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Published 2021-04-05 · Federal Register document 2021-06911

Airworthiness Directives; Airbus SAS Airplanes

Publication summary

The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A330-200 series and A330-300 series airplanes. This AD was prompted by reports of cracked flexible hoses in the courier area oxygen system (CAOS). This AD requires repetitive detailed inspections of the CAOS and replacement of affected parts if necessary. The FAA is issuing this AD to address the unsafe condition on these products.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:08.106391+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2021-9c919420683447c6
Source row
results[107]
Raw source SHA-256
9c919420683447c683ad0c877cb886e341c11862be32b47c536a001b1d76dcb5

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2021-06-07
Effective date printed in this edition
2021-04-20
Read 14 complete recorded clauses
Effective Date
(a) Effective Date

    This airworthiness directive (AD) becomes effective April 20, 
2021.

Exact source excerpt. Text positions 12158–12252, end exclusive, in the original decoded publication. SHA-256: 6d448c35a6798be4235e219be19f7aac506737c8051d7f29cf5ea7df18ded538

Affected ADs
(b) Affected ADs

    None.

Exact source excerpt. Text positions 12252–12281, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0

Applicability wording · Applicability
(c) Applicability

    This AD applies to the Airbus SAS airplanes specified in 
paragraphs (c)(1) and (2) of this AD, certificated in any category, 
converted to freighter airplanes in accordance with FAA supplemental 
type certificate (STC) ST04038NY and STC ST04045NY.
    (1) Model A330-201, -202, -203, -223, and -243 airplanes.
    (2) Model A330-301, -302, -303, -321, -322, -323, -341, -342, 
and -343 airplanes.

Exact source excerpt. Text positions 12281–12703, end exclusive, in the original decoded publication. SHA-256: 0367762192dc5225d387d7380bad227f6c8a27353e35a66b2b080f849be7f732

Subject
(d) Subject

    Air Transport Association (ATA) of America Code 35, Oxygen.

Exact source excerpt. Text positions 12703–12781, end exclusive, in the original decoded publication. SHA-256: beebdc11ca55a698e6bba23e8dc2d9b64bbafa16f2e35342201f0a7331ad0a62

Reason
(e) Reason

    This AD was prompted by reports of cracked flexible hoses in the 
courier area oxygen system (CAOS). The FAA is issuing this AD to 
address cracked CAOS hoses. This condition, if not addressed, could 
lead to oxygen leakage in the flexible hoses of the CAOS, which, in 
combination with in-flight depressurization or smoke evacuation 
procedure, could result in injury to occupants of the courier area.

Exact source excerpt. Text positions 12781–13201, end exclusive, in the original decoded publication. SHA-256: 2ce9e4b65a37fae373b0af7817c38118a0f94a6881215f2d4d99e9b48b141cef

Compliance
(f) Compliance

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

Exact source excerpt. Text positions 13201–13303, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3

Definitions
(g) Definitions

    The definitions in paragraphs (g)(1) and (2) of this AD apply.
    (1) An affected part is a 32209-series oxygen flexible hose used 
in the CAOS, having a part number specified in figure 1 to paragraph 
(g)(1) of this AD.
[GRAPHIC] [TIFF OMITTED] TR05AP21.000

    (2) A serviceable part is an affected part that is new (never 
previously installed), or that, before further flight after 
installation into the CAOS, has passed an inspection and functional 
test (no leakage or damage found) as specified in paragraph (h) of 
this AD.

Exact source excerpt. Text positions 13303–13860, end exclusive, in the original decoded publication. SHA-256: 5a29d7868853af17f609e0248cf2ef8bdd79f5c0182ee8019a17f91099abeb73

Required Actions
(h) Required Actions

    Within 1,600 flight hours after the effective date of this AD 
and thereafter at intervals not to exceed 1,600 flight hours: Do a 
detailed inspection (including functional testing) for leakage or 
damage of the CAOS and lavatory A oxygen system in accordance with 
the Accomplishment Instructions of Elbe Flugzeugwerke GmbH Service 
Bulletin EFW-SB-35-0001, dated March 8, 2019; or Elbe Flugzeugwerke 
GmbH Service Bulletin EFW-SB-35-0002, dated September 2, 2019; as 
applicable.

Exact source excerpt. Text positions 13860–14369, end exclusive, in the original decoded publication. SHA-256: 8e35dc6125ffe49c38da1554edd7241bcb06556fd1728f180816bd9e167bfb1a

Corrective Actions
(i) Corrective Actions

    If, during any inspection required by paragraph (h) of this AD, 
any leakage or damage (i.e., cracking) is found, replace the 
affected part before further flight, in accordance with the 
Accomplishment Instructions of Elbe Flugzeugwerke GmbH Service 
Bulletin EFW-SB-35-0001, dated March 8, 2019; or Elbe Flugzeugwerke 
GmbH Service Bulletin EFW-SB-35-0002, dated September 2, 2019; as 
applicable.

Exact source excerpt. Text positions 14369–14798, end exclusive, in the original decoded publication. SHA-256: 2d4cbd6d3c49cf4ef7f09811bde678521f8780cf7cca8016110ad09e8665a379

Parts Installation Limitation
(j) Parts Installation Limitation

    As of the effective date of this AD, installation of an affected 
part, as defined in paragraph (g)(1) of this AD, on any airplane is 
allowed, provided it is a serviceable part, as defined in paragraph 
(g)(2) of this AD.

Exact source excerpt. Text positions 14798–15061, end exclusive, in the original decoded publication. SHA-256: 5dc082da2fd9eaf8ec19333b23ea623020cb09cb9a5b432a63cb11665fc62722

No Reporting Requirement
(k) No Reporting Requirement

    Although Elbe Flugzeugwerke GmbH Service Bulletin EFW-SB-35-
0001, dated March 8, 2019; and Elbe Flugzeugwerke GmbH Service 
Bulletin EFW-SB-35-0002, dated September 2, 2019; specify to submit 
certain information to the manufacturer, this AD does not include 
that requirement.

Exact source excerpt. Text positions 15061–15375, end exclusive, in the original decoded publication. SHA-256: 2a79da8fc908af7b294b8d9426efec43fc69e8b22e103750a577027fa9b615cb

Other FAA AD Provisions
(l) 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,

[[Page 17515]]

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 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 the European Union Aviation Safety Agency (EASA); or 
Airbus SAS's EASA Design Organization Approval (DOA). If approved by 
the DOA, the approval must include the DOA-authorized signature.

Exact source excerpt. Text positions 15375–16652, end exclusive, in the original decoded publication. SHA-256: 1dc1962c67cb42922008d2a3bd4f631c9b18eceec5d0c6b4f882a7b17d3b6ba2

Related Information
(m) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA AD 2019-0215, dated September 4, 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-2021-0182.
    (2) For more information about this AD, contact Darren Gassetto, 
Aerospace Engineer, Mechanical Systems and Administrative Services 
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, 
Westbury, NY 11590; telephone 516-228-7323; fax 516-794-5531; email 
[email protected].

Exact source excerpt. Text positions 16652–17259, end exclusive, in the original decoded publication. SHA-256: 5f076e223c65a30c54daf249ab810aaa23a280aa5d6824755d408fca0ea0d3bd

Material Incorporated by Reference
(n) 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) Elbe Flugzeugwerke GmbH Service Bulletin EFW-SB-35-0001, 
dated March 8, 2019.
    (ii) Elbe Flugzeugwerke GmbH Service Bulletin EFW-SB-35-0002, 
dated September 2, 2019.
    (3) For service information identified in this AD, contact Elbe 
Flugzeugwerke GmbH Customer Support, Grenzstra[szlig]e 1 01109, 
Dresden, Germany; phone: +49 351 8839 2749; fax: +49 351 8839 2125; 
email: [email protected]; internet: https://www.elbeflugzeugwerke.com/en/.
    (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 [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

Exact source excerpt. Text positions 17259–18627, end exclusive, in the original decoded publication. SHA-256: 89a01178656ac0a0657c75218922aaab6130747746631924777b97ec2510a16b

No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.

Find all recorded historical references to AD 2021-06-07 · 1 printed reference observations in this pinned collection.

These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.

Why these observations are shown

They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.

Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 5ffbc0696e826c1f8a9ca1d5ed80e6cd64ec9fdecba8e66f72cce6c941e42fde. Source manifest: 827f09ad6f52009de186695659cff17401030a2b71348d48254d6a166cc9ee4e.

Official source · 2021-04-05

Publication text

This is the complete recorded text of this dated publication.

Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.

Read the complete official publication text
[Federal Register Volume 86, Number 63 (Monday, April 5, 2021)]
[Rules and Regulations]
[Pages 17512-17515]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-06911]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-0182; Product Identifier 2020-NM-072-AD; Amendment 
39-21474; AD 2021-06-07]
RIN 2120-AA64


Airworthiness Directives; Airbus SAS Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for 
certain Airbus SAS Model A330-200 series and A330-300 series airplanes. 
This AD was prompted by reports of cracked flexible hoses in the 
courier area oxygen system (CAOS). This AD requires repetitive detailed 
inspections of the CAOS and replacement of affected parts if necessary. 
The FAA is issuing this AD to address the unsafe condition on these 
products.

DATES: This AD becomes effective April 20, 2021.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of April 20, 
2021.
    The FAA must receive comments on this AD by May 20, 2021.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
    <bullet> Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
    <bullet> Fax: 202-493-2251.
    <bullet> 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.
    <bullet> Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    For service information identified in this final rule, contact Elbe 
Flugzeugwerke GmbH Customer Support, Grenzstra[szlig]e 1 01109, 
Dresden, Germany; phone: +49 351 8839 2749; fax: +49 351 8839 2125; 
email: [email protected]; internet: https://www.elbeflugzeugwerke.com/en/. You may view this referenced 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. It is 
also available on the internet at https://www.regulations.gov by 
searching for and locating Docket No. FAA-2021-0182.

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-
0182; or in person at the Docket Operations office between 9 a.m. and 5 
p.m., Monday through Friday, except Federal holidays. The AD docket 
contains this AD, any comments received, and other information. The 
street address for the Docket Operations office is listed above.

FOR FURTHER INFORMATION CONTACT: Darren Gassetto, Aerospace Engineer, 
Mechanical Systems and Administrative Services Section, FAA, New York 
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; 
telephone 516-228-7323; fax 516-794-5531; email [email protected].

SUPPLEMENTARY INFORMATION:

Discussion

    The European Union Aviation Safety Agency (EASA), which is the 
Technical Agent for the Member States of the European Union, has issued 
EASA AD 2019-0215, dated September 4, 2019 (referred to after this as 
the Mandatory Continuing Airworthiness Information, or the MCAI), to 
correct an unsafe condition for certain Airbus SAS Model A330-201, 
A330-202, A330-203, A330-223, A330-243, A330-301, A330-302, A330-303, 
A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 
airplanes. You may examine the MCAI on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-
0182.
    This AD was prompted by reports of cracked flexible hoses in the 
CAOS. The FAA is issuing this AD to address cracked CAOS hoses. This 
condition, if not addressed, could lead to oxygen leakage in the 
flexible hoses of the CAOS, which, in combination with in-flight 
depressurization or smoke evacuation procedure, could result in injury 
to occupants of the courier area. See the MCAI for additional 
background information.

[[Page 17513]]

Related Service Information Under 1 CFR Part 51

    Elbe Flugzeugwerke GmbH (EFW) has issued Service Bulletin EFW-SB-
35-0001, dated March 8, 2019; and Service Bulletin EFW-SB-35-0002, 
dated September 2, 2019. This service information describes procedures 
for repetitive detailed inspections (including functional tests) of the 
CAOS to detect any leakage or damage (cracking) in the 32209-series 
oxygen distribution hoses installed in the courier area and in lavatory 
A, and replacement.
    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.

FAA's Determination

    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 the State of Design Authority, 
the FAA has been notified of the unsafe condition described in the MCAI 
and service information referenced above. The FAA is issuing this AD 
because the FAA evaluated all pertinent information and determined the 
unsafe condition exists and is likely to exist or develop on other 
products of the same type design.

Requirements of This AD

    This AD requires accomplishing the actions specified in the service 
information described previously.

FAA's Justification and Determination of the Effective Date

    There are currently no domestic operators of these products. 
Therefore, the FAA finds that notice and opportunity for prior public 
comment are unnecessary and that good cause exists for making this 
amendment effective in less than 30 days.

Comments Invited

    The FAA invites you to send any written relevant data, views, or 
arguments about this AD. Send your comments to an address listed under 
ADDRESSES. Include ``Docket No. FAA-2021-0182; Product Identifier 2020-
NM-072-AD'' 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 
https://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 Darren 
Gassetto, Aerospace Engineer, Mechanical Systems and Administrative 
Services Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 
410, Westbury, NY 11590; telephone 516-228-7323; fax 516-794-5531; 
email [email protected]. Any commentary that the FAA receives 
which is not specifically designated as CBI will be placed in the 
public docket for this rulemaking.

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

    Currently, there are no affected U.S.-registered airplanes. If an 
affected airplane is imported and placed on the U.S. Register in the 
future, the FAA provides the following cost estimates to comply with 
this AD:

                  Estimated Costs for Required Actions
------------------------------------------------------------------------
                                                             Cost per
              Labor cost                   Parts cost        product
------------------------------------------------------------------------
20 work-hours x $85 per hour = $1,700.              $0           $1,700
------------------------------------------------------------------------

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

                 Estimated Costs of On-Condition Actions
------------------------------------------------------------------------
                                                             Cost per
              Labor cost                   Parts cost        product
------------------------------------------------------------------------
7 work-hours x $85 per hour = $595....         $13,485          $14,080
------------------------------------------------------------------------

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

[[Page 17514]]

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

    The FAA determined that 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.

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:

2021-06-07 Airbus SAS: Amendment 39-21474; Docket No. FAA-2021-0182; 
Product Identifier 2020-NM-072-AD.

(a) Effective Date

    This airworthiness directive (AD) becomes effective April 20, 
2021.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to the Airbus SAS airplanes specified in 
paragraphs (c)(1) and (2) of this AD, certificated in any category, 
converted to freighter airplanes in accordance with FAA supplemental 
type certificate (STC) ST04038NY and STC ST04045NY.
    (1) Model A330-201, -202, -203, -223, and -243 airplanes.
    (2) Model A330-301, -302, -303, -321, -322, -323, -341, -342, 
and -343 airplanes.

(d) Subject

    Air Transport Association (ATA) of America Code 35, Oxygen.

(e) Reason

    This AD was prompted by reports of cracked flexible hoses in the 
courier area oxygen system (CAOS). The FAA is issuing this AD to 
address cracked CAOS hoses. This condition, if not addressed, could 
lead to oxygen leakage in the flexible hoses of the CAOS, which, in 
combination with in-flight depressurization or smoke evacuation 
procedure, could result in injury to occupants of the courier area.

(f) Compliance

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

(g) Definitions

    The definitions in paragraphs (g)(1) and (2) of this AD apply.
    (1) An affected part is a 32209-series oxygen flexible hose used 
in the CAOS, having a part number specified in figure 1 to paragraph 
(g)(1) of this AD.
[GRAPHIC] [TIFF OMITTED] TR05AP21.000

    (2) A serviceable part is an affected part that is new (never 
previously installed), or that, before further flight after 
installation into the CAOS, has passed an inspection and functional 
test (no leakage or damage found) as specified in paragraph (h) of 
this AD.

(h) Required Actions

    Within 1,600 flight hours after the effective date of this AD 
and thereafter at intervals not to exceed 1,600 flight hours: Do a 
detailed inspection (including functional testing) for leakage or 
damage of the CAOS and lavatory A oxygen system in accordance with 
the Accomplishment Instructions of Elbe Flugzeugwerke GmbH Service 
Bulletin EFW-SB-35-0001, dated March 8, 2019; or Elbe Flugzeugwerke 
GmbH Service Bulletin EFW-SB-35-0002, dated September 2, 2019; as 
applicable.

(i) Corrective Actions

    If, during any inspection required by paragraph (h) of this AD, 
any leakage or damage (i.e., cracking) is found, replace the 
affected part before further flight, in accordance with the 
Accomplishment Instructions of Elbe Flugzeugwerke GmbH Service 
Bulletin EFW-SB-35-0001, dated March 8, 2019; or Elbe Flugzeugwerke 
GmbH Service Bulletin EFW-SB-35-0002, dated September 2, 2019; as 
applicable.

(j) Parts Installation Limitation

    As of the effective date of this AD, installation of an affected 
part, as defined in paragraph (g)(1) of this AD, on any airplane is 
allowed, provided it is a serviceable part, as defined in paragraph 
(g)(2) of this AD.

(k) No Reporting Requirement

    Although Elbe Flugzeugwerke GmbH Service Bulletin EFW-SB-35-
0001, dated March 8, 2019; and Elbe Flugzeugwerke GmbH Service 
Bulletin EFW-SB-35-0002, dated September 2, 2019; specify to submit 
certain information to the manufacturer, this AD does not include 
that requirement.

(l) 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,

[[Page 17515]]

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 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 the European Union Aviation Safety Agency (EASA); or 
Airbus SAS's EASA Design Organization Approval (DOA). If approved by 
the DOA, the approval must include the DOA-authorized signature.

(m) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA AD 2019-0215, dated September 4, 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-2021-0182.
    (2) For more information about this AD, contact Darren Gassetto, 
Aerospace Engineer, Mechanical Systems and Administrative Services 
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, 
Westbury, NY 11590; telephone 516-228-7323; fax 516-794-5531; email 
[email protected].

(n) 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) Elbe Flugzeugwerke GmbH Service Bulletin EFW-SB-35-0001, 
dated March 8, 2019.
    (ii) Elbe Flugzeugwerke GmbH Service Bulletin EFW-SB-35-0002, 
dated September 2, 2019.
    (3) For service information identified in this AD, contact Elbe 
Flugzeugwerke GmbH Customer Support, Grenzstra[szlig]e 1 01109, 
Dresden, Germany; phone: +49 351 8839 2749; fax: +49 351 8839 2125; 
email: [email protected]; internet: https://www.elbeflugzeugwerke.com/en/.
    (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 [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on March 10, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification 
Service.
[FR Doc. 2021-06911 Filed 4-2-21; 8:45 am]
BILLING CODE 4910-13-P


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