Airworthiness Directives; Airbus Helicopters, 30759-30761 [2021-12037]
Download as PDF
<![CDATA[
Federal Register / Vol. 86, No. 110 / Thursday, June 10, 2021 / Rules and Regulations
Spar Caps Replacement, dated June 9, 2012
(Piper Kit 764–394), as applicable.
Note 2 to paragraphs (h)(3): This note
applies to paragraphs (h)(3) and (7) of this
AD. Replacement parts for the left and right
wing spar fittings P/N 97712–00 and the
right, left, top, and bottom spar assemblies P/
Ns 97701–00 and 97701–01 are included
with Piper Kit 764–393 and Piper Kit 764–
394.
(4) Remove from service spar carry through
assembly P/N 97370–00 or 76824–02, as
applicable, and replace with an unused (zero
hours TIS) spar carry through assembly P/N
76824–02.
(5) Remove from service spar assembly P/
Ns 97701–00 and 97701–01, Revision P or
later revision, and replace with an unused
(zero hours TIS) spar assembly by following
the Instructions, sections B. and C., in Piper
Kit 764–393 or Piper Kit 764–394, as
applicable.
(6) Remove from service any spar carry
through assembly P/N 76767–00 or P/N
76824–02 and replace with an unused (zero
hours TIS) spar carry through assembly P/N
76824–02.
(7) Remove from service spar assemblies P/
Ns 97701–00 and 97701–01, Revision N or
earlier revision, and replace with an unused
(zero hours TIS) left spar cap replacement kit
P/N 764–393 and right spar cap replacement
kit P/N 764–394 by following the
Instructions, sections B. and C., in Piper Kit
764–393 or Piper Kit 764–394, as applicable.
(8) Remove from service wing attachment
lower bolt P/N 77245–00 and replace with an
unused (zero hours TIS) P/N 77245–00 bolt.
(i) Credit for Previous Actions
You may take credit for the actions
required by paragraph (g) of this AD if you
performed those actions before the effective
date of this AD using Piper Aircraft
Corporation Service Bulletin No. 552, dated
February 3, 1978.
khammond on DSKJM1Z7X2PROD with RULES
(j) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Atlanta ACO 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
certification office, send it to the attention of
the person identified in Related Information.
(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.
(3) AMOCs approved for AD 79–01–03 and
AD 83–20–03 are approved as AMOCs for the
corresponding provisions of this AD.
(k) Related Information
For more information about this AD,
contact Dan McCully, Aviation Safety
Engineer, FAA, Atlanta ACO Branch, 1701
Columbia Avenue, College Park, GA 30337;
phone: (404) 474–5548; fax: (404) 474–5606;
email: william.mccully@faa.gov.
VerDate Sep<11>2014
15:59 Jun 09, 2021
Jkt 253001
(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 the AD specifies otherwise.
(i) Piper Service Bulletin No. 552A, dated
August 3, 2018;
(ii) Piper Aircraft PA–36, Pawnee Brave Kit
764–394, Right Wing Main Spar Caps
Replacement, dated June 9, 2012; and
Note 3 to paragraph (l)(2)(ii): The Kit List
and Sketch A for Piper Aircraft PA–36,
Pawnee Brave Kit 764–394, Right Wing Main
Spar Caps Replacement, dated June 9, 2012;
and Piper Aircraft PA–36, Pawnee Brave Kit
764–393, Left Wing Main Spar Caps
Replacement, dated June 9, 2012, were
revised and dated June 9, 2012. The
instructions and sketches in the rest of the
documents were reformatted but retain the
previous date of March 30, 1982, because the
content of those pages was unchanged.
(iii) Piper Aircraft PA–36, Pawnee Brave
Kit 764–393, Left Wing Main Spar Caps
Replacement, dated June 9, 2012.
(3) For service information identified in
this AD, contact Piper Aircraft, Inc., 2926
Piper Drive, Vero Beach, FL 32960; phone:
(772) 567–4361; website: www.piper.com.
(4) You may view this service information
at FAA, Policy and Innovation Division, 901
Locust, Kansas City, MO 64106. For
information on the availability of this
material at the FAA, call (816) 329–4148.
(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: fedreg.legal@nara.gov, or go to:
https://www.archives.gov/federal-register/cfr/
ibr-locations.html.
Issued on May 19, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021–12043 Filed 6–9–21; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
30759
Airbus Helicopters Model EC 155B,
EC155B1, SA–365N, SA–365N1, AS–
365N2, and AS 365 N3 helicopters, as
identified in a European Aviation Safety
Agency (now European Union Aviation
Safety Agency) (EASA) AD. This AD
was prompted by a report of an in-flight
loss of engine and main gearbox (MGB)
cowlings. This AD requires inspecting
the MGB fixed cowling front fitting
(MGB front fitting), and depending on
findings, corrective action. This AD also
requires a new modification, which is a
terminating action for the inspection, as
specified in an EASA AD, which is
incorporated by reference. The FAA is
issuing this AD to address the unsafe
condition on these products.
This AD is effective July 15,
2021.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of July 15, 2021.
DATES:
For EASA material
incorporated by reference (IBR) in this
AD, contact the EASA, KonradAdenauer-Ufer 3, 50668 Cologne,
Germany; telephone +49 221 8999 000;
email ADs@easa.europa.eu; internet
www.easa.europa.eu. You may find this
material on the EASA website at https://
ad.easa.europa.eu. For Airbus
Helicopters service information, 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 https://
www.airbus.com/helicopters/services/
technical-support.html. 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 on the
internet at https://www.regulations.gov
by searching for and locating Docket No.
FAA–2020–1183.
ADDRESSES:
Federal Aviation Administration
Examining the AD Docket
14 CFR Part 39
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2020–
1183; 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,
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.
[Docket No. FAA–2020–1183; Project
Identifier 2019–SW–008–AD; Amendment
39–21565; AD 2021–11–03]
RIN 2120–AA64
Airworthiness Directives; Airbus
Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
SUMMARY:
PO 00000
Frm 00007
Fmt 4700
Sfmt 4700
E:\FR\FM\10JNR1.SGM
10JNR1
30760
Federal Register / Vol. 86, No. 110 / Thursday, June 10, 2021 / Rules and Regulations
FOR FURTHER INFORMATION CONTACT:
Blaine Williams, Aerospace Engineer,
Los Angeles ACO Branch, Compliance &
Airworthiness Division, 3960
Paramount Blvd., Lakewood, California
90712; telephone (562) 627–5371; email
blaine.williams@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
EASA, which is the Technical Agent
for the Member States of the European
Union, has issued EASA AD 2019–0008,
dated January 22, 2019 (EASA AD
2019–0008) to correct an unsafe
condition for certain Airbus Helicopters
(AH), formerly Eurocopter, Eurocopter
France, Aerospatiale, Model EC 155 B,
EC 155 B1, SA 365 N, SA 365 N1, AS
365 N2, and AS 365 N3 helicopters.
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to certain Model EC 155 B,
EC155B1, SA–365N, SA–365N1, AS–
365N2, and AS 365 N3 helicopters. The
NPRM published in the Federal
Register on March 5, 2021 (86 FR
12862). The NPRM was prompted by
reports of an in-flight loss of engine and
MGB cowlings. Subsequent
investigations revealed that the MGB
cowling attachment fittings failed
because of mounting stress in the MGB
front fitting and air intake bulkhead.
The NPRM proposed to require
inspecting and if necessary, replacing
the MGB front fitting. The NPRM also
proposed to require modifying the MGB
front fitting, as specified in an EASA
AD.
The FAA is issuing this AD to address
failure of an MGB front fitting and
subsequent detachment of the MGB or
engine cowlings. See EASA AD 2019–
0008 for additional background
information.
Discussion of Final Airworthiness
Directive
Comments
The FAA gave the public the
opportunity to participate in developing
this final rule. The FAA received no
comments on the NPRM or on the
determination of the cost to the public.
khammond on DSKJM1Z7X2PROD with RULES
Conclusion
The FAA reviewed the relevant data
and determined that air safety and the
public interest require adopting this
final rule as proposed.
Related Service Information Under 1
CFR Part 51
EASA AD 2019–0008 requires
inspecting the MGB front fittings within
110 flight hours after April 14, 2017 (the
VerDate Sep<11>2014
15:59 Jun 09, 2021
Jkt 253001
effective date of EASA AD 2017–0055,
dated March 31, 2017). If there is a
discrepancy, the EASA AD requires
applicable corrective action(s) before
next flight. EASA AD 2019–0008 also
requires modification of the MGB fixed
cowling attachments within 660 flight
hours or 23 months, whichever occurs
first, after the effective date described in
EASA AD 2019–0008. Accomplishing
the modification constitutes a
terminating action for the required
inspection.
The FAA also reviewed Airbus
Helicopters Alert Service Bulletin ASB
No. AS365–53.00.62 and ASB No.
EC155–53A038, each Revision 0 and
dated December 20, 2018 (ASB AS365–
53.00.62 and ASB EC155–53A038). ASB
AS365–53.00.62 applies to Model
AS365-series helicopters. ASB EC155–
53A038 applies to Model EC155-series
helicopters. This service information
specifies replacing the front bracket,
inspecting for stress of the MGB fixed
cowlings on the radiator bulkhead, and
installing an additional locking system.
This material 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 19 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.
Inspecting the MGB front fittings
takes about 2 work-hours for an
estimated cost of $170 per helicopter
and $3,230 for the U.S. fleet. If required,
replacing an MGB front fitting takes
about 2 work-hours and parts cost about
$590 for an estimated total cost of $760
per fitting. Other repairs will take up to
8 work-hours (excluding drying time)
and parts will cost a minimal amount
for an estimated cost of up to $680 per
helicopter.
Modifying the MGB fixed cowling
attachments takes about 5 work-hours
and parts cost about $630 for an
estimated cost of $1,055 per helicopter
and $20,045 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.
PO 00000
Frm 00008
Fmt 4700
Sfmt 4700
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
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
2021–11–03 Airbus Helicopters:
Amendment 39–21565; Docket No.
FAA–2020–1183; Project Identifier
2019–SW–008–AD.
(a) Effective Date
This airworthiness directive (AD) is
effective July 15, 2021.
E:\FR\FM\10JNR1.SGM
10JNR1
Federal Register / Vol. 86, No. 110 / Thursday, June 10, 2021 / Rules and Regulations
(b) Affected Airworthiness Directives (ADs)
None.
(c) Applicability
This AD applies to Airbus Helicopters
Model EC 155B, EC155B1, SA–365N, SA–
365N1, AS–365N2, and AS 365 N3
helicopters, certificated in any category, as
identified in European Aviation Safety
Agency (now European Union Aviation
Safety Agency) (EASA) AD 2019–0008, dated
January 22, 2019 (EASA AD 2019–0008).
(d) Subject
Joint Aircraft System Component (JASC)
Code: 7110, Engine Cowling System.
(e) Reason
This AD was prompted by a report of an
in-flight loss of main gearbox (MGB) and
engine cowlings. The FAA is issuing this AD
to address a failure of the MGB fixed cowling
front fitting, and subsequent MGB cowling or
engine cowling detachment, which could
result in damage to the helicopter, loss of
helicopter control, and possible injury to
persons on the ground.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
khammond on DSKJM1Z7X2PROD with RULES
(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, EASA AD 2019–0008.
(h) Exceptions to EASA AD 2019–0008
(1) Where EASA AD 2019–0008 refers to
April 14, 2017 (the effective date of EASA
AD 2017–0055, dated March 31, 2017), this
AD requires using the effective date of this
AD.
(2) Where EASA AD 2019–0008 refers to its
effective date, this AD requires using the
effective date of this AD.
(3) Where EASA AD 2019–0008 refers to
flight hours (FH), this AD requires using
hours time-in-service.
(4) Where EASA AD 2019–0008 requires
the modification within 660 flight hours or
23 months, whichever occurs first, this AD
requires the modification within 660 hours
time-in-service instead.
(5) Although the service information
referenced in EASA AD 2019–0008 specifies
to discard certain parts, this AD requires
removing those parts from service instead.
(6) Where the service information
referenced in EASA AD 2019–0008 specifies
to use tooling, equivalent tooling may be
used.
(7) The ‘‘Remarks’’ section of EASA AD
2019–0008 does not apply to this AD.
(8) Where paragraph (1) of EASA AD 2019–
0008 states to, ‘‘inspect the MGB fixed
cowling front fittings in accordance with the
instructions of paragraph 1.E.2 of the
applicable inspection ASB or in accordance
with the instructions of the applicable
modification ASB,’’ this AD requires
determining if Airbus Helicopters Alert
Service Bulletin No. 53.00.55, Revision 0,
dated March 13, 2017, or Revision 1, dated
December 20, 2018, has or has not been
VerDate Sep<11>2014
15:59 Jun 09, 2021
Jkt 253001
complied with and following the
instructions, ‘‘For helicopters on which
ALERT SERVICE BULLETIN No. 53.00.55
has not been complied with’’ or ‘‘For
helicopters on which ALERT SERVICE
BULLETIN No. 53.00.55 has been complied
with,’’ as applicable, in paragraph 1.E.2, of
Airbus Helicopters Alert Service Bulletin
ASB No. AS365–53.00.62 or ASB No. EC155–
53A038, each Revision 0 and dated December
20, 2018 (ASB AS365–53.00.62 or ASB
EC155–53A038), as applicable to your model
helicopter.
(9) Where paragraph (2) of EASA AD 2019–
0008 states to, ‘‘accomplish the applicable
corrective action(s) in accordance with
paragraph 1.E.2 of the applicable inspection
ASB or in accordance with the instructions
of the applicable modification ASB,’’ this AD
requires accomplishing the applicable
corrective actions by following ASB AS365–
53.00.62 or ASB EC155–53A038, as
applicable to your model helicopter.
(10) Where paragraph 3.B.2.e.3 of the
applicable modification ASB referenced in
EASA AD 2019–0008 refers to paragraph
3.B.e.3, this AD requires referring to
paragraph 3.B.3 of ASB AS365–53.00.62 or
ASB EC155–53A038, as applicable to your
model helicopter.
(i) Special Flight Permit
Special flight permits, as described in 14
CFR 21.197 and 21.199, are not allowed.
(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: 9-AVS-AIR730-AMOC@faa.gov.
(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.
(ii) Airbus Helicopters Alert Service
Bulletin ASB No. AS365–53.00.62, Revision
0, dated December 20, 2018.
(iii) Airbus Helicopters Alert Service
Bulletin ASB No. EC155–53A038, Revision 0,
dated December 20, 2018.
(3) For EASA AD 2019–0008, contact the
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; internet
www.easa.europa.eu. You may find this
EASA AD on the EASA website at https://
ad.easa.europa.eu. For Airbus Helicopters
service information, 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
https://www.airbus.com/helicopters/services/
technical-support.html.
(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
on the internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2020–1183.
(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 fedreg.legal@
nara.gov, or go to https://www.archives.gov/
federal-register/cfr/ibr-locations.html.
Issued on May 11, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021–12037 Filed 6–9–21; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2020–1074; Project
Identifier MCAI–2020–01257–A; Amendment
39–21574; AD 2021–11–12]
(k) Related Information
For more information about this AD,
contact Blaine Williams, Aerospace Engineer,
Los Angeles ACO Branch, Compliance &
Airworthiness Division, 3960 Paramount
Blvd., Lakewood, California 90712; telephone
(562) 627–5227; email blaine.williams@
faa.gov.
RIN 2120–AA64
(l) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) 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 Aviation Safety Agency
(EASA) AD 2019–0008, dated January 22,
2019.
SUMMARY:
PO 00000
Frm 00009
Fmt 4700
Sfmt 4700
30761
Airworthiness Directives; Pilatus
Aircraft Ltd. Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
Pilatus Aircraft Ltd. (Pilatus) Model PC–
24 airplanes. This AD results from
mandatory continuing airworthiness
information (MCAI) originated by an
aviation authority of another country to
identify and correct an unsafe condition
on an aviation product. The MCAI
identifies the unsafe condition as the
engine attachment hardware not
E:\FR\FM\10JNR1.SGM
10JNR1
]]>Agencies
[Federal Register Volume 86, Number 110 (Thursday, June 10, 2021)]
[Rules and Regulations]
[Pages 30759-30761]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-12037]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-1183; Project Identifier 2019-SW-008-AD; Amendment
39-21565; AD 2021-11-03]
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
certain Airbus Helicopters Model EC 155B, EC155B1, SA-365N, SA-365N1,
AS-365N2, and AS 365 N3 helicopters, as identified in a European
Aviation Safety Agency (now European Union Aviation Safety Agency)
(EASA) AD. This AD was prompted by a report of an in-flight loss of
engine and main gearbox (MGB) cowlings. This AD requires inspecting the
MGB fixed cowling front fitting (MGB front fitting), and depending on
findings, corrective action. This AD also requires a new modification,
which is a terminating action for the inspection, as specified in an
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 July 15, 2021.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of July 15,
2021.
ADDRESSES: For EASA material incorporated by reference (IBR) in this
AD, contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany;
telephone +49 221 8999 000; email [email protected]; internet
www.easa.europa.eu. You may find this material on the EASA website at
https://ad.easa.europa.eu. For Airbus Helicopters service information,
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 https://www.airbus.com/helicopters/services/technical-support.html. 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 on the internet at https://www.regulations.gov by searching
for and locating Docket No. FAA-2020-1183.
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-
1183; 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, 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.
[[Page 30760]]
FOR FURTHER INFORMATION CONTACT: Blaine Williams, Aerospace Engineer,
Los Angeles ACO Branch, Compliance & Airworthiness Division, 3960
Paramount Blvd., Lakewood, California 90712; telephone (562) 627-5371;
email [email protected].
SUPPLEMENTARY INFORMATION:
Background
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2019-0008, dated January 22, 2019
(EASA AD 2019-0008) to correct an unsafe condition for certain Airbus
Helicopters (AH), formerly Eurocopter, Eurocopter France, Aerospatiale,
Model EC 155 B, EC 155 B1, SA 365 N, SA 365 N1, AS 365 N2, and AS 365
N3 helicopters.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain Model EC 155 B,
EC155B1, SA-365N, SA-365N1, AS-365N2, and AS 365 N3 helicopters. The
NPRM published in the Federal Register on March 5, 2021 (86 FR 12862).
The NPRM was prompted by reports of an in-flight loss of engine and MGB
cowlings. Subsequent investigations revealed that the MGB cowling
attachment fittings failed because of mounting stress in the MGB front
fitting and air intake bulkhead. The NPRM proposed to require
inspecting and if necessary, replacing the MGB front fitting. The NPRM
also proposed to require modifying the MGB front fitting, as specified
in an EASA AD.
The FAA is issuing this AD to address failure of an MGB front
fitting and subsequent detachment of the MGB or engine cowlings. See
EASA AD 2019-0008 for additional background information.
Discussion of Final Airworthiness Directive
Comments
The FAA gave the public the opportunity to participate in
developing this final rule. The FAA received no comments on the NPRM or
on the determination of the cost to the public.
Conclusion
The FAA reviewed the relevant data and determined that air safety
and the public interest require adopting this final rule as proposed.
Related Service Information Under 1 CFR Part 51
EASA AD 2019-0008 requires inspecting the MGB front fittings within
110 flight hours after April 14, 2017 (the effective date of EASA AD
2017-0055, dated March 31, 2017). If there is a discrepancy, the EASA
AD requires applicable corrective action(s) before next flight. EASA AD
2019-0008 also requires modification of the MGB fixed cowling
attachments within 660 flight hours or 23 months, whichever occurs
first, after the effective date described in EASA AD 2019-0008.
Accomplishing the modification constitutes a terminating action for the
required inspection.
The FAA also reviewed Airbus Helicopters Alert Service Bulletin ASB
No. AS365-53.00.62 and ASB No. EC155-53A038, each Revision 0 and dated
December 20, 2018 (ASB AS365-53.00.62 and ASB EC155-53A038). ASB AS365-
53.00.62 applies to Model AS365-series helicopters. ASB EC155-53A038
applies to Model EC155-series helicopters. This service information
specifies replacing the front bracket, inspecting for stress of the MGB
fixed cowlings on the radiator bulkhead, and installing an additional
locking system.
This material 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 19 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.
Inspecting the MGB front fittings takes about 2 work-hours for an
estimated cost of $170 per helicopter and $3,230 for the U.S. fleet. If
required, replacing an MGB front fitting takes about 2 work-hours and
parts cost about $590 for an estimated total cost of $760 per fitting.
Other repairs will take up to 8 work-hours (excluding drying time) and
parts will cost a minimal amount for an estimated cost of up to $680
per helicopter.
Modifying the MGB fixed cowling attachments takes about 5 work-
hours and parts cost about $630 for an estimated cost of $1,055 per
helicopter and $20,045 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:
2021-11-03 Airbus Helicopters: Amendment 39-21565; Docket No. FAA-
2020-1183; Project Identifier 2019-SW-008-AD.
(a) Effective Date
This airworthiness directive (AD) is effective July 15, 2021.
[[Page 30761]]
(b) Affected Airworthiness Directives (ADs)
None.
(c) Applicability
This AD applies to Airbus Helicopters Model EC 155B, EC155B1,
SA-365N, SA-365N1, AS-365N2, and AS 365 N3 helicopters, certificated
in any category, as identified in European Aviation Safety Agency
(now European Union Aviation Safety Agency) (EASA) AD 2019-0008,
dated January 22, 2019 (EASA AD 2019-0008).
(d) Subject
Joint Aircraft System Component (JASC) Code: 7110, Engine
Cowling System.
(e) Reason
This AD was prompted by a report of an in-flight loss of main
gearbox (MGB) and engine cowlings. The FAA is issuing this AD to
address a failure of the MGB fixed cowling front fitting, and
subsequent MGB cowling or engine cowling detachment, which could
result in damage to the helicopter, loss of helicopter control, and
possible injury to persons on the ground.
(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, EASA AD 2019-0008.
(h) Exceptions to EASA AD 2019-0008
(1) Where EASA AD 2019-0008 refers to April 14, 2017 (the
effective date of EASA AD 2017-0055, dated March 31, 2017), this AD
requires using the effective date of this AD.
(2) Where EASA AD 2019-0008 refers to its effective date, this
AD requires using the effective date of this AD.
(3) Where EASA AD 2019-0008 refers to flight hours (FH), this AD
requires using hours time-in-service.
(4) Where EASA AD 2019-0008 requires the modification within 660
flight hours or 23 months, whichever occurs first, this AD requires
the modification within 660 hours time-in-service instead.
(5) Although the service information referenced in EASA AD 2019-
0008 specifies to discard certain parts, this AD requires removing
those parts from service instead.
(6) Where the service information referenced in EASA AD 2019-
0008 specifies to use tooling, equivalent tooling may be used.
(7) The ``Remarks'' section of EASA AD 2019-0008 does not apply
to this AD.
(8) Where paragraph (1) of EASA AD 2019-0008 states to,
``inspect the MGB fixed cowling front fittings in accordance with
the instructions of paragraph 1.E.2 of the applicable inspection ASB
or in accordance with the instructions of the applicable
modification ASB,'' this AD requires determining if Airbus
Helicopters Alert Service Bulletin No. 53.00.55, Revision 0, dated
March 13, 2017, or Revision 1, dated December 20, 2018, has or has
not been complied with and following the instructions, ``For
helicopters on which ALERT SERVICE BULLETIN No. 53.00.55 has not
been complied with'' or ``For helicopters on which ALERT SERVICE
BULLETIN No. 53.00.55 has been complied with,'' as applicable, in
paragraph 1.E.2, of Airbus Helicopters Alert Service Bulletin ASB
No. AS365-53.00.62 or ASB No. EC155-53A038, each Revision 0 and
dated December 20, 2018 (ASB AS365-53.00.62 or ASB EC155-53A038), as
applicable to your model helicopter.
(9) Where paragraph (2) of EASA AD 2019-0008 states to,
``accomplish the applicable corrective action(s) in accordance with
paragraph 1.E.2 of the applicable inspection ASB or in accordance
with the instructions of the applicable modification ASB,'' this AD
requires accomplishing the applicable corrective actions by
following ASB AS365-53.00.62 or ASB EC155-53A038, as applicable to
your model helicopter.
(10) Where paragraph 3.B.2.e.3 of the applicable modification
ASB referenced in EASA AD 2019-0008 refers to paragraph 3.B.e.3,
this AD requires referring to paragraph 3.B.3 of ASB AS365-53.00.62
or ASB EC155-53A038, as applicable to your model helicopter.
(i) Special Flight Permit
Special flight permits, as described in 14 CFR 21.197 and
21.199, are not allowed.
(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].
(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 Blaine Williams,
Aerospace Engineer, Los Angeles ACO Branch, Compliance &
Airworthiness Division, 3960 Paramount Blvd., Lakewood, California
90712; telephone (562) 627-5227; email [email protected].
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) 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 Aviation Safety Agency (EASA) AD 2019-0008, dated
January 22, 2019.
(ii) Airbus Helicopters Alert Service Bulletin ASB No. AS365-
53.00.62, Revision 0, dated December 20, 2018.
(iii) Airbus Helicopters Alert Service Bulletin ASB No. EC155-
53A038, Revision 0, dated December 20, 2018.
(3) For EASA AD 2019-0008, contact the EASA, Konrad-Adenauer-
Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email
[email protected]; internet www.easa.europa.eu. You may find this
EASA AD on the EASA website at https://ad.easa.europa.eu. For Airbus
Helicopters service information, 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 https://www.airbus.com/helicopters/services/technical-support.html.
(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 on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-
2020-1183.
(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 May 11, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2021-12037 Filed 6-9-21; 8:45 am]
BILLING CODE 4910-13-P
