[Federal Register Volume 88, Number 22 (Thursday, February 2, 2023)]
[Rules and Regulations]
[Pages 6976-6982]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-02009]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-0513; Project Identifier MCAI-2021-01162-T; 
Amendment 39-22241; AD 2022-24-01]
RIN 2120-AA64


Airworthiness Directives; Bombardier, Inc., Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for 
certain

[[Page 6977]]

Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes. This AD 
was prompted by reports that the thrust reverser correction factors 
presented in certain airplane flight manual (AFM) performance charts 
for landing on contaminated runways do not provide sufficient margin 
for stopping distances in certain conditions. This AD requires revising 
the existing AFM to correct the affected performance charts. The FAA is 
issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective March 9, 2023.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of March 9, 
2023.

ADDRESSES: 
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2022-0513; 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, Inc., 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 at 
regulations.gov under Docket No. FAA-2022-0513.

FOR FURTHER INFORMATION CONTACT: Gabriel Kim, 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 May 9, 2022 (87 FR 27533). The NPRM was 
prompted by AD CF-2021-35, dated October 26, 2021, issued by Transport 
Canada Civil Aviation (TCCA), which is the aviation authority for 
Canada (referred to after this as the MCAI). The MCAI states the thrust 
reverser correction factors presented in certain AFM performance charts 
for landing on contaminated runways do not provide sufficient margin 
for stopping distances in certain conditions. If not corrected, use of 
the affected performance charts could lead to longitudinal runway 
excursions.
    In the NPRM, the FAA proposed to require revising the existing AFM 
to correct the affected performance charts. 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-2022-0513.

Discussion of Final Airworthiness Directive

Comments

    The FAA received a comment from TCCA. The following presents the 
comment received on the NPRM and the FAA's response.

Request for Updating the AFM Revision Number

    TCCA requested that the reference to Bombardier Global 6000 
Airplane Flight Manual--Publication No. CSP 700-1V, Revision 39, dated 
August 16, 2021, be updated to Bombardier Global 6000 Airplane Flight 
Manual--Publication No. CSP 700-1V, Revision 42, dated May 19, 2022; 
and the reference to Bombardier Global 5000 Featuring Global Vision 
Flight Deck (GVFD) Airplane Flight Manual--Publication No. CSP 700-
5000-1V, Revision 39, dated August 16, 2021, be updated to Bombardier 
Global 5000 Featuring Global Vision Flight Deck (GVFD) Airplane Flight 
Manual--Publication No. CSP 700-5000-1V, Revision 42, dated May 19, 
2022. TCCA stated that Revisions 40 and 41 introduced errors in Figures 
07-35-02 and 07-35-04, which have been corrected in Revision 42.
    The FAA partially agrees. The FAA does not agree with mandating 
Bombardier Global 6000 Airplane Flight Manual--Publication No. CSP 700-
1V, Revision 42, dated May 19, 2022; and Bombardier Global 5000 
Featuring Global Vision Flight Deck (GVFD) Airplane Flight Manual--
Publication No. CSP 700-5000-1V, Revision 42, dated May 19, 2022, in 
this AD. TCCA issued CF-2022-49 on August 23, 2022 (TCCA AD CF-2022-49) 
to mandate the incorporation of Figure 07-35-02 of Bombardier Global 
6000 Airplane Flight Manual--Publication No. CSP 700-1V, Revision 42, 
dated May 19, 2022; and Figure 07-35-04 of Bombardier Global 5000 
Featuring Global Vision Flight Deck (GVFD) Airplane Flight Manual--
Publication No. CSP 700-5000-1V, Revision 42, dated May 19, 202; which 
are in supplement 35 of the AFMs. TCCA AD CF-2022-49 also added 
airplanes to the applicability. In order to mandate Revision 42 of 
these AFMs, the FAA would need to issue a supplemental NPRM.
    The FAA does not consider that delaying this action is warranted. 
Only paragraphs (g)(3)(viii) and (g)(5)(viii) of the proposed AD refer 
to supplement 35 of the AFMs specified in TCCA AD CF-2022-49. However, 
the proposed AD specifies to incorporate Revision 39 of the AFMs, which 
do not include any errors in the figures identified by TCCA. The 
proposed AD would not allow operators to incorporate the figures in 
Revision 40 and 41 of the AFM as those figures are not identical to the 
figures in Revision 39 of the AFMs specified in paragraphs (g)(3) and 
(5) of the proposed AD.
    The FAA has added Bombardier Global 6000 Airplane Flight Manual--
Publication No. CSP 700-1V, Revision 42, dated May 19, 2022, to 
paragraph (g)(3) of this AD; and Bombardier Global 5000 Featuring 
Global Vision Flight Deck (GVFD) Airplane Flight Manual--Publication 
No. CSP 700-5000-1V, Revision 42, dated May 19, 2022, to paragraph 
(g)(5) of this AD; as an optional source of service information for 
revising the AFM as specified in paragraphs (g)(3) and (5) of this AD. 
For this AD, operator may incorporate Figures 07-35-02 and 07-35-04 of 
either Revision 39 or 42 of the AFMs specified in paragraphs 
(g)(3)(viii) and (g)(5)(viii) of this AD.
    The FAA is considering further rulemaking to correspond with TCCA 
AD CF-2022-49 and mandate incorporating Figure 07-35-02 of Bombardier 
Global 6000 Airplane Flight Manual--Publication No. CSP 700-1V, 
Revision 42, dated May 19, 2022; and Figure 07-35-04 of Bombardier 
Global 5000 Featuring Global Vision Flight Deck (GVFD) Airplane Flight 
Manual--Publication No. CSP 700-5000-1V, Revision 42, dated May 19, 
2022.

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

[[Page 6978]]

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, considered the 
comment 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 
and any other changes described previously, 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 service information, which specifies 
revised AFM limitations and corrections to the performance charts for 
landing on contaminated runways. These documents are distinct since 
they apply to different airplane models and configurations.
    The following sections and supplements are of the Bombardier Global 
Express Airplane Flight Manual--Publication No. CSP 700-1, Revision 
109, dated August 16, 2021. (For obtaining these sections and 
supplements of the Bombardier Global Express Airplane Flight Manual--
Publication No. CSP 700-1, use Document Identification No. GL 700 AFM-
1.)
     Section 06-03 Take-Off Performance, of Chapter 6--
Performance. This section includes Paragraph C., Wet Runway Take-Off 
Field Length, of Section 2., Take-Off Performance--Slat Out/Flap 
6[deg]; and Paragraph C., Wet Runway Take-Off Field Length, of Section 
3., Take-Off Performance--Slat Out/Flap 16[deg].
     Section 06-08 Performance Data for Operation in Icing 
Conditions, of Chapter 6--Performance. This section includes Paragraph 
B., Effects of Cowl Anti-Ice On; and Paragraph C., Effects of Wing and 
Cowl Anti-Ice On/Ice Accumulation; of Section 2., Performance 
Corrections.
     Supplement 3, Operation on Contaminated Runways, of 
Chapter 7--Supplements.
     Supplement 5, Improved Climb Performance, of Chapter 7--
Supplements. This supplement includes Paragraph A., Improved Climb 
Performance, of Section 6--Performance.
     Supplement 20, Operations at Airport Elevations Above 
10,000 Feet, of Chapter 7--Supplements. This supplement includes 
Paragraph B., Take-Off Field Length; and Paragraph G., Operation in 
Icing Conditions; of Section 6--Performance.
    The following sections and supplements are of the Bombardier Global 
Express Airplane Flight Manual--Publication No. CSP 700-1A, Revision 
109, dated August 16, 2021. (For obtaining these sections and 
supplements of the Bombardier Global Express Airplane Flight Manual--
Publication No. CSP 700-1A, use Document Identification No. GL 700 AFM-
1A.)
     Section 06-03 Take-Off Performance, of Chapter 6--
Performance. This section includes Paragraph C., Wet Runway Take-Off 
Field Length, of Section 2., Take-Off Performance--Slat Out/Flap 
6[deg]; and Paragraph C., Wet Runway Take-Off Field Length, of Section 
3., Take-Off Performance--Slat Out/Flap 16[deg].
     Section 06-08 Performance Data for Operation in Icing 
Conditions, of Chapter 6--Performance. This section includes Paragraph 
B., Effects of Cowl Anti-Ice On; and Paragraph C., Effects of Wing and 
Cowl Anti-Ice On/Ice Accumulation; of Section 2., Performance 
Corrections.
     Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements.
     Supplement 5--Improved Climb Performance, of Chapter 7--
Supplements. This supplement includes Paragraph A., Improved Climb 
Performance, of Section 6--Performance.
     Supplement 20--Operations at Airport Elevations Above 
10,000 Feet, of Chapter 7--Supplements. This supplement includes 
Paragraph B., Take-Off Field Length; and Paragraph G., Operation in 
Icing Conditions; of Section 6--Performance.
    The following sections and supplements are of the Bombardier Global 
6000 Airplane Flight Manual--Publication No. CSP 700-1V, Revision 39, 
dated August 16, 2021. (For obtaining these sections and supplements of 
the Bombardier Global 6000 Airplane Flight Manual--Publication No. CSP 
700-1V, use Document Identification No. GL 6000 AFM.)
     Section 06-03 Take-Off Performance, of Chapter 6--
Performance. This section includes Paragraph C., Wet Runway Take-Off 
Field Length, of Section 2., Take-Off Performance--Slat Out/Flap 
6[deg]; and Paragraph C., Wet Runway Take-Off Field Length, of Section 
3., Take-Off Performance--Slat Out/Flap 16[deg].
     Section 06-08 Performance Data for Operation in Icing 
Conditions, of Chapter 6--Performance. This section includes Paragraph 
B., Effects of Cowl Anti-Ice On; and Paragraph C., Effects of Wing and 
Cowl Anti-Ice On/Ice Accumulation; of Section 2, Performance 
Corrections.
     Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements.
     Supplement 20--Operations at Airport Elevations Above 
10,000 Feet, of Chapter 7--Supplements. This supplement includes 
Paragraph B., Take-Off Field Length; and Paragraph G., Operation in 
Icing Conditions; of Section 6--Performance.
     Supplement 35--Operation on Wet Grooved Runways, of 
Chapter 7--Supplements. This supplement includes Paragraph A., Take-off 
on Wet Grooved Runways, of Section 6--Performance.
    The following sections and supplements are of the Bombardier Global 
6000 Airplane Flight Manual--Publication No. CSP 700-1V, Revision 42, 
dated May 19, 2022. (For obtaining these sections and supplements of 
the Bombardier Global 6000 Airplane Flight Manual--Publication No. CSP 
700-1V, use Document Identification No. GL 6000 AFM.)
     Section 06-03 Take-Off Performance, of Chapter 6--
Performance. This section includes Paragraph C., Wet Runway Take-Off 
Field Length, of Section 2., Take-Off Performance--Slat Out/Flap 
6[deg]; and Paragraph C., Wet Runway Take-Off Field Length, of Section 
3., Take-Off Performance--Slat Out/Flap 16[deg].
     Section 06-08 Performance Data for Operation in Icing 
Conditions, of Chapter 6--Performance. This section includes Paragraph 
B., Effects of Cowl Anti-Ice On; and Paragraph C., Effects of Wing and 
Cowl Anti-Ice On/Ice Accumulation; of Section 2., Performance 
Corrections.
     Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements.
     Supplement 20--Operations at Airport Elevations Above 
10,000 Feet, of Chapter 7--Supplements. This supplement includes 
Paragraph B., Take-Off Field Length; and Paragraph G., Operation in 
Icing Conditions; of Section 6--Performance.
     Supplement 35--Operation on Wet Grooved or Wet Porous 
Friction Course Runways, of Chapter 7--Supplements. This supplement 
includes Paragraph A., Take-off on Wet Grooved or Wet PFC Runways, of 
Section 6--Performance.
    The following sections and supplements are of the Bombardier Global 
5000 Airplane Flight Manual--Publication No. CSP 700-5000-1, Revision 
70, dated August 16, 2021. (For obtaining these sections and

[[Page 6979]]

supplements of the Bombardier Global 5000 Airplane Flight Manual--
Publication No. CSP 700-5000-1, use Document Identification No. GL 5000 
AFM.)
     Section 06-03 Take-Off Performance, of Chapter 6--
Performance. This section includes Paragraph C., Wet Runway Take-Off 
Field Length, of Section 2., Take-Off Performance--Slat Out/Flap 
6[deg]; and Paragraph C., Wet Runway Take-Off Field Length, of Section 
3., Take-Off Performance--Slat Out/Flap 16[deg].
     Section 06-08 Performance Data for Operation in Icing 
Conditions, of Chapter 6--Performance. This section includes Paragraph 
B., Effects of Cowl Anti-Ice On; and Paragraph C., Effects of Wing and 
Cowl Anti-Ice On/Ice Accumulation; of Section 2., Performance 
Corrections.
     Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements.
     Supplement 20--Operations at Airport Elevations Above 
10,000 Feet, of Chapter 7--Supplements. This supplement includes 
Paragraph B., Take-Off Field Length; and Paragraph G., Operation in 
Icing Conditions; of Section 6--Performance.
    The following sections and supplements are of the Bombardier Global 
5000 Featuring Global Vision Flight Deck (GVFD) Airplane Flight 
Manual--Publication No. CSP 700-5000-1V, Revision 39, dated August 16, 
2021. (For obtaining these sections and supplements of the Bombardier 
Global 5000 Featuring Global Vision Flight Deck Airplane Flight 
Manual--Publication No. CSP 700-5000-1V, use Document Identification 
No. GL 5000 GVFD AFM.)
     Section 06-03 Take-Off Performance, of Chapter 6--
Performance. This section includes Paragraph C., Wet Runway Take-Off 
Field Length, of Section 2., Take-Off Performance--Slat Out/Flap 
6[deg]; and Paragraph C., Wet Runway Take-Off Field Length, of Section 
3., Take-Off Performance--Slat Out/Flap 16[deg].
     Section 06-08 Performance Data for Operation in Icing 
Conditions, of Chapter 6--Performance. This section includes Paragraph 
B., Effects of Cowl Anti-Ice On; and Paragraph C., Effects of Wing and 
Cowl Anti-Ice On/Ice Accumulation; of Section 2, Performance 
Corrections.
     Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements.
     Supplement 20--Operations at Airport Elevations Above 
10,000 Feet, of Chapter 7--Supplements. This supplement includes 
Paragraph B., Take-Off Field Length; and Paragraph G., Operation in 
Icing Conditions; of Section 6--Performance.
     Supplement 35--Operation on Wet Grooved Runways, of 
Chapter 7--Supplements. This supplement includes Paragraph A., Take-off 
on Wet Grooved Runways, of Section 6--Performance.
    The following sections and supplements are of the Bombardier Global 
5000 Featuring Global Vision Flight Deck Airplane Flight Manual--
Publication No. CSP 700-5000-1V, Revision 42, dated May 19, 2022. (For 
obtaining these sections and supplements of the Bombardier Global 5000 
Featuring Global Vision Flight Deck Airplane Flight Manual--Publication 
No. CSP 700-5000-1V, use Document Identification No. GL 5000 GVFD AFM.)
     Section 06-03 Take-Off Performance, of Chapter 6--
Performance. This section includes Paragraph C., Wet Runway Take-Off 
Field Length, of Section 2., Take-Off Performance--Slat Out/Flap 
6[deg]; and Paragraph C., Wet Runway Take-Off Field Length, of Section 
3., Take-Off Performance--Slat Out/Flap 16[deg].
     Section 06-08 Performance Data for Operation in Icing 
Conditions. This section includes Paragraph B., Effects of Cowl Anti-
Ice On; and Paragraph C., Effects of Wing and Cowl Anti-Ice On/Ice 
Accumulation; of Section 2., Performance Corrections.
     Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements.
     Supplement 20--Operations at Airport Elevations Above 
10,000 Feet, of Chapter 7--Supplements. This supplement includes 
Paragraph B., Take-Off Field Length; and Paragraph G., Operation in 
Icing Conditions; of Section 6--Performance.
     Supplement 35--Operation on Wet Grooved or Wet Porous 
Friction Course Runways, of Chapter 7--Supplements. This supplement 
includes Paragraph A., Take-off on Wet Grooved or Wet PFC Runways, of 
Section 6--Performance.
    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 408 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          $34,680
----------------------------------------------------------------------------------------------------------------

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

[[Page 6980]]

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:

2022-24-01 Bombardier, Inc.: Amendment 39-22241; Docket No. FAA-
2022-0513; Project Identifier MCAI-2021-01162-T.

(a) Effective Date

    This airworthiness directive (AD) is effective March 9, 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, serial numbers 
9001 through 9860 inclusive, 9862 through 9871 inclusive, 9873 
through 9879 inclusive, 60005, 60024, 60030, 60032, 60037, 60043, 
60045, and 60049.

(d) Subject

    Air Transport Association (ATA) of America Code 27, Flight 
controls.

(e) Unsafe Condition

    This AD was prompted by reports that the thrust reverser 
correction factors presented in certain airplane flight manual (AFM) 
performance charts for landing on contaminated runways do not 
provide sufficient margin for stopping distances in certain 
conditions. The FAA is issuing this AD to address incorrect AFM 
performance charts, which if not corrected, could lead to 
longitudinal runway excursions.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) AFM Revision

    Within 30 days after the effective date of this AD: Do the 
applicable actions specified in paragraph (g)(1) through (5) of this 
AD.
    (1) For Model BD-700-1A10 airplanes with a Global Express 
marketing designation: Revise the existing AFM to incorporate the 
information specified in paragraphs (g)(1)(i) through (viii) of this 
AD. These sections and supplements are of the Bombardier Global 
Express Airplane Flight Manual--Publication No. CSP 700-1, Revision 
109, dated August 16, 2021.
    (i) Paragraph C., Wet Runway Take-Off Field Length, of Section 
2., Take-Off Performance--Slat Out/Flap 6[deg], of the Take-Off 
Performance section of Chapter 6--Performance.
    (ii) Paragraph C., Wet Runway Take-Off Field Length, of Section 
3., Take-Off Performance--Slat Out/Flap 16[deg], of the Take-Off 
Performance section of Chapter 6--Performance.
    (iii) Paragraph B., Effects of Cowl Anti-Ice On, of Section 2., 
Performance Corrections, of the Performance Data for Operation in 
Icing Condition section of Chapter 6--Performance.
    (iv) Paragraph C., Effects of Wing and Cowl Anti-Ice On/Ice 
Accumulation, of Section 2., Performance Corrections, of the 
Performance Data for Operation in Icing Condition section of Chapter 
6--Performance.
    (v) Supplement 3--Operation on Contaminated Runways, of Chapter 
7--Supplements.
    (vi) Paragraph A., Improved Climb Performance, of Section 6--
Performance, of Supplement 5--Improved Climb Performance, of Chapter 
7--Supplements.
    (vii) Paragraph B., Take-Off Field Length, of Section 6--
Performance, of Supplement 20--Operations at Airport Elevations 
Above 10,000 Feet, of Chapter 7--Supplements.
    (viii) Paragraph G., Operation in Icing Conditions, of Section 
6--Performance, of Supplement 20--Operations at Airport Elevations 
Above 10,000 Feet, of Chapter 7--Supplements.
    Note 1 to paragraph (g)(1): For obtaining these sections and 
supplements of the Bombardier Global Express Airplane Flight 
Manual--Publication No. CSP 700-1, use Document Identification No. 
GL 700 AFM-1.
    (2) For Model BD-700-1A10 airplanes with a Global Express XRS 
marketing designation: Revise the existing AFM to incorporate the 
information specified in paragraphs (g)(2)(i) through (viii) of this 
AD. These sections and supplements are of the Bombardier Global 
Express Airplane Flight Manual--Publication No. CSP 700-1A, Revision 
109, dated August 16, 2021.
    (i) Paragraph C., Wet Runway Take-Off Field Length, of Section 
2., Take-Off Performance--Slat Out/Flap 6[deg], of the Take-Off 
Performance section of Chapter 6--Performance.
    (ii) Paragraph C., Wet Runway Take-Off Field Length, of Section 
3., Take-Off Performance--Slat Out/Flap 16[deg], of the Take-Off 
Performance section of Chapter 6--Performance.
    (iii) Paragraph B., Effects of Cowl Anti-Ice On, of Section 2., 
Performance Corrections, of the Performance Data for Operation in 
Icing Condition section of Chapter 6--Performance.
    (iv) Paragraph C., Effects of Wing and Cowl Anti-Ice On/Ice 
Accumulation, of Section 2., Performance Corrections, of the 
Performance Data for Operation in Icing Condition section of Chapter 
6--Performance.
    (v) Supplement 3--Operation on Contaminated Runways, of Chapter 
7--Supplements.
    (vi) Paragraph A., Improved Climb Performance, of Section 6--
Performance, of Supplement 5--Improved Climb Performance, of Chapter 
7--Supplements.
    (vii) Paragraph B., Take-Off Field Length, of Section 6--
Performance, of Supplement 20--Operations at Airport Elevations 
Above 10,000 Feet, of Chapter 7--Supplements.
    (viii) Paragraph G., Operation in Icing Conditions, of Section 
6--Performance, of Supplement 20--Operations at Airport Elevations 
Above 10,000 Feet, of Chapter 7--Supplements.
    Note 2 to paragraph (g)(2): For obtaining these sections and 
supplements of the Bombardier Global Express Airplane Flight 
Manual--Publication No. CSP 700-1A, use Document Identification No. 
GL 700 AFM-1A.
    (3) For Model BD-700-1A10 airplanes with a Global 6000 marketing 
designation: Revise the existing AFM to incorporate the information 
specified in paragraphs (g)(3)(i) through (viii) of this AD. These 
sections and supplements are of the Bombardier Global 6000 Airplane 
Flight Manual--Publication No. CSP 700-1V, Revision 39, dated August 
16, 2021 (Bombardier Global 6000 AFM, Revision 39); or Bombardier 
Global 6000 Airplane Flight Manual--Publication No. CSP 700-1V, 
Revision 42, dated May 19, 2022 (Bombardier Global 6000 AFM, 
Revision 42).
    (i) Paragraph C., Wet Runway Take-Off Field Length, of Section 
2., Take-Off Performance--Slat Out/Flap 6[deg], of the Take-Off 
Performance section of Chapter 6--Performance.
    (ii) Paragraph C., Wet Runway Take-Off Field Length, of Section 
3., Take-Off Performance--Slat Out/Flap 16[deg], of the Take-Off 
Performance section of Chapter 6--Performance.
    (iii) Paragraph B., Effects of Cowl Anti-Ice On, of Section 2., 
Performance Corrections, of the Performance Data for Operation in 
Icing Condition section of Chapter 6--Performance.
    (iv) Paragraph C., Effects of Wing and Cowl Anti-Ice On/Ice 
Accumulation, of Section 2., Performance Corrections, of the 
Performance Data for Operation in Icing Condition section of Chapter 
6--Performance.
    (v) Supplement 3--Operation on Contaminated Runways, of Chapter 
7--Supplements.
    (vi) Paragraph B., Take-Off Field Length, of Section 6--
Performance, of Supplement 20--Operations at Airport Elevations 
Above 10,000 Feet, of Chapter 7--Supplements.
    (vii) Paragraph G., Operation in Icing Conditions, of Section 
6--Performance, of Supplement 20--Operations at Airport Elevations 
Above 10,000 Feet, of Chapter 7--Supplements.
    (viii) Paragraph A., Take-off on Wet Grooved Runways, of Section 
6--Performance, of Supplement 35--Operation on Wet Grooved Runways, 
of Chapter 7--Supplements of Bombardier Global 6000 AFM, Revision 
39; or Paragraph A., Take-off on Wet Grooved or Wet PFC Runways, of 
Section 6--Performance, of Supplement 35--

[[Page 6981]]

Operation on Wet Grooved or Wet Porous Friction Course Runways, of 
Chapter 7--Supplements of Bombardier Global 6000 AFM, Revision 42.
    Note 3 to paragraph (g)(3): For obtaining these sections and 
supplements of the Bombardier Global 6000 Airplane Flight Manual--
Publication No. CSP 700-1V, use Document Identification No. GL 6000 
AFM.
    (4) For Model BD-700-1A11 airplanes with a Global 5000 marketing 
designation: Revise the existing AFM to incorporate the information 
specified in paragraphs (g)(4)(i) through (vii) of this AD. These 
sections and supplements are of the Bombardier Global 5000 Airplane 
Flight Manual--Publication No. CSP 700-5000-1, Revision 70, dated 
August 16, 2021.
    (i) Paragraph C., Wet Runway Take-Off Field Length, of Section 
2., Take-Off Performance--Slat Out/Flap 6[deg], of the Take-Off 
Performance section of Chapter 6--Performance.
    (ii) Paragraph C., Wet Runway Take-Off Field Length, of Section 
3., Take-Off Performance--Slat Out/Flap 16[deg], of the Take-Off 
Performance section of Chapter 6--Performance.
    (iii) Paragraph B., Effects of Cowl Anti-Ice On, of Section 2., 
Performance Corrections, of the Performance Data for Operation in 
Icing Condition section of Chapter 6--Performance.
    (iv) Paragraph C., Effects of Wing and Cowl Anti-Ice On/Ice 
Accumulation, of Section 2., Performance Corrections, of the 
Performance Data for Operation in Icing Condition section of Chapter 
6--Performance.
    (v) Supplement 3--Operation on Contaminated Runways, of Chapter 
7--Supplements.
    (vi) Paragraph B., Take-Off Field Length, of Section 6--
Performance, of Supplement 20--Operations at Airport Elevations 
Above 10,000 Feet, of Chapter 7--Supplements.
    (vii) Paragraph G., Operation in Icing Conditions, of Section 
6--Performance, of Supplement 20--Operations at Airport Elevations 
Above 10,000 Feet, of Chapter 7--Supplements.
    Note 4 to paragraph (g)(4): For obtaining these sections and 
supplements of the Bombardier Global 5000 Airplane Flight Manual--
Publication No. CSP 700-5000-1, use Document Identification No. GL 
5000 AFM.
    (5) For Model BD-700-1A11 airplanes with a Global 5000 featuring 
Global Vision Flight Deck (GVFD) marketing designation: Revise the 
existing AFM to incorporate the information specified in paragraphs 
(g)(5)(i) through (viii) of this AD These sections and supplements 
are of the Bombardier Global 5000 Featuring Global Vision Flight 
Deck Airplane Flight Manual--Publication No. CSP 700-5000-1V, 
Revision 39, dated August 16, 2021 (Bombardier Global 5000 GVFD AFM, 
Revision 39); or Bombardier 5000 Featuring Global Vision Flight Deck 
Airplane Flight Manual--Publication No. CSP 700-5000-1V, Revision 
42, dated May 19, 2022 (Bombardier Global 5000 GVFD AFM, Revision 
42).
    (i) Paragraph C., Wet Runway Take-Off Field Length, of Section 
2., Take-Off Performance--Slat Out/Flap 6[deg], of the Take-Off 
Performance section of Chapter 6--Performance.
    (ii) Paragraph C., Wet Runway Take-Off Field Length, of Section 
3., Take-Off Performance--Slat Out/Flap 16[deg], of the Take-Off 
Performance section of Chapter 6--Performance.
    (iii) Paragraph B., Effects of Cowl Anti-Ice On, of Section 2., 
Performance Corrections, of the Performance Data for Operation in 
Icing Condition section of Chapter 6--Performance.
    (iv) Paragraph C., Effects of Wing and Cowl Anti-Ice On/Ice 
Accumulation, of Section 2., Performance Corrections, of the 
Performance Data for Operation in Icing Condition section of Chapter 
6--Performance.
    (v) Supplement 3--Operation on Contaminated Runways, of Chapter 
7--Supplements.
    (vi) Paragraph B., Take-Off Field Length, of Section 6--
Performance, of Supplement 20--Operations at Airport Elevations 
Above 10,000 Feet, of Chapter 7--Supplements.
    (vii) Paragraph G., Operation in Icing Conditions, of Section 
6--Performance, of Supplement 20--Operations at Airport Elevations 
Above 10,000 Feet, of Chapter 7--Supplements.
    (viii) Paragraph A., Take-off on Wet Grooved Runways, of Section 
6--Performance, of Supplement 35--Operation on Wet Grooved Runways, 
of Chapter 7--Supplements of Bombardier Global 5000 GVFD AFM, 
Revision 39; or Paragraph A., Take-off on Wet Grooved or Wet PFC 
Runways, of Section 6--Performance, of Supplement 35--Operation on 
Wet Grooved or Wet Porous Friction Course Runways, of Chapter 7--
Supplements of Bombardier Global 5000 GVFD AFM, Revision 42.
    Note 5 to paragraph (g)(5): For obtaining these sections and 
supplements of the Bombardier Global 5000 Featuring Global Vision 
Flight Deck Airplane Flight Manual--Publication No. CSP 700-5000-1V, 
use Document Identification No. GL 5000 GVFD AFM.

(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) Additional Information

    (1) Refer to TCCA AD CF-2021-35, dated October 26, 2021, for 
related information. This TCCA AD may be found in the AD docket at 
regulations.gov under Docket No. FAA-2022-0513.
    (2) For more information about this AD, contact Gabriel Kim, 
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) Section 06-03 Take-Off Performance, of Chapter 6--
Performance, of Bombardier Global Express Airplane Flight Manual--
Publication No. CSP 700-1, Revision 109, dated August 16, 2021.
    Note 6 to paragraph (j)(2)(i): This note applies to paragraphs 
(j)(2)(i) through (v) of this AD. For obtaining these sections and 
supplements of the Bombardier Global Express Airplane Flight 
Manual--Publication No. CSP 700-1, use Document Identification No. 
GL 700 AFM-1.
    (ii) Section 06-08 Performance Data for Operation in Icing 
Conditions, of Chapter 6--Performance, of Bombardier Global Express 
Airplane Flight Manual--Publication No. CSP 700-1, Revision 109, 
dated August 16, 2021.
    (iii) Supplement 3, Operation on Contaminated Runways, of 
Chapter 7--Supplements, of Bombardier Global Express Airplane Flight 
Manual--Publication No. CSP 700-1, Revision 109, dated August 16, 
2021.
    (iv) Supplement 5, Improved Climb Performance, of Chapter 7--
Supplements, of Bombardier Global Express Airplane Flight Manual--
Publication No. CSP 700-1, Revision 109, dated August 16, 2021.
    (v) Supplement 20, Operations at Airport Elevations Above 10,000 
Feet, of Chapter 7--Supplements, of Bombardier Global Express 
Airplane Flight Manual--Publication No. CSP 700-1, Revision 109, 
dated August 16, 2021.
    (vi) Section 06-03 Take-Off Performance, of Chapter 6--
Performance, of Bombardier Global Express Airplane Flight Manual--
Publication No. CSP 700-1A, Revision 109, dated August 16, 2021.
    Note 7 to paragraph (j)(2)(vi): This note applies to paragraphs 
(j)(2)(vi) through (x) of this AD. For obtaining these sections and 
supplements of the Bombardier Global Express Airplane Flight 
Manual--Publication No. CSP 700-1A, use Document Identification No. 
GL 700 AFM-1A.

[[Page 6982]]

    (vii) Section 06-08 Performance Data for Operation in Icing 
Conditions, of Chapter 6--Performance, of Bombardier Global Express 
Airplane Flight Manual--Publication No. CSP 700-1A, Revision 109, 
dated August 16, 2021.
    (viii) Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements, of Bombardier Global Express Airplane Flight 
Manual--Publication No. CSP 700-1A, Revision 109, dated August 16, 
2021.
    (ix) Supplement 5--Improved Climb Performance, of Chapter 7--
Supplements, of Bombardier Global Express Airplane Flight Manual--
Publication No. CSP 700-1A, Revision 109, dated August 16, 2021.
    (x) Supplement 20--Operations at Airport Elevations Above 10,000 
Feet, of Chapter 7--Supplements, of Bombardier Global Express 
Airplane Flight Manual--Publication No. CSP 700-1A, Revision 109, 
dated August 16, 2021.
    (xi) Section 06-03 Take-Off Performance, of Chapter 6--
Performance, of Bombardier Global 6000 Airplane Flight Manual--
Publication No. CSP 700-1V, Revision 39, dated August 16, 2021.
    Note 8 to paragraph (j)(2)(xi): This note applies to paragraphs 
(j)(2)(xi) through (xx) of this AD. For obtaining these sections and 
supplements of the Bombardier Global 6000 Airplane Flight Manual--
Publication No. CSP 700-1V, use Document Identification No. GL 6000 
AFM.
    (xii) Section 06-08 Performance Data for Operation in Icing 
Conditions, of Chapter 6--Performance, of Bombardier Global 6000 
Airplane Flight Manual--Publication No. CSP 700-1V, Revision 39, 
dated August 16, 2021.
    (xiii) Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements, of Bombardier Global 6000 Airplane Flight 
Manual--Publication No. CSP 700-1V, Revision 39, dated August 16, 
2021.
    (xiv) Supplement 20--Operations at Airport Elevations Above 
10,000 Feet, of Chapter 7--Supplements, of Bombardier Global 6000 
Airplane Flight Manual--Publication No. CSP 700-1V, Revision 39, 
dated August 16, 2021.
    (xv) Supplement 35--Operation on Wet Grooved Runways, of Chapter 
7--Supplements, of Bombardier Global 6000 Airplane Flight Manual--
Publication No. CSP 700-1V, Revision 39, dated August 16, 2021.
    (xvi) Section 06-03 Take-Off Performance, of Chapter 6--
Performance, of Bombardier Global 6000 Airplane Flight Manual--
Publication No. CSP 700-1V, Revision 42, dated May 19, 2022.
    (xvii) Section 06-08 Performance Data for Operation in Icing 
Conditions, of Chapter 6--Performance, of Bombardier Global 6000 
Airplane Flight Manual--Publication No. CSP 700-1V, Revision 42, 
dated May 19, 2022.
    (xviii) Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements, of Bombardier Global 6000 Airplane Flight 
Manual--Publication No. CSP 700-1V, Revision 42, dated May 19, 2022.
    (xix) Supplement 20--Operations at Airport Elevations Above 
10,000 Feet, of Chapter 7--Supplements, of Bombardier Global 6000 
Airplane Flight Manual--Publication No. CSP 700-1V, Revision 42, 
dated May 19, 2022.
    (xx) Supplement 35--Operation on Wet Grooved Runways, of Chapter 
7--Supplements, of Bombardier Global 6000 Airplane Flight Manual--
Publication No. CSP 700-1V, Revision 42, dated May 19, 2022.
    (xxi) Section 06-03 Take-Off Performance, of Chapter 6--
Performance, of Bombardier Global 5000 Airplane Flight Manual--
Publication No. CSP 700-5000-1, Revision 70, dated August 16, 2021.
    Note 9 to paragraph (j)(2)(xxi): This note applies to paragraphs 
(j)(2)(xxi) through (xxiv) of this AD. For obtaining these sections 
and supplements of the Bombardier Global 5000 Airplane Flight 
Manual--Publication No. CSP 700-5000-1, use Document Identification 
No. GL 5000 AFM.
    (xxii) Section 06-08 Performance Data for Operation in Icing 
Conditions, of Chapter 6--Performance, of Bombardier Global 5000 
Airplane Flight Manual--Publication No. CSP 700-5000-1, Revision 70, 
dated August 16, 2021.
    (xxiii) Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements, of Bombardier Global 5000 Airplane Flight 
Manual--Publication No. CSP 700-5000-1, Revision 70, dated August 
16, 2021.
    (xxiv) Supplement 20--Operations at Airport Elevations Above 
10,000 Feet, of Chapter 7--Supplements, of Bombardier Global 5000 
Airplane Flight Manual--Publication No. CSP 700-5000-1, Revision 70, 
dated August 16, 2021.
    (xxv) Section 06-03 Take-Off Performance, of Chapter 6--
Performance, of Bombardier Global 5000 Featuring Global Vision 
Flight Deck Airplane Flight Manual--Publication No. CSP 700-5000-1V, 
Revision 39, dated August 16, 2021.
    Note 10 to paragraph (j)(2)(xxv): This note applies to 
paragraphs (j)(2)(xxv) through (xxxiv) of this AD. For obtaining 
these sections of the Bombardier Global 5000 Featuring Global Vision 
Flight Deck Airplane Flight Manual--Publication No. CSP 700-5000-1V, 
use Document Identification No. GL 5000 GVFD AFM.
    (xxvi) Section 06-08 Performance Data for Operation in Icing 
Conditions, of Chapter 6--Performance, of Bombardier Global 5000 
Featuring Global Vision Flight Deck Airplane Flight Manual--
Publication No. CSP 700-5000-1V, Revision 39, dated August 16, 2021.
    (xxvii) Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements, of Bombardier Global 5000 Featuring Global 
Vision Flight Deck Airplane Flight Manual--Publication No. CSP 700-
5000-1V, Revision 39, dated August 16, 2021.
    (xxviii) Supplement 20--Operations at Airport Elevations Above 
10,000 Feet, of Chapter 7--Supplements, of Bombardier Global 5000 
Featuring Global Vision Flight Deck Airplane Flight Manual--
Publication No. CSP 700-5000-1V, Revision 39, dated August 16, 2021.
    (xxix) Supplement 35--Operation on Wet Grooved Runways, of 
Chapter 7--Supplements, of Bombardier Global 5000 Featuring Global 
Vision Flight Deck Airplane Flight Manual--Publication No. CSP 700-
5000-1V, Revision 39, dated August 16, 2021.
    (xxx) Section 06-03 Take-Off Performance, of Chapter 6--
Performance, of Bombardier 5000 Featuring Global Vision Flight Deck 
Airplane Flight Manual--Publication No. CSP 700-5000-1V, Revision 
42, dated May 19, 2022.
    (xxxi) Section 06-08 Performance Data for Operation in Icing 
Conditions, of Chapter 6--Performance, of Bombardier Global 5000 
Featuring Global Vision Flight Deck Airplane Flight Manual--
Publication No. CSP 700-5000-1V, Revision 42, dated May 19, 2022.
    (xxxii) Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements, of Bombardier Global 5000 Featuring Global 
Vision Flight Deck Airplane Flight Manual--Publication No. CSP 700-
5000-1V, Revision 42, dated May 19, 2022.
    (xxxiii) Supplement 20--Operations at Airport Elevations Above 
10,000 Feet, of Chapter 7--Supplements, of Bombardier Global 5000 
Featuring Global Vision Flight Deck Airplane Flight Manual--
Publication No. CSP 700-5000-1V, Revision 42, dated May 19, 2022.
    (xxxiv) Supplement 35--Operation on Wet Grooved Runways, of 
Chapter 7--Supplements, of Bombardier Global 5000 Featuring Global 
Vision Flight Deck Airplane Flight Manual--Publication No. CSP 700-
5000-1V, Revision 42, dated May 19, 2022.
    (3) For service information identified in this AD, contact 
Bombardier, Inc., 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: www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on January 24, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2023-02009 Filed 2-1-23; 8:45 am]
BILLING CODE 4910-13-P


