Published 2022-04-06 · Federal Register document 2022-07174
Airworthiness Directives; Airbus Helicopters
Publication summary
The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model AS33L2 and EC225LP helicopters. This AD was prompted by a discrepancy in the rotorcraft flight manual (RFM) where the rotorcraft stay-up flying capabilities for Category B operation were provided through performance data only, not as airworthiness limitations that are dependent upon on the number of passengers on board. This AD requires revising the existing RFM for your helicopter, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:11.345539+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2022-c0cc5a172b1306fa
- Source row
- results[129]
- Raw source SHA-256
- c0cc5a172b1306fa2cd8dc66863122ada13332e685d87687bd0becf2dab37a5e
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2022-07-09
- Effective date printed in this edition
- 2022-05-11
Read 12 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective May 11, 2022.
Exact source excerpt. Text positions 9318–9404, end exclusive, in the original decoded publication. SHA-256: 78c5b18fc6eeeece60d5f784278ad7133be7c6562e10b8a2cbfc61183c4a7287
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 9404–9433, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to all Airbus Helicopters Model AS332L2 and
EC225LP helicopters, certificated in any category.
Exact source excerpt. Text positions 9433–9569, end exclusive, in the original decoded publication. SHA-256: 489988c1ebe8da1d7e9f494919f39937c5b20423ea8b7cb30801668126bf9bd7
Subject
(d) Subject
Joint Aircraft Service Component (JASC) Code: 7600, Engine
Controls.
Exact source excerpt. Text positions 9569–9657, end exclusive, in the original decoded publication. SHA-256: 79b36ff18ca7e31f11ae8e2e28b74d3a0eca20fcd430405b58d875b9a5f60b2f
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by a discrepancy in the rotorcraft flight
manual (RFM) where the rotorcraft stay-up flying capabilities for
Category B operation were provided through performance data only,
not as airworthiness limitations that are dependent upon the number
of passengers on board. The FAA is issuing this AD to address this
discrepancy in the RFM, which, if not addressed, could lead to
incorrect determination of the stay-up flying capabilities of the
helicopter, resulting in reduced control of the helicopter.
Exact source excerpt. Text positions 9657–10210, end exclusive, in the original decoded publication. SHA-256: ab0fc2f2342c95067ba87ebeac6b9b5d61d39ec4ea253c386a6f79a5f9b9c122
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 10210–10312, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Requirements
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, European Union Aviation Safety Agency (EASA) AD
2021-0174, dated July 21, 2021 (EASA AD 2021-0174).
Exact source excerpt. Text positions 10312–10579, end exclusive, in the original decoded publication. SHA-256: 43a3de761b30407b39a2a7e459a7b7705b99a745e4d5c0d4c9f086997fcdd49c
Exceptions to EASA AD 2021-0174
(h) Exceptions to EASA AD 2021-0174
(1) Where EASA AD 2021-0174 refers to its effective date, this
AD requires using the effective date of this AD.
(2) Where paragraph (1) of EASA AD 2021-0174 specifies to
``inform all flight crew and, thereafter, operate the helicopter
accordingly,'' this AD does not require those actions.
(3) This AD does not mandate compliance with the ``Remarks''
section of EASA AD 2021-0174.
(4) Where paragraph (2) of EASA AD 2021-0174 specifies an
acceptable compliance method, replace the text ``which includes
information of equal effect to that presented'' with ``which
includes information identical to that presented.''
(5) The action required by paragraphs (1) and (2) of EASA AD
2021-0174 may be performed by the owner/operator (pilot) holding at
least a private pilot certificate and must be entered into the
aircraft records showing compliance with this AD in accordance with
14 CFR 43.9(a)(1) through (4) and 14 CFR 91.417(a)(2)(v). The record
must be maintained as required by 14 CFR 91.417 or 135.439.
Exact source excerpt. Text positions 10579–11654, end exclusive, in the original decoded publication. SHA-256: c11d897130a704f0ebd7719bfbc6196e97d32140beeecf42fa90a86875ca24b5
Special Flight Permit
(i) Special Flight Permit
Special flight permits may be permitted provided that there are
no passengers on board.
Exact source excerpt. Text positions 11654–11775, end exclusive, in the original decoded publication. SHA-256: a50746cbb02d92205a9b096fbca8f8da8b0edfd1da2a349fe623790aae086d9e
Alternative Methods of Compliance (AMOCs)
(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: [email protected].
[[Page 19793]]
(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.
Exact source excerpt. Text positions 11775–12582, end exclusive, in the original decoded publication. SHA-256: 405bf631abf8038fa03df403a761f60dbf63807f1f2163045b2f0b06c2a6fd24
Related Information
(k) Related Information
For more information about this AD, contact Andrea Jimenez,
Aerospace Engineer, COS Program Management Section, Operational
Safety Branch, Compliance & Airworthiness Division, FAA, 1600
Stewart Ave., Suite 410, Westbury, NY 11590; telephone (516) 228-
7330; email [email protected].
Exact source excerpt. Text positions 12582–12898, end exclusive, in the original decoded publication. SHA-256: 604b30e187f0ed4461a4c32e72ab8bd581fe31156e721b9af6d7bd9945f11a22
Material Incorporated by Reference
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) AD 2021-0174,
dated July 21, 2021.
(ii) [Reserved]
(3) For EASA AD 2021-0174, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
[email protected]; internet www.easa.europa.eu. You may find the
EASA material 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 at https://www.regulations.gov by searching
for and locating Docket No. FAA-2022-0018.
(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
[email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 12898–14305, end exclusive, in the original decoded publication. SHA-256: ffc77c2d1c1e7f2008509553ac9ccaf613f97f181c3816706ed5d472b2f78fa4
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 2022-07-09 · 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: 7a88d447c921b9674b658bc758d77321c3ed1c31e6fdebdb95f266ec1a188c56. Source manifest: f61a028c0c47c1c124b37d143b4eb2d80406139a8561a00f1de42926ad556327.
Official source · 2022-04-06
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 87, Number 66 (Wednesday, April 6, 2022)]
[Rules and Regulations]
[Pages 19791-19793]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-07174]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0018; Project Identifier MCAI-2021-00853-R;
Amendment 39-21997; AD 2022-07-09]
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 all
Airbus Helicopters Model AS33L2 and EC225LP helicopters. This AD was
prompted by a discrepancy in the rotorcraft flight manual (RFM) where
the rotorcraft stay-up flying capabilities for Category B operation
were provided through performance data only, not as airworthiness
limitations that are dependent upon on the number of passengers on
board. This AD requires revising the existing RFM for your helicopter,
as specified in a European Union Aviation Safety Agency (EASA) AD,
which is incorporated by reference. The FAA is issuing this AD to
address the unsafe condition on these products.
DATES: This AD is effective May 11, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of May 11,
2022.
ADDRESSES: For EASA material incorporated by reference (IBR) in this
final rule, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne,
Germany; telephone +49 221 8999 000; email [email protected]; internet
www.easa.europa. You may find the EASA 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 at https://www.regulations.gov by searching for and
locating Docket No. FAA-2022-0018.
Examining the AD Docket
You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2022-0018; or in person at
Docket Operations between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The AD docket contains this final rule, the
EASA AD, any comments received, and other information. The address for
Docket Operations is U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Andrea Jimenez, Aerospace Engineer,
COS Program Management Section, Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY
11590; telephone (516) 228-7330; email [email protected].
SUPPLEMENTARY INFORMATION:
Background
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2021-0174, dated July 21, 2021 (EASA
AD 2021-0174), to correct an unsafe condition for Airbus Helicopters,
formerly Eurocopter, Eurocopter France, and Aerospatiale, Model AS 332
L2 and EC 225 LP 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 AS332L2 and EC225LP helicopters. The NPRM published in the
Federal Register on January 31, 2022 (87 FR 4820). The NPRM was
prompted by a discrepancy in the RFM where the rotorcraft stay-up
flying capabilities for Category B operation were provided through
performance data only, not as airworthiness limitations that are
dependent upon on the number of passengers on board. The NPRM proposed
to require revising the existing RFM for your helicopter, as specified
in EASA AD 2021-0174.
The FAA is issuing this AD to address this discrepancy in the RFM,
which, if not addressed, could lead to incorrect determination of the
stay-up flying capabilities of the helicopter, resulting in reduced
control of the helicopter. See EASA AD 2021-0174 for additional
background information.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the costs.
Conclusion
These helicopters have been approved by EASA and are approved for
operation in the United States. Pursuant to the FAA's bilateral
agreement with the European Union, EASA has notified the FAA about the
unsafe condition described in its AD. The FAA reviewed the relevant
data and determined that air safety requires adopting this AD as
proposed. Accordingly, the FAA is issuing this AD to address the unsafe
condition on these helicopters. Except for minor editorial changes,
this AD is adopted as proposed in the NPRM.
Related Service Information Under 1 CFR Part 51
EASA AD 2021-0174 requires amending (revising) the Limitation
Section of the applicable RFM by incorporating new weight limitations
that are dependent upon the number of passengers on board.
This material is reasonably available because the interested
parties have access to it through their normal course
[[Page 19792]]
of business or by the means identified in the ADDRESSES section.
Differences Between This AD and the EASA AD
EASA AD 2021-0174 requires operators to ``inform all flight crew''
of revisions to the RFM and, thereafter, to ``operate the helicopter
accordingly.'' However, this AD does not specifically require those
actions.
14 CFR 91.9 requires that no person may operate a civil aircraft
without complying with the operating limitations specified in the RFM.
Therefore, including a requirement in this AD to operate the helicopter
according to the revised RFM would be redundant and unnecessary.
Further, compliance with such a requirement in an AD would be
impracticable to demonstrate or track on an ongoing basis; therefore, a
requirement to operate the helicopter in such a manner would be
unenforceable.
This AD allows the owner/operator (pilot) holding at least a
private pilot certificate to revise the existing RFM for your
helicopter and do the logbook entry, whereas EASA AD 2021-0174 does not
specify this. This AD requires these actions to be entered into the
aircraft records showing compliance with this AD in accordance with 14
CFR 43.9(a)(1) through (4) and 14 CFR 91.417(a)(2)(v), and the record
to be maintained as required by 14 CFR 91.417 or 135.439.
Costs of Compliance
The FAA estimates that this AD affects 38 helicopters of U.S.
Registry. Labor rates are estimated at $85 per work-hour. Based on
these numbers, the FAA estimates the following costs to comply with
this AD.
Revising the existing RFM for your helicopter takes about 0.50
work-hour for an estimated cost of $42.50 per helicopter and $1,615 for
the U.S. fleet.
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:
2022-07-09 Airbus Helicopters: Amendment 39-21997; Docket No. FAA-
2022-0018; Project Identifier MCAI-2021-00853-R.
(a) Effective Date
This airworthiness directive (AD) is effective May 11, 2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Airbus Helicopters Model AS332L2 and
EC225LP helicopters, certificated in any category.
(d) Subject
Joint Aircraft Service Component (JASC) Code: 7600, Engine
Controls.
(e) Unsafe Condition
This AD was prompted by a discrepancy in the rotorcraft flight
manual (RFM) where the rotorcraft stay-up flying capabilities for
Category B operation were provided through performance data only,
not as airworthiness limitations that are dependent upon the number
of passengers on board. The FAA is issuing this AD to address this
discrepancy in the RFM, which, if not addressed, could lead to
incorrect determination of the stay-up flying capabilities of the
helicopter, resulting in reduced 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 Union Aviation Safety Agency (EASA) AD
2021-0174, dated July 21, 2021 (EASA AD 2021-0174).
(h) Exceptions to EASA AD 2021-0174
(1) Where EASA AD 2021-0174 refers to its effective date, this
AD requires using the effective date of this AD.
(2) Where paragraph (1) of EASA AD 2021-0174 specifies to
``inform all flight crew and, thereafter, operate the helicopter
accordingly,'' this AD does not require those actions.
(3) This AD does not mandate compliance with the ``Remarks''
section of EASA AD 2021-0174.
(4) Where paragraph (2) of EASA AD 2021-0174 specifies an
acceptable compliance method, replace the text ``which includes
information of equal effect to that presented'' with ``which
includes information identical to that presented.''
(5) The action required by paragraphs (1) and (2) of EASA AD
2021-0174 may be performed by the owner/operator (pilot) holding at
least a private pilot certificate and must be entered into the
aircraft records showing compliance with this AD in accordance with
14 CFR 43.9(a)(1) through (4) and 14 CFR 91.417(a)(2)(v). The record
must be maintained as required by 14 CFR 91.417 or 135.439.
(i) Special Flight Permit
Special flight permits may be permitted provided that there are
no passengers on board.
(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: [email protected].
[[Page 19793]]
(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 Andrea Jimenez,
Aerospace Engineer, COS Program Management Section, Operational
Safety Branch, Compliance & Airworthiness Division, FAA, 1600
Stewart Ave., Suite 410, Westbury, NY 11590; telephone (516) 228-
7330; email [email protected].
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) AD 2021-0174,
dated July 21, 2021.
(ii) [Reserved]
(3) For EASA AD 2021-0174, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
[email protected]; internet www.easa.europa.eu. You may find the
EASA material 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 at https://www.regulations.gov by searching
for and locating Docket No. FAA-2022-0018.
(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
[email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on March 31, 2022.
Derek Morgan,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-07174 Filed 4-5-22; 8:45 am]
BILLING CODE 4910-13-P
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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.
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