Published 2018-02-28 · Federal Register document 2018-03930
Airworthiness Directives; AgustaWestland S.p.A. Helicopters
Publication summary
We are adopting a new airworthiness directive (AD) for certain AgustaWestland S.p.A. (AgustaWestland) Model AW189 helicopters. This AD requires replacing the seal and filler wedges of all emergency exit windows. This AD was prompted by a report that some windows were improperly glued when installed. The actions of this AD are intended to correct an unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:58.123663+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2018-258c65fa72d503e0
- Source row
- results[64]
- Raw source SHA-256
- 258c65fa72d503e0b0dfb928a28beb1793ddc7dd9218bce0413e53dfe11d78fb
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2018-05-02
- Effective date printed in this edition
- 2018-04-04
Some source clauses remain unstructured. Read the complete publication for conditions that have not been interpreted here.
Read 8 complete recorded clauses
Applicability wording · Applicability
(a) Applicability
This AD applies to Model AW189 helicopters, serial number 49007
through 49021, 49023, 49029, 49033, 49035, 89001, 89003, 89004,
92001, 92003, and 92005, certificated in any category.
Exact source excerpt. Text positions 9078–9287, end exclusive, in the original decoded publication. SHA-256: 1281812b6db5dfc4b47635a9321bde498858fdbf7af7d8466478b756717223a1
Unsafe Condition
(b) Unsafe Condition
This AD defines the unsafe condition as improperly glued
emergency exit windows. This condition could result in the window
failing to jettison, preventing the occupants from exiting the
helicopter during an emergency.
Exact source excerpt. Text positions 9287–9535, end exclusive, in the original decoded publication. SHA-256: 143679274f1de6903f81197263dfa7305ebd2926a4288b03f9c8db4e50680d60
Effective Date
(c) Effective Date
This AD becomes effective April 4, 2018.
Exact source excerpt. Text positions 9535–9601, end exclusive, in the original decoded publication. SHA-256: 38cdcef37237849942a59490593b9218a5c8386a8558d3e149fc2613204b26dd
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 9601–9788, end exclusive, in the original decoded publication. SHA-256: 56042b53a75a0db2af067b711f9b82d8091413842e43863752e31aeffdd54a72
Required Actions
(e) Required Actions
Within 75 hours time-in-service, replace the seal and filler
wedges of each cabin and cockpit door emergency exit window, except
bubble windows installed in accordance with bubble window kit part
number 8G5620F00111.
Exact source excerpt. Text positions 9788–10035, end exclusive, in the original decoded publication. SHA-256: c2be28f56cce0de48759760d8ccd266551f25e8e1025b775c6e7a49af716ecd1
Alternative Methods of Compliance (AMOCs)
(f) 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:
Martin R. Crane, Aviation Safety Engineer, Regulations & 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, we suggest 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 10035–10799, end exclusive, in the original decoded publication. SHA-256: 6441e80b18091a97c1cc8b96471cba026708093544c2b645d3da341aa7640859
Additional Information
(g) Additional Information
(1) Leonardo Helicopters Bollettino Tecnico No. 189-118, dated
October 20, 2016, which is not incorporated by reference, contains
additional information about the subject of this AD. For service
information identified in this AD, contact Leonardo S.p.A.
Helicopters, Matteo Ragazzi, Head of Airworthiness, Viale G.Agusta
520, 21017 C.Costa di Samarate (Va) Italy; telephone +39-0331-
711756; fax +39-0331-229046; or at http://www.leonardocompany.com/-/bulletins. You may review 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 Aviation
Safety Agency (EASA) AD No. 2016-0216, dated October 28, 2016. You
may view the EASA AD on the internet at http://www.regulations.gov
in AD Docket No. FAA-2017-0111.
Exact source excerpt. Text positions 10799–11703, end exclusive, in the original decoded publication. SHA-256: a4e4da3cf0f7389f856bf84727844f5b14b3628ed6312e3ea686e25941139225
Subject
(h) Subject
Joint Aircraft Service Component (JASC) Code: 5600, Window/
Windshield System.
Exact source excerpt. Text positions 11703–11800, end exclusive, in the original decoded publication. SHA-256: e6b664f2a6a1c3359c9e32313c5c07e92ad275ca538dc5214e95bd5d0bed334a
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 2018-05-02 · 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: f064e846d6087eb30af79db025740fe657dafba7ab47a5b44b5cec480dda4390. Source manifest: bbf6348df8354bae5f0cfc0b05001bb54d1ac97ba3e43cf2873f2f8efe0dc1e9.
Official source · 2018-02-28
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 83, Number 40 (Wednesday, February 28, 2018)]
[Rules and Regulations]
[Pages 8605-8606]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-03930]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
========================================================================
Federal Register / Vol. 83, No. 40 / Wednesday, February 28, 2018 /
Rules and Regulations
[[Page 8605]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2017-0111; Product Identifier 2016-SW-079-AD; Amendment
39-19211; AD 2018-05-02]
RIN 2120-AA64
Airworthiness Directives; AgustaWestland S.p.A. Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
AgustaWestland S.p.A. (AgustaWestland) Model AW189 helicopters. This AD
requires replacing the seal and filler wedges of all emergency exit
windows. This AD was prompted by a report that some windows were
improperly glued when installed. The actions of this AD are intended to
correct an unsafe condition on these products.
DATES: This AD is effective April 4, 2018.
ADDRESSES: For service information identified in this final rule,
contact Leonardo S.p.A. Helicopters, Matteo Ragazzi, Head of
Airworthiness, Viale G.Agusta 520, 21017 C.Costa di Samarate (Va)
Italy; telephone +39-0331-711756; fax +39-0331-229046; or at http://www.leonardocompany.com/-/bulletins. You may review the referenced
service information at the FAA, Office of the Regional Counsel,
Southwest Region, 10101 Hillwood Pkwy, Room 6N-321, Fort Worth, TX
76177.
Examining the AD Docket
You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017-
0111; 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 Aviation Safety Agency (EASA) AD, any
incorporated-by-reference service information, the economic evaluation,
any comments received, and other information. The street address for
Docket Operations (phone: 800-647-5527) 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: Martin R. Crane, Aviation Safety
Engineer, Regulations & Policy Section, Rotorcraft Standards Branch,
FAA, 10101 Hillwood Pkwy, Fort Worth, TX 76177; telephone (817) 222-
5110; email [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
On November 2, 2017, at 82 FR 50847, 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 AgustaWestland Model
AW189 helicopters. The NPRM proposed to require replacing the seal and
filler wedges of all emergency exit windows. The proposed requirements
were intended to prevent the failure of the windows from jettisoning
during an emergency.
The NPRM was prompted by AD No. 2016-0216, dated October 28, 2016,
issued by EASA, which is the Technical Agent for the Member States of
the European Union, to correct an unsafe condition for Leonardo
Helicopters (previously Finmeccanica S.p.A., previously AgustaWestland)
Model AW189 helicopters, serial numbers 49007 through 49021, 49023,
49029, 49033, 49035, 89001, 89003, 89004, 92001, 92003, and 92005. The
EASA AD does not apply to windows that have been reinstalled at least
once since helicopter delivery and windows that are part of bubble
window kit part number (P/N) 8G5620F00111.
EASA advises that some windows were installed with glue applied in
locations that were not in accordance with the approved design. This
condition, if not corrected, could prevent the jettisoning of
helicopter emergency exit windows, possibly affecting the evacuation of
crew and passengers during an emergency situation, EASA advises. EASA
consequently requires replacement of the seal and the filler wedges of
the emergency exit windows installed in the cockpit doors and cabin.
The FAA is in the process of updating AgustaWestland's name change
to Leonardo Helicopters on its type certificate. Because this name
change is not yet effective, this AD specifies AgustaWestland.
Comments
We gave the public the opportunity to participate in developing
this AD, but we received no comments on the NPRM.
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.
Related Service Information
We reviewed Leonardo Helicopters Bollettino Tecnico No. 189-118,
dated October 20, 2016. This service information specifies replacing
the seal and filler wedges on all cockpit door and cabin emergency exit
windows of Model AW189 helicopters, except on those windows that have
been replaced or that are part of bubble window kit P/N 8G5620F00111.
Costs of Compliance
We estimate that this AD affects 2 helicopters of U.S. Registry and
that labor costs average $85 per work-hour. Based on these estimates,
we expect that removing and replacing the window seals and fillers
requires 40 work-hours and that parts cost about $834, for a total cost
of $4,234 per helicopter and $8,468 for the U.S. fleet.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue
[[Page 8606]]
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):
2018-05-02 AgustaWestland S.p.A.: Amendment 39-19211; Docket No.
FAA-2017-0111; Product Identifier 2016-SW-079-AD.
(a) Applicability
This AD applies to Model AW189 helicopters, serial number 49007
through 49021, 49023, 49029, 49033, 49035, 89001, 89003, 89004,
92001, 92003, and 92005, certificated in any category.
(b) Unsafe Condition
This AD defines the unsafe condition as improperly glued
emergency exit windows. This condition could result in the window
failing to jettison, preventing the occupants from exiting the
helicopter during an emergency.
(c) Effective Date
This AD becomes effective April 4, 2018.
(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 75 hours time-in-service, replace the seal and filler
wedges of each cabin and cockpit door emergency exit window, except
bubble windows installed in accordance with bubble window kit part
number 8G5620F00111.
(f) 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:
Martin R. Crane, Aviation Safety Engineer, Regulations & 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, we suggest 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.
(g) Additional Information
(1) Leonardo Helicopters Bollettino Tecnico No. 189-118, dated
October 20, 2016, which is not incorporated by reference, contains
additional information about the subject of this AD. For service
information identified in this AD, contact Leonardo S.p.A.
Helicopters, Matteo Ragazzi, Head of Airworthiness, Viale G.Agusta
520, 21017 C.Costa di Samarate (Va) Italy; telephone +39-0331-
711756; fax +39-0331-229046; or at http://www.leonardocompany.com/-/bulletins. You may review 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 Aviation
Safety Agency (EASA) AD No. 2016-0216, dated October 28, 2016. You
may view the EASA AD on the internet at http://www.regulations.gov
in AD Docket No. FAA-2017-0111.
(h) Subject
Joint Aircraft Service Component (JASC) Code: 5600, Window/
Windshield System.
Issued in Fort Worth, Texas, on February 21, 2018.
Scott A. Horn,
Deputy Director for Regulatory Operations, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2018-03930 Filed 2-27-18; 8:45 am]
BILLING CODE 4910-13-P
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