Proposed Rule2021-28134
Airworthiness Directives; General Electric Company Turbofan Engines
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
December 29, 2021
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to supersede Airworthiness Directive (AD) 2019-22-05, which applies to all General Electric Company (GE) CF34-8C model turbofan engines. AD 2019-22-05 requires initial and repetitive inspections of the operability bleed valve (OBV) fuel tubes, OBV bleed air manifold link rod assemblies, and the OBV fuel fittings. AD 2019- 22-05 also requires replacement of OBVs or related OBV hardware that fail inspection. Since the FAA issued AD 2019-22-05, the manufacturer has redesigned the OBV, which terminates the need for the repetitive inspections. This proposed AD would require initial and repetitive inspections of the OBV fuel tubes, OBV bleed air manifold link rod assemblies, and the OBV fuel fittings. This proposed AD would also require replacement of OBVs or related OBV hardware that fail inspection. As a terminating action to the repetitive inspections, this proposed AD would require replacement of certain OBVs installed on GE CF34-8C and CF34-8E model turbofan engines. The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
<html>
<head>
<title>Federal Register, Volume 86 Issue 247 (Wednesday, December 29, 2021)</title>
</head>
<body><pre>
[Federal Register Volume 86, Number 247 (Wednesday, December 29, 2021)]
[Proposed Rules]
[Pages 73997-74000]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2021-28134]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-1167; Project Identifier AD-2021-00823-E]
RIN 2120-AA64
Airworthiness Directives; General Electric Company Turbofan
Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2019-22-05, which applies to all General Electric Company (GE) CF34-8C
model turbofan engines. AD 2019-22-05 requires initial and repetitive
inspections of the operability bleed valve (OBV) fuel tubes, OBV bleed
air manifold link rod assemblies, and the OBV fuel fittings. AD 2019-
22-05 also requires replacement of OBVs or related OBV hardware that
fail inspection. Since the FAA issued AD 2019-22-05, the manufacturer
has redesigned the OBV, which terminates the need for the repetitive
inspections. This proposed AD would require initial and repetitive
inspections of the OBV fuel tubes, OBV bleed air manifold link rod
assemblies, and the OBV fuel fittings. This proposed AD would also
require replacement of OBVs or related OBV hardware that fail
inspection. As a terminating action to the repetitive inspections, this
proposed AD would require replacement of certain OBVs installed on GE
CF34-8C and CF34-8E model turbofan engines. The FAA is proposing this
AD to address the unsafe condition on these products.
DATES: The FAA must receive comments on this proposed AD by February
14, 2022.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to <a href="https://www.regulations.gov">https://www.regulations.gov</a>. Follow the instructions for submitting comments.
<bullet> Fax: (202) 493-2251.
<bullet> Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
<bullet> Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this NPRM, contact General
Electric Company, 1 Neumann Way, Cincinnati, OH 45215; phone: (513)
552-3272; email: <a href="/cdn-cgi/l/email-protection#bfdec9d6decbd6d0d191d9d3dadacbcccacfcfd0cdcbffd8da91dcd0d2"><span class="__cf_email__" data-cfemail="e687908f87928f8988c8808a83839295939696899492a68183c885898b">[email protected]</span></a>; website: <a href="https://www.ge.com">https://www.ge.com</a>. You may view this service information at the Airworthiness
Products Section, Operational Safety Branch, FAA, 1200 District Avenue,
Burlington, MA 01803. For information on the availability of this
material at the FAA, call (817) 222-5110.
Examining the AD Docket
You may examine the AD docket at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by
searching for and locating Docket No. FAA-2021-1167; 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 NPRM, any comments
received, and other information. The street address for Docket
Operations is listed above.
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:
<a href="/cdn-cgi/l/email-protection#683b0b071c1c4625463b1c0d1e0d061b0706280e0909460f071e"><span class="__cf_email__" data-cfemail="2370404c57570d6e0d70574655464d504c4d634542420d444c55">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2021-1167; Project Identifier
AD-2021-00823-E'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
the proposal because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
<a href="https://www.regulations.gov">https://www.regulations.gov</a>, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact we receive about this proposed AD.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this
[[Page 73998]]
NPRM. Submissions containing CBI should be sent to Scott Stevenson,
Aviation Safety Engineer, ECO Branch, FAA, 1200 District Avenue,
Burlington, MA 01803. Any commentary that the FAA receives which is not
specifically designated as CBI will be placed in the public docket for
this rulemaking.
Background
The FAA issued AD 2019-22-05, Amendment 39-19784 (84 FR 63569,
November 18, 2019), (AD 2019-22-05), for all GE CF34-8C1, CF34-8C5,
CF34-8C5A1, CF34-8C5B1, CF34-8C5A2, and CF34-8C5A3 model turbofan
engines. AD 2019-22-05 was prompted by multiple reports of fuel leaks,
some leading to engine fires, that have occurred as a result of
malfunctions related to the OBV. AD 2019-22-05 requires initial and
repetitive inspections of the OBV fuel tubes, OBV bleed air manifold
link rod assemblies, and the OBV fuel fittings. AD 2019-22-05 also
requires replacement of OBVs or related OBV hardware that fail
inspection. The agency issued AD 2019-22-05 to prevent failure of the
OBV.
Actions Since AD 2019-22-05 Was Issued
Since the FAA issued AD 2019-22-05, the manufacturer redesigned the
OBV to eliminate the need for the repetitive inspections of the OBV
fuel tubes, OBV bleed air manifold link rod assemblies, and the OBV
fuel fittings. The manufacturer has issued service information
specifying procedures to replace certain OBVs installed on CF34-8C1,
CF34-8C5, CF34-8C5A1, CF34-8C5B1, CF34-8C5A2, CF34-8C5A3 (CF34-8C), and
GE CF34-8E2, CF34-8E2A1, CF34-8E5, CF34-8E5A1, CF34-8E5A2, CF34-8E6,
and CF34-8E6A1 (CF34-8E) model turbofan engines. Additionally, the FAA
determined that the CF34-8E model turbofan engines are susceptible to
the same unsafe condition as the CF34-8C model turbofan engines, and
therefore, added the CF34-8E model turbofan engines to the
applicability of this proposed AD. The FAA is proposing to require
installation of the newly-designed OBV as a terminating action to the
repetitive inspections required for CF34-8C model turbofan engines. The
FAA is also proposing to require replacement of certain OBVs installed
on CF34-8E model turbofan engines.
FAA's Determination
The FAA is issuing this NPRM after determining that the unsafe
condition described previously is likely to exist or develop on other
products of the same type design.
Related Service Information Under 1 CFR Part 51
The FAA reviewed GE CF34-8C Service Bulletin (SB) 75-0020 R04,
dated May 10, 2019 (GE SB 75-0020). The SB specifies procedures for
inspecting the bleed air manifold link rod assemblies; the supply,
return, and drain fuel fittings; and the fuel tubes on the OBV. The SB
also specifies procedures for performing corrective actions and
replacing any OBVs or related OBV hardware that fail the inspection
criteria. The Director of the Federal Register approved the
incorporation by reference of GE SB 75-0020 as of December 23, 2019 (84
FR 63569, November 18, 2019).
The FAA reviewed GE CF34-8C SB 75-0025 R01, dated August 1, 2019.
This SB describes procedures for replacing and upgrading the suspect
population of OBVs VIN 5000728-104 (part number (P/N) 4123T71P02), VIN
5000728-106 (P/N 4123T71P03), and VIN 5080046-101 (P/N 4123T71P04).
The FAA reviewed GE CF34-8E SB 75-0019 R01, dated August 1, 2019.
This SB describes procedures for replacing and upgrading the suspect
population of OBVs VIN 5000728-104 (P/N 4123T71P02), VIN 5000728-106
(P/N 4123T71P03), and VIN 5080046-101 (P/N 4123T71P04).
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.
Other Related Service Information
The FAA reviewed GE CF34-8C SB 75-0026 R00, dated February 21,
2020. This SB introduces OBV VIN 5080046-103 (P/N 4123T71P06).
The FAA also reviewed GE CF34-8E SB 75-0021 R00, dated February 21,
2020. This SB introduces OBV VIN 5080046-103 (P/N 4123T71P06).
Proposed AD Requirements in This NPRM
This proposed AD would retain certain requirements of AD 2019-22-
05. This proposed AD would require initial and repetitive inspections
of the OBV fuel tubes, OBV bleed air manifold link rod assemblies, and
the OBV fuel fittings and replacement of OBVs or related OBV hardware
that fail inspection. As a terminating action to the repetitive
inspections of the OBV fuel tubes, OBV bleed air manifold link rod
assemblies, and the OBV fuel fittings, this proposed AD would require
replacement of certain OBVs installed on GE CF34-8C model turbofan
engines. This proposed AD would also require replacement of certain
OBVs installed on CF34-8E model turbofan engines.
Differences Between This Proposed AD and the Service Information
GE SB 75-0020 specifies that the results of the inspections must be
documented in an inspection chart form and sent to GE Product Support
Engineering. This proposed AD would not mandate sending information to
GE Product Support Engineering.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 1,172 engines installed on airplanes of U.S. registry.
The FAA estimates the following costs to comply with this proposed
AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Replace OBV......................... 2 work-hours x $85 per $17,230 $17,400 $20,392,800
hour = $170.
Inspect OBV fuel tubes, assemblies, 1 work-hour x 85 per 0 85 99,620
and fittings. hour = 85.
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary
replacements that would be required based on the results of the
proposed inspection. The agency has no way of determining the number of
aircraft that might need this replacement.
[[Page 73999]]
On-Condition Costs
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product
----------------------------------------------------------------------------------------------------------------
Replace OBV tubes, clamps, support hardware... 2.25 work-hours x $85 per hour = $3,786.25 $3,977.50
$191.25.
----------------------------------------------------------------------------------------------------------------
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
The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 the proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would 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 Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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:
a. Removing Airworthiness Directive 2019-22-05, Amendment 39-19784
(84 FR 63569, November 18, 2019); and
b. Adding the following new airworthiness directive:
General Electric Company: Docket No. FAA-2021-1167; Project
Identifier AD-2021-00823-E.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) action by February 14, 2022.
(b) Affected ADs
This AD replaces AD 2019-22-05, Amendment 39-19784 (84 FR 63569,
November 18, 2019).
(c) Applicability
This AD applies to General Electric Company (GE) CF34-8C1, CF34-
8C5, CF34-8C5A1, CF34-8C5B1, CF34-8C5A2, CF34-8C5A3, CF34-8E2, CF34-
8E2A1, CF34-8E5, CF34-8E5A1, CF34-8E5A2, CF34-8E6, and CF34-8E6A1
model turbofan engines.
(d) Subject
Joint Aircraft System Component (JASC) Code 7532, Compressor
Bleed Valve.
(e) Unsafe Condition
This AD was prompted by multiple reports of fuel leaks, some
leading to engine fires, that have occurred as a result of
malfunctions related to the operability bleed valve (OBV). The FAA
is issuing this AD to prevent failure of the OBV. The unsafe
condition, if not addressed, could result in an engine fire and
damage to the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
(1) For CF34-8C1, CF34-8C5, CF34-8C5A1, and CF34-8C5B1 model
turbofan engines with serial numbers (S/Ns): 965101 through 965670
inclusive; 194101 through 194999 inclusive; and 195101 through
195653 inclusive:
(i) Within 880 flight hours (FHs) since the previous inspection,
500 FHs after December 23, 2019 (the effective date of AD 2019-22-
05), or 6,880 FHs since new, whichever occurs later, inspect the OBV
bleed air manifold link rod assemblies, the OBV fuel fittings, and
the OBV fuel tubes.
(ii) Thereafter, within every 880 FHs since the previous
inspection, perform additional repeat inspections of the OBV bleed
air manifold link rod assemblies, the OBV fuel fittings, and the OBV
fuel tubes.
(iii) Use the Accomplishment Instructions, paragraph 3.B., of GE
CF34-8C Service Bulletin (SB) 75-0020 R04, dated May 10, 2019 (GE SB
75-0020), to perform inspections required by paragraphs (g)(1)(i)
and (ii) of this AD and, per the inspection criteria in paragraph
3.B., of GE SB 75-0020 (the inspection criteria), do the following:
(A) Before further flight, if fuel leakage is observed at the
OBV fittings or the OBV fittings are loose, replace the OBV with a
part eligible for installation.
(B) Before further flight, if any OBV fuel tube clamp is found
to be outside the inspection criteria, re-torque the OBV fuel tube
clamp or replace the OBV fuel tube clamp.
(C) Within 50 flight cycles (FCs) after the inspections required
by paragraphs (g)(1)(i) and (ii) of this AD, replace any link rod
hardware found to be outside the inspection criteria. Until the worn
link rod hardware is replaced, the OBV fittings must be inspected
before the first flight of each day for leakage and looseness in
accordance with the inspection criteria. If the OBV fittings fail to
meet the inspection criteria, before further flight, replace the OBV
and worn link rod hardware.
(2) For CF34-8C5B1 model turbofan engines with S/Ns not listed
in paragraph (g)(1) of this AD and for all CF34-8C5A2 and CF34-8C5A3
model turbofan engines, perform the following:
(i) Within 880 FHs after the effective date of this AD or prior
to accumulating 6,880 FHs since new, whichever occurs later, perform
an initial inspection of the OBV bleed air manifold link rod
assemblies, OBV fuel fittings, and OBV fuel tubes.
(ii) Thereafter, within every 880 FHs since the last inspection,
repeat the inspection of the OBV bleed air manifold link rod
assemblies, OBV fuel fittings, and OBV fuel tubes.
(iii) Use the Accomplishment Instructions, paragraph 3.B., of GE
SB 75-0020, to perform the inspections in paragraph (g)(2)(i) or
(ii) of this AD and, per the inspection criteria in paragraph 3.B.,
of GE SB 75-0020, do the following:
(A) Before further flight, if fuel leakage is observed at the
OBV fittings or the OBV fittings are loose, replace the OBV with a
part eligible for installation.
(B) Before further flight, if any OBV fuel tube clamp is found
to be outside the inspection criteria, re-torque the OBV fuel tube
clamp or replace the OBV fuel tube clamp.
[[Page 74000]]
(C) Within 50 FCs after the inspections required by paragraphs
(g)(2)(i) and (ii) of this AD, replace any link rod hardware found
to be outside the inspection criteria. Until the worn link rod
hardware is replaced, the OBV fittings must be inspected before the
first flight of each day for leakage and looseness in accordance
with the inspection criteria. If the OBV fittings fail to meet the
inspection criteria, before further flight, replace the OBV and worn
link rod hardware.
(3) For all affected engines with an installed OBV, VIN 5000728-
104 part number (P/N) (P/N 4123T71P02), VIN 5000728-106 (P/N
4123T71P03), or VIN 5080046-101 (P/N 4123T71P04), having an OBV S/N
listed in Appendix A, paragraph 4., of GE CF34-8C SB 75-0025 R01,
dated August 1, 2019 (GE SB 75-0025), or Appendix A, paragraph 4.,
of GE CF34-8E SB 75-0019 R01, dated August 1, 2019 (GE SB 75-0019),
respectively, within 180 days after the effective date of this AD,
remove the OBV and replace with a part eligible for installation.
(4) For all affected engines with an installed OBV, VIN 5000728-
104 (P/N 4123T71P02), VIN 5000728-106 (P/N 4123T71P03), or VIN
5080046-101 (P/N 4123T71P04), having an OBV S/N not listed in
Appendix A, paragraph 4., of GE SB 75-0025 or Appendix A, paragraph
4., of GE SB 75-0019, respectively, remove the OBV and replace with
a part eligible for installation within the following compliance
times:
(i) Within 16 months after the effective date of this AD for an
OBV that has accumulated more than 25,000 FHs since new.
(ii) Within 32 months after the effective date of this AD for an
OBV that has accumulated between 12,500 to 25,000 FHs since new,
inclusive.
(iii) Within 48 months after the effective date of this AD for
an OBV with fewer than 12,500 FHs since new.
(5) For all affected engines with an installed OBV, VIN 5080046-
102 (P/N 4123T71P05), before the OBV accumulates 25,000 FHs since
new or within 10 years after the effective date of this AD,
whichever occurs first, remove the OBV and replace with a part
eligible for installation.
(h) Terminating Action
Installation of an OBV that meets the definition of a part
eligible for installation in paragraph (i) of this AD constitutes
terminating action for the inspections required by paragraphs (g)(1)
and (2) of this AD.
(i) Definition
For the purpose of this AD, a ``part eligible for installation''
is an OBV VIN 5080046-103 (P/N 4123T71P06) or an OBV reworked to VIN
5080046-103 (P/N 4123T71P06).
(j) No Reporting Requirement
The reporting instructions specified in GE SB 75-0020 are not
required by this AD.
(k) Credit for Previous Actions
You may take credit for the initial inspection required by
paragraph (g)(1)(i) or (2)(i), of this AD if you performed this
initial inspection before the effective of this AD using GE CF34-8C
SB 75-0019 R01, dated October 24, 2017, or R00, dated August 4,
2017; or GE CF34-8C-AL S/B 75-0020, Revision 03, dated December 14,
2018, as applicable.
(l) 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
ECO Branch, send it to the attention of the person identified in
paragraph (m)(1) of this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#fabbb4bfd7bbbed7bbb7b5b9ba9c9b9bd49d958c"><span class="__cf_email__" data-cfemail="54151a117915107915191b17143235357a333b22">[email protected]</span></a>.
(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.
(m) Related Information
(1) 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: <a href="/cdn-cgi/l/email-protection#3467575b40401a791a67405142515a475b5a745255551a535b42"><span class="__cf_email__" data-cfemail="7427171b00005a395a27001102111a071b1a341215155a131b02">[email protected]</span></a>.
(2) For service information identified in this AD, contact
General Electric Company, 1 Neumann Way, Cincinnati, OH 45215;
phone: (513) 552-3272; email: <a href="/cdn-cgi/l/email-protection#c2a3b4aba3b6abadaceca4aea7a7b6b1b7b2b2adb0b682a5a7eca1adaf"><span class="__cf_email__" data-cfemail="d8b9aeb1b9acb1b7b6f6beb4bdbdacabada8a8b7aaac98bfbdf6bbb7b5">[email protected]</span></a>; website:
<a href="https://www.ge.com">https://www.ge.com</a>. 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.
Issued on December 21, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2021-28134 Filed 12-28-21; 8:45 am]
BILLING CODE 4910-13-P
</pre><script data-cfasync="false" src="/cdn-cgi/scripts/5c5dd728/cloudflare-static/email-decode.min.js"></script></body>
</html>Indexed from Federal Register on December 29, 2021.
This is legal information, not legal advice. Laws vary by jurisdiction and change frequently. Always verify current law with official sources and consult a licensed attorney in your jurisdiction for advice on your specific situation.