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.

Proposed Rules Federal Register

27533 

Vol. 87, No. 89 

Monday, May 9, 2022 

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 Coˆte-Vertu Road West, 

Dorval, Que ́bec H4S 1Y9, Canada; 

telephone 514–855–2999; email ac.yul@

aero.bombardier.com; 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 9-avs-nyaco-cos@

faa.gov. 

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 9-avs-nyaco-cos@

faa.gov. 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. 


khammond on DSKJM1Z7X2PROD with PROPOSALS
27534 Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Proposed Rules 

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°, 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°, of the 

Take-Off Performance section of Chapter 

6—Performance. 

• Paragraph B., Effects of Cowl AntiIce 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°, 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°, of the 

Take-Off Performance section of Chapter 

6—Performance. 

• Paragraph B., Effects of Cowl AntiIce 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°, 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°, of the 

Take-Off Performance section of Chapter 

6—Performance. 

• Paragraph B., Effects of Cowl AntiIce 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°, 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°, of the 

Take-Off Performance section of Chapter 

6—Performance. 

• Paragraph B., Effects of Cowl AntiIce 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, 


khammond on DSKJM1Z7X2PROD with PROPOSALS
Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Proposed Rules 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°, 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°, of the 

Take-Off Performance section of Chapter 

6—Performance. 

• Paragraph B., Effects of Cowl AntiIce 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

Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

1 work-hour × $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 

■ 1. The authority citation for part 39 

continues to read as follows: 

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


khammond on DSKJM1Z7X2PROD with PROPOSALS
27536 Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Proposed Rules 

§ 39.13 [Amended] 

■ 2. The FAA amends § 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°, of the TakeOff 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°, of the TakeOff 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°, of the TakeOff 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°, of the TakeOff 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°, of the TakeOff 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°, of the TakeOff 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°, of the TakeOff 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°, of the TakeOff 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 


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Federal Register / Vol. 87, No. 89 / Monday, May 9, 2022 / Proposed Rules 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°, of the TakeOff 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°, of the TakeOff 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 9-avs-nyaco-cos@faa.gov. 

(3) For service information identified in 

this AD, contact Bombardier, Inc., Business 

Aircraft Customer Response Center, 400 CoˆteVertu Road West, Dorval, Que ́bec H4S 1Y9, 

Canada; telephone 514–855–2999; email 

ac.yul@aero.bombardier.com; internet 

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] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2022–0474; Airspace 

Docket No. 22–ACE–11] 

RIN 2120–AA66 

Proposed Amendment of Class E 

Airspace; Independence, IA 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: This action proposes to 

amend the Class E airspace at 

Independence, IA. The FAA is 

proposing this action as the result of an 

airspace review as part of the 

decommissioning of the Wapsie nondirectional beacon (NDB). The name 

and geographic coordinates of the 

airport would also be updated to 

coincide with the FAA’s aeronautical 

database. 

DATES: Comments must be received on 

or before June 23, 2022. 

ADDRESSES: Send comments on this 

proposal to the U.S. Department of 

Transportation, Docket Operations, 

West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE, 

Washington, DC 20590; telephone (202) 

366–9826, or (800) 647–5527. You must 

identify FAA Docket No. FAA–2022– 

0474/Airspace Docket No. 22–ACE–11 

at the beginning of your comments. You 

may also submit comments through the 

internet at https://www.regulations.gov. 

You may review the public docket 

containing the proposal, any comments 

received, and any final disposition in 

person in the Dockets Office between 

9:00 a.m. and 5:00 p.m., Monday 

through Friday, except federal holidays. 

FAA Order JO 7400.11F, Airspace 

Designations and Reporting Points, and 

subsequent amendments can be viewed 

online at https://www.faa.gov/air_

traffic/publications/. For further 

information, you can contact the 

Airspace Policy Group, Federal Aviation 

Administration, 800 Independence 

Avenue SW, Washington, DC 20591; 

telephone: (202) 267–8783. 

FOR FURTHER INFORMATION CONTACT: 

Jeffrey Claypool, Federal Aviation 

Administration, Operations Support 

Group, Central Service Center, 10101 

Hillwood Parkway, Fort Worth, TX 

76177; telephone (817) 222–5711. 

SUPPLEMENTARY INFORMATION: 


khammond on DSKJM1Z7X2PROD with PROPOSALS