Published 2020-03-20 · Federal Register document 2020-05667
Airworthiness Directives; Airbus Helicopters
Publication summary
The FAA is adopting a new airworthiness directive (AD) for Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, and AS332L2 helicopters. This AD requires removing the drain plugs from the fuel tank compartments located under the bottom structure. This AD was prompted by the discovery that a modification to the fuel tank could lead to fuel accumulating in an area containing electrical equipment and subsequent ignition of fuel vapors. The actions of this AD are intended to address an unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:04.586324+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2020-f01fbc4d7ab3dbaa
- Source row
- results[74]
- Raw source SHA-256
- f01fbc4d7ab3dbaae6a412acd9ff6cece48db77a6a882e46e8f8087200be3837
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2020-05-20
- Effective date printed in this edition
- 2020-04-24
Some source clauses remain unstructured. Read the complete publication for conditions that have not been interpreted here.
Read 10 complete recorded clauses
Applicability wording · Applicability
(a) Applicability
This AD applies to Airbus Helicopters Model AS332C, AS332C1,
AS332L, AS332L1, and AS332L2 helicopters, certificated in any
category, except those with modification 0726383 installed.
Exact source excerpt. Text positions 9342–9551, end exclusive, in the original decoded publication. SHA-256: 186b20f7cf3d084c656636e9cf974bce48ba9379d3cfccb674f953bf0ec0892a
Unsafe Condition
(b) Unsafe Condition
This AD defines the unsafe condition as closure of fuel tank
drains. This condition could result in fuel accumulating in an area
containing electrical equipment and ignition of fuel vapors. This
condition could result in a fire and subsequent damage to the
helicopter or injury to the occupants.
Exact source excerpt. Text positions 9551–9878, end exclusive, in the original decoded publication. SHA-256: 1494ad3f1920498fc0df7821acbde30b3f08c186de263771ba67542e367fc7ae
Effective Date
(c) Effective Date
This AD becomes effective April 24, 2020.
Exact source excerpt. Text positions 9878–9945, end exclusive, in the original decoded publication. SHA-256: 35b6bf2b17f52dc6092e1914678f819c9d021c330992d83966c2bb71f4a02687
Compliance
(d) Compliance
You are responsible for performing each action required by this
AD within the specified compliance time unless it has already been
accomplished prior to that time.
Exact source excerpt. Text positions 9945–10132, end exclusive, in the original decoded publication. SHA-256: 56042b53a75a0db2af067b711f9b82d8091413842e43863752e31aeffdd54a72
Required Actions
(e) Required Actions
Within 110 hours time-in-service or during the next scheduled
maintenance, whichever occurs first:
(1) For Model AS332C and AS332C1 helicopters, remove the 6 fuel
tank drain plugs by following the Accomplishment Instructions,
paragraph 3.B.2. of Airbus Helicopters Alert Service Bulletin No.
AS332-53.01.62, Revision 1, dated May 28, 2019 (ASB AS332-53.01.62),
except you are not required to place the drain plugs in stock.
(2) For Model AS332L, AS332L1, and AS332L2 helicopters, remove
the 7 fuel tank drain plugs by following the Accomplishment
Instructions, paragraph 3.B.2. of ASB AS332-53.01.62, except you are
not required to place the drain plugs in stock.
Exact source excerpt. Text positions 10132–10839, end exclusive, in the original decoded publication. SHA-256: efc4974696f772a9563af52c014b5ddcceb590f7902961fd9c46cad731d79440
Credit for Previous Actions
(f) Credit for Previous Actions
Actions accomplished before the effective date of this AD in
accordance with the procedures specified in Airbus Helicopters Alert
Service Bulletin No. AS332-53.01.62, Revision 0, dated June 7, 2018,
are considered acceptable for compliance with the corresponding
actions specified in paragraph (e) of this AD.
Exact source excerpt. Text positions 10839–11191, end exclusive, in the original decoded publication. SHA-256: 496212e5f4b7b0d9b3aa45cd2c1da9624cc41c1ffa6d56d826e8dae62c83ddc1
Alternative Methods of Compliance (AMOCs)
(g) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Safety Management Section, Rotorcraft Standards
Branch, FAA, may approve AMOCs for this AD. Send your proposal to:
James Blyn, Aviation Safety Engineer, Regulations and Policy
Section, Rotorcraft Standards Branch, FAA, 10101 Hillwood Pkwy.,
Fort Worth, TX 76177; telephone 817-222-5110; email [email protected].
(2) For operations conducted under a 14 CFR part 119 operating
certificate or under 14 CFR part 91, subpart K, the FAA suggests
that you notify your principal inspector, or lacking a principal
inspector, the manager of the local flight standards district office
or certificate holding district office, before operating any
aircraft complying with this AD through an AMOC.
Exact source excerpt. Text positions 11191–11957, end exclusive, in the original decoded publication. SHA-256: 90cb4f6f9c52ba48f552be24c95b15e773d1b6809c13a253e6f55e2e8c67af94
Additional Information
(h) Additional Information
(1) Airbus Helicopters Alert Service Bulletin No. AS332-
53.01.62, Revision 0, dated June 7, 2018, which is not incorporated
by reference, contains additional information about the subject of
this AD. For service information identified in this AD, contact
Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 75052;
telephone 972-641-0000 or 800-232-0323; fax 972-641-3775; or at
https://www.airbus.com/helicopters/services/technical-support.html.
You may view the referenced service information at the FAA, Office
of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy.,
Room 6N-321, Fort Worth, TX 76177.
(2) The subject of this AD is addressed in European Union
Aviation Safety Agency (previously European Aviation Safety Agency)
(EASA) AD No. 2018-0209, dated September 21, 2018. You may view the
EASA AD on the internet at https://www.regulations.gov in Docket No.
FAA-2019-0970.
Exact source excerpt. Text positions 11957–12904, end exclusive, in the original decoded publication. SHA-256: 31c8b531e54ee23010d2dd102199730046561ad6da0bb0452b1fe8b19336cb0e
Subject
(i) Subject
Joint Aircraft Service Component (JASC) Code: 2810, Fuel
Storage.
Exact source excerpt. Text positions 12904–12989, end exclusive, in the original decoded publication. SHA-256: 8b16d1373a7bf8004f5e4245cc29cac4c2a342b5fb9be8ef585ea342c40e17aa
Material Incorporated by Reference
(j) 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 the AD specifies otherwise.
(i) Airbus Helicopters Alert Service Bulletin No. AS332-
53.01.62, Revision 1, dated May 28, 2019.
(ii) [Reserved]
(3) For service information identified in this AD, contact
Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 75052;
telephone 972-641-0000 or 800-232-0323; fax 972-641-3775; or at
https://www.airbus.com/helicopters/services/technical-support.html.
(4) You may view this service information at 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.
(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 12989–14284, end exclusive, in the original decoded publication. SHA-256: 201de88aca11ab7cf0316cf355ffcd3c97b76904498606345f03e89d26ebc75b
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 2020-05-20 · 0 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: c8b56f5152889881df2a6f449a8bf18686ef8976f8ba0d17fa17aae72ca2f8cb. Source manifest: c966775f950d7412abb42e800b6cf8487ffac275bf698a2b8f274a2f33f2bec4.
Official source · 2020-03-20
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 85, Number 55 (Friday, March 20, 2020)]
[Rules and Regulations]
[Pages 15924-15926]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-05667]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-0970; Product Identifier 2018-SW-089-AD; Amendment
39-19870; AD 2020-05-20]
RIN 2120-AA64
Airworthiness Directives; Airbus Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, and AS332L2
helicopters. This AD requires removing the drain plugs from the fuel
tank compartments located under the bottom structure. This AD was
prompted by the discovery that a modification to the fuel tank could
lead to fuel accumulating in an area containing electrical equipment
and subsequent ignition of fuel vapors. The actions of this AD are
intended to address an unsafe condition on these products.
DATES: This AD is effective April 24, 2020.
The Director of the Federal Register approved the incorporation by
reference of a certain document listed in this AD as of April 24, 2020.
ADDRESSES: For service information identified in this final rule,
contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX
75052; telephone 972-641-0000 or 800-232-0323; fax 972-641-3775; or at
https://www.airbus.com/helicopters/services/technical-support.html. You
may view this referenced service information at the FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkwy, Room 6N-321,
Fort Worth, TX 76177. It is also available on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0970.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov in Docket No.
[[Page 15925]]
FAA-2019-0970; 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 European Union Aviation Safety Agency (previously
European Aviation Safety Agency) (EASA) AD, any service information
that is incorporated by reference, any comments received, and other
information. The street 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: James Blyn, Aviation Safety Engineer,
Regulations and Policy Section, Rotorcraft Standards Branch, FAA, 10101
Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222-5110; email
[email protected].
SUPPLEMENTARY INFORMATION:
Discussion
On December 3, 2019, at 84 FR 66080, the Federal Register published
the FAA's notice of proposed rulemaking (NPRM), which proposed to amend
14 CFR part 39 by adding an AD that would apply to Airbus Helicopters
Model AS332C, AS332C1, AS332L, AS332L1, and AS332L2 helicopters, except
those with modification 0726383 installed. The NPRM proposed to require
removing drain plugs from the fuel tank compartments. The proposed
requirements were intended to prevent fuel accumulating in an area
containing electrical equipment and ignition of fuel vapors, which
could result in a fire and subsequent damage to the helicopter or
injury to the occupants.
The NPRM was prompted by EASA AD No. 2018-0209, dated September 21,
2018 (EASA AD 2018-0209), issued by EASA, which is the Technical Agent
for the Member States of the European Union, to correct an unsafe
condition for Airbus Helicopters (formerly Eurocopter, Eurocopter
France, Aerospatiale) Model AS332C, AS332C1, AS332L, AS332L1, and
AS332L2 helicopters, except those with modification 0726383. EASA
advises that during production of AS332 helicopters, closure of the
fuel tank drains with plugs was implemented. EASA states that this
closure disregards compliance with an airworthiness certification
requirement and in the event of fuel leakage in flight, a closed fuel
drain creates the risk of fuel accumulation and/or migration to an
adjacent area. EASA advises this area may contain electrical equipment
that could be susceptible to creating a source of ignition.
Accordingly, EASA AD 2018-0209 requires modification of the draining
system of the fuel tank compartments by removing the drain plugs from
the fuel tank compartments located under the bottom structure.
Comments
The FAA gave the public the opportunity to participate in
developing this AD, but the FAA did not receive any comments on the
NPRM.
FAA's Determination
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 of the
unsafe condition described in its AD. The FAA is issuing this AD after
evaluating all information provided by EASA and determining the unsafe
condition exists and is likely to exist or develop on other helicopters
of these same type designs and that air safety and the public interest
require adopting the AD requirements as proposed.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Airbus Helicopters Alert Service Bulletin (ASB)
No. AS332-53.01.62, Revision 1, dated May 28, 2019 (ASB AS332-53.01.62,
Revision 1), which specifies procedures for removing the drain plugs
from the fuel tank compartments located under the bottom structure of
the helicopter. This service information also specifies that the number
of drain plugs varies depending on the version of the helicopter.
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.
Other Related Service Information
The FAA also reviewed Airbus Helicopters ASB No. AS332-53.01.62,
Revision 0, dated June 7, 2018 (AS332-53.01.62, Revision 0). AS332-
53.01.62, Revision 0, contains the same procedures as AS332-53.01.62,
Revision 1. However, AS332-53.01.62, Revision 1, also addresses
military versions.
Costs of Compliance
The FAA estimates that this AD affects 11 helicopters of U.S.
Registry. The FAA estimates that operators may incur the following
costs in order to comply with this AD. Labor costs are estimated at $85
per work-hour.
Removing the 6 drain plugs installed on Model AS332C and AS332C1
helicopters takes about 2 work-hours for an estimated cost of $170 per
helicopter and $170 for the U.S. fleet size of 1 helicopter.
Removing the 7 drain plugs installed on Model AS332L, AS332L1, and
AS332L2 helicopters takes about 2 work-hours for an estimated cost of
$170 per helicopter and $1,700 for the U.S. fleet size of 10
helicopters.
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 helicopters 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.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
[[Page 15926]]
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 (AD):
2020-05-20 Airbus Helicopters: Amendment 39-19870; Docket No. FAA-
2019-0970; Product Identifier 2018-SW-089-AD.
(a) Applicability
This AD applies to Airbus Helicopters Model AS332C, AS332C1,
AS332L, AS332L1, and AS332L2 helicopters, certificated in any
category, except those with modification 0726383 installed.
(b) Unsafe Condition
This AD defines the unsafe condition as closure of fuel tank
drains. This condition could result in fuel accumulating in an area
containing electrical equipment and ignition of fuel vapors. This
condition could result in a fire and subsequent damage to the
helicopter or injury to the occupants.
(c) Effective Date
This AD becomes effective April 24, 2020.
(d) Compliance
You are responsible for performing each action required by this
AD within the specified compliance time unless it has already been
accomplished prior to that time.
(e) Required Actions
Within 110 hours time-in-service or during the next scheduled
maintenance, whichever occurs first:
(1) For Model AS332C and AS332C1 helicopters, remove the 6 fuel
tank drain plugs by following the Accomplishment Instructions,
paragraph 3.B.2. of Airbus Helicopters Alert Service Bulletin No.
AS332-53.01.62, Revision 1, dated May 28, 2019 (ASB AS332-53.01.62),
except you are not required to place the drain plugs in stock.
(2) For Model AS332L, AS332L1, and AS332L2 helicopters, remove
the 7 fuel tank drain plugs by following the Accomplishment
Instructions, paragraph 3.B.2. of ASB AS332-53.01.62, except you are
not required to place the drain plugs in stock.
(f) Credit for Previous Actions
Actions accomplished before the effective date of this AD in
accordance with the procedures specified in Airbus Helicopters Alert
Service Bulletin No. AS332-53.01.62, Revision 0, dated June 7, 2018,
are considered acceptable for compliance with the corresponding
actions specified in paragraph (e) of this AD.
(g) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Safety Management Section, Rotorcraft Standards
Branch, FAA, may approve AMOCs for this AD. Send your proposal to:
James Blyn, Aviation Safety Engineer, Regulations and Policy
Section, Rotorcraft Standards Branch, FAA, 10101 Hillwood Pkwy.,
Fort Worth, TX 76177; telephone 817-222-5110; email [email protected].
(2) For operations conducted under a 14 CFR part 119 operating
certificate or under 14 CFR part 91, subpart K, the FAA suggests
that you notify your principal inspector, or lacking a principal
inspector, the manager of the local flight standards district office
or certificate holding district office, before operating any
aircraft complying with this AD through an AMOC.
(h) Additional Information
(1) Airbus Helicopters Alert Service Bulletin No. AS332-
53.01.62, Revision 0, dated June 7, 2018, which is not incorporated
by reference, contains additional information about the subject of
this AD. For service information identified in this AD, contact
Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 75052;
telephone 972-641-0000 or 800-232-0323; fax 972-641-3775; or at
https://www.airbus.com/helicopters/services/technical-support.html.
You may view the referenced service information at the FAA, Office
of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy.,
Room 6N-321, Fort Worth, TX 76177.
(2) The subject of this AD is addressed in European Union
Aviation Safety Agency (previously European Aviation Safety Agency)
(EASA) AD No. 2018-0209, dated September 21, 2018. You may view the
EASA AD on the internet at https://www.regulations.gov in Docket No.
FAA-2019-0970.
(i) Subject
Joint Aircraft Service Component (JASC) Code: 2810, Fuel
Storage.
(j) 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 the AD specifies otherwise.
(i) Airbus Helicopters Alert Service Bulletin No. AS332-
53.01.62, Revision 1, dated May 28, 2019.
(ii) [Reserved]
(3) For service information identified in this AD, contact
Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 75052;
telephone 972-641-0000 or 800-232-0323; fax 972-641-3775; or at
https://www.airbus.com/helicopters/services/technical-support.html.
(4) You may view this service information at 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.
(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 11, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2020-05667 Filed 3-19-20; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T02:03:22.636394+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- f033ffa1fc79552ee70012e4287ced01ec365c8f787312c07c47661ecc13cc75
- Text SHA-256
- c8b56f5152889881df2a6f449a8bf18686ef8976f8ba0d17fa17aae72ca2f8cb
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.