2022-22329. Airworthiness Directives; Bombardier, Inc., Airplanes  

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    AGENCY:

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

    ACTION:

    Final rule.

    SUMMARY:

    The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-700-2A12 airplanes. This AD was prompted by reports of insufficient clearance between the surrounding structure/skin of the aircraft and select bleed air ducts that supply the wing ice protection system (WIPS) in the rear fuselage. This AD requires inspecting the bleed air duct and surrounding structure for minimum clearance and damage, and applicable corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.

    DATES:

    This AD is effective November 25, 2022.

    The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of November 25, 2022.

    ADDRESSES:

    AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2022-0886; 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 mandatory continuing airworthiness information (MCAI), 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.

    Material Incorporated by Reference:

    • For service information identified in this final rule, contact Bombardier Business Aircraft Customer Response Center, 400 Côte-Vertu Road West, Dorval, Québec H4S 1Y9, Canada; telephone 514-855-2999; email ac.yul@aero.bombardier.com; website bombardier.com.

    • You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Start Printed Page 63939 Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. It is also available at regulations.gov under Docket No. FAA-2022-0886.

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    FOR FURTHER INFORMATION CONTACT:

    Elizabeth Dowling, Aerospace Engineer, Mechanical Systems and Administrative Services Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7300; email 9-avs-nyaco-cos@faa.gov.

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    SUPPLEMENTARY INFORMATION:

    Background

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain Bombardier, Inc., Model BD-700-2A12 airplanes. The NPRM published in the Federal Register on July 21, 2022 (87 FR 43462). The NPRM was prompted by AD CF-2022-05, dated February 24, 2022, issued by Transport Canada Civil Aviation (TCCA), which is the aviation authority for Canada (referred to after this as the MCAI). The MCAI states that insufficient clearance exists between the surrounding structure/skin of the aircraft and select bleed air ducts that supply the WIPS in the rear fuselage on the aircraft. Without sufficient clearance, the high pressure (HP) shroud could interfere with the surrounding structures and possibly compromise the HP ducting shroud's capability to provide bleed air leak routing, which could result in a bleed air leak being undetected. A significant undetected bleed air leak could expose the surrounding structure to heat stress, resulting in reduced structural integrity of the airplane.

    In the NPRM, the FAA proposed to require inspecting the bleed air duct and surrounding structure for minimum clearance and damage, and applicable corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.

    You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA-2022-0886.

    Discussion of Final Airworthiness Directive

    Comments

    The FAA received no comments on the NPRM or on the determination of the cost to the public.

    Conclusion

    This product has been approved by the aviation authority of another country and is approved for operation in the United States. Pursuant to the FAA's bilateral agreement with this State of Design Authority, it has notified the FAA of the unsafe condition described in the MCAI referenced above. The FAA reviewed the relevant data and determined that air safety requires adopting this AD as proposed. Accordingly, the FAA is issuing this AD to address the unsafe condition on this product. Except for minor editorial changes, this AD is adopted as proposed in the NPRM. None of the changes will increase the economic burden on any operator.

    Related Service Information Under 1 CFR Part 51

    Bombardier has issued Service Bulletin 700-36-7502, dated October 28, 2020. This service information describes procedures for inspecting the bleed air duct and surrounding structure for minimum clearance and damage (wear and chafing), and corrective actions. Corrective actions include adjusting the ductwork if clearance is below the minimum required, and repairing any damage. 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 8 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD:

    Estimated Costs for Required Actions

    Labor costParts costCost per productCost on U.S. operators
    1 work-hours × $85 per hour = $85$1$86$688

    Estimated Costs of On-Condition Actions

    Labor costParts costCost per product
    Up to 22 work-hours × $85 per hour = $1,870$0$1,870

    The FAA has included all known costs in its cost estimate. According to the manufacturer, however, some or all of the costs of this AD may be covered under warranty, thereby reducing the cost impact on affected operators.

    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.

    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.

    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 Start Printed Page 63940

    (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.

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    List of Subjects in 14 CFR Part 39

    • Air transportation
    • Aircraft
    • Aviation safety
    • Incorporation by reference
    • Safety
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    The Amendment

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

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    PART 39—AIRWORTHINESS DIRECTIVES

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

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

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    [Amended]
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    2. The FAA amends § 39.13 by adding the following new airworthiness directive:

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    2022-20-09 Bombardier, Inc.: Amendment 39-22193; Docket No. FAA-2022-0886; Project Identifier MCAI-2022-00261-T.

    (a) Effective Date

    This airworthiness directive (AD) is effective November 25, 2022.

    (b) Affected ADs

    None.

    (c) Applicability

    This AD applies to Bombardier, Inc., Model BD-700-2A12 airplanes, certificated in any category, serial numbers 70006, 70007, 70009 through 70019 inclusive, 70021 through 70029 inclusive, and 70031.

    (d) Subject

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

    (e) Unsafe Condition

    This AD was prompted by reports of insufficient clearance between the surrounding structure/skin of the aircraft and select bleed air ducts that supply the wing ice protection system (WIPS) in the rear fuselage. The FAA is issuing this AD to address possible interference between the high pressure (HP) shroud and the surrounding structures, which could compromise the HP ducting shroud's capability to provide bleed air leak routing and result in a bleed air leak being undetected. A significant undetected bleed air leak could expose the surrounding structure to heat stress, resulting in reduced structural integrity of the airplane.

    (f) Compliance

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

    (g) Required Actions

    Within 21 months after the effective date of this AD: Inspect the affected bleed air ducts and surrounding structure for minimum clearance and damage (wear or chafing), and do all applicable corrective actions in accordance with the Accomplishment Instructions of Bombardier Service Bulletin 700-36-7502, dated October 28, 2020. Do all applicable corrective actions before further flight.

    (h) No Reporting Requirement

    Although Bombardier Service Bulletin 700-36-7502, dated October 28, 2020, specifies to submit certain information to the manufacturer, this AD does not include that requirement.

    (i) Other 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 responsible Flight Standards 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. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office.

    (2) Contacting the Manufacturer: For any requirement in this AD to obtain instructions from a manufacturer, the instructions 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) Additional Information

    (1) Refer to TCCA AD CF-2022-05, dated February 24, 2022, for related information. This TCCA AD may be found in the AD docket at regulations.gov under Docket No. FAA-2022-0886.

    (2) For more information about this AD, contact Elizabeth Dowling, Aerospace Engineer, Mechanical Systems and Administrative Services Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7300; email 9-avs-nyaco-cos@faa.gov.

    (k) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the incorporation by reference 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 700-36-7502, dated October 28, 2020.

    (ii) [Reserved]

    (3) For service information identified in this AD, contact Bombardier Business Aircraft Customer Response Center, 400 Côte-Vertu Road West, Dorval, Québec H4S 1Y9, Canada; telephone 514-855-2999; email ac.yul@aero.bombardier.com; website bombardier.com.

    (4) You may view this service information at the FAA, Airworthiness Products Section, Operational Safety 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 fr.inspection@nara.gov, or go to: www.archives.gov/​federal-register/​cfr/​ibr-locations.html.

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    Issued on September 19, 2022.

    Christina Underwood,

    Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service.

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    [FR Doc. 2022-22329 Filed 10-20-22; 8:45 am]

    BILLING CODE 4910-13-P

Document Information

Effective Date:
11/25/2022
Published:
10/21/2022
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule.
Document Number:
2022-22329
Dates:
This AD is effective November 25, 2022.
Pages:
63938-63940 (3 pages)
Docket Numbers:
Docket No. FAA-2022-0886, Project Identifier MCAI-2022-00261-T, Amendment 39-22193, AD 2022-20-09
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
Topics:
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety
PDF File:
2022-22329.pdf
Supporting Documents:
» Airworthiness Directives: Bombardier, Inc., Airplanes
» Supporting AD Document
» Airworthiness Directives: Bombardier, Inc., Airplanes
CFR: (1)
14 CFR 39.13