Airworthiness Directives; Bombardier, Inc., Airplanes, 20754-20760 [2023-07134]
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approved by the DAO, the approval must
include the DAO-authorized signature.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
(l) Additional Information
(1) Refer to Transport Canada AD CF–
2022–18, dated April 14, 2022, for related
information. This Transport Canada AD may
be found in the AD docket at regulations.gov
under Docket No. FAA–2022–1308.
(2) For more information about this AD,
contact Gabriel Kim, Aerospace Engineer,
Airframe and Propulsion Section, FAA, New
York ACO Branch, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone
516–228–7300; email 9-avs-nyaco-cos@
faa.gov.
(m) Material Incorporated by Reference
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(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(3) The following service information was
approved for IBR on May 12, 2023.
(i) Airbus Canada Limited Partnership
A220 Airworthiness Limitations, BD500–
3AB48–11400–02, Issue 014.00, dated
February 3, 2022.
(ii) [Reserved]
(4) The following service information was
approved for IBR on March 30, 2021 (86 FR
10799, February 23, 2021).
(i) Airbus Canada Limited Partnership
A220 Airworthiness Limitations, BD500–
3AB48–11400–02, Issue 011.00, dated June
18, 2020.
(ii) [Reserved]
(5) For service information identified in
this AD, contact Airbus Canada Limited
Partnership, 13100 Henri-Fabre Boulevard,
Mirabel, Que´bec J7N 3C6, Canada; telephone
450–476–7676; email a220_
website a220world.airbus.com.
(6) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South 216th
St., Des Moines, WA. For information on the
availability of this material at the FAA, call
206–231–3195.
(7) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA,
email fr.inspection@nara.gov, or go to:
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on March 5, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–07096 Filed 4–6–23; 8:45 am]
BILLING CODE 4910–13–P
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14 CFR Part 39
[Docket No. FAA–2022–1661; Project
Identifier MCAI–2022–00714–T; Amendment
39–22380; AD 2023–05–11]
RIN 2120–AA64
• You may view this service
information at the FAA, Airworthiness
Products Section, Operational Safety
Branch, 2200 South 216th St., Des
Moines, WA. For information on the
availability of this material at the FAA,
call 206–231–3195. It is also available at
regulations.gov under Docket No. FAA–
2022–1661.
FOR FURTHER INFORMATION CONTACT:
Airworthiness Directives; Bombardier,
Inc., Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
Bombardier, Inc., Model BD–700–1A10
and BD–700–1A11 airplanes. This AD
was prompted by a report that in case
of a flap, slat, or slat-flap failure in
flight, resetting the slat flap control unit
(SFCU) to clear the error using the
airplane flight manual (AFM) could
result in the stall protection computer
(SPC) setting the low-speed cue to the
most conservative stall advance mode.
This AD requires revising the nonnormal procedures section of the
existing AFM to provide the flightcrew
with procedures for addressing failure
warnings in the slat and flap control
systems. The FAA is issuing this AD to
address the unsafe condition on these
products.
SUMMARY:
This AD is effective May 12,
2023.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of May 12, 2023.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2022–1661; 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 mandatory
continuing airworthiness information
(MCAI), any comments received, and
other information. The address for
Docket Operations is U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
Material Incorporated by Reference:
• For service information identified
in this final rule, contact Bombardier
Business Aircraft Customer Response
Center, 400 Coˆte-Vertu Road West,
Dorval, Que´bec H4S 1Y9, Canada;
telephone 514–855–2999; email ac.yul@
aero.bombardier.com; website
bombardier.com.
DATES:
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Elizabeth Dowling, Aerospace Engineer,
Mechanical Systems and Administrative
Services Section, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone
516–228–7300; email 9-avs-nyaco-cos@
faa.gov.
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 certain Bombardier, Inc., Model
BD–700–1A10 and BD–700–1A11
airplanes. The NPRM published in the
Federal Register on January 13, 2023
(88 FR 2286). The NPRM was prompted
by AD CF–2022–30, dated June 3, 2022,
(referred to after this as the MCAI)
issued by Transport Canada, which is
the aviation authority for Canada. The
MCAI states in case of a flap, slat, or
slat-flap failure in flight, resetting the
SFCU to clear the error using the AFM
could result in the SPC setting the lowspeed cue to the most conservative stall
advance mode instead of that published
in the AFM. This condition could result
in unexpected stall warnings (aural and
visual) as well as stick shaker activation
during approach for a landing,
increasing flightcrew workload during a
critical phase of flight. The higher
landing speed could consequently
require a greater landing distance and
possible diversion to a longer runway.
In the NPRM, the FAA proposed to
require revising the non-normal
procedures section of the existing AFM
to provide the flightcrew with
procedures for addressing failure
warnings in the slat and flap control
systems. The FAA is issuing this AD to
address the unsafe condition on these
products.
You may examine the MCAI in the
AD docket at regulations.gov under
Docket No. FAA–2022–1661.
Discussion of Final Airworthiness
Directive
Comments
The FAA received no comments on
the NPRM or on the determination of
the cost to the public.
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Conclusion
This product has been approved by
the aviation authority of another
country and is approved for operation in
the United States. Pursuant to the FAA’s
bilateral agreement with this State of
Design Authority, it has notified the
FAA of the unsafe condition described
in the MCAI referenced above. The FAA
reviewed the relevant data and
determined that air safety requires
adopting this AD as proposed.
Accordingly, the FAA is issuing this AD
to address the unsafe condition on this
product. Except for minor editorial
changes, this AD is adopted as proposed
in the NPRM. None of the changes will
increase the economic burden on any
operator.
Related Service Information Under 1
CFR Part 51
The FAA reviewed the following
Bombardier service information. This
service information specifies procedures
for revising the non-normal procedures
section of the existing AFM to provide
the flightcrew with procedures for
addressing failure warnings in the slat
and flap control systems. These
documents are distinct since they apply
to different airplane models.
• C. Flap Fail (Caution), D. Slat Fail
(Caution), E. Slat-Flap Fail (Caution),
and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution)
procedures of the Slat and Flap Control
System, Section 05–10, Flight Controls,
Chapter 5—Non Normal Procedure, of
the Bombardier Global Express AFM,
Publication No. CSP 700–1, Revision
112, dated May 19, 2022. (For obtaining
the procedures for Bombardier Global
Express AFM, Publication No. CSP 700–
1, use Document Identification No. GL
700 AFM–1.)
• C. Flap Fail (Caution), D. Slat Fail
(Caution), E. Slat-Flap Fail (Caution),
and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution)
procedures of the Slat and Flap Control
System, Section 05–10, Flight Controls,
Chapter 5—Non Normal Procedure, of
the Bombardier Global Express XRS
AFM, Publication No. CSP 700–1A,
Revision 112, dated May 19, 2022. (For
obtaining the procedures for Bombardier
Global Express XRS AFM, Publication
No. CSP 700–1A, use Document
Identification No. GL 700 AFM–1A.)
• C. Flap Fail (Caution), D. Slat Fail
(Caution), E. Slat-Flap Fail (Caution),
and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution)
procedures of the Slat and Flap Control
System, Section 05–10, Flight Controls,
Chapter 5—Non Normal Procedure, of
the Bombardier Global 5000 AFM,
Publication No. CSP 700–5000–1,
Revision 73, dated May 19, 2022. (For
obtaining the procedures for Bombardier
Global Express AFM, Publication No.
CSP 700–5000–1, use Document
Identification No. GL 5000 AFM.)
• C. Flap Fail (Caution), D. Slat Fail
(Caution), E. Slat-Flap Fail (Caution),
and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution)
procedures of the Slat and Flap Control
System, Section 05–10, Flight Controls,
Chapter 5—Non Normal Procedure, of
the Bombardier Global 5000 AFM,
Publication No. CSP 700–5000–1V,
Revision 42, dated May 19, 2022. (For
obtaining the procedures for Bombardier
Global Express AFM, Publication No.
CSP 700–5000–1V, use Document
Identification No. GL 5000 GVFD AFM.)
• C. Flap Fail (Caution), D. Slat Fail
(Caution), E. Slat-Flap Fail (Caution),
and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution)
procedures of the Slat and Flap Control
System, Section 05–10, Flight Controls,
20755
Chapter 5—Non Normal Procedure, of
the Bombardier Global 5500 AFM,
Publication No. CSP 700–5500–1,
Revision 14, dated May 19, 2022. (For
obtaining the procedures for Bombardier
Global Express AFM, Publication No.
CSP 700–5000–1V, use Document
Identification No. GL 5500 AFM.)
• C. Flap Fail (Caution), D. Slat Fail
(Caution), E. Slat-Flap Fail (Caution),
and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution)
procedures of the Slat and Flap Control
System, Section 05–10, Flight Controls,
Chapter 5—Non Normal Procedure, of
the Bombardier Global 6000 AFM,
Publication No. CSP 700–1V, Revision
42, dated May 19, 2022. (For obtaining
the procedures for Bombardier Global
Express AFM, Publication No. CSP 700–
1V, use Document Identification No. GL
6000 AFM.)
• C. Flap Fail (Caution), D. Slat Fail
(Caution), E. Slat-Flap Fail (Caution),
and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution)
procedures of the Slat and Flap Control
System, Section 05–10, Flight Controls,
Chapter 5—Non Normal Procedure, of
the Bombardier Global 6500 AFM,
Publication No. CSP 700–6500–1,
Revision 14, dated May 19, 2022. (For
obtaining the procedures for Bombardier
Global Express AFM, Publication No.
CSP 700–5000–1V, use Document
Identification No. GL 6500 AFM.)
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.
Costs of Compliance
The FAA estimates that this AD
affects 450 airplanes of U.S. registry.
The FAA estimates the following costs
to comply with this AD:
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ESTIMATED COSTS FOR REQUIRED ACTIONS
Labor cost
Parts cost
Cost per
product
Cost on U.S.
operators
1 work-hour × $85 per hour = $85 ..............................................................................................
$0
$85
$38,250
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
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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.
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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:
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Federal Register / Vol. 88, No. 67 / Friday, April 7, 2023 / Rules and Regulations
(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:
1. The authority citation for part 39
continues to read as follows:
■
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Authority: 49 U.S.C. 106(g), 40113, 44701.
16:44 Apr 06, 2023
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[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
2023–05–11 Bombardier, Inc.: Amendment
39–22380; Docket No. FAA–2022–1661;
Project Identifier MCAI–2022–00714–T.
(a) Effective Date
This airworthiness directive (AD) is
effective May 12, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc.,
Model BD–700–1A10 and BD–700–1A11
airplanes, certificated in any category, having
serial numbers 9001 through 9998 inclusive
and 60001 through 60097 inclusive.
(d) Subject
Air Transport Association (ATA) of
America Code 27, Flight controls.
PART 39—AIRWORTHINESS
DIRECTIVES
VerDate Sep<11>2014
§ 39.13
■
(e) Unsafe Condition
This AD was prompted by a report that in
case of a flap, slat, or slat-flap failure in
flight, resetting the slat flap control unit
PO 00000
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(SFCU) to clear the error using the airplane
flight manual (AFM) could result in the stall
protection computer (SPC) setting the lowspeed cue to the most conservative stall
advance mode. The FAA is issuing this AD
to address a flap, slat, or slat-flap failure
warning. The unsafe condition, if not
addressed, could result in unexpected stall
warnings (aural and visual) as well as stick
shaker activation during approach for a
landing, increasing flightcrew workload
during a critical phase of flight. The higher
landing speed could consequently require a
greater landing distance and possible
diversion to a longer runway.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Revision of the Existing AFM
Within 30 days after the effective date of
this AD: Revise the existing AFM to
incorporate the information specified in the
AFM sections of the applicable AFM
revisions specified in figure 1 to paragraph
(g) of this AD.
Figure 1 to paragraph (g)—AFM References
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Federal Register / Vol. 88, No. 67 / Friday, April 7, 2023 / Rules and Regulations
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, New York 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
responsible Flight Standards Office, as
appropriate. If sending information directly
to the manager of the New York ACO Branch,
mail it to ATTN: Program Manager,
Continuing Operational Safety, at the address
identified in paragraph (i)(2) of this AD or
email to: 9-avs-nyaco-cos@faa.gov. If mailing
information, also submit information by
email. Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
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(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, New York ACO Branch,
FAA; or Transport Canada; or Bombardier,
Inc.’s Transport Canada Design Approval
Organization (DAO). If approved by the DAO,
the approval must include the DAOauthorized signature.
(i) Additional Information
(1) Refer to Transport Canada AD CF–
2022–30, dated June 3, 2022, for related
information. This Transport Canada AD may
be found in the AD docket at regulations.gov
under Docket No. FAA–2022–1661.
(2) For more information about this AD,
contact Elizabeth Dowling, Aerospace
Engineer, Mechanical Systems and
Administrative Services Section, FAA, New
York ACO Branch, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone
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516–228–7300; email 9-avs-nyaco-cos@
faa.gov.
(j) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference of
the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(i) Slat and Flap Control System, Section
05–10, Flight Controls, Chapter 5—Non
Normal Procedures, of the Bombardier Global
Express AFM, Publication No. CSP 700–1,
Revision 112, dated May 19, 2022.
Note 1 to paragraph (j)(2)(i): For obtaining
the procedures for Bombardier Global
Express AFM, Publication No. CSP 700–1,
use Document Identification No. GL 700
AFM–1.
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(h) Additional AD Provisions
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(ii) Slat and Flap Control System, Section
05–10, Flight Controls, Chapter 5—Non
Normal Procedures, of the Bombardier Global
Express XRS AFM, Publication No. CSP 700–
1A, Revision 112, dated May 19, 2022.
Note 2 to paragraph (j)(2)(ii): For obtaining
the procedures for Bombardier Global
Express XRS AFM, Publication No. CSP 700–
1A, use Document Identification No. GL 700
AFM–1A.
(iii) Slat and Flap Control System, Section
05–10, Flight Controls, Chapter 5—Non
Normal Procedures, of the Bombardier Global
5000 AFM, Publication No. CSP 700–5000–
1, Revision 73, dated May 19, 2022.
Note 3 to paragraph (j)(2)(iii): For
obtaining the procedures for Bombardier
Global Express AFM, Publication No. CSP
700–5000–1, use Document Identification
No. GL 5000 AFM.
(iv) Slat and Flap Control System, Section
05–10, Flight Controls, Chapter 5—Non
Normal Procedures, of the Bombardier Global
5000 AFM, Publication No. CSP 700–5000–
1V, Revision 42, dated May 19, 2022.
Note 4 to paragraph (j)(2)(iv): For
obtaining the procedures for Bombardier
Global Express AFM, Publication No. CSP
700–5000–1V, use Document Identification
No. GL 5000 GVFD AFM.
(v) Slat and Flap Control System, Section
05–10, Flight Controls, Chapter 5—Non
Normal Procedures, of the Bombardier Global
5500 AFM, Publication No. CSP 700–5500–
1, Revision 14, dated May 19, 2022.
Note 5 to paragraph (j)(2)(v): For obtaining
the procedures for Bombardier Global
Express AFM, Publication No. CSP 700–
5000–1V, use Document Identification No.
GL 5500 AFM.
(vi) Slat and Flap Control System, Section
05–10, Flight Controls, Chapter 5—Non
Normal Procedures, of the Bombardier Global
6000 AFM, Publication No. CSP 700–1V,
Revision 42, dated May 19, 2022.
Note 6 to paragraph (j)(2)(vi): For
obtaining the procedures for Bombardier
Global Express AFM, Publication No. CSP
700–1V, use Document Identification No. GL
6000 AFM.
(vii) Slat and Flap Control System, Section
05–10, Flight Controls, Chapter 5—Non
Normal Procedures, of the Bombardier Global
6500 AFM, Publication No. CSP 700–6500–
1, Revision 14, dated May 19, 2022.
Note 7 to paragraph (j)(2)(vii): For
obtaining the procedures for Bombardier
Global Express AFM, Publication No. CSP
700–5000–1V, use Document Identification
No. GL 6500 AFM.
(3) For service information identified in
this AD, contact Bombardier Business
Aircraft Customer Response Center, 400 CoˆteVertu Road West, Dorval, Que´bec H4S 1Y9,
Canada; telephone 514–855–2999; email
ac.yul@aero.bombardier.com; website
bombardier.com.
(4) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South 216th
St., Des Moines, WA. For information on the
availability of this material at the FAA, call
206–231–3195.
(5) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA,
email fr.inspection@nara.gov, or go to:
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on March 9, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–07134 Filed 4–6–23; 8:45 am]
BILLING CODE 4910–13–P
SECURITIES AND EXCHANGE
COMMISSION
17 CFR Parts 229, 232, 240, and 249
[Release Nos. 33–11138; 34–96492; File No.
S7–20–21]
RIN 3235–AM86
Insider Trading Arrangements and
Related Disclosures
Correction
In rule document 2022–27675,
appearing on pages 80362–80432 in the
issue of Thursday, December 29, 2022,
make the following correction:
§ 229.601
[Corrected]
Beginning on page 80428, the ‘‘Exhibit
Table’’ is correct to read as set forth
below:
■
EXHIBIT TABLE
Securities act forms
S–1
*
(19) Insider trading policies and
procedures ...............................
*
S–3
SF–1
*
........
SF–3
S–4 1
S–8
*
........
..........
*
..........
S–11
Exchange act forms
F–1
*
..........
........
*
F–3
F–4 1
8–K 2
10
*
..........
........
*
........
10–D
*
..........
......
............
*
*
10–Q
10–K
ABS–EE
X
..............
*
..........
..........
*
1 An
exhibit need not be provided about a company if: (1) With respect to such company an election has been made under Form S–4 or F–4 to provide information
about such company at a level prescribed by Form S–3 or F–3; and (2) the form, the level of which has been elected under Form S–4 or F–4, would not require such
company to provide such exhibit if it were registering a primary offering.
2 A Form 8–K exhibit is required only if relevant to the subject matter reported on the Form 8–K report. For example, if the Form 8–K pertains to the departure of a
director, only the exhibit described in paragraph (b)(17) of this section need be filed. A required exhibit may be incorporated by reference from a previous filing.
[FR Doc. C1–2022–27675 Filed 4–6–23; 8:45 am]
BILLING CODE 0099–10–P
CENTRAL INTELLIGENCE AGENCY
32 CFR Part 1903
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Conduct on Agency Installations
Central Intelligence Agency.
Final rule.
AGENCY:
ACTION:
The Central Intelligence
Agency (CIA) is amending its
installation security regulations to
include Office of the Director of
National Intelligence (ODNI) property in
SUMMARY:
VerDate Sep<11>2014
17:04 Apr 06, 2023
Jkt 259001
the definition of Agency installation,
which reflects the Agency’s authority to
provide security on ODNI installations.
The CIA is also removing the exemption
for Federal officials or members of the
Armed Forces from its prohibition on
carrying weapons on Agency
installations, except when such persons
are either authorized by the CIA
Director of Security or otherwise
authorized by law for the performance
of official law enforcement duties. This
amendment also revises the definition
of weapon to permit small amounts of
irritant gas on Agency installations and
revises the penalties provision to clarify
that the penalty for a violation of these
PO 00000
Frm 00034
Fmt 4700
Sfmt 4700
regulations is up to a Class C
misdemeanor.
DATES:
This rule is effective April 7,
2023.
Court Liaison Officer, Office
of Security, Central Intelligence Agency,
Washington, DC 20505. Please include
‘‘Security Rulemaking’’ in the subject
line of the letter.
FOR FURTHER INFORMATION CONTACT:
Court Liaison Officer, (571) 280–3563.
SUPPLEMENTARY INFORMATION:
ADDRESSES:
Background
Section 15 of the Central Intelligence
Agency Act of 1949, as amended (50
E:\FR\FM\07APR1.SGM
07APR1
]]>Agencies
[Federal Register Volume 88, Number 67 (Friday, April 7, 2023)]
[Rules and Regulations]
[Pages 20754-20760]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-07134]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1661; Project Identifier MCAI-2022-00714-T;
Amendment 39-22380; AD 2023-05-11]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc., Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes.
This AD was prompted by a report that in case of a flap, slat, or slat-
flap failure in flight, resetting the slat flap control unit (SFCU) to
clear the error using the airplane flight manual (AFM) could result in
the stall protection computer (SPC) setting the low-speed cue to the
most conservative stall advance mode. This AD requires revising the
non-normal procedures section of the existing AFM to provide the
flightcrew with procedures for addressing failure warnings in the slat
and flap control systems. The FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective May 12, 2023.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of May 12, 2023.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-1661; 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 mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
address for Docket Operations is U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE, Washington, DC 20590.
Material Incorporated by Reference:
For service information identified in this final rule,
contact Bombardier Business Aircraft Customer Response Center, 400
C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada;
telephone 514-855-2999; email bombardier.com">[email protected]bombardier.com; website
bombardier.com.
You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200 South
216th St., Des Moines, WA. For information on the availability of this
material at the FAA, call 206-231-3195. It is also available at
regulations.gov under Docket No. FAA-2022-1661.
FOR FURTHER INFORMATION CONTACT: Elizabeth Dowling, Aerospace Engineer,
Mechanical Systems and Administrative Services Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7300; 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 certain Bombardier,
Inc., Model BD-700-1A10 and BD-700-1A11 airplanes. The NPRM published
in the Federal Register on January 13, 2023 (88 FR 2286). The NPRM was
prompted by AD CF-2022-30, dated June 3, 2022, (referred to after this
as the MCAI) issued by Transport Canada, which is the aviation
authority for Canada. The MCAI states in case of a flap, slat, or slat-
flap failure in flight, resetting the SFCU to clear the error using the
AFM could result in the SPC setting the low-speed cue to the most
conservative stall advance mode instead of that published in the AFM.
This condition could result in unexpected stall warnings (aural and
visual) as well as stick shaker activation during approach for a
landing, increasing flightcrew workload during a critical phase of
flight. The higher landing speed could consequently require a greater
landing distance and possible diversion to a longer runway.
In the NPRM, the FAA proposed to require revising the non-normal
procedures section of the existing AFM to provide the flightcrew with
procedures for addressing failure warnings in the slat and flap control
systems. The FAA is issuing this AD to address the unsafe condition on
these products.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2022-1661.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the cost to the public.
[[Page 20755]]
Conclusion
This product has been approved by the aviation authority of another
country and is approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with this State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI
referenced above. The FAA reviewed the relevant data and determined
that air safety requires adopting this AD as proposed. Accordingly, the
FAA is issuing this AD to address the unsafe condition on this product.
Except for minor editorial changes, this AD is adopted as proposed in
the NPRM. None of the changes will increase the economic burden on any
operator.
Related Service Information Under 1 CFR Part 51
The FAA reviewed the following Bombardier service information. This
service information specifies procedures for revising the non-normal
procedures section of the existing AFM to provide the flightcrew with
procedures for addressing failure warnings in the slat and flap control
systems. These documents are distinct since they apply to different
airplane models.
C. Flap Fail (Caution), D. Slat Fail (Caution), E. Slat-
Flap Fail (Caution), and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution) procedures of the Slat and Flap
Control System, Section 05-10, Flight Controls, Chapter 5--Non Normal
Procedure, of the Bombardier Global Express AFM, Publication No. CSP
700-1, Revision 112, dated May 19, 2022. (For obtaining the procedures
for Bombardier Global Express AFM, Publication No. CSP 700-1, use
Document Identification No. GL 700 AFM-1.)
C. Flap Fail (Caution), D. Slat Fail (Caution), E. Slat-
Flap Fail (Caution), and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution) procedures of the Slat and Flap
Control System, Section 05-10, Flight Controls, Chapter 5--Non Normal
Procedure, of the Bombardier Global Express XRS AFM, Publication No.
CSP 700-1A, Revision 112, dated May 19, 2022. (For obtaining the
procedures for Bombardier Global Express XRS AFM, Publication No. CSP
700-1A, use Document Identification No. GL 700 AFM-1A.)
C. Flap Fail (Caution), D. Slat Fail (Caution), E. Slat-
Flap Fail (Caution), and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution) procedures of the Slat and Flap
Control System, Section 05-10, Flight Controls, Chapter 5--Non Normal
Procedure, of the Bombardier Global 5000 AFM, Publication No. CSP 700-
5000-1, Revision 73, dated May 19, 2022. (For obtaining the procedures
for Bombardier Global Express AFM, Publication No. CSP 700-5000-1, use
Document Identification No. GL 5000 AFM.)
C. Flap Fail (Caution), D. Slat Fail (Caution), E. Slat-
Flap Fail (Caution), and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution) procedures of the Slat and Flap
Control System, Section 05-10, Flight Controls, Chapter 5--Non Normal
Procedure, of the Bombardier Global 5000 AFM, Publication No. CSP 700-
5000-1V, Revision 42, dated May 19, 2022. (For obtaining the procedures
for Bombardier Global Express AFM, Publication No. CSP 700-5000-1V, use
Document Identification No. GL 5000 GVFD AFM.)
C. Flap Fail (Caution), D. Slat Fail (Caution), E. Slat-
Flap Fail (Caution), and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution) procedures of the Slat and Flap
Control System, Section 05-10, Flight Controls, Chapter 5--Non Normal
Procedure, of the Bombardier Global 5500 AFM, Publication No. CSP 700-
5500-1, Revision 14, dated May 19, 2022. (For obtaining the procedures
for Bombardier Global Express AFM, Publication No. CSP 700-5000-1V, use
Document Identification No. GL 5500 AFM.)
C. Flap Fail (Caution), D. Slat Fail (Caution), E. Slat-
Flap Fail (Caution), and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution) procedures of the Slat and Flap
Control System, Section 05-10, Flight Controls, Chapter 5--Non Normal
Procedure, of the Bombardier Global 6000 AFM, Publication No. CSP 700-
1V, Revision 42, dated May 19, 2022. (For obtaining the procedures for
Bombardier Global Express AFM, Publication No. CSP 700-1V, use Document
Identification No. GL 6000 AFM.)
C. Flap Fail (Caution), D. Slat Fail (Caution), E. Slat-
Flap Fail (Caution), and F. Slat Fault (Caution) or Flap Fault
(Caution) or Slat-Flap Fault (Caution) procedures of the Slat and Flap
Control System, Section 05-10, Flight Controls, Chapter 5--Non Normal
Procedure, of the Bombardier Global 6500 AFM, Publication No. CSP 700-
6500-1, Revision 14, dated May 19, 2022. (For obtaining the procedures
for Bombardier Global Express AFM, Publication No. CSP 700-5000-1V, use
Document Identification No. GL 6500 AFM.)
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.
Costs of Compliance
The FAA estimates that this AD affects 450 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
1 work-hour x $85 per hour = $85............................. $0 $85 $38,250
----------------------------------------------------------------------------------------------------------------
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:
[[Page 20756]]
(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:
2023-05-11 Bombardier, Inc.: Amendment 39-22380; Docket No. FAA-
2022-1661; Project Identifier MCAI-2022-00714-T.
(a) Effective Date
This airworthiness directive (AD) is effective May 12, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc., Model BD-700-1A10 and BD-
700-1A11 airplanes, certificated in any category, having serial
numbers 9001 through 9998 inclusive and 60001 through 60097
inclusive.
(d) Subject
Air Transport Association (ATA) of America Code 27, Flight
controls.
(e) Unsafe Condition
This AD was prompted by a report that in case of a flap, slat,
or slat-flap failure in flight, resetting the slat flap control unit
(SFCU) to clear the error using the airplane flight manual (AFM)
could result in the stall protection computer (SPC) setting the low-
speed cue to the most conservative stall advance mode. The FAA is
issuing this AD to address a flap, slat, or slat-flap failure
warning. The unsafe condition, if not addressed, could result in
unexpected stall warnings (aural and visual) as well as stick shaker
activation during approach for a landing, increasing flightcrew
workload during a critical phase of flight. The higher landing speed
could consequently require a greater landing distance and possible
diversion to a longer runway.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Revision of the Existing AFM
Within 30 days after the effective date of this AD: Revise the
existing AFM to incorporate the information specified in the AFM
sections of the applicable AFM revisions specified in figure 1 to
paragraph (g) of this AD.
Figure 1 to paragraph (g)--AFM References
[[Page 20757]]
[GRAPHIC] [TIFF OMITTED] TR07AP23.012
[[Page 20758]]
[GRAPHIC] [TIFF OMITTED] TR07AP23.013
[[Page 20759]]
[GRAPHIC] [TIFF OMITTED] TR07AP23.014
(h) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York 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 responsible Flight Standards Office, as appropriate. If
sending information directly to the manager of the New York ACO
Branch, mail it to ATTN: Program Manager, Continuing Operational
Safety, at the address identified in paragraph (i)(2) of this AD or
email to: [email protected]. If mailing information, also
submit information by email. Before using any approved AMOC, notify
your appropriate principal inspector, or lacking a principal
inspector, the manager of the responsible Flight Standards Office.
(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, New York ACO
Branch, FAA; or Transport Canada; or Bombardier, Inc.'s Transport
Canada Design Approval Organization (DAO). If approved by the DAO,
the approval must include the DAO-authorized signature.
(i) Additional Information
(1) Refer to Transport Canada AD CF-2022-30, dated June 3, 2022,
for related information. This Transport Canada AD may be found in
the AD docket at regulations.gov under Docket No. FAA-2022-1661.
(2) For more information about this AD, contact Elizabeth
Dowling, Aerospace Engineer, Mechanical Systems and Administrative
Services Section, FAA, New York ACO Branch, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone 516-228-7300; email [email protected].
(j) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) Slat and Flap Control System, Section 05-10, Flight
Controls, Chapter 5--Non Normal Procedures, of the Bombardier Global
Express AFM, Publication No. CSP 700-1, Revision 112, dated May 19,
2022.
Note 1 to paragraph (j)(2)(i): For obtaining the procedures for
Bombardier Global Express AFM, Publication No. CSP 700-1, use
Document Identification No. GL 700 AFM-1.
[[Page 20760]]
(ii) Slat and Flap Control System, Section 05-10, Flight
Controls, Chapter 5--Non Normal Procedures, of the Bombardier Global
Express XRS AFM, Publication No. CSP 700-1A, Revision 112, dated May
19, 2022.
Note 2 to paragraph (j)(2)(ii): For obtaining the procedures for
Bombardier Global Express XRS AFM, Publication No. CSP 700-1A, use
Document Identification No. GL 700 AFM-1A.
(iii) Slat and Flap Control System, Section 05-10, Flight
Controls, Chapter 5--Non Normal Procedures, of the Bombardier Global
5000 AFM, Publication No. CSP 700-5000-1, Revision 73, dated May 19,
2022.
Note 3 to paragraph (j)(2)(iii): For obtaining the procedures
for Bombardier Global Express AFM, Publication No. CSP 700-5000-1,
use Document Identification No. GL 5000 AFM.
(iv) Slat and Flap Control System, Section 05-10, Flight
Controls, Chapter 5--Non Normal Procedures, of the Bombardier Global
5000 AFM, Publication No. CSP 700-5000-1V, Revision 42, dated May
19, 2022.
Note 4 to paragraph (j)(2)(iv): For obtaining the procedures for
Bombardier Global Express AFM, Publication No. CSP 700-5000-1V, use
Document Identification No. GL 5000 GVFD AFM.
(v) Slat and Flap Control System, Section 05-10, Flight
Controls, Chapter 5--Non Normal Procedures, of the Bombardier Global
5500 AFM, Publication No. CSP 700-5500-1, Revision 14, dated May 19,
2022.
Note 5 to paragraph (j)(2)(v): For obtaining the procedures for
Bombardier Global Express AFM, Publication No. CSP 700-5000-1V, use
Document Identification No. GL 5500 AFM.
(vi) Slat and Flap Control System, Section 05-10, Flight
Controls, Chapter 5--Non Normal Procedures, of the Bombardier Global
6000 AFM, Publication No. CSP 700-1V, Revision 42, dated May 19,
2022.
Note 6 to paragraph (j)(2)(vi): For obtaining the procedures for
Bombardier Global Express AFM, Publication No. CSP 700-1V, use
Document Identification No. GL 6000 AFM.
(vii) Slat and Flap Control System, Section 05-10, Flight
Controls, Chapter 5--Non Normal Procedures, of the Bombardier Global
6500 AFM, Publication No. CSP 700-6500-1, Revision 14, dated May 19,
2022.
Note 7 to paragraph (j)(2)(vii): For obtaining the procedures
for Bombardier Global Express AFM, Publication No. CSP 700-5000-1V,
use Document Identification No. GL 6500 AFM.
(3) For service information identified in this AD, contact
Bombardier Business Aircraft Customer Response Center, 400
C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada;
telephone 514-855-2999; email bombardier.com">[email protected]bombardier.com; website
bombardier.com.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th St., Des Moines, WA. For information on the availability
of this material at the FAA, call 206-231-3195.
(5) You may view this 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 March 9, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-07134 Filed 4-6-23; 8:45 am]
BILLING CODE 4910-13-P
