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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