AD 2021-05-06

[Federal Register Volume 86, Number 48 (Monday, March 15, 2021)]
[Rules and Regulations]
[Pages 14238-14241]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2021-05144]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0916; Product Identifier 2015-SW-055-AD; Amendment 
39-21449; AD 2021-05-06]
RIN 2120-AA64


Airworthiness Directives; Airbus Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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[[Page 14239]]

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for 
Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, EC 
155B, EC155B1, EC225LP, and SA330J helicopters. This AD requires 
inspecting the snap fasteners on the windows. This AD was prompted by 
incidents of difficulty unbuttoning the extraction tape on the windows. 
The actions of this AD are intended to address an unsafe condition on 
these products.

DATES: This AD is effective April 19, 2021.
    The Director of the Federal Register approved the incorporation by 
reference of certain documents listed in this AD as of April 19, 2021.

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 <a href="https://www.airbus.com/helicopters/services/technical-support.html">https://www.airbus.com/helicopters/services/technical-support.html</a>. 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 <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating 
Docket No. FAA-2020-0916.

Examining the AD Docket

    You may examine the AD docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2020-
0916; 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 (now European Union 
Aviation Safety Agency) (EASA) ADs, 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: David Hatfield, Aerospace Engineer, 
Aircraft Systems Section, Technical Innovation Policy Branch, Policy & 
Innovation Division, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; 
telephone (817) 222-5110; email <a href="/cdn-cgi/l/email-protection#b7d3d6c1ded399dfd6c3d1ded2dbd3f7d1d6d699d0d8c1"><span class="__cf_email__" data-cfemail="5034312639347e3831243639353c34103631317e373f26">[email&#160;protected]</span></a>.

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 Airbus Helicopters 
Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, EC 155B, EC155B1, 
EC225LP, and SA330J helicopters with window extraction tape with snap 
fasteners installed. The NPRM published in the Federal Register on 
October 22, 2020 (85 FR 67313). The NPRM proposed to require inspecting 
each internal and external snap fastener to determine whether they 
unbutton by hand. For external snap fasteners that do not unbutton by 
hand, the NPRM proposed to require replacing the male part of the snap 
fastener and installing self-gripping tape if it still does not 
unbutton by hand. Thereafter, the NPRM proposed to require a repetitive 
inspection of the external extraction tape and self-gripping tape and 
replacing any tape that is cracked, torn, disintegrated, worn, or 
missing, and replacing the snap fasteners. For internal snap fasteners 
that do not unbutton by hand, the NPRM proposed to require installing 
self-gripping tape and replacing the snap fasteners. The proposed 
requirements were intended to prevent failure of a window to jettison, 
preventing occupants from exiting the helicopter during an emergency.
    The NPRM was prompted by EASA AD No. 2015-0149, dated July 23, 2015 
(EASA AD 2015-0149), to correct an unsafe condition for Airbus 
Helicopters Model AS 322 and EC 225 LP helicopters; EASA AD No. 2015-
0168, dated August 13, 2015 (EASA AD 2015-0168), to correct an unsafe 
condition for Airbus Helicopters Model EC 155 B and EC 155 B1 
helicopters; and EASA AD No. 2015-0169, dated August 13, 2015 (EASA AD 
2015-0169), to correct an unsafe condition for Airbus Helicopters Model 
SA330 J helicopters, equipped with an extraction tape fitted with 
``press-studs'' (snap fasteners) on the windows. Each EASA AD was 
issued by EASA, which is the Technical Agent for the Member States of 
the European Union. EASA advises of difficulty unbuttoning the 
extraction tape during the manufacturing of a helicopter. Investigation 
concluded that the difficulty was caused by a bad male/female coupling, 
possibly resulting from miscrimping. This difficulty is known to have 
occurred on two additional helicopters. EASA states this condition, if 
not detected and corrected, could prevent the jettisoning of the 
helicopter window, possibly affecting the evacuation of passengers 
during an emergency situation. For these reasons, EASA AD 2015-0149, 
EASA AD 2015-0168, and EASA AD 2015-0169 require inspecting each press-
stud located on the extraction tapes of the window jettisoning system 
and depending on the findings, installing self-gripping tape and 
replacing the press-studs.

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 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. AS332-56.00.10, Revision 0, dated July 16, 2015, for Model AS332-
series helicopters; ASB No. EC155-56A006, Revision 0, dated August 10, 
2015, for Model EC155-series helicopters; ASB No. EC225-56A008, 
Revision 0, dated July 16, 2015, for Model EC225LP helicopters; and ASB 
No. SA330-56.02, Revision 0, dated August 10, 2015, for Model SA330J 
helicopters. This service information specifies procedures to inspect 
the internal and external press-studs and to install self-gripping tape 
for press-studs that do not unbutton or are difficult to unbutton. This 
service information also specifies procedures to replace internal 
press-studs that are difficult to unbutton and a repetitive inspection 
for affected external press-studs until they are replaced.
    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.

Costs of Compliance

    The FAA estimates that this AD affects 72 helicopters of U.S. 
Registry. Labor rates are estimated at $85 per work-hour. Based on 
these numbers, the FAA estimates that operators may incur the following 
costs in order to comply with this AD.

[[Page 14240]]

    Inspecting the snap fasteners takes about 1 work-hour for a cost of 
$85 per helicopter and $6,120 for the U.S. fleet. Installing self-
gripping tape takes about 0.3 work-hour and parts cost $200 for a cost 
of $226 per window. Inspecting the tape takes about 0.3 work-hour for a 
cost of $26 per window per inspection cycle. Replacing the extraction 
tape or self-gripping tape takes about 1 work-hour and parts cost $200 
for a total of $285 per window. Replacing a snap fastener takes about 1 
work-hour and parts cost $200 for a total of $285 per snap fastener.

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:

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:

2021-05-06 Airbus Helicopters: Amendment 39-21449; Docket No. FAA-
2020-0916; Product Identifier 2015-SW-055-AD.

(a) Applicability

    This airworthiness directive (AD) applies to Airbus Helicopters 
Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, EC 155B, EC155B1, 
EC225LP, and SA330J helicopters, certificated in any category, with 
window extraction tape with snap fasteners installed.

(b) Unsafe Condition

    This AD defines the unsafe condition as failure of a snap 
fastener to unbutton. This condition could result in failure of the 
window to jettison, preventing occupants from exiting the helicopter 
during an emergency.

(c) Effective Date

    This AD becomes effective April 19, 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

    Within 50 hours time-in-service (TIS), inspect each internal and 
external snap fastener to determine if it can be unbuttoned by hand.
    Note 1 to the introductory text of paragraph (e): Airbus 
Helicopters refers to the snap fastener as a ``press-stud.''
    (1) If all internal and external snap fasteners can be 
unbuttoned by hand, no further action is required by this AD.
    (2) If an external snap fastener does not unbutton by hand:
    (i) Before further flight, replace the male part of the snap 
fastener and determine if the snap fastener can be unbuttoned by 
hand force. If the snap fastener still does not unbutton by hand, 
before further flight, install self-gripping tape.
    (ii) Thereafter, at intervals not to exceed 15 hours TIS, 
inspect the external extraction tape and self-gripping tape for a 
crack, a tear, disintegration, or wear. If the extraction tape or 
self-gripping tape has a crack, a tear, any disintegration, wear, or 
is missing, before further flight, replace the tape. Replacing the 
extraction tape or self-gripping tape does not terminate this 
repetitive inspection.
    (iii) Within 100 hours TIS, replace each external snap fastener 
by following the Accomplishment Instructions, paragraph 3.B.4., of 
Airbus Helicopters Alert Service Bulletin (ASB) No. AS332-56.00.10, 
Revision 0, dated July 16, 2015 (ASB AS332-56.00.10); ASB No. EC155-
56A006, Revision 0, dated August 10, 2015 (ASB EC155-56A006); ASB 
No. EC225-56A008, Revision 0, dated July 16, 2015 (ASB EC225-
56A008); or ASB No. SA330-56.02, Revision 0, dated August 10, 2015 
(ASB SA330-56.02), as applicable to your model helicopter. Replacing 
the external snap fastener terminates the repetitive inspection 
requirements specified in paragraph (e)(2)(ii) of this AD.
    (3) If an internal snap fastener does not unbutton by hand:
    (i) Before further flight, install self-gripping tape by 
following the Accomplishment Instructions, paragraph 3.B.3., of 
AS332-56.00.10, ASB EC155-56A006, ASB EC225-56A008, or ASB SA330-
56.02, as applicable to your model helicopter.
    (ii) Within 900 hours TIS, replace each internal snap fastener 
by following the Accomplishment Instructions, paragraph 3.B.5., of 
ASB AS332-56.00.10, ASB EC155-56A006, ASB EC225-56A008, or ASB 
SA330-56.02, as applicable to your model helicopter.

(f) 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, send it to the attention of: David 
Hatfield, Aerospace Engineer, Aircraft Systems Section, Technical 
Innovation Policy Branch, Policy & Innovation Division, FAA, 10101 
Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222-5110. 
Information may be emailed to: <a href="/cdn-cgi/l/email-protection#6c55412d3a3f412d253e415b5f5c412d21232f2c0a0d0d420b031a"><span class="__cf_email__" data-cfemail="94adb9d5c2c7b9d5ddc6b9a3a7a4b9d5d9dbd7d4f2f5f5baf3fbe2">[email&#160;protected]</span></a>.
    (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.

(g) Additional Information

    The subject of this AD is addressed in European Aviation Safety 
Agency (now European Union Aviation Safety Agency) (EASA) AD No. 
2015-0149, dated July 23, 2015; EASA AD No. 2015-0168, dated August 
13, 2015; and EASA AD No. 2015-0169, dated August 13, 2015. You may 
view the EASA ADs on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> in 
Docket No. FAA-2020-0916.

(h) Subject

    Joint Aircraft Service Component (JASC) Code: 5600, Window/
Windshield System.

(i) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference of

[[Page 14241]]

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 (ASB) No. AS332-
56.00.10, Revision 0, dated July 16, 2015.
    (ii) Airbus Helicopters ASB No. EC155-56A006, Revision 0, dated 
August 10, 2015.
    (iii) Airbus Helicopters ASB No. EC225-56A008, Revision 0, dated 
July 16, 2015.
    (iv) Airbus Helicopters ASB No. SA330-56.02, Revision 0, dated 
August 10, 2015.
    (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 <a href="https://www.airbus.com/helicopters/services/technical-support.html">https://www.airbus.com/helicopters/services/technical-support.html</a>.
    (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.
    (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 <a href="/cdn-cgi/l/email-protection#8bedeeeff9eeeca5e7eeeceae7cbe5eaf9eaa5ece4fd"><span class="__cf_email__" data-cfemail="ccaaa9a8bea9abe2a0a9abada08ca2adbeade2aba3ba">[email&#160;protected]</span></a>, or go to: <a href="https://www.archives.gov/federal-register/cfr/ibr-locations.html">https://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.

    Issued on February 18, 2021.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness 
Division, Aircraft Certification Service.
[FR Doc. 2021-05144 Filed 3-12-21; 8:45 am]
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