Published 2015-02-10 · Federal Register document 2015-01809
Airworthiness Directives; Agusta S.p.A. (Type Certificate Currently Held by AgustaWestland S.p.A.) (Agusta) Helicopters
Publication summary
We are adopting a new airworthiness directive (AD) for Agusta AB139 and AW139 helicopters to require replacing certain single-braided flexible hydraulic hoses with double-braided flexible hydraulic hoses. This AD was prompted by occurrences of leaking flexible hydraulic hoses. The actions of this AD are intended to prevent loss of hydraulic power and subsequent loss of helicopter control.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:48.517946+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2015-3bb842c840a7e6e6
- Source row
- results[44]
- Raw source SHA-256
- 3bb842c840a7e6e6e43779ca68008e1e63ad8287ad840c3a981d1f66a934b14b
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2015-02-21
- Effective date printed in this edition
- 2015-03-17
Some source clauses remain unstructured. Read the complete publication for conditions that have not been interpreted here.
Read 9 complete recorded clauses
Applicability wording · Applicability
(a) Applicability
This AD applies to Agusta Model AB139 and AW139 helicopters with
a flexible hydraulic hose, part number (P/N) A494AE2E00E0670X,
A494AE3E00E0424X, A494AE3E00E0530X, A494AE3E00E0570X,
A494AE3E00E0580X, A494AE3E00E0620X, A494AE3E00E0930X,
A494AE6E14E0348X, or A494AE6E21E0330X, installed, certificated in
any category.
Exact source excerpt. Text positions 9267–9612, end exclusive, in the original decoded publication. SHA-256: e5a01b1c6a7173800a950ed80192248ddfd46d0f53740c20ac241eb19d8f148d
Unsafe Condition
(b) Unsafe Condition
This AD defines the unsafe condition as a leak in a hydraulic
system flexible hose. This condition could result in loss of
hydraulic power and subsequent loss of helicopter control.
Exact source excerpt. Text positions 9612–9823, end exclusive, in the original decoded publication. SHA-256: 45d8237e59702a65e89816b2b9a3797cbf11104c078192c4fe8474e5bb5cea13
Effective Date
(c) Effective Date
This AD becomes effective March 17, 2015.
Exact source excerpt. Text positions 9823–9890, end exclusive, in the original decoded publication. SHA-256: 7f01e5b2e31ef398ec89dada46412002e47e9c0bbebb2f4a0b66ed5d12104cf0
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 9890–10077, end exclusive, in the original decoded publication. SHA-256: 56042b53a75a0db2af067b711f9b82d8091413842e43863752e31aeffdd54a72
Required Actions
(e) Required Actions
(1) Within 300 hours time-in-service, replace each flexible
hydraulic hose with a double braided flexible hydraulic hose in
accordance with the Compliance Instructions, Part I, paragraphs 5
through 7; Part II, paragraphs 5 through 7; Part III, paragraphs 5
through 6; Part IV, paragraphs 5 through 6; and Part V, paragraphs 5
through 7; as applicable for your helicopter serial number and
configuration, of AgustaWestland Bolletino Tecnico No. 139-307,
dated June 19, 2013.
(2) Do not install a flexible hydraulic hose, P/N
A494AE2E00E0670X, A494AE3E00E0424X, A494AE3E00E0530X,
A494AE3E00E0570X, A494AE3E00E0580X, A494AE3E00E0620X,
A494AE3E00E0930X, A494AE6E14E0348X, or A494AE6E21E0330X, on any
helicopter.
Exact source excerpt. Text positions 10077–10827, end exclusive, in the original decoded publication. SHA-256: a5dfc2caf1a67c372ba6d3b77970c3658f2a24f2ad59e9a3e06f22da4c6da626
Alternative Methods of Compliance (AMOCs)
(f) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Safety Management Group, FAA, may approve AMOCs
for this AD. Send your proposal to: Matt Wilbanks, Aviation Safety
Engineer, Regulations and Policy Group, Rotorcraft Directorate, FAA,
2601 Meacham Blvd., Fort Worth, Texas 76137; 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, we suggest that you
notify your principal inspector, or
[[Page 7302]]
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 10827–11571, end exclusive, in the original decoded publication. SHA-256: 0cfc9aeb3f37c35d4ceda3e6d2ac3ea5016e31ab16f63d0da758bcec762fe44e
Additional Information
(g) Additional Information
The subject of this AD is addressed in European Aviation Safety
Agency (EASA) AD No. 2013-0177, dated August 8, 2013. You may view
the EASA AD on the Internet at http://www.regulations.gov in Docket
No. FAA-2014-0465.
Exact source excerpt. Text positions 11571–11825, end exclusive, in the original decoded publication. SHA-256: f2c2b6d7be635810675ff52c0bfddbb0930005ebdc9e1ed1818e7cefc7a755cb
Subject
(h) Subject
Joint Aircraft Service Component (JASC) Code: 2910, Hydraulic
System, Main.
Exact source excerpt. Text positions 11825–11920, end exclusive, in the original decoded publication. SHA-256: d8dfaeed14575069b62ecddfbb8a793924b858468a696c34997c61242c377867
Material Incorporated by Reference
(i) 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) AgustaWestland Bolletino Tecnico No. 139-307, dated June 19,
2013.
(ii) Reserved.
(3) For Agusta service information identified in this AD,
contact Agusta Westland, Customer Support & Services, Via Per
Tornavento 15, 21019 Somma Lombardo (VA) Italy, ATTN: Giovanni
Cecchelli; telephone 39- 0331-711133; fax 39 0331 711180; or at
http://www.agustawestland.com/technical-bullettins.
(4) You may view this service information at FAA, Office of the
Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663,
Fort Worth, Texas 76137. 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, call (202) 741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 11920–13227, end exclusive, in the original decoded publication. SHA-256: 122ddf650c0058aa346714684f049af53c44e9f36181ff88f0efed2b0cd9a1a7
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 2015-02-21 · 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: 54085faa1e02a43dff01269637296706f9a727d96c41b183ee9de74aa71670bd. Source manifest: ea11a7ab3dca54e63d0a5f28611621969c68e72e3b9852edac01b8a4aa5c57d1.
Official source · 2015-02-10
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 80, Number 27 (Tuesday, February 10, 2015)]
[Rules and Regulations]
[Pages 7300-7302]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-01809]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2014-0465; Directorate Identifier 2013-SW-044-AD;
Amendment 39-18089; AD 2015-02-21]
RIN 2120-AA64
Airworthiness Directives; Agusta S.p.A. (Type Certificate
Currently Held by AgustaWestland S.p.A.) (Agusta) Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for Agusta
AB139 and AW139 helicopters to require replacing certain single-braided
flexible hydraulic hoses with double-braided flexible hydraulic hoses.
This AD was prompted by occurrences of leaking flexible hydraulic
hoses. The actions of this AD are intended to prevent loss of hydraulic
power and subsequent loss of helicopter control.
DATES: This AD is effective March 17, 2015.
The Director of the Federal Register approved the incorporation by
reference of a certain document listed in this AD as of March 17, 2015.
ADDRESSES: For service information identified in this AD, contact
Agusta Westland, Customer Support & Services, Via Per Tornavento 15,
21019 Somma Lombardo (VA) Italy, ATTN: Giovanni Cecchelli; telephone
39- 0331-711133; fax 39 0331 711180; or at http://www.agustawestland.com/technical-bullettins. You may review the
referenced service information at the FAA, Office of the Regional
Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth,
Texas 76137. It is also available on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014-
0465.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov 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, the European Aviation Safety
Agency (EASA) AD, any incorporated-by-reference service information,
the economic evaluation, any comments received, and other information.
The street address for the Docket Operations Office (phone: 800-647-
5527) is U.S. Department of Transportation, Docket Operations Office,
M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue
SE., Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Matt Wilbanks, Aviation Safety
Engineer, Regulations and Policy Group, Rotorcraft Directorate, FAA,
2601 Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222-5110;
email [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
On July 16, 2014, at 79 FR 41464, the Federal Register published
our notice of proposed rulemaking (NPRM), which proposed to amend 14
CFR part 39 by adding an AD that would apply to Agusta Model AB139 and
AW139 helicopters with a flexible hydraulic hose, part number (P/N)
A494AE2E00E0670X, A494AE3E00E0424X, A494AE3E00E0530X, A494AE3E00E0570X,
A494AE3E00E0580X, A494AE3E00E0620X, A494AE3E00E0930X, A494AE6E14E0348X,
or A494AE6E21E0330X, installed. The NPRM proposed to require replacing
these single-braided flexible hydraulic hoses with double-braided
flexible hydraulic hoses. The proposed requirements were intended to
prevent loss of hydraulic power and subsequent loss of helicopter
control.
The NPRM was prompted by AD No. AD No. 2013-0177, dated August 8,
2013, issued by EASA, which is the Technical Agent for the Member
States of the European Union, to correct an unsafe condition for Agusta
Model AB139 and AW139 helicopters. EASA advises that leaking hydraulic
system flexible hoses have been reported on in-service helicopters. An
investigation indicated that single braided flexible hydraulic hoses,
which are part of the original design for Model AB139 and AW139
helicopters, may not be strong enough to cope with the hydraulic system
pressure over long periods. If not corrected, this condition could lead
to other hydraulic system leaks, possibly resulting in loss of
hydraulic power and reduced control of the helicopter, EASA
[[Page 7301]]
advises. EASA consequently requires that the flexible single-braided
hydraulic hoses be replaced with flexible double-braided hydraulic
hoses.
Comments
We gave the public the opportunity to participate in developing
this AD, but we received no comments on the NPRM (79 FR 41464, July 16,
2014).
FAA's Determination
These helicopters have been approved by the aviation authority of
Italy and are approved for operation in the United States. Pursuant to
our bilateral agreement with Italy, EASA, its technical representative,
has notified us of the unsafe condition described in the EASA AD. We
are issuing this AD because we evaluated all information provided by
EASA and determined 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.
Differences Between This AD and the EASA AD
The EASA AD requires replacing the flexible single-braided
hydraulic hoses within 300 flight hours or 6 months, whichever occurs
first. This AD requires that the flexible single-braided hydraulic
hoses be replaced within 300 hours time-in-service (TIS). TIS and
flight hours are synonymous.
Related Service Information Under 1 CFR Part 51
AgustaWestland Bolletino Tecnico No. 139-307, dated June 19, 2013
(BT), calls for replacing certain single braided flexible hydraulic
hoses with double braided flexible hydraulic hoses for Model AB139 and
AW139 helicopters. The BT states that the replacement should be
conducted within 300 flight hours or six months from receipt of the BT,
whichever comes first, to prevent in-service leaks. This service
information is reasonably available; see ADDRESSES for ways to access
this service information.
Costs of Compliance
We estimate that this AD affects 115 helicopters of U.S. Registry
and that labor costs average $85 per work-hour. Based on these
estimates, we expect that replacing the flexible single-braided
hydraulic hoses with flexible double-braided hydraulic flexible hoses
will require 6 work-hours for a labor cost of $510. Parts cost $3,089
for a total cost of $3,599 per helicopter, and $413,885 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.
We are 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) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979);
(3) Will not affect intrastate aviation in Alaska to the extent
that it justifies making a regulatory distinction; and
(4) 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.
We prepared an economic evaluation of the estimated costs to comply
with this AD and placed it in the AD docket.
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 (AD):
2015-02-21 Agusta S.p.A. (Type certificate currently held by
AgustaWestland S.p.A.) (Agusta) Helicopters: Amendment 39-18089;
Docket No. FAA-2014-0465; Directorate Identifier 2013-SW-044-AD.
(a) Applicability
This AD applies to Agusta Model AB139 and AW139 helicopters with
a flexible hydraulic hose, part number (P/N) A494AE2E00E0670X,
A494AE3E00E0424X, A494AE3E00E0530X, A494AE3E00E0570X,
A494AE3E00E0580X, A494AE3E00E0620X, A494AE3E00E0930X,
A494AE6E14E0348X, or A494AE6E21E0330X, installed, certificated in
any category.
(b) Unsafe Condition
This AD defines the unsafe condition as a leak in a hydraulic
system flexible hose. This condition could result in loss of
hydraulic power and subsequent loss of helicopter control.
(c) Effective Date
This AD becomes effective March 17, 2015.
(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) Within 300 hours time-in-service, replace each flexible
hydraulic hose with a double braided flexible hydraulic hose in
accordance with the Compliance Instructions, Part I, paragraphs 5
through 7; Part II, paragraphs 5 through 7; Part III, paragraphs 5
through 6; Part IV, paragraphs 5 through 6; and Part V, paragraphs 5
through 7; as applicable for your helicopter serial number and
configuration, of AgustaWestland Bolletino Tecnico No. 139-307,
dated June 19, 2013.
(2) Do not install a flexible hydraulic hose, P/N
A494AE2E00E0670X, A494AE3E00E0424X, A494AE3E00E0530X,
A494AE3E00E0570X, A494AE3E00E0580X, A494AE3E00E0620X,
A494AE3E00E0930X, A494AE6E14E0348X, or A494AE6E21E0330X, on any
helicopter.
(f) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Safety Management Group, FAA, may approve AMOCs
for this AD. Send your proposal to: Matt Wilbanks, Aviation Safety
Engineer, Regulations and Policy Group, Rotorcraft Directorate, FAA,
2601 Meacham Blvd., Fort Worth, Texas 76137; 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, we suggest that you
notify your principal inspector, or
[[Page 7302]]
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.
(g) Additional Information
The subject of this AD is addressed in European Aviation Safety
Agency (EASA) AD No. 2013-0177, dated August 8, 2013. You may view
the EASA AD on the Internet at http://www.regulations.gov in Docket
No. FAA-2014-0465.
(h) Subject
Joint Aircraft Service Component (JASC) Code: 2910, Hydraulic
System, Main.
(i) 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) AgustaWestland Bolletino Tecnico No. 139-307, dated June 19,
2013.
(ii) Reserved.
(3) For Agusta service information identified in this AD,
contact Agusta Westland, Customer Support & Services, Via Per
Tornavento 15, 21019 Somma Lombardo (VA) Italy, ATTN: Giovanni
Cecchelli; telephone 39- 0331-711133; fax 39 0331 711180; or at
http://www.agustawestland.com/technical-bullettins.
(4) You may view this service information at FAA, Office of the
Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663,
Fort Worth, Texas 76137. 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, call (202) 741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Fort Worth, Texas, on January 16, 2015.
Lance T. Gant,
Acting Directorate Manager, Rotorcraft Directorate, Aircraft
Certification Service.
[FR Doc. 2015-01809 Filed 2-9-15; 8:45 am]
BILLING CODE 4910-13-P
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- 3e94aa7539b40f78dea5d0ea084cb38574f7f75047d3f6c8dfb9e4d8892fd1ad
- Text SHA-256
- 54085faa1e02a43dff01269637296706f9a727d96c41b183ee9de74aa71670bd
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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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