[Federal Register Volume 90, Number 112 (Thursday, June 12, 2025)]
[Rules and Regulations]
[Pages 24737-24740]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2025-10683]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2025-0477; Project Identifier MCAI-2024-00422-T;
Amendment 39-23059; AD 2025-12-01]
RIN 2120-AA64
Airworthiness Directives; Bombardier Inc. Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Bombardier Inc. Model BD-700-1A10 and BD-700-1A11 airplanes.
This AD was prompted by a report that incorrect information was found
in certain calculation tables in a section of the airplane flight
manual (AFM) that addresses certain slat-flap conditions. This AD
requires revising the Non-Normal Procedures section of the existing AFM
to provide the flightcrew with corrected procedures to use in certain
slat-flap conditions. The FAA is issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective July 17, 2025.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of July 17,
2025.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2025-0477; 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 Bombardier material 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">ac.yul@aero.bombardier.com; website bombardier.com.
You may view this material 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-2025-0477.
FOR FURTHER INFORMATION CONTACT: Gabriel Kim, Aviation Safety Engineer,
FAA, 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 serial-numbered
Bombardier Inc. Model BD-700-1A10 and BD-700-1A11 airplanes. The NPRM
was published in the Federal Register on March 26, 2025 (90 FR 13709).
The NPRM was prompted by AD CF-2024-27, dated July 24, 2024, issued by
Transport Canada, which is the aviation authority for Canada (also
referred to as ``the MCAI''). The MCAI states that incorrect approach
speed adders and landing distance factors were discovered in the AFM
tables for the SLAT-FLAP FAIL (Caution) Crew Alerting System (CAS)
message and the jammed or inoperative slat/flap control lever (SFCL)
non-normal procedures. The incorrect speed adders and landing distance
factors present a potentially unsafe condition due to the shortfall
between the actual performance and the approved performance.
In the NPRM, the FAA proposed to require revising the Non-Normal
Procedures section of the existing AFM to provide the flightcrew with
corrected procedures to use in certain slat-flap conditions. The FAA is
issuing this AD to address incorrect speed adders and landing distance
factors in AFM tables. The unsafe condition, if not addressed, could
lead to increased workload for the flightcrew, possible stick shaker
activation (stall warning) due to a need to increase speed beyond the
published AFM speed adder, and increased landing distance beyond
published non-normal landing distance factors.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2025-0477.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the cost to the public.
Conclusion
These products have been approved by the civil aviation authority
of another country and are approved for operation in the United States.
Pursuant to the FAA's bilateral agreement with this State of Design
Authority, that authority has notified the FAA of the unsafe condition
described in the MCAI referenced above. The FAA reviewed the relevant
data, considered any comments received, and determined that air safety
requires adopting this AD as proposed. Accordingly, the FAA is issuing
this AD to address the unsafe condition on 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.
Material Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed the following Bombardier material. This material
describes procedures to address certain slat-flap conditions (i.e.,
Slat-flap fail (Caution) CAS message, or a jammed or inoperative SFCL).
These documents are distinct since they apply to different
configurations and different airplane models.
Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures (which includes the Jammed or Inoperative Slat/Flap Control
Lever Procedure and Slat-Flap Fail (Caution) procedure), Bombardier
Global Express AFM, Publication No. CSP 700-1, Revision 119, dated May
22, 2024. (For obtaining the procedures for Bombardier Global Express
AFM, Publication No. CSP 700-1, use Document Identification No. GL 700
AFM-1.)
Chapter 7--Supplement 20--Operations at Airport Elevations
Above 10,000 Feet (which includes Jammed or Inoperative Slat/Flap
Control Lever procedure and Slat-Flap Fail procedures); Bombardier
Global Express AFM, Publication No. CSP 700-1, Revision 119, dated May
22, 2024. (For obtaining the procedures for Bombardier Global Express
AFM, Publication No. CSP 700-1, use Document Identification No. GL 700
AFM-1.)
Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures (which includes the Jammed or Inoperative Slat/Flap Control
Lever Procedure and Slat-Flap Fail (Caution)
[[Page 24738]]
procedure), Bombardier Global Express AFM, Publication No. CSP 700-1A,
Revision 119, dated May 22, 2024. (For obtaining the procedures for
Bombardier Global Express AFM, Publication No. CSP 700-1A, use Document
Identification No. GL 700 AFM-1A.)
Chapter 7--Supplement 20--Operations at Airport Elevations
Above 10,000 Feet (which includes Jammed or Inoperative Slat/Flap
Control Lever procedure and Slat-Flap Fail procedures), Bombardier
Global Express AFM, Publication No. CSP 700-1A, Revision 119, dated May
22, 2024. (For obtaining the procedures for Bombardier Global Express
AFM, Publication No. CSP 700-1A, use Document Identification No. GL 700
AFM-1A.)
Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures (which includes the Jammed or Inoperative Slat/Flap Control
Lever Procedure and Slat-Flap Fail (Caution) procedure), Bombardier
Global 6000 AFM, Publication No. CSP 700-1V, Revision 49, dated May 22,
2024. (For obtaining the procedures for Bombardier Global 6000 AFM,
Publication No. CSP 700-1V, use Document Identification No. GL 6000
AFM.)
Chapter 7--Supplement 20--Operations at Airport Elevations
Above 10,000 Feet (which includes Jammed or Inoperative Slat/Flap
Control Lever procedure and Slat-Flap Fail procedures), Bombardier
Global 6000 AFM, Publication No. CSP 700-1V, Revision 49, dated May 22,
2024. (For obtaining the procedures for Bombardier Global 6000 AFM,
Publication No. CSP 700-1V, use Document Identification No. GL 6000
AFM.)
Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures (which includes the Jammed or Inoperative Slat/Flap Control
Lever Procedure and Slat-Flap Fail (Caution) procedure) Bombardier
Global 5000 AFM, Publication No. CSP 700-5000-1 AFM, Revision 80, dated
May 22, 2024. (For obtaining the procedures for Bombardier Global 5000
AFM, Publication No. CSP 700-5000-1, use Document Identification No. GL
5000 AFM.)
Chapter 7--Supplement 20--Operations at Airport Elevations
Above 10,000 Feet (which includes Jammed or Inoperative Slat/Flap
Control Lever procedure and Slat-Flap Fail procedures), Bombardier
Global 5000 AFM, Publication No. CSP 700-5000-1 AFM, Revision 80, dated
May 22, 2024. (For obtaining the procedures for Bombardier Global 5000
AFM, Publication No. CSP 700-5000-1, use Document Identification No. GL
5000 AFM.)
Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures (which includes the Jammed or Inoperative Slat/Flap Control
Lever Procedure and Slat-Flap Fail (Caution) procedure), Bombardier
Global 5000 Featuring Global Vision Flight Deck AFM, Publication No.
CSP 700-5000-1V, Revision 49, dated May 22, 2024. (For obtaining the
procedures for Bombardier Global 5000 Featuring Global Vision Flight
Deck AFM, Publication No. CSP 700-5000-1V, use Document Identification
No. GL 5000 GVFD AFM.)
Chapter 7--Supplement 20--Operations at Airport Elevations
Above 10,000 Feet (which includes Jammed or Inoperative Slat/Flap
Control Lever procedure and Slat-Flap Fail procedures), Bombardier
Global 5000 Featuring Global Vision Flight Deck AFM, Publication No.
CSP 700-5000-1V, Revision 49, dated May 22, 2024. (For obtaining the
procedures for Bombardier Global 5000 Featuring Global Vision Flight
Deck AFM, Publication No. CSP 700-5000-1V, use Document Identification
No. GL 5000 GVFD AFM.)
Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures (which includes the Jammed or Inoperative Slat/Flap Control
Lever Procedure and Slat-Flap Fail (Caution) procedure), Bombardier
Global 5500 AFM, Publication No. CSP 700-5500-1, Revision 21, dated May
22, 2024. (For obtaining the procedures for Bombardier Global 5500 AFM,
Publication No. CSP 700-5500-1, use Document Identification No. GL 5500
AFM.)
Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures (which includes the Jammed or Inoperative Slat/Flap Control
Lever Procedure and Slat-Flap Fail (Caution) procedure), Bombardier
Global 6500 AFM, Publication No. CSP 700-6500-1, Revision 21, dated May
22, 2024. (For obtaining the procedures for Bombardier Global 6500 AFM,
Publication No. CSP 700-6500-1, use Document Identification No. GL 6500
AFM.)
This material 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 476 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 x $85 per hour = $85........ None...................... $85 $40,460
----------------------------------------------------------------------------------------------------------------
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.
[[Page 24739]]
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:
2025-12-01 Bombardier Inc.: Amendment 39-23059; Docket No. FAA-2025-
0477; Project Identifier MCAI-2024-00422-T.
(a) Effective Date
This airworthiness directive (AD) is effective July 17, 2025.
(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
9002 through 60086 inclusive, 60088 through 60091 inclusive, 60098,
60100, 60105, 60107, and 60111.
(d) Subject
Air Transport Association (ATA) of America Code 27, Flight
Controls.
(e) Unsafe Condition
This AD was prompted by a report that incorrect information was
found in certain calculation tables in a section of the airplane
flight manual (AFM) that addresses certain slat-flap conditions. The
FAA is issuing this AD to address incorrect speed adders and landing
distance factors in AFM tables. The unsafe condition, if not
addressed, could lead to increased workload for the flightcrew,
possible stick shaker activation (stall warning) due to a need to
increase speed beyond the published AFM speed adder, and increased
landing distance beyond published non-normal landing distance
factors.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Revision of Existing AFM
Within 30 days after the effective date of this AD, revise the
existing AFM to incorporate the information in the applicable
sections of the applicable AFMs identified in table 1 to paragraph
(g) of this AD.
Table 1 to Paragraph (g)--AFM References
----------------------------------------------------------------------------------------------------------------
Bombardier airplane model AFM supplement, if AFM revision and
(marketing designation) AFM AFM section applicable issue date
----------------------------------------------------------------------------------------------------------------
BD-700-1A10 (Global Express).... Bombardier Global Jammed or Jammed or Revision 119,
Express AFM, Inoperative Slat/ Inoperative Slat/ dated May 22,
Publication No. Flap Control Flap Control 2024.
CSP 700-1 \1\. Lever Procedure Lever procedure
and Slat-Flap and Slat-Flap
Fail (Caution) Fail procedure,
procedure, Slat Landing Distance
and Flap Control Factors
Systems subsection of Non-
subsection, Normal Procedures
Section 05-10 section of
Flight Controls, Chapter 7--
of Chapter 5--Non- Supplement 20--
Normal Procedures. Operations at
Airport
Elevations Above
10,000 Feet.
BD-700-1A10 (Global Express XRS) Bombardier Global Jammed or Jammed or Revision 119,
Express AFM, Inoperative Slat/ Inoperative Slat/ dated May 22,
Publication No. Flap Control Flap Control 2024.
CSP 700-1A \2\. Lever Procedure Lever procedure
and Slat-Flap and Slat-Flap
Fail (Caution) Fail procedure,
procedure, Slat Landing Distance
and Flap Control Factors
Systems subsection of Non-
subsection, Normal Procedures
Section 05-10 section of
Flight Controls, Chapter 7--
of Chapter 5--Non- Supplement 20--
Normal Procedures. Operations at
Airport
Elevations Above
10,000 Feet.
BD-700-1A10 (Global 6000)....... Bombardier Global Jammed or Jammed or Revision 49, dated
6000 AFM, Inoperative Slat/ Inoperative Slat/ May 22, 2024.
Publication No. Flap Control Flap Control
CSP 700-1V \3\. Lever Procedure Lever procedure
and Slat-Flap and Slat-Flap
Fail (Caution) Fail procedure,
procedure, Slat Landing Distance
and Flap Control Factors
Systems subsection of Non-
subsection, Normal Procedures
Section 05-10 section of
Flight Controls, Chapter 7--
of Chapter 5--Non- Supplement 20--
Normal Procedures. Operations at
Airport
Elevations Above
10,000 Feet.
BD-700-1A10 (Global 6500)....... Bombardier Global Jammed or None.............. Revision 21, dated
6500 AFM, Inoperative Slat/ May 22, 2024.
Publication No. Flap Control
CSP-700-6500-1 Lever Procedure
\4\. and Slat-Flap
Fail (Caution)
procedure, Slat
and Flap Control
Systems
subsection,
Section 05-10
Flight Controls,
of Chapter 5--Non-
Normal Procedures.
BD-700-1A11 (Global 5000)....... Bombardier Global Jammed or Jammed or Revision 80, dated
5000 AFM, Inoperative Slat/ Inoperative Slat/ May 22, 2024.
Publication No. Flap Control Flap Control
CSP 700-5000-1 Lever Procedure Lever procedure
\5\. and Slat-Flap and Slat-Flap
Fail (Caution) Fail procedure,
procedure, Slat Landing Distance
and Flap Control Factors
Systems subsection of Non-
subsection, Normal Procedures
Section 05-10 section of
Flight Controls, Chapter 7--
of Chapter 5--Non- Supplement 20--
Normal Procedures. Operations at
Airport
Elevations Above
10,000 Feet.
BD-700-1A11 (Global 5000 Bombardier Global Jammed or Jammed or Revision 49, dated
Featuring Global Vision Flight 5000 Featuring Inoperative Slat/ Inoperative Slat/ May 22, 2024.
Deck). Global Vision Flap Control Flap Control
Flight Deck AFM, Lever Procedure Lever procedure
Publication No. and Slat-Flap and Slat-Flap
CSP 700-5000-1V Fail (Caution) Fail procedure,
\6\. procedure, Slat Landing Distance
and Flap Control Factors
Systems subsection of Non-
subsection, Normal Procedures
Section 05-10 section of
Flight Controls, Chapter 7--
of Chapter 5--Non- Supplement 20--
Normal Procedures. Operations at
Airport
Elevations Above
10,000 Feet.
BD-700-1A11 (Global 5500)....... Bombardier Global Jammed or None.............. Revision 21, dated
5500 AFM, Inoperative Slat/ May 22, 2024.
Publication No. Flap Control
CSP 700-5500-1 Lever Procedure
\7\. and Slat-Flap
Fail (Caution)
procedure, Slat
and Flap Control
Systems
subsection,
Section 05-10
Flight Controls,
of Chapter 5--Non-
Normal Procedures.
----------------------------------------------------------------------------------------------------------------
\1\ For obtaining the procedures for Bombardier Global Express AFM, Publication No. CSP 700-1, use Document
Identification No. GL 700 AFM-1.
\2\ For obtaining the procedures for Bombardier Global Express AFM, Publication No. CSP 700-1A, use Document
Identification No. GL 700 AFM-1A.
\3\ For obtaining the procedures for Bombardier Global 6000 AFM, Publication No. CSP 700-1V, use Document
Identification No. GL 6000 AFM.
\4\ For obtaining the procedures for Bombardier Global 6500 AFM, Publication No. CSP 700-6500-1, use Document
Identification No. GL 6500 AFM.
[[Page 24740]]
\5\ For obtaining the procedures for Bombardier Global 5000 AFM, Publication No. CSP 700-5000-1, use Document
Identification No. GL 5000 AFM.
\6\ For obtaining the procedures for Bombardier Global 5000 Featuring Global Vision Flight Deck AFM, Publication
No. CSP 700-5000-1V, use Document Identification No. GL 5000 GVFD AFM.
\7\ For obtaining the procedures for Bombardier Global 5500 AFM, Publication No. CSP 700-5500-1, use Document
Identification No. GL 5500 AFM.
(h) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Validation Branch, FAA, has the authority to approve
AMOCs for this AD, if requested using the procedures found in 14 CFR
39.19. In accordance with 14 CFR 39.19, send your request to your
principal inspector or responsible Flight Standards Office, as
appropriate. If sending information directly to the manager of the
International Validation Branch, send it to the attention of the
person identified in paragraph (i) of this AD and email to:
[email protected]. 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, International
Validation Branch, FAA; or Transport Canada; or Bombardier's
Transport Canada Design Approval Organization (DAO). If approved by
the DAO, the approval must include the DAO-authorized signature.
(i) Additional Information
For more information about this AD, contact Gabriel Kim,
Aviation Safety Engineer, FAA, 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 material listed in this paragraph
under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this material as applicable to do the actions
required by this AD, unless this AD specifies otherwise.
(i) Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures, Bombardier Global Express Airplane Flight Manual (AFM),
Publication No. CSP 700-1, Revision 119, dated May 22, 2024.
Note 1 to paragraph (j)(2)(i): For obtaining the procedure
specified in paragraph (j)(2)(i) and (viii) of this AD for
Bombardier Global Express AFM, Publication No. CSP 700-1, use
Document Identification No. GL 700 AFM-1.
(ii) Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures Bombardier Global Express AFM, Publication No. CSP 700-
1A, Revision 119, dated May 22, 2024.
Note 2 to paragraph (j)(2)(ii): For obtaining the procedures
specified in paragraph (j)(2)(ii) and (ix) of this AD for Bombardier
Global Express AFM, Publication No. CSP 700-1A, use Document
Identification No. GL 700 AFM-1A.
(iii) Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures, Bombardier Global 6000 AFM, Publication No. CSP 700-1V,
Revision 49, dated May 22, 2024.
Note 3 to paragraph (j)(2)(iii): For obtaining the procedures
specified in paragraphs (j)(2)(iii) and (x) of this AD for
Bombardier Global 6000 AFM, Publication No. CSP 700-1V, use Document
Identification No. GL 6000 AFM.
(iv) Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures, Bombardier Global 6500 AFM, Publication No. CSP 700-
6500-1, Revision 21, dated May 22, 2024.
Note 4 to paragraph (j)(2)(iv): For obtaining the procedures
specified in paragraph (j)(2)(iv) of this AD for Bombardier Global
6500 AFM, Publication No. CSP 700-6500-1, use Document
Identification No. GL 6500 AFM.
(v) Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures, Bombardier Global 5000 AFM, Publication No. CSP 700-
5000-1 AFM, Revision 80, dated May 22, 2024.
Note 5 to paragraph (j)(2)(v): For obtaining the procedures
specified in paragraphs (j)(2)(v) and (xi) of this AD for Bombardier
Global 5000 AFM, Publication No. CSP 700-5000-1, use Document
Identification No. GL 5000 AFM.
(vi) Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures, Bombardier Global 5000 Featuring Global Vision Flight
Deck AFM, Publication No. CSP 700-5000-1V, Revision 49, dated May
22, 2024.
Note 6 to paragraph (j)(2)(vi): For obtaining the procedures
specified in paragraphs (j)(2)(vi) and (xii) of this AD for
Bombardier Global 5000 Featuring Global Vision Flight Deck AFM,
Publication No. CSP 700-5000-1V, use Document Identification No. GL
5000 GVFD AFM.
(vii) Section 05-10 Flight Controls, Chapter 5--Non-Normal
Procedures, Bombardier Global 5500 AFM, Publication No. CSP 700-
5500-1, Revision 21, dated May 22, 2024.
Note 7 to paragraph (j)(2)(vii): For obtaining the procedures
specified in paragraph (j)(2)(vii) of this AD for Bombardier Global
5500 AFM, Publication No. CSP 700-5500-1, use Document
Identification No. GL 5500 AFM.
(viii) Chapter 7--Supplement 20--Operations at Airport
Elevations Above 10,000 Feet, Bombardier Global Express AFM,
Publication No. CSP 700-1, Revision 119, dated May 22, 2024.
(ix) Chapter 7--Supplement 20--Operations at Airport Elevations
Above 10,000 Feet, Bombardier Global Express AFM, Publication No.
CSP 700-1A, Revision 119, dated May 22, 2024.
(x) Chapter 7--Supplement 20--Operations at Airport Elevations
Above 10,000 Feet, Bombardier Global 6000 AFM, Publication No. CSP
700-1V, Revision 49, dated May 22, 2024.
(xi) Chapter 7--Supplement 20--Operations at Airport Elevations
Above 10,000 Feet, Bombardier Global 5000 AFM, Publication No. CSP
700-5000-1 AFM, Revision 80, dated May 22, 2024.
(xii) Chapter 7--Supplement 20--Operations at Airport Elevations
Above 10,000 Feet, Bombardier Global 5000 Featuring Global Vision
Flight Deck AFM, Publication No. CSP 700-5000-1V, Revision 49, dated
May 22, 2024.
(3) For Bombardier material 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">ac.yul@aero.bombardier.com; website
bombardier.com.
(4) You may view this material 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 material at the National Archives and
Records Administration (NARA). For information on the availability
of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email [email protected].
Issued on June 4, 2025.
Steven W. Thompson,
Acting Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2025-10683 Filed 6-11-25; 8:45 am]
BILLING CODE 4910-13-P