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Start Preamble
AGENCY:
Federal Aviation Administration (FAA), DOT.
ACTION:
Final rule; request for comments.
SUMMARY:
The FAA is superseding Airworthiness Directive (AD) 2019-20-03, which applied to various transport airplanes. AD 2019-20-03 required modification of certain universal serial bus (USB) receptacles located in the flight deck. Since the FAA issued AD 2019-20-03, it has been determined that additional airplanes are affected by the unsafe condition. This AD continues to require the modification and expands the applicability, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD also prohibits the installation of affected parts. The FAA is issuing this AD to address the unsafe condition on these products.
DATES:
This AD is effective August 12, 2022.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of August 12, 2022.
The FAA must receive comments on this AD by September 12, 2022.
ADDRESSES:
You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:
• Federal eRulemaking Portal: Go to www.regulations.gov. Follow the instructions for submitting comments.
• Fax: 202-493-2251.
• Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590.
• Hand Delivery: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For material incorporated by reference (IBR) in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find this IBR material on the EASA website at https://ad.easa.europa.eu. You may view this material 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. It is also available in the AD docket at www.regulations.gov by searching for and locating Docket No. FAA-2022-0883.
Examining the AD Docket
You may examine the AD docket at www.regulations.gov by searching for and locating Docket No. FAA-2022-0883; 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 AD, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The street address for Docket Operations is listed above.
Start Further InfoFOR FURTHER INFORMATION CONTACT:
Dan Rodina, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 206-231-3225; email dan.rodina@faa.gov.
End Further Info End Preamble Start Supplemental InformationSUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written data, views, or arguments about this final rule. Send your comments to an address listed under ADDRESSES . Include “Docket No. FAA-2022-0883; Project Identifier MCAI-2021-01179-T” at the beginning of your comments. The most helpful comments reference a specific portion of the final rule, explain the reason for any recommended change, and include supporting data. The FAA will consider all comments received by the closing date and may amend this final rule because of those comments.
Except for Confidential Business Information (CBI) as described in the following paragraph, and other information as described in 14 CFR 11.35, the FAA will post all comments received, without change, to Start Printed Page 45244 www.regulations.gov, including any personal information you provide. The agency will also post a report summarizing each substantive verbal contact received about this final rule.
Confidential Business Information
CBI is commercial or financial information that is both customarily and actually treated as private by its owner. Under the Freedom of Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public disclosure. If your comments responsive to this AD contain commercial or financial information that is customarily treated as private, that you actually treat as private, and that is relevant or responsive to this AD, it is important that you clearly designate the submitted comments as CBI. Please mark each page of your submission containing CBI as “PROPIN.” The FAA will treat such marked submissions as confidential under the FOIA, and they will not be placed in the public docket of this AD. Submissions containing CBI should be sent to Dan Rodina, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 206-231-3225; email dan.rodina@faa.gov. Any commentary that the FAA receives which is not specifically designated as CBI will be placed in the public docket for this rulemaking.
Background
The FAA issued AD 2019-20-03, Amendment 39-19756 (84 FR 55036, October 15, 2019) (AD 2019-20-03), which applied to various transport airplanes. AD 2019-20-03 required modification of certain USB receptacles located in the flight deck. The FAA issued AD 2019-20-03 to address smoke and fumes in the flight deck, which could result in excessive flightcrew workload and injury to flight deck occupants.
Actions Since AD 2019-20-03 Was Issued
Since the FAA issued AD 2019-20-03, the European Union Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2021-0234, dated October 28, 2021 (EASA AD 2021-0234) (also referred to after this as the Mandatory Continuing Airworthiness Information, or the MCAI), to correct an unsafe condition for various transport airplanes. EASA AD 2021-0234 superseded EASA AD 2018-0259R1, dated February 7, 2019. FAA AD 2019-20-03 corresponded to EASA AD 2018-0259R1. EASA AD 2021-0234 retained the requirements of EASA AD 2018-0259R1 and expanded the applicability. You may examine the MCAI in the AD docket on the internet at www.regulations.gov by searching for and locating Docket No. FAA-2022-0883.
This AD was prompted by reports of smoke and fumes in the flight deck. The FAA is issuing this AD to address smoke and fumes in the flight deck, which could result in excessive flightcrew workload and injury to flight deck occupants. See the MCAI for additional background information.
Although this AD expands the applicability, none of the newly added airplanes are on the U.S. Register.
Explanation of Retained Requirements
Although this AD does not explicitly restate the requirements of AD 2019-20-03, this AD retains all of the requirements of AD 2019-20-03. Those requirements are referenced in EASA AD 2021-0234, which, in turn, is referenced in paragraph (g) of this AD.
Related Service Information Under 1 CFR Part 51
EASA AD 2021-0234 specifies procedures for modification of certain USB receptacles located in the flight deck.
This material 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.
FAA's Determination
These products have been approved by the aviation authority of another country and are 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 described above. The FAA is issuing this AD after determining that the unsafe condition described previously is likely to exist or develop on other products of these same type designs.
Requirements of This AD
This AD requires accomplishing the actions specified in EASA AD 2021-0234 described previously, except for any differences identified as exceptions in the regulatory text of this AD. This AD also prohibits the installation of affected parts.
Explanation of Required Compliance Information
In the FAA's ongoing efforts to improve the efficiency of the AD process, the FAA developed a process to use some civil aviation authority (CAA) ADs as the primary source of information for compliance with requirements for corresponding FAA ADs. The FAA has been coordinating this process with manufacturers and CAAs. As a result, EASA AD 2021-0234 is incorporated by reference in this AD. This AD requires compliance with EASA AD 2021-0234 in its entirety through that incorporation, except for any differences identified as exceptions in the regulatory text of this AD. Using common terms that are the same as the heading of a particular section in EASA AD 2021-0234 does not mean that operators need comply only with that section. For example, where the AD requirement refers to “all required actions and compliance times,” compliance with this AD requirement is not limited to the section titled “Required Action(s) and Compliance Time(s)” in EASA AD 2021-0234. Service information required by EASA AD 2021-0234 for compliance will be available at www.regulations.gov by searching for and locating Docket No. FAA-2022-0883 after this AD is published.
FAA's Justification and Determination of the Effective Date
None of the airplanes added to the applicability of this AD are currently on the U.S. Register. Accordingly, notice and opportunity for prior public comment are unnecessary, pursuant to 5 U.S.C. 553(b)(3)(B). In addition, for the forgoing reason(s), the FAA finds that good cause exists pursuant to 5 U.S.C. 553(d) for making this amendment effective in less than 30 days.
Regulatory Flexibility Act (RFA)
The requirements of the RFA do not apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and comment. Because the FAA has determined that it has good cause to adopt this rule without notice and comment, RFA analysis is not required.
Costs of Compliance
The FAA estimates that this AD affects 14 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD: Start Printed Page 45245
Estimated Costs for Required Actions
Action Labor cost Parts cost Cost per product Cost on U.S. operators Retained actions in AD 2019-20-03 3 work-hours × $85 per hour = $255 $0 $255 $3,470 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, and
(2) Will not affect intrastate aviation in Alaska.
Start List of SubjectsList of Subjects in 14 CFR Part 39
- Air transportation
- Aircraft
- Aviation safety
- Incorporation by reference
- Safety
The Amendment
Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
Start PartPART 39—AIRWORTHINESS DIRECTIVES
End Part Start Amendment Part1. The authority citation for part 39 continues to read as follows:
End Amendment Part[Amended]2. The FAA amends § 39.13 by:
End Amendment Part Start Amendment Parta. Removing Airworthiness Directive (AD) 2019-20-03, Amendment 39-19756 ( 84 FR 55036, October 15, 2019); and
End Amendment Part Start Amendment Partb. Adding the following new AD:
End Amendment Part2022-15-08 Transport Category Airplanes: Amendment 39-22128; Docket No. FAA-2022-0883; Project Identifier MCAI-2021-01179-T.
(a) Effective Date
This airworthiness directive (AD) is effective August 12, 2022.
(b) Affected ADs
This AD replaces AD 2019-20-03, Amendment 39-19756 (84 FR 55036, October 15, 2019) (AD 2019-20-03).
(c) Applicability
This AD applies to the airplanes identified in EASA AD 2021-0234, dated October 28, 2021 (EASA AD 2021-0234), certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 46, Information systems.
(e) Unsafe Condition
This AD was prompted by reports of smoke and fumes in the flight deck. The FAA is issuing this AD to address smoke and fumes in the flight deck, which could result in excessive flightcrew workload and injury to flight deck occupants.
(f) Compliance
Comply with this AD within the compliance times specified, unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 2021-0234.
(h) Exceptions to EASA AD 2021-0234
(1) Where EASA AD 2021-0234 refers to the effective date of December 14, 2018 (the effective date of the original issue of EASA AD 2018-0259) this AD requires using November 19, 2019 (the effective date of AD 2019-20-03).
(2) Where EASA AD 2021-0234 refers to its effective date, this AD requires using the effective date of this AD.
(3) The “Remarks” section of EASA AD 2021-0234 does not apply to this AD.
(i) Parts Installation Prohibition
After modification of an airplane as required by paragraph (g) of this AD, no person may install an affected part on any airplane.
(j) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, Large Aircraft Section, International Validation 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 Large Aircraft Section, International Validation Branch, send it to the attention of the person identified in paragraph (k) of this AD. Information may be emailed to: 9-AVS-AIR-730-AMOC@faa.gov/ATTN: Program Manager, Continuing Operational Safety, FAA. 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, Large Aircraft Section, International Validation Branch, FAA; or EASA; or Fokker Services B.V.'s EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature.
(k) Related Information
For more information about this AD, contact Dan Rodina, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 206-231-3225; email dan.rodina@faa.gov.
(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) European Union Aviation Safety Agency (EASA) AD 2021-0234, dated October 28, 2021.
(ii) [Reserved]
(3) For EASA AD 2021-0234, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; internet Start Printed Page 45246 www.easa.europa.eu. You may find this EASA AD on the EASA website at https://ad.easa.europa.eu.
(4) You may view this material 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. This material may be found in the AD docket at www.regulations.gov by searching for and locating Docket No. FAA-2022-0883.
(5) You may view this material 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.
Start SignatureIssued on July 15, 2022.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness Division, Aircraft Certification Service.
[FR Doc. 2022-16083 Filed 7-27-22; 8:45 am]
BILLING CODE 4910-13-P
Document Information
- Effective Date:
- 8/12/2022
- Published:
- 07/28/2022
- Department:
- Federal Aviation Administration
- Entry Type:
- Rule
- Action:
- Final rule; request for comments.
- Document Number:
- 2022-16083
- Dates:
- This AD is effective August 12, 2022.
- Pages:
- 45243-45246 (4 pages)
- Docket Numbers:
- Docket No. FAA-2022-0883, Project Identifier MCAI-2021-01179-T, Amendment 39-22128, AD 2022-15-08
- 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:
- 2022-16083.pdf
- Supporting Documents:
- » U.S. DOT/FAA - Supplemental AD Document (EASA_AD_2021_0234)
- » Airworthiness Directives: Various Transport Airplanes
- CFR: (1)
- 14 CFR 39.13