This site displays a prototype of a “Web 2.0” version of the daily
Federal Register. It is not an official legal edition of the Federal
Register, and does not replace the official print version or the official
electronic version on GPO’s govinfo.gov.
The documents posted on this site are XML renditions of published Federal
Register documents. Each document posted on the site includes a link to the
corresponding official PDF file on govinfo.gov. This prototype edition of the
daily Federal Register on FederalRegister.gov will remain an unofficial
informational resource until the Administrative Committee of the Federal
Register (ACFR) issues a regulation granting it official legal status.
For complete information about, and access to, our official publications
and services, go to
About the Federal Register
on NARA's archives.gov.
The OFR/GPO partnership is committed to presenting accurate and reliable
regulatory information on FederalRegister.gov with the objective of
establishing the XML-based Federal Register as an ACFR-sanctioned
publication in the future. While every effort has been made to ensure that
the material on FederalRegister.gov is accurately displayed, consistent with
the official SGML-based PDF version on govinfo.gov, those relying on it for
legal research should verify their results against an official edition of
the Federal Register. Until the ACFR grants it official status, the XML
rendition of the daily Federal Register on FederalRegister.gov does not
provide legal notice to the public or judicial notice to the courts.
Rule
Enter a search term or FR citation e.g.
88 FR 38230 FR 78782024-13208USDA09/05/24RULE0503-AA39SORN
Choosing an item from
full text search results
will bring you to those results. Pressing enter in the search box
will also bring you to search results.
Choosing an item from
suggestions
will bring you directly to the content.
This table of contents is a navigational tool, processed from the
headings within the legal text of Federal Register documents.
This repetition of headings to form internal navigation links
has no substantive legal effect.
Document page views are updated periodically throughout the day and are
cumulative counts for this document. Counts are subject to sampling,
reprocessing and revision (up or down) throughout the day.
Page views
161
as of
08/16/2026 at 8:15 pm EDT
Other Formats
Enhanced Content - Other Formats
This document is also available in the following formats:
This PDF is FR Doc. 2021-03660 as it appeared on Public Inspection on
02/24/2021 at 8:45 am.
It was viewed
5
times while on Public Inspection.
If you are using public inspection listings for legal research, you
should verify the contents of the documents against a final, official
edition of the Federal Register. Only official editions of the
Federal Register provide legal notice of publication to the public and judicial notice
to the courts under 44 U.S.C. 1503 & 1507.
Learn more here.
Published Document: 2021-03660 (86 FR 11410)
This document has been published in the Federal Register. Use the PDF linked in the document sidebar for the official electronic format.
AGENCY:
Federal Aviation Administration (FAA), DOT.
ACTION:
Final rule.
SUMMARY:
The FAA is adopting a new airworthiness directive (AD) for certain Leonardo S.p.a. (Leonardo) Model AB139 and AW139 helicopters. This AD requires removing certain engine mounting rods from service and prohibits their installation on any helicopter. This AD was prompted by a report of non-conforming engine mounting rods. The actions of this AD are intended to address an unsafe condition on these products.
DATES:
This AD is effective April 1, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain document listed in this AD as of April 1, 2021.
( printed page 11411)
ADDRESSES:
For service information identified in this final rule, contact Leonardo S.p.a. Helicopters, Emanuele Bufano, Head of Airworthiness, Viale G.Agusta 520, 21017 C.Costa di Samarate (Va) Italy; telephone +39-0331-225074; fax +39-0331-229046; or at
https://www.leonardocompany.com/en/home.
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. It is also available on the internet at
https://www.regulations.gov
by searching for and locating Docket No. FAA-2020-0649.
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-2020-0649; 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 (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:
Kristi Bradley, Aviation Safety Engineer, General Aviation & Rotorcraft Section, International Validation Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222-5110; email
kristin.bradley@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to Leonardo Model AB139 and AW139 helicopters with certain serial-numbered engine mounting rods part number (P/N) 3G7120V00132. The NPRM published in the
Federal Register
on July 9, 2020 (85 FR 41219). The NPRM proposed to require removing the affected engine mounting rods from service and proposed to prohibit installing an affected engine mounting rod on any helicopter. The proposed requirements were intended to prevent failure of an affected engine mounting rod, which could possibly result in loss of control of the helicopter.
The NPRM was prompted by EASA AD No. 2019-0149, dated June 24, 2019, issued by EASA, which is the Technical Agent for the Member States of the European Union, to correct an unsafe condition for Leonardo S.p.a. (formerly Finmeccanica S.p.A., AgustaWestland S.p.A., Agusta S.p.A.; and AgustaWestland Philadelphia Corporation, formerly Agusta Aerospace Corporation) Model AB139 and AW139 helicopters with certain serial numbered engine mounting rods P/N 3G7120V00132 installed. EASA advises of reports of a production non-conformity on a specific batch of these engine mounting rods. EASA further advises that this non-conformity degrades the material strength of the engine mounting rods.
EASA states this condition, if not corrected, could lead to failure of an affected engine mounting rod, possibly resulting in loss of control of the helicopter. Accordingly, the EASA AD requires removing from service each affected engine mounting rod, emailing a completed “Scrap Report” to Leonardo Helicopters Division, and installing a serviceable engine mounting rod. The EASA AD also prohibits installing an affected engine mounting rod on any helicopter.
Comments
The FAA gave the public the opportunity to participate in developing this final rule, but the FAA did not receive any comments on the NPRM or on the determination of the cost to the public.
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 of the information provided by EASA and determining the unsafe condition exists and is likely to exist or develop on other helicopters of the same type designs and that air safety and the public interest require adopting the AD requirements as proposed.
Differences Between This AD and the EASA AD
The EASA AD requires emailing a completed “Scrap Report” to Leonardo Helicopters Division at the same compliance time as the engine mounting rod removal, whereas this AD does not.
The FAA reviewed Leonardo Helicopters Alert Service Bulletin (ASB) No. 139-593, Revision A, dated June 14, 2019 (ASB 139-593, Revision A), which specifies procedures to replace the engine outboard and inboard mounting rods from the Number 1 and Number 2 engines.
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 reviewed Leonardo Helicopters ASB No. 139-593, dated June 11, 2019. This service information contains the same procedures as ASB 139-593, Revision A. However, ASB 139-593, Revision A expands the applicability from certain serial-numbered Model AB139 and AW139 helicopters to all Model AB139 and AW139 helicopters with affected engine mounting rods installed.
The FAA also reviewed Leonardo Helicopters AMP DM 39-A-71-21-05-00A-520A-B, AMP DM 39-A-71-21-05-00A-720A-B, AMP DM 39-A-71-21-06-00A-520A-B, AMP DM 39-A-71-21-06-00A-720A-B, AMP DM 39-A-71-21-07-00A-520A-B, AMP DM 39-A-71-21-07-00A-720A-B, AMP DM 39-A-71-21-08-00A-520A-B, and AMP DM 39-A-71-21-08-00A-720A-B, all dated October 4, 2019. This service information specifies instructions for removing and installing the outboard and inboard engine mounting rods.
Costs of Compliance
The FAA estimates that this AD affects up to 126 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.
Replacing an engine mounting rod requires about 8 work-hours and parts cost about $1,000 for an estimated cost of $1,680 per engine mounting rod.
According to Leonardo Helicopter's service information, some of the costs of this AD may be covered under warranty, thereby reducing the cost impact on affected individuals. The FAA does not control warranty coverage by Leonardo Helicopters. Accordingly, all costs are included in this cost estimate.
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.
( printed page 11412)
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:
(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.
This airworthiness directive (AD) applies to Leonardo S.p.a. Model AB139 and AW139 helicopters, certificated in any category, with an engine mounting rod part number (P/N) 3G7120V00132 with a serial number (S/N) listed in Figures 2 or 3 of Leonardo Helicopters Alert Service Bulletin No. 139-593, Revision A, dated June 14, 2019 (ASB 139-593), installed.
(b) Unsafe Condition
This AD defines the unsafe condition as a non-conforming engine mounting rod. This condition could result in structural failure of the engine mounting rod and subsequent loss of control of the helicopter.
(c) Effective Date
This AD becomes effective April 1, 2021.
(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
(1) Before further flight, determine the total hours time-in-service (TIS) of each engine mounting rod.
(2) Before reaching 225 total hours TIS or within 25 hours TIS, whichever occurs later, with the battery and any other electrical power supply disconnected, remove from service the engine mounting rod as follows:
(i) For the Number 1 engine outboard mounting rod, remove from service the Number 1 engine outboard mounting rod and install an airworthy Number 1 engine outboard mounting rod as shown in Detail “B” of Figure 1 of ASB 139-593 and by following the Accomplishment Instructions, paragraphs 3.1 and 3.2 of ASB 139-593, except you are not required to discard the Number 1 engine outboard mounting rod or comply with the “Scrap Report” instruction in paragraph 3.1 of ASB 139-593.
Note 1 to paragraphs (e)(2)(i) through (iv):
Figure 1 of ASB 139-593 shows the engine outboard and inboard mounting rod assemblies for the left-hand side only, the right-hand side is symmetrical.
(ii) For the Number 1 engine inboard mounting rod, remove from service the Number 1 engine inboard mounting rod and install an airworthy Number 1 engine inboard mounting rod as shown in Detail “C” of Figure 1 of ASB 139-593 and by following the Accomplishment Instructions, paragraphs 3.3 and 3.4 of ASB 139-593, except you are not required to discard the Number 1 engine inboard mounting rod or comply with the “Scrap Report” instruction in paragraph 3.3 of ASB 139-593.
(iii) For the Number 2 engine outboard mounting rod, remove from service the Number 2 engine outboard mounting rod and install an airworthy Number 2 engine outboard mounting rod as shown in Detail “B” of Figure 1 of ASB 139-593 and by following the Accomplishment instructions, paragraphs 4.1 and 4.2 of ASB 139-593, except you are not required to discard the Number 2 engine outboard mounting rod or comply with the “Scrap Report” instruction in paragraph 4.1 of ASB 139-593.
(iv) For the Number 2 engine inboard mounting rod, remove from service the Number 2 engine inboard mounting rod and install an airworthy Number 2 engine inboard mounting rod as shown in Detail “C” of Figure 1 of ASB 139-593 and by following the Accomplishment instructions, paragraphs 4.3 and 4.4 of ASB 139-593, except you are not required to discard the Number 2 engine inboard mounting rod or comply with the “Scrap Report” instruction in paragraph 4.3 of ASB 139-593.
(3) As of the effective date of this AD, do not install on any helicopter an engine mounting rod with a P/N and S/N listed in paragraph (a) of this AD.
(f) Credit for Previous Actions
Actions accomplished before the effective date of this AD in accordance with the procedures specified in Leonardo Helicopters Alert Service Bulletin No. 139-593, dated June 11, 2019, are considered acceptable for compliance with the corresponding actions specified in paragraphs (e)(1) and (2) of this AD.
(g) Alternative Methods of Compliance (AMOCs)
(1) The Manager, International Validation Branch, FAA, may approve AMOCs for this AD. Send your proposal to: Kristi Bradley, Aviation Safety Engineer, General Aviation & Rotorcraft Section, International Validation Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222-5110; email
9-AVS-AIR-730-AMOC@faa.gov.
(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) Leonardo Helicopters Alert Service Bulletin No. 139-593, dated June 11, 2019, and Leonardo Helicopters AMP DM 39-A-71-21-05-00A-520A-B, AMP DM 39-A-71-21-05-00A-720A-B, AMP DM 39-A-71-21-06-00A-520A-B, AMP DM 39-A-71-21-06-00A-720A-B, AMP DM 39-A-71-21-07-00A-520A-B, AMP DM 39-A-71-21-07-00A-720A-B, AMP DM 39-A-71-21-08-00A-520A-B, and AMP DM 39-A-71-21-08-00A-720A-B, all dated October 4, 2019, which are not incorporated by reference, contain additional information about the subject of this AD. For service information identified in this AD, contact Leonardo S.p.a. Helicopters, Emanuele Bufano, Head of Airworthiness, Viale G.Agusta 520, 21017 C.Costa di Samarate (Va) Italy; telephone +39-0331-225074; fax +39-0331-229046; or at
https://www.leonardocompany.com/en/home. You may view a copy of the 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 (EASA) AD No. 2019-0149, dated June 24, 2019. You may view the EASA AD on the internet at
https://www.regulations.gov
in Docket No. FAA-2020-0649.
( printed page 11413)
(i) Subject
Joint Aircraft Service Component (JASC) Code: 7120, Engine Mount Section.
(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) Leonardo Helicopters Alert Service Bulletin No. 139-593, Revision A, dated June 14, 2019.
(ii) [Reserved]
(3) For service information identified in this AD, contact Leonardo S.p.a. Helicopters, Emanuele Bufano, Head of Airworthiness, Viale G.Agusta 520, 21017 C.Costa di Samarate (Va) Italy; telephone +39-0331-225074; fax +39-0331-229046; or at
https://www.leonardocompany.com/en/home.
(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.