Airworthiness Directives; Bell Textron Canada Limited Helicopters, 30768-30770 [2021-12042]
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Federal Register / Vol. 86, No. 110 / Thursday, June 10, 2021 / Rules and Regulations
identical to page 2–8 of BHT–206B–FM–1 or
page 2–10 of BHT–206B3–FM–1, as
applicable to your helicopter, is acceptable
for compliance with the requirements of this
paragraph.
(iii) Remove placard part number (P/N)
230–075–213–121, if installed.
(iv) Install placard P/N 230–075–213–129
or placard P/N 230–075–213–131 on the
instrument panel directly below the dual
tachometer.
(2) For Bell Model 206L helicopters:
(i) Revise the existing RFM for your
helicopter by inserting Section 1, Operating
Limitations, page 1–4B, of Bell Model 206L
RFM BHT–206L–FM–1, Revision 31, dated
May 30, 2018 (BHT–206L–FM–1). Inserting a
different document with ‘‘Steady-state
operation’’ information identical to page
1–4B of BHT–206L–FM–1 is acceptable for
compliance with the requirements of this
paragraph.
(ii) Revise the existing RFM for your
helicopter by inserting Section 2, Normal
Procedures, page 2–10 of BHT–206L–FM–1.
Inserting a different document with
‘‘Continuous Operation’’ information
identical to page 2–10 of BHT–206L–FM–1 is
acceptable for compliance with the
requirements of this paragraph.
(iii) Remove placard P/N 230–075–213–
123, if installed.
(iv) Install placard P/N 230–075–213–129
or placard P/N 230–075–213–131 on the
instrument panel below the dual tachometer.
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(h) 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 (i)(1) 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.
(i) Related Information
(1) For more information about this AD,
contact Michael Hughlett, Aviation Safety
Engineer, General Aviation & Rotorcraft
Section, International Validation Branch,
FAA, 10101 Hillwood Pkwy., Fort Worth, TX
76177; telephone (817) 222–5889; email
Michael.Hughlett@faa.gov.
(2) Bell Alert Service Bulletin (ASB) 206–
07–115, Revision D, for Model 206A and
206B helicopters, and ASB 206L–07–146,
Revision C, for Model 206L helicopters, each
dated July 9, 2018, which are not
incorporated by reference, contain additional
information about the subject of this AD.
This service information is available at the
contact information specified in paragraphs
(j)(3) and (4) of this AD.
(3) The subject of this AD is addressed in
Transport Canada AD CF–2018–23, dated
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15:59 Jun 09, 2021
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August 22, 2018. You may view the
Transport Canada AD on the internet at
https://www.regulations.gov in Docket No.
FAA–2020–1175.
(j) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference of
the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless the AD specifies otherwise.
(i) Page 1–2A of Section 1, Operating
Limitations, and page 2–8 of Section 2,
Normal Procedures, of Bell Model 206B
Rotorcraft Flight Manual (RFM) BHT–206B–
FM–1, Revision B–54, dated May 30, 2018.
(ii) Page 1–5 of Section 1, Limitations, and
page 2–10 of Section 2, Normal Procedures,
of Bell Model 206B3 RFM BHT–206B3–FM–
1, Revision 17, dated May 30, 2018.
(iii) Page 1–4B of Section 1, Operating
Limitations, and page 2–10 of Section 2,
Normal Procedures, of Bell Model 206L RFM
BHT–206L–FM–1, Revision 31, dated May
30, 2018.
(3) For service information identified in
this AD, contact Bell Textron Canada
Limited, 12,800 Rue de l’Avenir, Mirabel,
Quebec J7J1R4; telephone (450) 437–2862 or
(800) 363–8023; fax (450) 433–0272; or at
https://www.bellcustomer.com.
(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: fedreg.legal@nara.gov, or go to:
https://www.archives.gov/federal-register/cfr/
ibr-locations.html.
Issued on May 12, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021–12040 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–2020–1170; Project
Identifier MCAI–2020–00720–R; Amendment
39–21575; AD 2021–11–13]
RIN 2120–AA64
Airworthiness Directives; Bell Textron
Canada Limited Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
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The FAA is adopting a new
airworthiness directive (AD) for Bell
Textron Canada Limited (Bell) Model
429 helicopters. This AD requires
inspecting certain serial-numbered
Emergency Flotation System (EFS)
inflation hoses and depending on the
results of those inspections, marking
certain parts or removing certain parts
from service. This AD was prompted by
a report that a float compartment on an
EFS did not inflate. 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 a certain document listed in this AD
as of July 15, 2021.
ADDRESSES: For Safran Aerosystems
Services service information identified
in this final rule, contact Bell Textron
Canada Limited, 12,800 Rue de l’Avenir,
Mirabel, Quebec J7J1R4; telephone 450–
437–2862 or 800–363–8023; fax 450–
433–0272; or at https://
www.bellcustomer.com. You may view
the referenced service information at the
FAA, Office of the Regional Counsel,
Southwest Region, 10101 Hillwood
Pkwy., Room 6N–321, Fort Worth, TX
76177. It is also available on the internet
at https://www.regulations.gov by
searching for and locating Docket No.
FAA–2020–1170.
SUMMARY:
Examining the AD Docket
You may examine the AD docket at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2020–1170; 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, the Transport Canada AD, any
service information that is incorporated
by reference, any comments received,
and other information. The street
address for Docket Operations is U.S.
Department of Transportation, Docket
Operations, M–30, West Building
Ground Floor, Room W12–140, 1200
New Jersey Avenue SE, Washington, DC
20590.
FOR FURTHER INFORMATION CONTACT: Matt
Fuller, AD Program Manager,
Operational Safety Branch,
Airworthiness Products Section,
General Aviation & Rotorcraft Unit,
FAA, 10101 Hillwood Pkwy., Fort
Worth, TX 76177; telephone 817–222–
5110; email matthew.fuller@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
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Federal Register / Vol. 86, No. 110 / Thursday, June 10, 2021 / Rules and Regulations
part 39 by adding an AD that would
apply to Bell Model 429 helicopters
with a Bell EFS kit part number (P/N)
429–706–069–101/–103/–105/–121/–
123/–125/–139/–141/–143/or –157
manufactured before July 2019, with a
float supply hose manufactured before
January 2014, installed, except for float
supply hoses marked with ‘‘SB 025–69–
21’’ above the external identification
marking. The NPRM published in the
Federal Register on March 23, 2021 (86
FR 15434). In the NPRM, the FAA
proposed to require within 100 hours
time-in-service (TIS), removing each
EFS supply hose and inspecting each
end (also referred to as fitting or banjo)
of the EFS supply hose using a certain
plastic cable tie, and depending on the
results of those inspections, removing
from service certain parts and replacing
those parts with airworthy parts. The
NPRM also proposed to require marking
a green dot on the base of certain supply
hoses and writing ‘‘SB 025–69–21’’
above the external identification
marking of the EFS with indelible ink.
Finally, the NPRM proposed to prohibit
installing any EFS supply hose
manufactured before January 2014
unless it has been inspected in
accordance with the NPRM. The NPRM
was prompted by Canadian AD CF–
2020–21R1, issued August 19, 2020
(Transport Canada AD CF–2020–21R1),
by Transport Canada, which is the
aviation authority for Canada, to correct
an unsafe condition for all serialnumbered Bell Model 429 helicopters.
Transport Canada advises that during
maintenance on an EFS, the third
compartment of the left forward float
did not inflate. Transport Canada also
advises that an investigation determined
the supply hose for the gas flow from
the pressurized cylinder to the float
compartment was blocked due to a
manufacturing defect. Bell advised that
similar supply hoses are installed on
various EFS part numbers, which could
be installed on different helicopter type
designs. Transport Canada further
advises that this condition, if not
detected and corrected, could result in
partial inflation of the EFS during an
emergency landing on water, preventing
a timely egress from the helicopter, and
injury to helicopter occupants.
Accordingly, Transport Canada AD
CF–2020–21R1 requires a one-time
special detailed inspection of the
affected system to verify that there is no
blockage through the EFS supply hoses
and replacement, as required, of the
affected supply hoses. Transport Canada
AD CF–2020–21R1 also renders any
affected EFS supply hoses not eligible as
VerDate Sep<11>2014
15:59 Jun 09, 2021
Jkt 253001
a replacement part on Bell Model 429
helicopters.
Discussion of Final Airworthiness
Directive
Comments
The FAA received no comments on
the NPRM or on the determination of
the costs.
Conclusion
These helicopters have been approved
by the aviation authority of Canada and
are approved for operation in the United
States. Pursuant to the FAA’s bilateral
agreement with Canada, Transport
Canada, its technical representative, has
notified the FAA of the unsafe condition
described in its AD. The FAA reviewed
the relevant data and determined that
air safety requires adopting this AD as
proposed. Accordingly, the FAA is
issuing this AD to address the unsafe
condition on these helicopters.
Related Service Information Under 1
CFR Part 51
The FAA reviewed Safran
Aerosystems Services Service Bulletin
No. 025–69–21, Revision 00, dated
March 23, 2020 (SB 025–69–21). SB
025–69–21 is attached to Bell Alert
Service Bulletin No. 429–20–52, dated
March 30, 2020 (ASB 429–20–52). SB
025–69–21 is incorporated by reference
in this AD. ASB 429–20–52 is not
incorporated by reference in this AD. SB
025–69–21 specifies, for certain EFSs
manufactured before July 2019, and any
float supply hose manufactured before
January 2014, performing a special
inspection to verify that there is no
blockage through the float supply hoses
of the EFS inflation system.
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.
Differences Between This AD and the
Transport Canada AD
The Transport Canada AD requires
compliance within 600 hours air time or
within the next 24-month inspection of
the EFS, whichever occurs first, whereas
this AD requires compliance within 100
hours TIS. The Transport Canada AD
limits the applicability to certain EFS
supply hoses listed in SB 025–69–21,
whereas this AD applies to certain EFS
supply hoses manufactured before
January 2014 but excludes EFS supply
hoses marked with ‘‘SB 025–69–21.’’
Costs of Compliance
The FAA estimates that this AD
affects 110 helicopters of U.S. Registry
and that operators may incur the
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30769
following costs in order to comply with
this AD. Labor costs are estimated at $85
per work-hour.
Removing and inspecting each EFS
supply hose will take about 0.75 workhour, for an estimated cost of $64 per
hose.
Installing or replacing each EFS
supply hose will take about 0.10 workhour with a minimal parts cost, for an
estimated cost of $9 per hose.
Marking each EFS supply hose with a
green dot and the applicable service
bulletin number will take a minimal
amount of time at a nominal cost.
According to Safran’s service
information, some of the costs of this
AD may be covered under warranty,
thereby reducing the cost impact on
affected individuals. The FAA does not
control warranty coverage by Safran;
accordingly, all costs are included in
this cost estimate.
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. Subtitle VII:
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
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
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Federal Register / Vol. 86, No. 110 / Thursday, June 10, 2021 / Rules and Regulations
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:
■
2021–11–13 Bell Textron Canada Limited:
Amendment 39–21575; Docket No.
FAA–2020–1170; Project Identifier
MCAI–2020–00720–R.
(a) Applicability
This airworthiness directive (AD) applies
to Bell Textron Canada Limited (Bell) Model
429 helicopters, certificated in any category,
with a Bell Emergency Flotation System
(EFS) kit part number (P/N) 429–706–069–
101/–103/–105/–121/–123/–125/–139/–141/–
143/or –157 manufactured before July 2019,
with a float supply hose manufactured before
January 2014, installed, except for float
supply hoses marked with ‘‘SB 025–69–21’’
above the external identification marking.
(b) Unsafe Condition
This AD defines the unsafe condition as a
blocked float supply hose installed on an
EFS. This condition could result in partial
inflation of an EFS float during an emergency
landing on water and subsequently
preventing a timely egress from the
helicopter.
(c) Effective Date
This AD is effective July 15, 2021.
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(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 100 hours time-in-service (TIS):
(i) Remove each EFS supply hose from the
float and inspect each end of the EFS supply
hose by inserting a plastic cable tie, 300 mm
minimum × 5 mm maximum (11.811 in.
minimum × .196 in. maximum), into the
holes of the related fitting as shown in Figure
1 of Safran Aerosystems Services Service
Bulletin No. 025–69–21, Revision 00, dated
March 23, 2020 (SB 025–69–21).
Note 1 to paragraph (e)(1)(i): Each end of
the supply hose may also be referred to as
fitting or banjo.
VerDate Sep<11>2014
15:59 Jun 09, 2021
Jkt 253001
(ii) If the cable tie does not pass through
the hose, before further flight, remove the
EFS supply hose from service and replace it
with an airworthy part.
(iii) If the cable tie passes through the
supply hose, mark a green dot with indelible
ink on the base of the supply hose and write
‘‘SB 025–69–21’’ above the external
identification marking of the EFS with
indelible ink.
(2) As of the effective date of this AD, do
not install an EFS supply hose manufactured
before January 2014 on any helicopter unless
the requirements in paragraph (e)(1) of this
AD have been completed.
(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 of the International Validation
Branch, send it to the attention of the person
identified in paragraph (g)(1) 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.
(g) Related Information
(1) For more information about this AD,
contact Matt Fuller, AD Program Manager,
Operational Safety Branch, Airworthiness
Products Section, General Aviation &
Rotorcraft Unit, FAA, 10101 Hillwood Pkwy.,
Fort Worth, TX 76177; telephone 817–222–
5110; email matthew.fuller@faa.gov.
(2) The subject of this AD is addressed in
Transport Canada AD CF–2020–212R1, dated
August 19, 2020. You may view the
Transport Canada AD on the internet at
https://www.regulations.gov in Docket No.
FAA–2020–1170.
(h) 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) Safran Aerosystems Services Service
Bulletin No. 025–69–21, Revision 00, dated
March 23, 2020 (SB 025–69–21).
Note 2 to paragraph (h)(2)(i): SB 025–69–
21 is attached to Bell Alert Service Bulletin
No. 429–20–52, dated March 30, 2020, which
is not incorporated by reference in this AD.
(ii) [Reserved]
(3) As the design approval holder for the
product identified in paragraph (a) of this
AD, contact Bell Textron Canada Limited for
the Safran Aerosystems Services service
information identified in this AD, at Bell
Textron Canada Limited, 12,800 Rue de
l’Avenir, Mirabel, Quebec J7J1R4; telephone
450–437–2862 or 800–363–8023; fax 450–
PO 00000
Frm 00018
Fmt 4700
Sfmt 4700
433–0272; or at https://
www.bellcustomer.com.
(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: fedreg.legal@nara.gov, or go to:
https://www.archives.gov/federal-register/cfr/
ibr-locations.html.
Issued on May 18, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021–12042 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–2021–0187; Project
Identifier AD–2020–01664–E; Amendment
39–21583; AD 2021–11–21]
RIN 2120–AA64
Airworthiness Directives; CFM
International, S.A. Turbofan Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
CFM International, S.A. (CFM) LEAP–
1A model turbofan engines. This AD
was prompted by a report of a
manufacturing quality escape found
during an inspection of a high-pressure
turbine (HPT) case. This AD requires the
removal from service of the affected
HPT case. 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 a certain publication listed in this AD
as of July 15, 2021.
ADDRESSES: For service information
identified in this final rule, contact CFM
International, S.A., Aviation Operations
Center, 1 Neumann Way, M/D Room
285, Cincinnati, OH 45125; phone: (877)
432–3272; email:
aviation.fleetsupport@ge.com. You may
view this service information at the
FAA, Airworthiness Products Section,
Operational Safety Branch, 1200 District
SUMMARY:
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]]>Agencies
[Federal Register Volume 86, Number 110 (Thursday, June 10, 2021)]
[Rules and Regulations]
[Pages 30768-30770]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-12042]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-1170; Project Identifier MCAI-2020-00720-R;
Amendment 39-21575; AD 2021-11-13]
RIN 2120-AA64
Airworthiness Directives; Bell Textron Canada Limited Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
Bell Textron Canada Limited (Bell) Model 429 helicopters. This AD
requires inspecting certain serial-numbered Emergency Flotation System
(EFS) inflation hoses and depending on the results of those
inspections, marking certain parts or removing certain parts from
service. This AD was prompted by a report that a float compartment on
an EFS did not inflate. 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 a certain document listed in this AD as of July 15, 2021.
ADDRESSES: For Safran Aerosystems Services service information
identified in this final rule, contact Bell Textron Canada Limited,
12,800 Rue de l'Avenir, Mirabel, Quebec J7J1R4; telephone 450-437-2862
or 800-363-8023; fax 450-433-0272; or at https://www.bellcustomer.com.
You may view the referenced service information at the FAA, Office of
the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-
321, Fort Worth, TX 76177. It is also available on the internet at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2020-1170.
Examining the AD Docket
You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2020-1170; 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, the
Transport Canada AD, any service information that is incorporated by
reference, any comments received, and other information. The street
address for Docket Operations is U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Matt Fuller, AD Program Manager,
Operational Safety Branch, Airworthiness Products Section, General
Aviation & Rotorcraft Unit, FAA, 10101 Hillwood Pkwy., Fort Worth, TX
76177; telephone 817-222-5110; email [email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR
[[Page 30769]]
part 39 by adding an AD that would apply to Bell Model 429 helicopters
with a Bell EFS kit part number (P/N) 429-706-069-101/-103/-105/-121/-
123/-125/-139/-141/-143/or -157 manufactured before July 2019, with a
float supply hose manufactured before January 2014, installed, except
for float supply hoses marked with ``SB 025-69-21'' above the external
identification marking. The NPRM published in the Federal Register on
March 23, 2021 (86 FR 15434). In the NPRM, the FAA proposed to require
within 100 hours time-in-service (TIS), removing each EFS supply hose
and inspecting each end (also referred to as fitting or banjo) of the
EFS supply hose using a certain plastic cable tie, and depending on the
results of those inspections, removing from service certain parts and
replacing those parts with airworthy parts. The NPRM also proposed to
require marking a green dot on the base of certain supply hoses and
writing ``SB 025-69-21'' above the external identification marking of
the EFS with indelible ink. Finally, the NPRM proposed to prohibit
installing any EFS supply hose manufactured before January 2014 unless
it has been inspected in accordance with the NPRM. The NPRM was
prompted by Canadian AD CF-2020-21R1, issued August 19, 2020 (Transport
Canada AD CF-2020-21R1), by Transport Canada, which is the aviation
authority for Canada, to correct an unsafe condition for all serial-
numbered Bell Model 429 helicopters. Transport Canada advises that
during maintenance on an EFS, the third compartment of the left forward
float did not inflate. Transport Canada also advises that an
investigation determined the supply hose for the gas flow from the
pressurized cylinder to the float compartment was blocked due to a
manufacturing defect. Bell advised that similar supply hoses are
installed on various EFS part numbers, which could be installed on
different helicopter type designs. Transport Canada further advises
that this condition, if not detected and corrected, could result in
partial inflation of the EFS during an emergency landing on water,
preventing a timely egress from the helicopter, and injury to
helicopter occupants.
Accordingly, Transport Canada AD CF-2020-21R1 requires a one-time
special detailed inspection of the affected system to verify that there
is no blockage through the EFS supply hoses and replacement, as
required, of the affected supply hoses. Transport Canada AD CF-2020-
21R1 also renders any affected EFS supply hoses not eligible as a
replacement part on Bell Model 429 helicopters.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the costs.
Conclusion
These helicopters have been approved by the aviation authority of
Canada and are approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with Canada, Transport Canada, its
technical representative, has notified the FAA of the unsafe condition
described in its AD. The FAA reviewed the relevant data and determined
that air safety requires adopting this AD as proposed. Accordingly, the
FAA is issuing this AD to address the unsafe condition on these
helicopters.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Safran Aerosystems Services Service Bulletin No.
025-69-21, Revision 00, dated March 23, 2020 (SB 025-69-21). SB 025-69-
21 is attached to Bell Alert Service Bulletin No. 429-20-52, dated
March 30, 2020 (ASB 429-20-52). SB 025-69-21 is incorporated by
reference in this AD. ASB 429-20-52 is not incorporated by reference in
this AD. SB 025-69-21 specifies, for certain EFSs manufactured before
July 2019, and any float supply hose manufactured before January 2014,
performing a special inspection to verify that there is no blockage
through the float supply hoses of the EFS inflation system.
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.
Differences Between This AD and the Transport Canada AD
The Transport Canada AD requires compliance within 600 hours air
time or within the next 24-month inspection of the EFS, whichever
occurs first, whereas this AD requires compliance within 100 hours TIS.
The Transport Canada AD limits the applicability to certain EFS supply
hoses listed in SB 025-69-21, whereas this AD applies to certain EFS
supply hoses manufactured before January 2014 but excludes EFS supply
hoses marked with ``SB 025-69-21.''
Costs of Compliance
The FAA estimates that this AD affects 110 helicopters of U.S.
Registry and that operators may incur the following costs in order to
comply with this AD. Labor costs are estimated at $85 per work-hour.
Removing and inspecting each EFS supply hose will take about 0.75
work-hour, for an estimated cost of $64 per hose.
Installing or replacing each EFS supply hose will take about 0.10
work-hour with a minimal parts cost, for an estimated cost of $9 per
hose.
Marking each EFS supply hose with a green dot and the applicable
service bulletin number will take a minimal amount of time at a nominal
cost.
According to Safran's service information, some of the costs of
this AD may be covered under warranty, thereby reducing the cost impact
on affected individuals. The FAA does not control warranty coverage by
Safran; accordingly, all costs are included in this cost estimate.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
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
[[Page 30770]]
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:
2021-11-13 Bell Textron Canada Limited: Amendment 39-21575; Docket
No. FAA-2020-1170; Project Identifier MCAI-2020-00720-R.
(a) Applicability
This airworthiness directive (AD) applies to Bell Textron Canada
Limited (Bell) Model 429 helicopters, certificated in any category,
with a Bell Emergency Flotation System (EFS) kit part number (P/N)
429-706-069-101/-103/-105/-121/-123/-125/-139/-141/-143/or -157
manufactured before July 2019, with a float supply hose manufactured
before January 2014, installed, except for float supply hoses marked
with ``SB 025-69-21'' above the external identification marking.
(b) Unsafe Condition
This AD defines the unsafe condition as a blocked float supply
hose installed on an EFS. This condition could result in partial
inflation of an EFS float during an emergency landing on water and
subsequently preventing a timely egress from the helicopter.
(c) Effective Date
This AD is effective July 15, 2021.
(d) Compliance
You are responsible for performing each action required by this
AD within the specified compliance time unless it has already been
accomplished prior to that time.
(e) Required Actions
(1) Within 100 hours time-in-service (TIS):
(i) Remove each EFS supply hose from the float and inspect each
end of the EFS supply hose by inserting a plastic cable tie, 300 mm
minimum x 5 mm maximum (11.811 in. minimum x .196 in. maximum), into
the holes of the related fitting as shown in Figure 1 of Safran
Aerosystems Services Service Bulletin No. 025-69-21, Revision 00,
dated March 23, 2020 (SB 025-69-21).
Note 1 to paragraph (e)(1)(i): Each end of the supply hose may
also be referred to as fitting or banjo.
(ii) If the cable tie does not pass through the hose, before
further flight, remove the EFS supply hose from service and replace
it with an airworthy part.
(iii) If the cable tie passes through the supply hose, mark a
green dot with indelible ink on the base of the supply hose and
write ``SB 025-69-21'' above the external identification marking of
the EFS with indelible ink.
(2) As of the effective date of this AD, do not install an EFS
supply hose manufactured before January 2014 on any helicopter
unless the requirements in paragraph (e)(1) of this AD have been
completed.
(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 of the International Validation Branch, send
it to the attention of the person identified in paragraph (g)(1) 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.
(g) Related Information
(1) For more information about this AD, contact Matt Fuller, AD
Program Manager, Operational Safety Branch, Airworthiness Products
Section, General Aviation & Rotorcraft Unit, FAA, 10101 Hillwood
Pkwy., Fort Worth, TX 76177; telephone 817-222-5110; email
[email protected].
(2) The subject of this AD is addressed in Transport Canada AD
CF-2020-212R1, dated August 19, 2020. You may view the Transport
Canada AD on the internet at https://www.regulations.gov in Docket
No. FAA-2020-1170.
(h) 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) Safran Aerosystems Services Service Bulletin No. 025-69-21,
Revision 00, dated March 23, 2020 (SB 025-69-21).
Note 2 to paragraph (h)(2)(i): SB 025-69-21 is attached to Bell
Alert Service Bulletin No. 429-20-52, dated March 30, 2020, which is
not incorporated by reference in this AD.
(ii) [Reserved]
(3) As the design approval holder for the product identified in
paragraph (a) of this AD, contact Bell Textron Canada Limited for
the Safran Aerosystems Services service information identified in
this AD, at Bell Textron Canada Limited, 12,800 Rue de l'Avenir,
Mirabel, Quebec J7J1R4; telephone 450-437-2862 or 800-363-8023; fax
450-433-0272; or at https://www.bellcustomer.com.
(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: [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on May 18, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2021-12042 Filed 6-9-21; 8:45 am]
BILLING CODE 4910-13-P
