Airworthiness Directives; Dassault Aviation Airplanes, 63827-63830 [2019-24834]
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Federal Register / Vol. 84, No. 223 / Tuesday, November 19, 2019 / Proposed Rules
This AD requires doing the repair and
applicable on-condition actions before
further flight using a method approved in
accordance with the procedures specified in
paragraph (i) of this AD.
DEPARTMENT OF TRANSPORTATION
(i) Alternative Methods of Compliance
(AMOCs)
[Docket No. FAA–2019–0870; Product
Identifier 2019–NM–125–AD]
(1) The Manager, Seattle ACO 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 (j)(1) of
this AD. Information may be emailed to: 9ANM-Seattle-ACO-AMOC-Requests@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.
(3) An AMOC that provides an acceptable
level of safety may be used for any repair,
modification, or alteration required by this
AD if it is approved by The Boeing Company
Organization Designation Authorization
(ODA) that has been authorized by the
Manager, Seattle ACO Branch, FAA, to make
those findings. To be approved, the repair
method, modification deviation, or alteration
deviation must meet the certification basis of
the airplane, and the approval must
specifically refer to this AD.
(j) Related Information
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(1) For more information about this AD,
contact Greg Rutar, Aerospace Engineer,
Airframe Section, FAA, Seattle ACO Branch,
2200 South 216th St., Des Moines, WA
98198; phone and fax: 206–231–3529; email:
greg.rutar@faa.gov.
(2) For service information identified in
this AD, contact Boeing Commercial
Airplanes, Attention: Contractual & Data
Services (C&DS), 2600 Westminster Blvd.,
MC 110–SK57, Seal Beach, CA 90740–5600;
telephone 562–797–1717; internet https://
www.myboeingfleet.com. You may view this
referenced service information at the FAA,
Transport Standards Branch, 2200 South
216th St., Des Moines, WA. For information
on the availability of this material at the
FAA, call 206–231–3195.
Issued in Des Moines, Washington, on
November 5, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2019–24835 Filed 11–18–19; 8:45 am]
BILLING CODE 4910–13–P
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Federal Aviation Administration
14 CFR Part 39
RIN 2120–AA64
Airworthiness Directives; Dassault
Aviation Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to
supersede Airworthiness Directive (AD)
2018–19–27 and AD 2014–16–12, which
apply to certain Dassault Aviation
Model FALCON 2000EX airplanes.
Those ADs require revising the
maintenance or inspection program, as
applicable, to incorporate new
maintenance requirements and
airworthiness limitations. Since AD
2018–19–27 and AD 2014–16–12 were
issued, the FAA has determined that
new or more restrictive airworthiness
limitations are necessary. This proposed
AD would require revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
restrictive airworthiness limitations.
The FAA is proposing this AD to
address the unsafe condition on these
products.
SUMMARY:
The FAA must receive comments
on this proposed AD by January 3, 2020.
ADDRESSES: You may send comments,
using the procedures found in 14 CFR
11.43 and 11.45, by any of the following
methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: 202–493–2251.
• 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.
• 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 Dassault Falcon Jet
Corporation, Teterboro Airport, P.O.
Box 2000, South Hackensack, NJ 07606;
phone: 201–440–6700; internet: https://
www.dassaultfalcon.com. You may
view this referenced service information
at the FAA, Transport Standards
Branch, 2200 South 216th St., Des
Moines, WA. For information on the
DATES:
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63827
availability of this material at the FAA,
call 206–231–3195.
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2019–
0870; 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, the
regulatory evaluation, any comments
received, and other information. The
street address for Docket Operations is
listed above. Comments will be
available in the AD docket shortly after
receipt.
FOR FURTHER INFORMATION CONTACT: Tom
Rodriguez, Aerospace Engineer,
International Section, Transport
Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198;
phone and fax: 206–231–3226.
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 the ADDRESSES section. Include
‘‘Docket No. FAA–2019–0870; Product
Identifier 2019–NM–125–AD’’ at the
beginning of your comments. The FAA
specifically invites comments on the
overall regulatory, economic,
environmental, and energy aspects of
this proposed AD. The FAA will
consider all comments received by the
closing date and may amend this
proposed AD based on those comments.
The FAA will post all comments
received, without change, to https://
www.regulations.gov, including any
personal information you provide. The
FAA will also post a report
summarizing each substantive verbal
contact received about this proposed
AD.
Discussion
The FAA issued AD 2018–19–27,
Amendment 39–19428 (83 FR 50479,
October 9, 2018) (‘‘AD 2018–19–27’’),
for certain Dassault Aviation Model
FALCON 2000EX airplanes. AD 2018–
19–27 requires revising the maintenance
or inspection program, as applicable, to
incorporate new maintenance
requirements and airworthiness
limitations. AD 2018–19–27 resulted
from a determination that new or more
restrictive maintenance requirements
and airworthiness limitations are
necessary. AD 2018–19–27 specifies that
accomplishing the actions required by
paragraph (g) of that AD terminates the
requirements of AD 2014–16–12,
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Federal Register / Vol. 84, No. 223 / Tuesday, November 19, 2019 / Proposed Rules
Amendment 39–17936 (79 FR 52187,
September 3, 2014) (‘‘AD 2014–16–12’’),
but it does not supersede AD 2014–16–
12. In addition, AD 2018–19–27
specifies that accomplishing paragraph
(g) of that AD terminates the
requirements of paragraph (g)(1) of AD
2010–26–05, Amendment 39–16544 (75
FR 79952, December 21, 2010) (‘‘AD
2010–26–05’’), for Dassault Aviation
Model FALCON 2000EX airplanes. This
terminating provision of certain
requirements of AD 2010–26–05 is
included in this proposed AD.
This AD proposes to supersede AD
2018–19–27 and AD 2014–16–12, but
does not propose to supersede AD
2010–26–05.
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Actions Since AD 2018–19–27 Was
Issued
Since the FAA issued AD 2018–19–
27, the FAA has determined that new or
more restrictive airworthiness
limitations are necessary.
The European Union Aviation Safety
Agency (EASA), which is the Technical
Agent for the Member States of the
European Union, has issued EASA AD
2019–0154, dated July 3, 2019 (referred
to after this as the Mandatory
Continuing Airworthiness Information,
or ‘‘the MCAI’’), to correct an unsafe
condition for all Dassault Aviation
Model FALCON 2000EX airplanes. You
may examine the MCAI in the AD
docket on the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2019–
0870.
This proposed AD was prompted by
a determination that new or more
restrictive airworthiness limitations are
necessary. The FAA is proposing this
AD to address reduced structural
integrity of the airplane. See the MCAI
for additional background information.
Related Service Information Under 1
CFR Part 51
Dassault has issued Chapter 5–40,
Airworthiness Limitations, DGT 113877,
Revision 12, dated November 2018, of
the Dassault Falcon 2000EX
Maintenance Manual. This service
information describes instructions
applicable to airworthiness and safe life
limitations.
This proposed AD would also require
Chapter 5–40, Airworthiness
Limitations, DGT 113877, Revision 11,
dated November 2017, of the Dassault
Falcon 2000EX Maintenance Manual,
which the Director of the Federal
Register approved for incorporation by
reference as of November 13, 2018 (83
FR 50479, October 9, 2018).
This service information is reasonably
available because the interested parties
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have access to it through their normal
course of business or by the means
identified in the ADDRESSES section.
FAA’s Determination
This product has been approved by
the aviation authority of another
country, and is approved for operation
in the United States. Pursuant to our
bilateral agreement with the State of
Design Authority, The FAA has been
notified of the unsafe condition
described in the MCAI and service
information referenced above. The FAA
is proposing this AD because the FAA
evaluated all the relevant information
and determined the unsafe condition
described previously is likely to exist or
develop on other products of the same
type design.
Proposed Requirements of This NPRM
This proposed AD would retain all
requirements of AD 2018–19–27. This
proposed AD would also require
revising the existing maintenance or
inspection program, as applicable, to
incorporate new or more restrictive
airworthiness limitations.
This proposed AD would require
revisions to certain operator
maintenance documents to include new
actions (e.g., inspections). Compliance
with these actions is required by 14 CFR
91.403(c). For airplanes that have been
previously modified, altered, or repaired
in the areas addressed by this proposed
AD, the operator may not be able to
accomplish the actions described in the
revisions. In this situation, to comply
with 14 CFR 91.403(c), the operator
must request approval for an alternative
method of compliance according to
paragraph (l)(1) of this proposed AD.
Costs of Compliance
The FAA estimates that this proposed
AD affects 173 airplanes of U.S. registry.
The FAA estimates the following costs
to comply with this proposed AD:
The FAA estimates the total cost per
operator for the retained actions from
AD 2018–19–27 to be $7,650 (90 workhours × $85 per work-hour).
The FAA has determined that the new
revision of the existing maintenance or
inspection program takes an average of
90 work-hours per operator, although
the FAA recognizes that this number
may vary from operator to operator. In
the past, the FAA has estimated that this
action takes 1 work-hour per airplane.
Since operators incorporate
maintenance or inspection program
changes for their affected fleet(s), the
FAA has determined that a per-operator
estimate is more accurate than a perairplane estimate. Therefore, the FAA
estimates the total cost per operator to
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be $7,650 (90 work-hours × $85 per
work-hour).
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.
This proposed AD is issued in
accordance with authority delegated by
the Executive Director, Aircraft
Certification Service, as authorized by
FAA Order 8000.51C. In accordance
with that order, issuance of ADs is
normally a function of the Compliance
and Airworthiness Division, but during
this transition period, the Executive
Director has delegated the authority to
issue ADs applicable to transport
category airplanes and associated
appliances to the Director of the System
Oversight Division.
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 this proposed regulation:
(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.
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Federal Register / Vol. 84, No. 223 / Tuesday, November 19, 2019 / Proposed Rules
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
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:
a. Removing Airworthiness Directive
(AD) 2018–19–27, Amendment 39–
19428 (83 FR 50479, October 9, 2018);
and AD 2014–16–12, Amendment 39–
17936 (79 FR 52187, September 3,
2014); and
■ b. Adding the following new AD:
■
■
Dassault Aviation: Docket No. FAA–2019–
0870; Product Identifier 2019–NM–125–
AD.
(a) Comments Due Date
The FAA must receive comments by
January 3, 2020.
(b) Affected ADs
(1) This AD replaces AD 2018–19–27,
Amendment 39–19428 (83 FR 50479, October
9, 2018) (‘‘AD 2018–19–27’’); and AD 2014–
16–12, Amendment 39–17936 (79 FR 52187,
September 3, 2014) (‘‘AD 2014–16–12’’).
(2) This AD affects AD 2010–26–05,
Amendment 39–16544 (75 FR 79952,
December 21, 2010) (‘‘AD 2010–26–05’’).
(c) Applicability
This AD applies to Dassault Aviation
Model FALCON 2000EX airplanes,
certificated in any category, with an original
airworthiness certificate or original export
certificate of airworthiness issued on or
before January 15, 2019.
(d) Subject
Air Transport Association (ATA) of
America Code 05, Time limits/maintenance
checks.
(e) Reason
This AD was prompted by a determination
that new or more restrictive airworthiness
limitations are necessary. The FAA is issuing
this AD to address reduced structural
integrity of the airplane.
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(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Retained Revision of Maintenance or
Inspection Program, With No Changes
This paragraph restates the requirements of
paragraph (g) of AD 2018–19–27, with no
changes. Within 90 days after November 13,
2018 (the effective date of AD 2018–19–27),
revise the existing maintenance or inspection
program, as applicable, to incorporate the
information specified in Chapter 5–40,
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Airworthiness Limitations, DGT 113877,
Revision 11, dated November 2017, of the
Dassault Falcon 2000EX Maintenance
Manual. The initial compliance times for
doing the tasks are at the time specified in
Chapter 5–40, Airworthiness Limitations,
DGT 113877, Revision 11, dated November
2017, of the Dassault Falcon 2000EX
Maintenance Manual, or within 90 days after
November 13, 2018, whichever occurs later;
except for task number 52–20–00–610–801–
01, the initial compliance time is within 24
months after October 8, 2014 (the effective
date of AD 2014–16–12). The term ‘‘LDG’’ in
the ‘‘First Inspection’’ column of any table in
Chapter 5–40, Airworthiness Limitations,
DGT 113877, Revision 11, dated November
2017, means total airplane landings. The
term ‘‘FH’’ in the ‘‘First Inspection’’ column
of any table in Chapter 5–40, Airworthiness
Limitations, DGT 113877, Revision 11, dated
November 2017, means total flight hours. The
term ‘‘FC’’ in the ‘‘First Inspection’’ column
of any table in Chapter 5–40, Airworthiness
Limitations, DGT 113877, Revision 11, dated
November 2017, means total flight cycles.
(h) Retained Provision: No Alternative
Actions or Intervals, With a New Exception
This paragraph restates the requirements of
paragraph (h) of AD 2018–19–27, with a new
exception. Except as required by paragraph
(i) of this AD, after the maintenance or
inspection program has been revised as
required by paragraph (g) of this AD, no
alternative actions (e.g., inspections) or
intervals may be used unless the actions or
intervals are approved as an alternative
method of compliance (AMOC) in
accordance with the procedures specified in
paragraph (l)(1) of this AD.
(i) New Maintenance or Inspection Program
Revision
Within 90 days after the effective date of
this AD, revise the existing maintenance or
inspection program, as applicable, to
incorporate the information specified in
Chapter 5–40, Airworthiness Limitations,
DGT 113877, Revision 12, dated November
2018, of the Dassault Falcon 2000EX
Maintenance Manual. The initial compliance
times for doing the tasks are at the time
specified in Chapter 5–40, Airworthiness
Limitations, DGT 113877, Revision 12, dated
November 2018, of the Dassault Falcon
2000EX Maintenance Manual, or within 90
days after the effective date of this AD,
whichever occurs later; except for task
number 52–20–00–610–801–01, the initial
compliance time is within 24 months after
October 8, 2014 (the effective date of AD
2014–16–12). The term ‘‘LDG’’ in the ‘‘First
Inspection’’ column of any table in the
service information specified in this
paragraph means total airplane landings. The
term ‘‘FH’’ in the ‘‘First Inspection’’ column
of any table in the service information
specified in this paragraph means total flight
hours. The term ‘‘FC’’ in the ‘‘First
Inspection’’ column of any table in the
service information specified in this
paragraph means total flight cycles. Doing the
revision required by this paragraph
terminates the actions required by paragraph
(g) of this AD.
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63829
(j) New Provision: No Alternative Actions or
Intervals
After the existing maintenance or
inspection program has been revised as
required by paragraph (i) of this AD, no
alternative actions (e.g., inspections) or
intervals may be used unless the actions or
intervals are approved as an AMOC in
accordance with the procedures specified in
paragraph (l)(1) of this AD.
(k) Terminating Action for Certain Actions
in AD 2010–26–05
Accomplishing the actions required by
paragraph (g) or (i) of this AD terminates the
requirements of paragraph (g)(1) of AD 2010–
26–05, for Dassault Aviation Model FALCON
2000EX airplanes.
(l) Other FAA AD Provisions
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Section, Transport Standards 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 International Section, send it
to the attention of the person identified in
paragraph (m)(2) of this AD. Information may
be emailed to 9-ANM-116-AMOCREQUESTS@faa.gov.
(i) 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.
(ii) AMOCs approved previously for AD
2018–19–27 are not approved as AMOCs for
this AD.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain instructions
from a manufacturer, the instructions must
be accomplished using a method approved
by the Manager, International Section,
Transport Standards Branch, FAA; or the
European Union Aviation Safety Agency
(EASA); or Dassault Aviation’s EASA Design
Organization Approval (DOA). If approved by
the DOA, the approval must include the
DOA-authorized signature.
(m) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA AD
2019–0154, dated July 3, 2019, for related
information. This MCAI may be found in the
AD docket on the internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2019–0870.
(2) For more information about this AD,
contact Tom Rodriguez, Aerospace Engineer,
International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des
Moines, WA 98198; phone and fax: 206–231–
3226.
(3) For service information identified in
this AD, contact Dassault Falcon Jet
Corporation, Teterboro Airport, P.O. Box
2000, South Hackensack, NJ 07606; phone:
201–440–6700; internet: https://www.dassault
falcon.com. You may view this service
information at the FAA, Transport Standards
Branch, 2200 South 216th St., Des Moines,
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Federal Register / Vol. 84, No. 223 / Tuesday, November 19, 2019 / Proposed Rules
WA. For information on the availability of
this material at the FAA, call 206–231–3195.
Issued in Des Moines, Washington, on
November 7, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2019–24834 Filed 11–18–19; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF JUSTICE
Bureau of Prisons
28 CFR Part 541
[Docket No. BOP–1172–P]
RIN 1120–AB72
Inmate Discipline Program: New
Prohibited Act Code for Pressuring
Inmates for Legal Documents
Bureau of Prisons, Department
of Justice.
ACTION: Proposed rule.
AGENCY:
In this document, the Bureau
of Prisons (Bureau) proposes to add a
new code to the list of prohibited act
codes in the inmate discipline
regulations which will clarify that the
Bureau may discipline inmates for
pressuring or otherwise intimidating
other inmates into producing copies of
their own legal documents, such as presentence reports (PSRs), or statement of
reasons (SORs).
DATES: Submit written comments on or
before January 21, 2020.
ADDRESSES: Rules Unit, Office of
General Counsel, Bureau of Prisons, 320
First Street NW, Washington, DC 20534.
FOR FURTHER INFORMATION CONTACT:
Rules Unit, Office of General Counsel,
Bureau of Prisons, phone (202) 353–
8248.
SUMMARY:
SUPPLEMENTARY INFORMATION:
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Posting of Public Comments
Please note that all comments
received are considered part of the
public record and made available for
public inspection online at
www.regulations.gov. Such information
includes personal identifying
information (such as your name,
address, etc.) voluntarily submitted by
the commenter.
If you want to submit personal
identifying information (such as your
name, address, etc.) as part of your
comment, but do not want it to be
posted online, you must include the
phrase ‘‘PERSONAL IDENTIFYING
INFORMATION’’ in the first paragraph
of your comment. You must also locate
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all the personal identifying information
you do not want posted online in the
first paragraph of your comment and
identify what information you want
redacted.
If you want to submit confidential
business information as part of your
comment but do not want it to be posted
online, you must include the phrase
‘‘CONFIDENTIAL BUSINESS
INFORMATION’’ in the first paragraph
of your comment. You must also
prominently identify confidential
business information to be redacted
within the comment. If a comment
contains so much confidential business
information that it cannot be effectively
redacted, all or part of that comment
may not be posted on
www.regulations.gov.
Personal identifying information
identified and located as set forth above
will be placed in the agency’s public
docket file, but not posted online.
Confidential business information
identified and located as set forth above
will not be placed in the public docket
file. If you wish to inspect the agency’s
public docket file in person by
appointment, please see the FOR
FURTHER INFORMATION CONTACT
paragraph.
Proposed Rule
In this document, the Bureau
proposes to add a new code to Table 1—
Prohibited Acts and Available Sanctions
in the inmate discipline regulations. See
28 CFR 541.3. The new code will clarify
that the Bureau may discipline inmates
for pressuring or otherwise intimidating
other inmates into producing copies of
their own legal documents, such as presentence reports (PSRs), statement of
reasons (SORs), or other such
documents. New code 231 will put
inmates on notice that they may be
disciplined for ‘‘[r]equesting,
demanding, pressuring, or otherwise
intentionally creating a situation which
causes an inmate to produce or display
his/her own court documents for any
purpose to another inmate.’’
The Bureau has found that inmates, or
inmate groups, frequently pressure other
inmates for copies of their PSRs, SORs,
or other similar sentencing documents
from criminal judgments, to learn if they
are informants, gang members, have
financial resources, to find others
involved in offenses, to prove
affiliations, etc. Some inmates who
produced, or refused to produce, the
documents were threatened, assaulted,
and/or sought protective custody, all of
which jeopardized the Bureau’s ability
to safely manage its institutions.
The Bureau holds inmates
accountable for threatening and coercive
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behavior under existing provisions of
the disciplinary code. This provision,
however, will clarify that this specific
behavior may result in sanctions. The
defense bar, federal sentencing courts
and the Bureau identified this issue as
one of concern that requires heightened
disciplinary attention. We therefore
propose to add the aforementioned code
provision to underscore the severity of
the conduct described.
Regulatory Analyses
Executive Orders 12866, 13563, and
13771
This rule falls within a category of
actions that the Office of Management
and Budget (OMB) has determined do
not constitute ‘‘significant regulatory
actions’’ under section 3(f) of Executive
Order 12866 and, accordingly, it was
not reviewed by OMB. The economic
effects of this regulation are limited to
the Bureau’s appropriated funds. It takes
an average of 7.5 hours of staff time to
process an incident report. One of the
expected outcomes of this clarifying
regulation is that inmates may be
deterred from engaging in the prohibited
behavior because violations are better
defined. This expected outcome would
save staff resources required to process
incident reports. At this time, however,
the Bureau cannot estimate precisely
how many incidents will be avoided or
the monetary value of the resulting cost/
resource savings. Further, the Bureau
would expect any anticipated savings
generated by this rule to have minimal
effect on the economy.
Executive Order 13132
This regulation will not have
substantial direct effect on the States, on
the relationship between the national
government and the States, or on
distribution of power and
responsibilities among the various
levels of government. Under Executive
Order 13132, we determine that this
regulation does not have sufficient
federalism implications to warrant the
preparation of a Federalism Assessment.
Regulatory Flexibility Act
The Director of the Bureau of Prisons,
under the Regulatory Flexibility Act (5
U.S.C. 605(b)), reviewed this regulation
and certifies that it will not have a
significant economic impact upon a
substantial number of small entities.
This regulation pertains to the
correctional management of offenders
committed to the custody of the
Attorney General or the Director of the
Bureau of Prisons, and its economic
impact is limited to the Bureau’s
appropriated funds.
E:\FR\FM\19NOP1.SGM
19NOP1
Agencies
[Federal Register Volume 84, Number 223 (Tuesday, November 19, 2019)]
[Proposed Rules]
[Pages 63827-63830]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-24834]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-0870; Product Identifier 2019-NM-125-AD]
RIN 2120-AA64
Airworthiness Directives; Dassault Aviation Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2018-19-27 and AD 2014-16-12, which apply to certain Dassault Aviation
Model FALCON 2000EX airplanes. Those ADs require revising the
maintenance or inspection program, as applicable, to incorporate new
maintenance requirements and airworthiness limitations. Since AD 2018-
19-27 and AD 2014-16-12 were issued, the FAA has determined that new or
more restrictive airworthiness limitations are necessary. This proposed
AD would require revising the existing maintenance or inspection
program, as applicable, to incorporate new or more restrictive
airworthiness limitations. 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 January 3,
2020.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
Fax: 202-493-2251.
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.
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 Dassault
Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, South
Hackensack, NJ 07606; phone: 201-440-6700; internet: https://www.dassaultfalcon.com. You may view this referenced service
information at the FAA, Transport Standards Branch, 2200 South 216th
St., Des Moines, WA. For information on the availability of this
material at the FAA, call 206-231-3195.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0870; 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, the regulatory evaluation, any comments received, and other
information. The street address for Docket Operations is listed above.
Comments will be available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
International Section, Transport Standards Branch, FAA, 2200 South
216th St., Des Moines, WA 98198; phone and fax: 206-231-3226.
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 the ADDRESSES section. Include ``Docket No. FAA-2019-0870;
Product Identifier 2019-NM-125-AD'' at the beginning of your comments.
The FAA specifically invites comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. The
FAA will consider all comments received by the closing date and may
amend this proposed AD based on those comments.
The FAA will post all comments received, without change, to https://www.regulations.gov, including any personal information you provide.
The FAA will also post a report summarizing each substantive verbal
contact received about this proposed AD.
Discussion
The FAA issued AD 2018-19-27, Amendment 39-19428 (83 FR 50479,
October 9, 2018) (``AD 2018-19-27''), for certain Dassault Aviation
Model FALCON 2000EX airplanes. AD 2018-19-27 requires revising the
maintenance or inspection program, as applicable, to incorporate new
maintenance requirements and airworthiness limitations. AD 2018-19-27
resulted from a determination that new or more restrictive maintenance
requirements and airworthiness limitations are necessary. AD 2018-19-27
specifies that accomplishing the actions required by paragraph (g) of
that AD terminates the requirements of AD 2014-16-12,
[[Page 63828]]
Amendment 39-17936 (79 FR 52187, September 3, 2014) (``AD 2014-16-
12''), but it does not supersede AD 2014-16-12. In addition, AD 2018-
19-27 specifies that accomplishing paragraph (g) of that AD terminates
the requirements of paragraph (g)(1) of AD 2010-26-05, Amendment 39-
16544 (75 FR 79952, December 21, 2010) (``AD 2010-26-05''), for
Dassault Aviation Model FALCON 2000EX airplanes. This terminating
provision of certain requirements of AD 2010-26-05 is included in this
proposed AD.
This AD proposes to supersede AD 2018-19-27 and AD 2014-16-12, but
does not propose to supersede AD 2010-26-05.
Actions Since AD 2018-19-27 Was Issued
Since the FAA issued AD 2018-19-27, the FAA has determined that new
or more restrictive airworthiness limitations are necessary.
The European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Union, has issued
EASA AD 2019-0154, dated July 3, 2019 (referred to after this as the
Mandatory Continuing Airworthiness Information, or ``the MCAI''), to
correct an unsafe condition for all Dassault Aviation Model FALCON
2000EX airplanes. You may examine the MCAI in the AD docket on the
internet at https://www.regulations.gov by searching for and locating
Docket No. FAA-2019-0870.
This proposed AD was prompted by a determination that new or more
restrictive airworthiness limitations are necessary. The FAA is
proposing this AD to address reduced structural integrity of the
airplane. See the MCAI for additional background information.
Related Service Information Under 1 CFR Part 51
Dassault has issued Chapter 5-40, Airworthiness Limitations, DGT
113877, Revision 12, dated November 2018, of the Dassault Falcon 2000EX
Maintenance Manual. This service information describes instructions
applicable to airworthiness and safe life limitations.
This proposed AD would also require Chapter 5-40, Airworthiness
Limitations, DGT 113877, Revision 11, dated November 2017, of the
Dassault Falcon 2000EX Maintenance Manual, which the Director of the
Federal Register approved for incorporation by reference as of November
13, 2018 (83 FR 50479, October 9, 2018).
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.
FAA's Determination
This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with the State of Design Authority, The FAA
has been notified of the unsafe condition described in the MCAI and
service information referenced above. The FAA is proposing this AD
because the FAA evaluated all the relevant information and determined
the unsafe condition described previously is likely to exist or develop
on other products of the same type design.
Proposed Requirements of This NPRM
This proposed AD would retain all requirements of AD 2018-19-27.
This proposed AD would also require revising the existing maintenance
or inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations.
This proposed AD would require revisions to certain operator
maintenance documents to include new actions (e.g., inspections).
Compliance with these actions is required by 14 CFR 91.403(c). For
airplanes that have been previously modified, altered, or repaired in
the areas addressed by this proposed AD, the operator may not be able
to accomplish the actions described in the revisions. In this
situation, to comply with 14 CFR 91.403(c), the operator must request
approval for an alternative method of compliance according to paragraph
(l)(1) of this proposed AD.
Costs of Compliance
The FAA estimates that this proposed AD affects 173 airplanes of
U.S. registry. The FAA estimates the following costs to comply with
this proposed AD:
The FAA estimates the total cost per operator for the retained
actions from AD 2018-19-27 to be $7,650 (90 work-hours x $85 per work-
hour).
The FAA has determined that the new revision of the existing
maintenance or inspection program takes an average of 90 work-hours per
operator, although the FAA recognizes that this number may vary from
operator to operator. In the past, the FAA has estimated that this
action takes 1 work-hour per airplane. Since operators incorporate
maintenance or inspection program changes for their affected fleet(s),
the FAA has determined that a per-operator estimate is more accurate
than a per-airplane estimate. Therefore, the FAA estimates the total
cost per operator to be $7,650 (90 work-hours x $85 per work-hour).
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.
This proposed AD is issued in accordance with authority delegated
by the Executive Director, Aircraft Certification Service, as
authorized by FAA Order 8000.51C. In accordance with that order,
issuance of ADs is normally a function of the Compliance and
Airworthiness Division, but during this transition period, the
Executive Director has delegated the authority to issue ADs applicable
to transport category airplanes and associated appliances to the
Director of the System Oversight Division.
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 this proposed
regulation:
(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.
[[Page 63829]]
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:
0
a. Removing Airworthiness Directive (AD) 2018-19-27, Amendment 39-19428
(83 FR 50479, October 9, 2018); and AD 2014-16-12, Amendment 39-17936
(79 FR 52187, September 3, 2014); and
0
b. Adding the following new AD:
Dassault Aviation: Docket No. FAA-2019-0870; Product Identifier
2019-NM-125-AD.
(a) Comments Due Date
The FAA must receive comments by January 3, 2020.
(b) Affected ADs
(1) This AD replaces AD 2018-19-27, Amendment 39-19428 (83 FR
50479, October 9, 2018) (``AD 2018-19-27''); and AD 2014-16-12,
Amendment 39-17936 (79 FR 52187, September 3, 2014) (``AD 2014-16-
12'').
(2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR
79952, December 21, 2010) (``AD 2010-26-05'').
(c) Applicability
This AD applies to Dassault Aviation Model FALCON 2000EX
airplanes, certificated in any category, with an original
airworthiness certificate or original export certificate of
airworthiness issued on or before January 15, 2019.
(d) Subject
Air Transport Association (ATA) of America Code 05, Time limits/
maintenance checks.
(e) Reason
This AD was prompted by a determination that new or more
restrictive airworthiness limitations are necessary. The FAA is
issuing this AD to address reduced structural integrity of the
airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Retained Revision of Maintenance or Inspection Program, With No
Changes
This paragraph restates the requirements of paragraph (g) of AD
2018-19-27, with no changes. Within 90 days after November 13, 2018
(the effective date of AD 2018-19-27), revise the existing
maintenance or inspection program, as applicable, to incorporate the
information specified in Chapter 5-40, Airworthiness Limitations,
DGT 113877, Revision 11, dated November 2017, of the Dassault Falcon
2000EX Maintenance Manual. The initial compliance times for doing
the tasks are at the time specified in Chapter 5-40, Airworthiness
Limitations, DGT 113877, Revision 11, dated November 2017, of the
Dassault Falcon 2000EX Maintenance Manual, or within 90 days after
November 13, 2018, whichever occurs later; except for task number
52-20-00-610-801-01, the initial compliance time is within 24 months
after October 8, 2014 (the effective date of AD 2014-16-12). The
term ``LDG'' in the ``First Inspection'' column of any table in
Chapter 5-40, Airworthiness Limitations, DGT 113877, Revision 11,
dated November 2017, means total airplane landings. The term ``FH''
in the ``First Inspection'' column of any table in Chapter 5-40,
Airworthiness Limitations, DGT 113877, Revision 11, dated November
2017, means total flight hours. The term ``FC'' in the ``First
Inspection'' column of any table in Chapter 5-40, Airworthiness
Limitations, DGT 113877, Revision 11, dated November 2017, means
total flight cycles.
(h) Retained Provision: No Alternative Actions or Intervals, With a New
Exception
This paragraph restates the requirements of paragraph (h) of AD
2018-19-27, with a new exception. Except as required by paragraph
(i) of this AD, after the maintenance or inspection program has been
revised as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections) or intervals may be used unless the
actions or intervals are approved as an alternative method of
compliance (AMOC) in accordance with the procedures specified in
paragraph (l)(1) of this AD.
(i) New Maintenance or Inspection Program Revision
Within 90 days after the effective date of this AD, revise the
existing maintenance or inspection program, as applicable, to
incorporate the information specified in Chapter 5-40, Airworthiness
Limitations, DGT 113877, Revision 12, dated November 2018, of the
Dassault Falcon 2000EX Maintenance Manual. The initial compliance
times for doing the tasks are at the time specified in Chapter 5-40,
Airworthiness Limitations, DGT 113877, Revision 12, dated November
2018, of the Dassault Falcon 2000EX Maintenance Manual, or within 90
days after the effective date of this AD, whichever occurs later;
except for task number 52-20-00-610-801-01, the initial compliance
time is within 24 months after October 8, 2014 (the effective date
of AD 2014-16-12). The term ``LDG'' in the ``First Inspection''
column of any table in the service information specified in this
paragraph means total airplane landings. The term ``FH'' in the
``First Inspection'' column of any table in the service information
specified in this paragraph means total flight hours. The term
``FC'' in the ``First Inspection'' column of any table in the
service information specified in this paragraph means total flight
cycles. Doing the revision required by this paragraph terminates the
actions required by paragraph (g) of this AD.
(j) New Provision: No Alternative Actions or Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (i) of this AD, no alternative
actions (e.g., inspections) or intervals may be used unless the
actions or intervals are approved as an AMOC in accordance with the
procedures specified in paragraph (l)(1) of this AD.
(k) Terminating Action for Certain Actions in AD 2010-26-05
Accomplishing the actions required by paragraph (g) or (i) of
this AD terminates the requirements of paragraph (g)(1) of AD 2010-
26-05, for Dassault Aviation Model FALCON 2000EX airplanes.
(l) Other FAA AD Provisions
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Section, Transport Standards 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 International Section, send it to the attention of
the person identified in paragraph (m)(2) of this AD. Information
may be emailed to [email protected].
(i) 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.
(ii) AMOCs approved previously for AD 2018-19-27 are not
approved as AMOCs for this AD.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, International
Section, Transport Standards Branch, FAA; or the European Union
Aviation Safety Agency (EASA); or Dassault Aviation's EASA Design
Organization Approval (DOA). If approved by the DOA, the approval
must include the DOA-authorized signature.
(m) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD 2019-0154, dated July 3, 2019, for related
information. This MCAI may be found in the AD docket on the internet
at https://www.regulations.gov by searching for and locating Docket
No. FAA-2019-0870.
(2) For more information about this AD, contact Tom Rodriguez,
Aerospace Engineer, International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; phone and
fax: 206-231-3226.
(3) For service information identified in this AD, contact
Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000,
South Hackensack, NJ 07606; phone: 201-440-6700; internet: https://www.dassaultfalcon.com. You may view this service information at the
FAA, Transport Standards Branch, 2200 South 216th St., Des Moines,
[[Page 63830]]
WA. For information on the availability of this material at the FAA,
call 206-231-3195.
Issued in Des Moines, Washington, on November 7, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2019-24834 Filed 11-18-19; 8:45 am]
BILLING CODE 4910-13-P