2022-12183. Airworthiness Directives; Airbus Helicopters

AGENCY:

Federal Aviation Administration (FAA), DOT.

ACTION:

Final rule.

SUMMARY:

The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model AS355E, AS355F, AS355F1, AS355F2, AS-365N2, AS 365 N3, SA-365N, SA-365N1, EC 155B, and EC155B1 helicopters. This AD was prompted by investigation results from an engine compartment fire, which determined some of the internal parts of the engine upper fixed cowling (engine cowling) were painted with finish paint on top of the primer layer. This AD requires a one-time inspection of certain part-numbered engine cowlings, and corrective actions if necessary, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.

DATES:

This AD is effective July 13, 2022.

The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of July 13, 2022.

ADDRESSES:

For EASA material incorporated by reference (IBR) in this final rule, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone [phone]; email [e-mail]; internet www.easa.europa.eu. You may find the EASA material on the EASA website at https://ad.easa.europa.eu. For Airbus Helicopters service information identified in this final rule, contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 75052; telephone [phone] or [phone]; fax [phone]; or at https://www.airbus.com/​helicopters/​services/​technical-support.html. You may view this material at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call [phone]. Service information that is IBRed is also available in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-0381.

Examining the AD Docket

You may examine the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-0381; 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 EASA AD, 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:

Andrea Jimenez, Aerospace Engineer, COS Program Management Section, Operational Safety Branch, Compliance & Airworthiness Division, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 11590; telephone [phone]; email [e-mail].

SUPPLEMENTARY INFORMATION:

Background

EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2021-0265, dated November 23, 2021 (EASA AD 2021-0265), to correct an unsafe condition for Airbus Helicopters (AH), formerly Eurocopter, Eurocopter France, Aerospatiale, Sud Aviation, Model SA 365 N, SA 365 N1, AS 365 N2, AS 365 N3, EC 155 B, EC 155 B1, AS 355 E, AS 355 F, AS 355F 1 and AS 355 F2 helicopters, all serial numbers.

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to all Airbus Helicopters Model AS355E, AS355F, AS355F1, AS355F2, AS-365N2, AS 365 N3, SA-365N, SA-365N1, EC 155B, and EC155B1 helicopters. The NPRM published in the Federal Register on March 29, 2022 (87 FR 17955). The NPRM was prompted by investigation results from an engine compartment fire, which determined some of the internal parts of the engine cowling were painted with finish paint on top of the primer layer. The NPRM proposed to require a one-time inspection of certain part-numbered engine cowlings, and corrective actions if necessary, as specified in EASA AD 2021-0265.

The FAA is issuing this AD to detect finish paint inside the duct of the engine cowling. The unsafe condition, if not addressed, could result in fire propagation in case of exposure to high temperature, damage to the helicopter, and injury to the occupants. See EASA AD 2021-0265 for additional background information.

Discussion of Final Airworthiness Directive

Comments

The FAA received no comments on the NPRM or on the determination of the costs.

Conclusion

These helicopters have been approved by EASA and are approved for operation in the United States. Pursuant to the FAA's bilateral agreement with the European Union, EASA has notified the FAA about the unsafe condition described in its AD. The FAA reviewed the relevant data and determined that air safety requires adopting this AD as proposed, except for minor editorial changes. Accordingly, the FAA is issuing this AD to address the unsafe condition on these helicopters.

Related Service Information Under 1 CFR Part 51

EASA AD 2021-0265 requires a one-time inspection of certain part-numbered engine cowlings ( e.g., an affected part as defined in EASA AD 2021-0265) for finish paint and depending on the inspection results, accomplishment of applicable corrective actions. EASA AD 2021-0265 also allows an affected part to be installed on any helicopter, provided it is a serviceable part as defined in EASA AD 2021-0265. Corrective actions include repainting the affected part and replacing the affected part.

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.

Other Related Service Information

The FAA reviewed Airbus Helicopters Alert Service Bulletin (ASB) No. AS355-53.00.38, ASB No. AS365-53.00.65, and ASB No. EC155-53A040, all Revision 0, and all dated October 27, 2021, which specify procedures for inspecting the inside of the duct of the engine cowling for finish paint and corrective actions.

Differences Between This AD and EASA AD 2021-0265

Service information referenced in EASA AD 2021-0265 specifies recording compliance with the applicable ASBs, whereas this AD does not.

Costs of Compliance

The FAA estimates that this AD affects 93 helicopters of U.S. Registry. Labor rates are estimated at $85 per work-hour. Based on these numbers, the FAA estimates the following costs to comply with this AD.

Inspecting each engine cowling takes about 1 work-hour for an estimated cost of $85 per helicopter and $7,905 for the U.S. fleet.

Repainting each engine cowling with primer takes about 8 work-hours for an estimated cost of $680 per helicopter.

Replacing an engine cowling with a “serviceable part” as defined in EASA AD 2021-0265 takes about 4 work-hours and parts cost up to $7,800 for an estimated cost of up to $8,140 per replacement.

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

(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

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:

2022-11-18 Airbus Helicopters: Amendment 39-22068; Docket No. FAA-2022-0381; Project Identifier MCAI-2021-01314-R.

(a) Effective Date

This airworthiness directive (AD) is effective July 13, 2022.

(b) Affected ADs

None.

(c) Applicability

This AD applies to all Airbus Helicopters Model AS355E, AS355F, AS355F1, AS355F2, AS-365N2, AS 365 N3, SA-365N, SA-365N1, EC 155B, and EC155B1 helicopters, certificated in any category.

(d) Subject

Joint Aircraft Service Component (JASC) Code: 7110, Engine Cowling System.

(e) Unsafe Condition

This AD was prompted by investigation results from an engine compartment fire, which determined some of the internal parts of the engine upper fixed cowling (engine cowling) were painted with finish paint on top of the primer layer. The FAA is issuing this AD to detect finish paint inside the duct of the engine cowling. The unsafe condition, if not addressed, could result in fire propagation in case of exposure to high temperature, damage to the helicopter, and injury to the 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, European Union Aviation Safety Agency (EASA) AD 2021-0265, dated November 23, 2021 (EASA AD 2021-0265).

(h) Exceptions to EASA AD 2021-0265

(1) Where EASA AD 2021-0265 requires compliance in terms of flight hours (FH), this AD requires using hours time-in-service.

(2) Where EASA AD 2021-0265 refers to its effective date, this AD requires using the effective date of this AD.

(3) Where paragraph (1) of EASA AD 2021-0265 specifies “in accordance with the instructions of paragraph 3.B of the applicable ASB,” for this AD replace “in accordance with the instructions of paragraph 3.B of the applicable ASB” with “in accordance with the Accomplishment Instructions, paragraphs 3.B.2.a. through 3.B.2.b. of the applicable ASB.”

(4) Where paragraph (2) of EASA AD 2021-0265 specifies to repaint or replace the affected part, replace the text “repaint (with primer layer only) that affected part or replace it with a serviceable part in accordance with the instructions of paragraph 3.B. of the applicable ASB,” with “repaint (with primer layer only) that affected part in accordance with the instructions of paragraph 3.B.2.b. of the applicable ASB, or replace the affected part with a `serviceable part' as defined in EASA AD 2021-0265.”

(5) Where the service information referenced in EASA AD 2021-0265 specifies “identify again the engine upper fixed cowling (a), refer to paragraph 3.C.,” this AD does require modifying your helicopter by marking “ASB No. 53.00.38,” “ASB No. 53A40,” or “ASB No. 53.00.65,” as applicable to your helicopter, after the old P/N on the engine cowling with indelible ink, but does not require compliance with paragraph 3.C. of the “applicable ASB” as defined in EASA AD 2021-0265.

(6) Where the service information referenced in EASA AD 2021-0265 specifies during the interpretation of results from the visual check of the inside of the duct of the engine cowling, if there is any finish paint inside the duct, obey with paragraph 3.B.2.b. ( i.e., perform corrective actions) not more than 6 months after you complied with paragraph 3.B.2.a., for this AD, if there is any finish paint inside the duct of the engine cowling, perform the corrective actions not more than 6 months after you complied with paragraph 3.B.2.a. Work Card 20-04-05-402 (MTC), referenced in the Accomplishment Instructions, paragraph 3.B.2.b. of the “applicable ASB” as defined in EASA AD 2021-0265 is for reference only and is not required for the actions in this AD.

(7) Where the Accomplishment Instructions, paragraph 3.B.2.b of Airbus Helicopters Alert Service Bulletin (ASB) No. AS365-53.00.65, and ASB EC155-53A040, both Revision 0, and both dated October 27, 2021, specify to refer to Work Card 53-50-00-402 (MET), or Task 53-54-00-061(AMM), to remove and install the engine cowling, for this AD those instructions are for reference only and are not required for the actions in this AD.

(8) This AD does not mandate compliance with the “Remarks” section of EASA AD 2021-0265.

(i) No Reporting Requirement

Although the service information referenced in EASA AD 2021-0265 specifies to submit certain information to the manufacturer, this AD does not include that requirement.

(j) Special Flight Permit

Special flight permits may be issued in accordance with 14 CFR 21.197 and 21.199, provided no passengers are onboard.

(k) Alternative Methods of Compliance (AMOCs)

(1) The Manager, 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 local Flight Standards District Office, as appropriate. If sending information directly to the manager of the International Validation Branch, send it to the attention of the person identified in paragraph (l) of this AD. Information may be emailed to: [e-mail].

(2) 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.

(l) Related Information

For more information about this AD, contact Andrea Jimenez, Aerospace Engineer, COS Program Management Section, Operational Safety Branch, Compliance & Airworthiness Division, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 11590; telephone [phone]; email [e-mail].

(m) 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) European Union Aviation Safety Agency (EASA) AD 2021-0265, dated November 23, 2021.

(ii) [Reserved]

(3) For EASA AD 2021-0265, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone [phone]; email [e-mail]; internet www.easa.europa.eu. You may find EASA AD 2021-0265 on the EASA website at https://ad.easa.europa.eu.

(4) You may view this service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call [phone]. This material may be found in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-0381.

(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 [e-mail], or go to: https://www.archives.gov/​federal-register/​cfr/​ibr-locations.html.

Issued on May 24, 2022.

Ross Landes,

Deputy Director for Regulatory Operations, Compliance & Airworthiness Division, Aircraft Certification Service.