Document ID: FAA-2022-0513-0001
Agency: faa
Document Type: Proposed Rule
Title: Airworthiness Directives: Bombardier, Inc., Airplanes
Posted Date: 2022-05-09T04:00Z

[Federal Register Volume 87, Number 89 (Monday, May 9, 2022)]
[Proposed Rules]
[Pages 27533-27537]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-09680]

 ========================================================================
 Proposed Rules
                                                 Federal Register
 ________________________________________________________________________
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 This section of the FEDERAL REGISTER contains notices to the public of 
 the proposed issuance of rules and regulations. The purpose of these 
 notices is to give interested persons an opportunity to participate in 
 the rule making prior to the adoption of the final rules.
 
 ========================================================================
 

  Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Proposed 
Rules  

[[Page 27533]]

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-0513; Project Identifier MCAI-2021-01162-T]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc., Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

-----------------------------------------------------------------------

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 
airplanes. This proposed 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 proposed AD would require revising the existing AFM to correct the 
affected performance charts. The FAA is proposing this AD to address 
the unsafe condition on these products.

DATES: The FAA must receive comments on this proposed AD by June 23, 
2022.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
     Fax: 202-493-2251.
     Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE, Washington, DC 20590.
     Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    For service information identified in this NPRM, contact 
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 [email protected]; internet 
https://www.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.

Examining the AD Docket

    You may examine the AD docket at https://www.regulations.gov by 
searching for and locating 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 NPRM, the 
mandatory continuing airworthiness information (MCAI), any comments 
received, and other information. The street address for Docket 
Operations is listed above.

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: 

Comments Invited

    The FAA invites you to send any written relevant data, views, or 
arguments about this proposal. Send your comments to an address listed 
under ADDRESSES. Include ``Docket No. FAA-2022-0513; Project Identifier 
MCAI-2021-01162-T'' at the beginning of your comments. The most helpful 
comments reference a specific portion of the proposal, explain the 
reason for any recommended change, and include supporting data. The FAA 
will consider all comments received by the closing date and may amend 
the proposal because of those comments.
    Except for Confidential Business Information (CBI) as described in 
the following paragraph, and other information as described in 14 CFR 
11.35, the FAA will post all comments received, without change, to 
https://www.regulations.gov, including any personal information you 
provide. The agency will also post a report summarizing each 
substantive verbal contact received about this NPRM.

Confidential Business Information

    CBI is commercial or financial information that is both customarily 
and actually treated as private by its owner. Under the Freedom of 
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public 
disclosure. If your comments responsive to this NPRM contain commercial 
or financial information that is customarily treated as private, that 
you actually treat as private, and that is relevant or responsive to 
this NPRM, it is important that you clearly designate the submitted 
comments as CBI. Please mark each page of your submission containing 
CBI as ``PROPIN.'' The FAA will treat such marked submissions as 
confidential under the FOIA, and they will not be placed in the public 
docket of this NPRM. Submissions containing CBI should be sent to 
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]. Any commentary that the FAA receives which is not 
specifically designated as CBI will be placed in the public docket for 
this rulemaking.

Background

    Transport Canada Civil Aviation (TCCA), which is the aviation 
authority for Canada, has issued TCCA AD CF-2021-35, dated October 26, 
2021 (TCCA AD CF-2021-35) (also referred to after this as the MCAI), to 
correct an unsafe condition for certain Bombardier, Inc., Model BD-700-
1A10 and BD-700-1A11 airplanes. You may examine the MCAI in the AD 
docket at https://www.regulations.gov by searching for and locating 
Docket No. FAA-2022-0513.
    This proposed AD was prompted by reports that 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. The FAA is proposing this AD 
to address incorrect AFM performance charts, which if not corrected, 
could lead to longitudinal runway excursions. See the MCAI for 
additional background information.

[[Page 27534]]

Related Service Information Under 1 CFR Part 51

    Bombardier, Inc., has issued 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 paragraphs and supplements of the Bombardier Global 
Express Airplane Flight Manual--Publication No. CSP 700-1, Revision 
109, dated August 16, 2021. (For obtaining this section of the 
Bombardier Global Express Airplane Flight Manual--Publication No. CSP 
700-1, use Document Identification No. GL 700 AFM-1.)
     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.
     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.
     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.
     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.
     Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements.
     Paragraph A., Improved Climb Performance, of Section 6--
Performance, of Supplement 5--Improved Climb Performance, of Chapter 
7--Supplements.
     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.
     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.
    The following paragraphs and supplements of the Bombardier Global 
Express Airplane Flight Manual--Publication No. CSP 700-1A, Revision 
109, dated August 16, 2021. (For obtaining this section of the 
Bombardier Global Express Airplane Flight Manual--Publication No. CSP 
700-1A, use Document Identification No. GL 700 AFM-1A.)
     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.
     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.
     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.
     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.
     Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements.
     Paragraph A., Improved Climb Performance, of Section 6--
Performance, of Supplement 5--Improved Climb Performance, of Chapter 
7--Supplements.
     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.
     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.
    The following paragraphs and supplements of the Bombardier Global 
6000 Airplane Flight Manual--Publication No. CSP 700-1V, Revision 39, 
dated August 16, 2021. (For obtaining this section of the Bombardier 
Global 6000 Airplane Flight Manual--Publication No. CSP 700-1V, use 
Document Identification No. GL 6000 AFM.)
     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.
     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.
     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.
     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.
     Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements.
     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.
     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.
     Paragraph A., Take-off on Wet Grooved Runways, of Section 
6--Performance, of Supplement 35--Operation on Wet Grooved Runways, of 
Chapter 7--Supplements.
    The following paragraphs and supplements of the Bombardier Global 
5000 Airplane Flight Manual--Publication No. CSP 700-5000-1, Revision 
70, dated August 16, 2021. (For obtaining this section of the 
Bombardier Global 5000 Airplane Flight Manual--Publication No. CSP 700-
5000-1, use Document Identification No. GL 5000 AFM.)
     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.
     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.
     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.
     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.
     Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements.
     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.
     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.
    The following paragraphs and supplements of the Bombardier Global 
5000 Featuring Global Vision Flight Deck (GVFD) Airplane Flight 
Manual--Publication No. CSP 700-5000-1V,

[[Page 27535]]

Revision 39, dated August 16, 2021. (For obtaining this section 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.)
     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.
     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.
     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.
     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.
     Supplement 3--Operation on Contaminated Runways, of 
Chapter 7--Supplements.
     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.
     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.
     Paragraph A., Take-off on Wet Grooved Runways, of Section 
6--Performance, of Supplement 35--Operation on Wet Grooved Runways, of 
Chapter 7--Supplements.
    This service information is reasonably available because the 
interested parties have access to it through their normal course of 
business or by the means identified in the ADDRESSES section.

FAA's Determination

    This product has been approved by the aviation authority of another 
country, and is approved for operation in the United States. Pursuant 
to the FAA's bilateral agreement with the State of Design Authority, 
the FAA has been notified of the unsafe condition described in the MCAI 
and service information referenced above. The FAA is proposing this AD 
because the FAA evaluated all the relevant information and determined 
the unsafe condition described previously is likely to exist or develop 
on other products of the same type design.

Proposed AD Requirements in This NPRM

    This proposed AD would require accomplishing the actions specified 
in the service information already described.
    TCCA AD CF-2021-35 requires operators to ``advise all flight 
crews'' of revisions to the AFM, and thereafter to ``operate the 
aeroplane accordingly.'' However, this proposed AD would not 
specifically require those actions as those actions are already 
required by FAA regulations. FAA regulations require operators furnish 
to pilots any changes to the AFM (for example, 14 CFR 121.137), and to 
ensure the pilots are familiar with the AFM (for example, 14 CFR 
91.505). As with any other flightcrew training requirement, training on 
the updated AFM content is tracked by the operators and recorded in 
each pilot's training record, which is available for the FAA to review. 
FAA regulations also require pilots to follow the procedures in the 
existing AFM including all updates. 14 CFR 91.9 requires that any 
person operating a civil aircraft must comply with the operating 
limitations specified in the AFM. Therefore, including a requirement in 
this proposed AD to operate the airplane according to the revised AFM 
would be redundant and unnecessary.

Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would 
affect 408 airplanes of U.S. registry. The FAA estimates the following 
costs to comply with this proposed 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

    The FAA determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would not 
have a substantial direct effect on the States, on the relationship 
between the national Government and the States, or on the distribution 
of power and responsibilities among the various levels of government.
    For the reasons discussed above, I certify this proposed 
regulation:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Would not affect intrastate aviation in Alaska, and
    (3) Would 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 Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority:  49 U.S.C. 106(g), 40113, 44701.

[[Page 27536]]

Sec.  39.13   [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive:

Bombardier, Inc.: Docket No. FAA-2022-0513; Project Identifier MCAI-
2021-01162-T.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) by June 23, 2022.

(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 paragraphs and supplements are of the Bombardier Global 
Express Airplane Flight Manual--Publication No. CSP 700-1, Revision 
109, dated August 16, 2021.
    Note 1 to paragraph (g)(1): For obtaining this section of the 
Bombardier Global Express Airplane Flight Manual--Publication No. 
CSP 700-1, use Document Identification No. GL 700 AFM-1.
    (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.
    (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 paragraphs and supplements are of the Bombardier Global 
Express Airplane Flight Manual--Publication No. CSP 700-1A, Revision 
109, dated August 16, 2021.
    Note 2 to paragraph (g)(2): For obtaining this section of the 
Bombardier Global Express Airplane Flight Manual--Publication No. 
CSP 700-1A, use Document Identification No. GL 700 AFM-1A.
    (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.
    (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 
paragraphs and supplements are of the Bombardier Global 6000 
Airplane Flight Manual--Publication No. CSP 700-1V, Revision 39, 
dated August 16, 2021.
    Note 3 to paragraph (g)(3): For obtaining this section of the 
Bombardier Global 6000 Airplane Flight Manual--Publication No. CSP 
700-1V, use Document Identification No. GL 6000 AFM.
    (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.
    (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 
paragraphs and supplements are of the Bombardier Global 5000 
Airplane Flight Manual--Publication No. CSP 700-5000-1, Revision 70, 
dated August 16, 2021.
    Note 4 to paragraph (g)(4): For obtaining this section of the 
Bombardier Global 5000 Airplane Flight Manual--Publication No. CSP 
700-5000-1, use Document Identification No. GL 5000 AFM.
    (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

[[Page 27537]]

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.
    (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 paragraphs 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.
    Note 5 to paragraph (g)(5): For obtaining this section 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.
    (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.

(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-2021-35, dated October 26, 2021, for related 
information. This MCAI may be found in the AD docket on the internet 
at https://www.regulations.gov by searching for and locating Docket 
No. FAA-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].
    (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 [email protected]; internet 
https://www.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.

    Issued on April 30, 2022.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness 
Division, Aircraft Certification Service.
[FR Doc. 2022-09680 Filed 5-6-22; 8:45 am]
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