Airworthiness Directives; General Electric Company Turbofan Engines, 8172-8174 [2022-03008]
Download as PDF
8172
Federal Register / Vol. 87, No. 30 / Monday, February 14, 2022 / Rules and Regulations
the procedures and tests identified as RC can
be done and the airplane can be put back in
an airworthy condition. Any substitutions or
changes to procedures or tests identified as
RC require approval of an AMOC.
(j) Related Information
For more information about this AD,
contact Vladimir Ulyanov, Aerospace
Engineer, Large Aircraft Section, FAA,
International Validation Branch, 2200 South
216th St., Des Moines, WA 98198; telephone
and fax 206–231–3229; email
vladimir.ulyanov@faa.gov.
(k) 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 2021–0136, dated June 4, 2021.
(ii) [Reserved]
(3) For EASA AD 2021–0136, contact
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 material at the FAA,
Airworthiness Products Section, Operational
Safety Branch, 2200 South 216th St., Des
Moines, WA. For information on the
availability of this material at the FAA, call
206–231–3195.
(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 24, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022–02996 Filed 2–11–22; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2021–1016; Project
Identifier AD–2021–00625–E; Amendment
39–21936; AD 2022–03–19]
jspears on DSK121TN23PROD with RULES1
RIN 2120–AA64
Airworthiness Directives; General
Electric Company Turbofan Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
VerDate Sep<11>2014
16:05 Feb 11, 2022
The FAA is adopting a new
airworthiness directive (AD) for all
General Electric Company (GE) Passport
20–17BB1A, Passport 20–18BB1A, and
Passport 20–19BB1A model turbofan
engines. This AD was prompted by a
report of a manufacturing quality escape
that requires a reduction to the life limit
of certain high-pressure turbine (HPT)
rotor stage 1 disks. This AD requires
revising the airworthiness limitations
section (ALS) of the existing
maintenance manual and the operator’s
existing approved continuous
airworthiness maintenance program
(CAMP) to incorporate a reduced life
limit for certain HPT rotor stage 1 disks.
The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective March 21,
2022.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of March 21, 2022.
ADDRESSES: For service information
identified in this final rule, contact
General Electric Company, 1 Neumann
Way, Cincinnati, OH 45215, United
States; phone: (513) 552–3272; email:
aviation.fleetsupport@ge.com; website:
www.ge.com. You may view this service
information at the FAA, Airworthiness
Products Section, Operational Safety
Branch, 1200 District Avenue,
Burlington, MA 01803. For information
on the availability of this material at the
FAA, call (817) 222–5110. It is also
available at https://www.regulations.gov
by searching for and locating Docket No.
FAA–2021–1016.
SUMMARY:
Examining the AD Docket
You may examine the AD docket at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2021–1016; 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.
FOR FURTHER INFORMATION CONTACT:
Scott Stevenson, Aviation Safety
Engineer, ECO Branch, FAA, 1200
District Avenue, Burlington, MA 01803;
phone: (781) 238–7132; fax: (781) 238–
7199; email: Scott.M.Stevenson@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
Jkt 256001
PO 00000
Frm 00034
Fmt 4700
Sfmt 4700
part 39 by adding an AD that would
apply to all GE Passport 20–17BB1A,
Passport 20–18BB1A, and Passport 20–
19BB1A model turbofan engines. The
NPRM published in the Federal
Register on November 29, 2021 (86 FR
67669). The NPRM was prompted by a
report from GE of a manufacturing
quality escape that identified a certain
population of HPT rotor stage 1 disks
that did not meet the design
specification. GE determined that
machining and inspection of the
affected HPT rotor stage 1 disks was
inconsistent with the engineering
drawing. Further analysis by GE
determined that the nonconformance at
the forward and aft hooks of the HPT
rotor stage 1 disks may cause the disks
to fail prematurely and, therefore, the
life limit of the affected HPT rotor stage
1 disks requires reduction. As a result,
GE decreased the life limit of the
affected HPT rotor stage 1 disks. In the
NPRM, the FAA proposed to require
revising the ALS of the GE Passport 20
Line Maintenance Manual, GEK 112062,
and the operator’s existing approved
CAMP to incorporate a reduced life
limit for certain HPT rotor stage 1 disks.
The FAA is issuing this AD to address
the unsafe condition on these products.
Discussion of Final Airworthiness
Directive
Comments
The FAA received one comment, from
GE. The following presents the
comment received on the NPRM and the
FAA’s response.
Request To Update Date of Service
Information
GE requested that the FAA correct the
date of GE Service Bulletin (SB)
PASSPORT20–A–72–00–0116–00A–
930A–D, Issue 002, in this AD from July
22, 2021, to August 13, 2021. GE
commented that the NPRM included the
date of the draft SB and not the date of
the published SB. GE stated that there
was no change to the document content
between the draft and publication dates.
The FAA agrees and has revised this
AD as requested.
Conclusion
The FAA reviewed the relevant data,
considered any comments received, 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
products. Except for minor editorial
changes and any other changes
described previously, this AD is
adopted as proposed in the NPRM.
None of the changes will increase the
economic burden on any operator.
E:\FR\FM\14FER1.SGM
14FER1
8173
Federal Register / Vol. 87, No. 30 / Monday, February 14, 2022 / Rules and Regulations
Related Service Information Under 1
CFR Part 51
The FAA reviewed GE SB
PASSPORT20–A–72–00–0116–00A–
930A–D, Issue 002, dated August 13,
2021. This service information describes
procedures for removing a certain
population of HPT rotor stage 1 disks
from service and provides serial
numbers of the affected HPT rotor stage
1 disks. 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
ADDRESSES.
Costs of Compliance
The FAA estimates that this AD
affects 78 engines installed on airplanes
of U.S. registry.
The FAA estimates the following
costs to comply with this AD:
jspears on DSK121TN23PROD with RULES1
ESTIMATED COSTS
Action
Labor cost
Revise the ALS of the Line Maintenance Manual and the operator’s existing approved CAMP.
1 work-hour × $85 per hour =
$85.
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.
(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.
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:
■
VerDate Sep<11>2014
16:05 Feb 11, 2022
Jkt 256001
Cost per
product
Parts cost
$0
Cost on U.S.
operators
$85
$6,630
(a) Effective Date
This airworthiness directive (AD) is
effective March 21, 2022.
(b) Affected ADs
None.
(c) Applicability
List of Subjects in 14 CFR Part 39
This AD applies to General Electric
Company (GE) Passport 20–17BB1A, Passport
20–18BB1A, and Passport 20–19BB1A model
turbofan engines.
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
(d) Subject
Joint Aircraft System Component (JASC)
Code 7250, Turbine Section.
The Amendment
(e) Unsafe Condition
This AD was prompted by a manufacturing
quality escape that requires a reduction to the
life limit for certain high-pressure turbine
(HPT) rotor stage 1 disks. The FAA is issuing
this AD to prevent failure of the HPT rotor
stage 1 disk. The unsafe condition, if not
addressed, could result in uncontained disk
release, damage to the engine, and damage to
the airplane.
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:
■
2022–03–19 General Electric Company:
Amendment 39–21936; Docket No.
FAA–2021–1016; Project Identifier AD–
2021–00625–E.
PO 00000
Frm 00035
Fmt 4700
Sfmt 4700
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Action
Within 120 days after the effective date of
this AD, revise the airworthiness limitations
section of the existing maintenance manual
for your engine and the operator’s existing
approved continuous airworthiness
maintenance program by adding Figure 1 to
paragraph (g) of this AD.
E:\FR\FM\14FER1.SGM
14FER1
Federal Register / Vol. 87, No. 30 / Monday, February 14, 2022 / Rules and Regulations
Note 1 to paragraph (g): Where Figure 1 to
paragraph (g) refers to ‘‘Life Cycles,’’ for the
purpose of this AD, this refers to life cycles
since new.
(h) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, ECO 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 paragraph (i) of this AD.
Information may be emailed to: ANE-ADAMOC@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
For more information about this AD,
contact Scott Stevenson, Aviation Safety
Engineer, ECO Branch, FAA, 1200 District
Avenue, Burlington, MA 01803; phone: (781)
238–7132; fax: (781) 238–7199; email:
Scott.M.Stevenson@faa.gov.
(i) General Electric Company Service
Bulletin PASSPORT20–A–72–00–0116–00A–
930A–D, Issue 002, dated August 13, 2021.
(ii) [Reserved]
(3) For service information identified in
this AD, contact General Electric Company,
1 Neumann Way, Cincinnati, OH 45215;
phone: (513) 552–3272; email:
aviation.fleetsupport@ge.com; website:
www.ge.com.
(4) You may view this referenced service
information at the FAA, Airworthiness
Products Section, Operational Safety Branch,
1200 District Avenue, Burlington, MA 01803.
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: fr.inspection@nara.gov, or go to:
https://www.archives.gov/federal-register/cfr/
ibr-locations.html.
Issued on January 26, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022–03008 Filed 2–11–22; 8:45 am]
BILLING CODE 4910–13–P
jspears on DSK121TN23PROD with RULES1
(j) 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 the AD specifies otherwise.
VerDate Sep<11>2014
16:05 Feb 11, 2022
Jkt 256001
PO 00000
Frm 00036
Fmt 4700
Sfmt 4700
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–0019; Project
Identifier MCAI–2021–00371–R; Amendment
39–21930; AD 2022–03–13]
RIN 2120–AA64
Airworthiness Directives; Airbus
Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
The FAA is superseding
Airworthiness Directive (AD) 2014–21–
03, which applied to Airbus Helicopters
Model AS332L2 helicopters with a
certain yaw control damper support
(support) installed. AD 2014–21–03
required repetitively inspecting the
support attachment points for a crack.
Since the FAA issued AD 2014–21–03,
an improved (reinforced) support was
developed. This AD retains the
inspection requirements of AD 2014–
21–03 and requires installing the
improved support as specified in a
European Union Aviation Safety Agency
(EASA) AD, which is incorporated by
reference. The FAA is issuing this AD
to address the unsafe condition on these
products.
DATES: This AD becomes effective
March 1, 2022.
SUMMARY:
E:\FR\FM\14FER1.SGM
14FER1
ER14FE22.000
8174
Agencies
[Federal Register Volume 87, Number 30 (Monday, February 14, 2022)]
[Rules and Regulations]
[Pages 8172-8174]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-03008]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-1016; Project Identifier AD-2021-00625-E;
Amendment 39-21936; AD 2022-03-19]
RIN 2120-AA64
Airworthiness Directives; General Electric Company Turbofan
Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
General Electric Company (GE) Passport 20-17BB1A, Passport 20-18BB1A,
and Passport 20-19BB1A model turbofan engines. This AD was prompted by
a report of a manufacturing quality escape that requires a reduction to
the life limit of certain high-pressure turbine (HPT) rotor stage 1
disks. This AD requires revising the airworthiness limitations section
(ALS) of the existing maintenance manual and the operator's existing
approved continuous airworthiness maintenance program (CAMP) to
incorporate a reduced life limit for certain HPT rotor stage 1 disks.
The FAA is issuing this AD to address the unsafe condition on these
products.
DATES: This AD is effective March 21, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of March 21,
2022.
ADDRESSES: For service information identified in this final rule,
contact General Electric Company, 1 Neumann Way, Cincinnati, OH 45215,
United States; phone: (513) 552-3272; email:
[email protected]; website: www.ge.com. You may view this
service information at the FAA, Airworthiness Products Section,
Operational Safety Branch, 1200 District Avenue, Burlington, MA 01803.
For information on the availability of this material at the FAA, call
(817) 222-5110. It is also available at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-1016.
Examining the AD Docket
You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-1016; 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.
FOR FURTHER INFORMATION CONTACT: Scott Stevenson, Aviation Safety
Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803;
phone: (781) 238-7132; fax: (781) 238-7199; email:
[email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to all GE Passport 20-
17BB1A, Passport 20-18BB1A, and Passport 20-19BB1A model turbofan
engines. The NPRM published in the Federal Register on November 29,
2021 (86 FR 67669). The NPRM was prompted by a report from GE of a
manufacturing quality escape that identified a certain population of
HPT rotor stage 1 disks that did not meet the design specification. GE
determined that machining and inspection of the affected HPT rotor
stage 1 disks was inconsistent with the engineering drawing. Further
analysis by GE determined that the nonconformance at the forward and
aft hooks of the HPT rotor stage 1 disks may cause the disks to fail
prematurely and, therefore, the life limit of the affected HPT rotor
stage 1 disks requires reduction. As a result, GE decreased the life
limit of the affected HPT rotor stage 1 disks. In the NPRM, the FAA
proposed to require revising the ALS of the GE Passport 20 Line
Maintenance Manual, GEK 112062, and the operator's existing approved
CAMP to incorporate a reduced life limit for certain HPT rotor stage 1
disks. The FAA is issuing this AD to address the unsafe condition on
these products.
Discussion of Final Airworthiness Directive
Comments
The FAA received one comment, from GE. The following presents the
comment received on the NPRM and the FAA's response.
Request To Update Date of Service Information
GE requested that the FAA correct the date of GE Service Bulletin
(SB) PASSPORT20-A-72-00-0116-00A-930A-D, Issue 002, in this AD from
July 22, 2021, to August 13, 2021. GE commented that the NPRM included
the date of the draft SB and not the date of the published SB. GE
stated that there was no change to the document content between the
draft and publication dates.
The FAA agrees and has revised this AD as requested.
Conclusion
The FAA reviewed the relevant data, considered any comments
received, 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 products. Except for minor editorial changes and any
other changes described previously, this AD is adopted as proposed in
the NPRM. None of the changes will increase the economic burden on any
operator.
[[Page 8173]]
Related Service Information Under 1 CFR Part 51
The FAA reviewed GE SB PASSPORT20-A-72-00-0116-00A-930A-D, Issue
002, dated August 13, 2021. This service information describes
procedures for removing a certain population of HPT rotor stage 1 disks
from service and provides serial numbers of the affected HPT rotor
stage 1 disks. 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 ADDRESSES.
Costs of Compliance
The FAA estimates that this AD affects 78 engines installed on
airplanes 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
----------------------------------------------------------------------------------------------------------------
Revise the ALS of the Line Maintenance 1 work-hour x $85 per $0 $85 $6,630
Manual and the operator's existing hour = $85.
approved CAMP.
----------------------------------------------------------------------------------------------------------------
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:
2022-03-19 General Electric Company: Amendment 39-21936; Docket No.
FAA-2021-1016; Project Identifier AD-2021-00625-E.
(a) Effective Date
This airworthiness directive (AD) is effective March 21, 2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to General Electric Company (GE) Passport 20-
17BB1A, Passport 20-18BB1A, and Passport 20-19BB1A model turbofan
engines.
(d) Subject
Joint Aircraft System Component (JASC) Code 7250, Turbine
Section.
(e) Unsafe Condition
This AD was prompted by a manufacturing quality escape that
requires a reduction to the life limit for certain high-pressure
turbine (HPT) rotor stage 1 disks. The FAA is issuing this AD to
prevent failure of the HPT rotor stage 1 disk. The unsafe condition,
if not addressed, could result in uncontained disk release, damage
to the engine, and damage to the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Action
Within 120 days after the effective date of this AD, revise the
airworthiness limitations section of the existing maintenance manual
for your engine and the operator's existing approved continuous
airworthiness maintenance program by adding Figure 1 to paragraph
(g) of this AD.
[[Page 8174]]
[GRAPHIC] [TIFF OMITTED] TR14FE22.000
Note 1 to paragraph (g): Where Figure 1 to paragraph (g) refers
to ``Life Cycles,'' for the purpose of this AD, this refers to life
cycles since new.
(h) Alternative Methods of Compliance (AMOCs)
(1) The Manager, ECO 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 paragraph (i) 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.
(i) Related Information
For more information about this AD, contact Scott Stevenson,
Aviation Safety Engineer, ECO Branch, FAA, 1200 District Avenue,
Burlington, MA 01803; phone: (781) 238-7132; fax: (781) 238-7199;
email: [email protected].
(j) 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 the AD specifies otherwise.
(i) General Electric Company Service Bulletin PASSPORT20-A-72-
00-0116-00A-930A-D, Issue 002, dated August 13, 2021.
(ii) [Reserved]
(3) For service information identified in this AD, contact
General Electric Company, 1 Neumann Way, Cincinnati, OH 45215;
phone: (513) 552-3272; email: [email protected]; website:
www.ge.com.
(4) You may view this referenced service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 1200
District Avenue, Burlington, MA 01803. 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 January 26, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2022-03008 Filed 2-11-22; 8:45 am]
BILLING CODE 4910-13-P