Airworthiness Directives; Bombardier, Inc., Airplanes, 56259-56264 [2022-19778]
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Federal Register / Vol. 87, No. 177 / Wednesday, September 14, 2022 / Rules and Regulations
or a Form EOIR–28 with the
immigration court, or has previously
entered a limited appearance using a
Form EOIR–60 in connection with
document assistance under paragraph
(g)(2) of this section.
(ii) Effect of filing Form EOIR–27. A
practitioner who enters an appearance
using Form EOIR–27 is the practitioner
of record and must appear before the
Board on behalf of the respondent, file
all documents on behalf of the
respondent, and accept service of
process of all documents filed in the
proceedings, consistent with 8 CFR
1292.5. Filing a Form EOIR–27 provides
the practitioner with access to the
record of proceedings during the course
of proceedings. A respondent shall be
considered represented for the
proceedings in which a Form EOIR–27
has been filed.
(iii) Withdrawal or substitution. A
practitioner who enters an appearance
on behalf of a respondent before the
Board by filing a Form EOIR–27 remains
the practitioner of record unless the
Board permits withdrawal or
substitution during proceedings only
upon written motion submitted without
fee.
(2) Entering a limited appearance for
document assistance using Form EOIR–
60. A practitioner who provides
assistance to a pro se respondent with
the drafting, completion, or filling in of
blank spaces of a motion, brief, form, or
other specific document or set of
documents intended to be filed with the
Board, regardless of whether such
assistance is considered ‘‘practice’’ or
‘‘preparation’’ as defined in § 1001.1,
must disclose such limited assistance to
the Board using Form EOIR–60, unless
pursuant to paragraph (g)(1) the
practitioner has filed a Form EOIR–27 to
become the practitioner of record.
(i) Filing Form EOIR–60. A Form
EOIR–60 must not be filed as a
standalone document. The single Form
EOIR–60 must be filed with the Board
at the same time as the document or set
of documents with which the
practitioner assisted. Any subsequent
filing of a document or set of documents
with which a practitioner assisted must
be accompanied by a new Form EOIR–
60.
(ii) Effect of Filing Form EOIR–60. A
practitioner who enters a limited
appearance using Form EOIR–60 is not
the practitioner of record, is not
required to appear before the Board, and
is not required to submit a motion to
withdraw or substitute. The submission
of a Form EOIR–60 does not create
additional ongoing obligations between
the practitioner, the respondent, and
EOIR. An appearance through Form
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EOIR–60 does not provide the
practitioner with access to the record of
proceedings. A respondent who
received assistance pursuant to this
paragraph is not represented, remains
pro se, and is subject to service of
process of all documents filed in the
proceedings, consistent with 8 CFR
1292.5.
(3) Completing an appearance form,
proof of qualification, disclosure
requirements, and identification. The
practitioner must properly complete and
sign any Form EOIR–27 or Form EOIR–
60, as required by the form instructions.
A practitioner’s personal appearance or
signature on the Form EOIR–27 or Form
EOIR–60 constitutes a representation
that the person is authorized and
qualified to appear as a practitioner in
accordance with 8 CFR 1292.1. Further
proof that the practitioner meets the
qualifications of a practitioner as
defined in 8 CFR 1292.1 may be
required. The completion of a Form
EOIR–27 or Form EOIR–60 in
connection with an application or form
that requires disclosure of the preparer
does not relieve a practitioner from
complying with the particular
disclosure requirements of the
application or form.
Notwithstanding the filing of a Form
EOIR–27 or Form EOIR–60, the
practitioner must identify themselves by
name, accompanied by their signature,
on any document filed or intended to be
filed with the Board pursuant to an
appearance under paragraph (g)(1) or (2)
of this section.
■ 8. In § 1003.101, revise paragraph (b)
to read as follows:
§ 1003.101
General provisions.
*
*
*
*
*
(b) Persons subject to sanctions.
Persons subject to sanctions include any
practitioner. Attorneys employed by the
Department of Justice shall be subject to
discipline pursuant to § 1003.109.
Nothing in this regulation shall be
construed as authorizing persons who
do not meet the definition of
practitioner to represent individuals
before the Board and the immigration
courts or the DHS.
*
*
*
*
*
■ 9. Amend § 1003.102 by:
■ a. Removing the words ‘‘Immigration
Court’’ in paragraphs (d) and (j) and
adding in their place the words
‘‘immigration court’’;
■ b. Removing the words ‘‘Immigration
Courts’’ in paragraph (f)(2)(i) and adding
in their place the words ‘‘immigration
courts’’;
■ c. Revising paragraphs (t) and (u); and
■ d. Adding paragraph (w).
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56259
The revisions and addition read as
follows:
§ 1003.102
Grounds.
*
*
*
*
*
(t) Repeatedly fails to submit a signed
and completed entry of appearance
using the appropriate form in
compliance with applicable rules and
regulations, including 8 CFR 292.4(a),
1003.17, and 1003.38;
(u) Repeatedly drafts notices, motions,
briefs, or claims that are filed with DHS
or EOIR that reflect little or no attention
to the specific factual or legal issues
applicable to a client’s case, but rather
rely on boilerplate language indicative
of a substantial failure to competently
and diligently represent the client;
*
*
*
*
*
(w) Repeatedly fails to sign any
pleading, application, motion, petition,
brief, or other document prepared,
drafted, or filed with DHS or EOIR. The
practitioner’s signature must be in the
practitioner’s individual name and must
be handwritten or electronically in
conformity with the rules and
instructions of the applicable system.
Dated: September 9, 2022.
Merrick B. Garland,
Attorney General.
[FR Doc. 2022–19882 Filed 9–13–22; 8:45 am]
BILLING CODE 4410–30–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–0398; Project
Identifier MCAI–2020–00881–T; Amendment
39–22085; AD 2022–12–13]
RIN 2120–AA64
Airworthiness Directives; Bombardier,
Inc., Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
Bombardier, Inc., Model CL–600–1A11
(600), CL–600–2A12 (601), and CL–600–
2B16 (601–3A and 601–3R Variants)
airplanes. This AD was prompted by
reports that during certain operating
modes, the flight guidance/autopilot
does not account for engine failure
while capturing an altitude. This AD
requires revising the existing airplane
flight manual (AFM) to provide the
flightcrew with a new limitation and
procedure for operation during certain
SUMMARY:
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Federal Register / Vol. 87, No. 177 / Wednesday, September 14, 2022 / Rules and Regulations
flight modes. The FAA is issuing this
AD to address the unsafe condition on
these products.
DATES: This AD is effective October 19,
2022.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of October 19, 2022.
ADDRESSES: 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; internet
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 on the internet at
regulations.gov by searching for and
locating Docket No. FAA–2022–0398.
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Examining the AD Docket
You may examine the AD docket on
the internet at regulations.gov by
searching for and locating Docket No.
FAA–2022–0398; 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.
FOR FURTHER INFORMATION CONTACT:
Steven Dzierzynski, Aerospace
Engineer, Avionics and Electrical
Systems Section, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone
516–228–7367; email 9-avs-nyaco-cos@
faa.gov.
SUPPLEMENTARY INFORMATION:
Background
Transport Canada Civil Aviation
(TCCA), which is the aviation authority
for Canada, has issued TCCA AD CF–
2020–02, dated February 13, 2020
(TCCA AD CF–2020–02), to correct an
unsafe condition for certain Bombardier,
Inc., Model CL–600–1A11 (600), CL–
600–2A12 (601), and CL–600–2B16
(601–3A, 601–3R, and 604 Variants)
airplanes.
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
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apply to certain Bombardier, Inc., Model
CL–600–1A11 (600), CL–600–2A12
(601), and CL–600–2B16 (601–3A, 601–
3R, and 604 Variants) airplanes. The
NPRM published in the Federal
Register on April 11, 2022 (87 FR
21037). The NPRM was prompted by
reports that during certain operating
modes, the flight guidance/autopilot
does not account for engine failure
while capturing an altitude. The NPRM
proposed to require revising the existing
AFM to provide the flightcrew with a
new limitation and procedure for
operation during certain flight modes.
The FAA is issuing this AD to address
a possible engine failure during or
before a climb while in ALTSEL, ASEL
or ALTS CAP mode, which could cause
the airspeed to drop significantly below
the safe operating speed. Prompt crew
intervention may be required to
maintain a safe operating speed.
Discussion of Final Airworthiness
Directive
Comments
The FAA received no comments on
the NPRM or on the determination of
the cost to the public.
Change to the Applicability
Since the FAA issued the NPRM,
TCCA revised AD CF–2020–02 and
issued TCCA AD CF–2020–02R1, dated
August 11, 2022 (TCCA AD CF–2020–
02R1) (also referred to as the MCAI).
TCCA stated the applicability was
revised to remove Model CL–600–2B16
(604 Variants) as it was determined that
these airplanes do not utilize ALTSEL,
ASEL and ALTS CAP modes in their
configurations. TCCA also stated that
the AFM references for these airplanes
were removed from the TCCA AD. You
may examine the MCAI in the AD
docket on the internet at regulations.gov
by searching for and locating Docket No.
FAA–2022–0398.
The FAA concurs with the change to
the applicability because Model CL–
600–2B16 (604 Variants) airplanes are
not affected by the identified unsafe
condition. The FAA has revised the
applicability of this AD accordingly.
The FAA has also removed the AFM
references for these airplanes from this
final rule and revised the Costs of
Compliance paragraph in this final rule
to specify there are 123 affected U.S.
airplanes.
Conclusion
The FAA reviewed the relevant data
and determined that air safety requires
adopting this AD as proposed. Except
for minor editorial changes and the
changes described previously, this AD is
adopted as proposed in the NPRM.
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None of the changes will increase the
economic burden on any operator.
Accordingly, the FAA is issuing this AD
to address the unsafe condition on these
products.
Related Service Information Under 1
CFR Part 51
Bombardier has issued the following
service information. This service
information contains a new AFM
limitation and procedure for operation
during certain flight modes. These
documents are distinct since they apply
to different airplane configurations.
These configurations may include the
presence or absence of winglets,
incorporation of service bulletin 601–
0300 which introduces an airspeed
limitation placard, and the type of
engine installed on the airplane.
• Automatic Flight Control System,
Systems Limitations, Limitations,
Bombardier Canadair Challenger Model
CL–600–2A12, AFM, Product Support
Publication (PSP) No. 601–1B–1,
Revision 85, dated June 16, 2021.
• Engine Failure in Climb During
ALTSEL, Airplane Handling Procedures
Following Engine Failure, Abnormal
Procedures, Bombardier Canadair
Challenger Model CL–600–2A12, AFM,
PSP No. 601–1B–1, Revision 85, dated
June 16, 2021.
• Automatic Flight Control System,
Systems Limitations, Limitations,
Bombardier Canadair Challenger Model
CL–600–2B16, AFM, PSP No. 601A–1–
1, Revision 96, dated June 16, 2021.
• Engine Failure in Climb During
ASEL, Airplane Handling Procedures
Following Engine Failure, Abnormal
Procedures, Bombardier Canadair
Challenger Model CL–600–2B16, AFM,
PSP No. 601A–1–1, Revision 96, dated
June 16, 2021.
• Automatic Flight Control System,
Systems Limitations, Limitations,
Canadair Challenger Model CL–600–
1A11, AFM, Product Publication No.
600, Revision A115, dated June 16,
2021.
• Engine Failure in Climb During
ALTSEL, Airplane Handling Procedures
Following Engine Failure, Normal
Procedures, Canadair Challenger Model
CL–600–1A11, AFM, Product
Publication No. 600, Revision A115,
dated June 16, 2021.
• Automatic Flight Control System,
Systems Limitations, Limitations,
Canadair Challenger Model CL–600–
1A11, AFM, PSP No. 600–1, Revision
107, dated June 16, 2021.
• Engine Failure in Climb During
ALTSEL, Airplane Handling Procedures
Following Engine Failure, Abnormal
Procedures, Canadair Challenger Model
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Federal Register / Vol. 87, No. 177 / Wednesday, September 14, 2022 / Rules and Regulations
CL–600–1A11, AFM, PSP No. 600–1,
Revision 107, dated June 16, 2021.
• Automatic Flight Control System,
Systems Limitations, Limitations,
Canadair Challenger Model CL–600–
2A12, AFM, PSP No. 601–1A, Revision
129, dated June 16, 2021.
• Engine Failure in Climb During
ALTSEL, Airplane Handling Procedures
Following Engine Failure, Abnormal
Procedures, Canadair Challenger Model
CL–600–2A12, AFM, PSP No. 601–1A,
Revision 129, dated June 16, 2021.
• Automatic Flight Control System,
Systems Limitations, Limitations,
Canadair Challenger Model CL–600–
2A12, AFM, PSP No. 601–1A–1,
Revision 83, dated June 16, 2021.
• Engine Failure in Climb During
ALTSEL, Airplane Handling Procedures
Following Engine Failure, Abnormal
Procedures, Canadair Challenger Model
CL–600–2A12, AFM, PSP No. 601–1A–
1, Revision 83, dated June 16, 2021.
• Automatic Flight Control System
Systems Limitations, Limitations,
Canadair Challenger Model CL–600–
2A12, AFM, PSP No. 601–1B, Revision
87, dated June 16, 2021.
• Engine Failure in Climb During
ALTSEL, Airplane Handling Procedures
Following Engine Failure, Abnormal
Procedures, Canadair Challenger Model
CL–600–2A12, AFM, PSP No. 601–1B,
Revision 87, dated June 16, 2021.
• Automatic Flight Control System,
Systems Limitations, Limitations,
Canadair Challenger Model CL–600–
56261
2B16, AFM, PSP No. 601A–1, Revision
107, dated June 16, 2021.
• Engine Failure in Climb During
ASEL, Airplane Handling Procedures
Following Engine Failure, Abnormal
Procedures, Canadair Challenger Model
CL–600–2B16, AFM, PSP No. 601A–1,
Revision 107, dated June 16, 2021.
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 123 airplanes of U.S. registry.
The FAA estimates the following costs
to comply with this AD:
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
$10,455
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.
(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
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
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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:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
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§ 39.13
[Amended]
(c) Applicability
This AD applies to the Bombardier, Inc.,
airplanes, certificated in any category,
identified in paragraphs (c)(1) through (3) of
this AD.
(1) Model CL–600–1A11 (600), serial
numbers 1001 through 1085 inclusive.
(2) Model CL–600–2A12 (601), serial
numbers 3001 through 3066 inclusive.
(3) Model CL–600–2B16 (601–3A and 601–
3R Variants), serial numbers 5001 through
5194 inclusive.
(d) Subject
Air Transport Association (ATA) of
America Code 22, Auto flight.
(e) Reason
This AD was prompted by reports that
during certain operating modes, the flight
guidance/autopilot does not account for
engine failure while capturing an altitude.
The FAA is issuing this AD to address a
possible engine failure during or before a
climb while in ALTSEL, ASEL or ALTS CAP
mode, which could cause the airspeed to
drop significantly below the safe operating
speed. Prompt crew intervention may be
required to maintain a safe operating speed.
(f) Compliance
■
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
Comply with this AD within the
compliance times specified, unless already
done.
2022–12–13 Bombardier, Inc.: Amendment
39–22085; Docket No. FAA–2022–0398;
Project Identifier MCAI–2020–00881–T.
(g) Revision of the Existing Airplane Flight
Manual (AFM)
(a) Effective Date
This airworthiness directive (AD) is
effective October 19, 2022.
(b) Affected Airworthiness Directives (ADs)
None.
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Within 30 days after the effective date of
this AD: Revise the existing AFM to
incorporate the information specified in the
limitation and procedure specified in the
applicable AFM specified in figure 1 to
paragraph (g) of this AD.
BILLING CODE 4910–13–P
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Federal Register / Vol. 87, No. 177 / Wednesday, September 14, 2022 / Rules and Regulations
Airplane Serial
Numbers
Model CL-600lAl 1 (600
variant), serial
numbers 1001
through 1085 for
non-winglets
Model CL-600lAl 1 (600
variant), serial
numbers 1001
through 1085 for
winglets
Model CL-6002A12 (601
variant), serial
numbers 3001
through 3066
Model CL-6002A12 (601
variant), serial
numbers 3001
through 3066 with
Service Bulletin
(SB) 601-0360
incorporated
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Model CL-6002A12 (601
variant), serial
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New Limitation and
Procedure
Automatic Flight Control
System, Systems
Limitations, Limitations;
and Engine Failure in
Climb During AL TSEL,
Airplane Handling
Procedures Following
Engine Failure, Normal
Procedures
Automatic Flight Control
System, Systems
Limitations, Limitations;
and Engine Failure in
Climb During AL TSEL,
Airplane Handling
Procedures Following
Engine Failure, Abnormal
Procedures
Automatic Flight Control
System, Systems
Limitations, Limitations;
and Engine Failure in
Climb During AL TSEL,
Airplane Handling
Procedures Following
Engine Failure, Abnormal
Procedures
Automatic Flight Control
System, Systems
Limitations, Limitations;
and Engine Failure in
Climb During AL TSEL,
Airplane Handling
Procedures Following
Engine Failure, Abnormal
Procedures
Automatic Flight Control
System, Systems
Limitations, Limitations;
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AFM
Revision
Canadair
Challenger Model
CL-600-lAl 1,
AFM, Product
Publication No.
600
Revision Al 15,
dated June 16,
2021
Canadair
Challenger Model
CL-600-lAl 1,
AFM, Product
Support
Publication (PSP)
No. 600-1
Revision 107,
dated June 16,
2021
Canadair
Challenger Model
CL-600-2A12,
AFM,PSPNo.
601-lA
Revision 129,
dated June 16,
2021
Bombardier
Canadair
Challenger Model
CL-600-2A12,
AFM,PSPNo.
601-lA-1
Revision 83,
dated
June 16, 2021
Canadair
Challenger Model
CL-600-2A12,
Revision 87,
dated June 16,
2021
Sfmt 4725
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Figure 1 to paragraph (g) - AFM Revisions
Federal Register / Vol. 87, No. 177 / Wednesday, September 14, 2022 / Rules and Regulations
New Limitation and
Procedure
numbers 3001
through 3066 with
-3A engine
and Engine Failure in
Climb During AL TSEL,
Airplane Handling
Procedures Following
Engine Failure, Abnormal
Procedures
Automatic Flight
Control System,
Systems Limitations,
Limitations; and Engine
Failure in Climb During
AL TSEL, Airplane
Handling Procedures
Following Engine
Failure, Abnormal
Procedures
Automatic Flight
Control System,
Systems Limitations,
Limitations; and Engine
Failure in Climb During
ASEL, Airplane
Handling Procedures
Following Engine
Failure, Abnormal
Procedures
Automatic Flight
Control System,
Systems Limitations,
Limitations; and Engine
Failure in Climb During
ASEL, Airplane
Handling Procedures
Following Engine
Failure, Abnormal
Procedures
Model CL-6002A 12, serial
numbers 3001
through 3066 with
-3A engine and SB
601-0360
incorporated
Model CL-6002B16 (601-3A/3R
variant), serial
numbers 5001
through 5194
Model CL-6002B16 (601-3A/3R
variant), serial
numbers 5001
through 5194 with
SB 601-0360
incorporated
BILLING CODE 4910–13–C
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(h) Other FAA 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
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AFM
AFM,PSPNo.
601-lB
Bombardier
Canadair
Challenger
Model CL-6002A12, AFM,
PSPNo.
601-lB-1
Revision 85,
dated June 16,
2021
Canadair
Challenger
Model CL-6002B16,AFM,
PSP No. 601A-1
Revision 107,
dated
June 16, 2021
Bombardier
Canadair
Challenger
Model CL-6002B16,AFM,
PSPNo.
601A-1-1
Revision 96,
dated
June 16, 2021
appropriate. If sending information directly
to the manager of the certification office,
send it to ATTN: Program Manager,
Continuing Operational Safety, FAA, New
York ACO Branch, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone
516–228–7300. 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
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Revision
Sfmt 4700
from a manufacturer, the instructions must
be accomplished using a method approved
by the Manager, New York ACO Branch,
FAA; or Transport Canada Civil Aviation
(TCCA); or Bombardier, Inc.’s TCCA Design
Approval Organization (DAO). If approved by
the DAO, the approval must include the
DAO-authorized signature.
(i) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) TCCA AD
CF–2020–02R1, dated August 11, 2022, for
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ER14SE22.004</GPH>
Airplane Serial
Numbers
56263
56264
Federal Register / Vol. 87, No. 177 / Wednesday, September 14, 2022 / Rules and Regulations
khammond on DSKJM1Z7X2PROD with RULES
related information. This MCAI may be
found in the AD docket on the internet at
regulations.gov by searching for and locating
Docket No. FAA–2022–0398.
(2) For more information about this AD,
contact Steven Dzierzynski, Aerospace
Engineer, Avionics and Electrical Systems
Section, FAA, New York ACO Branch, 1600
Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 516–228–7367; email 9-avsnyaco-cos@faa.gov.
(j) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(i) Automatic Flight Control System,
Systems Limitations, Limitations,
Bombardier Canadair Challenger Model CL–
600–2A12, Airplane Flight Manual (AFM),
Product Support Publication (PSP) No. 601–
1B–1, Revision 85, dated June 16, 2021.
(ii) Engine Failure in Climb During
ALTSEL, Airplane Handling Procedures
Following Engine Failure, Abnormal
Procedures, Bombardier Canadair Challenger
Model CL–600–2A12, AFM, PSP No. 601–
1B–1, Revision 85, dated June 16, 2021.
(iii) Automatic Flight Control System,
Systems Limitations, Limitations,
Bombardier Canadair Challenger Model CL–
600–2B16, AFM, PSP No. 601A–1–1,
Revision 96, dated June 16, 2021.
(iv) Engine Failure in Climb During ASEL,
Airplane Handling Procedures Following
Engine Failure, Abnormal Procedures,
Bombardier Canadair Challenger Model CL–
600–2B16, AFM, PSP No. 601A–1–1,
Revision 96, dated June16, 2021.
(v) Automatic Flight Control System,
Systems Limitations, Limitations, Canadair
Challenger Model CL–600–1A11, AFM,
Product Publication No. 600, Revision A115,
dated June 16, 2021.
(vi) Engine Failure in Climb During
ALTSEL, Airplane Handling Procedures
Following Engine Failure, Normal
Procedures, Canadair Challenger Model CL–
600–1A11, AFM, Product Publication No.
600, Revision A115, dated June 16, 2021.
(vii) Automatic Flight Control System,
Systems Limitations, Limitations, Canadair
Challenger Model CL–600–1A11, AFM, PSP
No. 600–1, Revision 107, dated June 16,
2021.
(viii) Engine Failure in Climb During
ALTSEL, Airplane Handling Procedures
Following Engine Failure, Abnormal
Procedures, Canadair Challenger Model CL–
600–1A11, AFM, PSP No. 600–1, Revision
107, dated June 16, 2021.
(ix) Automatic Flight Control System,
Systems Limitations, Limitations, Canadair
Challenger Model CL–600–2A12, AFM, PSP
No. 601–1A, Revision 129, dated June 16,
2021.
Note 1 to paragraph (ix): The page date for
page i of the Limitations Contents specified
in the List of Effective Pages of the Canadair
Challenger Model CL–600–2A12, AFM, PSP
No. 601–1A, Revision 129, dated June 16,
VerDate Sep<11>2014
16:35 Sep 13, 2022
Jkt 256001
2021, is incorrect; the correct page date is
April 16, 2020.
(x) Engine Failure in Climb During
ALTSEL, Airplane Handling Procedures
Following Engine Failure, Abnormal
Procedures, Canadair Challenger Model CL–
600–2A12, AFM, PSP No. 601–1A, Revision
129, dated June 16, 2021.
(xi) Automatic Flight Control System,
Systems Limitations, Limitations, Canadair
Challenger Model CL–600–2A12, AFM, PSP
No. 601–1A–1, Revision 83, dated June 16,
2021.
Note 2 to paragraph (xi): The page date for
page i of the Limitations Contents specified
in the List of Effective Pages of the Canadair
Challenger Model CL–600–2A12, AFM, PSP
No. 601–1A–1, Revision 83, dated June 16,
2021, is incorrect; the correct page date is
April 16, 2020.
(xii) Engine Failure in Climb During
ALTSEL, Airplane Handling Procedures
Following Engine Failure, Abnormal
Procedures, Canadair Challenger Model CL–
600–2A12, AFM, PSP No. 601–1A–1,
Revision 83, dated June 16, 2021.
(xiii) Automatic Flight Control System,
Systems Limitations, Limitations, Canadair
Challenger Model CL–600–2A12, AFM, PSP
No. 601–1B, Revision 87, dated June 16,
2021.
Note 3 to paragraph (xiii): Page iii of the
Limitations Contents specified in the List of
Effective Pages of the Canadair Challenger
Model CL–600–2A12, AFM, PSP No. 601–1B,
Revision 87, dated June 16, 2021, does not
exist.
(xiv) Engine Failure in Climb During
ALTSEL, Airplane Handling Procedures
Following Engine Failure, Abnormal
Procedures, Canadair Challenger Model CL–
600–2A12, AFM, PSP No. 601–1B, Revision
87, dated June 16, 2021.
(xv) Automatic Flight Control System,
Systems Limitations, Limitations, Canadair
Challenger Model CL–600–2B16, AFM, PSP
No. 601A–1, Revision 107, dated June 16,
2021.
(xvi) Engine Failure in Climb During ASEL,
Airplane Handling Procedures Following
Engine Failure, Abnormal Procedures,
Canadair Challenger Model CL–600–2B16,
AFM, PSP No. 601A–1, Revision 107, dated
June 16, 2021.
(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; internet
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:
archives.gov/federal-register/cfr/ibrlocations.html.
PO 00000
Frm 00018
Fmt 4700
Sfmt 4700
Issued on August 16, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022–19778 Filed 9–13–22; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 97
[Docket No. 31445; Amdt. No. 4023]
Standard Instrument Approach
Procedures, and Takeoff Minimums
and Obstacle Departure Procedures;
Miscellaneous Amendments
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
This rule establishes, amends,
suspends, or removes Standard
Instrument Approach Procedures
(SIAPS) and associated Takeoff
Minimums and Obstacle Departure
procedures (ODPs) for operations at
certain airports. These regulatory
actions are needed because of the
adoption of new or revised criteria, or
because of changes occurring in the
National Airspace System, such as the
commissioning of new navigational
facilities, adding new obstacles, or
changing air traffic requirements. These
changes are designed to provide safe
and efficient use of the navigable
airspace and to promote safe flight
operations under instrument flight rules
at the affected airports.
DATES: This rule is effective September
14, 2022. The compliance date for each
SIAP, associated Takeoff Minimums,
and ODP is specified in the amendatory
provisions.
The incorporation by reference of
certain publications listed in the
regulations is approved by the Director
of the Federal Register as of September
14, 2022.
ADDRESSES: Availability of matters
incorporated by reference in the
amendment is as follows:
SUMMARY:
For Examination
1. U.S. Department of Transportation,
Docket Ops–M30. 1200 New Jersey
Avenue SE, West Bldg., Ground Floor,
Washington, DC 20590–0001.
2. The FAA Air Traffic Organization
Service Area in which the affected
airport is located;
3. The office of Aeronautical
Information Services, 6500 South
MacArthur Blvd., Oklahoma City, OK
73169 or,
E:\FR\FM\14SER1.SGM
14SER1
]]>Agencies
[Federal Register Volume 87, Number 177 (Wednesday, September 14, 2022)]
[Rules and Regulations]
[Pages 56259-56264]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-19778]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0398; Project Identifier MCAI-2020-00881-T;
Amendment 39-22085; AD 2022-12-13]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc., Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Bombardier, Inc., Model CL-600-1A11 (600), CL-600-2A12 (601),
and CL-600-2B16 (601-3A and 601-3R Variants) airplanes. This AD was
prompted by reports that during certain operating modes, the flight
guidance/autopilot does not account for engine failure while capturing
an altitude. This AD requires revising the existing airplane flight
manual (AFM) to provide the flightcrew with a new limitation and
procedure for operation during certain
[[Page 56260]]
flight modes. The FAA is issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective October 19, 2022.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of October 19,
2022.
ADDRESSES: 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; internet
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 on the
internet at regulations.gov by searching for and locating Docket No.
FAA-2022-0398.
Examining the AD Docket
You may examine the AD docket on the internet at regulations.gov by
searching for and locating Docket No. FAA-2022-0398; 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.
FOR FURTHER INFORMATION CONTACT: Steven Dzierzynski, Aerospace
Engineer, Avionics and Electrical Systems Section, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone
516-228-7367; email [email protected].
SUPPLEMENTARY INFORMATION:
Background
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued TCCA AD CF-2020-02, dated February 13,
2020 (TCCA AD CF-2020-02), to correct an unsafe condition for certain
Bombardier, Inc., Model CL-600-1A11 (600), CL-600-2A12 (601), and CL-
600-2B16 (601-3A, 601-3R, and 604 Variants) airplanes.
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 CL-600-1A11 (600), CL-600-2A12 (601), and CL-600-2B16 (601-
3A, 601-3R, and 604 Variants) airplanes. The NPRM published in the
Federal Register on April 11, 2022 (87 FR 21037). The NPRM was prompted
by reports that during certain operating modes, the flight guidance/
autopilot does not account for engine failure while capturing an
altitude. The NPRM proposed to require revising the existing AFM to
provide the flightcrew with a new limitation and procedure for
operation during certain flight modes. The FAA is issuing this AD to
address a possible engine failure during or before a climb while in
ALTSEL, ASEL or ALTS CAP mode, which could cause the airspeed to drop
significantly below the safe operating speed. Prompt crew intervention
may be required to maintain a safe operating speed.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the cost to the public.
Change to the Applicability
Since the FAA issued the NPRM, TCCA revised AD CF-2020-02 and
issued TCCA AD CF-2020-02R1, dated August 11, 2022 (TCCA AD CF-2020-
02R1) (also referred to as the MCAI). TCCA stated the applicability was
revised to remove Model CL-600-2B16 (604 Variants) as it was determined
that these airplanes do not utilize ALTSEL, ASEL and ALTS CAP modes in
their configurations. TCCA also stated that the AFM references for
these airplanes were removed from the TCCA AD. You may examine the MCAI
in the AD docket on the internet at regulations.gov by searching for
and locating Docket No. FAA-2022-0398.
The FAA concurs with the change to the applicability because Model
CL-600-2B16 (604 Variants) airplanes are not affected by the identified
unsafe condition. The FAA has revised the applicability of this AD
accordingly. The FAA has also removed the AFM references for these
airplanes from this final rule and revised the Costs of Compliance
paragraph in this final rule to specify there are 123 affected U.S.
airplanes.
Conclusion
The FAA reviewed the relevant data and determined that air safety
requires adopting this AD as proposed. Except for minor editorial
changes and the changes described previously, this AD is adopted as
proposed in the NPRM. None of the changes will increase the economic
burden on any operator. Accordingly, the FAA is issuing this AD to
address the unsafe condition on these products.
Related Service Information Under 1 CFR Part 51
Bombardier has issued the following service information. This
service information contains a new AFM limitation and procedure for
operation during certain flight modes. These documents are distinct
since they apply to different airplane configurations. These
configurations may include the presence or absence of winglets,
incorporation of service bulletin 601-0300 which introduces an airspeed
limitation placard, and the type of engine installed on the airplane.
Automatic Flight Control System, Systems Limitations,
Limitations, Bombardier Canadair Challenger Model CL-600-2A12, AFM,
Product Support Publication (PSP) No. 601-1B-1, Revision 85, dated June
16, 2021.
Engine Failure in Climb During ALTSEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Bombardier
Canadair Challenger Model CL-600-2A12, AFM, PSP No. 601-1B-1, Revision
85, dated June 16, 2021.
Automatic Flight Control System, Systems Limitations,
Limitations, Bombardier Canadair Challenger Model CL-600-2B16, AFM, PSP
No. 601A-1-1, Revision 96, dated June 16, 2021.
Engine Failure in Climb During ASEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Bombardier
Canadair Challenger Model CL-600-2B16, AFM, PSP No. 601A-1-1, Revision
96, dated June 16, 2021.
Automatic Flight Control System, Systems Limitations,
Limitations, Canadair Challenger Model CL-600-1A11, AFM, Product
Publication No. 600, Revision A115, dated June 16, 2021.
Engine Failure in Climb During ALTSEL, Airplane Handling
Procedures Following Engine Failure, Normal Procedures, Canadair
Challenger Model CL-600-1A11, AFM, Product Publication No. 600,
Revision A115, dated June 16, 2021.
Automatic Flight Control System, Systems Limitations,
Limitations, Canadair Challenger Model CL-600-1A11, AFM, PSP No. 600-1,
Revision 107, dated June 16, 2021.
Engine Failure in Climb During ALTSEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Canadair
Challenger Model
[[Page 56261]]
CL-600-1A11, AFM, PSP No. 600-1, Revision 107, dated June 16, 2021.
Automatic Flight Control System, Systems Limitations,
Limitations, Canadair Challenger Model CL-600-2A12, AFM, PSP No. 601-
1A, Revision 129, dated June 16, 2021.
Engine Failure in Climb During ALTSEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Canadair
Challenger Model CL-600-2A12, AFM, PSP No. 601-1A, Revision 129, dated
June 16, 2021.
Automatic Flight Control System, Systems Limitations,
Limitations, Canadair Challenger Model CL-600-2A12, AFM, PSP No. 601-
1A-1, Revision 83, dated June 16, 2021.
Engine Failure in Climb During ALTSEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Canadair
Challenger Model CL-600-2A12, AFM, PSP No. 601-1A-1, Revision 83, dated
June 16, 2021.
Automatic Flight Control System Systems Limitations,
Limitations, Canadair Challenger Model CL-600-2A12, AFM, PSP No. 601-
1B, Revision 87, dated June 16, 2021.
Engine Failure in Climb During ALTSEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Canadair
Challenger Model CL-600-2A12, AFM, PSP No. 601-1B, Revision 87, dated
June 16, 2021.
Automatic Flight Control System, Systems Limitations,
Limitations, Canadair Challenger Model CL-600-2B16, AFM, PSP No. 601A-
1, Revision 107, dated June 16, 2021.
Engine Failure in Climb During ASEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Canadair
Challenger Model CL-600-2B16, AFM, PSP No. 601A-1, Revision 107, dated
June 16, 2021.
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 123 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 $10,455
----------------------------------------------------------------------------------------------------------------
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2022-12-13 Bombardier, Inc.: Amendment 39-22085; Docket No. FAA-
2022-0398; Project Identifier MCAI-2020-00881-T.
(a) Effective Date
This airworthiness directive (AD) is effective October 19, 2022.
(b) Affected Airworthiness Directives (ADs)
None.
(c) Applicability
This AD applies to the Bombardier, Inc., airplanes, certificated
in any category, identified in paragraphs (c)(1) through (3) of this
AD.
(1) Model CL-600-1A11 (600), serial numbers 1001 through 1085
inclusive.
(2) Model CL-600-2A12 (601), serial numbers 3001 through 3066
inclusive.
(3) Model CL-600-2B16 (601-3A and 601-3R Variants), serial
numbers 5001 through 5194 inclusive.
(d) Subject
Air Transport Association (ATA) of America Code 22, Auto flight.
(e) Reason
This AD was prompted by reports that during certain operating
modes, the flight guidance/autopilot does not account for engine
failure while capturing an altitude. The FAA is issuing this AD to
address a possible engine failure during or before a climb while in
ALTSEL, ASEL or ALTS CAP mode, which could cause the airspeed to
drop significantly below the safe operating speed. Prompt crew
intervention may be required to maintain a safe operating speed.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Revision of the Existing Airplane Flight Manual (AFM)
Within 30 days after the effective date of this AD: Revise the
existing AFM to incorporate the information specified in the
limitation and procedure specified in the applicable AFM specified
in figure 1 to paragraph (g) of this AD.
BILLING CODE 4910-13-P
[[Page 56262]]
[GRAPHIC] [TIFF OMITTED] TR14SE22.003
[[Page 56263]]
[GRAPHIC] [TIFF OMITTED] TR14SE22.004
BILLING CODE 4910-13-C
(h) Other FAA 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 certification
office, send it to ATTN: Program Manager, Continuing Operational
Safety, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300. 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 Civil Aviation (TCCA); or
Bombardier, Inc.'s TCCA Design Approval Organization (DAO). If
approved by the DAO, the approval must include the DAO-authorized
signature.
(i) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) TCCA AD CF-2020-02R1, dated August 11, 2022, for
[[Page 56264]]
related information. This MCAI may be found in the AD docket on the
internet at regulations.gov by searching for and locating Docket No.
FAA-2022-0398.
(2) For more information about this AD, contact Steven
Dzierzynski, Aerospace Engineer, Avionics and Electrical Systems
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7367; email [email protected].
(j) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) Automatic Flight Control System, Systems Limitations,
Limitations, Bombardier Canadair Challenger Model CL-600-2A12,
Airplane Flight Manual (AFM), Product Support Publication (PSP) No.
601-1B-1, Revision 85, dated June 16, 2021.
(ii) Engine Failure in Climb During ALTSEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Bombardier
Canadair Challenger Model CL-600-2A12, AFM, PSP No. 601-1B-1,
Revision 85, dated June 16, 2021.
(iii) Automatic Flight Control System, Systems Limitations,
Limitations, Bombardier Canadair Challenger Model CL-600-2B16, AFM,
PSP No. 601A-1-1, Revision 96, dated June 16, 2021.
(iv) Engine Failure in Climb During ASEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Bombardier
Canadair Challenger Model CL-600-2B16, AFM, PSP No. 601A-1-1,
Revision 96, dated June16, 2021.
(v) Automatic Flight Control System, Systems Limitations,
Limitations, Canadair Challenger Model CL-600-1A11, AFM, Product
Publication No. 600, Revision A115, dated June 16, 2021.
(vi) Engine Failure in Climb During ALTSEL, Airplane Handling
Procedures Following Engine Failure, Normal Procedures, Canadair
Challenger Model CL-600-1A11, AFM, Product Publication No. 600,
Revision A115, dated June 16, 2021.
(vii) Automatic Flight Control System, Systems Limitations,
Limitations, Canadair Challenger Model CL-600-1A11, AFM, PSP No.
600-1, Revision 107, dated June 16, 2021.
(viii) Engine Failure in Climb During ALTSEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Canadair
Challenger Model CL-600-1A11, AFM, PSP No. 600-1, Revision 107,
dated June 16, 2021.
(ix) Automatic Flight Control System, Systems Limitations,
Limitations, Canadair Challenger Model CL-600-2A12, AFM, PSP No.
601-1A, Revision 129, dated June 16, 2021.
Note 1 to paragraph (ix): The page date for page i of the
Limitations Contents specified in the List of Effective Pages of the
Canadair Challenger Model CL-600-2A12, AFM, PSP No. 601-1A, Revision
129, dated June 16, 2021, is incorrect; the correct page date is
April 16, 2020.
(x) Engine Failure in Climb During ALTSEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Canadair
Challenger Model CL-600-2A12, AFM, PSP No. 601-1A, Revision 129,
dated June 16, 2021.
(xi) Automatic Flight Control System, Systems Limitations,
Limitations, Canadair Challenger Model CL-600-2A12, AFM, PSP No.
601-1A-1, Revision 83, dated June 16, 2021.
Note 2 to paragraph (xi): The page date for page i of the
Limitations Contents specified in the List of Effective Pages of the
Canadair Challenger Model CL-600-2A12, AFM, PSP No. 601-1A-1,
Revision 83, dated June 16, 2021, is incorrect; the correct page
date is April 16, 2020.
(xii) Engine Failure in Climb During ALTSEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Canadair
Challenger Model CL-600-2A12, AFM, PSP No. 601-1A-1, Revision 83,
dated June 16, 2021.
(xiii) Automatic Flight Control System, Systems Limitations,
Limitations, Canadair Challenger Model CL-600-2A12, AFM, PSP No.
601-1B, Revision 87, dated June 16, 2021.
Note 3 to paragraph (xiii): Page iii of the Limitations Contents
specified in the List of Effective Pages of the Canadair Challenger
Model CL-600-2A12, AFM, PSP No. 601-1B, Revision 87, dated June 16,
2021, does not exist.
(xiv) Engine Failure in Climb During ALTSEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Canadair
Challenger Model CL-600-2A12, AFM, PSP No. 601-1B, Revision 87,
dated June 16, 2021.
(xv) Automatic Flight Control System, Systems Limitations,
Limitations, Canadair Challenger Model CL-600-2B16, AFM, PSP No.
601A-1, Revision 107, dated June 16, 2021.
(xvi) Engine Failure in Climb During ASEL, Airplane Handling
Procedures Following Engine Failure, Abnormal Procedures, Canadair
Challenger Model CL-600-2B16, AFM, PSP No. 601A-1, Revision 107,
dated June 16, 2021.
(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; internet
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: archives.gov/federal-register/cfr/ibr-locations.html.
Issued on August 16, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-19778 Filed 9-13-22; 8:45 am]
BILLING CODE 4910-13-P
