Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters, 7701-7703 [2022-02757]
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Federal Register / Vol. 87, No. 28 / Thursday, February 10, 2022 / Rules and Regulations
(k) Alternative Methods of Compliance
(AMOCs)
DEPARTMENT OF TRANSPORTATION
(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 (l) 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.
Federal Aviation Administration
(l) Related Information
For more information about this AD,
contact Hal Jensen, Aerospace Engineer,
Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 950 L’Enfant
Plaza N SW, Washington, DC 20024;
telephone (202) 267–9167; email hal.jensen@
faa.gov.
jspears on DSK121TN23PROD with RULES1
(m) 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 Union Aviation Safety Agency
(EASA) AD 2021–0126, dated May 10, 2021.
(ii) [Reserved]
(3) For EASA AD 2021–0126, 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.
(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–2021–1184.
(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
fr.inspection@nara.gov, or go to https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on January 7, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022–02760 Filed 2–9–22; 8:45 am]
BILLING CODE 4910–13–P
VerDate Sep<11>2014
16:22 Feb 09, 2022
Jkt 256001
14 CFR Part 39
[Docket No. FAA–2021–1007; Project
Identifier MCAI–2021–00324–R; Amendment
39–21917; AD 2022–02–20]
RIN 2120–AA64
Airworthiness Directives; Airbus
Helicopters Deutschland GmbH (AHD)
Helicopters
The FAA is adopting a new
airworthiness directive (AD) for all
Airbus Helicopters Deutschland GmbH
(AHD) Model MBB–BK 117 C–2 and
MBB–BK 117 D–2 helicopters. This AD
was prompted by report that a collective
bellcrank-K was found incorrectly
installed on a helicopter. This AD
requires inspecting the collective
bellcrank-K to determine if it is
correctly installed and has a correct
position marking and, depending on the
findings, applicable corrective actions,
as specified in a European Union
Aviation Safety Agency (EASA) AD,
which is incorporated by reference. This
AD also allows installation of an
affected collective bellcrank-K, provided
certain instructions are followed. The
FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective March 17,
2022.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of March 17, 2022.
ADDRESSES: For EASA material
incorporated by reference (IBR) in this
final rule, contact 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 the
EASA material on the EASA website at
https://ad.easa.europa.eu. 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 at https://www.regulations.gov
by searching for and locating Docket No.
FAA–2021–1007.
SUMMARY:
Examining the AD Docket
You may examine the AD docket at
https://www.regulations.gov by
Frm 00023
Fmt 4700
Sfmt 4700
searching for and locating Docket No.
FAA–2021–1007; 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 EASA AD, 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.
Hal
Jensen, Aerospace Engineer, Operational
Safety Branch, FAA, 950 L’Enfant Plaza
SW, Washington, DC 20024; telephone
(202) 267–9167; email hal.jensen@
faa.gov.
FOR FURTHER INFORMATION CONTACT:
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
PO 00000
7701
SUPPLEMENTARY INFORMATION:
Background
EASA, which is the Technical Agent
for the Member States of the European
Union, has issued EASA AD 2021–0074,
dated March 15, 2021 (EASA AD 2021–
0074), to correct an unsafe condition for
all Airbus Helicopters Deutschland
GmbH (AHD) (formerly Eurocopter
Deutschland GmbH; and Airbus
Helicopters Inc., formerly American
Eurocopter LLC) Model MBB–BK117 C–
2 and MBB–BK117 D–2 helicopters.
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to all Airbus Helicopters
Deutschland GmbH Model MBB–BK 117
C–2 and MBB–BK 117 D–2 helicopters.
The NPRM published in the Federal
Register on November 26, 2021 (86 FR
67364). The NPRM was prompted by a
report that a collective bellcrank-K
(affected part) was found incorrectly
installed on a helicopter. Subsequent
investigations revealed that the affected
part was an in-service replacement, and
that the position marking on that part
was incorrect. The NPRM proposed to
require inspecting the collective
bellcrank-K to determine if it is
correctly installed and has a correct
position marking and, depending on the
findings, applicable corrective actions,
as specified in EASA AD 2021–0074.
The NPRM also proposed to allow
installation of an affected collective
bellcrank-K, provided certain
instructions are followed.
The FAA is issuing this AD to address
incorrect installation of a collective
bellcrank-K, which could lead to
unwanted collective input, resulting in
reduced control of the helicopter. See
EASA AD 2021–0074 for additional
background information.
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Federal Register / Vol. 87, No. 28 / Thursday, February 10, 2022 / Rules and Regulations
Discussion of Final Airworthiness
Directive
for minor editorial changes, this AD is
adopted as proposed in the NPRM.
Comments
Related Service Information Under 1
CFR Part 51
The FAA received no comments on
the NPRM or on the determination of
the costs.
Conclusion
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 about 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. Except
EASA AD 2021–0074 requires a onetime inspection of an affected part for
correct installation by measuring the
distance between the front edge of the
bearing block and the front edge of the
affected part, and for correct application
of position markings, and, depending on
the findings, accomplishment of
applicable corrective actions. If an
affected part is incorrectly installed, the
corrective actions include inspecting for
signs of chafing on the bearing block,
the control lever, the forked lever, the
sliding sleeve, and the bearing ring,
replacing any parts that have signs of
chafing, and installing a serviceable
bellcrank-K with an applied position
marking. If an affected part is correctly
installed but the position marking is not
correct, the corrective actions include
re-working the affected part or replacing
the affected part with a serviceable part
that has an applied position marking.
EASA AD 2021–0074 also allows
installation of an affected part, provided
certain instructions are followed.
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 140 helicopters of U.S. Registry.
The FAA estimates the following costs
to comply with this AD.
ESTIMATED COSTS
Action
Labor cost
Inspection for correct installation and position
marking.
0.50 work-hour × $85 per hour = $42.50 .......
The FAA estimates the following
costs to do any necessary replacements
or rework that would be required based
on the results of the inspection. The
agency has no way of determining the
Cost per
product
Parts cost
$0
Cost on U.S.
operators
$42.50
$5,950
number of helicopters that might need
this replacement or rework:
jspears on DSK121TN23PROD with RULES1
ON-CONDITION COSTS
Action
Labor cost
Parts cost
Replace collective bellcrank-K .....................................
Rework collective bellcrank-K ......................................
8 work-hours × $85 per hour = $680 ...........................
2 work-hours × $85 per hour = $170 ...........................
Cost per
product
$4,018
0
$4,698
170
Authority for This Rulemaking
Regulatory Findings
List of Subjects in 14 CFR Part 39
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.
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.
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
VerDate Sep<11>2014
16:22 Feb 09, 2022
Jkt 256001
PO 00000
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:
■
2022–02–20 Airbus Helicopters
Deutschland GmbH (AHD): Amendment
Frm 00024
Fmt 4700
Sfmt 4700
E:\FR\FM\10FER1.SGM
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Federal Register / Vol. 87, No. 28 / Thursday, February 10, 2022 / Rules and Regulations
39–21917; Docket No. FAA–2021–1007;
Project Identifier MCAI–2021–00324–R.
(a) Effective Date
This airworthiness directive (AD) is
effective March 17, 2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Airbus Helicopters
Deutschland GmbH (AHD) Model MBB–BK
117 C–2 and MBB–BK 117 D–2 helicopters,
certificated in any category.
(d) Subject
Joint Aircraft Service Component (JASC)
Code: 6230, Main Rotor Mast/Swashplate.
(e) Unsafe Condition
This AD was prompted by a report that a
collective bellcrank-K (affected part) was
found incorrectly installed on a helicopter.
Subsequent investigations found that the
affected part was an in-service replacement,
and that the position marking on that part
was incorrect. The FAA is issuing this AD to
address incorrect installation of a collective
bellcrank-K, which could lead to unwanted
collective input, resulting in reduced control
of the helicopter.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
jspears on DSK121TN23PROD with RULES1
(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, European Union Aviation
Safety Agency (EASA) AD 2021–0074, dated
March 15, 2021 (EASA AD 2021–0074).
(h) Exceptions to EASA AD 2021–0074
(1) Where EASA AD 2021–0074 requires
compliance in terms of flight hours, this AD
requires using hours time-in-service.
(2) Where EASA AD 2021–0074 refers to its
effective date, this AD requires using the
effective date of this AD.
(3) Where the service information
referenced in EASA AD 2021–0074 specifies
discarding a part, this AD requires removing
that part from service.
(4) Where the service information
referenced in EASA AD 2021–0074 specifies
contacting Airbus Helicopters for
instructions to rework a bellcrank-K, the
rework must be accomplished using a
method approved by the Manager, General
Aviation & Rotorcraft Section, International
Validation Branch, FAA; or EASA; or Airbus
Helicopters’ EASA Design Organization
Approval (DOA). If approved by the DOA,
the approval must include the DOAauthorized signature.
(5) Where the service information
referenced in EASA AD 2021–0074 specifies
to ‘‘forecast the compliance time of Part IV
and schedule the accomplishment
accordingly,’’ for clarification, this AD
requires doing the correction of the position
marking of the bellcrank-K at the time
specified in paragraph (3) of EASA AD 2021–
0074.
VerDate Sep<11>2014
16:22 Feb 09, 2022
Jkt 256001
(6) Where the service information
referenced in EASA AD 2021–0074 specifies
contacting Airbus Helicopters if there is
mechanical damage or corrosion on the
bushings of the bellcrank assembly, this AD
does not require that action.
(7) This AD does not mandate compliance
with the ‘‘Remarks’’ section of EASA AD
2021–0074.
(i) No Reporting Requirement
Although the service information
referenced in EASA AD 2021–0074 specifies
to submit certain information to the
manufacturer, this AD does not include that
requirement.
(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.
(k) Related Information
For more information about this AD,
contact Hal Jensen, Aerospace Engineer,
Operational Safety Branch, FAA, 950
L’Enfant Plaza SW, Washington, DC 20024;
telephone (202) 267–9167; email hal.jensen@
faa.gov.
(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 this AD specifies otherwise.
(i) European Union Aviation Safety Agency
(EASA) AD 2021–0074, dated March 15,
2021.
(ii) [Reserved]
(3) For EASA AD 2021–0074, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu. You may
find the EASA material on the EASA website
at https://ad.easa.europa.eu.
(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
at https://www.regulations.gov by searching
for and locating Docket No. FAA–2021–1007.
(5) You may view this material that is
incorporated by reference at the National
Archives and Records Administration
PO 00000
Frm 00025
Fmt 4700
Sfmt 4700
7703
(NARA). For information on the availability
of this material at NARA, email
fr.inspection@nara.gov, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on January 18, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022–02757 Filed 2–9–22; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2021–1014; Project
Identifier MCAI–2021–00428–T; Amendment
39–21928; AD 2022–03–11]
RIN 2120–AA64
Airworthiness Directives; Bombardier,
Inc., Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for all
Bombardier, Inc., Model BD–100–1A10
airplanes. This AD was prompted by a
report that the design of the spoiler
control system causes certain engine
indication and crew alerting system
(EICAS) messages to be posted
intermittently and repetitively during
flight and on the ground, and
flightcrews must action the appropriate
checklist each time these messages
appear. This AD requires revising the
Non-Normal Procedures section of the
existing airplane flight manual (AFM)
associated with the spoiler electronic
control unit (SECU) EICAS messages.
The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective March 17,
2022.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of March 17, 2022.
ADDRESSES: For service information
identified in this final rule, contact
Bombardier Business Aircraft Customer
Response Center, 400 Coˆte-Vertu Road
West, Dorval, Que´bec H4S 1Y9, Canada;
telephone 514–855–2999; email ac.yul@
aero.bombardier.com; internet https://
www.bombardier.com. You may view
this service information at the FAA,
Airworthiness Products Section,
Operational Safety Branch, 2200 South
216th St., Des Moines, WA. For
SUMMARY:
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]]>Agencies
[Federal Register Volume 87, Number 28 (Thursday, February 10, 2022)]
[Rules and Regulations]
[Pages 7701-7703]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-02757]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-1007; Project Identifier MCAI-2021-00324-R;
Amendment 39-21917; AD 2022-02-20]
RIN 2120-AA64
Airworthiness Directives; Airbus Helicopters Deutschland GmbH
(AHD) Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Airbus Helicopters Deutschland GmbH (AHD) Model MBB-BK 117 C-2 and MBB-
BK 117 D-2 helicopters. This AD was prompted by report that a
collective bellcrank-K was found incorrectly installed on a helicopter.
This AD requires inspecting the collective bellcrank-K to determine if
it is correctly installed and has a correct position marking and,
depending on the findings, applicable corrective actions, as specified
in a European Union Aviation Safety Agency (EASA) AD, which is
incorporated by reference. This AD also allows installation of an
affected collective bellcrank-K, provided certain instructions are
followed. The FAA is issuing this AD to address the unsafe condition on
these products.
DATES: This AD is effective March 17, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of March 17,
2022.
ADDRESSES: For EASA material incorporated by reference (IBR) in this
final rule, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne,
Germany; telephone +49 221 8999 000; email [email protected]; internet
www.easa.europa.eu. You may find the EASA material on the EASA website
at https://ad.easa.europa.eu. 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 at https://www.regulations.gov by searching for and
locating Docket No. FAA-2021-1007.
Examining the AD Docket
You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-1007; 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
EASA AD, 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.
FOR FURTHER INFORMATION CONTACT: Hal Jensen, Aerospace Engineer,
Operational Safety Branch, FAA, 950 L'Enfant Plaza SW, Washington, DC
20024; telephone (202) 267-9167; email [email protected].
SUPPLEMENTARY INFORMATION:
Background
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2021-0074, dated March 15, 2021
(EASA AD 2021-0074), to correct an unsafe condition for all Airbus
Helicopters Deutschland GmbH (AHD) (formerly Eurocopter Deutschland
GmbH; and Airbus Helicopters Inc., formerly American Eurocopter LLC)
Model MBB-BK117 C-2 and MBB-BK117 D-2 helicopters.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to all Airbus Helicopters
Deutschland GmbH Model MBB-BK 117 C-2 and MBB-BK 117 D-2 helicopters.
The NPRM published in the Federal Register on November 26, 2021 (86 FR
67364). The NPRM was prompted by a report that a collective bellcrank-K
(affected part) was found incorrectly installed on a helicopter.
Subsequent investigations revealed that the affected part was an in-
service replacement, and that the position marking on that part was
incorrect. The NPRM proposed to require inspecting the collective
bellcrank-K to determine if it is correctly installed and has a correct
position marking and, depending on the findings, applicable corrective
actions, as specified in EASA AD 2021-0074. The NPRM also proposed to
allow installation of an affected collective bellcrank-K, provided
certain instructions are followed.
The FAA is issuing this AD to address incorrect installation of a
collective bellcrank-K, which could lead to unwanted collective input,
resulting in reduced control of the helicopter. See EASA AD 2021-0074
for additional background information.
[[Page 7702]]
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 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 about 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. Except for minor editorial changes,
this AD is adopted as proposed in the NPRM.
Related Service Information Under 1 CFR Part 51
EASA AD 2021-0074 requires a one-time inspection of an affected
part for correct installation by measuring the distance between the
front edge of the bearing block and the front edge of the affected
part, and for correct application of position markings, and, depending
on the findings, accomplishment of applicable corrective actions. If an
affected part is incorrectly installed, the corrective actions include
inspecting for signs of chafing on the bearing block, the control
lever, the forked lever, the sliding sleeve, and the bearing ring,
replacing any parts that have signs of chafing, and installing a
serviceable bellcrank-K with an applied position marking. If an
affected part is correctly installed but the position marking is not
correct, the corrective actions include re-working the affected part or
replacing the affected part with a serviceable part that has an applied
position marking. EASA AD 2021-0074 also allows installation of an
affected part, provided certain instructions are followed.
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 140 helicopters of U.S.
Registry. The FAA estimates the following costs to comply with this AD.
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Inspection for correct installation 0.50 work-hour x $85 per $0 $42.50 $5,950
and position marking. hour = $42.50.
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary
replacements or rework that would be required based on the results of
the inspection. The agency has no way of determining the number of
helicopters that might need this replacement or rework:
On-Condition Costs
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product
----------------------------------------------------------------------------------------------------------------
Replace collective bellcrank-K................ 8 work-hours x $85 per hour = $4,018 $4,698
$680.
Rework collective bellcrank-K................. 2 work-hours x $85 per hour = 0 170
$170.
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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]
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2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2022-02-20 Airbus Helicopters Deutschland GmbH (AHD): Amendment
[[Page 7703]]
39-21917; Docket No. FAA-2021-1007; Project Identifier MCAI-2021-
00324-R.
(a) Effective Date
This airworthiness directive (AD) is effective March 17, 2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Airbus Helicopters Deutschland GmbH (AHD)
Model MBB-BK 117 C-2 and MBB-BK 117 D-2 helicopters, certificated in
any category.
(d) Subject
Joint Aircraft Service Component (JASC) Code: 6230, Main Rotor
Mast/Swashplate.
(e) Unsafe Condition
This AD was prompted by a report that a collective bellcrank-K
(affected part) was found incorrectly installed on a helicopter.
Subsequent investigations found that the affected part was an in-
service replacement, and that the position marking on that part was
incorrect. The FAA is issuing this AD to address incorrect
installation of a collective bellcrank-K, which could lead to
unwanted collective input, resulting in reduced control of the
helicopter.
(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, European Union Aviation Safety Agency (EASA) AD
2021-0074, dated March 15, 2021 (EASA AD 2021-0074).
(h) Exceptions to EASA AD 2021-0074
(1) Where EASA AD 2021-0074 requires compliance in terms of
flight hours, this AD requires using hours time-in-service.
(2) Where EASA AD 2021-0074 refers to its effective date, this
AD requires using the effective date of this AD.
(3) Where the service information referenced in EASA AD 2021-
0074 specifies discarding a part, this AD requires removing that
part from service.
(4) Where the service information referenced in EASA AD 2021-
0074 specifies contacting Airbus Helicopters for instructions to
rework a bellcrank-K, the rework must be accomplished using a method
approved by the Manager, General Aviation & Rotorcraft Section,
International Validation Branch, FAA; or EASA; or Airbus
Helicopters' EASA Design Organization Approval (DOA). If approved by
the DOA, the approval must include the DOA-authorized signature.
(5) Where the service information referenced in EASA AD 2021-
0074 specifies to ``forecast the compliance time of Part IV and
schedule the accomplishment accordingly,'' for clarification, this
AD requires doing the correction of the position marking of the
bellcrank-K at the time specified in paragraph (3) of EASA AD 2021-
0074.
(6) Where the service information referenced in EASA AD 2021-
0074 specifies contacting Airbus Helicopters if there is mechanical
damage or corrosion on the bushings of the bellcrank assembly, this
AD does not require that action.
(7) This AD does not mandate compliance with the ``Remarks''
section of EASA AD 2021-0074.
(i) No Reporting Requirement
Although the service information referenced in EASA AD 2021-0074
specifies to submit certain information to the manufacturer, this AD
does not include that requirement.
(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 Hal Jensen,
Aerospace Engineer, Operational Safety Branch, FAA, 950 L'Enfant
Plaza SW, Washington, DC 20024; telephone (202) 267-9167; email
[email protected].
(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 this AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) AD 2021-0074,
dated March 15, 2021.
(ii) [Reserved]
(3) For EASA AD 2021-0074, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
[email protected]. You may find the EASA material on the EASA
website at https://ad.easa.europa.eu.
(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 at https://www.regulations.gov by searching
for and locating Docket No. FAA-2021-1007.
(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 January 18, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2022-02757 Filed 2-9-22; 8:45 am]
BILLING CODE 4910-13-P
