Aerospace Engineer, Airframe and Propulsion Section, FAA, New York 
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; 
telephone 516-228-7329; fax 516-794-5531; email [email protected].

(k) 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) Task 251700-202, ``Functional Check of the Flight 
Compartment Door Decompression Latches,'' of Section 1, ``Systems 
and Power Plant Program,'' Subject 1-25, ``Equipment and 
Furnishings,'' of the Bombardier Model CL-600-2C10, CL-600-2D15, CL-
600-2D24, and CL-600-2E25 Series 700/705/900/1000 Maintenance Review 
Board Report, Maintenance Requirements Manual--Part 1, Volume 1, CSP 
B-053, Revision 18, dated July 25, 2018.
    (ii) [Reserved]
    (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, email [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on January 3, 2020.
John P. Piccola,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2020-02837 Filed 2-12-20; 8:45 am]
BILLING CODE 4910-13-P
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