[Federal Register Volume 86, Number 96 (Thursday, May 20, 2021)]
[Rules and Regulations]
[Pages 27271-27273]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-10608]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-0105; Project Identifier MCAI-2020-01422-R; 
Amendment 39-21543; AD 2021-10-10]
RIN 2120-AA64


Airworthiness Directives; Airbus Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all 
Airbus Helicopters Model SA330J helicopters. This AD was prompted by 
the failure of a second stage planet gear installed in the main gearbox 
(MGB). This AD requires repetitively inspecting the MGB particle 
detector and the MGB bottom housing (oil sump) for metal particles, 
analyzing any metal particles that are found, and replacement of the 
MGB if necessary, as specified in a European Aviation Safety Agency 
(now 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 June 24, 2021.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of June 24, 
2021.

ADDRESSES: For material incorporated by reference (IBR) in this AD, 
contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; 
phone: +49 221 8999 000; email: ADs@easa.europa.eu; internet: 
www.easa.europa.eu. You may find this material on the EASA website at 
https://ad.easa.europa.eu. 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 817-222-5110. It is also available in 
the AD docket on the internet at https://www.regulations.gov by 
searching for and locating Docket No. FAA-2021-0105.

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-2021-
0105; 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, 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: Mahmood G. Shah, Aviation Safety 
Engineer, Fort Worth ACO Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, 
TX 76177; phone: 817-222-5538; email: mahmood.g.shah@faa.gov.

SUPPLEMENTARY INFORMATION:

Background

    The EASA, which is the Technical Agent for the Member States of the 
European Union, has issued EASA AD 2018-0272, dated December 13, 2018 
(EASA AD 2018-0272) (also referred to as the Mandatory Continuing 
Airworthiness Information, or the MCAI), to correct an unsafe condition 
for all Airbus Helicopters Model SA330J helicopters.
    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 SA330J helicopters. The NPRM published in the Federal Register on 
March 2, 2021 (86 FR 12127). The NPRM was prompted by the failure of a 
second stage planet gear installed in the MGB. The NPRM proposed to 
require repetitively inspecting the MGB particle detector and the MGB 
bottom housing (oil sump) for metal particles, analyzing any metal 
particles that are found, and replacement of the MGB if necessary, as 
specified in an EASA AD.
    The FAA is issuing this AD to address failure of an MGB second 
stage planet gear, which could result in failure of the MGB and 
subsequent loss of control of the helicopter. See the MCAI for 
additional background information.

Discussion of Final Airworthiness Directive

Comments

    The FAA gave the public the opportunity to participate in 
developing this final rule. The FAA received no comments on the NPRM or 
on the determination of the cost to the public.

Conclusion

    The FAA reviewed the relevant data 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

    EASA AD 2018-0272 specifies procedures for repetitively inspecting 
the MGB particle detector and the MGB bottom housing (oil sump) for 
metal particles, analyzing any metal particles that are found, and 
replacement of the MGB if necessary. 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.

Interim Action

    The FAA considers this AD interim action. If final action is later 
identified, the FAA might consider further rulemaking then.

[[Page 27272]]

Costs of Compliance

    The FAA estimates that this AD affects 15 helicopters of U.S. 
registry. The FAA estimates the following costs to comply with this AD:

                                      Estimated Costs for Required Actions
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                                                                                    Cost per       Cost on U.S.
                          Labor cost                              Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
5 work-hours x $85 per hour = $425...........................              $0             $425           $6,375
----------------------------------------------------------------------------------------------------------------

    The FAA estimates the following costs to do any necessary on-
condition replacements that would be required based on the results of 
any required actions. The FAA has no way of determining the number of 
helicopters that might need these on-condition replacements:

                 Estimated Costs of On-Condition Actions
------------------------------------------------------------------------
                                                             Cost per
           Labor cost                   Parts cost            product
------------------------------------------------------------------------
40 work-hours x $85 per hour =   $600,000 (overhauled)..        $603,400
 $3,400.
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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

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:

2021-10-10 Airbus Helicopters: Amendment 39-21543; Docket No. FAA-
2021-0105; Project Identifier MCAI-2020-01422-R.

(a) Effective Date

    This airworthiness directive (AD) is effective June 24, 2021.

(b) Affected Airworthiness Directives (ADs)

    None.

 (c) Applicability

    This AD applies to all Airbus Helicopters Model SA330J 
helicopters, certificated in any category.

 (d) Subject

    Joint Aircraft System Component (JASC) Code 6320, Main Rotor 
Gearbox.

 (e) Reason

    This AD was prompted by a failure of a second stage planet gear 
installed in the main gearbox (MGB). The FAA is issuing this AD to 
address failure of an MGB second stage planet gear, which could 
result in failure of the MGB and subsequent loss of control of the 
helicopter.

 (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 Aviation Safety Agency (now European Union 
Aviation Safety Agency) (EASA) AD 2018-0272, dated December 13, 2018 
(EASA AD 2018-0272).

 (h) Exceptions to EASA AD 2018-0272

    (1) Where EASA AD 2018-0272 refers to its effective date, this 
AD requires using the effective date of this AD.
    (2) Where EASA AD 2018-0272 refers to March 30, 2018 (the 
effective date of EASA AD 2018-0065, dated March 23, 2018), this AD 
requires using the effective date of this AD.
    (3) The ``Remarks'' section of EASA AD 2018-0272 does not apply 
to this AD.
    (4) Where EASA AD 2018-0272 refers to flight hours (FH), this AD 
requires using hours time-in-service.
    (5) Where paragraph (1) of EASA AD 2018-0272 specifies to 
inspect the MGB particle detector ``in accordance with the 
instructions of Section 3 of the ASB'' for this AD use ``in 
accordance with the instructions in step 3.B.2.a. of the ASB.''
    (6) Where paragraph (2) of EASA AD 2018-0272 specifies to 
inspect the MGB bottom housing (oil sump) ``in accordance with the 
instructions of Section 3 of the ASB'' for this AD use ``in 
accordance with the instructions in step 3.B.2.b. of the ASB.''

[[Page 27273]]

    (7) Where the service information referenced in EASA AD 2018-
0272 specifies to perform a metallurgical analysis and contact the 
manufacturer if unsure about the characterization of the particles 
collected, this AD does not require contacting the manufacturer to 
determine the characterization of the particles collected.
    (8) Although the service information referenced in EASA AD 2018-
0272 specifies that if any 16NCD13 particles are found to contact 
the manufacturer and send a 1-liter sample of oil to the 
manufacturer, this AD does not require that action.
    (9) Although the service information referenced in EASA AD 2018-
0272 specifies returning certain parts to the manufacturer, this AD 
does not require that action.
    (10) Where EASA AD 2018-0272 specifies actions be done after the 
last flight of the day or ``ALF,'' this AD requires doing those 
actions before the first flight of the day.
    (11) Although the service information referenced in EASA AD 
2018-0272 specifies discarding certain parts, this AD requires 
removing the parts from service.

 (i) Special Flight Permit

    Special flight permits may be issued in accordance with 14 CFR 
21.197 and 21.199 to operate the helicopter to a location where the 
helicopter can be modified (if the operator elects to do so), 
provided that the helicopter is operated during the day, under 
visual flight rules, and with no passengers onboard.

 (j) 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 (k) of 
this AD. Information may be emailed to: 9-AVS-AIR-730-AMOC@faa.gov.
    (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.

 (k) Related Information

    For more information about this AD, contact Mahmood G. Shah, 
Aviation Safety Engineer, Fort Worth ACO Branch, FAA, 10101 Hillwood 
Pkwy., Fort Worth, TX 76177; phone: 817-222-5538; email: 
mahmood.g.shah@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 Aviation Safety Agency (EASA) AD 2018-0272, dated 
December 13, 2018.
    (ii) [Reserved]
    (3) For EASA AD 2018-0272, contact the EASA, Konrad-Adenauer-
Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999 000; email: 
ADs@easa.europa.eu; Internet: 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 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 817-222-5110. This material may be 
found in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-
2021-0105.
    (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 
fedreg.legal@nara.gov, or go to https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on May 3, 2021.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness 
Division, Aircraft Certification Service.
[FR Doc. 2021-10608 Filed 5-19-21; 8:45 am]
BILLING CODE 4910-13-P


