[Federal Register Volume 87, Number 204 (Monday, October 24, 2022)]
[Rules and Regulations]
[Pages 64152-64156]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-22593]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-1074; Project Identifier MCAI-2021-00447-R; 
Amendment 39-22195; AD 2022-20-11]
RIN 2120-AA64


Airworthiness Directives; Bell Textron Canada Limited Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for 
certain Bell Textron Canada Limited Model 429 helicopters. This AD was 
prompted by reports of failed rivets between the tailboom skin and the 
tail rotor (TR) gearbox support assembly. This AD requires visually 
inspecting the external surface of the TR gearbox support assembly, 
borescope inspecting or visually inspecting the inside of the tailboom 
for certain conditions, and performing a tactile inspection. Depending 
on the results of the inspections, this AD requires removing certain 
rivets from service or repairing gaps in accordance with an approved 
method. This AD also requires repeating these inspections within 
certain intervals. The FAA is issuing this AD to address the unsafe 
condition on these products.

DATES: This AD is effective November 28, 2022.
    The Director of the Federal Register approved the incorporation by 
reference of a certain document listed in this AD as of November 28, 
2022.

ADDRESSES: For service information identified in this final rule, 
contact Bell Textron Canada Limited, 12,800 Rue de l'Avenir, Mirabel, 
Quebec J7J 1R4, Canada; telephone 1-450-437-2862 or 1-800-363-8023; fax 
1-450-433-0272; email [email protected]; or at 
bellflight.com/support/contact-support. 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. For information on the availability of this material at the FAA, 
call (817) 222-5110. Service information that is incorporated by 
reference is also available at regulations.gov by searching for and 
locating Docket No. FAA-2021-1074.

Examining the AD Docket

    You may examine the AD docket at regulations.gov by searching for 
and locating Docket No. FAA-2021-1074; 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 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: Andrea Jimenez, Aerospace Engineer, 
COS Program Management Section, Operational Safety Branch, Compliance & 
Airworthiness Division, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 
11590; telephone (516) 228-7330; 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 Bell Textron Canada 
Limited Model 429 helicopters, serial numbers (S/N) 57001 and 
subsequent. The NPRM published in the Federal Register on December 23, 
2021 (86 FR 72891). In the NPRM, the FAA proposed to require visually 
inspecting the external surface of the TR gearbox support assembly, 
borescope inspecting or visually inspecting the inside of the tailboom 
for certain conditions, and performing a tactile inspection. Depending 
on the results of the inspections, the NPRM proposed to require 
removing certain rivets from service or repairing gaps in accordance 
with FAA-approved methods. The NPRM also proposed to require repeating 
these inspections within certain intervals.

[[Page 64153]]

    The NPRM was prompted by Transport Canada AD CF-2021-15, dated 
April 14, 2021 (Transport Canada AD CF-2021-15), issued by Transport 
Canada, which is the aviation authority for Canada, to correct an 
unsafe condition for Bell Textron Canada Limited Model 429 helicopters, 
S/N 57001 and subsequent. Transport Canada advises of multiple in-
service reports of failed rivets at the joint between the tailboom skin 
and the TR gearbox support assembly part number (P/N) 429-034-701-101 
or P/N 429-035-705-101. Transport Canada states that in-service reports 
also revealed a quality escape resulted in a gapping condition between 
the tailboom skin and the TR gearbox support fitting at some locations 
around the joint, and that rivets of inadequate grip length have been 
installed at the affected joint. This condition, if not addressed, 
could result in progressive deterioration of the joint structural 
integrity, detachment of the TR gearbox support assembly and loss of 
control of the helicopter.
    Accordingly, Transport Canada AD CF-2021-15 requires, for certain 
serial-numbered helicopters, an initial visual inspection of the rivets 
at the TR gearbox support assembly for signs of failed rivets or 
inadequate grip length. Transport Canada AD CF-2021-15 also requires, 
for all serial-numbered helicopters defined in the applicability, 
repeating the initial visual inspection at intervals not to exceed 400 
hours air time or 12 months, whichever occurs first. Transport Canada 
AD CF-2021-15 also requires repair or replacement of affected parts if 
discrepancies are found. Transport Canada considers its AD an interim 
action and states that further AD action may follow.
    After the FAA issued the NPRM, the FAA issued a supplemental notice 
of proposed rulemaking (SNPRM) to amend 14 CFR part 39 by adding an AD 
that would apply to Bell Textron Canada Limited Model 429 helicopters, 
S/N 57001 and subsequent. The SNPRM published in the Federal Register 
on April 22, 2022 (87 FR 24077). The SNPRM proposed to require visually 
inspecting the external surface of the TR gearbox support assembly, 
borescope inspecting or visually inspecting the inside of the tailboom 
for certain conditions, and performing a tactile inspection. Depending 
on the results of the inspections, the SNPRM proposed to require 
removing certain rivets from service or repairing gaps in accordance 
with FAA-approved methods. The SNPRM also proposed to require repeating 
these inspections within certain intervals.
    The SNPRM was prompted by the FAA's determination that due to 
thermal cycling, the compliance times in the NPRM should be revised to 
include calendar compliance times. According to Bell, thermal cycling 
is independent of flight hours (FH) and can occur when an aircraft is 
stationary and is also a significant contributor to the unsafe 
condition. Accordingly, the FAA determined the proposed paragraph (g) 
of the NPRM had to be revised by including calendar compliance times. 
Also, after the NPRM was issued, the FAA determined the proposed 
paragraph (g)(1)(iii) of the NPRM had to be revised by deleting the 
word ``not'' when referring to whether or not a rivet comes out when 
pulled with pliers or when pulled by hand. This wording was incorrect 
and the correct wording should only state ``does.'' Accordingly, these 
changes were included in the SNPRM.

Discussion of Final Airworthiness Directive

Comments

    The FAA received one comment from Air Methods. The following 
presents the comment received on the SNPRM and the FAA's response.

Request for More Information

    The commenter stated Transport Canada AD CF-2021-15 requires 
replacing any rivets and repairing any gaps that exceed 0.005 in (0.127 
mm) in accordance with an approved Bell structural repair scheme, 
whereas the proposed AD would require removing the rivets from service 
and repairing gaps in accordance with an FAA-approved method instead. 
The commenter stated that Bell does not normally provide FAA-approved 
documentation and requested that the FAA clarify whether the FAA is 
mandating receiving both a Bell Canada approval document and a separate 
8110 from the FAA.
    The FAA has revised paragraphs (g)(1)(i)(B) and (g)(1)(ii)(A)(2) of 
this final rule from ``repair the gaps in accordance with an FAA-
approved method'' to ``repairing any gaps in accordance with a method 
approved by the Manager, General Aviation & Rotorcraft Section, 
International Validation Branch, FAA; or Transport Canada; or Bell 
Textron Canada Limited's Transport Canada Design Approval Organization 
(DAO). If approved by the DAO, the approval must include the DAO-
authorized signature.'' The FAA also revised the Costs of Compliance 
section of this final rule to reflect these changes. These revisions 
clarify that operators are not limited to a single method of repair in 
order for a helicopter to be approved for return to service.

Additional Changes Since the SNPRM was Issued

    Since the FAA issued the SNPRM, the FAA has revised paragraphs 
(g)(1)(i)(A) and (B) of this final rule by adding the words ``replace 
the rivets removed from service by paragraph (g)(1)(i) of this AD with 
airworthy rivets.'' The FAA determined this revision clarifies which 
rivets should be replaced and that an airworthy rivet must be installed 
when these rivets are removed from service.
    The FAA has also revised paragraphs (g)(1)(i) and (g)(1)(ii)(A) and 
(B) of this final rule by adding the words ``remove these rivets from 
service.'' The FAA determined this revision clarifies which rivets 
should be removed from service. Additionally, the FAA revised this 
final rule by adding paragraphs (g)(1)(ii)(A)(1) and (2) to this final 
rule, which describe the corrective actions that are required as a 
result of paragraph (g)(1)(ii)(A). The FAA determined this revision was 
necessary to clarify which rivets should be removed from service and 
replaced after the gap measurements.
    The FAA has also revised paragraph (g)(1)(ii)(B) of this final rule 
by adding the words ``replace them with airworthy rivets.'' The FAA 
determined this revision clarifies that an airworthy rivet must be 
installed to replace the rivet(s) that were removed from service.
    Additionally, the FAA revised the corrective action for any gaps 
that equal 0.005 in (0.127 mm). In the SNPRM, the FAA proposed 
repairing those gaps in accordance with an FAA-approved method and 
removing the rivets from service. In this final rule, the FAA requires 
removing certain rivets from service and replacing them with airworthy 
rivets for that condition instead.
    Finally, the FAA revised paragraph (g)(1)(iii) of this final rule 
by adding the words ``remove any rivet from service that comes out when 
pulled with pliers or when pulled by hand and replace with an airworthy 
rivet.'' The FAA determined this revision was necessary to clarify 
which rivets should be removed from service if corrective action is 
needed as a result of the tactile inspection and that an airworthy 
rivet must be installed to replace the rivet that was removed from 
service.

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

[[Page 64154]]

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, considered the comment 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 helicopters. Except for minor editorial changes and any other 
changes described previously, this AD is adopted as proposed in the 
SNPRM.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed Bell Alert Service Bulletin (ASB) 429-19-47, 
Revision B, dated January 27, 2021. This service information specifies 
procedures for an initial and repetitive general visual inspections and 
detailed inspections of the affected rivets at the joint between the 
tailboom skin and the TR gearbox support assembly. This service 
information also specifies procedures for replacing the affected rivets 
and repairing the gaps in accordance with an approved Bell structural 
repair scheme.
    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.

Other Related Service Information

    The FAA also reviewed Bell ASB 429-19-47, dated August 28, 2019 
(ASB 429-19-47), and Bell ASB 429-19-47, Revision A, dated November 2, 
2020 (ASB 429-19-47 Rev A). ASB 429-19-47 specifies the same general 
visual inspection as ASB 429-19-47 Rev A however, ASB 429-19-47 Rev A 
introduces a repetitive inspection and specifies corrective actions if 
any discrepant rivets are found. ASB 429-19-47 Rev A specifies the same 
procedures for the initial and repetitive general visual inspections 
and detailed inspections as ASB 429-19-47 Rev B however, ASB 429-19-47 
Rev B revises the compliance section, description section, and 
materials section, and also the accomplishment instructions.

Interim Action

    The FAA considers this AD to be an interim action. Once final 
action has been identified, the FAA might consider further rulemaking.

Differences Between This AD and the Transport Canada AD

    If there are any gaps that exceed 0.005 in (0.127 mm), Transport 
Canada AD CF-2021-15 requires replacing the rivets, repairing the gaps 
in accordance with an approved Bell structural repair scheme, and 
submitting certain information to the manufacturer. Whereas, if there 
are any gaps that exceed 0.005 in (0.127 mm), this AD requires removing 
the rivets from service and replacing the rivets with airworthy rivets. 
This AD also requires repairing those gaps in accordance with a method 
approved by the Manager, General Aviation & Rotorcraft Section, 
International Validation Branch, FAA; or Transport Canada; or Bell 
Textron Canada Limited's Transport Canada DAO instead. If there are any 
gaps that are 0.005 in (0.127 mm) or less, Transport Canada AD CF-2021-
15 requires replacing the rivets, whereas this AD requires removing the 
rivets from service and replacing them with airworthy rivets.

Costs of Compliance

    The FAA estimates that this AD affects 120 helicopters of U.S. 
Registry. Labor rates are estimated at $85 per work-hour. Based on 
these numbers, the FAA estimates the following costs to comply with 
this AD.
    Visually inspecting the surface of the TR gearbox support assembly 
takes about 0.5 work-hour for an estimated cost of $43 per helicopter 
per inspection and $5,160 for the U.S. fleet per inspection.
    If required, replacing an affected rivet takes about 1 work-hour 
and parts cost about $110 per rivet for an estimated cost of $195 per 
rivet replacement.
    If required, measuring gaps takes about 0.5 work-hour for an 
estimated cost of $43 per helicopter.
    If required, repairing a gap in accordance with an FAA-approved 
method takes up to about 1 work-hour for an estimated cost of up to $85 
per repair. The FAA has no way to determine the cost estimate of 
repairing a gap using a method approved by Transport Canada, or Bell 
Textron Canada Limited's Transport Canada DAO.
    Visually inspecting or borescope inspecting the inside of the 
tailboom takes about 0.5 work-hour for an estimated cost of $43 per 
helicopter per inspection and $5,160 for the U.S. fleet per inspection.
    Performing a tactile inspection takes about 0.5 work-hour for an 
estimated cost of $43 per helicopter per inspection and $5,160 for the 
U.S. fleet per inspection.

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:

2022-20-11 Bell Textron Canada Limited: Amendment 39-22195; Docket 
No. FAA-2021-1074; Project Identifier MCAI-2021-00447-R.

[[Page 64155]]

(a) Effective Date

    This airworthiness directive (AD) is effective November 28, 
2022.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Bell Textron Canada Limited Model 429 
helicopters, serial numbers (S/N) 57001 and subsequent, certificated 
in any category.

(d) Subject

    Joint Aircraft Service Component (JASC) Code: 5302, Rotorcraft 
tailboom.

(e) Unsafe Condition

    This AD was prompted by reports of failed rivets between the 
tailboom skin and the tail rotor (TR) gearbox support assembly. The 
FAA is issuing this AD to detect failed rivets and rivets with 
inadequate grip length. The unsafe condition, if not addressed, 
could result in deterioration of the joint structural integrity, 
detachment of the TR gearbox support assembly, and loss of 
helicopter control.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Required Actions

    (1) As of the effective date of this AD, for Model 429 
helicopters S/N 57002 through 57210 inclusive and S/N 57212 and 
subsequent that have accumulated less than 300 total hours time-in-
service (TIS), within 100 hours TIS or 6 months after accumulating 
300 total hours TIS, whichever occurs first; or for Model 429 
helicopters S/N 57002 through 57210 inclusive and S/N 57212 and 
subsequent that have replaced the TR gearbox support assembly part 
number (P/N) 429-034-701-101 or P/N 429-035-705-101 and the 
helicopter has accumulated less than 300 total hours TIS since the 
replacement of the TR gearbox support assembly, within 100 hours TIS 
or 6 months after accumulating 300 total hours TIS since the 
replacement, whichever occurs first:
    (i) Visually inspect the external surface of the TR gearbox 
support assembly for any rivet heads that have separated from their 
tail. If there are any rivet heads that have separated from their 
tail, before further flight, remove these rivets from service and 
measure any gaps between the TR gearbox support assembly and the 
tailboom skin by following the Accomplishment Instructions, Part I, 
paragraphs 9.b. through 9.d. of Bell Alert Service Bulletin 429-19-
47, Revision B, dated January 27, 2021 (ASB 429-19-47 Rev B).
    (A) If there are no gaps or if any gap measures 0.005 in (0.127 
mm) or less, before further flight, replace the rivets removed from 
service by paragraph (g)(1)(i) of this AD with airworthy rivets.
    (B) If there are any gaps that exceed 0.005 in (0.127 mm), 
before further flight, repair the gaps, and replace the rivets 
removed from service by paragraph (g)(1)(i) of this AD with 
airworthy rivets. This AD requires repairing any gaps in accordance 
with a method approved by the Manager, General Aviation & Rotorcraft 
Section, International Validation Branch, FAA; or Transport Canada; 
or Bell Textron Canada Limited's Transport Canada Design Approval 
Organization (DAO). If approved by the DAO, the approval must 
include the DAO-authorized signature.
    (ii) Borescope inspect or use a light source and mirror to 
visually inspect each rivet inside the tailboom for any missing 
rivet tails, any rivet tails resting at the bottom of the tailboom, 
and any rivet tails not resting against the tailboom skin.
    (A) If there are any missing rivet tails, or any rivet tails 
resting at the bottom of the tailboom, before further flight, remove 
these rivets from service, and measure any gaps between the TR 
gearbox support assembly and the tailboom skin by following the 
Accomplishment Instructions, Part I, paragraphs 9.b. through 9.d. of 
ASB 429-19-47 Rev B.
    (1) If there are no gaps or if any gap measures 0.005 in (0.127 
mm) or less, before further flight, replace the rivets removed from 
service by paragraph (g)(1)(ii)(A) of this AD with airworthy rivets.
    (2) If there are any gaps that exceed 0.005 in (0.127 mm), 
before further flight, repair the gaps, and replace the rivets 
removed from service by paragraph (g)(1)(ii)(A) of this AD with 
airworthy rivets. This AD requires repairing any gaps in accordance 
with a method approved by the Manager, General Aviation & Rotorcraft 
Section, International Validation Branch, FAA; or Transport Canada; 
or Bell Textron Canada Limited's Transport Canada DAO. If approved 
by the DAO, the approval must include the DAO-authorized signature.
    (B) If there are any rivet tails not resting against the 
tailboom skin, before further flight, remove these rivets from 
service and replace them with airworthy rivets.
    (iii) Perform a tactile inspection of the rivets identified in 
Figure 1 of ASB 429-19-47 Rev B, by pulling on each rivet tail with 
pliers or pulling by hand. If any rivet does come out when pulled 
with pliers or when pulled by hand, before further flight, remove 
any rivet from service that comes out when pulled with pliers or 
when pulled by hand and replace with an airworthy rivet.
    (2) For Model 429 helicopters S/N 57002 through 57210 inclusive 
and S/N 57212 and subsequent that are not identified in paragraph 
(g)(1) of this AD, within 100 hours TIS or 6 months after the 
effective date of this AD, whichever occurs first, perform the 
actions as specified in paragraphs (g)(1)(i) through (iii) of this 
AD.
    (3) For Model 429 helicopters S/N 57002 through 57210 inclusive 
and S/N 57212 and subsequent, within 400 hours TIS or 12 months, 
whichever occurs first after the initial inspections required by 
paragraph (g)(1) or (2) of this AD, as applicable to your 
helicopter, and thereafter at intervals not to exceed 400 hours TIS 
or 12 months, whichever occurs first, accomplish the actions 
required by paragraphs (g)(1)(i) through (iii) of this AD.
    (4) For Model 429 helicopters S/N 57001 and 57211, within 400 
hours TIS or 12 months after the effective date of this AD, 
whichever occurs first, and thereafter at intervals not to exceed 
400 hours TIS or 12 months, whichever occurs first, accomplish the 
actions required by paragraphs (g)(1)(i) through (iii) of this AD.

(h) Credit for Previous Actions

    This paragraph provides credit for the actions specified in 
paragraphs (g)(1) and (2) of this AD, if those actions were 
performed before the effective date of this AD using Bell Alert 
Service Bulletin 429-19-47, Revision A, dated November 2, 2020; or 
Bell Alert Service Bulletin 429-19-47, dated August 28, 2019.

(i) 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 (j)(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.

(j) Related Information

    (1) For more information about this AD, contact Andrea Jimenez, 
Aerospace Engineer, COS Program Management Section, Operational 
Safety Branch, Compliance & Airworthiness Division, FAA, 1600 
Stewart Ave., Suite 410, Westbury, NY 11590; telephone (516) 228-
7330; email [email protected].
    (2) Bell Alert Service Bulletin 429-19-47, Revision A, dated 
November 2, 2020; and Bell Alert Service Bulletin 429-19-47, dated 
August 28, 2019, 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 (k)(3) and (4) of this AD.
    (3) The subject of this AD is addressed in Transport Canada AD 
CF-2021-15, dated April 14, 2021. You may view the Transport Canada 
AD on the internet at regulations.gov in Docket No. FAA-2021-1074.

(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 the AD specifies otherwise.
    (i) Bell Alert Service Bulletin 429-19-47, Revision B, dated 
January 27, 2021.
    (ii) [Reserved]
    (3) For Bell service information identified in this AD, contact 
Bell Textron Canada Limited, 12,800 Rue de l'Avenir, Mirabel, Quebec 
J7J 1R4, Canada; telephone 1-450-437-2862 or 1-800-363-8023; fax 1-
450-

[[Page 64156]]

433-0272; email [email protected]; or at bellflight.com/support/contact-support.
    (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: www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on September 19, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2022-22593 Filed 10-21-22; 8:45 am]
BILLING CODE 4910-13-P